Saturday 21 April 2012

Mirrors - Update





It is unclear how long the mirrors remained on 304 and 305, the last two Labradors with mirrors.

Stability Augmentation System and Pitot Tubes

Both Labradors and Voyageurs use a stability augmentation system (SAS) to keep the aircraft stable in flight and in the case of 113s to keep the aft rotors from trying to catch up to the front rotors.  While the helicopter could be flown with the SAS off, it was much more challenging and certainly not as smooth a flight.  If the SAS kicked off while in the hover or unexpectedly, it made things potentially dangerous.  The two-channel SAS system utilized SAS (static) ports on both the nose and fuselage of both variants.

Where they differed was in the number and location of the static ports.  Both types had four ports on the nose, two on the left and two on the right. As previously mentioned, the location of those on the Voyageur differed slightly because of the extra nose glass.  The Labrador also had three static ports on either side of the fuselage, the Voyageur just two. I do not know if the third static port meant the Labrador at one time had a back up channel or if it was tied to another function?

The red circles on the nose of this early Labrador encircle the SAS system static ports. The large red circles around the ports will eventually be much smaller. Photo DND

Voyageur static ports

 
 The shape of the two outer glass panels is in part determined by the relocation of the static ports on Voyageurs. Photo courtesy of Derek Heyes





The two DND photos above show the three static ports on each side of the red, white and blue Labradors.


Problems with the cable cutter cartridges prompted this 103 RU innovation called "SARMUG". Note that the yellow Labrador still has three static ports on each side of the fuselage. Photo Randy Brown collection.

Voyageur 313 in variegated camo livery. Note the two static ports just aft of the door. Photo via Pat Mercer


Voyageur 409 shows the two left side static ports. There were two more on the right side of the fuselage. Note the emergency exit door and the silver circle ahead of the nose gear. Photo via Mike Belcher

The pitot static system also utilized a port to provide among other things, airspeed. When the Labradors were purchased, they were equipped with two pitot static tubes on the right side and one on the left side of the fuselage.  They were located above and aft of the cockpit doors.  Voyageurs had only the set of two pitot tubes on the right side fuselage.  At some undetermined point in time the left side single pitot tube was removed from all Labradors.  At the same time, the number of SAS ports on both sides of the fuselage was reduced from three to two. On the right side of the fuselage, the SAS static ports were just aft of the lower Dutch Door and on the left just aft of the bottom of the emergency door.  Photographic evidence reveals that aircraft 304 was the last to shed the left side pitot tube but only after it had been through SARCUP.!

Labradors were originally fitted with a single pitot tube on the left side. Note there is no vent behind the cockpit door. Photo via Pat Mercer
A close up look at the right side pitot tube common to both the Labrador and Voyageur. Photo courtesy of Scott Hemsley

The photo above shows the location of the right side pitot tube. Photo courtesy of Derek Heyes
The above photo shows a SARCUP modified Labrador sporting both mirrors and the left side pitot tube...neither of which survived until Labradors were retired. Photo DND

Hover Lights

Labradors as stated earlier use their fully articulating landing lights in a variety situations from landing, to search or when in the hover because they can.  To enhance its’ single articulating light, the Voyageur was fitted with a hover light just aft of the center hatch and slightly to the left of midline.  This light, as the name implies, was used for those situations were the Voyageur was required to hover at night.  My presumption is that the light was likely located here to give the Flight Engineer a better look at the ground or objects below during SAR procedures. As Voyageurs were mobilized for SAR duties, the center hatch was used more often to facilitate SAR procedures and was the position from where Flight Engineers coordinated hoist and sling operations. Slinging at night would be but one example of where the hover light would be of use.


Hover light
 

Unlike Voyageurs, Labradors were not originally fitted with center fuselage hover lights. Photo DND


Note that the Labrador in the above picture does not have a hover light in the area of the centre hatch. Photo via Randy Ward.



Labradors were not purchased with hover lights and as late as the “Speedline” series of modifications and it seems they were not fitted with them.  As near as I can confirm through photos, hover lights were installed on Labradors as part of “SARCUP”.!

Aft Pylon
Likely, the most noticeable difference, to the educated, between Labradors and Voyageurs is the inclusion of a tail mounted auxiliary power unit (APU) on the Voyageurs.  In addition to a change in the basic profile of the tail, the auxiliary power unit installation meant relocating, albeit only a matter of inches, the white aft navigation light.

Photographer Derek Heyes has superbly captured the shape of the Voyageur's tail.  Photo courtesy of Derek Heyes


Location of the navigation light on a Labrador would be here
 


White navigation light on a Voyageur
 

The photo above shows how the shape of the tail is affected by the built-in APU. Photo courtesy of Derek Heyes
Voyageur APU exposed. Photo courtesy Bill Ewing

Close up of APU from left side. Photo courtesy Bill Ewing

Labradors began life without auxiliary power units relying on start carts to power up when starting at home bases or suitably equipped airports.  The nature of search and rescue work, however meant operating unsupported in remote areas where start carts were a luxury they would have to operate without.  Labradors therefore relied on very taxing and potentially dangerous battery starts.  The solution was to strap a portable APU cart on the ramp.  It was not until late in SARCUP that Labradors were modified with a tail mounted APU. 305 For one was not modified with a Voyageur tail until after 1980, and was probably one of the last, if not the last, airframe to be modified with the new tail and APU.


Aircraft 305 sits in front of 103 Rescue Unit's hangar in Gander, Newfoundland sometime after 1980. Photo Randy Brown collection

Because of unspecified incidents, Labradors 404 lost it’s rear end shortly after being purchased and was fitted with Voyageur style tail early. Aircraft 402 however lost its tail in a landing accident at Coldfish Lake, B.C. in November of 1968. In both cases, while Voyageur shaped, the new tail did not include the APU.  The opening for the APU exhaust being blanked off and the navigation light relocated accordingly.

Another aft pylon feature that differentiated the two variants was the addition of drain covers on the Labrador.  Most pictures of Labradors wearing the 400 series numbers reveal that early Labradors did not have drain covers, while those in300 series numbers always seem to have the covers. The covers were fitted over all drains on both sides of the aft fuselage.  This difference also remained until the aircraft were retired.!


Close examination of 302's tail will reveal a Voyageur style tail but no APU. The photo shows 302's SAR Techs (in wetsuits) transferring a patient to a waiting Buffalo. The author is wearing the tan flying suit with a dark green flight jacket. Photos Randy Brown collection

Labradors were fitted with drain covers, which remained in place until their retirement. The covers were on both sides of the airframe. Photo courtesy of John Davies

Static Discharge Cords

Only Labradors 302 and 303 were equipped with static discharge cords at the back of the aft pylon, each had four.  It appears that the static cords were affixed sometime after the aircraft were renumbered from the 400 series. Since other aircraft never received the cords it can be assumed that those that were so equipped were done so on a trial basis.  It is therefore probable the static cords did not meet expectations. Given the size, speed and materiel makeup of the tandem rotors, it was likely hoped that the cords would dissipate some if not all of the static electricity generated by the turning rotors.

In addition to the four static discharge cords, the picture shows a red, white and blue 302 with a Voyageur tail. Photo via Mike Belcher

Aircraft 303 stripped for repainting still wearing the static cords. Photo via Pat Mercer
The tremendous amount of static caused some problems for those being hoisted. To dissipate the built up static charge persons being hoisted down wore a weighted length of light weight chain covered by rubber tubing that dangled a few inches below the persons feet so the chain would come in contact with the ground before the person. On one occasion, I was one of those hapless souls who neglected to attach the chain to the hook…when I contacted the ground the build up static charge reminded me why we used the chain. When on the ground, or a ship, waiting to be hoisted back into the helicopter we made a point of letting the hook touch the ground first so as not to get unceremoniously zapped.

By the time Labradors had been modified with tail mounted APUs, only aircraft 302 was left with the cords.  303 When modified for the APU received a completely new tail resulting in the elimination of the static cords, whereas 302 had received a new Voyageur style tail following its early incident.  As noted previously, 302 received the tail, but no APU…that is until all Labradors were fitted with the tail mounted APU.!

In addition to the static discharge cords, note the position of the Squadron badge. Photo DND



Hydraulics vs. Electrics (Ramp)

While the ramps of the CH-113 and CH-113A were for a time functionally different, visually they were almost identical.  It is unlikely the average modeler will take the time to deal with the comparatively trivial differences.

Labrador ramps were electrically operated whereas Voyageur ramps were hydraulically operated.  The Labrador ramp could be operated using switches located at the front of the cabin or at the left rear of the cabin, but slightly ahead of the engines.  There were also switches on the left side, and outside, of the tail below the aft pylon.   Once activated the ramp movement, up or down, was facilitated with screw jacks located one on either of the ramp a few inches aft of the ramp/fuselage hinge.  Essentially large worm gears, the screw jacks were dark gray, almost black, in colour.


Aft ramp/hatch switches
 


Parachute anchor line cable
 

Several things in this picture of a Labrador interior are worth noting if you intend to have your model showing the interior. Notice the hoist location and cover; the door leading to the cockpit; the lack of gauges on the SAS closet and the cabin insulation. The hoist above is rigged to assist in the recovery of a hung up parachutist. Photo Randy Brown collection

Voyageur ramp movement was initiated by one set of controls; two control levers, located below the engine compartment and aft of the ramp/fuselage hinge.  The same levers could be accessed from the inside or from the outside by reaching through a small hatch.  A pair of ramp actuators that were silver in colour facilitated movement of the ramp.  At some point late in the service life of the Labradors, probably SARCUP, hydraulics replaced some electrically operated functions such as the ramp and the internal back up hoist.
Voyageur ramp controls, as seen above, were in one location at the back of the aircraft, but could be accessed from either inside or outside of the helicopter. Photo Randy Brown collection

The only other ramp difference was the existence of rollers on ramps of Voyageurs, a continuation of those on the fuselage floor, which will be discussed, in later paragraphs.  Rollers were an Army requirement not considered for Labradors. When Voyageurs were transferred to the Air Force for SAR duties, the rollers were at some point removed.  A lack of relevant photographs makes it difficult to narrow the period of their removal down.!

Nice shot of a Labrador ramp and ramp extensions. Other things in this photo of use to the modeler are the left side drain covers and the silver hydraulic ramp actuators on either side of the ramp for years more commonly associated with Voyageurs (Labradors had screw jacks). Photo courtesy Jeff Wilson

The above photo shows the Voyageur ramp with the roller channels, but not rollers. Photo courtesy Scott Hemsley


Engine Inlet Screens

Pictures show that Labradors, when purchased, did not have engine inlet screens. Whether Voyageurs did or did not is not clear. In any case, both variants were fitted with the same conical shaped screens early in their service life.  The purpose of the screens was to prevent debris from being ingested into and damaging the engines.  When looked at from head on it is interesting to note that the inlets screens are neither exactly conical in shape nor symmetrical when comparing left with right screens.  In part, the asymmetrical shape is because the sync shaft tunnel is not centered on the top of the fuselage.

Note the lack of engine inlet covers on airframe 11401. Photo via Pat Mercer


Note the shape of the engine inlet screens and their position relative to the sync shaft tunnel. Photo Randy Brown collection

In the spring of 1989 as my time on Labradors was ending, there were discussions regarding new engine inlet screens.  From what I can recall, it seems the conical screens while effective against foreign object damage (FOD) had a tendency to ice up enough to reduce airflow to the engines in certain weather conditions.  I believe the larger screens were thought more likely to cancel out the potential for engine failure from weather conditions.!

Newly installed "top hat" engine inlet screens. Photo via Pat Mercer

The above photo shows the right side engine inlet screen. Photo courtesy Jeff Wilson

Stability Augmentation System (SAS) Closet

At the front of the cabin on the right side of the fwd bulkhead is the SAS closet.  Unlike their American counterparts, Canadian aircraft had covers over the SAS bay. Voyageurs SAS closet covers, because of the greater use of hydraulics, differed from Labradors by having two gauges located on the upper SAS closet cover.


Electric hoist replaced with a hydraulic hoist.
 


Crash axe stowage and the securing strap above it.  Because this aircraft is on public display, the crash axe has been removed.
 

The interior look of Labradors changed several times over the years. The above photo shows the resultant changes. Note the rolled up blackout curtain to the left of the door leading to the cockpit; the location of the door brace near the front door; the absence of gauges on the SAS closet. Photo courtesy Jeff Wilson

Where the Voyageur had the two gauges, Labradors had a crash axe. In Voyageurs, the crash axe was a few inches below where it was on the Labs.  Moreover, because the Voyageur differed from the Labrador in that it had a soft blackout curtain instead of the Labrador’s blackout door, the Voyageur’s map case was located on the lower SAS closet cover. The map case on Labrador was on the cabin side of its’ blackout door. The last thing to go on the SAS cover was the lower Dutch Door brace.!
On the Voyageur SAS closet covers in the photo above you can see the two gauges, the crash axe, door brace and to the right of the brace the map case.  A portion of the black out curtain can also be seen. Photo courtesy Scott Hemsley

Black out curtain/door

As mentioned in the foregoing paragraph both variants utilized, albeit different style, black out methods to allow Para Rescue personnel (eventually Rescue Specialists then SAR Techs) to prepare for an mission or to carry out medical care on patients in a lit cabin while not negatively affecting pilot night vision in the cockpit, a light barrier was required.  In the Labrador, the barrier was a door, while on the Voyageur a zippered blackout curtain was employed. Labrador blackout doors were eventually removed and replaced by the more practical blackout curtain.!

The map case can be seen on the lower part and back of the padded and closed door leading to the cockpit. Photo Randy Brown collection

Cabin Insulation

Yet, another feature that will likely be ignored by all but the most thorough of modelers, especially in larger scales, is the cabin insulation.  The most noticeable difference between the insulation on one variant compared with the other was colour.  Early insulation on the Voyageur was a very pale green compared with a light to medium gray on the Labrador.  The two different insulation materials do not lend themselves well to scale modelers so will be avoided, that said, as insulation wore out and was replaced the difference in insulation slowly disappeared until eventually all insulation was that of the Labrador.

The picture above clearly captures the difference in colour of the original Voyageur insulation and that of Labradors. The lighter green insulation used originally in Voyageurs can be seen on the cabin ceiling and wire/tubing tunnel covers. The walls are adorned with gray replacement insulation more commonly associated with Labradors. The aircraft above is from 103 Rescue Squadron (Gander, NL) and is participating in Search and Rescue Exercise (SAREX), thus the reason all eyes are in the windows. Photo DND

The insulation on either variant is straightforward. The criss-cross pattern often associated with aircraft insulation is incorrect for Labradors and Voyageurs. On these helicopters, the insulation was nothing more than a padded material that did not have cross-stitching. It was held on to the airframe in one of two manners and in some cases or locations both. The older method (although still used to a degree) was to use snaps. The second method was Velcro.  Here is where it could get tricky modeling insulation if you were really into the accuracy thing. Before, an airframe arrived back at the unit (after being in Arnprior for thorough maintenance) the insulation was installed (or reinstalled) before fixtures and fittings were put back into the cabin. Everything...including the radio boxes, which were set into a position essentially recessed behind the insulation, had covers. It did not take long for these covers and other similar covers to go missing leaving structural components including the outer skin, exposed. Also behind the insulation were the 28 volt outlets, heating duct controls and for a time the hoist controls. Access to these areas was frequent and the constant tugging and pulling of the insulation resulted in Velcro strips glued to the airframe coming off leaving the insulation hanging. It would only be a nuisance for so long before someone would "store” a part of the insulation, notably the blanket in front of the hoist station, for safekeeping.

To model the insulation, two methods I would consider are simply to paint the area using a “tromp loie” effect or tissue painted with a white glue/water mixture. In my opinion detailing the insulation is easier and less tedious that adding the wires, tubing and pipes of the Lab/Voyageur, although it would certainly be less dramatic.

The 424 Transport and Rescue (T & R) Squadron, Trenton Voyageur trains CASARA spotters. Wire/tubing tunnels unique to the Voyageur can be seen on both sides of the cabin at a point where the walls transition into the ceiling. Photo courtesy of Terry Cooper

Looking at the point were the cabin walls merge into the ceiling, it is clear there are no wire/tubing tunnel covers in the Labrador. Photo courtesy Jeff Wilson

A difference in insulation that did not disappear was the use of wire and tubing covers in the Voyageur. The pictures above clearly show the covers, which ran the length the fuselage, on both sides of Voyageurs only.!

Pilot Seats

A difference that is seldom mentioned is the difference in seats styles, including the difference between the pilot seats of the Labrador and Voyageur. On the left is the Labrador seat, on the right the Voyageur seat. This is a difference I believe remained for the life of the aircraft.

 



Flight Engineer Seat
While the Flight Engineer seat in the space between the cockpit and cabin differed in the two early 113 variants, there was no difference by the time SARCUP was completed.  For the time being, I lack photographic evidence to support my recollection that the seats once differed, however after conferring with an FE friend, I have some specifics.

One of the things I remember well was that the Voyageur FE station was considerably less comfortable than the Labrador version. This is due to a couple of things. As can be seen in the pictures below, the Voyageur station had the rather large cabinet on the left side that the Labradors did not. The cabinet reduced the width of the space by several inches. The purpose of the cabinet is two fold. What can be seen at the top of the cabinet is the circuit breaker panel. On the Labrador the breaker panel is behind the copilot’s seat, a portion of which can be seen in the picture on the right and below.

The second purpose of the cabinet is that it housed some of the extra hydraulics the Voyageur used. Of particular note is the hydraulic hoist used in Voyageurs was situated directly above the companionway door leading to the cockpit and where the FE sat. Originally, Labradors used an electric hoist so did not need the bulky cabinet. As part of the many modification, both variants used the externally mounted, hydraulically operated hoist with an internally mounted hydraulically operated hoist as a back up. This required Labradors to be modified to accept the hydraulics and thus the new hydraulics cabinet.


Back of FE seat
 
 
While the two pictures above show the Flight Engineer (FE) seat on a Voyageur, there is little difference on a Labrador. The picture on the left shows the FE seat stowed on the right side of the tunnel. The picture on the right shows the back of the FE seat hanging limply on the aft portion of the breaker box (to the left of the coiled intercom cord). Both photos courtesy of Scott Hemsley

The second reason the Labrador FE seat was more comfortable, is that the Lab seat was wider, had the same tube frame structure for not only the seat, but the seat back as well, which was sufficiently padded for comfort. As can be seen in the picture above right, the Voyageur seatback was basically a strap. While not a significant difference, the final difference in FE seats is that the Voyageur FE seat was stored on the right side of the companion way, the Labrador seat was folded up on the left side of the companion way.

Spotter Seats

There is on the other hand plenty of documentation to demonstrate the difference in spotter seats.  The seats located at the forward search blisters were an essential part of SAR Labradors, but unnecessary weight and bulk in the troop carrying Voyageur.  Voyageurs, as one might expect of an Army transport helicopter made use of troop seats when carrying personnel.  Troop seats were of the standard red nylon variety typical of all Canadian aircraft.

 
The picture on the left above and the drawing on the right above show the original seat fitted on the Labrador. The seat was less crashworthy than its' replacement, due in part to its' short back. Photo Randy Brown collection
 
While Labrador seats were originally painted black, they like all Voyageur seats were predominately gray. Seat covers on both style seats varied from green, to red or orange. Photo courtesy Scott Hemsley

When Voyageurs became part of the Air Force SAR inventory, proper spotter seats became a necessity, however where to get seats?  The answer, I believe, was in the Argus.  The Argus seats, if in fact they are Argus, seats were taller and more robust than those of the Labrador, so it made sense to eventually replace the Labrador seats as well.  When the Labrador seats were replaced and the source of the new seats is unclear, but I suspect the source of the seats was the Argus, which was being replaced by the Aurora.!

Box seats

Along the right cabin wall behind the right spotter seat were three box seats that doubled as equipment storage.  Technically, the boxes differ, but in size and colour only so from a modelers perspective hardly worth the effort to acknowledge the difference.  The main difference in the seats was the colour of the cushions and the boxes themselves. Along the wall, both variants used the back of the red nylon troop seats.

Labrador seat cushions arrived from the factory covered in red nylon.  Voyageur seats were locally manufactured, accounting in part for the different size, so the cushions were covered in whatever material was locally available.  In my experience, red, blue or tan leatherette were common.

The locally manufactured boxes used in the Voyageurs were made of sturdy gauge aluminum that was left unpainted for several years.  Labrador boxes were painted the same colour gray as other interior features.!


As can be seen in the above photo, the two back seats have two lids each, while the forward most box has a single lid. Photo courtesy of Derek Heyes


Hot Cups

Internally, for the most part modelers will consider several differences inconsequential.  For the sake of a few lines of text, I have included them for that modeler who might want to build a larger scale version or the modeler who might want to do a cutaway version for example.

At the time of purchase, neither the Lab nor Voyageur had hot cups to heat water for a hot drink on the all too frequent long flights or cold days.  Originally fitted in the C-47 Dakota, the Labrador was the first SAR helicopter to be fitted with hot cups.  Two cups were installed one above the other on the right side of the cabin wall immediately ahead of the search blister.  The bottom cup was only inches above the floor and just a couple of inches ahead of the station inline with front of the front search blister.

As the Voyageurs integrated into the SAR fleet, crews heated their hot water in a single hot cup attached to the aircraft electrical system by a long umbilical power cord.  The single hot cup was eventually replaced by two hot cups attached to the front of the radio rack that was eventually installed ahead of the left side SAR Tech chair on the left side of the cabin.  To the best of my knowledge, Labrador hot cups were eventually relocated to the left side of the cabin as well.!

The hot cups were affixed to the front of the radio rack on the left side of the aircraft slight aft of the left side emergency door. Photo DND


Section 3

Operational Differences


Operational differences will look at equipment or features of the Labrador and Voyageur from an operational perspective.  Because both of these aircraft served in the search and rescue role for most of their existence the majority of the discussion will focus on SAR.!

Antenna

It is in all probability doubtful that the antennae on one aircraft matched exactly that of another such was the pace of change with radios and navigational equipment.  For this reason alone I will not get too much into the various antennae, save for two notable examples; High frequency (HF) and Search and Rescue homing (beacon).  It is incumbent on the modeler to check photos carefully if accuracy is your aim with respect to antennae. I will where possible be identifying the various antenna, if the antenna is identifiable.

HF Antenna Masts
 



HF Antenna
 


At the time of the helicopter purchase radios and navigational aides were barely out of infancy compared to what aircraft of the ‘70s, ‘80s and beyond would have.  Perhaps one of the most important pieces of equipment was, and maybe still is, is the High Frequency (HF) radio.  HF gives aircraft crews the ability, under the right conditions, to transmit/receive to and from another station anywhere in the world.  HF radios have been a part of the Labrador’s communications arsenal since the earliest days and continued to be so until retirement. Pictures of HF radio antennae as they changed over the years illustrate changes in HF antenna design and location that are representative of antennae evolution for all radios and navigation aids. One picture in Mr. Pat Martin’s book shows 305 with a blade HF antenna painted green whereas the more common colour was blue. Yet, another picture shows a yellow aircraft carrying the blade antenna on the left side, which became the standard. In Pat Martin’s newest book, “Royal Canadian Air Force – Aircraft Finish and Markings 1947-1968 – Volume 2”, there is a picture of a RWB Labrador with the blade antenna just aft of the front door on the right side of the aircraft…I am of the opinion that this was part of HF trials. To further illustrate my point regarding antenna location, a couple of pictures show Labrador 301 with the final version of the HF antenna in the same location as the HF antenna on Voyageurs. A picture from a later date shows the HF antenna on 301 in the standard location for Labradors. It is unclear why there is a difference in the HF locations on the later date Labs and Voyageurs, but it is a certainty the difference was maintained until retirement.

The object of our attention is actually Labrador 405 in the background. Of note is the green HF blade antenna on a Labrador still wearing its' 400 series number. Photo DND

The HF blade shaped antenna was fitted to the fuselage just aft of the left side emergency door and far enough ahead of the front search blister so as not to be too restrictive to the spotter on the left side during searches. Photo courtesy of Dave Marshall

Pre-SARCUP Labrador 305 sports a yellow paint scheme, a yellow HF blade antenna and black "RESCUE" titles. Photo via Pat Mercer

I seriously doubt that even the most ardent of modeler is going to model the instrument panel and console to follow the changes in the various radios and nav aids, indeed it might be impossible in scales smaller than 1:48, however the change in antennae is doable. One of the earliest antennas that present the modeler with a manageable challenge is SARAH. Radios early in their developmental stages were comparatively unsophisticated and of limited function; so much, so that it was uncommon for downed aircraft to be able to communicate with searchers. Additionally, searchers lacked any real technological means to locate the downed aircraft. “SARAH”, (search and rescue homing beacon) changed that.

The photo above shows the positioning of the HF antenna overtop of the lightning stripe on the Voyageur. Photo courtesy Derek Heyes

Unlike the Voyageur, the Labrador's HF antenna is positioned above the lightning stripe. Photo courtesy Jeff Wilson
Unfortunately, I have virtually no information on early Voyageur antennae. This is particularly so for the early years through to the time when Voyageurs were painted yellow and modifications were being undertaken to make them SAR capable.!

The above photo gives you a close look at the right side SARAH antenna. A second identical antenna is located in the same position on the left side. Photo Randy Brown collection

In addition to the left side SARAH antenna, the above photo shows the forward HF antenna mast and the HF antenna entering the fuselage through the lightning stripe. Photo via Pat Mercer



Floors

Voyageurs were purchased by the Army to move equipment and personnel from rear echelon positions to positions closer to the action.  The distance between the two positions was relatively short so as has been noted Voyageurs were not fitted with long- range fuel tanks.  If greater range was needed internal, fuel bladders could be added a modification that took, as I understand it, about three years to implement.  Operationally, the role of the Voyageur was essentially that of a transport.

To accommodate expedient loading and unloading the floor of the Voyageur was more robust than that of Labradors.  The center panels of Voyageurs were built to handle heavier loads of vehicles and military pallets.  On either side of the center panels was a row of rollers and outside of the rollers were vehicle tread ways designed to handle rubber-tired (as opposed to tracked) wheel loads.

Rollers were in place the full length of the fuselage and ramp.  The cargo ramp also had two smaller folding ramps that could be positioned at any point along the width of the ramp to accommodate a variety of different sized loads.

Although the rollers have been removed, the roller channels are clearly visible.  At the end of and to the outer edges of the ramp are the two ramp extensions. Photo courtesy Scott Hemsley

The floor of Labradors was unlike all other CH-46/KV-107 models in that the construction of the floor was lighter and lacked the rollers.  At some point in their SAR careers rollers were deemed expendable and removed from Voyageurs, although the roller tracks and small ramps additions remained.!

The Labrador did not have rollers as can be seen on the ramp above. In the above photo it also easier to see the two ramp extensions. Photo courtesy Jeff Wilson

The above photo gives us a clear look at the rollers. Photo DND

Hoists

In keeping with the Army’s, transport role for the Voyageurs the CH-113A was equipped with a robust hoist that was geared primarily to “pull” heavy equipment and vehicles into the cabin.  In addition to the slow rate of operation, the hydraulically operated hoist used a shorter thicker cable than that of the SAR Labradors.

Even after external hoists had been installed, external hydraulic hoists were retained as a back up on both variants.  Photo courtesy Scott Hemsley

While the Voyageur was a credible secondary SAR resource, it still lacked an efficient rescue hoist. As Voyageurs were absorbed by the Air Force into the primary SAR role their limitations where recognized as a serious impediment since the Voyageur hoist was used through the floor at center of the fuselage.

Master Corporal Dave Aalto of 413 Squadron demonstrates use of the "Sky Genie" friction descent device and the Voyageur's center hatch hoist. Photo Randy Brown collection


Designed for search and rescue, the Labrador counted on versatility to ensure reliability.  While the Labrador had only one hoist, that hoist could be used in different configurations.  With a longer hoist cable, the electrically driven hoist was geared to operate faster than its’ Army counterpart.  The 113-hoist cable was routed through a series of three pulleys from the forward bulkhead aft to the ceiling, to the left side of the cabin opposite the open door and through a bell housing on the internally mounted (Swedish) boom hoist.  The Swedish boom, was then extended forward through the open doors to facilitate a rescue procedure.


ELT
 


Swedish boom bell housing.
 

In addition to the location of the Labrador's hoist and the cover on the bottom of the hoist, note the position of the bell housing on the Swedish boom when the boom is in the vertical position. The hoist above is rigged for para-drops. The fact the parachute anchor line cable runs along the cabin wall indicates the photo is late 1980s at the earliest and more likely 1981. Photo Randy Brown collection

Occasionally, as might be expected, the infrequent problem with the Swedish boom necessitated use of the hoist through the center hatch.  Like the Voyageur, the cable was routed from the forward bulkhead along the center of the ceiling to a hard point and pulley system directly above the hatch.


With the Speedline modification program, all 113s were equipped with a much faster hoist with a longer cable.  The new hoist was capable of carrying 600 pounds up or down compared with the 600 pounds up and 300 pounds down for the older Labrador hoist.  By the time, all aircraft were equipped external hoists both Labradors and Voyageurs utilized hydraulic hoists as a back up to the Speedline upgrade.

One last aside, the earlier electric hoist used by the Labrador was more compact and was affixed to the cabin bulkhead above the companionway leading to the cockpit. While it was not centered exactly, it was more centered than the hydraulic hoist of the Voyageur. The reason lies in the size of the hydraulic hoist and the extensive array of hydraulic lines. A lack of space to accommodate the hydraulic lines, the only option was to move the larger Voyageur hoist slightly to the left.!

The 1971 photo above shows both the position of the lower Dutch door and the Swedish boom in the hoisting position. Note the position of the bell housing during hoisting. Photo Randy Brown collection
The photo above gives you a good look at the multitude of lines running to and from the external hoist. Photo courtesy Derek Heyes

Scott Hemsley gives us a good look at the hoist from below. Photo courtesy Scott Hemsley



Water Dam

Amphibious helicopters, both the Voyageur and Labrador exercised regularly and often in the water.  At times both variants conducted water borne procedures that necessitated opening the ramp and upper hatch.  To keep water from out of the cabin and from sinking the aircraft, a water dam was used.


Once a routine procedure for SAR Labradors and Voyageurs, the boat launch and recovery procedure was eventually phased out. Here Rescue Specialists exit the helicopter as they prepare to lower the outboard motor. Photo Randy Brown Collection

The dam of each variant differed only marginally, and perhaps not enough for the modeler to notice.  Firstly, the dams were constructed of different materials and finished differently.  The Labrador ramp was made of lightweight metals and finished in the same gray as the interior of the cabin.  The Labrador dam, when in place at the end of the bench seats and ahead of the ramp was no taller than the box seats.

In the Voyageur, the ramp was made of wood and finished with a clear varnish or lacquer, so looked like a finished sheet of plywood.  Voyageur dams were slightly taller than that of the Labrador with the top of the dam above the top of the box seats.

Another noticeable difference between the dams of these two aircraft was their storage location when not in use.  It was common for the dam to be in place, especially when the aircraft was on SAR standby, however this was not a hard and fast rule.
At one time, the two variants stored their water dams in different locations, but that eventually changed and both stored the dam on the left side of the ramp inner fuselage. Photo courtesy Jeff Wilson

On either bird, the dam was occasionally stored behind the stretchers at the rear of the cabin, however the more usual storage location was on the ramp area sidewalls, the Lab dam stored on the right side the Voyageur’s stored on the left side.  Since the Voyageur had a hydraulic hand pump at the forward end of the ramp on the right sidewall, placement of the dam in this location was impractical, so the same location on the left side was selected.

In later years, the water dam was stored in the same location on both variants. Photo courtesy Jeff Wilson


Although the Labrador above has the hydraulic hand pump in the same location as a Voyageur, the style of the handle is somewhat different. Before being modified with a hydraulic ramp, Labradors stored the water dam in this location. Photo courtesy of Jeff Wilson

Despite practicing, several different waterborne procedures frequently right up until the late 1980s there are only a handful of rescues where the aircraft was actually put into the water to conduct the rescue. As an exclamation mark to the aging aircraft’s declining ability to conduct water ops, 424 Squadron Trenton almost lost a helicopter during a rescue because the crew forgot to put drain plugs in place…at one time an instinctive procedure for all crew members.!

The different style hydraulic hand pump handle can be seen clearly in the above photo. Photo via Pat Mercer
Labrador 304 performing a rare operational water borne rescue off Vancouver Island. Photo DND

March 18 – 1978; Labrador 304 from 442 T&R Squadron, CFB Comox crewed by Major Mike Angelsey (AC), Captain Mike Clark (FO), Flight Engineers Dennis (BJ) B., Bob Ardelien(sp) and Rescue Specialists Don Lane and Danno Schut prepares to recover five survivors from the life raft of the fishing vessel (FV) Mothers Three. The crew of 304 was deployed to Tofino to watch the herring fleet when RCC diverted them to the Mothers Three. A Comox based Argus was assigned as top cover for the Labrador when it took the above picture.

Attempts to hoist the survivors from the raft were aborted. It was later learned the rafts’ sea anchor was not deployed causing the rotor wash to blow the raft aimlessly about the calm sea. Following a short discussion, it was decided that Rescue Specialist Team Leader Don Lane would swim to raft with rope in hand. Once on board the raft, the now six persons would pull themselves towards the helicopter’s right side door. After being adrift on the Pacific for five days, the crew of Mothers Three was returned to dry land via Port Hardy and a short hospital stay.

An interesting aside to the story is that the rope used to pull the raft to the helicopter was tied around the right spotter seat post and may have contributed to the seat breaking…and by extension perhaps a contributing factor in the reason Labrador seats were replaced with Argus seats?  Danno Schut provided details of the rescue. !


SAR Mewasige, a 424 Squadron Trenton Voyageur picks up survivors from a grounded boat off Mississagi Island, Ontario. Photo Courtesy Ted Brown (424 Squadron Buffalo Flight Engineer)
Chapter 2 – Evolution to Common Features

In Chapter two, the discussion will move from differences to traits and features that were common to the Voyageur and Labrador.  While some of these features were present from the outset, other commonalities were arrived at through evolution, either from one variant’s feature being employed on the other or an entirely new feature new to both variants.  Rolled into one discussion are the common structural, functional, operational and visual features.!

Section 1
 
Visible Features

This section will deal with the areas of detail that contributed to the “look” of both 113s and 113As starting with some short lived differences before moving on to what eventually became the “common look” of the two variants in the SAR role.  Some of the things I will cover herein may not be covered in Pat Martin’s books (although I could be wrong) or anywhere else because they are obscure and/or mundane, such as the colour of door handles and/or, the colour of wheel rims. Also covered are aspects of markings that do not constitute a full-blown paint job.

Both the Labrador and Voyageur were given paint schemes commensurate with their respective roles.  The Voyageur was green overall while the Labrador was assigned the red, white and blue scheme of aircraft working on northern radar sites of the MID Canada Line where high visibility was essential.  Clearly both types would benefit from a change to yellow while working as primary SAR resources. A personal note: while I liked the look of the yellow livery, which would become synonymous with SAR, I with my many, many hours of search time cannot possibly believe that yellow was the most effective colour to paint a SAR aircraft especially in the fall months.!

Anti-skid patches

On both the Voyageur and Labrador, upper surface markings were authorized to be painted either gray or black. These areas included a nearly fuselage length walkway to the left of the sync shaft tunnel, a small step area behind and slightly aft of the forward pylon and walkways on the aft portion of the stub wings. For further information regarding the shape and colour specifications, refer to Pat Martin’s books.  Some photos show later schemes with a small patch to the right of the sync shaft tunnel and slightly aft of the forward pylon.!

Walkway areas may be gray or black. Note the gray areas on the tanks in the above photo are one piece and appear rectangular. Photo courtesy Derek Heyes

When comparing the walkway areas on the two photos above, not that the walkway areas on the bottom photo are narrower at the bottom of the walkway than those in the top photo. The walkways in the bottom photo appear black not gray, but this may be a result of us?  Photo courtesy Derek Heyes

Walkways on the above pre-SARCUP Voyageur are painted on the stub wings in two pieces and are gray. Photo DND

The extra walkway area on the right side of the forward pylon originated on Voyageurs, however it is likely that both variants shared the same painted on walkways by the time SARCUP was implemented. Photo courtesy Scott Hemsley
Photo courtesy Scott Hemsley

Aft pylon

While differences in the colour of red/orange used on the aft pylon are documented, some painting omissions are not. One area of note is the absence of red on the forward part of the aft pylon on Labradors as they were accepted into inventory.  Additionally, there is a black strip painted on the front of the aft pylon’s clamshell doors as can be seen in the photo at the top of the next page.

 
Note the differences in how the forward part of the aft fuselage is painted. The photo on the left is a Labrador as it was delivered to the RCAF. The painting omission appeared on early Labradors painted with 400 series numbers. Both photos courtesy of DND

The black strip on the forward part of the aft fuselage starts at the bottom of the clamshell doors on 400 series Labradors and likely appeared for only a short period. Photo DND

Labradors were delivered to the Air Force with a narrow strip of the aft pylon painted black to hide exhaust. Photo DND

 
It did not take long before the black area on the aft fuselage was enlarged as the photo above and left shows. The change occurred while the aircraft were still using white 400 series numbers. Photo DND
While the two photos above show that while the black exhaust area remained generally the same size, the shape would evolve as can be seen in the photos above and below. All four photos DND

 

With respect to the exhaust path on the aft pylon, refer to Pat Martin’s books where Pat addresses the size of the area to be painted black. Pictures illustrate this feature.!


Fuselage underside
As per RCAF directives, a red rectangle was painted on the underside of the fuselage.  The rectangle measured 6’ by 2’.  Other markings on the underside that are not addressed in Pat Martin’s books are the two circles, one black the other silver. It is my assumption, that the silver circle is an access panel, but for what equipment is anyone’s guess. It may very well have something to do with access to the attachment of the nose gear?  As for the black circle on the underside of the forward fuselage, I am at a complete loss.!

The red area on the bottom of Labrador fuselages was unique to red, white and blue Labradors. Photo DND


The black circle on Labrador fuselages is visible in the photo above. Photo courtesy Derek Heyes
The silver circle in front of the main gear is clearly visible in the photo above. Photo DND


Wheels

While there were specific colours authorized for the wheel rims on both 113 variants, the reality was more of a smorgasbord of coloured rims.  While each variant was being maintained, within their own element, it is likely; there was little deviation from prescribed directives; silver (aluminum?) or green for the Army and white, or aluminum I believe for the Air Force variant.  Real changes started when Voyageurs were accepted into Air Force inventory.  Red, white and blue Labradors were commonly seen with white wheel rims, however it was just as common to see them with silver or green rims as well after the Voyageurs arrived at SAR bases.

Labrador 401 in the early red, white and blue livery that included blue wheel rims. Photo DND
Labrador 402 sporting the 400 series numbers, but the later version red, white and blue livery and aluminum wheel rims. Photo DND


Aircraft 403 with black 400 series numbers shown above with aluminum nose wheel rims and blue main wheel rims. Photo DND

While they do exist, I do not have a picture suitable for inclusion here that shows a red, white and blue Labrador with green wheel rims.
Labrador involved with CPI trials has white rims all around. Photo via Mike Belcher

Voyageurs while in Army inventory could be found with either green or silver rims. Like the Labrador, there was no consistency in use of the various coloured rims.  One or more of the four main rims might be green and the remainder silver.   Once the Voyageurs transitioned to SAR, they were the first to be repainted yellow. As they came out of the paint shop all of their wheel rims were presumably yellow, however in short order you could find yellow Voyageurs and then eventually yellow Labradors that had wheel rims that were, silver, green (for a short time), white and/or yellow.

Voyageur 410 in early Army colours, which included green wheel rims. Photo DND
Voyageur 315 in interim SAR livery as shown above has aluminum wheel rims. Photo via Pat Mercer


Voyageur 308 show here in early yellow SAR colours and aluminum wheel rims. Photo DND


The photo above taken in Gander while 308 served with 103 Rescue Unit shows her in new SAR yellow livery with the early RESCUE titles and yellow wheel rims all round. Photo DND


Voyageur 308 in new SAR yellow scheme with updated RESCUE titles shown here with yellow main wheel rims and white nose wheel rims. Photo DND


Yet another view of Voyageur 308, however this photo shows 308 with white wheel rims all round. Photo DND

The inconsistent use of coloured rims gives the modeler a great deal of latitude to create a subtle uniqueness to their version of the Labrador or Voyageur.  As aircraft were being rotated through, the paint shop in their maintenance cycles yellow aircraft could still be found to have white rims. It seems that there was consistency only at the time of purchase and after all aircraft had been painted yellow and fitted with radar.!

Mirrors

As previously mentioned, only Labradors had mirrors.  While still using the 400 series aircraft numbers, the mirrors were painted overall blue.  In time and as the aircraft switched to the 300 series, red, white and blue Labradors had their mirrors painted predominantly red with white candy striped supports.  Once all the helicopters were painted SAR yellow, the only change with respect to the mirrors was that the white striping changed to yellow.  To the best of my recollections, on at least one aircraft for at least a short time, the red mirrors lacked any striping.  Whether this was a one off or not is pure conjecture, but I believe this was the case. Eventually mirrors were removed on all 113s before they were retired.!
It is unclear how long the mirrors remained on 304 and 305, the last two Labradors with mirrors.         Photo DND

Stability Augmentation System and Pitot Tubes

Both Labradors and Voyageurs use a stability augmentation system (SAS) to keep the aircraft stable in flight and in the case of 113s to keep the aft rotors from trying to catch up to the front rotors.  While the helicopter could be flown with the SAS off, it was much more challenging and certainly not as smooth a flight.  If the SAS kicked off while in the hover or unexpectedly, it made things potentially dangerous.  The two-channel SAS system utilized SAS (static) ports on both the nose and fuselage of both variants.

Where they differed was in the number and location of the static ports.  Both types had four ports on the nose, two on the left and two on the right. As previously mentioned, the location of those on the Voyageur differed slightly because of the extra nose glass.  The Labrador also had three static ports on either side of the fuselage, the Voyageur just two. I do not know if the third static port meant the Labrador at one time had a back up channel or if it was tied to another function?

The red circles on the nose of this early Labrador encircle the SAS system static ports. The large red circles around the ports will eventually be much smaller. Photo DND

Voyageur static ports
 


 
The shape of the two outer glass panels is in part determined by the relocation of the static ports on Voyageurs. Photo courtesy of Derek Heyes


3 Static ports
 
 
The two DND photos above show the three static ports on each side of the red, white and blue Labradors.

Problems with the cable cutter cartridges prompted this 103 RU innovation called "SARMUG". Note that the yellow Labrador still has three static ports on each side of the fuselage. Photo Randy Brown collection.

Voyageur 313 in variegated camo livery. Note the two static ports just aft of the door. Photo via Pat Mercer


Voyageur 409 shows the two left side static ports. There were two more on the right side of the fuselage. Note the emergency exit door and the silver circle ahead of the nose gear. Photo via Mike Belcher

The pitot static system also utilized a port to provide among other things, airspeed. When the Labradors were purchased, they were equipped with two pitot static tubes on the right side and one on the left side of the fuselage.  They were located above and aft of the cockpit doors.  Voyageurs had only the set of two pitot tubes on the right side fuselage.  At some undetermined point in time the left side single pitot tube was removed from all Labradors.  At the same time, the number of SAS ports on both sides of the fuselage was reduced from three to two. On the right side of the fuselage, the SAS static ports were just aft of the lower Dutch Door and on the left just aft of the bottom of the emergency door.  Photographic evidence reveals that aircraft 304 was the last to shed the left side pitot tube but only after it had been through SARCUP.!

Labradors were originally fitted with a single pitot tube on the left side. Note there is no vent behind the cockpit door. Photo via Pat Mercer
A close up look at the right side pitot tube common to both the Labrador and Voyageur. Photo courtesy of Scott Hemsley

The photo above shows the location of the right side pitot tube. Photo courtesy of Derek Heyes
The above photo shows a SARCUP modified Labrador sporting both mirrors and the left side pitot tube...neither of which survived until Labradors were retired. Photo DND

Hover Lights

Labradors as stated earlier use their fully articulating landing lights in a variety situations from landing, to search or when in the hover because they can.  To enhance its’ single articulating light, the Voyageur was fitted with a hover light just aft of the center hatch and slightly to the left of midline.  This light, as the name implies, was used for those situations were the Voyageur was required to hover at night.  My presumption is that the light was likely located here to give the Flight Engineer a better look at the ground or objects below during SAR procedures. As Voyageurs were mobilized for SAR duties, the center hatch was used more often to facilitate SAR procedures and was the position from where Flight Engineers coordinated hoist and sling operations. Slinging at night would be but one example of where the hover light would be of use.


Hover light
 

Unlike Voyageurs, Labradors were not originally fitted with center fuselage hover lights. Photo DND


Note that the Labrador in the above picture does not have a hover light in the area of the centre hatch. Photo via Randy Ward.



Labradors were not purchased with hover lights and as late as the “Speedline” series of modifications and it seems they were not fitted with them.  As near as I can confirm through photos, hover lights were installed on Labradors as part of “SARCUP”.!

Aft Pylon
Likely, the most noticeable difference, to the educated, between Labradors and Voyageurs is the inclusion of a tail mounted auxiliary power unit (APU) on the Voyageurs.  In addition to a change in the basic profile of the tail, the auxiliary power unit installation meant relocating, albeit only a matter of inches, the white aft navigation light.

Photographer Derek Heyes has superbly captured the shape of the Voyageur's tail.  Photo courtesy of Derek Heyes


Location of the navigation light on a Labrador would be here
 


White navigation light on a Voyageur
 

The photo above shows how the shape of the tail is affected by the built-in APU. Photo courtesy of Derek Heyes
Voyageur APU exposed. Photo courtesy Bill Ewing

Close up of APU from left side. Photo courtesy Bill Ewing

Labradors began life without auxiliary power units relying on start carts to power up when starting at home bases or suitably equipped airports.  The nature of search and rescue work, however meant operating unsupported in remote areas where start carts were a luxury they would have to operate without.  Labradors therefore relied on very taxing and potentially dangerous battery starts.  The solution was to strap a portable APU cart on the ramp.  It was not until late in SARCUP that Labradors were modified with a tail mounted APU. 305 For one was not modified with a Voyageur tail until after 1980, and was probably one of the last, if not the last, airframe to be modified with the new tail and APU.


Aircraft 305 sits in front of 103 Rescue Unit's hangar in Gander, Newfoundland sometime after 1980. Photo Randy Brown collection

Because of unspecified incidents, Labradors 404 lost it’s rear end shortly after being purchased and was fitted with Voyageur style tail early. Aircraft 402 however lost its tail in a landing accident at Coldfish Lake, B.C. in November of 1968. In both cases, while Voyageur shaped, the new tail did not include the APU.  The opening for the APU exhaust being blanked off and the navigation light relocated accordingly.

Another aft pylon feature that differentiated the two variants was the addition of drain covers on the Labrador.  Most pictures of Labradors wearing the 400 series numbers reveal that early Labradors did not have drain covers, while those in300 series numbers always seem to have the covers. The covers were fitted over all drains on both sides of the aft fuselage.  This difference also remained until the aircraft were retired.!


Close examination of 302's tail will reveal a Voyageur style tail but no APU. The photo shows 302's SAR Techs (in wetsuits) transferring a patient to a waiting Buffalo. The author is wearing the tan flying suit with a dark green flight jacket. Photos Randy Brown collection

Labradors were fitted with drain covers, which remained in place until their retirement. The covers were on both sides of the airframe. Photo courtesy of John Davies

Static Discharge Cords

Only Labradors 302 and 303 were equipped with static discharge cords at the back of the aft pylon, each had four.  It appears that the static cords were affixed sometime after the aircraft were renumbered from the 400 series. Since other aircraft never received the cords it can be assumed that those that were so equipped were done so on a trial basis.  It is therefore probable the static cords did not meet expectations. Given the size, speed and materiel makeup of the tandem rotors, it was likely hoped that the cords would dissipate some if not all of the static electricity generated by the turning rotors.

In addition to the four static discharge cords, the picture shows a red, white and blue 302 with a Voyageur tail. Photo via Mike Belcher

Aircraft 303 stripped for repainting still wearing the static cords. Photo via Pat Mercer
The tremendous amount of static caused some problems for those being hoisted. To dissipate the built up static charge persons being hoisted down wore a weighted length of light weight chain covered by rubber tubing that dangled a few inches below the persons feet so the chain would come in contact with the ground before the person. On one occasion, I was one of those hapless souls who neglected to attach the chain to the hook…when I contacted the ground the build up static charge reminded me why we used the chain. When on the ground, or a ship, waiting to be hoisted back into the helicopter we made a point of letting the hook touch the ground first so as not to get unceremoniously zapped.

By the time Labradors had been modified with tail mounted APUs, only aircraft 302 was left with the cords.  303 When modified for the APU received a completely new tail resulting in the elimination of the static cords, whereas 302 had received a new Voyageur style tail following its early incident.  As noted previously, 302 received the tail, but no APU…that is until all Labradors were fitted with the tail mounted APU.!

In addition to the static discharge cords, note the position of the Squadron badge. Photo DND



Hydraulics vs. Electrics (Ramp)

While the ramps of the CH-113 and CH-113A were for a time functionally different, visually they were almost identical.  It is unlikely the average modeler will take the time to deal with the comparatively trivial differences.

Labrador ramps were electrically operated whereas Voyageur ramps were hydraulically operated.  The Labrador ramp could be operated using switches located at the front of the cabin or at the left rear of the cabin, but slightly ahead of the engines.  There were also switches on the left side, and outside, of the tail below the aft pylon.   Once activated the ramp movement, up or down, was facilitated with screw jacks located one on either of the ramp a few inches aft of the ramp/fuselage hinge.  Essentially large worm gears, the screw jacks were dark gray, almost black, in colour.


Aft ramp/hatch switches
 


Parachute anchor line cable
 

Several things in this picture of a Labrador interior are worth noting if you intend to have your model showing the interior. Notice the hoist location and cover; the door leading to the cockpit; the lack of gauges on the SAS closet and the cabin insulation. The hoist above is rigged to assist in the recovery of a hung up parachutist. Photo Randy Brown collection

Voyageur ramp movement was initiated by one set of controls; two control levers, located below the engine compartment and aft of the ramp/fuselage hinge.  The same levers could be accessed from the inside or from the outside by reaching through a small hatch.  A pair of ramp actuators that were silver in colour facilitated movement of the ramp.  At some point late in the service life of the Labradors, probably SARCUP, hydraulics replaced some electrically operated functions such as the ramp and the internal back up hoist.
Voyageur ramp controls, as seen above, were in one location at the back of the aircraft, but could be accessed from either inside or outside of the helicopter. Photo Randy Brown collection

The only other ramp difference was the existence of rollers on ramps of Voyageurs, a continuation of those on the fuselage floor, which will be discussed, in later paragraphs.  Rollers were an Army requirement not considered for Labradors. When Voyageurs were transferred to the Air Force for SAR duties, the rollers were at some point removed.  A lack of relevant photographs makes it difficult to narrow the period of their removal down.!

Nice shot of a Labrador ramp and ramp extensions. Other things in this photo of use to the modeler are the left side drain covers and the silver hydraulic ramp actuators on either side of the ramp for years more commonly associated with Voyageurs (Labradors had screw jacks). Photo courtesy Jeff Wilson

The above photo shows the Voyageur ramp with the roller channels, but not rollers. Photo courtesy Scott Hemsley


Engine Inlet Screens

Pictures show that Labradors, when purchased, did not have engine inlet screens. Whether Voyageurs did or did not is not clear. In any case, both variants were fitted with the same conical shaped screens early in their service life.  The purpose of the screens was to prevent debris from being ingested into and damaging the engines.  When looked at from head on it is interesting to note that the inlets screens are neither exactly conical in shape nor symmetrical when comparing left with right screens.  In part, the asymmetrical shape is because the sync shaft tunnel is not centered on the top of the fuselage.

Note the lack of engine inlet covers on airframe 11401. Photo via Pat Mercer


Note the shape of the engine inlet screens and their position relative to the sync shaft tunnel. Photo Randy Brown collection

In the spring of 1989 as my time on Labradors was ending, there were discussions regarding new engine inlet screens.  From what I can recall, it seems the conical screens while effective against foreign object damage (FOD) had a tendency to ice up enough to reduce airflow to the engines in certain weather conditions.  I believe the larger screens were thought more likely to cancel out the potential for engine failure from weather conditions.!

Newly installed "top hat" engine inlet screens. Photo via Pat Mercer

The above photo shows the right side engine inlet screen. Photo courtesy Jeff Wilson

Stability Augmentation System (SAS) Closet

At the front of the cabin on the right side of the fwd bulkhead is the SAS closet.  Unlike their American counterparts, Canadian aircraft had covers over the SAS bay. Voyageurs SAS closet covers, because of the greater use of hydraulics, differed from Labradors by having two gauges located on the upper SAS closet cover.


Electric hoist replaced with a hydraulic hoist.
 


Crash axe stowage and the securing strap above it.  Because this aircraft is on public display, the crash axe has been removed.
 

The interior look of Labradors changed several times over the years. The above photo shows the resultant changes. Note the rolled up blackout curtain to the left of the door leading to the cockpit; the location of the door brace near the front door; the absence of gauges on the SAS closet. Photo courtesy Jeff Wilson

Where the Voyageur had the two gauges, Labradors had a crash axe. In Voyageurs, the crash axe was a few inches below where it was on the Labs.  Moreover, because the Voyageur differed from the Labrador in that it had a soft blackout curtain instead of the Labrador’s blackout door, the Voyageur’s map case was located on the lower SAS closet cover. The map case on Labrador was on the cabin side of its’ blackout door. The last thing to go on the SAS cover was the lower Dutch Door brace.!
On the Voyageur SAS closet covers in the photo above you can see the two gauges, the crash axe, door brace and to the right of the brace the map case.  A portion of the black out curtain can also be seen. Photo courtesy Scott Hemsley

Black out curtain/door

As mentioned in the foregoing paragraph both variants utilized, albeit different style, black out methods to allow Para Rescue personnel (eventually Rescue Specialists then SAR Techs) to prepare for an mission or to carry out medical care on patients in a lit cabin while not negatively affecting pilot night vision in the cockpit, a light barrier was required.  In the Labrador, the barrier was a door, while on the Voyageur a zippered blackout curtain was employed. Labrador blackout doors were eventually removed and replaced by the more practical blackout curtain.!

The map case can be seen on the lower part and back of the padded and closed door leading to the cockpit. Photo Randy Brown collection

Cabin Insulation

Yet, another feature that will likely be ignored by all but the most thorough of modelers, especially in larger scales, is the cabin insulation.  The most noticeable difference between the insulation on one variant compared with the other was colour.  Early insulation on the Voyageur was a very pale green compared with a light to medium gray on the Labrador.  The two different insulation materials do not lend themselves well to scale modelers so will be avoided, that said, as insulation wore out and was replaced the difference in insulation slowly disappeared until eventually all insulation was that of the Labrador.

The picture above clearly captures the difference in colour of the original Voyageur insulation and that of Labradors. The lighter green insulation used originally in Voyageurs can be seen on the cabin ceiling and wire/tubing tunnel covers. The walls are adorned with gray replacement insulation more commonly associated with Labradors. The aircraft above is from 103 Rescue Squadron (Gander, NL) and is participating in Search and Rescue Exercise (SAREX), thus the reason all eyes are in the windows. Photo DND

The insulation on either variant is straightforward. The criss-cross pattern often associated with aircraft insulation is incorrect for Labradors and Voyageurs. On these helicopters, the insulation was nothing more than a padded material that did not have cross-stitching. It was held on to the airframe in one of two manners and in some cases or locations both. The older method (although still used to a degree) was to use snaps. The second method was Velcro.  Here is where it could get tricky modeling insulation if you were really into the accuracy thing. Before, an airframe arrived back at the unit (after being in Arnprior for thorough maintenance) the insulation was installed (or reinstalled) before fixtures and fittings were put back into the cabin. Everything...including the radio boxes, which were set into a position essentially recessed behind the insulation, had covers. It did not take long for these covers and other similar covers to go missing leaving structural components including the outer skin, exposed. Also behind the insulation were the 28 volt outlets, heating duct controls and for a time the hoist controls. Access to these areas was frequent and the constant tugging and pulling of the insulation resulted in Velcro strips glued to the airframe coming off leaving the insulation hanging. It would only be a nuisance for so long before someone would "store” a part of the insulation, notably the blanket in front of the hoist station, for safekeeping.

To model the insulation, two methods I would consider are simply to paint the area using a “tromp loie” effect or tissue painted with a white glue/water mixture. In my opinion detailing the insulation is easier and less tedious that adding the wires, tubing and pipes of the Lab/Voyageur, although it would certainly be less dramatic.

The 424 Transport and Rescue (T & R) Squadron, Trenton Voyageur trains CASARA spotters. Wire/tubing tunnels unique to the Voyageur can be seen on both sides of the cabin at a point where the walls transition into the ceiling. Photo courtesy of Terry Cooper

Looking at the point were the cabin walls merge into the ceiling, it is clear there are no wire/tubing tunnel covers in the Labrador. Photo courtesy Jeff Wilson

A difference in insulation that did not disappear was the use of wire and tubing covers in the Voyageur. The pictures above clearly show the covers, which ran the length the fuselage, on both sides of Voyageurs only.!

Pilot Seats

A difference that is seldom mentioned is the difference in seats styles, including the difference between the pilot seats of the Labrador and Voyageur. On the left is the Labrador seat, on the right the Voyageur seat. This is a difference I believe remained for the life of the aircraft.

 



Flight Engineer Seat
While the Flight Engineer seat in the space between the cockpit and cabin differed in the two early 113 variants, there was no difference by the time SARCUP was completed.  For the time being, I lack photographic evidence to support my recollection that the seats once differed, however after conferring with an FE friend, I have some specifics.

One of the things I remember well was that the Voyageur FE station was considerably less comfortable than the Labrador version. This is due to a couple of things. As can be seen in the pictures below, the Voyageur station had the rather large cabinet on the left side that the Labradors did not. The cabinet reduced the width of the space by several inches. The purpose of the cabinet is two fold. What can be seen at the top of the cabinet is the circuit breaker panel. On the Labrador the breaker panel is behind the copilot’s seat, a portion of which can be seen in the picture on the right and below.

The second purpose of the cabinet is that it housed some of the extra hydraulics the Voyageur used. Of particular note is the hydraulic hoist used in Voyageurs was situated directly above the companionway door leading to the cockpit and where the FE sat. Originally, Labradors used an electric hoist so did not need the bulky cabinet. As part of the many modification, both variants used the externally mounted, hydraulically operated hoist with an internally mounted hydraulically operated hoist as a back up. This required Labradors to be modified to accept the hydraulics and thus the new hydraulics cabinet.


Back of FE seat
 
 
While the two pictures above show the Flight Engineer (FE) seat on a Voyageur, there is little difference on a Labrador. The picture on the left shows the FE seat stowed on the right side of the tunnel. The picture on the right shows the back of the FE seat hanging limply on the aft portion of the breaker box (to the left of the coiled intercom cord). Both photos courtesy of Scott Hemsley

The second reason the Labrador FE seat was more comfortable, is that the Lab seat was wider, had the same tube frame structure for not only the seat, but the seat back as well, which was sufficiently padded for comfort. As can be seen in the picture above right, the Voyageur seatback was basically a strap. While not a significant difference, the final difference in FE seats is that the Voyageur FE seat was stored on the right side of the companion way, the Labrador seat was folded up on the left side of the companion way.

Spotter Seats

There is on the other hand plenty of documentation to demonstrate the difference in spotter seats.  The seats located at the forward search blisters were an essential part of SAR Labradors, but unnecessary weight and bulk in the troop carrying Voyageur.  Voyageurs, as one might expect of an Army transport helicopter made use of troop seats when carrying personnel.  Troop seats were of the standard red nylon variety typical of all Canadian aircraft.

 
The picture on the left above and the drawing on the right above show the original seat fitted on the Labrador. The seat was less crashworthy than its' replacement, due in part to its' short back. Photo Randy Brown collection
 
While Labrador seats were originally painted black, they like all Voyageur seats were predominately gray. Seat covers on both style seats varied from green, to red or orange. Photo courtesy Scott Hemsley

When Voyageurs became part of the Air Force SAR inventory, proper spotter seats became a necessity, however where to get seats?  The answer, I believe, was in the Argus.  The Argus seats, if in fact they are Argus, seats were taller and more robust than those of the Labrador, so it made sense to eventually replace the Labrador seats as well.  When the Labrador seats were replaced and the source of the new seats is unclear, but I suspect the source of the seats was the Argus, which was being replaced by the Aurora.!

Box seats

Along the right cabin wall behind the right spotter seat were three box seats that doubled as equipment storage.  Technically, the boxes differ, but in size and colour only so from a modelers perspective hardly worth the effort to acknowledge the difference.  The main difference in the seats was the colour of the cushions and the boxes themselves. Along the wall, both variants used the back of the red nylon troop seats.

Labrador seat cushions arrived from the factory covered in red nylon.  Voyageur seats were locally manufactured, accounting in part for the different size, so the cushions were covered in whatever material was locally available.  In my experience, red, blue or tan leatherette were common.

The locally manufactured boxes used in the Voyageurs were made of sturdy gauge aluminum that was left unpainted for several years.  Labrador boxes were painted the same colour gray as other interior features.!


As can be seen in the above photo, the two back seats have two lids each, while the forward most box has a single lid. Photo courtesy of Derek Heyes


Hot Cups

Internally, for the most part modelers will consider several differences inconsequential.  For the sake of a few lines of text, I have included them for that modeler who might want to build a larger scale version or the modeler who might want to do a cutaway version for example.

At the time of purchase, neither the Lab nor Voyageur had hot cups to heat water for a hot drink on the all too frequent long flights or cold days.  Originally fitted in the C-47 Dakota, the Labrador was the first SAR helicopter to be fitted with hot cups.  Two cups were installed one above the other on the right side of the cabin wall immediately ahead of the search blister.  The bottom cup was only inches above the floor and just a couple of inches ahead of the station inline with front of the front search blister.

As the Voyageurs integrated into the SAR fleet, crews heated their hot water in a single hot cup attached to the aircraft electrical system by a long umbilical power cord.  The single hot cup was eventually replaced by two hot cups attached to the front of the radio rack that was eventually installed ahead of the left side SAR Tech chair on the left side of the cabin.  To the best of my knowledge, Labrador hot cups were eventually relocated to the left side of the cabin as well.!

The hot cups were affixed to the front of the radio rack on the left side of the aircraft slight aft of the left side emergency door. Photo DND


Section 3

Operational Differences


Operational differences will look at equipment or features of the Labrador and Voyageur from an operational perspective.  Because both of these aircraft served in the search and rescue role for most of their existence the majority of the discussion will focus on SAR.!

Antenna

It is in all probability doubtful that the antennae on one aircraft matched exactly that of another such was the pace of change with radios and navigational equipment.  For this reason alone I will not get too much into the various antennae, save for two notable examples; High frequency (HF) and Search and Rescue homing (beacon).  It is incumbent on the modeler to check photos carefully if accuracy is your aim with respect to antennae. I will where possible be identifying the various antenna, if the antenna is identifiable.

HF Antenna Masts
 



HF Antenna
 


At the time of the helicopter purchase radios and navigational aides were barely out of infancy compared to what aircraft of the ‘70s, ‘80s and beyond would have.  Perhaps one of the most important pieces of equipment was, and maybe still is, is the High Frequency (HF) radio.  HF gives aircraft crews the ability, under the right conditions, to transmit/receive to and from another station anywhere in the world.  HF radios have been a part of the Labrador’s communications arsenal since the earliest days and continued to be so until retirement. Pictures of HF radio antennae as they changed over the years illustrate changes in HF antenna design and location that are representative of antennae evolution for all radios and navigation aids. One picture in Mr. Pat Martin’s book shows 305 with a blade HF antenna painted green whereas the more common colour was blue. Yet, another picture shows a yellow aircraft carrying the blade antenna on the left side, which became the standard. In Pat Martin’s newest book, “Royal Canadian Air Force – Aircraft Finish and Markings 1947-1968 – Volume 2”, there is a picture of a RWB Labrador with the blade antenna just aft of the front door on the right side of the aircraft…I am of the opinion that this was part of HF trials. To further illustrate my point regarding antenna location, a couple of pictures show Labrador 301 with the final version of the HF antenna in the same location as the HF antenna on Voyageurs. A picture from a later date shows the HF antenna on 301 in the standard location for Labradors. It is unclear why there is a difference in the HF locations on the later date Labs and Voyageurs, but it is a certainty the difference was maintained until retirement.

The object of our attention is actually Labrador 405 in the background. Of note is the green HF blade antenna on a Labrador still wearing its' 400 series number. Photo DND

The HF blade shaped antenna was fitted to the fuselage just aft of the left side emergency door and far enough ahead of the front search blister so as not to be too restrictive to the spotter on the left side during searches. Photo courtesy of Dave Marshall

Pre-SARCUP Labrador 305 sports a yellow paint scheme, a yellow HF blade antenna and black "RESCUE" titles. Photo via Pat Mercer

I seriously doubt that even the most ardent of modeler is going to model the instrument panel and console to follow the changes in the various radios and nav aids, indeed it might be impossible in scales smaller than 1:48, however the change in antennae is doable. One of the earliest antennas that present the modeler with a manageable challenge is SARAH. Radios early in their developmental stages were comparatively unsophisticated and of limited function; so much, so that it was uncommon for downed aircraft to be able to communicate with searchers. Additionally, searchers lacked any real technological means to locate the downed aircraft. “SARAH”, (search and rescue homing beacon) changed that.

The photo above shows the positioning of the HF antenna overtop of the lightning stripe on the Voyageur. Photo courtesy Derek Heyes

Unlike the Voyageur, the Labrador's HF antenna is positioned above the lightning stripe. Photo courtesy Jeff Wilson
Unfortunately, I have virtually no information on early Voyageur antennae. This is particularly so for the early years through to the time when Voyageurs were painted yellow and modifications were being undertaken to make them SAR capable.!

The above photo gives you a close look at the right side SARAH antenna. A second identical antenna is located in the same position on the left side. Photo Randy Brown collection

In addition to the left side SARAH antenna, the above photo shows the forward HF antenna mast and the HF antenna entering the fuselage through the lightning stripe. Photo via Pat Mercer



Floors

Voyageurs were purchased by the Army to move equipment and personnel from rear echelon positions to positions closer to the action.  The distance between the two positions was relatively short so as has been noted Voyageurs were not fitted with long- range fuel tanks.  If greater range was needed internal, fuel bladders could be added a modification that took, as I understand it, about three years to implement.  Operationally, the role of the Voyageur was essentially that of a transport.

To accommodate expedient loading and unloading the floor of the Voyageur was more robust than that of Labradors.  The center panels of Voyageurs were built to handle heavier loads of vehicles and military pallets.  On either side of the center panels was a row of rollers and outside of the rollers were vehicle tread ways designed to handle rubber-tired (as opposed to tracked) wheel loads.

Rollers were in place the full length of the fuselage and ramp.  The cargo ramp also had two smaller folding ramps that could be positioned at any point along the width of the ramp to accommodate a variety of different sized loads.

Although the rollers have been removed, the roller channels are clearly visible.  At the end of and to the outer edges of the ramp are the two ramp extensions. Photo courtesy Scott Hemsley

The floor of Labradors was unlike all other CH-46/KV-107 models in that the construction of the floor was lighter and lacked the rollers.  At some point in their SAR careers rollers were deemed expendable and removed from Voyageurs, although the roller tracks and small ramps additions remained.!

The Labrador did not have rollers as can be seen on the ramp above. In the above photo it also easier to see the two ramp extensions. Photo courtesy Jeff Wilson

The above photo gives us a clear look at the rollers. Photo DND

Hoists

In keeping with the Army’s, transport role for the Voyageurs the CH-113A was equipped with a robust hoist that was geared primarily to “pull” heavy equipment and vehicles into the cabin.  In addition to the slow rate of operation, the hydraulically operated hoist used a shorter thicker cable than that of the SAR Labradors.

Even after external hoists had been installed, external hydraulic hoists were retained as a back up on both variants.  Photo courtesy Scott Hemsley

While the Voyageur was a credible secondary SAR resource, it still lacked an efficient rescue hoist. As Voyageurs were absorbed by the Air Force into the primary SAR role their limitations where recognized as a serious impediment since the Voyageur hoist was used through the floor at center of the fuselage.

Master Corporal Dave Aalto of 413 Squadron demonstrates use of the "Sky Genie" friction descent device and the Voyageur's center hatch hoist. Photo Randy Brown collection


Designed for search and rescue, the Labrador counted on versatility to ensure reliability.  While the Labrador had only one hoist, that hoist could be used in different configurations.  With a longer hoist cable, the electrically driven hoist was geared to operate faster than its’ Army counterpart.  The 113-hoist cable was routed through a series of three pulleys from the forward bulkhead aft to the ceiling, to the left side of the cabin opposite the open door and through a bell housing on the internally mounted (Swedish) boom hoist.  The Swedish boom, was then extended forward through the open doors to facilitate a rescue procedure.


ELT
 


Swedish boom bell housing.
 

In addition to the location of the Labrador's hoist and the cover on the bottom of the hoist, note the position of the bell housing on the Swedish boom when the boom is in the vertical position. The hoist above is rigged for para-drops. The fact the parachute anchor line cable runs along the cabin wall indicates the photo is late 1980s at the earliest and more likely 1981. Photo Randy Brown collection

Occasionally, as might be expected, the infrequent problem with the Swedish boom necessitated use of the hoist through the center hatch.  Like the Voyageur, the cable was routed from the forward bulkhead along the center of the ceiling to a hard point and pulley system directly above the hatch.


With the Speedline modification program, all 113s were equipped with a much faster hoist with a longer cable.  The new hoist was capable of carrying 600 pounds up or down compared with the 600 pounds up and 300 pounds down for the older Labrador hoist.  By the time, all aircraft were equipped external hoists both Labradors and Voyageurs utilized hydraulic hoists as a back up to the Speedline upgrade.

One last aside, the earlier electric hoist used by the Labrador was more compact and was affixed to the cabin bulkhead above the companionway leading to the cockpit. While it was not centered exactly, it was more centered than the hydraulic hoist of the Voyageur. The reason lies in the size of the hydraulic hoist and the extensive array of hydraulic lines. A lack of space to accommodate the hydraulic lines, the only option was to move the larger Voyageur hoist slightly to the left.!

The 1971 photo above shows both the position of the lower Dutch door and the Swedish boom in the hoisting position. Note the position of the bell housing during hoisting. Photo Randy Brown collection
The photo above gives you a good look at the multitude of lines running to and from the external hoist. Photo courtesy Derek Heyes

Scott Hemsley gives us a good look at the hoist from below. Photo courtesy Scott Hemsley



Water Dam

Amphibious helicopters, both the Voyageur and Labrador exercised regularly and often in the water.  At times both variants conducted water borne procedures that necessitated opening the ramp and upper hatch.  To keep water from out of the cabin and from sinking the aircraft, a water dam was used.


Once a routine procedure for SAR Labradors and Voyageurs, the boat launch and recovery procedure was eventually phased out. Here Rescue Specialists exit the helicopter as they prepare to lower the outboard motor. Photo Randy Brown Collection

The dam of each variant differed only marginally, and perhaps not enough for the modeler to notice.  Firstly, the dams were constructed of different materials and finished differently.  The Labrador ramp was made of lightweight metals and finished in the same gray as the interior of the cabin.  The Labrador dam, when in place at the end of the bench seats and ahead of the ramp was no taller than the box seats.

In the Voyageur, the ramp was made of wood and finished with a clear varnish or lacquer, so looked like a finished sheet of plywood.  Voyageur dams were slightly taller than that of the Labrador with the top of the dam above the top of the box seats.

Another noticeable difference between the dams of these two aircraft was their storage location when not in use.  It was common for the dam to be in place, especially when the aircraft was on SAR standby, however this was not a hard and fast rule.
At one time, the two variants stored their water dams in different locations, but that eventually changed and both stored the dam on the left side of the ramp inner fuselage. Photo courtesy Jeff Wilson

On either bird, the dam was occasionally stored behind the stretchers at the rear of the cabin, however the more usual storage location was on the ramp area sidewalls, the Lab dam stored on the right side the Voyageur’s stored on the left side.  Since the Voyageur had a hydraulic hand pump at the forward end of the ramp on the right sidewall, placement of the dam in this location was impractical, so the same location on the left side was selected.

In later years, the water dam was stored in the same location on both variants. Photo courtesy Jeff Wilson


Although the Labrador above has the hydraulic hand pump in the same location as a Voyageur, the style of the handle is somewhat different. Before being modified with a hydraulic ramp, Labradors stored the water dam in this location. Photo courtesy of Jeff Wilson

Despite practicing, several different waterborne procedures frequently right up until the late 1980s there are only a handful of rescues where the aircraft was actually put into the water to conduct the rescue. As an exclamation mark to the aging aircraft’s declining ability to conduct water ops, 424 Squadron Trenton almost lost a helicopter during a rescue because the crew forgot to put drain plugs in place…at one time an instinctive procedure for all crew members.!

The different style hydraulic hand pump handle can be seen clearly in the above photo. Photo via Pat Mercer
Labrador 304 performing a rare operational water borne rescue off Vancouver Island. Photo DND

March 18 – 1978; Labrador 304 from 442 T&R Squadron, CFB Comox crewed by Major Mike Angelsey (AC), Captain Mike Clark (FO), Flight Engineers Dennis (BJ) B., Bob Ardelien(sp) and Rescue Specialists Don Lane and Danno Schut prepares to recover five survivors from the life raft of the fishing vessel (FV) Mothers Three. The crew of 304 was deployed to Tofino to watch the herring fleet when RCC diverted them to the Mothers Three. A Comox based Argus was assigned as top cover for the Labrador when it took the above picture.

Attempts to hoist the survivors from the raft were aborted. It was later learned the rafts’ sea anchor was not deployed causing the rotor wash to blow the raft aimlessly about the calm sea. Following a short discussion, it was decided that Rescue Specialist Team Leader Don Lane would swim to raft with rope in hand. Once on board the raft, the now six persons would pull themselves towards the helicopter’s right side door. After being adrift on the Pacific for five days, the crew of Mothers Three was returned to dry land via Port Hardy and a short hospital stay.

An interesting aside to the story is that the rope used to pull the raft to the helicopter was tied around the right spotter seat post and may have contributed to the seat breaking…and by extension perhaps a contributing factor in the reason Labrador seats were replaced with Argus seats?  Danno Schut provided details of the rescue. !


SAR Mewasige, a 424 Squadron Trenton Voyageur picks up survivors from a grounded boat off Mississagi Island, Ontario. Photo Courtesy Ted Brown (424 Squadron Buffalo Flight Engineer)
Chapter 2 – Evolution to Common Features

In Chapter two, the discussion will move from differences to traits and features that were common to the Voyageur and Labrador.  While some of these features were present from the outset, other commonalities were arrived at through evolution, either from one variant’s feature being employed on the other or an entirely new feature new to both variants.  Rolled into one discussion are the common structural, functional, operational and visual features.!

Section 1
 
Visible Features

This section will deal with the areas of detail that contributed to the “look” of both 113s and 113As starting with some short lived differences before moving on to what eventually became the “common look” of the two variants in the SAR role.  Some of the things I will cover herein may not be covered in Pat Martin’s books (although I could be wrong) or anywhere else because they are obscure and/or mundane, such as the colour of door handles and/or, the colour of wheel rims. Also covered are aspects of markings that do not constitute a full-blown paint job.

Both the Labrador and Voyageur were given paint schemes commensurate with their respective roles.  The Voyageur was green overall while the Labrador was assigned the red, white and blue scheme of aircraft working on northern radar sites of the MID Canada Line where high visibility was essential.  Clearly both types would benefit from a change to yellow while working as primary SAR resources. A personal note: while I liked the look of the yellow livery, which would become synonymous with SAR, I with my many, many hours of search time cannot possibly believe that yellow was the most effective colour to paint a SAR aircraft especially in the fall months.!

Anti-skid patches

On both the Voyageur and Labrador, upper surface markings were authorized to be painted either gray or black. These areas included a nearly fuselage length walkway to the left of the sync shaft tunnel, a small step area behind and slightly aft of the forward pylon and walkways on the aft portion of the stub wings. For further information regarding the shape and colour specifications, refer to Pat Martin’s books.  Some photos show later schemes with a small patch to the right of the sync shaft tunnel and slightly aft of the forward pylon.!

Walkway areas may be gray or black. Note the gray areas on the tanks in the above photo are one piece and appear rectangular. Photo courtesy Derek Heyes

When comparing the walkway areas on the two photos above, not that the walkway areas on the bottom photo are narrower at the bottom of the walkway than those in the top photo. The walkways in the bottom photo appear black not gray, but this may be a result of us?  Photo courtesy Derek Heyes

Walkways on the above pre-SARCUP Voyageur are painted on the stub wings in two pieces and are gray. Photo DND

The extra walkway area on the right side of the forward pylon originated on Voyageurs, however it is likely that both variants shared the same painted on walkways by the time SARCUP was implemented. Photo courtesy Scott Hemsley
Photo courtesy Scott Hemsley

Aft pylon

While differences in the colour of red/orange used on the aft pylon are documented, some painting omissions are not. One area of note is the absence of red on the forward part of the aft pylon on Labradors as they were accepted into inventory.  Additionally, there is a black strip painted on the front of the aft pylon’s clamshell doors as can be seen in the photo at the top of the next page.

 
Note the differences in how the forward part of the aft fuselage is painted. The photo on the left is a Labrador as it was delivered to the RCAF. The painting omission appeared on early Labradors painted with 400 series numbers. Both photos courtesy of DND

The black strip on the forward part of the aft fuselage starts at the bottom of the clamshell doors on 400 series Labradors and likely appeared for only a short period. Photo DND

Labradors were delivered to the Air Force with a narrow strip of the aft pylon painted black to hide exhaust. Photo DND

 
It did not take long before the black area on the aft fuselage was enlarged as the photo above and left shows. The change occurred while the aircraft were still using white 400 series numbers. Photo DND
While the two photos above show that while the black exhaust area remained generally the same size, the shape would evolve as can be seen in the photos above and below. All four photos DND

 

With respect to the exhaust path on the aft pylon, refer to Pat Martin’s books where Pat addresses the size of the area to be painted black. Pictures illustrate this feature.!


Fuselage underside
As per RCAF directives, a red rectangle was painted on the underside of the fuselage.  The rectangle measured 6’ by 2’.  Other markings on the underside that are not addressed in Pat Martin’s books are the two circles, one black the other silver. It is my assumption, that the silver circle is an access panel, but for what equipment is anyone’s guess. It may very well have something to do with access to the attachment of the nose gear?  As for the black circle on the underside of the forward fuselage, I am at a complete loss.!

The red area on the bottom of Labrador fuselages was unique to red, white and blue Labradors. Photo DND


The black circle on Labrador fuselages is visible in the photo above. Photo courtesy Derek Heyes
The silver circle in front of the main gear is clearly visible in the photo above. Photo DND


Wheels

While there were specific colours authorized for the wheel rims on both 113 variants, the reality was more of a smorgasbord of coloured rims.  While each variant was being maintained, within their own element, it is likely; there was little deviation from prescribed directives; silver (aluminum?) or green for the Army and white, or aluminum I believe for the Air Force variant.  Real changes started when Voyageurs were accepted into Air Force inventory.  Red, white and blue Labradors were commonly seen with white wheel rims, however it was just as common to see them with silver or green rims as well after the Voyageurs arrived at SAR bases.

Labrador 401 in the early red, white and blue livery that included blue wheel rims. Photo DND
Labrador 402 sporting the 400 series numbers, but the later version red, white and blue livery and aluminum wheel rims. Photo DND


Aircraft 403 with black 400 series numbers shown above with aluminum nose wheel rims and blue main wheel rims. Photo DND

While they do exist, I do not have a picture suitable for inclusion here that shows a red, white and blue Labrador with green wheel rims.
Labrador involved with CPI trials has white rims all around. Photo via Mike Belcher

Voyageurs while in Army inventory could be found with either green or silver rims. Like the Labrador, there was no consistency in use of the various coloured rims.  One or more of the four main rims might be green and the remainder silver.   Once the Voyageurs transitioned to SAR, they were the first to be repainted yellow. As they came out of the paint shop all of their wheel rims were presumably yellow, however in short order you could find yellow Voyageurs and then eventually yellow Labradors that had wheel rims that were, silver, green (for a short time), white and/or yellow.

Voyageur 410 in early Army colours, which included green wheel rims. Photo DND
Voyageur 315 in interim SAR livery as shown above has aluminum wheel rims. Photo via Pat Mercer


Voyageur 308 show here in early yellow SAR colours and aluminum wheel rims. Photo DND


The photo above taken in Gander while 308 served with 103 Rescue Unit shows her in new SAR yellow livery with the early RESCUE titles and yellow wheel rims all round. Photo DND


Voyageur 308 in new SAR yellow scheme with updated RESCUE titles shown here with yellow main wheel rims and white nose wheel rims. Photo DND


Yet another view of Voyageur 308, however this photo shows 308 with white wheel rims all round. Photo DND

The inconsistent use of coloured rims gives the modeler a great deal of latitude to create a subtle uniqueness to their version of the Labrador or Voyageur.  As aircraft were being rotated through, the paint shop in their maintenance cycles yellow aircraft could still be found to have white rims. It seems that there was consistency only at the time of purchase and after all aircraft had been painted yellow and fitted with radar.!

Mirrors - Update

It was my intent today to simply discuss the colour of mirrors on Labradors, however as I was searching teh Internet yet again for pictures of Labradors and/or Voyageurs I came across a most interesting picture that as it happens fits nicely into today's blog about mirrors. The picture below is the picture I make reference to. As you can see, the Boeing Vertol aircraft before it was delivered to the RCAF is fitted with mirrors, although they are not the mirrors we have become used to seeing on RCAF Labradors.



As was previously mentioned (in an earlier post), only Labradors had mirrors.  While still using the 400 series aircraft numbers, the mirrors were painted overall blue.  In time and as the aircraft switched to the 300 series, red, white and blue Labradors had their mirrors painted predominantly red with white candy striped supports.  Once all the helicopters were painted SAR yellow, the only change with respect to the mirrors was that the white striping changed to yellow.  To the best of my recollections, on at least one aircraft for at least a short time, the red mirrors lacked any striping.  Whether this was a one off or not is pure conjecture, but I believe this was the case. Eventually mirrors were removed on all 113s before they were retired.!

The mirrors seen in the picture at the beginning of the post are not fitted on 401 in the above picture, which is now in RCAF inventory. So we know that the Labradors were delivered without mirrors.


Mirrors are painted blue without any "barber poling".

Mirrors are now located in a different position than when the aircraft was a Boeing Vertol asset. Lots of detail here to help date the aircraft should that be important to you.



"No Push" is barely visible in white lettering on the back of the two piece mirror. The mirror is not one piece...there are two small rectangle mirror lens that make up the mirror.  The "No" and the "Push" are each on the back of their own mirror.


Fresh out of Boeing Arnprior , same mirrors, different colours...predominantly red with yellow barber pole striping.

Red mirrors with yellow barber poling on preSARCUP 303.
Most SARCUP Labradors did not have mirrors.
This is the one picture I have seen mirrors painted in a solid red...no yellow striping. 306 Is a SARCUP modified airframe.
306 Now without mirrors.

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