This catalogue provides a sample of some of the modifications and/or products for which Field Aviation Company inc. has obtained Transport Canada and FAA certification. Field Aviation has also developed and obtained TC/FAA/JAA certification for other specific modifications but they are not included in this catalogue. If you find that any of the products listed do not fit your specific requirements or are needed for a different aircraft type, please contact us to see what we can do to meet your needs. Field
Aviation would also be interested in developing and certifying other modifications or products to fit your requirements. Our in house Transport Canada Design Approval Organization (DAO) helps reduce many of the delays found in certification programs.
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STCs - AIRFRAME
Benefits
Removal of Auxiliary Power Unit (APU)
Applicability
DHC-8 100, 200, & 300 Series
Description
Provides the operator with a procedure for removing the de Havilland Special Order Option (SOO
8155) Auxiliary Power Unit (APU).
Removal of the APU involves the following:
• Removal of the APU, Starter Generator and miscellaneous accessories
• Removal of the APU Structural Mounting Provisions
• Removing the associated ducting AFT of the pressure bulkhead
• Removing drain lines and welded drain mast and installing blanking doublers
• Capping and stowing the associated electrical harness
• Capping, stowing and draining APU fuel supply lines
• Removing the control heads for the APU system. Blanking provisions will be installed at locations where the control head is removed
Manpower:
• 170 man hours are required to accomplish full removal and installation of blanking plates.
Weight and Balance:
• Weight: -250.4 lbs
Certification:
• Transport Canada STC No. SA98-30
FAA STC No. ST00801NY
Contact Field Aviation for a price quote
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STCs - AIRFRAME
Benefits
Continued Aircraft Operation while Auxiliary
Power Unit (APU) is removed.
Applicability
DHC-8 Q400 Series
Description
The aircraft Maintenance Manual provides instructions for the removal of the APU while the aircraft is undergoing maintenance, however this does not allow the aircraft to operate with the APU removed. This modification allows for continued operation of the aircraft with the APU removed. In addition, the aircraft Minimum Equipment List Procedures Manual does not list the APU and APU
Bleed Air System as required equipment for dispatch and provides maintenance procedures for dispatch with the APU and APU Bleed Air System inoperative. These maintenance procedures are incorporated into this modification.
The modification involves removal of the APU Starter / Generator and the APU Engine. The remaining APU system components such as the FADEC and the APU fuel pump are disabled.
Remaining APU provisions such as fuel and bleed air lines and electrical cables are capped, stowed and secured to existing aircraft structure.
Manpower:
• 16 man hours are required to accomplish full removal and installation of blanking plates.
Certification:
• Transport Canada
STC No. C-LSA03-009/D
Contact Field Aviation for a price quote
21

STCs - AIRFRAME
Benefits
This modification provides an auxiliary heating system to provide additional heat to the cockpit in cold weather operations. The installation is independent of the existing aircraft air-conditioning system, simplifying the installation, maintenance, and operation.
• Improved Pilot Comfort
• Additional Heat as Required
• Easy to maintain.
Applicability
Dash 8 300 Series. Others available upon request.
Description
The heating system consists of an inline type heater mounted under the cockpit floor, which heats air cycled from the cockpit. The heater includes an integral 80 CFM inline fan, which draws air directly from the cockpit just aft of the center console. To distribute the heated air, two sets of flexible ducts are installed to direct the air at both pilots’ feet and chest area.
A single On/Off heater control and On light are provided on the center console to allow easy access for both pilots.
The power supply for the heater comes from the aircraft’s RH 115 V AC variable frequency bus.
The heater is protected by a 5-amp circuit breaker located on the AC VAR frequency circuit breaker panel located behind the copilot’s position. A 1-amp circuit breaker for the control relay for the heater is located on the RH secondary DC bus.
Manpower:
• Estimated installation time is 40 hours
Certification:
• Transport Canada STC No. SA00-149
• JAA STC No. ACG.21NE.010
Contact Field Aviation for a price quote
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STCs - AIRFRAME
Benefits
Customer cost reduction by allowing customer to rebuild versus procurement of new.
Applicability
Bell 206A/B Helicopters
Description
Field Aviation Company inc. holds Transport Canada approval for the rebuild of part numbers 206-
031-200-001/005/065/007/009/129 Main Cabin Beam (Box Beam).
Certification:
• FAA STC No. SR00071NY
• Transport Canada STC No. SH93-47
Contact Field Aviation for a price quote
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STCs - AIRFRAME
Benefits
The Cabin Class Dividers provide separation between business and economy class. The dividers are easily movable by cabin crew to allow for changes in class sizes between flights. The attractive modern design matches the aircraft interior and the clear portion of the divider can be etched with the airline logo.
Applicability
CRJ 100, 200 with C & D interior.
Description
The Cabin Class Divider provides separation for two-class service. The divider is moveable to adjust to class size.
The class divider attaches to two rails that are installed under the left hand and right hand overhead storage bins. A latch mechanism is provided at the inboard attach point to secure the divider in place. The divider assembly consists of a clear polycarbonate panel that allows the flight attendants a clear view of all seat rows. Etching of a horizontal line pattern and aircraft logo is optional
(pattern must be approved to ensure visibility is not effected).
The rails (1.0 x 0.5 extrusion) run from fuselage station 409 + 11 to the aft cabin bulkhead allowing for the divider to be installed at each eat back, except immediately forward of the over wing emergency exits. The divider can be installed immediately forward of the aft bulkhead when no cabin class separation is required
Rail lengths can be changed to match special customer requirements but costs may be affected.
Manpower:
• Approximately 50 man hours to install the rails.
Kit Contents:
• LH & RH class divider
• Mounting rails
• All installation hardware
• Modification instruction and installation drawing.
Weight & Balance:
• The installation weighs 73 lbs
Certification:
• Transport Canada STC No. SA01-52
• JAA STC No. ACG.21NE.049
Contact Field Aviation for a price quote
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STCs - AIRFRAME
Benefits
The Cabin Class Dividers provide separation between business and economy class. The dividers are easily movable by cabin crew to allow for changes in class sizes between flights. The attractive modern design matches the aircraft interior and the clear portion of the divider can be etched with the airline logo.
Applicability
DHC-8-300 with Hunting or C&D interiors, 50 passenger configuration
Description
The Cabin Class Divider provides separation for two-class service. The divider is moveable to adjust the class size.
The class divider attaches to two rails that are installed under the left hand and right hand overhead storage bins. A latch mechanism is provided at the inboard attach point to secure the divider in place. The divider assembly consists of a clear polycarbonate panel that allows the flight attendants a clear view of all seat rows. Etching of a horizontal line pattern and aircraft logo is optional
(pattern must be approved to ensure visibility is not affected).
The rails (1.0 x 0.5 extrusion) run from fuselage station X220 to the aft cabin bulkhead allowing for the divider to be installed at each seat back, except immediately forward of the under wing emergency exits. For storage, the dividers can be installed immediately forward of the aft bulkhead behind the aft seat row.
Rail lengths and divider positions can be changed to match special customer requirements but costs may be affected.
Kit Contents:
• LH & RH class divider
• Mounting rails
• All installation hardware
• Modification instruction and installation drawing.
Weight & Balance:
• The installation weighs 78 lbs
Certification:
• Transport Canada STC No. SA01-50
• JAA STC No. ACG.21NE.050
Contact Field Aviation for a price quote
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STCs - AIRFRAME
Benefits
The Cabin Class Dividers provide separation between business and economy class. The dividers are easily movable by cabin crew to allow for changes in class sizes between flights. The attractive modern design matches the aircraft interior and the clear portion of the dividers can be etched with the airline logo.
Applicability
DHC-8-400 equipped with baggage bin handrails.
Description
The Cabin Class Divider provides separation for two-class service. The divider is moveable to adjust to cabin class size.
The class divider attaches to the existing extrusion along the PSU lights and the handrail along the inboard edge of the overhead storage bins. A latch mechanism is provided at the inboard attach point to secure the divider in place. The divider assembly consists of a clear polycarbonate panel that does not block the passenger’s view of no-smoking and seatbelt signs and allows the flight attendants a clear view of all seat rows.
The divider can be installed at each seat back, except immediately forward of the under wing emergency exits. The divider can be installed immediately forward of the aft bulkhead for stowage when no cabin class separation is required
Manpower:
• The divider is easily installed by the cabin crew in seconds.
Kit Contents:
• LH & RH class divider
• Modification instruction and installation drawing.
Weight & Balance:
• The installation weighs 9 lbs
Certification:
• Transport Canada STC No. SA01-55
• JAA STC No. ACG.21NE2.085
Contact Field Aviation for a price quote
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STCs - AIRFRAME
CRJ Aircraft
Applicability
Description
This is a repair for the CRJ crew escape hatch handle. The flush mount design of the handle that fits into the escape hatch is subject to corrosion. The steel shaft of the handle assembly is replaced with a stainless steel shaft and is repined to the existing handle grip.
Field Aviation can offer a Transport Canada approved repair to your Bombardier CRJ Crew Escape
Hatch. The repair replaces the standard steel shaft with a stainless steel shaft handle. The repair reuses the existing handle grip.
Certification:
• Transport Canada RDC No. C-RAP03-
038/D
Contact Field Aviation for a price quote
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STCs - AIRFRAME
Benefits
Installation of an Auxiliary Power Unit provides:
• On-ground Electrical Power Supply
• On-ground Air Conditioning
Applicability
DHC-8-100, 200, 300 series aircraft
Description
This retrofit installation provides ground operable APU.
Manpower:
• Installation time is approximately 1,400 hours
STC Kit Contents:
• Installation kit available with or without
APU and Generator (Overhauled or New condition)
• Support structure and installation
Hardware
• Documentation included in the kit:
• Maintenance Manual Supplement
• IPC supplement
Electrical Load Data
• No change to Aircraft Electrical Load
Analysis, as the APU installation is restricted to ground operation only.
Weight & Balance:
APU installation affects weight and balance as follows:
• 336lbs at Arm 661.1 inches AFT of datum
Certification:
• Transport Canada STC No. SA97-39
• FAA STC No. ST01858NY
• JAA STC No. MOT.21NE2.135
• EASA STC No. 2004-4153
Contact Field Aviation for a price quote
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Applicability
Importing/Exporting a Bombardier CRJ
STCs - AIRFRAME
Description
This modification converts the existing fuel control panel from either metric to imperial or from imperial to metric units to meet aircraft import/export requirements.
Field Aviation can offer a Transport Canada approved Supplemental Type Certificate for the conversion of fuel indication either from Metric to Imperial or from Imperial to Metric.
Certification:
• Transport Canada STC No. SA03-39
• FAA STC No. ST01692NY
Contact Field Aviation for a price quote
29

STCs - AIRFRAME
Benefits
Installation of Passenger Window Blinds enhances Passenger comfort and assists in cabin cooling.
Applicability
DHC-8-100, 200, 300 series aircraft
Description
The Passenger Sliding Window Blind Installation provides the passengers with a means of blocking out the windows. Each blind is adjustable allowing passengers to select their own personal comfort level. This modification is a minor change to the interior of the aircraft and does not involve any structural modification.
Manpower:
• Installation time would run 4 hours per window allowing installation to be completed in stages over night.
Certification:
• Transport Canada STC No. SA98-48
• FAA STC No. ST00868NY
Weight & Balance:
Based on adding window blinds to all cabin
STC Kit Contents:
Kits are provided on a per-window basis. Each kit includes:
• Blind
• Track
• Hardware
• Installation Instructions
• IPC supplement
DHC-8-100/200
Weight (lb)
28.8
DHC-8-300 48.6
Electrical Load Data
• No change to Aircraft Electrical Load
Analysis, as the APU installation is restricted to ground operation only.
Contact Field Aviation for a price quote
30

STCs - AIRFRAME
Benefits
Provisions for securing two 2/3 KSSU size meal Trolley carts.
Applicability
DHC-8-100, 200, 300 series aircraft
Description
The Forward Baggage Compartment has been modified to store two 2/3 KSSU size meal trolley carts. One trolley cart is secured to the forward compartment bulkhead and one to the aft compartment bulkhead. To accommodate the catering trolley carts, it is necessary to raise the baggage compartment shelf to provide the proper clearance.
The method of stowing both trolley carts in the forward baggage compartment is to strap one trolley cart to the forward compartment bulkhead and one to the aft compartment bulkhead. Both trolley carts will be restrained using a standard cargo strap. Rub strips along both compartments are also incorporated to protect the bulkhead and the trolley from damage.
Manpower:
• 10 man hours are required to accomplish full modification.
Certification:
• Transport Canada STC No. C-LSA02-
185/D
• CAA- Norway – BSL-B 3-2 item 6.4 and
BSL/JAR OPS 1.890(a)(6)
Contact Field Aviation for a price quote
31

STCs - AIRFRAME
Benefits
The VIP Interior module provides an upgraded seating arrangement which is:
• Easily convertible
• Adaptable to various passenger and cargo configurations
• Cost effective
Applicability
• Dash 8 Series 200 available
• Dash 8 Series 100, 300 & 400 are available upon request
• Aircraft equipped with the deHavilland or C&D (Hunting) Interiors.
Description
The convertible VIP interior allows various VIP and passenger configurations on all Dash 8 aircraft equipped with either the deHavilland or C&D/Hunting interiors. VIP and cargo configurations are available for the Series100/200 fitted with the optional provisions for moveable bulkhead.
The VIP seating consists of forward & aft facing single and double executive seats with two and four place tables. The seating and tables can be finished to customer specifications.
Quick convertibility of the VIP installation is achieved through the use of adaptor mounting pallets.
The pallet sections are secured to the seat tracks. Seats and tables are mounted to the adaptor pallets. Ramps are located at the forward and aft end of the VIP section for a smooth transition to the existing floor for passenger/crew and trolley cart movement.
As an option, life raft stowage installations are also available to suit head count requirements
Documentation Included with the Kit:
• Installation Manual
• Operation Manual
• Maintenance Manual Supplement
• Illustrated Parts Catalogue
Electrical Load Data:
• This modification has no effect on the aircraft electrical system.
Certification:
• Transport Canada LSTC No. C-LSA01-143
Weight & Balance Data:
• Typical Series 200 VIP interior passenger installation (2 doubles/2 singles) increases the aircraft weight by approximately 500 lb. The overall aircraft take off weight will decrease due to the reduction of passengers onboard from 37 to 27.
Contact Field Aviation for a price quote
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STCs - AIRFRAME
Contact Field Aviation for a price quote
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