MODIFICATIONS OF Field Aviation (88)

EFI-890R FLIGHT DECK MODERNIZATION

The FIELD AVIATION EFI-890R Flight Deck Modernization is a state of the art replacement of the existing legacy mechanical (EFIS/analogue) cockpit instruments with five Universal Avionics EFI-890R high definition LCD flat panel displays. Please click on "Front sheet" link for a copy of our brochure.
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G3 GALLEY CONVECTION OVENS

The FIELD AVIATION G3 Galley Convection Ovens provides airlines with the opportunity to offer hot meal service to passengers. Please click on "Front sheet" link above for a copy of our brochure
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AIR OPERABLE DOOR

The FIELD AVIATION designed Air Operable Door (AOD) allows special mission operators to open the aft cargo door in flight. Please click on "Front Sheet" link above for a copy of our brochure.
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VIP INTERIOR

The FIELD AVIATION VIP Interior for the DHC-8-100/200/300 aircraft provides executive seating and conference tables in the forward passenger cabin. Economy seating is retained in the aft cabin for a mixed class configuration. Please click on "Front sheet" link above for a copy of our brochure.
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COCKPIT DOOR HOLD OPEN LATCH

The FIELD AVIATION designed Cockpit Door Hold Open Latch provides a method for holding the cockpit door open during maintenance or ground operations (regulations permitting). Please click on "Front Sheet" link above for a copy of our brochure.
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2ND HONEYWELL PRIMUS® HF-1050

The FIELD AVIATION 2nd Honeywell Primus HF-1050 STC provides a second HF-1050 system to compliment the OEM installed single HF-1050 System. Please click on "Front Sheet" link above for a copy of our brochure.  
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WAAS/SBAS FLIGHT MANAGEMENT SYSTEM WITH LPV UPGRADE

The FIELD AVIATION Wide Area Augmentation System (WAAS) / Satellite Based Augmentation System (SBAS) FMS upgrade is founded on the experience gained during our Local Area Augmentation System (LAAS) precision landing upgrade program which has logged thousands of successful flying hours to date. Please click on "Front sheet" link for a copy of our brochure.
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SKYPAD™ IN-FLIGHT ENTERTAINMENT SYSTEM

The SkyPad In-Flight Entertainment (IFE) System provides wireless audio/video on-demand (AVOD) entertainment for passengers on board the aircraft via iPad® devices. Please click on "Front sheet" link above for a copy of our brochure.
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SKY CONNECT FLEET TRACKER SYSTEM

The FIELD AVIATION Sky Connect FLEET Tracker System STC provides a complete aircraft tracking and cockpit communications solution over the Iridium® satellite network. Please click on "Front sheet" link for a copy of our brochure.
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AUXILIARY (LONG RANGE) FUEL TANKS

The FIELD AVIATION Auxiliary (Long Range) Fuel Tanks STC was designed specifically for retrofit installations into existing aircraft and to meet latest SFAR 88 requirements. This upgrade is available in both Metric and Imperial units. Please click on "Front sheet" link for a copy of our brochure.
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SOLID STATE DATA TRANSFER UNIT

The FIELD AVIATION STC for the installation of the Universal Avionics Solid State Data Transfer Unit (SSDTU) allows the user to replace the existing aircraft DTU (either floppy or Zip drive) with a solid state unit. With Zip drives becoming increasingly difficult to procure and repair, the SSDTU represents the next generation of data upload/download equipment. Please click on "Front sheet" link for a copy of ...
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EXTERNAL DOOR LOCKS.

The FIELD AVIATION External Door Locks are available for all series of DHC-8 aircraft. Please click on "Front sheet" link for a copy of our brochure.
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VIP INTERIOR

The FIELD AVIATION VIP Interior for the DHC-8-400 aircraft provides executive seating in the passenger cabin with luxurious seats, functional work areas and increased leg room. Economy seating can be retained in the aft cabin for a mixed class configuration, with class divider partitions providing separation between the passenger zones. Please click on "Front sheet" link for a copy of our brochure.
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EXTERNAL DOOR LOCKS

The FIELD AVIATION External Door Locks are available for all series of DHC-8 aircraft. Please click on "Front sheet" link for a copy of our brochure.
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EMPOWER® IN-SEAT AC POWER SYSTEM

The EmPOWER In-seat AC Power System provides individual AC power outlets for passenger and flight crew use. The EmPOWER system provides the highest available power, up to 150 VA per outlet, to support laptops and personal electronic devices. Please click on "Front sheet" link for a copy of our brochure.
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CABIN CLASS DIVIDER

The FIELD AVIATION Cabin Class Divider provides a visual separation for two-class service in the passenger cabin. Please click on "Front sheet" link for a copy of our brochure.
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AUXILIARY POWER UNIT (APU) REMOVAL

The FIELD AVIATION temporary Auxiliary Power Unit (APU) Removal STC allows for continued operations of the aircraft with the APU removed. Please click on "Front sheet" link for a copy of our brochure.
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THREE FREQUENCY ELT

The FIELD AVIATION STC for the Artex 406 MHz three frequency Emergency Locator Transmitter (ELT) provides transmission on all 3 emergency frequencies (121.5, 243.0 and 406 MHz). This third generation ELT system is designed to meet or exceed the requirements of TSO-C91a, FAR Part 91 and CAR Part V, Subpart 551.104. Please click on "Front sheet" link for a copy of our brochure.
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ENHANCED GROUND PROXIMITY WARNING SYSTEM (EGPWS)

The FIELD AVIATION EGPWS STC is a fully integrated Honeywell MK VIII Enhanced Ground Proximity Warning System installation. It was specifically designed to replace the existing MK II GPWS and provide commonality with factory installations on later production DHC-8 aircraft. Please click on "Front sheet" link for a copy of our brochure.
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AUXILIARY POWER UNIT (APU) REMOVAL.

The FIELD AVIATION APU removal STC for the DHC-8 provides the operator with a procedure for removing the OEM Installed Hamilton Sundstrand T-62T-40C7B Auxiliary Power Unit. Please click on "Front sheet" link for a copy of our brochure.
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FUEL PANEL METRIC/IMPERIAL CONVERSION

The FIELD AVIATION Metric to Imperial Conversion STC provides conversion of the fuel indication from Metric to Imperial (or from Imperial to Metric).
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HELICOPTER LONG RANGE FUEL SEAT TANK

The FIELD AVIATION Long Range Fuel Seat Tank STC was custom designed specifically for the Aerospatiale AS332 Super Puma helicopter. TC, EASA and FAA STCs are avaialble. Please click on "Front Sheet" link above for a detailed brochure.
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MAX TAKE-OFF AND RAMP WEIGHT INCREASE

STC for a 1,000 Lb increase in Max Take-Off and Ramp Weight.
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DE-ICER BOOTS INSTALLATION,REV. 1 OF EASA STC 10030757 COVERS INSTALLATION...

De-icer Boots Installation,Rev. 1 of EASA STC 10030757 covers installation of Aerazur Type 51 Wingand Tail De-icer Boots (Configuration 1)This revision of EASA STC 10030757 Rev 1 covers the allowance forinstallation of an alternativePN 51SP209 for Aerazur Wing and TailDe-icer Boots (Configura...
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MAXIMUM GROSS TAKEOFF WEIGHT INCREASE TO 37.300 LBS (C/W MZFW...

Maximum Gross Takeoff Weight Increase to 37.300 lbs (c/w MZFW Increaseand Ground Spoiler Options)
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INSTALLATION OF EFB NAVAERO T-BAG C2 TO RETROFIT OF SWEDISHCOASTGUARDMARITIME...

Installation of EFB navAero t-Bag C2 to Retrofit of SwedishCoastguardMaritime Patrol Modification as defined in STC EASA.IM.A.S.02323.
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AFT CABIN BULKHEAD REPLACEMENT INSTALLATION IN ACCORDANCE WITH FIELD AVIATION...

Aft Cabin Bulkhead Replacement Installation in accordance with Field Aviation Ltd. Modification Data Summary Number MDL-25150000 Revision IR; dated July 15 2010; or later Transport Canada approved revision.
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INSTALLATION OF COLLINS ELEMENTARY SURVEILLANCE CAPABLE TDR-94D DUAL MODE-S TRANSPONDERS...

Installation of Collins Elementary Surveillance capable TDR-94D Dual Mode-S Transponders and associated Collins CTL92E Controller.
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INSTALLATION RETROFIT OF COLLINS CMU-900 COMMUNICATION MANAGEMENT UNIT AND MILTOPE...

Installation retrofit of Collins CMU-900 Communication Management Unit and Miltope TP4429 printer appliances.
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INSTALLATION OF A HONEYWELL TCAS II WITH DUAL MODE S...

Installation of a Honeywell TCAS II with Dual Mode S Transponders. (DHC-8-300 SERIES 221, 250, 274, 279, 375, and 393)
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INSTALLATION OF GOODRICH DE-ICER BOOTS ON THE AIRCRAFT WINGS, HORIZONTAL...

Installation of Goodrich De-icer Boots on the Aircraft Wings, Horizontal Stabilizer and Vertical Stablilizer.
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INSTALLATION OF A MODIFIED SUPPORT STRUCTURE FOR AUXILIARY POWER UNIT...

Installation of a modified support structure for auxiliary power unit (APU) to accommodate a right-hand ground air conditioning port.
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FLIGHT CREW, ZODIAC MF20-517 FULL FACE OXYGEN/ SMOKE MASK UPGRADE.REV....

Flight Crew, Zodiac MF20-517 Full Face Oxygen/ Smoke Mask Upgrade.Rev. 1 was issued to correct a mistake in the STC holder name. Limitations: Installation must be in accordance with TCCA approved FACI MasterDrawing List designated 25780000, Revision A.Instructions for Continued Airworthiness:Maintenance must be performed in accordance with TCCA accepted FACI Maintenance Manual Supplement d (...) Conditions: Prior to installation of this design change it must be ...
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DE-ICER BOOT INSTALLATION LIMITATIONS: INSTALLATION OF AERAZUR TYPE 51 DE-ICE...

De-Icer Boot Installation Limitations: Installation of Aerazur Type 51 De-Ice Boots in accordance with Fields Aviation Company inc. Drawing List No. 33644; Issue 2Instructions for Continued Airworthiness Maintenance must be done in accordance with Fields Aviation Company inc.Maintenance Man (...) Conditions: None.
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DUAL UNIVERSAL UNS-1E(W) FLIGHT MANAGEMENT SYSTEM UPGRADE LIMITATIONS: INSTALLATION MUST...

Dual Universal UNS-1E(w) Flight Management System Upgrade Limitations: Installation must be performed in accordance with FACI Master Drawing and Data List N° 25670000, Rev. IR<(>,<)>Operations must be performed in accordance with FACI Flight Manual Supplement N° 25673000, Rev. IR<(>,<)>Maintenance must be performed in (...) Conditions: Limited to Serial Numbers 477, 488, 496, 498 and 504 with EASA STC10028595 (Advanced Avionics Technology) installed.
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INSTALLATION OF PROTECTIVE BREATHING EQUIPMENT (PBE)TCCA STC SA 12-57, ISSUE...

Installation of Protective Breathing Equipment (PBE)TCCA STC SA 12-57, Issue 1 Limitations: None. Conditions: Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product.
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AUXILIARY GROUND HEATER SYSTEM TCCA STC C- LSA12-128/D, ISSUE 1...

Auxiliary Ground Heater System TCCA STC C- LSA12-128/D, Issue 1 Limitations: Installation is limited to Serial Numbers 435, 440, 441, 445 and 446. Conditions: Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product.
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RH REAR FACING SEAT INSTALLATION.TCCA STC C-LSA12-006/D, ISSUE 1. LIMITATIONS:...

RH Rear Facing Seat Installation.TCCA STC C-LSA12-006/D, Issue 1. Limitations: The modification is limited to Serial numbers 435, 440 and 441 withpost-1990 Hunting or C<(>&<)>D interiors only.,,. Conditions: Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product.
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HONEYWELL AHRS TO SFIM APIRS CONVERSION PROVISIONS TCCA STC C-LSA08-056/D,...

Honeywell AHRS to SFIM APIRS Conversion Provisions TCCA STC C-LSA08-056/D, Issue 2 Limitations: Installation is limited to Serial Numbers 435, 440, 441 and 407. Conditions: Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product.
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INSTALLATION OF UPGRADED CABIN FLOOR PANELSTCCA STC C-LSA12-014/D, ISSUE 1...

Installation of upgraded Cabin Floor PanelsTCCA STC C-LSA12-014/D, Issue 1 Limitations: The modification is limited to Serial numbers 445, 446 with post-1990Hunting interiors only.Floor loads of 75 lbs/ft(s) only in conjunction with underfloor supportstructure modified per Bombardier CR 853CH2003 or equivalent.. Conditions: Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will ...
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CABIN DROP DOWN OXYGEN SYSTEM REMOVAL AND CABIN INTERIOR REFURBISHMENTTCCA...

Cabin Drop Down Oxygen System Removal and Cabin Interior RefurbishmentTCCA STC O-LSA11-177/D, Issue 1 Limitations: The modification is limited to Serial numbers 445, 446.. Conditions: Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product.
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RETROFIT INSTALLATION OF UNIVERSAL AVIONICS SYSTEMS CORP. UNS-1F FMS FORSOFTWARE...

Retrofit Installation of Universal Avionics Systems Corp. UNS-1F FMS forSoftware versions SCN 801/802 and 803Ref. TCCA SA02-48, Issue 5 Limitations: Configuration B Single UNS-1F with Software Version SCN 801, EFISEquipped Aircraft- deHavilland factory installed single UNS-1B or UNS-1B+ FlightManagement System Electrical and Structural provisions are aprerequisite to the Universal UNS-1F Flight Manageme. Conditions: Prior to installation of this modification the installer must determinethat the interrelationship between ...
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TCCA STC O-LSA06-139/D, ISSUE 2RETROFIT INSTALLATION OF A HONEYWELL KHF-950...

TCCA STC O-LSA06-139/D, Issue 2Retrofit installation of a Honeywell KHF-950 HF Radio System. Limitations: The modification is limited to Serial numbers 335, 337, 445, 446.. Conditions: Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product.
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TCCA STC O-LSA06-111/D, ISSUE 2RETROFIT OF AIRCELL ST3100 SATELLITE TELEPHONE...

TCCA STC O-LSA06-111/D, Issue 2Retrofit of AirCell ST3100 Satellite Telephone and Tracking System. Limitations: The modification is limited to Serial numbers 445, 446.. Conditions: Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product.
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INSTALLATION OF DUAL ROCKWELL COLLINS VHF-422C (8.33 KHZ) CAPABLE VHF-AM...

Installation of Dual Rockwell Collins VHF-422C (8.33 Khz) Capable VHF-AM Radio in accordance with Field Aviation East Limited Master Drawing and Data List DDL-1098 Revision IR approved December 20, 2002 or later Transport Canada approved revision.
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INSTALLATION OF RIGHT HAND GROUND AIR CONNECTIONTCCA STC C-LSA11-043/D, ISSUE...

Installation of Right Hand Ground Air ConnectionTCCA STC C-LSA11-043/D, Issue 1 Limitations: OEM installed APU must be removed in accordance with EASA STC 10035887or TCCA STC SA98-30, Issue 3.. Conditions: Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product.
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INSTALLATION OF FLIGHT COMPARTMENT REFUEL/DEFUEL PANEL INTERTECHNIQUE 798-114-5 TO REPLACE...

Installation of Flight Compartment Refuel/Defuel Panel Intertechnique 798-114-5 to replace OEM standard re-fuel/defuel panel in accordance with FAEL Master Drawing and Data List designated DDL-1100 Revision IR, dated December 11, 2002 or later Transport Canada approved revision
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1. CONFIGURATION 1- INSTALLATION OF COLLINS TCAS II /MODE-S TRANSPONDER...

1. Configuration 1- Installation of Collins TCAS II /Mode-S Transponder in accordance with Field Aviation Master Drawing and Data List designated DDL-1017, Rev. DD, or later TCCA Approved Revision. 2. Configuration 2- Installation of Collins ACAS II /Mode-S Transponder in accordance with Field Aviation Master Drawing and Data List Designated DDL-1017, Rev. DD, or later TCCA Approved Revision.
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INSTALLATION OF AFT BAGGAGE BAY DIVIDER NETSTCCA LSTC C-LSA09-212/D LIMITATIONS:...

Installation of Aft Baggage Bay Divider NetsTCCA LSTC C-LSA09-212/D Limitations: The modification is applicable only when the necessary structuralprovisions are pre-existing.. Conditions: Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product.
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G3 WATER SYSTEM MODIFICATION: TCCA LSTC C- LSA08-018/D, ISSUE 3,...

G3 Water System Modification: TCCA LSTC C- LSA08-018/D, Issue 3, dated 14September 2009. Limitations: None.. Conditions: The installation of this modification by third persons is subject towritten permission of the approval holder and holding and disposal ofthe approved appropriate documentation. Prior to installation of this modification the installer must determinethat the
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CHELTON HGA-7000 HIGH GAIN SATCOM ANTENNA AND CHELTON DAU-7050 DIPLEXER...

Chelton HGA-7000 High Gain SATCOM Antenna and Chelton DAU-7050 Diplexer / LNA on Models DHC-8-101, -102, -103, -106, -201, -202, -301, -311, -315
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DE-ICER BOOT INSTALLATION LIMITATIONS: NONE.. CONDITIONS: 1. PRIOR TO INSTALLATION...

De-Icer Boot Installation Limitations: None.. Conditions: 1. Prior to installation of this modification the installer mustdetermine that the ,,interrelationship between this modification and anyother previously installed ,,modification will introduce no adverseeffect upon the airworthiness of the product.2. The i
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INSTALLATION OF A 320CUFT BAGGAGE COMPARTMENT AND INSTALLATION OF PBE'S...

Installation of a 320cuft baggage compartment and installation of PBE's and O2 bottle into the cabin (Ref. TCCA LSTC C-LSA06-010/D) Limitations: n/a. Conditions: n/a
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VHF COMM REPLACEMENT FOR 8.33 KHZ SPACING, REF. TCCA LST...

VHF Comm Replacement for 8.33 kHz Spacing, ref. TCCA LST C-LSA08-023/D. Limitations: Prior to installation of this modification the installer must determine that the interrelationship between this modification and any other previously installed modification will introduce no adverse effect upon the airworthiness of the product. The install. Conditions: n/a
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INSTALLATION OF LIFE RAFTS. CERTIFICATION BASIS LIMITATIONS FIELD AVIATION COMPANY...

Installation of Life Rafts. Certification Basis Limitations Field Aviation Company Inc. (FACI) Modification Instructions 213610, Revision - original issue-, dated September 7, 2007or later approved revision.TCCA LSTC No. C- LSA07-322/D Conditions Aircraft Serial No. 8049 only
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INSTALLATION OF LIFE RAFTS. LIMITATIONS: AIRCRAFT SERIAL NO. 8049 ONLY....

Installation of Life Rafts. Limitations: Aircraft Serial No. 8049 only. Conditions: n/a
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INSTALLATION OF CORPORATE SHUTTLE INTERIOR. LIMITATIONS: LIMITED TO SERIAL NO....

Installation of Corporate Shuttle Interior. Limitations: Limited to serial no. 8049. Conditions: n/a
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INSTALLATION OF CORPORATE SHUTTLE INTERIOR. CERTIFICATION BASIS LIMITATIONS STC C-LSA07-021/D,...

Installation of Corporate Shuttle Interior. Certification Basis Limitations STC C-LSA07-021/D, Issue 1 dated 16 September 2007.Installation of the corporate shuttle interior must be in accordancewith Transport Canada Civil Aviation (TCCA), approved FieldAviation Company inc. (FACi) Modification instruction 204910, Revision (...) Conditions Limited to serial no. 8049
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COLLINS CTL-94E CONTROLLER FOR ELEMENTARY SURVEILLANCE LIMITATIONS: N/A. CONDITIONS: N/A

Collins CTL-94E Controller for Elementary Surveillance Limitations: n/a. Conditions: n/a
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RETROFIT OF HONEYWELL 1152106-3 400 AMP APU STARTER GENERATOR AND...

Retrofit of Honeywell 1152106-3 400 amp APU Starter Generator and Honeywell 1152108-6 Generator Control Unit.
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INSTALLATION OF ALTIMETER-METRIC INDICATOR PER FIELD AVIATION EAST LIMITED MASTER...

Installation of Altimeter-Metric Indicator per Field Aviation East Limited Master Drawing and Data List DDL-1102 latest revision.
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CONFIGURATION A (ELECTRICAL AND STRUCTURAL PROVISIONS ONLY): INSTALLATION OF BRITAX...

Configuration A (Electrical and Structural Provisions Only): Installation of Britax (Sell) Oven and relocation of TIA Coffee Makers. Configuration B: Installation of Britax (Sell) Oven and relocation of TIA coffee makers Bombardier G1 Galley (FWD), 601R40611, Series CR 25-31-301, must be used as the prerequisite to the modifications on Configurations A and B.
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REMOVAL/DISABLING AND REINSTALLATION/REENABLING OF DEHAVILLAND DITCHING DAM CR803SO00002/SB 8-92-16 PER...

Removal/disabling and reinstallation/reenabling of deHavilland Ditching Dam CR803SO00002/SB 8-92-16 per Field Aviation Company, Inc. (FACi) Modification Instruction 140901 dtd 7/30/2002.
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INSTALLATION OF AN HF ANTENNA INSIDE VERTICAL STABILIZER LEADING EDGE...

Installation of an HF Antenna inside Vertical Stabilizer Leading Edge for AlliedSignal KHF-950 HF transceiver.
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REBUILDING OF THE UPPER CABIN ROOF BEAM (BOX BEAM).

Rebuilding of the Upper Cabin Roof Beam (Box Beam).
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INSTALLATION OF ULTRA ELECTRONICS ACTIVE NOISE AND VIBRATION CONTROL (ANVC)...

Installation of Ultra Electronics Active Noise and Vibration Control (ANVC) System and Propeller Balancing and Monitoring System (PBMS).
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INSTALLATION AND MAINTENANCE OF AERAZUR ENGINE INLET DE-ICER BOOT.

Installation and maintenance of Aerazur Engine Inlet De-Icer Boot.
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INSTALLATION OF SHOULDER BELTS.

Installation of shoulder belts.
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INSTALLATION OF GROUND UTILITY WINTERIZATION KIT CONSISTING OF ENGINE HEATERS,...

Installation of Ground Utility Winterization Kit consisting of engine heaters, a battery warmer, cockpit heaters and a cabin outlet for a cabin heater.
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SLIDING WINDOW BLINDS IN DHC-8 WITH HUNTING INTERIOR

Installation of passenger sliding window blinds in Hunting interior equipped aircraft.
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