# Fairchild F-27F - Type: Aircraft model (FAA registry) - Registry code: 3373008 - Manufacturer (registry): FAIRCHILD - Model: F-27F - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 2 · Turbo-prop - Seats: 61 - Weight class: 20,000 lb and over - Cruise speed: 225 mph - Certification: Type certificated - Data sheet: [TCDS 7A1](https://openairdocs.org/tcds/7A1) (OpenAirDocs) - Holder: Maryland Air Industries Inc. - Registered aircraft: 1 - Page: https://openairdocs.org/model/fairchild-f-27f Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker. ## ADs that may apply (OpenAirDocs) Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment. - [AD 2008-22-02](https://openairdocs.org/ad/2008-22-02): Instructions for maintenance and inspection of the fuel tank systems · Maryland Air Industries F-27, F-27A, F-27B and 9 more. Effective Nov 28, 2008 - [AD 2004-22-01](https://openairdocs.org/ad/2004-22-01): Cargo restraint strap assemblies · Cargo restraint straps (Airline Container Manufacturing STC ST01004NY). Effective Dec 1, 2004 - [AD 99-19-09](https://openairdocs.org/ad/99-19-09): AFM - Limitation Section - Ice Protection System · Maryland Air Industries F-27, F-27A, F-27B and 9 more. Effective Dec 27, 1999 - [AD 98-04-31](https://openairdocs.org/ad/98-04-31): AFM - Limitations Section - Icing · Maryland Air Industries F-27, F-27A, F-27B and 9 more. Effective Mar 25, 1998 - [AD 97-23-15](https://openairdocs.org/ad/97-23-15): AFM - Limitations - Power Levers · Maryland Air Industries F-27, F-27A, F-27B and 9 more. Effective Dec 18, 1997 - [AD 90-17-13](https://openairdocs.org/ad/90-17-13): Wing Skin Stringers · Maryland Air Industries F-27, F-27A, F-27B and 4 more. Effective Sep 17, 1990 - [AD 90-13-10](https://openairdocs.org/ad/90-13-10): Cockpit Voice & Flight Data Recorders · Maryland Air Industries F-27, F-27A, F-27B and 4 more. Effective Jul 23, 1990 - [AD 90-08-10](https://openairdocs.org/ad/90-08-10): Wing Inspection · Maryland Air Industries F-27, F-27A, F-27B and 9 more. Effective May 14, 1990 - [AD 87-05-51](https://openairdocs.org/ad/87-05-51): Floor Proximity Lighting · Boeing 707-100 Long Body, 707-100B Long Body, 707-100B Short Body and 48 more. Effective May 18, 1987 - [AD 87-07-05](https://openairdocs.org/ad/87-07-05): Wing-To-Fuselage Fairing · Maryland Air Industries F-27, F-27A, F-27B and 4 more. Effective Apr 20, 1987 - [AD 86-05-09](https://openairdocs.org/ad/86-05-09): Upper Main Undercarriage Drag Stay · Maryland Air Industries F-27, F-27A, F-27B and 9 more. Effective Apr 13, 1986 - [AD 85-21-04](https://openairdocs.org/ad/85-21-04): Rod Assembly · Maryland Air Industries F-27, F-27A, F-27B and 9 more. Effective Nov 14, 1985 - [AD 82-22-51](https://openairdocs.org/ad/82-22-51): Moisture Separator Assembly · Maryland Air Industries F-27, F-27A, F-27B and 9 more. Effective Feb 3, 1983 - [AD 80-18-11](https://openairdocs.org/ad/80-18-11): Horizontal Stabilizer · Maryland Air Industries F-27, F-27A, F-27B and 9 more. Effective Sep 4, 1980 - [AD 73-12-05](https://openairdocs.org/ad/73-12-05): Vertical Stabilizer Fittings · Maryland Air Industries F-27, F-27A, F-27B and 9 more. Effective Aug 29, 1979 - [AD 66-30-04](https://openairdocs.org/ad/66-30-04): Firewall Support Tube Bracket · Maryland Air Industries F-27, F-27A, F-27B and 9 more. Effective Apr 13, 1977 - [AD 76-13-08](https://openairdocs.org/ad/76-13-08): Engine Mount Bolts · Maryland Air Industries F-27, F-27A, F-27B and 9 more. Effective Jul 7, 1976 - [AD 76-10-07](https://openairdocs.org/ad/76-10-07): Large Cargo Door · Maryland Air Industries F-27, F-27A, F-27B and 4 more. Effective Jun 14, 1976 - [AD 74-24-09](https://openairdocs.org/ad/74-24-09): Auxiliary Power Units · Airbus BAC 1-11 200 Series, BAC 1-11 400 Series, Auxiliary Power Units and 63 more. Effective Nov 19, 1975 - [AD 73-20-01](https://openairdocs.org/ad/73-20-01): Front and Rear Spar Fittings · Maryland Air Industries F-27, F-27A, F-27B and 9 more. Effective Dec 31, 1974 - [AD 72-07-12](https://openairdocs.org/ad/72-07-12): Stewardess Jump Seat · Maryland Air Industries F-27, F-27A, F-27B and 9 more. Effective Apr 6, 1972 - [AD 76-07-01](https://openairdocs.org/ad/76-07-01): Terminal Board Assembly · Maryland Air Industries F-27, F-27A, F-27B and 9 more. Effective Apr 2, 1972 - [AD 71-08-05](https://openairdocs.org/ad/71-08-05): Main Gear Drag Strut · Maryland Air Industries F-27, F-27A, F-27B and 9 more. Effective Oct 14, 1971 - [AD 70-12-03](https://openairdocs.org/ad/70-12-03): Flap Jackscrew · Maryland Air Industries F-27, F-27A, F-27B and 9 more. Effective Jun 19, 1970 - [AD 69-25-04](https://openairdocs.org/ad/69-25-04): Flap Screw Jack End · Maryland Air Industries F-27, F-27A, F-27B and 9 more. Effective Dec 6, 1969 - [AD 69-20-04](https://openairdocs.org/ad/69-20-04): Door Locking Mechanism · Maryland Air Industries F-27, F-27A, F-27B and 9 more. Effective Nov 3, 1969 - [AD 69-21-02](https://openairdocs.org/ad/69-21-02): Cabin Superchargers · British Aerospace Argosy AW.650 Series 101, F27 Mark 100, F27 Mark 300 and 18 more. Effective Oct 9, 1969 - [AD 69-20-07](https://openairdocs.org/ad/69-20-07): Flap Operating System · Maryland Air Industries F-27, F-27A, F-27B and 9 more. Effective Oct 3, 1969 - [AD 69-16-04](https://openairdocs.org/ad/69-16-04): Landing Gear Door Trolley Lever · Maryland Air Industries F-27, F-27A, F-27B and 9 more. Effective Sep 1, 1969 - [AD 69-13-06](https://openairdocs.org/ad/69-13-06): Wing Fuel Access Door Bolts · Maryland Air Industries F-27, F-27A, F-27B and 4 more. Effective Jul 9, 1969 - [AD 69-08-06](https://openairdocs.org/ad/69-08-06): Landing Gear Retraction System · Maryland Air Industries F-27, F-27A, F-27B and 9 more. Effective Apr 23, 1969 - [AD 69-08-01](https://openairdocs.org/ad/69-08-01): Horizontal Stabilizer · Maryland Air Industries F-27, F-27A, F-27B and 9 more. Effective Apr 16, 1969 - [AD 69-06-05](https://openairdocs.org/ad/69-06-05): Inverter · Maryland Air Industries F-27, F-27A, F-27B and 9 more. Effective Apr 15, 1969 - [AD 69-06-01](https://openairdocs.org/ad/69-06-01): Flap Drive System · Maryland Air Industries F-27, F-27A, F-27B and 4 more. Effective Mar 26, 1969 - [AD 69-01-01](https://openairdocs.org/ad/69-01-01): Engine Fire Extinguisher · Maryland Air Industries F-27, F-27A, F-27B and 9 more. Effective Feb 1, 1969 - [AD 69-01-03](https://openairdocs.org/ad/69-01-03): Lower Wing Access Door · Maryland Air Industries F-27, F-27A, F-27B and 9 more. Effective Jan 4, 1969 - [AD 68-23-01](https://openairdocs.org/ad/68-23-01): Cabin Superchargers · British Aerospace Argosy AW.650 Series 101, F27 Mark 100, F27 Mark 300 and 18 more. Effective Nov 21, 1968 - [AD 68-08-03](https://openairdocs.org/ad/68-08-03): Combustion Heater System · Maryland Air Industries F-27, F-27A, F-27B and 4 more. Effective May 19, 1968 - [AD 68-01-05](https://openairdocs.org/ad/68-01-05): Flap Drive System · Maryland Air Industries F-27, F-27A, F-27B and 9 more. Effective Jan 9, 1968 - [AD 67-30-03](https://openairdocs.org/ad/67-30-03): Rudder Skin Cracks · Maryland Air Industries F-27A, F-27F, F-27G and 6 more. Effective Nov 1, 1967 - [AD 67-29-02](https://openairdocs.org/ad/67-29-02): Navigation Instruments · Maryland Air Industries F-27, F-27A, F-27B and 9 more. Effective Oct 27, 1967 - [AD 67-25-04](https://openairdocs.org/ad/67-25-04): Elongated Rivet Holes · Maryland Air Industries F-27, F-27A, F-27B and 9 more. Effective Sep 8, 1967 - [AD 67-17-03](https://openairdocs.org/ad/67-17-03): Horizontal Stabilizer · Maryland Air Industries F-27, F-27A, F-27B and 9 more. Effective May 16, 1967 - [AD 67-15-02](https://openairdocs.org/ad/67-15-02): Electrical System Modification · Maryland Air Industries F-27, F-27A, F-27B and 9 more. Effective May 6, 1967 - [AD 67-12-04](https://openairdocs.org/ad/67-12-04): Rudder Horn Assembly · Maryland Air Industries F-27, F-27A, F-27B and 9 more. Effective Apr 8, 1967 - [AD 67-12-02](https://openairdocs.org/ad/67-12-02): Nose Landing Gear · Maryland Air Industries F-27, F-27A, F-27B and 9 more. Effective Apr 5, 1967 - [AD 67-11-02](https://openairdocs.org/ad/67-11-02): Cracks in Lower Fuselage Exterior · Maryland Air Industries F-27, F-27A, F-27B and 4 more. Effective Apr 5, 1967 - [AD 67-08-05](https://openairdocs.org/ad/67-08-05): Stewardess Seat Assembly · Maryland Air Industries F-27, F-27A, F-27B and 4 more. Effective Mar 11, 1967 - [AD 67-08-04](https://openairdocs.org/ad/67-08-04): Elevator Torque Tubes and Rings · Maryland Air Industries F-27, F-27A, F-27B and 9 more. Effective Mar 7, 1967 - [AD 66-16-04](https://openairdocs.org/ad/66-16-04): Flap Asymmetry Switches · Maryland Air Industries F-27, F-27A, F-27B and 3 more. Effective Jul 30, 1966 Historical (superseded or no longer in force): - [AD 74-08-09 R2](https://openairdocs.org/ad/74-08-09-R2) (historical): Waste Receptacles · Aero Spacelines 377, 377MG, 377SGT and 268 more. Effective Jul 29, 1996 All 72: https://openairdocs.org/model/fairchild-f-27f/ads.md ## Registered aircraft (1) - [N127HP](https://openairdocs.org/aircraft/N127HP): [Hagerstown Aviation Museum Inc](https://openairdocs.org/faa-owner/HAGERSTOWN%20AVIATION%20MUSEUM%20INC), [Hagerstown, MD](https://openairdocs.org/faa-place/MD/Hagerstown), built 1959, S/N 33 ## NTSB investigations None matched to aircraft with this model. ## FAA accident and incident reports (6) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 20040919023319I](https://openairdocs.org/incident/20040919023319I), Sep 19, 2004: Frchld F27F (N366SB), Las Vegas, NV, Minor damage. (-23) The flight originated at brown field in san diego area (sdm). On arrival there was a windstorm out of the south. The company's standard procedure is to… - [Incident 20010212001779I](https://openairdocs.org/incident/20010212001779I), Feb 12, 2001: Frchld F27F (N222DG), Spokane, WA. (-23) After landing at geg, mechanics discovered that the right inboard main wheel assembly, part number 9541587, was missing. A/c was enroute to geg from ykm… - [Incident 19930518018759I](https://openairdocs.org/incident/19930518018759I), May 18, 1993: Frchld F27F (N4425B), Boise, ID, Minor damage. Lost right inboard main landing wheel assembly on takeoff. Continued flight. Lack of lubrication on wheel bearing. - [Incident 19870512022229I](https://openairdocs.org/incident/19870512022229I), May 12, 1987: Frchld F27F (N222DG), Wainwright, AK, Minor damage. The airstair door came unlatched on rotation. Aircraft returned safely. Damper clip missing. - [Incident 19840125011819I](https://openairdocs.org/incident/19840125011819I), Jan 25, 1984: Frchld F27F (N222DG), Everett, WA, Minor damage. Nose gear would not extend fully. Landed without nose gear extended. - [Incident 19831010066449I](https://openairdocs.org/incident/19831010066449I), Oct 10, 1983: Frchld F27J (N108AS), Kenai, AK, Minor damage. No. 1 engine autofeathered. Fire warning light came on. Engine shutdown. Five wires in wiring bundle shorted. ## Service difficulty reports (20) As reported by operators and repair stations, by the model named in the report. - [SDR CA040519003](https://openairdocs.org/sdr/CA040519003), May 4, 2004: TIRE. SEPARATED. (CAN) UPON LANDING, THE LT IB TIRE RE-TREAD SEPARATED FROM THE TIRE. - [SDR COEA0204222](https://openairdocs.org/sdr/COEA0204222), Dec 11, 2002: CONTROL UNIT. MALFUNCTIONED. LEFT DEICE ALTERNATOR FAILED IN FLIGHT DURING CLIMB. MAINTENANCE PERSONNEL REPLACED AC CONTROL UNIT. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR CA010411004](https://openairdocs.org/sdr/CA010411004), Mar 12, 2001: SKIN. CRACKED. (CAN) CRACK FOUND AT TOP REAR CORNER OF FRONT CARGO DOOR FRAME (FUSELAGE). THE PROBLEM IS ONE BAD FLUSH RIVET CRACK FROM RIVET TO SKIN EDGE. CRACK FOUND ON DAIL - [SDR COEA0101222](https://openairdocs.org/sdr/COEA0101222), Feb 12, 2001: WHEEL. DEPARTED. AFTER LANDING, MAINTENANCE DISCOVERED THAT THE RT MLG WHEEL ASSEMBLY WAS MISSING. AXLE NUT AND SECURING BOLT WERE NOT RECOVERED. NO DAMAGE TO LANDING GEAR AXLE - [SDR CA001102005](https://openairdocs.org/sdr/CA001102005), Oct 10, 2000: SKIN. CRACKED. (CAN) A 1.5 INCH CRACK WAS FOUND AT FS 33.662 AND WL +50 APPROX. THE CRACK WAS FOUND BY X-RAY AND CONFRIMED BY EDDY CURRENT DURING A SPECIAL INSPECTION. - [SDR CA000110096](https://openairdocs.org/sdr/CA000110096), Dec 17, 1999: COMPRESSOR. SEPARATED. (CAN) STAGE 2 CYLINDER FOUND SEPARATED FROM PNEUMATIC COMPRESSOR CAUSING CASING CAUSING GEAR BOX OIL LOSS. - [SDR CA991231004](https://openairdocs.org/sdr/CA991231004), Dec 1, 1999: ANGLE. CRACKED. (CAN) DURING INSPECTION CARRIED OUT IAW AD 64-21-04, CRACK WAS FOUND ON THE REINFORCEMENT ANGLE AT THE AFT END OF THE RIB AT W.L. 201.575 - [SDR CA990907080](https://openairdocs.org/sdr/CA990907080), Aug 22, 1999: TRANSMITTER. MALFUNCTIONED. (CAN) OIL PRESSURE FLUCTUATIONS INDICATING. TRANSMITTER REPLACED. - [SDR CA990707063](https://openairdocs.org/sdr/CA990707063), Jun 3, 1999: CYLINDER. FAILED. (CAN) DURING FLIGHT, NR 2 ENGINE OIL PRESSURE BEGAN FLUCTUATING. CREW SECURED ENGINE. INVESTIGATION REVEALED THAT THE CYLINDER CAP ON THE AIR COMPRESSOR ON NR 2 - [SDR 99ZZZX2763](https://openairdocs.org/sdr/99ZZZX2763), Jun 1, 1999: ALTIMETER. MALFUNCTIONED. FOUND ENCODING ALTIMETER GRAY CODE INOPERATIVE. REPLACED ENCODING ALTIMETER SYSTEM FUNCTION, TESTED GOOD. - [SDR CA990119005](https://openairdocs.org/sdr/CA990119005), Jan 19, 1999: TRANSFORMER. FAILED. (CAN) RESISTANCE ON WINDSHIELD HAD INCREASED. NEW WINDOW ORDERED. NEXT APPLICATION OF WINDSHIELD HEAT, THE TRANSFORMER OVERHEATED AND FILLED THE COCKPIT WITH SM - [SDR CA981230043](https://openairdocs.org/sdr/CA981230043), Dec 9, 1998: WHEEL. RUPTURED. (CAN) AFTER LANDING AND DURING TAXI, THE LEFT OUTBOARD WHEEL HALF SEPARATED ALONG THE CIRCUMFERENCE. THE WHEEL HAD BEEN INSPECTED AT THE LAST TIRE CHANGE AND WA - [SDR CA980317052](https://openairdocs.org/sdr/CA980317052), Jan 15, 1998: FUEL CONTROL. DAMAGED. (CAN) FUEL CONTROL UNIT WAS LEAKING. INLET SIDE FROM FUEL PUMP WAS ENLARGED CAUSING O RING ON TUBE TO ALLOW FUEL TO ESCAPE. FCU WAS REPLACED WITH ONE OFH IGHER - [SDR CA970530010](https://openairdocs.org/sdr/CA970530010), May 15, 1997: ACTUATOR. FAILED. (CAN) A JUST OVERHAULED MAIN LANDING GEAR ACTUATOR HAD BEEN INSTALLED. DURING GROUND RETRACTION TEST, WHEN WHEELS WERE LOWERED, THE ACTUATOR DID NOT HAVE ANY DA - [SDR COEA9622202](https://openairdocs.org/sdr/COEA9622202), Dec 11, 1996: TRANSFORMER. FAILED. WHILE EN ROUTE FROM YVR-OAK, CO-PILOT'S DME INDICATOR DISPLAY WENT BLANK. LATER THE NR 1 DE-ICING GENERATOR FAILURE LIGHT ILLUMINATED ACCOMPANIED BY A SLIGHT SM - [SDR 97ZZZM81](https://openairdocs.org/sdr/97ZZZM81), Dec 11, 1996: RELAY. FAILED. WHILE EN ROUTE FROM YVR-OAK, CO-PILOT'S DME INDICATOR DISPLAY WENT BLANK. LATER THE NR 1 DE-ICING GENERATOR FAILURE LIGHT ILLUMINATED ACCOMPANIED BY A SLIGHT SM - [SDR COEA9622201](https://openairdocs.org/sdr/COEA9622201), Oct 18, 1996: ENGINE. FAILED. OAK/YVR - WHILE EN ROUTE WITH MODERATE TURBULENCE AND MODERATE ICING CONDITIONS, LT ENGINE AUTOFEATHERED IN CRUISE. CREW INITIATED AIRSTART PROCEDURES. ENGINE W - [SDR CA960103534](https://openairdocs.org/sdr/CA960103534), Nov 29, 1995: PIPE FUEL SERVO. BLISTERED. (CAN)DURING FIFTY HOUR ROUTINE (SERVICE BULLETIN) INSPECTION OF THE SERVO FUEL PIPE, WHICH RUNS FROM THE HIGH PRESSURE FUEL PUMP TO THE FUEL CONTROL UNIT, WAS F - [SDR COEA9522205](https://openairdocs.org/sdr/COEA9522205), Nov 21, 1995: STRIKER PLATE. LOOSE. MAF - ON APPROACH INTO MIDLAND, TX, CREW LOWERED LANDING GEAR BUT WAS UNABLE TO GET A POSITIVE DOWN & LOCKED INDICATION FOR NOSE LANDING GEAR. APPROACH ABORTED. - [SDR COEA9522202](https://openairdocs.org/sdr/COEA9522202), May 12, 1995: DUCT. OUT OF POSITION. FLT 7378 - MSY - DURING CRUISE CREW STARTED THE APU FOR BACKUP AFTER NOTICING THEIR BATTERIES WERE DISCHARGING. AFTER THE APU WAS STARTED THE FIRE WARNING ALARM ## STCs that may be installed (OpenAirDocs) (75, first 50) Approved for this model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has. - [STC SA2622NM](https://openairdocs.org/stc/SA2622NM): Installation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101). Precise Flight Inc - [STC SA3413NM](https://openairdocs.org/stc/SA3413NM): Installation of Floor Proximity Emergency Escape path Marking System. Bruce Aerospace Inc - [STC ST04359CH](https://openairdocs.org/stc/ST04359CH): Reduction of payload to 7500 lbs. Installation of placard per Rezich & Rezich drawing RR004, Revision NONE, dated August 25, 2017,, or later FAA approved revision. Rezich and Rezich Aviation Consulting Inc - [STC SA43SW](https://openairdocs.org/stc/SA43SW): Structural installation of Collins 137Y-1 doppler antenna and Collins 621C-1 transmitter-receiver. Associated Air Center, Inc. - c/o CT Corporation System - [STC ST00384WI](https://openairdocs.org/stc/ST00384WI): Installation of Keddeg Company P/N 21BC116 Coalescer Assembly. Purolator Facet, Inc - [STC SA2016NM](https://openairdocs.org/stc/SA2016NM): Installation of a de-icing system on the Rolls Royce P/N RK29954A engine inlet cowl. ROBERT W. MURRAY - [STC SA302WE](https://openairdocs.org/stc/SA302WE): Incorporate a de-icing system (as manufactured by applicant) externally on Rotol propeller spinner as an alternate to Dowty Rotol internal elements. If applied to original spinner, Montgomery Systems Tech., Inc. P/N 72196-2 will apply. If applied to a new aluminum nose spinner P/N 72196-1 will apply. Dowty Rotol Service Bulletin Section 61-170 pages 1 and 2 outlines a revised spinner de-icing system. This is a Napier external system. Approval of the A.R.B. is indicated. (Continued on page 3). ROBERT W. MURRAY - [STC SA253CE](https://openairdocs.org/stc/SA253CE): Installation of Hoskins Supplemental, Model E, High Intensity Wing Tip Lights, Model C Tail Light, with or without Model 2 High Intensity Fuselage Lights. BF Goodrich Aerospace - [STC SA392CE](https://openairdocs.org/stc/SA392CE): Install Hoskins Twilighter Mk V supplementary lighting system including Model E wing tip lights and Model C tal lights. BF Goodrich Aerospace - [STC ST177CH](https://openairdocs.org/stc/ST177CH): Installation of AlliedSignal expanded parameter flight data recorders and associated sensors. Canard Aerospace Corporation - [STC ST178CH](https://openairdocs.org/stc/ST178CH): Installation of a BFGoodrich Aerospace Jet Electronics and Technology, standby attitude indicator and power supply. Canard Aerospace Corporation - [STC SA2246WE](https://openairdocs.org/stc/SA2246WE): Installation of large cargo door. (F27 S/N 21 AND SUBS). Fokker50Freighter STC Corporation - [STC SA120SW](https://openairdocs.org/stc/SA120SW): Installation of Collins Autopilot AP-101E with flight director computer 562A-6 or 562A-4A. Rockwell Collins Inc - [STC SA190SW](https://openairdocs.org/stc/SA190SW): Installation of Collins Automatic pilot AP-103. Rockwell Collins Inc - [STC SA1610SW](https://openairdocs.org/stc/SA1610SW): Installation of Safeway Deicer Boot P/N 5651 and/or Semsa Lead P/N S.2002 in lieu of Dowty Rotol Boot and/or Leads on Dowty Rotol propeller model R193/4-30-4/50 with blades P/N RA 25907. UNC Accessory Service - [STC ST00296NY](https://openairdocs.org/stc/ST00296NY): Installation of a Class E cargo interior. Field Aviation Co, Inc - [STC SA5161NM](https://openairdocs.org/stc/SA5161NM): Installation of passenger seats and floor modification. Flight Structures Inc - [STC SA1419GL](https://openairdocs.org/stc/SA1419GL): Installation of Norton lightning diverters. Norton Company, Performance Plactics - [STC SA1314WE](https://openairdocs.org/stc/SA1314WE): Installation of either United Control Data Division #V-557 or Fairchild #A-100 cockpit voice recorder system. Northwest Airlines, Inc. Lists F27 Series - [STC SA1333WE](https://openairdocs.org/stc/SA1333WE): Northern Aero Industries, Ltd. cyclic deicing system Model78-10055. Northwest Airlines, Inc. Lists F27 Series - [STC SA153WE](https://openairdocs.org/stc/SA153WE): Replacement of nacelle tail cone originally constructed of fibre-glass with a West Coast manufactured tail cone of2024T3 material. Northwest Airlines, Inc. Lists F27 Series - [STC SA1571WE](https://openairdocs.org/stc/SA1571WE): Relocation of Fairchild Model F-542 flight data recorder. Northwest Airlines, Inc. Lists F27 Series - [STC SA3096WE](https://openairdocs.org/stc/SA3096WE): Installation of Collins Radio Co. Model FPC-75 ground proximity warning system. Northwest Airlines, Inc. Lists F27 Series - [STC SA4-1209](https://openairdocs.org/stc/SA4-1209): Cabin air-conditioning modification and addition of inflight cabin air recirculation. Northwest Airlines, Inc. Lists F27 Series - [STC SA488SW](https://openairdocs.org/stc/SA488SW): Installation of #1 and #2 VHF communication system, VHF navigation system, #2 compass system, flight data recorder wiring modification, transponder antenna bracket and RCA AVQ-60D transponder. Northwest Airlines, Inc - [STC SA631SW](https://openairdocs.org/stc/SA631SW): Installation of Fairchild A-100 voice recorder system. Northwest Airlines, Inc - [STC SA632SW](https://openairdocs.org/stc/SA632SW): Installation of United Data F-542 recorder. Northwest Airlines, Inc - [STC SA853WE](https://openairdocs.org/stc/SA853WE): Bendix 4B39 solid state voltage and frequency control modification to Jack & Heintz F-35-5 rotary inverter. Northwest Airlines, Inc. Lists F27 Series - [STC SA1005GL](https://openairdocs.org/stc/SA1005GL): Install enclosed overhead baggage bins fabricated. Britt Airways, Inc - [STC SA2153CE](https://openairdocs.org/stc/SA2153CE): Modification of the nose gear snubber. Peterein Mike - [STC SA2155NM](https://openairdocs.org/stc/SA2155NM): Interior modification. Flight Structures Inc - [STC SA2916WE](https://openairdocs.org/stc/SA2916WE): Installation of emblem lights on tip of horizontal tail. DeVore Aviation Corporation of America, a New Mexico Corporation - [STC SA29PC](https://openairdocs.org/stc/SA29PC): ONE ONLY STC, SN 31, N222DG: Installation of a large cargo door with integral emergency exit door in fuselage forebody. Air Asia Company LTD - [STC SA1179SW](https://openairdocs.org/stc/SA1179SW): Installation of Hartman vertical scale engine instruments. Tiger Air Svc Center, Inc - [STC SA384SW](https://openairdocs.org/stc/SA384SW): Installation of radio racks with associated changes. Tiger Air Svc Center, Inc - [STC SA386SW](https://openairdocs.org/stc/SA386SW): To fabricate wiring harness and make complete radio installation. Tiger Air Svc Center, Inc - [STC SA578SW](https://openairdocs.org/stc/SA578SW): Fabrication and installation of rack for radar in nose wheel area. Tiger Air Svc Center, Inc - [STC SA622SW](https://openairdocs.org/stc/SA622SW): Relocation of United Data recorder Model F-542 to aft cabin area. Tiger Air Svc Center, Inc - [STC SA1463CE](https://openairdocs.org/stc/SA1463CE): Installation of microwave landing system airborne equipment. Wilcox Electric, Inc - [STC SA610NW](https://openairdocs.org/stc/SA610NW): Installation of passenger seating configurations. Pacific Alaska Airlines Inc - [STC SA364SW](https://openairdocs.org/stc/SA364SW): Collins AP-103E autopilot on aircraft with gross weight up to and including 42,000 pounds. Tiger Air Svc Center, Inc - [STC SA2569WE](https://openairdocs.org/stc/SA2569WE): Installation of battery temperature monitor system. K S Avionics, Inc - [STC SA36NW](https://openairdocs.org/stc/SA36NW): Installation of Sundstrand Ground Proximity Warning System. Sundstrand Data Control Inc - [STC SA119SW](https://openairdocs.org/stc/SA119SW): Interior modification. Ward Intl Aircraft Service. Lists F27 Series - [STC SA245SW](https://openairdocs.org/stc/SA245SW): Interior modification. Ward Intl Aircraft Service. Lists F27 Series - [STC SA306SW](https://openairdocs.org/stc/SA306SW): Aft cabin window. Ward Intl Aircraft Service. Lists F27 Series - [STC SA487SW](https://openairdocs.org/stc/SA487SW): Rotating beacon. Ward Intl Aircraft Service. Lists F27 Series - [STC SA54SW](https://openairdocs.org/stc/SA54SW): Interior installation. Ward Intl Aircraft Service. Lists F27 Series - [STC SA56SW](https://openairdocs.org/stc/SA56SW): Interior modification. Ward Intl Aircraft Service. Lists F27 Series - [STC SA591SW](https://openairdocs.org/stc/SA591SW): Interior modification. Ward Intl Aircraft Service. Lists F27 Series All 75: https://openairdocs.org/model/fairchild-f-27f/stcs.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.