# N702M: Fairchild SA227-AC, registration cancelled 2005-01-21 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: January 21, 2005 - Status when cancelled: Valid registration - Airframe: [Fairchild SA227-AC](https://openairdocs.org/model/fairchild-sa227-ac) (registry code 3377509) - Engine: [AiResearch TPE331 series](https://openairdocs.org/engine/airesearch-tpe331-series) (registry code 01514) - Data sheets: [TCDS A8SW](https://openairdocs.org/tcds/A8SW) (OpenAirDocs) - Serial number: AC-702 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, normal - Airworthiness date: February 29, 1988 - Certificate issued: August 11, 2004 - Last registry action: August 11, 2004 - Mode S code: A95D0F - Owner when cancelled: [Ibc Airways Inc](https://openairdocs.org/faa-owner/IBC%20AIRWAYS%20INC) - Location: [Doral, FL](https://openairdocs.org/faa-place/FL/Doral) - Owner type: Corporation - Owner's area on the map: 25.7795° N, 80.2996° W: Placed by OpenAirDocs at the center of ZIP code 33126, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N702M - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=702M - Page: https://openairdocs.org/deregistered/N702M-2005-01-21 From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Fairchild SA227-AC: https://openairdocs.org/model/fairchild-sa227-ac.md ## Service difficulty reports (37) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR 2002F00419](https://openairdocs.org/sdr/2002F00419), Jan 29, 2002: DOOR SEAL. FAILED. CABIN ALTITUDE WARNING LIGHT CAME ON ABOVE 10,000 FEET. CREW GOT AIRCRAFT TO PRESSURIZE IN EITHER AUTOMATIC OR MANUAL MODE. CREW RETURNED TO STATION. PASSENGER - [SDR 2002F00353](https://openairdocs.org/sdr/2002F00353), Jan 29, 2002: SEAL. DAMAGED. DEN - FLT 1314 - CABIN ALTITUDE WARNING LIGHT CAME ON ABOVE 10,000 FEET. CREW COULD NOT GET AIRCRAFT TO PRESSURIZE IN EITHER AUTOMATIC OR MANUAL MODE. CREW RETU - [SDR 2002F00522](https://openairdocs.org/sdr/2002F00522), Dec 5, 2001: HYDRAULIC LINE. LEAKING. WDG - FLT 1322 - ON CLIMB-OUT, BOTH HYD LIGHTS CAME ON AND HYDRAULIC PRESSURE GAUGE WENT TO '0'. CREW LANDED AFTER DECLARING EMERGENCY AND MANUALLY EXTENDING TH - [SDR 2002F00421](https://openairdocs.org/sdr/2002F00421), Dec 5, 2001: LINE. LEAKING. ON CLIMB-0UT, BOTH HYDRAULIC LIGHTS CAME ON AND HYDRAULIC PRESSURE GAGE WENT TO ZERO. CREW LANDED AFTER DECLARING EMERGENCY AND MANUALLY EXTENDING THE GEAR. SUS - [SDR 2002F00095](https://openairdocs.org/sdr/2002F00095), Dec 5, 2001: HYDRAULIC LINE. LEAKING. FLT 1322 - ON CLIMB-OUT, BOTH HYD LIGHTS CAME ON AND HYDRAULIC PRESSURE GATE WENT TO '0'. CREW LANDED AFTER DECLARING EMERGENCY AND MANUALLY EXTENDING THE GEAR. - [SDR 20010212SG007](https://openairdocs.org/sdr/20010212SG007), Jan 19, 2001: HYDRAULIC LINE. LEAKING. BIL - FLT 2573 - CREW WS ON DOWNWIND LEG WHEN THE HYDRAULIC PRESSURE LIGHTS STARTED COMING ON INTERMITTENTLY. AFTR FLAPS WERE SELECTED TO 1/2 AND WENT TO THAT S - [SDR 20010112SG027](https://openairdocs.org/sdr/20010112SG027), Nov 6, 2000: INDICATOR. FAULTY. FLT 1318 - DFW - GEAR WAS EXTENDED FOR LANDING AT ELD. THE NLG GREEN DOWN LIGHT DIDN''T COME ON. BULBS AND LIGHT MODULES WERE SWAPPED AND LIGHT DIDN''T COME ON. - [SDR 20010112SG028](https://openairdocs.org/sdr/20010112SG028), Oct 1, 2000: ENGINE. DETERIORATED. FLT 2570 - BIL - LEFT ENGINE TORQUE DROPPED 15 PERCENT DURING TAEOFF ROLL. MAINTENANCE VERIFIED LOW TORQUE DURING ENGINE RUNS. HOT SECTION DETERIORATION IS SUSP - [SDR 20010112SG030](https://openairdocs.org/sdr/20010112SG030), Sep 19, 2000: WIRE. DAMAGED. FLT 2584 - BIL - CREW NOTICED CABIN DOOR WARNING LIGHT CAME ON AT APPROX 5.7 TO 6.0 CABIN PRESSURE PSID. INTERMITTENT WIRING PROBLEM. REPLACED WIRING FROM DOOR - [SDR 20010103AP006](https://openairdocs.org/sdr/20010103AP006), Sep 6, 2000: WIRE. MISINSTALLED. OLF - FLT 2571 - CABIN DOOR WARNING LIGHT CAME ON ABOVE 10,000 FT OR WHEN CABIN PRESS AS ABOVE 4.5 PSID. INTERMITTENT WIRING PROBLEM. ANNUNCIATOR PNL WAS CHANGE - [SDR BSAA200000026](https://openairdocs.org/sdr/BSAA200000026), Sep 6, 2000: DIODE. FAILED. CABIN DOOR WARNING LIGHT CAME ON ABOVE 10,000 FEET OR WHEN THE CABIN PRESSURIZATION WAS ABOVE 4.5 PSID. MAINTENANCE TRACKED TROUBLE TO 4 BAD DIODES IN THE RL-5 - [SDR 20001011AP007](https://openairdocs.org/sdr/20001011AP007), May 8, 2000: CLAMP. LOOSE. GTF - FLT 2550 - LEFT WING OVERHEAT LIGHT CAME ON FLASHING DURING CLIMB-OUT. FLASHING IS 250 CELSIUS SENSOR. CREW FOLLOWED EMERGENCY PROCEDURES, SHUT OFF LEFT G - [SDR 20000717AP006](https://openairdocs.org/sdr/20000717AP006), May 8, 2000: CLAMP. LOOSE. FLT 2550 - GTF - LEFT WING OVERHEAT LIGHT CAME ON FLASHING DURING CLIMB-OUT. FLASHING IS 250 C SENSOR. CREW FOLLOWED EMERGENCY PROCEDURES, SHUT OFF LEFT GEN AND - [SDR 20000717AP005](https://openairdocs.org/sdr/20000717AP005), May 8, 2000: CLAMP. LOOSE. FLT 2550 - GTF - LEFT WING OVERHEAT LIGHT CAME ON FLASHING DURING CLIMB-OUT. FLASHING IS 250 C SENSOR. CREW FOLLOWED EMERGENCY PROCEDURES, SHUT OFF LEFT GEN AND - [SDR 20000614SH004](https://openairdocs.org/sdr/20000614SH004), May 8, 2000: CLAMP. LOOSE. GTF - FLT 2550 - LT WING OVERHEAT LIGHT CAME ON FLASHING DURING CLIMBOUT. (FLASHING IS 250 C SENSOR). CREW FOLLOWED EMERGENCY PROCEDURES, SHUT OFF LT GEN AND LT - [SDR 20000602SH014](https://openairdocs.org/sdr/20000602SH014), May 8, 2000: CLAMP. LOOSE. GTF - FLT 2550 - LEFT WING OVERHEAT LIGHT CAME ON FLASHING DURING CLIMB-OUT. (FLASHING IS 250 C SENSOR). CREW FOLLOWED EMERGENCY PROCEDURES, SHUT OFF LEFT GENER - [SDR 98ZZZX3817](https://openairdocs.org/sdr/98ZZZX3817), Sep 25, 1998: TACH GENERATOR. FAILED. HOT/HRO - FLT 1215 - AIRRAFT WAS RELEASED FOR TAKEOFF FORM HOT TO HRO. WHILE EN ROUTE TO HRO, THE LT RPM GAUGE SLOWLY DROPPED TO ZERO WITH NO APPARENT DROP IN A - [SDR 98ZZZX3818](https://openairdocs.org/sdr/98ZZZX3818), Sep 24, 1998: BELT. BROKEN. HOT/HRO - FLT 1217 - AIRCRAFT WAS RELEASED FOR TAKEOFF FROM HOT TO HRO. WHILE IN CLIMB TO HRO, THE CREW HEARD A LOUD BANG FROM THE FRONT OF THE AIRCRAFT. THERE - [SDR ASE98001](https://openairdocs.org/sdr/ASE98001), Jan 2, 1998: RETRACT MECH. MALFUNCTIONED. DFW-ELD - FLT 1253 - AFTER TAKEOFF, WHEN GEAR WAS SELECTED UP, GEAR FAILED TO RETRACT. CONTINUED CLIMB TO SAFE LEVEL AND COMPLETED CHECKLIST, CONTACTED ATC FOR - [SDR 98ZZZM108](https://openairdocs.org/sdr/98ZZZM108), Nov 24, 1997: 'X' SCREW. OUT OF ADJUST. DFW - FLT 1231 - BOTH ENGINES REPORTED LOW TORQUE DURING TAKEOFF ROLL, LEFT TORQUE 40 PERCENT, RIGHT TORQUE 80 PERCENT. TAKEOFF ABORTED. AIRCRAFT RETURNED TO GA - [SDR 98ZZZM107](https://openairdocs.org/sdr/98ZZZM107), Nov 23, 1997: 'X' SCREW. OUT OF ADJUST. DFW - FLT 1231 - LEFT ENGINE READS 80 PERCENT TORQUE AND RIGHT ENGINE READS 95 PERCENT TORQUE AT 100 PERCENT RPM IN FLIGHT. EGT 620 DEGREES. AIRCRAFT RETURNED T - [SDR COMA9720010](https://openairdocs.org/sdr/COMA9720010), Feb 7, 1997: CONTROL ROD. CREASED. DURING COMPLIANCE OF A.D. 97-02-02 PER S/B 227-27-041, THE ELEVATOR CONTROL ROD, BETWEEN CONTROL COLUMN AND WALKING BEAM, ROD END BEARING RETAINER/DUST COVER WA - [SDR COMA9720009](https://openairdocs.org/sdr/COMA9720009), Feb 7, 1997: CONTROL ROD. CREASED. DURING COMPLIANCE OF A.D. 97-02-02 PER S/B 227-27-041, THE ELEVATOR CONTROL ROD, BETWEEN CONTROL COLUMN AND WALKING BEAM, ROD END BEARING RETAINER/DUST COVER WA - [SDR COMA9720008](https://openairdocs.org/sdr/COMA9720008), Feb 7, 1997: BEARING. WORN. DURING COMPLIANCE OF A.D. 97-02-02 PER S/B 227-27-041, THE COPILOT'S CONTROL COLUMN ROLLER BEARING FAILED THE TORQUE CHECK. THE BEARING AND THE DOUBLER IT IS AT - [SDR COMA9720007](https://openairdocs.org/sdr/COMA9720007), Feb 7, 1997: BEARING. WORN. DURING COMPLIANCE OF A.D.97-02-02 PER S/B 227-27-041, THE PILOT'S CONTROL COLUMN ROLLER BEARING FAILED THE TORQUE CHECK. THE BEARING AND THE DOUBLER IT IS ATTAC - [SDR COMA9720006](https://openairdocs.org/sdr/COMA9720006), Jan 28, 1997: TORQUE TUBE. CORRODED. DURING COMPLIANCE OF AD 96-21-05, THE RT ELEVATOR TORQUE TUBE WAS FOUND TO HAVE INTERNAL CORROSION BEYOND ACCEPTABLE LIMITS. THE TORQUE TUBE WAS REPLACED WITH A - [SDR COMA9720005](https://openairdocs.org/sdr/COMA9720005), Jan 28, 1997: TORQUE TUBE. CORRODED. DURING COMPLIANCE OF AD 96-21-05, THE LT ELEVATOR TORQUE TUBE WAS FOUND TO HAVE INTERNAL CORROSION BEYOND ACCEPTABLE LIMITS. THE TORQUE TUBE WAS REPLACED WITH A - [SDR COMA9620016](https://openairdocs.org/sdr/COMA9620016), Sep 17, 1996: FUEL NOZZLES. MALFUNCTIONED. LEFT ENGINE DOES NOT ACHIEVE REQUIRED TORQUE FOR TAKEOFF. REPLACED THE ENGINE FUEL NOZZLES. - [SDR COMA9620012](https://openairdocs.org/sdr/COMA9620012), Jul 12, 1996: DOWNLOCK SWITCH. FAILED. THE RIGHT MLG WOULD NOT INDICATE DOWN AND LOCKED UNTIL CYCLED 3 TIMES. REPLACED THE RIGHT MLG OUTBOARD DOWNLOCK SWITCH. - [SDR COMA9620009](https://openairdocs.org/sdr/COMA9620009), Jun 27, 1996: PROPELLER. LEAKING. OIL IS DRIPPING FROM THE LEFT ENGINE PROPELLER. REPLACED PROPELLER. - [SDR COMA9620003](https://openairdocs.org/sdr/COMA9620003), Feb 29, 1996: EGT COMPENSATOR. OUT OF ADJUST. RT ENGINE TORQUE ROLLBACK FROM 87 PERCENT TO 82 PERCENT DURING TAKEOFF. RECALIBRATED THE EGT COMPENSATOR. - [SDR COM20381](https://openairdocs.org/sdr/COM20381), Jun 29, 1995: WHEEL HALF. CRACKED. RAMP AGENT NOTICED A PART 0F THE OTBD WHEEL HALF CAME APART, WHILE THE AIRCRFT WAS TAXIING INTO GATE AREA. REMOVED WHEEL S/N FEB88-192 AND TOOK IT OUT OF SERVIC - [SDR COM20380](https://openairdocs.org/sdr/COM20380), Jun 27, 1995: TUBE ASSY. BROKEN. HYDRAULIC LEAK LT MLG AREA. REPLACED BROKEN FLAP HYDRAULIC LINE ASSY. - [SDR COM20368](https://openairdocs.org/sdr/COM20368), May 15, 1995: SAS CONTROL. DEFECTIVE. SAS ARM INDICATOR REMAINED ON ABOVE 145 KNOTS. REPLACED THE SAS CONTROL BOX. - [SDR COM20367](https://openairdocs.org/sdr/COM20367), Apr 30, 1995: ATTITUDE GYRO. DEFECTIVE. COPILOTS ATTITUDE INDICATOR CIRCUIT BREAKER TRIPPED, WILL NOT RESET. REPLACED COPILOTS ATTITUDE INDICATOR. - [SDR COM20359](https://openairdocs.org/sdr/COM20359), Mar 11, 1995: DOUBLER. CRACKED. FOUND PAX DOOR UPPER FORWARD CORNER FRAME DOUBLER TO BE CRACKED. FURTHER INSPECTION REVEALED UPPER FORWARD CORNER FRAME ALSO TO BE CRACKED. REPLACED PARTS WITH - [SDR COM20358](https://openairdocs.org/sdr/COM20358), Mar 11, 1995: FRAME. CRACKED. FOUND PASSENGER DOOR UPPER FORWARD CORNER FRAME TO BE CRACKED. FIRST NOTICED CORNER DOUBLER (COVER) TO BE CRACKED. WHEN DOUBLER WAS REMOVED FOUND FRAME TO ALSO ## FAA accident and incident reports (4) 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 19980912038809I](https://openairdocs.org/incident/19980912038809I), Sep 12, 1998: Swrngn SA227AC (N702M), Hot Springs, AR. (-5) After a normal landing, when reverse thrust was applied, the number 1 engine lost power. The asymmetrical reverse thrust caused the aircraft to veer off… - [Incident 19900411020219I](https://openairdocs.org/incident/19900411020219I), Apr 11, 1990: Swrngn SA227AC (N702M), Louisville, KY. Loss of oil pressure. Shut down and landed. Left engine prop governor reset oil line cracked. Balanced propeller. - [Incident 19900410014539I](https://openairdocs.org/incident/19900410014539I), Apr 10, 1990: Swrngn SA227AC (N702M), Dayton, OH. NR1 engine oil pressure warning. Shut down and made emergency landing. Prop governor reset line replaced. - [Incident 19900406020609I](https://openairdocs.org/incident/19900406020609I), Apr 6, 1990: Swrngn SA227AC (N702M), Fort Wayne, IN. Engine oil pressure light flickering. Precautionary landing. Left engine prop governor reset oil line cracked. ## Other aircraft with N702M - [Cancelled 1935-04-01](https://openairdocs.org/deregistered/N702M-1935-04-01): Curtiss Robin 3PCLM, S/N 641. Owner: [Frank Harris Jr](https://openairdocs.org/faa-owner/FRANK%20HARRIS%20JR), [Brooklyn, NY](https://openairdocs.org/faa-place/NY/Brooklyn) --- 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.