# N808MA: 1988 Boeing 727-231, registration cancelled 2002-06-20 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: June 20, 2002 - Exported to: Canada - Status when cancelled: Valid registration - Airframe: [Boeing 727-231](https://openairdocs.org/model/boeing-727-231) (registry code 1384079) - Engine: [Pratt & Whitney JT8D series](https://openairdocs.org/engine/pratt-whitney-jt8d-series) (registry code 52053) - Data sheets: [TCDS A3WE](https://openairdocs.org/tcds/A3WE) (OpenAirDocs) - Serial number: 21988 - Year built: 1988 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: December 31, 1992 - Certificate issued: June 20, 2002 - Last registry action: June 20, 2002 - Mode S code: AB00A9 - Owner when cancelled: [Wells Fargo Bank Northwest Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NORTHWEST%20NA%20TRUSTEE) - Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City) - Owner type: Corporation - Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N808MA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=808MA - Page: https://openairdocs.org/deregistered/N808MA-2002-06-20 From the FAA registry file of October 28, 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 Boeing 727-231: https://openairdocs.org/model/boeing-727-231.md ## Service difficulty reports (23) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR 2001F00454](https://openairdocs.org/sdr/2001F00454), Sep 6, 2001: DOOR. OUT OF ADJ. ON TAKEOFF ROLL, FORWARD ENTRY L1 DOOR LIGHT CAME ON, HANDLE UNSEATED. ADJUSTED/TEST DOOR IAW MM 52-11-01. PRESSURIZED AIRCRAFT TO 1 PSI IAW MM 21-31-00. NO DOO - [SDR 2001F00120](https://openairdocs.org/sdr/2001F00120), Jun 12, 2001: HYDRAULIC LINE. CHAFED. DURING CRUISE FLIGHT, LOST ALL 'A' HYDRAULIC SYSTEM FLUID. ACCOMPLISHED ABNORMAL CHECKLIST. DIVERTED TO INDIANAPOLIS. FOUND NR 2 ENGINE HYDRAULIC PUMP PRESSURE - [SDR 20010111SG025](https://openairdocs.org/sdr/20010111SG025), Aug 28, 2000: LONGERON. CRACKED. DURING C-CHECK, FOUND AFT CARGO COMPARTMENT BS 950E AT STRINGER 29R HAS CORROSION. REMOVED CORROSION FROM STRINGER AND FOUND CRACK IN STRINGER AT STATION 950E. - [SDR 20010111SG029](https://openairdocs.org/sdr/20010111SG029), Aug 16, 2000: SEAT TRACK. CRACKED. DURING C-CHECK, FOUND SEAT TRACK LEFT, OUTBOARD OF CENTER, TRACK CORRODED AT OUTER EDGES BETWEEN BS 1030 AND 1070. REMOVED CORROSION FROM TRACK, FOUND TRACK CRA - [SDR 20010111SG026](https://openairdocs.org/sdr/20010111SG026), Aug 16, 2000: SEAT TRACK. CORRODED. DURING C-CHECK, FOUND SEAT TRACK LEFT OUTBOARD BETWEEN BS 1110-1130 CORRODED ON UPPER FACE. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-10-2, 51-30-2 AND 53-10-5 - [SDR 20010111SG028](https://openairdocs.org/sdr/20010111SG028), Aug 8, 2000: STRINGER. CORRODED. DURING C-CHECK, FOUND LEFT FUSELAGE STATION 1160 TO 1183 STRINGER 22L HAS SURFACE CORROSION. REMOVED AND REPLACED DAMAGED STRINGER 24.5 INCHES AT LT FS 1160-118 - [SDR 20010117SG001](https://openairdocs.org/sdr/20010117SG001), Aug 8, 2000: STRUCTURE. DAMAGED. DURING C-CHECK, FOUND 1 INCH DAMAGE TO LEFT HORIZONTAL STAB LOWER FORWARD CHORD OF FORWARD SPAR STATION 101. CUT OUT DAMAGED SECTION OF CHORD. FABRICATED AND IN - [SDR 20010111SG027](https://openairdocs.org/sdr/20010111SG027), Jul 26, 2000: WEB. CRACKED. DURING C-CHECK, FOUND FUSELAGE UPPER LOBE INTERIOR AFT LEFT FLOOR PLATE BETWEEN STATION BS 1050 AND BS 1183 AND BETWEEN LEFT OUTBOARD OF CENTER TRACK TO THE WAL - [SDR 20000522AP001](https://openairdocs.org/sdr/20000522AP001), Mar 24, 2000: VALVE. FAILED. UPON REACHING CRUISE ALT FL310, AIRCRAFT EXPERIENCED TOTAL SYSTEM A HYD FAILURE. ACCOMPLISHED ''A'' SYSTEM HYDRAULIC FAILURE CHECKLIST, IAW AOM VOL 1 EMERGENCY - [SDR MYWA2000ADB00](https://openairdocs.org/sdr/MYWA2000ADB00), Mar 10, 2000: TRANSMISSION. WORN. FLAPS WILL NOT RETRACT FULLY DUE TO RT. MID FLAP FAIRING BEARING WORN(I/B). - [SDR 2000ZZZM84](https://openairdocs.org/sdr/2000ZZZM84), Dec 8, 1999: COUPLER. DAMAGED. MIA - ON CLIMB-OUT, WITH AUTO PILOT ENGAGED AT 10000 PLUS 250-260 KTS RUDDER SPLIT AND AUTO PILOT COULD NOT CONTROL AIRCRAFT. DISCONNECTED AUTO PILOT AND FOUND - [SDR 2000ZZZX474](https://openairdocs.org/sdr/2000ZZZX474), Dec 5, 1999: BUFFET. DETECTED. ON TAKEOFF FROM ACA WHILE CLIMBING THROUGH 18,000 FEET, FELT AIRCRAFT JOLT. RETURNED TO ACA FOR GROUND INSPECTION. RETURNED TO ACA AFTER DUMPING FUEL TO OBTAIN - [SDR 99ZZZM297](https://openairdocs.org/sdr/99ZZZM297), Apr 7, 1999: ECCENTRIC. MISSING. DURING P/T WALK AROUND, FOUND LEFT WING INBOARD T/E MID FLAP CARRIAGE MISSING UPPER INBOARD ECCENTRIC, LOCKING TAB WASHER AND NUT ON OUTBOARD CARRIAGE. REPLACED - [SDR 99ZZZM37](https://openairdocs.org/sdr/99ZZZM37), Jan 3, 1999: BATTERY PACK. DISCHARGED. ON PREFLIGHT, TRANSIT FOUND RIGHT FORWARD OVERWING EMERGENCY LIGHT WILL NOT TURN OFF. REPLACED BATTERY PACK, OPS CHECK NORMAL IAW 33-50-00. (M) - [SDR 98ZZZM617](https://openairdocs.org/sdr/98ZZZM617), Aug 14, 1998: BATTERY PACK. DISCHARGED. ON 'A' SERVICE, FOUND RIGHT OVEWING EMERENCY LIGHT INOPERATIVE. TROUBLESHOT SYTEM. FOUND RIGHT OVERWING BATTERY PACK LOW CHARGE. REPLACED BATTERY PACK. OPERATIO - [SDR 98ZZZM585](https://openairdocs.org/sdr/98ZZZM585), Aug 5, 1998: FIRE LOOP. MALFUNCTIONED. PASSING THROUGH FL190 ON TAKEOFF WHEEL WELL FIRE WARNING LIGHT ILLUMINATED. FOLLOWED COMPANY EMERGENCY CHECKLIST PROCEDURES. FIRE WARNING LIGHT EXTINGUISHED WIT - [SDR 98ZZZM586](https://openairdocs.org/sdr/98ZZZM586), Aug 2, 1998: FIRE LOOP. MALFUNCTIONED. PASSING THROUGH FL190 WHEEL WELL FIRE WARNING LIGHT ILLUMINATED. FOLLOWED COMPANY EMERGENCY CHECKLIST PROCEDURES. FIRE WARNING LIGHT EXTINGUISHED WITH GEAR EXTE - [SDR 98ZZZX2876](https://openairdocs.org/sdr/98ZZZX2876), Jul 18, 1998: LIGHT. INOPERATIVE. LOG PAGE: 24839: ON PRE-FLIGHT TRANSIT, FOUND ESCAPE PATH LIGHTING R2 DOOR NOT LIGHTING. TROUBLESHOT SYSTEM. REPAIRED WIRING. OPS CHECKED OK IAW 33-50-01. (X) - [SDR 98ZZZX2877](https://openairdocs.org/sdr/98ZZZX2877), Jul 16, 1998: CONTROL UNIT. MALFUNCTIONED. LOG PAGE: 24836 - DURING CRUISE, WHEEL WELL FIRE WARNING LIGHT AND BELL CAME ON. COMPLETED AOM PROCEDURES AND INDICATION DID NOT RETURN. THE NGU TROUBLESHOT SYS - [SDR MYWA970049](https://openairdocs.org/sdr/MYWA970049), Nov 16, 1997: BATTERY PACK. DISCHARGED. DURING PREFLIGHT TRANSIT CHECK, FOUND EMERGENCY EXIT LIGHT LOCATED IN THE MAIN CABIN CEILING ABOVE SEAT ROW NR 4 IS INOPERATIVE. INSTALLED BATTERY PACK. (M) - [SDR 96ZZZX3650](https://openairdocs.org/sdr/96ZZZX3650), Jun 12, 1996: STATIC FITTING. LOOSE. IAH - RETURN FROM FLIGHT - UPON CLIMB-OUT, FOUND CABIN PRESSURIZATION UNCONTROLLABLE IN AUTO AND STANDBY. SWITCHED MANUAL DC. CABIN RATE NOT CONTROLLABLE. SHUT - [SDR 96ZZZM1141](https://openairdocs.org/sdr/96ZZZM1141), Jun 12, 1996: FITTING. LOOSE. IAH - RETURN FROM FLIGHT, UPON CLIMB-OUT, FOUND CABIN PRESSURIZATION UNCONTROLLABLE IN AUTO AND STANDBY. SWITCHED TO MANUAL DC. CABIN RATE NOT CONTROLLABLE. SHU - [SDR 96ZZZM688](https://openairdocs.org/sdr/96ZZZM688), Mar 1, 1996: SLAT ACTUATOR. FAILED. RETURN FROM FLIGHT, AFTER TAKEOFF AT FLL, NR 1 LE SLAT WOULD NOT RETRACT. CYCLED FLAPS, NO HELP. RETURNED TO FLL. REPLACED THE NR 1 SLAT ACTUATOR IAW MM 27-81-3 ## Other aircraft with N808MA - [Registered now](https://openairdocs.org/aircraft/N808MA): Cessna 208B, S/N 208B2427, built 2013 - [Cancelled 2010-02-09](https://openairdocs.org/deregistered/N808MA-2010-02-09): Piper PA-34-220T, S/N 3449316, built 2005. Exported to Brazil. Owner: [North Atlantic Aircraft Services Corp](https://openairdocs.org/faa-owner/NORTH%20ATLANTIC%20AIRCRAFT%20SERVICES%20CORP), [Boca Raton, FL](https://openairdocs.org/faa-place/FL/Boca%20Raton) --- 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.