# N368PA: Boeing 727-221, registration cancelled 1997-12-05 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: December 5, 1997 - Exported to: Canada - Status when cancelled: Valid registration - Airframe: [Boeing 727-221](https://openairdocs.org/model/boeing-727-221) (registry code 1384071) - Data sheets: [TCDS A3WE](https://openairdocs.org/tcds/A3WE) (OpenAirDocs) - Serial number: 22540 - Type of aircraft: Fixed wing multi engine - Certificate issued: May 22, 1997 - Last registry action: May 22, 1997 - Mode S code: A42B4A - Owner when cancelled: [Prewitt Leasing Inc](https://openairdocs.org/faa-owner/PREWITT%20LEASING%20INC) - Location: [Bedford, TX](https://openairdocs.org/faa-place/TX/Bedford) - Owner type: Corporation - Owner's area on the map: 32.8530° N, 97.1304° W: Placed by OpenAirDocs at the center of ZIP code 76021, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N368PA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=368PA - Page: https://openairdocs.org/deregistered/N368PA-1997-12-05 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 Boeing 727-221: https://openairdocs.org/model/boeing-727-221.md ## Service difficulty reports (22) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR EISA97106](https://openairdocs.org/sdr/EISA97106), Jun 3, 1997: SWITCH. INOP. L/E FLAP NR 5 FAILED TO RETRACT AFTER TAKEOFF. REPLACED L/E NR 5 FLAP SWITCH PER MM 27-80. (M) - [SDR EISA97083](https://openairdocs.org/sdr/EISA97083), Apr 23, 1997: O-RING. DAMAGED. NR 3 ENGINE HAD OIL LOSS ON FINAL. INDICATIONS AT SHUT DOWN, QTY 0, PRESSURE IN YELLOW BAND AND YELLOW OIL LIGHT ILLUMINATED. REPLACED DAMAGED O-RING ON OIL RET - [SDR EISA96286](https://openairdocs.org/sdr/EISA96286), Dec 23, 1996: RELIEF VALVE. OUT OF ADJUST. DURING TAKEOFF, NR 2 OIL PRESSURE ROSE ABOVE RED LINE (APPROX 80 PSPSI). TROUBLESHOT ENGINE OIL PRESSURE RELIEF VALVE AND ADJUSTED PER MM, LEAK AND OPS CHECK GO - [SDR EISA96282](https://openairdocs.org/sdr/EISA96282), Dec 1, 1996: OUTFLOW VLV. INOPERATIVE. CABIN PRESSURE CONTROL SYSTEM MALFUNCTIONED IN CLIMB. FAILED IN STANDBY MODE TO FULL CABIN DESCENT, SWITCHED TO MANUAL DC FAILED OPS PER AOM VOL 1. REMOVED AND - [SDR EISA96196](https://openairdocs.org/sdr/EISA96196), Oct 22, 1996: FITTING. LOOSE. ENGINE NR 3 OIL QTY BEGAN RAPIDLY DROPPING ON APPROACH AND OIL TEMPERATURE ENTERED YELLOW BAND. ENGINE SHUTDOWN ACCOMPLISHED APPROXIMATELY 1/4 GALLON REMAINING - [SDR EISA95431](https://openairdocs.org/sdr/EISA95431), Nov 20, 1995: CHANNEL. DENTED. AFT CARGO LOWER BILGE HAT CHANNEL DENTED, AT STATION 967 ABOVE AND BETWEEN STRINGER 30 AND 29L. REMOVED HAT CHANNEL AND DENT, FABRICATED REPAIR PER SRM 51-40-1 - [SDR EISA95437](https://openairdocs.org/sdr/EISA95437), Nov 18, 1995: STRINGER. CRACKED. STATION 990, STRINGER 29R HAS CORROSION ON OUTBOARD FLANGE. REMOVED CORROSION AND FOUND 2 INCH CRACK. STOP DRILLED CRACK PER SRM 51-10-1. HFEC CONFIRMS CRACK CO - [SDR EISA95436](https://openairdocs.org/sdr/EISA95436), Nov 18, 1995: RIB. CRACKED. INSIDE VERTICAL STAB THROUGH ACCESS PANEL 9504, FOURTH COMPARTMENT UP FROM ENTRANCE, THE EIGHTH RIB FROM THE TOP IS CRACKED. REPAIRED CRACK IN RIB PER SRM 55-30 - [SDR EISA95435](https://openairdocs.org/sdr/EISA95435), Nov 18, 1995: TIE CLIP. CRACKED. DITCHING PAN CLIP CRACKED, STATION 1183, BL 37 LEFT. REMOVED TIE CLIP AND FABRICATED PER SRM 51-30-2. TREATED, PRIMED AND INSTALLED PER SRM 51-10-2 AND 51-10-5. - [SDR EISA95434](https://openairdocs.org/sdr/EISA95434), Nov 18, 1995: CHANNEL. CRACK. CORROSION AT HAT CHANNEL UNDER RIGHT LAV DOOR WAY, APPROXIMATELY STATION 303-320. CORRODED HAT CHANNEL, FABRICATED NEW SECTION, INSTALLED PER SRM 51-30-2. (M) - [SDR EISA95433](https://openairdocs.org/sdr/EISA95433), Nov 18, 1995: SKIN. CRACKED. VERTICAL STABILIZER RIGHT SIDE, JUST BELOW NR 7 VORTEX GENERATOR FROM TOP, SKIN CRACKED AT RIVET HEAD. STOP DRILLED CRACK PER SRM 55-30-3. HFEC CONFIRMED CRACK - [SDR EISA95432](https://openairdocs.org/sdr/EISA95432), Nov 18, 1995: FLANGE. CORRODED. FOUND CORROSION, AT STRINGER 950D LOWER FLANGE. REMOVED FLANGE PER SRM 51-10-1, FABRICATED NEW FLANGE AND INSTALLED PER SRM 51-10-6 AND 51-10-2. (M) - [SDR EISA95430](https://openairdocs.org/sdr/EISA95430), Nov 18, 1995: ANGLE. CORRODED. PRESSURE BULKHEAD STATION 1183, FORWARD SIDE RBL HORIZONTAL ANGLE AND TIE CLIP CORRODED. INSTALLED ALL PARTS, REMOVED AND FABRICATED PER SRM 51-81-1. (M) - [SDR EISA95429](https://openairdocs.org/sdr/EISA95429), Nov 18, 1995: TIE CLIP. CRACKED. DITCHING PAN TIE CLIP CRACKED STATION 1183, RBL 47. FABRICATED NEW TIE CLIP AND INSTALLED PER SRM 51-40. (M) - [SDR EISA95428](https://openairdocs.org/sdr/EISA95428), Nov 18, 1995: TIE CLIP. CRACKED. DITCHING PAN TIE CLIP CRACKED STATION 1183, RBL 37. REMOVED CLIP, FABRICATED NEW CLIP PER SRM 51-30-2, INSTALLED CLIP PER SRM 51-10-1. (M) - [SDR EISA95427](https://openairdocs.org/sdr/EISA95427), Nov 18, 1995: TIE CLIP. CRACKED. DITCHING PAN TIE CLIP CRACKED AT STATION 1183, BL 27L. FABRICATED NEW TIE CLIP PER SRM 51-30-2. INSTALLED NEW TIE CLIP PER SRM 51-30-2. (M) - [SDR EISA95426](https://openairdocs.org/sdr/EISA95426), Nov 18, 1995: DOUBLER. DAMAGED. REPAIR DAMAGED ELONGATED HOLE, STATION 600, TOP OF FORWARD CARGO DOOR CUT OUT. REMOVED DAMAGED DOUBLER IAW SRM 51-10-1, FABRICATED NEW DOUBLER 51-10-1, TREATED - [SDR EISA95425](https://openairdocs.org/sdr/EISA95425), Nov 18, 1995: SKIN. DAMAGED. REPAIR BENT DAMAGED STATION 580 TOP OF FWD CARGO DOOR CUT OUT. REMOVED DAMAGED DOUBLER IAW SRM 51-10-1, FABRICATED NEW DOUBLER IAW 51-10-1. TREATED PRIMED AND I - [SDR EISA95424](https://openairdocs.org/sdr/EISA95424), Nov 18, 1995: PANEL. CORROSION. RT WING PANEL AT NR 7 SLAT ACTUATOR HAS EXFOLIATING CORROSION. REMOVED RIGHT WING PANEL, NR 7 SLAT FROM AIRCRAFT FABRICATED NEW HORSESHOE BRACKET AND FACE PANEL - [SDR EISA95439](https://openairdocs.org/sdr/EISA95439), Nov 16, 1995: LE RIB. CORRODED. CORROSION AT RIB AND STIFFENER INSIDE LEFT WING LE AFT OF NR 2 LE FLAP AND 14 INCHES OUTBOARD OF ACTUATOR. FABRICATED REPAIR PARTS PER SRM 51-40-4. INSTALLED PE - [SDR EISA95438](https://openairdocs.org/sdr/EISA95438), Nov 16, 1995: RIB. CRACKED. CRACK INDICATION, FORWARD 2 FASTENER HOLES, BS 760 LBL 70.5 RIB CHORD VERTICAL FLANGE. REMOVED ANGLE AND SUPPORT. REMOVED FASTENERS FOR NDT, ACCOMPLISHED HFEC T - [SDR EISA95290](https://openairdocs.org/sdr/EISA95290), Oct 7, 1995: FUEL CONTROL. FAILED. NR 3 ENGINE QUIT AT 800 FEET AFTER TAKEOFF, NO WARNING, SHUTTERED AND QUIT. REMOVED AND REPLACED NR 3 ENGINE FUEL CONTROL IAW 73-21-1. OPS AND LEAK CHECK GOOD I ## FAA accident and incident reports (1) 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 19821102065849I](https://openairdocs.org/incident/19821102065849I), Nov 2, 1982: Boeing 727 (N368PA), Houston, TX. Right main gear exited taxiway. Maintenance inspected gear. Used engine power to return to taxiway. Flight resumed. ## Other aircraft with N368PA - [Registered now](https://openairdocs.org/aircraft/N368PA): Mcdonnell Douglas Helicopter MD 900, S/N 900-00012, built 1994 --- 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.