# N64319: 1969 Boeing 727-231, registration cancelled 2012-10-09

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: October 9, 2012
- Status when cancelled: Sale reported, pending cancellation
- Airframe: [Boeing 727-231](https://openairdocs.org/model/boeing-727-231) (registry code 1384079)
- Engine: [Pratt & Whitney JT8D-1](https://openairdocs.org/engine/pratt-whitney-jt8d-1) (registry code 52044)
- Data sheets: [TCDS A3WE](https://openairdocs.org/tcds/A3WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs)
- Serial number: 20052
- Year built: 1969
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: April 11, 1969
- Last registry action: April 13, 2001
- Mode S code: A872FD
- Location: [Xxx, OK](https://openairdocs.org/faa-place/OK/Xxx)
- Owner type: Individual
- The mark today: https://openairdocs.org/aircraft/N64319
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=64319
- Page: https://openairdocs.org/deregistered/N64319-2012-10-09

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 727-231: https://openairdocs.org/model/boeing-727-231.md

## Service difficulty reports (45)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR 2000ZZZX209](https://openairdocs.org/sdr/2000ZZZX209), Dec 20, 1999: FRAME. CORRODED. DURING A C-CHECK, CORROSION NOTED ON FRAME AT STA 228.5, BL ZERO.
- [SDR 98ZZZX4639](https://openairdocs.org/sdr/98ZZZX4639), Nov 12, 1998: FITTING. CORRODED. DURING A C-CHECK, CORROSION WAS NOTED ON NR 9 GROUND SPOILER MOUNT LUG.
- [SDR 98ZZZX4638](https://openairdocs.org/sdr/98ZZZX4638), Nov 12, 1998: FLOOR BEAM. CORRODED. DURING A C-CHECK, CORROSION NOTED ON FLOOR BEAM FS 1110 RBL 24 TO LBL 24.
- [SDR 98ZZZX4299](https://openairdocs.org/sdr/98ZZZX4299), Nov 5, 1998: FRAME. CORRODED. DURING A C-CHECK, CORROSION NOTED ON FRAME 950 ABOVE STR 23R.
- [SDR 98ZZZX4298](https://openairdocs.org/sdr/98ZZZX4298), Nov 5, 1998: STRINGER. CORRODED. DURING A C-CHECK, CORROSION NOTED ON STR 18L STA 620 - STA 640.
- [SDR 98ZZZX4297](https://openairdocs.org/sdr/98ZZZX4297), Nov 5, 1998: FLOOR BEAM. CORRODED. DURING A C-CHECK, CORROSION NOTED ON TOP OF FLOOR BEAM AT ST 1110, LBL 55.
- [SDR 98ZZZX4296](https://openairdocs.org/sdr/98ZZZX4296), Nov 5, 1998: SEAT TRACK. CORRODED. DURING A C-CHECK, CORROSION NOTED ON SEAT TRACK FS 1030 - FS 1130, LBL 45.
- [SDR 98ZZZX4295](https://openairdocs.org/sdr/98ZZZX4295), Nov 5, 1998: SKIN. CORRODED. DURING A C-CHECK, CORROSION NOTED ON RT WING NR 4 LE FLAP. PITTING AROUND BOLT HOLE.
- [SDR 98ZZZX4294](https://openairdocs.org/sdr/98ZZZX4294), Nov 5, 1998: SKIN. CORRODED. DURING A C-CHECK, CORROSION NOTED ON SKIN AT FS 720, STR 23R.
- [SDR 98ZZZX4293](https://openairdocs.org/sdr/98ZZZX4293), Nov 5, 1998: WEB. CORRODED. DURING A C-CHECK, CORROSION NOTED ON RIGHT WING WBL: 203, BOTTOM WEB REAR SPAR
- [SDR 98ZZZX4292](https://openairdocs.org/sdr/98ZZZX4292), Oct 30, 1998: SEAT TRACK. CORRODED. DURING A C-CHECK, CORROSION NOTED ON SEAT TRACK FS 420, LBL 24.
- [SDR 98ZZZX4291](https://openairdocs.org/sdr/98ZZZX4291), Oct 30, 1998: ANGLE. CORRODED. DURING A C-CHECK, CORROSION NOTED ON FORWARD END OF SEAT TRACK ON ANGLE FS 420 RBL 55.
- [SDR 98ZZZX4290](https://openairdocs.org/sdr/98ZZZX4290), Oct 30, 1998: FLOOR BEAM. CORRODED. DURING A C-CHECK, CORROSION NOTED ON FLOOR BEAM UPPER T-CHORD FS 344 LBL 24 - RBL 12.
- [SDR 98ZZZX4289](https://openairdocs.org/sdr/98ZZZX4289), Oct 30, 1998: SEAT TRACK. CORRODED. DURING A C-CHECK, CORROSION NOTED ON SEAT TRACK STA 420, RBL 24.
- [SDR 98ZZZX4288](https://openairdocs.org/sdr/98ZZZX4288), Oct 30, 1998: BRACKET. CORRODED. DURING A C-CHECK, CORROSION NOTED ON L-1 DOOR INTERIOR BOTTOM BRACKET FOR DOOR SLIDE.
- [SDR 98ZZZX4287](https://openairdocs.org/sdr/98ZZZX4287), Oct 30, 1998: FLOOR BEAM. CORRODED. DURING A C-CHECK, CORROSION NOTED ON FLOOR BEAM FS 400, RBL 3, APPROXIMATE.
- [SDR 98ZZZX4286](https://openairdocs.org/sdr/98ZZZX4286), Oct 30, 1998: SEAT TRACK. CORRODED. DURING A C-CHECK, CORROSION NOTED ON SEAT TRACK FS 1030 - FS 1130, LBL 24.
- [SDR 98ZZZX4285](https://openairdocs.org/sdr/98ZZZX4285), Oct 30, 1998: STRINGER. CORRODED. DURING A C-CHECK, CORROSION NOTED ON STR 23R STA 680 - STA 700.
- [SDR 98ZZZX4284](https://openairdocs.org/sdr/98ZZZX4284), Oct 30, 1998: SEAT TRACK. CORRODED. DURING A C-CHECK, CORROSION NOTED ON SEAT TRACK FS 1030 APPROXIMATELY LBL 55.
- [SDR 98ZZZX4283](https://openairdocs.org/sdr/98ZZZX4283), Oct 30, 1998: STEP. CORRODED. DURING A C-CHECK, CORROSION NOTED ON AFT AIR STAIRS (2ND STEP FROM TOP)
- [SDR 98ZZZX4282](https://openairdocs.org/sdr/98ZZZX4282), Oct 30, 1998: SEAT TRACK. CORRODED. DURING A C-CHECK, CORROSION NOTED ON SEAT TRACK FS 420 RBL 45.
- [SDR 98ZZZX4158](https://openairdocs.org/sdr/98ZZZX4158), Oct 28, 1998: SUPPORT. CORRODED. DURING C-CHECK, CORROSION NOTED ON FLOOR SUPPORT FS 1110 - FS 1130, LBL 12.
- [SDR 98ZZZX4157](https://openairdocs.org/sdr/98ZZZX4157), Oct 28, 1998: SUPPORT. CORRODED. DURING C-CHECK, CORROSION NOTED ON FLOOR SUPPORT FS 1070, LBL 45 - LBL 60.
- [SDR 98ZZZX4156](https://openairdocs.org/sdr/98ZZZX4156), Oct 28, 1998: FLOORBEAM. CORRODED. DURING C-CHECK, CORROSION WAS NOTED ON FLOORBOARD SUPPORT STA 1130 - STA 1148 - LBL 12.
- [SDR 98ZZZX4155](https://openairdocs.org/sdr/98ZZZX4155), Oct 28, 1998: SUPPORT. CORRODED. DURING C-CHECK, CORROSION WAS NOTED ON FLOORBEAM FS 420, RBL 12 - RBL 24.
- [SDR 98ZZZX4154](https://openairdocs.org/sdr/98ZZZX4154), Oct 28, 1998: SEAT TRACK. CORRODED. DURING C-CHECK, CORROSION NOTED ON CABIN FLOOR STRUCTURE, SEAT TRACK FS 1070 - FS 1130 LBL 55 (APPROXIMATE).
- [SDR 98ZZZX4153](https://openairdocs.org/sdr/98ZZZX4153), Oct 28, 1998: FRAME. CORRODED. DURING C-CHECK, CORROSION NOTED ON UPPER LOBE FRAME 1166 AT STR 17R.
- [SDR 99ZZZX2401](https://openairdocs.org/sdr/99ZZZX2401), Oct 27, 1998: BALLAST. FAILED. DURING C-CHECK, VISUAL INSPECTION OF UPPER LOBE, NOTED THAT BALLAST ABOVE AFT ENTRY DOOR BURNED. STA 1183 BETWEEN S1 AND S2R.
- [SDR 99ZZZX2351](https://openairdocs.org/sdr/99ZZZX2351), Oct 27, 1998: BALLAST. FAILED. DURING C-CHECK, VISUAL INSPECTION OF UPPER LOBE, NOTED THAT BALLAST ABOVE AFT ENTRY DOOR BURNED, STA 1183, BETWEEN S1 AND S2R.
- [SDR 98ZZZX4152](https://openairdocs.org/sdr/98ZZZX4152), Oct 26, 1998: HINGE. CORRODED. DURING C-CHECK, CORROSION WAS NOTED ON AFT LAVATORY SERVICE DOOR HINGE PAIRS (UPPER AND LOWER).
- [SDR 98ZZZX4151](https://openairdocs.org/sdr/98ZZZX4151), Oct 26, 1998: SKIN. CORRODED. DURING C-CHECK, CORROSION NOTED ON EXTERIOR FUSELAGE AFT LAVATORY SERVICE DOOR, INTERIOR SURFACE.
- [SDR 98ZZZX4150](https://openairdocs.org/sdr/98ZZZX4150), Oct 26, 1998: HINGE. CORRODED. DURING C-CHECK, CORROSION NOTED ON EXTERIOR AIRCRAFT GROUND ACCESS DOOR HINGES.
- [SDR 98ZZZX4149](https://openairdocs.org/sdr/98ZZZX4149), Oct 26, 1998: BRACKET. CORRODED. DURING C-CHECK, CORROSION NOTED ON BRACKET FOR PANEL NR 3346, STA 720C.
- [SDR TWAA9711702](https://openairdocs.org/sdr/TWAA9711702), Sep 30, 1997: RIB. CRACKED. MCI - REPAIRED CRACK AT NR 6 LEADING EDGE SLAT 1ST RIB OUTBOARD OF OUTBOARD TRACK AT LOWER END. (M)
- [SDR TWAA9711701](https://openairdocs.org/sdr/TWAA9711701), Sep 30, 1997: SKIN. CORRODED. MCI - CORROSION REMOVED AND AREA REPAIRED IN SKIN AROUND ANTENNA MOUNT PLATE RING INSIDE CARGO BIN RADIO ALTIMETER NR 1. (M)
- [SDR TWAA9799001](https://openairdocs.org/sdr/TWAA9799001), Aug 23, 1997: ACTUATOR. LEAKING. STL - FLT 228 - DURING CLIMB FOLLOWING GEAR RETRACTION THE 'A' SYSTEM HYDRAULIC QTY WENT TO ZERO. REMOVED AND REPLACED THE NR 6 LEADING EDGE FLAP ACTUATOR, MFG 
- [SDR 96ZZZX1198](https://openairdocs.org/sdr/96ZZZX1198), Feb 25, 1996: RELEASE ACTUATOR. FAILED. LGA - FLT 396 - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, NLG DID NOT EXTEND. CYCLED LANDING GEAR. FOUND NLG LOCK RELEASE ACTUATOR BYPASSING HYDRAULIC PRE
- [SDR 96ZZZX1195](https://openairdocs.org/sdr/96ZZZX1195), Feb 24, 1996: TRANSFER CYL. MALFUNCTIONED. LGA - FLT 460 - DURING APPROACH WHEN LANDING GEAR EXTENDED, NLG DID NOT EXTEND. CYCLED LANDING GEAR. FOUND NLG HYDRAULIC TRANSFER CYLINDER NOT OPERATING PROPERL
- [SDR 96ZZZX1197](https://openairdocs.org/sdr/96ZZZX1197), Feb 23, 1996: RETRACT MECH. LACK OF LUBE. LGA - FLT 300 - DURING APPROACH WHEN LANDING GEAR EXTENDED, NLG DID NOT EXTEND. CYCLED LANDING GEAR. LUBRICATED NLG TRUNNION, BEARINGS AND DRAG BRACE. NLG OPERA
- [SDR 96ZZZM193](https://openairdocs.org/sdr/96ZZZM193), Jan 5, 1996: RIB. CRACKED. MCI - DURING C-CHECK, FOUND A CRACK AT WS 629 RIB LOWER HOLE, STRINGER 2. STOP DRILLED PER SRM 57-10-5 AND REPAIRED PER SRM 57-10-5, FIGURE 2 AND TWA STANDARD P
- [SDR 96ZZZM192](https://openairdocs.org/sdr/96ZZZM192), Jan 5, 1996: CHORD. CRACKED. MCI - DURING C-CHECK, FOUND CRACK ON LOWER CHORD ATTACH BOLT HEAD FLANGE ABOVE EXCESS HOLE, RIGHT WING, W.5738.5. REPAIRED PER SRM 57-10-05, PAGE 3-5, AND TWA S
- [SDR 96ZZZM187](https://openairdocs.org/sdr/96ZZZM187), Dec 11, 1995: SKIN. CRACKED. MCI - DURING SPECIAL CHECK, FOUND 1.25 INCH CRACK IN FUSELAGE SKIN AT STRINGER 1, STRINGER BOX 1090, INSIDE CENTER ENGINE INLET HOUSING THROUGH BOTH SIDES OF RI
- [SDR 95ZZZX3413](https://openairdocs.org/sdr/95ZZZX3413), Jun 19, 1995: STRUCTURE. CRACKED. MCI - DURING AIRCRAFT SERVICE NR 4, FOUND A 1 INCH CRACK AT LBL 57, STA 940. REPAIRED BY INSTALLING DOUBLER PER ARA 9335. AIRCRAFT TOTAL TIME: 64,349 HOURS; 43,
- [SDR 95ZZZX3412](https://openairdocs.org/sdr/95ZZZX3412), Jun 19, 1995: STRUCTURE. CRACKED. MCI - DURING AIRCRAFT SERVICE NR 4, FOUND A .75 INCH CRACK AND A 1 INCH CRACK AT LBL 60, STA 948. REPAIRED BY INSTALLING DOUBLER PER ARA 9335. AIRCRAFT TOTAL TI
- [SDR 96ZZZM190](https://openairdocs.org/sdr/96ZZZM190), Jan 5, 1995: DOOR FRAME. CRACKED. MCI - DURING C-CHECK, FOUND A 1.5 INCH CRACK IN CABIN FORWARD DOOR FRAME RIGHT SIDE. REPAIRED PER SRM 51-40-3, FIGURE 1 AND TWA STANDARD PRACTICES. (M)

## 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 19920305007239I](https://openairdocs.org/incident/19920305007239I), Mar 5, 1992: Boeing 727231 (N64319), Kansas City, MO. Cabin pressurization problems at altitude. Diverted to Kansas City. Found right pack pressure regulator failure.
- [Incident 19900811058149I](https://openairdocs.org/incident/19900811058149I), Aug 11, 1990: Boeing 727231 (N64319), Boston, MA, Minor damage. Wing tip hit runway on landing. Damage found on post flight walk around. Pilot stated he had minor wind shear.
- [Incident 19890822049929I](https://openairdocs.org/incident/19890822049929I), Aug 22, 1989: Boeing 72731 (N64319), St Louis, MO. Left gear would not extend. Used manual extension. Landed safely. Had uplock actuator attach mount failure.
- [Incident 19890506021159I](https://openairdocs.org/incident/19890506021159I), May 6, 1989: Boeing 727231 (N64319), Indianapolis, IN. Rapid uncontrollable cabin pressure climb at FL310. Oxygen masks dropped. Emergency descent. Outflow valves changed

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