# N267US: 1969 Boeing 727-251, registration cancelled 2003-11-03 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: November 3, 2003 - Exported to: Swaziland - Status when cancelled: Valid registration - Airframe: [Boeing 727-251](https://openairdocs.org/model/boeing-727-251) (registry code 138408H) - Engine: [Pratt & Whitney JT8D-5](https://openairdocs.org/engine/pratt-whitney-jt8d-5) (registry code 52046) - Data sheets: [TCDS A3WE](https://openairdocs.org/tcds/A3WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs) - Serial number: 20289 - Year built: 1969 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: August 11, 1969 - Certificate issued: January 27, 1989 - Last registry action: November 5, 2002 - Mode S code: A29AD1 - 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/N267US - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=267US - Page: https://openairdocs.org/deregistered/N267US-2003-11-03 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 727-251: https://openairdocs.org/model/boeing-727-251.md ## Service difficulty reports (53, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR S84A005](https://openairdocs.org/sdr/S84A005), Jan 13, 2000: POWER SUPPLY. INOPERATIVE. LEFT FORWARD O-RING EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY. OPS OK PER MM 33-50-00. (M) - [SDR S84A2000004](https://openairdocs.org/sdr/S84A2000004), Jan 12, 2000: POWER SUPPLY. INOPERATIVE. RIGHT AFT 'O' WING EMERGENCY EXIT LIGHT INOPERABLE. RELAMPED RT AFT 'O' WING EMERGENCY EXIT LIGHT. OPS CHECKED OK. ALSO, REMOVED AND REPLACED POWER SUPPLY, P/N - [SDR S84A2000003](https://openairdocs.org/sdr/S84A2000003), Jan 12, 2000: LIGHT. INOPERATIVE. RIGHT AFT 'O' WING EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED RIGHT AFT 'O' WING EMERGENCY EXIT LIGHT. OPS CHECKED OK. (X) - [SDR S84A2000002](https://openairdocs.org/sdr/S84A2000002), Jan 12, 2000: LIGHT. INOPERATIVE. RELAMPED LEFT FORWARD OVERWING EMERGENCY EXIT LIGHT. OPS CHECKED OK. (X) - [SDR S84A9900004](https://openairdocs.org/sdr/S84A9900004), Dec 3, 1999: BATTERY PACK. DISCHARGED. RIGHT AFT EMERGENCY EXIT LIGHT OUT (EXTERIOR). (X) - [SDR S84A990006](https://openairdocs.org/sdr/S84A990006), Dec 2, 1999: BULB. FAILED. FORWARD EXTERIOR REAR EXIT LIGHT OUT (LEFT SIDE). RELAMPED. OPS CHECKED OK. (X) - [SDR S84A98](https://openairdocs.org/sdr/S84A98), Sep 12, 1999: BULB. LOOSE. EWR - DURING A-CHECK, FOUND AFT ENTRY DOOR EMERGENCY LIGHT BULB OUT. FOUND LIGHT BULB LOOSE. RE-INSTALLED. (X) - [SDR S84A97](https://openairdocs.org/sdr/S84A97), Sep 12, 1999: BATTERY. DISCHARGED. EWR - DURING A-CHECK, FOUND AIRSTAIR EMERGENCY LIGHT OUT. CHARGED BATTERIES. OPS CHECK OK. (X) - [SDR S84A96](https://openairdocs.org/sdr/S84A96), Sep 12, 1999: BATTERY. DISCHARGED. EWR - DURING A-CHECK, FOUND RIGHT AFT (CARGO DOOR) EMERGENCY LIGHT OUT. CHARGED BATTERIES. OPS CHECK OK. (X) - [SDR S84A95](https://openairdocs.org/sdr/S84A95), Sep 12, 1999: BATTERY. DISCHARGED. EWR - DURING A-CHECK, FOUND LEFT AFT (OPPOSITE CARGO DOOR) EMERGENCY LIGHT OUT. CHARGED BATTERIES, OPS CHECK OK. (X) - [SDR S84A94](https://openairdocs.org/sdr/S84A94), Sep 12, 1999: CONNECTOR. LOOSE. EWR - DURING A-CHECK, FOUND AFT FLIGHT ATTENDANT STATION EMERGENCY LIGHT SWITCH DID NOT TURN ON LIGHTS. TIGHTENED LOOSE CONNECTION ON SWITCH. (X) - [SDR 99ZZZX3644](https://openairdocs.org/sdr/99ZZZX3644), Aug 18, 1999: LIGHT. INOPERABLE. EMERGENCY LIGHT IN AFT AIRSTAIR AREA INOPERABLE. REMOVED AND REPLACED LIGHT ASSY IAW 33-50-0. M14/M25. - [SDR 99ZZZX3643](https://openairdocs.org/sdr/99ZZZX3643), Aug 18, 1999: LIGHT. INOPERABLE. EMERGENCY LIGHT IN AFT AIRSTAIR AREA INOPERABLE. REMOVED AND REPLACED LIGHT ASSY IAW 33-50-0. M14/M25. - [SDR 99ZZZX3637](https://openairdocs.org/sdr/99ZZZX3637), Aug 18, 1999: BATTERY CHARGER. FAILED. LEFT AFT OVERWING EMERGENCY LIGHT INOPERABLE. REMOVED AND REPLACED BATTERY CHARGER IAW 33-50-22. - [SDR 99ZZZX3636](https://openairdocs.org/sdr/99ZZZX3636), Aug 18, 1999: BATTERY CHARGER. FAILED. LEFT FORWARD OVERWING EMERGENCY LIGHT INOPERABLE. REMOVED AND REPLACED BATTERY CHARGER IAW 33-50-22. - [SDR 99ZZZX3635](https://openairdocs.org/sdr/99ZZZX3635), Aug 18, 1999: BATTERY PACK. DISCHARGED. RIGHT WING FORWARD EMERGENCY LIGHT INOPERABLE. REMOVED AND REPLACED BATTERY PACK IAW 33-50-22. - [SDR 99ZZZM346](https://openairdocs.org/sdr/99ZZZM346), Apr 17, 1999: FUEL PUMP. FAILED. ON SIX MILE FINAL, NR 2 ENGINE FLAMED OUT. FOUND NR 2 ENGINE FUEL PUMP SHAFT SHEARED. REMOVED AND REPLACED NR 2 ENGINE FUEL PUMP PER MM 73-11-1. PERFORMED ENGIN - [SDR S84A9900005](https://openairdocs.org/sdr/S84A9900005), Jan 2, 1999: BULB. FAILED. R1 DOOR EMERGENCY EXIT LIGHT INOPERABLE (OVER DOOR). RELAMPED. OPS CHECKED GOOD. (X) - [SDR 97ZZZX4368](https://openairdocs.org/sdr/97ZZZX4368), Sep 29, 1997: LIGHT. INOPERATIVE. AFT EXIT EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY. - [SDR 97ZZZX3845](https://openairdocs.org/sdr/97ZZZX3845), Aug 10, 1997: DOWNLOCK SWITCH. INTERMITTENT. UPON DESCENT INTO MIA WHEN LANDING GEAR LEVER PLACED IN DOWN POSITION, NOSE GEAR INDICATED UNSAFE. CREW PERFORMED THE A.F.M. ABNORMAL PROCEDURES AND VERIFIED TH - [SDR 97ZZZX1523](https://openairdocs.org/sdr/97ZZZX1523), Oct 9, 1996: WEB. CORRODED. DURING C-CHECK INSPECTION, CORROSION WAS NOTED ON RT SIDE NOSE WHEELWELL BOX EXTENDING FROM STA 243 TO STA 259. - [SDR 97ZZZX1522](https://openairdocs.org/sdr/97ZZZX1522), Oct 9, 1996: STRINGER. CORRODED. DURING C-CHECK INSPECTION, CORROSION WAS NOTED ON STRINGER S29L EXTENDING FROM STA 360 TO STA 380. - [SDR 97ZZZX1521](https://openairdocs.org/sdr/97ZZZX1521), Oct 9, 1996: STRINGER. CORRODED. DURING C-CHECK INSPECTION, CORROSION WAS NOTED ON STRINGER S18L EXTENDING FROM STA 360 TO STA 380. - [SDR 97ZZZX1520](https://openairdocs.org/sdr/97ZZZX1520), Oct 9, 1996: STRINGER. CORRODED. DURING C-CHECK INSPECTION, CORROSION WAS NOTED ON STRINGER S21L EXTENDING FROM STA 380 TO STA 400. - [SDR 97ZZZX1519](https://openairdocs.org/sdr/97ZZZX1519), Oct 9, 1996: STRINGER. CORRODED. DURING C-CHECK INSPECTION, CORROSION WAS NOTED ON STRINGER S24L AFT OF STA 360. - [SDR 97ZZZX1518](https://openairdocs.org/sdr/97ZZZX1518), Oct 9, 1996: STRINGER. CORRODED. DURING C-CHECK INSPECTION, CORROSION WAS NOTED ON STRINGER S26R EXTENDING FROM STA 360 TO STA 380. - [SDR 97ZZZX1517](https://openairdocs.org/sdr/97ZZZX1517), Oct 9, 1996: STRINGER. CORRODED. DURING C-CHECK INSPECTION, CORROSION WAS NOTED ON STRINGER S25L FROM STA 277 TO STA 294. - [SDR 97ZZZX1516](https://openairdocs.org/sdr/97ZZZX1516), Oct 9, 1996: STRINGER. CORRODED. DURING C-CHECK INSPECTION, CORROSION WAS NOTED ON STRINGER S25L JUST FORWARD OF STA 360. - [SDR 97ZZZX1515](https://openairdocs.org/sdr/97ZZZX1515), Oct 9, 1996: STRINGER. CORRODED. DURING C-CHECK INSPECTION, CORROSION WAS NOTED ON STRINGER S24R EXTENDING FROM STA 400 TO STA 440. - [SDR 97ZZZX1514](https://openairdocs.org/sdr/97ZZZX1514), Oct 9, 1996: STRINGER. CORRODED. DURING C-CHECK INSPECTION, CORROSION WAS NOTED ON STRINGER S25R EXTENDING FROM STA 400 TO STA 440. - [SDR 97ZZZX1513](https://openairdocs.org/sdr/97ZZZX1513), Oct 9, 1996: STRINGER. CORRODED. DURING C-CHECK INSPECTION, CORROSION WAS NOTED ON STRINGER S27R EXTENDING FROM STA 420 TO STA 480. - [SDR 97ZZZX1512](https://openairdocs.org/sdr/97ZZZX1512), Oct 9, 1996: FRAME. CORRODED. DURING C-CHECK INSPECTION, CORROSION WAS NOTED ON TOP CHORD OF FRAME STA 360 APPROXIMATE RBL 10. - [SDR 97ZZZX1511](https://openairdocs.org/sdr/97ZZZX1511), Oct 9, 1996: STRINGER. CORRODED. DURING C-CHECK INSPECTION, CORROSION WAS NOTED ON STRINGER S28R EXTENDING FROM STA 460 TO STA 480. - [SDR 97ZZZX1510](https://openairdocs.org/sdr/97ZZZX1510), Oct 9, 1996: STRINGER. CORRODED. DURING C-CHECK INSPECTION, CORROSION WAS NOTED ON STRINGER S20R EXTENDING FROM STA 360 TO STA 380. - [SDR 97ZZZX1509](https://openairdocs.org/sdr/97ZZZX1509), Oct 9, 1996: STRINGER. CORRODED. DURING C-CHECK INSPECTION, CORROSION WAS NOTED ON STRINGER S18R EXTENDING FROM STA 312 TO STA 328. - [SDR 97ZZZX1508](https://openairdocs.org/sdr/97ZZZX1508), Oct 9, 1996: GEARBOX. CORRODED. DURING C-CHECK INSPECTION, CORROSION WAS NOTED ON LOWER NOSE LANDING GEAR BOX CHORD FROM STA 320 TO STA 328. - [SDR 97ZZZX1507](https://openairdocs.org/sdr/97ZZZX1507), Oct 9, 1996: STRINGER. CORRODED. DURING C-CHECK INSPECTION, CORROSION WAS NOTED ON STRINGER S19R EXTENDING FROM STA 312 TO STA 344. - [SDR 97ZZZX1506](https://openairdocs.org/sdr/97ZZZX1506), Oct 9, 1996: STRINGER. CORRODED. DURING C-CHECK INSPECTION, CORROSION WAS NOTED ON STRINGER S23R EXTENDING FROM STA 360 - STA 440. - [SDR 97ZZZX1505](https://openairdocs.org/sdr/97ZZZX1505), Oct 9, 1996: STRINGER. CORRODED. DURING C-CHECK INSPECTION, CORROSION WAS NOTED ON STRINGER S21R EXTENDING FROM STA 380 - STA 440. - [SDR 97ZZZX1504](https://openairdocs.org/sdr/97ZZZX1504), Oct 9, 1996: FRAME. CRACKED. DURING C-CHECK INSPECTION, A CRACK WAS NOTED IN FRAME 420 AT S21R. - [SDR 97ZZZX1503](https://openairdocs.org/sdr/97ZZZX1503), Oct 9, 1996: STRINGER. CORRODED. DURING C-CHECK INSPECTION, CORROSION WASNOTED ON STRINGER S22R EXTENDING FROM STA 380 TO STA 440. - [SDR 97ZZZX1502](https://openairdocs.org/sdr/97ZZZX1502), Oct 9, 1996: STRINGER. CORRODED. DURING C-CHECK INSPECTION, CORROSION WAS NOTED ON STRINGER S22L FORWARD OF STA 312 - [SDR 97ZZZX1501](https://openairdocs.org/sdr/97ZZZX1501), Oct 9, 1996: STRINGER. CORRODED. DURING C-CHECK INSPECTION, CORROSION WAS NOTED ON STRINGER S20L FORWARD OF STA 312. - [SDR 97ZZZX1500](https://openairdocs.org/sdr/97ZZZX1500), Oct 9, 1996: STRINGER. CORRODED. DURING C-CHECK INSPECTION, CORROSION WAS NOTED ON STRINGER S21L EXTENDING FROM STA 312 - STA 344. - [SDR 97ZZZX1499](https://openairdocs.org/sdr/97ZZZX1499), Oct 9, 1996: BULKHEAD. CORRODED. DURING C-CHECK INSPECTION, INTERGRANULAR CORROSION WAS NOTED ON LOWER CHORD OF BULKHEAD STA 351 BETWEEN S21L EXTENDING TO S26L. - [SDR 97ZZZX1498](https://openairdocs.org/sdr/97ZZZX1498), Oct 9, 1996: SKIN. CORRODED. DURING C-CHECK INSPECTION, BROKEN FASTENERS AND CORROSION WAS NOTED UNDER SKIN PANEL BELOW LT AFT LAV SERVICE COMPARTMENT, STA 1166, S22L. - [SDR 97ZZZX1497](https://openairdocs.org/sdr/97ZZZX1497), Oct 9, 1996: SKIN. CORRODED. DURING C-CHECK INSPECTION, CORROSION WAS NOTED ON SKIN RT FORWARD FUSELAGE AT STA 440 EXTENDING FROM S18R TO S21R. - [SDR 97ZZZX1496](https://openairdocs.org/sdr/97ZZZX1496), Oct 9, 1996: SKIN. CORRODED. DURING C-CHECK INSPECTION, CORROSION WAS NOTED ON SKIN, RT FORWARD FUSELAGE STA 294 TO STA 360, EXTENDING UNDER LAP S19R. - [SDR IXKA9600074](https://openairdocs.org/sdr/IXKA9600074), Sep 2, 1996: CONTROLLER. FAILED. FLT 73 - ATL-MCO - PRESSURIZATION WAS ERRATIC, SWITCHED TO MANUAL, UNABLE TO CONTROL. RETURNED TO ATL. REMOVED AND REPLACED AND REPLACED MANUAL CONTROLLER, PERF - [SDR IXKA960033](https://openairdocs.org/sdr/IXKA960033), May 15, 1996: POWER PACK. INOPERATIVE. ON POST FLIGHT INSPECTION, FOUND L1 DOOR PORTABLE EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED INOP BATTERY POWER PACK. OPS CHECK OK. (M) All 53: https://openairdocs.org/deregistered/N267US-2003-11-03/reports.md ## 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 19980316036529I](https://openairdocs.org/incident/19980316036529I), Mar 16, 1998: Boeing 727251 (N267US), Miami, FL. (-5) On flight from montego bay, jamaica, to newark, new jersey, N267US, a Boeing 727, lost cabin pressure. The crew declared an emergency, descended to a… --- 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.