# N7465U: 1980 Boeing 727-222, registration cancelled 2007-09-12

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: September 12, 2007
- Status when cancelled: Triennial form not returned
- Airframe: [Boeing 727-222](https://openairdocs.org/model/boeing-727-222) (registry code 1384073)
- Engine: [Pratt & Whitney JT8D-15](https://openairdocs.org/engine/pratt-whitney-jt8d-15) (registry code 52051)
- Data sheets: [TCDS A3WE](https://openairdocs.org/tcds/A3WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs)
- Serial number: 21919
- Year built: 1980
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 27, 1980
- Certificate issued: July 29, 2004
- Last registry action: July 17, 2007
- Mode S code: AA0BEE
- Owner when cancelled: [Pacific Aviation Group LLC](https://openairdocs.org/faa-owner/PACIFIC%20AVIATION%20GROUP%20LLC)
- Location: [Victorville, CA](https://openairdocs.org/faa-place/CA/Victorville)
- Owner type: Corporation
- Owner's area on the map: 34.5670° N, 117.3629° W: Placed by OpenAirDocs at the center of ZIP code 92394, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N7465U
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=7465U
- Page: https://openairdocs.org/deregistered/N7465U-2007-09-12

From the FAA registry file of October 31, 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 727-222: https://openairdocs.org/model/boeing-727-222.md

## Service difficulty reports (12)

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

- [SDR 2001UALA00959](https://openairdocs.org/sdr/2001UALA00959), Jun 7, 2001: SENSOR. BROKEN. UNABLE TO MOVE GEAR HANDLE PAST OFF POSITION. SUPPLEMENTAL DATA UPDATE FOUND BROKEN WIRE AT AIR SAFETY SENSOR. REPLACED AIR SAFETY SENSOR. OPERATION CHECK NORMA
- [SDR 2001UALA00629](https://openairdocs.org/sdr/2001UALA00629), Apr 27, 2001: PUMP. FAILED. AIRCRAFT RETURNED TO DEN DUE TO LOSS OF THE SECOND FUEL BOOST PUMP IN THE CENTER TANK. BOOST PUMP FAILED. REPLACED THE BOOST PUMP.
- [SDR 2001UALA00263](https://openairdocs.org/sdr/2001UALA00263), Mar 9, 2001: RIB. CRACKED. NR 6 SLAT ACTUATOR MOUNT RIBS CRACKED ON BOTH INBOARD AND OUTBOARD SIDES.
- [SDR 2001UALA00258](https://openairdocs.org/sdr/2001UALA00258), Mar 9, 2001: FITTING. CRACKED. RT WHEEL WELL AT STA 870 REPAIR FITTING CRACKED UNDER TRAPEZOID FITTING. REPLACED CRACKED WEB PER BAC DWG 65-25370 AND INSTALLED PER SRM 51-30-02.
- [SDR 2000UALA00426](https://openairdocs.org/sdr/2000UALA00426), Jul 13, 2000: CSD. FAILED. AFTER TAKEOFF, NR 3 GENERATOR FREQUENCY WENT TO 420 AND BUS 1 AND 2 TRIPPED WITH OVEREXCITE INDICATION. DECLARED AMBER ALERT AND RETURNED TO TUL. *S/D* REPLACED
- [SDR 2000UALA00174](https://openairdocs.org/sdr/2000UALA00174), Apr 6, 2000: BATTERY. INOPERATIVE. EXIT SIGN ABOVE AIRSTAIR DOOR DOES NOT COME ON WHEN EMERGENCY SWITCH IS ON. *S/D* REPLACED CHARGER AND BATTERY.
- [SDR 2000UALA00108](https://openairdocs.org/sdr/2000UALA00108), Mar 4, 2000: VALVE. MALFUNCTIONED. UNABLE TO CONTROL CABIN ALTITUDE AT 24,000 FT. MANUAL OR STANDBY NO HELP. OUTFLOW VALVE INDICATED CLOSED. DESCENDED TO I0,000 AND REGAINED MANUAL CONTROL. RETUR
- [SDR 99UAL900123](https://openairdocs.org/sdr/99UAL900123), Feb 22, 1999: BALLAST. FAILED. STRONG ELECTRICAL SMELL FROM THE FORWARD LAVATORY. CREW ISOLATED THE SMELL TO A PANEL WHERE THE LIGHT SWITCH IS LOCATED. CIRCUIT BREAKERS PULLED. SMELL DID NOT 
- [SDR 99UAL900077](https://openairdocs.org/sdr/99UAL900077), Feb 3, 1999: TRANSFORMER. FAILED. ALL NAVIGATION LIGHTS ARE INOPERATIVE. AIRPLANE RESTRICTED TO DAYLIGHT OPERATION ONLY. *S/D* REPLACED TRANSFORMER T16.
- [SDR 97UAL900777](https://openairdocs.org/sdr/97UAL900777), Oct 16, 1997: BATTERY. CORRODED. CENTER CABIN CEILING EMERGENCY LIGHT INOPERABLE. CLEANED BATTERY CONTACTS AND REPLACED MISSING HARDWARE ON CEILING EMERGENCY LIGHT AT ROW 10, CHECKS OK.
- [SDR 96UAL900127](https://openairdocs.org/sdr/96UAL900127), Feb 19, 1996: RIB. CRACKED. RIGHT ELEVATOR LOWER SURFACE INBD END HAD POPPED AND HAD LOOSE RIVETS. AFTER REMOVAL OF ACCESS PANEL FOUND STIFFENER RIB CRACKED. MANUFACTURED AND INSTALLED NEW
- [SDR 96UAL900010](https://openairdocs.org/sdr/96UAL900010), Jan 5, 1996: LIGHT WIRES. DAMAGED. LEFT WING TRAILING EDGE WHITE LIGHT INOPERATIVE. POWER AND GROUND WIRES FOUND BURNT IN VICINITY OF LIGHT. REPLACED WIRES. CAUSE UNDETERMINED, POSSIBLE LIGHTNING

---
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.