# N421AV: Boeing 767-200ER, registration cancelled 2011-09-14

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: September 14, 2011
- Status when cancelled: Valid registration
- Airframe: [Boeing 767-200ER](https://openairdocs.org/model/boeing-767-200er) (registry code 1385160)
- Engine: [Pratt & Whitney PW4000 series](https://openairdocs.org/engine/pratt-whitney-pw4000-series) (registry code 52119)
- Serial number: 25421
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 22, 1999
- Certificate issued: June 21, 1999
- Last registry action: August 9, 2000
- Mode S code: A4FF6A
- Owner when cancelled: [Aerousa Inc](https://openairdocs.org/faa-owner/AEROUSA%20INC)
- Location: [Fort Lauderdale, FL](https://openairdocs.org/faa-place/FL/Fort%20Lauderdale)
- Owner type: Corporation
- Owner's area on the map: 26.1213° N, 80.1279° W: Placed by OpenAirDocs at the center of ZIP code 33301, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N421AV
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=421AV
- Page: https://openairdocs.org/deregistered/N421AV-2011-09-14

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 767-200ER: https://openairdocs.org/model/boeing-767-200er.md

## Service difficulty reports (8)

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

- [SDR MU1Z2011020200002](https://openairdocs.org/sdr/MU1Z2011020200002), Feb 22, 2011: ANGLE. CRACKED. DURING HFEC INSPECTION CLOSE OUT ANGLE OF THE RT PYLON WAS FOUND CRACKED.
- [SDR ANCF2010100900068](https://openairdocs.org/sdr/ANCF2010100900068), Oct 9, 2010: ENGINE. LEAKING. RIGHT PACK INOP LIGHT ILLUMINATED EICAS MESSAGE RT PACK TEMP DISPLAYED. LIGHT DID NOT EXTINGUISH WHEN STBY SELECTED. RESET PUSHED, LIGHT EXTINGUISHED THEN RE-IL
- [SDR ANCF2009051500043](https://openairdocs.org/sdr/ANCF2009051500043), May 15, 2009: MODULE. FAULTY. AFTER LIFT OFF FIRE AURAL WARNING SOUND CONTINUOSLY WITHOUT ANY INDICATION UNTIL ON GROUND, C/B H35 WAS PULLED IAW FIM 31-51-00 FIG 103 BLOCKS 1 TO 6 AND 50 AND
- [SDR 2008FA0000466](https://openairdocs.org/sdr/2008FA0000466), Jul 11, 2008: COMPUTER. FAILED. AIR TURNBACK DUE PILOT REPORT 4273256-1; EICAS MSG L FMC FAIL DISPLAYED. FIM 34-61-00 FOLLOWED L FMC PWR RESET ALL INDICATIONS NORMAL. PLS MONITOR FURTHER. AS A
- [SDR ANCF200400051](https://openairdocs.org/sdr/ANCF200400051), Jun 5, 2005: HEATER. DEFECTIVE. ELECTRICAL SMOKE OF UNKNOW ORIGIN FROM THE CAPTAIN'S SIDE, BETWEEN THE LIGHT CONTROL PANEL AND THE GLARESHIELD PANEL, ACCORDING TO THE ABNORMAL CHECKLIST THE RE
- [SDR ANCF200300027](https://openairdocs.org/sdr/ANCF200300027), Dec 9, 2003: APU. LEAKING. SMOKE ODOR THROUGH THE PASSENGER CABIN WITH NO SMOKE EVIDENCE. SMOKE DETECTORS ACTIVATED ON THE AFT AND FORWARD LAVATORIES. UTILITY BUSES WERE TURNED OFF WITH N
- [SDR ANCF200200015](https://openairdocs.org/sdr/ANCF200200015), Jul 29, 2002: COUPLING. DAMAGED. TRANSMISSION ON BOTH HF INOPERATIVE AT ALL STATIONS.CORRECTIVE ACTION:PERFORMED FIM 23-11-00 OPERATION FOUND NORMAL ON LH HF, ON RH SYSTEM WAS REPLACED HF COUPL
- [SDR ANCF200000002](https://openairdocs.org/sdr/ANCF200000002), Nov 9, 2000: CONTROLLER. MALFUNCTIONED. DURING CRUISE, LT ENGINE BLEED OFF DISPLAYED AND ENGINE BLEED AIR VALVE OFF LIGHT ILLUMINATED, WITH SWITCH ON. DUCT PRESS WAS ZERO PSI, NACELLE ANTI-ICE OPERATI

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