# N767UA: Boeing 777-222, registration cancelled 2011-12-19 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: December 19, 2011 - Exported to: Ireland - Status when cancelled: Valid registration - Airframe: [Boeing 777-222](https://openairdocs.org/model/boeing-777-222) (registry code 1385219) - Data sheets: [TCDS T00001SE](https://openairdocs.org/tcds/T00001SE) (OpenAirDocs) - Serial number: 26918 - Type of aircraft: Fixed wing multi engine - Certificate issued: September 3, 2010 - Last registry action: September 3, 2010 - Mode S code: AA5D4C - 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/N767UA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=767UA - Page: https://openairdocs.org/deregistered/N767UA-2011-12-19 From the FAA registry file of November 12, 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 777-222: https://openairdocs.org/model/boeing-777-222.md ## Service difficulty reports (24) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR 2004UALA00008](https://openairdocs.org/sdr/2004UALA00008), Jan 6, 2004: ENGINE. FLAMED OUT. NR 1 ENGINE FLAMEOUT IN FLIGHT. CREW UNABLE TO RESTART ON 2 ATTEMPTS. FUEL PUMP MAIN STAGE FAILURE. IMPLEMENTING SOFT TIME THRESHOLD FOR OVERHAUL OF PUMPS AT SH - [SDR 2003UALA00797](https://openairdocs.org/sdr/2003UALA00797), Oct 23, 2003: ACTUATOR. FAILED. COULD NOT PRESSURIZE AIRCRAFT ON CLIMBOUT. DOWNLINKED CMC DATABASE SHOWED MAINTENANCE MESSAGE 21-39080, THE CABIN PRESSURE COULD NOT BE CONTROLLED DUE TO FAILED - [SDR 2003UALA00342](https://openairdocs.org/sdr/2003UALA00342), Mar 1, 2003: WEDGE. DELAMINATED. T/E WEDGE DELAMINATED - NR 12 SLAT MAJOR REPAIR ACCOMPLISHED. T/E WEDGE REPAIRED. - [SDR 2003UALA00209](https://openairdocs.org/sdr/2003UALA00209), Feb 19, 2003: SKIN. DELAMINATED. TRAILING EDGE WEDGE, SLAT NR 1, DELAMINATED ON LOWER SURFACE. OUTBOARD END SEAL PLUG MISSING. REPAIRED TRAILING EDGE WEDGE. REPLACED OUTBOARD SEAL PLUG. - [SDR 2003UALA00207](https://openairdocs.org/sdr/2003UALA00207), Feb 19, 2003: SKIN. DELAMINATED. LOWER SKIN DELAMINATED ON TRAILING EDGE WEDGE, SLAT NR 11. REPAIRED TRAILING EDGE WEDGE, SLAT NR 11. - [SDR 2003UALA00205](https://openairdocs.org/sdr/2003UALA00205), Feb 19, 2003: SKIN. DELAMINATED. TRAILING EDGE WEDGE, SLAT NR 5, DELAMINATED. SEAL FOAM CORE MISSING SECTION. REPAIRED TRAILING EDGE WEDGE, SLAT NR 5. REPLACED SEAL FOAM CORE. - [SDR 2003UALA00204](https://openairdocs.org/sdr/2003UALA00204), Feb 19, 2003: SKIN. DELAMINATED. DELAMINATED SKIN ON TRAILING EDGE WEDGE, SLAT NR 3, AND SEAL FOAM CORE MISSING SECTION. REPAIRED TRAILING EDGE WEDGE SLAT NR 3. REPLACED SEAL FOAM CORE SECTION. - [SDR 2003UALA00208](https://openairdocs.org/sdr/2003UALA00208), Feb 17, 2003: WEDGE. DELAMINATED. DELAMINATION OF LOWER SKIN ON T/E WEDGE, RIGHT WING. REPAIRED T/E WEDGE, LOWER SKIN, RIGHT WING - [SDR 2003UALA00206](https://openairdocs.org/sdr/2003UALA00206), Feb 16, 2003: SKIN. DELAMINATED. DELAMINATED TRAILING EDGE WEDGE SKIN (SLAT NR 10). REPAIRED TRAILING EDGE WEDGE, SLAT NR 10. - [SDR 2003UALA00296](https://openairdocs.org/sdr/2003UALA00296), Feb 10, 2003: RIB. CRACKED. LT O/B HORIZONTAL STABILIZER CLOSE-OUT RIB POST IS DAMAGED/CRACKED. MAJOR REPAIR ACCOMPLISHED. CRACKED RIB POST WAS REPLACED. - [SDR 2002UALA01140](https://openairdocs.org/sdr/2002UALA01140), Jul 5, 2002: IDG. MALFUNCTIONED. LOSS OF RIGHT ENGINE GENERATOR ON CLIMBOUT. ENGINE NOT SHUTDOWN. MAINTENANCE MESSAGE 24-31712 WAS PRESENT. MAINTENANCE ACCOMPLISHED CH5588 WITH NO DISCREPANCIES - [SDR 2001UALA02238](https://openairdocs.org/sdr/2001UALA02238), Nov 8, 2001: ACTUATOR. SEIZED. AIRCRAFT DIVERTED INTO SLC DUE TO NR 2 ENGINE OSCILLATING. N1 AND N2 DROPPED TO IDLE WITH EGT INCREASING; EGT 570 DEG. ENGINE SHUT DOWN BY FLT CREW. SUPPLEMENTA - [SDR 2001UALA01041](https://openairdocs.org/sdr/2001UALA01041), Jun 10, 2001: WARNING HORN. ACTIVATED. ABORTED TAKEOFF AT APPROX 80 KTS DUE TO ENG FAILURE WARNING HORN SOUNDING. - [SDR 2001UALA00192](https://openairdocs.org/sdr/2001UALA00192), Mar 2, 2001: STIFFENER. CRACKED. STA 246 BUCKLED VERTICAL STIFFENERS AT LBL - 7.88, 26.05, 48 RBL - 7.88, 13.55, 20, 29.5, 47,53. *S/D* REPLACED STIFFENERS PER SRM 53-10-51, REPAIR 3. - [SDR 99UAL900560](https://openairdocs.org/sdr/99UAL900560), Oct 29, 1999: ACM. FAILED. CREW REPORTED SMOKE IN COCKPIT AND AFT CABIN AREAS DURING FLIGHT. *S/D* LEFT HAND AIR CYCLE MACHINE (ACM PN:810209-3) WAS REPLACED PRECAUTIONARY. AIRCRAFT WENT - [SDR 99UAL900207](https://openairdocs.org/sdr/99UAL900207), Mar 14, 1999: STIFFENER. DAMAGED. VERTICAL STIFFENERS AT STA 246 FLOORBEAM BUCKLED AND/OR CRACKED IN BEND RADIUS. LOCATIONS WERE AT RBL 50.0 (P/N 144W8518-69), RBL 44.95 (P/N 141W8518-69), RBL 3 - [SDR 98ZZZX2022](https://openairdocs.org/sdr/98ZZZX2022), May 13, 1998: BEARING. FAILED. ENGINE REMOVED ON 5-6-98 DUE IN-FLIGHT SHUT DOWN FOLLOWING OIL FILTER BYPASS LIGHT AND LOW OIL PRESSURE LIGHT. DISASSEMBLY INSPECTION REVEALED FAILED NR 1 MAIN - [SDR 98UAL900178](https://openairdocs.org/sdr/98UAL900178), May 6, 1998: BEARING. STALLED. EICAS (ENGINE INDICATION AND CREW ALERT SYSTEM) MESSAGE ENG OIL FILTER R DISPLAYED IN FLIGHT AT 1700Z. AT 1920Z OIL PRESSURE STARTED DOWNWARD STEADILY UNTIL LOW - [SDR 97UAL900326](https://openairdocs.org/sdr/97UAL900326), Apr 23, 1997: SKIN. CRACKED. NR 6 LEADING EDGE SLAT (PN 114W4508-29) CRACKED AT INBOARD TRACK CUTOUT. ONE CRACK THREE INCHES LONG AND THE SECOND IS FIVE INCHES LONG. *S/D* INTERIM REPAIR AC - [SDR 96UAL900980](https://openairdocs.org/sdr/96UAL900980), Dec 27, 1996: GENERATOR. FAILED. EN ROUTE, LOST RIGHT ENGINE DRIVEN GENERATOR. RETURNED TO MIA. - [SDR 96UAL900774](https://openairdocs.org/sdr/96UAL900774), Oct 7, 1996: FRAME. CRACKED. NR 2 PYLON STRUT AFT FAIRING FRAME NR 5 INBOARD ATTACH FITTING CRACKED. *S/D* FITTING WAS ADJACENT TO PREVIOUSLY REPLACED FITTING. SUSPECT PRELOAD CONDITION INT - [SDR 96UAL900316](https://openairdocs.org/sdr/96UAL900316), May 6, 1996: PWR CONT UNIT. FAILED. SPOILERS EICAS MESSAGE DURING LANDING ROLL. *S/D* REPLACED NUMBER FOUR SPOILER POWER CONTROL UNIT. - [SDR 95UAL900030](https://openairdocs.org/sdr/95UAL900030), Jul 3, 1995: CIRCUIT BREAKER. DAMAGED. A/C RETURNED TO FIELD WITH LEFT ENGINE EEC AND BLEED PROBLEMS. REPLACED CIRCUIT BREAKER AND WIRE. PER BOEING ANALYSIS THE SCREW HOLDING THE WIRES IN THE CIRCUIT - [SDR 95UAL777001](https://openairdocs.org/sdr/95UAL777001), Jun 2, 1995: RETRACT MECH. MALFUNCTIONED. ON TAKEOFF GEAR WOULD NOT RETRACT, WOULD RAISE WITH OVER RIDE SWITCH. ## 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 20011108033369I](https://openairdocs.org/incident/20011108033369I), Nov 8, 2001: Boeing 777222 (N767UA), Salt Lake City, UT. (-23) Shutdown of #2 engine in flight. Aircraft enroute sfo to ord in cruise at flight level 370 when crew heard three loud bangs. After third bang power was… --- 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, except the copies of manufacturers’ service documents, which belong to their rights holders.