# N922FT: Boeing 747-2U3B, registration cancelled 2009-04-23

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: April 23, 2009
- Status when cancelled: Triennial form not returned
- Airframe: [Boeing 747-2U3B](https://openairdocs.org/model/boeing-747-2u3b) (registry code 1384846)
- Engine: [Pratt & Whitney JT9D series](https://openairdocs.org/engine/pratt-whitney-jt9d-series) (registry code 52054)
- Serial number: 22768
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 1, 1999
- Certificate issued: December 3, 1998
- Last registry action: November 18, 2008
- Mode S code: ACC627
- 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/N922FT
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=922FT
- Page: https://openairdocs.org/deregistered/N922FT-2009-04-23

From the FAA registry file of November 4, 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 747-2U3B: https://openairdocs.org/model/boeing-747-2u3b.md

## Service difficulty reports (59, newest 50)

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

- [SDR WRNA200600018](https://openairdocs.org/sdr/WRNA200600018), Jun 6, 2006: ENGINE. MALFUNCTIONED. DURING TAKEOFF, A BALL OF FIRE FROM THE LEFT SIDE WAS REPORTED ACCOMPANIED WITH A LOUD BANG, CREW BELIEVED NR 1 ENGINE HAD FAILED AND ABORT OF TAKEOFF WAS INITI
- [SDR WRNA200600014](https://openairdocs.org/sdr/WRNA200600014), May 25, 2006: STATIC LINE. BROKEN. RUDDER RATIO LIGHT CAME ON IN CLIMB, .84M SPEED 300K ALT 32,000. STAYED -ON- CRUISE 39,000 AT 261K, UPPER RUDDER 2 DEGREES LEFT, LOWER RUDDER 0 DEGREES, LIGHT W
- [SDR WRNA200600005](https://openairdocs.org/sdr/WRNA200600005), Feb 26, 2006: FILTER. UNKNOWN. WHEN LEVELING FL 380, MACH SPD .84, WHILE SLOWLY REDUCING POWER, NR 1 ENGINE AUDIBLY COMPRESSOR STALLED, EPR FLUX ALONG WITH INCREASE IN EGT, AMBER/HIGH EGT LIG
- [SDR WRNA200500018](https://openairdocs.org/sdr/WRNA200500018), Jul 3, 2005: LINE. UNSERVICEABLE. T/O FROM TPE, LANDING GEAR HANDLE WOULD NOT MOVE TO UP POSITION. AIRCRAFT RETURNED TO BASE, LANDING NORMAL. FOUND HYDRAULIC LINE TO TRUCK POSITION ACTUATOR LEAK
- [SDR WRNA200500016](https://openairdocs.org/sdr/WRNA200500016), Jun 21, 2005: ENGINE. DAMAGED. VERY LOUD RUMBLE ON TAKE OFF. UPON LANDING, NR 2 ENGINE WAS FOUND TO HAVE COILS MISSING FROM LT SIDE. RT SIDE DAMAGED, ALONG WITH VARIOUS OTHER AREAS OF DAMAGE 
- [SDR WRNA200500013](https://openairdocs.org/sdr/WRNA200500013), May 21, 2005: ENGINE. DAMAGED. NR1 ENGINE COMPRESSOR STALLED AT FL 11.5, AIRCRAFT RETURNED. LANDING NORMAL. ENGINE BOROSCOPE COMPLIED WITH, NO DISCREPANCIES NOTED. NR 1 ENGINE FAN CASING ACOU
- [SDR P5CA0401032](https://openairdocs.org/sdr/P5CA0401032), Jan 29, 2004: PUSHROD. SHEARED. MAIN DECK CARGO DOOR FWD HOOK SHAFT PUSH ROD SHEARED ON OPEN SEQUENCE. INSTALLED FWD HOOK SHAFT PUSH ROD, OPS NORMAL IAW 52-32-11.
- [SDR P5CA0401017](https://openairdocs.org/sdr/P5CA0401017), Dec 23, 2003: PUSHROD. BROKEN. SIDE CARGO DOOR FAILS TO OPEN. FOUND PUSH ROD BROKEN HOOK ACTUATOR FWD SIDE. REMOVED AND REPLACED ROD AS PER MM 52-32-00, OPS CHECK, OPERATION CHECK NORMAL.
- [SDR P5CA0301016](https://openairdocs.org/sdr/P5CA0301016), Dec 21, 2003: SKIN. DAMAGED. MAIN DECK CRG DOOR FAILED TO CLOSE - DOOR SKIN DAMAGED. PERFORMED TIME LIMITED REPAIR TO DOOR IAW SL TLS-JFK 03-00243H AND SRM COI WAS ISSED AND DOOR DEFERRED E
- [SDR P5CA0301009](https://openairdocs.org/sdr/P5CA0301009), Dec 19, 2003: ROD. DEFECTIVE. SIDE CARGO DOOR FAILS TO CLOSE. REPLACED INPUT ROD TO FWD HOOK TORQUE TUBE IAW 52-32-11.
- [SDR P5CA0300991](https://openairdocs.org/sdr/P5CA0300991), Nov 16, 2003: ENGINE. FAILED. NR 2 ENGINE FAILED IN FLT LOUD RUMBLE FOLLOWED BY LOSS OF POWER HIGH EGT VIBRATION OIL LOSS. REPLACED NR 2 ENG PER MM 71-00-002.
- [SDR P5CA0300977](https://openairdocs.org/sdr/P5CA0300977), Oct 31, 2003: FRAME. DAMAGED. MAIN DECK CARGO AREA, FUSELAGE FRAME, STA 1700 RT SIDE S-1 TO S-11 FRAME DAMAGE. REMOVED DAMAGED PORTION OF FRAME SECTION. REPAIR ACCOMPLISHED IAW SRM 53-10-04.
- [SDR P5CA0300956](https://openairdocs.org/sdr/P5CA0300956), Sep 22, 2003: SKIN. CRACKED. RT OUTBOARD MID FLAP COVE PNL DELAMINATED / CRACKED - 24 INCH LONG - WBL 660. REPAIRED DAMAGE AREA
- [SDR P5CA0300933](https://openairdocs.org/sdr/P5CA0300933), Aug 31, 2003: PUMP. LEAKING. LOSS HYD FLUID NR 4 SYS. NR 4 EDP REMOVED AND DEACTIVATED INSTALLED DEACTIVATION KIT IAW MEL 29-01-A TRASFERRED TO DMI 31340.
- [SDR P5CA0300924](https://openairdocs.org/sdr/P5CA0300924), Aug 24, 2003: HYDRAULIC LINE. RUPTURED. NR 1 HYDRAULIC SYS QUANITITY AND PRESSURE DROPPED TO ZERO AT STARTUP. SWAPPED PRESSURE LINE FROM NR 2 TO NR 1. CAPPED NR 2 ADP LINE FITTINGS. PERFORMED LEAK CHE
- [SDR P5CA0300896](https://openairdocs.org/sdr/P5CA0300896), Jun 3, 2003: COUPLING. SHEARED. NR N2 INDICATION ON NR 3 ENGINE, DURING START - ENGINE DID NOT START PYLON AND START VALVE LIGHTS SHOW AIR PRESS TO STARTER BUT NO ROTATION. REMOVED AND REPLACE
- [SDR P5CA03000885](https://openairdocs.org/sdr/P5CA03000885), May 30, 2003: WARNING LIGHT. ILLUMINATED. ON T/O NR 4 ENG FIRE DET A-LOOP ILLUMINATED FIRE LIGHT. B-LOOP NORMAL. ITEM WAS DEFERRED PER THE DDPG AFTER IT WAS DETERMINED THAT ONE LOOP WAS OPERATIONAL. DEF
- [SDR P5CA0300884](https://openairdocs.org/sdr/P5CA0300884), May 28, 2003: CLAMP. LOOSE. BOTH A&B NR 2 NACELLE TEMP SPIKING RETARDED THROTTLE NACELLE INDICATIONS NORMAL. ON LEAK CK FOUND FAILED DUCT CLAMP BETWEEN HEAT EXCHANGER & ENG DUCT. INSTALLED
- [SDR P5CA0300883](https://openairdocs.org/sdr/P5CA0300883), May 28, 2003: BULKHEAD. CRACKED. CRACKS FOUND ON AFT TORQUE BULKHEAD ON NR 1 & 4 PYLONS. REPAIRED PER SB 54-2201 BOEING PAO R11-03-00004H.
- [SDR P5CA0300882](https://openairdocs.org/sdr/P5CA0300882), May 28, 2003: BULKHEAD. CRACKED. CRACK FOUND ON 1480 LWR BULKHEAD RT SIDE. REPAIRED PER S/B 53-2390.
- [SDR P5CA0300872](https://openairdocs.org/sdr/P5CA0300872), Apr 24, 2003: NOZZLE. LEAKING. DURING FUELING LEAK WAS OBSERVED FROM LT WING FUEL JETTISON NOZZLE VALVE. REPLACED LT FUEL JETTISON NOZZLE VALVE.
- [SDR P5CA0300738](https://openairdocs.org/sdr/P5CA0300738), Jan 23, 2003: FRAME. CRACKED. CRACK, APPROX. 1", FOUND #4 PYLON REAR ENG. MOUNT BULKHEAD TOP MOST L/H FRAME ON HORIZONTAL FLANGE, STARTING FROM TOP EDGE. FRAME REPAIR CARRIED OUT PER SRM 54-
- [SDR P5CA0300737](https://openairdocs.org/sdr/P5CA0300737), Jan 23, 2003: FRAME. CRACKED. CRACK 1-1/2" FOUND #3 PYLON REAR ENG. MOUNT BULKHEAD TOP MOST L/H FWD FRAME REAPIR ANGLE, STARTING FROM TOP EDGE RADIUS. FRAME REPAIR ANGLE REPLACED PER SRM 54-
- [SDR P5CA0300736](https://openairdocs.org/sdr/P5CA0300736), Jan 23, 2003: FRAME. CRACKED. 5 CRACKS TOTAL FOUND #2 PYLON REAR ENG. MOUNT BULKHEAD TOP MOST FWD FRAME. L/H: (1) 2" CRACK ON L/H SIDE FRAME, STARTING FROM TOP EDGE ON VERTICAL FLANGE. R/H: 
- [SDR P5CA0300735](https://openairdocs.org/sdr/P5CA0300735), Jan 23, 2003: FRAME. CRACKED. CRACK FOUND #1 PYLON REAR ENG. MOUNT BULKHEAD L/H FWD FRAME APPROX. 1/2" FROM TOP RADIUS. FRAME REPAIR CARRIED OUT PER SRM 54-10-03 & FAA FORM 8110-3.
- [SDR P5CA0300734](https://openairdocs.org/sdr/P5CA0300734), Jan 22, 2003: SKIN. CRACKED. EVIDENCE OF CRACK ON MAIN ENTRY DOOR 1 L/H, AFT LWR OUTER SKIN EMANATING FROM A FASTENER HEAD COMMON TO THE VERT. INTERCOSTAL. CRACKED SKIN CUT OUT. DOOR SKIN R
- [SDR P5CA0300733](https://openairdocs.org/sdr/P5CA0300733), Jan 22, 2003: SKIN. CRACKED. EVIDENCE OF CRACK ON MAIN ENTRY DOOR 1 R/H, AFT LWR OUTER SKIN EMANATING FROM A FASTENER HEAD COMMON TO VERT. INTERCOSTAL. CRACKED SKIN CUT OUT. DOOR SKIN REPAI
- [SDR P5CA0300732](https://openairdocs.org/sdr/P5CA0300732), Jan 22, 2003: FITTING. CORRODED. CORROSION LEVEL 1 FOUND ON LINE SHROUD FITTING DURING REMOVAL OF APU FUEL LINE SHROUD FIBERGLASS CLOSE OUT PANEL. NEW SHROUD LINE FITTING INSTALLED & LEAK CHECK
- [SDR P5CA0300731](https://openairdocs.org/sdr/P5CA0300731), Jan 20, 2003: PANEL. DELAMINATED. DELAMINATION FOUND L/H WING LEADING EDGE TOP PANEL AT FSSD 1550 (O/B MOST). PANEL REPAIR CARRIED OUT PER SRM 51-40-12 & SRM 51-30-20.
- [SDR P5CA0300730](https://openairdocs.org/sdr/P5CA0300730), Jan 20, 2003: SUPPORT ANGLE. CRACKED. CRACK APPROX. 2-3/4" FOUND #4 PYLON AFT ENG. BULKHEAD FRAME AT NAC STA 221.90 MID SPARE WEB LWR LATERAL SUPPORT ANGLE AT MID SECTION & JOINTING 3 FASTENERS. REP
- [SDR P5CA0300729](https://openairdocs.org/sdr/P5CA0300729), Jan 19, 2003: FRAME. CRACKED. CRACK FOUND #4 PYLON REAR ENG. MOUNT BULKHEAD FRAME ASSY BELOW NAC WL 167.0 ON L/H FWD, R/H FWD & AFT AT FASTENER HOLE. REPLACEMENT OF CRACKED FRAME ASSY CARRIE
- [SDR P5CA0300725](https://openairdocs.org/sdr/P5CA0300725), Jan 14, 2003: BRACE. GOUGED. NICK/GOUGE FOUND AT SAILBOAT AREA OF PYLON #1 DIAGONAL BRACE - LOCATED APPROX 10:00 O'CLOCK POSITION, 29" FROM FWD END AT ZONE 5. DAMAGED AREA BLEND-OUT CARRIED
- [SDR P5CA0300724](https://openairdocs.org/sdr/P5CA0300724), Jan 12, 2003: STIFFENER. CORRODED. CORROSION LEVEL 1 FOUND R/H WING LEADING EDGE FRONT SPAR "L" STIFFENER AT FSSI 1435 LOWER PORTION. REPAIR CARRIED OUT IAW SRM 51-30-02.
- [SDR P5CA0300723](https://openairdocs.org/sdr/P5CA0300723), Jan 12, 2003: STIFFENER. CORRODED. CORROSION LEVEL 1 FOUND LEADING EDGE TOP PANEL SUPPORT RIB AT STA. FSS 1336.00, "L" ANGLE STIFFENER TO FRONT SPAR. "L" ANGLE REPAIR CARRIED OUT AS PER SRM 51-30
- [SDR P5CA0300722](https://openairdocs.org/sdr/P5CA0300722), Jan 12, 2003: FITTING. CRACKED. SIX CRACKS TOTAL FOUND NR 4 REAR ENG MOUNT BATHTUB FITTING: I/B FASTENER HOLE HAS 3 CRACKS - (1) .125 INCH, (1) .1875 INCH & (1) .75 INCH RADIALLY. O/B FASTENER
- [SDR P5CA0300721](https://openairdocs.org/sdr/P5CA0300721), Jan 12, 2003: FITTING. CRACKED. FIVE CRACKS TOTAL FOUND NR 3 PYLON REAR ENG MOUNT BULKHEAD BATHTUB FITTING: I/B FASTENER HOLE HAS 2 CRACKS - (1) APPROX 1.5 INCH & (1) .75 INCH RADIALLY. O/B FA
- [SDR P5CA0300720](https://openairdocs.org/sdr/P5CA0300720), Jan 12, 2003: FITTING. CRACKED. FIVE CRACKS TOTAL FOUND NR 2 PYLON REAR ENG MOUNT BULKHEAD BATHTUB FITTING: I/B FASTENER HOLE HAS 2 CRACKS - (1) APPROX 1 INCH & (1) .875 INCH RADIALLY/ O/B FAS
- [SDR P5CA0300718](https://openairdocs.org/sdr/P5CA0300718), Jan 9, 2003: FITTING. CRACKED. TWO CRACKS FOUND AROUND INBOARD AND OUTBOARD FASTENER HOLES NR 1 PYLON REAR ENGINE MOUNT BULKHEAD BATHTUB FITTING. - I/B: (1) .75 INCH, (1) .125 INCH RADIALLY. 
- [SDR P5CA0300728](https://openairdocs.org/sdr/P5CA0300728), Dec 31, 2002: ROD. CORRODED. CORROSION LEVEL 1 FOUND ON L/H INBD ELEVATOR POWER CONTROL PACKAGE ROD END, WITH TEFLON SEAL ADRIFT. POWER CONTROL PACKAGE REPLACED IAW MM 27-31-07.
- [SDR P5CA0200655](https://openairdocs.org/sdr/P5CA0200655), Feb 26, 2002: PLUG. MISSING. PDU NR 4 DRAIN PLUG MISSING. INSTALLED PLUG AND FILLED PDU IAW 12-13-12. PDU RAN OK.
- [SDR P5CA0200653](https://openairdocs.org/sdr/P5CA0200653), Feb 26, 2002: PANEL. CRACKED. CRACK LT WING REAR SPAR TO INBOARD AILERON TRAILING EDGE UPPER PANEL (573ST). PANEL ASSY REPLACED REF SRM 51-10-01.
- [SDR P5CA0200654](https://openairdocs.org/sdr/P5CA0200654), Feb 25, 2002: PANEL. DAMAGED. DAMAGE LT WING UPPER PANEL STATION WS 440.62, ABOVE KRUEGER FLAPS 11/13. NO CRACK FOUND. REPAIR CARRIED OUT WITH REF TO SRM 51-40-09 & 51-40-15.
- [SDR P5CA0100594](https://openairdocs.org/sdr/P5CA0100594), Sep 20, 2001: ENGINE. MALFUNCTIONED. WHEN THROTTLES WERE RETARDED FOR DESCENT, NR 2 ENG HAD EXCESSIVE VIBRATION FOLLOWED BY UNCLEARABLE STALL CONDITION. ENG SHUTDOWN WAS ACCOMPLISHED NORMALLY. LUBR
- [SDR P5CA0100484](https://openairdocs.org/sdr/P5CA0100484), Feb 28, 2001: STRINGER. CRACKED. CRACK 2.1 LONG BS 1000 LHS STR 46. REPAIRED PER SB747-53-2316.
- [SDR P5CA0100480](https://openairdocs.org/sdr/P5CA0100480), Feb 26, 2001: INTERCOSTAL. CRACKED. CRACK 2.25 INCH FOUND ON INTERCOSTAL BS 434 STR 26. REPAIRED PER SRM 53-30-02.
- [SDR P5CA0100479](https://openairdocs.org/sdr/P5CA0100479), Feb 26, 2001: SKIN. CRACKED. CRACK FOUND BS 434 STR 26 & 27. REPAIRED PER SRM 53-30-02.
- [SDR P5CA0100478](https://openairdocs.org/sdr/P5CA0100478), Feb 26, 2001: SKIN. CRACKED. CRACK FOUND AT BS 1000 STR 46-47 RT 1.8 LONG. REPAIRED PER S/B 747-53-2316.
- [SDR P5CA0100477](https://openairdocs.org/sdr/P5CA0100477), Feb 26, 2001: SKIN. CORRODED. LEVEL 1 CORROSION BETWEEN STA 1700-1720 STR 50L AND51L. REPAIRED PER 53-30-03.
- [SDR P5CA0100476](https://openairdocs.org/sdr/P5CA0100476), Feb 26, 2001: PANEL. CRACKED. CRACK FOUND AT CANTED RPESSURE BULKHEAD R/L CLOSURE PANELS AT WEB STA 1240. REPAIRED PER SRM 53-10-02 AND 8110-3 SB 747-53-2329.
- [SDR P5CA0100475](https://openairdocs.org/sdr/P5CA0100475), Feb 26, 2001: SKIN. DENTED. DENT AT 3 LOCATIONS STA 1830 TO 1840 STR 39L TO 40L. REPAIRED PER SRM 53-30-03.

All 59: https://openairdocs.org/deregistered/N922FT-2009-04-23/reports.md

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB DCA06WA049](https://openairdocs.org/ntsb/DCA06WA049), Jun 7, 2006: Boeing 747-200 (N922FT), Rio Negro, Colombia, substantial damage

## 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.

- [Accident 20060607031139A](https://openairdocs.org/incident/20060607031139A), Jun 7, 2006: Boeing 7472U3B (N922FT), Rio Negro, CP, Substantial damage. (-23) On take off run, the aircraft appeared to have suffered an engine failure. The pilots aborted the take off but were unable to prevent an overrun.. The…

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