# N369UA: 1989 Boeing 737-322, registration cancelled 2011-04-05

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: April 5, 2011
- Status when cancelled: Valid registration
- Airframe: [Boeing 737-322](https://openairdocs.org/model/boeing-737-322) (registry code 138447Y)
- Engine: [CFM International CFM56 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802)
- Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (OpenAirDocs)
- Serial number: 24538
- Year built: 1989
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 2, 1989
- Certificate issued: January 19, 2011
- Last registry action: January 19, 2011
- Mode S code: A42F7E
- 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/N369UA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=369UA
- Page: https://openairdocs.org/deregistered/N369UA-2011-04-05

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 737-322: https://openairdocs.org/model/boeing-737-322.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 2008UALA04166](https://openairdocs.org/sdr/2008UALA04166), Aug 6, 2008: LAMP. INOPERATIVE. LEFT OVERWING HATCH ILLUMINATION EMERGENCY LIGHTS INOP. *S/D* RELAMPED WITH 2EA LAMPS.
- [SDR 2008UALA04164](https://openairdocs.org/sdr/2008UALA04164), Aug 6, 2008: LAMP. INOPERATIVE. FLIGHT DECK EMERGENCY LIGHT INOP. *S/D* RELAMPED, OP CHECKS OKAY.
- [SDR 2008UALA02662](https://openairdocs.org/sdr/2008UALA02662), May 8, 2008: SPINDLE. CORRODED. CORROSION SUSPECTED AT LT OB FLAP, INBD SPINDLE.
- [SDR 2008UALA02074](https://openairdocs.org/sdr/2008UALA02074), Apr 10, 2008: FITTING. FAILED. CAPTAINS O2 FITTING SNAPPED OFF IN STOWAGE BOX. REPLACED CAPTS O2 MASK BOX PER MM 35-12-96. AC OK FOR SERVICE. 
- [SDR 2007UALA05175](https://openairdocs.org/sdr/2007UALA05175), Dec 19, 2007: EXTINGUISHER. LOW PRESSURE. FWD GALLEY HALON FIRE EXTINGUISHER PRESSURE APPEARS LOW. REPLACED HALON EXTINGUISHER IN FWD GALLEY.
- [SDR 2007UALA04363](https://openairdocs.org/sdr/2007UALA04363), Oct 20, 2007: SKIN. DAMAGED. FUSELAGE SKIN 16 INCHES FWD OF FWD CARGO DOOR CUTOUT IS DENTED WITH A GOUGE IN MIDDLE OF DENT. MEASURES 3.5" LONG, .25" WIDE, .080" DEPTH AND RUNS THROUGH 2 RIV
- [SDR 2007UALA03591](https://openairdocs.org/sdr/2007UALA03591), Sep 5, 2007: FIRE BOTTLE. LOW PRESSURE. LEFT ENGINE (FORWARD) FIRE BOTTLE LOW PSI, READS 700 PSI.
- [SDR 2007UALA02541](https://openairdocs.org/sdr/2007UALA02541), Jul 10, 2007: TERMINAL. LOOSE. GEAR WARNING HORN SOUNDS WITH THROTTLES IN IDLE AND FLAPS UP. FOUND GROUND GD2858 DC LOOSE AT TERMINAL STUD SECURED LUG,
- [SDR 2007UALA02482](https://openairdocs.org/sdr/2007UALA02482), Jul 7, 2007: KEELBEAM. WORN. WEAR ON UPPER KEEL BEAM RIGHT HAND FROM 2 PANEL FASTENER RBL 7 STA 720-722. [07-27-07] MAJOR REPAIR: INSTALLED AN ANGLE, CUTOUT FILLER AND REPAIR FILLER. ACCOMP
- [SDR 2007UALA02481](https://openairdocs.org/sdr/2007UALA02481), Jul 7, 2007: LIGHT. INOPERATIVE. RIGHT LOWER AFT FUSELAGE EMERGENCY EXIT LIGHT IS INOP. [07-27-07] RELAMPED RT LOWER AFT FUSELAGE EMERGENCY
- [SDR 2007UALA02480](https://openairdocs.org/sdr/2007UALA02480), Jul 6, 2007: SKIN. WORN. EXTERNAL CROWN SKIN HAS WEAR DAMAGE UNDER DORSAL LANDING ON LEFT SIDE FROM BS 908-965. [07-27-07] MAJOR REPAIR: INSTALLED DOUBLER, TEAR STRAP DOUBLER, AND TAPE 
- [SDR 2007UALA02479](https://openairdocs.org/sdr/2007UALA02479), Jul 6, 2007: DOOR FRAME. CRACKED. FWD PIT DOORWAY CUTOUT FWD FRAME IS CRACKED AT LWR DOOR STOP FITTING. [07-27-07] MAJOR REPAIR: REMOVED CRACK AND ACCOMPLISHED ANGLE REPAIR PER MM 53-30-75.
- [SDR 2007UALA02478](https://openairdocs.org/sdr/2007UALA02478), Jul 6, 2007: BEARING. LOOSE. FWD ENTRY DOOR CUTOUT HAS AN AFT STOP PAD LOOSE. [07-20-07] REMOVED AND REPLACED BEARING STOP PAD.
- [SDR 2007UALA02474](https://openairdocs.org/sdr/2007UALA02474), Jul 6, 2007: BEARING. LOOSE. FWD ENTRY DOOR CUTOUT FWD & AFT STOP PADS ARE LOOSE. [07-20-07] REMOVED & REPLACED BEARING STOP PAD.
- [SDR 2007UALA02473](https://openairdocs.org/sdr/2007UALA02473), Jul 6, 2007: CABLE. MISROUTED. RIGHT AILERON CABLE MISROUTED ABOVE CONTROL QUADRANT CASTING DAMAGE TO CABLE AND AILERON QUADRANT ATTACH HARDWARE. [07-31-07] REMOVED AND REPLACED MISROUTED CAB
- [SDR 2007UALA02472](https://openairdocs.org/sdr/2007UALA02472), Jul 6, 2007: SKIN. DAMAGED. UPPER FUSELAGE ATC ANTENNA HAD A DEEP SCRIBE IN SKIN FOUND AFTER ANTENNA REMOVED. [07-27-07] MAJOR REPAIR: INSTALLED A DOUBLER PER EA 1070451 REV IR.
- [SDR 2007UALA02471](https://openairdocs.org/sdr/2007UALA02471), Jul 6, 2007: SKIN. DENTED. LWR AFT FUSELAGE BELLY SKIN, BS 807 BL 0 BETWEEN STRINGERS 27L-27R HAS LARGE DENT ADJACENT TO FRAME CAUSING FASTENER PROTRUSION. [07-27-07] MAJOR REPAIR: REMOVE
- [SDR 2007UALA02470](https://openairdocs.org/sdr/2007UALA02470), Jul 6, 2007: SHEAR TIE. CRACKED. AFT PIT STA 807 BETWEEN STR 27R AND 27L AT BL 0, SHEAR TIE IS CRACKED IN RADIUS AT OUTER SKIN. [07-27-07] MAJOR REPAIR: ACCOMPLISHED SHEAR TIE REPLACEMENT AT ST
- [SDR 2007UALA02469](https://openairdocs.org/sdr/2007UALA02469), Jul 6, 2007: SUPPORT ANGLE. CRACKED. AFT PIT STA 807, BETWEEN STR 26R AND 25R LOWER DOOR SILL SUPPORT ANGLE IS CRACKED. [07-27-07] MAJOR REPAIR: REPLACED SUPPORT ANGLE AT STA 807 BETWEEN STR 26R AN
- [SDR 2007UALA02468](https://openairdocs.org/sdr/2007UALA02468), Jul 6, 2007: SKIN. DENTED. FUSELAGE SKIN DENTED AT STA 870 STR 28R TO STR 28L. [07-27-07] MAJOR REPAIR: REMOVED DAMAGE. ACCOMPLISHED A DOUBLER REPAIR. ALSO REPLACED THE CRACKED SHEAR TIE 
- [SDR 2007UALA02467](https://openairdocs.org/sdr/2007UALA02467), Jul 6, 2007: TORQUE TUBE. EXCESS PLAY. AFT GALLEY DOOR CUTOUT TORQUE TUBE HAS MOVEMENT BEYOND .003. [07-31-07] REMOVED TORQUE TUBE, SPIGOT, AND BOTH GUIDE PLATES WITH BEARINGS. REINSTALLED BOTH GUIDE
- [SDR 2007UALA02466](https://openairdocs.org/sdr/2007UALA02466), Jul 6, 2007: TORQUE TUBE. EXCESS PLAY. AFT ENTRY DOOR CUTOUT TORQUE TUBE HAS MOVEMENT BEYOND .003 INCH. [07-31-07] REMOVED TORQUE TUBE, SPIGOT, AND BOTH GUIDE PLATES WITH BEARINGS. REINSTALLED BOTH G
- [SDR 2007UALA02426](https://openairdocs.org/sdr/2007UALA02426), Jul 5, 2007: BUSHING. CORRODED. LEFT HORIZONTAL STAB FWD SPAR UPPER LUG AFT FACE 8 - 11 O'CLOCK POS HAS CORROSION OUTSIDE OF THE SPOT FACE. MAJOR REPAIR ACCOMPLISHED: REMOVED CORROSION. MANUFA
- [SDR 2007UALA02425](https://openairdocs.org/sdr/2007UALA02425), Jul 5, 2007: BUSHING. CORRODED. LEFT HORIZONTAL STAB, UPPER FRONT SPAR TO CTR SECTION ATTACH LUG HAS CORROSION EMITTING FROM BUSHING. MAJOR REPAIR ACCOMPLISHED: REMOVED CORROSION. MANUFACTURED
- [SDR 2007UALA02424](https://openairdocs.org/sdr/2007UALA02424), Jul 5, 2007: TORQUE TUBE. EXCESS PLAY. FWD ENTRY DOOR CUTOUT TORQUE TUBE HAS MOVEMENT BEYOND .003. REMOVED & REPLACED BODY TORQUE TUBE.
- [SDR 2007UALA02423](https://openairdocs.org/sdr/2007UALA02423), Jul 5, 2007: STRUCTURE. CRACKED. FWD ENTRY DOOR UPPER HINGE CUTOUT 5EA FASTENER HOLES ARE CRACKED. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE. INSTALLED DOUBLER & STRUCTURAL FILLER REPAIR.
- [SDR 2007UALA02422](https://openairdocs.org/sdr/2007UALA02422), Jul 5, 2007: STRUCTURE. CRACKED. FWD ENTRY DOOR CUTOUT, UPPER AND LOWER HINGE CUTOUTS CRACKED OUT OF FASTENER HOLES. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE. MFG'D & INSTALLED 2EA STRUCTURAL 
- [SDR 2007UALA02421](https://openairdocs.org/sdr/2007UALA02421), Jul 5, 2007: STRINGER SPLICE. CRACKED. FUSELAGE STRINGER SPLICE IS CRACKED AT LOWER FLANGE AND UPPER FLANGE BS360 STR 15L. MAJOR REPAIR ACCOMPLISHED: REMOVED & REPLACED STRINGER SPLICE 15L AT STA 360
- [SDR 2007UALA02391](https://openairdocs.org/sdr/2007UALA02391), Jul 3, 2007: STRUCTURE. DENTED. AFT CARGO HAS DENT 9 INCHES FROM UPPER AFT CORNER AND 8 INCHES DOWN FROM TOP. REMOVED DAMAGE. INSTALLED DOUBLER REPAIR.
- [SDR 2007UALA02390](https://openairdocs.org/sdr/2007UALA02390), Jul 3, 2007: SKIN. DAMAGED. FWD CARGO DOOR S/N 1783 EXTERNAL SKIN HAS LARGE AREA OF DAMAGE CREASED 9 INCHES FROM FWD TO 9 INCHES FROM AFT AND 18 INCHES FROM TOP TO 27 INCHES FROM TOP. REMO
- [SDR 2007UALA02257](https://openairdocs.org/sdr/2007UALA02257), Jun 26, 2007: SKIN. CHAFED. UPPER EXTERNAL FUSE SKIN HAS CHAFING WEAR AT DORSAL FIN LANDING FROM BS 860 - 907 BL 0 - LBL 8. MAJOR REPAIR: BLENDED CROWN SKIN WEAR. APPLIED .020 WEAR STRIPS 
- [SDR 2007UALA02161](https://openairdocs.org/sdr/2007UALA02161), Jun 21, 2007: SEAT TRACK. CORRODED. AFT RT LAV AREA FLOOR STRUCTURE OB SEAT TRACK STA 995-1016 LBL 39 LBL40 WL 208-208 UPPER SURFACE HAS CORROSION. REMOVED AND REPLACED FLOOR TRACK AND WEB.
- [SDR 2007UALA02160](https://openairdocs.org/sdr/2007UALA02160), Jun 21, 2007: FLOORBEAM. CORRODED. AFT CABIN FLOORBEAM CAP UPPER SURFACE STA 985-987 RBL 40 TO RBL 45 WL 208 HAS CORROSION.
- [SDR 2007UALA02159](https://openairdocs.org/sdr/2007UALA02159), Jun 21, 2007: SKIN. CRACKED. PASSENGER CABIN BELOW FLOOR LEVEL BD 663 LBL 32, PRESSURE DECK UPPER SKIN CRACKED. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED DOUBLER/FILLER REPAIR.
- [SDR 2007UALA02123](https://openairdocs.org/sdr/2007UALA02123), Jun 20, 2007: SKIN. GOUGED. FWD UPPER FUSELAGE CROWN AT STA 290 STR 2L SKIN IS GOUGED. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE. FABRICATED AND INSTALLED DOUBLER, TRIPLER AND FILLER.
- [SDR 2007UALA02122](https://openairdocs.org/sdr/2007UALA02122), Jun 20, 2007: SKIN. CRACKED. EXTERNAL FUSELAGE SKIN CRACKED BS 470 STR 14R. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGED SECTION. INSTALLED DOUBLER/FILLER REPAIR.
- [SDR 2007UALA02114](https://openairdocs.org/sdr/2007UALA02114), Jun 19, 2007: CREASE BEAM. CORRODED. AFT CABIN FLOOR CREASE BEAM HAS AREAS OF CORROSION JUST BELOW AFT ENTRY DOOR CUTOUT BS 967-986. MAJOR REPAIR ACCOMPLISHED: INSTALLED NEW INNER CREASE BEAM.
- [SDR 2007UALA02029](https://openairdocs.org/sdr/2007UALA02029), Jun 15, 2007: ANGLE. CRACKED. LEFT WW AREA BS 695 INNER CHORD ANGLE CRACKED IN RADIOUS LOCATED JUST ABOVE AND AFT OF UPLOCK. MAJOR REPAIR ACCOMPLISHED: REMOVED & REPLACED THE ANGLE.
- [SDR 2007UALA00072](https://openairdocs.org/sdr/2007UALA00072), Sep 26, 2006: ADC. FAULTY. RETURNED TO LAX, DUE TO LOSS OF FIRST OFFICERS INSTRUMENTS. FAULTY ADC. ADC HAD LOOSE SCREW IN IT FROM T2 A9. REPLACED ADC IN A/C. SCREW ON REMOVED UNIT HAS BEE
- [SDR 2006UALA00314](https://openairdocs.org/sdr/2006UALA00314), Feb 16, 2006: LIGHT. INOPERATIVE. DOOR 1 LEFT EEL LIGHT INDICATIONS INOP. ALSO FWD CENTER AISLE EXIT SIGN AND DOOR 1 RIGHT SLIDE LIGHT INOP.
- [SDR 2004UALA01041](https://openairdocs.org/sdr/2004UALA01041), Nov 10, 2004: OVERHEAT LOOP. MALFUNCTIONED. DIVERTED TO COS DUE TO WING BODY OVERHEAT INDICATION. EXPERIENCED RIGHT WING BODY OVERHEAT WARNING IN FLIGHT WITH ENGINE SUPPLYING AIR. ISOLATED TO RIGHT WING L
- [SDR 2003UALA00767](https://openairdocs.org/sdr/2003UALA00767), Oct 9, 2003: ACCESS PANEL. DAMAGED. LEFT WING INBOARD FLAP LOWER ACCESS PANEL 8407L DAMAGED AT ATTACH HOLE COUNTERSINK. MAJOR REPAIR ACCOMPLISHED. REPLACED PANEL.
- [SDR 2003UALA00723](https://openairdocs.org/sdr/2003UALA00723), Sep 28, 2003: FLOORBEAM. CORRODED. CABIN FLOORBEAM AT STA 294.4 HAS CORROSION FROM RBL 24 TO RBL45. MAJOR REPAIR ACCOMPLISHED, INSTALLED REPLACEMENT WITH ANGLE SPLICE.
- [SDR 2003UALA00730](https://openairdocs.org/sdr/2003UALA00730), Sep 27, 2003: SKIN. DENTED. THREE DENTS IN FUSELAGE SKIN ABOUT 24 INCHES AFT OF DOOR 2R, JUST FWD OF APU INLET. MAJOR REPAIR ACCOMPLISHED, INSTALLED REPLACEMENT PANEL.
- [SDR 2003UALA00720](https://openairdocs.org/sdr/2003UALA00720), Sep 25, 2003: FRAME. CORRODED. STA 805 FUSE FRAME HAS CORROSION ON THE AFT SIDE, JUST ABOVE AND FWD OF THE CARGO DOOR THRESHOLD. MAJOR REPAIR ACCOMPLISHED, INSTALLED DOUBLER REPAIR.
- [SDR 2003UALA00717](https://openairdocs.org/sdr/2003UALA00717), Sep 25, 2003: DOOR FRAME. DAMAGED. FWD LOWER FRAME OF THE FWD RT DOOR CUT-OUT HAS A PIECE MISSING. MAJOR REPAIR ACCOMPLISHED, INSTALLED DOUBLER REPAIR.
- [SDR 2003UALA00715](https://openairdocs.org/sdr/2003UALA00715), Sep 24, 2003: FLOORBEAM. GOUGED. CABIN FLOORBEAM IS GOUGED AT STA 360 AND BL 0. MAJOR REPAIR ACCOMPLISHED, INSTALLED DOUBLER REPAIR.
- [SDR 2003UALA00714](https://openairdocs.org/sdr/2003UALA00714), Sep 24, 2003: FLOORBEAM. CRACKED. CABIN FLOORBEAM IS CRACKED IN THE RADIUS AT STA 927 RBL 45. MAJOR REPAIR ACCOMPLISHED, INSTALLED DOUBLER REPAIR.
- [SDR 2002UALA00447](https://openairdocs.org/sdr/2002UALA00447), Mar 13, 2002: COFFEEMAKER. MALFUNCTIONED. UNSCHEDULED LANDING DUE TO BURNING ODOR. FORWARD COFFEEMAKER HEATING ELEMENT MALFUNCTIONED. REPLACED COFFEEMAKER. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE W
- [SDR 97UAL900260](https://openairdocs.org/sdr/97UAL900260), Apr 6, 1997: LIGHT. INOPERATIVE. EMERGENCY EXIT LIGHTS, FLOOR LIGHT DAMAGED AT 7B LIGHT ASSEMBLY RAISED OFF FLOOR. SECURED TRACK, OPS CHECK GOOD.

All 53: https://openairdocs.org/deregistered/N369UA-2011-04-05/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 19980928036539I](https://openairdocs.org/incident/19980928036539I), Sep 28, 1998: Boeing 737322 (N369UA), San Jose, CA, Minor damage. (-5)At approximately 0930 PST, a Boeing 737, N369UA, flight 2622, operated by united airlines contacted the left wing, with a passenger loading stand. At the…

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