# N327UA: 1988 Boeing 737-322, registration cancelled 2012-08-10

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 10, 2012
- Status when cancelled: Valid registration
- Airframe: [Boeing 737-322](https://openairdocs.org/model/boeing-737-322) (registry code 138447Y)
- Engine: [GE CFM56 series](https://openairdocs.org/engine/ge-cfm56-series) (registry code 30016)
- Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (OpenAirDocs)
- Serial number: 24147
- Year built: 1988
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 5, 1988
- Certificate issued: May 20, 2010
- Last registry action: April 10, 2012
- Mode S code: A38A14
- 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: 40.8659° N, 112.0391° W: Placed by OpenAirDocs at the center of ZIP code 84116, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N327UA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=327UA
- Page: https://openairdocs.org/deregistered/N327UA-2012-08-10

From the FAA registry file of November 7, 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 (50)

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

- [SDR UALA2009072102154](https://openairdocs.org/sdr/UALA2009072102154), Jul 21, 2009: LIGHT. INOPERATIVE. FLOOR EMERGENCY EXIT LIGHTING INOP FROM SEAT ROW 15-21 AND GALLEY STRIP AFT OF ROW 21. REPLACED LIGHT SEGMENTS.
- [SDR UALA2009072002129](https://openairdocs.org/sdr/UALA2009072002129), Jul 20, 2009: BATTERY. MALFUNCTIONED. ELECTRICAL SYSTEM ISSUE, FLIGHT DIVERTED. BOTH IRS DC FAIL LIGHTS ILLUMINATED. BATTERY VOLTAGE SLOWLY DROPPED TO 14 VOLTS. REPLACED BATTERY, BATTERY CHARGER AND
- [SDR UALA2009072002120](https://openairdocs.org/sdr/UALA2009072002120), Jul 18, 2009: LIGHT. INOPERATIVE. FLOOR EEL LIGHTS FROM ROW 15 AFT INOP. CLEANED CONNECTIONS AT LIGHT STRIP IN AFT GALLEY, OPS CHECKS NORMAL NOW.
- [SDR UALA2009051301353](https://openairdocs.org/sdr/UALA2009051301353), May 11, 2009: INSULATOR. BROKEN. NR 1 ENGINE CORE OVHT-FIRE DETECTOR LOOP HAS A BROKEN CERAMIC INSULATOR. INBD SIDE (M1122) REPLACED DETECTOR. FIRE TEST PASSED ON GROUND.
- [SDR UALA2009033000920](https://openairdocs.org/sdr/UALA2009033000920), Mar 29, 2009: LIGHT. INOPERATIVE. OVERWING EMERGENCY LIGHT LT INOP. RELAMPED EMERGENCY LIGHT. OP CHECK NORMAL.
- [SDR UALA2009020200352](https://openairdocs.org/sdr/UALA2009020200352), Jan 31, 2009: PIN. BROKEN. AFT END OF EEL STRIP IS BROKEN. REPLACED AFT MOST EEL STRIP BY AFT GALLEY CARTS. FOUND BROKEN PINS ON CONNECTOR. CHECKS GOOD.
- [SDR UALA2008111706525](https://openairdocs.org/sdr/UALA2008111706525), Nov 14, 2008: LIGHT. LOOSE. EMERGENCY FLOOR LIGHTS LOOSE NEAR ROW 6 ABC. SECURED EMERGENCY LIGHTS.
- [SDR 2008UALA06213](https://openairdocs.org/sdr/2008UALA06213), Oct 21, 2008: SKIN. DELAMINATED. RT OUTBOARD TRAILING EDGE FLAP OUTBOARD LOWER SURFACE DELAMINATED APPROX 72 SQ INCHES. REPLACED DAMAGED OUTBOARD AFT FLAP ON RT WING. OP CHECKED GOOD. ACFT OK F
- [SDR 2008UALA04266](https://openairdocs.org/sdr/2008UALA04266), Aug 13, 2008: STRUCTURE. DENTED. FUSELAGE ON LEFT SIDE FWD OF ENGINE IS DENTED.
- [SDR 2008UALA04108](https://openairdocs.org/sdr/2008UALA04108), Aug 3, 2008: LIGHT. INOPERATIVE. EEL LIGHTS ARE INOP FROM ROW 16 AFT. *S/D* REMOVED & REPLACED EEL LIGHTS FROM ROW 16 AFT. OPS CHECK NORMAL.
- [SDR 2008UALA02587](https://openairdocs.org/sdr/2008UALA02587), May 2, 2008: LIGHT. FAULTY. EEL LIGHTS FROM ROW 15 ON BACK DO NOT ILLUMINATE. REPLACED LIGHT ASSEMBLY OP CHECKED GOOD. AC OK FOR SERVICE.
- [SDR 2008UALA00187](https://openairdocs.org/sdr/2008UALA00187), Jan 10, 2008: LIGHT. INOPERATIVE. AFT SECTION OF EEL LIGHTS INOP. CLEANED AND REPLACED SHORTED POWER STRIP.
- [SDR 2007UALA03703](https://openairdocs.org/sdr/2007UALA03703), Sep 13, 2007: CONTROLLER. FAILED. CABIN PRESSURE NOT CONTROLLED ON DESCENT IN STANDBY MODE. AT 5.0 PRESSURE BUMP & CABIN CLIMBED TO MATCH ACFT ALT. NO TIME TO SELECT MANUAL. FOUND CABIN PRESSURE
- [SDR 2007UALA03255](https://openairdocs.org/sdr/2007UALA03255), Aug 17, 2007: DOOR FRAME. GOUGED. AFT CARGO DOOR OPENING, FWD FRAME HAS DEEP GOUGE AT LOWER END, MAJOR REPAIR ACCOMPLISHED: REMOVED AND REPLACED FRAME.
- [SDR 2007UALA03215](https://openairdocs.org/sdr/2007UALA03215), Aug 16, 2007: THRESHOLD. CORRODED. AFT PIT DOOR THRESHOLD CORRODED: WEB IS CORRODED AT STA 819 RLB 21 APPROX 2 IN FROM UPPER FLANGE. MAJOR REPAIR ACP AFT CARGO PIT DOOR THRESHOLD WEB. 
- [SDR 2007UALA03214](https://openairdocs.org/sdr/2007UALA03214), Aug 16, 2007: CREASE BEAM. DAMAGED. AFT PIT OPENING, NEED TO CUT RT CREASE BEAM INNER CHORD AT CABIN FLOOR STR 17R TO REMOVE SEGMENT TO FACILITATE FRAME REPAIR AT BS 781. REPAIRED PER SRM 51-70-12
- [SDR 2007UALA03213](https://openairdocs.org/sdr/2007UALA03213), Aug 16, 2007: DOOR FRAME. CRACKED. FWD CARGO DOOR OPENING, AFT FRAME IS CRACKED AT LOWER STOP FITTING. REPAIRED FWD CARGO DOOR AFT FRAME PER MM 53-30-75 PG 801-815.
- [SDR 2007UALA00777](https://openairdocs.org/sdr/2007UALA00777), Mar 15, 2007: CONNECTOR. FAULTY. LAST 20 INCHES OF EEL LIGHTING IN AFT MAIN CABIN IS INOP. CLEANED MOISTURE FROM AFT CONNECTION BETWEEN GALLEY EEL STRIP AND MAIN EEL.
- [SDR 2007UALA00378](https://openairdocs.org/sdr/2007UALA00378), Feb 9, 2007: SKIN. SCRATCHED. UPPER FUSELAGE OUTER SKIN SCRATCHED AT STA 288 S23L. MAJOR REPAIR. REMOVED DAMAGE, FABRICATED AND INSTALLED DOULBER, FILLER AND STRUCTURAL FILLER PER SRM 53-00-
- [SDR 2007UALA00418](https://openairdocs.org/sdr/2007UALA00418), Feb 9, 2007: PLATE. DAMAGED. FWD GALLEY DOOR BODY TORQUE TUBE LOWER HINGE UPPER STOP PLATE HAS A GAP. REPLACED UPPER AND LOWER TORQUE TUBE BEARINGS.
- [SDR 2007UALA00347](https://openairdocs.org/sdr/2007UALA00347), Feb 7, 2007: NUT PLATE. BROKEN. FWD GALLEY DOOR INTERIOR HANDLE TRIM CRACKED ALSO DOOR SLIDE ATTACH POINT HAS BROKEN NUT PLATE. MAJOR REPAIR. REMOVED AND REPLACED DOOR HANDLE COVER PER MM 52-4
- [SDR 2006UALA01895](https://openairdocs.org/sdr/2006UALA01895), Sep 14, 2006: COLLAR. BROKEN. THE R1 DOOR GIRT BAR COLLAR BROKEN. REPLACED THE GIRT BAR SLEEVE.
- [SDR 2006UALA01647](https://openairdocs.org/sdr/2006UALA01647), Aug 23, 2006: SEAT. FAILED. FOUND LOW BOTTLE PRESSURE. CAUSED BY BALL SEAT LEAKING. REPLACED BALL SEAT.
- [SDR 2006UALA01583](https://openairdocs.org/sdr/2006UALA01583), Aug 13, 2006: WIRE HARNESS. DAMAGED. WITH APU SHUTDOWN, THE APU DET INOP LIGHT ON AND 5 MINS LATER THE APU FIRE WARNING LIGHT AND BELL CAME ON. FOUND APU FIRE DETECTION LOOP HARNESS SHORTED. REPLAC
- [SDR 2006UALA01447](https://openairdocs.org/sdr/2006UALA01447), Jul 22, 2006: SKIN. DENTED. FOUND FUSELAGE DENT AT RT FWD SIDE OF STR 21R BETWEEN STA 240-250. FOUND 12 IN SCRIBE MARK AT LAP JOINT LWR SKIN. FABRICATED AND INSTALLED DOUBLER AND TRIPLER R
- [SDR 2005UALA01331](https://openairdocs.org/sdr/2005UALA01331), Nov 22, 2005: WINDOW. CRACKED. L4 WINDOW CRACKED EN ROUTE. L4 WINDOW MIDDLE PANE SHATTERED, REPLACED WINDOW PER MM 56-11-31.
- [SDR 2005UALA00977](https://openairdocs.org/sdr/2005UALA00977), Sep 11, 2005: ROD. OUT OF ADJUST. DOOR 1R HANDLE MOVES IN FLIGHT. *S/D* ADJUSTED COCKING ROD AND LATCH FITTINGS AND STOP PINS. REF MM 52- 00-96-0100A AND MM 52-41-00.
- [SDR 2005UALA00932](https://openairdocs.org/sdr/2005UALA00932), Sep 3, 2005: FLOORBEAM. CORRODED. CABIN FLOOR BS 312 LBL 1 AND LBL 6 SMALL AREA OF CORROSION ON UPPER SURFACE OF FLOORBEAM.
- [SDR 2005UALA00931](https://openairdocs.org/sdr/2005UALA00931), Sep 3, 2005: BULKHEAD. GOUGED. AFT PRESSURE BULKHEAD HAS SEVERAL GOUGES AND SCRATCHES AT UPPER ELECTRICAL CONDUIT THROUGH LT SIDE LBL 5 TO LBL 3 WL 84.
- [SDR 2005UALA00914](https://openairdocs.org/sdr/2005UALA00914), Aug 29, 2005: SHEAR TIE. DENTED. EXTERNAL FUSELAGE STA 807 BETWEEN 28L AND 28R HAS A DENT AND SHEAR TIE BENT AT RADIUS.
- [SDR 2005UALA00913](https://openairdocs.org/sdr/2005UALA00913), Aug 29, 2005: DOOR FRAME. CORRODED. R1 DOOR FRAME STA 296 RBL 54 CORRODED, S17R, WL 208.
- [SDR 2005UALA00893](https://openairdocs.org/sdr/2005UALA00893), Aug 26, 2005: DOOR FRAME. CORRODED. FWD GALLEY DOOR STUB FRAME AT STA 296 AND RBL 54 CORRODED AT STRINGER S-17R AND WL 208.
- [SDR 2005UALA00885](https://openairdocs.org/sdr/2005UALA00885), Aug 25, 2005: FRAME. CRACKED. FWD GALLEY DOOR FRAME CRACKED AFT SIDE LOWER STOP FITTING.
- [SDR 2005UALA00884](https://openairdocs.org/sdr/2005UALA00884), Aug 25, 2005: FRAME. CRACKED. FWD GALLEY DOOR AFT FRAME IS CRACKED AT 3RD AND 4TH STOP FITTING CUTOUTS.
- [SDR 2005UALA00869](https://openairdocs.org/sdr/2005UALA00869), Aug 22, 2005: FLOORBEAM. CORRODED. CABIN FLOOR, STA 294.5 LBL 7, FLOORBEAM UPPER SURFACE, CORROSION.
- [SDR 2005UALA00868](https://openairdocs.org/sdr/2005UALA00868), Aug 22, 2005: SUPPORT. WORN. EE ACCESS DOOR CUTOUT, RT DOOR CUTOUT, SUPPORT FRAME STR 27R STA 338 IS WORN ABOVE DOOR LATCH FITTING.
- [SDR 2005UALA00867](https://openairdocs.org/sdr/2005UALA00867), Aug 22, 2005: FLOORBEAM. CORRODED. CABIN FLOORBEAM TOP CORRODED IN SEVERAL PLACES.
- [SDR 2005UALA00847](https://openairdocs.org/sdr/2005UALA00847), Aug 18, 2005: STRUCTURE. DENTED. AFT CARGO DOOR HAS SEVERAL OVERLAPPING DENTS AND SKIN IS DAMAGED ON FWD SIDE. INSTALLED A REPAIR DOUBLER 53 BY 48 INCHES REF SRM 52-00-01 AND SRM 51-00-01 FIG 2
- [SDR 2005UALA00846](https://openairdocs.org/sdr/2005UALA00846), Aug 18, 2005: ANGLE. CORRODED. AFT GALLEY DOOR THRESHOLD ZEE ANGLE CORRODED STA 978 TO 984 RBL 62.5 STR 17 WL 208.
- [SDR 2005UALA00845](https://openairdocs.org/sdr/2005UALA00845), Aug 18, 2005: FLOOR SUPPORT. CORRODED. CABIN FLOOR SUPPORT AT AFT ENTRY DOOR HAS CORROSION STA 957-986 LBL 62.5 WL 208 AND LBL 63.0 WL 208.
- [SDR 2005UALA00815](https://openairdocs.org/sdr/2005UALA00815), Aug 14, 2005: STRINGER CLIP. CRACKED. AFT PIT STA 907 STR 24R STRINGER CLIP BENT AND CRACKED. REMOVED AND REPLACED STRINGER CLIP.
- [SDR 2005UALA00814](https://openairdocs.org/sdr/2005UALA00814), Aug 14, 2005: STRINGER CLIP. BENT. AFT PIT STA 727D STR 20L STRINGER CLIP BENT AND CRACKED. REMOVED AND REPLACED STRINGER CLIP.
- [SDR 2005UALA00104](https://openairdocs.org/sdr/2005UALA00104), Jan 29, 2005: UNKNOWN. UNKNOWN. RETURNED TO SFO DUE TO PRESSURIZATION PROBLEM. FOUND EXCESSIVE LEAK AROUND E&E COMPARTMENT DOOR. REPLACED E&E COMPARTMENT DOOR SEAL.
- [SDR 2001UALA02313](https://openairdocs.org/sdr/2001UALA02313), Nov 22, 2001: PANEL. DEPARTED. SERVICE PANEL DEPARTED NR 2 ENGINE ON ROTATION. REINSTALLED PANEL. INSPECTED AREA FOR DAMAGE. NO DEFECTS NOTED.
- [SDR 2001UALA02103](https://openairdocs.org/sdr/2001UALA02103), Oct 8, 2001: SKIN. DAMAGED. FORWARD PIT DOOR HAS EXTERIOR SKIN DAMAGED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER.
- [SDR 2001UALA02102](https://openairdocs.org/sdr/2001UALA02102), Oct 8, 2001: SHEAR TIE. CRACKED. STRINGER 12R AT STA 344 SHEAR TIE CRACKED AFT OF DOOR R1 CENTER LINE. MAJOR REPAIR ACCOMPLISHED. REPLACED THE SHEAR TIE AT STRINGER 12R STA 344.
- [SDR 2001UALA00177](https://openairdocs.org/sdr/2001UALA00177), Mar 3, 2001: CIRCUIT BREAKER. MALFUNCTIONED. NOSE GEAR UNSAFE LIGHT ON WHEN THE GEAR WAS EXTENDED FOR LANDING. SUPPLEMENTAL DATA UPDATE RESET BREAKER C404 AND NORMAL GEAR INDICATION RETURNED. REPLACED THE 
- [SDR 2000UALA00216](https://openairdocs.org/sdr/2000UALA00216), Apr 27, 2000: INDICATOR. MALFUNCTIONED. NR 1 ENGINE LOST 9 - 10 PERCENT OF THRUST FROM TARGET CLIMB N1. *S/D* REPLACED THE NR 1 N1 INDICATOR.
- [SDR 97UAL900343](https://openairdocs.org/sdr/97UAL900343), May 2, 1997: CONNECTOR. LOOSE. AFT 5 FEET OF EMERGENCY FLOOR LIGHTS OUT. SECURED LOOSE CONNECTOR, OPS CHECK GOOD.
- [SDR 95UAL737068](https://openairdocs.org/sdr/95UAL737068), May 17, 1995: EEL. INOP. EMERGENCY ESCAPE PATH LIGHT STRIPS INOP IN AFT CABIN AND CARPET IS WET. REPLACE EMERGENCY ESCAPE PATH LIGHT AND DRIED CABLE. CHECKS OK.

## 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 19960826030129I](https://openairdocs.org/incident/19960826030129I), Aug 26, 1996: Boeing 737322 (N327UA), Eugene, OR, Minor damage. Narrative: upon landing at Eugene airport, OR on 8/26/96 at 5:50 p.m., aircraft N327UA, flight no. 1211, ingested an owl in the no. 2 engine. The owl was on…

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