# N313UA: 1987 Boeing 737-322, registration cancelled 2014-12-22

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: December 22, 2014
- Status when cancelled: Registration expired, pending cancellation
- 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: 23674
- Year built: 1987
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 13, 1998
- Certificate issued: January 14, 1988
- Last registry action: September 18, 2007
- Mode S code: A353B9
- Owner when cancelled: [Wilmington Trust Company Trustee](https://openairdocs.org/faa-owner/WILMINGTON%20TRUST%20COMPANY%20TRUSTEE)
- Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington)
- Owner type: Corporation
- Owner's area on the map: 39.7357° N, 75.5321° W: Placed by OpenAirDocs: center of Wilmington, DE, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N313UA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=313UA
- Page: https://openairdocs.org/deregistered/N313UA-2014-12-22

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 (70, newest 50)

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

- [SDR 2008UALA05574](https://openairdocs.org/sdr/2008UALA05574), Sep 3, 2008: SMOKE DETECTOR. FAILED. FWD PIT FIRE DETECTOR LOOP -A SHOWS FAILED AND CANNOT BE RESET. FOUND FAULTY SMOKE DETECTOR. REPLACED FWD "A" LOOP FWD PIT SMOKE DETECTOR. OP CHECKS NORMAL. ACF
- [SDR 2008UALA04207](https://openairdocs.org/sdr/2008UALA04207), Aug 9, 2008: INVERTER. INOPERATIVE. EMERGENCY LIGHTS INOP ROWS 9-15. REPLACED INVERTER M1388. OP TEST OKAY.
- [SDR 2008UALA02721](https://openairdocs.org/sdr/2008UALA02721), May 10, 2008: DOOR FRAME. DAMAGED. AFT CARGO DOOR CUTOUT FWD FRAME JUST ABOVE LWR DOOR STOP FITTING, MIS-DRILLED HOLE IN FRAME. MAJOR REPAIR ACCOMPLISHED, REPLACED FRAME AT BS 794.3.
- [SDR 2008UALA02720](https://openairdocs.org/sdr/2008UALA02720), May 10, 2008: DOOR FRAME. CRACKED. DURING LAP JOINT INSP, FOUND RIGHT FWD SERVICE DOOR FRAME CRACKED AT THE AFT LOWER CORNER. MAJOR REPAIR ACCOMPLISHED, TRIMMED OUT THE DAMAGE. VERIFIED DAMAGE RE
- [SDR 2008UALA02719](https://openairdocs.org/sdr/2008UALA02719), May 10, 2008: RIB. GOUGED. LT INBOARD WING FIXED LEADING EDGE WSTA 208 AIRLOAD RIB IS GOUGED. MAJOR REPAIR ACCOMPLISHED, BLENDED THE GOUGE. VERIFIED CRACK FREE WITH HFEC. INSTALLED REPAIR
- [SDR 2008UALA02715](https://openairdocs.org/sdr/2008UALA02715), May 9, 2008: DOUBLER. CRACKED. NR 1 SLAT JUST INBOARD OF REPAIR DOUBLER IS CRACKED AT AFT ROW OF FASTENERS. REMOVED EXISTING DOUBLER AND DAMAGED AREA. INSTALLED REPAIR SPLICE AND FILLER.
- [SDR 2008UALA02714](https://openairdocs.org/sdr/2008UALA02714), May 9, 2008: DOUBLER. CRACKED. NR 2 SLAT INBOARD OF EXISTING REPAIR DOUBLER IS CRACKED AT AFT ROW OF FASTENERS. REMOVED THE EXISTING DOUBLER AND THE DAMAGED AREA. INSTALLED REPAIR SPLICE AND 
- [SDR 2008UALA02734](https://openairdocs.org/sdr/2008UALA02734), May 9, 2008: LAMP. INOPERATIVE. LT EXTERNAL FUSELAGE EEL LIGHT INOP AFT OF INBOARD AFT FLAP. SUSPECT FAULTY LAMP. REPLACED LAMP OP CHECKED GOOD. AC OK FOR SERVICE.
- [SDR 2008UALA02682](https://openairdocs.org/sdr/2008UALA02682), May 6, 2008: WINDOW. MISSING. AFT GALLEY DOOR SLIDE MISSING PRESS GAUGE WINDOW. NEW WINDOW INSTALLED PER GNMM 6-0-2-50.AC OK FOR SERVICE.
- [SDR 2008UALA02645](https://openairdocs.org/sdr/2008UALA02645), May 6, 2008: SLIDE. OUT OF POSITION. FWD ENTRY DOOR SLIDE IS HANGING OUT OF COVER ASSY. REINSTALLED SLIDE REF MM 25-61-35. AC OK FOR SERVICE.
- [SDR 2008UALA02586](https://openairdocs.org/sdr/2008UALA02586), May 2, 2008: DOOR FRAME. CRACKED. RIGHT FWD SERVICE DOOR FRAME CRACKED AFT LOWER CORNER. MAJOR REPAIR ACCOMPLISHED WITH EXTERNAL FUSELAGE DOUBLER/TRIPLER REPAIR.
- [SDR 2008UALA02494](https://openairdocs.org/sdr/2008UALA02494), Apr 28, 2008: STRAP. CRACKED. TIE STRAP AT BS 348.2 STR 16L IS CRACKED. REPAIR ACCOMPLISHED: REPLACED TIE.
- [SDR 2008UALA02454](https://openairdocs.org/sdr/2008UALA02454), Apr 27, 2008: INTERCOSTAL. DAMAGED. INTERCOSTAL WEB AT STR 15 BETWEEN STA 348 AND 360 HAS 7 EACH ELONGATED HOLES. INSTALLED REPAIR ANGLES.
- [SDR 2008UALA02401](https://openairdocs.org/sdr/2008UALA02401), Apr 24, 2008: FITTING. CRACKED. FRAME CLIP CRACKED AT BS 360 STR 14L,10L AND BS 349 STR 16L SUPPLEMENTAL DATA UPDATE MAJOR REPAIR, REPAIRED PER UA-EVA-71481 AND UA-EVA-71482 AND REO-L01065.
- [SDR 2008UALA02400](https://openairdocs.org/sdr/2008UALA02400), Apr 24, 2008: INTERCOSTAL. CRACKED. INTERCOSTAL WEB CRACKED AT AFT SIDE OF BS 294.5 STR 7L UPPER SURFACE INBD. REPAIRED PER UA-EVA 71481 AND REO-L-01065.
- [SDR 2008UALA02399](https://openairdocs.org/sdr/2008UALA02399), Apr 23, 2008: STRINGER. CRACKED. STRINGER CHANNEL CRACKED AT STRINGER 14L, 15L AND 16L BS 359. REPAIRED PER UA-EVA-71481 AND UA-EVA-71482 AND REO-O1065.
- [SDR UALA2008111301538](https://openairdocs.org/sdr/UALA2008111301538), Mar 18, 2008: FUEL NOZZLE. LOOSE. STRONG FUEL ODOR DETECTED IN CABIN. LOWER FUEL NOZZLE AT 6 O'CLOCK POSITION MISSING BOLT. THREADED INSERT IS STRIPPED CANNOT SECURE BOLT. RAN APU AND FOUND FUEL
- [SDR 2008UALA01538](https://openairdocs.org/sdr/2008UALA01538), Mar 18, 2008: UNKNOWN. ODOR. STRONG FUEL ODOR DETECTED IN CABIN.
- [SDR UALA2008111301396](https://openairdocs.org/sdr/UALA2008111301396), Mar 12, 2008: FUEL NOZZLE. FAULTY. FUEL SMELL WITH APU IN USE, SMOKE ALSO NOTED AT TAIL. FOUND FUEL NOZZLE LINE B-NUT AT 2 O'CLOCK POS BACKED OFF WHICH ALLOWED FUEL LEAK. DIFFICULT ACCESS, MAY RE
- [SDR 2008UALA01396](https://openairdocs.org/sdr/2008UALA01396), Mar 12, 2008: UNKNOWN. ODOR. FUEL SMELL W-APU IN USE SMOKE ALSO NOTED AT TAIL.
- [SDR 2008UALA01319](https://openairdocs.org/sdr/2008UALA01319), Mar 9, 2008: BATTERY PACK. INOPERATIVE. FOUND CENTER EEL LIGHT INOPERATIVE. FOUND FAULTY BATTERY PACK. REPLACED FEEDER AND STRIP AND BATTERY OPS CHECK GOOD PER MM 33-51-92 MM 33-51-91 MM 33-51 -90. AC
- [SDR 2007UALA04913](https://openairdocs.org/sdr/2007UALA04913), Nov 30, 2007: LAMP. INOPERATIVE. EXTERIOR EMERGENCY LIGHT OUT AT RT EMERGENCY EXIT DOOR. FOUND LAMP BURNED OUT. RELAMPED FIXTURE, TESTED OK.
- [SDR 2007UALA04349](https://openairdocs.org/sdr/2007UALA04349), Oct 23, 2007: SENSOR. MALFUNCTIONED. AMBER ALERT. NLG UNSAFE LIGHT ON WITH GEAR UP. ON LANDING NLG GREEN WENT INTERMITTENT THEN NO INDICATION. FOUND FAULTY S845 SENSOR (NOSE GEAR DOWN). REPLACED S8
- [SDR 2007UALA04082](https://openairdocs.org/sdr/2007UALA04082), Oct 5, 2007: MODULE. FAULTY. FAULT LIGHT ON FIRE TEST NORMAL TEST WITH NR 2 ENG OVHT DET SWITCH PLACED IN "A" POSITION. SUSPECT FIRE DETECTION MODULE FAULTY. REPLACED FIRE DETECTION MODULE 
- [SDR 2007UALA03062](https://openairdocs.org/sdr/2007UALA03062), Aug 6, 2007: INDICATOR. MALFUNCTIONED. LANDED UNDER AMBER ALERT DUE TO NO FLAP MOVEMENT. FOUND FLAP POSITION INDICATOR FAILURE. REPLACED THE FLAP POSITION INDICATOR. FLAPS CYCLED THROUGH SEVERAL TIME
- [SDR 2007UALA02834](https://openairdocs.org/sdr/2007UALA02834), Jul 24, 2007: WARNING HORN. ACTIVATED. DURING CLIMB ENCOUNTERED T/O WARNING HORN WITH FLAPS RETRACTED. REPLACED M983 CARD AND ACP CHECKS OF CARDS M983, M989, M990, M991, AND M1110 PER MM32-09-20, ALS
- [SDR 2007UALA02047](https://openairdocs.org/sdr/2007UALA02047), Jun 17, 2007: UNKNOWN. UNKNOWN. AFTER TAKEOFF LANDING GEAR WOULD NOT RETRACT. CREW USED OVERRIDE TRIGGER TO RETRACT GEAR, WITH FLAP RETRACT TAKEOFF WARNING HORN SOUNDED. [07-06-07] FOUND RELAY
- [SDR 2007UALA00419](https://openairdocs.org/sdr/2007UALA00419), Feb 11, 2007: CONTROL MODULE. INOPERATIVE. PER CREW FAULT LIGHT ON ENGINE AND APU FIRE CONTROL MODULE INOPERATIVE. FOUND FAULTY APU/ENGINE FIRE CONTROL MODULE. REPLACED THE FIRE CONTROL MODULE. SHOP FOUN
- [SDR 2007UALA00131](https://openairdocs.org/sdr/2007UALA00131), Jan 18, 2007: SHEAR TIE. DAMAGED. STA 360 INBOARD OF STR 27 LEFT SHEAR TIE HAS A DAMAGED HOLE. MAJOR REPAIR: FABRICATED AND INSTALLED NEW SHEAR TIE PER SRM 53-00-07 PAGE 201.
- [SDR 2007UALA00130](https://openairdocs.org/sdr/2007UALA00130), Jan 18, 2007: STRUCTURE. DAMAGED. DAMAGE FOUND AT STA 410, STA 430, AND STA 450 AT BL 0. MAJOR REPAIR: INSTALLED REPAIR DOUBLER AND SPACER AT STA 410, 430, AND 450. REFERENCE MM 53-30-99 AND SB 
- [SDR 2006UALA02348](https://openairdocs.org/sdr/2006UALA02348), Dec 9, 2006: SEAL. FAILED. AIRCRAFT WOULD NOT PRESSURIZE DURING ASCENT. FOUND APU PNEUMATIC DUCT FOWARD PRESSURE SEAL NOT SECURED (CLAMP OFF). SECURED PRESSURE SEAL.
- [SDR 2006UALA02156](https://openairdocs.org/sdr/2006UALA02156), Nov 7, 2006: DOOR FRAME. CRACKED. FWD CARGO DOOR CUT-OUT AFT FRAME CRACKED AT 2 EA LOCATION AT BS 492 NEAR STR S-24R. REMOVED DAMAGE. FABRICATED AND INSTALLED NESTED ANGLES REPAIR. REFERENCE AAR
- [SDR 2005UALA01112](https://openairdocs.org/sdr/2005UALA01112), Oct 9, 2005: ELEVATOR. MALFUNCTIONED. ABORTED TAKE OFF AT 140 KNOTS DUE TO NO ELEVATOR MOVEMENT. UNSECURED ELEVATOR BALANCE WEIGHT BECAME LODGED BETWEEN LOWER SURFACE OF BALANCE BAY & ANGLE USED TO 
- [SDR 2005UALA00956](https://openairdocs.org/sdr/2005UALA00956), Sep 7, 2005: LIGHT. INOPERATIVE. AFT GALLEY FLOOR EEL LIGHTS INOP. REPLACED LAMP STRIP AT AFT GALLEY.
- [SDR 2005UALA00550](https://openairdocs.org/sdr/2005UALA00550), May 29, 2005: RIB. CRACKED. LT HORIZONTAL STAB L/E RIB LOWER FLANGE AT STA 151.8 WAS FOUND CRACKED. *S/D* REPAIR ACP' D PER EVA-50305, FABRICATED REPAIR ANGLE REPAIR SCHEME AT HMV-4.
- [SDR 2005UALA00549](https://openairdocs.org/sdr/2005UALA00549), May 29, 2005: SKIN. CRACKED. EXTERNAL FUSELAGE SKIN CRACKED AT AFT EDGE OF EQ COOLING EXHAUST OUTLET BS 378 LBL 02. *S/D* DURING REPAIR DETAILED IN MM53-30-99 (DOUBLER INSTALLATION), THE EX
- [SDR 2005UALA00487](https://openairdocs.org/sdr/2005UALA00487), May 29, 2005: SKIN. DENTED. FWD CARGO DOOR HAS SEVERAL DENTS ON EXTERIOR SKIN. REPAIRED PER SRM52-30-01, LARGE 20 X 40 INCH DOUBLER INSTALLED ON OUTER EXT SKIN AT HMV-4.
- [SDR 2005UALA00548](https://openairdocs.org/sdr/2005UALA00548), May 28, 2005: DOOR FRAME. CRACKED. FWD GALLEY DOOR 2 EACH CRACKS FOUND AFT FRAME, FIRST CRACK AFT FRAME CUTOUT OF THE 3RD STOP, SECOND CRACK AROUND THE FASTENER HOLE ADJACENT TO THE LWR STOP. *S/
- [SDR 2005UALA00547](https://openairdocs.org/sdr/2005UALA00547), May 27, 2005: FRAME. DENTED. EXTERNAL FUSELAGE HAS A DENT AT FRAME STA 807 STR 28L & STR 28R. *S/D* REMOVED DAMAGE, FABRICATED AND INSTALLED NEW SHEAR TIE CLIP SUPPORT ANGLE PER SRM 51-40-0
- [SDR 2005UALA00546](https://openairdocs.org/sdr/2005UALA00546), May 27, 2005: DOOR FRAME. CRACKED. AFT CARGO DOOR FWD BS 795 FRAME WAS FOUND CRACKED AT JOINT WITH LOWER FRAME SECTION. *S/D* REPAIR ACP' D PER AAR EA I050096. FRAME SECTION WAS REPLACED USING A 
- [SDR 2005UALA00486](https://openairdocs.org/sdr/2005UALA00486), May 27, 2005: FRAME. CRACKED. CABIN OVERWING BS 616 LT SIDE FRAME WEB INNER CHORD IS CRACKED THROUGH FIRST FASTENER APPROX 7 INCHES BELOW FLOOR. REPAIRED WEB AT BS 616 LT PER MM 53-11-81 AND
- [SDR 2005UALA00480](https://openairdocs.org/sdr/2005UALA00480), May 25, 2005: SKIN. DAMAGED. RT AFT FUSELAGE SKIN REPLACEMENT NEEDS DOUBLER REMOVAL AND INSTALLATION AFTER AFT SKIN IS REPLACED. REMOVED THE DOUBLER, ACCOMPLISHED HFEC OF THE HOLES. FOUND N
- [SDR 2005UALA00471](https://openairdocs.org/sdr/2005UALA00471), May 20, 2005: STRINGER CLIP. CRACKED. AFT PIT STA 727A STR 25L STR CLIP TO FRAME HAS A GAP. REMOVED AND REPLACED STR CLIP REF SRM 51-40-02.
- [SDR 2005UALA00470](https://openairdocs.org/sdr/2005UALA00470), May 20, 2005: STRINGER. CORRODED. AFT PIT STA787+2 TO 787+4 STR 25L UPPER FLANGE IS EXFOLIATED LBL24-24. FABRICATED AND INSTALLED PARTS PER SRM 53-00-03.
- [SDR 2005UALA00458](https://openairdocs.org/sdr/2005UALA00458), May 19, 2005: SKIN. DENTED. EXTERIOR FUSELAGE BELOW 1R BETWEEN FRAMES 277 AND 294 STR 22R AND 23R BELOW A REPAIR DENTED. REMOVED THE DAMAGE FABRICATED A DOUBLER AND TRIPLER PER SRM 53-00-0
- [SDR 2005UALA00543](https://openairdocs.org/sdr/2005UALA00543), May 12, 2005: STRINGER CLIP. DAMAGED. AFT PIT STA 747 STR 23L & STR 22L ARE DAMAGED. REMOVED AND REPLACED STRINGER CLIPS.
- [SDR 2005UALA00545](https://openairdocs.org/sdr/2005UALA00545), May 12, 2005: STRINGER CLIP. DAMAGED. AFT PIT STRINGER CLIP DAMAGED, STR 20L STA 727A. *S/D* REPLACED STRINGER CLIP PER SRM 51-40-02.
- [SDR 2005UALA00544](https://openairdocs.org/sdr/2005UALA00544), May 12, 2005: STRINGER CLIP. DAMAGED. AFT PIT STA 727D STR 23 LEFT STRINGER CLIP DAMAGED. *S/D* REMOVED AND REPLACED STRINGER CLIP REF SRM 51-40-02.
- [SDR 2005UALA00559](https://openairdocs.org/sdr/2005UALA00559), May 6, 2005: SHEAR TIE. DAMAGED. OVERSIZE HOLES WERE FOUND COMMON TO SHEAR TIE AT STA 727D BETWEEN S23R, S24R AND THE SKIN. FUSELAGE FRAME SHEAR TIE WAS REPLACED AND REINFORCED PER SRM 51-00-04
- [SDR 2005UALA00558](https://openairdocs.org/sdr/2005UALA00558), May 6, 2005: PRESSURE PANEL. WORN. LOWER SURFACE OF THE MID CABIN FLOOR PRESSURE WEB AT BS 670 RBL 20 WAS FOUND WORN. REPAIR DOUBLER FABRICATED, FORMED TO FIT AROUND EXISTING BEAD-UP AREA AND INS

All 70: https://openairdocs.org/deregistered/N313UA-2014-12-22/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 CHI00LA269](https://openairdocs.org/ntsb/CHI00LA269), Aug 1, 2000: Boeing 737-322 (N313UA), Chicago, IL, no damage. Probable cause: the evasive maneuver performed by the pilot. A factor was the activation of the collision avoidance system.

## FAA accident and incident reports (2)

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 20051009025399I](https://openairdocs.org/incident/20051009025399I), Oct 9, 2005: Boeing 737322 (N313UA), Seattle, WA, Minor damage. (-23) Pilot aborted take off at rotation, reported aircraft did not respond to elevator inputs during take off roll. Returned to gate. Uala maintenance…
- [Accident 20000731037109A](https://openairdocs.org/incident/20000731037109A), Jul 31, 2000: Boeing 737322 (N313UA), Chicago, IL, No damage. (-23) Subject flight encountered unexpected clear air turbulence during descent into ord. A passenger exiting lavatory was thrown to the floor, fracturing his…

## Other aircraft with N313UA

- [Cancelled 2026-01-31](https://openairdocs.org/deregistered/N313UA-2026-01-31): Spektreworks COBALT-CR, S/N CBCR-2B-0823-GVTOL-513. Sale reported, canceled. Owner: [Phoenix, AZ](https://openairdocs.org/faa-place/AZ/Phoenix)

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