# N932UA: 1992 Boeing 737-522, registration cancelled 2016-04-18

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: April 18, 2016
- Status when cancelled: Valid registration
- Airframe: [Boeing 737-522](https://openairdocs.org/model/boeing-737-522) (registry code 138449F)
- 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: 26658
- Year built: 1992
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 26, 1992
- Certificate issued: April 1, 2013
- Last registry action: December 11, 2015
- Mode S code: ACEEDA
- Owner when cancelled: [United Airlines Inc](https://openairdocs.org/faa-owner/UNITED%20AIRLINES%20INC)
- Location: [Chicago, IL](https://openairdocs.org/faa-place/IL/Chicago)
- Owner type: Corporation
- Owner's area on the map: 41.8813° N, 87.6375° W: Placed by OpenAirDocs at the center of ZIP code 60606, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N932UA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=932UA
- Page: https://openairdocs.org/deregistered/N932UA-2016-04-18

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 737-522: https://openairdocs.org/model/boeing-737-522.md

## Service difficulty reports (54, newest 50)

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

- [SDR 2008UALA03321](https://openairdocs.org/sdr/2008UALA03321), Jun 10, 2008: UNKNOWN. MALFUNCTIONED. ACFT WILL NOT TAXI STRAIGHT, PULLS TO THE LEFT.
- [SDR 2008UALA02874](https://openairdocs.org/sdr/2008UALA02874), May 17, 2008: BATTERY. DISCHARGED. AFT EMERGENCY FLASHLIGHT INOPERATIVE. SUSPECT FAULTY BATTERY. REPLACED BATTERY, OP CHECKED GOOD. AC OK FOR SERVICE.
- [SDR 2008UALA02278](https://openairdocs.org/sdr/2008UALA02278), Apr 18, 2008: RADAR. MALFUNCTIONED. FLIGHT DIVERTED DUE TO WEATHER RADAR PROBLEM. RESET WEATHER RADAR R/T.
- [SDR 2008UALA02010](https://openairdocs.org/sdr/2008UALA02010), Apr 8, 2008: FIRE DETECTOR. INOPERATIVE. APU FIRE SUPPRESSION SYS INOP. REPLACED APU FIRE EXTINGUISHER BOTTLE ASSY. ENGINE & APU FIREX BOTTLE RUPTURE DISC ASSY & ENG/APU FIRE CONTROL P8-1 MODULE PRINTE
- [SDR 2008UALA01934](https://openairdocs.org/sdr/2008UALA01934), Apr 5, 2008: WARNING LIGHT. FALSE INDICATION. RTFL DUE TO APU FIRE WARNING. NO SIGNS OF FIRE FOUND.
- [SDR 2008UALA01543](https://openairdocs.org/sdr/2008UALA01543), Mar 18, 2008: MODULE. FAULTY. CREW REPORTS 1 ENG B FIRE LOOP WILL NOT TEST, A FIRE LOOP TESTS GOOD. SUSPECT FIRE TEST MODULE. REPLACED ENGINE AND APU FIRE CONTROL MODULE REFERENCE AMM 26-21-
- [SDR 2007UALA04744](https://openairdocs.org/sdr/2007UALA04744), Nov 18, 2007: SIGN. UNSECURE. EMERGENCY EXIT SIGN OVER RIGHT SIDE OVERWING HAS FALLEN OFF. SECURED SIGN.
- [SDR 2007UALA04022](https://openairdocs.org/sdr/2007UALA04022), Oct 1, 2007: SLIDE. OUT OF POSITION. AFT GALLEY DOOR EVAC SLIDE GIRT, LOWER AFT PORTION HANGING OUT TOO FAR.
- [SDR 2007UALA02351](https://openairdocs.org/sdr/2007UALA02351), Jul 2, 2007: UNKNOWN. NONE. RTFL DUE TO SUSPECTED FUEL LEAK. [07-24-07] PERFORMED TROUBLESHOOTING. NO LEAK FOUND. ALL OPERATIONAL CHECKS PASSED.
- [SDR 2007UALA01490](https://openairdocs.org/sdr/2007UALA01490), May 12, 2007: WIRE HARNESS. DAMAGED. RTFL UNDER AMBER ALERT DUE TO APU FIRE LIGHT. FOUND BAD CONNECTOR ON OVERHEAT LOOP HARNESS. REPLACED HARNESS.
- [SDR 2007UALA00701](https://openairdocs.org/sdr/2007UALA00701), Mar 5, 2007: COMPRESSOR. STALLED. ON DESCENT NR 1 ENG COMPRESSOR STALLED WITH AUDIBLE BANGS. TWO BANGS WHEN THROTTLE RETARDED AT FL370, ENG BANGED LIGHTLY DOWN TO FL 150 AND BETWEEN FL 150-100 V
- [SDR 2006UALA01071](https://openairdocs.org/sdr/2006UALA01071), Jun 4, 2006: ODOR. DETECTED. BURNING SMELL NOTICED AROUND SEATS 6-7.
- [SDR 2006UALA00762](https://openairdocs.org/sdr/2006UALA00762), Apr 23, 2006: SKIN. CORRODED. RT AIRFONE ANTENNA SCREWS FROZE IN NUTPLATE, UNABLE TO REMOVE, AND EXTERNAL SKIN SURFACE CORRODED. INST'D SINGLE DOUBLER AROUND BASE OF ANTENNA REF AAR EA-I0601
- [SDR 2006UALA00765](https://openairdocs.org/sdr/2006UALA00765), Apr 22, 2006: STIFFENER. CRACKED. RT NR 6 FLAP TRACK FAIRING AFT INBD STIFFENER CRACKED IN UPPER RADIUS THRU FASTENER HOLE AND CRACKED IN HALF, THRU CENTER OF PART. REMOVED AND REPLACED THE STIF
- [SDR 2006UALA00761](https://openairdocs.org/sdr/2006UALA00761), Apr 22, 2006: FRAME. CRACKED. FOUND FRAME BS 727 HAS A CRACK LOCATED JUST BELOW STRINGER 14L. REMOVED DAMAGE, FABRICATED FILLER AND SPLICE ANGLE AND INSTALLED PER AAR EA I060181 AND UAL EVA 
- [SDR 2006UALA00760](https://openairdocs.org/sdr/2006UALA00760), Apr 22, 2006: SKIN. TOOL DAMAGE. AFTER REMOVAL OF BOTTOM AIRFONE ANTENNA FOUND DRILL START NEXT TO MOUNT HOLE. REMOVED DAMAGE FABRICATED FILLER AND DOUBLER AND INSTALLED PER EA I060196 AND EA I
- [SDR 2006UALA00759](https://openairdocs.org/sdr/2006UALA00759), Apr 22, 2006: FRAME. GOUGED. FWD ENTRY DOOR SN 392 METAL GOUGED ON UPPER FWD FRAME OF THE DOOR BY LATCH BEARING HOUSING.
- [SDR 2006UALA00758](https://openairdocs.org/sdr/2006UALA00758), Apr 22, 2006: SKIN. DENTED. FOUND LOWER FUSELAGE BS 203 STR 27L SKIN DENTED. REMOVED DAMAGE, FABRICATED DOUBLER AND STRAPS AND INSTALLED PER AAR EA I06187 AND UA-EVA-60238.
- [SDR 2006UALA00757](https://openairdocs.org/sdr/2006UALA00757), Apr 22, 2006: SKIN. CRACKED. AFT GALLEY DOOR FUSELAGE TORQUE TUBE CUTOUT SKIN UPPER FWD CORNER CRACKED. REMOVED CRACK, ACCOMPLISHED A DOUBLER AND FILLER REPAIR PER SRM 53-60-01 REPAIR 5.
- [SDR 2006UALA00750](https://openairdocs.org/sdr/2006UALA00750), Apr 20, 2006: SKIN. DENTED. LEFT FUSELAGE SKIN HAS 2 EA DENTS AT STA 1001 NEAR STR 12L. REPLACED SKIN AT STR 13 SECTION STA 986 TO 1016 PER SRM 51-40-02.
- [SDR 2006UALA00741](https://openairdocs.org/sdr/2006UALA00741), Apr 20, 2006: CLIP. CRACKED. BS 360 CLIP CRACKED ON INTERCOSTAL AT STR 11L. REMOVED CRACKED CLIP & ACP NDT OF HOLES FOR CRACKS. INSTALLED NEW CLIP.
- [SDR 2006UALA00740](https://openairdocs.org/sdr/2006UALA00740), Apr 20, 2006: FRAME. CRACKED. FUSELAGE FRAME CRACKED AT BS 294 & STR 2R. CUT OUT DAMAGE, FABRICATED & INSTALLED ANGLE REPAIR DOUBLER REF SRM 53-00-07 REPAIR 2.
- [SDR 2006UALA00739](https://openairdocs.org/sdr/2006UALA00739), Apr 19, 2006: INTERCOSTAL. CRACKED. CABIN INTERCOSTALS AT BS 294.5 NEAR STR'S 8L, 11L & 16L & AT THE SHEAR TIE AT BS 360 NEAR STR 11L FOUND CRACKED. FABRICATED AND INSTALLED NEW INTERCOSTALS AND S
- [SDR 2006UALA00738](https://openairdocs.org/sdr/2006UALA00738), Apr 19, 2006: WEB. CRACKED. FWD CABIN DOOR 1L CUTOUT STA 296 AND STR 16 HAS 3 INCH CRACK IN WEB. FABRICATED NEW INTERCOSTAL PER EA I060176.
- [SDR 2006UALA00737](https://openairdocs.org/sdr/2006UALA00737), Apr 19, 2006: WEB. CRACKED. FWD CABIN DOOR 1L CUTOUT, STA. 294 STR 8L WEB CRACKED IN CORNER. FABRICATED & INSTALLED NEW INTERCOSTAL WEB PER EA I060177, 8100-9.
- [SDR 2006UALA00736](https://openairdocs.org/sdr/2006UALA00736), Apr 19, 2006: ACTUATOR. GOUGED. NR 8 SPOILER ACTUATOR, INBD ACTUATOR ATTACH LUG, AND TOP OF ACTUATOR GOUGED.
- [SDR 2006UALA00735](https://openairdocs.org/sdr/2006UALA00735), Apr 19, 2006: DOOR FRAME. GOUGED. FWD CARGO DOOR LWR AFT FRAME CORNER IS GOUGED AROUND 3 EA RIVETS ON INNER SURFACE JUST BELOW LWR STOP FITTING.
- [SDR 2006UALA00734](https://openairdocs.org/sdr/2006UALA00734), Apr 19, 2006: REPAIR. MISINSTALLED. FWD GALLEY DOOR LWR FRAME REPAIR DOUBLER PLATE HAS 8 FASTENER HOLES WITH LESS THAN 2D EDGE DISTANCE.
- [SDR 2006UALA00733](https://openairdocs.org/sdr/2006UALA00733), Apr 19, 2006: DOOR FRAME. CRACKED. FWD GALLEY DOOR LOWER AFT FRAME CRACKED AT THE LOWER STOP FITTING.
- [SDR 2006UALA00728](https://openairdocs.org/sdr/2006UALA00728), Apr 18, 2006: DOOR FRAME. CORRODED. AFT PIT DOOR CUTOUT, FWD FRAME BS 794.3 CORRODED FROM RBL 16" - 20". INSTALLED NEW FRAME REPLACEMENT REPAIR PER SRM 51-40-02.
- [SDR 2006UALA00727](https://openairdocs.org/sdr/2006UALA00727), Apr 18, 2006: FRAME. CRACKED. CABIN FRAME CRACKED AT STA 663, AFT SIDE OF FRAME, JUST I/B OF STR 2R. INSTALLED NESTED ANGLE FRAME REPAIR AND NEW STR SPLICE SECTIONS AT STR'S 2R & 3R PER SRM 
- [SDR 2006UALA00726](https://openairdocs.org/sdr/2006UALA00726), Apr 18, 2006: SKIN. GOUGED. LEFT UPPER FUSELAGE EXTERNAL SKIN HAS A 2 INCH GOUGE BETWEEN STRINGERS 6L & 7L AT STA 589. INSTALLED SINGLE EXT FUSE DOUBLER AND INTERNAL TEAR REPAIR DOUBLERS P
- [SDR 2006UALA00696](https://openairdocs.org/sdr/2006UALA00696), Apr 16, 2006: SKIN. DENTED. FWD CARGO DOOR HAS 5 EA DENTS, LOCATION FROM TOP AND FWD EDGE AS FOLLOWS,16" & 16" IS .33" BY .045" DEEP, 16.75"& 21.5 " IS .45" BY 0.20" DEEP, 16" & 26" IS 1" 
- [SDR 2006UALA00695](https://openairdocs.org/sdr/2006UALA00695), Apr 16, 2006: KEELBEAM. CRACKED. AFT PIT KEELBEAM CRACKED, BS 727 STR 27R. INSTALLED NEW KEELBEAM ANGLE PER SRM 51-40-02.
- [SDR 2006UALA00694](https://openairdocs.org/sdr/2006UALA00694), Apr 15, 2006: STRINGER CLIP. CRACKED. STRINGER CLIPS CRACKED AT BS 907 AT STRINGER 1. REMOVED & REPLACED STR CLIPS AT EACH LOCATION REF SRM 51-40-02.
- [SDR 2006UALA00683](https://openairdocs.org/sdr/2006UALA00683), Apr 13, 2006: ATTACH FITTING. CORRODED. LEFT HORIZ STAB FWD UPPER ATTACH FITTING IS CORRODED & HAS TWO VISIBLE CRACK INDICATIONS AT 1 & 11 O'CLOCK POSITIONS AT BS 1096 & STAB STA 67.54. CORROSION AND 
- [SDR 2006UALA00676](https://openairdocs.org/sdr/2006UALA00676), Apr 11, 2006: FRAME. DAMAGED. BS 360 FRAME AT STR 8R OUTBOARD FLANGE INNER SURFACE HAS TOOLING GOUGES. REMOVED DAMAGE AND FOUND BLEND OUT OF LIMITS. FABRICATED & INSTALLED NESTED ANGLE REPAI
- [SDR 2006UALA00675](https://openairdocs.org/sdr/2006UALA00675), Apr 11, 2006: FLOORBEAM. CORRODED. FLOORBEAM AT BS 986 CORRODED ON UPPER T-CAP & GOUGED AT RBL 24-48. REMOVED DAMAGED TEE CAP FROM RBL 24 TO OUTBD END. FABRICATED REPLACEMENT CAP AND INSTALLED NE
- [SDR 2006UALA00674](https://openairdocs.org/sdr/2006UALA00674), Apr 11, 2006: FLOORBEAM. GOUGED. CABIN FLOORBEAM UPPER CAP HAS A DEEP GOUGE COMING OUT OF FWD HOLE AT STA 520 RBL 24.75. NESTED ANGLE REPAIR INSTALLED PER MM 53-10-95 RPR NR 6.
- [SDR 2006UALA00673](https://openairdocs.org/sdr/2006UALA00673), Apr 11, 2006: SKIN. DENTED. LEFT FUSELAGE SKIN HAS A DENT AT STA 1032 ON STR 13L, A-Y RATIO IS WITHIN LIMITS, BUT DENT IS COMMON TO STR 12L. INSTALLED NEW STR SECTION AND EXTERNAL SKIN DOU
- [SDR 2006UALA00665](https://openairdocs.org/sdr/2006UALA00665), Apr 8, 2006: FRAME. CRACKED. CABIN BS 400, BS 727B, BS 827, BS 867 AND 907 FRAME CRACKED BETWEEN STRINGER 8R & 9R. REMOVED CRACKS, FABRICATED AND INSTALLED TWO EACH ANGLE DOUBLER PER MM 53-
- [SDR 2006UALA00664](https://openairdocs.org/sdr/2006UALA00664), Apr 7, 2006: FRAME. CRACKED. FRAME CRACKED AT FASTENER AT STATION 400 8L & 9L BS 747 8L & 9L, BS 747 8R & 9R, BS 787 8L & 9L, BS 907 8L & 9L. DAMAGE RMVD, HFEC ACP REF MM53-10-84, NDT MAN P
- [SDR 2006UALA00652](https://openairdocs.org/sdr/2006UALA00652), Apr 7, 2006: FRAME. CRACKED. FOUND BODY STATION 787 FRAME IS CRACKED BETWEEN STR 8R AND 9R BEHIND PSU RAIL. REMOVED DAMAGE & VERIFIED CRACK CONTAINMENT. FABRICATED & INSTALLED TWO EACH NEST
- [SDR 2006UALA00651](https://openairdocs.org/sdr/2006UALA00651), Apr 6, 2006: SKIN. DENTED. RT HORIZ STAB LEADING EDGE DENTED APPROX 5 FT FROM FUSELAGE. DAMAGE REMOVED AND A FLUSH REPAIR WAS INSTALLED PER SRM 55-10-01 REPAIR NR 2.
- [SDR 2006UALA00650](https://openairdocs.org/sdr/2006UALA00650), Apr 6, 2006: FLOORBEAM. CORRODED. FOUND FLOORBEAM AT STA 947 CORRODED FROM RBL 29 TO RBL 39. BLENDED CORRODED AREA. ACP NDT FOR CRACKS BLEND OUT OF LIMITS. FABRICATED & INSTALLED NESTED ANGLE RE
- [SDR 2006UALA00613](https://openairdocs.org/sdr/2006UALA00613), Mar 30, 2006: FRAME. CRACKED. FOUND FUSELAGE FRAME AT STA 440 CRACKED BETWEEN STR 8R AND 9R CRACK RADIATING FROM INBD RIVET OF FRAME. DAMAGE & CHECK FOR CRACK CONTAINMENT WITH NDT. FABRICATE
- [SDR 2006UALA00612](https://openairdocs.org/sdr/2006UALA00612), Mar 29, 2006: FRAME. CRACKED. FOUND FUSELAGE FRAME AT STA 440 CRACKED BETWEEN STR 8L AND 9L PSU RAIL ATTACH BRACKET. REMOVED DAMAGE & CHECK FOR CRACK CONTAINMENT USING NDT. FABRICATED & INST
- [SDR 2006UALA00611](https://openairdocs.org/sdr/2006UALA00611), Mar 29, 2006: FRAME. CRACKED. FRAME STA 927 IS CRACKED BETWEEN STR 8L AND 9L AT THE INBD RIVET OF THE PSU RAIL SUPPORT BRACKET. REMOVED DAMAGE & CHECK FOR CRACK CONTAINMENT USING NDT. FABRIC
- [SDR 2005UALA01402](https://openairdocs.org/sdr/2005UALA01402), Dec 4, 2005: GENERATOR. FAILED. DIVERTED, DUE TO A FAILED NR 1 GENERATOR AND WEATHER RADAR. MAINTENANCE REPAIRED WIRE W1502-201-18R AT THE NR 1 GENERATOR. THIS WIRE PROVIDES FIELD CURRENT TO T
- [SDR 2004UALA01132](https://openairdocs.org/sdr/2004UALA01132), Nov 10, 2004: SKIN. CRACKED. AFT SERVICE DOOR OPENING HAS CRACK AT FWD LOWER CORNER. *S/D* MAJOR REPAIR ACCOMPLISHED. INSTALLED SCUFF PLATE AND TAPERED SHIM.

All 54: https://openairdocs.org/deregistered/N932UA-2016-04-18/reports.md

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