# N545UA: 1991 Boeing 757-222, registration cancelled 2018-11-17

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: November 17, 2018
- Status when cancelled: Sale reported, canceled
- Airframe: [Boeing 757-222](https://openairdocs.org/model/boeing-757-222) (registry code 1384956)
- Engine: [Pratt & Whitney PW2040](https://openairdocs.org/engine/pratt-whitney-pw2040) (registry code 52121)
- Data sheets: [TCDS A2NM](https://openairdocs.org/tcds/A2NM), [TCDS E17NE](https://openairdocs.org/tcds/E17NE) (OpenAirDocs)
- Serial number: 25323
- Year built: 1991
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 13, 1991
- Last registry action: March 6, 2018
- Mode S code: A6EC42
- Location: [Stuttgart, AR](https://openairdocs.org/faa-place/AR/Stuttgart)
- Owner type: Individual
- Owner's area on the map: 34.4428° N, 91.5297° W: Placed by OpenAirDocs at the center of ZIP code 72160, within about 10 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N545UA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=545UA
- Page: https://openairdocs.org/deregistered/N545UA-2018-11-17

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 757-222: https://openairdocs.org/model/boeing-757-222.md

## Service difficulty reports (262, newest 50)

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

- [SDR CALA2015030293183](https://openairdocs.org/sdr/CALA2015030293183), Feb 28, 2015: UNKNOWN. MALFUNCTIONED. LEADING EDGE & TE FLAP DISAGREE AT 20. CREW SELECTED FLAP 30, BUT FLAP WAS STOPPED AT 22, USED ALT TO PUT FLAP AT 20 & DIVERTED. TEST ON FSEU IAW AMM 27-51-01, 
- [SDR CALA2015021293147](https://openairdocs.org/sdr/CALA2015021293147), Feb 9, 2015: SMOKE DETECTOR. DEFECTIVE. AFT CABIN AFT LAVATORY SMOKE DETECTOR GREEN LIGHT IS OFF. REPLACED AFT LAVATORY SMOKE DETECTOR ASSEMBLY. OPERATIONS CHECKED NORMAL.
- [SDR CALA2014081391972](https://openairdocs.org/sdr/CALA2014081391972), Aug 8, 2014: APU. FAULTY. APU HAD SHUTDOWN, FAULT LIGHT ILLUMINATED & EICAS MSG APU FAULT DISPLAYED. ADDED 6 QTS OIL, RAN APU, HAD AUTO SHUTDOWN WITHIN 4 MINUTES WITH HEAVY WHITE SMOKE C
- [SDR CALA2014042190880](https://openairdocs.org/sdr/CALA2014042190880), Apr 19, 2014: SKIN. DAMAGED. DAMAGED SKIN CUT OUT & A DOUBLER REPAIR INSTALLED IAW SRM 53-00-01, REPAIR NR 3. IAW SRM TABLE V, THIS IS A CAT B REPAIR IN ZONE A. WHERE THINNEST ORIGINAL SKIN
- [SDR CALA2014041090800](https://openairdocs.org/sdr/CALA2014041090800), Apr 10, 2014: DOOR FRAME. DAMAGED. FUSELAGE FRAME ON FWD SIDE OF L1 DOOR IS CRACKED & BENT. REPAIRED L1 DOORWAY BS 338 UPPER FRAME INBD CHORD IAW ECRA 5300-01886.
- [SDR CALA2014040890788](https://openairdocs.org/sdr/CALA2014040890788), Apr 5, 2014: SKIN. DENTED. DENT REPORTED BY CS APPROXIMATE 3FT AFT OF DOOR 3RT & 4FT UP FROM BOTTOM OF DOOR. DENT IS .075 INCH DEEP BY .5 INCHES WIDE. INSTALLED REPAIR DOUBLER IAW SRM 53-
- [SDR CALA2014040890787](https://openairdocs.org/sdr/CALA2014040890787), Apr 5, 2014: SKIN. DAMAGED. DOUBLER REPAIR INSTALLED 3FT AFT OF DOOR 3 RT BS 1703 AT STRINGER 12RT SKIN THICKNESS IN REPAIR AREA IS .056. REPAIR INSTALLED IAW SRM 53-00-01 RPR 3 FG 201.
- [SDR CALA2014040390760](https://openairdocs.org/sdr/CALA2014040390760), Mar 31, 2014: SKIN. DENTED. REF PREVIOUSLY ARCHIVED DENT CF9088, DAMAGED SKIN CUT OUT & A DOUBLER REPAIR INSTALLED IAW SRM 53-00-01, RPR 3 IAW SRM TABLE V, THIS IS A CAT B REPAIR IN ZONE A
- [SDR CALA2014033190732](https://openairdocs.org/sdr/CALA2014033190732), Mar 30, 2014: SKIN. DENTED. FUSELAGE HAS DENT APPROXIMATELY 4FT FWD OF OUTFLOW VLV. =1 & Y=.047 & DENT IS IN MIDDLE OF BAY NOT AFFECTING INTERNAL STRUCTURE & SMOOTH. CUT OUT DAMAGED SKIN A
- [SDR CALA2014032790712](https://openairdocs.org/sdr/CALA2014032790712), Mar 27, 2014: FLOORBEAM. CORRODED. CORROSION ON CABIN FLOORBEAM UPPER CAP AT BS 1661, WL 208.10 & LBL 8-19. REMOVED CORROSION & MATERIAL REMAINING IS OUT OF LIMITS IAW SRM 53-00-51, FIG 101 & DET
- [SDR CALA2014032790711](https://openairdocs.org/sdr/CALA2014032790711), Mar 27, 2014: ANGLE. CORRODED. CORROSION ON CHORD JUST BELOW RT OVERWING EXIT DOOR CUT OUT STATION 960, JUST ABOVE STRINGER 17. REPLACED T CHORD ANGLE, PN 144N8611-28 IAW SRM 51-40-2 & DWG 14
- [SDR CALA2013120593483](https://openairdocs.org/sdr/CALA2013120593483), Dec 4, 2013: SENSOR. MISSING. IAW DF0035, FWD CARGO LOADING SYS IS MISSING RETRACT LIMIT SWITCH SENSOR & SUPPORT BRACKET ON MODULE 3. WORK IN PROGRESS MEL 2553A IS NOT ACTIVE. REPLACED SENSO
- [SDR CALA2013120593482](https://openairdocs.org/sdr/CALA2013120593482), Dec 4, 2013: DIODE. WEAK. LT REVERSE FAILS TO DEPLOY. IAW WDM 32-09-11 PG5C SH2 FOUND WEAK DIODE R10319. CHECKED WIRING FROM K199 X2 TO K177 12. WIRING CONTINUITY GOOD & NO SHORTS TO GND
- [SDR CALA2013120293352](https://openairdocs.org/sdr/CALA2013120293352), Nov 27, 2013: IDG. FAULTY. RT GEN KICKED OFF WENT TO THRUST. PERFORMED BITE CHECK OF BSCU FOUND OVER SPEED FAULT. REPLACED NR 2 ENG IDG IAW AMM & RAN ENG IAW JRH CHECKED OK.
- [SDR CALA2013111993043](https://openairdocs.org/sdr/CALA2013111993043), Nov 16, 2013: MOTOR. LEAKING. LT WING HAS EVIDENCE OF A HYD LEAK ON LOWER FWD WING ROOT TO BODY FAIRING. FOUND HYD MOTOR LEAKING FROM DRAIN TUBE. REPLACED HYD MOTOR IAW AMM 27-81-08, LEAK CH
- [SDR CALA2013110592666](https://openairdocs.org/sdr/CALA2013110592666), Nov 5, 2013: SHIM. MIGRATED. ACCOMPLISHED INSPECTION OR RECHECK IAW CF9081. RT WING WSS 298 ABOVE INBD FLAP, OTBD FLAP TRACK, SHIM MIGRATING FROM UNDER WING SUPPORT BRACKET.
- [SDR CALA2013110592665](https://openairdocs.org/sdr/CALA2013110592665), Nov 5, 2013: ADI. MALFUNCTIONED. CAPTAIN ADI & HSI NOT GOING INTO TEST MODE.
- [SDR CALA2013103192542](https://openairdocs.org/sdr/CALA2013103192542), Oct 30, 2013: ATTACH FITTING. MISSING. AFT CARGO BAY , FWD RT CARGO NET MISSING CLIP. REPLACED DAMAGED NET.
- [SDR CALA2013100791775](https://openairdocs.org/sdr/CALA2013100791775), Oct 4, 2013: STARTER. FAULTY. DURING LEFT ENGINE START ATTEMPT, WHILE ENGINE WAS ROTATING, HAD EICAS ENGINE STARTER MESSAGE, ABORTED START. MX CLEANED CONNECTOR & PERFORMED ENGINE MOTOR VALV
- [SDR CALA2013091091171](https://openairdocs.org/sdr/CALA2013091091171), Sep 9, 2013: COVER. CONTAMINATED. AMMONIA OR FERMENT SMELL IN FWD GALLEY UNABLE TO DETERMINE SOURCE. PASSENGER IN ROW 1 EYES BURN. DUE TO REPORTS OF A STRONG AMMONIA SMELL AT ROW 31, REPLACE ALL
- [SDR CALA2013082190626](https://openairdocs.org/sdr/CALA2013082190626), Aug 20, 2013: LANYARD. OUT OF POSITION. DOOR WILL NOT ARM: 4R FOUND SURVIVAL LANYARD IN BRIDAL ON GIRT BAR. STOWED ROPE BACK IN BRIDAL, OPS CHECKED NORMAL. DOOR NOW ARMS AND DISARMS.
- [SDR CALA2013082290671](https://openairdocs.org/sdr/CALA2013082290671), Aug 19, 2013: VALVE. FAULTY. FLIGHT DECK TOO HOT WITH LT A/C PACK IN AUTO. ALSO TOO HOT WITH COCKPIT TRIM AIR OFF. REPLACED FLIGHT DECK TRIM AIR VALVE PER MM, OPERATIONS CHECKED NORMAL
- [SDR CALA2013080890258](https://openairdocs.org/sdr/CALA2013080890258), Aug 6, 2013: O-RING. LEAKING. RT ENGINE THRUST REVERSER INOPERATIVE, HYD LEAK AT OTBD CENTER THRUST REVERSER ACTUATOR UPPER FLEX SHAFT. REPLACED O-RING, OPS CHECKED GOOD, NO LEAKS FOUND.
- [SDR CALA2013082690774](https://openairdocs.org/sdr/CALA2013082690774), Aug 5, 2013: SHAFT. LEAKING. RT ENGINE REVERSER IS INOPERATIVE. ACCOUNT OF HYDRAULIC LEAK AT OUTBOARD CENTER REVERSER. ACTUATOR UPPER FLEX SHAFT.
- [SDR CALA2013080690187](https://openairdocs.org/sdr/CALA2013080690187), Aug 5, 2013: O-RING. LEAKING. RT ENGINE REVERSER IS INOPERATIVE DUE TO HYD LEAK AT OTBD CENTER REV ACTUATOR UPPER FLEX SHAFT. REPLACED O-RING, OPS CHECKED, NO LEAKS FOUND.
- [SDR UALA2013071905087](https://openairdocs.org/sdr/UALA2013071905087), Jul 18, 2013: ISOLATION VALVE. INOPERATIVE. NR 1 ENGINE LT THRUST REVERSER INOPERATIVE. REPLACED LT THRUST REVERSER ISOLATION VALVE.
- [SDR UALA2013071204869](https://openairdocs.org/sdr/UALA2013071204869), Jul 11, 2013: FILTER. FAULTY. DURING TAXI OUT, EQUPMENT OVERHEAT EICAS WITH EQUPMENT COOLING FLOW STATUS MESSAGE. SAME INDICATION IN ALTERNATE POSITION. REPLACED EQUPMENT COOLING FILTER.
- [SDR UALA2013062704499](https://openairdocs.org/sdr/UALA2013062704499), Jun 26, 2013: FAN. NOISY. COMMUNICATION IMPOSSIBLE WITH RT RECIRCULATION FAN ON. REPLACED RT RECIRCULATION FAN, OPS CHECKED OK. NO LEAKS NOTED.
- [SDR UALA2013062604427](https://openairdocs.org/sdr/UALA2013062604427), Jun 24, 2013: PLATE. CRACKED. FWD CARGO BAY THRESHOLD PLATE HAS ONE PREVIOUSLY WELD REPAIR THAT IS CRACKED. STOP DRILLED ONE INCH CRACK IAW ECRA 5310-04203. FILLED CRACK WITH SEALANT APPLIED
- [SDR UALA2013061304070](https://openairdocs.org/sdr/UALA2013061304070), Jun 13, 2013: SMOKE DETECTOR. FAILED. L1 LAVATORY SMOKE DETECTOR INOPERATIVE. REPLACED SMOKE DETECTOR, OPS CHECKED GOOD.
- [SDR UALA2013060303846](https://openairdocs.org/sdr/UALA2013060303846), May 31, 2013: START VALVE. FAILED. NR 1 ENGINE HUNG START BEFORE STARTER CUTOUT. REPLACED STARTER AND VALVE IAW AMM.
- [SDR UALA2013050603147](https://openairdocs.org/sdr/UALA2013050603147), May 3, 2013: CONTROL UNIT. MALFUNCTIONED. ACFT IS NOT SENDING TAKEOFF DATA POINTS. FOUND INCORRECT SOFTWARE INSTALLED AND "DMM" LIGHT ON FRONT OF UNIT WOULDN'T EXTINGUISH. INSTALLED SOFTWARE, NO HELP. R
- [SDR UALA2013042502871](https://openairdocs.org/sdr/UALA2013042502871), Apr 24, 2013: FRAME. DENTED. AFT CARGO BAY FRAME DENTED BS 1400 S26L. CUT OUT DAMAGED AREA AND FABRICATED A REPAIR ANGLE AND INSTALLED PER SRM 53-00-07, REPAIR 5. MAJOR REPAIR.
- [SDR UALA2013042502870](https://openairdocs.org/sdr/UALA2013042502870), Apr 24, 2013: SKIN. DENTED. DENT IN FUSELAGE BS 628 S26-27L. FOUND TO BE OUT OF LIMITS PER SRM 53-00-01. CUT OUT DAMAGED SKIN AND FABRICATED AND INSTALLED A REPAIR DOUBLER PER SRM 53-00-01
- [SDR UALA2013041102484](https://openairdocs.org/sdr/UALA2013041102484), Apr 11, 2013: CONNECTOR. DAMAGED. STAB TRIM LIGHT AND UPPER EICAS ILLUMINATED WHEN STAB MOVED. STAB TRIM SHUTOFF LEFT CIRCUIT BREAKER ON P-11 WILL NOT RESET. FOUND D1851 CONNECTOR INSULATION DAM
- [SDR UALA2013041102483](https://openairdocs.org/sdr/UALA2013041102483), Apr 9, 2013: O-RING. LEAKING. HYDRAULIC QUANTITY DECREASED TO 47. QUANTITY STABLE WITH PUMPS OFF, LEFT SYSTEM. CONFERENCE WITH CREW FOLLOWING QRH 130.2 FLUID LEAKING FROM ENGINE DRIVEN PUMP 
- [SDR UALA2013040302205](https://openairdocs.org/sdr/UALA2013040302205), Mar 31, 2013: SWITCH. FAILED. LEFT A/C PACK BITE EICAS MESSAGE. REPLACED CABIN ALTERNATE SWITCH IAW AMM, BITE CHECKED GOOD.
- [SDR UALA2013040302204](https://openairdocs.org/sdr/UALA2013040302204), Mar 31, 2013: MODULE. FAILED. EICAS MESSAGE 'STAB TRIM' DISPLAYED AND STAB TRIM LIGHT ON. REPLACED RIGHT STAB TRIM ASSY MODULE.
- [SDR UALA2013040302203](https://openairdocs.org/sdr/UALA2013040302203), Mar 31, 2013: STARTER. FAILED. APU WILL NOT START, APU FADEC SHOWS LRU STARTER FAULT . REPLACED STARTER.
- [SDR UALA2013040102106](https://openairdocs.org/sdr/UALA2013040102106), Mar 31, 2013: GIRT BAR. DIRTY. L1 DOOR SLIDE LIGHT DOES NOT COME ON WITH SLIDE ARMED. CLEANED GIRT BAR AREA AND CYCLED DOOR. ARM LIGHT CHECKED OKAY.
- [SDR UALA2013032902046](https://openairdocs.org/sdr/UALA2013032902046), Mar 28, 2013: LIGHT. UNSECURE. LEFT EMERGENCY ESCAPE TEST 1 LIGHT INOP. SECURED LIGHT IN SOCKET.
- [SDR UALA2013021500901](https://openairdocs.org/sdr/UALA2013021500901), Feb 14, 2013: SEAT. LOOSE. LAV AT 2L HAS A BROKEN TOILET SEAT FOUND SEAT ASSY JUST LOOSE. SECURED AND INSTALLED MISSING PLACARD.
- [SDR UALA2013020700753](https://openairdocs.org/sdr/UALA2013020700753), Feb 6, 2013: PRESSURE SWITCH. FAILED. LEFT ENGINE LOW PRESSURE LIGHT TESTED OK. LIGHT OFF WITH ENGINE SHUT DOWN. REPLACED LOW PRESSURE EDP SWITCH AS PER AMM, LIGHT OPS NORMAL.
- [SDR UALA2013020400692](https://openairdocs.org/sdr/UALA2013020400692), Feb 3, 2013: UNKNOWN. ODOR. FAINT ODOR LIKE BURNING RUBBER ON F/O'S SIDE ONLY, INTERMITTENT. NO SIGNS OF ANY OVERHEATING. PER CREW, NOT AN ELECTRICAL ODOR. RAN PACKS BOTH HOT AND COLD, OPE
- [SDR UALA2013012800479](https://openairdocs.org/sdr/UALA2013012800479), Jan 21, 2013: GROUND WIRE. DAMAGED. LEFT PACK, GROUNDING WIRE PULLED FROM SHIELD SPLICE AT PACK COMPRESSOR OUTLET TEMP SENSOR. REPAIRED GROUND WIRE FOR SHIELD SPLICE PER SWPM 20-10-15.
- [SDR UALA2013012100357](https://openairdocs.org/sdr/UALA2013012100357), Jan 21, 2013: HEAT EXCHANGER. CRACKED. LEFT A/C PACK SECONDARY HEAT EXCHANGER IS CRACKED. REMOVED LEFT PACK PRIMARY AND SECONDARY HEAT EXCHANGERS.
- [SDR UALA2012111906677](https://openairdocs.org/sdr/UALA2012111906677), Nov 16, 2012: JACK. INOPERATIVE. NR 2 MINITEL MICROPHONE JACK INOPERATIVE. HAND MICROPHONE OPERATES NORMALLY. REPLACED F/O MICROPHONE JACK. OPS CHECKED GOOD.
- [SDR UALA2012111206489](https://openairdocs.org/sdr/UALA2012111206489), Nov 12, 2012: LIGHT. INOPERATIVE. DURING SHUTDOWN OF LEFT ENGINE FUEL VALVE LIGHT DID NOT ILLUM, NEEDS FURTHER TROUBLESHOOTING. SPAR VLV OPS OK, ONLY ENGINE VLV LIGHT DOES NOT ILLUMINATE AT ALL.
- [SDR UALA2012110806441](https://openairdocs.org/sdr/UALA2012110806441), Nov 7, 2012: DOOR. OBSTRUCTED. FLIGHT ATTENDANT REPORTS DOOR 1R WILL NOT ARM. REMOVED WATER BOTTLE CAP FROM DOOR SILL AREA. CLEANED AND LUBRICATED SLIDE GIRT BAR.
- [SDR UALA2012110606373](https://openairdocs.org/sdr/UALA2012110606373), Nov 6, 2012: CONTROLLER. MALFUNCTIONED. AT CRUISE LEFT DUCT PRESS AT 38 PSI & RIGHT AT 22 PSI. PLACED ON MEL CW MEL DDP LOCKED VALVE CLOSED AND PILOT PLUG DISCONNECTED. REPLACED HIGH STAGE PILOT CONTR

All 262: https://openairdocs.org/deregistered/N545UA-2018-11-17/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 19930530018869I](https://openairdocs.org/incident/19930530018869I), May 30, 1993: Boeing 757222 (N545UA), Washington, DC. NR2 engine indicated 703 max EGT and overspeed condition. Shutdown and returned. Landed safely.

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