# N520UA: 1990 Boeing 757-222, registration cancelled 2018-08-28

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 28, 2018
- Status when cancelled: Sale reported, pending cancellation
- 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: 24890
- Year built: 1990
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 21, 1990
- Last registry action: March 6, 2018
- Mode S code: A68AB1
- 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/N520UA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=520UA
- Page: https://openairdocs.org/deregistered/N520UA-2018-08-28

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

## Service difficulty reports (112, newest 50)

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

- [SDR CALA2013122793980](https://openairdocs.org/sdr/CALA2013122793980), Dec 26, 2013: PUMP. FAULTY. LT HYD ELEC PUMP LOW PRESS LIGHT ON WITH ITS CB POPPED. REPLACED LT ELEC IAW AMM 29-11-01. PRESS & CASE RETURN FILTER IAW AMM 29-11-18. OPERATIONS & PRESS CHECK
- [SDR CALA2013090591032](https://openairdocs.org/sdr/CALA2013090591032), Sep 4, 2013: STRIKER. DIRTY. COCKPIT DOOR WONT UNLOCK EVEN WITH FLIGHT DECK ACCESS SWITCH OFF. REMOVED & CLEANED STRIKER ASSEMBLY IAW AMM. OPENED & CLOSED DOOR SEVERAL TIMES. OPERATIONS CHE
- [SDR CALA2013082890815](https://openairdocs.org/sdr/CALA2013082890815), Aug 27, 2013: UNKNOWN. MALFUNCTIONED. FIRST OFFICERS FLIGHT DIRECTOR AZIMUTH BAR DISAPPEARED WHEN MODE CHANGED FROM LATERAL NAVIGATION TO HEADING SELECT, NO LAST FLIGHT FAULTS. REPLACED FCC R PRECAU
- [SDR UALA2013072405211](https://openairdocs.org/sdr/UALA2013072405211), Jul 23, 2013: WINDOW. FAILED. F/O FWD WINDOW EXTREMELY HOT TO TOUCH AND MUCH HOTTER THAN CAPTAIN`S FWD WINDOW. INSPECTED WINDOW, IN THE UPPER INBD CORNER AND THE LOWER RT HAND CORNER HAVE BR
- [SDR UALA2013052403632](https://openairdocs.org/sdr/UALA2013052403632), May 24, 2013: CAP. MISSING. EMERGENCY LIGHT END CAP IS MISSING AT SEAT 1B. REPLACED FLOOR EMERGENCY LIGHT END CAP.
- [SDR UALA2013050803233](https://openairdocs.org/sdr/UALA2013050803233), May 7, 2013: COFFEEMAKER. LEAKING. COFFEE MAKER LEAKING. DR-1R FWD-CABIN FWD GALLE. CREW COMMENTS: COFFEEMAKER SPEWS WHEN DISPENSES (1ST CLASS GALLEY). REMOVED AND REPLACED FWD GALLEY COFFEEMAKER
- [SDR UALA2013042302800](https://openairdocs.org/sdr/UALA2013042302800), Apr 21, 2013: LIGHT. MISSING. REF FCD 2527-01070, DID NOT LOCATE EEL LIGHT ADJACENT TO MID LAV (LAV S). INSTALLED EEL LIGHT ASSY ADJACENT TO MID LAV (LAV S), OPS CHECK NORMAL. REF EEL DWG 15
- [SDR UALA2013042202783](https://openairdocs.org/sdr/UALA2013042202783), Apr 21, 2013: LIGHT. MISSING. REF FCD 2527-01070, DID NOT LOCATE EEL LIGHT ADJACENT TO FWD CLOSET. INSTALLED EEL LIGHT ASSY ADJACENT TO FWD CLOSET. OPS CHECK NORMAL. REF EEL DWG 15F6889 & AM
- [SDR UALA2013012500465](https://openairdocs.org/sdr/UALA2013012500465), Jan 24, 2013: SHAFT. OUT OF ADJUST. CAPTAIN'S WINDOW DOES NOT CLOSE. ACCOMPLISHED ADJUSTMENT TEST OF LOWER ROLLER SHAFT IAW AMM, OPS CHECKED NORMAL.
- [SDR UALA2013012100349](https://openairdocs.org/sdr/UALA2013012100349), Jan 20, 2013: SKIN. DENTED. EXTERIOR SKIN DENTED BS 401 BETWEEN S21-22R. REMOVED DAMAGE & REPAIRED SKIN PER ECRA5311-01577.
- [SDR UALA2013010900170](https://openairdocs.org/sdr/UALA2013010900170), Jan 8, 2013: SKIN. DENTED. SKIN DENTED BS 687-710 S17-18R. REPAIRED SKIN PER ECRA 5330-04399.
- [SDR UALA2013010900169](https://openairdocs.org/sdr/UALA2013010900169), Jan 8, 2013: SKIN. DENTED. FUSELAGE SKIN DENTED BS 610 S17L. FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE AND REPAIRED SKIN PER ECRA5330-04386.
- [SDR UALA2013010900168](https://openairdocs.org/sdr/UALA2013010900168), Jan 8, 2013: SKIN. DENTED. FUSELAGE SKIN DENTED BS 530 S28-29L. FOUND TO BE OUT OF LIMITS. PERFORMED HFEC NO DEFECTS NOTED. REPAIRED PER SRM 53-00-01 RPR 3 CAT B.
- [SDR UALA2013010900166](https://openairdocs.org/sdr/UALA2013010900166), Jan 8, 2013: SKIN. DENTED. FUSELAGE SKIN DENTED AT BS 401 BETWEEN STR 21 - 22R. FOUND WITHIN LIMITS OF SRM 53-00-01 FIG 101 ACP HFEC NO CRACKS FOUND. REMOVED DAMAGE AND REPAIRED.
- [SDR UALA2013010900165](https://openairdocs.org/sdr/UALA2013010900165), Jan 8, 2013: SKIN. DENTED. DURING C6 CHECK, FOUND DENT ON FUSELAGE SKIN BS 368 STR 18R. REPAIRED IAW ECRA 5310-05639.
- [SDR UALA2013010900160](https://openairdocs.org/sdr/UALA2013010900160), Jan 8, 2013: CREASE BEAM. CORRODED. BS 1681.8 CREASE BEAM HAS UPPER SURFACE CORROSION AROUND FASTENER HOLE. MAJOR REPAIR ACCOMPLISHED. REMOVED CORROSION FROM PASSENGER CABIN CREASE BEAM UPPER SURF
- [SDR UALA2013010900167](https://openairdocs.org/sdr/UALA2013010900167), Jan 8, 2013: CREASE BEAM. CORRODED. PASSENGER COMPARTMENT BS 1681.8 -14 CREASE BEAM AT RBL 56 HAS UPPER SURFACE CORROSION AROUND FASTENER HOLE. MAJOR REPAIR ACCOMPLISHED. REMOVED CORROSION FROM PA
- [SDR UALA2013010900162](https://openairdocs.org/sdr/UALA2013010900162), Jan 7, 2013: PCU. FAILED. LEFT STAB I/B ELEVATOR PCU FAILED DURING FREEPLAY CHECK. PCU WAS INTERNALLY BYPASSING DURING FREEPLAY CHECK. REMOVED & REPLACED LEFT ELEV INBD PCU PER MM 27-31-
- [SDR UALA2013010900164](https://openairdocs.org/sdr/UALA2013010900164), Jan 7, 2013: PANEL. CORRODED. AFT LAV SERVICE DOOR, CORROSION ON INSIDE OF DOOR PANEL. REMOVED CORROSION AFT LAV SERVICE DOOR IAW SRM. REMOVED & REPLACED AFT LAV SERVICE DOOR P/N 146N3650 PE
- [SDR UALA2013010900163](https://openairdocs.org/sdr/UALA2013010900163), Jan 7, 2013: CREASE BEAM. CORRODED. CREASE BEAM INBOARD ANGLE IS CORRODED BS 688-732. REMOVED CORROSION FROM CREASE BEAM IAW SRM 53-30-13 ORG. OUT OF LIMITS IAW SRM 53-30-13. REMOVED & REPLACED BE
- [SDR UALA2013010900130](https://openairdocs.org/sdr/UALA2013010900130), Jan 7, 2013: ANGLE. DENTED. FORWARD CARGO DOOR CUTOUT, SEAL RETAINER ANGLE DENT AT TOP STOP PIN FITTING. REMOVED AND REPLACED FWD CARGO DOOR CUTOUT SEAL RETAINER ANGLE IAW SRM 51-40-02 & D
- [SDR UALA2013010900117](https://openairdocs.org/sdr/UALA2013010900117), Jan 6, 2013: SKIN. DENTED. FUSELAGE SKIN BS 1620+9 S18R WL 203-205 DENTED. REPAIRED DENTS & INSTALLED DOUBLER & TRIPLERS PER ECRA 5360-01242.
- [SDR UALA2013010900115](https://openairdocs.org/sdr/UALA2013010900115), Jan 6, 2013: FLOOR SUPPORT. CORRODED. CABIN FLOOR SUPPORT CORRODED BS 720 - 732 RBL 62 WL 208. REPLACED FLOOR SUPPORT IAW DWG 143N5400 & SRM 51-40-02. CORROSION FOUND TO BE OUT OF LIMITS.
- [SDR UALA2013010900114](https://openairdocs.org/sdr/UALA2013010900114), Jan 6, 2013: WIRE. DAMAGED. FORWARD LAVATORY OCCUPIED LIGHT WIRE W3572-0125-20 IS DAMAGED. REPLACED WIRE IAW SWPM 20-10-13 AND AMM33-26-00&GMM 05-30-05.
- [SDR UALA2013010900116](https://openairdocs.org/sdr/UALA2013010900116), Jan 6, 2013: FLOOR SUPPORT. CORRODED. CABIN FLOOR SUPPORT CORRODED BS 688-700 RBL 62 WL 208. REMOVED & REPLACED FLOOR SUPPORT IAW DWG 154N5400 & SRM 51-40-02. CORROSION OUT OF LIMITS.
- [SDR UALA2013010900112](https://openairdocs.org/sdr/UALA2013010900112), Jan 5, 2013: WIRE. DAMAGED. WIRE W2038-0003-20 HAS DAMAGE TO OUTER JACKET. INSPECTED GROUND BRAIDED WIRE W2038-0003-20 FOUND NO INTERNAL DAMAGE. OPS CHECKED ACFT EXT POWER RELPT. BSWP 20-1
- [SDR UALA2013010900111](https://openairdocs.org/sdr/UALA2013010900111), Jan 5, 2013: WIRE. BROKEN. L1 DOOR UPPER SURROUND PANEL, EMERGENCY LIGHT TEST SWITCH HAS BROKEN WIRE AT TERMINAL LUG. REPLACED BROKEN WIRES W35 32-0035-22 & W3532-0036-22 AT TERMINAL LUG 
- [SDR UALA2013010900113](https://openairdocs.org/sdr/UALA2013010900113), Jan 5, 2013: FLOORBEAM. CORRODED. MAIN CABIN FLOORBEAM BS 334 RBL 26 TO 40 UPPER SURFACE HAS CORROSION. REMOVED AND REPLACED.
- [SDR UALA2013010700069](https://openairdocs.org/sdr/UALA2013010700069), Jan 4, 2013: FLOORBEAM. CORRODED. PASSENGER CABIN FLOORBEAM TEE SECTION HAS HEAVY SURFACE CORROSION AT BS 365 BL 0 TO RBL 62. REMOVED AND REPLACED TEE LBL16-62 PER ECRA 5310-05536 & SRM 53-00-51
- [SDR UALA2013010700110](https://openairdocs.org/sdr/UALA2013010700110), Jan 4, 2013: SLIDE. NO TEST. L1 DOOR SLIDE FAILED TEST. ESCAPE SLIDE REPLACED.
- [SDR UALA2013010700070](https://openairdocs.org/sdr/UALA2013010700070), Jan 4, 2013: SKIN. GOUGED. LOWER FUSELAGE AT BS 778 AND 1 INCH RIGHT OF BL 0 SKIN GOUGED FROM FAIRING PANEL. REMOVED DAMAGE ON LOWER FUSELAGE AT BS 778 AND 1 INCH RIGHT OF BL 0 IAW SRM. I
- [SDR UALA2012123107474](https://openairdocs.org/sdr/UALA2012123107474), Dec 30, 2012: INTERCOSTAL. CORRODED. MAIN CABIN FLOOR AT STA 324 TO 336 RBL 40 INTERCOSTAL UPPER SURFACE HAS MULTIPLE AREAS OF CORROSION. REMOVED CORROSION IAW SRM 53-00-04, FOUND OUT OF LIMITS IAW
- [SDR UALA2012123107473](https://openairdocs.org/sdr/UALA2012123107473), Dec 30, 2012: FLOORBEAM. CORRODED. MAIN CABIN FLOOR STRUCTURE STA 324 RBL 45 TO RBL 61 FLOORBEAM UPPER FLANGE UPPER AND LOWER SURFACE HAS CORROSION. REMOVED CORR, REMAINING MATERIAL OUT OF LIMIT.
- [SDR UALA2012123107471](https://openairdocs.org/sdr/UALA2012123107471), Dec 30, 2012: SPLICE PLATE. CORRODED. AFT CABIN FLOOR, STA 1680 BL 0, FLOOR PAN TO INTERCOSTAL, SPLICE PLATE CORRODED UPPER SURFACE. BLENDED CORR FROM SPLICE PLATE. REMAINING DAMAGE OUT OF LIMIT. FA
- [SDR UALA2012123107470](https://openairdocs.org/sdr/UALA2012123107470), Dec 30, 2012: SKIN. CORRODED. INTERNAL EMPENNAGE TAIL COMP BETWEEN STA 1787 TO 1825, JUST ABOVE STR 5R SKIN IS CORRODED UNDER APU INLET ATTACH FLANGE. REMOVED CORR, FOUND REMAINING DAMAGE OU
- [SDR UALA2012123107469](https://openairdocs.org/sdr/UALA2012123107469), Dec 30, 2012: PAN. CORRODED. AFT PASSENGER CABIN FLOOR PAN WEB STA 1680 LBL 10 TO RBL 55 UPPER SURFACE CORR BULGING BETWEEN WEB AND FLOOR BEAM AT NUT PLATE HOLES 2EA PLACES. REMOVED CORR, F
- [SDR UALA2012123107468](https://openairdocs.org/sdr/UALA2012123107468), Dec 30, 2012: FLOORBEAM. CORRODED. AFT CABIN FLOORBEAM STA 1640 RBL 12 TO LBL 20, UPPER AND LOWER SURFACE CORRODED AT NUT PLATE HOLES. REMOVED CORROSION IAW SRM 53- 00-51. REMAINING DAMAGE WAS OU
- [SDR UALA2012123107458](https://openairdocs.org/sdr/UALA2012123107458), Dec 28, 2012: SKIN. CORRODED. EMPENNAGE TAIL COMP FWD STA 1825 BETWEEN 3R & 5R STR SKIN HAS CORROSION UNDER APU INLET ATTACH FLANGE. MAJOR REPAIR ACCOMPLISHED: REMOVED CORROSION AT STA 1825 
- [SDR UALA2012120607057](https://openairdocs.org/sdr/UALA2012120607057), Dec 4, 2012: ANGLE. CORRODED. MAIN CABIN FLOOR STRUCTURE STA 301 RBL 60 CREASE BEAM INNER CORD ANGLE HAS CORROSION. INSTALLED NEW CORD ANGLE IAW DWS141N8422 AND SRM 51-40-02.
- [SDR UALA2012120306917](https://openairdocs.org/sdr/UALA2012120306917), Dec 1, 2012: STIFFENER. CORRODED. PASSENGER COMP BS 1664+9 RBL 61 THRESHOLD SUPPORT HAS UPPER SURFACE CORROSION AROUND FASTENER HOLE. MAJOR REPAIR ACCOMPLISHED. REMOVED AND REPLACED NEW STIFFENE
- [SDR UALA2012120406958](https://openairdocs.org/sdr/UALA2012120406958), Nov 29, 2012: ATTACH FITTING. CORRODED. PASSENGER COMP BS 1681.8 MINUS 10' LBL 61 THRESHOLD ATTACH FITTING CORRODED. REMOVED & REPLACED ATTACH FITTING P/N 146N8769U47 ATA9-A26091 IAW DWG 146N8722 AND 
- [SDR UALA2012113006894](https://openairdocs.org/sdr/UALA2012113006894), Nov 29, 2012: ATTACH FITTING. CORRODED. PASSENGER COMP BS 1681.8 MINUS 10" LBL 61 THRESHOLD ATTACH FITTING CORRODED. REMOVED & REPLACED ATTACH FITTING P-N 146N8769U47 ATA9-A26091.
- [SDR UALA2012110606374](https://openairdocs.org/sdr/UALA2012110606374), Nov 5, 2012: LIGHT. INOPERATIVE. EMERGENCY LIGHTS OVERHEAD 6A, 3, E, F INOPERATIVE.
- [SDR UALA2012102206019](https://openairdocs.org/sdr/UALA2012102206019), Oct 21, 2012: STRUCTURE. CRACKED. CRACK NOTED ON RIGHT SIDE EXHAUST AREA ON LEFT ENGINE. MEASURED LENGTH OF CRACK DETERMINED TO BE 1.75 INCHES. REF SRM 54-31-01 THIS IS WITHIN SERVICEABLE LIMITS
- [SDR UALA2012100505659](https://openairdocs.org/sdr/UALA2012100505659), Oct 4, 2012: DOOR. OBSTRUCTED. DOOR 4L NOT ARMING CORRECTLY. CLEANED OBSTRUCTION ON BOTTOM OF DOOR SILL, OPERATED DOOR SEVERAL TIMES, OKAY.
- [SDR UALA2012072604063](https://openairdocs.org/sdr/UALA2012072604063), Jul 25, 2012: BYPASS VALVE. LEAKING. FOUND RT ENGINE FUEL OIL COOLER LEAKING. REMOVED AND REPLACED RT FUEL/OIL COOLER BYPASS VALVE. OPS CHECKED GOOD.
- [SDR UALA2012071803904](https://openairdocs.org/sdr/UALA2012071803904), Jul 16, 2012: DUCT. CRACKED. LEFT PACK HOT AIR LINE FROM CONDENSOR TO COMPRESSOR OUTLET DUCT IS CRACKED AND ALSO TUBE THAT CONNECTS TO CONDENSOR HAS A HOLE WORN THROUGH IT BLOWING HOT AIR.
- [SDR UALA2012070103500](https://openairdocs.org/sdr/UALA2012070103500), Jun 30, 2012: IDG. FAULTED. RIGHT GEN FAIL ON TAKEOFF ROLL AT 75 KNOTS. SERVICED IDG OIL TO FULL, RAN NR 2 ENG FOR IDG TEST, OPS CHECKS OKAY. CF CREATED TO RE-CHECK OIL LEVEL IN IDG WITHIN
- [SDR UALA2012062903429](https://openairdocs.org/sdr/UALA2012062903429), Jun 22, 2012: TRANSMITTER. FAILED. ENGINE OIL PRESSURE READS 9 PSI STATIC ENG :REF: MIT 79-32-00-500A. OIL TRANSMITTER REPLACED 25 HRS. REPLACED NR 2 ENGINE OIL PRESSURE TRANSMITTER, LEAK CHECKED
- [SDR UALA2012021000801](https://openairdocs.org/sdr/UALA2012021000801), Feb 9, 2012: ACCESSORY UNIT. MALFUNCTIONED. CABIN INTERPHONE INOPERATIVE. REPLACED AUDIO ACCESSORY UNIT, CHECKS OKAY OPBLM.

All 112: https://openairdocs.org/deregistered/N520UA-2018-08-28/reports.md

## 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 20111221029339I](https://openairdocs.org/incident/20111221029339I), Dec 21, 2011: Boeing 757-222 (N520UA), Spokane, WA, No damage. The aircraft departed geg. During gear and flap retraction, the aircraft lost hydraulic pressure and quantity on the left hydraulic system. The crew returned…
- [Incident 20060222002579I](https://openairdocs.org/incident/20060222002579I), Feb 22, 2006: Boeing 757222 (N520UA), Omaha, NE. (-23) N520UA, B-757-222, being operated as united airlines flight 696 enroute from den to oma advised ATC that they had a flight control problem. The crew had…

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