# N522UA: 1990 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: 24931
- Year built: 1990
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 19, 1990
- Last registry action: January 12, 2018
- Mode S code: A6921F
- Location: [Oklahoma City, OK](https://openairdocs.org/faa-place/OK/Oklahoma%20City)
- Owner type: Individual
- Owner's area on the map: 35.4253° N, 97.6495° W: Placed by OpenAirDocs at the center of ZIP code 73179, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N522UA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=522UA
- Page: https://openairdocs.org/deregistered/N522UA-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 (125, newest 50)

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

- [SDR CALA2014072191478](https://openairdocs.org/sdr/CALA2014072191478), Jul 18, 2014: LIGHT. INOPERATIVE. DOOR 4L EXTERIOR EMER EXIT LIGHT INOPERATIVE. RELAMPED EXTERIOR EMER LIGHT. OPERATIONS CHECKED OK.
- [SDR CALA2014063091373](https://openairdocs.org/sdr/CALA2014063091373), Jun 29, 2014: BLEED AIR SYS. MALFUNCTIONED. CREW REPORT APU BLEED AIR INOPERATIVE ON GATE. APU ELEC OK. CYCLED BLEED SWITCH WITH NORMAL PRESS EACH TIME. RAN PACK MAINTAINED 28 PSI. TAXI CREW INDICATING NO
- [SDR CALA2014062091320](https://openairdocs.org/sdr/CALA2014062091320), Jun 20, 2014: FLOORBEAM. CORRODED. CORROSION ON FLOORBEAM LOWER SURFACE BS 1860 RBL 42 IN MAIN CABIN. R & R THE UPPER CHORD OF BS 1681 FLOORBEAM IAW ECRA 5300-01939.
- [SDR CALA2014062091319](https://openairdocs.org/sdr/CALA2014062091319), Jun 20, 2014: SKIN. DENTED. DENTS IN EXTERNAL SKIN DOUBLER ON FS 215.25, 15 INCHES BELOW WL LT SIDE. REPAIRED EXT FUSELAGE SKIN FROM BS 207 TO 234, STRINGER 17L. THE FUSELAGE SKIN REPAIR R
- [SDR CALA2014062091318](https://openairdocs.org/sdr/CALA2014062091318), Jun 20, 2014: SKIN. DENTED. DENTS IN EXTERNAL SKIN FS 200.37, 44 INCHES BELOW WL L-H SIDE. REPAIRED FUSE SKIN AT BS 199 - 205 FROM STRINGER 26L & 27L IAW ECRA5311-01697. BS 199 - 205, STRI
- [SDR CALA2014061391259](https://openairdocs.org/sdr/CALA2014061391259), Jun 10, 2014: STRINGER SPLICE. CRACKED. BS 1681, RBL 70 STRINGER SPLICE CRACKED AT ATTACHMENT HOLES. R & R SPLICE CHANNEL PN 146N 3820-86 IAW SRM 51-40-02, PAR 7C FIG 3 & 12 & DWG 146N3820.
- [SDR CALA2014060991247](https://openairdocs.org/sdr/CALA2014060991247), Jun 8, 2014: SKIN. DENTED. DENT IN EXTERNAL FUSELAGE SKIN AT BS 570 BETWEEN STRINGER 23L & 24L. REPAIRED EXTERNAL FUSELAGE SKIN AT BS 570 BETWEEN STRINGER 23L& 24L IAW SRM 53-00-01 FIG 20
- [SDR CALA2014060291190](https://openairdocs.org/sdr/CALA2014060291190), May 29, 2014: ATTACH ANGLE. CORRODED. CORROSION ON FLOORBOARD ATTACH ANGLE BS 1183 RBL 64 IN MAIN CABIN. BS 1183 RBL 64 CREASE BEAM. INSTALLED REPAIR CORD & 3 SPLICE REPAIR STRAP BETWEEN BS 1180 - 1
- [SDR CALA2014051991070](https://openairdocs.org/sdr/CALA2014051991070), May 19, 2014: FLOORBEAM. SCRATCHED. SCRATCHES ON TOP OF MAIN CABIN FLOORBEAM AT BS 680 BETWEEN LBL 23 TO RBL 23. REPAIRED CABIN FLOORBEAM BS 680 RBL 24 IAW ECRA 5310-05536. REMOVED SCRATCHES ON FL
- [SDR CALA2014031090571](https://openairdocs.org/sdr/CALA2014031090571), Mar 10, 2014: SLIDE. OUT OF POSITION. FOUND SLIDE PACK OUT OF UPPER GUIDE PLATES, INTERFERING WITH LOWER GATE & GIRT OPERATION. REPLACED SLIDE IAW MM 25-66-01. DOOR OPERATES NORMALLY FROM INSIDE OR 
- [SDR CALA2014012490218](https://openairdocs.org/sdr/CALA2014012490218), Jan 24, 2014: LIGHT. BROKEN. EMERGENCY EXIT LIGHT STRIP BROKEN AT DOOR, FWD AFT LAVATORY. PERMANENT REPAIR SPLICE INSTALLED ICW AMM 33-51-96, OPERATIONS OK.
- [SDR CALA2013123094038](https://openairdocs.org/sdr/CALA2013123094038), Dec 29, 2013: ATTACH BOLT. LOOSE. FOUND FWD ATTACH BOLT LEAKING. NR 7 FLAP TRACK CLEANED & RESEALED ALL FOUR FWD ATTACH BOLTS AT NR 7 FLAP TRACK.
- [SDR CALA2013120593498](https://openairdocs.org/sdr/CALA2013120593498), Dec 3, 2013: SLIDE. LOW PRESSURE. SLIDE PACK GAUGE IN RED 4L. REPLACED L4 DOOR SLIDE, OK TO CONTINUE.
- [SDR CALA2013110892753](https://openairdocs.org/sdr/CALA2013110892753), Nov 8, 2013: BLADE. BENT. LT ENG HAS BENT BLADE. IAW MM 72-31-02 FOR ALLOWABLE LIMITS. BLENDED LE AT AREA 1 IAW AMM 72-31-02, DAMAGE REMOVAL IS WITHIN LIMITS.
- [SDR CALA2013103092527](https://openairdocs.org/sdr/CALA2013103092527), Oct 29, 2013: LIGHT. BURNED. POSSIBLE ELECTRICAL SMOKE SMELL, SOURCE NOT IDENTIFIED. SMELL DISSIPATED NO OBVIOUS IRREGULARITIES NOTED. DID FIND NO SMOKING FASTEN SEAT SIGN LIGHT BULBS BURNT
- [SDR CALA2013102192202](https://openairdocs.org/sdr/CALA2013102192202), Oct 16, 2013: FUEL LINE. LEAKING. LT WING HAS EVIDENCE OF FUEL LEAKING OUT OF TWO DRY BAY DRAIN HOLES.. REPLACED MAIN ENG FUEL LINE THRU DRY BAY, LEAK CHECKED OK.
- [SDR CALA2013093091542](https://openairdocs.org/sdr/CALA2013093091542), Sep 26, 2013: LIGHT. LOOSE. EMERGENCY EXIT LIGHT STRIP LOOSE 32 ROW. REPLACED 3' SECTION OF EMERGENCY EXIT LIGHT COVER & ONE PIECE OF MISSING EMERGENCY EXIT LIGHT STRIP. CHECKED EMERGENCY 
- [SDR UALA2013071905090](https://openairdocs.org/sdr/UALA2013071905090), Jul 18, 2013: LAMP. INOPERATIVE. LAMPS INSIDE ARM LIGHT BURNED OUT. REPLACED LAMP, OP CHECKED NORMAL. SLIDE ARMS NORMALLY.
- [SDR UALA2013070804722](https://openairdocs.org/sdr/UALA2013070804722), Jul 5, 2013: PANEL. DAMAGED. ON 2 SRV WALK AROUND FOUND THREE GOUGES ON INLET COWL ACOUSTIC PANELS AT 7, 5 AND 10 O'CLOCK POSITIONS.
- [SDR UALA2013070204616](https://openairdocs.org/sdr/UALA2013070204616), Jun 28, 2013: WIRE. BROKEN. NO MAIN BATTERY VOLTS DISPLAYED ON EICAS ELEC PAGE. BROKEN WIRE FROM D40246P TO D40904P, REF WD 24-34-11. ACCOMPLISHED WIRING INTERIM REPAIR IAW ECRA 2434-01044
- [SDR UALA2013062004310](https://openairdocs.org/sdr/UALA2013062004310), Jun 19, 2013: OXYGEN SYSTEM. MALFUNCTIONED. CREW OXYGEN AT 0 THEN 1670 PSI. VISUALLY INSPECTED CREW OXYGEN BOTTLE AND OTHER OXYGEN COMPONENTS. NO DISCREPANCIES NOTED. R & R OXYGEN TRANSDUCER. LEAK AND OPS
- [SDR UALA2013060703964](https://openairdocs.org/sdr/UALA2013060703964), Jun 6, 2013: CONTROLLER. INOPERATIVE. LEFT WINDOW HEAT IS INOPERATIVE. LEFT CONTROLLER WILL NOT SELF TEST, REPLACED CONTROLLER IAW AMM. TESTED GOOD. NOW SHOWING LT SIDE WINDOW NR 3 FAILURE.
- [SDR CALA2013082690770](https://openairdocs.org/sdr/CALA2013082690770), May 12, 2013: NUT. CRACKED. WHEEL TIE BOLT NUT CRACKED 4 COUNTERCLOCKWISE FROM VALVE STEM MARKED. REPLACED WHEEL & TIRE ASSEMBLY IAW MM.
- [SDR UALA2013042302834](https://openairdocs.org/sdr/UALA2013042302834), Apr 22, 2013: LIGHT. DAMAGED. EMERGENCY LIGHT ASSY IN FRONT OF LAVATORY INOPERATIVE. FOUND LIGHT ASSY LEADS DAMAGED. LIGHT ASSY 30 INCH LONG. REPLACED LIGHT ASSY, GROUND CHECKED NORMAL.
- [SDR UALA2013032001701](https://openairdocs.org/sdr/UALA2013032001701), Mar 19, 2013: STRAP. CRACKED. AFT CARGO COMPARTMENT AT BS 1380 WL 199 RBL 46 STABILIZER STRAP IS CRACKED & BROKEN. INSTALLED STABILIZER STRAP REPAIR IAW ECRA 5315-01063.
- [SDR UALA2013031801639](https://openairdocs.org/sdr/UALA2013031801639), Mar 17, 2013: PANEL. CRACKED. RIGHT HORIZONTAL STABILIZER FORWARD LOWER SLIDING PANEL CRACKED BS 1780, STR 17R. REPAIRED RIGHT HORIZONTAL STABILIZER FORWARD LOWER SLIDING PANEL IAW ECRA 5387
- [SDR UALA2013031801620](https://openairdocs.org/sdr/UALA2013031801620), Mar 16, 2013: SKIN. MISREPAIRED. SKIN MISREPAIRED BS 1657 BETWEEN STR 29R AND 29L. REPAIRED IAW REO-M0611 AND ECRA NR 5361-01045.
- [SDR UALA2013031801619](https://openairdocs.org/sdr/UALA2013031801619), Mar 16, 2013: STRUCTURE. CORRODED. CORROSION ON AFT CARGO BAY DOOR CUT THRESHOLD UPPER STRUCTURE BS 1398, RBL 21, WL 146. BLENDED MEASUREMENT ON AFT CARGO BAY DOOR CUT THRESHOLD UPPER STRUCTURE B
- [SDR UALA2013031501574](https://openairdocs.org/sdr/UALA2013031501574), Mar 14, 2013: FLOOR SUPPORT. CORRODED. CORROSION ON LONGERON BETWEEN BS 350-365 RBL 61 4 EACH. MAJOR REPAIR ACCOMPLISHED. REMOVED & REPLACED LONGERON BETWEEN BS 350 AND BS 365 RBL 61 IAW B757-200 SRM
- [SDR UALA2013031501573](https://openairdocs.org/sdr/UALA2013031501573), Mar 14, 2013: SUPPORT. CORRODED. CORROSION AT RIGHT NR 4 DOOR SILL SUPPORT BS 1640 TO BS 1680. REMOVED AND REPLACED DOOR SILL SUPPORT AT RIGHT NR 4 DOOR IAW B757-200 SRM 51-40-02 PAR 7D FIG 12.
- [SDR UALA2013031401534](https://openairdocs.org/sdr/UALA2013031401534), Mar 14, 2013: FLOORBEAM. CORRODED. CORROSION ON REPAIR DOUBLER ON FLOORBEAM BS 366 RBL 26. MAJOR REPAIR ACCOMPLISHED. REMOVED AND REPLACED REPAIR DOUBLER ON FLOORBEAM AT STA 366 RBL 26 IAW TIMCO 
- [SDR UALA2013031401533](https://openairdocs.org/sdr/UALA2013031401533), Mar 14, 2013: ATTACH BRACKET. CORRODED. CORROSION ON AFT CARGO COMPARTMENT DOOR CENTER AFT THRESHOLD ATTACH BRACKET BS 1420. REMOVED AND REPLACED AFT CARGO DOOR CENTER AFT THRESHOLD ATTACH BRACKET BS 
- [SDR UALA2013031401531](https://openairdocs.org/sdr/UALA2013031401531), Mar 14, 2013: WEB. CORRODED. CORROSION ON AFT CARGO BAY WEB AT BS 1449 RBL 22 WL 147. REMOVED AND REPLACED WEB IN AFT CARGO BAY AT BS 1449 RBL 22 WL 147 IAW B757-200 SRM 51-40-02 PAR 4 AND 
- [SDR UALA2013031401507](https://openairdocs.org/sdr/UALA2013031401507), Mar 13, 2013: PLATE. DENTED. RAMP REPORTS SMALL DENT ON FWD CARGO COMPMENT SCUFF PLATE MEASURES APPROX 1.25 LONG. DEPTH IS APPROX 3-16TH INCH. NO CRACKS NOTED. DENT IS ON FWD CARGO THRESHOL
- [SDR UALA2013031401506](https://openairdocs.org/sdr/UALA2013031401506), Mar 13, 2013: WEB. CORRODED. CORROSION ON AFT CARGO BAY WEB AT BS 1449 RBL 22 WL 147. REMOVED AND REPLACED WEB IN AFT CARGO BAY AT BS 1449 RBL 22 WL 147 IAW B757-200 SRM 51-40-02 PAR 4 AND 
- [SDR UALA2013030601329](https://openairdocs.org/sdr/UALA2013030601329), Mar 6, 2013: SKIN. DEBONDED. A 1.5 INCH DIA AREA OF DISBOND ON LOWER SURFACE T/E WEDGE OF NR 10 SLAT 8 INCHES FROM T/E AND 5 INCHES FROM OUTBD EDGE. REPAIR ON NON ROUTINE 24007 DISBONDED AR
- [SDR UALA2013030601328](https://openairdocs.org/sdr/UALA2013030601328), Mar 6, 2013: SKIN. DEBONDED. TWO INCH DIA AREA OF DISBOND ON LWR SURFACE OF NR 10 SLAT T/E WEDGE 8 INCHES FROM T/E AND 20 INCHES FROM O/B EDGE. REPAIR DISBONDED AREA ON LOWER SURFACE OF NR 
- [SDR UALA2013030601327](https://openairdocs.org/sdr/UALA2013030601327), Mar 6, 2013: WEDGE. DAMAGED. MULTIPLE DRILL HOLES ON UPPER AND LWR AFT SURFACE OF NR 10 SLAT WS 738. REPAIR UPPER AND LOWER AFT SURFACE OF NR 10 SLAT T/E WEDGE AT WS 738.
- [SDR UALA2013030601326](https://openairdocs.org/sdr/UALA2013030601326), Mar 5, 2013: SKIN. GOUGED. BS 1525-1530 HAS GOUGE HEAVY DENT BETWEEN STRINGER 23 AND 24 RIGHT. REPAIRED DAMAGE ON FUSELAGE SKIN BETWEEN BS 1525-1530 STR 23R AND 24R IAW B757-200 SRM 53-00
- [SDR UALA2013030501304](https://openairdocs.org/sdr/UALA2013030501304), Mar 5, 2013: WEB. CRACKED. MAIN CABIN WEB CRACKED BELOW FLOOR LEVEL AT FWD LIGHTNING HOLE BETWEEN STA 324 AND STA 345 BL 0. MAJOR REPAIR ACCOMPLISHED. ACP REMOVED AND REPLACED MAIN CABIN 
- [SDR UALA2013030501303](https://openairdocs.org/sdr/UALA2013030501303), Mar 2, 2013: ACTUATOR. LEAKING. RRCM P/N 3800022-108 S/N 0521 LEAKING. REMOVED AND REPLACED RUDDER RATIO CHANGER ACTUATOR IAW B757 27-21-13-002-001 AND 27-21-13-402-032. LEAK AND OPS CHECK GOO
- [SDR UALA2013030401248](https://openairdocs.org/sdr/UALA2013030401248), Mar 1, 2013: FLOORBEAM. CORRODED. CORROSION IN SEVERAL PLACES BS 1661 RBL 60 TO BL 0 FLOORBEAM. REMOVED CORROSION FOUND ALL AREAS TO BE IN LIMITS IAW B757-200 SRM 53-00-51 FIG 101 DETAI L III EX
- [SDR UALA2013030101223](https://openairdocs.org/sdr/UALA2013030101223), Feb 28, 2013: FLOORBEAM. CORRODED. CORROSION ON FLOORBEAM BS 365 BL 0-RBL 63 15EA. FLOORBEAM BS 365 BL 0 - RBL 63 IAW ECRA 5310-05536 REPAIR 3 FIG 203.
- [SDR UALA2013030101222](https://openairdocs.org/sdr/UALA2013030101222), Feb 28, 2013: STRUCTURE. CORRODED. CORROSION IN BOLT HOLES, BS 1640, BL 0 TO RBL 64 WL 208. REMOVED CORROSION AT BOLT HOLES FLOORBEAM BS 1640 RBL 64 WL 208 IAW B757-200 SRM 51-10-02-0G PAR 14 FIG
- [SDR UALA2013030101221](https://openairdocs.org/sdr/UALA2013030101221), Feb 28, 2013: STRUCTURE. CORRODED. CORROSION ON FLOORBOARD DIVIDER BS 367 RBL 61. MAJOR REPAIR ACCOMPLISHED. REMOVED AND REPLACED FLOORBOARD DIVIDER BS 367 RBL 61 IAW B757-200 SRM 51-40-02 PAR 7D
- [SDR UALA2013022801204](https://openairdocs.org/sdr/UALA2013022801204), Feb 27, 2013: FLOORBEAM. CORRODED. CORROSION IN SEVERAL PLACES, BS 1640 LBL 65 BL 0 WL 208 FLOORBEAM. MAJOR REPAIR ACCOMPLISHED. REMOVED CORROSION AT BS 1640 LBL 14, 31 AND 56 IAW B757-200 SRM 51
- [SDR UALA2013022801203](https://openairdocs.org/sdr/UALA2013022801203), Feb 27, 2013: FLOORBEAM. CORRODED. CORROSION IN SEVERAL PLACES, BS 1640 LBL 65 BL 0 WL 208 FLOORBEAM. MAJOR REPAIR ACCOMPLISHED. REMOVED CORROSION AT BS 1640 LBL 14, 31, AND 56 IAW B757-200 SRM 5
- [SDR UALA2013022701176](https://openairdocs.org/sdr/UALA2013022701176), Feb 26, 2013: FLOORBEAM. CORRODED. CORROSION ON AFT CABIN FLOORBEAM REPAIR ANGLE LOWER SURFACE BS 1680 RBL 47 WL 208. REMOVED LWR REPAIR ANGLES. LOCATED, DRILLED AND INSTALLED REPAIR ANGLE IAW SR
- [SDR UALA2013022701175](https://openairdocs.org/sdr/UALA2013022701175), Feb 26, 2013: STRUCTURE. CORRODED. CORROSION ON LONGERON BETWEEN RBL 65-72. BLENDED CORROSION ON LONGERON BS 369 IAW SRM 51-10-02 PAR 15 FIGS 1&5. REMOVED AND REPLACED LONGERON IAW SRM 51-40-02 P
- [SDR UALA2013022701171](https://openairdocs.org/sdr/UALA2013022701171), Feb 26, 2013: FLOORBEAM. CORRODED. CORROSION ON FLOORBEAM WEB UPPER SURFACE BS 1042 LBL 72. REMOVED AND REPLACED FLOORBEAM WEB IAW SRM 51-40-02 FIG 12. FABRICATED NEW FLOORBEAM WEB IAW SRM 51-30-

All 125: https://openairdocs.org/deregistered/N522UA-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 19950526018819I](https://openairdocs.org/incident/19950526018819I), May 26, 1995: Boeing 757222 (N522UA), Sidney, NE. Encountered severe turbulence. Flight attendant injured. Diverted to slc.

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