# N522US: 1987 Boeing 757-251, registration cancelled 2017-07-21 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: July 21, 2017 - Status when cancelled: Valid registration - Airframe: [Boeing 757-251](https://openairdocs.org/model/boeing-757-251) (registry code 1384970) - Engine: [Amateur-built UNKNOWN ENG](https://openairdocs.org/engine/amateur-built-unknown-eng) (registry code 99999) - Data sheets: [TCDS A2NM](https://openairdocs.org/tcds/A2NM) (OpenAirDocs) - Serial number: 23616 - Year built: 1987 - Type of aircraft: Fixed wing multi engine - Airworthiness: Standard, transport - Airworthiness date: January 14, 1987 - Certificate issued: September 9, 2016 - Last registry action: September 9, 2016 - Mode S code: A6922F - Owner when cancelled: [Delta Air Lines Inc](https://openairdocs.org/faa-owner/DELTA%20AIR%20LINES%20INC) - Location: [Atlanta, GA](https://openairdocs.org/faa-place/GA/Atlanta) - Owner type: Corporation - Owner's area on the map: 33.6604° N, 84.3865° W: Placed by OpenAirDocs at the center of ZIP code 30354, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N522US - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=522US - Page: https://openairdocs.org/deregistered/N522US-2017-07-21 From the FAA registry file of October 29, 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 757-251: https://openairdocs.org/model/boeing-757-251.md ## Service difficulty reports (42) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DALA14036405522](https://openairdocs.org/sdr/DALA14036405522), Jun 17, 2014: BATTERY PACK. INOPERATIVE. FOUND EMERGENCY LIGHTS, FLOOR, FROM ROW 22 TO FWD OF THE R3 DOOR INOPERATIVE. R & R BATTERY PACK IAW AMM 35-51. OPS CHECKED GOOD, OK FOR SERVICE. - [SDR DALA14027385522](https://openairdocs.org/sdr/DALA14027385522), Apr 30, 2014: PLATE. CORRODED. L1 DOOR LOWER HINGE LOWER CAM PLATE RUSTED. REMOVED CORROSION FROM LOWER CAM PLATE AT L1 DOOR IAW ERA 476391-14MA, REV B, SECTION 1. PAINTED AND REPAIRED LOWER - [SDR DALA14027005522](https://openairdocs.org/sdr/DALA14027005522), Apr 29, 2014: CAM. CORRODED. R1 DOOR LOWER HINGE UPPER AND LOWER CAM PLATES RUSTED. REMOVED CORROSION IAW ERA 476391-14MA, REV B. CORROSION LEVEL 1. REPAIRED IAW ERA 476391-14MA, REV B, SEC - [SDR DALA14010625522](https://openairdocs.org/sdr/DALA14010625522), Feb 18, 2014: WIRE. BROKEN. EMERGENCY LIGHT HAS A BROKEN WIRE. REPAIRED WIRING AT 20D. INSTALLED NEW LAMP. OK FOR SERVICE. - [SDR DALA14007015522](https://openairdocs.org/sdr/DALA14007015522), Jan 31, 2014: LIGHT. INOPERATIVE. DURING SERVICE CHECK, FOUND EMERGENCY LIGHT 26L BULLNOSE INOPERATIVE. SECURED 26L BULLNOSE EMERGENCY LIGHT, OPS CHECKED GOOD, OK FOR SERVICE. - [SDR DALA13044435522](https://openairdocs.org/sdr/DALA13044435522), Sep 12, 2013: SKIN. SCRATCHED. FOUND A 7 INCH LONG SCRATCH IN FUSELAGE APPOXIMATELY 12 INCHES AFT OF L3 COCKPIT WINDOW LOWER AFT CORNER AND 10 INCHES BELOW LAP SEAM. BLENDED AND ACCOMPLISHED - [SDR DALA13033975522](https://openairdocs.org/sdr/DALA13033975522), Jul 7, 2013: CONNECTOR. LOOSE. EMERGENCY LIGHTS ARE NOT LIGHTING IN THE AFT PART OF CABIN RESEATED CONNECTOR PLUG AT BATTERY PACK M734 IN AFT GALLEY OVERHEAD OPERATED LIGHTS ON AND OFF SEVERA - [SDR DALA13031445522](https://openairdocs.org/sdr/DALA13031445522), Jun 20, 2013: STRUCTURE. PUNCTURED. ACS REPORTED FORWARD CARGO DOOR C1, AFT LOWER CORNER EDGE PUNCTURED .75 X .25. ACFT PREPARED FOR MX FERRY FOR MAJOR REPAIRS. ACFT CURRENTLY OUT OF SERVICE. - [SDR DALA13006585522](https://openairdocs.org/sdr/DALA13006585522), Feb 10, 2013: BATTERY PACK. INOPERATIVE. DOOR 4L EMERGENCY EXIT LIGHT INOPERATIVE. R & R BATTERY PACK, OPS CHECKED GOOD IAW AMM 33-51. - [SDR DALA12007405522](https://openairdocs.org/sdr/DALA12007405522), Sep 16, 2012: SPAR CAP. CORRODED. REAR SPAR CAP CORRODED AT RT HORIZONTAL STAB STA 318.949, COMPLIED WITH ERA 506884-14 REV. ORIG STEPS 1-14 ON PRI ERA 506884-14 REV ORIG AND REV 1. - [SDR DALA12006965522](https://openairdocs.org/sdr/DALA12006965522), Sep 11, 2012: SILL. CORRODED. SMALL AREA OF CORROSION NR 2 CARGO DOOR LOWER SILL BS 1420. CLEANED AREA, REMOVED CORROSION PER SRM 53-60-15. AREA OUT OF LIMITS PER SRM 53-60-15. REMOVED FITTI - [SDR DALA1238905522](https://openairdocs.org/sdr/DALA1238905522), Jun 23, 2012: CONNECTOR. DAMAGED. DURING FLIGHT, EMERGENCY EXIT DOOR AND CELING LIGHTS COME ON AT DOOR 3 BOTH SIDES AND DOOR 2 RIGHT SIDE. EMERGENCY EXIT FLOOR LIGHTS COME ON IN FLIGHT FROM DOOR - [SDR DALA1159625522](https://openairdocs.org/sdr/DALA1159625522), Oct 24, 2011: BATTERY PACK. DISCHARGED. EXIT LIGHT ABOVE L3 DOOR INOP. REPLACED BATTERY PACK PER AMM 33-51. OPS CHECK NORMAL. - [SDR DALA1106595522](https://openairdocs.org/sdr/DALA1106595522), Jan 27, 2011: POWER SUPPLY. INOPERATIVE. DURING A LINE CHECK, MX FOUND THE EMERGENCY PATH LIGHTS BETWEEN ROWS 22 AND 32 INOPERATIVE. MX REPLACED THE POWER SUPPLY. OPS CHECK WAS GOOD. - [SDR DALA1102185522](https://openairdocs.org/sdr/DALA1102185522), Nov 24, 2010: TAB. DELAMINATED. LT ELEVATOR CONTROL TAB DELAMINATED APPROX 8 SQUARE INCHES. R & R RT ELEVATOR CONTROL TAB IAW AMM 27-30-03. ADJUSTMENT/TEST GOOD IAW MM 27-30-03-201 CORRECTED B - [SDR DALA1023405522](https://openairdocs.org/sdr/DALA1023405522), Sep 18, 2010: BATTERY PACK. INOPERATIVE. DURING A LINE CHECK, MX FOUND THE EMERGENCY EXIT LIGHT AT DOOR 2 LT INOPERATIVE. MX REPLACED THE BATTERY AND POWER SUPPLY. OPS CHECK WAS GOOD. - [SDR DALA1023315522](https://openairdocs.org/sdr/DALA1023315522), Sep 17, 2010: GATE. CORRODED. DURING M-CHECK FOUND CORROSION ON R1 DOOR LOWER GATE. REPAIRED IAW SRM 51-40-02, SRM 52-11-38-004. - [SDR DALA1022275522](https://openairdocs.org/sdr/DALA1022275522), Sep 12, 2010: BULKHEAD WEB. DAMAGED. DURING M-CHECK FOUND DAMAGE TO BULKHEAD WEB IN NR 2 PYLON MID SPAR BULKHEAD FITTING FWD FACE. REPAIRED IAW ERA 484910-14. - [SDR DALA1022265522](https://openairdocs.org/sdr/DALA1022265522), Sep 10, 2010: SKIN. DENTED. DURING M-CHECK FOUND DENT AND SCRATCH ON FUSELAGE SKIN AT BS 620 S16L. REPAIRED IAW ERA 484243-14. - [SDR DALA1020805522](https://openairdocs.org/sdr/DALA1020805522), Aug 31, 2010: FLOOR SUPPORT. CORRODED. CORROSION ON CABIN FLOOR SUPPORT BEAM FROM STA 345-377 BL'0'. REMOVED CORROSION FROM FLOOR SUPPORT BEAM BL'0' BTW STA 345-377 IAW SRM 51-10-02. ORIGINAL MAT. .0 - [SDR DALA1020795522](https://openairdocs.org/sdr/DALA1020795522), Aug 31, 2010: FLOOR SUPPORT. CORRODED. CORROSION ON CABIN FLOOR SUPPORT BEAM STA 405 RBL24 STA BFM. REMOVED CORROSION DIM. L=2.5" W=.800" D=.071" FOUND TO BE OUT LIMITS IAW SRM 53-00-51. REMOVED FLOO - [SDR DALA1020785522](https://openairdocs.org/sdr/DALA1020785522), Aug 31, 2010: FLOORBEAM. CORRODED. CORROSION ON CABIN FLOORBEAM STA 377,BL'0' TO LBL18 AND AT RBL13. RII: Y BLENDED AREA ORG .125 L=3" X W=1.2" X D=.035 REMAINING .090 OUT OF LIMITS IAW SRM 53-00 - [SDR DALA1020775522](https://openairdocs.org/sdr/DALA1020775522), Aug 28, 2010: WEDGE. DAMAGED. RT WING, SLAT NR7, T/E WEDGE, APPROX 36" FROM OTBD EDGE IS DAMAGED. REMOVED DAMAGED SKIN AND CORE AND BONDED NEW CORE INTERNAL DOUBLER FILLER AND EXTERNAL DOUBL - [SDR DALA1020765522](https://openairdocs.org/sdr/DALA1020765522), Aug 28, 2010: SKIN. DAMAGED. RT WING SLAT NR 7 T/E WEDGE, APPROX 36" FROM INBD EDGE IS DAMAGED. REMOVED DAMAGED SKIN AND CORE AND BONDED NEW CORE, INTERNAL DOUBLER FILLER, AND EXTERNAL DOUB - [SDR DALA1020755522](https://openairdocs.org/sdr/DALA1020755522), Aug 28, 2010: WEDGE. DAMAGED. RT WING SLAT NR 8 T/E WEDGE APPROX 36" FROM INBD EDGE IS DAMAGED. RII: Y. REMOVED INNER SKIN, CORE AND EXTERNAL SKIN. FABRICATED NEW SKIN AND CORE AND BONDED IA - [SDR DALA1020745522](https://openairdocs.org/sdr/DALA1020745522), Aug 28, 2010: FLOORBEAM. CORRODED. CORROSION ON CABIN FLOORBEAM UPPER CHORD AT STA 365 FROM RBL 63-BL'0'. BLENDED AREA DIM. L=5' W=2" D=.060" FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, REMOVED O - [SDR DALA1020515522](https://openairdocs.org/sdr/DALA1020515522), Aug 26, 2010: FLOORBEAM. CORRODED. DURING "M" CHECK FOUND CORROSION ON FLOORBEAM AT BS 1640. REPAIRED IAW SRM 51-40-02 & SRM 53-00-01, FIG 201. - [SDR DALA1020505522](https://openairdocs.org/sdr/DALA1020505522), Aug 26, 2010: WEB. CORRODED. DURING "M" CHECK FOUND CORROSION ON FLOOR WEB AT BS 1718 BL 0 TO RBL 31. REPAIRED IAW SRM 51-40-02, SRM 53-60-51 REPAIR NR 2. - [SDR DALA1020495522](https://openairdocs.org/sdr/DALA1020495522), Aug 26, 2010: FLOORBEAM. CORRODED. DURING M-CHECK FOUND CORROSION ON FLOORBEAM UPPER CHORD BS 345 BL 0 TO LBL 18. REPAIRED IAW SRM 53-00-51 REPAIR NR 5. - [SDR DALA1020325522](https://openairdocs.org/sdr/DALA1020325522), Aug 24, 2010: WEB. CORRODED. DURING M-CHECK, FOUND CORROSION ON WEB AT STRINGER 27R BETWEEN BS 1360 & BS 1380. REPAIRED IAW SRM 51-40-02. - [SDR DALA1019535522](https://openairdocs.org/sdr/DALA1019535522), Aug 17, 2010: SKIN. DENTED. DURING M-CHECK FOUND DENT IN LOWER FUSELAGE SKIN BETWEEN BS 660 & BS 680 STRINGER 23L & STRINGER 24L. REPAIRED IAW SRM 53-00-01 FIG 201, SRM 51-42-11. - [SDR 0103795522](https://openairdocs.org/sdr/0103795522), Oct 22, 2001: SLIDE. RUPTURED. DURING SLIDE SHOP TEST, INFLATABLE SUB ASSEMBLY SEAM RUPTURED AT NORMAL OPERATING PRESSURE. NEW INFLATABLE SUB ASSEMBLY WAS INSTALLED. - [SDR 0101295522](https://openairdocs.org/sdr/0101295522), Apr 4, 2001: ANNUNCIATOR. SMOKE. UPON ARRIVAL TO GATE, FLIGHT CREW NOTICED SMOKE COMING FROM THE LANDING GEAR CONTROL HANDLE OPENING. FIRE EQUIPMENT WAS CALLED OUT. AFTER SHUTDOWN OF ENGINE, AP - [SDR 9719055522](https://openairdocs.org/sdr/9719055522), Oct 13, 1997: FSEU. MALFUNCTIONED. DURING FINAL APPROACH, L/E FLAP ASSYM ANNUNCIATED. FLIGHT CREW DECLARED AN EMERGENCY AND PERFORMED AN UNEVENTFUL LANDING. MAINTENANCE REMOVED AND REPLACED NR 1 - [SDR 9719045522](https://openairdocs.org/sdr/9719045522), Oct 12, 1997: FSEU. MALFUNCTIONED. DURING FINAL APPROACH, L/E FLAP ASSYM AND LEADING EDGE CAUTION LIGHT ILLUMINATED. GO-AROUND ACCOMPLISHED FOLLOWED BY UNEVENTFUL LANDING. MAINTENANCE REPLACED NR - [SDR 9716945522](https://openairdocs.org/sdr/9716945522), Sep 8, 1997: FITTING. CORRODED. DURING TRANSITION CHECK, FOUND CORROSION ON THE THIRD FROM FORWARD FITTING AT THE FORWARD CARGO DOOR THRESHOLD AT FS 580. REPLACED FITTING PER SRM 51-10-00. - [SDR 9716935522](https://openairdocs.org/sdr/9716935522), Sep 8, 1997: FITTING. CORRODED. DURING TRANSITION CHECK, FOUND CORROSION ON THE SECOND FROM AFT FITTING AT THE FORWARD CARGO DOOR THRESHOLD FS 610. REPLACED FITTING PER SRM 51-10-00. - [SDR 9716925522](https://openairdocs.org/sdr/9716925522), Sep 8, 1997: FITTING. CORRODED. DURING TRANSITION CHECK, FOUND CORROSION ON THE SECOND FROM FORWARD FITTING AT THE FORWARD CARGO DOOR THRESHOLD FS 570. REPLACED FITTING PER SRM 51-10-00. - [SDR 9717315522](https://openairdocs.org/sdr/9717315522), Sep 4, 1997: FLOORBEAM. CORRODED. DURING TRANSITION CHECK, FOUND CORROSION ON TOP OF FLOORBEAM AT SEVERAL LOCATIONS FROM LBL 54 TO RBL 24, FS 1680. REPAIRED PER EA 55-151991. - [SDR 9610005522](https://openairdocs.org/sdr/9610005522), Apr 26, 1996: FLOOR BEAM. CORRODED. DURING P-CHECK, FOUND CORROSION ON THE BS 1681 FLOOR BEAM UPPER CHORD AT LBL 32. REPAIRED CHORD (P/N 146N5091) PER EA 55-102159. - [SDR 9510465522](https://openairdocs.org/sdr/9510465522), Jul 8, 1995: OUTFLOW ACT. MALFUNCTIONED. DURING CLIMB, BOTH AUTO PRESSURE CONTROLLERS WERE INOPERATIVE WITH CABIN AUTO INOPERATIVE STATUS MESSAGE. AIRCRAFT RETURNED TO MSP. REPLACED OUTFLOW VALVE ACTUA - [SDR 9508755522](https://openairdocs.org/sdr/9508755522), May 28, 1995: BLEED VALVE. FAILED. DURING CLIMB, THE NR 2 COMPRESSOR STALLED TWICE. TWO LOUD BANGS AND A BRIGHT FLASH WERE OBSERVED. NO ABNORMAL ENGINE INDICATIONS WERE OBSERVED. AIRCRAFT WAS RET ## 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. - [Accident 20070603015099A](https://openairdocs.org/incident/20070603015099A), Jun 3, 2007: Boeing 757251 (N522US), Denver, CO, No damage. (-23) Flight 1221 encountered unforecast, moderate turbulence during descent between 10,000-7,000 feet while descending into den. While passing 7,000' and… - [Incident 19880808039819I](https://openairdocs.org/incident/19880808039819I), Aug 8, 1988: Boeing 757251 (N522US), Las Vegas, NV. Lost oil pressure. Diverted. Found chip detector unit came loose due cross threading. APU unit also malfunctioned. ## Other aircraft with N522US - [Registered now](https://openairdocs.org/aircraft/N522US): Costruzioni Aeronautiche Tecna P2008, S/N 225, built 2025 --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.