# N632DL: 1987 Boeing 757-232, registration cancelled 2017-05-16 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: May 16, 2017 - Status when cancelled: First renewal notice - Airframe: [Boeing 757-232](https://openairdocs.org/model/boeing-757-232) (registry code 1384965) - Engine: [Pratt & Whitney PW2037](https://openairdocs.org/engine/pratt-whitney-pw2037) (registry code 52117) - Data sheets: [TCDS A2NM](https://openairdocs.org/tcds/A2NM), [TCDS E17NE](https://openairdocs.org/tcds/E17NE) (OpenAirDocs) - Serial number: 23613 - Year built: 1987 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: December 3, 1987 - Certificate issued: June 23, 2010 - Last registry action: May 8, 2014 - Mode S code: A84580 - 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/N632DL - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=632DL - Page: https://openairdocs.org/deregistered/N632DL-2017-05-16 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 757-232: https://openairdocs.org/model/boeing-757-232.md ## Service difficulty reports (30) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DALA1243550632](https://openairdocs.org/sdr/DALA1243550632), Jul 30, 2012: SKIN. DAMAGED. MAINTENANCE PERFORMED A LIGHTNING STRIKE INSPECTION AND FOUND 21 LIGHTNING STRIKES ON THE CROWN OF THE AIRCRAFT BETWEEN BS 540 THROUGH 1440. COMPLIED WITH PERMA - [SDR DALA1243450632](https://openairdocs.org/sdr/DALA1243450632), Jul 27, 2012: SKIN. DAMAGED. FOUND ONE LIGHTNING STRIKE AT BS 600 AND ON S4L. REPAIRED PER ERA 5050791-14 REV 0 AND IS A TIME LIMITED REPAIR. - [SDR DALA1237050632](https://openairdocs.org/sdr/DALA1237050632), Jun 12, 2012: POWER SUPPLY. INOPERATIVE. DURING SERVICE CHECK, MAINTENANCE DISCOVERED EMERGENCY LIGHTS ON SEATS 1-6 INOPERATIVE. MAINTENANCE FOUND M9101 POWER SUPPLY INOPERATIVE. REMOVED AND REPLACED P - [SDR DALA1100170632](https://openairdocs.org/sdr/DALA1100170632), Jan 1, 2011: SKIN. DAMAGED. LOG ITEM J614634-001, POSSIBLE RT SIDE ACFT LIGHTENING STRIKE. ACFT INSPECTED IAW AMM 05-51-19. DAMAGE TRANSFERRED TO NR'S 1 THRU 9. DAMAGE ON N/R'S 1-3 AND 5-9 - [SDR DL757100874](https://openairdocs.org/sdr/DL757100874), Apr 10, 2010: B-NUT. LOOSE. AFTER T/O RAISED GEAR, MAIN GEAR DID NOT RETRACT, NOSE GEAR DID. RAN THE GEAR DISAGREE CHECKLIST, THEN GOT A L HYD QTY EICAS MSG. RAN THAT CHECKLIST. LANDED TAX - [SDR DL757091928](https://openairdocs.org/sdr/DL757091928), Dec 4, 2009: ANTI-ICE VALVE. FAILED. RT ENG ANTI ICE EICAS MESSAGE WITH SWITCH ON, CIRCUIT BREAKER POPPED, RESET BREAKER, POPPED AGAIN INSPECTED WIRES NO DEFECT NOTED SHOOK DOWN HARNESS AT D42322P. - [SDR DL757091294](https://openairdocs.org/sdr/DL757091294), Aug 1, 2009: TEE FITTING. CRACKED. REPLACED TEE CLIP 146N8748-17 WITH P/N 146N8748U17 FOR DOOR STOP NR 3 AT L4 DOOR STA 1681.8 REPLACED TEE CLIP 146N8748-21 WITH P/N 146N8748U21 FOR DOOR STOP NR - [SDR DL757060774](https://openairdocs.org/sdr/DL757060774), Sep 22, 2006: MOUNT. CORRODED. DURING THE CURRENT HMV3 CHECK, THE NR 2 PYLON P/N 311N3211 -1 FORWARD ENGINE MOUNT FITTING WAS FOUND WITH FRETTING CORROSION ON THE LOWER SURFACE AROUND THE MOU - [SDR DL757060773](https://openairdocs.org/sdr/DL757060773), Sep 22, 2006: MOUNT. CORRODED. DURING THE CURRENT HMV3 CHECK, THE NR 1 PYLON P/N 311N3211-1 FORWARD ENGINE MOUNT FITTING WAS FOUND WITH FRETTING CORROSION ON THE LOWER SURFACE AROUND THE MOUN - [SDR DL757060772](https://openairdocs.org/sdr/DL757060772), Sep 22, 2006: MOUNT. CORRODED. NR 2 ENGINE FORWARD LOWER MOUNT FITTING HAD PITTING, REMOVED BY BLENDING. ACCOMPLISHED PERMANENT REPAIR PER PRODUCTION PERMIT B757-71-25751 REF ERA 457048-14. - [SDR DL757060771](https://openairdocs.org/sdr/DL757060771), Sep 22, 2006: MOUNT. CORRODED. NR 1 ENGINE FORWARD LOWER MOUNT ON PYLON WAS BLENDED TO A DEPTH OF .003 INCHES TO REMOVE DAMAGE. ACCOMPLISHED PERMANENT REPAIR PER ACTS PRODUCTION PERMIT B757-7 - [SDR DL757060766](https://openairdocs.org/sdr/DL757060766), Sep 21, 2006: FITTING. DAMAGED. NR 2 PYLON STRUT FITTINGS HAVE ELONGATED HOLES. ACCOMPLISHED PERMANENT REPAIR PER ACTS PRODUCTION PERMIT B757-54-25720. REFERENCE ERA 456938-14. - [SDR DL757060751](https://openairdocs.org/sdr/DL757060751), Sep 15, 2006: SKIN. CRACKED. THE L1 DOOR OPENING, UPPER FORWARD CORNER, HAS A CRACK IN THE FUSELAGE SKIN. THE CRACKED SKIN WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED. - [SDR DL757060762](https://openairdocs.org/sdr/DL757060762), Sep 13, 2006: FITTING. OVERSIZED. NR 2 PYLON UPPER LINK WING FITTING WAS FOUND WITH AN INNER LUG DIA. GREATER THAN ALLOWED. THE HOLE WAS OVERSIZED AND INSPECTED. AN OVERSIZED BUSHING WAS INSTALL - [SDR DL757060744](https://openairdocs.org/sdr/DL757060744), Sep 12, 2006: FITTING. MISREPAIRED. THE NR 1 PYLON INBOARD MID SPAR FITTING WAS INCORRECTLY OVERSIZED. THE HOLE WAS OVERSIZED TO THE NEXT SIZE FASTENER AND A LARGER FASTENER WAS INSTALLED REF 2003 - [SDR DL757060322](https://openairdocs.org/sdr/DL757060322), Apr 24, 2006: WINDOW. CRACKED. DURING FLIGHT, R-1 WINDOW BEGAN TO ARC AND DELAMINATE. FOLLOW POM PROCEDURES AND TURNED OFF WINDOW HEAT. R-1 WINDOW THEN SPIDER WEB CRACKED. REPLACED R-1 WINDOW - [SDR DL757060148](https://openairdocs.org/sdr/DL757060148), Feb 20, 2006: CIRCUIT BREAKER. FAULTY. EMERGENCY LIGHTS ALONG MAIN AISLE FLOOR ILLUMINATED WITH COCKPIT SW IN ARMED POS AND FLT ATTENDANT PANEL SW IN NORMAL POS. REPLACED C/B TO CHARGER. - [SDR DL757050222](https://openairdocs.org/sdr/DL757050222), Apr 16, 2005: ANNUNCIATOR. SHORTED. ENTRY DOOR LIGHT ON OVERHEAD INDICATOR PANEL SHORTING OUT AND TRIPPING R IND LIGHT C/B. REMOVED AND REPLACED OVERHEAD IND LIGHT PANEL PER MM, CHECKS OK. - [SDR DL757040592](https://openairdocs.org/sdr/DL757040592), Jun 23, 2004: PIN. CRACKED. CRACKS WERE NOTED IN THE FUSE PINS ON THE NR 1 PYLON DIAGONAL BRACE. COMPLIED WITH ERA 091408-14AD. - [SDR DL757030257](https://openairdocs.org/sdr/DL757030257), Mar 17, 2003: ACTUATOR. UNSERVICEABLE. UNCOMMANDED ROLL TO THE RIGHT. SPOILER MESSAGE DISPLAYED. REPLACED NR 12 SPOILER PCA. ADJUSTED AND TEST PER AMM. - [SDR DL757020456](https://openairdocs.org/sdr/DL757020456), Apr 19, 2002: BOTTLE. INOPERATIVE. EMERGENCY ESCAPE TEST 2 BOTTLE PRESSURE INOP ON RIGHT SIDE. REPLACED BOTTLE ASSY PER M/M, TESTS GOOD. - [SDR DL757020369](https://openairdocs.org/sdr/DL757020369), Mar 25, 2002: SWITCH. FAULTY. ON L/O CHECK, AFT CARGO LIGHT SWITCH CAUGHT ON FIRE. REPLACED SWITCH. - [SDR DL757011048](https://openairdocs.org/sdr/DL757011048), Jun 23, 2001: OVEN. MALFUNCTIONED. F/C AFT OVEN WORKING INTERMITTENTLY, MAY HAVE SEEN SPARKS ABOVE BUN WARMER. OVEN APPEARS TO OPERATE NORMAL AT GATE. FOR PRECAUTION C/B PULLED AND COLLARED. OVEN - [SDR DL757001493](https://openairdocs.org/sdr/DL757001493), Aug 7, 2000: SKIN. DENTED. THE FUSELAGE SKIN AND UNDERLYING BEARSTRAP WERE FOUND DENTED AND GOUGED JUST FWD OF THE LOWER AFT CORNER OF THE C2 DOOR. THE DAMAGE WAS REMOVED WITH A 6 X 1 INC - [SDR DL757001494](https://openairdocs.org/sdr/DL757001494), Aug 4, 2000: SKIN. LIGHTNING STRIKE. THE FUSELAGE SKIN WAS FOUND WITH SEVERAL LIGHTNING STRIKE AREAS BETWEEN FS 440 & 460 AND BETWEEN STRINGERS 18R. THE LIGHTNING STRIKES WERE REMOVED WITH 3 SMALL - [SDR DL757992538](https://openairdocs.org/sdr/DL757992538), Nov 15, 1999: CABLE FRAYED. STAB TRIM LEVERS MOVE WHEN SPEEDBRAKE IS DEPLOYED APPEARS THAT THE LEFT STAB TRIM LEVER BINDS ACTS AS IF THE SPRING IS BROKEN. FOUND STAB TRIM CABLE STB1/STB2 M - [SDR DL757960836](https://openairdocs.org/sdr/DL757960836), Apr 10, 1996: LIGHT. INOPERATIVE. FWD RIGHT OVERWING EMERGENCY EXIT TRACK LIGHT SIGN INOP. REPLACED LIGHT ASSY, OPN OK. - [SDR DL757960449](https://openairdocs.org/sdr/DL757960449), Feb 15, 1996: SKIN. DELAMINATED. DURING SHOP INSPECTION FOR NR 2 L/E SLAT, FOUND T/E WEDGE DELAMINATED. REPAIRED PER SRM 57-43-02. - [SDR DL757952988](https://openairdocs.org/sdr/DL757952988), Jul 6, 1995: PRESS CONTROLLER. MALFUNCTIONED. LOG ITEM-CABIN PRESS EICAS MSG RED AND CABIN WARN SOUNDED AT FL 330. EMERG DESCENT ACCOMPLISHED. MANUAL CONT WORKS OK. STATUS MSG CABIN ALT AUTO 1 AND CABIN ALT - [SDR DL757951037](https://openairdocs.org/sdr/DL757951037), Mar 8, 1995: ACTUATOR. FAULTY. DURING CRUISE, HAD SVA FAILSAFE MSG, NR 2 ENGINE FLAMED-OUT. LANDED RDU. RAN ENGINE PER PFHB TEST 14 SVA, TEST NORMAL. FERRIED AC TO ATL. REPLACED STATOR VANE A ## 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 19950308009109I](https://openairdocs.org/incident/19950308009109I), Mar 8, 1995: Boeing 757232 (N632DL), Raleigh-Durham, NC. Narrative: during flight from atl to iad, crew observed a right engine primary control and right engine sva fail status light at which time right engine shut… - [Incident 19890815049849I](https://openairdocs.org/incident/19890815049849I), Aug 15, 1989: Boeing 757232 (N632DL), St Louis, MO. NR2 engine oil quantity low. Pressure fluxing. Shut down and diverted. O rings seals on main oil filter leaking. --- 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.