# N641DL: 1988 Boeing 757-232, registration cancelled 2018-03-28 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: March 28, 2018 - Status when cancelled: Valid registration - 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: 23995 - Year built: 1988 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: November 30, 1988 - Certificate issued: November 22, 2013 - Last registry action: October 12, 2016 - Mode S code: A86948 - 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/N641DL - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=641DL - Page: https://openairdocs.org/deregistered/N641DL-2018-03-28 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 (42) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DALA1157020641](https://openairdocs.org/sdr/DALA1157020641), Oct 4, 2011: SMOKE WARNING. FALSE ACTIVATION. FLT 853 DTW-RSW SHIP 641. FIRE RESCUE RESPONDED TO AIRCRAFT DUE FORWARD CARGO FIRE WARNING. FIRE BOTTLES USED. FIRE DEPT HAS INSPECTED AND FOUND NO INDICATION O - [SDR DALA1147970641](https://openairdocs.org/sdr/DALA1147970641), Aug 15, 2011: CONTROL PANEL. SHORTED. SMOKE-FUMES EMITTED FROM THE VOR/DME CONTROL PANEL. MAINTENANCE INSPECTED WIRING AND REPLACED THE CONTROL PANEL. OPERATIONAL CHECK WAS GOOD. - [SDR DALA1146170641](https://openairdocs.org/sdr/DALA1146170641), Jul 28, 2011: SKIN. GOUGED. FUSELAGE SKIN BETWEEN STA 1681 AND STA 1701 BETWEEN STR 14L AND STR 16L. REPAIRED PER ERA 494959-14 REV ORIG. - [SDR DL757100023](https://openairdocs.org/sdr/DL757100023), Jan 4, 2010: BALLAST. SMOKE. MULTIPLE ELECT FAILURE AND ELECTRICAL SMOKE OCCURED DURING APPROACH. F/C LIGHTS BLINKED REPEATEDLY DURING EVENT. SMOKE WAS FROM ROW 5 FWD. STRONGEST ON LT SIDE. - [SDR DL757090260](https://openairdocs.org/sdr/DL757090260), Feb 20, 2009: WIRE. SHORTED. WHILE TROUBLESHOOTING INBOUND WRITE UP, IRU DC FAIL MSG. FOUND WIRE BUNDLE W0072, W0066, AND W0074 ALL CHAFING AND SHORTED AGAINST SUPPORT BRACKET BEHIND P6-1 P - [SDR DL757090094](https://openairdocs.org/sdr/DL757090094), Jan 24, 2009: SENSOR. OUT OF ADJUST. REJECTED TO FOR RT AFT ENTRY DOOR LIGHT 90-100KTS. ABORT/ROLLOUT UNEVENTFUL. PERFORMED INSPECTION OF RT AFT ENTRY DOOR, NTF FWD TO MCO. PERFORMED HIGH ENERGY ST - [SDR DL757080807](https://openairdocs.org/sdr/DL757080807), May 31, 2008: STRINGER. CORRODED. STA 1710 STR 27L HAS EXFOLIATING CORROSION AFT CARGO BAY. REPLACED STR SECTION PER SRM 53-00-03 FIG 201 REF NR 78981650001. - [SDR DL757080806](https://openairdocs.org/sdr/DL757080806), May 31, 2008: CHANNEL. CORRODED. AFT CARGO STA 1720 STR 21L IS CORRODED/SPLICED IN NEW HAT CHANNEL PER SRM 53-00-03 FIG 201 REF NR78980200001. - [SDR DL757080805](https://openairdocs.org/sdr/DL757080805), May 31, 2008: STRINGER. CORRODED. AFT OF AFT CARGO BAY CORROSION AT STR 24L STA 1710/SPLICED STR HAT SECTION FROM STA 1690 TO 1720 PER SRM 53-00-03 FIG 201 AND 51-20-01 ON SAA N/R 78980240001. - [SDR DL757080813](https://openairdocs.org/sdr/DL757080813), May 30, 2008: STRINGER. CORRODED. STR 23L AT STA 1700, FOUND CORROSION. REPAIRED PER SRM 53-00-03 FIG 201. - [SDR DL757080811](https://openairdocs.org/sdr/DL757080811), May 30, 2008: STRINGER. CORRODED. STR 22L AT STA 1710, FOUND CORROSION. REPAIRED PER SRM 53-00-03 FIG 201. - [SDR DL757080810](https://openairdocs.org/sdr/DL757080810), May 30, 2008: STRINGER. CORRODED. STR 26L AT STA 1710 WAS FOUND TO HAVE CORROSION UNDER STRINGER. REPAIRED PER SRM 53-80-08 FIG 201. - [SDR DL757080809](https://openairdocs.org/sdr/DL757080809), May 30, 2008: STRINGER. CORRODED. STR 28 L HAS 2 AREAS OF CORROSION BETWEEN STA 1460 AND 1480/SRM 51-40-05. REPAIR REPORTED PER SRM 53-00-03. - [SDR DL757080808](https://openairdocs.org/sdr/DL757080808), May 30, 2008: SKIN. DENTED. DENT ON STR BETWEEN STR 28R AND 29R AT STA 192. REPAIRED DENT PER SRM 53-00-01 REF SAA N/R 78986200001. - [SDR DL757080804](https://openairdocs.org/sdr/DL757080804), May 30, 2008: STRUCTURE. CORRODED. DURING HMV FOUND AFT CHORD CORRODED AROUND SEVERAL HOLES AFTER STR STR 27L TO 20L. REPLACED A SECTION OF THE CHORD PER SMR 53-80-08D REF SAA N/R 78986090001. - [SDR DL757080793](https://openairdocs.org/sdr/DL757080793), May 30, 2008: STRUCTURE. CORRODED. DURING HMV AT SAA, CORROSION WAS FOUND ON THE HORIZONTAL AFT CHORD OF THE AFT PRESSURE BULKHEAD, FORWARD SIDE AT STA 1720, S-19L. THE CORROSION WAS REPAIRED PER - [SDR DL757080812](https://openairdocs.org/sdr/DL757080812), May 30, 2008: STRINGER. CORRODED. STR 20L AT 1680 AND STA 1700 FOUND CRACKED AND CORRODED. REMOVED DAMAGE, FABRICATED STRINGER, SPLICED, TREATED, IAW 757 SRM 51-40-05 F 201, - [SDR DL757080782](https://openairdocs.org/sdr/DL757080782), May 28, 2008: FITTING. DAMAGED. DURING HMV AT SAA, A HOLE WAS MISDRILLED COMMON TO THE NR 2 PYLON MIDSPAR FITTING, WEB, CHORD AND DOUBLER. THE HOLE WAS REAMED, BUSHED, AND REDRILLED PER BOEING - [SDR DL757080779](https://openairdocs.org/sdr/DL757080779), May 28, 2008: BULKHEAD. WORN. THE NR 1 PYLON AFT BULKHEAD O/B VERTICAL FLANGE AT NAC STA 203 WAS FOUND WITH WEAR. THIS WEAR WAS CAUSED BY THE RUBBING OF THE PYLON AFT FAIRING UPPER SPAR FLAN - [SDR DL757080781](https://openairdocs.org/sdr/DL757080781), May 27, 2008: FITTING. DAMAGED. DURING ACCOMPLISHMENT OF THE SIP MOD PER S/B 757-54-0034 REV 1, THE NR 2 PYLON MID SPAR FITTING UPPER HORIZONTAL TANGE WAS MISDRILLED IN A FORWARD MOST HOLE LOC - [SDR DL757080780](https://openairdocs.org/sdr/DL757080780), May 27, 2008: BRACE. DAMAGED. DURING ACCOMPLISHMENT OF THE SIP MOD, S/B 757-54-0034 REV 1, THE DIAGONAL BRACE LOWER/FWD I/B LUG WAS INADVERTENTLY OVERSIZED TO 2.003" INSTEAD OF THE REQUIRED - [SDR DL757080384](https://openairdocs.org/sdr/DL757080384), Mar 17, 2008: MANIFOLD. BROKEN. RT ENG OIL QTY AT ZERO AND OIL PRESSURE DROPPING WITH OIL PRESS LIGHT FLICKERING AT CRUISE. MX FOUND THE MAIN BEARING BREATHER MANIFOLD BROKEN. REPLACED SAME, R - [SDR DL75K060548](https://openairdocs.org/sdr/DL75K060548), Jun 30, 2006: SKIN. CRACKED. THE FUSELAGE SKIN HAS A 4 INCH CRACK RUNNING FROM THE FORWARD UPPER CORNER OF HTE L-1 DOOR OPENING. THE CRACK IS IN THE SKIN AND BEARSTRAP. THE CRACKED SKIN WAS - [SDR DL75K060538](https://openairdocs.org/sdr/DL75K060538), Jun 30, 2006: SKIN. FATIGUED. FOUR INCH CRACK IN FUSELAGE SKIN AND BEAR STRAP AT THE UPPER FWD CORNER OF L1 DOOR OPENING. EXTERNAL DOUBLER/TRIPLER/QUADRUPLER INSTALLED PER DELTA ERA 456338-1 - [SDR DL757050051](https://openairdocs.org/sdr/DL757050051), Jan 21, 2005: WIRE. DAMAGED. EMERGENCY LIGHT AT 23D INOP. FOUND BROKEN WIRE UNDER SEAT 23F. REPAIRED WIRE. - [SDR DL757040692](https://openairdocs.org/sdr/DL757040692), Jul 25, 2004: BATTERY. UNSERVICEABLE. EMERGENCY ESCAPE LIGHTING IN F/C VERY DIM ON TEST. REPLACED BATTERY PACK IN EMERGENCY ESCAPE PATH PWR SUPPLY M9101 IAW AMM. CKS GOOD. - [SDR DL757020361](https://openairdocs.org/sdr/DL757020361), Mar 22, 2002: GARLOCK SEAL. LEAKING. LEFT ENG OIL QTY DECREASING DURING FLIGHT. DECREASED TO -0- ON APPROACH. REPLACED NUMBER 5 BEARING COVER GARLOCK SEAL. - [SDR DL757020351](https://openairdocs.org/sdr/DL757020351), Mar 20, 2002: SKIN. GOUGED. FUSELAGE / SKIN / FS 1708 / STRG. 17L : GOUGE CUTOUT REPAIR THE FUSELAGE SKIN WAS FOUND GOUGED AT FS 1708 JUST BELOW STRINGER 17L. THE GOUGE WAS REMOVED WITH A - [SDR DL757010702](https://openairdocs.org/sdr/DL757010702), May 2, 2001: SIGN. BROKEN. FOUND DURING LAYOVER EMERGENCY EXIT IDENTIFIER AT R2 DOOR F/A SEAT BROKEN REPLACED SIGN BASE AND LENS COVER. OPERATIONAL CK OK. - [SDR DL757010701](https://openairdocs.org/sdr/DL757010701), May 2, 2001: LIGHT. INOPERATIVE. SEAT MOUNTED ESCAPE PATH LIGHTING INOP AT SEAT 1CD. RELAMPED SAME, NO HELP. REMOVED/REPLACED ILLUMINATOR ASSY OPS CKS OK. - [SDR DL757010700](https://openairdocs.org/sdr/DL757010700), May 2, 2001: SEAL. MISSING. SURVIVAL KIT FOR 2L DOOR MISSING LEAD SEAL. REMOVED AND REPLACED SURVIVAL KIT FOR 2L DOOR. - [SDR DL757010699](https://openairdocs.org/sdr/DL757010699), May 2, 2001: LIGHT. MISSING. SEAT MOUNTED ESCPAPE PATH LIGHTING COMPLETELY MISSING AT SEAT 2CD REPLACED ILLUMINATOR ASSY. OPS CKS OK. - [SDR DL757010235](https://openairdocs.org/sdr/DL757010235), Feb 9, 2001: BATTERY. DISCHARGED. FWD FLIGHT ATTENDANT EMERGENCY FLASHLIGHT HAS WEAK BATTERY. REPLACED BATTERY, OPS NORMAL. - [SDR DL757000848](https://openairdocs.org/sdr/DL757000848), Apr 29, 2000: HEATER. INOPERATIVE. SMOKE AND FUMES IN COCKPIT COMING FROM UNDER F/O GLARESHIELD. DIVERTED TO KIAH. FOUND LOWER TERMINAL R-1 WINDOW BURNED AND BROKEN OFF. REPLACED WINDSHIELD AND C - [SDR DL757991266](https://openairdocs.org/sdr/DL757991266), Jun 5, 1999: BULB. FAILED. WHEN GEAR EXTENDED LEFT MAIN DID NOT GO GREEN. ALTERNATE GEAR EXTENSION PER POM, NO HELP. RELAMPED INDICATOR. - [SDR DL757981483](https://openairdocs.org/sdr/DL757981483), Jul 16, 1998: ENGINE. FAILED. ON CLIMB-OUT, FL 260, LT ENG STALLED AND QUIT ALL ENG IND WENT BLANK CLB 2 SELECTED SHUTDOWN CK LIST C/W RETURNED TO CVG. REPLACED NR 1 ENG PMA AND ROTOR SHAFT - [SDR DL757981471](https://openairdocs.org/sdr/DL757981471), Jul 14, 1998: STATOR. FAILED. NR 1 ENG STALLED AT V1 AND AUTO SHUT DOWN HARD CARD AND POM EMERGENCY PROCEDURES FOLLOWED RETURNED TO RUNWAY 9L. BORESCOPED OK OF 6TH STAGE LPT - 16TH STAGE HPC - [SDR DL757981416](https://openairdocs.org/sdr/DL757981416), Jul 6, 1998: ECU. FAILED. APU FLAMED OUT IN FLT FOLLOWED PROCEDURES AND GOT APU FAULT LIGHT, NO START ALLOWED. ONE ENG GEN PREV DEFERRED, ROBBED APU CONTROL ECU FROM A/C 628. INSTALLED B - [SDR DL757971596](https://openairdocs.org/sdr/DL757971596), Aug 2, 1997: WEDGE. DELAMINATED. NUMBER 1, 6, 7 AND 9 SLAT WEDGE DELAMINATED. REPLACED ALL FOUR SLATS. - [SDR DL757971282](https://openairdocs.org/sdr/DL757971282), Jul 2, 1997: BULB. FAILED. ON GEAR EXT LEFT MAIN DID NOT GO GREEN. TOWER THOUGHT LEFT GEAR WAS UP. USED ALT EXT, NO GREEN. FOUND BOTH LEFT GEAR IND LIGHTS INOP. RELAMPED SAME, OPN NORM ON - [SDR DL757952322](https://openairdocs.org/sdr/DL757952322), May 28, 1995: TE WEDGE. DELAMINATED. T/E WEDGE DELAMINATED. COMPLIED WITH AD 90-23-06 PER SRM 57-54-02 FIG 202, FOR NR 2 L/E SLAT AT SHOP INSPECTION. - [SDR DL757952324](https://openairdocs.org/sdr/DL757952324), May 25, 1995: SKIN. DELAMINATED. TRAILING EDGE WEDGE DELAMINATED. REPLACED TRAILING EDGE WEDGE PER SRM 57-43-02 FIG. 202, DURING SHOP INSPECTION OF NR 3 L/E SLAT. ## 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 19930225006399I](https://openairdocs.org/incident/19930225006399I), Feb 25, 1993: Boeing 757232 (N641DL), Covington - Cin, OH. Lost all power on left engine after takeoff. Shut engine down. Returned. Rear turbine in engine had failed. --- 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.