# N624DL: 1987 Boeing 757-232, registration cancelled 2018-03-29 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: March 29, 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: 22914 - Year built: 1987 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: January 19, 1987 - Certificate issued: September 16, 2013 - Last registry action: July 25, 2016 - Mode S code: A8256F - 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/N624DL - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=624DL - Page: https://openairdocs.org/deregistered/N624DL-2018-03-29 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 757-232: https://openairdocs.org/model/boeing-757-232.md ## Service difficulty reports (43) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DALA1012580624](https://openairdocs.org/sdr/DALA1012580624), Jun 2, 2010: WIRE. DAMAGED. DURING LAYOVER CHECK, MX FOUND EMERGENCY PATH LIGHTS ROW 27 TO 37 INOPERATIVE. MX REPAIRED WIRES AT SEAT ROW 27DEF. OPS CHECK WAS GOOD. (DL757101438) - [SDR DALA1012130643](https://openairdocs.org/sdr/DALA1012130643), Jun 2, 2010: LIGHT. INOPERATIVE. DURING LAYOVER CHECK, MX FOUND EMERGENCY PATH LIGHTS ROW 27 TO 37 INOPERATIVE. MX REPAIRED WIRES AT SEAT ROW 27DEF. OPS CHECK WAS GOOD. - [SDR DL757091182](https://openairdocs.org/sdr/DL757091182), Jul 3, 2009: FAILSAFE. MISINSTALLED. DURING WIFI RACK INSTALLATION THE FUSELAGE FRAME FAILSAFE WAS MISDRILLED AT FS 1540 BETWEEN S21R AND S22R IN THE AFT CARGO BIN RIGHT LOWER LOBE. REPAIR ACCOMPLI - [SDR DALA1115460624](https://openairdocs.org/sdr/DALA1115460624), Jun 19, 2009: SKIN PANEL. PUNCTURED. RUDDER STA 115, LT SKIN PANEL PUNCTURED. REPAIRED IAW ERA 475576-14. - [SDR DALA1121490624](https://openairdocs.org/sdr/DALA1121490624), Apr 19, 2008: GEAR. DEFECTIVE. TRAILING EDGE FLAP TRANSMISSION GEAR REPLACED IAW EA 06-097281-03, ME02, ME04. - [SDR DL757071571](https://openairdocs.org/sdr/DL757071571), Nov 29, 2007: WIRE HARNESS. SPARKS. CLIMBING THROUGH 17000 FEET NOTICED A STRONG ELEC SMELL. CAPT NOTICED SPARKING IN LOWER LEFT SIDE OF WINDOW L1. FOUND L1 WINDOW J5 WINDOW HEAT CONNECTION LOOSE. - [SDR DL757071562](https://openairdocs.org/sdr/DL757071562), Nov 27, 2007: UNKNOWN. ODOR. AFTER DESCENT, PILOTS SMELLED ELECTRICAL ODOR IN COCKPIT. RAN ENGINES TO TAKEOFF POWER WITH FULL ELECTRICAL LOAD. NO ODORS NOTED, RELAMP SWITCH LIGHTS RT ENG BL - [SDR DL757070379](https://openairdocs.org/sdr/DL757070379), Apr 27, 2007: ROLLER. DAMAGED. AFTER TAKEOFF WHEN GEAR WAS RETRACTED DOOR LIGHT REMAINED ON WITH ASSOC EICAS GEAR MESSAGE. RTN TO CVG WITH UNEVENTFUL LANDING. FLT CREW REPORTED FLT ATTENDANT - [SDR DL757070049](https://openairdocs.org/sdr/DL757070049), Jan 19, 2007: SKIN. WORN. THE FUSELAGE SKIN WAS BURNISHED OUT OF SRM LIMITS AT STA 508 APPROX 3.5" INBOARD OF STR 28L. THE DAMAGED SKIN WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED. - [SDR DL757060650](https://openairdocs.org/sdr/DL757060650), Aug 11, 2006: SKIN. CRACKED. A CRACK WAS FOUND AT THE UPPER FORWARD L1 DOOR OPENING IN THE FUSELAGE SKIN. THE DAMAGED SKIN WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED. - [SDR DALA1121690624](https://openairdocs.org/sdr/DALA1121690624), Jul 31, 2006: SKIN. CORRODED. LOWER FUSELAGE SKIN PANEL BS 495, B/L 0 ANTENNA OPENING PAD CORROSION REPAIRED IAW ERA 099979-14. - [SDR DL757060125](https://openairdocs.org/sdr/DL757060125), Feb 12, 2006: RELIEF VALVE. MALFUNCTIONED. CREW ON FLT 1148/12 SLC-BWI RADIOED THAT AT FL340 CABIN ALTITUDE WARNING SOUNDED AND CREW REALIZED CABIN ALTITUDE WAS 11K AND CLIMBING AT 1000FT/MIN. REPLACED L - [SDR DL757060010](https://openairdocs.org/sdr/DL757060010), Jan 3, 2006: ENGINE. FAILED. CREW SHUT ENGINE DOWN IN FLIGHT. EICAS L ENG STATOR, ENG FAILED W/ PWR REDUCTION. REPLACED STATOR VANE ACTUATOR. - [SDR DU4R0508178](https://openairdocs.org/sdr/DU4R0508178), Aug 9, 2005: SKIN. CORRODED. CORROSION ON BELLY SKIN JUST AFT OF MEC DOOR. - [SDR DU4R0508177](https://openairdocs.org/sdr/DU4R0508177), Aug 9, 2005: FLOORBEAM. CORRODED. CORROSION RUNNING UNDER REPAIR DOUBLER AT STA. 377.7 LBL 59. - [SDR 176](https://openairdocs.org/sdr/176), Aug 5, 2005: SEAT TRACK. CORRODED. CORROSION ON SEAT TRACKS LT SIDE IB AND OB AT BS 780 - 800. S/O 283001, DELTA NR NR21386. - [SDR 175](https://openairdocs.org/sdr/175), Aug 5, 2005: CLIP. CORRODED. CORROSION, AFT CARGO ACCS AREA SHEAR CLIP BS 1681 S-22-S-23. S/O 283001, DELTA N//R NR 21000. - [SDR 174](https://openairdocs.org/sdr/174), Aug 5, 2005: SHEAR WEB. CORRODED. CORROSION ON SHEAR WEB SURFACE FROM BS 1681.8 TO 1720 BL 0 TO BL60L INCLUDING FASTENER HOLES. S/O 283001, DELTA N//R NR 21000. - [SDR 173](https://openairdocs.org/sdr/173), Aug 5, 2005: STRINGER. CORRODED. CORROSION AT STR. 28R AT BS 650. S/O 283001, DELTA N//R NR 22590 - [SDR 172](https://openairdocs.org/sdr/172), Aug 5, 2005: THRESHOLD. CORRODED. CORROSION AT STA. 1440 ON MAIN STRUCTURE UNDER THRESHOLD Z-ANGLE CORROSION AT 6 FASTENERS. S/O 283001, DELTA N//R NR22456 - [SDR DU4R0507171](https://openairdocs.org/sdr/DU4R0507171), Jul 28, 2005: DOOR. DENTED. R-4 DOOR IS DENTED ON THE LOWER AFT CORNER. - [SDR DU4R0507170](https://openairdocs.org/sdr/DU4R0507170), Jul 28, 2005: DOOR FRAME. CRACKED. RT NR 2 DOOR ON FRAME 27 IS CRACKED. - [SDR DU4R0507168](https://openairdocs.org/sdr/DU4R0507168), Jul 28, 2005: SUPPORT. CRACKED. CRACKED/TORN METAL SUPPORT IN CABIN FUSELAGE AT BS 1040 - 1060 JUST AFT OF FLOORBOARD 1020A. - [SDR DU4R0507167](https://openairdocs.org/sdr/DU4R0507167), Jul 28, 2005: FLOORBEAM. CRACKED. CRACKED CAP ON FLOORBEAM AT BS 900 BL 54L TO 64L WL 208.1. - [SDR DU4R0507166](https://openairdocs.org/sdr/DU4R0507166), Jul 28, 2005: CREASE BEAM. CORRODED. CORROSION ON CREASE BEAM AT 364 - 371 RBL 65. - [SDR DU4R0507165](https://openairdocs.org/sdr/DU4R0507165), Jul 28, 2005: SHEAR WEB. CORRODED. CORROSION IN SHEAR WEB SURFACE FROM BS 1681.8 - 1720 BL 0 - BL 60R INCLUDING FASTENERS. - [SDR DU4R0507164](https://openairdocs.org/sdr/DU4R0507164), Jul 28, 2005: SHEAR WEB. CORRODED. CORROSION IN SHEAR WEB SURFACE FROM BS 1681.8 - 1720 BL 0 - BL 60R INCLUDING FASTENERS. - [SDR DU4R0507163](https://openairdocs.org/sdr/DU4R0507163), Jul 28, 2005: FRAME. DENTED. DENT IN AFT CARGO COMPARTMENT BS 1520 FRAME UPPER FLANGE BETWEEN S-25 TO S-26L. - [SDR DU4R0507162](https://openairdocs.org/sdr/DU4R0507162), Jul 28, 2005: FRAME. CRACKED. CRACK IN FRAME UPPER SURFACE IN AFT CARGO COMPARTMENT BS 1540. - [SDR DU4R0507161](https://openairdocs.org/sdr/DU4R0507161), Jul 28, 2005: FRAME. CRACKED. AFT BAG PIT LT BS 1500 AT S-26L MAIN FRAME HAS DENT/CRACK. - [SDR DU4R0507160](https://openairdocs.org/sdr/DU4R0507160), Jul 28, 2005: FRAME. DENTED. AFT CARGO BAY LT BS 1480 AT S-25L MAIN FRAME HAS DENTS. - [SDR DU4R0507159](https://openairdocs.org/sdr/DU4R0507159), Jul 28, 2005: FRAME. DENTED. AFT CARGO BAY LT BS 1340 AT S-25L MAIN FRAME HAS DENT. - [SDR DL757050146](https://openairdocs.org/sdr/DL757050146), Mar 2, 2005: SEAL. LEAKING. CABIN ALTITUDE DISCRETE ON EICAS AND OVERHEAD PANEL AT FL335. FOUND RT AFT OVERWING EXIT HATCH SEAL LEAKING. REPLACED SEAL. - [SDR DL757030787](https://openairdocs.org/sdr/DL757030787), Aug 26, 2003: PUMP. FAILED. DURING ROUTINE DISASSEMBLY OF A FAILED FUEL BOOST PUMP, SEVERE BEARING AND HOUSING WEAR WAS DISCOVERED, TO THE EXTENT THAT END CAP FAILURE WAS IMMINENT. ROTOR A - [SDR DL757020415](https://openairdocs.org/sdr/DL757020415), Apr 6, 2002: FIRE. DETECTED. DURING ENGINE START ON RT ENG, FLT ATT REPORTED A FIRE ON THE RIGHT ENG. REPORTED SMOKE AND FLAMES OUT THE RIGHT TAIL PIPE. SMOKE IN CABIN. ENG FUEL WAS CUT OFF - [SDR DL757010992](https://openairdocs.org/sdr/DL757010992), Jun 16, 2001: LIGHT. INOPERATIVE. FOUND ON L/O, R-3 EMERGENCY DOOR LIGHT INOP. RELAMPED SAME. - [SDR DL757001744](https://openairdocs.org/sdr/DL757001744), Sep 9, 2000: HEATER. MALFUNCTIONED. F/A REPORTED LIGHT SMOKE WITH ELECTRICAL BURNING ODOR COMING FROM MID GALLEY AREA. WALL ALSO REPORTED TO BE HOT AND WATER DISPENSER PRODUCING BOILING WATER. SMO - [SDR DL757001532](https://openairdocs.org/sdr/DL757001532), Aug 12, 2000: PANEL. ODOR. PA IN USE LIGHT APPEARED TO BE INOP, EMITTED ODOR WHEN PUSHED. FOUND PA CAPSUL PIN BURNED. REPLACED PANEL, NO FURTHER ODOR PRESENT. UNIT OPS CHECK NORMAL. - [SDR DL757000808](https://openairdocs.org/sdr/DL757000808), Apr 25, 2000: MODULE. INOPERATIVE. INTERIOR AFT CABIN SEAT EMERGENCY LIGHTS INOP. REPLACED LIGHT MODULE. - [SDR DL757991339](https://openairdocs.org/sdr/DL757991339), May 13, 1999: SKIN. DELAMINATION. RT ELEVATOR LOWER L/E SKIN, FS 52, 112, 136, 160, 170 AND 220: DELAMINATION. MULTIPLE INTER-PLY DELAMINATION AREAS WERE FOUND AT THE ABOVE STATION LOCATIONS TYP - [SDR DL757982621](https://openairdocs.org/sdr/DL757982621), Dec 24, 1998: MEGAPHONE. INOPERATIVE. BOTH CABIN MEGAPHONES INOP. FOUND BY CABIN CREW ON PREDEPARTURE CHECK, P/N 237702242 (2) EACH. - [SDR DL757970796](https://openairdocs.org/sdr/DL757970796), Apr 25, 1997: FITTING. WORN. THE SIX BOLTS THAT ATTACH THE NR 3 FLAP INBD FLAP TRACK FWD SUPPORT FITTING TO THE MLG BEAM WERE FOUND TO BE LOOSE CAUSING THE BOLTS TO WEAR INTO THE BEAM AND T - [SDR DL757950507](https://openairdocs.org/sdr/DL757950507), Feb 4, 1995: RATIO MODULE. FAILED. ON CLIMB-OUT RUDDER RATIO EICAS MSG AND RUDDER RATIO OVERHEAD LIGHT ILLUMINATED WITH UNCOMMANDED RUDDER MOVEMENT. FOUND PCA FAULT BALL SET ON RT RUDDER RATIO MO --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. 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