# N639DL: 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: 23993
- Year built: 1988
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 3, 1988
- Certificate issued: December 5, 1988
- Last registry action: April 13, 2016
- Mode S code: A85F81
- 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/N639DL
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=639DL
- Page: https://openairdocs.org/deregistered/N639DL-2018-03-28

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 (36)

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

- [SDR DALA1316240639](https://openairdocs.org/sdr/DALA1316240639), Jun 27, 2013: PIN. DAMAGED. DECLARED AN EMERGENCY DUE TO LEFT ENGINE IN FLIGHT SHUTDOWN. FOUND PUSHED PIN GOING TO N2 SPEED CARD. RESET PIN. R & R NR 1 ENGINE FUEL CONTROL IAW AMM 73-21-01
- [SDR DALA1315300639](https://openairdocs.org/sdr/DALA1315300639), Jun 13, 2013: SKIN. CORRODED. ON WALKAROUND, FOUND CORROSION ON FUSELAGE SKIN AFT OF BS 1720 BETWEEN S27-29R. REPAIRED IAW ERA 516090-14, REV ORIG PERMANENT REPAIR.
- [SDR DALA1305190639](https://openairdocs.org/sdr/DALA1305190639), Feb 22, 2013: FUSE. INOPERATIVE. FIRST CLASS SEAT ALL SEAT MOUNTED EMERGENCY ESCAPE PATHLIGHTS INOPERATIVE. TROUBLESHOT IAW AMM 33-51 AND WDM 33-51-16, FOUND F2 FUSE BAD ON PWR SUPPLY PACK M900
- [SDR DALA1244150639](https://openairdocs.org/sdr/DALA1244150639), Aug 4, 2012: TIRE. FAILED. DECLARED AN EMERGENCY DUE TO A MAIN TIRE ISSUE. ON ARRIVAL, FOUND NR 6 TIRE BLOWN AND DAMAGE TO INBOARD LT FLAP. REPLACED NR 5 AND NR 6 TIRE. REPLACED LT INBD T
- [SDR DALA1243700639](https://openairdocs.org/sdr/DALA1243700639), Jul 31, 2012: BATTERY PACK. INOPERATIVE. DURING SERVICE CHECK, MAINTENANCE DISCOVERED AISLE EMERGENCY EXIT LIGHTS OUT. REMOVED AND REPLACED BATTERY PACK FOR F/C EXIT LIGHTS. OPS CHECKED GOOD.
- [SDR DL757100972](https://openairdocs.org/sdr/DL757100972), Apr 21, 2010: CONNECTOR. DAMAGED. DURING LAYOVER CHECK, MX FOUND DOOR 2R RED EMERGENCY PATH LIGHT INOPERATIVE. MX REPAIRED THE LIGHT CONNECTION. OPS CHECK WAS GOOD.
- [SDR DL757100357](https://openairdocs.org/sdr/DL757100357), Feb 10, 2010: CONNECTOR. DAMAGED. SEAT 41 EMERGENCY LIGHT INOP. REPLACED CONNECTOR LIGHT OPN OK.
- [SDR DU4R2007156](https://openairdocs.org/sdr/DU4R2007156), Jul 19, 2007: FLOOR PANEL. CORRODED. FOUND AFT DECK PLATE BS 1713 TO BS 1717 RBL 6 TO RBL 26 CORRODED. REPAIRED BY FABRICATING AND INSTALLING DOUBLER REPAIR 7-3/8 BY 6-3/4 FROM 2024-T3 .063 IAW B75
- [SDR DU4R2007155](https://openairdocs.org/sdr/DU4R2007155), Jul 19, 2007: SILL. CORRODED. FOUND AFT CARGO LWR DOOR SILL CORRODED FROM BS 1390 TO BS 1440 S-27R. REPAIRED BY REMOVING DOOR SILL AND INSTALLING P/N 146N8522-52 IAW B757 SRM 51-40-02, 53-60
- [SDR DU4R2007154](https://openairdocs.org/sdr/DU4R2007154), Jul 19, 2007: SKIN. GOUGED. FOUND GOUGE IN FUSELAGE SKIN AT PREVIOUS REPAIR ON LT SIDE BS 660, S-17L. REPAIRED BY FABRICATING AND INSTALLING DOUBLER REPAIR 13 BY 10 BY 11-3/8 BY 8-1/2 AND 
- [SDR DU4R2007153](https://openairdocs.org/sdr/DU4R2007153), Jul 19, 2007: TORQUE TUBE. CORRODED. FOUND RT I/B FLAP I/B TORQUE TUBE CORRODED. REPAIRED BY REMOVING AND REPLACING TUBE WITH P/N 113N2108-1 AND 113N2105-2 IAW B757 AMM 27-51-05 AND DELTA EA 06-097
- [SDR DU4R2007152](https://openairdocs.org/sdr/DU4R2007152), Jul 19, 2007: TORQUE TUBE. CORRODED. FOUND LT I/B FLAP I/B TORQUE TUBE CORRODED. REPAIRED BY REMOVING AND REPLACING TUBE WITH P/N’S 113N2105-1 AND 113N2108-1 IAW B757 AMM 27-51-05 AND DELTA EA 06-0
- [SDR DL757070941](https://openairdocs.org/sdr/DL757070941), Jul 19, 2007: SKIN. DENTED. DURING HMV, INSPECTION NOTED 2 DENTS AND AN EXISTING EXTERNAL DOUBLER ON THE FUSELAGE SKIN, LEFT SIDE. THE TWO DENTS WERE CUTOUT, AND THE EXISTING REPAIR WAS RE
- [SDR DU4R2007161](https://openairdocs.org/sdr/DU4R2007161), Jul 16, 2007: FITTING. CORRODED. FOUND FITTING AT C-2 DOOR CORRODED (AT NUTPLATES) THRESHOLD BS 1440 S-27R. REPAIRED BY REMOVING FITTING AND INSTALLING P/N 69-45578-7 IAW B757 SRM 51-40-02 AND 
- [SDR DU4R2007160](https://openairdocs.org/sdr/DU4R2007160), Jul 16, 2007: RIB. CRACKED. FOUND LT INBB FLAP MAIN FLAP RIB (3RD FROM I/B END) CRACKED. REPAIRED BY REMOVING RIB AND INSTALLING RIB FABRICATED (ON N/R 25000)16.780 BY 8.550 FROM 7050-T745
- [SDR DU4R2007159](https://openairdocs.org/sdr/DU4R2007159), Jul 11, 2007: FLOOR PANEL. CORRODED. FOUND CORRODED AFT DECK PLATE BS 1681.8 FROM LBL 14 TO LBL 29. REPAIRED BY CUTTING OUT CORRODED SHEAR SKIN AT B/L 25L AND SECTION OF FLOORBEAM. FABRICATED AND I
- [SDR DU4R2007158](https://openairdocs.org/sdr/DU4R2007158), Jul 3, 2007: FLOOR PANEL. CORRODED. FOUND CORRODED AFT DECK PLATE BS 1681.8 FROM LBL 1 TO LBL 14. REPAIRED BY FABRICATING AND INSTALLING REPAIR DOUBLER 6-1/2 BY 14 FROM 2024-T3 .063 IAW B757 SRM 5
- [SDR DU4R2007157](https://openairdocs.org/sdr/DU4R2007157), Jul 3, 2007: FLOOR PANEL. CORRODED. FOUND CORRODED AFT DECK PLATE BS 1681.8 FROM LBL 1 TO LBL 14. REPAIRED BY FABRICATING AND INSTALLING REPAIR DOUBLER 6-1/2 BY 14 FROM 2024-T3 .063 IAW B757 SRM 5
- [SDR DL75K050363](https://openairdocs.org/sdr/DL75K050363), Jul 11, 2005: COUPLING. LEAKING. L BLEED DUCT LK EICAS MSG AND OVERHEAD DUCT LEAK LIGHT ON LEFT SIDE ILLUMINATED AFTER T/O. FOUND BUSTED CLAMP ON DUCT LEADING TO LT WING A/I VALVE ON TOP OF LT 
- [SDR DL75K050279](https://openairdocs.org/sdr/DL75K050279), May 17, 2005: BATTERY. DISCHARGED. F/C EMERGENCY FLASHLIGHT INOP. REPLACED EMERGENCY FLASHLIGHT BATTERY, CKS GOOD.
- [SDR DL757021140](https://openairdocs.org/sdr/DL757021140), Sep 25, 2002: CIRCUIT CARD. FAULTY. FL 310 LT ENG BLEED OFF, A/I VALVE, LT ENG WING LT VALVE ON. REINSTATED A/I THROUGH ISOL VALVE. RT BLEED OFF. NO PRESS SOURCE. CABIN CLIMBED TO 8000FT REINSTATE
- [SDR DL757020458](https://openairdocs.org/sdr/DL757020458), Apr 19, 2002: SLIDE. DEPLOYED. SLIDE DEPLOYED BY CABIN SERVICE_C/A REPLACED SLIDE
- [SDR DL757011393](https://openairdocs.org/sdr/DL757011393), Aug 23, 2001: SKIN. CORRODED. FUSELAGE / SKIN / FS 1473 / RBL 3.2 / LOWER AFT VHF ANTENNA:CORROSION REPAIR THE FUSELAGE SKIN WAS FOUND CORRODED AT THE VHF ANTENNA MOUNT AT FS 1473 AND RBL 3.
- [SDR DL757011389](https://openairdocs.org/sdr/DL757011389), Aug 23, 2001: SKIN. DENTED. THE FUSELAGE SKIN WAS FOUND DENTED AT FS 454 AND STRINGER 27R NEAR THE E&E DOOR OPENING. THE DAMAGE WAS REMOVED IN THE SKIN AND IN THE UNDERLYING BEARSTRAP. REP
- [SDR DL757011391](https://openairdocs.org/sdr/DL757011391), Aug 22, 2001: SKIN. GOUGED. FUSELAGE / SKIN / FS 1715 / STRG. 19R : GOUGE REPAIR THE FUSELAGE SKIN WAS FOUND GOUGED AND FS 1715 AND STRINGER 19R. THE GOUGE WAS REMOVED WITH AN 8" X 3" CUTO
- [SDR DL757010918](https://openairdocs.org/sdr/DL757010918), Jun 5, 2001: POWER SUPPLY. FAILED. ON A-CHECK FOUND FWD ENTRY DOOR EMERGENCY LITE INOP REPLACED POWER SUPPLY-OPS OK
- [SDR DL757010841](https://openairdocs.org/sdr/DL757010841), May 25, 2001: EEC. MALFUNCTIONED. ALL RT ENG INSTRUMENTS FLUCTUATED DURING INITIAL CLIMB OUT. AT 10K LEVEL OFF (250K) IND STABILIZED BUT RESUMED FLUX ON SUBSEQUENT CLIMB TO 14K. RETURNED TO SLC.
- [SDR DL757002276](https://openairdocs.org/sdr/DL757002276), Nov 20, 2000: BATTERY. OVERHEATED. BEFORE PUSHBACK, FLT ATT REPORTED ACRID SMELL IN CABIN. EVACUATED AIRCRAFT VIA MAIN L2 DOOR. FOUND APU BATTERY DEFECTIVE, CAUSING FUMES IN AFT CARGO COMPARTMENT
- [SDR DL757002000](https://openairdocs.org/sdr/DL757002000), Oct 13, 2000: UNKNOWN. ODOR. AT CRUISE STRONG ELECTRICAL SMELL IN AFT CABIN, SPREAD TO FWD /MID CABIN. TURNED OFF UTILITY BUSSES, ODOR WENT AWAY. FOUND RT RECIRCULATION FAN AT FAULT. FWD TO
- [SDR DL757001191](https://openairdocs.org/sdr/DL757001191), Jun 20, 2000: WINDOW. OVERHEATED. CO-PILOTS WINDOW OVERHEATED INDICATED BY SCALDING ON LOWER PORTION AND SLIGHT ODOR. RIGHT FORWARD WINDOW. REPLACED R-1 WINDOW ASSY AND CONTROLLER PER MM.
- [SDR DL757980919](https://openairdocs.org/sdr/DL757980919), Apr 28, 1998: WHEEL. DAMAGED. NR 5 MAIN DEPARTED A/C ON LDG. REPLACED WHEEL ASSY.
- [SDR DL757972369](https://openairdocs.org/sdr/DL757972369), Nov 14, 1997: OVERHEAT SWITCH. MALFUNCTIONED. PASSING FL 260, RT BLEED, RT PACK AND RT BLEED VALVE LIGHT CAME ON. FOLLOWED CHECKLIST, RESET VALVE AND OPERATED NORMAL FOR A FEW SECONDS AND THEN ALL 3 LIGHTS 
- [SDR DL757971067](https://openairdocs.org/sdr/DL757971067), May 23, 1997: WEDGE. DELAMINATED. T/E WEDGE UPPER FWD EDGE DELAMINATED. REPLACED T/E WEDGE PER SRM 57-43-02.
- [SDR DL757953829](https://openairdocs.org/sdr/DL757953829), Sep 26, 1995: EEL BULB. MISSING. TRACK LIGHTING AT 30ABC OUT OF TRACK. REPLACED LIGHT BULB AND LENS COVER. OPS CK GOOD.
- [SDR DL757953135](https://openairdocs.org/sdr/DL757953135), Jul 21, 1995: TE WEDGE. DELAMINATED. UPON INITIAL INSPECTION, THE T/E WEDGE WAS FOUND TO BE DELAMINATED. REPLACED PER SRM 57-43-02, FOR NR 3 L/E SLAT PANEL.
- [SDR DL757950134](https://openairdocs.org/sdr/DL757950134), Jan 10, 1995: IDG. FAILED. DURING CLIMB-OUT, LEFT GENERATOR DRIVE LIGHT ILLUMINATED ACCOMPANIED WITH ENGINE VIBRATION, DISCONNECTED IDG, STARTED APU, 10 MINUTES LATER APU AUTO SHUTDOWN. R

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