# N653DL: 1990 Boeing 757-232, registration cancelled 2018-08-21

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 21, 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: 24393
- Year built: 1990
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 5, 1990
- Certificate issued: October 2, 2017
- Last registry action: October 2, 2017
- Mode S code: A89835
- 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/N653DL
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=653DL
- Page: https://openairdocs.org/deregistered/N653DL-2018-08-21

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 DL757101266](https://openairdocs.org/sdr/DL757101266), May 17, 2010: WIRE HARNESS. DAMAGED. DURING LAYOVER CHECK, MX FOUND THE EMERGENCY PATH LIGHT AT ROW 38DEF INOPERATIVE. MX REPLACED THE LIGHT HARNESS. OPS CHECK WAS GOOD.
- [SDR DL757100509](https://openairdocs.org/sdr/DL757100509), Feb 22, 2010: WIRE. UNSECURE. SEVERAL CABIN EPATH LIGHTS INOP AT ROWS 4, 19, 26 AND 34. RESECURED WIRES AT AFFECTED SEATS. CHECKS OK.
- [SDR DL757091464](https://openairdocs.org/sdr/DL757091464), Aug 29, 2009: FITTING. DAMAGED. ONE (1) EA HOLE IS ELONGATED ON LT WING O/B SIDELOAD FITTING. C/W ERA 476269-14 REV O.
- [SDR DL757091466](https://openairdocs.org/sdr/DL757091466), Aug 26, 2009: BULKHEAD. GOUGED. FOUND GOUGE ON SURFACE NR 1 PYLON BULKHEAD. C/W ERA 472263-14 REV O.
- [SDR DL757091465](https://openairdocs.org/sdr/DL757091465), Aug 26, 2009: SKIN. DAMAGED. FOUND TWO (2) EA HOLES TO BE .500 AT RT STA 116.05. C/W ERA 476265-14 REV O.
- [SDR DL757091463](https://openairdocs.org/sdr/DL757091463), Aug 26, 2009: STRUCTURE. DAMAGED. AFTER REMOVAL OF LT SIDE NR 2 PYLON, FOUND 1 EA HOLE TO BE .500 AT LT STA 116.05. C/W ERA 476264-14 REV O.
- [SDR DL757091467](https://openairdocs.org/sdr/DL757091467), Aug 24, 2009: BULKHEAD. CHAFED. NR 1 PYLON BULKHEAD CHAFED. C/W ERA 476263 REV O.
- [SDR DL757061027](https://openairdocs.org/sdr/DL757061027), Dec 13, 2006: LIGHT. INOPERATIVE. ON APP GEAR SELECTED DOWN LEFT GEAR GREEN LIGHT DID NOT ILLUMINATE CHECKED LIGHT TEST BULB WAS OK AFTER GA. QRH PROCEDURE FOLLOWED AFTER RECYCLE OF GEAR LIGHT R
- [SDR DU4R2006294](https://openairdocs.org/sdr/DU4R2006294), Mar 4, 2006: SUPPORT. CORRODED. LOWER WING TO BODY FAIRING STRUCTURE CORRODED RT BS 880. REMOVED CORRODED T-ANGLE, FABRICATED AND INSTALLED REPAIR T-ANGLE 36.800" FROM BAC1505-101029 IAW B757 
- [SDR DU4R2006290](https://openairdocs.org/sdr/DU4R2006290), Mar 3, 2006: FRAME. DENTED. AFT PIT STA 1320 S-25R - S-26R FRAME DENTED. REMOVED PREVIOUS REPAIR. FABRICATED AND INSTALLED FRAME REPAIR 26 X 5 INCHES FROM 7075-T6. 071 IAW B757 SRM 51-70-1
- [SDR DU4R2006287](https://openairdocs.org/sdr/DU4R2006287), Mar 1, 2006: FRAME. BENT. FRAME AS STA 1440 , S-26L IS BENT. CUT OUT BENT PORTION. FABRICATED AND INSTALLED FRAME SECTION REPAIR 10.5 X 2.5 INCHES FROM 7075-T6 .063 AND CLIP P/N 3.30 X 1
- [SDR DU4R2006292](https://openairdocs.org/sdr/DU4R2006292), Feb 28, 2006: FLOOR PANEL. CORRODED. CORROSION ON FWD PIT FLOOR PANEL LT NR 5 BS 750 - 845. REMOVED CORROSION IAW B757 SRM 51-10-02 FOUND L00 PERCENT MATERIAL LOSS IAW B757 SRM 53-00-53. FABRICATED
- [SDR DU4R2006282](https://openairdocs.org/sdr/DU4R2006282), Feb 28, 2006: FRAME. BENT. FRAME AS STA 1300, S-26L IS BENT. CUT OUT BENT PORTION. FABRICATED AND INSTALLED FRAME SECTION REPAIR 11.40 X 2.50 INCHES FROM 7075-T6 .071 IAW B757 SRM 51-70-1
- [SDR DU4R2006286](https://openairdocs.org/sdr/DU4R2006286), Feb 28, 2006: FRAME. BENT. FRAME AS STA 1240, S-26R IS BENT. CUT OUT BENT PORTION. FABRICATED AND INSTALLED FRAME SECTION REPAIR 10.4 X 2.5 INCHES FROM 7075-T6 .080 IAW B757 SRM 51-70-11,
- [SDR DU4R2006285](https://openairdocs.org/sdr/DU4R2006285), Feb 28, 2006: FRAME. BENT. FRAME AS STA 1480, S-26L IS BENT. CUT OUT BENT PORTION. FABRICATED AND INSTALLED FRAME SECTION REPAIR 10 X 2.4 INCHES FROM 7075-T6 .063 IAW B757 SRM 51-70-11, 5
- [SDR DU4R2006284](https://openairdocs.org/sdr/DU4R2006284), Feb 25, 2006: FRAME. BENT. FRAME AS STA 1320, S-26R IS BENT. CUT OUT BENT PORTION. FABRICATED AND INSTALLED FRAME SECTION REPAIR 13 X 4 FROM 7075-T6 .071 AND CLIP P/N 140N2063-56 IAW B757
- [SDR DU4R2006283](https://openairdocs.org/sdr/DU4R2006283), Feb 25, 2006: FRAME. BENT. FRAME AS STA 1340, S-26R IS BENT. CUT OUT BENT PORTION. FABRICATED AND INSTALLED FRAME SECTION REPAIR 13 X 4 INCHES FROM 7075-T6 .071 AND CLIP IAW B757 SRM 51-7
- [SDR DU4R2006278](https://openairdocs.org/sdr/DU4R2006278), Feb 24, 2006: SKIN. DENTED. C-2 DOOR INTERNAL SKIN HAS 2EA DENTS (WITH CREASE MARKS) AT STA 1400. MEASURED DENTS A=.400", Y= .029 A/Y RATIO 13. FABRICATED AND INSTALLED INTERNAL FLUSH REPA
- [SDR DU4R2006279](https://openairdocs.org/sdr/DU4R2006279), Feb 24, 2006: SKIN. CRACKED. C-2 DOOR INTERNAL SKIN LWR AFT CORNER HAS CRACK STA 1440. CUT OUT EDGE CRACK ON C-2 DOOR EXTERNAL SKIN AT LOWER AFT CORNER STA 1140. FOUND WITHIN LIMITS IAW B75
- [SDR DUR42006293](https://openairdocs.org/sdr/DUR42006293), Feb 23, 2006: FLOOR PANEL. CORRODED. FWD CARGO COMPT PIT FLOOR PANEL RT NR 5 CORRODED AT BS 750 - 845. REMOVED CORROSION IAW B757 SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW B757 SRM 53-00-53. FABR
- [SDR DU4R2006289](https://openairdocs.org/sdr/DU4R2006289), Feb 20, 2006: SEAT TRACK. GOUGED. MAIN CABIN SEAT TRACK FROM STA 760 TO STA 880 LBL 45 INNER SURFACE HAS MULTIPLE GOUGES. REMOVED GOUGED SECTIONOF SEAT TRACK. CUT, DRILLED UP AND INSTALLED NEW S
- [SDR DU4R2006281](https://openairdocs.org/sdr/DU4R2006281), Feb 20, 2006: FRAME. BENT. FRAME AS STA 1400, S-25L IS BENT. CUT OUT BENT PORTION. FABRICATED AND INSTALLED FRAME SECTION REPAIR 22.5 X 3.75 INCHES FROM 7075-T6 .063, AND 2EA CLIPS P/N 14
- [SDR DU4R2006280](https://openairdocs.org/sdr/DU4R2006280), Feb 20, 2006: FRAME. BENT. FRAME AS STA 1420, S-26L IS BENT. CUT OUT BENT PORTION. FABRICATED AND INSTALLED FRAME SECTION REPAIR 11.625 X 3.75 INCHES FROM 7075-T6 .063, FILLER AND CLIP P/
- [SDR DU4R2006291](https://openairdocs.org/sdr/DU4R2006291), Feb 18, 2006: FLOOR SUPPORT. DENTED. FWD CARGO FLOOR SUPPORT HAS DENTS BETWEEN STA 580 & 600 AT LBL 2. CUT OUT DENTED SECTION. FABRICATED AND INSTALLED REPAIR 40.80 INCHES AND 2 EA SPLICES 10.00 X 
- [SDR DU4R2006288](https://openairdocs.org/sdr/DU4R2006288), Feb 10, 2006: SKIN. DENTED. DENT LEFT SIDE FUSELAGE SKIN 7 FEET FWD OF L-2 DOOR. CUT OUT DENTED PORTION. FABRICATED AND INSTALLED REPAIR DOUBLER 9.5 X 9.5 INCHES FROM 2024-T3 .020 CLAD AND
- [SDR DL757040719](https://openairdocs.org/sdr/DL757040719), Aug 4, 2004: ODOR. DETECTED. DURING FLIGHT TO DAY, BURNING PLASTIC SMELL IN MID GALLEY, THIS PER FLT ATTENDANT REPORT. CALLED CONTRACT MTC TO INVESTIGATE. CONTRACT MTC TURNED ON ALL MID GAL
- [SDR DL757030966](https://openairdocs.org/sdr/DL757030966), Oct 29, 2003: CONTROL PANEL. OVERHEATED. SMOKE OBSERVED DURING FINAL APPROACH, AFTER NOSE GEAR LANDING LIGHT, TAXI LIGHT AND TURNOFF LIGHT WERE ILLUM. SMOKE OBSERVED AT LWR PORTION OF O/H PNL JUST BELO
- [SDR DL757030182](https://openairdocs.org/sdr/DL757030182), Feb 22, 2003: EEC. UNSERVICEABLE. LT ENGINE PRIMARY CONTROL STATUS MSG, LT ENGINE FAILED. REPLACED NR 1 ENGINE EEC. PERFORMED WINDMILL INSPECTION ON ENGINE. NO DEFECTS NOTED.
- [SDR DL757010477](https://openairdocs.org/sdr/DL757010477), Mar 23, 2001: SLAT TRACK. DAMAGED. LE FLAP ASSY ON FLAP RETRACTION - DECLARED EMERGENCY AND LANDED WITH NO INCIDENT. MTC IN WORK - FOUND NR 2 LE SLAT TRACK BROKEN LOOSE ON ARRIVAL.
- [SDR DL757001074](https://openairdocs.org/sdr/DL757001074), May 31, 2000: SKIN. LIGHTNING STRIKE. THE FUSELAGE CROWN SKIN SUFFERED A LIGHTNING BURN AT FS 590 AND STRINGER 1, ADJACENT TO THE ANTI-COLLISION LIGHT INSTALLATION. THE SKIN DAMAGE WAS REMOVED WITH 
- [SDR DL757001073](https://openairdocs.org/sdr/DL757001073), May 31, 2000: SKIN. LIGHTNING STRIKE. THE FUSELAGE CROWN SKIN BETWEEN FS 680 & 700 AND STRINGERS 1 AND 2L SUFFERED TWO LIGHTNING BURNS. THE TWO LOCATIONS WERE REMOVED WITH 1 INCH DIAMETER CUTOUTS IN
- [SDR DL757001054](https://openairdocs.org/sdr/DL757001054), May 28, 2000: SKIN. LIGHTNING STRIKE. THE FUSELAGE SKIN WAS FOUND WITH LIGHTNING STRIKE DAMAGE BETWEEN FS 460 AND 500 NEAR STRINGER 2R. THE DAMAGE WAS REMOVED WITH THREE SMALL 1 INCH CUTOUTS IN THE 
- [SDR DL757972504](https://openairdocs.org/sdr/DL757972504), Dec 1, 1997: SKIN. CRACKED. DURING INSPECTION OF A PREVIOUSLY ACCOMPLISHED REPAIR ON THE NR 1 ENGINE NACELLE STRUT SKIN AN ADDITIONAL CRACK WAS FOUND EMANATING FROM THE CUTOUT. REPAIRED PE
- [SDR DL757972503](https://openairdocs.org/sdr/DL757972503), Dec 1, 1997: SILL. CORRODED. CORROSION WAS FOUND ON THE C1 DOOR LWR SILL OUTBD CHORD. REPAIRED PER ERA 331050-14.
- [SDR DL757962731](https://openairdocs.org/sdr/DL757962731), Dec 9, 1996: BUSHING. WORN. DURING ACCOMPLISHMENT OF INSPECTION PER OPN 8201, OUTBOARD MIDSPAR FITTING BUSHING ON THE NR 2 ENGINE WAS FOUND TO HAVE MIGRATED .150 AND WAS LOOSE. THIS ER/A A
- [SDR DL757954798](https://openairdocs.org/sdr/DL757954798), Dec 10, 1995: SKIN. CRACKED. PYLON SKIN CRACKED NR 2 PYLON O/B SIDE AT FWD ACCESS HOLE, 1 PLACE. REMOVED FASTENERS/CRACK PER SRM 54-51-01 AND INSTALLED DOUBLER PER SRM 54-51-01.
- [SDR DL757954797](https://openairdocs.org/sdr/DL757954797), Dec 10, 1995: SKIN. CRACKED. PYLON SKIN CRACKED NR 2 PYLON I/B SIDE AT FWD ACCESS HOLE, 2 PLACES. DRILLED OUT ALL FASTENERS, CUT OUT DAMAGED AREA, DRILLED AND INSTALLED REPAIR PER 54-50-01 
- [SDR DL757953931](https://openairdocs.org/sdr/DL757953931), Oct 7, 1995: LATCHING MECH. OUT OF RIG. CLIMBING THROUGH 2500 FT, CENTER ENTRY DOOR LIGHT ILLUMINATED. DOOR HANDLE WAS HELD CLOSED BY FLIGHT ATTENDANT TO PREVENT IT MOVING TO OPEN POSITION. INSPECTED 
- [SDR DL757952622](https://openairdocs.org/sdr/DL757952622), Jun 14, 1995: RADOME. DELAMINATED. RADOME WAS ROUTED TO SHOP FOR DELAMINATION, DUE TO LIGHTNING STRIKE. REPAIRED PER SRM 53-10-72.
- [SDR DL757951938](https://openairdocs.org/sdr/DL757951938), May 8, 1995: SKIN. DELAMINATED. DURING SHOP INSP, THE T/E WEDGE WAS FOUND TO BE DELAMINATED. REPLACED T/E WEDGE PER SRM 57-43-02 FIG 202.
- [SDR DL757951905](https://openairdocs.org/sdr/DL757951905), May 4, 1995: TE SKIN. CRACKED. FOUND DURING LETTER CHECK, I/B FLAP BOTTOM T/E CRACKED O/B OF AFT TRUNNION FAIRING, LT WING. REPAIRED PER SRM 51-70-07 AND PAINTED.
- [SDR DL757951904](https://openairdocs.org/sdr/DL757951904), May 4, 1995: RADOME. DENTED. DURING LETTER CHECK, FOUND RADOME WITH DAMAGED AREA AT RBL 34.5, WL 190, A 1 BY 7 DENT ON RT SIDE. REPAIRED DAMAGED AREA OF RADOME AS PER SRM 53-10-72 AND PAINT
- [SDR DL757951849](https://openairdocs.org/sdr/DL757951849), May 2, 1995: SKIN. DELAMINATED. UPPER OUTBOARD SECTION OF TRAILING EDGE WEDGE DELAMINATED. LOWER SKIN OF TRAILING EDGE WEDGE PUNCTURED. REPLACED TRAILING EDGE WEDGE AS PER SRM 57-43-02. FOUND 

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