# N610DL: 1985 Boeing 757-232, registration cancelled 2019-02-12

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 12, 2019
- Status when cancelled: Valid registration
- Airframe: [Boeing 757-232](https://openairdocs.org/model/boeing-757-232) (registry code 1384965)
- Data sheets: [TCDS A2NM](https://openairdocs.org/tcds/A2NM) (OpenAirDocs)
- Serial number: 22817
- Year built: 1985
- Type of aircraft: Fixed wing multi engine
- Certificate issued: January 4, 2018
- Last registry action: January 4, 2018
- Mode S code: A7EF14
- 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/N610DL
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=610DL
- Page: https://openairdocs.org/deregistered/N610DL-2019-02-12

From the FAA registry file of November 4, 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 (67, newest 50)

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

- [SDR DALA2014110605970](https://openairdocs.org/sdr/DALA2014110605970), Nov 2, 2014: COVER. DAMAGED. AFT RT R4 BUSTLE DAMAGED. REPLACED BUSTLE COVER.
- [SDR DALA2014081104411](https://openairdocs.org/sdr/DALA2014081104411), Aug 9, 2014: WARNING MESSAGE. FALSE ACTIVATION. LT ENGINE FIRE EICAS MESSAGE ILLUMINATED IN FLIGHT. PERFORMED ENGINE FIRE AND OVERHEAT DETECTION SYSTEM BITE IAW MM 26-11. BITE TESTED GOOD.
- [SDR DALA14014260610](https://openairdocs.org/sdr/DALA14014260610), Mar 1, 2014: DOUBLER. CRACKED. RIGHT APU COMPARTMENT DOOR 316AR REPAIR DOUBLER AT THE MIDDLE CLOSE LATCH HAS TWO CRACKS AT CUTOUT. REMOVED CRACKS AS REQUIRED. NDT ACCOMPLISHED-NO DEFECTS FOUN
- [SDR DALA14014250610](https://openairdocs.org/sdr/DALA14014250610), Mar 1, 2014: SKIN. DAMAGED. LOWER EXTERIOR FUSELAGE, E & E COMPARTMENT DOOR EXTERIOR SKIN HAS A DENT WITH GOUGE IN CENTER. BLEENDED SKIN OF E/E DOOR IAW SRM B757 52-40-01. FOUND TO BE OUT 
- [SDR DALA1318100610](https://openairdocs.org/sdr/DALA1318100610), Sep 2, 2013: LATCH. FAILED. SHIP 610, DURING PASS OXYGEN DOOR DEPLOYMENT TEST THE FOLLOWING DOORS FAILED TO OPEN. 20ABC, 21ABC, 27DEF, 29ABC, 33ABC, 38ABC, 41DEF. REPLACED AFFECTED DOORLAT
- [SDR DALA1318090610](https://openairdocs.org/sdr/DALA1318090610), Sep 2, 2013: LATCH. FAILED. MASKS FAILED TO DEPLOY WHEN LOSS OF CABIN PRESSURE -3A/B, 26ABC, 36DEF. REPLACED DOOR LATCH ACTUATORS 3A/B AND 26ABC. OPS CHECKED OK INCLUDING 36DEF. REF AMM 35
- [SDR DALA1317950610](https://openairdocs.org/sdr/DALA1317950610), Sep 2, 2013: CONTROLLER. FAILED. AUTO INOP LIGHT ILLUMINATED WITH CABIN ALTITUDE, DEPLOYED PASSENGER OXYGEN MASKS. BITE CHECKED BOTH CABIN PRESSURE CONTROLLERS NR 1 FAULTS AC PWER LOSS REPLACED
- [SDR DALA1317410610](https://openairdocs.org/sdr/DALA1317410610), Aug 15, 2013: LIGHT. INOPERATIVE. EMERGENCY LIGHT ABOVE SEAT 1B AND 4B INOPERATIVE, REPLACED LIGHT ASSY AT 1B AND FUSE ON POWER SUPPLY, OPS NORMAL.
- [SDR DALA1317240610](https://openairdocs.org/sdr/DALA1317240610), Aug 2, 2013: CHARGER. INOPERATIVE. EMERGENCY LIGHTS OUT AT ROW 40C. R & R AFT EMERGENCY LIGHT BATTERY CHARGER IAW AMM 33-51. OPS CHECKED GOOD.
- [SDR DALA1309040610](https://openairdocs.org/sdr/DALA1309040610), Apr 9, 2013: DOUBLER. CORRODED. SURFACE CORROSION FOUND ON LWR TCAS ANTENNA AND DOUBLER. REMOVED OLD DOUBLER AND CLEANED IAW SRM 43-00-01. PERFORMED DETAILED INSPECTION. TREATED AND PRIMED IAW
- [SDR DALA1301060610](https://openairdocs.org/sdr/DALA1301060610), Jan 11, 2013: STANCHION. DAMAGED. DURING OPS 25505, FOUND ONE STANCHION MISSING OFF RT SIDE OF RESTRAINT AFT OF DOOR. REPAIRED AND INSTALLED STANCHION IAW SRM 51-70-11, FIG 1.
- [SDR DALA1300480610](https://openairdocs.org/sdr/DALA1300480610), Jan 4, 2013: FILTER. LEAKING. SUSPECTED LT ENG FUEL LEAK DUE TO FUEL CONFIG LIGHT ILLUM WITH 3.7 IN LT TANK AND 6.3 IN RT TANK. LT FUEL QTY DROPPING. MX REPLACED THE FUEL PUMP FILTER AND RAN
- [SDR DALA1232480610](https://openairdocs.org/sdr/DALA1232480610), May 16, 2012: WIRE. BROKEN. DURING INSPECTION, MAINTENANCE DISCOVERED SEAT ROW 42D EMERGENCY LIGHTS INOPERATIVE. FOUND BROKEN LIGHT ASSY WIRING AND REPLACED LIGHT ASSY. OPERATES NORMAL.
- [SDR DALA1156940610](https://openairdocs.org/sdr/DALA1156940610), Oct 4, 2011: FLOOR SUPPORT. PUNCTURED. DUE ERA 49384-14MA TIME LIMITED REPAIR AT PUNCTURE AFT CARGO FLOOR STATION 1380. DRILLED UP REPAIR DOUBLER AND CLEANED UP HOLE PER ERA 489384-14MA REV C. HFEC I
- [SDR DALA1156930610](https://openairdocs.org/sdr/DALA1156930610), Oct 4, 2011: FLOOR SUPPORT. PUNCTURED. PUNCTURE IN AFT CARGO FLOOR CENTERLINE AT STA 1380. DRILLED UP REPAIR DOUBLER AND CLEANED UP HOLE PER ERA 489384-14MA. HFEC INSP PER ERA 489384-14MA REV C. NO C
- [SDR DALA1125210610](https://openairdocs.org/sdr/DALA1125210610), Apr 9, 2011: LIGHT. INOPERATIVE. DURING A LAYOVER CHECK, MAINTENANCE FOUND THE AFT TWO OVERHEAD COMPARTMENT EMERGENCY PATH LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY. OPERATIONAL
- [SDR DALA1011760610](https://openairdocs.org/sdr/DALA1011760610), May 28, 2010: UNKNOWN. ODOR. BURNED BALLAST SMELL NOTED IN OVERHEAD ABOVE SEAT 3DEF. TURNED LIGHTS OFF AND ODOR DISSIPATED. INSPECTED OVERHEAD LIGHTS, BALLASTS, PSUS AROUND ROW 31DEF. RAN B
- [SDR DL757100237](https://openairdocs.org/sdr/DL757100237), Feb 1, 2010: POWER SUPPLY. INOPERATIVE. DURING EMERGENCY EGRESS LIGHTING TEST, AISLE LIGHTING AT ROWS 39-44 FAILED AFTER ONE MINUTE. REPLACED AFT POWER SUPPLY AND BATTEY PACK, CHECKS OK.
- [SDR DL757081815](https://openairdocs.org/sdr/DL757081815), Dec 30, 2008: MOUNT. WORN. DURING HMV, THE RT MLG DOOR CENTER MOUNT FITTING, HINGE SUPPORT AND BRACKET ATTACHMENT HOLES WERE FOUND TO BE WORN AND ELONGATED. THE HOLES WERE CLEANED UP TO R
- [SDR DL757081802](https://openairdocs.org/sdr/DL757081802), Dec 29, 2008: SKIN. CORRODED. DURING HMV, CORROSION WAS FOUND UNDER THE AIRFONE ANTENNA BLANKING DOUBLER AT STA 1510, RT. THE CORRODED SKIN SECTION WAS CUT OUT AND AN SRM SKIN REPAIR WAS INS
- [SDR DL757081811](https://openairdocs.org/sdr/DL757081811), Dec 29, 2008: SKIN. CORRODED. EXTERNAL SKIN AT BS 1510-1520 UNDER RT AIRPHONE ANTENNA HAS CORROSION. COMPLIED WITH AT SAA, SAT ON NON ROUTINE 81723520001.
- [SDR DL757081810](https://openairdocs.org/sdr/DL757081810), Dec 29, 2008: SILL. CORRODED. AFT CARGO COMP BETWEEN BS 1380 TO 1440 RBL 21 HAS THE LOWER SILL OF NR 2 CARGO DOOR WITH SEVERAL CORRODED AREAS AT UPPER SURFACE, CP53-156-021/COMPLIED WITH AT 
- [SDR DL757081809](https://openairdocs.org/sdr/DL757081809), Dec 29, 2008: STRINGER. CORRODED. AFT CARGO FUSELAGE S28L BS 1506 HAS EXFOLIATION CORROSION C/W AT SAA - SAT ON NON ROUTINE 81720380001.
- [SDR DL757081805](https://openairdocs.org/sdr/DL757081805), Dec 29, 2008: STRINGER. CORRODED. AFT CARGO BETWEEN STA, 1500 AND STA, 1520 STRINGER S-29R FOUND WITH CORROSION AS MARKED. COMPLIED WITH AT SAA, SAT ON NON-ROUTINE 8172105000.
- [SDR DL757081804](https://openairdocs.org/sdr/DL757081804), Dec 29, 2008: SEAT TRACK. CORRODED. CABIN COMPARTMENT FLOOR SEAT TRACK FOUND WITH CORRSION ON TOP SURFACE INBD FLANGE AT SAT, 1435 LBL48 AS MARKED W/L 208-10/COMPLIED WITH AT SAA -SAT ON NON- ROUT
- [SDR DL757081803](https://openairdocs.org/sdr/DL757081803), Dec 29, 2008: INTERCOSTAL. CORRODED. AFT CARGO BETWEEN SAT, 1540 - SAT: 1560 BETWEEN STRINGERS S-26R AND S-27R FOUND SUPPORT WEB (INTERCOSTAL) WITH CORROSION AS MARKED C53-162-01L, COMPLIED WITH AT
- [SDR DL757081797](https://openairdocs.org/sdr/DL757081797), Dec 27, 2008: SEAT TRACK. CORRODED. CABIN COMPT FLOOR SEAT TRACK FOUND WITH CORROSION ON TOP SURFACE INBOARD FLANGE AT BS 1435 LBL 48 AS MARKEDW/L08-10. COMPLIED WITH AT SAA- SAT ON NON ROUTINE 81
- [SDR DL757081796](https://openairdocs.org/sdr/DL757081796), Dec 27, 2008: O2 GENERATOR. DAMAGED. FOUND ONE BLOWN OXYGEN CHEMICAL GENERATOR SN ARYD-F010-510 ON INSPECTION OF OXYGEN GENERATORS. COMPLIED WITH AT SAA- SAT ON N/R 81698450001 AND N/R 81707610001.
- [SDR DL757081795](https://openairdocs.org/sdr/DL757081795), Dec 27, 2008: FAILSAFE. CORRODED. FAIL/SAFE STRAP CORRODED AT STA 900 SKIN BUTT JOINT BELOW WINDOW BELT RT SIDE OF FUSELAGE. COMPLIED WITH AT SAA SAT ON NON ROUTINE 81716550001.
- [SDR DL757081793](https://openairdocs.org/sdr/DL757081793), Dec 27, 2008: FITTING. CORRODED. FITTING AT BOTTOM OF AFT CARGO DOOR OPENING CORRODED ON BOTTOM STA 1400, NEW DOOR FITTING EXISTING PLATE AND NEW TIE DOWN FITTING INSTALLED IAW SRM 51-40-02 PG 
- [SDR DL757081790](https://openairdocs.org/sdr/DL757081790), Dec 24, 2008: BELLMOUTH. CRACKED. DURING HMV, CRACKS WERE FOUND IN THE APU AIR INTAKE PLENUM BELLMOUTH. THE CRACKING WAS ADDRESSED IN BOEING SERVICE BULLETIN 757-49-0011 AND THE CRACKED BELLMOUT
- [SDR DL757081305](https://openairdocs.org/sdr/DL757081305), Oct 6, 2008: SKIN. DAMAGED. LIGHTNING STRIKE DAMAGE WAS FOUND IN THE FUSELAGE SKIN FORWARD OF STA 560 AT S-9R. THE DAMAGE WAS CUT OUT AND REPAIRED PER ER/A 06-450569-14 WITH BOEING APPROVA
- [SDR DL757080833](https://openairdocs.org/sdr/DL757080833), May 4, 2008: DUCT. CRACKED. AT FLT LVL 240 WITH ENGINE AND WING ANTI-ICE ON LEFT ENG BLEED LIGHT ILLUMINATED. FOLLOWED QRH SHUT BLEED SW OFF. OPENED ISOLATION VLV AT FLT LVL 260 RIGHT ENGI
- [SDR DL757070631](https://openairdocs.org/sdr/DL757070631), May 26, 2007: SKIN. DAMAGED. LIGHTNING DAMAGE IN FUSELAGE SKIN S-4L LAP SPLICE. CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLERS.
- [SDR DL75K060561](https://openairdocs.org/sdr/DL75K060561), Jul 8, 2006: SKIN. LIGHTNING STRIKE. REPAIR TO LIGHTNING STRIKE REQUIRED REMOVAL AND INSTALLATION WITH SOLID FASTENERS. CORRECTIVE ACTION PER ERA 450656-14 REV B.
- [SDR DL75K060401](https://openairdocs.org/sdr/DL75K060401), May 17, 2006: VALVE. MALFUNCTIONED. ON T/O FROM LGA, HAD DOOR LIGHT ILLUMINATE AND GEAR DOOR EICAS MSG WITH GEAR HANDLE UP, SAME LIGHT WHEN PUT GEAR DOWN T/S PER M/M CYCLED NOSE GEAR DOOR OPS NML.
- [SDR DL757081592](https://openairdocs.org/sdr/DL757081592), Oct 27, 2005: SKIN. CRACKED. SUPPLEMENTAL SDR FUSELAGE/SKIN L-1 DOOR CUTOUT/UPPER FWD CORNER-CRACK IAW ERA 090914-14. C/W ERA 090914-14.
- [SDR DL75K050610](https://openairdocs.org/sdr/DL75K050610), Sep 23, 2005: SKIN PANEL. DAMAGED. LIGHTNING STRIKE DAMAGE TO THE FUSELAGE SKIN AT FS 520 ABOVE STR 10R. INSTALLED REPAIR DOUBLER PER ER/A 450613-14.
- [SDR DL75K050595](https://openairdocs.org/sdr/DL75K050595), Sep 23, 2005: SKIN. LIGHTNING STRIKE. LIGHTNING STRIKE DAMAGE TO THE FUSELAGE SKIN AT FS 878, ABOVE STRINGER 4R. DAMAGE TO OUTER SKIN ONLY AT A PRODUCTION FASTENER LOCATION. REPAIR DOUBLER INSTALLED
- [SDR DL757030991](https://openairdocs.org/sdr/DL757030991), Nov 8, 2003: PSEU. FAULTY. DIVERSION TO PHX - APPARENT GROUND PROX SYS ERROR-AT CRUISE ALT GOT F/O PITOT- RT AUX PITOT- TAT - A/T DISC - PROBE HEAT CAUTIONS. LEFT GREEN SIDE OF NOSE AND R
- [SDR DL757030033](https://openairdocs.org/sdr/DL757030033), Jan 3, 2003: FITTING. CRACKED. DURING ACCOMPLISHMENT OF EO 6-75079-3 OPN 0206, A CRACK WAS FOUND IN THE RIGHT WING UPPER LINK WING FITTING OUTBOARD LUG. REPAIRED PER ER/A 389433-14. BORE OVER
- [SDR DL757030017](https://openairdocs.org/sdr/DL757030017), Jan 2, 2003: SILL. CORRODED. THE OUTER CHORD OF THE C2 DOOR OPENING WAS FOUND CORRODED. TO REMOVE THE CHORD, THE FS 1440 FRAME OUTER CHORD AND WEB WERE CUT AND THE LOWER ENDS REMOVED. A NEW
- [SDR DL757030016](https://openairdocs.org/sdr/DL757030016), Jan 2, 2003: FLOORBEAM. CORRODED. THE UPPER CAP OF THE FS 377 FLOORBEAM WAS FOUND CORRODED. THE UPPER CAP WAS TRIMMED OFF AND A NEW SECTION FABRICATED. DURING INSTALLATION OF THE NEW SECTION, SE
- [SDR DL757030015](https://openairdocs.org/sdr/DL757030015), Jan 2, 2003: SKIN. DENTED. FUSELAGE / SKIN / FS 1694 / STRG. 13L-15L : DENT REPAIR THE FUSELAGE SKIN WAS FOUND DENTED ABOVE AN EXISTIN REPAIR FOR A SMALL CUTOUT. THE DENT WAS CUTOUT AND T
- [SDR DL757030014](https://openairdocs.org/sdr/DL757030014), Jan 2, 2003: FLOORBEAM. CORRODED. THE UPPER CAP OF THE FS 1681 FLOORBEAM WAS FOUND WITH SEVERAL AREAS OF CORROSION. TO REMOVE ALL OF THE DAMAGE, THE UPPER CAP WAS TRIMMED OFF FROM LBL 60 TO RBL 
- [SDR DL757030013](https://openairdocs.org/sdr/DL757030013), Dec 31, 2002: SILL. CORRODED. THE INNER CHORD OF THE LOWER SILL OF THE C1 DOOR OPENING WAS FOUND WITH CORROSION AND TOOLING DAMAGE. THE INNER CHORD WAS REMOVED AND DISCARDED. A NEW CHORD WAS
- [SDR DL757021485](https://openairdocs.org/sdr/DL757021485), Dec 29, 2002: SKIN. GOUGED. FUSELAGE / SKIN / FS 600 / STRG. 26L-27L : GOUGE REPAIR THE FUSELAGE SKIN WAS FOUND WITH 3 GOUGES AT FS 600 BETWEEN STRINGERS 26L & 27L. THE GOUGES WERE REMOVED
- [SDR DL757021454](https://openairdocs.org/sdr/DL757021454), Dec 17, 2002: SUPPORT FITTING. DAMAGED. DURING COMPLETION OF PYLON MOD EO 6-70332-3AD, HOLE NR 2 IN LEFT WING SUPPORT FITTING HAD DAMAGE THAT REQUIRED REMOVAL PRIOR TO FASTENER INSTALLATION. REPAIRED 
- [SDR DL757021453](https://openairdocs.org/sdr/DL757021453), Dec 17, 2002: SUPPORT FITTING. TOOL DAMAGE. DURING ACCOMPLISHMENT OF PYLON MOD EO 6-70332-3AD, HOLE 5 IN THE LEFT WING SUPPORT FITTING HAD DAMAGE THAT REQUIRED REMOVAL PRIOR TO FASTENER INSTALLATION. REPA
- [SDR DL757021452](https://openairdocs.org/sdr/DL757021452), Dec 17, 2002: FITTING. GOUGED. WHILE WORKING PYLON MOD EO 6-70332-3AD, HOLE NR 65 IN RIGHT WING SIDE LOAD FITTING WAS GOUGED. REPAIRED PER ER/A 389430-14AD. REPAIR OVERSIZED HOLE TO REMOVE DA

All 67: https://openairdocs.org/deregistered/N610DL-2019-02-12/reports.md

## 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 20080710856279I](https://openairdocs.org/incident/20080710856279I), Jul 10, 2008: Boeing 757232 (N610DL), Birmingham, AL, No damage. On 07/10/2008, delta airlines flight 772 encountered compressor stalls on the #1 engine while cruising at FL 390. The Boeing 757 enroute from dfw to atl…
- [Incident 19911028059759I](https://openairdocs.org/incident/19911028059759I), Oct 28, 1991: Boeing 757232 (N610DL), Columbus, OH, Minor damage. Aluminum ladder sucked into NR1 engine intake prior to shut down. Ladder not in storage area.

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