# N135DL: 1991 Boeing 767-332, registration cancelled 2017-07-21

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: July 21, 2017
- Status when cancelled: Valid registration
- Airframe: [Boeing 767-332](https://openairdocs.org/model/boeing-767-332) (registry code 1385101)
- Engine: [GE CF6-80 series](https://openairdocs.org/engine/ge-cf6-80-series) (registry code 30025)
- Data sheets: [TCDS A1NM](https://openairdocs.org/tcds/A1NM), [TCDS E13NE](https://openairdocs.org/tcds/E13NE) (OpenAirDocs)
- Serial number: 25145
- Year built: 1991
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 1, 1991
- Certificate issued: August 3, 2010
- Last registry action: October 24, 2014
- Mode S code: A08E1A
- 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/N135DL
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=135DL
- Page: https://openairdocs.org/deregistered/N135DL-2017-07-21

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 767-332: https://openairdocs.org/model/boeing-767-332.md

## Service difficulty reports (62, newest 50)

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

- [SDR DALA1170460135](https://openairdocs.org/sdr/DALA1170460135), Mar 14, 2011: SKIN. DELAMINATED. DELAMINATION ON UPPER SKIN. ER/A PERFORMED TO REPLACE UPPER SKIN AND CORE. ER/A 492681-14 REV A. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS
- [SDR DL76S091399](https://openairdocs.org/sdr/DL76S091399), Aug 25, 2009: SKIN. DENTED. HAIL DAMAGE DENTS FOUND ON UPPER SKIN OF INBOARD AFT FLAP DURING MTC. DENTS TOO CLOSE TO EXISTING DOUBLERS FOR NEW LOCAL REPAIRS. REPLACEMENT OF UPPER SKIN AND 
- [SDR DL76S091521](https://openairdocs.org/sdr/DL76S091521), Jan 27, 2009: FITTING. FRACTURED. NR 2 PYLON INBOARD MIDSPAR FITTING WAS REPAIRED IAW ERA 472678-14. C/W 472678-14.
- [SDR DL76S090115](https://openairdocs.org/sdr/DL76S090115), Jan 27, 2009: FITTING. FRACTURED. DURING ACCOMPLISHMENT OF INSPECTIONS PER ROUTINE OPN 5281AD (EA 01-074944-12AD, ME-02) THE AFT MOST INBOARD BOLT THROUGH THE NR 2 PYLON INBOARD MIDSPAR FITTING 
- [SDR DL76S090011](https://openairdocs.org/sdr/DL76S090011), Jan 3, 2009: SLIDE. DAMAGED. UPON ARRIVAL TO GATE T-1 IN ATL AFTER ENGINE SHUTDOWN AND BEFORE JETWAY ARRIVAL THE L-1 DOOR SLIDE DEPLOYED. FOUND L-1 DOOR SLIDE RIPPED BY JETWAY REMOVED AND R
- [SDR DL76S071163](https://openairdocs.org/sdr/DL76S071163), Sep 2, 2007: SKIN. CRACKED. REPAIR REMOVED THAT WAS OUT OF SCOPE FOR AD2006-09-09. UNDERLYING CHORD FOUND CRACKED. DAMAGE WAS CUTOUT AND REPAIR DOUBLER AND TRIPLER WAS INSTALLED.
- [SDR DL76S071157](https://openairdocs.org/sdr/DL76S071157), Aug 28, 2007: SUPPORT BEAM. CORRODED. FROM NR 185 PSV 15, NUMBER 4 FLAP SUPPORT BEAM HAS PITTING IN FORWARD MOUNT HOLES. REPAIRED PER ERA 089397-14MA REV O.
- [SDR DL76S071095](https://openairdocs.org/sdr/DL76S071095), Aug 18, 2007: GRND AIR VALVE. OPEN. AFTER TAKEOFF, GOT FWD EQPT OVHT EICAS WENT TO STBY AS PER QRH. 5 MINS LATER CAME BACK ON WENT TO OVRD AS PER QRH. AT 35K, ALT CABIN PRESS CLIMBED ABOVE 11K AND
- [SDR DL76S070173](https://openairdocs.org/sdr/DL76S070173), Feb 28, 2007: ENGINE. MAKING METAL. LT ENG INOP, ON DESCENT LOUD BOOM AND SERVERE VIBS-ENG CONT TO RUN UNTIL SHUTDOWN-THRUST LOST. FOUND METAL IN TAILPIPE. REMOVED AND REPLACED NR 1 ENGINE ON ROUN
- [SDR DL76S060479](https://openairdocs.org/sdr/DL76S060479), Jun 9, 2006: GASKET. OUT OF POSITION. CLIMBING THROUGH 10000 FT LEFT ENGINE FAILED TO A NEAR FLIGHT IDLE CONDITION. OPENED ENGINE FOUND FUEL LEAK AT MANIFOLD TO FUEL/OIL COOLER REALIGNED GASKET PLAT
- [SDR DL76S060337](https://openairdocs.org/sdr/DL76S060337), Apr 29, 2006: ENGINE. LEAKING. LEFT ENGINE HOC B SUMP LEAKING, ITEM WILL REQUIRE A ENGINE CHANGE. FOUND OIL LEAKING FROM NR 6 BEARING B-SUMP BREATHER EXHAUST REPLACED NR 1 ENG PER TRANS 1T144
- [SDR DL76S050694](https://openairdocs.org/sdr/DL76S050694), Nov 10, 2005: LINE. LEAKING. IN FLIGHT EICAS MESSAGES C-HYD PRESS AND C-HYD QTY SHOWED .07RF, LATER WENT TO ZERO. CENTER ELEC 1 AND 2 PRESS AND CENTER AIR PRESS LIGHTS ILLUMINATED. C/W QRH 
- [SDR DL76S050139](https://openairdocs.org/sdr/DL76S050139), Feb 28, 2005: CONTROLLER. MALFUNCTIONED. NR 1 ENG WOULD NOT ACHIEVE T/O POWER WITH ANTI-ICE ON OR OFF. RETURNED TO GATE. REPLACED MAIN ENGINE CONTROLLER.
- [SDR DL76S040501](https://openairdocs.org/sdr/DL76S040501), May 30, 2004: TURBINE BLADES. DAMAGED. RT ENGINE EGT 950 ON TAKEOFF FOR LESS THAN ONE MINUTE. FOUND LPT BLADES DAMAGED AND BROKEN PER FIM. REPLACED NR 2 ENGINE PER JIC CARD DECK 1T145. C/W NR 2 ENGIN
- [SDR DL76S040407](https://openairdocs.org/sdr/DL76S040407), May 7, 2004: CHARGER. MALFUNCTIONED. MAIN BATTERY CHARGER STATUS MSG. REPLACED MAIN BATTERY CHARGER PER M/M, NO HELP. REPLACED MAIN SHIPS BATTERY PER M/M. ALL CKS NORMAL PER M/M.
- [SDR DL76S031021](https://openairdocs.org/sdr/DL76S031021), Nov 16, 2003: CIRCUIT BREAKER. TRIPPED. AT CRUISE, F/A REPORTED ELECTRICAL ODOR THRU OUT CABIN. DID ELECTRICAL SMOKE CHECKLIST AND PULLED C/BS ON VIDEO SYS. TURNED OFF RT RECIR FAN, THAT WAS REPORTED 
- [SDR DL76S030533](https://openairdocs.org/sdr/DL76S030533), Jun 10, 2003: POWER SUPPLY. INOPERATIVE. EMERGENCY LIGHTS FROM ROW 34 AND BACK BOTH SIDES INOP. FOUND SHORTED SEAT HARNESS AT SEAT 36AB REPAIRED SAME. REPLACED PWR SUPPLY D9048 DUE TO BLOWN FUSE.
- [SDR DL76S020676](https://openairdocs.org/sdr/DL76S020676), Jun 16, 2002: SWITCH. LOOSE. STANDY BY POWER SWITCH LOOSE INTERNALLY CAUSING ALL THREE IRS'S TO FAIL . THIS HAPPENED IN FLIGHT ON PREV LEG. REF LOG SHEETS 792866 ITEM 2 AND 792871 ITEM 1 FO
- [SDR DL76S011012](https://openairdocs.org/sdr/DL76S011012), Jun 19, 2001: PIN. BACKED OUT. PAX SEAT 31A EMERGENCY LIGHTS WON`T TEST. FOUND PULLED/BACKED OUT PIN IN SEAT HARNESS. REPAIRED SAME.
- [SDR DL76S010934](https://openairdocs.org/sdr/DL76S010934), Jun 8, 2001: GASKET. LEAKING. LT ENG FIRE INDICATIONS SHORTLY AFTER TAKEOFF THROTTLE. RETARDED TO IDLE AND FIRE INDICATION WENT OUT. FOUND ALL THERMOCOUPLE GASKETS LEAKING. REPLACED GASKETS,
- [SDR DL76S010656](https://openairdocs.org/sdr/DL76S010656), Apr 21, 2001: LIGHT. INOPERATIVE. FOUND RED EMERGENCY LIGHT INOP AT AFT R/H LAV. RELAMPED SAME OPS CK. GOOD.
- [SDR DL76S992156](https://openairdocs.org/sdr/DL76S992156), Sep 26, 1999: BULKHEAD CHORD. CRACKED. THE FS 1809.5 BULKHEAD OUTER CAP WAS FOUND WITH A CRACK TYPICAL OF BAC S/B 767-53-0078. THE CRACKED UPPER END OF THE CHORD WAS CUT AND REMOVED. A NEW SECTION WA
- [SDR DL76S991610](https://openairdocs.org/sdr/DL76S991610), Jul 18, 1999: SHUTOFF VALVE. CRACKED. CENTER HYDRAULIC RESERVIOR NEEDS FLUID. FOUND NR 10 SPOILER ELECTRONIC SHUTOFF VALVE LEAKING. REPLACED SAME.
- [SDR DL76S991016](https://openairdocs.org/sdr/DL76S991016), May 8, 1999: ENGINE. FAILED. LEFT ENGINE FAILED AT 6,000 FT. CLIMBOUT EGT REACHED 1,100, LITE ENGINE VIBRATION FELT FOLLOWED BY EGT SPIKE. REPLACED ENGINE.
- [SDR DL76S982620](https://openairdocs.org/sdr/DL76S982620), Dec 24, 1998: SWITCH. DIRTY. ON T/O, THE AMBER GEAR DOOR LIGHT REMAINED ILLUM FOR A UNUSUALLY LONG TIME AFTER GEAR RETRACT. ON APPROACH WITH GEAR EXTENDED AND THREE GREEN THE AMBER GEAR DOO
- [SDR DL76S981833](https://openairdocs.org/sdr/DL76S981833), Sep 3, 1998: SKIN. CRACKED. A CRACK WAS FOUND IN THE FUSELAGE SKIN NEAR AN EXISTING REPAIR. A SECTION OF SKIN PANEL IN THIS REGION WAS REMOVED AND A NEW ONE SPLICED IN BETWEEN STA 1197+77 
- [SDR DL76S980747](https://openairdocs.org/sdr/DL76S980747), Mar 31, 1998: SKIN. TORN. THE FUSELAGE SKIN AT FS 1197+110 WAS BADLY DAMAGED BY AN IMPACT FROM GROUND EQUIPMENT. THE SKIN WAS CUTOUT BETWEEN STR 35R AND 39L RESULTING IN A 15.5 X 19.5 CU
- [SDR DL76S972093](https://openairdocs.org/sdr/DL76S972093), Oct 18, 1997: POWER SUPPLY. INOPERATIVE. EMERGENCY FLOOR TRACK LIGHTS BETWEEN SEATS 10 AND 13 BOTH SIDES ARE OUT. REPLACED EMERGENCY FLOOR TRACK LIGHTS POWER SUPPLY ASSY M9008, OPS CK NORMAL.
- [SDR DL76S972092](https://openairdocs.org/sdr/DL76S972092), Oct 18, 1997: BULB. FAILED. LT AFT OVERWING EMERGENCY LIGHT OUT. RELAMPED SAME, OPS CK NORMAL.
- [SDR DL76S971563](https://openairdocs.org/sdr/DL76S971563), Aug 9, 1997: POWER SUPPLY. INOPERATIVE. LEFT WING SLIDE EMERGENCY ILLUMINATION LIGHTS AT STATION 1197, 1230 AND LEFT AFT DOOR EMERGENCY ILLUMINATION LIGHT INOP. REPLACED M738 POWER SUPPLY AND BATTERY 
- [SDR DL76S951930](https://openairdocs.org/sdr/DL76S951930), May 8, 1995: SKIN. DENTED. DURING SHOP VISIT, NR 6 L/E SLAT WEDGE WAS REPLACED DUE TO HAIL DAMAGE PER CMM 57-43-61.
- [SDR DL76S952287](https://openairdocs.org/sdr/DL76S952287), May 6, 1995: TE WEDGE. DENTED. T/E WEDGE DENTED TOP SURFACE. INSTALLED WEDGE PER CMM 57-43-55, FOR NR 4 L/E SLAT AT SHOP INSPECTION.
- [SDR DL76S951861](https://openairdocs.org/sdr/DL76S951861), May 3, 1995: TE WEDGE. DENTED. DURING SHOP INSPECTION, RT WING L/E SLAT PANEL WAS FOUND WITH HAIL DAMAGE TO T/E WEDGE. REPLACED WEDGE PER MM 57-43-55.
- [SDR DL76S952100](https://openairdocs.org/sdr/DL76S952100), May 2, 1995: SKIN. DELAMINATED. LT WING O/B AFT FLAP T/E WEDGE HAS SEVERAL DELAMINATED AREAS UPPER SURFACE. MADE REPAIRS PER SRM 51-70-17 REF 57-53-01 AND COMPLY WITH ERA 270849-14. DAMAGE FRO
- [SDR DL76S952099](https://openairdocs.org/sdr/DL76S952099), May 1, 1995: SKIN. DAMAGED. RT INBOARD ELEVATOR UPPER SURFACE DAMAGED BY HAIL. MADE BONDING REPAIRS. REPAIRED PER ERA 270806-14. DAMAGE FROM HAIL.
- [SDR DL76S951867](https://openairdocs.org/sdr/DL76S951867), May 1, 1995: SKIN. DENTED. NR 11 SLAT T/E WEDGE UPPER SURFACE DENTED. REPLACED WEDGE PER CMM 57-43-61.
- [SDR DL76S952252](https://openairdocs.org/sdr/DL76S952252), Apr 30, 1995: SKIN. DAMAGED. DURING SHOP INSPECTION, NR 9 L/E SLAT T/E WEDGE WAS REPAIRED FOR HAIL DAMAGE. REPAIRS ACCOMPLISHED PER SMR 57-43-55.
- [SDR DL76S952098](https://openairdocs.org/sdr/DL76S952098), Apr 30, 1995: SKIN. DENTED. RT WING UPPER SURFACE NR 8 SPOILER DENTED, REMOVED. REPAIRED PER B767 SRM 57-70-01 REF 51-70-17. DAMAGE FROM HAIL.
- [SDR DL76S952097](https://openairdocs.org/sdr/DL76S952097), Apr 30, 1995: SKIN. DENTED. RT WING O/B AFT FLAP UPPER SURFACE DENTED. REPAIRED AS PER SRM 51-70-06. DAMAGE FROM HAIL.
- [SDR DL76S952096](https://openairdocs.org/sdr/DL76S952096), Apr 30, 1995: SKIN. DENTED. RT WING I/B AFT FLAP UPPER SURFACE DENTED. REPAIRED TWO BONDED AREAS PER SRM 57-53-01 REF 51-70-10. FILLED AND SANDED ALL OTHER DENTS AND ALODINED PER 51-70-01.
- [SDR DL76S952095](https://openairdocs.org/sdr/DL76S952095), Apr 30, 1995: SKIN. DENTED. LT WING UPPER SURFACE OF I/B AILERON DENTED. REPAIRED AS PER SRM 57-60-01 REF 51-70-17. DAMAGE FROM HAIL.
- [SDR DL76S952094](https://openairdocs.org/sdr/DL76S952094), Apr 30, 1995: SKIN. DENTED. LT WING UPPER SURFACE OF NR 6 SPOILER DENTED. REMOVED AND INSTALLED ON RC7. REMOVED PANEL, REMOVED DAMAGE AND FABRICATED REPLACEMENT AS PER SRM 51070-17. REPAIR
- [SDR DL76S952093](https://openairdocs.org/sdr/DL76S952093), Apr 30, 1995: SKIN. DENTED. LT WING UPPER SURFACE OF NR 2 SPOILER DENTED. REPAIRED PER SRM 57-70-01. DAMAGE FROM HAIL.
- [SDR DL76S952092](https://openairdocs.org/sdr/DL76S952092), Apr 30, 1995: SKIN. DENTED. LT WING UPPER SURFACE NR 5 SPOILER DENTED. REMOVED AND REPAIRED PER SRM 51-70-17 REF FROM 57-70-01. DAMAGE FROM HAIL.
- [SDR DL76S952091](https://openairdocs.org/sdr/DL76S952091), Apr 30, 1995: SKIN. DAMAGED. RT ELEVATOR UPPER SURFACE DAMAGED. OUTBOARD ELEVATOR. SANDED AND POTTED AREAS OF DAMAGE AS PER SRM 55-70-01. REPAIRED PER SRM 55-70-01. REPAIRED PER ERA 270814-
- [SDR DL76S952090](https://openairdocs.org/sdr/DL76S952090), Apr 30, 1995: SKIN. DAMAGED. RT ELEVATOR UPPER SURFACE DAMAGED. OUTBOARD ELEVATOR. SANDED AND POTTED AREAS OF DAMAGE AS PER SRM 55-70-01. REPAIRED PER ERA 270814-14 AND SRM 55-70-01. DAMAGE
- [SDR DL76S952089](https://openairdocs.org/sdr/DL76S952089), Apr 30, 1995: SKIN. DENTED. LT WING UPPER SURFACE NR 6 SPOILER DENTED. REMOVED AND INSTALLED ON RC7. REMOVED PANEL. REMOVED DAMAGE AND FABRICATED REPLACEMENT CORE AS PER SRM 51-70-17. REPA
- [SDR DL76S952088](https://openairdocs.org/sdr/DL76S952088), Apr 30, 1995: SKIN. DAMAGED. RT ELEVATOR UPPER SURFACE DAMAGED, OUTBOARD ELEVATOR. SEALED AND POTTED AREAS OF DAMAGE AS PER SRM 59-70-00. REPAIRED PER ERA 270814-14. DAMAGE FROM HAIL.
- [SDR DL76S951907](https://openairdocs.org/sdr/DL76S951907), Apr 30, 1995: SKIN. DENTED. SLAT T/E WEDGE HAIL DAMAGED. REPAIRED PER CMM 57-43-61, FOR NR 3 L/E SLAT DURING SHOP VISIT.
- [SDR DL76S951885](https://openairdocs.org/sdr/DL76S951885), Apr 30, 1995: WEDGE. DENTED. DURING INSPECITON NR 1 SLAT WEDGE WAS FOUND DENTED FROM HAIL. REPLACED WEDGE PER SRM 57-43-61.

All 62: https://openairdocs.org/deregistered/N135DL-2017-07-21/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 20001213031499I](https://openairdocs.org/incident/20001213031499I), Dec 13, 2000: Boeing 767332 (N135DL), Salt Lake City, UT, Minor damage. (-23) Delta Boeing 767 (flight 1008) was taxiing for take off on runway 16R at Salt Lake City International Airport behind an air transport international…
- [Incident 19930412018139I](https://openairdocs.org/incident/19930412018139I), Apr 12, 1993: Boeing 767332 (N135DL), San Juan, Puerto Rico, No damage. Pilot aborted takeoff when he heard loud noise. Found metal particles in NR1 engine tail pipe.

## Other aircraft with N135DL

- [Registered now](https://openairdocs.org/aircraft/N135DL): Bellanca 8KCAB, S/N 3372

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