# N139DL: 1992 Boeing 767-332, registration cancelled 2017-05-10

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: May 10, 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: 25984
- Year built: 1992
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 8, 1992
- Certificate issued: May 11, 1992
- Last registry action: February 16, 2017
- Mode S code: A09CF6
- 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/N139DL
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=139DL
- Page: https://openairdocs.org/deregistered/N139DL-2017-05-10

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 (87, newest 50)

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

- [SDR DALA2016110108194](https://openairdocs.org/sdr/DALA2016110108194), Oct 30, 2016: LENS. DAMAGED. R1 EXTERIOR EMERGENCY LIGHT LENS DAMAGED. REPLACED LENS. SYSTEM OPERATION IS NORMAL.
- [SDR DALA2016103107974](https://openairdocs.org/sdr/DALA2016103107974), Oct 28, 2016: HOUSING. LOOSE. L1 DOOR SLIDE HOUSING FOUND LOOSE AND REINSTALLED. SYSTEM OPS NORMAL.
- [SDR DALA2016102807829](https://openairdocs.org/sdr/DALA2016102807829), Oct 27, 2016: PLATE. DAMAGED. SLIDE INDICATION LIGHT INOPERATIVE. REPLACED BASE PLATE. SYSTEM OPERATION IS NORMAL.
- [SDR DALA2016012800675](https://openairdocs.org/sdr/DALA2016012800675), Jan 27, 2016: WIRE. CUT. LAVATORY DOOR L4 RED MOUNTED EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE FOUND WIRE CUT AT CARPET AND KICK PANEL IS LOOSE, FED TEMP WIRE THROUGH HOLE AND REPL
- [SDR DALA2015100806009](https://openairdocs.org/sdr/DALA2015100806009), Oct 7, 2015: SUPPORT. DAMAGED. RIGHT WING OTBD T/E FLAP, THREE HOLES ON NR 7 SUPPORT 1-2-3 BEAM FASTNER HOLES HAS TOOLING DAMAGE. REPAIRED IAW ERA 539808-14.
- [SDR DALA2015100105910](https://openairdocs.org/sdr/DALA2015100105910), Oct 1, 2015: ANGLE. CRACKED. AT C-CHECK, BS 1809, RT OF HORIZONTAL ANGLE WL 257, BL 28, CRACKED AT FASTENER HOLE. ANGLE REPAIRED IAW SRM 53-80-08, REPAIR 10.
- [SDR DALA2015082705238](https://openairdocs.org/sdr/DALA2015082705238), Aug 15, 2015: LAMP. INOPERATIVE. EMERGENCY SEAT MOUNTED LIGHT DAMAGED AT SEAT 12B. REPLACED BUMPER, SHROUD AND REPLACED THE LAMP. SYSTEM OPS NORMAL.
- [SDR DALA2015060903950](https://openairdocs.org/sdr/DALA2015060903950), Jun 10, 2015: FILTER. NOT REPORTED. THE CREW SHUTDOWN RT ENGINE IAW QRH DUE TO LOSS OF FUEL FROM RT TANK. CREW ALSO REPORTED A RT HYDRAULIC EICAS MESSAGE. REPLACED RT ENGINE FUEL FILTER. SYSTEM OP
- [SDR DALA2014081904603](https://openairdocs.org/sdr/DALA2014081904603), Aug 18, 2014: SKIN. DENTED. DURING WALK AROUND, FOUND A DENT IN NR 4 SLAT ON LT WING. REPLACED THE SLAT.
- [SDR DALA13018610139](https://openairdocs.org/sdr/DALA13018610139), Apr 22, 2013: CONNECTOR. DAMAGED. SEAT EMERGENCY PATH LIGHTS FROM ROW 34-46AB ARE INOPERATIVE. MX RESET PIN 9 ON CONNECTOR D9048. SYS OPS IS NORMAL.
- [SDR DALA13018620139](https://openairdocs.org/sdr/DALA13018620139), Apr 21, 2013: POWER SUPPLY. INOPERATIVE. IN SEAT EMERGENCY PATH LIGHTING ROW 34AB-46 ARE INOPERATIVE. MX REPLACED THE POWER SUPPLY. SYS OPS IS NORMAL.
- [SDR DALA1309870139](https://openairdocs.org/sdr/DALA1309870139), Apr 16, 2013: WIRE. LOOSE. DURING SERVICE CHECK, FOUND EMERGENCY LIGHTS INOPERATIVE FROM ROW 34AB. MX FOUND LOOSE CONNECTOR AT SEAT 33AB. SECURED WIRE AND CONNECTOR, SYS OPS IS NORMAL.
- [SDR DALA1233060139](https://openairdocs.org/sdr/DALA1233060139), May 18, 2012: LIGHT. DAMAGED. EMERGENCY MOUNTED LIGHTING AT SEAT 37B DAMAGED AND INOPERATIVE. MAINTENANCE SECURED LIGHT MOUNTED. SYSTEM OPERATION IS NORMAL.
- [SDR DALA1220810139](https://openairdocs.org/sdr/DALA1220810139), Apr 1, 2012: BATTERY PACK. INOPERATIVE. DURING INSPECTION, EMERGENCY LIGHTING WAS FOUND INOPERATIVE FROM ROW 34 TO 45 ON THE RIGHT SIDE SEATS. MAINTENANCE REPLACED THE BATTERY PACK AT ROW 45. SYSTEM O
- [SDR DALA1207770139](https://openairdocs.org/sdr/DALA1207770139), Feb 13, 2012: FAIRING. DELAMINATED. RT WING I/B MAIN FLAP O/B FAIRING IS DELAMINATED AND REPAIRED PER B767-300 SRM 57-53-01 REPAIR 1 AND SRM 51-70-05 FIG 5 .
- [SDR DALA1207760139](https://openairdocs.org/sdr/DALA1207760139), Feb 13, 2012: SKIN. DENTED. RT WING O/B FLAP T/E LOWER SURFACE IS DENTED AND REPAIRED PER B767-300 SRM 57-53-01 REPAIR 1 AND SRM 51-70-06 FIG 9.
- [SDR DALA1207750139](https://openairdocs.org/sdr/DALA1207750139), Feb 13, 2012: SKIN. DELAMINATED. LT WING O/B FLAP UPPER SURFACE IS DELAMINATED JUST O/B OF THE NR 1 FLAP TRACK FAIRING AREA AND REPAIRED PER B767-300 SRM 57-53-01. REPAIR 1 AND SRM 51-70-06 FIG
- [SDR DALA1207740139](https://openairdocs.org/sdr/DALA1207740139), Feb 13, 2012: SKIN. DELAMINATED. LT WING O/B FLAP T/E UPPER SURFACE IS DELAMINATED JUST I/B OF NR 2 FLAP TRACK FAIRING AREA AND REPAIRED PER B767-300 SRM 57-53-01. REPAIR 1 AND SRM 51-70-06 FIG
- [SDR DALA1207730139](https://openairdocs.org/sdr/DALA1207730139), Feb 13, 2012: SKIN. DELAMINATED. RT WING O/B FLAP UPPER SURFACE IS DELAMINATED O/B OF THE NR 7 FLAP TRACK AREA AND REPAIRED PER THE B767-300 SRM 57-53-01. REPAIR 1 AND SRM 51-70-06 FIG 9.
- [SDR DALA1207720139](https://openairdocs.org/sdr/DALA1207720139), Feb 13, 2012: SKIN. DELAMINATED. RT WING O/B FLAP UPPER SURFACE IS DELAMINATED AT THE NR 7 FLAP TRACK AREA AND REPAIRED PER B767-300 SRM 57-53-01. REPAIR 1 AND SRM 51-70-06 FIG 9.
- [SDR DALA1207710139](https://openairdocs.org/sdr/DALA1207710139), Feb 13, 2012: SKIN. DELAMINATED. LT WING O/B FLAP UPPER SURFACE IS DELAMINATED APPROX 50" FROM I/B END AND REPAIRED PER B767-300 SRM 57-53-01. REPAIR 1 AND SRM 51-70-06 FIG 9.
- [SDR DALA1207700139](https://openairdocs.org/sdr/DALA1207700139), Feb 13, 2012: SKIN. DELAMINATED. RT WING O/B FLAP UPPER SURFACE IS DELAMINATED I/B OF THE NR 7 FLAP TRACK AREA AND REPAIRED PER B767-300 SRM 57-53-01 REPAIR 1 AND SRM 51-70-06 FIG 9 (NRC 50813)
- [SDR DALA1207020139](https://openairdocs.org/sdr/DALA1207020139), Feb 9, 2012: FITTING. DEFECTIVE. NR 2 PYLON UPPER LINK PITCH LOAD FITTING T-CLIPS 112T7010-14 O/B AND 112T7010-16 I/B HAVE SHORT EDGE MARGIN AT FASTENER HOLES (NRC 52406).
- [SDR DALA1207010139](https://openairdocs.org/sdr/DALA1207010139), Feb 9, 2012: FITTING. DEFECTIVE. NR 1 PYLON UPPER LINK PITCH LOAD FITTING T-CLIPS 112T7010-13 O/B AND 112T7010-15 I/B HAVE SHORT EDGE MARGIN (NRC 52405).
- [SDR DALA1206980139](https://openairdocs.org/sdr/DALA1206980139), Feb 8, 2012: FLOORBEAM. CORRODED. FS 1197 + 132 LBL 22 FLOORBEAM UPPER CHORD IS CORRODED AND REPLACED PER B767-300 SRM 51-10-02 PG 2 PARA 9 AND DWG 146T1229 SH 1.
- [SDR DALA1206850139](https://openairdocs.org/sdr/DALA1206850139), Feb 8, 2012: SEALANT. CRACKED. NR 1 PYLON UPPER SPAR FITTING AFT BUSHING SEALANT IS CRACKED AND REPAIRED PER B767-300 SRM 54-51-90 REPAIR 2 FIG 201.
- [SDR DALA1206830139](https://openairdocs.org/sdr/DALA1206830139), Feb 8, 2012: BUSHING. MIGRATED. NR 1 PYLON LWR AFT FITTING BUSHING MIGRATED AND REPAIRED PER B767-300 SRM 54-51-90 REPAIR 4 FIG 201.
- [SDR DALA1206820139](https://openairdocs.org/sdr/DALA1206820139), Feb 8, 2012: SEALANT. ACTIVATED. NR 2 PYLON LWR SPAR FITTING AFT BUSHING SEALANT CRACKED AND REPAIRED PER B767-300 SRM 54-51-90 REPAIR 4 FIG 201.
- [SDR DALA1206800139](https://openairdocs.org/sdr/DALA1206800139), Feb 8, 2012: SEALANT. CRACKED. NR 2 PYLON UPPER SPAR FITTING AFT BUSHING SEALANT IS CRACKED AND REPAIRED PER B767-300 SRM 54-51-90 REPAIR 2 FIG 201.
- [SDR DALA1206050139](https://openairdocs.org/sdr/DALA1206050139), Feb 6, 2012: FAIRING. CRACKED. RUDDER L/E FAIRING 324KL FOUND CRACKED. COMPOSITE PREPREG HOT BOND REPAIR CARRIED OUT AT CRACKED AREA AS PER B767-300 SRM 55-40-01 REPAIR 1 AND B767-300 SRM 51-
- [SDR DALA1206040139](https://openairdocs.org/sdr/DALA1206040139), Feb 6, 2012: PANEL. DAMAGED. RT HORIZONTIAL STAB L/E PANEL 342DR INNER SURFACE DETACHED. METAL HOT BOND REPAIR PERFORMED ON DETACHED AREA AS PER B767-300 SRM 55-10-01 REPAIR 1 FIGURE 201 AN
- [SDR DALA1206030139](https://openairdocs.org/sdr/DALA1206030139), Feb 6, 2012: FAIRING. CRACKED. RUDDER L/E FAIRING 324ML FOUND CRACKED. COMPOSITE PREPREG REPAIR CARRIED OUT AT CRACKED AREA AS PER B767-300 SRM 55-40-01 REPAIR 1 AND B767-300 SRM 51-70-04 FIG
- [SDR DALA1209440139](https://openairdocs.org/sdr/DALA1209440139), Feb 5, 2012: FASTENER. MISSING. NR 1 PYLON HAS FASTENER MISSING. FASTENER INSTALLED ACCOMPLISHED AS PER VA81913AD REV A.
- [SDR DALA1205960139](https://openairdocs.org/sdr/DALA1205960139), Feb 4, 2012: FASTENER. ACTIVATED. NR 1 PYLON MOD ERA 38671-14AD DWG 624T0016 SHEET 1. PRODUCTION FASTENER MISSING; PRI ISSUED NO FINAL REPAIR DATA AT THIS TIME.
- [SDR DALA1205950139](https://openairdocs.org/sdr/DALA1205950139), Feb 4, 2012: FASTENER. MISSING. NR 2 PYLON MOD ERA 389672-14AD DWG 624T0016 SHEET 1. PRODUCTION FASTENER MISSING; PRI ISSUED FOR WORK TO CONTINUE NO FURTHER REPAIR DATA AT THIS TIME.
- [SDR DALA1205940139](https://openairdocs.org/sdr/DALA1205940139), Feb 4, 2012: SPAR. MISREPAIRED. NR 1 PYLON FWD UPPER SPAR WEB; EXISTING REPAIR FASTENER PATTERN NOT SAME AS INDICATED IN SB767-54-008 REV 2 FIGURE 10. PRI REQUESTED FOR REPAIR. NO REPAIR DATA 
- [SDR DALA1209480139](https://openairdocs.org/sdr/DALA1209480139), Feb 1, 2012: SPAR. MISREPAIRED. NR 1 PYLON FWD UPPER SPAR WEB MISREPAIRED. REPAIRED PER ERA 499056-14.
- [SDR DALA1205540139](https://openairdocs.org/sdr/DALA1205540139), Feb 1, 2012: FAIRING. DELAMINATED. RIGHT WING I/B MAIN FLAP LEADING EDGE O/B FAIRING FOUND DELAMINATED.
- [SDR DALA1209980139](https://openairdocs.org/sdr/DALA1209980139), Jan 31, 2012: BULKHEAD. DAMAGED. NR 2 PYLON MIDSPAR AFT BULKHEAD AREA FASTENER HOLES LARGER THAN SB 767-54-0081 REV 1 DWG 624T0016 INDICATED. REPAIRED PER ERA 499052-14AD REV ORIG.
- [SDR DALA1209960139](https://openairdocs.org/sdr/DALA1209960139), Jan 31, 2012: BULKHEAD. DAMAGED. NR 1 PYLON MIDSPAR AFT BULKHD AREA FASTENER HOLES LARGER THAN SB 767-54-0081 REV 1 DWG 624T0016 INDICATES. REPAIRED PER ERA 499052-14AD REV ORIG.
- [SDR DALA1209470139](https://openairdocs.org/sdr/DALA1209470139), Jan 31, 2012: BULKHEAD WEB. CRACKED. NR 1 PYLON AFT BULKHEAD LEFT MID SPAR FITTING AFT BULKHEAD WEB CRACKED APPROX 1/16". CRACK REPAIRED PER ERA 499059-14AD REV ORIG.
- [SDR DALA1205390139](https://openairdocs.org/sdr/DALA1205390139), Jan 31, 2012: BULKHEAD. CRACKED. NR 1 PYLON AFT BULKHEAD LT MID SPAR FTG AFT BLKHD WEB NR 2 FASTENER HOLE CRACK APPROX 1/16 INCH.
- [SDR DALA1204900139](https://openairdocs.org/sdr/DALA1204900139), Jan 30, 2012: BULKHEAD. DAMAGED. NR 2 PYLON MID SPAR AFT BULKHEAD AREA EXISTING FASTENER HOLES LARGER THAN SB 767-54-0081 REV 1 DWG 624T0016 ST 1 INDICATES.
- [SDR DALA1204890139](https://openairdocs.org/sdr/DALA1204890139), Jan 30, 2012: BULKHEAD. DAMAGED. NUMBER 1 PYLON MID SPAR AFT BULKHEAD AREA EXISTING FASTENER HOLES LARGER THAN SB 767-54-0081 REV 1 DWG 624T0016 ST 1.
- [SDR DALA1204910139](https://openairdocs.org/sdr/DALA1204910139), Jan 30, 2012: SKIN. BULGED. RT WING 11 L/E SLAT WEDGE SKIN FOUND BULGED. HOT METAL BOND REPAIR PERFORMED ON AREA AS PER SRM 57-43-02 REPAIR 1 FIGURE 201 AND SRM 51-70-10 REPAIR 4 FIG 202.
- [SDR DALA1204860139](https://openairdocs.org/sdr/DALA1204860139), Jan 30, 2012: SKIN. CORRODED. CORROSION FOUND AFT CARGO INTERIOR FUSELAGE SKIN AT FS 1077 STRINGER 39L.
- [SDR DALA1204850139](https://openairdocs.org/sdr/DALA1204850139), Jan 30, 2012: SKIN. CORRODED. CORROSION FOUND AFT CARGO INTERIOR SKIN AREA FS STA 1077 FROM STRINGER 39L TO 39R. CP53-151-02I/CP53-152-02I (NRC 51757)
- [SDR DALA1204840139](https://openairdocs.org/sdr/DALA1204840139), Jan 30, 2012: FAIRING. CRACKED. DURING HMV 3 VISIT FOUND RT WING INBOARD MAIN FLAP OUTBOARD LEADING EGDE FAIRING CRACKED. COMPOSITE REPAIR CARRIED OUT AS PER B767-300 SRM 57-53-01 REPAIR 1 AND
- [SDR DALA1209970139](https://openairdocs.org/sdr/DALA1209970139), Jan 25, 2012: FRAME. CRACKED. MAIN DECK BS 903 RBL 89 FRAME CRACKED. REPAIRED PER ERA 499047-14AD REV ORIG SECT 1.
- [SDR DALA1209840139](https://openairdocs.org/sdr/DALA1209840139), Jan 25, 2012: FRAME. CRACKED. MAIN DECK BS 903 LBL 89 FRAME CRACKED. REPAIRED PER ERA 499046-14AD REV ORIG.

All 87: https://openairdocs.org/deregistered/N139DL-2017-05-10/reports.md

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB ENG14IA019](https://openairdocs.org/ntsb/ENG14IA019), Jul 11, 2014: Boeing 767 332 (N139DL), Los Angeles, CA, incident, minor damage. Probable cause: The combination of fuel leaking from the integrated drive generator (IDG) fuel/oil heat exchanger and the coincident arcing of the IDG power feeder cables that ignited the leaking fuel. Contributing…

## FAA accident and incident reports (1)

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 19930815041069I](https://openairdocs.org/incident/19930815041069I), Aug 15, 1993: Boeing 767332 (N139DL), Salt Lake City, UT. Passenger stated wifes neck was injured due to a hard landing in Salt Lake City. No hard landing was recorded.

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