# N125DL: 1988 Boeing 767-332, registration cancelled 2018-12-06

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: December 6, 2018
- 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: 24075
- Year built: 1988
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 31, 1988
- Certificate issued: March 26, 2014
- Last registry action: December 21, 2016
- Mode S code: A0669B
- 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/N125DL
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=125DL
- Page: https://openairdocs.org/deregistered/N125DL-2018-12-06

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 (63, newest 50)

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

- [SDR DALA2016021101130](https://openairdocs.org/sdr/DALA2016021101130), Feb 7, 2016: WIRE. CUT. EMERGENCY LIGHT ON MID OTBD LAV WALL ARE INOPERATIVE. MAINTENANCE REPAIRED CUT WIRE. SYSTEM OPERATION IS NORMAL.
- [SDR DALA2016021101129](https://openairdocs.org/sdr/DALA2016021101129), Feb 7, 2016: WIRE. CUT. EMERGENCY LIGHTS ON AFT RT LAV WALL ARE INOPERATIVE. MAINTENANCE FOUND WIRE CUT BELOW CARPET AND REPAIRED. SYSTEM OPERATION IS NORMAL.
- [SDR DALA2015022301796](https://openairdocs.org/sdr/DALA2015022301796), Feb 22, 2015: STRUCTURE. DAMAGED. 2 EACH HOLES DAMAGED ON INSIDE OF 1809 FWD CORD, COMMON TO THE SKIN ON LT SIDE BELOW LOWER DAMAGE.
- [SDR DALA2015022301795](https://openairdocs.org/sdr/DALA2015022301795), Feb 22, 2015: FAILSAFE. CRACKED. FUSELAGE, FRAME, STA 859.5, LT SIDE FAIL SAFE INNER CHORD/CRACK REPAIRED IAW ERA 532633-14.
- [SDR DALA2015022001604](https://openairdocs.org/sdr/DALA2015022001604), Feb 19, 2015: SUPPORT BEAM. DAMAGED. NR 1 FLAP SUPPORT BEAM 2 EA HOLES DAMAGED ON INBD SIDE, 2ND FROM AFT FASTENERS FWD OF LARGE BUSHING. C/W ERA 5326396-14.
- [SDR DALA2015022001602](https://openairdocs.org/sdr/DALA2015022001602), Feb 19, 2015: SUPPORT BEAM. DAMAGED. NR 1 FLAP SUPPORT BEAM: HOLE DAMAGED ON INBD SIDE OF BEAM, AFT UPPER FASTENER OF SIDE BRACE MOUNT FITTING HOLE. C/W ERA 532696-01.
- [SDR DALA2015021901603](https://openairdocs.org/sdr/DALA2015021901603), Feb 18, 2015: SUPPORT BEAM. CRACKED. NR 8 FLAP SUPPORT BEAM "C" FASTENER HOLE INDICATE CRACKED C/W ERA 532817-14.
- [SDR DALA2015021701295](https://openairdocs.org/sdr/DALA2015021701295), Feb 16, 2015: SUPPORT BEAM. CRACKED. NR 7 FLAP SUPPORT BEAM CRACKED. REPAIRED IAW ERA 532683-14.
- [SDR DALA2015021701293](https://openairdocs.org/sdr/DALA2015021701293), Feb 16, 2015: BEAM. CRACKED. BEAM CRACKED. REPAIRED IAW ERA 532683-14.
- [SDR DALA2015021301288](https://openairdocs.org/sdr/DALA2015021301288), Feb 12, 2015: SKIN. CRACKED. FUSELAGE SKIN IS CRACKED. EMANATING FROM UNDER AFT SCUFF PLATE OF L-1 DOOR AND PROGRESSING DOWN AND AFT. REPAIRED IAW SRM 53-10-01.
- [SDR DALA2015020200977](https://openairdocs.org/sdr/DALA2015020200977), Feb 1, 2015: SKIN. CRACKED. NR 1 PYLON, OTBD SIDE STRUT ASSY. SKIN AT UPPER AFT CORNER OF 442AL ACCESS DOOR CUTOUT CRACKED. C/W PRI 532568-14.
- [SDR DALA13049610125](https://openairdocs.org/sdr/DALA13049610125), Sep 29, 2013: LIGHT. INOPERATIVE. DURING SERVICE CHECK, FOUND COCKPIT EMERGENCY LIGHTS INOPERATIVE. MX REPLACED THE LIGHT ASSY AND BATTERIES. SYS OPERATION IS NORMAL.
- [SDR DALA13027370125](https://openairdocs.org/sdr/DALA13027370125), May 24, 2013: WIRE. DAMAGED. SEAT 25 A/B RED AISLE EMERGENCY LIGHTS ARE INOPERATIVE. MX REPAIRED WIRES. SYS OPERATION IS NORMAL.
- [SDR DALA13018630125](https://openairdocs.org/sdr/DALA13018630125), Apr 23, 2013: CONNECTOR. DAMAGED. EMERGENCY PATH LIGHTS AT ROW 41GF ARE INOPERATIVE. MX SECURED PATH LIGHT PLUG SYS OPERATION IS NORMAL.
- [SDR DALA1303660125](https://openairdocs.org/sdr/DALA1303660125), Feb 8, 2013: FITTING. DAMAGED. WHILE ACCOMPLISHING EA 01-499898-03 AD NEW LONGERON FITTING, WAS FOUND WITH SHORT EDGE MARGIN ON INBD FLANGE SIDE OF FITTING FASTENER HOLES. NEW REPLACEMENT LON
- [SDR DALA1303700125](https://openairdocs.org/sdr/DALA1303700125), Jan 11, 2013: WASHER. MIGRATED. WHILE ACCOMPLISHMENT OF EA 01-499890-03AD ME12 WORK CARD STEP 30, FOUND TENSION BOLT'S SELF AUGMENT WASHER RIDING ON RADIUS OF INTERNAL BATHTUB FITTING. INSTALL
- [SDR DALA1303850125](https://openairdocs.org/sdr/DALA1303850125), Jan 10, 2013: WEB. MISREPAIRED. NR 1 PYLON LT UPPER WEB FOUND EXISTING REPAIR IAW ERA 267062-14 NOT IAW SRM AND UPON NDT INSPECTION FOUND CRACK AT ANTI-ICE DUCT CUT-OUT ON WEB. NR 1 PYLON UPPE
- [SDR DALA1303380125](https://openairdocs.org/sdr/DALA1303380125), Jan 4, 2013: FLOORBEAM. CORRODED. BS 325, FLOORBEAM UPPER TEE AT RBL25 FOUND CORRODED. EXISTING T-CHORD REPAIR FROM RBL8 TO RBL93. AREA PREVIOUSLY REPAIR IAW SRM 53-00-51, FIG 201, REPAIR 1. EXI
- [SDR DALA1303820125](https://openairdocs.org/sdr/DALA1303820125), Jan 2, 2013: SKIN. MISREPAIRED. HMV2, DURING ACCOMPLISHMENT OF EA 01-487658, REV A MEO1. FOUND NR 1 PYLON NS 150-180 RT SIDE ACCESS DOOR CUT OUT EXISTING REPAIR NOT IAW THE SRM EXISTING REPAIR
- [SDR DALA1303680125](https://openairdocs.org/sdr/DALA1303680125), Dec 17, 2012: SUPPORT. CRACKED. FWD CARGO BETWEEN BS 654 AND 742 LT SIDEWALL UPPER SUPPORT. (STABILIZATION ANGLE) FOUND DAMAGED. FWD CARGO LT SIDE STABILIZATION ANGLE, PN, 143T5401-82 DAMAGED 
- [SDR DALA1303690125](https://openairdocs.org/sdr/DALA1303690125), Dec 16, 2012: SUPPORT. CRACKED. AFT CARGO BS 1105-1280 LT UPPER SUPPORT FOUND DAMAGED. AFT CARGO LT SIDE STABILIZATION ANGLE, DAMAGED PORTION CUT AND REMOVED AND REPAIRED IAW PRI ER/A 510625-1
- [SDR DALA1303870125](https://openairdocs.org/sdr/DALA1303870125), Dec 15, 2012: STRINGER. CORRODED. AFT CARGO BS 1313, STR 35L FOUND CORRODED. STRINGER REPAIRED IAW ER/A 510073-14, REV ORIG.
- [SDR DALA1303860125](https://openairdocs.org/sdr/DALA1303860125), Dec 15, 2012: SKIN. CORRODED. AFT CARGO BS 1200-1219 STRINGER 36R CAP JOINT SKIN CORROSION. REPAIRED IAW ER/A 509718-14, REV 0.
- [SDR DALA1303840125](https://openairdocs.org/sdr/DALA1303840125), Dec 13, 2012: FLOORBEAM. CORRODED. CABIN FLOORBEAM UPPER TEE AT BS 347, RBL 25 TO 31 FOUND CORRODED. FLOORBEAM SECTION REMOVED AND NEW FABRICATED REPAIR FLOORBEAM SECTION INSTALLED IAW ER/A 45840
- [SDR DALA1303390125](https://openairdocs.org/sdr/DALA1303390125), Dec 13, 2012: FLOORBEAM. CORRODED. CABIN FLOORBEAM UPPER TEE AT BS 347 BET RBL 25 TO RBL 31. FOUND CORROSION. AREA OF FLOORBEAM IS PREVIOUSLY SECTIONAL CUT-OUT AT RBL3102 AND LBL 3102 AND REPAIRE
- [SDR DALA1204970125](https://openairdocs.org/sdr/DALA1204970125), Jan 27, 2012: BATTERY PACK. DISCHARGED. EMERGENCY EXIT LIGHT AFT R3 ARE INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK. SYSTEM OPERATION IS NORMAL.
- [SDR DALA1256700125](https://openairdocs.org/sdr/DALA1256700125), Jul 26, 2011: FAILSAFE. CRACKED. A CRACK WAS FOUND DURING INSPECTION OF THE FAILSAFE FITTING IN THE RT AND LT MAIN LANDING GEAR WHEEL WELL. REPAIR IAW 479305-14.
- [SDR DALA1112880125](https://openairdocs.org/sdr/DALA1112880125), Feb 22, 2011: WIRE. BROKEN. EMERGENCY LIGHTS RED ON LAVATORY L2 ARE INOPERATIVE. MAINTENANCE FOUND WIRE BROKEN AT FLOOR LEVEL AND REPAIRED. SYSTEM OPERATION IS NORMAL.
- [SDR DALA1012540125](https://openairdocs.org/sdr/DALA1012540125), Jun 6, 2010: LIGHT. INOPERATIVE. PASSENGER SEAT 05C EMERGENCY LIGHTING FLOOR LIGHTS INOP. RESET SYS. OPS CK OK.
- [SDR DL76S100244](https://openairdocs.org/sdr/DL76S100244), Dec 14, 2009: FAILSAFE. CRACKED. INSPECTIONS SI 01-086393-12AD FOUND CORROSION IN THE RT AND LT FAILSAFE STRAPS WHICH REQUIRED TRIMMING IAW SB INSTRUCTIONS UPON REMOVAL OF THE CUT SECTIONS CORR
- [SDR DL76S100243](https://openairdocs.org/sdr/DL76S100243), Dec 14, 2009: FAILSAFE. CRACKED. AT PSV INSPECTIONS PRE SI 01-086393-12AD FOUND THE FAILSAFE CRACKED BOTH LT AND RT SIDES AND REQUIRED TRIMMING IAW SB 767-53-0100 REV 1. UPON REMOVAL OF THE CUT
- [SDR DL76S100242](https://openairdocs.org/sdr/DL76S100242), Dec 14, 2009: FITTING. CORRODED. WHILE ACCOMPLISHING INSPECTIONS OF THE FS 955 REAR SPAR BULKHEAD AND FAILSAFE STRAPS FOR CORROSION AND FATIGUE CRACKS IAW DAL SI01-086393-12AD CORROSION WAS FOU
- [SDR DL76S071641](https://openairdocs.org/sdr/DL76S071641), Dec 20, 2007: SKIN. DAMAGED. MINOR SKIN BLENDS AT FS 1219-1270 ALONG S-21R TO S-26R.
- [SDR DL76S071639](https://openairdocs.org/sdr/DL76S071639), Dec 18, 2007: SKIN. DAMAGED. MINOR SKIN BLENDS AT FS 1438 TO 1540, ALONG S-19L TO S-26L. REPAIRED PER ER/A 459229-14ADREVA.
- [SDR DL76S071631](https://openairdocs.org/sdr/DL76S071631), Dec 18, 2007: SKIN. DAMAGED. SKIN BLENDS FS 1444 AND S-39R, AND FS 1448 AND S-38L. REPAIRED PER ER/A 459236-14 REV A.
- [SDR DL76S071621](https://openairdocs.org/sdr/DL76S071621), Dec 3, 2007: SKIN. DAMAGED. FUSELAGE SKIN BLENDS, FS 1285, AND STR 36R. REPAIRED PER ER/A 459263-14 REV A.
- [SDR DL76S071600](https://openairdocs.org/sdr/DL76S071600), Nov 28, 2007: SKIN. DAMAGED. FUSELAGE SKIN BLENDS AT FS 1286.5 AND 32L DUE TO GROUND DAMAGE PER ER/A 459209-14 REV A.
- [SDR DL76S070818](https://openairdocs.org/sdr/DL76S070818), Jun 24, 2007: FITTING. CORRODED. RT NLG TRUNNION BORE CORRODED AND TOOLING DAMAGE FOUND ON WEB. BORE OVERSIZED AND AN OVERSIZED BUSHING INSTALLED. TOOLING DAMAGE OVERSIZED AND A BUSHING INSTALL
- [SDR DL76S070211](https://openairdocs.org/sdr/DL76S070211), Mar 16, 2007: STARTER. INOPERATIVE. STRONG SMELL NOTICED BOTH INSIDE AND OUTSIDE AIRCRAFT SMELL STARTED AFTER POWER TRANSFER TO APU AND PACKS WERE TURNED ON. GROUND PERSONNEL ALSO REPORTED STRONG 
- [SDR DL76S061058](https://openairdocs.org/sdr/DL76S061058), Dec 23, 2006: SKIN. LIGHTNING STRIKE. AT HMV, LIGHTNING STRIKES WERE FOUND JUST AFT OF FS 347 AND ABOVE S33R AND REPAIRED PER SRM 53-00-01, FIGURE 201, REPAIR 14. THIS REPAIR IS LOCATED JUST ABOVE A
- [SDR DL76S061057](https://openairdocs.org/sdr/DL76S061057), Dec 22, 2006: SKIN. NICKED. AT HMV, TWO NICKS WERE NOTED IN THE FUSELAGE SKIN AT FS 654 +4-+9 BETWEEN STR 35L AND 36L. THE RESULTING BLENDS EXCEEDED THE SRM ALLOWABLE DAMAGE REQUIREMENTS. 
- [SDR DL76S061056](https://openairdocs.org/sdr/DL76S061056), Dec 22, 2006: SKIN. NICKED. AT HMV, SIX NICKS TO THE FUSELAGE SKIN WERE FOUND AND BLENDED PER SRM. THE RESULTING BLENDS EXCEEDED SRM ALLOWABLE LIMITS. ERA 459158-14 ACCOMPLISHED REPAIR.
- [SDR DL76S061055](https://openairdocs.org/sdr/DL76S061055), Dec 22, 2006: SKIN PANEL. CORRODED. CORROSION WAS FOUND AT FS 1585 AND STR 38R-39R, 148T3251-4 SKIN PANEL. THE CORROSION WAS FOUND AT HMV AND WAS REPAIRED PER ERA 458836-14.
- [SDR DL76S061054](https://openairdocs.org/sdr/DL76S061054), Dec 22, 2006: FLOORBEAM. CRACKED. FIVE CRACKS WERE FOUND IN THE FS 347 FLOORBEAM UPPER CAP. THREE OF THE CRACKS EXTENDED INTO THE WEB. THE DAMAGE WAS FOUND AT HMV AND REPAIRED PER ERA 458406-14.
- [SDR DL76S061053](https://openairdocs.org/sdr/DL76S061053), Dec 22, 2006: SKIN. DAMAGED. DAMAGE WAS DISCOVERED IN THE FUSELAGE SKIN AT FS 654 +22 TO +66 AND STR 3R - 4R THAT RESULTED IN TWO SRM REPAIRS 4.875" APART. A DTA WAS ACCOMPLISHED AND THE IN
- [SDR DL76S061050](https://openairdocs.org/sdr/DL76S061050), Dec 21, 2006: FRAME. CRACKED. A CRACK WAS FOUND IN THE INNER CHORD OF THE STA 883.5 FRAME AT WL 190 ON THE RT SIDE. THE CRACK WAS TRIMMED OUT AND A REPAIR ANGLE WAS INSTALLED.
- [SDR DL76S061049](https://openairdocs.org/sdr/DL76S061049), Dec 21, 2006: FRAME. CRACKED. A CRACK WAS FOUND ON THE INNER CHORD OF THE STA 903.5 FRAME. THE CRACK WAS TRIMMED OUT AND A REPAIR ANGLE WAS INSTALLED.
- [SDR DL76S060990](https://openairdocs.org/sdr/DL76S060990), Nov 16, 2006: WEB. CRACKED. THE NR 1 STRUT MIDSPAR WEB WAS FOUND CRACKED. THE CRACKED WEB REINFORCED WITH A DOUBLER.
- [SDR DL76S040343](https://openairdocs.org/sdr/DL76S040343), Apr 15, 2004: SWITCH. OVERHEATED. ON DESCENT STARTED TO DETECTED A SLIGHT BURNING ODOR, ELECTRICAL ODOR. CREW DECLARED AN EMERGENCY. FOUND GPWS MODULE OVERHEATED. REMOVED MODULE AND FORWARDED TO
- [SDR DL76S010370](https://openairdocs.org/sdr/DL76S010370), Mar 2, 2001: SKIN. TOOL DAMAGE. DURING ACCOMPLISHMENT OF A SRM SKIN REPAIR, TOOLING DAMAGE OCCURRED TO STR 39L. THIS DOCUMENT PROVIDES A REPAIR OF BOTH THE STRINGER AND SKIN. THE DAMAGE IS LOC

All 63: https://openairdocs.org/deregistered/N125DL-2018-12-06/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 SEA96LA062](https://openairdocs.org/ntsb/SEA96LA062), Feb 20, 1996: Boeing 767-332 (N125DL), Portland, OR, no damage. Probable cause: the passenger's unsuccessful (improper) evacuation of the aircraft. The malfunctioning APU was a related factor in that it torched and produced smoke, due to a faulty fuel control unit and/or gearbox…

## 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.

- [Accident 19960220045989A](https://openairdocs.org/incident/19960220045989A), Feb 20, 1996: Boeing 767332 (N125DL), Portland, OR. (.4)While the Boeing 767 was taxiing for departure, the crew of another aircraft reported that there was smoke and flames coming from the Boeing 767 APU…
- [Incident 19900803047909I](https://openairdocs.org/incident/19900803047909I), Aug 3, 1990: Boeing 767332 (N125DL), Dallas-Ft Worth, TX. Advised of bomb threat on approach. Landed and evacuated. Had chute malfunctions. No bomb found.

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.