# N124DE: 1987 Boeing 767-332, registration cancelled 2018-05-16

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: May 16, 2018
- Status when cancelled: Registration expired
- 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: 23438
- Year built: 1987
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 4, 1987
- Certificate issued: April 10, 2015
- Last registry action: April 10, 2015
- Mode S code: A062DE
- 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/N124DE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=124DE
- Page: https://openairdocs.org/deregistered/N124DE-2018-05-16

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 (48)

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

- [SDR DALA2015011200438](https://openairdocs.org/sdr/DALA2015011200438), Jan 11, 2015: DOOR FRAME. CORRODED. LEFT FORWARD OVERWING EXIT DOOR FRAME IS CORRODED AT FORWARD LOWER CORNER. REMOVED AND FABRICATED NEW ANGLE.
- [SDR DALA2014091805094](https://openairdocs.org/sdr/DALA2014091805094), Sep 17, 2014: SKIN. DAMAGED. FUSELAGE SKIN DAMAGED. REPAIRED IAW ERA 528965-14.
- [SDR DALA2014091805093](https://openairdocs.org/sdr/DALA2014091805093), Sep 17, 2014: SKIN. DAMAGED. FUSELAGE SKIN DAMAGED. REPAIRED IAW ERA 528966-14.
- [SDR DALA2014091805092](https://openairdocs.org/sdr/DALA2014091805092), Sep 17, 2014: SKIN. DAMAGED. FUSELAGE SKIN GROUND DAMAGED. REPAIRED IAW ERA 528964-14.
- [SDR DALA2014091705090](https://openairdocs.org/sdr/DALA2014091705090), Sep 16, 2014: STRINGER. CRACKED. RT SIDE FUSELAGE STRINGER 30R CRACKED BS 1530-1540. REMOVED STRINGER IAW SRM 53-00-01,. PERFORMED HFEC FOR DAMAGE CONTAINMENT, NO FINDINGS.
- [SDR DALA13028270124](https://openairdocs.org/sdr/DALA13028270124), Jun 7, 2013: FLOORBEAM. CRACKED. CABIN BS 347 FLOORBEAM UPPER TEE FOUND CRACKED AT RBL 2.0 AND RBL 8.0 & LBL 9.0. REPAIRED IAW 514023-14 (LP 0917476).
- [SDR DALA13028260124](https://openairdocs.org/sdr/DALA13028260124), Jun 7, 2013: FAILSAFE. CRACKED. CRACK ON RT BULKHEAD FAIL SAFE STRAP AT BS 955. REPAIRED IAW PRI 514007-14AD, REV 0.
- [SDR DALA13023700124](https://openairdocs.org/sdr/DALA13023700124), May 21, 2013: STRINGER. CORRODED. FWD CARGO -BS 412-434, STRINGER 38R CORRODED. REPAIR CARRIED OUT IAW SRM 53-00-03, FIG 201, REPAIR 2, REV 92.00.
- [SDR DALA13023690124](https://openairdocs.org/sdr/DALA13023690124), May 21, 2013: STRINGER. CORRODED. FWD CARGO BS 412-434, STRINGER 36R CORRODED. REPAIR CARRIED OUT IAW SRM 53-00-03, FIG 201, REPAIR 2, REV 92.00.
- [SDR DALA13023680124](https://openairdocs.org/sdr/DALA13023680124), May 21, 2013: STRINGER. CORRODED. FWD CARGO BS 412-434, STRINGER 34R CORRODED. REPAIR CARRIED OUT IAW SRM 53-00-03, FIG 201, REPAIR 2, REV 92.00.
- [SDR DALA13023670124](https://openairdocs.org/sdr/DALA13023670124), May 21, 2013: STRINGER. CORRODED. FWD CARGO BS 412-434 STRINGER 27R CORRODED. REPAIR CARRIED OUT IAW SRM 53-00-03 FIG 201, REPAIR 2, REV 92.00.
- [SDR DALA13023660124](https://openairdocs.org/sdr/DALA13023660124), May 21, 2013: STRINGER. CORRODED. FWD CARGO BS 412-434 STRINGER 39R CORRODED. REPAIR CARRIED OUT IAW SRM 53-00-03, FIG 201, REPAIR 2, REV 92.00.
- [SDR DALA13023650124](https://openairdocs.org/sdr/DALA13023650124), May 21, 2013: STRINGER. CORRODED. FWD CARGO BS 412-434, STRINGER 35R CORRODED, REPAIR CARRIED OUT IAW SRM 53-00-03 FIG 201, REPAIR 2, REV 92.00.
- [SDR DALA13023490124](https://openairdocs.org/sdr/DALA13023490124), May 20, 2013: FRAME. CRACKED. DURING HFEC INSPECTION ON BS 1809, BULKHEAD LT FORWARD OUTER FRAME S6-7L FOUND CRACKED. REPAIRED FRAME.
- [SDR DALA13028310124](https://openairdocs.org/sdr/DALA13028310124), May 8, 2013: STRUCTURE. CORRODED. WING CENTER SECTION UPPER SURFACE BETWEEN BS 857 AND 859, LBL 88. REWORKED IAW PRI 514634-14, REV 0, REV 1, REV 2, REV 3 AND REV 4.
- [SDR DALA13028300124](https://openairdocs.org/sdr/DALA13028300124), May 8, 2013: STRUCTURE. CORRODED. WING CENTER SECTION UPPER SURFACE AT BS 927, LBL 90. REPAIR CARRIED OUT IAW- PRI 514016-14, REV 0, REV 1, REV 2, REV 3, REV 4, REV 5 AND REV 6. AND COMPLIED WIT
- [SDR DALA2015082707893](https://openairdocs.org/sdr/DALA2015082707893), Aug 14, 2012: SKIN. CRACKED. CRACK AT BS 687, STRINGER 36R AT CARRY THOUGH HOLE, RT AIRFONE BLANKING PLATE, 1/8TH INCH CRACK.
- [SDR DALA1245820124](https://openairdocs.org/sdr/DALA1245820124), Aug 14, 2012: SKIN. CRACKED. SKIN CRACKED ONE EIGTH INCH CRACK RT AIRFONE BLANKING PLATE INST STA 687 STR 36R AT CARRY THRU HOLE LOC MARKED REF ERA 389647-14 REV A. REPAIRED PER SRM B767-30
- [SDR DALA1102330124](https://openairdocs.org/sdr/DALA1102330124), Jan 11, 2011: SKIN. DELAMINATED. RT WING OTBD FLAP LWR SURFACE MID INSPAR PANEL SKIN DELAMINATED AT APPROX 66"FROM INBD AND 24" FRM BOTTOM; CA: REPAIR DOUBLER AND FILLER FABRICATED IAW SRM 57-5
- [SDR DALA1102320124](https://openairdocs.org/sdr/DALA1102320124), Jan 11, 2011: WEDGE. DELAMINATED. LT WING L/E NR2 SLAT WEDGE UPPER SURFACE FOUND DELAMINATED; CA: LT WING L/E NR2 SLAT WEDGE UPPER SURFACE, REPAIR FILLER AND DOUBLER FABRICATED IAW 51-70-10 OTIS
- [SDR DALA1102060124](https://openairdocs.org/sdr/DALA1102060124), Jan 10, 2011: SKIN. DENTED. LT V-STAB EXTERIOR AROUND FS STA 270.784 FOUND DENT DURING HMV INSP AT SIN; C/A-DENTED SURFACE TRIMMED OFF. REPAIR PART FABRICATED IAW SRM 51-70-01, FIG 201, OT
- [SDR DL76S071392](https://openairdocs.org/sdr/DL76S071392), Oct 27, 2007: INDICATOR. MALFUNCTIONED. AFTER TO, F/O AIRSPEED INDICATOR BECAME UNREADABLE AND ROSE STEADILY TO 400 KTS. NO FLAGS OR OTHER INDICATIONS, OTHER THAN OVERSPEED WARNING. ACTUAL AIRSPEED ON
- [SDR DL76S071386](https://openairdocs.org/sdr/DL76S071386), Oct 24, 2007: TRUNNION. CORRODED. LT AND RT NOSE LANDING GEAR TRUNNION FITTINGS CORRODED IN THE INNER DIAMETER. CORROSION CLEANED UP AND OVERSIZED BUSHINGS WERE INSTALLED.
- [SDR DL76S071046](https://openairdocs.org/sdr/DL76S071046), Aug 8, 2007: MEC. MALFUNCTIONED. RTO DUE TO RT ENGINE WOULD NOT MAKE TAKEOFF POWER. REPLACED RT ENGINE MEC. AFTER RUNUP ENGINE MAKES TAKEOFF POWER.
- [SDR DL76S070504](https://openairdocs.org/sdr/DL76S070504), May 9, 2007: CHARGER. MISSING. EMERGENCY LIGHT EXIT SIGN INOP AT L1 AND R1 DOOR. INSTALLED NEW BATTERY AND CHARGER TRA, FOUND TRAY AND BATTERY PACK ASSY MISSING AT L1 POSITION.
- [SDR DL76S060797](https://openairdocs.org/sdr/DL76S060797), Sep 28, 2006: FLOORBEAM. CORRODED. CABIN FLOORBEAM UPPER CHORD STA 287 CORRODED AT RBL 51 TO RBL 62 AND ALSO EXISTING SPLICE PLATE CORRODED AT RBL 10 TO RBL 15. REPAIRED PER SRM 53-00-51D FIGURE 
- [SDR DL76S060796](https://openairdocs.org/sdr/DL76S060796), Sep 28, 2006: FLOORBEAM. CRACKED. CABIN FLOORBEAM AT STA 325 LBL 32 UPPER STRUCTURE BENT AND CRACKED IN RADIUS AS MARKED. REPAIRED PER SRM 53-00-51D FIGURE 201.
- [SDR DL76S060793](https://openairdocs.org/sdr/DL76S060793), Sep 28, 2006: FITTING. FATIGUED. DURING REWORK OF THE FORWARD UPPER SPAR FITTING PER SIP EO, CRACKING INDICATIONS WERE FOUND AT AFT OUTBOARD FASTENER LOCATIONS COMMON TO MIDSTRUT BULKHEAD FITTI
- [SDR DL76S060792](https://openairdocs.org/sdr/DL76S060792), Sep 28, 2006: FITTING. FATIGUED. CRACK INDICATIONS WERE FOUND AT THE FORWARD OUTBOARD BOLT HOLE LOCATION OF THE AFT PITCH LOAD FITTING, NR 1 PYLON. CRACK IS IN LOWER WING SKIN ALSO, AND REQUIRE
- [SDR DL76S060791](https://openairdocs.org/sdr/DL76S060791), Sep 28, 2006: FRAME. CRACKED. FUSELAGE STATION 903.5 FRAME INNER CHORD FOUND CRACKED. ON BOTH LT AND RT AT TRANSITION BETWEEN CHORD FLANGES. AREA TRIMMED AND REPAIR INSTALLED.
- [SDR DL76S060790](https://openairdocs.org/sdr/DL76S060790), Sep 28, 2006: RIB. CORRODED. RT WING RIB NR 8, LOWER OUTBOARD HOLE WAS FOUND WITH CORROSION PITTING. DAMAGE WAS REMOVED BY OVERSIZED HOLE, BUSHING INSTALLATION.
- [SDR DL76S060695](https://openairdocs.org/sdr/DL76S060695), Aug 23, 2006: LINKAGE. MISINSTALLED. DURING INSPECTION OF THE LT OFF WING ESCAPE SLIDE PER JIC 6075 THE TECHNICIAN FOUND THAT THE INTEGRATOR LOCK HANDLE HAD TO BE FORCED INTO THE SAFETY POSITION. U
- [SDR DL76S060467](https://openairdocs.org/sdr/DL76S060467), May 23, 2006: SKIN. LIGHTNING STRIKE. FUSELAGE SKIN WAS STRUCK BY LIGHTNING BETWEEN BS 257 AND 277 BELOW S-11L. THE DAMAGED SKIN WAS REMOVED AND A DOUBLER WAS INSTALLED.
- [SDR DL76S060140](https://openairdocs.org/sdr/DL76S060140), Feb 15, 2006: BOLT. MISSING. NR 2 SLAT I/B ACTUATOR COVER DAMAGED. REINSTALLED MISSING HARDWARE, RAN SLATS, ALL OK.
- [SDR DL76S030503](https://openairdocs.org/sdr/DL76S030503), Jun 2, 2003: SKIN. CRACKED. MECHANIC FOUND 2 INCH CRACK IN FUSELAGE SKIN RT SIDE STA 1654.5 STR 3R. ALSO, FOUND STRINGER 3R AND 3L CRACKED AT SAME LOCATION. REPAIRED CRACK.
- [SDR DL76S020842](https://openairdocs.org/sdr/DL76S020842), Jul 18, 2002: SKIN. DENTED. FUSELAGE / SKIN / FS 287-303 / STRG. 37R : DENT REPAIR THE FUSELAGE SKIN WAS DENTED AT THE STRINGER 37R SKIN LAP JOINT BETWEEN FS 287 & 303. THE LAPJOINT WAS CU
- [SDR DL76S020565](https://openairdocs.org/sdr/DL76S020565), May 17, 2002: POWER SUPPLY. DISCHARGED. OVERHEAD AISLE LIGHTS FIRST CLASS LEFT SIDE INOP. REPLACED BATTERY PACK AND RACK.
- [SDR DL76S020406](https://openairdocs.org/sdr/DL76S020406), Apr 4, 2002: SKIN. CRACKED. WHILE ACCOMPLISHING THE FS 1809.5 BULKHEAD OUTER CHORD MOD PER BAC S/B 767-53-0078 AND AD 2001-09-13, A CRACK WAS FOUND IN THE SKIN COMMON TO A FASTENER HOLE FO
- [SDR DL76S011920](https://openairdocs.org/sdr/DL76S011920), Dec 10, 2001: BATTERY PACK. DISCHARGED. LEFT FORWARD OVERHEAD EMERGENCY LIGHTS INOP IN CABIN. REMOVED AND REPLACED BATTERY PACK FOR LEFT FORWARD OVERHEAD EMERGENCY LIGHTS, CHECKS GOOD.
- [SDR DL76S011516](https://openairdocs.org/sdr/DL76S011516), Sep 10, 2001: ENGINE. UNSERVICEABLE. ON CLIMB OUT RIGHT ENGINE STALLED. ACCOMPLISHED POM "ENGINE SURGE OR STALL" PROCEDURE. THROTTLE REDUCED TO IDLE. ENGINE SHUT DOWN AFTER LANDING. EGT MAX 895 FOR
- [SDR DL76S010388](https://openairdocs.org/sdr/DL76S010388), Mar 10, 2001: PROBE. MALFUNCTIONED. RTB FOR INSP. DUE TO SMOKE COMING FROM LT NOSE AREA OVER RADOME. J/C VISUAL INSPECTION OF NLG AREA, FWD AND MAIN E/E COMPARTMENTS. ALSO VISUALLY INSPECTED OF LT
- [SDR DL76S010170](https://openairdocs.org/sdr/DL76S010170), Jan 26, 2001: FRAME. CORRODED. CORROSION WAS FOUND ON THE FWD FRAME AT THE CUTOUT FOR THE FWD LT PASSENGER DOOR. THE CORROSION WAS LOCATED ON THE AFT SURFACE OF THE FRAME WEB SURROUNDING THE 
- [SDR DL76S010171](https://openairdocs.org/sdr/DL76S010171), Jan 25, 2001: SKIN. DENTED. FUSELAGE SKIN WAS DENTED DUE TO NOSE TIRE BLOWOUT. THE DENTS WERE APPROVED FOR INTERIM SERVICE PER ER/A 269377-14. THE DAMAGE WAS PERMANENTLY REPAIRED PER ER/A 
- [SDR DL76S992442](https://openairdocs.org/sdr/DL76S992442), Nov 4, 1999: LIGHT. INOP. FOUR AISLE EMERGENCY LIGHTS INOP AFT RIGHT SIDE. REPLACED POWER SUPPLY, SYSTEM CHECKS NORMAL.
- [SDR DL76S990692](https://openairdocs.org/sdr/DL76S990692), Mar 29, 1999: MASK. FELL. THE O2 MASK ZONE C HANGING DOWN. REINSTALLED MASK AND SECURED PANEL.
- [SDR DL76S981698](https://openairdocs.org/sdr/DL76S981698), Aug 12, 1998: SKIN. CORRODED. CORROSION WAS FOUND ON THE WING CENTER SECTION. DAMAGE LOCATED ON AFT SKIN PANEL, FWD EDGE ON THE LT OUTBD END. REPAIRED PER ERA 331990-14.
- [SDR DL76S981265](https://openairdocs.org/sdr/DL76S981265), Jun 15, 1998: POWER SUPPLY. INOPERATIVE. ON L/O, FOUND ZONE EMERGENCY TRACK LIGHTS INOP BOTH AISLES. REPLACED PWR SUPPLY M9010. LIGHTS OPS NML.
- [SDR DL76S971347](https://openairdocs.org/sdr/DL76S971347), Jul 1, 1997: SKIN. DELAMINATED. THE NR 9 LE SLAT TRAILING EDGE WEDGE WAS FOUND TO HAVE A 3.5 DIAMETER SECTION OF THE UPPER SKIN DELAMINATED. THE DAMAGE IS LOCATED IN THE CENTER OF THE SLAT WED

## 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 19881126067229I](https://openairdocs.org/incident/19881126067229I), Nov 26, 1988: Boeing 767332 (N124DE), Memphis, TN. Passenger believed to have cardiac arrest. Diverted to Memphis International. Passenger taken to a hospital.

---
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.