# N122DL: 1987 Boeing 767-332, registration cancelled 2009-12-03 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: December 3, 2009 - Exported to: Nigeria - Status when cancelled: Triennial form not returned - 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: 23436 - Year built: 1987 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: March 3, 1987 - Certificate issued: June 25, 1987 - Last registry action: July 21, 2009 - Mode S code: A05B76 - Owner when cancelled: [Wilmington Trust Co Owner Trustee](https://openairdocs.org/faa-owner/WILMINGTON%20TRUST%20CO%20OWNER%20TRUSTEE) - Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington) - Owner type: Corporation - Owner's area on the map: 39.7357° N, 75.5321° W: Placed by OpenAirDocs: center of Wilmington, DE, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N122DL - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=122DL - Page: https://openairdocs.org/deregistered/N122DL-2009-12-03 From the FAA registry file of October 31, 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 (28) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DL76S071307](https://openairdocs.org/sdr/DL76S071307), Oct 7, 2007: WARNING LIGHT. ILLUMINATED. DURING T/O ROLL, RT ENG FUEL FILTER ADVISORY STATUS MSG INDICATED. OCCURRED APPROX 100-110 KNTS T/S PER FIM. REMOVED FUEL FILTER ELEMENT INSP FOR DEBRIS, NONE F - [SDR DL76S060844](https://openairdocs.org/sdr/DL76S060844), Oct 13, 2006: SKIN. CORRODED. CORROSION WAS FOUND IN THE SKIN AROUND THE RHS DME ANTENNA CABLE. CORROSION WAS BLENDED AND A BOEING APPROVED REPAIR INSTALLED PER ERA 456420-14. - [SDR DL76S060843](https://openairdocs.org/sdr/DL76S060843), Oct 13, 2006: FLOORBEAM. CRACKED. UPPER CHORD OF THE STA 999 AT LBL 33 FLOORBEAM WAS FOUND CRACKED IN THE VERTICAL FLANGE FROM THE AFT SLOTTED CUTOUT TO THE END OF THE CHORD. THE CRACK WAS REMOV - [SDR DL76S060846](https://openairdocs.org/sdr/DL76S060846), Oct 10, 2006: SKIN. GOUGED. GOUGES WERE FOUND IN THE FUSELAGE SKIN PANEL IN THE VICINITY OF AN EXISTING REPAIR. EXISTING REPAIR REMOVED AND ONE LARGE EXTERNAL REPAIR DOUBLER INSTALLED PER - [SDR DL76S060633](https://openairdocs.org/sdr/DL76S060633), Aug 6, 2006: COFFEEMAKER. ODOR. FLT ATTENDANT SMELLED BURNT PLASTIC IN AFT GALLEY FROM A CEILING PANEL IN PROX OF COFFEEMAKERS. NO HEAT FELT ON PANEL, F/A TURNED OFF ALL COFFEEMAKERS AND PULLE - [SDR DL76S060603](https://openairdocs.org/sdr/DL76S060603), Jul 21, 2006: FITTING. CRACKED. THE NR 2 PYLON OUTBOARD PITCH LOAD FITTING WAS FOUND CRACKED. THE CRACKED HOLE WAS OVERSIZED TO REMOVE THE DAMAGE AND AN OVERSIZED FASTENER WAS INSTALLED REF AD - [SDR DL76S060601](https://openairdocs.org/sdr/DL76S060601), Jul 18, 2006: FITTING. DAMAGED. DURING MODIFICATION OF THE PYLON MIDSPAR FITTING, TWO HOLES WERE DAMAGED DURING FASTENER REMOVAL. THE HOLES WERE OVERSIZED TO REMOVE THE DAMAGE AND OVERSIZED FA - [SDR DL76S060586](https://openairdocs.org/sdr/DL76S060586), Jul 13, 2006: FITTING. DAMAGED. DURING ACCOMPLISHMENT OF S/B 767-54-0081, THE SIDE LINK FITTING WAS SPOTFACED IN THE WRONG LOCATION. A FILLER WAS INSTALLED IN THE SPOTFACED AREA. - [SDR DL76S060585](https://openairdocs.org/sdr/DL76S060585), Jul 13, 2006: FRAME. CRACKED. THE LT BS 903.5 FRAME HAS A CRACK IN THE LOWER END BETWEEN CHORD FLANGES. THE CRACKED AREA WAS REMOVED AND A REPAIR ANGLE WAS INSTALLED. - [SDR DL76S060584](https://openairdocs.org/sdr/DL76S060584), Jul 13, 2006: FITTING. CRACKED. THE FORWARD UPPER SPAR FITTINGS ARE CRACKED AT A FASTENER HOLE. THE HOLES WERE OVERSIZED TO REMOVE THE CRACK AND BUSHINGS WERE INSTALLED. - [SDR DL76S050543](https://openairdocs.org/sdr/DL76S050543), Sep 13, 2005: ENGINE. LEAKING. ODOR DETECTED AND SEVERAL SMOKE DETECTORS WENT OFF. ODOR DISSIPATED WITH UTILITY BUSSES OFF, BUT RETURNED WHEN POWER LEVERS ADVANCED. OIL LEAK NR 1 ENGINE. REPL - [SDR DL76S040472](https://openairdocs.org/sdr/DL76S040472), May 27, 2004: ECU. MALFUNCTIONED. MCO - APU STARTER CONTINUOUSLY POWERED CAUSING OVERHEATING AND SMELL IN APU AIR. REPLACED ECU AND K117 CONTACTOR. - [SDR DL76S040301](https://openairdocs.org/sdr/DL76S040301), Apr 3, 2004: ODOR. DETECTED. ELECTRICAL SMOKE ODOR FROM VIDEO EQUIP RACK, WHEN SHUT OFF SMOKE DISSIPATED. RAN VCP 1 AND VCP 2 FOR 15 MINUTES EACH, NO SMOKE ODOR NOTICED. REMOVED VCP 1 AND V - [SDR DL76S030756](https://openairdocs.org/sdr/DL76S030756), Aug 13, 2003: SUPPORT BEAM. CORRODED. CORROSION WAS FOUND IN THE HOLE BORES OF 4 ATTACH FASTENERS ON THE 9-10 BEAM ASSEMBLY FOR THE OUTBOARD SUPPORT OF THE INBD FLAP ATTACH ASSEMBLY. THE HOLES WERE - [SDR DL76S030547](https://openairdocs.org/sdr/DL76S030547), Jun 13, 2003: LENS. BROKEN. ONE WHITE EMERGENCY LIGHT IS BROKEN ON SEAT 2B. REPLACED LENS AND SHROUD. - [SDR DL76S020783](https://openairdocs.org/sdr/DL76S020783), Jul 7, 2002: FAN. DAMAGED. ON APPROACH, BURNING SMELL IN COCKPIT ALL THE WAY BACK TO ROW 4. SMELL DISSIPATED WITHIN 2 MINUTES. ISOLATED PROBLEM TO LEFT RECIRC FAN. FOUND FAN DAMAGED BY DE - [SDR DL76S011789](https://openairdocs.org/sdr/DL76S011789), Nov 12, 2001: ENGINE. DAMAGED. CLIMBING THRU 19000FT, LOUD BANG ON THE RIGHT SIDE. TEMP ONNO 2 ENG WENT TO 959 DEG. PULLED ENG TO IDLE. SUBSEQUENT ENG OIL EICAS MSG. SHUT DOWN ENG. ON ARRIVAL - [SDR DL76S010414](https://openairdocs.org/sdr/DL76S010414), Mar 12, 2001: SKIN. CRACKED. THE FUSELAGE SKIN WAS FOUND WITH A 9.5 INCH CRACK ADJACENT TO THE LOWER AFT VHF ANTENNA AT FS 1197+95 BETWEEN STRINGERS 39L & 39R. THE CRACK WAS REMOVED WITH A - [SDR DL76S000210](https://openairdocs.org/sdr/DL76S000210), Jan 25, 2000: SKIN. PUNCTURED. FUSELAGE SKIN PUNCTURE DISCOVERED AT STA 1443 (GROUND DAMAGE DURING HMV) AND STR 37R. ADDITIONALLY THE STRINGER WAS DENTED. ER/A 334052-14 REV A. - [SDR DL76S990604](https://openairdocs.org/sdr/DL76S990604), Mar 21, 1999: LIGHT. INOPERATIVE. ON L/O, FOUND SEAT 41F EMERGENCY ESCAPE PATH LIGHT INOP. REPLACED LIGHT ASSY. - [SDR DL76S982582](https://openairdocs.org/sdr/DL76S982582), Dec 17, 1998: HOSE. RUPTURED. CENTER HYD QUANITY LIGHT CAME ON. QTY INDICATED .47 ON DOWN WIND WHEN LIGHT CAME ON. FOUND HYD LINE PN AS115-04K0146 RUPTURED ON STAB TRIM CONTROL MODULE. IPC L - [SDR DL76S982184](https://openairdocs.org/sdr/DL76S982184), Oct 20, 1998: SKIN. TORN. FUSELAGE SKIN, FS 1439 STRG 36L-39L : GROUND DAMAGE REPAIR. THE FUSELAGE SKIN AT FS 1439 BETWEEN STRINGERS 36L AND 39L WAS DENTED OR TORN DUE TO CONTACT WITH GR - [SDR DL76S962187](https://openairdocs.org/sdr/DL76S962187), Sep 27, 1996: HOSE. LEAKING. AFTER T/O UPON GEAR RETRACTION, GOT GEAR DOOR MSG AND GEAR DISAGREE MSG ON EICAS. LT MAIN GEAR GREEN LIGHT REMAINED ILLUMINATED. FOUND UP PRESSURE LINE TO LT GE - [SDR DL76S962146](https://openairdocs.org/sdr/DL76S962146), Sep 20, 1996: BULB. FAILED. ON FAA INSP FOUND EMERGENCY FLOOR TRACK WHITE LIGHT OUT, SEAT 45FG. - [SDR DL76S953488](https://openairdocs.org/sdr/DL76S953488), Aug 24, 1995: EEL BULB. FAILED. FOUND RT OVERWING EMERGENCY ESCAPE LIGHT INOP. RELAMPED, OPERATION NORMAL. - [SDR DL76S951575](https://openairdocs.org/sdr/DL76S951575), Apr 7, 1995: TE WEDGE. DELAMINATION. DURING LTR CHECK, THE NR 1 L/E SLAT TRAILING EDGE WEDGE WAS FOUND TO HAVE THE UPPER SKIN DELAMINATED. THE DELAMINATED AREA IS APPROXIMATELY 5 INCHES IN DIAMETER - [SDR DL76S951429](https://openairdocs.org/sdr/DL76S951429), Apr 6, 1995: SKIN. PUNCTURE. FOUND DURING LETTER CHECK INSP, DENT AND PUNCTURE ON UNDERSIDE OF OUTBOARD AFT FLAP BEHIND NR 11 SPOILER R5T WING. REPAIRED PER SRM 57-53-01, PAINTED AREA. - [SDR DL76S951428](https://openairdocs.org/sdr/DL76S951428), Apr 6, 1995: SKIN. DENTED. FOUND DURING LETTER CHECK INSP, DENT ON UNDERSIDE OF OUTBOARD FLAP OUTBOARD END RT WING. REMOVED DAMAGED AREA AND STARTED REPAIR PER SRM 57-53-01, OK TO PAINT F ## FAA accident and incident reports (3) 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 19990411019219I](https://openairdocs.org/incident/19990411019219I), Apr 11, 1999: Boeing 7673P6 (N122DL), Albuquerque, NM. On April 11, 1999, at approximately 2255 MDT, delta flight 241, a B-767, landed at Albuquerque, NM, (abq), due to an electrical problem. The aircraft's left… - [Incident 19950616016429I](https://openairdocs.org/incident/19950616016429I), Jun 16, 1995: Boeing 767300 (N122DL), Covington/Cinci, KY. Narrative: while descending through 20,000 feet, for a landing at greater Cincinnati airport. The flight encountered turbulence. The cabin crew was conducting… - [Incident 19880210010519I](https://openairdocs.org/incident/19880210010519I), Feb 10, 1988: Boeing 767332 (N122DL), Omaha, NE. Passenger had a medical problem. Diverted to Omaha. Medical people met aircraft. Flight continued to destination. ## Other aircraft with N122DL - [Registered now](https://openairdocs.org/aircraft/N122DL): Czech Sport Aircraft A S SPORTCRUISER, S/N C0567, built 2016 --- 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.