# N120DL: 1986 Boeing 767-332, registration cancelled 2018-02-28

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 28, 2018
- Status when cancelled: Registration expired, pending cancellation
- 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: 23279
- Year built: 1986
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 4, 1986
- Certificate issued: September 24, 2013
- Last registry action: September 24, 2013
- Mode S code: A05408
- Owner when cancelled: [Executive Jet Group 1 LLC](https://openairdocs.org/faa-owner/EXECUTIVE%20JET%20GROUP%201%20LLC)
- Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington)
- Owner type: Corporation
- Owner's area on the map: 39.7236° N, 75.5412° W: Placed by OpenAirDocs at the center of ZIP code 19801, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N120DL
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=120DL
- Page: https://openairdocs.org/deregistered/N120DL-2018-02-28

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 (49)

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

- [SDR DALAFAR145SDR103](https://openairdocs.org/sdr/DALAFAR145SDR103), Nov 5, 2010: FLOORBEAM. CORRODED. FOUND CORROSION ON FLOORBEAM UPPER CAP AT FS 325 RBL 30 TO RBL 51. CONDITION FOUND DURING FLOOR COVERING REPLACEMENT. REF DAL NON-ROUTINE CARD 336. REPAIRED PER
- [SDR RYNA2010001020035](https://openairdocs.org/sdr/RYNA2010001020035), Oct 7, 2010: OIL SYSTEM. LOW. THE RIGHT ENGINE IDG WAS PLACED ON MEL, DURING THE FLIGHT HAD TO RUN THE APU DUE TO MEL. DURING THE FLIGHT THE APU LOW OIL QTY MESSAGE CAME ON. THE CREW HAD TO 
- [SDR RYNA2010008020026](https://openairdocs.org/sdr/RYNA2010008020026), Aug 20, 2010: FMC. MALFUNCTIONED. ON CLIMBOUT RECEIVED EICAS MESSAGE "L" FAILED. SELECTED ALTERNATE OF FMC INST SIYRCE SEKECTIR & R. AUTOPILOT CMO. PERFORMED FIM 34-61-00 F16180A 1-3423. PERFORM
- [SDR RYNA2010007020023](https://openairdocs.org/sdr/RYNA2010007020023), Jul 22, 2010: INDICATION SYS. MALFUNCTIONED. WHILE PERFORMING CONTROL WHEEL SURFACE CHECKS, LEFT O/B AILERON SHOWED NO MOVEMENT ON LOWER EICAS SCREEN. SWAPPED RT & LT STAB TRIM/AILERON LOCKOUT MODULES FOR 
- [SDR RYNA200912080025](https://openairdocs.org/sdr/RYNA200912080025), Dec 6, 2009: FMC. FAILED. DURING CRUISE EICAS STATUS MESSAGE R FMC FAIL APPEARED WITH CORRESPONDING LOSS OF FIRST OFFICERS, FMC DISPLAY ALONG WITH THE FIRST OFFICERS LOSS OF MAP AND NAVI
- [SDR RYNA200912070024](https://openairdocs.org/sdr/RYNA200912070024), Dec 5, 2009: BATTERY PACK. DISCHARGED. ON 12/05/2009, ON AIRCRAFT 120DL, INSPECTION OF THE CABIN REVEALED THE EMERGENCY LIGHTS AT SEAT ROWS 17-28 WILL NOT STAY ILLUMINATED FOR VERY LONG DURING THE RE
- [SDR RYNA200908170015](https://openairdocs.org/sdr/RYNA200908170015), Aug 15, 2009: SELECTOR VALVE. LEAKING. DURING CRUISE HYDRAULIC FLUID APPEARED TO BE MIGRATING FROM THE RT SYSTEM TO THE CENTER DIVERTED TO SUITABLE AIRPORT READINGS UPON LANDING INDICATED .45 CENTER 
- [SDR RYNA200908110013](https://openairdocs.org/sdr/RYNA200908110013), Aug 4, 2009: DOOR FRAME. CRACKED. WHILE PERFORMING MAINTENANCE ON AIRCRAFT 120DL DURING THE INSPECTION PROCESS A DENT AND CRACK ON THE C2 CARGO DOOR OPENING FRAME WEB AT FS 1270 WL 162.5. THE CR
- [SDR RYNA20090811014](https://openairdocs.org/sdr/RYNA20090811014), Jul 31, 2009: STRUCTURE. CORRODED. WHILE PERFORMING MAINTENANCE ON AIRCRAFT 120DL DURING THE INSPECTION PROCESS CORROSION DAMAGE WAS DISCOVERED BETWEEN FS 632 TO FS 654 ALONG STRINGERS 35L TO 36L
- [SDR RYNA200908040010](https://openairdocs.org/sdr/RYNA200908040010), Jul 24, 2009: BATTERY PACK. DISCHARGED. DURING ACCOMPLISHMENT OF TASK-CARD 767-33-033-01 EMERGENCY LIGHT POWER SUPPLIES ON C-CHECK 1C/2C/S1C/S2C ALL BATTERY PACKS FAILED THE CAPACITY CHECK AND RT EXTE
- [SDR RYNA200908040011](https://openairdocs.org/sdr/RYNA200908040011), Jul 16, 2009: CABLE ASSY. OUT OF RIG. DURING INSPECTION OF EMERGENCY ESCAPE SYSTEM ON C-CHECK 1C/2C/S1C/S2C BOTH THE LT AND RT OFF-WING SLIDE BOTTLE INFLATION CABLES WERE FOUND OUT OF RIG. INSTALLED
- [SDR RYN2008F00003](https://openairdocs.org/sdr/RYN2008F00003), Jun 30, 2008: SLIDE. UNWANTED DEPLOY. FLIGHT ATTENDANT DEPLOYED L2 PASSENGER ENTRY DOOR SLIDE. ACFT MADE A FERRY FLIGHT KWI TO BAH FOR DOOR SLIDE REPLACEMENT. INSTALLED SERVICEABLE L2 DOOR SLIDE IAW
- [SDR DL76S060889](https://openairdocs.org/sdr/DL76S060889), Oct 16, 2006: BULKHEAD. CRACKED. THE NLG BULKHEAD AFT WEB AND CHORD AT STA. 287, RBL 25 HAS DRILL DAMAGE TO THE WEB AND CHORD AND THE CHORD WAS STOP DRILLED INSTEAD OF CUT OUT AS REQUIRED PER T
- [SDR DL76S060839](https://openairdocs.org/sdr/DL76S060839), Oct 11, 2006: SPAR. CRACKED. CRACK WAS FOUND IN LOWER OB FASTENER HOLE IN REAR SPAR. THE CRACK WAS REMOVED BY OVERSIZING HOLE AND INSTALLATION OF A FLANGED BUSHING IAW MFG INSTRUCTIONS. REP
- [SDR DL76S060838](https://openairdocs.org/sdr/DL76S060838), Oct 11, 2006: WEB. DAMAGED. WEB AT STA 654+121, LBL 40 WAS FOUND DAMAGED, CARGO COMPARTMENT JUST BELOW INNER CHORD. REPAIR WILL INVOLVE CUTTING THE WEB, SPLICING IAW INSTRUCTIONS. REPAIRED
- [SDR DL76S060834](https://openairdocs.org/sdr/DL76S060834), Oct 10, 2006: SKIN. CORRODED. DURING ROUTINE MTC CORROSION AND MINOR CRACKS WERE FOUND IN FUSELAGE SKIN AT 789.5 AND S-38L. SKIN WAS TRIMMED, DOUBLER AND TRIPLER INSTALLED IAW 455466-14 IAW 
- [SDR DL76S060716](https://openairdocs.org/sdr/DL76S060716), Aug 29, 2006: FITTING. CORRODED. THE LT MLG ATTACH FITTING DRAG BRACE BORE IS CORRODED. THE BORE WAS OVERSIZED TO REMOVE THE CORROSION.
- [SDR DL76S060715](https://openairdocs.org/sdr/DL76S060715), Aug 29, 2006: FITTING. CORRODED. THE RT MLG DRAG BRACE FITTING HAD CORROSION IN THE BORE. THE CORROSION WAS REMOVED BY OVERSIZING THE BORE.
- [SDR DL76S060423](https://openairdocs.org/sdr/DL76S060423), May 24, 2006: FRAME. CRACKED. CRACKS WERE FOUND IN THE INNER CHORD OF THE BS 903.5 LT AND RT FRAMES. THE CRACK WAS TRIMMED OUT AND A REPAIR ANGLE WAS INSTALLED REF AD 2003-18-10.
- [SDR DL76S050474](https://openairdocs.org/sdr/DL76S050474), Aug 22, 2005: BATTERY. INOPERATIVE. 1L DOOR FLASHLIGHT WON`T TEST. REPLACED BATTERY.
- [SDR DL76S050473](https://openairdocs.org/sdr/DL76S050473), Aug 22, 2005: SMOKE DETECTOR. INOPERATIVE. MID LEFT SMOKE DETECTOR WOULD NOT SILENCE. REPLACED SMOKE DETECTOR.
- [SDR DL76S040581](https://openairdocs.org/sdr/DL76S040581), Jun 20, 2004: ROD. BROKEN. ON TAKEOFF HAD GEAR DISAGREE LIGHT ON EICAS WITH WARNING, GEAR HANDLE UP. LEFT MAIN GEAR INDICATED DOWN WITH DOORS LIGHT ON AND GEAR LIGHT ON. PUT GEAR DOWN AND
- [SDR DL76S040185](https://openairdocs.org/sdr/DL76S040185), Feb 20, 2004: FILTER. DIRTY. FLIGHT ATT REPORTS THAT FIRST CLASS GALLEY CHILLER HAS OVERHEATED. ALSO REPORTED AN ELECTIRICAL ODOR THAT APPEARED TO ORIGINATE NEAR THE TRASH BIN. INSPECTED FR
- [SDR DL76S030132](https://openairdocs.org/sdr/DL76S030132), Feb 6, 2003: FRAME. CRACKED. INSPECTION OF THE FS 1809.5 BULKHEAD OUTER FRAMES PER BAC S/B 767-53-0078 AND AD 2001-09-13 REVEALED A CRACK IN THE FWD FRAME AND THE AFT FRAME ON THE RT SIDE N
- [SDR DL76S011656](https://openairdocs.org/sdr/DL76S011656), Oct 11, 2001: SKIN. WORN. DURING ACCOMPLISHMENT OF SIP MOD ON THE NR 2 PYLON WEAR DAMAGE FROM A HYDRAULIC LINE CLAMP SCREW WAS FOUND ON THE LOWER WING SKIN. THE DAMAGE IS LOCATED AT APPR
- [SDR DL76S011650](https://openairdocs.org/sdr/DL76S011650), Oct 11, 2001: BULKHEAD. CRACKED. DURING ACCOMPLISHMENT OF PYLON SIP MOD, CRACK INDICATIONS WERE FOUND IN THE MID STRUT BULKHEAD LAYER. REPAIR ER/A 398051-14AD.
- [SDR DL76S010953](https://openairdocs.org/sdr/DL76S010953), Jun 12, 2001: UNKNOWN. ODOR. AT FL 410 TERRAIN SYSTEM STARTED WARNING OF TERRAIN, NOTICED ODOR OF MELTING PLASTIC. CK UNDER O-CARE SHIELD WIRING OR ODOR FOUND FIBERGLASS ON F/O ALT. REPOSIT
- [SDR DL76S002287](https://openairdocs.org/sdr/DL76S002287), Nov 19, 2000: SKIN. PUNCTURED. FUSELAGE / SKIN / FS 390-412 / STRG. 33R-34R : PUNCTURE REPAIR . THE FUSELAGE SKIN WAS PUNCTURED BY GROUND EQUIPMENT BETWENN FS 390 & 412 AND BETWEEN STRINGERS 
- [SDR DL76S992807](https://openairdocs.org/sdr/DL76S992807), Dec 16, 1999: FRAME. DENTED. EXISTING REPAIR REMOVED AT C-1 DOORWAY AFT EDGE. REVEALING DAMAGE TO SKIN BEARSTRAP AND FRAME OUTER CHORD. DAMAGE LOCATED BETWEEN STR-31R AND 32R AT STA 615. SK
- [SDR DL76S992775](https://openairdocs.org/sdr/DL76S992775), Dec 6, 1999: FRAME. CORRODED. FS 1562 FRAME FAIL-SAFE CHORD WAS FOUND CORRODED BETWEEN STR 38L AND STR 38R. THE (P/N 146T1223-30) CHORD WAS REPLACED PER DWG 146T1223.
- [SDR DL76S992777](https://openairdocs.org/sdr/DL76S992777), Dec 1, 1999: SHEAR TIE. CORRODED. THE FUSELAGE TO FRAME SHEAR TIE AT STA 1562 LOCATED ON THE FWD SIDE OF THE FRAME BETWEEN STR 38L AND 38R WAS FOUND CORRODED. THE (P/N 150T2102-656) SHEAR TIE WA
- [SDR DL76S992776](https://openairdocs.org/sdr/DL76S992776), Dec 1, 1999: SHEAR TIE. CORRODED. THE FUSELAGE SKIN TO FRAME SHEAR TIE LOCATED ON THE AFT SIDE OF FRAME STA 1562 WAS FOUND CORRODED. THE (P/N 140T2102-23) SHEAR TIE WAS REPLACED PER DWG 146T1223
- [SDR DL76S992774](https://openairdocs.org/sdr/DL76S992774), Dec 1, 1999: SPLICE. CORRODED. STRINGER 37R SPLICE WAS FOUND CORRODED AT FS 434. THE (P/N 140T0115-16) SPLICE WAS REPLACED PER SRM 51-10-00. NO DAMAGE TO THE STRINGER WAS FOUND.
- [SDR DL76S992773](https://openairdocs.org/sdr/DL76S992773), Dec 1, 1999: SPLICE. CORRODED. STRINGER 34L SPLICE WAS FOUND CORRODED AT FS 434. THE (P/N 140T0115-16) SPLICE WAS REPLACED PER SRM 51-10-00. NO DAMAGE TO THE STRINGER WAS FOUND.
- [SDR DL76S992772](https://openairdocs.org/sdr/DL76S992772), Dec 1, 1999: SPLICE. CORRODED. STRINGER 37L SPLICE WAS FOUND CORRODED AT FS 434. THE (P/N 140T0115-16) SPLICE WAS REPLACED PER SRM 51-10-00. NO DAMAGE TO THE STRINGER WAS FOUND.
- [SDR DL76S992771](https://openairdocs.org/sdr/DL76S992771), Dec 1, 1999: SPLICE. CORRODED. STRINGER 38L SPLICE WAS FOUND CORRODED AT FS 434. THE (P/N 140T0115-16) SPLICE WAS REPLACED PER SRM 51-10-00. NO DAMAGE TO THE STRINGER WAS FOUND.
- [SDR DL76S992770](https://openairdocs.org/sdr/DL76S992770), Dec 1, 1999: SPLICE. CORRODED. STRINGER 39L SPLICE WAS FOUND CORRODED AT FS 434. THE (P/N 140T0115-16) SPLICE WAS REPLACED PER SRM 51-10-00. NO DAMAGE WAS FOUND ON THE STRINGER.
- [SDR DL76S980522](https://openairdocs.org/sdr/DL76S980522), Feb 13, 1998: BULB. FAILED. EXTERIOR EMERG LIGHT AFT OF WING INOP, LEFT SIDE. RELAMPED, CK GOOD.
- [SDR DL76S972111](https://openairdocs.org/sdr/DL76S972111), Oct 10, 1997: SKIN. CORROSION. DURING ACCOMPLISHMENT OF EO 1-60000-3, CORROSION WAS FOUND DIRECTLY UNDER THE DRAIN SCREEN LOCATED AT APPROXIMATELY LBL 70. THE RESULTING BLENDS, WITH A MAXIMUM
- [SDR DL76S971922](https://openairdocs.org/sdr/DL76S971922), Sep 18, 1997: FLOORBEAM. CRACKED. THE FUSELAGE SEAT TRACKS LOCATED AT RBL 33, LBL 54, AND RBL 54 WERE FOUND CRACKED IN THE VERTICAL WEB OF THE UPPER CHORD AT APPROXIMATELY FS 786 AS DESCRIBED IN
- [SDR DL76S971264](https://openairdocs.org/sdr/DL76S971264), Jun 29, 1997: BULB. SHORTED. DURING CRUISE 37000 FT 1 HR INTO FLT, SMELLED ELECTRICAL SMELL. SHUT OFF UTILITY BUSSES PULLED C/BS U6 U33. F/A REPORTED, WORSE IN LT HAND F/C TURNED OFF LT PAC
- [SDR DL76S971108](https://openairdocs.org/sdr/DL76S971108), Jun 9, 1997: VALVE. INOPERATIVE. NOSE GEAR DID NOT RETRACT ON T/O, DURING GEAR RETRACTION A/C SHUDDERED, CENTER HYD SYS EICAS MSG CAME ON, CENTER HYD PUMP LOW PRESS LTS CAME ON. DEMAND PUMP LOW
- [SDR DL76S961254](https://openairdocs.org/sdr/DL76S961254), May 22, 1996: ENGINE. MALFUNCTIONED. RT ENG FLAME-OUT JUST AFTER ROTATION. ALL INDICATIONS NORMAL AT LIFTOFF, THEN FLAME-OUT OCCURRED. REPLACED LEAKING FUEL MANIFOLD LINE AND LEAKING FUEL NOZZLE, L
- [SDR DL76S960908](https://openairdocs.org/sdr/DL76S960908), Apr 2, 1996: TE WEDGE. DELAMINATION. THE NR 5 LEADING EDGE SLAT TRAILING EDGE WEDGE WAS FOUND TO HAVE UPPER SKIN DELAMINATED. THE DELAMINATED AREA IS APPROX 3 INCH BY 3 INCH AND IS LOCATED AT THE I
- [SDR DL76S960106](https://openairdocs.org/sdr/DL76S960106), Jan 15, 1996: LINE. CRACKED. ON APPROACH TO ATL, HAD SMOKE OR BURNING ODOR IN AFT AND MID CABIN. FOUND SLAT PRESSURE HYD LINE CRACKED AT WING ROOT FUSELAGE FITTING. REPLACED HYD LINE, NO LE
- [SDR DL76S954237](https://openairdocs.org/sdr/DL76S954237), Nov 3, 1995: EEL. INOPERATIVE. LEFT WING LWR AFT EMERGENCY LIGHT INOP. RELAMPED, CKS OK.
- [SDR DL76S953919](https://openairdocs.org/sdr/DL76S953919), Oct 3, 1995: EEL LAMP. FAILED. RIGHT AFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. LOCATED AFT OF R2 ENTRANCE DOOR. RELAMPED, CHECKS GOOD.
- [SDR DL76S952463](https://openairdocs.org/sdr/DL76S952463), Jun 3, 1995: PNEUMATIC SYS. CONTAMINATED. ON TAKEOFF AND CLIMB, HAD SMOKE ODOR AND FUMES IN MID GALLEY LAV AREA, RETURNED FLT TO ATL. FOUND COMPRESSOR WASH FLUID CONTAMINATION IN NR 2 ENGINE INLET. RAN 
- [SDR DL76S952238](https://openairdocs.org/sdr/DL76S952238), May 19, 1995: HOSE. LEAKING. AFTER TAKEOFF, RT MAIN LANDING GEAR WOULD NOT RETRACT, RETURNED MCO. FOUND RT MLG TRUCK TILT PRESSURE LINE BROKEN. REPLACED LINE OPERATION NORMAL.

## 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 ATL88FA239](https://openairdocs.org/ntsb/ATL88FA239), Aug 27, 1988: Boeing 767 (N120DL), Charleston, SC, no damage

## 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 19911119056779I](https://openairdocs.org/incident/19911119056779I), Nov 19, 1991: Boeing 767332 (N120DL), New York, NY, Minor damage. Right wing tip of aircraft struck left elevator of another aircraft during taxi.
- [Accident 19880826070269A](https://openairdocs.org/incident/19880826070269A), Aug 26, 1988: Boeing 767332 (N120DL), Charleston, SC. Saw build-up ahead,tried to turn TO0 late. Aircraft encountered severe turbulence injuring passengers and stewardess

## Other aircraft with N120DL

- [Registered now](https://openairdocs.org/aircraft/N120DL): Eurocopter EC120B, S/N 1634, built 2010

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