# N123DN: 1987 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: 23437 - Year built: 1987 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: November 3, 1987 - Certificate issued: July 25, 2013 - Last registry action: July 25, 2013 - Mode S code: A05F2F - Owner when cancelled: [Jet Midwest Group LLC](https://openairdocs.org/faa-owner/JET%20MIDWEST%20GROUP%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/N123DN - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=123DN - Page: https://openairdocs.org/deregistered/N123DN-2018-02-28 From the FAA registry file of November 7, 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 (40) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR RYNA201207250031](https://openairdocs.org/sdr/RYNA201207250031), Jul 25, 2012: CONNECTOR. LOOSE. FOUND EMERGENCY LIGHTING WIRE HARNESS CONNECTOR LOOSE UNDER SEAT 26B AND 25F. RECONNECTED CONNECTOR AND SECURED WIRE HARNESS UNDER SEAT 26B AND25F AND EMERGENCY - [SDR RYNA201206150026](https://openairdocs.org/sdr/RYNA201206150026), Jun 15, 2012: BATTERY PACK. DISCHARGED. EMERGENCY LIGHTS INOPERATIVE AT ALL PASSENGER SEATS AND LOWER EXIT SIGNS AT ALL DOORS. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS AT SEATS 2A, 29A, AND - [SDR RYNA201203200015](https://openairdocs.org/sdr/RYNA201203200015), Mar 20, 2012: ACTUATOR VALVE. INOPERATIVE. NR 2 ENGINE WILL NOT START- ENGINE VALVE LIGHT ILLUMINATED ON OVERHEAD PANEL. EICAS MESSAGE "RIGHT ENGINE VALVE-NO START". REMOVED AND REPLACED ENGINE CONDITION - [SDR RYNA2011082000018](https://openairdocs.org/sdr/RYNA2011082000018), Aug 20, 2011: BATTERY PACK. INOPERATIVE. RIGHT/LEFT AFT, L1 AND R1 EMERGENCY EXIT THRESHOLD LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK PER MM 33-51-07. OPERATIONAL CHECKED GOOD. - [SDR RYNA2010002260005](https://openairdocs.org/sdr/RYNA2010002260005), Feb 5, 2010: BATTERY PACK. DISCHARGED. THE FOLLOWING ITEMS WERE NOTED REGARDING THE EMERGENCY LIGHTING SYSTEM DURING THE INSPECTION AND TESTING OF THE C-CHECK ON AIRCRAFT N123DN: EMERGENCY LIGHT OUTS - [SDR RYNA201002040003](https://openairdocs.org/sdr/RYNA201002040003), Jan 30, 2010: STRAP. CRACKED. DURING THE ACCOMPLISHMENT OF EO RN767-53-02 RELATED TO BOEING SB 767-53A0100 AND AD 2004-19-06-R1 .1875 INCH CRACK WAS FOUND ON THE RT REAR BULKHEAD SIDE FITTIN - [SDR RYNA2010002040002](https://openairdocs.org/sdr/RYNA2010002040002), Jan 30, 2010: STRAP. CRACKED. DURING THE ACCOMPLISHMENT OF EO RN767-53-02 RELATED TO BOEING SB 767-53A0100 AND AD 2004-19-06 R1 A .0937 INCH CRACK WAS FOUND ON THE LT REAR BULKHEAD SIDE FITT - [SDR RYNA200910300021](https://openairdocs.org/sdr/RYNA200910300021), Oct 29, 2009: UNKNOWN. MALFUNCTIONED. DURING CLIMB EICAS E/E LIGHT ILLUMINATED, CABIN CONTINUED SLIGHT CLIMB. PERFORMED AIR TURNBACK. PLACARD THE LOWER LOBE ELECTRONIC EQUIPMENT ACCESS DOOR ITEM DEF - [SDR RYNA200909180019](https://openairdocs.org/sdr/RYNA200909180019), Sep 14, 2009: STRUCTURE. CRACKED. PERFORMING FLEET CAMPAIGN DIRECTIVE (FCD) 53-205 FOUND CRACKING WITHIN STA 287 AT WL 159 WHICH EXTENDS APPROXIMATELY 0.375 INCHES ABOVE WL 159 AND APPROXIMATELY - [SDR RYNA200908210016](https://openairdocs.org/sdr/RYNA200908210016), Aug 18, 2009: PROXIMITY SENSOR. FAULTY. DURING PREFLIGHT INSPECTION THE PILOT’S OVERHEAD EMERGENCY ADVISORY LIGHT CAME ON. PLACARD THE PILOT’S OVERHEAD EMERGENCY ADVISORY LIGHT PER MEL 52-71-1 DMI REF - [SDR RYNA200906170007](https://openairdocs.org/sdr/RYNA200906170007), Jun 15, 2009: B-NUT. LOOSE. LEFT HYDRAULIC SYSTEM PRESSURE, RUDDER RATIO, LEFT HYDRAULIC QUANTITY, YAW DAMPER, AND SPOILER EICAS MESSAGES. TIGHTENED B NUT THAT BACKED OFF ON NR 1 ENGINE HY - [SDR RYNA200800044](https://openairdocs.org/sdr/RYNA200800044), Nov 28, 2008: FAN BLADE. OUT OF BALANCE. DURING CLIMB AND LEVEL OFF AT F/L 370 RIGHT ENGINE VIBRATION REACHED 3.9 UNITS. THE AIRCRAFT DIVERTED TO ATLANTA FOR MAINTENANCE TO DELTA AIRLINES MAINTENANCE C - [SDR RYN2008F00010](https://openairdocs.org/sdr/RYN2008F00010), Aug 6, 2008: RADIO. FAILED. ACFT DIVERTED DUE TO LOSS OF THE RT HF COMMUNICATION SYSTEM. THE LT HF IS ALREADY ON DEFERRAL PER MEL 23-11-1-2. TROUBLESHOOTING IN WORK (ISSUED MEL 23-11-1-2OH - [SDR DL76S071016](https://openairdocs.org/sdr/DL76S071016), Aug 4, 2007: WINDOW. CRACKED. F/O WINDSHIELD CRACKED AND IS ARCHING. REPLACED R1 WINDOW WINDOW HEAT CONTROL UNIT PER AMM. BITE CHECKED CONTROL UNIT IT VERIFIED GOOD. - [SDR DL76S060877](https://openairdocs.org/sdr/DL76S060877), Oct 20, 2006: FLOORBEAM. CORRODED. CORROSION WAS FOUND AROUND THE NUT PLATES ON THE LOWER TEE OF THE 1502 FLOORBEAM. THE CORROSION WAS REMOVED AND REPAIR PARTS INSTALLED PER BOEING INSTRUCTIONS A - [SDR DL76S060876](https://openairdocs.org/sdr/DL76S060876), Oct 20, 2006: SKIN. CRACKED. THE FUSELAGE SKIN WAS FOUND CRACKED AT THE NR 3 VHF ANTENNA, FS 1197+90, AT STR 39L 39R. REPAIR INVOLVED CUTTING OUT THE DAMAGE AND INSTALLATION OF BOEING APPRO - [SDR DL76S060875](https://openairdocs.org/sdr/DL76S060875), Oct 20, 2006: FITTING. CORRODED. CORROSION WAS IDENTIFIED ON THE INBOARD FORWARD SURFACE OF THE REAR SPAR BULKHEAD TERMINAL FITTING. THE BOEING APPROVED REPAIR INVOLVED REMOVING BOLTS FOR ACCES - [SDR DL76S060873](https://openairdocs.org/sdr/DL76S060873), Oct 20, 2006: SPAR. CRACKED. THE NUMBER 1 PYLON UPPER SPAR FITTING, RHS AT ATTACH FITTING HOLE SHOWED A CRACK INDICATION. THE SUBJECT HOLE WAS OVERSIZED, AND THE BOEING APPROVED REPAIR INVO - [SDR DL76S060871](https://openairdocs.org/sdr/DL76S060871), Oct 20, 2006: BULKHEAD. DAMAGED. DURING ACCOMPLISHMENT OF THE SIP MOD ON THE AIRCRAFT, AN EXISTING FREEZE PLUG REPAIR WAS FOUND ON THE NR 1 PYLON LHS UPPER ATTACH HOLE FOR GSE FITTING. THE PLUG - [SDR DL76S060870](https://openairdocs.org/sdr/DL76S060870), Oct 20, 2006: SPAR. DAMAGED. DURING ACCOMPLISHMENT OF EO 01-074906-03 THE NUMBER 2 PYLON SPLICE PLATE UPPER OUTBOARD HOLE WAS FOUND TO ALREADY BE OVERSIZED TO BEYOND MAX EO LIMIT. THE BOEIN - [SDR DL76S060869](https://openairdocs.org/sdr/DL76S060869), Oct 20, 2006: FITTING. DAMAGED. THE NUMBER 2 PYLON UPPER SPAR FITTING WAS FOUND TO HAVE A PREVIOUSLY OVERSIZED HOLE, AT THE AFT OUTER PERIMETER FASTENER. A BOEING APPROVED REPAIR WAS INSTALLED - [SDR DL76S060868](https://openairdocs.org/sdr/DL76S060868), Oct 20, 2006: SKIN. MISREPAIRED. A PREVIOUS REPAIR FOUND ON THE FUSELAGE SKIN AT 500 AND S36L DOES NOT CONFORM TO SRM AND NO RECORDS WERE FOUND. REPAIR WAS REMOVED AND A BOEING APPROVED REPAIR - [SDR DL76S060658](https://openairdocs.org/sdr/DL76S060658), Aug 11, 2006: FRAME. CRACKED. FUSELAGE FRAME FS 883.5 RHS LOWER INNER CHORD CRACK. CRACK WAS LOCATED ON THE LOWER END OF THE .25 RADIUS TRANSITION BETWEEN CHORD FLANGES. - [SDR DL76S060649](https://openairdocs.org/sdr/DL76S060649), Aug 11, 2006: FRAME. CRACKED. CRACKS WERE FOUND ON THE INNER CHORD OF THE FS 903 FRAME, RT SIDE. DAMAGE WAS CUT OUT AND A REPAIR ANGLE WAS INSTALLED. - [SDR DL76S060583](https://openairdocs.org/sdr/DL76S060583), Jul 13, 2006: FITTING. MISALIGNED. THE NR 1 PYLON INBOARD PITCH LOAD FITTING UPPER LINK BUSHING HAS MIGRATED 0.004 INCH. THE MIGRATED BUSHING WAS REPLACED. AD 2004-16-12, B767-57-0053. - [SDR DL76S060701](https://openairdocs.org/sdr/DL76S060701), Jun 27, 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 DL76S020312](https://openairdocs.org/sdr/DL76S020312), Mar 15, 2002: LIGHT. INOPERATIVE. SVC CHECK FOUND EMERGENCY OVERHEAD LIGHT AT ROW 17 LT SIDE INOP. REPLACED EMERGENCY LIGHT ASSY AT ROW 17 LT SIDE, CHECKS OK. - [SDR DL76S011436](https://openairdocs.org/sdr/DL76S011436), Aug 30, 2001: BATTERY PACK. DISCHARGED. RT EMERGENCY ESCAPE SQUIB WILL NOT TEST. REPLACED RT BATTERY PACK TEST OK. - [SDR DL76S001594](https://openairdocs.org/sdr/DL76S001594), Aug 18, 2000: BATTERY. DISCHARGED. EMERGENCY LIGHT BATTERY PACK AND POWER SUPPLY INOP. REPLACED BATTERY. - [SDR DL76S990685](https://openairdocs.org/sdr/DL76S990685), Mar 29, 1999: POWER SUPPLY. INOPERATIVE. DURING ROUTINE MAINTENANCE, THE LEFT AND RIGHT EMERGENCY EXIT THRESHOLD LIGHTS FOUND INOP. REPLACED POWER SUPPLY, OPS CK NORMAL. - [SDR DL76S980655](https://openairdocs.org/sdr/DL76S980655), Mar 24, 1998: WEDGE. DELAMINATED. WINGS NR 1 SLAT TRAILING EDGE WEDGE, REPAIR FOR DELAMINATION. THE NR 1 SLAT TRAILING EDGE WEDGE WAS FOUND WITH A 3 BY 4 AREA OF DELAMINATION ON THE UPPER SKIN. - [SDR DL76S980654](https://openairdocs.org/sdr/DL76S980654), Mar 24, 1998: WEDGE. DELAMINATED. WINGS NR 2 SLAT TRAILING EDGE WEDGE, REPAIR FOR DELAMINATION. THE NR 2 SLAT TRAILING EDGE WEDGE WAS FOUND WITH A 7 BY 4.5 AREA OF DELAMINATION ON THE UPPER SKIN - [SDR DL76S980653](https://openairdocs.org/sdr/DL76S980653), Mar 24, 1998: WEDGE. DELAMINATED. WINGS NR 8 SLAT TRAILING EDGE WEDGE, REPAIR FOR DELAMINATION. THE NR 8 SLAT TRAILING EDGE WEDGE WAS FOUND WITH A 5 BY 9 AREA OF DELAMINATION ON THE UPPER SKIN. - [SDR DL76S980652](https://openairdocs.org/sdr/DL76S980652), Mar 24, 1998: SKIN. DELAMINATED. WINGS LEADING EDGE SLAT NR 11, TRAILING EDGE WEDGE, SKIN DELAMINATION REPAIR. THE UPPER SKIN OF THE NR 11 SLAT TRAILING EDGE WEDGE WAS FOUND WITH A 3 BY 6 AREA - [SDR DL76S970585](https://openairdocs.org/sdr/DL76S970585), Mar 30, 1997: BATTERY PACK. DISCHARGED. RIGHT AND LEFT AFT SERVICE DOOR INTERIOR EMERGENCY EXIT LIGHT SIGNS INOP. REPLACED BATTERY PACK, CHECKS GOOD. - [SDR DL76S970341](https://openairdocs.org/sdr/DL76S970341), Feb 24, 1997: SKIN. DELAMINATION. THE NR 10 LEADING EDGE SLAT TRAILING EDGE WEDGE WAS FOUND TO HAVE THE UPPER SKIN DELAMINATED AT THE INBD CORNER. THE DAMAGE CUTOUT MEASURES 8 FWD-AFT AND 6 INBD - [SDR DL76S961847](https://openairdocs.org/sdr/DL76S961847), Aug 2, 1996: TE WEDGE. DELAMINATED. THE NRS 10, 11, 12 LEADING EDGE SLATS' TRAILING EDGE WEDGES WERE FOUND TO HAVE AREAS OF DELAMINATION. THE AREAS MEASURE 4 INCHES BY 6 INCHES, 2 INCHES BY 3 INCH - [SDR DL76S960203](https://openairdocs.org/sdr/DL76S960203), Jan 26, 1996: CHECK VALVE. CRACKED. INFLIGHT GOT EICAS FOR LT SYS HYDRAULIC'S, FOLLOWED IMMEDIATELY BY LEFT HYDRAULIC SYS PRESSURE MESSAGE. STATUS PAGE SHOWS LT QTY AT 0.04. FOUND CHECK VALVE AT G - [SDR DL76S952151](https://openairdocs.org/sdr/DL76S952151), May 16, 1995: SKIN. LIGHTNING STRIKE. FOUND DURING LETTER CHECK, LIGHTNING STRIKES ABOVE COCKPIT SECTION OF FUSELAGE. BURNISHED OUT DAMAGES, FOUND ONE LIGHTING STRIKE OUT OF LIMITS. REPLACED RIVETS - [SDR DL76S950698](https://openairdocs.org/sdr/DL76S950698), Feb 19, 1995: SKIN. LIGHTNING STRIKE. DURING LETTER CHECK, FOUND SEVERAL LIGHTNING STIKES TO FUSELAGE SKIN. RT SIDE REPAIRED PER SRM 53-00-01 ITEM 3. --- 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.