# N8926E: 1967 Douglas DC-9-31, registration cancelled 2010-11-23 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: November 23, 2010 - Status when cancelled: Valid registration - Airframe: [Douglas DC-9-31](https://openairdocs.org/model/douglas-dc-9-31) (registry code 3022065) - Engine: [Pratt & Whitney JT8D-1](https://openairdocs.org/engine/pratt-whitney-jt8d-1) (registry code 52044) - Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs) - Serial number: 45863 - Year built: 1967 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: March 21, 1977 - Certificate issued: December 31, 2009 - Last registry action: December 31, 2009 - Mode S code: AC4FF1 - 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/N8926E - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=8926E - Page: https://openairdocs.org/deregistered/N8926E-2010-11-23 From the FAA registry file of November 3, 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 Douglas DC-9-31: https://openairdocs.org/model/douglas-dc-9-31.md ## Service difficulty reports (42) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR NWAA093359946](https://openairdocs.org/sdr/NWAA093359946), Sep 24, 2009: WEB. BUCKLED. DURING ENGINE CHANGE FOUND PYLON VERTICAL WEB BUCKLED BETWEEN UPPER AND LOWER SPARS FOR AFT ENGINE MOUNT AT XN39.250. REPAIRED PER EA 99-216590. - [SDR NWAA074359946](https://openairdocs.org/sdr/NWAA074359946), Dec 21, 2007: SKIN. CRACKED. DURING "H" CHECK, FOUND CRACKS IN SKIN AT FORWARD PASSENGER ENTRY DOOR CUTOUT AT AFT DOOR STOPS NR 3 AND NR 4. REPAIRED PER EA 99-211049. - [SDR NWAA072859946](https://openairdocs.org/sdr/NWAA072859946), Aug 16, 2007: BATTERY PACK. INOPERATIVE. TAIL CONE PATH LIGHTS INOP. REPLACED BATTERY PACK. OPERATION CHECKS GOOD. - [SDR NWAA072809946](https://openairdocs.org/sdr/NWAA072809946), Aug 8, 2007: POWER SUPPLY. INOPERATIVE. TAIL COMPARTMENT EMERGENCY ESCAPE PATH LIGHTING INOP. REPLACED POWER SUPPLY. - [SDR NWAA072799946](https://openairdocs.org/sdr/NWAA072799946), Jul 26, 2007: BATTERY PACK. INOPERATIVE. AFT EMERGENCY CAT-WALK LIGHT OUT DURING EMERGENCY LIGHT CHECK. REPLACED BATTERY PACK. - [SDR 0300749946](https://openairdocs.org/sdr/0300749946), Apr 7, 2003: LINE. LEAKING. ON CLIMB SHORTLY AFTER GEAR RETRACTION THE RIGHT HYDRAULIC PRESSURE BEGAN FLUCTUATING BY FLUID LOSS. THE THE LEFT HYDRAULIC SYSTEM LOST PRESSURE AND LOST FLUID. - [SDR 0200159946](https://openairdocs.org/sdr/0200159946), Jan 14, 2002: WEB. CRACKED. During Hck in ATL, A crack was found in the lower outboard corner of the diagonal web in the L/H engine pylon just forward of the rear spar. Repaired per EA 99- - [SDR 0200139946](https://openairdocs.org/sdr/0200139946), Jan 9, 2002: FLOORBEAM. CRACKED. DURING HCK IN ATL, A CRACK WAS FOUND IN THE UPPER VERTICLE FLANGE OF THE STATION 237 FLOORBEAM AT X=6. REPAIRED PER EA 99-185447. - [SDR 0200149946](https://openairdocs.org/sdr/0200149946), Jan 8, 2002: SKIN. CORRODED. During HCK in ATL, corrosion was found on the R/H wing upper skin doubler flange attachment holes for the fuel access door. Repaired per EA 99-185451. - [SDR 9809329946](https://openairdocs.org/sdr/9809329946), May 17, 1998: WIRE. BROKEN. DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHTS ON CATWALK ILLUMINATED WITH SWITCH IN OFF POSITION. REPAIRED BROKEN WIRING TO SPLICE NEAR TAILCONE BA - [SDR 9800229946](https://openairdocs.org/sdr/9800229946), Jan 5, 1998: BATTERY CHARGER. FAILED. BATTERY CHARGER ANNUNCIATOR LIGHT ILLUMINATED AFTER TAKEOFF. FLIGHT WAS RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED BATTERY CHARGER AND MA - [SDR 9720339946](https://openairdocs.org/sdr/9720339946), Oct 11, 1997: BULKHEAD. CORRODED. DURING LINE CHECK, FOUND CORROSION ON AFT PRESSURE BULKHEAD AT RADIAL NR 9 APPROXIMATELY 12 INCHES FROM OUTBOARD END. REPAIRED PER EA 99-152220. - [SDR 9716369946](https://openairdocs.org/sdr/9716369946), Sep 1, 1997: BATTERY. DISCHARGED. DURING PERIODIC CHECK, FORWARD SERVICE DOOR EVACUATION SLIDE FAILED BATTERY TEST. REPLACED SLIDE. - [SDR 9707809946](https://openairdocs.org/sdr/9707809946), Apr 17, 1997: DOWNLOCK SWITCH. MALFUNCTIONED. DURING APPROACH INTO MEM, THE RIGHT MAIN LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE AFTER GEAR EXTENSION. RECYCLED GEAR AND NORMAL INDICATIONS WERE ACHIEVED. A - [SDR 9702769946](https://openairdocs.org/sdr/9702769946), Feb 7, 1997: DOWNLOCK SWITCH. FAILED. DURING APPROACH, THE RIGHT MAIN LANDING GEAR GREEN LIGHT FAILED TO ILLUMINATE AFTER GEAR EXTENSION. RECYCLED GEAR AND NORMAL INDICATIONS WERE ACHIEVED. MAINTENA - [SDR 9622509946](https://openairdocs.org/sdr/9622509946), Oct 16, 1996: WIRE. BROKEN. DURING LINE MAINTENANCE INSPECTION, FOUND FLOOR PROXIMITY EMERGENCY LIGHTS AT ROW 13 INOPERATIVE. MAINTENANCE FOUND BROKEN WIRE ON CONNECTOR UNDER SEAT. REPAIRE - [SDR 9620589946](https://openairdocs.org/sdr/9620589946), Sep 25, 1996: LIGHTS. LOOSE. DURING LINE MAINTENANCE INSPECTION, FOUND TAILCONE EMERGENCY LIGHT AND POWER SUPPLY LOOSE FROM BRACKET. REPLACED POWER SUPPLY AND BATTERIES, OPERATIONAL CHECK N - [SDR 9619499946](https://openairdocs.org/sdr/9619499946), Sep 7, 1996: AIR CYCLE MACH. OVERSERVICED. FLIGHT ATTENDANT REPORTED HAZE AND SMOKE IN CABIN AFTER TAKEOFF. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND RIGHT AIR CYCLE MACHINE O - [SDR 9616589946](https://openairdocs.org/sdr/9616589946), Jul 30, 1996: BATTERY PACK. MALFUNCTIONED. DURING LINE MAINTENANCE INSPECTION, FOUND AFT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. - [SDR 9608659946](https://openairdocs.org/sdr/9608659946), Apr 15, 1996: POWER SUPPLY. INOPERATIVE. DURING LINE MAINTENANCE INSPECTION, FOUND TAIL COMPARTMENT EMERGENCY LIGHT POWER SUPPLY BROKEN. REPLACED POWER SUPPLY AND OPERATIONAL CHECK NORMAL. - [SDR 9518499946](https://openairdocs.org/sdr/9518499946), Nov 17, 1995: TRANSDUCER. FAILED. DURING CLIMB, THE STALL WARNING SYSTEM ACTIVATED AND THE RED STALL LIGHT ILLUMINATED. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURE AND SYSTEM MALFUNCTION CONTINU - [SDR 9519199946](https://openairdocs.org/sdr/9519199946), Nov 9, 1995: SEAT TRACK. CORRODED. DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE RBL 44 SEAT TRACK AT FS 284. REPAIRED TRACK (P/N 2772660), PER EA 99-103090. - [SDR 9519159946](https://openairdocs.org/sdr/9519159946), Nov 6, 1995: SKIN. CORRODED. DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FUSELAGE SKIN FS 94 TO 110 AT LONGERON 24L AND ON THE T-CAP, FS 110 BETWEEN LONGERONS 24L T - [SDR 9519149946](https://openairdocs.org/sdr/9519149946), Nov 6, 1995: LONGERON. CORRODED. DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON LONGERON 19L BETWEEN FS 541 TO 579. REPAIRED LONGERON (P/N 5920354-1), PER EA 99-103115. - [SDR 9519139946](https://openairdocs.org/sdr/9519139946), Nov 3, 1995: BULKHEAD TEE. CORRODED. DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FS 756 T-CAP AT LONGERON 30. REPAIRED T-CAP (P/N 3915182-502), PER EA 99-103092. - [SDR 9519129946](https://openairdocs.org/sdr/9519129946), Nov 2, 1995: WEB. CRACKED. DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE FS 83 FLIGHT COMPARTMENT PRESSURE PANEL WEB, RIGHT SIDE. REPAIRED WEB (P/N 9910073), PER EA 9 - [SDR 9519119946](https://openairdocs.org/sdr/9519119946), Oct 30, 1995: BULKHEAD TEE. CRACKED. DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE FS 996 AFT PRESSURE BULKHEAD FLOOR TEE AT RBL 34. REPAIRED TEE (P/N 5910163-139), PER EA 99-1 - [SDR 9519109946](https://openairdocs.org/sdr/9519109946), Oct 11, 1995: FRAME. CORRODED. DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE FS 996 FRAME ANGLE AT THE T-CAP BETWEEN LONGERONS 26R TO 27R. REPAIRED PER EA 99-102943. - [SDR 9515579946](https://openairdocs.org/sdr/9515579946), Oct 10, 1995: LONGERON. CORRODED. DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE LONGERON 29L TO 30 FITTINGS AT FS 756. REPLACED FITTINGS PER SRM 51-05. - [SDR 9519099946](https://openairdocs.org/sdr/9519099946), Oct 3, 1995: INTERCOSTAL. CORRODED. DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FS 190 INTERCOSTAL ABOVE THE FORWARD STAIR CUTOUT. REPAIRED INTERCOSTAL (P/N 9957838-3), PE - [SDR 9519089946](https://openairdocs.org/sdr/9519089946), Sep 30, 1995: ANGLE. CORRODED. DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE NOSE GEAR FORWARD LEFT DOOR JAMB INNER ANGLE FS 43. REPAIRED ANGLE PER EA 99-102962. - [SDR 9515219946](https://openairdocs.org/sdr/9515219946), Sep 30, 1995: FITTING. CRACKED. DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACKS AND CORROSION IN THE FS 980 TO 996 FLOORBEAM END FITTINGS, LEFT AND RIGHT SIDES. REPLACED ALL FOUR FI - [SDR 9515159946](https://openairdocs.org/sdr/9515159946), Sep 27, 1995: FITTING. CORRODED. DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE LONGERON 26L END FITTINGS AT FS 996. REPLACED FITTING PER SRM 51-01. - [SDR 9518139946](https://openairdocs.org/sdr/9518139946), Sep 14, 1995: SKIN. CORRODED. DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FUSELAGE SKIN FS 746 BETWEEN LONGERON 20R TO 21R. REPAIRED SKIN (P/N 5911420-3), PER EA 99- - [SDR 9514139946](https://openairdocs.org/sdr/9514139946), Sep 7, 1995: CASTING. CRACKED. DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE ATTACH CASTING LOCATED AT FS 691, LEFT OF THE CENTER LINE IN THE LEFT MAIN LANDING GEAR WHEEL - [SDR 9514129946](https://openairdocs.org/sdr/9514129946), Sep 7, 1995: CASTING. CRACKED. DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE ATTACH CASTING BETWEEN THE FS 756 BULKHEAD AND LONGERON 29L IN THE LEFT MAIN LANDING GEAR WHE - [SDR 9519079946](https://openairdocs.org/sdr/9519079946), Sep 5, 1995: SPAR WEB. CRACKED. DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE HORIZONTAL STABILIZER REAR SPAR WEB AT STA 104. REPAIRED WEB (P/N 9918401-103), PER EA 99-102 - [SDR 9513969946](https://openairdocs.org/sdr/9513969946), Sep 5, 1995: BULKHEAD. CORRODED. DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION BETWEEN THE LONGERON 29L AND 30 ATTACH CASTINGS AND THE FS 756 BULKHEAD. REPLACED BOTH CASTINGS PE - [SDR 9513489946](https://openairdocs.org/sdr/9513489946), Aug 28, 1995: FITTING. CRACKED. DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE RIGHT T-CAP TIE FITTING, FS 604 AT LONGERON 30. REPLACED FITTING PER SRM 51-01. - [SDR 9513019946](https://openairdocs.org/sdr/9513019946), Aug 22, 1995: SKIN. CRACKED. DURING ACCEPTANCE CHECK, FOUND SKIN CRACKED BETWEEN FS 148 AND 150, LONGERON 27L. FABRICATED DOUBLER AND INSTALLED PER EA 99-102752 AND SRM 53-04 FIG 8. - [SDR 9512469946](https://openairdocs.org/sdr/9512469946), Aug 10, 1995: FITTING. CRACKED. DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE LONGERON 25L END FITTING AT FS 110. REPLACED FITTING PER SRM 51-01. - [SDR 9519059946](https://openairdocs.org/sdr/9519059946), Jul 13, 1995: BLKHD WEB. CORRODED. DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FS 604 BULKHEAD WEB LOWER AFT EDGE. REPAIRED WEB (P/N 5914865-23), PER EA 99-92255. ## FAA accident and incident reports (5) 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 20030407006779I](https://openairdocs.org/incident/20030407006779I), Apr 7, 2003: Doug DC931 (N8926E), Indianapolis, IN, Minor damage. (-23) On April 7, 2003 northwest airlines flight 1478 declared an emergency due to hydraulic system fluid loss and diverted to Indianapolis, IN. Maintenance… - [Incident 20000914027239I](https://openairdocs.org/incident/20000914027239I), Sep 14, 2000: Doug DC931 (N8926E), Buffalo, NY, Minor damage. (-23)On Thursday, September 14, 2000, at 2003 local, a DC-9-30, N8926E, operated by northwest airlines, after landing on runway 23 at Buffalo niagra… - [Incident 19841027066499I](https://openairdocs.org/incident/19841027066499I), Oct 27, 1984: Doug DC931 (N8926E), Mobile, AL, Minor damage. Aircraft touched down right wing low due to wind shear. Go around executed. Right wing flap struck runway light. - [Incident 19780710042989I](https://openairdocs.org/incident/19780710042989I), Jul 10, 1978: Doug DC9 (N8926E), Boston, MA, Minor damage. Gear doors did not close after gear extension. Landing made with gear doors open. - [Incident 19780303016089I](https://openairdocs.org/incident/19780303016089I), Mar 3, 1978: Doug DC9 (N8926E), Flushing, NY, Minor damage. Aircraft damaged while parked at gate by a rolling, driverless vehicle. --- 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.