N915RW1967 Douglas DC-9-31
This N-number isn't registered right now. Below is its last known registration, canceled Nov 19, 2013.
Safety record in brief:No NTSB accidents or incidents since 1982No ADs since 1998 matched55 service difficulty reports
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 20, 2026- Last registered owner
- Delta Air Lines INC
- Owner type
- Corporation
- City, state
- Atlanta, GA
- Certificate issued
- Dec 31, 2009
- Canceled
- Nov 19, 2013
- Airworthiness
- Standard · Transport
- Airworthiness date
- Sep 18, 1990
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Airframe & engine
FAA Registry + type dataAirframe
- Manufacturer
- Douglas
- Model
- DC-9-31
- Year
- 1967
- Serial number
- 47139
- Aircraft type
- Fixed wing multi engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 85
- Engines
- 2
- Max takeoff weight
- 20,000 and over lb
- Mode S code
- ACAACA
Engine
- Make and model
- P & W Jt8d-15
- Type
- Turbo-jet
- Power
- 15,500 lb thrust
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2009 – 2013Delta Air Lines INCAtlanta, GA
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
ADs published since 1998 that may apply (0)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
No ADs published since 1998 matched this airframe or engine model.
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (55)
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
- Lights · battery pack · dischargedDec 16, 2009
DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 11-13 AND 18-21 OF THE CABIN WERE TOO DIM TO PROVIDE ESCAPE GUIDANCE IF OBSCURED BY SMOKE OR DARKNESS. MAINTENANCE REPLACED THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Lights · wire · corrodedMay 30, 2009
DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING FOR THE CATWALK IN THE TAIL COMPARTMENT WAS INOPERATIVE. MAINTENANCE FOUND A CORRODED WIRE FOR THE TAIL COMPARTMENT LIGHTS AND REPAIRED IT. FUNCTIONAL CHECK WAS GOOD.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Lights · battery pack · inoperativeMar 24, 2009
DURING LINE CHECK, MX FOUND THAT THE LT SIDE EXTERIOR EMERGENCY OVERWING EMERGENCY FLOOD LIGHT WAS INOPERATIVE. MX REPLACED THE BATTERY PACK AND THE LIGHT RETURNED TO AN OPERATIONAL CONDITION. (K)
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Lights · power supply · dischargedFeb 7, 2009
DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 5-7 OF THE CABIN WERE INOPERATIVE. MX REPLACED THE EMERGENCY LIGHT PWR SUPPLY AND OPERATIONALLY CHECKED THE SYS. (K)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin · damagedMar 2, 2008
DURING GROUND OPERATIONS, FUSELAGE SKIN WAS DAMAGED AT BS 1121 L26L AND L28L. REPAIRED PER EA 99-212444.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · frame · crackedMay 13, 2007
DURING "H" CHECK, FOUND CRACKS IN FRAME AT BS 1004 BETWEEN L28R AND L29R AND L28L AND L30L. REPAIRED PER EA 99-209582.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin · crackedMay 12, 2007
DURING "H" CHECK, FOUND CRACK IN LT FUSELAGE SKIN AT THE UPPER FORWARD CORNER OF FORWARD PASSENGER DOOR JAMB. REPAIRED PER EA 99-209571.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin · crackedFeb 23, 2001
During an H-check found a 3" long skin crack at shear clip attach under dorsal attach front fairings. Repaired per EA. 99-180941
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · frame · crackedAug 12, 1999
DURING L CHECK AND WITH COMPLIANCE WITH SB DC9-53-280 REV 1. A CRACK WAS NOTED ON THE FUSELAGE SKIN AFT OF THE FORWARD PASSENGER DOOR AT DOORSTOP NR 6. REPAIRED PER EA 99-167024.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Flight controls · rudder valve · out of adjustApr 12, 1998
DURING CLIMBOUT, THE FLAP/RUDDER STOP INOPERATIVE INDICATION ILLUMINATED. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. THE FLIGHT CREW NOTED THAT THE RUDDER/STOP INDICATION LIGHT EXTINGUISHED WHEN FLAPS WERE EXTENDED FOR LANDING. MAINTENANCE ADJUSTED AND TESTED THE AUXILIARY RUDDER THROW…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Showing the 10 most recent of 55 reports.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026