# N941AX: Douglas DC-9-31, registration cancelled 2016-03-31 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: March 31, 2016 - Status when cancelled: Second renewal notice - Airframe: [Douglas DC-9-31](https://openairdocs.org/model/douglas-dc-9-31) (registry code 3022065) - Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (OpenAirDocs) - Serial number: 47419 - Type of aircraft: Fixed wing multi engine - Airworthiness: Standard, transport - Airworthiness date: November 6, 1989 - Certificate issued: December 10, 2008 - Last registry action: March 19, 2013 - Mode S code: AD10F5 - Owner when cancelled: [Logistic Air Inc](https://openairdocs.org/faa-owner/LOGISTIC%20AIR%20INC) - Location: [Fernley, NV](https://openairdocs.org/faa-place/NV/Fernley) - Owner type: Corporation - Owner's area on the map: 39.6708° N, 119.0064° W: Placed by OpenAirDocs at the center of ZIP code 89408, within about 12 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N941AX - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=941AX - Page: https://openairdocs.org/deregistered/N941AX-2016-03-31 From the FAA registry file of October 28, 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 (101, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ABXA060096](https://openairdocs.org/sdr/ABXA060096), Feb 16, 2006: DOUBLER. CRACKED. RIGHT CLEARVIEW WINDOW STEEL SHIM WAS CRACKED AT RIVET. REMOVED NOTED SHIM DOUBLER AND INSTALLED NEW DOUBLER IAW DC9 DRAWING 5754088. - [SDR ABXA060095](https://openairdocs.org/sdr/ABXA060095), Feb 16, 2006: DOUBLER. CRACKED. LEFT CLEARVIEW WINDOW STEEL SHIM WAS CRACKED AT TWO RIVETS. REMOVED AND REPLACED DOUBLER ON LEFT CLEARVIEW UPPER AFT CORNER IAW DC9 SRM 51-30-2 AND 51-30-1. - [SDR ABXA060093](https://openairdocs.org/sdr/ABXA060093), Feb 14, 2006: FRAME. CRACKED. RIGHT FORWARD MAIN FRAME WAS CRACKED BEYOND LIMITS OF REPAIR. REMOVED AND REPLACED MAIN FRAME ON JOB CARD EA 53400322-001-2. - [SDR ABXA060094](https://openairdocs.org/sdr/ABXA060094), Feb 14, 2006: DOOR. CRACKED. DOUBLER AT RIGHT UPPER AFT, AFT PRESSURE BULKHEAD DOOR CORNER HAD A .875 INCH RADIAL CRACK. REPAIRED AREA IAW REA D953-53267MR. - [SDR ABXA060092](https://openairdocs.org/sdr/ABXA060092), Feb 13, 2006: FITTING. CRACKED. FITTING CRACKED FORWARD OF INBOARD DOOR ACTUATOR. REMOVED AND REPLACED FITTING IAW DC9 SRM 51-30-5. - [SDR ABXA040169](https://openairdocs.org/sdr/ABXA040169), Apr 28, 2004: FITTING. CRACKED. LEFT FLAP HAD CRACKED FITTING AT SPLICE BETWEEN NR 4 AND 5 REMOVEABLE TRAILING EDGE SEGMENTS. REPLACED 2 EACH NEW FITTINGS IAW DC-9 SRM 51-30-2 AND 51-30-1. P/N - [SDR ABXA040168](https://openairdocs.org/sdr/ABXA040168), Apr 27, 2004: PANEL. CRACKED. LT AND RT ANGLES INSIDE WRAP PANEL FORWARD OF RAM AIR SCOOP WERE CRACKED. REPLACED ANGLES IAW DC-9 SRM 51-30-2 AND 51-30-5. P/N: 5912188-49 AND -50. - [SDR ABXA040167](https://openairdocs.org/sdr/ABXA040167), Apr 26, 2004: DOOR FRAME. CRACKED. AFT PRESSURE BULKHEAD DOOR JAMB LEFT UPPER STOP FITTING CRACKED ON HORIZONTAL LEG. REPLACED FITTING IAW DC-9 SRM 51-30-2. - [SDR ABXA040166](https://openairdocs.org/sdr/ABXA040166), Apr 26, 2004: LONGERON. CRACKED. LONGERON 29 LT CRACKED AT STA. 588. REPAIRED LONGERON 29 LT IAW DC-9 SRM 53-02 AND REA D953-49676MR. - [SDR ABXA040165](https://openairdocs.org/sdr/ABXA040165), Apr 26, 2004: LONGERON. CRACKED. LONGERON 30 CRACKED, STA. 588. REPAIRED LONGERON 30 IAW REA D953-49676MR. REPAIRED FRAME AT FS 579 IAW DC-9 SRM 53-03. - [SDR ABXA040164](https://openairdocs.org/sdr/ABXA040164), Apr 23, 2004: SKIN. CORRODED. LEFT ELEVATOR LOWER SKIN WAS BULGED AND CORRODED AROUND FASTENERS AND DOUBLER. REPAIRED ELEVATOR IAW DC-9 SRM. - [SDR ABXA040163](https://openairdocs.org/sdr/ABXA040163), Apr 23, 2004: DOOR FRAME. CRACKED. ANGLE CRACKED ON FORWARD SIDE OF LEFT FORWARD OVERWING EXIT DOOR JAMB AT FS 617, LONGERON 15 LT. REPLACED ANGLE IAW DC-9 SRM 51-30-2. - [SDR ABXA040162](https://openairdocs.org/sdr/ABXA040162), Apr 22, 2004: PANEL. CORRODED. LEFT FLAP LOWER OUTBOARD SURFACE HAD NUMEROUS PLACES WITH SURFACE CORROSION AND EVIDENCE OF INNER CORROSION. SKIN BULGED AROUND RIVET HEADS. REPAIRED TRAILING E - [SDR ABXA030190](https://openairdocs.org/sdr/ABXA030190), Jun 9, 2003: SPACER. WORN. GEAR DOOR OPEN LIGHT AND LEFT GEAR UNSAFE LIGHT ILLUMINATED AFTER TAKEOFF. FOUND LEFT MAIN DOOR LATCH SWITCH ACTUATOR BINDING. REMOVED AND REPLACED SPACER, REIN - [SDR ABXA020224](https://openairdocs.org/sdr/ABXA020224), Sep 30, 2002: ATTACH ANGLE. CORRODED. FORWARD CARGO DOOR AFT HINGE FORWARD ATTACH ANGLE ON HINGE HAD CORROSION. REPLACED ATTACH ANGLE IAW DC-9 SRM. - [SDR ABXA020222](https://openairdocs.org/sdr/ABXA020222), Sep 16, 2002: ATTACH ANGLE. CRACKED. PYLON LOWER ATTACH ANGLE FORWARD END WAS CRACKED. REPAIRED PYLON LOWER ATTACH ANGLE FORWARD END IAW DC-9 SRM 54-04 AND SSRM DWG #K07439. - [SDR ABXA020223](https://openairdocs.org/sdr/ABXA020223), Sep 16, 2002: LONGERON. CRACKED. LONGERON 4 LEFT, CRACKED AT F.S. 200. REPLACED LONGERON IAW DC-9 SRM. - [SDR ABXA010582](https://openairdocs.org/sdr/ABXA010582), Nov 9, 2001: TERMINAL. DIRTY. EMERGENCY LIGHTS INOPERATIVE. CLEANED TERMINALS ON BATTERIES IN EMERGENCY BATTERY PACK AS REQUIRED. OPS CHECKED GOOD IAW DC-9 MM. - [SDR ABXA010497](https://openairdocs.org/sdr/ABXA010497), Sep 20, 2001: SWITCH. DEFECTIVE. A NOSE LANDING GEAR UNSAFE LIGHT ILLUMINATED IN FLIGHT. MAINTENANCE INSPECTED AND ADJUSTED THE NOSE LANDING GEAR DOWN LOCK SENSOR AND REPLACED THE LEFT FORWARD - [SDR ABXA010081](https://openairdocs.org/sdr/ABXA010081), Mar 7, 2001: SPOILER. CRACKED. THE RIGHT WING OUTBOARD SPOILER HAD A LARGE AREA THAT WAS CORRODED. THE SPOILER WAS ALSO FOUND TO BE CRACKED. MAINTENANCE INSPECTED AND REPLACED THE SPOILER IAW - [SDR ABXA010082](https://openairdocs.org/sdr/ABXA010082), Mar 7, 2001: PAN. CRACKED. FORWARD LOWER CARGO DOOR PAN WAS CRACKED AT THE NR 3, 4 AND 10 DOOR STOPS. MAINTENANCE INSPECTED AND REPLACED THE FORWARD CARGO DOOR IAW DC-9 MM 52-31-00. - [SDR ABXA010083](https://openairdocs.org/sdr/ABXA010083), Mar 7, 2001: WEB. CORRODED. CORROSION WAS FOUND AT FUSELAGE STATION 1121 ON FWD SIDE OF WEB, JUST OUTBOARD AND BELOW PULLY BRACKET. MAINTENANCE INSPECTED AND REPAIRED THE CORRODED AREA IAW - [SDR ABXA010084](https://openairdocs.org/sdr/ABXA010084), Mar 7, 2001: WEB. CRACKED. WEB AT FS 200 STRINGER 8L WAS CRACKED AND MISSING A SECTION OF MATERIAL. MAINTENANCE INSPECTED AND REPLACED THE WEB. - [SDR ABXA010085](https://openairdocs.org/sdr/ABXA010085), Mar 7, 2001: FLOORBEAM. CRACKED. FLOORBEAM UPPER ANGLE AT FUSELAGE STATION 996 HAD A 4 INCH CRACK. MAINTENANCE INSPECTED AND REPAIRED THE AREA IAW ABX REA D953-40085. - [SDR ABXA010086](https://openairdocs.org/sdr/ABXA010086), Mar 7, 2001: SKIN. CORRODED. CORROSION WAS FOUND BENEATH LEFT SIDE OF FUSELAGE STATIC PORT FS 446 AND 465. MAINTENANCE INSPECTED AND REPAIRED THE AREA IAW DC-9 SRM 53-04. - [SDR ABXA9900581](https://openairdocs.org/sdr/ABXA9900581), Jul 20, 1999: LATCH. STUCK. COCKPIT DOOR LATCH WAS STUCK IN LOCKED POSITION. DISASSEMBLED AND REALIGNED THE DOOR LATCH ASSEMBLY. - [SDR ABXA990559](https://openairdocs.org/sdr/ABXA990559), Jun 30, 1999: TAB. DELAMINATED. DURING C-CHECK, FOUND RUDDER TRIM TAB DELAMINATED. REPLACED RUDDER TRIM TAB IAW DC9 MM 27-20-2. - [SDR ABXA9900558](https://openairdocs.org/sdr/ABXA9900558), Jun 24, 1999: PANEL. CORRODED. DURING C-CHECK, FOUND LEFT WING UPPER TRAILING EDGE PANEL AT STATION XRS 111.500. REPLACED PANEL IAW DC9 SRM 51-30-1 AND 51-10-4. - [SDR ABXA9900524](https://openairdocs.org/sdr/ABXA9900524), Jun 22, 1999: PAN. CRACKED. DURING C-CHECK, FOUND SERVICE DOOR PAN CRACKED. REPAIRED IAW DC9 SRM 52-03-00 AND 51-30-1. - [SDR ABXA9900523](https://openairdocs.org/sdr/ABXA9900523), Jun 22, 1999: LONGERON. CRACKED. DURING C-CHECK, FOUND LONGERON 13 RIGHT CRACKED AT STATION 965. REPLACED LONGERON SECTION IAW DC9 SRM 53-02-0. - [SDR ABXA9900526](https://openairdocs.org/sdr/ABXA9900526), Jun 21, 1999: PANEL. DELAMINATED. DURING C-CHECK, FOUND RIGHT WING TRAILING EDGE UPPER HONEYCOMB PANEL DELAMINATED. REPLACED PANEL IAW DC9 SRM 51-30-1. - [SDR ABXA9900525](https://openairdocs.org/sdr/ABXA9900525), Jun 21, 1999: FRAME. CRACKED. DURING C-CHECK, FOUND MAIN FRAME CRACKED IN UPPER CARGO COMPARTMENT. REPAIRED IAW DC9 S/B 53-131 AND DWG 5935650-503. - [SDR ABXA9800818](https://openairdocs.org/sdr/ABXA9800818), Sep 8, 1998: LATCH. BINDING. COCKPIT DOOR LATCHING MECHANISM BINDING AND STICKS IN CLOSED POSITION. DISASSEMBLED, CLEANED, LUBRICATED AND REASSEMBLED LATCH ASSEMBLY. OPS CHECKED GOOD. - [SDR ABXA9800707](https://openairdocs.org/sdr/ABXA9800707), Aug 1, 1998: POWER SUPPLY. INOPERATIVE. EMERGENCY LIGHTS WERE EXTREMELY DIM. REPLACED EMERGENCY LIGHT POWER SUPPLY. - [SDR ABXA9800632](https://openairdocs.org/sdr/ABXA9800632), Jul 16, 1998: BATTERY. DISCHARGED. EMERGENCY EXIT LIGHTS WERE FLICKERING AND VERY DIM. REPLACED EMERGENCY LIGHT BATTERIES. - [SDR ABXA9800369](https://openairdocs.org/sdr/ABXA9800369), Apr 21, 1998: BATTERY. DISCHARGED. EMERGENCY EXIT LIGHTS WERE DIM. REPLACED EMERGENCY LIGHT BATTERIES. - [SDR ABXA9800254](https://openairdocs.org/sdr/ABXA9800254), Mar 23, 1998: BATTERY. DISCHARGED. COCKPIT EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED COCKPIT EMERGENCY LIGHT BATTERIES, OPS CHECKED GOOD. - [SDR ABXA9701836](https://openairdocs.org/sdr/ABXA9701836), Nov 14, 1997: FRAME. CRACKED. DURING C-CHECK, FOUND FRAME AT STA 965 LOWER FLANGE CRACKED AT FASTENER HOLE ABOVE LONGERON 30. REPAIRED FRAME IAW DC9 SRM 53-03. - [SDR ABXA9701822](https://openairdocs.org/sdr/ABXA9701822), Nov 13, 1997: DOUBLER. CORRODED. DURING C-CHECK, FOUND NR 1 DME ANTENNA INTERNAL DOUBLER EXFOLIATED. FABRICATED INTERNAL DOUBLER (P/N 5911408-39) AND REPAIR DOUBLER (P/N J060258-3) AND INSTALLE - [SDR ABXA9701821](https://openairdocs.org/sdr/ABXA9701821), Nov 13, 1997: FLOORBEAM. CRACKED. DURING C-CHECK, FOUND FLOORBEAM CRACKED AT PULLEY BRACKET ATTACH HOLE, STA 351, LBL 6. REPAIRED FLOORBEAM IAW DC9 SRM 53-05. - [SDR ABXA9701820](https://openairdocs.org/sdr/ABXA9701820), Nov 13, 1997: JAMB. CORRODED. DURING C-CHECK, FOUND FWD LOWER CARGO COMPARTMENT DOOR JAMB WEB HEAVILY CORRODED IN SEVERAL AREAS ON THE UPPER SURFACE BETWEEN STA 370 AND 427. REPLACED THE DOO - [SDR ABXA9701819](https://openairdocs.org/sdr/ABXA9701819), Nov 13, 1997: FRAME. CRACKED. DURING C-CHECK, FOUND FUSELAGE FRAME CRACKED AT STA 980 AND LONGERON 16L. REPLACED FRAME AND SHEAR TIE IAW DC9 SRM 51-30-5 AND 51-30-2. - [SDR ABXA9701818](https://openairdocs.org/sdr/ABXA9701818), Nov 13, 1997: LONGERON. CORRODED. DURING C-CHECK, FOUND LONGERON 29L CORRODED BETWEEN STA 870 AND 919. REPAIRED LONGERON IAW DC9 SRM 51-10-3 AND ABX REA D953-21614-MR. - [SDR ABXA9701817](https://openairdocs.org/sdr/ABXA9701817), Nov 13, 1997: SKIN. CORRODED. DURING C-CHECK, FOUND CORROSION UNDER THE WATER DEFLECTOR FOR THE APU AT STA 990. REPAIRED SKIN IAW ABX REA D953-21621-MR. - [SDR ABXA9701816](https://openairdocs.org/sdr/ABXA9701816), Nov 13, 1997: LONGERON. CRACKED. DURING C-CHECK, FOUND LONGERON 30 CRACKED ON BOTH HORIZONTAL LEGS APPROX 5 INCHES LONG AT STA 418. REPLACED LONGERON IAW DC9 SRM 53-02, FIG 14. - [SDR ABXA9701815](https://openairdocs.org/sdr/ABXA9701815), Nov 13, 1997: BULKHEAD FITTING. CORRODED. DURING C-CHECK, FOUND THE CENTER FITTING AT LONGERON 30 THAT ATTACHES TO THE AFT PRESSURE BULKHEAD T-CAP HEAVILY CORRODED. REPLACED FITTING IAW ABX NEA 53120035 - [SDR ABXA9701814](https://openairdocs.org/sdr/ABXA9701814), Nov 13, 1997: INTERCOSTAL. CRACKED. DURING C-CHECK, FOUND INTERCOSTAL BETWEEN FS 917 TO 937, AND BL 0 CRACKED. REPLACED THE INTERCOSTAL IAW DC9 SRM 51-30-2. - [SDR ABXA9701813](https://openairdocs.org/sdr/ABXA9701813), Nov 13, 1997: BULKHEAD WEB. CORRODED. DURING C-CHECK, FOUND CORROSION ON THE AFT PRESSURE BULKHEAD WEB FWD SIDE, LONGERON 23R TO 23L. REPAIRED AFT PRESSURE BULKHEAD WEB IAW DC9 SRM 53-03. - [SDR ABXA9701812](https://openairdocs.org/sdr/ABXA9701812), Nov 13, 1997: BULKHEAD RADIAL. CRACKED. DURING C-CHECK, FOUND AFT PRESS BULKHEAD RADIAL AFT SIDE AT FS 996, LONGERON 25L IS CRACKED IN THE RADIUS. REPAIRED RADIAL IAW DC9 ABX SSRM DRAWING K05159. - [SDR ABXA9701811](https://openairdocs.org/sdr/ABXA9701811), Nov 13, 1997: LONGERON. CRACKED. DURING C-CHECK, FOUND LONGERON 30 CORRODED AT STA 965 TO 980. REPLACED LONGERON IAW DC9 SRM 51-30-2 AND 51-30-5. All 101: https://openairdocs.org/deregistered/N941AX-2016-03-31/reports.md --- 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.