# N982AX: 1968 Mcdonnell Douglas DC-9-32, registration cancelled 2018-03-08

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 8, 2018
- Status when cancelled: Registration expired, pending cancellation
- Airframe: [Mcdonnell Douglas DC-9-32](https://openairdocs.org/model/mcdonnell-douglas-dc-9-32) (registry code 302206C)
- 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: 47317
- Year built: 1968
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: April 11, 1991
- Certificate issued: December 10, 2008
- Last registry action: March 19, 2013
- Mode S code: ADB2A8
- 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/N982AX
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=982AX
- Page: https://openairdocs.org/deregistered/N982AX-2018-03-08

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 Mcdonnell Douglas DC-9-32: https://openairdocs.org/model/mcdonnell-douglas-dc-9-32.md

## Service difficulty reports (131, newest 50)

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

- [SDR ABXA070076](https://openairdocs.org/sdr/ABXA070076), Mar 20, 2007: UNKNOWN. ODOR. AIRCRAFT HAS STRONG ODOR OF FUEL OR SOLVENT IN COCKPIT AND CARGO AREA. NO FUEL LEAK OR ODOR NOTED IAW DC9 MM 28-00-00.
- [SDR ABXA050164](https://openairdocs.org/sdr/ABXA050164), Jun 17, 2005: DOOR FRAME. CRACKED. LEFT AFT UPPER DOOR JAMB CRACKED, EMERGENCY EXIT, IN 2 PLACES. REPAIRED LEFT AFT UPPER DOOR JAMB IAW DC-9 SRM 53-05.
- [SDR ABXA050163](https://openairdocs.org/sdr/ABXA050163), Jun 16, 2005: THRESHOLD. CORRODED. SERVICE DOOR THRESHOLD SKIN BULGING AT STA 176, RIGHT BUTT LINE 58. REPAIRED AREA IAW DC-9 SRM 51-10-2.
- [SDR ABXA050162](https://openairdocs.org/sdr/ABXA050162), Jun 15, 2005: FRAME. CRACKED. SHEAR TIE CRACKED IN RADIUS FRAME STA 813 BETWEEN LONGERON 29 LEFT AND 30. REPAIRED SHEAR TIE IAW DC-9 SRM 53-03 AND DWG SR09530212.
- [SDR ABXA050161](https://openairdocs.org/sdr/ABXA050161), Jun 14, 2005: FLOORBEAM. CORRODED. LOWER LEG OF FLOORBEAM WAS CORRODED ON UPPER AND LOWER SURFACE AT STA 313, BUTTLINE 38 RIGHT. REPAIRED FLOORBEAM IAW DC-9 SRM 53.
- [SDR ABXA050159](https://openairdocs.org/sdr/ABXA050159), Jun 14, 2005: RETAINER. CRACKED. STA 756, LONGERON 15 RIGHT, HAD CRACK AT WINDOW RETAINER. REMOVED AND REPLACED DAMAGED CLIP. FABRICATED AND INSTALLED NEW CLIP IAW DACO DWG 3914137 AND DC-9 SRM
- [SDR ABXA050160](https://openairdocs.org/sdr/ABXA050160), Jun 14, 2005: RETAINER. CRACKED. STA 598, LONGERON 10 RT, HAD CRACK AT WINDOW RETAINER. REPAIRED WINDOW RETAINER AT FS 598, LONGERON 10 RIGHT IAW DC-9 SSRM DWG K07226.
- [SDR ABXA040385](https://openairdocs.org/sdr/ABXA040385), Nov 26, 2004: WARNING LIGHT. ILLUMINATED. NOSE LANDING GEAR LIGHT WAS NOT ILLUMINATED ON GEAR EXTENSION. RECYCLED GEAR, LIGHT CAME ON. INSPECTED NOSE LANDING GEAR WIRING FOR CONTINUITY & PIN ENGAGEMENT 
- [SDR ABXA030446](https://openairdocs.org/sdr/ABXA030446), Nov 21, 2003: WIRE. BURNED. WIRE BURNED ON PHASE C, GROUND SERVICE BUS POWER PANEL, WIRE HV X22810C. REMOVED BURNED AREA OF WIRE AND REPLACED WIRE END CONNECTOR. INSTALLED WIRE TO GROUND S
- [SDR ABXA030414](https://openairdocs.org/sdr/ABXA030414), Oct 15, 2003: FRAME. CRACKED. FRAME CRACKED AT FS 1076 AND LONGERON 19 LEFT. REPAIRED FRAME AT FS 1076 IAW DC-9 SRM 53-03.
- [SDR ABXA030413](https://openairdocs.org/sdr/ABXA030413), Oct 15, 2003: ANGLE. CRACKED. CRACK IN FRAME ATTACH ANGLE AT STA 1038 ABOVE LONGERON 18 LT. REPAIRED ANGLE IAW DC-9 SSRM DWG K05159.
- [SDR ABXA030408](https://openairdocs.org/sdr/ABXA030408), Oct 14, 2003: RIB. CRACKED. LEFT SIDE OF REMOVABLE LEADING EDGE HAD A CRACK ON A RIB TOWARD THE TOP END OF THE PANEL. REPAIRED AREA IAW DC-9 SSRM DWG K05159.
- [SDR ABXA030409](https://openairdocs.org/sdr/ABXA030409), Oct 14, 2003: RIB. CRACKED. LEFT SIDE OF REMOVABLE LEADING EDGE HAD A CRACK ON A RIB IN THE MIDDLE OF THE PANEL. REPAIRED AREA IAW DC-9 SSRM DWG K05159.
- [SDR ABXA030412](https://openairdocs.org/sdr/ABXA030412), Oct 14, 2003: RIB. CRACKED. END OF LEADING EDGE RIB RIGHT WING CRACKED AT STA 353. REPAIRED DAMAGED RIB IAW DC-9 SRM 57-06.
- [SDR ABXA030411](https://openairdocs.org/sdr/ABXA030411), Oct 14, 2003: RIB. CRACKED. RIGHT SIDE OF REMOVABLE LEADING EDGE HAD A CRACK ON RIB IN THE MIDDLE OF THE PANEL. REPAIRED AREA IAW DC-9 SSRM DWG K05159.
- [SDR ABXA030410](https://openairdocs.org/sdr/ABXA030410), Oct 14, 2003: RIB. CRACKED. RIGHT SIDE OF REMOVABLE LEADING EDGE HAD A CRACK ON A RIB AT THE BOTTOM OF THE PANEL. REPAIRED AREA IAW DC-9 SSRM DWG K05159.
- [SDR ABXA030151](https://openairdocs.org/sdr/ABXA030151), May 20, 2003: PANEL. CRACKED. WHILE PERFORMING ROUTINE LINE MAINTENANCE, A FUEL LEAK WAS DISCOVERED AT THE LT WING FUEL PANEL 1307. FURTHER INSPECTION REVEALED A CRACK ON THE FUEL PANEL FLAN
- [SDR ABXA020076](https://openairdocs.org/sdr/ABXA020076), Aug 12, 2002: DUCT. DISCONNECTED. AT FL 350, CABIN ALTITUDE INCREASED TO 9,500 ALONG WITH THE RIGHT GENERATOR TRIPPING OFF LINE. RESET GENERATOR. PERFORMED DESCENT TO 14,000 CABIN ALTITUDE WAS R
- [SDR ABXA010782](https://openairdocs.org/sdr/ABXA010782), Mar 20, 2002: WIRE. BROKEN. ON LANDING AT BDL, NO GREEN GEAR LIGHT. RECYCLED LANDING GEAR, THE GREEN LIGHT ILLUMINATED. REPAIRED BROKEN WIRES TO THE NOSE GEAR UP LIMIT SWITCH CONNECTOR (P1
- [SDR ABXA010755](https://openairdocs.org/sdr/ABXA010755), Mar 1, 2002: SWITCH. DEFECTIVE. ON INITIAL GEAR EXTENSION AT ILN, NOSE GEAR DID NOT INDICATE DOWN/LOCKED. SUBSEQUENT RETRACTION/EXTENSION CYCLE YIELDED NORMAL INDICATION. REPLACED THE NOSE GEA
- [SDR ABXA010754](https://openairdocs.org/sdr/ABXA010754), Feb 28, 2002: WARNING SYSTEM. MALFUNCTIONED. ON INITIAL GEAR EXTENSION AT ILN, NOSE LANDING GEAR DID NOT INDICATE DOWN/LOCKED. SUBSEQUENTIAL RETRACT/EXTENSION CYCLE YIELDED NORMAL INDICATION. PERFORMED FUN
- [SDR ABXA010749](https://openairdocs.org/sdr/ABXA010749), Feb 19, 2002: RIB. CRACKED. RIGHT WING LEADING EDGE RIB (JUST INBOARD OF #2 SLAT TRACK) CRACKED AT THE LOWER ATTACH FASTENER. REPAIRED RIB IAW DC-9 REA D957-43342.
- [SDR ABXA010748](https://openairdocs.org/sdr/ABXA010748), Feb 13, 2002: WEB. CRACKED. CUSP WEB CRACKED (AFT WEB) AT FS 236, LONGERON 18 LEFT. REPAIRED AREA IAW DC-9 SRM 53-01.
- [SDR ABXA010746](https://openairdocs.org/sdr/ABXA010746), Feb 13, 2002: DOOR FRAME. CRACKED. CRACK IN FORWARD ACCESSORY COMPARTMENT DOOR JAMB, APPROXIMATELY 1.5 INCH LONG, LOCATED ALONG THE UPPER AFT SIDE OF JAMB. REPAIRED DOOR JAMB IAW DC-9 SRM 51-10-3
- [SDR ABXA010745](https://openairdocs.org/sdr/ABXA010745), Feb 13, 2002: SHEAR TIE. CORRODED. HEAVY CORROSION ON FRAME SPLICE ANGLE ON AFT SIDE OF FRAME AT STATION 943, ABOVE LONGERON 29 LEFT. REPLACED SPLICE ANGLE IAW DC-9 SRM 51-30-5.
- [SDR ABXA010744](https://openairdocs.org/sdr/ABXA010744), Feb 13, 2002: FRAME. CORRODED. HEAVY CORROSION ON UPPER CARGO FLOOR FRAME AT STATION 929 ABOVE TWO FASTENERS THAT HOLD THE AFT LOWER CARGO DOOR HOLD OPEN HOOK. REMOVED CORROSION AND INSTALLED
- [SDR ABXA010747](https://openairdocs.org/sdr/ABXA010747), Feb 13, 2002: FRAME. CORRODED. FRAME WAS CORRODED AT STATION 332, FROM LONGERON 29 LEFT TO LONGERON 29 RIGHT. REPAIRED FRAME IAW DC-9 SRM.
- [SDR ABXA010743](https://openairdocs.org/sdr/ABXA010743), Feb 13, 2002: WEB. CRACKED. CUSP WEB CRACKED BETWEEN FS 945 AND 965, LEFT SIDE. REPAIRED CRACKED AREA IAW DC-9 SRM 53-01.
- [SDR ABXA010742](https://openairdocs.org/sdr/ABXA010742), Feb 13, 2002: WEB. CRACKED. FRAME FOOT, WEB CRACKED AT FS 996, LONGERON 18 LEFT. REPLACED WEB IAW DC-9 SRM 53-11-3 AND 51-30-5.
- [SDR ABXA010750](https://openairdocs.org/sdr/ABXA010750), Feb 12, 2002: FITTING. CRACKED. LONGERON 29 RIGHT HAD CRACKED END FITTING AFT OF F.S. 604 "P" DOME. REPLACED END CAP IAW DC-9 SRM 51-30-5.
- [SDR ABXA010741](https://openairdocs.org/sdr/ABXA010741), Feb 12, 2002: INTERCOSTAL. CRACKED. CRACK IN INTERCOSTAL LONGERON 27 LEFT, STATION 761. REPAIRED AREA IAW DC-9 DOUGLAS DWG 9915574.
- [SDR ABXA010740](https://openairdocs.org/sdr/ABXA010740), Feb 12, 2002: FITTING. CRACKED. LONGERON 28 RIGHT HAD CRACKED END FITTING AFT OF F.S. 604 "P" DOME. REPLACED END CAP IAW DC-9 SRM 51-30-5.
- [SDR ABXA010536](https://openairdocs.org/sdr/ABXA010536), Oct 15, 2001: ENGINE. FAILED. CLIMBING THROUGH FL 190, CREW HEARD A LOUD POP AND NOTICED THE LEFT ENGINE HAD DECREASED TO 1.35 EPR AND THE EGT HAD INCREASED TO 550. OPERATED ENGINE AT REDUCE
- [SDR ABXA010456](https://openairdocs.org/sdr/ABXA010456), Aug 29, 2001: LIGHT. INOPERATIVE. CREW REPORTED ON APPROACH DOOR OPEN LIGHT WOULD NOT PRESS TO TEST. DID FLY BY, TOWER REPORTED DOORS CLOSED. RELAMPED GEAR DOOR OPEN LIGHT PRESS TO TEST INDICATO
- [SDR ABXA0100013](https://openairdocs.org/sdr/ABXA0100013), Jan 16, 2001: BATTERY. DISCHARGED. EMERGENCY LIGHTS WOULD NOT OPERATE WHEN SWITCH WAS SELECTED ON. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT BATTERY IAW DC-9 MM 33-52-02.
- [SDR ABXA0100012](https://openairdocs.org/sdr/ABXA0100012), Jan 16, 2001: CONTACTOR. DIRTY. EMERGENCY LIGHTS WOULD NOT TEST DURING PRE-DEPARTURE CHECK. MAINTENANCE INSPECTED AND CLEANED THE EMERGENCY LIGHT BATTERY CONTACTS AND RESEATED BATTERIES IN THE
- [SDR ABXA000328](https://openairdocs.org/sdr/ABXA000328), Jun 26, 2000: ANGLE. CRACKED. DURING C-CHECK, FOUND INTERCOSTAL TO FLOORBEAM ATTACH ANGLE CRACKED AT STATION 617, LEFT BL 44. REPLACED ANGLE IAW DC9 SRM 51-30-5.
- [SDR ABXA000327](https://openairdocs.org/sdr/ABXA000327), Jun 26, 2000: PANEL. CRACKED. DURING C-CHECK, FOUND RIGHT TRAP PANEL CRACKED AT TOP OUTBOARD FLANGE. REPLACED RIGHT TRAP PANEL IAW DC9 SRM 51-30-5, AND DC9 S/B 53-182.
- [SDR ABXA000331](https://openairdocs.org/sdr/ABXA000331), Jun 22, 2000: INTERCOSTAL. CRACKED. DURING C-CHECK, FOUND THE FORWARD LOWER CARGO INTERCOSTAL WEB CRACKED. REPLACED FORWARD CARGO DOOR WEB IAW DC9 SRM 51-30-2.
- [SDR ABXA000309](https://openairdocs.org/sdr/ABXA000309), Jun 22, 2000: SPLICE. CRACKED. DURING C-CHECK FOUND FLOOR SUPPORT TO INTERCOSTAL STRAP CRACKED AT STATION 737 OUTBOARD OF RIGHT BL 22. INSTALLED SPLICE IAW DC9 SRM 51-30-02.
- [SDR ABXA000330](https://openairdocs.org/sdr/ABXA000330), Jun 14, 2000: PAN. CRACKED. DURING C-CHECK, FOUND FORWARD LOWER CARGO DOOR OUTER PAN CRACKED. REPAIRED IAW DC9 SRM 52-03.
- [SDR ABXA000329](https://openairdocs.org/sdr/ABXA000329), Jun 14, 2000: INTERCOSTAL. CRACKED. DURING C-CHECK, FOUND FORWARD LOWER CARGO DOOR INTERCOSTAL CRACKED. REPLACED INTERCOSTAL IAW DC9 SRM 51-30-2.
- [SDR ABXA000326](https://openairdocs.org/sdr/ABXA000326), Jun 14, 2000: ATTACH FITTING. CRACKED. DURING C-CHECK, FOUND CRACK AT UPPER ANTI-COLLISION LIGHT ATTACH PLATE. REPAIRED IAW ABX REA D953-37600MR.
- [SDR ABXA000073](https://openairdocs.org/sdr/ABXA000073), Jan 24, 2000: BATTERY. DISCHARGED. EMERGENCY LIGHTS WOULD NOT ILLUMINATE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES.
- [SDR ABXA9900794](https://openairdocs.org/sdr/ABXA9900794), Nov 16, 1999: CIRCUIT BREAKER. FAILED. EMERGENCY LIGHTS WOULD NOT TEST. REPLACED EMERGENCY LIGHTING 5 AMP CIRCUIT BREAKER IAW DC9 MM 33-53, OPS CHECKED GOOD.
- [SDR ABXA9801137](https://openairdocs.org/sdr/ABXA9801137), Dec 1, 1998: WEB. CORRODED. DURING C-CHECK, FOUND PRESSURE DECK WEB CORRODED BEYOND LIMITS AT STATION 756 TO 752, RBL 15. REPAIRED PRESSURE DECK WEB IAW DC9 SRM 53-04.
- [SDR ABXA9801140](https://openairdocs.org/sdr/ABXA9801140), Nov 30, 1998: BRACKET. CORRODED. DURING C-CHECK, FOUND LEFT FLAP INBOARD AFT HINGE BRACKET CORRODED AT PIVOT POINT. REPLACED AFT HINGE BRACKET IAW DC9 SRM.
- [SDR ABXA9801139](https://openairdocs.org/sdr/ABXA9801139), Nov 30, 1998: FRAME. CRACKED. DURING C-CHECK, FOUND FRAME 1076 CRACKED AT LONGERONS 2L AND 2R. REPAIRED FRAME IAW DC9 SRM 53-03.
- [SDR ABXA9801138](https://openairdocs.org/sdr/ABXA9801138), Nov 30, 1998: BLKHD STIFFENER. CRACKED. DURING C-CHECK, FOUND STIFFENER CRACKED AT AFT SIDE OF BULKHEAD 1087, BL 0.0. REPLACED STIFFENER IAW DC9 SRM 51-30-5 AND 51-10-4.
- [SDR ABXA9801176](https://openairdocs.org/sdr/ABXA9801176), Nov 23, 1998: FRAME. CRACKED. DURING C-CHECK, FOUND FRAME AT STATION 980 CRACKED BETWEEN LONGERONS 14R AND 17R. REPAIRED FRAME IAW DC9 SRM 53-03.

All 131: https://openairdocs.org/deregistered/N982AX-2018-03-08/reports.md

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