# N925AX: 1965 Mcdonnell Douglas DC-9-14, registration cancelled 2007-04-25

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: April 25, 2007
- Status when cancelled: Triennial form not returned
- Airframe: [Mcdonnell Douglas DC-9-14](https://openairdocs.org/model/mcdonnell-douglas-dc-9-14) (registry code 302203F)
- Engine: [Pratt & Whitney JT8D series](https://openairdocs.org/engine/pratt-whitney-jt8d-series) (registry code 52053)
- Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (OpenAirDocs)
- Serial number: 45728
- Year built: 1965
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: May 16, 1991
- Certificate issued: August 10, 1983
- Last registry action: January 16, 2007
- Mode S code: ACD0D3
- Owner when cancelled: [Abx Air Inc](https://openairdocs.org/faa-owner/ABX%20AIR%20INC)
- Location: [Wilmington, OH](https://openairdocs.org/faa-place/OH/Wilmington)
- Owner type: Corporation
- Owner's area on the map: 39.4607° N, 83.8443° W: Placed by OpenAirDocs at the center of ZIP code 45177, within about 7 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N925AX
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=925AX
- Page: https://openairdocs.org/deregistered/N925AX-2007-04-25

From the FAA registry file of November 5, 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-9-14: https://openairdocs.org/model/mcdonnell-douglas-dc-9-14.md

## Service difficulty reports (82, newest 50)

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

- [SDR ABXA040302](https://openairdocs.org/sdr/ABXA040302), Aug 30, 2004: PAN. CORRODED. WHILE PERFORMING AN X-RAY OF THE FORWARD LOWER CARGO COMPARTMENT DOOR JAMB, FOUND THE LOWER DOOR JAMB PAN PRIOR SERVICE REWORK REPAIR CORRODED BEYOND LIMITS. RE
- [SDR ABXA040078](https://openairdocs.org/sdr/ABXA040078), Feb 18, 2004: BATTERY. DISCHARGED. OVERHEAD EMERGENCY LIGHTS IN COCKPIT STAYED ON AFTER POWER SHUT DOWN. REPLACED BATTERY POWER SUPPLY WITH SEVICEABLE UNIT. OPS CHECKED GOOD IAW DC-9 MM.
- [SDR ABXA040077](https://openairdocs.org/sdr/ABXA040077), Feb 17, 2004: BATTERY. DISCHARGED. OVERHEAD EMERGENCY LIGHTS IN COCKPIT STAYED ON AFTER POWER SHUT DOWN. RESEATED BATTERIES IN EMERGENCY LIGHT POWER SUPPLY. LIGHTS FUNCTIONED NORMALLY IAW DC-9 MM
- [SDR ABXA030443](https://openairdocs.org/sdr/ABXA030443), Oct 31, 2003: FLOOR SUPPORT. CRACKED. FLOOR SUPPORT STRAP, ATTACH ANGLE CRACKED, FS 768 AT LONGERON 27 RIGHT. REPLACED ANGLE IAW DC-9 SRM 51-30-5.
- [SDR ABXA030442](https://openairdocs.org/sdr/ABXA030442), Oct 31, 2003: FLOOR SUPPORT. CORRODED. STA 218 FLOOR SUPPORT WAS CORRODED ABOVE LONGERON 30. REPAIRED FRAME AT FS 218, LONGERON 30 IAW DC-9 SRM 53-03.
- [SDR ABXA030441](https://openairdocs.org/sdr/ABXA030441), Oct 30, 2003: SKIN. CORRODED. RIGHT WING UPPER SKIN CORRODED AND PULLED RIVETS JUST INBOARD OF SPOILER ACTUATOR. REPLACED SECTION OF STRINGER AND SPLICE IAW DC-9 SRM 51-70-5 AND 51-30-5.
- [SDR ABXA030440](https://openairdocs.org/sdr/ABXA030440), Oct 30, 2003: FITTING. CRACKED. AFT LOWER CARGO DOOR, TRAILING EDGE NR 5 BEAM END FITTING CRACKED. INSTALLED NEW FITTING IAW DC-9 SRM 51-30-5 AND 51-30-2.
- [SDR ABXA030081](https://openairdocs.org/sdr/ABXA030081), Feb 19, 2003: WIRE. BURNED. PRIMARY TRIM NR 1 CIRCUIT BREAKER TRIPPED. FOUND WIRES C104C10, C1203C10, C1202C10, C1202B10, C1203B10, C1204B10, C1213A10, C1213B10, C1211B10 BURNED. FOUND WIR
- [SDR ABXA020123](https://openairdocs.org/sdr/ABXA020123), Aug 23, 2002: LINK. CRACKED. NR 2 LOWER AFT LEFT THRUST REVERSER DRIVER LINK WAS CRACKED. REPLACED THE NR 2 LOWER LEFT DRIVE LINK IAW DC-9 MM 78-31-05-2-0001, NEA 7830001, TASK NEA 13435, A
- [SDR ABXA010776](https://openairdocs.org/sdr/ABXA010776), Mar 4, 2002: STIFFENER. CRACKED. OUTBOARD STATION 91.00, FRONT SPAR VERTICAL STIFFENER, UPPER PORTION WAS CRACKED. REPLACED STIFFENER IAW DC-9 SRM.
- [SDR ABXA010775](https://openairdocs.org/sdr/ABXA010775), Feb 28, 2002: SKIN. CRACKED. RIGHT MAIN LANDING GEAR DOOR INNER SKIN CRACKED JUST AFT OF THE FORWARD HINGE FITTING. REPAIRED CRACKED AREA IAW DC-9 SRM 52-01.
- [SDR ABXA010774](https://openairdocs.org/sdr/ABXA010774), Feb 27, 2002: FRAME. CRACKED. AUXILIARY SUPPORT FRAME CRACKED IN AFT ACCESSORY COMPARTMENT FLOOR SUPPORT, FORWARD OF MAIN FRAME AT STATION 908. REPLACED FRAME IAW DC-9 SRM DWG 505159 AND DC-
- [SDR ABXA010773](https://openairdocs.org/sdr/ABXA010773), Feb 27, 2002: FITTING. CRACKED. LEFT OVER WING EXIT DOOR PAN STIFFENER ANGLES ON OUTER PAN CRACKED 5 INCHES. REPLACED STOPS IAW DC-9 SRM 51-30-2 AND 51-30-5.
- [SDR ABXA010772](https://openairdocs.org/sdr/ABXA010772), Feb 26, 2002: ANGLE. CRACKED. OUTBOARD LOWER FASTENER HOLE ON ATTACH ANGLE CRACKED WHERE WING TO FUSELAGE FAIRING ATTACHES AT F.S. 585. REPLACED ANGLE IAW DC-9 SRM 51-30-1 AND DC-9 DWG 99155
- [SDR ABXA010771](https://openairdocs.org/sdr/ABXA010771), Feb 25, 2002: FINGER DOUBLER. DEBONDED. OUTBOARD REMOVABLE TRAILING EDGE LOWER SKIN FINGER DOUBLERS WERE DEBONDED. REPLACED UPPER/LOWER SKINS IAW REA D957-43379.
- [SDR ABXA010676](https://openairdocs.org/sdr/ABXA010676), Jan 16, 2002: CONTROL CABLE. LACK OF LUBE. FINAL APPROACH, AIRCRAFT IN A TRIMMED DESCENT ON GLIDESLOPE, FLAPS 30, N1-60 PERCENT ON BOTH ENGINES, SPEED 10 + OVER TARGET 139. WENT TO FLAP 40, AIRCRAFT ROLL
- [SDR ABXA000400](https://openairdocs.org/sdr/ABXA000400), Aug 24, 2000: INDICATOR. SHORTED. AFTER SELECTING LANDING GEAR DOWN, NOSE GEAR SAFE LIGHT DID NOT ILLUMINATE. NO RED GEARWARNING LIGHT. PERFORMED ABNORMAL PROCEDURES AND GO-AROUND. VISUALLY CHEC
- [SDR ABXA000349](https://openairdocs.org/sdr/ABXA000349), Jul 19, 2000: FLOORBEAM. CORRODED. FLOORBEAM WEB AT STATION 786 AND LBL 13.0 IS EXFOLIATED. REPAIRED IAW ABX REA D957-38011.
- [SDR ABXA000343](https://openairdocs.org/sdr/ABXA000343), Jul 12, 2000: STIFFENER. CRACKED. LEFT AND RIGHT RADIAL STIFFENERS NR 14 WERE CRACKED. REPLACED IAW DC9 SRM 51-30-5.
- [SDR ABXA000344](https://openairdocs.org/sdr/ABXA000344), Jul 11, 2000: LONGERON. CORRODED. LONGERONS 23 AND 24 LEFT WERE CORRODED AT STATIONS 817 - 823. REPAIRED LONGERONS 23 AND 24 LEFT IAW DC9 SRM 50-02.
- [SDR ABXA000342](https://openairdocs.org/sdr/ABXA000342), Jul 10, 2000: SHEAR TIE. CRACKED. EXTRUSION FORWARD OF AFT PRESSURE BULKHEAD T-CAP AT LONGERON 18 LEFT WAS CRACKED AT FLOOR LINE. REPLACED SHEAR TIE ANGLE IAW DC9 SRM 51-30-2.
- [SDR ABXA000341](https://openairdocs.org/sdr/ABXA000341), Jul 10, 2000: FLOOR SUPPORT. CRACKED. FLOOR SUPPORT WAS CRACKED AT CUSP LINE JUST FORWARD OF PRESSURE DOME ON RIGHT SIDE. REPAIRED IAW DC9 SRM.
- [SDR ABXA000340](https://openairdocs.org/sdr/ABXA000340), Jul 10, 2000: FRAME. CRACKED. FRAME OUTSIDE FLANGE CRACKED AT STATION 801 AND LONGERON 17 LEFT. REPLACED FRAME IAW DC9 SRM 52-03.
- [SDR ABXA000339](https://openairdocs.org/sdr/ABXA000339), Jul 7, 2000: FITTING. CRACKED. LONGERON FITTING CRACKED AT STATION 585 AND LONGERON 11 LEFT. REPLACED FITTING IAWDC9 SRM 51-30-5.
- [SDR ABXA000337](https://openairdocs.org/sdr/ABXA000337), Jul 7, 2000: PAN. CRACKED. FORWARD LOWER CARGO DOOR INBOARD SIDE OF PAN WAS CRACKED. INSTALLED DOUBLER IAW DC9 SRM 52-05.
- [SDR ABXA000334](https://openairdocs.org/sdr/ABXA000334), Jul 7, 2000: STIFFENER. CRACKED. REAR SPAR STIFFENER WAS CRACKED AT STATION XRS 313. REPLACED STIFFENER IAW DC9 SRM 51-30-5.
- [SDR ABXA000338](https://openairdocs.org/sdr/ABXA000338), Jul 6, 2000: LONGERON. CORRODED. LONGERON 30 HAD LEVEL 2 CORROSION AT STATION 642. REPLACED LONGERON IAW DC9 SRM 53-02.
- [SDR ABXA000336](https://openairdocs.org/sdr/ABXA000336), Jul 5, 2000: SKIN. DELAMINATED. RIGHT INBOARD SPOILER WAS DELAMINATED. REPLACED SPOILER IAW DC9 MM 27-62-01.
- [SDR ABXA000335](https://openairdocs.org/sdr/ABXA000335), Jul 5, 2000: HINGE. CRACKED. RIGHT FLAP HINGE CRACKED AT STATION 351. REPLACED FLAP HINGE.
- [SDR ABXA9900692](https://openairdocs.org/sdr/ABXA9900692), Sep 3, 1999: WINDOW. STUCK. CAPTAIN'S CLEAR VIEW WINDOW (EMERG EXIT) WOULD NOT OPEN. LUBRICATED CAPTAIN'S CLEAR VIEW WINDOW TRACK. OPS CHECKED GOOD.
- [SDR ABXA9900060](https://openairdocs.org/sdr/ABXA9900060), Feb 1, 1999: LINK. OUT OF ADJUST. AFTER TAKEOFF WITH GEAR HANDLE IN UP POSITION, THE NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED. GEAR CYCLED DOWN NORMALLY. ON RETRACTION, NOSE GEAR UNSAFE LIGHT
- [SDR ABXA9801182](https://openairdocs.org/sdr/ABXA9801182), Dec 10, 1998: RETAINER. CRACKED. DURING C-CHECK, FOUND LEFT WINDOW RETAINER CRACKED. REPAIRED CRACK IAW DC9 SERVICE REWORK DRAWING 5952965.
- [SDR ABXA9801155](https://openairdocs.org/sdr/ABXA9801155), Dec 2, 1998: JAMB. CRACKED. DURING C-CHECK, FOUND SERVICE DOOR JAMB INTERNAL WEB CRACKED 2 PLACES AT UPPER HINGE CUTOUT, STATION 160. REPAIRED IAW ABX REA D953-25631.
- [SDR ABXA9801154](https://openairdocs.org/sdr/ABXA9801154), Dec 2, 1998: ANGLE. CRACKED. DURING C-CHECK, FOUND NR 1 LOWER PYLON ATTACH ANGLE CRACKED IN RADIUS ON FORWARD EDGE. REPAIRED ANGLE IAW DC9 SRM 54-04.
- [SDR ABXA9801136](https://openairdocs.org/sdr/ABXA9801136), Nov 30, 1998: FITTING. CRACKED. DURING C-CHECK, FOUND LEFT FLAP INBOARD FIXED VANE OUTBOARD ATTACH SUPPORT FITTING BROKEN. REPLACED FITTING IAW DC9 SRM 51-30-2, 52-30-5, AND DACO DWG 9957773.
- [SDR ABXA9800405](https://openairdocs.org/sdr/ABXA9800405), Apr 22, 1998: LATCH. LOOSE. COCKPIT DOOR EXTREMELY DIFFICULT TO OPEN FROM CABIN. TIGHTENED DOOR HANDLE/LATCH ASSEMBLY, OPS CHECKED GOOD.
- [SDR ABXA9700927](https://openairdocs.org/sdr/ABXA9700927), Apr 22, 1997: SPAR CAP. CORRODED. DURING C-CHECK, FOUND THE CENTER WING SPAR AFT VERTICAL FACE OF THE SPAR CAP AT STA XCW -40 SEVERLY CORRODED. REPAIRED IAW ABX REA D957-19174-MR.
- [SDR ABXA9700926](https://openairdocs.org/sdr/ABXA9700926), Apr 22, 1997: FLOORBEAM. CORRODED. DURING C-CHECK, FOUND THE FLOORBEAM AT F/STA 786 CORRODED AT LBL 27 ON TOP SIDE. REPAIRED IAW ABX REA D953-19248-MR.
- [SDR ABXA9700925](https://openairdocs.org/sdr/ABXA9700925), Apr 22, 1997: BULKHEAD WEB. CRACKED. DURING C-CHECK, FOUND THE UPPER CARGO BULKHEAD AT F/STA 786 LT WEB CRACKED. REPAIRED IAW ABX REA D953-19255-MR.
- [SDR ABXA9700924](https://openairdocs.org/sdr/ABXA9700924), Apr 22, 1997: WEB. CORRODED. DURING C-CHECK, FOUND THE CUSP WEB AT F/STA 786 LT CORRODED. REPLACED CUSP WEB IAW DC9 SRM 51-30-2.
- [SDR ABXA9700923](https://openairdocs.org/sdr/ABXA9700923), Apr 22, 1997: FITTING. CRACKED. DURING C-CHECK, FOUND THE FLOORBEAM FITTING AT F/STA 786 LT CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-5 AND 51-30-1.
- [SDR ABXA9700922](https://openairdocs.org/sdr/ABXA9700922), Apr 22, 1997: RIB. CRACKED. DURING C-CHECK, FOUND THE RIGHT WING LEADING EDGE RIB AT STA 172 CRACKED. CUTOUT CRACKED SECTION OF RIB, AND REPAIRED IAW ABX REA D957-19252.
- [SDR ABXA9700921](https://openairdocs.org/sdr/ABXA9700921), Apr 22, 1997: BULKHEAD FITTING. CRACKED. DURING C-CHECK, FOUND THE RIGHT WING BULKHEAD FITTING AT W/STA XRS 69 BETWEEN STRINGERS 12 AND 13 INSIDE LT WING FUEL TANK CRACKED. REPLACED FITTING IAW DC9 SRM
- [SDR ABXA9700920](https://openairdocs.org/sdr/ABXA9700920), Apr 22, 1997: DOOR PAN. CRACKED. DURING C-CHECK, FOUND THE FORWARD CARGO COMPARTMENT DOOR PAN CRACKED BOTH SIDES OF NR 1 PRESSURE STOP. REPAIRED UPPER CRACK IAW DC9 SRM 52-05, FIGURE 50 AND LOW
- [SDR ABXA9700919](https://openairdocs.org/sdr/ABXA9700919), Apr 22, 1997: SKIN. CRACKED. DURING C-CHECK, FOUND THE FUSELAGE SKIN CRACKED 4 INCHES LONG AT LONGERON 18R, FS 544. REPAIRED CRACKED SKIN IAW DC9 SRM 53-04, FIGURE 12B.
- [SDR ABXA9700914](https://openairdocs.org/sdr/ABXA9700914), Apr 19, 1997: TRAPEZOIDAL PNL. CRACKED. DURING C-CHECK, FOUND THE RT TRAPEZOIDAL PANEL CRACKED JUST ABOVE THE RT MLG FIXED STRUT ATTACH POINT. REPLACED TRAPEZOIDAL PANEL IAW DC9 SRM 57-09, FIGURE 34 A
- [SDR ABXA9700913](https://openairdocs.org/sdr/ABXA9700913), Apr 19, 1997: FITTING. CRACKED. DURING C-CHECK, FOUND FORWARD INTERCOSTAL FS 218 BETWEEN LONG 27 AND 28 L CRACKED. REPLACED ATTACH ANGLE (FITTING) P/N 5956034-527 PER DC9 SRM 51-30-2.
- [SDR ABXA9700912](https://openairdocs.org/sdr/ABXA9700912), Apr 19, 1997: SKIN. DAMAGED. DURING C-CHECK, FOUND FUSELAGE SKIN DAMAGED AT STA 408, LONGERON 21L. REPAIRED SKIN IAW DC9 SRM 53-04, FIGURE 38, SHT 20.
- [SDR ABXA9700911](https://openairdocs.org/sdr/ABXA9700911), Apr 19, 1997: FLOORBEAM. CRACKED. DURING C-CHECK, FOUND FLOORBEAM AT FS 503 AND LBL 57 CRACKED. REPLACED FLOORBEAM IAW DC9 SRM.
- [SDR ABXA9700910](https://openairdocs.org/sdr/ABXA9700910), Apr 19, 1997: FRAME. CRACKED. DURING C-CHECK, FOUND FUSELAGE FRAME STA 801 CRACKED AT LONGERON 17R. REMOVED AND REPLACED CRACKED SECTION OF FRAME IAW DC9 SRM 53-03, FIGURE 32.

All 82: https://openairdocs.org/deregistered/N925AX-2007-04-25/reports.md

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