# N812AX: 1970 Mcdonnell Douglas DC-8-63F, registration cancelled 2008-06-16 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: June 16, 2008 - Exported to: United Arab Emirates - Status when cancelled: Valid registration - Airframe: [Mcdonnell Douglas DC-8-63F](https://openairdocs.org/model/mcdonnell-douglas-dc-8-63f) (registry code 302198H) - Engine: [Pratt & Whitney JT3D series](https://openairdocs.org/engine/pratt-whitney-jt3d-series) (registry code 52035) - Data sheets: [TCDS 4A25](https://openairdocs.org/tcds/4A25) (OpenAirDocs) - Serial number: 46126 - Year built: 1970 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: July 27, 1990 - Certificate issued: January 7, 2008 - Last registry action: January 7, 2008 - Mode S code: AB10E0 - Owner when cancelled: [Azima Farhad](https://openairdocs.org/faa-owner/AZIMA%20FARHAD) - Location: [Kansas City, MO](https://openairdocs.org/faa-place/MO/Kansas%20City) - Owner type: Individual - Owner's area on the map: 38.9578° N, 94.5986° W: Placed by OpenAirDocs at the center of ZIP code 64114, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N812AX - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=812AX - Page: https://openairdocs.org/deregistered/N812AX-2008-06-16 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-8-63F: https://openairdocs.org/model/mcdonnell-douglas-dc-8-63f.md ## Service difficulty reports (85, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ABXA070265](https://openairdocs.org/sdr/ABXA070265), Aug 2, 2007: HINGE PIN. SHEARED. DURING MAINTENANCE ON WO 600267980, UPPER FORWARD CARGO DOOR FORWARD HINGE PIN WAS SHEARED. REMOVED AND REPLACED FORWARD HINGE PIN IAW DC8 AMM 20-10-0. - [SDR ABXA060222](https://openairdocs.org/sdr/ABXA060222), Apr 28, 2006: SPAR. CORRODED. LEFT WING REAR SPAR AFT FACE HAD CORROSION AT WING ROOT XRS 5. ACCOMPLISHED REPAIR IAW REA D857-53586-MR, REV. IR AT LEFT WING REAR SPAR. - [SDR ABXA060221](https://openairdocs.org/sdr/ABXA060221), Apr 27, 2006: SKIN. DAMAGED. RIGHT ELEVATOR LOWER SKIN AT XS 77.0, HAD "OIL CAN" CONDITION AT HINGE NR 2 SMALL ACCESS HOLE. ACCOMPLISHED REPAIR IAW REA D855-53583-MR, REV. IR AT RIGHT ELEVA - [SDR ABXA060220](https://openairdocs.org/sdr/ABXA060220), Apr 24, 2006: SKIN. DAMAGED. UPPER CARGO MAIN CARGO DOOR FUSELAGE CUT OUT PLATING DAMAGE, SEVERAL AREAS MISSING STA. 160 - 180, LONGERON 6 LEFT. ACCOMPLISHED REPAIR AT DOOR CUT OUT IAW REA - [SDR ABXA060219](https://openairdocs.org/sdr/ABXA060219), Apr 20, 2006: SKIN. CORRODED. LEFT INBOARD HORIZONTAL STABILIZER LEADING EDGE SECTION OUTBOARD UPPER SURFACE AT XSTA 177, HAD INTERGRANULAR CORROSION AT SCREW HOLE AREA. INSTALLED REPAIR AT - [SDR ABXA060217](https://openairdocs.org/sdr/ABXA060217), Apr 5, 2006: SKIN. CRACKED. CRACK IN RIGHT WING LEADING EDGE PANEL ASSEMBLY INNER (WAFFLED) SKIN 8" FROM INBOARD EDGE, STA. XFS 304. STOP DRILLED CRACK AND INSTALLED REPAIR IAW REA D857-53 - [SDR ABXA060218](https://openairdocs.org/sdr/ABXA060218), Apr 5, 2006: SKIN. CRACKED. RIGHT WING LEADING EDGE PANEL ASSEMBLY INNER (WAFFLED) SKIN HAD 3 EACH CRACKS AT APPROX. XFS 410 - 423. REPAIRED CRACKS IAW REA D857-53581, REV. IR. - [SDR ABXA060195](https://openairdocs.org/sdr/ABXA060195), Apr 5, 2006: SKIN. CRACKED. RIGHT WING LEADING EDGE PANEL ASSEMBLY INNER (WAFFLED) SKIN HAD 3 EACH CRACKS AT XFS 410 - 423. REPAIRED CRACKS IAW REA D857-53581, REV IR. - [SDR ABXA060194](https://openairdocs.org/sdr/ABXA060194), Apr 5, 2006: SKIN. CRACKED. CRACK IN RIGHT WING LEADING EDGE PANEL ASSEMBLY INNER (WAFFLED) SKIN 8 INCHES FROM INBOARD EDGE STA XFS 304. STOP DRILLED CRACK AND INSTALLED REPAIR IAW REA D85 - [SDR ABXA060216](https://openairdocs.org/sdr/ABXA060216), Apr 2, 2006: LONGERON. CORRODED. EXFOLIATION CORROSION IN LONGERON 27 LEFT, STA. 1220 - 1240. ACCOMPLISHED REPAIR IAW REA D853-53585-MR, REV. IR, ON LONGERON 27 LEFT, STA. 1220 - 1240. - [SDR ABXA060215](https://openairdocs.org/sdr/ABXA060215), Mar 30, 2006: SKIN. CORRODED. LEFT HORIZONTAL STABILIZER OUTBOARD LEADING EDGE UPPER STRUCTURE HAD INTERGRANULAR CORROSION ON AFT TRAILING EDGE FROM XFS 178 - 341. ACCOMPLISHED REPAIR OF LEF - [SDR ABXA060213](https://openairdocs.org/sdr/ABXA060213), Mar 29, 2006: PANEL. CORRODED. RIGHT HORIZONATL STABILIZER LEADING EDGE OUTBOARD SECTION UPPER TRAILING EDGE INTERGRANULAR CORROSION AT 3 LOCATIONS: XFS260, 316 & 332. CUT OUT DAMAGED AREA AN - [SDR ABXA060214](https://openairdocs.org/sdr/ABXA060214), Mar 29, 2006: SKIN. CRACKED. THREE CRACKS ALONG THE UPPER EDGE OF CUT OUT, IN THE INNER SKIN OF THE AFT CARGO DOOR. TRIMMED OUT CRACKS IAW REA D852-53568. - [SDR ABXA060211](https://openairdocs.org/sdr/ABXA060211), Mar 29, 2006: SKIN. CORRODED. RIGHT HORIZONTAL STABILIZER INBOARD LEADING EDGE SECTION AT UPPER TRAILING EDGE MID AREA AT XSTA 140, HAD INTERGRANULAR CORROSION AROUND SCREW HOLES. INSTALLED - [SDR ABXA060212](https://openairdocs.org/sdr/ABXA060212), Mar 29, 2006: PANEL. CORRODED. RIGHT HORIZONTAL STABILIZER OUTBOARD LEADING EDGE SECTION AT INBOARD UPPER LEADING EDGE HAD INTERGRANULAR CORROSION AT HILOC HOLE. INSTALLED REPAIR IAW REA D855 - [SDR ABXA060192](https://openairdocs.org/sdr/ABXA060192), Mar 29, 2006: SKIN. CORRODED. RIGHT HORIZONTAL STABILIZER LEADING EDGE OUTBOARD SECTION UPPER TRAILING EDGE HAD INTERGRANULAR CORROSION AT 3 LOCATIONS: XFS 260, 316 AND 332. CUT OUT DAMAGED - [SDR ABXA060193](https://openairdocs.org/sdr/ABXA060193), Mar 29, 2006: SKIN. CRACKED. THREE CRACKS ALONG THE UPPER EDGE OF CUTOUT, IN THE INNER SKIN OF THE AFT CARGO DOOR. TRIMMED OUT CRACKED IAW REA D852-53568. - [SDR ABXA060191](https://openairdocs.org/sdr/ABXA060191), Mar 29, 2006: SKIN. CORRODED. RIGHT HORIZONTAL STABILIZER LEADING EDGE OUTBOARD UPPER SKIN HAD INTERGRANULAR CORROSION AT XFS 178.750. CUT OUT DAMAGED AREA AND INSTALLED REPAIR IAW REA D855- - [SDR ABXA060207](https://openairdocs.org/sdr/ABXA060207), Mar 28, 2006: SKIN PANEL. CORRODED. PERMANENT REPAIR OF CORROSION ON LONGERON L36 (KEEL BEAM) PER COI 50571 AND SKIN PANELS AT STA. 670 AND 683 PER COI 50570 AND COI 50572. REPAIR ACCOMPLISHED IAW - [SDR ABXA060208](https://openairdocs.org/sdr/ABXA060208), Mar 28, 2006: LONGERON. DAMAGED. REMOVE AND REPLACE EXISTING DISCREPANT LONGERON 24 RIGHT IN RIGHT WHEEL WELL, STA. 857 - 980, DUE TO PREVIOUS DAMAGE WITH AN INTERIM REPAIR IAW REA D853-52752-M - [SDR ABXA060209](https://openairdocs.org/sdr/ABXA060209), Mar 28, 2006: SKIN. CORRODED. LEFT WING LEADING EDGE UPPER AFT EDGE OF OUTER MOST LEADING EDGE ASSEMBLY AT XFS 291 - 422 LEFT, HAD EXFOLIATION AROUND SCREWS. ACCOMPLISHED REPAIR IAW REA D857 - [SDR ABXA060206](https://openairdocs.org/sdr/ABXA060206), Mar 25, 2006: LONGERON. CORRODED. FORWARD CARGO COMPARTMENT LNOGERON 31 LEFT HAD CORROSION AT STA. 520. ACCOMPLISHED REPAIR IAW REA D853-53595-MR, REV. IR, ON LONGERON 31 LEFT. - [SDR ABXA060205](https://openairdocs.org/sdr/ABXA060205), Mar 25, 2006: LONGERON. CORRODED. CORROSION AT LONGERON 31 LEFT, F.S. 560 - 600. ACCOMPLISHED REPAIR OF LONGERON 31 LEFT, F.S. 560 - 600 IAW REA D853-53592-MR, REV. IR. - [SDR ABXA060210](https://openairdocs.org/sdr/ABXA060210), Mar 24, 2006: SKIN. CORRODED. RIGHT HORIZONTAL STABILIZER LEADING EDGE OUTBOARD UPPER SKIN HAD INTERGRANULAR CORROSION AT XFS 178.750. CUT OUT DAMAGED AREA AND INSTALLED REPAIR IAW REA D855- - [SDR ABXA060204](https://openairdocs.org/sdr/ABXA060204), Mar 21, 2006: LONGERON. CORRODED. SEVERAL AREAS OF CORROSION ON LONGERON 24 LEFT, F.S. 857 - 980 IN LEFT WHEEL WELL. REPLACED LONGERON 24 LEFT, F.S. 857 - 980 IN LEFT WHEEL WELL IAW REA D853-530 - [SDR ABXA060203](https://openairdocs.org/sdr/ABXA060203), Mar 20, 2006: SKIN. CORRODED. RIGHT FUSELAGE SKIN HAD BULGE AND RIVETS POPPED OFF AT STA. 1600, LONGERON 27 RIGHT. EXISTING REPAIR REMOVED AND SKIN AND INNER DOUBLER CUT TO REMOVE ALL CORROS - [SDR ABXA060190](https://openairdocs.org/sdr/ABXA060190), Mar 20, 2006: SKIN. CORRODED. RIGHT FUSELAGE SKIN HAD BULGE AND RIVETS POPPED OFF AT STA 1600, LONGERON 27 RIGHT. EXISTING REPAIR REMOVED, AND SKIN AND INNER DOUBLER CUT TO REMOVE ALL CORROS - [SDR ABXA060081](https://openairdocs.org/sdr/ABXA060081), Feb 14, 2006: FUEL CONTROL. DEFECTIVE. NR 3 ENGINE FAILED TO ACCELERATE IN-FLIGHT. EET 20 DEGREES N2 48%, FF AT 1000 LBS. ATTEMPTED RE-LIGHT TO NO AVAIL. SHUT DOWN NR 3 ENGINE AT 0518Z, 4 PSI INDICAT - [SDR ABXA060056](https://openairdocs.org/sdr/ABXA060056), Jan 16, 2006: FITTING. CRACKED. FITTING AT LONGERON 24, FS 879, CRACKED. REPAIRED FITTING IAW REA D853-53104. - [SDR ABXA050293](https://openairdocs.org/sdr/ABXA050293), Nov 29, 2005: LONGERON. CORRODED. CORROSION FOUND ON LONGERON 24 RIGHT AT STATION 879. REA D853-52752MR PERFORMS AN INTERIM REPAIR TO THE LONGERON. - [SDR ABXA050292](https://openairdocs.org/sdr/ABXA050292), Nov 29, 2005: SKIN. CORRODED. CORROSION FOUND ON THE WING TO FUSELAGE SKIN AT STATION 670 AND LONGERON 36. REA D853-52756MR PERFORMS AN INTERIM REPAIR SIMILAR TO SRM 53-2-1, FIG. 7, AS OPERA - [SDR ABXA050289](https://openairdocs.org/sdr/ABXA050289), Nov 21, 2005: WINDOW. LACK OF LUBE. CAPTAIN'S CLEARVIEW WINDOW WOULD NOT OPEN. LUBRICATED CAPTAIN'S CLEARVIEW WINDOW ASSEMBLY IAW DC-8 MM 56-00-00. OPS CHECKED GOOD. - [SDR ABXA050094](https://openairdocs.org/sdr/ABXA050094), Apr 18, 2005: SKIN. CORRODED. FUSELAGE SKIN COMMON TO THE FACTORY ANTENNA DOUBLER, CORRODED. FABRICATED SKIN AND DOUBLER FOR ANTENNA AND INSTALLED IAW REA D853-51782 ON WO NR 600221026. - [SDR ABXA040352](https://openairdocs.org/sdr/ABXA040352), Oct 19, 2004: LAMP. INOPERATIVE. EMERGENCY EXIT LIGHTS ARMED AMBER LIGHT INOPERTATIVE. RELAMPED, OPS CHECKED GOOD IAW DC-8 MM 33-50-02. - [SDR ABXA040299](https://openairdocs.org/sdr/ABXA040299), Aug 15, 2004: FITTING. CRACKED. INTERCOSTAL END FITTING AT STA 1140, LONGERON 35 LEFT WAS CRACKED. REPLACED END FITTING IAW DC-9 SRM 51-1-20D. - [SDR ABXA040300](https://openairdocs.org/sdr/ABXA040300), Aug 15, 2004: FITTING. CRACKED. INTERCOSTAL END FITTING AT STA 1160, LONGERON 35 RIGHT WAS CRACKED. END FITTING WAS REPLACED IAW DC-8 SRM 51-1-20D. - [SDR ABXA040301](https://openairdocs.org/sdr/ABXA040301), Aug 14, 2004: SKIN. CORRODED. AFT FUSELAGE SKIN FORWARD OF NR 3 CARGO DOOR HAD BULGED REPAIR. REPAIRED AREA IAW REA D853-50277MR. - [SDR ABXA040264](https://openairdocs.org/sdr/ABXA040264), Jul 12, 2004: LONGERON. CRACKED. LT MAIN LANDING GEAR WHEEL WELL LONGERON 24 CRACKED ON LOWER FLANGE AT BOTTLE BOLT CAVITY. REPAIRED AREA IAW REA D853-49163MR. - [SDR ABXA040263](https://openairdocs.org/sdr/ABXA040263), Jul 7, 2004: FITTING. CRACKED. FITTING CRACKED AT MOST FORWARD FASTENER HOLES. FABRICATED REPAIR PARTS IAW REA D853-49975MR. ALODINED AND PRIMED IAW SRM 51-1-8. INSTALLED IAW SRM 51-1-20B. - [SDR ABXA040111](https://openairdocs.org/sdr/ABXA040111), Mar 17, 2004: FUEL CONTROL. DEFECTIVE. NR 4 ENGINE, AFTER SETTING POWER FOR CRUISE, NR 4 ENGINE ROLLED BACK .15 EPR. EGT, FUEL FLOW N1 AND N2 ALL DROPPED. THROTTLE DID NOT MOVE. REPLACED NR 4 ENGINE - [SDR ABXA040110](https://openairdocs.org/sdr/ABXA040110), Mar 17, 2004: BLEED VALVE. DEFECTIVE. AFTER TAKEOFF 2000 FEET, HEARD SHARP LOUD BANG/POP. NR 2 EPR DROPPED .18 AND BACK. FELT SLIGHT LEFT YAW. REPLACED NR 2 ENGINE COMPRESSOR BLEED VALVE AND CONTROL - [SDR ABXA030029](https://openairdocs.org/sdr/ABXA030029), Jan 10, 2003: LINK. BROKEN. DURING SERVICE CHECK, FOUND THE NR 5 INBOARD GROUND SPOILER WITH 2 EACH CENTER CRANK ASSEMBLIES AND INBOARD SPOILER OVERCENTER LINK BROKEN. REMOVED THE LEFT WIN - [SDR ABXA020272](https://openairdocs.org/sdr/ABXA020272), Oct 19, 2002: FRAME. CRACKED. MAIN CABIN FRAME AT STA 240 RIGHT SIDE WAS CRACKED AT FLOOR LEVEL. INSTALLED DOUBLER REPAIR AT STA 240 MAIN CABIN RIGHT SIDE IAW DRAWING K04888 AND DC-8 SRM. - [SDR ABXA020271](https://openairdocs.org/sdr/ABXA020271), Oct 19, 2002: FRAME. CRACKED. MAIN CABIN FRAME AT STA 220 RIGHT SIDE WAS CRACKED AT FLOOR LEVEL. INSTALLED DOUBLER REPAIR AT STA 220 RIGHT AT FLOOR LEVEL IAW DRAWING K04888 AND DC-8 SRM. - [SDR ABXA020267](https://openairdocs.org/sdr/ABXA020267), Oct 19, 2002: SKIN. CRACKED. FUSELAGE RIGHT AFT DOOR X-RAY SHOWED CRACK AT AFT UPPER CORNER OF DOOR CUTOUT. INSTALLED REPAIR DOUBLER AT RIGHT AFT DOOR UPPER CORNER IAW DC-8 DRAWING SRO 8530 - [SDR ABXA020273](https://openairdocs.org/sdr/ABXA020273), Oct 7, 2002: SKIN. CRACKED. A/C EXHAUST DUCT SKIN WAS CRACKED AT THE FORWARD UPPER CORNER AT FS 50, STRINGER 28 LEFT. CUT OUT DAMAGE AND INSTALLED REPAIR IAW DRAWING SR08530020 AND DC-8 SR - [SDR ABXA020290](https://openairdocs.org/sdr/ABXA020290), Oct 2, 2002: FLOORBEAM. CORRODED. CORROSION FOUND ON NOSE LANDING GEAR WELL HORIZONTAL PRESSURE PANEL, BETWEEN FS 12 TO FS 27. ALSO FOUND CORROSION ON FLOORBEAM LOWER FLANGE AT FS 12, BUTT LINE - [SDR ABXA020270](https://openairdocs.org/sdr/ABXA020270), Oct 2, 2002: DOOR FRAME. CRACKED. CRACK AT FORWARD ENTRY DOOR CUTOUT AFT LOWER CORNER. CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLER AND TRIPLER IAW DC-8 SRM 53-2-0. - [SDR ABXA020269](https://openairdocs.org/sdr/ABXA020269), Oct 1, 2002: DOOR FRAME. DAMAGED. EXISTING REPAIR AT PASSENGER DOOR FORWARD UPPER CORNER DID NOT CONFORM TO DRAWING ES00863. REMOVED AND REPLACED REPAIR IAW DC-8 SRM 53-2-0. - [SDR ABXA020268](https://openairdocs.org/sdr/ABXA020268), Oct 1, 2002: LONGERON. CRACKED. FUSELAGE LONGERON 11 RIGHT HAD A 1 INCH CRACK AT FS 1660. REPAIRED LONGERON 11 IAW REA D853-41973MR. All 85: https://openairdocs.org/deregistered/N812AX-2008-06-16/reports.md ## FAA accident and incident reports (1) 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 19901212063809I](https://openairdocs.org/incident/19901212063809I), Dec 12, 1990: Doug DC863F (N812AX), Phoenix, AZ, Minor damage. Unable to retract gear after takeoff. Returned. Utilized heavy braking on rollout. Had fire in brake. --- 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.