# N812FD: 1994 Airbus Industrie A310-324, registration cancelled 2024-02-06 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: February 6, 2024 - Status when cancelled: Valid registration - Airframe: [Airbus Industrie A310-324](https://openairdocs.org/model/airbus-industrie-a310-324) (registry code 3930318) - Engine: [Pratt & Whitney PW4000 series](https://openairdocs.org/engine/pratt-whitney-pw4000-series) (registry code 52119) - Data sheets: [TCDS A35EU](https://openairdocs.org/tcds/A35EU) (OpenAirDocs) - Serial number: 467 - Year built: 1994 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: January 16, 2006 - Certificate issued: December 14, 2004 - Last registry action: July 18, 2023 - Mode S code: AB114B - Owner when cancelled: [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP) - Location: [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis) - Owner type: Corporation - Owner's area on the map: 35.0351° N, 89.9272° W: Placed by OpenAirDocs at the center of ZIP code 38118, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N812FD - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=812FD - Page: https://openairdocs.org/deregistered/N812FD-2024-02-06 From the FAA registry file of October 31, 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 Airbus Industrie A310-324: https://openairdocs.org/model/airbus-industrie-a310-324.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 FDEA201403120491](https://openairdocs.org/sdr/FDEA201403120491), Mar 12, 2014: CHECK VALVE. LEAKING. LOST GREEN HYD AIR AT FLT LEVEL 390 IAW QRH QTY WAS MONITORED AFTER 1 MIN GREEN HYD QTY FLUCTUATED & PEGGED AT MAX. IAW QRH GREEN HYD PUMPS 1 & 2 WERE SECURED, - [SDR FDEA201312102953](https://openairdocs.org/sdr/FDEA201312102953), Dec 10, 2013: CONTROLLER. FAILED. ON DESCENT TO KMDT RECEIVED CAD REG 2 FAULT, RESET NO HELP. ON LANDING, ACFT SHOWED 3300 CAB ALT, WENT TO MANUAL, TURNED OFF BLEEDS & PACKS. CABIN OUTFLOW VLVS - [SDR FDEA201308021750](https://openairdocs.org/sdr/FDEA201308021750), Aug 2, 2013: JACKSCREW. CONTAMINATED. NR 1 & 2 SLAT SYSTEMS FAULTED ON APPROACH. COMPLIED WITH PHASE 1, NO HELP. COMPLIED WITH ECAM AND QRH. ON CONFIGURING FOR LANDING IAW QRH SLAT EXTENDED NORMALLY - [SDR FDEA201301170121](https://openairdocs.org/sdr/FDEA201301170121), Jan 17, 2013: CONNECTOR. FAILED. CAPTAIN'S RA DOES NOT PROPERLY AGREE WITH FO'S RA. DURING TROUBLESHOOTING NR 1 R/A WOULD FLUCTUATE BETWEEN 150FT AND 450FT, THEN GO ABOVE 2500FT. DISCONNECTED B - [SDR FDEA201212244367](https://openairdocs.org/sdr/FDEA201212244367), Dec 24, 2012: SKIN. DELAMINATED. RIGHT WING INBD LOWER FLAP T/E MID SECTION FOUND DELAMINATED. REMOVED DELAMINATED DOUBLER & DAMAGED HONEYCOMB CORE IAW SRM 57-52-12/201. MADE NEW SKIN DOUBLER I - [SDR FDEA201212244368](https://openairdocs.org/sdr/FDEA201212244368), Dec 24, 2012: SKIN. DELAMINATED. LEFT WING OTBD FLAP T/E LOWER SURFACE FOUND DELAMINATED, FROM INBD TO OTBD 2000 MM, DIM:16" X 7". REMOVED DELAMINATED LOWER SKIN IAW SRM 57-53-12/201. MADE NEW - [SDR FDEA201212154307](https://openairdocs.org/sdr/FDEA201212154307), Dec 15, 2012: FITTING. CORRODED. LEFT WING-MLG FITTING-INSPECTION OF RIB 5 FORWARD LUG CORROSION EXCEED LIMITS. REMOVED CORROSION IAW REPAIR DWG R57249389, ISSUE B, STEP 1B. IAW EA6-5710-163164 - [SDR FDEA201212144299](https://openairdocs.org/sdr/FDEA201212144299), Dec 14, 2012: SPAR. CRACKED. CENTER WING RT REAR SPAR NR 61 HOLE FOUND CRACKED. REAMED HOLE AT 0.4MM THROUGH ALL LAYERS PER EA6-5710-163167. INSPECTED PER NTM51-10-01,NO CRACK FOUND. REAMED - [SDR FDEA201212144297](https://openairdocs.org/sdr/FDEA201212144297), Dec 14, 2012: PLATE. CRACKED. FOUND A CRACK ABOUT 5MM IN LENGTH, 1MM IN DEPTH INITIATED FROM THE NR 2 FASTENER HOLE OF THE RT WING UPPER CORNER ANGLE AT FR40. REAMED NR 2 HOLE AT 0.4MM THROU - [SDR FDEA201109294213](https://openairdocs.org/sdr/FDEA201109294213), Sep 29, 2011: SOLENOID VALVE. LEAKING. GREEN HYD SYS LO RSVR INDICATION INFLIGHT FOLLOWED QRH, AFTER LANDING GREEN SYS REVR INDICATION RETURNED TO NORMAL. RESTORED FREE FALL EXTENSION SYSTEM TO NORMA - [SDR FDEA201011164400](https://openairdocs.org/sdr/FDEA201011164400), Nov 16, 2010: SKIN. CORRODED. FUSELAGE SKIN EXTERIOR SURFACE FOUND CORROSION UNDER BULK CARGO DOOR SCUFF PLATE (FWD LWR CORNER). REMOVE THE CORROSION IAW SRM 51-74-10. APPLY ALODINE IAW SRM - [SDR FDEA201009263716](https://openairdocs.org/sdr/FDEA201009263716), Sep 26, 2010: COMPUTER. MALFUNCTIONED. ON TAKEOFF ROLL, MASTER WARNING REPETITIVE CHIME, AT APPROX 130 KTS RTO. ECAM SHOWED PITCH TRIM 2 YD 2 OFF. PITCH TRIM 2 YD 2 BOTH RESET OK. BRAKE 3 670 DEGREES - [SDR FDEA201003301032](https://openairdocs.org/sdr/FDEA201003301032), Mar 30, 2010: B-NUT. LEAKING. HYD GREEN SYS SERVICED WITHIN LIMITS, 10 MINUTES AFTER DEPARTURE, QTY IN AMBER BAN D. TURNED OFF NR 1 ENG HYD PUMP PRIOR TO TO RED DOT IN AMBER BAND AT FLT LEVE - [SDR FDEA201003070672](https://openairdocs.org/sdr/FDEA201003070672), Mar 7, 2010: JACKSCREW. FAILED. RECEIVED SLAT SYS 1 AND SYS 2 FAULT. SLAT STUCK AT APPROX 2 DEG, LANDED SLATS 2 DEG AND FLAPS 40 DEG, REPEAT WRITE UP. CYCLED ON THE GROUND PRIOR TO DEPARTURE A - [SDR FDEA200911204098](https://openairdocs.org/sdr/FDEA200911204098), Nov 20, 2009: BRAKE SYS. MALFUNCTIONED. DURING TRO WITH MAX BRAKES SELECTED, ONLY WHEEL BRAKES ON NR1,2,5,6 (LT SIDE) OPERATED NORMALLY. ACFT STARTED ABRUPT PULL TO LT DESELECTED AUTO BRAKES AND STOPP - [SDR FDEA200911204097](https://openairdocs.org/sdr/FDEA200911204097), Nov 20, 2009: ANTI-ICE SYSTEM. FAULTED. DURING T/O POWER APPLICATION, WHEN TOGA PWR WAS SELECTED THE GREEN A/THR LIGHT ILLUMINATED HOWEVER THE THROTTLES WOULD NOT MOVE. ACCOMPLISHED RTO AT 25 KTS. VER - [SDR FDEA200911204095](https://openairdocs.org/sdr/FDEA200911204095), Nov 20, 2009: ANTI-ICE VALVE. FAULTED. DURING TAKEOFF ROLL AT 85KTS ECAM WARNING "ENG NAC ANTI ICE VALVE". ACCOMPLISHED RTO (ENG NR1) ENG ANTI ICE WAS ON DURING TAKE OFF. VERIFIED AT BLOCK IN NR 1 EN - [SDR FDEA200911204093](https://openairdocs.org/sdr/FDEA200911204093), Nov 20, 2009: ANTI-ICE VALVE. WARNING MESSAGE. DURING TAKEOFF ROLL WITH ANTI-ICE ON, RECEIVED ECAM MESSAGE "ENG NR1 ANTI-ICE NAC VALVE". ACCOMPLISHED RTO AT 70 KTS. (RTO 1 OF 2) SEE WRI 30-20/3659 FOR DEFERR - [SDR FDEA200811184905](https://openairdocs.org/sdr/FDEA200811184905), Nov 18, 2008: CONTROL UNIT. BINDING. SECOND REJECTED T/O DUE TO BLUE RUDDER SERVO CONTROL JAM, ECAM WARNING CAME ON AT 40-50 PERCENT N1. NO FAULT FOUND ON 1ST RTO. RAN ENGINE & CHECKED ALL FLT CONT - [SDR 08FDEA04905](https://openairdocs.org/sdr/08FDEA04905), Nov 18, 2008: CONTROL UNIT. INOPERATIVE. 2ND REJECTED TAKEOFF DUE TO BLUE RUDDER SERVO CTL JAM, ECAM WARNING CAME ON AT 40-50 PERCENT N1. NO FAULT FOUND ON 1ST RTO, RAN ENG AND CHECKED ALL FLT CONTROL - [SDR 08FDEA03353](https://openairdocs.org/sdr/08FDEA03353), Aug 9, 2008: SKIN. DAMAGED. UPON INSPECTION OF RUDDER BY THERMOGRAPHY IAW EO 6-5530-7-5004 PT 2 PARA 8 STEP C AND D THE FOLLOWING DEFECTS WERE NOTED IN ADDITION TO ORIGINAL FINDINGS REF EA - [SDR 08FDEA03264](https://openairdocs.org/sdr/08FDEA03264), Aug 5, 2008: SKIN. DENTED. EXTERNAL LT FUSELAGE SKIN HAS 2 DENTS. NR 1 AT FRAME 60 BETWEEN STRINGER 43 AND 44L 4 INCHES ABOVE BOTTOM SKIN LAP MEASURES 6 INCHES LONG BY .800 INCHES WIDE BY - [SDR 08FDEA03263](https://openairdocs.org/sdr/08FDEA03263), Aug 5, 2008: SKIN. DENTED. DENT IN RT NR 1 LEADING EDGE SLAT, DENT MEASURES 4 INCH LONG BETWEEN RIBS 7 AND 8, 35 INCHES FROM INBD EDGE, 5 1/2 INCHES BELOW PAINTED SURFACE, AND 5/32 INCH D - [SDR 07FDEA03644](https://openairdocs.org/sdr/07FDEA03644), Sep 13, 2007: ANGLE. MISMANUFACTURED. LESS EDGE MARGIN (5-6 MM) AT ANGLES STRG 26 RT AT FRAME 69 AND STRG 26 LT FRAME 63 AND 65. IT'S IMPOSSIBLE TO INSTALL DAN5-6X OR DAN5-8 FASTENER DURING PTOF. RE - [SDR 07FDEA03642](https://openairdocs.org/sdr/07FDEA03642), Sep 13, 2007: FITTING. CRACKED. CRACKED ATTACHMENT HOLES IN CORNER PROFILE AT FRAME 25A BETWEEN STRG. 28-34 RT. REPLACEMENT OF CORNER PROFILE IAW SRM 51-72-10 AND PTOF DRW, R255B0061. - [SDR 07FDEA03641](https://openairdocs.org/sdr/07FDEA03641), Sep 13, 2007: FITTING. CRACKED. CRACKED ATTACHMENT HOLES IN CORNER PROFILE AT FRAME 25A BETWEEN STRG 28-34 RT. REPLACEMENT OF CORNER PROFILE IAW SRM 51-72-10 AND PTOF DRW, R255B0061. - [SDR 07FDEA03634](https://openairdocs.org/sdr/07FDEA03634), Sep 13, 2007: BRACKET. CRACKED. CRACKED BRACKET AT FRAME 19, STRG 50 LT. REPLACEMENT OF BRACKET IAW SRM 51-72-10. - [SDR 07FDEA03633](https://openairdocs.org/sdr/07FDEA03633), Sep 13, 2007: BRACKET. CRACKED. CRACKED BRACKET AT FRAME 19, STRG 49 LT . REPLACEMENT OF BRACKET IAW SRM 51-72-10. - [SDR 07FDEA03632](https://openairdocs.org/sdr/07FDEA03632), Sep 13, 2007: BRACKET. CRACKED. CRACKED BRACKET AT FRAME 19, STRG 46 LT. REPLACEMENT OF BRACKET IAW SRM 51-72-10. - [SDR 07FDEA03663](https://openairdocs.org/sdr/07FDEA03663), Sep 13, 2007: FITTING. DAMAGED. FOUND MISDRILLED HOLE IN CORNER FITTING ADJACENT AND LESS MARGIN TO ROLLER TRACK HOLE, FRAME 60, CARGO FLOOR STRUCTURE, Y1460 LT. REPAIR PERFORMED BY CREATING A - [SDR 07FDEA03662](https://openairdocs.org/sdr/07FDEA03662), Sep 13, 2007: DOOR FRAME. DAMAGED. TOOLING IMPACTS FOUND ON DOOR FRAME 14 UNDER DOOR STOP 8 LH, PAX DOOR 1. REPAIR PERFORMED BY SMOOTH BLEND OUT, DVI INSPECTING OF FASTENER HOLES AND HFEC INSPECT - [SDR 07FDEA03659](https://openairdocs.org/sdr/07FDEA03659), Sep 13, 2007: FRAME. DENTED. TOOL IMPACT CAUSES DENT IN FRAME 71, STRG 15 RHS. SPLICE REPAIR PERFORMED IAW SRM 53-10-13 / PG 210, 213 / FIG 203. - [SDR 07FDEA03658](https://openairdocs.org/sdr/07FDEA03658), Sep 13, 2007: FRAME. DENTED. TOOL IMPACT CAUSES DENT IN FRAME 70, STRG 15 RHS. SPLICE REPAIR PERFORMED IAW SRM 53-10-13 / PG 210, 213/FIG 203. - [SDR 07FDEA03656](https://openairdocs.org/sdr/07FDEA03656), Sep 13, 2007: FRAME. CORRODED. HEAVY CORROSION FOUND ON THE T-SECTION AT FRAME 92, BETWEEN STRG 19-23 LT (TAILCONE). REPAIR PERFORMED BY CUT OUT THE T-SECTION AND INSTALLING NEW PORTION AND R - [SDR 07FDEA03653](https://openairdocs.org/sdr/07FDEA03653), Sep 13, 2007: FLOOR SUPPORT. CORRODED. HEAVY CORROSION ON FLOOR SUPPORT BETWEEN FRAME 14-17, STRINGER 26, Y-1959 RT. REPAIR PERFORMED BY REINFORCING WITH ANGLE IAW SRM 53-12-15/FIG 207. - [SDR 07FDEA03651](https://openairdocs.org/sdr/07FDEA03651), Sep 13, 2007: FITTING. DAMAGED. MISDRILLED HOLE IN CORNER FITTING FRAME 54.1 RT DUE TO FAILED INSTALLED ROLLERTRACK ON CARGO FLOOR STRUCTURE. REPLACEMENT OF CORNERFITTING IAW SRM 51-72-10. - [SDR 07FDEA03650](https://openairdocs.org/sdr/07FDEA03650), Sep 13, 2007: ANGLE. FAILED. LESS MARGIN AT ONE HOLE AT FRAME 59, STRG 26 LT. NEW SUPPORT CAN'T BE INSTALLED BETWEEN FRAME 59 AND SEAT TRACK AS PER DRW, R539H0112. REPAIR PERFORMED BY INSTA - [SDR 07FDEA03648](https://openairdocs.org/sdr/07FDEA03648), Sep 13, 2007: SKIN. CORRODED. HEAVY CORROSION UNDER ANTI-CHAFING PLATE ON SKIN PANEL BETWEEN FRAME 92-94, STRG 9-13 LT AND RT, OUT OF LIMIT. REPLACEMENT OF BOTH SKIN-PANELS (FABRICATED BY EF - [SDR 07FDEA03647](https://openairdocs.org/sdr/07FDEA03647), Sep 13, 2007: STRINGER. DAMAGED. SEVERAL MISDRILLED HOLES ON STRINGER 33 RT BETWEEN FRAME 69-70. STRINGER SPLICE REPAIR PERFORMED IAW SRM 53-10-14/FIG 201 / SEC "C-C". - [SDR 07FDEA03645](https://openairdocs.org/sdr/07FDEA03645), Sep 13, 2007: SKIN. DENTED. DENT IN BOTTOM SKIN OF LT ELEVATOR TRAILING EDGE (30X30X1,5). REPAIR PERFORMED IAW SRM 55-21-11/CONFIG 1/PARA 5D/FIG 204. - [SDR 07FDEA03637](https://openairdocs.org/sdr/07FDEA03637), Sep 13, 2007: PLATE. CRACKED. CRACKED SHEAR PLATES BETWEEN FRAME 79-80/82, STRG 26 LT AND RT. REPLACEMENT OF BOTH SHEAR PLATES IAW SRM 51-72-10. - [SDR 07FDEA03631](https://openairdocs.org/sdr/07FDEA03631), Sep 13, 2007: SKIN PANEL. CHAFED. CHAFING MARKS FOUND AROUND MANHOLE 9 APERTURE ON THE UPPER SURFACE OF THE BOTTOM WING SKIN PANEL NR 2 BETWEEN RIB 14-15, BOTH WINGS. REPAIR PERFORMED BY SMOOTH - [SDR 07FDEA03616](https://openairdocs.org/sdr/07FDEA03616), Sep 12, 2007: SKIN. CORRODED. FOUND SKIN BULGE (CORROSION) ON LEADING EDGE OF RT WING INBOARD FLAP, NEAR TO TRACK 1. REPLACEMENT OF L/E SKIN AT FLAP IAW SRM 51-72-10. - [SDR 07FDEA03615](https://openairdocs.org/sdr/07FDEA03615), Sep 12, 2007: TUBE. CRACKED. DAMAGED (CRACKED) TUBE ASSY BETWEEN FRAME 24-25, STRG 52 RT. REPLACEMENT OF TUBE ASSY IAW SRM 51-72-10. - [SDR 07FDEA03628](https://openairdocs.org/sdr/07FDEA03628), Sep 12, 2007: STRINGER. CORRODED. CORROSION ON STRINGER 53, 54 AND 55 LHS BETWEEN FRAME 70-71. STRINGER SPLICE REPAIRS PERFORMED IAW SRM 53-10-14/FIG 201. - [SDR 07FDEA03627](https://openairdocs.org/sdr/07FDEA03627), Sep 12, 2007: WEB. DAMAGED. FOUND DAMAGED WEB PLATE BETWEEN FRAME 86-87, STRG 36 LT. REPLACEMENT OF WEB PLATE IAW SRM 51-72-10 AND SRM 53-19-18/PG 76/ ITEM 40. - [SDR 07FDEA03626](https://openairdocs.org/sdr/07FDEA03626), Sep 12, 2007: WEB. DAMAGED. FOUND DAMAGED WEB PLATE BETWEEN FRAME 86-87, STRG 39 RT. REPLACEMENT OF WEB PLATE IAW SRM 51-72-10 AND SRM 53-19-18 / PG 76 / ITEM 10. - [SDR 07FDEA03625](https://openairdocs.org/sdr/07FDEA03625), Sep 12, 2007: WEB. DAMAGED. FOUND DAMAGED WEB PLATES BETWEEN FRAME 86-87, STRG 33 LT AND RT. REPLACEMENT OF WEB PLATES IAW SRM 51-72-10 AND SRM 53-19-18/PG 53. - [SDR 07FDEA03624](https://openairdocs.org/sdr/07FDEA03624), Sep 12, 2007: FITTING. CORRODED. CORROSION ON FITTING AT FRAME 63, STR 41-45 LT, OUT OF LIMIT. REPLACEMENT OF FITTING IAW SRM 51-72-10. - [SDR 07FDEA03623](https://openairdocs.org/sdr/07FDEA03623), Sep 12, 2007: LONGERON. MISREPAIRED. FOUND SPLICE REPAIR ON EXTRUSION BETWEEN FRAME 12A-14, Y-953 RT, MATERIAL NOT CONFORM TO SRM 53-12-15/FIG 207. SPLICE REPAIR ON EXTRUSION RENEWED IAW SRM 53-12- All 85: https://openairdocs.org/deregistered/N812FD-2024-02-06/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.