# Airbus A310 - Type: Aircraft model (FAA registry) - Registry code: 3930338 - Manufacturer (registry): AIRBUS - Model: A310 - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 2 · Turbo-jet - Seats: 280 - Weight class: 20,000 lb and over - Certification: Type certificated - Registered aircraft: 0 - Page: https://openairdocs.org/model/airbus-a310 Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker. ## ADs that may apply (OpenAirDocs) Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment. Historical (superseded or no longer in force): - [AD 2006-15-10](https://openairdocs.org/ad/2006-15-10) (historical): Trimmable horizontal stabilizer actuator (THSA) · Airbus A300-600 Series (all), A300B4-601, A300B4-603 and 17 more. Effective Aug 29, 2006 - [AD 2006-15-09](https://openairdocs.org/ad/2006-15-09) (historical): Wing and center fuel tanks · Airbus A300-600 Series (all), A300 Series (all), A300B4-601 and 18 more. Effective Aug 29, 2006 - [AD 2004-15-16](https://openairdocs.org/ad/2004-15-16) (historical): Wires in the Right-Hand Wing · Airbus A310 Series (all). Effective Sep 3, 2004 - [AD 2004-09-01](https://openairdocs.org/ad/2004-09-01) (historical): Integrated Drive Generator (IDG) Electrical Harness and Pyramid Arm · Airbus A300-600 Series (all), A300 B4-600 Series (all), A300 B4-600R Series (all) and 4 more. Effective May 13, 2004 - [AD 2003-16-15](https://openairdocs.org/ad/2003-16-15) (historical): Honeywell Inertial Reference Units (IRU) · Airbus A300-600 Series (all), A300 B4-600 Series (all), A300 B4-600R Series (all) and 3 more. Effective Sep 22, 2003 - [AD 2002-08-14](https://openairdocs.org/ad/2002-08-14) (historical): Parking Brake Operated Valves (PBOV) · Airbus A300-B2 Series (all), A300-B4 Series (all), A300 B4-600 Series (all) and 4 more. Effective May 8, 2002 - [AD 2000-26-14](https://openairdocs.org/ad/2000-26-14) (historical): Prevent Reduced Structural Integrity · Airbus A310 Series (all). Effective Feb 9, 2001 - [AD 2000-18-07](https://openairdocs.org/ad/2000-18-07) (historical): Transformer Rectifier Units (TRU) · Airbus A300-600 Series (all), A300 Series (all) and A310 Series (all). Effective Oct 13, 2000 - [AD 98-16-11](https://openairdocs.org/ad/98-16-11) (historical): Pylon Trust And Wing Sideload Fitting Inspection · Airbus A300 Model B2-1A, A300 Model B2-1C, A300 Model B2-203 and 12 more. Effective Sep 4, 1998 - [AD 98-14-13](https://openairdocs.org/ad/98-14-13) (historical): Landing Gear · Airbus A300-600 Series (all), A300 Series (all) and A310 Series (all). Effective Aug 12, 1998 - [AD 98-15-51](https://openairdocs.org/ad/98-15-51) (historical): Alternate Braking System · Airbus A300-600 Series (all), A300 Series (all), A310 Series (all) and 5 more. Effective Aug 5, 1998 - [AD 98-01-09](https://openairdocs.org/ad/98-01-09) (historical): Thrust Control Computer · Airbus A300-600 Series (all) and A310 Series (all). Effective Jan 22, 1998 - [AD 97-22-06](https://openairdocs.org/ad/97-22-06) (historical): Ram Air Turbine · Airbus A300-600 Series (all), A300 Series (all) and A310 Series (all). Effective Dec 2, 1997 - [AD 97-18-09](https://openairdocs.org/ad/97-18-09) (historical): Horizontal Stabilizer · Airbus A300-600 Series (all) and A310 Series (all). Effective Oct 3, 1997 - [AD 96-08-07](https://openairdocs.org/ad/96-08-07) (historical): Horizontal Stabilizer · Airbus A300-600 Series (all) and A310 Series (all). Effective May 23, 1996 - [AD 96-01-52](https://openairdocs.org/ad/96-01-52) (historical): Horizontal Stabilizer · Airbus A300-600 Series (all) and A310 Series (all). Effective Feb 5, 1996 - [AD 95-08-07](https://openairdocs.org/ad/95-08-07) (historical): Emergency Exit Door · Airbus A310 Series (all). Effective May 2, 1995 - [AD 95-04-12](https://openairdocs.org/ad/95-04-12) (historical): Lavatory Smoke Detection System · Airbus A300-600 Series (all), A310 Series (all) and A320 Series (all). Effective Mar 17, 1995 - [AD 95-01-51](https://openairdocs.org/ad/95-01-51) (historical): Cockpit Sliding Window · Airbus A300-600 Series (all), A300 Series (all), A310 Series (all) and 2 more. Effective Feb 14, 1995 - [AD 94-26-05](https://openairdocs.org/ad/94-26-05) (historical): Brakes · Airbus A300-600 Series (all), A300 Series (all), A310 Series (all) and 1 more. Effective Jan 23, 1995 - [AD 93-24-51](https://openairdocs.org/ad/93-24-51) (historical): Feel and Limitation Computers · Airbus A300-600 Series (all) and A310 Series (all). Effective Jan 20, 1994 - [AD 90-12-13](https://openairdocs.org/ad/90-12-13) (historical): Rudders · Airbus A300-600 Series (all) and A310 Series (all). Effective Jun 20, 1990 - [AD 88-06-03](https://openairdocs.org/ad/88-06-03) (historical): Rear Pressure Bulkhead · Airbus A310 Series (all). Effective Apr 22, 1988 - [AD 87-16-06](https://openairdocs.org/ad/87-16-06) (historical): Nose Landing Gear · Airbus A300 Series (all) and A310 Series (all). Effective Sep 3, 1987 - [AD T95-01-51](https://openairdocs.org/ad/T95-01-51) (historical): Cockpit Sliding Window · Airbus A300-600 Series (all), A300 Series (all), A310 Series (all) and 2 more ## Registered aircraft None registered with this model now. ## NTSB investigations None matched to aircraft with this model. ## FAA accident and incident reports None matched to aircraft with this model. ## Service difficulty reports (606, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR CA190722001](https://openairdocs.org/sdr/CA190722001), Jul 20, 2019: LINE. LEAKING. (CAN) PILOT REPORTS GREEN SYSTEM LOW QUANTITY MESSAGE ON ECAM, QRH HAS BEEN PERFORMED, QUANTITY LEVEL IS AT THE RED DOT, SAME. DISPATCH FOUND THAT THE AIRCRAFT - [SDR CA190708001](https://openairdocs.org/sdr/CA190708001), Jul 5, 2019: ACTUATOR. FAULTED. (CAN) AT TAKEOFF PHASE, MESSAGE ON ECAM, LDG DOOR NOT CLOSE. AIRCRAFT DIVERT. AS PER INVESTIGATION, FOUND L/H NOSE DOOR UPLOCK FAULT WITH MICROSWITCHES. MICROSW - [SDR CA190401010](https://openairdocs.org/sdr/CA190401010), Mar 31, 2019: CONTROL LEVER. FAULTED. (CAN) AFTER TAKEOFF L/G LEVER INTERLOCK ECAM UNABLE TO RAISE GEAR ON SYSTEM 1 AND 2 ACCOMPLISHED CB RESET #U52 AS PER QRH SYSTEM RESET AND WAS UNSUCCESSFUL ON S - [SDR FDEA201706291786](https://openairdocs.org/sdr/FDEA201706291786), Jun 29, 2017: ACTUATOR. FAILED. DURING CLIMB. RIGHT OUTER TANK DECREASEED TO 3.32 LBS AND RIGHT INNER INCREASEDTO 14.4. LEFT OUTER WAS 6.13 & LEFT INNER WAS 11.91. WAS ABLE TO STOP R/O DECREAS - [SDR FDEA201705011301](https://openairdocs.org/sdr/FDEA201705011301), May 1, 2017: PUMP. INOPERATIVE. IN CRUISE FL360 GOT GREEN HYD SYSTEM OVERHEAT. ECAM ADVISED TO TURN OFF GREEN ENGINE PUMPS 1 AND 2. ENG HYD 1 PUMP SHUT OFF NORMALLY. ENG HYD 2 GREEN PUMP TURNE - [SDR CA151223003](https://openairdocs.org/sdr/CA151223003), Dec 21, 2015: TUBE. BROKEN. (CAN) ENGINE NR 2 THROTTLE JAMMED DUE TO A RUPTURE THRUST REVERSER AIR TUBE. THE SAME TUBE WAS INSTALLED ON SEPT 02, 2015 IN THE EXACT LOCATION FOR THE SAME REA - [SDR FDEA201511083515](https://openairdocs.org/sdr/FDEA201511083515), Nov 8, 2015: BATTERY PACK. DISCHARGED. EMERGENCY LIGHTS WILL NOT TEST IN COURIER AREA. R & R EMER POWER SUPPLY BATTERY PACK IAW AMM 33-51-14-4. OPERATIONS CHECKED GOOD. PART NAME, EMER POWER, BATTERY - [SDR FDEA201504141229](https://openairdocs.org/sdr/FDEA201504141229), Apr 14, 2015: CROSSBEAM. CORRODED. AFT CARGO CROSSBEAM RT SIDE FITTING, CORRODED AT FRAME 62. REPLACED THE RT SIDE CORRODED FITTING, CROSSBEAM, IAW SRM 51-40-21. - [SDR FDEA201402110305](https://openairdocs.org/sdr/FDEA201402110305), Feb 11, 2014: RELAY. BURNED. FIRST OFFICER`S TAT PROBE, FAULT LIGHT ON AT FL300, ECAM MONITOR. 5 MINS LATER SMELL OF ELEC ORIGIN, NO VISUAL SMOKE, ODOR GONE AFTER LANDING. FOUND DET SENSOR - [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 FDEA201301230166](https://openairdocs.org/sdr/FDEA201301230166), Jan 23, 2013: ADAPTER. DAMAGED. IMPACT DAMAGE AT SCALLOP REMOVED CLEVIS ADAPTER BETWEEN SEAT TRACK 2R & 3R AT FR 54.2 IAW SRM 51-72-10 MATCH DRILLED REAMED NEW CLEVIS ADAPTER IAW SRM 51-40-44. - [SDR CA110719003](https://openairdocs.org/sdr/CA110719003), Jul 18, 2011: BEARING. SEIZED. ON CLIMB OUT, ON FLAP RETRACTION, CREW RECEIVED A FLAP SYS 1 & 2 FAULT WITH FLAP JAM MESSAGE. ACFT RETURNED TO DEPARTURE AIRPORT AND LANDING WAS UNEVENTFUL. INV - [SDR FDEA201101040006](https://openairdocs.org/sdr/FDEA201101040006), Jan 4, 2011: SKIN. DENTED. LEFT INBOARD FLAP LOWER SKIN IS DENTED 70" FROM THE INBOARD EDGE AND 40" FROM THE TRAILING EDGE. DAMAGED AREA FOUND TO BE OUT OF LIMITS IAW A310-200 57-52-12, F - [SDR FDEA201012034563](https://openairdocs.org/sdr/FDEA201012034563), Dec 3, 2010: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT STRUCTURE, Y 450, HAS CORROSION FROM 6" INCHES AFT OF FR 14 TO 8" INCHES FWD OF FR 14 ON THE TOPSIDE. R & R FLOOR SUPPORT STRUCTURE Y450, FROM FR - [SDR FDEA201010214133](https://openairdocs.org/sdr/FDEA201010214133), Oct 21, 2010: SKIN. DENTED. PREVIOUS REPAIRED DENTS NOT LISTED IN THE MCMRT AT RT FLAP INBD LOWER SKIN. DENT 1 - BTW RIB 5 & RIB 6 AND BTW FRONT SPAR & STRINGER 9. DENT 2 AND DENT 3 - BTW - [SDR FDEA201010053934](https://openairdocs.org/sdr/FDEA201010053934), Oct 5, 2010: LUG. CORRODED. FOUND CORROSION IN RT MAIN LANDING GEAR FORWARD LUG AT RIB 5 DURING RIB 5 INSPECTION. REMOVED CORROSION BY OVERSIZING THE BORE AND SPOTFACING THE SURFACES, PERF - [SDR FDEA201010023862](https://openairdocs.org/sdr/FDEA201010023862), Oct 2, 2010: SKIN. CORRODED. RIGHT ELEVATOR UPPER SKIN AFT EDGE FOUND CORROSIN. REMOVE TOP SKIN UNTIL THE REAR SPAR. PERFORM SRM 55-21-11 CONG-1 FIG 209 WITH THE FOLLOWING PROVISIONS: INSTA - [SDR FDEA201010013848](https://openairdocs.org/sdr/FDEA201010013848), Oct 1, 2010: FRAME. CORRODED. FOUND LEVEL ONE CORROSION IN LOWER FORWARD CARGO COMPARTMENT AROUND MANHOLE COVER BETWEEN FRAME 38.1 AND FRAME 38.2, FROM STR 53L TO STR 53R. REMOVED CORRODIED - [SDR FDEA201009303821](https://openairdocs.org/sdr/FDEA201009303821), Sep 30, 2010: FILTER. LEAKING. DURING DESCENT RECEIVED ECAM GREEN HYD SYS LOW LEVEL WARNING. HYD QUANTITY ON OVERHEAD PANEL INDICATED ZERO. CONSULTED THE QRH AND MANUALLY EXTENDED THE LANDING - [SDR FDEA201007292716](https://openairdocs.org/sdr/FDEA201007292716), Jul 29, 2010: SELECTOR VALVE. FAILED. L/G WOULD NOT RETRACT. COMPLIED WITH ECAM AND QRH. RETURNED TO DEPARTURE. PERFORMED PROX DETECTOR PROCESSING UNIT MEMORY RECALL IAW TSM 32-61-00. FOUND MEMORY E - [SDR FDEA201007082404](https://openairdocs.org/sdr/FDEA201007082404), Jul 8, 2010: UNKNOWN. MULTIPLE FAIL. AFTER TAKEOFF GEAR WOULD NOT RETRACT USING SYS 2 OR SYS1. TRANSPONDER REPORTED INOP BY DEPARTURE. ACFT WOULD NOT PRESSURIZE. AUTO THROTTLES INOP. AUTOPILOTS WHE - [SDR FDEA201006272203](https://openairdocs.org/sdr/FDEA201006272203), Jun 27, 2010: AUTOTHROTTLE SYS. MALFUNCTIONED. ON TAKE OFF WITH ONLY NR 2 ATS OPERATIVE, THE NR 2 THROTTLE KEPT TRYING TO ADVANCE TO FIREWALL AFTER 90 KNOTS, EGT WENT UP TO 940, T/0 ABORTED AT 100 KIAS, BRAK - [SDR FDEA200908143019](https://openairdocs.org/sdr/FDEA200908143019), Aug 14, 2009: FLOOR SUPPORT. CORRODED. FWD CABIN FLOOR STRUCTURE - SUPPORT FLOOR AT Y730 BTW FR12A AND 13A FOUND CORRODED. SUPPORT FLOOR REPLACED IAW SRM 51-72-10. - [SDR FDEA200908072945](https://openairdocs.org/sdr/FDEA200908072945), Aug 7, 2009: GEARBOX. LEAKING. SLAT SYS 1 & 2 FAULT DURING ACFT CONFIGURATION REMOVED AND REPLACED LEFT WING SLAT NR 2 LINE GEARBOX PER AMM 27-84-16. REMOVED AND REPLACED RT WING SLAT IN LINE - [SDR FDEA200907233101](https://openairdocs.org/sdr/FDEA200907233101), Jul 23, 2009: TRUNNION. DAMAGED. LT WING - NR 1 EXTERIOR TRUNNION FOUND DAMAGED. THE AFFECTED TRUNNION WAS REPAIRED IAW CMM 57-53-12. - [SDR FDEA200907022465](https://openairdocs.org/sdr/FDEA200907022465), Jul 2, 2009: SKIN. DENTED. ON WALK AROUND FOUND DENT ON LOWER FUSELAGEAFT OF RADOME BETWEEN FRAME O AND FRAME 1 CUT OUT DAMAGED AREA IAW A310 SRM 53-11-12 FIG. 201. INSTALLED PERMANENT RE - [SDR FDEA200903301736](https://openairdocs.org/sdr/FDEA200903301736), Mar 30, 2009: HINGE FITTING. CORRODED. AFT CARGO DOOR HINGE FITTING WAS FOUND WITH CORROSION AT FRAME 62. THE FITTING WAS REPAIRED AS PER FEDEX EA 6-5310-129288. - [SDR FDEA200903261074](https://openairdocs.org/sdr/FDEA200903261074), Mar 26, 2009: FLOOR PANEL. DAMAGED. CABIN FLOOR PANEL 242 LK IS BROKEN. REPAIRED PANEL 242 LK WITH THE FABRICATION OF A NEW PANEL USING THE OLD PANEL AS A TEMPLATE IAW DWG SRZ25-005; REV "H". - [SDR FDEA200903261073](https://openairdocs.org/sdr/FDEA200903261073), Mar 26, 2009: FLOOR PANEL. CRACKED. CABIN FLOOR BOARD 282 KF IS CRACKED. REPAIRED PANEL 282 KF WITH THE FABRICATION OF A NEW PANEL USING THE OLD PANEL AS A TEMPLATE IAW DWG SRZ25-005; REV "H". - [SDR FDEA200903261056](https://openairdocs.org/sdr/FDEA200903261056), Mar 26, 2009: FLOOR PANEL. DAMAGED. FWD CARGO COMPARTMENT FLOOR PANEL 132 RF IS CRACKED AT THE PDU CUTOUT. REPAIRED PANEL 132 RF WITH THE FABRICATION OF A NEW PANEL USING THE OLD PANEL AS A TEMPLA - [SDR FDEA200903261052](https://openairdocs.org/sdr/FDEA200903261052), Mar 26, 2009: FLOOR PANEL. DAMAGED. FWD CARGO COMPARTMENT FLOOR PANEL 131 RF IS BROKEN AT THE PDU CUTOUT. REPAIRED PANEL 131 RF WITH THE FABRICATION OF A NEW PANEL USING THE OLD PANEL AS A TEMPLAT - [SDR FDEA200903261070](https://openairdocs.org/sdr/FDEA200903261070), Mar 26, 2009: SILL. CORRODED. MAIN DECK, R-2 DOOR SILL AREA HAS A STRINGER ANGLE CORRODED AT FRAME 74, BS 3998 THRU 4005; STRINGER 26R. REMOVED CORROSION IN REF TO SRM 51-74-40. ORIGINAL MAT - [SDR FDEA200903261069](https://openairdocs.org/sdr/FDEA200903261069), Mar 26, 2009: FLOOR PANEL. PUNCTURED. AFT CARGO COMPARTMENT FLOOR PANEL 152 AF HAS MULTIPLE PUNCTURES ON THE BACK. REPAIRED PANEL 152 AF WITH THE FABRICATION OF A NEW PANEL USING THE OLD PANEL AS A - [SDR FDEA200903261068](https://openairdocs.org/sdr/FDEA200903261068), Mar 26, 2009: FLOOR PANEL. DELAMINATED. AFT CARGO COMPARTMENT FLOOR PANEL 152 FF HAS DELAMINATION AND EDGE DAMAGE. REPAIRED PANEL 152 FF WITH THE FABRICATION OF A NEW PANEL USING THE OLD PANEL AS A TE - [SDR FDEA200903261064](https://openairdocs.org/sdr/FDEA200903261064), Mar 26, 2009: FLOOR PANEL. PUNCTURED. BULK CARGO COMPARTMENT FLOOR PANEL 162 DF IS PUNCTURED. FABRICATED NEW FLOOR PANEL AND TOP SHEET IAW SRZ 25-005, REV "H" & SRZ 25-055, REV "C". - [SDR FDEA200903251742](https://openairdocs.org/sdr/FDEA200903251742), Mar 25, 2009: SKIN. CORRODED. CENTER WING BOX LOWER SKIN EXTERNAL SURFACE FOUND WITH SEVERAL SPOTS OF CORROSION - REFER TO EA6-5710-129280 FOR DETAILS. REPAIR WAS ACCOMPLISHED AS PER EA 6-57 - [SDR FDEA200903241734](https://openairdocs.org/sdr/FDEA200903241734), Mar 24, 2009: BEAM. CORRODED. RT FWD PAX DOOR - SPOTS OF CORROSION AT BEAM 3. BEAM 3 WAS REPLACED AS PER SRM 51-72-10. - [SDR FDEA200901120164](https://openairdocs.org/sdr/FDEA200901120164), Jan 12, 2009: FLOOR PANEL. DAMAGED. MAIN CARGO DECK COMPARTMENT, ZONE 231 FLOOR PANEL 231 XH HAS STRUCTURAL DAMAGES FABRICATED NEW MAIN DECK CARGO COMPARTMENT FLOOR PANEL 231 XH PER SAMPLE IAW SRZ - [SDR FDEA200901120163](https://openairdocs.org/sdr/FDEA200901120163), Jan 12, 2009: FLOOR PANEL. DAMAGED. MANI DECK CARGO COMPARTMENT,ZONE 251 FLOOR PANEL 251 ZH HAS STRUCTURAL DAMAGES. FABRICATED NEW MAIN DECK CARGO COMPARTMENT FLOOR PANEL 251 ZH PER SAMPLE IAW SRZ - [SDR FDEA200901060044](https://openairdocs.org/sdr/FDEA200901060044), Jan 6, 2009: FITTING. INOPERATIVE. RIGHT MLG FWD TRUNNION WILL NOT TAKE GREASE. COMPLIED WITH E.A. 6-3210-123696. - [SDR FDEA200901050031](https://openairdocs.org/sdr/FDEA200901050031), Jan 5, 2009: FLOOR PANEL. DAMAGED. MAIN DECK CARGO COMPARTMENT FLOOR PANEL IS DAMAGED BETWEEN FRAME 41 AND FRAME 43; RBL 31.0. - [SDR FDEA200901020005](https://openairdocs.org/sdr/FDEA200901020005), Jan 2, 2009: SKIN. DENTED. THE L-3 DOOR OUTER SKIN HAS 1 DENT AT FRAME 75 AND STR 25L. CHECKED DENT & FOUND IT TO BE OUT OF LIMITS IN REF TO SRM 52-10-00; FIG 102. REMOVED DAMAGED AREA & - [SDR FDEA200901020004](https://openairdocs.org/sdr/FDEA200901020004), Jan 2, 2009: SKIN. DENTED. THE L-3 DOOR OUTER SKIN HAS 1 SMALL DENT; AFT OF FRAME 74 AND STRINGER 26L. CHECKED DENT & FOUND IT TO BE OUT OF LIMITS IN REF TO SRM 52-10-00; FIG 102. REMOVED - [SDR FDEA200812315322](https://openairdocs.org/sdr/FDEA200812315322), Dec 31, 2008: SENSOR. MALFUNCTIONED. AFTER T/O LANDING GEAR FAILED TO RETRACT. ECAM DISPLAYED L/G RETRACTION INOP. ACFT LOST AUTO-THROTTLES. FOUND TARGET SENSORS 9GA AND 11GA LOS SE AND OUT OF "C" - [SDR FDEA200812305320](https://openairdocs.org/sdr/FDEA200812305320), Dec 30, 2008: FLOOR PANEL. CRACKED. FWD CARGO COMPARTMENT FLOOR PANELS, ZONE 131, FLOOR PANEL 131 HG HAS STRUCTURAL DAMAGES FABRICATED NEW FWD CARGO COMPARTMENT FLOOR PANEL, IAW SAMPLE,PANEL 131 H - [SDR FDEA200812245291](https://openairdocs.org/sdr/FDEA200812245291), Dec 24, 2008: SHEAR TIE. CORRODED. FWD PIT BILGE FRAME NR 37 BETWEEN STRINGER 51L AND STRINGER 52L SHEAR TIE HAS CORROSION ON THE AFT SURFACE. REMOVED SHEAR TIE FROM FRAME 37 IAW SRM 51-40-21. RE - [SDR FDEA200812205246](https://openairdocs.org/sdr/FDEA200812205246), Dec 20, 2008: FLOOR PANEL. DELAMINATED. L/H TAIL COMPARTMENT FLOORBOARD IS DELAMINATED AT THE AFT CORNER ACCESS THRU 312 AR. FABBED A NEW FLOOR PANEL USING THE OLD PANEL AS A TEMPLATE. MATERIAL ID; LO - [SDR FDEA200812205251](https://openairdocs.org/sdr/FDEA200812205251), Dec 20, 2008: FLOOR PANEL. DAMAGED. MAIN CABIN FLOOR PANEL 242 RJ IS DAMAGED. FABBED NEW PANEL USING THE OLD PANEL AS A TEMPLATE. MATERIAL ID; LOCATED HOLES USING THE THE OLD PANEL; COUNTERBORED H - [SDR FDEA200812205250](https://openairdocs.org/sdr/FDEA200812205250), Dec 20, 2008: FLOOR PANEL. DENTED. FWD CARGO PIT FLOOR PANEL 132 ZF IS DAMAGED. FABBED NEW PANEL USING THE OLD PANEL AS A TEMPLATE. MATERIAL ID; LOCATED HOLES USING THE THE OLD PANEL; COUNTERBORE - [SDR FDEA200812205249](https://openairdocs.org/sdr/FDEA200812205249), Dec 20, 2008: FLOOR PANEL. DENTED. BULK CARGO PIT FLOOR PANEL 162 HF HAS SEVERAL DENTS. FABBED NEW PANEL USING THE OLD PANEL AS A TEMPLATE. MATERIAL ID; LOCATED HOLES USING THE THE OLD PANEL; COU All 606: https://openairdocs.org/model/airbus-a310/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.