Airbus A310-324

Service difficulty reports · 1,439

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duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = 'A310324'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR FDEA201201080045Seat Track · chafedMAIN DECK SEAT TRACK CHAFED BETWEEN FR 54.2 AND FR 54.3, Y1456. FABRICATED THE SEAT TRACK IAW SRM 51-40-21 AND DWG NR 16, A53274256. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jan 8, 2012 · N804FD · Airbus A310324 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201112295456Oil System · overtempNR 2 ENG, HIGH OIL TEMP - ABOVE 180 DEG - SHUT ENG DOWN. ALL OTHER ENG PARAMETERS OK. INSPECTED NR2 ENG INLET & EXHAUST AREA; NIL ABNORMALTIES NOTED. VISUAL CK OIL QTY; NORMAL. R & R NR 2 ENGINE IAW WC 44T0105-2 AND 44T0708-2. RUN ENG IAW JRH LEAK CHECKEDDec 29, 2011 · N808FD · Airbus A310324 · Turbine Engine Oil SystemSDR FDEA201111305081Controller · inoperativeACFT CABIN PRESS CLIMB ABOVE 10000. REQUESTED LOWER ALTITUDE FROM ATC. BRIEFING WITH FLIGHT CREW, NO WARNING MESSAGE DISPLAYED ON ECAM. PERFORMED CPC 1 AND CPC 2 OPS TEST SATIS IAW AMM21-31-00-05-0. R & R THE NR 2 CPC IAW AMM21-31-11-04-0, AND PERFORMED THNov 30, 2011 · N811FD · Airbus A310324 · Cabin Pressure ControllerSDR FDEA201110214611Battery · inoperativeR1 DOOR WILL NOT ARM. R & R THE EMERGENCY POWER SUPPLY BATTERY NR 1 AND NR 2, AND THE AUTO STANDBY UNIT IAW AMM 52-73-18-04-0, AND PERFORMED THE TEST IAW AMM 52-73-00, P BLOCK 501, TESTED NORMAL. ECAM SLIDE DOOR R1 INDICATION NORMAL. AC OK FOR SVC. R & R BOct 21, 2011 · N811FD · Airbus A310324 · Escape SlideSDR FDEA201110174555Engine · failedCLIMBING THRU FL300 F/O FELT SLIGHT VIBRATION, BUT NO INDICATIOINS OR ECAM AT FL 355, THERE WAS A YAW AND LOUD BANGING, EPR HAD DROPPED TO BELOW 1, OTHER ENGINE INSTRUMENTS LOOKED NORMAL, BUT THE LOUD BANGING CONTINUED WITH THROTTLE AT IDLE. OIL PRESSURE WASOct 17, 2011 · N804FD · Airbus A310324 · Engine (Turbine/Turboprop)SDR FDEA201110154517Skin · corrodedLEFT WING TOP SKIN CORRODED AT REAR SPAR RIB 4. ACCOMPLISHED REPAIR IAW EA 6-5730-149020. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Oct 15, 2011 · N801FD · Airbus A310324 · Wing, Plate/SkinSDR FDEA201110154518Skin · corrodedFORWARD CARGO COMPARTMENT BILGE AREA OF S45R, SKIN CORRODED BETWEEN FR 38.2 AND FR 39. CUT OUT THE DAMAGED AREA. REPAIRED WITH DOUBLER AND FASTENERS IAW SRM 53-10-14. REPAIR CLASSIFIED AS MAJOR IAW G.M.M. 6-2-100.Oct 15, 2011 · N801FD · Airbus A310324 · Fuselage Main, Plate/SkinSDR FDEA201110154523Floor Panel · dentedCARGO COMPARTMENT 162HF FLOOR PANEL DENTED. REMOVED FLOOR PANEL IAW AMM 53-10-35-04. FABRICATED A NEW FLOOR PANEL IAW SRM 53-10-20, AND DRAWING 47 A532799620. REPAIR CLASSIFIED AS MINOR IAW G.M.M. 6-2-100. INSTALLED FLOOR PANEL IAW AMM 53-10-35-04.Oct 15, 2011 · N801FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201110154522Floor Panel · brokenCARGO COMPARTMENT 161GF FLOOR PANEL BROKEN. REMOVED FLOOR PANEL IAW AMM 53-10-35-04. FABRICATED A NEW FLOOR PANEL IAW SRM 53-10-20, AND DRAWING 48 A532799630. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. INSTALLED FLOOR PANEL IAW AMM 53-10-35-04.Oct 15, 2011 · N801FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201110154521Floor Panel · dentedCARGO COMPARTMENT 161BF FLOOR PANEL DENTED. REMOVED FLOOR PANEL IAW AMM 53-10-35-04. FABRICATED A NEW FLOOR PANEL IAW SRM 53-10-20, AND DRAWING 50 A532799650. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. INSTALLED FLOOR PANEL IAW AMM 53-10-30-04.Oct 15, 2011 · N801FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201110154520Floor Panel · damagedBULK CARGO COMPARTMENT 162AF FLOOR PANEL UPPER SKIN DAMAGED. REMOVED FLOOR PANEL IAW AMM 53-10-35-04. FABRICATED A NEW FLOOR PANEL IAW SRM 53-10-20, AND DRAWING 51 A532799660. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. INSTALLED FLOOR PANEL IAW AMM 53-10-Oct 15, 2011 · N801FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201110154516Floor Panel · dentedMAIN DECK CARGO COMPARTMENT FLOOR PANEL 242UJ DENTED. REMOVED FLOOR PANEL IAW AMM 53-10-25-04. FABRICATED A FLOOR PANEL IAW SRM 53-10-20, AND DRAWING 27-R532B1231001. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. INSTALLED FLOOR PANEL IAW AMM 53-10-25-04.Oct 15, 2011 · N801FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201110154515Floor Panel · dentedMAIN DECK CARGO COMPARTMENT FLOOR PANEL 242EK DENTED. REMOVED FLOOR PANEL IAW AMM 53-10-25-04. FABRICATED A NEW FLOOR PANEL IAW SRM 53-10-20, AND DRAWING 85-R532B1231003. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. INSTALLED FLOOR PANEL IAW AMM 53-10-25-Oct 15, 2011 · N801FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201110154514Floor Panel · dentedMAIN DECK CARGO COMPARTMENT FLOOR PANEL 252GF DENTED. REMOVED FLOOR PANEL IAW AMM 53-10-25-04. FABRICATED A NEW PANEL IAW SRM 53-10-20, AND DRAWING 09-R532B1175009. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. INSTALLED FLOOR PANEL IAW AMM 53-10-25-04.Oct 15, 2011 · N801FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201110154513Floor Panel · dentedMAIN DECK CARGO COMPARTMENT FLOOR PANEL 252PH DENTED. REMOVED FLOOR PANEL IAW AMM 53-10-25-04. FABRICATED A NEW FLOOR PANEL IAW SRM 53-10-20, AND DRAWING 21-B53270276015. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. INSTALLED FLOOR PANEL IAW AMM 53-10-25-0Oct 15, 2011 · N801FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201110154512Floor Panel · dentedMAIN DECK CARGO COMPARTMENT FLOOR PANEL 252UH DENTED. REMOVED FLOOR PANEL IAW AMM 53-10-25-04. FABRICATED A NEW FLOOR PANEL IAW SRM 53-10-20, AND DRAWING 34-R532B1177004. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. INSTALLED FLOOR PANEL IAW AMM 53-10-25-04Oct 15, 2011 · N801FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201110094389Skin · puncturedLT WING INBD FLAP LWR SKIN JUST AFT OF THE CARRIAGE FOUND PUNCTURED. CUT OUT THE DAMAGED LOWER SKIN PER SRM 57-52-12/201 FIG205.Oct 9, 2011 · N813FD · Airbus A310324 · Trailing Edge FlapsSDR FDEA201109294213Solenoid Valve · leakingGREEN HYD SYS LO RSVR INDICATION INFLIGHT FOLLOWED QRH, AFTER LANDING GREEN SYS REVR INDICATION RETURNED TO NORMAL. RESTORED FREE FALL EXTENSION SYSTEM TO NORMAL CONDITION AS PER AMM 32-33-00-2. PRESSURED GREEN HYD SYS AS PER AMM29-00-00-06, FOUND KRUEGER SSep 29, 2011 · N812FD · Airbus A310324 · Hydraulic Indicating SystemSDR FDEA201109284176Skin · chafedFLUSH DOUBLER REPAIR ON L/E OF D-NOSE SKIN CHAFED AT TRACK NR 1. REPAIRED IAW EA6-5741-103419Sep 28, 2011 · N813FD · Airbus A310324 · Wing, Plate/SkinSDR FDEA201109274146Fitting · corrodedNR 1 ENG PYLON SPIGOT RECEPTACLE UPPER AND LOWER FITTING CORRODED. REMOVED THE SPIGOT FITTINGS PER SRM51-40-21 MACHINE THE MATING SURFACE OF THE NEW SPIGOT LOWER FITTING PER DWG A54611053. HORNED THE BORES C/T THE LOWER AND UPPER SPIGOT FITTINGS PER DWG A54Sep 27, 2011 · N813FD · Airbus A310324 · Nacelle/Pylon Miscellaneous StructureSDR FDEA201109264124Skin · scratchedLEFT WING OTBD FLAP UPPER SURFACE NEAR FLAP TRACK NR 3, FOUND SURFACE WITH 8" SCRATCH MARK UNDER RUBSTRIP. REPLACED THE O/B FLAP PER AMM 27-50-12-04-0Sep 26, 2011 · N805FD · Airbus A310324 · Trailing Edge FlapsSDR FDEA201109244113Angle · crackedCENTER WING FUEL TANK REAR SPAR INNER ANGLE FOUND CRACKED. REPAIRED IAW SRM 51-40-44, EO 6-5710-7-3322 &SRM 51-40-21. NO CRACK FOUND IAW NTM51-10-18.Sep 24, 2011 · N813FD · Airbus A310324 · Wing Miscellaneous StructureSDR FDEA201109203976Cabin Pressure · malfunctionedRED CABIN ALTITUDE WARNING, PERFORMED DESCENT TO 10,000 FT ON CABIN PRESSURE SYS PAGE, BOTH OUTFLOW VALVES SHOW AMBER & FULL OPEN - NO ECAM MESSAGE, CABIN ALTITUDE 10,000 FT. UNABLE TO CONTROL CABIN ALTITUDE . PACK VALVES SHOW AMBER AND CLOSED INTERMITTENTSep 20, 2011 · N808FD · Airbus A310324 · Cabin Pressure Control SystemSDR FDEA201109193958Angle · crackedCENTER WING FUEL TANK REAR SPAR INTERNAL ANGLE FOUND CRACKED. COMPLIED WITH EA 6-5710-153425. REAMED HOLE IAW EA:6-5710-7-3322, B1, PART 1.Sep 19, 2011 · N813FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR FDEA201109163902Slat Track · damagedLEFT WING SLAT NR 3, NR 9 TRACK BLEND OUT AREA EXCEEDED THE LIMITS (WIDTH=56.21MM). COMPLIED WITH EA 6-5741-103381, PART 3. REPLACED SLAT TRACK IAW AMM27-80-14-04. PERFORMED TEST OF SLAT IAW AMM27-80-14-04. TESTED OK.Sep 16, 2011 · N813FD · Airbus A310324 · Wing, Attach FittingsSDR FDEA201108273530Power Supply · failedL1 & R1 DOORS ESCAPE SLIDE RELEASE WARNING LIGHTS SYSTEM INOPERATIVE. R & R AUTONOMOUS STANDBY POWER SUPPLY UNIT (70WN). OPS CHECKED GOOD REF MM 52-73-18-04. OK FOR SERVICE.Aug 27, 2011 · N807FD · Airbus A310324 · Door Warning SystemSDR FDEA201108103196Indicator · failedAT ALTITUDE CABIN PRESSURE INDICATED 20460 AND COMMANDED DESCENT. DONED MASKS AND DESECNDED TO 10K, DIVERTED. CABIN PRESS INDICATIONS DELTA P XX (ORANGE) V/S= 2950 (ORANGE) CABIN ALTITUDE 20460 (RED) WHEN EVENT OCCURRED BOTH CREW HAD EARS POP. BELL SOUNDEAug 10, 2011 · N811FD · Airbus A310324 · Cabin Pressure Control SystemSDR FDEA201108103195Controller · failedAT ALTITUDE CABIN PRESSURE INDICATED 20460 AND COMMANDED DESCENT. DONED MASKS AND DESCENDED TO 10K, DIVERTED. CABIN PRESS INDICATIONS DELTA P XX (ORANGE) V/S= 2950 (ORANGE) CABIN ALTITUDE 20460 (RED) WHEN EVENT OCCURRED BOTH CREW HAD EARS POP. BELL SOUNDEAug 10, 2011 · N811FD · Airbus A310324 · Cabin Pressure Control SystemSDR FDEA201106122214Thrust Reverser · malfunctionedAT APPRX 70KTS, NR 2 THRUST REVERSER UNLOCK AMBER LIGHT ON. REJECTED T/O, AFTER STOWING THRUST REVERSER, LIGHT OUT. REVERSER APPEARED TO OPERATE NORMAL. RELEASED FOR SERVICE PER MEL. PERFORMED TROUBLESHOOTING AS PER AMM 78-30-00-02. CARRIED OUT RIGGINGJun 12, 2011 · N805FD · Airbus A310324 · Engine Thrust ReverserSDR FDEA201106062200Battery · inoperativeCOURIER COMPARTMENT EMERGENCY LIGHT TEST INOP. R & R 29WL1 POWER SUPPLY BATTERY IAW MM 33-55-00-05, NO HELP, REINSTALLED ORIGINAL BATTERY, SUSPECT POWER SUPPLY UNIT 29WL1 BAD. R & R PWR SUPPLY MM 33-55-00-05. NO HELP, SUSPECT BATTERY. PREMATURE REMOVAL/IJun 6, 2011 · N809FD · Airbus A310324 · Emergency LightingSDR FDEA201105292020Skin · delaminatedTHERMOGRAPHY AND ULTRASONIC INSP CARRIED OUT FOUND TRAPPED WATER ON RT RUDDER SKIN AT T/E BELOW NR 37 SCREW LINE AREAS APPROX 600 SQ MM. ACCOMPLISHED EA 6-5540-150322.May 29, 2011 · N809FD · Airbus A310324 · Rudder, Plate/SkinSDR FDEA201105171851Transmitter · leakingLOST YELLOW SYS HYD ENROUTE. COMPLIED WITH ECAM & QRH. HYD FLUID LEAKING FROM YELLOW HYD SYS PRESSURE TRANSMITTER 16WV HSG CAP & CGO DOOR HYD SELECTOR VALVE 10MJ THE CONTROL SHAFT. R & I 16WV & 10MJ ASSY, REPLENISH YELLOW HYD RESERVOIR & LEAK CHECKED OK, May 17, 2011 · N806FD · Airbus A310324 · Hydraulic Indicating SystemSDR FDEA201105141841Stringer · corrodedFUSELAGE AFT PRESSURE BULKHEAD FORWARD FACE AT RIGHT HAND STGR 31 FOUND STRINGER END TOP SURFACE WITH CORROSION FUSELAGE AFT PRESSURE BULKHEAD FORWARD FACE AT RIGHT HAND STGR 31 STRINGER END CORRODED PART REMOVED AND REPALCED PER A310-300 SRM 51-40-21 AND SRMay 14, 2011 · N809FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR FDEA201105141840Stringer · corrodedFUSELAGE AFT PRESSURE BULKHEAD FORWARD FACE AT RIGHT HAND STGR28 FOUND STRINGER END TOP SURFACE WITH CORROSION FUSELAGE AFT PRESSURE BULKHEAD FORWARD FACE AT RIGH HAND STGR28 CORRODED STRINGER END REMOVED AND REPLACED GER SRM 51-40-21 AND 51-72-10 REV 79. May 14, 2011 · N809FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR FDEA201104182042Battery · failedON PREDISPATCH CK, FOUND ON COURIER COMPARTMENT EMERGENCY LT TEST INOP. REMOVED AND REPLACED EMG POWER SUPPLY UNIT AND EMERGENCY SUPPLY BATTERY, REF MM 33-51-14-04-09. OPS CK GOOD. OK FOR SERVICE. (CLOSED)Apr 18, 2011 · N807FD · Airbus A310324 · Emergency LightingSDR FDEA201104171509Slide · unwanted deployRT CABIN DOOR INADVERTENTLY OPENED IN ARMED CONDITION. RELEASED FOR SERVICE IAW MEL: 52-11-01-02 CATEGORY: C EXPIRATION: 27APR11, "MEL 52-11-01-02: R1 CREW ENTRY ESCAPE SLIDE -INOP. THE R1 DOOR ESCAPE SLIDE ASSY IS REMOVED FROM ACFT IAW EA 6-5210-150158, SApr 17, 2011 · N815FD · Airbus A310324 · Escape SlideSDR 2011FA0000222Jackscrew · out of positionDURING O/H, MX PERFORMED ON THE SCREW JACK ASSY, FE140 SN 125, IDENTIFICATION OF THE WRONG POSITIONING OF THE RATCHET WHEEL (ITEM 3-620 OF CMM 27-44-13), ASSEMBLED ON THE OPPOSITE POSITION COMPARED TO THE SPEC MENTIONED ON THE CMM 27-44-13. LETTER LT-S9-11-10Feb 18, 2011 · N807FD · Airbus A310324 · Stabilizer Control SystemSDR FDEA201102040472Outflow Valve · failed1 HR INTO FLIGHT, CABIN PRESSURE EXCEEDED TOLERANCE (AROUND 9.0 ON DEFFERENTIAL PRESSURE) AND BOTH CONTROLLERS FAILED. HAD TO SELECT MANUAL AGAIN TO BRING PRESSURE BACK DOWN. REACTIVED AFT OUTFLOW VALVE IAW MEL21-31-04-01-A, PERFORMED BITE TEST FOUND "AFT VAFeb 4, 2011 · N810FD · Airbus A310324 · Pressure Regulator/Outflow ValveSDR FDEA201102010448Fluid · odorON TAKEOFF AT 4000FT. ECAM ALERT OF MAIN DECK CARGO SMOKE. FOLLOWED QRH AND RETURNED TO DEPARTURE. WE HAD EXTENSIVE ICE ON ACFT WHICH REQUIRED 1 HR 45 MIN OF DEICING. EMERGENCY DECLARED. IAW CREW DEBRIEF, SMOKE INDICATIONS CEASED. VERY STRONG ODOR OF DEICFeb 1, 2011 · N813FD · Airbus A310324 · Air Distribution SystemSDR FDEA201012204727Power Supply · failedEMERGENCY LIGHTS FAIL OPS CHECK FROM COURIER AREA TEST SWITCH. R & R THE POWER SUPPLY UNIT AND BATTERY IAW AMM 33-51-14-04. PERFORMED A SATISFACTORY TEST OF THE EMERGENCY LIGHTS IAW AMM 33-51-14-04.Dec 20, 2010 · N803FD · Airbus A310324 · Emergency LightingSDR FDEA201012164699Rib · damagedLT WING T/E RIB AT WIAX 62.70 HAS EDGE DAMAGE ON THE SPAR ATTACH FLANGE. REMOVED DAMAGE FROM THE SPAR AREA IAW EA 6-5730-136705.Dec 16, 2010 · N803FD · Airbus A310324 · Wing, Rib/BulkheadSDR FDEA201011194431Limiter · failedSLATS SYS 1 AND SLATS SYS 2 FLAPS, REPEAT ITEM, NO SLATS LANDING. PERFORMED LGAV, T/S SYS IAW FIM 27-80-02, FIG 101, SHEET 1. FOUND TORQUE LIMITER POPED. R AND R TORQUE LIMITER IAW MM 27-84-12-04. ALSO SERVICED LT WING SLATS, SCREW JACKS AND GEAR BOXES INov 19, 2010 · N801FD · Airbus A310324 · Leading Edge Slat Control SystemSDR FDEA201011164400Skin · corrodedFUSELAGE 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 51-21-10. MEASURE REMAIN THICKNESS OF THE REWORKED AREA IAW NTM51-10-04 (REMAINING THICKNESS WANov 16, 2010 · N812FD · Airbus A310324 · Fuselage Main, Plate/SkinSDR FDEA201011034244Crossbeam · corrodedFR63 AFT CARGO LBL 10 "T" EXTRUSION EXFOLIATED ON LOWER FWD SIDE INSTALLED SPLICE REPAIR "T EXTRUSION AND L EXTRUSION" AT FR63 AFT CARGO LBL 10 TO RBL 12 ON LOWER FWD SIDE IAW SRM 53-10-15, PAGE 259/260, FIGURE 209, SHEET 1.Nov 3, 2010 · N815FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR FDEA201010284182Panel · crackedNR 2 PYLON OTBD SIDE AT RIB 8 FWD SCEW HOLE HAS A 0.250 CRACK GOING UPWARDS. TRIMMED OUT CRACK AND REPAIRED PYLON NR 2 SIDE PANEL IAW SRM 54-51-31 FO\IG 201 PAGE 203 TO 207. THIS REPAIR MUST BE INSPECTED AT DEFINED INTERVALS . THE INSP INSTRUCTION REF IS Oct 28, 2010 · N815FD · Airbus A310324 · Nacelle/Pylon, Plate/SkinSDR FDEA201010284181Fitting · corrodedNR1 ENG PYLON RIB 18 FWD SIDE CORRODED ABOVE THE BRG REMOVED NR1 PYLON AFT ATTACH FITTING AT RIB 18 IAW AMM 54-51-75-04. REMOVED CORROSION FROM RIB 18 LUG IAW SRM 51-74-10 , CHECKED FOR LIMITS FOUND OUT OF LIMITS IAW SRM 54-51-71, PAGE 110. INSTALLED NEW FITTOct 28, 2010 · N815FD · Airbus A310324 · Nacelle/Pylon, Longeron/StringerSDR FDEA201010254167Fairing · crackedNR 1 PYLON INBD APRON FAIRING SKIN IS CRACKED. INSTALLED REPAIR DOUBLER ON THE NR1 PYLON INBD APRON FAIRING IN REF TO SRM 54-56-10, FIG 201.Oct 25, 2010 · N803FD · Airbus A310324 · Nacelle/Pylon Miscellaneous StructureSDR FDEA201010204125Seat Track · corrodedSEAT TRACK 2L IS CORRODED IN 2 EA LOCATIONS BETWEEN FR 19 AND FR14 REMOVED CORROSION AT SEAT TRACK 2L IAW SRM 53-10-16, PAGE 103, FIG 101. AREA FOUND OUT OF LIMIT. R & R SEAT TRACK IAW SRM 53-10-16 AND SRM 51-40-21.Oct 20, 2010 · N815FD · Airbus A310324 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201010204124Seat Track · corrodedSEAT TRACK 2R IS CORRODED BETWEEN FR 16 AND FR 15 APPROX 12 INCH LONG REMOVED CORROSION WITH 65 PERCENT MATERIAL LOSS IAW SRM 53-10-16, PAGE 108, FIG 101 R & R SEAT TRACK NR 2R BETWEEN FR16 AND FR 15 IAW SRM 53-10-16, FIG 101 AND SRM 51-40-21.Oct 20, 2010 · N815FD · Airbus A310324 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201010204123Seat Track · corrodedSEAT TRACK 3R IS CORRODED BETWEEN FR 18 AND FR 17 APPROX 3 SQ. INCH REMOVED CORROSION WITH 58 PERCENT MATERIAL LOSS FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16, PAGE 108, FIG 101. R & R SEAT TRACK 3R BETWEEN FR 17 AND FR 18 IAW SRM 53-10-16, PAGE 108, FIG 1Oct 20, 2010 · N815FD · Airbus A310324 · Fuselage, Seat/Cargo Attach Fittings
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