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"

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SDR FDEA201909112203Gearbox · failedPDIS 809 27-80 2171 11SEP19 SAT OPEN U LOGPAGES:2553291 DURING EXTENSION OF FLAPS AT 40 DEGREES, RECEIVED SLATS FAULT SYS 1 AND 2. CYCLED PER ECAM, FAULT REILLUMINATED. FOLLOWED ECAM AND QRH PROCEDURES. DECLARED EMERGENCY IN SAT. LANDED WITHOUT Sep 11, 2019 · N809FD · Airbus A310324 · Leading Edge Slat Control SystemSDR FDEA201909102197Computer · faultyPDIS 809 27-80 2168 10SEP19 AFW OPEN U DURING ARRIVAL TO KAFW WHILE EXTENDING THE SLATS HAD SLATS 1&2 FAULT. SLATS WERE STUCK AT 5 DEGREE. RETRACTED SLATS AND IMMEDIATELY GOT SLATS 1&2 FAULT. THE SLATS WERE STUCK AT 0 DEGREES. FOLLOWED QRH AND LANSep 10, 2019 · N809FD · Airbus A310324 · Leading Edge Slat Control SystemSDR FDEA2019060311203Sequence Valve · misaligned6685 ON GEAR EXTENSION RECEIVED UNSAFE INDICATION FOR RT MLG ON SYS 1 SYS 2. COMPLIED WITH QRH PROCEDURES AND LG GRAVITY EXTENSION CHECKLIST. GEAR DOORS REMAINED OPEN, UNEVENTFULL LANDING KLRD. (ON LOW APPROACH, TOWER CONFIRMED RT MLG HUNG UP). TROUBMay 31, 2019 · N807FD · Airbus A310324 · Landing Gear Retraction/Extension SystemSDR FDEA201903010528Linkage · brokenPDIS 811 32-30 4584 01MAR19 GRR DURING LANDING GEAR RETRACTION. L/G RETRACTION FAULT. THE LEFT GEAR DOOR AMBER LIGHT WAS LIT AND THE RED UNLOCKED LIGHT WAS LIT. FOLLOWED QRH ECAM. RETURNED TO KGRR. FACT 02MAR19 23:19 GRR JACKED AIRCRAFT REF 07-11-00-00. CMar 1, 2019 · N811FD · Airbus A310324 · Landing Gear Retraction/Extension SystemSDR FDEA201902120385Strut · inoperativeON APPROACH INITIAL GEAR EXTENSION DID NOT SHOW NOSE GEAR GREEN LOCKED INDICATION BUT RED UNLOCKED. RAN QRH AND ATTEMPTED MANUAL GEAR EXTENSION. ON FIRST ATTEMPT MANUAL DID NOT WORK. WENT INTO E&E COMPT. GREEN INDICATION NOT VISIBLE. SECOND ATTEMPT TO INSURE MFeb 12, 2019 · N808FD · Airbus A310324 · Nose/Tail Landing Gear Strut/AxleSDR FDEA2019020870269Sequence Valve · malfunctionedON APPR FOR 20 YEG, GEAR DOWN SELECTED, GOT AN UNSAFE GEAR INDICATION ON NOSE GEAR. FOLLOWED ECAM & QRH. EXTENDED GEAR W/GRAVITY PROCEDURE. TUG TO GATE. CARRIED OUT LUBE SERVICING INSTRUCTIONS ON NOSE GEAR ASSEMBLE AS PER AIRBUS AMM 12-22-32-00. NOSE GEARFeb 7, 2019 · N808FD · Airbus A310324 · Landing Gear Door Retract SectionSDR FDEA201901030010Actuator · malfunctionedAT FL340 GOT YELLOW SYS HYD RESERVOIR ECAM WITH CONFIRMED LOW QTY. EMER RTN TO MEM. COMPLETED INSTALL OF #4 LH SPOILER ACTUATOR REFERENCE AIRBUS A310-300 AMM 27-64-14-04. OPERATION TJan 3, 2019 · N811FD · Airbus A310324 · Drag Control ActuatorSDR FDEA2018040853507Arm · failedAFTER EXTENDING THE LANDING GEAR, THE NOSE GEAR INDICATED UNLOCKED ON SYSTEM 1 AND 2. AFTER ABOUT 3 MINUTES,, SHOWED LOCKED ON SYSTEM 1 AND 2. REMOVED AND REPLACED NOSE GEAR TELESCOPIC DRAG STRUT ROCKER ARM ASSY. (40GB) ADJUSTED (49GB) IAW AMM 32-31-24-04Dec 15, 2018 · N808FD · Airbus A310324 · Landing Gear Retraction/Extension SystemSDR FDEA201812153507Warning System · malfunctionedAFTER EXTENDING THE LANDING GEAR, THE NOSE GEAR INDICATED UNLOCKED ON SYSTEM 1 AND 2. AFTER ABOUT 3 MINUTES, SHOWED LOCKED ON SYSTEM 1 AND 2.Dec 15, 2018 · N808FD · Airbus A310324 · Landing Gear Position and WarningSDR FDEA201811053107Tee Fitting · crackedCNTR WING INSP REAR SPAR INTERNAL ANGLE/TEE FITTING FR44 RT SIDE FWD HOLE WITH CRACK SIGNAL. COMPLIED WITH EA:6-5710-T0343040 PT1 REPAIRED CENTER WING REAR SPAR RIB1 INTERNAL ANGLE/TEE FITTING AT FR44 RH SIDE FWD HOLE(#34A). MAJOR REPAIR IAW FEDEX GMM6-2-Nov 5, 2018 · N809FD · Airbus A310324 · Wing Miscellaneous StructureSDR FDEA201811053106Tee Fitting · crackedCNTR WING INSP REAR SPAR INTERNAL ANGLE/TEE FITTING FR44 LT SIDE MID HOLE WITH CRACK SIGNAL. COMPLIED WITH EA:6-5710-T0343040 PT1 REPAIRED CENTER WING REAR SPAR RIB1 INTERNAL ANGLE/TEE FITTING AT FR44 LH SIDE MID HOLE(#35A). CATEGORY "B" REPAIR.FIRST INSPENov 5, 2018 · N809FD · Airbus A310324 · Wing Miscellaneous StructureSDR FDEA201810202960Support Beam · damagedMDCC FWD UTILITY AREA FR14-FR17, -Y1456 LONGITUDINAL SUPPORT BEAM FOUND 1EA HOLE ENLARGED REFER TO SRM 53-12-15 FIG. 207 REPAIRED THE -Y1456 LONGITUDINAL SUPPORT BEAM AT MDCC FWD UTILITY AREA BETWEEN FR14-FR17. THIS IS CATEGORY "B" REPAIR AND MUST BE INSPECT AOct 20, 2018 · N809FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR FDEA2018042601120Power Supply · failedEMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED THE POWER SUPPLY AND BATTERY 29WLI IAW AMM 33-51-14-04-09. OPS CHECKED GOOD.Apr 25, 2018 · N807FD · Airbus A310324 · Emergency LightingSDR FDEA201802220470Slat System · faultedDURING APPROACH, SLATS SYSTEMS 1 & 2 FAULTED, SLATS STUCK IN THE RETRACTED POSITION, RAN THE QRH, PERFORMED A NO SLAT LANDING. NO TRIPPED INDICATIONS. COMPLIED WITH TSM 27-80-02, FIG 101, & 102, REPEAT OCCURRENCE FOR BINDING, ALL SLAT SCREWJACK'S LOCK-Feb 22, 2018 · N801FD · Airbus A310324 · Leading Edge Slat Control SystemSDR FDEA201802140400Bushing · wornR1 DOOR HARD TO OPEN FROM THE INSIDE AND OUTSIDE. INSPECTED THE R1 DOOR, AND FOUND UPPER AND LOWER HINGE SUPPORT ARM HAT BUSHINGS MIGRATED. NO DAMAGE FOUND ON R1 DOOR IAW MM 52-10-11-06. COMPLETED VISUAL INSPECTION OF R1 DOOR LOCKING & LATCHING COMPONEFeb 14, 2018 · N801FD · Airbus A310324 · Service DoorsSDR FDEA201710193010Slide · inoperativeL1 DOOR SLIDE IS INOPERATIVE.Oct 19, 2017 · N808FD · Airbus A310324 · Escape SlideSDR FDEA201709182589Stiffener · corrodedLOWER SKIN STIFFENER CORRODED BETWEEN FRAMES 43 & 46, Y1456. COMPLIED WITH EA6-5710-T0335320 P1. MAJOR REPAIR IAW GMM6-2-100.Sep 18, 2017 · N811FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR FDEA201709132525Stiffener · corrodedLOWER SKIN STIFFENER CORRODED,BETWEEN FRAMES 43 AND 47, Y-1456. COMPLIED WITH EA 6-5710-T0335320 P1. MAJOR REPAIR IAW GMM6-2-100.Sep 13, 2017 · N811FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR FDEA201709072463Stringer · damagedAFT CABIN UNDERFLOOR COMPT FR74-FR75, S45R STRINGER 1EA FASTENER HOLE DAMAGED. AFT CABIN UNDERFLOOR COMPT FR74-FR75,S-45R STRINGER 1EA FASTENER HOLE DAMAGED. REPAIRED THE DAMAGED STRINGER PER SRM53-10-14 FIG 201 SHT 2 VIEW H & J.Sep 7, 2017 · N811FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR FDEA201708282387Spar · crackedLEFT REAR SPAR INTERNAL ANGLE NR 1 HOLE FOUND CRACKED DURING AN NDT INSPECTION. REPAIRED IAW EA 6-5710-T0335292 P1. MAJOR REPAIR IAW GMM 6-2-100.Aug 28, 2017 · N811FD · Airbus A310324 · Wing SparSDR FDEA201708282385Spar · crackedLEFT REAR SPAR INTERNAL ANGLE NR 4 HOLE FOUND CRACKED DURING AN NDT INSPECTION. REPAIRED IAW EA 6-5710-T0335292 P1. MAJOR REPAIR IAW GMM 6-2-100.Aug 28, 2017 · N811FD · Airbus A310324 · Wing SparSDR FDEA201708282384Spar · crackedLEFT REAR SPAR INTERNAL ANGLE NR 10 HOLE FOUND CRACKED DURING AN NDT INSPECTION. REPAIRED IAW EA 6-5710-T0335292 P1. MAJOR REPAIR IAW GMM 6-2-100.Aug 28, 2017 · N811FD · Airbus A310324 · Wing SparSDR FDEA201708282383Spar · crackedLEFT REAR SPAR INTERNAL ANGLE NR 52 HOLE FOUND CRACKED DURING AN NDT INSPECTION. REPAIRED IAW EA 6-5710-T0335292 P1. MAJOR REPAIR IAW GMM 6-2-100.Aug 28, 2017 · N811FD · Airbus A310324 · Wing SparSDR FDEA201708282382Spar · crackedLEFT REAR SPAR INTERNAL ANGLE NR 60 HOLE FOUND CRACKED DURING AN NDT INSPECTION. REPAIRED IAW EA:6-5710-T0335292 P1. MAJOR REPAIR IAW GMM 6-2-100.Aug 28, 2017 · N811FD · Airbus A310324 · Wing SparSDR FDEA201708282381Spar · crackedLEFT REAR SPAR INTERNAL ANGLE NR 62 HOLE FOUND CRACKED DURING AN NDT INSPECTION. REPAIRED IAW EA 6-5710-T0335292 P1. MAJOR REPAIR IAW GMM 6-2-100.Aug 28, 2017 · N811FD · Airbus A310324 · Wing SparSDR FDEA201708282380Spar · crackedRIGHT REAR SPAR INTERNAL ANGLE NR 2 HOLE FOUND CRACKED DURING AN NDT INSPECTION. REPAIRED IAW EA 6-5710-T0335292 P1. MAJOR REPAIR IAW GMM 6-2-100.Aug 28, 2017 · N811FD · Airbus A310324 · Wing SparSDR FDEA201708282379Spar · crackedRIGHT REAR SPAR INTERNAL ANGLE NR 8 HOLE FOUND CRACKED DURING AN NDT INSPECTION. REPAIRED IAW EA:6-5710-T0335292 P1. MAJOR REPAIR IAW GMM 6-2-100.Aug 28, 2017 · N811FD · Airbus A310324 · Wing SparSDR FDEA201708282378Spar · crackedRIGHT REAR SPAR INTERNAL ANGLE, NR 14 HOLE FOUND CRACKED DURING AN NDT INSPECTION. REPAIRED IAW EA:6-5710-T0335292 P1. MAJOR REPAIR IAW GMM 6-2-100.Aug 28, 2017 · N811FD · Airbus A310324 · Wing SparSDR FDEA201708282377Frame Angle · crackedRIGHT REAR FRAME INTERNAL ANGLE NR 23 HOLE, NDT INSPECTION FOUND A CRACK. REPAIRED IAW EA:6-5710-T0335292 P1. MAJOR REPAIR IAW GMM 6-2-100.Aug 28, 2017 · N811FD · Airbus A310324 · Fuselage Main, FrameSDR FDEA201707151956Spar · crackedRIGHT WING REAR SPAR INTERNAL ANGLE NR 60 HOLE, NDT INSPECTION FOUND A CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0334453, P1. MAJOR REPAIR IAW GMM 6-2-100.Jul 15, 2017 · N808FD · Airbus A310324 · Wing SparSDR FDEA201707151951Spar · crackedRIGHT WING REAR SPAR INTERNAL ANGLE NR 16 HOLE, NDT INSPECTION FOUND CRACK SIGNAL. COMPLED WITH EA 6-5710-T0334453, P1. MAJOR REPAIR IAW GMM 6-2-100.Jul 15, 2017 · N808FD · Airbus A310324 · Wing SparSDR FDEA201707151950Spar · crackedRIGHT WING REAR SPAR INTERNAL ANGLE NR 12 HOLE, NDT INSPECTION FOUND A CRACK SIGNAL. COMPLED WITH EA 6-5710-T0334453, P1. MAJOR REPAIR IAW IAW GMM 6-2-100.Jul 15, 2017 · N808FD · Airbus A310324 · Wing SparSDR FDEA201707151949Spar · crackedRIGHT REAR SPAR INTERNAL ANGLE NR 7 HOLE, NDT INSPECTION FOUND A CRACK SIGNAL. COMPLED WITH EA 6-5710-T0334453, P1. MAJOR REPAIR IAW GMM 6-2-100.Jul 15, 2017 · N808FD · Airbus A310324 · Wing SparSDR FDEA201707151948Angle · crackedLEFT REAR SPAR INTERNAL ANGLE NR 61 HOLE, NDT INSPECTION FOUND A CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0334453 P1. MAJOR REPAIR IAW GMM 6-2-100.Jul 15, 2017 · N808FD · Airbus A310324 · Wing SparSDR FDEA201707151947Spar · crackedLEFT WING REAR SPAR INTERNAL ANGLE NR 13 HOLE, NDT INSPECTION FOUND A CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0334453 P1. MAJOR REPAIR IAW GMM 6-2-100.Jul 15, 2017 · N808FD · Airbus A310324 · Wing SparSDR FDEA201707151959Skin · crackedRIGHT WING RIB 11, CRACKED ON LOWER SKIN ACROSS A FASTENER HOLE APPROX 1.0 INCH IN LENGTH NEAR ACCESS PANEL 681AB. COMPLIED WITH EA 6-5730-T0334254 P1. MAJOR REPAIR IAW IAW GMM 6-2-100.Jul 15, 2017 · N808FD · Airbus A310324 · Wing, Plate/SkinSDR FDEA201707151958Skin · crackedLEFT WING RIB 11, CRACKED ON THE LOWER SKIN ACCROSS A FASTENER HOLE APPROX 1.5 INCH IN LENGTH, NEAR ACCESS PANEL 581AB. COMPLIED WITH EA 6-5730-T0334254, P1. MAJOR REPAIR IAW GMM 6-2-100.Jul 15, 2017 · N808FD · Airbus A310324 · Wing, Plate/SkinSDR FDEA201707151946Angle · crackedLEFT REAR SPAR INTERNAL ANGLE NR 53 HOLE, NDT INSPECTION FOUND A CRACK SIGNAL. REAM THE HOLE IAW SRM 51-40-44, PERFORM ROTOTEST INSPECTION OF THE HOLE IAW NTM51-10-01 & NTM51-10-18 AND NO CRACK FOUND. WET INSTALLED A FASTENER IAW SRM 51-40-21 & EO 6-5710-7Jul 15, 2017 · N808FD · Airbus A310324 · Wing SparSDR FDEA201707151957Spar · crackedRIGHT REAR SPAR INTERNAL ANGLE NR 63 HOLE NDT INSPECTION FOUND CRACK SIGNAL. RIGHT REAR SPAR INTERNAL ANGLE 63 HOLE NDT INSPECTION FOUND CRACK SIGNAL. REAM THE AFFECTED HOLE THROUGH ALL LAYERS STEP BY STEP WITH INCREASING DIA OF 0.4 MM IAW SRM 51-40-44, PERJul 15, 2017 · N808FD · Airbus A310324 · Wing SparSDR FDEA201707151955Spar · crackedRIGHT WING REAR SPAR INTERNAL ANGLE NR 38 HOLE, NDT INSPECTION FOUND A CRACK SIGNAL. REAMED THE HOLE IAW SRM 51-40-44, PERFORM ROTOTEST INSPECTION IAW NTM 51-10-01, & NTM 51-10-18 AND NO CRACK FOUND. WET INSTALLED A FASTENER IAW SRM 51-40-21, & 6-5710-7-3Jul 15, 2017 · N808FD · Airbus A310324 · Wing SparSDR FDEA201707151954Spar · crackedRIGHT WING REAR SPAR INTERNAL ANGLE NR 35 HOLE, NDT INSPECTION FOUND A CRACK SIGNAL. REAMED THE HOLE IAW SRM 51-40-44, PERFORM ROTOTEST INSPECTION IAW NTM 51-10-01, & NTM 51-10-18 AND NO CRACK FOUND. WET INSTALLED A FASTENER IAW SRM 51-40-21, & EO 6-5710Jul 15, 2017 · N808FD · Airbus A310324 · Wing SparSDR FDEA201707151953Spar · crackedRIGHT WING REAR SPAR INTERNAL ANGLE NR 33 HOLE, NDT INSPECTION FOUND A CRACK SIGNAL. REAMED THE HOLE IAW SRM 51-40-44, PERFORM ROTOTEST INSPECTION OF THE HOLE IAW NTM51-10-01, & NTM51-10-18 AND NO CRACK WAS FOUND. WET INSTALLED A FASTENER IAW SRM 51-40-21, Jul 15, 2017 · N808FD · Airbus A310324 · Wing SparSDR FDEA201707151952Spar · crackedRIGHT REAR SPAR INTERNAL ANGLE NR 30 HOLE, NDT INSPECTION FOUND A CRACK SIGNAL. REAM THE HOLE IAW SRM 51-40-44, PERFORM ROTOTEST INSPECTION OF THE HOLE IAW NTM51-10-01 & NTM51-10-18 AND NO CRACK FOUND. WET INSTALLED A FASTENER IAW SRM 51-40-21 & EO 6-571Jul 15, 2017 · N808FD · Airbus A310324 · Wing SparSDR FDEA201707151945Spar · crackedLEFT REAR SPAR INTERNAL ANGLE NR 35 HOLE NDT INSPECTION FOUND A CRACK SIGNAL. REAMED THE AFFECTED HOLE THROUGH ALL LAYERS IAW SRM 51-40-44, PERFORM ROTOTEST INSPECTION OF THE HOLE IAW NTM51-10-01 & NTM51-10-18 AFTER EACH STEP AND NO CRACK FOUND. WET INSTAJul 15, 2017 · N808FD · Airbus A310324 · Wing SparSDR FDEA201707111907Angle · crackedLEFT WING REAR SPAR INERNAL ANGLE 16 HOLE FOUND CRACKED. REPAIRED IAW EA 6-5710-T0334453 P1. MAJOR REPAIR IAW GMM 6-2-100.Jul 11, 2017 · N808FD · Airbus A310324 · Wing Miscellaneous StructureSDR FDEA201707051852Skin · corrodedFWD TOILET SERVICE PANEL LOWER CUTOUT SKIN DELAMINATED. INSPECTED FOUND SKIN INNER STIFFENER CORRODED AND OUT OF LIMITS IAW SRM 51-40-21, & SRM 53-12-18, FIG 2, SHEET 3, ITEM 205, REPLACEED THE STIFFENER. . MAJOR REPAIR IAW GMM 6-2-100.Jul 5, 2017 · N808FD · Airbus A310324 · Fuselage Main, Plate/SkinSDR FDEA201706201716Pitot Tube · obstructedDURING TAKEOFF, FIRST OFFICER`S AIRSPEED TAPE SHOWED BETWEEN 40 - 45 KNTS, WITH CAPTAIN`S AIRSPEED TAPE AND STANDBY AIRSPEED BETWEEN 100 - 110 KNTS. ABORTED SHORTLY THERE AFTER. PERFORMED RTO CHECK LIST, NO OTHER DESCRPENCIES NOTED. INSPECTED THE FIRSTJun 20, 2017 · N803FD · Airbus A310324 · Pitot/Static SystemSDR FDEA201706011556Indication Sys · intermittentR1 ENTRY DOOR SLIDE ARMED INDICATOR DOES NOT SHOW ARMED ON ECAM. CLEANED CONNECTOR ON 14WN RT DOOR ESCAPE SLIDE ARM SWITCH. CLOSED AND ARMED R1 DOOR SLIDE AND SLIDE ARM INDICATION CHECKS NORMAL ON ECAM IAW ASM 52-73-00. ACFT OK FOR SERVICE.Jun 1, 2017 · N809FD · Airbus A310324 · Door Warning SystemSDR FDEA201705031343Jackscrew · lack of lubeWHEN SELECTING FLAPS TO 15, NOTICE BINDING LEAVING THE SLATS/FLAPS 15/0 GATE AT FLAPS 15 RECEIVED FLAP FAULT SYS 1 AND 2. CYCLED THE FLAP HANDLE, NO CHANGE. QRH PROCDURES COMPLETED. LANDED FLAPS 0. REMOVED AND REPLACED THE FLAP/SLAT HANDLE COMMAND SENSMay 3, 2017 · N807FD · Airbus A310324 · Trailing Edge Flap Control SystemSDR FDEA201704261272Power Supply · inoperativeR1 DOOR SLIDE FAIL TO ARM. REMOVED AND REPLACED AUTONOMOUS STANDBY POWER SUPPLY UNIT 70WN AND BATTERY 1 IAW AMM 52-73-18-04, BITE TESTED OK, R1 SLIDE INDICATION CHECKS OK IAW AMM 52-73-00.Apr 26, 2017 · N809FD · Airbus A310324 · Emergency Equipment
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