Airbus A310-324
Service difficulty reports · 1,439
Newest first. General aviation reporting is voluntary.
Query with SQL
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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
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 SDR 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 LANSDR 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). TROUBSDR 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. CSDR 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 MSDR 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 GEARSDR 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 TSDR 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 32-31-24-04SDR 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.SDR 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-SDR 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 INSPESDR 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 ASDR FDEA2018042601120Power Supply · failedEMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED THE POWER SUPPLY AND BATTERY 29WLI IAW AMM 33-51-14-04-09. OPS CHECKED GOOD.SDR 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-SDR 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 COMPONESDR FDEA201710193010Slide · inoperativeL1 DOOR SLIDE IS INOPERATIVE.SDR FDEA201709182589Stiffener · corrodedLOWER SKIN STIFFENER CORRODED BETWEEN FRAMES 43 & 46, Y1456. COMPLIED WITH EA6-5710-T0335320 P1. MAJOR REPAIR IAW GMM6-2-100.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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 6-5710-7SDR 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, PERSDR 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, & 6-5710-7-3SDR 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 6-5710SDR 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, SDR 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 6-571SDR 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 INSTASDR 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.SDR 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.SDR 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 FIRSTSDR 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.SDR 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 SENSSDR 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.
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