# Service difficulty reports: Airbus A310-324 A list on [Airbus A310-324](https://openairdocs.org/model/airbus-a310-324.md). Newest first. General aviation reporting is voluntary. Page 1 of 29 · 1,439 reports - [SDR FDEA201909112203](https://openairdocs.org/sdr/FDEA201909112203.md): Gearbox · failed · Sep 11, 2019 · N809FD · Airbus A310324 · Leading Edge Slat Control System > PDIS 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 FDEA201909102197](https://openairdocs.org/sdr/FDEA201909102197.md): Computer · faulty · Sep 10, 2019 · N809FD · Airbus A310324 · Leading Edge Slat Control System > PDIS 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 LAN - [SDR FDEA2019060311203](https://openairdocs.org/sdr/FDEA2019060311203.md): Sequence Valve · misaligned · May 31, 2019 · N807FD · Airbus A310324 · Landing Gear Retraction/Extension System > 6685 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). TROUB - [SDR FDEA201903010528](https://openairdocs.org/sdr/FDEA201903010528.md): Linkage · broken · Mar 1, 2019 · N811FD · Airbus A310324 · Landing Gear Retraction/Extension System > PDIS 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. C - [SDR FDEA201902120385](https://openairdocs.org/sdr/FDEA201902120385.md): Strut · inoperative · Feb 12, 2019 · N808FD · Airbus A310324 · Nose/Tail Landing Gear Strut/Axle > ON 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 M - [SDR FDEA2019020870269](https://openairdocs.org/sdr/FDEA2019020870269.md): Sequence Valve · malfunctioned · Feb 7, 2019 · N808FD · Airbus A310324 · Landing Gear Door Retract Section > ON 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 GEAR - [SDR FDEA201901030010](https://openairdocs.org/sdr/FDEA201901030010.md): Actuator · malfunctioned · Jan 3, 2019 · N811FD · Airbus A310324 · Drag Control Actuator > AT 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 T - [SDR FDEA2018040853507](https://openairdocs.org/sdr/FDEA2018040853507.md): Arm · failed · Dec 15, 2018 · N808FD · Airbus A310324 · Landing Gear Retraction/Extension System > AFTER 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 32-31-24-04 - [SDR FDEA201812153507](https://openairdocs.org/sdr/FDEA201812153507.md): Warning System · malfunctioned · Dec 15, 2018 · N808FD · Airbus A310324 · Landing Gear Position and Warning > AFTER 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 FDEA201811053107](https://openairdocs.org/sdr/FDEA201811053107.md): Tee Fitting · cracked · Nov 5, 2018 · N809FD · Airbus A310324 · Wing Miscellaneous Structure > CNTR 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 FDEA201811053106](https://openairdocs.org/sdr/FDEA201811053106.md): Tee Fitting · cracked · Nov 5, 2018 · N809FD · Airbus A310324 · Wing Miscellaneous Structure > CNTR 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 INSPE - [SDR FDEA201810202960](https://openairdocs.org/sdr/FDEA201810202960.md): Support Beam · damaged · Oct 20, 2018 · N809FD · Airbus A310324 · Fuselage Miscellaneous Structure > MDCC 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 A - [SDR FDEA2018042601120](https://openairdocs.org/sdr/FDEA2018042601120.md): Power Supply · failed · Apr 25, 2018 · N807FD · Airbus A310324 · Emergency Lighting > EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED THE POWER SUPPLY AND BATTERY 29WLI IAW AMM 33-51-14-04-09. OPS CHECKED GOOD. - [SDR FDEA201802220470](https://openairdocs.org/sdr/FDEA201802220470.md): Slat System · faulted · Feb 22, 2018 · N801FD · Airbus A310324 · Leading Edge Slat Control System > DURING 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 FDEA201802140400](https://openairdocs.org/sdr/FDEA201802140400.md): Bushing · worn · Feb 14, 2018 · N801FD · Airbus A310324 · Service Doors > R1 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 COMPONE - [SDR FDEA201710193010](https://openairdocs.org/sdr/FDEA201710193010.md): Slide · inoperative · Oct 19, 2017 · N808FD · Airbus A310324 · Escape Slide > L1 DOOR SLIDE IS INOPERATIVE. - [SDR FDEA201709182589](https://openairdocs.org/sdr/FDEA201709182589.md): Stiffener · corroded · Sep 18, 2017 · N811FD · Airbus A310324 · Fuselage Miscellaneous Structure > LOWER SKIN STIFFENER CORRODED BETWEEN FRAMES 43 & 46, Y1456. COMPLIED WITH EA6-5710-T0335320 P1. MAJOR REPAIR IAW GMM6-2-100. - [SDR FDEA201709132525](https://openairdocs.org/sdr/FDEA201709132525.md): Stiffener · corroded · Sep 13, 2017 · N811FD · Airbus A310324 · Fuselage Miscellaneous Structure > LOWER SKIN STIFFENER CORRODED,BETWEEN FRAMES 43 AND 47, Y-1456. COMPLIED WITH EA 6-5710-T0335320 P1. MAJOR REPAIR IAW GMM6-2-100. - [SDR FDEA201709072463](https://openairdocs.org/sdr/FDEA201709072463.md): Stringer · damaged · Sep 7, 2017 · N811FD · Airbus A310324 · Fuselage Main, Longeron/Stringer > AFT 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 FDEA201708282387](https://openairdocs.org/sdr/FDEA201708282387.md): Spar · cracked · Aug 28, 2017 · N811FD · Airbus A310324 · Wing Spar > LEFT 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 FDEA201708282385](https://openairdocs.org/sdr/FDEA201708282385.md): Spar · cracked · Aug 28, 2017 · N811FD · Airbus A310324 · Wing Spar > LEFT 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 FDEA201708282384](https://openairdocs.org/sdr/FDEA201708282384.md): Spar · cracked · Aug 28, 2017 · N811FD · Airbus A310324 · Wing Spar > LEFT 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 FDEA201708282383](https://openairdocs.org/sdr/FDEA201708282383.md): Spar · cracked · Aug 28, 2017 · N811FD · Airbus A310324 · Wing Spar > LEFT 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 FDEA201708282382](https://openairdocs.org/sdr/FDEA201708282382.md): Spar · cracked · Aug 28, 2017 · N811FD · Airbus A310324 · Wing Spar > LEFT 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 FDEA201708282381](https://openairdocs.org/sdr/FDEA201708282381.md): Spar · cracked · Aug 28, 2017 · N811FD · Airbus A310324 · Wing Spar > LEFT 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 FDEA201708282380](https://openairdocs.org/sdr/FDEA201708282380.md): Spar · cracked · Aug 28, 2017 · N811FD · Airbus A310324 · Wing Spar > RIGHT 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 FDEA201708282379](https://openairdocs.org/sdr/FDEA201708282379.md): Spar · cracked · Aug 28, 2017 · N811FD · Airbus A310324 · Wing Spar > RIGHT 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 FDEA201708282378](https://openairdocs.org/sdr/FDEA201708282378.md): Spar · cracked · Aug 28, 2017 · N811FD · Airbus A310324 · Wing Spar > RIGHT 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 FDEA201708282377](https://openairdocs.org/sdr/FDEA201708282377.md): Frame Angle · cracked · Aug 28, 2017 · N811FD · Airbus A310324 · Fuselage Main, Frame > RIGHT 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 FDEA201707151956](https://openairdocs.org/sdr/FDEA201707151956.md): Spar · cracked · Jul 15, 2017 · N808FD · Airbus A310324 · Wing Spar > RIGHT 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 FDEA201707151951](https://openairdocs.org/sdr/FDEA201707151951.md): Spar · cracked · Jul 15, 2017 · N808FD · Airbus A310324 · Wing Spar > RIGHT 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 FDEA201707151950](https://openairdocs.org/sdr/FDEA201707151950.md): Spar · cracked · Jul 15, 2017 · N808FD · Airbus A310324 · Wing Spar > RIGHT 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 FDEA201707151949](https://openairdocs.org/sdr/FDEA201707151949.md): Spar · cracked · Jul 15, 2017 · N808FD · Airbus A310324 · Wing Spar > RIGHT 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 FDEA201707151948](https://openairdocs.org/sdr/FDEA201707151948.md): Angle · cracked · Jul 15, 2017 · N808FD · Airbus A310324 · Wing Spar > LEFT 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 FDEA201707151947](https://openairdocs.org/sdr/FDEA201707151947.md): Spar · cracked · Jul 15, 2017 · N808FD · Airbus A310324 · Wing Spar > LEFT 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 FDEA201707151959](https://openairdocs.org/sdr/FDEA201707151959.md): Skin · cracked · Jul 15, 2017 · N808FD · Airbus A310324 · Wing, Plate/Skin > RIGHT 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 FDEA201707151958](https://openairdocs.org/sdr/FDEA201707151958.md): Skin · cracked · Jul 15, 2017 · N808FD · Airbus A310324 · Wing, Plate/Skin > LEFT 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 FDEA201707151946](https://openairdocs.org/sdr/FDEA201707151946.md): Angle · cracked · Jul 15, 2017 · N808FD · Airbus A310324 · Wing Spar > LEFT 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 6-5710-7 - [SDR FDEA201707151957](https://openairdocs.org/sdr/FDEA201707151957.md): Spar · cracked · Jul 15, 2017 · N808FD · Airbus A310324 · Wing Spar > RIGHT 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, PER - [SDR FDEA201707151955](https://openairdocs.org/sdr/FDEA201707151955.md): Spar · cracked · Jul 15, 2017 · N808FD · Airbus A310324 · Wing Spar > RIGHT 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, & 6-5710-7-3 - [SDR FDEA201707151954](https://openairdocs.org/sdr/FDEA201707151954.md): Spar · cracked · Jul 15, 2017 · N808FD · Airbus A310324 · Wing Spar > RIGHT 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 6-5710 - [SDR FDEA201707151953](https://openairdocs.org/sdr/FDEA201707151953.md): Spar · cracked · Jul 15, 2017 · N808FD · Airbus A310324 · Wing Spar > RIGHT 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 FDEA201707151952](https://openairdocs.org/sdr/FDEA201707151952.md): Spar · cracked · Jul 15, 2017 · N808FD · Airbus A310324 · Wing Spar > RIGHT 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 6-571 - [SDR FDEA201707151945](https://openairdocs.org/sdr/FDEA201707151945.md): Spar · cracked · Jul 15, 2017 · N808FD · Airbus A310324 · Wing Spar > LEFT 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 INSTA - [SDR FDEA201707111907](https://openairdocs.org/sdr/FDEA201707111907.md): Angle · cracked · Jul 11, 2017 · N808FD · Airbus A310324 · Wing Miscellaneous Structure > LEFT WING REAR SPAR INERNAL ANGLE 16 HOLE FOUND CRACKED. REPAIRED IAW EA 6-5710-T0334453 P1. MAJOR REPAIR IAW GMM 6-2-100. - [SDR FDEA201707051852](https://openairdocs.org/sdr/FDEA201707051852.md): Skin · corroded · Jul 5, 2017 · N808FD · Airbus A310324 · Fuselage Main, Plate/Skin > FWD 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 FDEA201706201716](https://openairdocs.org/sdr/FDEA201706201716.md): Pitot Tube · obstructed · Jun 20, 2017 · N803FD · Airbus A310324 · Pitot/Static System > DURING 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 FIRST - [SDR FDEA201706011556](https://openairdocs.org/sdr/FDEA201706011556.md): Indication Sys · intermittent · Jun 1, 2017 · N809FD · Airbus A310324 · Door Warning System > R1 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 FDEA201705031343](https://openairdocs.org/sdr/FDEA201705031343.md): Jackscrew · lack of lube · May 3, 2017 · N807FD · Airbus A310324 · Trailing Edge Flap Control System > WHEN 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 SENS - [SDR FDEA201704261272](https://openairdocs.org/sdr/FDEA201704261272.md): Power Supply · inoperative · Apr 26, 2017 · N809FD · Airbus A310324 · Emergency Equipment > R1 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. Next page: https://openairdocs.org/model/airbus-a310-324/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/model/airbus-a310-324/reports --- 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.