Airbus A310-203
Service difficulty reports · 2,392
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 = 'A310203' 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 = 'A310203' 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 FDEA201107142710Floor Panel · damagedFLOOR PANEL 232XH HAS 3 EA CRUNCHED AREAS, 24 SQ IN TOTAL.SDR FDEA201107142709Floor Panel · crackedFLOOR PANEL 242QJ HAS 3 EA, 8 INCH CRACKS. FABRICATED FLOOR PANEL 242QJ IAW DWG SRZ -25 -005, REV J.SDR FDEA201107142708Floor Panel · crackedFLOOR PANEL 252GF HAS 1 EA, 12 INCH CRACK.SDR FDEA201107142707Sidewall Panel · damagedSIDEWALL PANEL 152DW HAS 5 EA FASTENER HOLES DAMAGED AND 25 SQ IN, OF SKIN MISSING. FABRICATED REPLACEMENT PANEL 152 DW IAW AIM 2001, REV D.SDR FDEA201107142706Panel · damagedSIDEWALL PANEL 151GW HAS 25 SQ IN OF UPPER SKIN MISSING. FABRICATED REPLACEMENT PANEL 151GW IAW MCG AIM 2001 REV D.SDR FDEA201107142705Panel · damagedCEILING PANEL 152BC HAS 20 SQ IN OD DELAMINATION. FABRICATED REPLACEMENT PANEL 152BL IAW MCG AIM 2001, REV D.SDR FDEA201107142704Panel · damagedCEILING PANEL 152AC HAS 20 SQ IN OF SKIN MISSING. FABRICATED REPLACEMENT CEILING PANEL 152AC IAW AIM 2001 REV DSDR FDEA201107142702Floor Panel · damagedOFF ACFT PART--FLOOR PANEL 242EK HAS 6 EA CRUSHED AREAS FABRICATED NEW PANEL 242EK IAW DWG SRZ-25-005, REV J.SDR FDEA201107142700Floor Panel · crackedFLOOR PANEL 231QH HAS 1 EA 10 IN CRACK FABRICATED NEW FLOOR PANEL 231QH IAW DWG SRZ 25-5-005, REV J.SDR FDEA201107142699Floor Panel · crackedFLOOR PANEL 232LT HAS 2 EA. 10 IN CRACKS FABRICATED NEW FLOOR PANEL 232LH IAW DWG SRZ 25-5-005, REV J.SDR FDEA201107142698Floor Panel · crackedFLOOR PANEL 252PH HAS 2 EA. 12 IN. CRACKS FABRICATED NEW FLOOR PANEL 252PH IAW DWG SRZ 25-5-005 REV J.SDR FDEA201107142697Floor Panel · crackedFLOOR PANEL 252BF HAS 1 EA, 10 IN CRACK, FABRICATED NEW PANEL 252BF IAW DWG SRZ 25-5-005, REV J.SDR FDEA201107142694Floor Panel · damagedOFF ACFT PART--FWD CARGO FLOOR PANEL 131YF HAS 14 SQ IN EDGE DAMAGE AND 6 IN CRACK, FABRICATED NEW PANEL 131YF IAW DWG SRZ 25-5-005 REV J.SDR FDEA201107132674Skin · dentedRAMP REPORTED DENT 17 IN AFT OF FWD LOWER CARGO DOOR AND APPROX 57 IN UP FROM BOTTOM OF DOOR OPENING. INSP IAW SRM 53-10-12 DIAGRAM 109 WITIN LIMITS OF "B" NO REPAIR REQUIRED. REINSPECT WITHIN 3000 FC. ACFT OK TO CONTINUE. NO RESTRICTION REF: SRM 53-10SDR FDEA201107132672Floor Panel · crackedFLOOR PANEL 251RH HAS 1EA, 10 INCH CRACK. FABRICATED REPLACEMENT PANEL 251RH IAW DWG SRZ-25-005, REV J AND IDENTIFIED REPLACEMENT PANEL IAW GMM 7-0-1001.SDR FDEA201107082612Transfer Sys · leakingINFLIGHT YELLOW SYS RESERVOIR DECREASED TO RED DOT. FLUCTUATED SOME BUT NEVER WENT OUT OF YELLOW BAND. R & R GREEN/YELLOW POWER TRANSFER UNIT AS REQUIRED IAW MM 29-23-11-04.SDR FDEA201107012552Computer · malfunctionedREJECTED TAKEOFF AT APPROX 78 KTS. NR1 ENGINE EXCEEDED THE SELECTED FLEX POWER SETTING N1(101.4). THE NR2 ENGINE ENGINE MOMENTARITLY STABLIZED AT 101.4 N1 THEN INCRESED UNSYMETERICALLY TO THRUST LIMIT OFF 107.1. CLEARED RUNWAY AND CHECKED ALL GUAGES FOR EXCESDR FDEA201106192338Target · looseAFTER TAKEOFF, GEAR LEVER WOULD NOT GO PAST NEUTRAL. SWITCHED FROM SYS 1 TO SYS 2 WITH SAME RESULT. ALL 3 LANDING GEAR REMAINED DOWN AND LOCKED. AFTER APPROX 2 MINS, ALL PITCH TRIM AND LEVERS TRIPPED OFF AND WOULD NOT RESET, UNTIL AFTER LANDING. T/S FOUNDSDR FDEA201106072153Reservoir · leakingBLUE HYD LEAK, AFTER SECURING PUMP LEAK STOPPED. REMOVED AND INSP BLUE HYD SYS MANIFOLD PRESS SW AND REINSTALLED WITH NEW PACKING REF MM 29-12-12-04. AS PRECAUTION. NEEDS LEAK CK. FOUND BLUE SYS RESERVIOR LEAKING, NEEDS RESERVIOR. R & R BLUE HUD SYS RESERVSDR FDEA201106032104Fitting · crackedTWO LOWER HOLES WERE FOUND INDICATION AT LT & RT SIDE OF FR43A. REMOVED LT AND RT FRAME FITTINGS. OVERSIZED LT RIB LOWER HOLE TO 0.402" DIA. PERFORMED NDI INSPECTION ON ALL SEPERATED STRUCTURE AND FOUND THE CRACK IS ONLY ON THE FRAME FITTING. FABRICATED CRSDR FDEA201106022095Angle · crackedANGLE FOUND CRACKED. REMOVED ANGLE, OVERSIZED HOLES TO 0.199". PERFORMED NDI INSPECTION ON ALL SEPERATED STRUCTURE AND FOUND CRACK ONLY ON ANGLE. FABRICATED ANGLE PER DRAWING A53812589200. INSTALLED ANGLE IAW SRM 51-40-21. THE REPAIR CLASSIFIED AS MAJORSDR FDEA201106012072Tube · crackedMAIN DECK COMPT LT LOWER SIDEWALL AREA FOUND SMOKE DETECTOR SNIFFER TUBE BROKEN AT 2EA PLACES, LOCATION BETWEEN FR 40/41 AND FR 45. IAW AMM 26-19-09 REOVED THE SNIFFER TUBE AT FR 40/41 LT. COMPLIED WITH E.A. 6-2610-149004. REPAIR CLASSIFIED AS MINOR PER GMSDR FDEA201106012073Floorbeam · crackedCENTER MAIN DECK COMPARTMENT FLOOR AREA BETWEEN R2 AND R3 SEAT TRACK FOUND 5 EA CROSSBEAM ASSY CRACKED AREA FROM FR40/411 TO FR45/-Y450 AND -Y953. R & R CENTER MAIN DECK SOMPARTMENT FR40 / 41 TO FR45 / -Y953 5 EA CROSS BEAMS IAW AMM20-21-12. THE REPAIR CLASSDR FDEA201106012038Battery · failedON PRE DISPATCH CK, FOUND ON COURIER COMPARTMENT EMERGENCY LT TEST INOP. R & R EMERGENCY POWER SUPPLY BATTERY. MM 33-51-14-04-0. OPS CK GOOD. OK FOR SERVICE.SDR FDEA201105302029Panel · debonded1EA DISBONDED AREA (2" X 3") WAS FOUND AT 321AL PANEL R/H SIDE. ( 14" FROM LEADING EDGE AND 20" FROM BOTTOM EDGE.) CLEANED & EVALUATED THE DISBONDED AREA 3"X2.5". REINFORCED REPAIR THE AREA WITH THE RESIN COMPOUND AND FIBERGLASS CLOTH REFER TO A310 SRM 55-SDR FDEA201105302028Panel · debonded1EA DISBONDED ARE WAS FOUND AT LT SIDE INTERIOR ARE (11" X 17") OF 324AT PANEL. ( 1.9" FROM LEADING EDGE AND 1.5" FROM BOTTOM EDGE.) CLEANED & EVALUATED THE DISBONDED AREA 11" X 17". REINFORCED REPAIR THE AREA WITH THE RESIN COMPOUND AND FIBERGLASS CLOTH IAWSDR FDEA201105302027Panel · debonded1EA DISBONDED AREA (2.5" X 1.8") WAS FOUND AT 322BL PANEL L/H SIDE. (6" FROM LEADING EDGE, 27" FROM BOTTOM EDGE.) CLEANED & EVALUATED THE DIMENSION OF THE DISBONDED AREA 9" X 8.5". REINFORCED REPAIR THE AREA WITH THE RESIN COMPOUND AND FIBERGLASS CLOTH REFSDR FDEA201105302030Floor Panel · crackedCARGO COMPARTMENT 162HF FLOOR PANEL GOT IMPACT DAMAGED. FABRICATED A NEW FLOOR PANEL FOR REPLACING IAW DRAWING 17A53279962 & SRM 53-10-20 AND MCG IRM 9701 REVISION G.SDR FDEA201105251978Rib · crackedREMOVE HINGE SUPPORT RIB, FOUND ANOTHER SIDE RIB MATING SURFACE GOT CRACK AT RIB 20, 19 INCH. REMOVED THE CRACKED BOX RIB IAW SRM 51-40-21. FABRICATED RIB MATERIAL 7075-T7651 IAW DWG A57247040. TRANSFERED DRILL THE FASTENER'S HOLE AND ASSEMBLED RIB IAW SRM 5SDR FDEA201105251980Duct · chafedENG 2, LT T/R COWL INNER DUCT AFT EDGE GOT CHAFING ATTACH TO CORE COWL AREA UPPER SIDE.SDR FDEA201105221929Rib · crackedLT WING T/E BOX RIB LOWER CORNER BOTH SIDE GOT CRACKS BETWEEN NR 5 AND NR 6 SPOILER. REMOVED THE CRACKED BOX RIBS IAW SRM 51-40-21. REPLACED THE RIBS WITH NEW PARTS BY FASTENERS IAW SRM 51-72-10 AND 51-40-21. THE REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR FDEA201105181861Skin · corrodedFWD CARGO COMPARTMENT BILGE SKIN AREA AROUND MAIN HOLE SKIN GOT CORROSION BETWEEN FR38.1 AND FR38.2 POSITION. REMOVED THE CORROSION AREA. MEASURED THE DIMENSION 2.5"L X 2.2"W X 0.078"D OVER LIMIT REF. TO SRM 53-14-12. REPAIRED THE DAMAGE AREA WITH DOUBLER ANDSDR FDEA201105121806Rib · crackedRIGHT WING NR 5 SPOILER O/B HINGE SUPPORT RIB CRACKED. REMOVED CRACKED BOX RIB IAW SRM 51-40-21. FABRICATED RIB IAW DWG A57247040. TRANSFERRED HOLES AND ASSEMBLED RIB IAW SRM 51-40-21. WET INSTALLED SUPPORT RIB IAW A310 SRM 51-40-21 AND 51-72-10. THE REPAISDR FDEA201105091781Wedge · damagedRT WING T/E INBD FLAP T/E DAMAGED ABOUT 5" X 20" BETWEEN RIB 18 AND 21. REMOVED FLAP T/E WEDGE. REPLACED WITH NEW T/E WEDGE PER E.A. 6-5750-149005. 3. PAINT TOUCHED-UP. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR FDEA201105061766Fitting · crackedFWD CARGO COMPARTMENT DOOR SILL AREA FITTING CRACKED ABOVE NR 6 LATCH FITTING. REMOVED THE CRACKED FITTING. INSTALLED THE NEW FITTING FOR REPLACING IAW SRM 51-72-10.SDR FDEA201105061767Seat Track · chafedAFT MAIN DECK COMPARTMENT FOUND L4 LONGITUDINAL SEAT TRACK FLANGE GOT A EXCESS CHAFED MARK LOCATION AT FR79 AND Y1447.8 POSITION. REMOVED THE DAMAGE SEAT TRACK. FABRICATED NEW SEAT TRACK REF. TO DRAWING NR A53279232. INSTALLED NEW TRACK WITH FASTENER REF. TSDR FDEA201105061768Gcu · failedON TAKEOFF ROLL AT APPROX 50 KNOTS, GEN NR2 FAILED. ABORTED TAKEOFF. INTEROGATED GPCU, SHOWS RT GENERATOR, UNDER FREQ TRIP, IDG /PMG / WIRING, GCU FAILED CODE 9E. REMOVED AND REPLACED ENG.2 GCU(2XU) AND ENG NR 1 GCU IAW MM 24-22-12-04. RAN ENG PER JRH CHP.SDR FDEA201104221588Bracket · wornPERFORM W/C 47C0201 FOUND NLG MAIN DOOR RT SELECTOR VALVE FIXED BRACKET THREAD WORN OUT. REMOVED THE WORN OUT BRACKET, THEN INSTALLED A NEW ONE FOR REPLACEMENT IAW EA NR6-3220-150288 (LANDING GEARS, NOSE GEAR AND DOORS: SHAFT INSTALLATION, THREAD DAMAGE ON NLSDR FDEA201104201538Transceiver · inoperativeSTATIC ON RADIOS AT 380 DOWN TO 120 WAS SO BAD AN EMERGENCY WAS DECLARED DUE TO NO RADIO CONDITION. INSTALLED NEW NR1 VHF RECEIVER AND CHECKED GOOD IAW MM 23-12-33-04-0.SDR FDEA201104201535Panel · misrepairedDOUBLER HAD TO BE REMOVED. PERFORMED FUSELAGE, PLATES AND SKIN: RT FUSE SKIN PANEL, FR54, STR 44R, REDUNDANT FASTENER, PERMANENT REPAIR DURING PERFORMED 41 X 5141 ALI STEP ID. ONE FASTENER IS COVERED BY DOUBLER IAW EA NR 6-5330-1502 81.SDR FDEA201104141484Rib · crackedREAR FUSELAGE INTERNAL FOUND 1 RIB CRACKED AT FR86 STR32R. REMOVED THE CRACKED RIB. FABRICATED A NEW RIB FOR REPLACEMENT IAW SRM 51-72-10 AND IAW DWG A53986743205.SDR FDEA201104141483Floorbeam · crackedMAIN DECK COMPT FLOOR AREA FOUND CROSSBEAM GOT A CRACK AT FR 42 LOCATION BETWEEN -Y450 AND -Y953. REMOVED THE NR 242RH. NR 242QJ, NR 242SH FLOOR PANELS FOR CROSSBEAM REPLACEMENT IAW AMM 53-10-25-4. R & R THE CROSSBEAM WITH CHECK OK FOR SERVICE IAW SRM 51-72-SDR FDEA201104121445Skin · corrodedRIGHT WING UPPER SURFACE FOUND CORROSION POSITION AT O /B GROUND POINT ABOUT RIB 27-28 PERFORMED WINGS, SKIN AND PLATES: PERMANENT REPAIR REF. TO EA 6-5730-150286. PER GMM 6-2-100 CLASSIFIED MAJOR.SDR FDEA201104121444Skin · corrodedLT WING FOR SKIN GOT CORROSION AT STA 845 SURROUND GROUNDING STUD (RIB 13-14, STR7-8).SDR FDEA201104121447Crossbeam · corrodedUPPER SUPPORT CROSSBEAM GOT CORROSION AT FR86 STG R12L. REPLACED THE DAMAGED CROSSBEAM BY NEW ONE IAW SRM 51-40-21. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED MINOR.SDR FDEA201104121446Floorbeam · corrodedUPPER SUPPORT STRUCTURE GOT MINOR CORROSION AT FR86 STG 12R. REMOVED THE CORRODED CROSS BEAM. FABRICATED A NEW CROSS BEAM I.A.W. DRAWING NO.: A53988624201. INSTALLED THE NEW CROSS BEAM FOR REPLACING.SDR FDEA201104051323Fuel Filter · contaminatedDURING GO-AROUND WITH APPROX 4.5 THOUSAND POUNDS OF FUEL IN EACH OUTER TANK, NR 1 ENG FUEL CLOG LIGHT ILLUMINATED. IT EXTINGUISHED, THEN RE-ILLUMINATED IN LEVEL FLIGHT, THEN EXTINGUISHED. NO ENGINE SECONDARIES. CREW REPORTED NO NOTICED FLUCTUATION OF NR 1SDR FDEA201103171055Skin · corrodedCORROSION FOUND AT LT WING UPPER SKIN AT FUEL PORT AND UNDER GROUND POINT. COMPLIED WITH E.A. 6-5730-145575 WINGS - LT OVERWING.SDR FDEA201103171054Skin · corrodedFUSELAGE TAIL SECTION EXTERNAL SKIN AT FR87, BETWEEN STR5L AND 6L, CORROSION ON SPLICE PLATE, ABOUT 4 SQUARE INCHES. REPAIRED FUSELAGE EXTERIOR SKIN AT FR87 BETWEEN STR 5L AND STR 6L IAW EA,6-5310-145562 FUSELAGE -FR87 SKIN.SDR FDEA201103171053Stiffener · corrodedCORROSION AT LOWER END OF WASTE WATER SERVICING BOX BETWEEN PAN AND FUSELAGE SKIN. LT FUSELAGE BETWEEN FRAMES 12 AND 12A. R & R SKIN STIFFENER AT WASTE WATER SERVICING BOX CUTOUT INTERIOR FR12-12A STR36L TO STR43L IAW SRM 51-72-10, PGS 1-3.
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