JASC 5280
Service difficulty reports · 3,557
Reports filed under 5280 · Landing Gear Doors, newest first.
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 jasc_code = '5280' 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 jasc_code = '5280' 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 04FDEA03361Structure · crackedRIGHT MAIN LANDING GEAR WHEEL WELL MAIN GEAR DOOR FOUND CRACKED AT HOLE PLUG AREA. CRACK REPAIRED AS PER SRM 52-10-00 FIG 13 VOL I. REPAIR DOUBLER FABRICATED AS PER SRM 52-10-00 FIG 13 VOL I.SDR CA041224004Door · separated(CAN) WHILE CLIMBING THRU 16,000 FT, THE FLT CREW HEARD A STRANGE NOISE. ALL COCKPIT INDICATIONS WERE NORMAL. UPON POST FLT INSPECTION, MAINTENANCE FOUND THE RT MAIN GEAR DOOR MISSING.SDR DHL2004873528Angle · crackedRIGHT WING T/E MLG DOOR JAMB ZEE ANGLE CRACKED 2.000, STA XW 3.125. REMOVED CRACKED ZEE ANGLE IAW SRM 51-1-21 PG 1. FABRICATED ZEE ANGLE (AL2024 -0- 0.050) IAW DWG 5651221. HEAT TREATED IAW DADO DPS 7.00. CLEANED, TREATED AND PRIMED AREA AND ZEE ANGLE IAW SDR UPS04443554Door Frame · crackedRT AFT BODY GEAR DOOR ATTACH FRAME CRACKED. REMOVED CRACKED CHANNEL; OK TO INSTALL REPLACEMENT FRAME; BEGAN INSTALLATION; OF NEW FRAME 8EA FASTENERS AT AFT BULKHEAD REQUIRE INSTALLATION; FINISHED INSTALLATION AS PER SRM 51-30-02.SDR ANCF200400036Door · damagedAFTER TAKEOFF AND AFTER LANDING GEAR RETRACTION THE RED GEAR LIGHT REMAIN ON ALONG WITH THE GEAR DOOR OPEN LIGHT. CHECKIST WAS PERFORMED AND THE GEAR WAS CYCLED WITH NO HELP. RETURNED WAS MADE THE GEAR WHEN DONE OK, AND THE GEAR DOOR OPEN LIGHT WHEN OFF NORMSDR 04FDEA03218Structure · crackedLEFT MAIN LANDING GEAR WHEEL WELL MAIN GEAR DOOR FOUND CRACKED AT FORWARD OF STRUT FITTING NEAR HINGE AREA. CRACK REPAIRED AND REPAIR DOUBLER FABRICATED AS PER SRM 52-10-00 FIG 13 VOL I.SDR 04FDEA03217Structure · crackedLEFT MAIN LANDING GEAR WHEEL WELL MAIN GEAR DOOR FOUND CRACKED AT HOLE PLUG AREA OF STRUT FITTING. CRACK REPAIRED AS PER SRM 52-10-00 FIG 13 VOL I. REPAIR DOUBLER FABRICATED AS PER SRM 52-10-00 FIG 13 VOL I.SDR MALA040845Door · crackedDURING C-CHECK INSPECTION IN YYC, LT I/B MLG DOOR INNER SKIN FWD CUTOUT FWD RADIUS IS CRACKED. MAINTENANCE REPAIRED IAW EO A52033. AIRCRAFT RETURNED TO SERVICE 11/23/04.SDR MALA040844Door · crackedDURING C-CHECK INSPECTION IN YYC, LT MLG DOOR INNER SKIN FWD CUTOUT I/B AFT RADIUS IS CRACKED. MAINTENANCE REPAIRED IAW EO A52033. AIRCRAFT RETURNED TO SERVICE 11/23/04.SDR MALA040843Door · crackedDURING C-CHECK INSPECTION IN YYC, LT MLG DOOR INNER SKIN AFT CUTOUT I/B FWD RADIUS IS CRACKED. MAINTENANCE REPAIRED IAW EO A52033. AIRCRAFT RETURNED TO SERVICE 11/23/04.SDR MALA040842Door · crackedDURING C-CHECK INSPECTION IN YYC, LT MLG DOOR INNER SKIN AFT CUTOUT INBOARD AFT RADIUS IS CRACKED. MAINTENANCE REPAIRED IAW EO A52033. AIRCRAFT RETURNED TO SERVICE 11/23/04.SDR CA041125001Bracket · broken(CAN) UPON ARRIVAL, MAINTENANCE PERSONEL NOTED THE NOSE LANDING GEAR DOORS HANGING OPEN. FURTHER INSPECTION FOUND THE BRACKET FOR THE DOOR OPERATION ROD BROKEN. SEE IPC 32-30-00-06 ITEM 89. BRACKET AND HARDWARE REPLACED AND GEAR SWINGS CARRIED OUT, AND A/C SDR CA041224005Door · separated(CAN) FOLLOWING DEPARTURE, FLIGHT CREW HEARD A BUMP. POST FLT INSPECTION REVEALED THAT THE RT INBOARD MLG DOOR WAS MISSING. IN ADDITION IT WAS FOUND THAT THE RT IB FLAP SUFFERED SEVERAL DEEP GOUGES, THE RT PROXIMITY HARNESS CONDUIT WAS DENTED, THE RT OB MLSDR QXEA200400783Door · departedTHE NR 2 INBOARD GEAR DOOR BROKE OFF DURING CLIMBOUT OF MFR. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE INBOARD DOOR MISSING, AND THE CONNECTING ROD BROKEN OFF AT THE MOUNT BOLT. DAMAGE TO THE INBOARD FLAP WAS ALSO FOUND. MAINTENANCE REMOVED THE REMAISDR 04FDEA03168Door · vibrates14000 FT HEAVY VIBRATION SLOWED AND LANDED WITH NO PROBLEM, EVEN WITH GEAR DOWN HAD VIBRATION. "DECLARED EMERGENCY" HAD FIRE TRUCKS STANDING BY. REMOVED AND REPLACED LT NOSE GEAR DOOR PER MM 32-23-01-2. ACCOMLISHED GEAR SWING AND DOOR FIT CHECK PER EA 8-3SDR GTIA040847Skin · crackedLP NR 0167013; LT MAIN GEAR DOOR SKIN CRACKED ABOVE AND BELOW SKIN PLATE. UNSCHEDULED CHANGE OF AIRCRAFT EN ROUTE. PERFORMED REPAIR AND INSTALLED DOUBLER.SDR ASAA0410491Skin · debondedOKC - LT MAIN LANDING GEAR, UPPER STRUT DOOR FWD AND AFT HINGE AREA DISBONDING. REMOVED DAMAGE, COMPLIED WITH COMPOSITE REPAIR IAW EA.SDR MALA040795Door · bentDURING C-CHECK INSPECTION IN YYC, MAINTENANCE FOUND LEFT NOSE GEAR DOOR LOWER EDGE BENT. MAINTENANCE REPLACED RIVETS AND REPAIRED IAW SRM 51-42-00, 51-43-00 & 51-10-02. AIRCRAFT WAS RETURNED TO SERVICE 11/08/04.SDR DL76K040996Door · missingRT MAIN LANDING GEAR LOWER STRUT DOOR MISSING UPON ARRIVAL. FERRIED A/C TO FOR FURTHER EVALUATION.SDR AC2A099708Hinge · corrodedNOSE GEAR DOOR WAS FOUND HANGING DOWN BY PILOT AS AIRCRAFT WAS SITTING ON THE PAD. ONE HINGE WAS CORRODED AND HAD BROKEN ALLOWING THE DOOR TO BECOME PARTIALLY DETACHED FROM AIRCRAFT. NOSE WHEEL HAD ROLLED OVER DOOR AND CAUSED DAMAGE TO THE DOOR.SDR QXEA200400734Door · crackedPDX - RIGHT HAND MAIN LANDING GEAR DOOR INBOARD DOOR SECTION HAS CRACK AT OUTER TIP FROM LEADING EDGE. REPAIRED IAW CRJ 700 SRM 51-25-01-001-001-A01.SDR QXEA200400733Door · crackedPDX - LEFT HAND MAIN LANDING GEAR DOOR INBOARD DOOR SECTION HAS CRACK AT OUTER TIP FROM LEADING EDGE. REPAIRED IAW SRM 51-25-01-001-001-A01.SDR YDA2005F00000Hinge · damagedTHE LT NOSE GEAR DOOR CENTER HINGE AND NOSE GEAR DOOR ACTUATOR LINK QUIDE, BENT. THE NOSE GEAR DOORS WERE DISCONNECTED FOR AN INSPECTION. THE LT MAIN GEAR DOORS WERE RIGGED AND A RETRACTION TEST WAS PERFORMED. A LOAD POPPING NOISE WAS HEARD. UPON INSPECTIOSDR OIK2004F00000Hinge · brokenON 10/17/04, APPROXIMATELY 12:30 PM, DURING CRUISE, PILOT NOTICED THE LANDING GEAR UNLOCK LIGHT ILLUMINATED. PILOT RETURNED TO AIRPORT. UPON POST FLIGHT INSPECTION, THE RT MAIN GEAR IB DOOR HINGES WERE FOUND BROKEN. (WP13200505092)SDR ANCF200400034Door · inoperativeAFTER TAKE OFF, THERE WAS INDICATION OF (GEAR DOOR OPEN LIGHT, LT MAIN GEAR UNSECURED) RED LIGHT ON WITH LANDING GEAR HANDLE UP WAS PERFORMED. AFTER ASKING CONTROL TOWER ABOUT ANY ABNORMALITIES, GEAR WAS RECYCLED, IN THIS CONDITION IT SHOWS GEAR DOOR OPEN LIGSDR UPS04243393Door · crackedINSPECTION TYPE:C, BRACKET CRACKED ON WING DOOR FWD OF HINGE CASTING. STOP DRILLED CRACK IAW SRM 51-10-01. HFEC CARRIED OUT AROUND STOP DRILLED AREA IAW B727 NDTM 51-00-00 PT 6 FIG 4. CRACK CONTAINED WITHIN STOP DRILLED AREA. REPAIRED IAW SRM 51-20-01.SDR CALA0400664Beam · crackedLEFT MAIN LANDING GEAR DOOR PAN CRACKED AFT OUTBOARD SIDE OF DOOR. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 52-05 FIG 28.SDR EIA2004117Skin · crackedRT BLG I/B STRUT DOOR FOUND CORROSION AND CRACK ON EXT FACE OF OUTER DOOR-SKIN AT AFT EDGE. TRIM CORROSION AND CRACK IN 0.040 OUTER SKIN AT BS 1483.7, RBL 55.6, AND INSTALLED REPAIR DOUBLER BONDED TO FILLER. INSTALLED THREE (3) ROWS OF BLIND RIVETS AROUND THSDR 371PA0048Skin · delaminatedLEFT AND RIGHT MAIN LANDING GEAR DOORS HAVE DELAMINATION IN THE SKIN AT THE DOOR ATTACH FITTING. REPAIRED DAMAGE PER SRM 51-70-17 AND EA 53-258.SDR A6WA200460043Skin · crackedFOUND LEFT MLG DOOR HAS A CRACK ON FORWARD CUT OUT FOR THE SIDE STAY ON INNER SKIN ON LOWER FORWARD CORNER OF DISHED SKIN, REPAIR IN PROGRESS. (M)SDR AWXA200401066Structure · damagedON CLIMB-OUT OF PHX EN ROUTE TO RNO AT FL 200, FELT STRONG AIRFRAME VIBRATION ASSOCIATED WITH A WITH A LOAD RUMBLE, REDUCED SPEED FROM 340 KTS TO 320 KTS AND VIBRATION WENT AWAY, LANDING LIGHTS RETRACTED AT FL 100. MAINTENANCE PERFORMED ELEVATOR FREE PLAY CHESDR MALA040715Door · crackedDURING C1 INSPECTION IN YYC, RT MLG DOOR AFT RECESS IS CRACKED AT FWD INBOARD CORNER. MAINTENANCE REPAIRED IAW EO A52033. AIRCRAFT RETURNED TO SERVICE 9/14/04.SDR COMA0460495Skin · crackedSKIN AFT OF NOSE LANDING GEAR DOOR CRACKED RIGHT HAND CORNER RADIUS. REPAIRED IAW REO 601R-53-11-048.SDR UPS04243174Skin · crackedINSPECTION TYPE:C, RIGHT WING DOOR LOWER SKIN HAS TWO SUSPECT CRACKS IN SKIN AT FWD END MID WAY ON DOOR. WING DOOR REPLACED ON NRC 733172.SDR WLDA200434Panel · separatedATL/IAH AIR TURNBACK DUE TO LEFT WHEEL WELL DOOR PANEL FELL OFF DURING TAKEOFF ROLL. REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE & RETRACT CYLINDER. REPLACED LEFT MAIN OUTER DOOR. OPERATION CHECK & GEAR SWING CHECK ALL NORMAL PER MM PROCEDURES.SDR UPS04243008Web · crackedLT MLG WING DOOR LWR END WEB CRACKED. CRACK STOP DRILLED IAW SRM 51-10-1. HFEC INSPECTION CARRIED OUT. CRACK CONTAINED IN STOP DRILLED HOLE. REPAIRED IAW 51-40-02.SDR UPS04243002Skin · crackedINSPECTION TYPE: C, CRACK ON LT MLG WING DOOR INNER SKIN AT TE. HFEC CARRIED OUT AND CRACK CONFIRMED. CRACK STOP DRILLED IAW SRM 51-10-1.HFEC CARRIED OUT AND CRACK CONTAINED WITHIN DRILLED AREA. REPAIR CARRIED OUT IAW SRM 52-80-2 FIG 5.SDR UPS04242963Structure · crackedINSPECTION TYPE: C, LT MLG WING DOOR AFT Z-SECTION CRACKED. Z-SECTION REMOVED IAW SRM 51-30-02 Z-SECTION FABRICATED IAW SRM 51-20-1 Z-SECTION INSTALLED IAW SRM 51-30-02.SDR UPS04242966Web · crackedINSPECTION TYPE: C, RT MLG WING DOOR UPPER FWD WEB CRACKED AT AFT END REPAIR CARRIED OUT IAW SRM 51-30-02 & 51-40-3.SDR P5CA0401161Skin · delaminatedLEFT WING GEAR STRUT LWR DOOR AFT LWR END IS DELAMINATED AT LWR SIDE HAS EXFOLIATING CORROSION. REPAIRED IAW SRM 51-40-06 & 51-10-02.SDR 04FDEA02084Fitting · corrodedRIGHT MAIN GEAR DOOR FWD UPPER H-11 BOLT POSITION NR 1 PER DWG ARC2859 HAS GOUGES AND CORROSION. REMOVED FITTING AND FOUND TO BE OUT OF LIMITS. INSTALLED NEW FITTING IAW EO 8-5710-7-5005 AND DWG ARC2859 AND SRM 51-31-01.SDR DHL2004804511Skin · crackedLEFT MLG INBOARD DOOR INTERNAL SKIN CRACKED 0.500 AT STA 912.000 (LWR PART). REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END AND FABRICATED DOUBLER (AL 7075-T6 0.050) IAW SRM 52-2-0 PG 1-2. CLEANED, TREATED AND PRIMED AREA AND DOUBLSDR 04FDEA01864Channel · crackedLEFT MLG DOOR AFT Z-CHANNEL APPEARS CRACKED. REMOVED AND REPLACED PAN IAW SRM 51-31-01 AT MAE.SDR MWEA040103Support · crackedLEFT MAIN LANDING GEAR DOOR ACTUATOR SUPPORT FITTINGS IS CRACKED. REMOVED AND REPLACED SUPPORT FITTING.SDR MWEA040102Support · crackedRIGHT MAIN LANDING GEAR DOOR ACTUATOR FITTING SUPPORT IS CRACKED. REMOVED AND REPLACED SUPPORT RIGHT SIDE.SDR MWEA040092Support · crackedRT MAIN LANDING GEAR DOOR RETRACT ACTUATOR UPPER FORWARD SUPPORT CRACKED. STOP DRILLED CRACK.SDR W1X2004F00000Hinge · brokenSTEEL HINGE (PW 4752932) FAILED PRIOR TO AD 2000-25-01 INTERVAL. (GL13200409283)SDR COMA0460335Skin · crackedSKIN CRACKED BEHIND NOSE LANDING GEAR AFT DOOR ON RIGHT HAND SIDE APPROX .500 IN LENGTH. COMPLIED WITH REO 601R-52-11-048 AS INSTRUCTED.SDR KBM2004F00064Pin · unlatchedLT MAIN DOOR POPPED OPEN IN FLIGHT, TOP PIN UNLATCHED. FILED DOWN A GROVE AND THE UPPER STAPLE AS NEEDED.SDR AUS20040380Roller · mismanufactured(AUS) MAIN DOOR LOCKING ROLLER INTERNAL DIAMETER WAS TOO SMALL TO FIT OVER THE STEEL STUD IN THE DOOR FRAME. ROLLER WAS A NEW ITEM AND WAS BEING FITTED TO THE DOOR. SUSPECT FAULTY MANUFACTURE.
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