JASC 5280
Service difficulty reports · 3,556
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 AALA201508179005Hinge Fitting · wornC11 CHECK, RT MLG DOOR FWD HINGE FITTING ON KEEL BEAM, INBD INNER EDGE OF AFT CLEVIS IS WORN. R & R HINGE FITTING IAW SRM 51-72-11.SDR AALA201508139010Attach Fitting · wornC11 CHECK, LT MLG DOOR ACTUATOR TOP ATTACH FITTING WORN. REPLACED LT MLG DOOR ACTUATOR TOP ATTACH FITTING IAW EA 105872D.SDR P5CA2015081100081Skin · dentedRIGHT MLG INBD AFT STRUT DOOR EXTERNAL OUTER SKIN FOUND DENT, RT BLG INBD AFT STRUT DOOR EXTERNAL OUTER SKIN DENT AREAS AND DAMAGED RIB REPAIRED IAW R1-52-80-11002, REV B.SDR DALA2015080704829Frame · gougedRIGHT MLG DOOR, FWD FRAME, FWD OTBD EDGE, GOUGED. REPLACED DOUBLER IAW DWG 5930584.SDR AALA20150804004Hinge · wornAIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CLIMB VIBRATION WAS FELT IN THE NLG AREA. CONTINUED AROUND THE TRAFFIC PATTERN UNTIL THE NLG WAS LOWERED. POST FLIGHT WALK AROUND REVEALED THAT THE LT GEAR DOOR WAS CLOSED & THE SDR CA150807001Door · detached(CAN) THE NLG AFT DOOR SEPERATED FROM THE AIRCRAFT DURING LANDING AND FELL ON TAXIWAY.SDR FDEA201507312445Door · delaminatedLEFT MLG DOOR DELAMINATED. MISSING SECTION CRAZ COMPLY WITH EA F-5280-T0319221 REV NR POS P3. R & R MLG DOOR IAW MM 32-12-01-4 & EA F-5280-T0319221.SDR AALA201507229008Attach Fitting · wornLEFT MLG DOOR FWD ATTACH FITTING TO RIB 5 IS WORN. REPLACED LT MLG DOOR FWD ATTACH FITTING IAW CMM 52-81-18 STEP A1.SDR 7C7A20150715064Door · out of adjustGAP OF LT MLG AFT DOORS TO NACELLE & EACH OTHER EXCEEDS AMM LIMITS.SDR 2015FA0000323Door · crackedFOUND LT MLG DOOR CRACKED AT THE FORWARD HINGE AREA.SDR FDEA201507102188Door · crackedA CRACK WAS FOUND ON LEFT STRUT DOOR STRUCTURE AT FWD HINGE. REPAIRED DOOR IAW SRM 52-82-07-2R.SDR UG8A2015070602Former · crackedLEFT INBD MLG DOOR FWD FORMER CRACKED. CRACK IS 1" LONG IN THE INSIDE RADIUS STARTING AT OTBD EDGE OF DOOR & TRAVELING INBD.SDR AALA201507069012Door · wornAIRCRAFT HAS NOTICEABLE AIRFRAME VIBRATION INFLIGHT AT CRUISE. HIGHEST ENG VIBRATION WAS 0.8 N1 ON NR 1 ENG, ALL OTHERS 0.0. REPLACED THE NLG LT AFT DOOR IAW AMM 32-22-13-400-001A. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.SDR CA150606002Bracket · broken(CAN) DURING A SNAG RECTIFICATION THE ENGINEER FOUND THAT THE NOSE GEAR DOOR RETRACTION ROD WAS DISCONNECTED FROM THE DOOR. THE BRACKET THAT THE ROD ATTACHES TO WAS BROKEN OUT AT THE ATTACHMENT HOLE. THE ROD WAS MOVING FREELY AND THE ROD ENDS WERE NOT SEIZEDSDR AALA201506019002Hinge · wornAFTER TAKEOFF & GEAR RETRACTION, DEVELOPED LOUD AIR NOISE & MINOR AIR FRAME VIBRATION BELOW & FWD OF COCKPIT. BELOW 25000 FT 280 KTS AMBER XXXX ON NOSE GEAR DOOR ECAM WHEEL PAGE, GEAR EXT ALL NORMAL. FOUND AFT RT NLG DOOR FWD HINGE ASSEMBLY WORN & REPLACED ISDR DALA2016111008480Structure · corrodedCORROSION ON RUB STRIP SETTLEMENT AREA AT RT MLG OUTBOARD DOOR. THE DOOR WAS REMOVED IAW AMM 32-12-21 201. AREAS WAS BLENDED (UT) WAS ACCOMPLISHED, FOUND OUT OF LIMITS. THE DOOR WAS REPLACED IAW SRM 51-10-03, 52-01, AND NDT SPM 04-00-07.SDR DALA2016111008479Structure · corrodedCORROSION ON RUB STRIP SETTLEMENT AREA AT LT MLG OUTBOARD DOOR. FIXED DOOR WAS REMOVED IAW AMM 32-12-21-201. AREA WAS BLENDED, UT WAS ACCOMPLISHED,FOUND OUT OF LIMITS. REPLACED IAW SRM 51-10-03, 52-10, AND NDT SPM 04-00-07.SDR CALA2015052200421Door · vibrationUPON GEAR RETRACTION EXTREMELY LOUD VIBRATION & AIR NOISE IN COCKPIT FLOOR & A ZONE GALLEY. SPEED NEVER ABOVE 250 KNOTS DUMPED 50,000 LBS FUEL & RETURNED. IAW NR`S 4916081, 4916090, 4916093, 4916086, 4916089, 4916100 & 4916094 ACFT OK FOR SERVICE. RT AFT NOSDR SWIA201541300Arm · gougedLEFT NLG DOOR AFT HINGE ARM HAS A GOUGE. REPAIRED LT NLG AFT HINGE ARM IAW STS EA.SDR CA150525015Door · detached(CAN) CREW REPORTED NOISE WHEN EXTENDING THE GEARS, WHILE TAXIING TO THE GATE, NOT ABLE TO TURN LEFT. AFT NLG DOOR FOUND HANGING DOWN WITH CONNECTING RODS BENT & BRACKET ATTACHING THE CONNECTING RODS TO THE NLG STRUT DAMAGED.SDR ASOA2015060413003Structure · damagedRT MLG DOOR AFT MID HAS DAMAGE. STS EA 32-2015-198 PERMANENT REPAIR IS COMPLIED WITH. EA 32-2015-198 HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOUCMENTED AND SIGNED FOR ON A NON-ROUTINE WC.SDR YENA20150510111Door · shearedON WALKAROUND, FOUND LT MAIN GEAR HINGED FAIRING DOOR SHEARED OFF. INSTALLED AND ADJUSTED FAIRING REF AMM 32-12-13-400-001. REPAIRED ASSOCIATED DAMAGE AT FR 55-56, STR 26-27 IAW SRM 53-00-11, FIG 209.SDR UIEA2015050500258Door Seal · defectiveGEAR DISAGREE & GEAR DOOR EICAS WHEN LG WAS FIRST LOWERED. ACCOMPLISHED QRH & GEAR INDICATED DOWN. RT WING MAIN GEAR INDICATED IN TRANSIT. R & R RT BODY OTBD GEAR DOOR SEAL IAW AMM 52-09-00. PSEU GND TEST PASSED IAW AMM 32-09-03/501.SDR DALA2015042903029Skin · damagedLIGHTINING STRIKE ON LT NLG DOOR APPROXIMATELY BS 379. BLENDED SURFACE AREA IAW SRM 53-00-01. DAMAGE CONTAINED. OK TO ALODINE AND PAINT A CONE. INSPECTED AREA WITH 10X. DAMAGE REMOVED.SDR DALA2015042903024Skin · damagedLIGHTINING STRIKE AT BS 283, RT NLG DOOR. BLENDED SURFACE AREA IAW SRM 53-00-01. DAMAGE CONTAINED OK TO ALODINE AND PAINT. INSPECTED WITH A 10X. DAMAGE REMOVED.SDR SWIA201541154Skin · gougedLEFT MLG DOOR GOUGE ON INNER SKIN INBD FWD, MARKED. REPAIRED LT MLG DOOR GOUGE ON INNER SKIN INBD FWD REF STS EA.SDR SWAA2015042438881Bracket · crackedLEFT MLG MID DOOR AFT ATTACHMENT TO STRUT BRACKET CRACKED. R & R DOOR BRACKET IAW MM.SDR DALA2015041402755Skin · wornWEAR ON LT MLG STRUT DOOR INBD SKIN ON FWD LWR EDGE AND LWR AFT EDGE. LT MLG STRUT DOOR WAS REPAIRED IAW AC 0966 CARD 2000-8149-02, JOB 000-0004 AND ETI-88-15-116, REV 1, ER/A 534333-14, REV ORIGINAL, LP 1903243 .SDR DALA2015040902716Channel · crackedCRACKS ON CHANNEL STA Y=953 AT LT MLG INBD DOOR. FASTENERS WAS REMOVED, CRACK WAS STOP DRILL AND DOUBLER REPAIR WAS FABRICATED, TREATED AND PAINTED IAW SRM 51-30-2, 52-05, FIG 6, 51-10-3, PAR 14/21 AND INSTALLED IAW SRM 52-05, FIG 60. LP 1896870.SDR SWIA201541096Structure · chafedRT MLG DOOR AFT OTBD EDGE CHAFED. C-CHECK, RO 4/22/15, COMPLIED WITH REPAIR OF RT MLG DOOR OTBD EDGE REF REO.SDR SWAA2015050839493Support · crackedRIGHT WW DOOR CROSS BAR LOWER SUPPORT CRACKED. R & R CROSS BAR IAW SRM.SDR SWAA2015043039168Fitting · crackedLEFT MLG WW DOOR AFT UPPER INTERNAL FITTING CRACKED. R & R FITTING IAW DWG.SDR USAA2015032700004Hinge Fitting · wornRIGHT MLG DOOR AFT HINGE BRASS BUSHING HAS EXCESSIVE PLAY IN MOUNT BRACKET. R & R REAR HINGE FITTING IAW CMM 52-81-18.SDR SWAA2015032637896Door · crackedLEFT MLG MIDDLE DOOR & AFT ATTACH FITTING CRACKED. R & R DOOR IAW MM.SDR SWAA2015032337709Door · delaminatedLEFT MLG INNER DOOR DELAMINATED. R & R DOOR IAW AMM.SDR SWAA2015042438932Skin · crackedLEFT MLG DOOR INNER SKIN FWD OTBD CORNER CRACKED. REPAIRED SKIN IAW EA.SDR SWAA2015042238785Skin · crackedLEFT MLG DOOR INNER SKIN FWD OTBD CORNER CRACKED. REPAIRED DOOR IAW FAS EA.SDR SWIA201540982Structure · chafedLEFT MLG DOOR HAS CHAFE DAMAGE ON INTERIOR SIDE AT DOUBLER, LOWER FWD CORNER AREA, C-CHECK, RO 4/2/15, CHAFING DAMAGE IS CONTAINED TO INNER SKIN FILLER FROM PREVIOUS REPAIR AND IS NOT WITHIN LIMITS IAW SRM. R & R REPAIR FILLER, PN 601R-52-82-016-3 IAW SRM .SDR USAA2015040100018Hinge Fitting · worn3S CHECK, RT MLG DOOR FWD HINGE FITTING HAS EXCESSIVE PLAY. REPLACED HINGE FITTING IAW CMM 52-81-18-400-009-A01.SDR FDEA201503040647Skin · damagedRIGHT MLG STRUT DOOR HAS A TWO INCH LONG HOLE IN THE OUTER SKIN. REPAIR DAMAGE IAW SRM 51-71-00. PREP & PAINT IAW SRM 51-21-02.SDR SWAA2015040238788Fitting · crackedLEFT MLG WW DOOR LOWER FWD CORNER CLIP CRACKED. R & R CLIP IAW SRM & DWG.SDR DALA2015030401940Channel · wornWORN SPLICE ON AFT CHANNEL AT RT INBD MLG DOOR. REMOVED DAMAGE. FABRICATED AND INSTALLED REPAIR ANGLE IAW EA 469617-14, REV AFC.SDR DALA2015030301932Channel · crackedCRACKED LOWER CHANNEL, RT INBD MLG DOOR, AFT SECTION. REPAIRED IAW SRM 52-80-02, FIG 2.SDR DALA2015022701784Channel · wornWORN PREVIOUS DOUBLER REPAIR ON AFT CHANNEL AT RT INBD MLG DOOR. REMOVED DOUBLER. FABRICATED AND INSTALLED NEW DOUBLER IAW SRM 52-80-02, FIG 8, 51-10-05, 51-10-03 AND 51-30-02.SDR SWIA201540871Skin · damagedLIGHTNING STRIKE ON RT NLG DOOR, C-CHECK, REPAIRED LIGHTING STRIKE ON RT NLG DOOR IAW STS EA.SDR DALA2015022601661Intercostal · crackedCRACKED INTERCOSTAL ON LT INBD MLG DOOR BETWEEN STA Y=948-953. CRACKED INTERCOSTAL WAS REMOVED IAW SRM 51-30-2. NEW INTERCOSTAL WAS FABRICATED IAW SRM AND DWG 51-10-2, 5930583-257, DWG 5930583, REV CK. NEW INTERCOSTAL WAS TREATED AND PAINTED IAW SRM 51-10-3SDR CA150220008Door · departed(CAN) DURING THE WALKAROUND AFTER LANDING, THE CREW NOTICED LT MLG DOOR MISSING. THERE IS NO DAMAGE NOTICED TO AIRFRAME OR FLAPS. DISPATCH FIGURES THAT THE FUEL BURNS WERE BANG ON FOR THIS FLIGHT SUCH THAT PERHAPS IT DEPARTED THE A/C CLOSER TO LANDING. MAINTESDR IXXA20150331084Hinge Fitting · crackedAIRCRAFT ON GND FOR HEAVY MX, FAILSAFE INSPECTION. FWD FITTING AT BODY DOOR CTR HINGE BEAM CRACKED. R & R RT MLG DOOR HINGE FITTING AT CTR BEAM TO DOOR CTR IAW SRM 51-40-02. OPERATIONAL CHECKED SATISFACTORY. NO LEAKS NOTED IAW AMM 32-32-12.SDR DALA2015022001489Door · crackedCRACK ON AFT NLG WHEEL WELL DOOR RT. NLG WHEEL WELL DOOR RT WAS REMOVED IAW AMM 32-22-01. NLG WHEEL DOOR RT SERVICIABLE WAS INSTALLED IAW AMM 32-22-01.SDR DALA2015022101528Skin · corrodedCORROSION ON SKIN OF RT MAIN GEAR STRUT DOOR BELOW RUBSTRIP. DOOR WAS REMOVED IAW AMM 32-12-01. CORROSION OF RT MAIN GEAR STRUT DOOR WAS REMOVED IAW SRM 52-01. AREA WAS MEASURED IAW NDT SPM 04-00-07. ORIGINAL THICKNES 0.063 REMAINING THICKNESS 0.041. THERE
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