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 08FDEA00793Skin · delaminatedRT MAIN LANDING GEAR DOOR EXTERNAL SKIN HAS DELAMINATION 34" FROM THE FWD END. REMOVED DAMAGE AT THE TWO EACH AREAS. PERPARED AREA FOR REPAIR PLY LAY UP. LAYED UP, BAGGED & CURED REPAIR PLYS. APPLIED & CURED ROSIN COAT, RESTORED FINISH IAW SRM 52-81-10 & 51SDR 08FDEA00788Panel · damagedRT MLG ZONE 742 STRUT DOOR LOWER AFT SECTION HAS A DEEP NICK AND THE EDGE IS CHIPPED AWAY. REMOVED DAMAGE AND REPAIRED IAW SRM 52-81-11 PB 201 & 51-77-11 CHAP 4D.SDR CDN2008F00001Door · missingAT 10,000 FT, CREW OBSERVED A LANDING GEAR UNSAFE LIGHT, FOLLOWED BY VIBRATION AND AIR NOISE. AC WAS SLOWED TO BELOW 250 KTS AND THEN CREW HEARD A (BANG) NOISE. AFTER LANDING IT WAS NOTICED THA THE RT OB GEAR DOOR HAD SEPARATED FROM THE AIRCRAFT. (K)SDR CDN2008F00000Hinge · crackedCREW NOTICED A LANDING GEAR DOOR UNSAFE INDICATION IN FLIGHT. THE GEAR WAS LOWERED WITH GEAR DOWN AND LOCKED INDICATIONS NORMAL. INSPECTION REVEALED THAT THE OB RT GEAR DOOR HINGE WAS CRACKED WHICH CAUSED THE DOOR TO NOT FULLY CLOSE. THE CONDITION WAS AGRIVSDR QXEA200800258Bushing · migratedPDX - C4 - LEFT NACELLE, FORWARD INBOARD DOOR, AFT HINGE, FORWARD BUSHING HAS MIGRATED OUT OF NACELLE HINGE FITTING. REMOVED ATTACH HINGE AND INSTALLED NEW HINGE IAW DASH 8 Q400 SRM 51-42-05, 51-40-15, 51-42-15, 51-42-45.SDR A6WA200840138Door · damagedLT MLG FIXED DOOR FOUND WORN ON LT END SECTION. REPAIRED IAW REO 601R-52-82-034 SHEET 1 THROUGH 4. (M)SDR A6WA200840137Door · wornRIGHT MLG FIXED DOOR FOUND WORN ON L/E END SECTION. RIGHT MLG FIXED DOOR REPAIRED IAW REO 601R-52-82-016 SHEET 1 THROUGH 4. (M)SDR P5CA0801546Door · delaminatedRIGHT WING GEAR INBD STRUT DOOR HAS SKIN DELAMINATION. ACCOMPLISHED PART 1 OF THE TIME LIMITED REPAIR OF MA NR A45280-02:00. COI NR 453-031 WAS OPENED FOR A 5-CYCLE VISUAL INSPECTION.SDR HALA0800298Structure · damagedLIGHTNING STRIKE ON RT FWD NOSE GEAR DOOR GAP SEAL FASTENERS, 17 EACH SCREW HEADS. CLEANED, TREATED AND PRIMED PER SRM 53-00-01 PAINT PEND. AREA PAINTED AS PER 51-22-01.SDR HALA0800300Seal · damagedLIGHTNING STRIKE ON RT FWD NOSE GEAR DOOR GAP SEAL FASTENERS (17 EACH SCREW HEADS). CLEANED, TREATED AND PRIMED PER SRM 53-00-01 PAINT PEND. AREA PAINTED AS PER 51-22-01.SDR HALA0800341Channel · crackedCRACK ON RT MLG I/B DOOR, FWD "Z" CHANNEL. REPAIR IN WORK.SDR HALA0800328Door · corrodedLEVEL 1 CORROSION ON INNER SURFACE OF RT MLG OUTBOARD DOOR. REPAIR IN WORK.SDR HALA0800329Door · corrodedLEVEL 1 CORROSION ON THE EXTERIOR SURFACE OF THE RT MLG OTBD DOOR. REPAIR IN WORK.SDR HALA0800296Structure · corrodedSURFACE CORROSION AND PAINT PEELING ON LT MLG DOOR ON LEADING EDGE, REPAIR IN WORK.SDR HALA0800294Skin · corrodedRT MLG DOOR HAS SURFACE CORROSION ON OUTER SKIN. REPAIR IN WORK.SDR HALA0800293Intercostal · crackedRT MLG DOOR INTERCOSTAL CRACKED SEEN INSIDE FWD MID ACCESS PANEL. REPAIR IN WORK.SDR HALA0800295Skin · corrodedLT MLG DOOR HAS SURFACE CORROSION ON OUTER SKIN. REPAIR IN WORK.SDR HALA0800292Door · crackedRT MLG DOOR RAMP CRACKED AT INBD MOUNT BRACKET. REPAIR IN WORK.SDR 08FDEA00422Door · wornRT MLG WW, FOUND DOOR ASSEMBLY PANEL NR 741AL WITH EDGES WORN. REPAIRED AS PER EA 1-5280-117392, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR ABXR080070Door · crackedRIGHT MAIN LANDING GEAR INBOARD DOOR CRACKED, UPPER AFT CORNER. REPAIRED CRACKED AREA IAW DC9 REA D952-57026.SDR 2008FA0000070Hinge · brokenDURING FLIGHT WHEN THE LANDING GEAR WAS OPERATED, THERE WAS A NOISE HEARD BY THE CREW. UPON LANDING THE LT MAIN LANDING GEAR DOOR WAS ATTACHED ONLY BY THE LOWER DOOR CONTROL LINK. THE REAR GEAR DOOR HINGE, AFT BRACKET HAD BROKEN AT THE WELD OF THE PIECE BOLTEDSDR USAA920080343Hinge Fitting · crackedSAL - MAJOR REPAIR - BC2 CHECK - NR 6038208, NOSE LANDING GEAR RIGHT DOOR CENTER HINGE FITTING CRACKED. REPLACED THE NOSE LANDING GEAR RIGHT DOOR CENTER HINGE FITTING IAW A320 SRM 51-72-11.SDR 2008FA0000274Door · damagedTHE PILOT WAS INFORMED BY THE FUEL TRUCK DRIVER THAT THE LT MLG IB DOOR WAS NOT PROPERLY LOCKED IN THE UP POSITION, AND THE OB PORTION OF THE DOOR HAD MADE CONTACT WITH THE RUNWAY DURING LANDING. ENGINEERING DEPT RECOMMENDED THAT THE AIRPLANE BE FLOWN BACK UNSDR UIEA200800020Structure · delaminatedLT MAIN LANDING GEAR OUTBOARD STRUT DOOR HAS AN 18.0 INCH LONG SECTION AT LEADING EDGE OF MATERIAL SEPARATING. PERMANENT REPAIR ACCOMPLISHED AS PER SRM 51-40-09 FIG 12 SHEET 1 AND 4 AND SRM 51-40-12, PREPREG 250 DEGREES F CURE. ALSO REFERENCE EO NR 4752A129.SDR QXEA200800040Door · missingONT- FLIGHT 2509 (PDX-ONT) - WHEN CLIMBING OUT OF 10,000 FEET AFTER DEPARTURE FROM PDX, A BANG WAS HEARD AND A SHUDDER WAS FELT FOR A MOMEMENT WHICH FELT LIKE IT WAS FROM THE FORWARD BELLY AREA. ALL INDICATIONS NORMAL. CONTINUED TO ONT AND ACCOMPLISHED A UNEVSDR ASAA0842525Skin · crackedLT MLG INNER GEAR DOOR AFT EDGE CRACKED PREPARED DAMAGED AREA APPLIED SEVERAL LAYERS OF BMS 3 FIBERGLASS CLOTH AND BONDED IN ACCORDANCE WITH B737 400 SRM 52 80 02 REPAIR 2 AND 52 40 02 PG 203.SDR IXXA08SMN012SDoor · delaminatedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING (MLG/FUSELAGE) UPPER DOOR DELAMINATED SKIN. REMOVED DAMAGED DOOR. INSTALLED NEW DOOR. PERFORMED OPS CHECK FOR HYD SYSTEM LEAKS GOOD IAW DC8 MAINTENANCE MANUAL 32-12-1 PAGE 401, DC8 27-10-0, 27-20-0, 27-40-0SDR IXXA08SMN011SSkin · delaminatedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING (MLG/FUSELAGE) MIDDLE DOOR DELAMINATED SKIN. REMOVED DELAMINATED DOOR. INSTALLED NEW MID DOOR. PERFORMED OPS CHECK FOR HYD SYSTEM LEAKS GOOD IAW DC8 MM 32-12-1 PAGE 404, DC8 MM 27-10-0, 27-20-0, 27-40-0, 27SDR IXXA08SMN010SDoor · delaminatedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING (MLG/FUSELAGE) UPPER DOOR DELAMINATED SKIN. REMOVED RIGHT MAIN LANDING GEAR OUTBOARD DOOR. INSTALLED NEW DOOR. PERFORMED OPS CHECK FOR HYD SYSTEM LEAKS GOOD IAW DC8 MM 32-12-1 PAGE 404, DC8 MAINTENANCE MANSDR 08FDEA00129Frame · crackedRIGHT MAIN LANDING GEAR DOOR, NEAR INBOARD STRUT FAIRING UPPER MOUNTING AREA, FOUND CRACKED. CRACK AT RIGHT MAIN LANDING GEAR DOOR, NEAR INBOARD STRUT FAIRING UPPER MOUNTING AREA REPAIRED AS PER FEDEX EA NR 1-3210-116535, TITLE: LANDING GEAR, MAIN GEAR DOORSDR 08FDEA00128Frame · crackedLEFT MAIN LANDING GEAR DOOR, NEAR INBOARD STRUT FAIRING UPPER MOUNTING AREA FOUND CRACKED. CRACK AT LEFT MAIN LANDING GEAR DOOR, NEAR INBOARD STRUT FAIRING UPPER MOUNTING AREA. REPAIRED AS PER FEDEX EA NR 1-3210-116534, TITLE: LANDING GEAR MAIN GEAR DOOR LSDR 2008FA0000273Door · damagedAFTER ROUTINE FLIGHT, THE PILOT WAS PERFORMING HIS PREFLIGHT WALKAROUND INSP IN PREPARATION FOR THE NEXT LEG OF THE FLIGHT. HE NOTICED THAT BOTH MLG OUTER DOORS WERE DAMAGED. MECH/ MAINT WENT TO EVALUATE THE DAMAGE TO THE DOORS. RECOMMENDED THAT THE AIRPLANSDR 2008FA0000272Door · damagedAFTER ROUTINE FLIGHT, THE PILOT WAS PERFORMING HIS PREFLIGHT WALKAROUND INSP IN PREPARATION FOR THE NEXT LEG OF THE FLIGHT. HE NOTICED THAT BOTH MLG OUTER DOORS WERE DAMAGED. MECHANIC/MAINT WENT TO EVALUATE THE DAMAGE TO THE DOORS. RECOMMENDED THAT THE AIRPSDR 08FDEA00108Door · chafedRT MLG FLIPPER DOOR FORWARD SIDE FOUND CHAFED. RT MLG FLIPPER DOOR FORWARD SIDE CHAFFED EDGE SMOOTHENED OFF AND FOUND WITHIN LIMIT AS PER SRM 52-00-01 FIGURE 1 VOLUME I. RT MLG AND GEAR WHEEL DOOR OPERATION CHECK CARRIED OUT AS PER AMM 32-31-00-700-803. SDR UPS08851537Fitting · damagedINSPECTION TYPE:C2 RT MLG DOOR SWITCH MOUNT HOLES ARE ELONGATED. FABRICATED AND INSTALLED REPAIR DOUBLER ON RT MLG DOOR MOUNT SWITCH FITTING IAW EO DC8-3260-16914-A.SDR UPS08851536Door · damagedINSPECTION TYPE:C2 L/MLG DOOR SWITCH MOUNT HOLES ARE ELONGATED. FABRICATED AND INSTALLED REPAIR DOUBLER ON LT MLG DOOR SWITCH MOUNT FRAME IAW EO DC8-3260-16914-A.SDR DLM90080064Skin · corrodedLMLG DOOR EXTERIOR SKIN CORRODED ALONG HINGE LINE. REPLACED LMLG DOOR.SDR DLM90080063Skin · corrodedRMLG DOOR EXTERIOR SKIN CORRODED OVER ENTIRE SURFACE. REPLACED RMLG DOOR.SDR MASA200800014Fastener · damagedDURING INSPECTION OF LT MLG DOOR PANEL FOUND LT PANEL DOOR AFT BRACKET FASTENER WORN/DAMAGED. REPLACED DOOR.SDR UPS08851432Skin · crackedINSPECTION TYPE:C2 REPAIR DOUBLER CRACKED ON R/MLG INBD DOOR INTERIOR SKIN, BOTTOM. REMOVED CRACKED REPAIR DOUBLER ON R/MLG INBD DOOR INTERIOR SKIN IAW SRM 51-01-21A. FABRICATED AND INSTALLED REPAIR DOUBLER ON R/MLG INBD DOOR INTERIOR IAW SRM 52-06-00 FIG 1.SDR 07FDEA05121Hinge · crackedRT AFT NLG DOOR FWD HINGE FITTING CRACKED REMOVED AND REPLACED FWD HINGE FITTING ASSY. ON RT AFT NLG DOOR REF A310-200, CMM 52-82-12 AND AIRBUS INDUSTRY PMS 01-05-58.SDR 07FDEA05077Hinge Fitting · crackedLT AFT NLG DOOR, AFT HINGE CRACKED. REMOVED AND REPLACED LT AFT NLG AFT HINGE FITTING IAW A310-200 CMM 52-82-12 P 204.SDR CA071214011Bolt · missing(CAN) PILOT NOTICED ON PRE-FLIGHT, ABNORMAL ANGLE OF GEAR DOOR. IT WAS DISCOVERED THAT THE BOLT SECURING THE DOOR WAS MISSING. THIS STRESSED THE AFT BRACKET TO THE POINT OF CRACKING WHICH ALSO CAUSED THE DOOR TO CRACK ALONG THE BOLT HOLES. (TC NR 20071214011)SDR 1218363020708Stiffener · crackedSTIFFENER BROKEN ON FORWARD LEFT SIDE OF NOSE LANDING GEAR DOOR. LEFT AFT NOSE LANDING GEAR DOOR STIFFENER REPLACED IN ACCORDANCE WITH SRM.SDR UIEA200700489Structure · crackedLT WING GEAR INBOARD STRUT DOOR HAS FORWARD EDGE COMPOSITE CRACK. PERMANENT REPAIR ACCOMPLISHED AS PER B747-300 SRM 51-40-09, FIG 12, SHEETS 1, 2 AND 3.SDR TRAX200701906Bracket · crackedPAX DOOR SURROUND 255DW, 255EW IN CRACKED. NLG FWD LT DOOR FWD STOP BRACKET REPLACED IAW SRM 51-25-01REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH S.P. 663 AND FAR 43, APPENDIX A. REPAIR CCOMPLISHED IN ACCORDANCE WITH SRM 51-25-01.SDR A6WA200740691Skin · damagedON MLG DOOR RIGHT INNER SKIN, ABRASION EXIST ON FORWARD SIDE OF DOOR, LOWER AND UPPER. (M) REPAIRED IAW REO 601R-52-82-016 AND REO 601R-52-82-102. (K)SDR A6WA200740690Skin · damagedON LT MLG DOOR INNER SKIN, FOUND ABRASION ON FORWARD SIDE OF DOOR, LOWER AND UPPER. (M) REPAIRED IAW REO 601R-52-82-016 AND REO 601R-52-82-102. (K)SDR TRAX200701898Bracket · crackedNLG FWD LT DOOR, FWD STOP BRACKET CRACKED.
SDR DALA1134409222Pan · crackedLEFT MAIN LANDING GEAR DOOR PAN CRACK REPAIR. REPAIRED PER BOEING MESSAGE 1-691375741-2.
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