JASC 5300
Service difficulty reports · 8,206
Reports filed under 5300 · Fuselage Structure (General), 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 = '5300' 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 = '5300' 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 SWIA201440072Panel · damagedPANEL 221BLC HAS A MISSING TAB AND PANEL SEAL IS DISBONDED. REPAIRED PANEL IAW EA AND SRM.SDR SWIA201440070Panel · crackedPANEL 221CLC IS CRACKED AROUND A MOUNTING HOLE. REPAIRED DAMAGED AREAS IAW EA.SDR DALA2014102005630Structure · corrodedDURING INSPECTION, FOUND CORROSION ON FWD LOWER CORNER AT FRAME 16 RT OF FWD PASSENGER/CREW DOOR CUTOUT. REPLACED IAW SRM 51-72-11 AND DWG D53112109.SDR DALA2014101905629Structure · corrodedDURING INSPECTION, FOUND CORROSION ON AFT LOWER CORNER , RT OF FWD PASSENGER/CREW DOOR CUTOUT AT FRAME 20. REPLACED IAW SRM 51-72-11 AND DWG D53112109.SDR DALA2014101605564Unknown · corrodedDURING INSPECTION, FOUND CORROSION ON SECTION CONNECTOR LOCATED AT LEVEL OF FRAME 67 AND STR 27L. L=1", W=0.500", D= 0.010" APPROXIMATELY, SSI 534144. REPLACED SECTION CONNECTING LOCATED AT LEVEL OF FRAME 67 AND STR 27L IAW SRM 51-72-11 AND DWG, D53480009.SDR WVER201410150005Unknown · crackedCORROSION DETECTED AT FS 280 AT LBL 12, RBL 12, RBL 27, RBL 36, AND A CRACK DETECTED AT LBL 12.SDR DALA2014101605567Unknown · corrodedDURING INSPECTION, FOUND CORROSION ON SECTION CONNECTION LOCATED AT LEVEL OF FRAME 67 AND STR 31L. L=1.50", W=0.700", D=0.010" APPROXIMATELY, SSI 534144. REPLACED SECTION CONNECTING LOC AT LEVEL OF FRAME 67 AND STR 31L IAW SRM 51-72-11 AND DWG D53480009.SDR SWIA201439363Shroud · debondedPANEL 520JL HAS SHROUD TO SKIN DEBONDING IN SERVERAL SPOTS. BONDED PANEL 520JL, SHROUD TO SKIN L/E, REF REO. (2014NM060066)SDR WVER0904201492405Floorbeam · crackedTHE RT AND LT COCKPIT FLOORBEAM ATTACH FLANGES AT BS 280 ARE CRACKED AT THE RADIUS APPROX. .750 LONG. REPAIRED FLOORBEAM IAW REO 690-53-11-695, REV.SDR DXTR2014072101Unknown · vibrationAT FL210, HAD AN AIRFRAME VIBRATION NOTICED AT 300 KIAS AND INCREASED AS AIRSPEED INCREASED. INTENSITY INCREASED IN LT TURNS, CLIMBS, DESCENTS, AUTO-PILOT ON & OFF, YAW DAMPER ON & OFF, RUDDER BIAS ON & OFF. HAD NO EFFECT. THERE WAS NO ABNORMAL VIBRATION IN SDR DALA2014070403888Unknown · corrodedDURING INSPECTION, FOUND CORROSION ON FWD LOWER CORNER LOCATED FRAME 66 AND STRINGER 23L. REPLACED LOWER CORNER LOCATED FRAME 66 AND STR 23L AFT PAX CABIN IAW SRM 51-72-11, AND DWG D534 80009.SDR DALA2014070403889Unknown · corrodedDURING INSPECTION, FOUND CORROSION ON AFT LOWER CORNER LOCATED FRAME 68 AND STR 23L. REPLACED LOWER CORNER LOCATED FRAME 68 AND STR 23L AFT PAX CABIN IAW SRM 51-72-11, AND DWG D53480009.SDR R61A201406250844Unknown · corrodedDURING HEAVY CHECK, RT STBILIZER UPPER SURFACE AT FRAME 14 HAS CORROSION. MX R & R RT SEAT TRACK IAW SRM 51-40-02, 51-41-01. REPAIRED T-CLIP AT FRAME 17 IAW ETD 2014-170-053968, REV A. PN 170-03263-001, TRACK RT.SDR SWIA201438551Panel · crackedPANEL 326DR IS CRACKED. C-CHECK, PERFORMED REPAIR TO PANEL 326DR IAW EA.SDR CA140630014Unknown · vibration(CAN) DURING REVENUE FLIGHT IN CRUISE, THE CREW FELT A HIGH VIBRATION IN THE CABIN AND ELECTED TO DIVERT. AN UNEVENTFUL LANDING WAS CARRIED OUT. TROUBLESHOOTING IN PROGRESS. BOROSCOPE OF THE ENGINE IS UNDERWAY.SDR ASAA2014053107985Unknown · vibrationCREW NOTED ODD VIBRATION, CYCLICAL TWO CYCLES A SECOND APRROXIMATELY FIVE MINUTES PRIOR TO CENTER TANK FUEL LOW PRESSURE LIGHTS ILLUMINATED. ON SHUTTING OFF CENTER TANK PUMPS, VIBRATION WENT AWAY FOR REMAINDER OF FLIGHT. ACFT GROUNDED. PERFORMED CENTER BOSDR VNAA2014051500009Structure · damagedCREW REPORTED POSSIBLE LIGHTNING STRIKE ON LT SIDE OF ACFT. MAINTENANCE PERFORMED LIGHTNING STRIKE INSPECTION AND R & R THE LOWER VHF ANTENNA AND STATIC WICKS ON HORIZONTAL STABILIZER. REPAIR PERFORMED FOR BURN MARK ON LT SIDE AFT TAIL CONE. MAINTENANCE PERSDR DALA2018032701976Doubler · crackedEXTERNAL REPAIR DOUBLER WAS FOUND CRACKED. THE REPAIR DOUBLER WAS REPLACED IAW SRM 53-20-15-2R-12, FIG 201.SDR 2014FA0000181Screw · wrong partSCREWS ON THE OUTER PANELS ON THE FUSELAGE ARE HITTING THE FRAME ALL AROUND THE LOWER SECTION OF THE FRAME. SCREWS SEEM TO BE TO LONG AND ARE ERODING THE FRAME TUBING IN CERTAIN AREAS. THIS SEEMS TO BE A FLAW IN THE DESIGN OF THE MANUFACTURER. IT SEEMS THE SCRSDR SWIA201437748Structure · mechanic errorDURING REMOVAL OF FS 621 FIREBLOCK, FOUND A DRILL START ADJACENT TO FASTENER HOLE AT LBL 33.75, WL .126 APPROX .023" DEEP. C-CHECK. REPAIRED FS 621.00 BULKHEAD WEB BETWEEN LBL 27.50 AND LBL 36.20 IAW REO.SDR XCGA20140322001Bonding · unserviceablePILOT REPORTED COMM RADIOS UNUSABLE BELOW 130.000 MHZ WHILE IN FLIGHT. HIGH PITCHED SQUEAL INTERFERENCE HEARD. BACKUP HANDHELD TRANSCEIVER WAS ALSO AFFECTED IN THE SAME FREQUENCY RANGE. PILOTS SQUAWKED 7600 & PROCEEDED VFR IAW 14 CFR 91.185. PILOTS USED SASDR ASOA2014033110248Post · crackedFOUND FS 409.0+128 VERTICAL POST RBL 18.0 INBD AND OTBD SIDES HAVE CRACK INDICATIONS IN AFT FLANGE RADIUS APPROX .3 INCH IN LENGTH 50 PERCENT FSH. REMOVED POST IAW SRM 51-42-06. LOCATED, DRILLED AND ASSEMBLED NEW POST IAW SRM 51-40-11, 51-42-06. INSTALLED PSDR SWIA201436727Unknown · corrodedCORROSION FOUND BETWEEN BS 409+128 AND 559 RT SIDE. PERFORMED REPAIR IAW REO.SDR DALA14010483146Structure · corrodedCORROSION STRUCTURE FRAME 68, Y1162 S23L. REPLACED STRUCTURE IAW SRM 51-72-11 AND DWG D534-70150.SDR VNAA2014020900004Unknown · crackedDURING SCHEDULED MAINTENANCE FS 379.0, STRINGER 3L WAS CRACKED. THE AREA WAS INSPECTED AND REPAIRED USING AMM. ACFT WAS RELEASED FOR SERVICE.SDR VIBR20140219003Bracket · leakingBAROMETRIC SWITCH BOX ASSEMBLY LOOSES PRESSURE AT 1000 FT. HAS LEAK AT MOUNT BRACKET RIVETS.SDR 2013FA0000646Nut · crackedDURING A SCHEDULED MAINTENANCE EVENT, FOUND SEVERAL CRACKED AND MISSING MS21042 TYPE NUTS ON RETARDANT TANK STRUCTURE. WE HAVE INVESTIGATED THIS ISSUE AND FOUND THAT SEVERAL OTHER OPERATOR'S/FOREIGN COUNTRY'S HAVE HAD THE EXACT SAME TYPE FAILURES (HYDROGEN ESDR VNAA2013111700008Unknown · crackedDURING SCHEDULED MAINTENANCE, FS 280 HAD A POSSIBLE CRACK. THE AREA WAS INSPECTED AND REPAIRED USING AMM. AIRCRAFT WAS RELEASED FOR SERVICE.SDR ASOA20131116432Unknown · vibrationACFT WAS FERRIED FOR AN CHECK FOR STRONG VIBRATION IN FLIGHT CONTROLS ON CLIMBOUT AND DESCENT. MAINTENANCE PERFORMED VARIOUS TESTS AND INSPECTIONS, COMPLETED A CHECK FLIGHT THAT WAS FOUND GOOD. ACFT WAS RELEASED TO SERVICE.SDR 2013FA0000658Structure · damagedCOMPOSITE DAMAGE NOTED ON FUSELAGE RT VENTRAL FIN OTBD FACE, SEVERAL LOCATIONS BETWEEN FS 756.0 AND 768.5. DAMAGE DETERMINED TO BE BEYOND SRM LIMITS. DAMAGE REPAIRED IAW PRINCIPLES OF SRM, CH 53-90-10 IAW REPAIR STATEMENT 340SDS034517.SDR DALA13050553715Unknown · crackedDURING INSPECTION, FOUND OTBD AFT BOLT HOLE SHOWS CRACK INDICATION AT LBL 45.5. MX REPAIRED IAW ERA 519357-14, REV O.SDR DALA13050543715Unknown · crackedDURING INSPECTION, FOUND INBD FWD BOLT HOLE AND BOTH OTBD BOLT HOLES SHOW CRACK INDICATION AT LBL 24.75. MX REPAIRED IAW ERA 519357-14, REV O.SDR DALA13050533715Unknown · crackedDURING INSPECTION, FOUND FWD INBD HOLE HAS CRACK INDICATION, RBL 45.5. MX REPAIRED IAW ERA 519357-14, REV O.SDR ASOA2013092709113Structure · chafedFUSELAGE HAS CHAFE DAMAGE AT APPROX BS 913.00 STR 27. REPAIRED IAW REO 670-53-00-290. REPAIR CLASSIFIED AS MAJOR.SDR 2013FA0000611Turnbuckle · crackedONE CABLE HAS FRAYED STRANDS, THE OTHER CABLE HAS STRESS CRACKS IN TURNBUCKLE END. CABLES WERE FOUND ON ANNUAL INSPECTION AND AD COMPLIANCE. REPLACED CABLES.SDR 2013FA0000610Cable · frayedONE CABLE HAS FRAYED STRANDS, THE OTHER CABLE HAS STRESS CRACKS IN TURNBUCKLE END. CABLES WERE FOUND ON ANNUAL INSPECTION AND AD COMPLIANCE. REPLACED CABLES.SDR CALA2013081690497Drain · cloggedNR 2 J BOX DRAIN NEEDS TO BE CHECKED, DRAIN IS CLOGGED UP, MOISTURE WAS IN CONNECTORS. CLEANED "J" BOX DRAIN OF CLOG.SDR A6WA2013082741171Drag Angle · crackedCRACKED DRAG ANGLE. R & R DRAG ANGLE.SDR CALA2013080590128Unknown · vibrationAT DEPARTURE, FLT CREW REPORTED VIBRATION IN AFT GALLEY.SDR DALA13036160958Pin · wornMX DISCOVERED THAT THE TEE PIN AND THE TEE PIN BUSHING WERE WORN BEYOND ALLOWABLE LIMITS AND REQUIRED REPLACEMENT.SDR UALA2013071905066Seat Track · corrodedMAIN DECK BS 1830, LBL 33, SEAT TRACK FLANGE AROUND TIE DOWN FOUND CORROSION. REPLACED SEAT TRACK IAW SRM 51-40-02. MAJOR REPAIR.SDR UALA2013071705006Unknown · unknownVERY LOUD SQUEALING NOISE IN BACK OF ACFT. SEEMS LOUDEST IN-BETWEEN DOORS. PRESSURIZED ACFT AND NO FAULTS FOUND. INSPECTED L2 AND R2 DOORS AND VHF ANTENNA AND NO DEFECTS NOTED.SDR UALA2013071504932Unknown · damagedTWO SCRATCHES IN RVSM AREA ON RT SIDE. BUFFED OUT AND WAVINESS INSPECTION COMPLETED.SDR UALA2013071004819Unknown · noiseLOUD HUM OR SQUEAL OVERHEAD IN AFT ROWS AND LT AND RIGHT NR 2 DOORS. ONLY OCCURS BELOW 10,000 FT. INSPECTED DOOR SEALS, WI- FI ANTENNA POD SEALS, AFT VHF ANTENNA SEAL, OUTFLOW VALVE OPERATION. NO DAMAGE NOTED TO SEALS. OUTFLOW OPS NORMAL. PERFORMED GENERALSDR SIMA20130710008Unknown · vibrationDURING CRUISE AT 24000 FT, NOTICED A LOUD NOISE ACCOMPANIED BY A CONTINOUS VIBRATION. DECELLERATED FROM 300 KTS TO 200KTS (APPROX). NOISE DECREASED BUT DID NOT GO AWAY. SUSPECT NOSE GEAR DOORS DEPLOYED PREMATURELY AS NOISE WAS MORE PRONOUNCED IN NOSE OF ACFTSDR 7AJA20130711004Unknown · vibrationTAXI TO RWY, , ADDING POWER FOR TAKEOFF, AT 1000 FT TORQUE ITT WAS AT 670 LE AND 680 RE. AT ROTATION, 95 KNOTS EXPERIENCED STRONG VIBRATION FROM THE SEAT NOT YOKE. AIRPLANE WASN’T PERFORMING NORMALLY, IT COULD BARELY CLIMB, STALL WARNING WAS GOING ON AND OSDR R61A201307300665Seat Track · corrodedDURING HEAVY CHECK. RT OTBD SEAT TRACK FROM BS 571.5 - 670 FOUND CORRODED. MX R & R SEAT TRACK IAW SRM 51-42-05 AND 51-40-15.SDR R61A201307300672Seat Track · corrodedDURING HEAVY CHECK. LT OTBD SEAT TRACK FROM BS 571.5 - 568 HAD CORROSION AND PITTING THROUGHOUT ENTIRE LENGTH. MX R & R SEAT TRACK IAW SRM 51-42-05 AND 51-40-15.SDR QXEA2013060301050Panel · corrodedSEVERAL AREAS OF SUSPECTED CORROSION ON PANEL 144JZ. REMOVED OLD PANEL IAW SRM 51-41-00-00-01. TRANSFERRED HOLES FROM OLD PANEL TO NEW PANEL IAW SRM 51-40-07-02-01. COUNTERBORED ALL HOLES ON NEW PANEL USING A MICRO STOP AND COUNTERSINK. TREATED BARE METAL INSDR DALA13025530126Unknown · corrodedFWD CARGO BAY BS 775, S35L FOUND CORRODED. MAINTENANCE REPLACED IAW SRM 53-00-03, REPAIR 2, FIG 201.
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