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 2008UALA04037Beam · corrodedBEAM 150 CORRODED.SDR P5CA0801571Structure · damagedDURING GROUND HANDLING THE TAIL JACK STRUCK THE TAIL SECTION OF THE AIRCRAFT NEAR THE TAIL POST FITTING IN SECTION 48 AT BS 2602. ACCOMPLISHED INTERIM REPAIR ACCORDING TO EO 4453A189, SRM 53-00-01 FIG 201, REPAIR 11. INITIAL AND REPEAT INSPECTIONS TO BE SCHESDR 2008UALA03909Unknown · vibrationVIBRATION AT SLOWER SPEEDS, GREATER INTENSITY DURING MANUVERING AT HIGHER ANGLE. WENT AWAY AT HIGHER SPEED, VIBRATION RETURNED DESCENDING FL 320-2 70 WITH SPEED INCREASING TO 300. LEFT TURN SLOWING TO 210 NOTICABLE VIBRATION. VIBRATION DIMINISHED AT FLAP 5.SDR TRAX200800908Structure · corrodedCORROSION FOUND AT FS 559 RBL 44. REMOVED CORROSION AT FS 559 RBL 44 IAW SRM 51-21-06. MATERIAL LOSS .002 FOUND TO BE WITHIN LIMITS IAW CRJ 200 SRM 51-21-06. RESTORED FINISH IAW SRM 51-25-00. (S)SDR DXTA200803104Bushing · wornCLIMBING THROUGH 5000 FT/250KTS/SMOOTH AIR VIBRATION FELT THROUGH OUT FLIGHT DECK. VIBRATION NOTICED DURING DESCENT AS WELL. REMOVED AND REPLACED UPPER AND LOWER RUDDER TRIM TAB BUSHINGS 2 WITH NEW BUSHINGS. FOR WORK ACCOMPLISHED REF MM 27-20-00SDR CA080528004Fitting · cracked(CAN) CRACK DETECTED ON FITTING DURING ROUTINE INSPECTION.SDR HALA0800563Skin · corrodedLEVEL 2 CORROSION ON THE CENTER HORIZONTAL STAB UPPER SURFACE SKIN AT LBL 35 STR 10, AROUND 2 FASTENERS. REMOVED CORROSION IAW SRM 55-10-01, FIG 101 REV 76. REWORK APPROVED BY TI FILE NR 588030.SDR 2008UALA01783Unknown · vibrationAFTER TAKEOFF, THE FLIGHT EXPERIENCED AIRFRAME VIBRATIONS UPON FLAP RETRACTION. STOPPED AFTER LEVEL OFF AND CONTINUED TO DESTINATION. PERFORMED SEVERAL FLAP TESTS, ACCOMPLISHED EFCS1 & EFCS2 ELEVATOR DAMPING AND AILERON DAMPING TEST -NO FAULTS NOTED OPERATIOSDR TRAX200800175Bulkhead · crackedFWD PRESSURE BULKHEAD CRACKED WHERE PARKING BRAKE CABLE PASSES THROUGH. COMPLIED WITH REO 601R-53-11-563 AND EO 600-53-217 C/W TO REPAIR THE FWD PRESSURE BULKHEAD.SDR HALA0800116Seat Track · corrodedLEVEL 1 CORROSION SECTION 45 SEAT TRACK AT LBL 11, HAS DAMAGE TO SEAT TRACK CROWN AT STA 1065. CORROSION REMOVED, CONFIRMED BY 10X MAGNIFICATION, IAW SRM 51-10-02, REV 76. BLENDED WITHIN LIMITS, IAW SRM 53-00-52/101, REV 75.SDR ABXA080049Stringer · crackedSTRINGER 36 RIGHT CRACKED BELOW SPLICE REPAIR, BETWEEN FS 566 AND 588. REPAIRED LONGERON 36 RIGHT IAW B767 SRM 53-00-03, FIGURE 201 AND SRM 51-40-1.SDR TSAA0753064Skin · crackedWHILE PERFORMING INSPECTIONS TO COMPLY WITH AD 03-14-06 A CRACK APPROXIMATELY 1.5 LONG WAS DISCOVERED 1 BELOW STR 21L AT BS 967+6.SDR TRAX200701796Unknown · corrodedRT FR 37 CORRODED AT FLOOR LEVEL. RT FR 37 AT FLOOR LEVEL CORROSION REMOVED AS PER SRM 51-21-42 FABRICATION OF FR 37 REPAIERD PARTS COVER ON W/C 2000-245 FR 37 REPAIRED IAW SRM 53-67-70 FIG 402 MATERIAL THICKNESS: 0.080 MATERIAL REMOVED: 0.030 OUT OF LISDR 07FDEA04860Fitting · crackedDURING MODIFICATION MD10 TO ACF (ADVANCED COMMON FLIGHT DECK), VANE AIR CONDITION LT SIDE BAY JAMB STRUCTURE FRAME TO STA 528 DEFORMED CORROSION AND CRACK LONG 2" ON SUPPORT FITTING. REPLACED FRAME ACA3347-3 AND FITTING ACA3799-501 FOR SRM 51-35-01 VOL II.SDR 07FDEA04789Lock Fastener · crackedEMPENNAGE AFT FUSELAGE COMPARTMENT UPPER DOG HOUSE AT STA 2102 FRAME CLIP AROUND 1 LOCK FASTENER FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR DJFA2007128Unknown · vibrationAIR TURN BACK TO DEPARTURE DUE TO A LOUD VIBRATION FELT ON CLIMB OUT. THE AIRCRAFT LANDED OVERWEIGHT. ALTHOUGH NO EMERGENCY WAS DECLARED THE AIRCRAFT WAS MET BY AIRPORT EMERGENCY CREW. MAINTENANCE COULD NOT IDENTIFY THE SOURCE OF THE VIBRATION BUT ADJUSTED SDR 2007UALA04328Crease Beam · corrodedFWD CABIN CREASE BEAM AT DOOR 1L CORRODED, BS 310-350. REPLACED FORWARD ENTRY DOOR WAY CABIN FLOOR CREASE BEAM.
SDR HALA0700394Seat Track · corrodedLEVEL 1 CORROSION SECTION 45 SEAT TRACK RBL 54-75. CORROSION AT STATION 927,939, AND 1053. AREAS REWORKED AND FOUND WITHIN LIMITS PER SRM 53-00-52. REWORKED AREAS ALODINED AND PAINTED.SDR 09152007TBNone · noneTHE EMS FLIGHT WAS ENROUTE WITH PATIENT ON BOARD, CREW HEARD LOUD BAND SOUND OUTSIDE OF AIRCRAFT, NO INSTRUMENTATION WARNINGS, PILOT ELECTED PRECAUTIONARY LANDING A CLOSEST AIRPORT. EMS FLIGHT CONTINUED WITH ANOTHER AIRCRAFT, BASE MECHANIC RESPONDED, FOUND EVISDR DLM88071127Angle · crackedCRACKED FITTING BETWEEN FRAME AND INTERCOSTAL AT STA 787 BETWEEN LONGERON 27 LH AND 28LH. REPLACED FITTING PER DRWG 5956034 ON N/R T0065338 IN HMV AT GDL.SDR 2007UALA03063Control Box · looseRTFL DUE TO ENGINE VIBRATION SHORTLY AFTER TAKEOFF. 09-07-07 RESECURED LOB. VIBE SURVEY FLIGHT (TEST FLIGHT) PERFORMED, NO VIBES NOTED.SDR USA2007F00011Structure · corrodedCORRODED RIVET TAILS WERE FOUND IN FUSELAGE CARGO COMPARTMENT BETWEEN FRAME 26 TO 35.8 STRINGER 38R TO 38L. APPROX 1500 RIVETS WERE REPLACED. A RESIDUE OF SODIUM CHLORIDE ATTACKED THE RIVETS. NUMEROUS OTHER RIVETS HAD THE PAINT FLAKING OFF THE RIVET TAILS TSDR QXEA200701118Unknown · corrodedC3 OKC - FS 280 AT RBL 9 AFT SIDE HAS CORROSION. REPAIRED IAW SRM 51-42-06, 51-42-21.SDR 2007UALA02010Structure · damagedRAMP REPORTED A GOUGE 1FT AFT OF AFT CARGO DOOR. [07-10-07] MAJOR REPAIR ACCOMPLISHED: REPAIRED CRACK PER EVA-70345.SDR 2007UALA02009Structure · damagedLEFT EXTERNAL FUSELAGE AT STA 204, STR 24L IS DAMAGED. *S/D* MAJOR REPAIR ACCOMPLISHED: INSTALLED DOUBLER REPAIR.SDR 07FDEA02118Skin · unknownEXISTING SKIN REPAIR EXT FUSELAGE FWD JAMB AFT CARGO DOOR APPLIED SEALANT IAW SRM 51-41-01 VOL 2 AND APPLIED PRIMER IAW SRM 51-21-01 VOL 2.SDR 07FDEA02117Frame · noneEXISTING FRAME REPAIR MAIN CABIN PERFORMED INSPECTION OF REPAIR AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.SDR 07FDEA02116Frame · noneEXISTING FRAME REPAIR INTERNAL FUSELAGE CAC PERFORMED INSPECTION OF REPAIR AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.SDR 07FDEA02115Longeron · noneEXISTING 3 EA LONG SPLICE REPAIR AFT CARGO COMPT PERFORMED INSPECTION OF REPAIR AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P.2.SDR 07FDEA02114Longeron · noneEXISTING LONGERON SPLICE REPAIR FWD CARGO COMPT PERFORMED INSPECTION OF REPAIR AND FOUND IN COMPLIANCE WITH CRITERIA REQUESTED BY EO 8-5100-7-5001 P2.SDR 07FDEA02112Skin · unknownEXISTING REPAIR EXT FUSELAGE REPLACED REPAIR PER SRM 53-20-00 FIG 6 VOL 1.SDR 07FDEA02111Skin · noneEXISTING REPAIR EXTERNAL FUSELAGE. PERFORMED INSPECTION OF REPAIR AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P1.SDR 2007FA0000576Structure · misinstalledTHE AIRCRAFT ARRIVED NEW FROM THE FACTORY FOR AVIONICS MODIFICATIONS AND DURING OUR INCOMING INSPECTION A TECH NOTED MISSING RIVETS IN (2) STRINGER CLIPS. THE CLIPS ARE LOCATED AT FS 386 ON THE RT NR3 AND RT NR 5 STRINGERS AS NOTED USING THE UPPER CENTERLINE SDR DLM88070689Structure · corrodedCORROSION AT STA Y=275 BETWEEN LONGERONS 3 RT AND 6 LT. REPAIRED IAW SRM 51-30-5 NR T0056455.SDR A6WA200740303Unknown · crackedFOUND FS 280 CLIPS INBOARD AND OUTBOARD AT LBL 9 ARE CRACKED. (M) [07-31-07] MAINTENANCE REMOVED AND REPLACED CLIPS AT FS 280, LBL 9 WITH NEW CLIPS PN 601R3111357. (K)SDR 07FDEA01950Membrane · corrodedCOCKPIT CORROSION CON EXFOLIATION ON MEMBRANE, AND 1 CRACK.SDR KNNA200700029Skin · damagedLOWER LOBE/FUSELAGE SKIN, SHOWS SIGNS OF HAVING LOOSE ATTACH RIVETS FROM BS 807 TO BS 827 AT BBL-0. FOUND CORROSION AT THE TIME FASTENER REMOVAL. ACO NR 075369 PROVIDE REPAIRS INSTRUCTIONS ON SKIN REPAIR AT BS 807-827 BBL 0, SRM 53-10-4 FIGURE 6.SDR N865F1134011Unknown · corrodedFOUND COCKPIT SUBFLOOR WITH CORROSION AT STA.-67.00 L21L CPCP455L 0552.SDR TRAX200700388Intercostal · crackedSTA 484 RBL 36 INTERCOSTAL REPAIR ANGLE CRACKED IN RADIUS.SDR 07FDEA00884Unknown · corrodedFOUND CORROSION EXIST AT AVIONICS COMPARTMENT STA 1315/ FR 17 STGR 45 LT 2' BY 2' INCHES BELOW ACCESS PNL 121 PF ZONE 120 COMPLIED WITH EA 6-5330-107691.SDR 2007UALA00750Unknown · damagedUPPER FUSELAGE FROM APPROX STA 875 TO STA 887 LBL 4 TO LBL 5 AND RBL 3 TO RBL 4 2EA LONG GOUGES-WEAR. MAJOR REPAIR ACCOMPLISHED: INCORPORATED INTO SAME REPAIR AS PTT 0922100 - (INSTALLED EXTERNAL FUSE SKIN DOUBLER-TRIPLER, INTERNAL TEAR STRAP DOUBLERS & WEAR SDR 2007UALA00748Structure · damagedSTA 12267, STR 42 RIVET HAS LIGHTNING DAMAGE. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED AREA & INSTALLED DOUBLER REPAIR.SDR COEA0704908Frame · crackedCRACK FOUND ON FUSELAGE FRAME 5 LOWER FLANGE CLOSE TO LT NLG WHEEL WELL. CRACK REMOVED AND REINFORCING ANGLE INSTALLED PER ATR REPAIR INSTRUCTIONS DO/TS-3825/06-7654. REF SRAS DO/TS-3825/06...3816. (M)SDR 07FDEA00675Latch · corrodedFOUND CORROSION ON Y-Z LATCH SUPPORT AT C25A RT. REPAIR WAS PERFORMED IAW SRM 53-13-13, FIG 204, SHEET 1, 2.SDR 07FDEA00614Unknown · crackedCAC 2 EA CRACKS 1.5" LONG AND 3" LONG ON STRIP AT STA 1156 Z= -74 X= -6 AND X= 6. STRIPPED PAINT FROM DAMAGED AREA IAW SRM 51-21-01 PAR C PAG 26 VOL 2. PERFORM NDI CONTROL AND CONFIRMED LENGTH AND END OF CRACK. PERFORMED REPAIR IAW SRM 53-40-00 FIG 17. FABSDR DU4R2007061Skin · corrodedFOUND PREV REPAIRED AREA AT FS 332 TO FS 355 BETWEEN L-23L AND L-26L. REPAIRED BY REMOVING SECTION OF SKIN AND 2 EXISTING REPAIRS IAW DC-9/MD-80 SRM 53-04 FIG 12C. FABRICATED AND INSTALLED SKIN REPAIR 31.75 BY 25.5 FROM 2024-T3 .050, 3 SKIN REPAIRS 17.75 BY SDR SWIA200717997Unknown · crackedAFT EQUIP BAY AT FS 654.50 STR12R CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CLIP AT FS 654.50 STR 12 IAW CRJ200 SRM 51-42-20 PG 23.SDR 07FDEA00394Unknown · misrepairedPREVIOUS REPAIR FOUND LOCATED RT, FS 1446-1461, FR 20-20A AND STR 38-41. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR SDR TRAX200700141Seat Track · corrodedCORROSION AND CHAFING ON LEFT AND RIGHT SIDE SEAT RAILS AS MARKED FROM FS 379.00 TO FS 977.00.SDR 07FDEA00154Sill · maint errorMAIN CARGO DOOR CUTOUT AT BS 620 AND UPPER SILL HAS DOUBLE DRILLED HOLES AND DRILL STARTS ON LOWER SURFACES. REF DRAWING 53FX1286 FABRICATED 2EA. TENSION CLIPS ON WO 11701/2000/0013 AND INSTALLED REF. SRM 51-30-02 ALSO WORK ACCOMPLISHED ON WO 35039/N01449
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