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 05FDEA04280Repair · unknownLOWER FUSELAGE BELLY SKIN FOUND AN EXTERNAL DOUBLER REPAIR AT STA 1205 LONG 52 DIM 4" BY 4". PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 53-40-00 FIG 20 VOL 1. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO# 8-5100-7-5001 P1.SDR QXEA200600277Unknown · unknownYYC - C3 FUSELAGE INTERIOR RIGHT SIDE FS 597-605 AT STRINGER 12R SEVEN RIVETS DUMPED. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01.SDR VNAA0512006Structure · bird strikeTHE CREW REPORTED A BIRD STRIKE DURING LANDING APPROACH. MAINTENANCE COMPLIED WITH A BIRD STRIKE INSPECTION AND FOUND A DENT ON THE RT FUSELAGE NOSE SECTION BELOW THE ADG DOOR, THE ADG DOOR WAS CRACKED, AND THE LT WING LEADING EDGE PANEL 530BL WAS DENTED. ALSDR VNAA0512003Radome · ground damageWHILE PARKED FOR THE NIGHT THE RADOME WAS STRUCK AND DAMAGED BY A LAV SERVICING TRUCK. AFTER INSPECTING THE AIRCRAFT MAINTENANCE REMOVED AND INSTALLED A SERVICEABLE RADOME. NO OTHER DAMAGE WAS FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE.SDR 2005UALA01315Crease Beam · corrodedFWD GALLEY CREASE BEAM CORRODED FROM STA 294 TO STA 336 AT STR 17, RBL 57 WL 208. REPL'D CREASE BEAM REF SRM51-40-02.SDR ASOA051026Intercostal · crackedDURING A C-CHECK IN TUS, THE FS 484 INTERCOSTAL, AT BL 36, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE FS 484 INTERCOSTAL, AT BL 36, IAW ASA EO 600-53-0098. (M)SDR UPS05845687Unknown · corrodedFOUND CORROSION IN LT W/W. AIRCRAFT BEING FERRIED NR 9157 TO SAA FOR REPAIR. CUT OUT CORROSION FROM EXTERNAL SKIN, AND FAB'D AND INSTALLED REPAIR PARTS FOR SKIN REPAIR. ALL WORK PERFORMED IAW SAA SK 840-727258 & UPS EO DC8-53-20523.SDR IXXA0500208SRepair · temporaryDURING ROUTINE C-CHECK, TO COMPLY WITH DTA REQUIREMENTS, REMOVED EXISTING EXTERNAL FUSELAGE DOUBLER AT STATION 1715 LONGERON 26 RIGHT. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED NEW DOUBLER REPAIR AT STATION 1670 TO 1753, LONGERSDR QXEA200501411Seat Track · corrodedYYC - FUSELAGE INT, LEFT O/B SEAT RAIL AT FS 398 HAS PITTING CORROSION ON I/B FACING SURFACE. MAINTENANCE REPAIRED IAW REO 670-53-00-013 REV A.SDR ASOA05911Retainer · corrodedDURING A C-CHECK IN YUL, THE SEAL RETAINERS, AT FS 45 AND FS 46, WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE SEAL RETAINERS, AT FS 45 AND FS 48, IAW SRM 51-21-42 AND AMM 20-21-12. (M)SDR SIMA200526401Sill · corrodedSAW - DURING CPCP INSPECTION, FOUND SERVICE DOOR SILL IS CORRODED BETWEEN FRAMES 20 AND 22. MAINTENANCE INSTALLED A NEW SERVICE DOOR SILL IAW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR EIA20005156Skin · corrodedBS 2460-2484 STR 23L FUS SKIN EXT SURFACE CORROSION. REPAIR FUSE SKIN BS 2460-2484 PER EA-52-0992.SDR ASOA05620Frame · crackedDURING C-CHECK, THE FUSELAGE FRAME AND DOUBLER AT FS 718, STRINGER 10-12 LT SIDE WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FUSELAGE FRAME AND DOUBLER AT FS 718, STRINGER 10-12 LT SIDE IAW EO. (K)SDR USAA050870Beam · corrodedPIT - FOUND BEAM CORRODED 10 INCHES BY 2 INCHES, BETWEEN FRAME 16 AND 20 Y254. INSTALLED BEAM PER SRM 51-72-11. (M)SDR DU4R05060313Panel · puncturedRT CABIN STA. 655 AND 674 PANEL B8 HAS PUNCTURES.SDR DU4R05060312Panel · puncturedR/H CABIN STA. 335 PANEL B2 IS PUNCTURED.SDR DU4R05060311Panel · puncturedRT CABIN STA 350.5 PANEL D2 IS PUNCTURED.SDR DU4R05060310Panel · puncturedRT CABIN STA 693 PANEL D9 IS PUNCTURED.SDR ASAA0580270Floorboard · damagedOKC - DURING C-CHECK, FOUND CABIN FLOORBOARD STATION 886 TO 946 RBL 22 TO LBL 22 HAS FIBER DAMAGE ON UPPER FACE AD TORN OUT INSERTS. REMOVED AND REPLACED FLOORBOARD. (M)SDR ASAA0590094Structure · damagedPAE - DURING C-CHECK, FOUND DAMAGED FASTENER HOLE AT BS 500J. REPAIRED IAW SRM 51-30-01. (M)SDR ASAA0590093Structure · damagedPAE - DURING C-CHECK, FOUND DAMAGED FASTENER HOLE AT BS 500A. REPAIRED IAW SRM 51-30-01. (M)SDR AMTA200500386Skin · damagedFOUND SKIN SCRATCHED, SCRIBE MARKS, FS 440-660, S4L-S4R. COMPLIED WITH ERA 757-53R-5866. (M)SDR IXXA0500142SFastener · missingDURING A ROUTINE C CHECK INSPECTION, FOUND AFT CENTER SECTION LOWER PLATING DRAIN HOLE REPAIR ONE ROW FASTENERS MISSING STA 1380.000 L-35 RT L-36. MAJOR REPAIR ACCOMPLISHED REMOVAL OF EXISTING REPAIR. REMOVED DAMAGED SECTION AND PERFORMED NDT INSPECTION. FASDR A6WA200540057Angle · crackedFOUND FS 484 LBL 9 ANGLE CRACKED APPROX .40 INCH RADIUS. REPLACED ANGLE IAW BRAS EO 601R-53-5983. (M)SDR 2005F00063Sight Glass · missingFLT - 711 - MIA-MEX - CREW REPORTED UNABLE TO PRESSURIZE IN FLIGHT, DUMPED FUEL AND RETURNED TO MIA. FOUND RIGHT MAIN GEAR DOWNLOCK VIEWING WINDOW MISSING, INSTALLED VIEWING WINDOW (P/N 66-16515-1), REPLACED SEAL (P/N 66-16514-1) AND CLIPS (P/N 66-14269-1) PESDR 2006UALA00125Rivet · crackedCRACKED RIVETS. REPLACED RIVETS REF SRM 51-40-02 & 53-00-01.SDR 2005UALA00062Drain Valve · not closedAT FL250 UNABLE TO HOLD CABIN ALTITUDE. CABIN CLIMBING AT 1000 FPM. DRAIN VALVE IN BOTH THE AFT CARGO PIT AND E/E DOOR NOT CLOSING. LUBED FWD ONE AND CLEANED DEBRIS FROM AFT PIT DOOR VALVE.SDR USAA040081AFlange · crackedFOUND FLANGE CRACKED .5 INCH,PANEL 582-8R OPENING IN RT PYLON. STOP DRILLED THE CRACK, INSTALLED DOUBLER PER TYPICAL REPAIR 54-30-07. (M)SDR LCQ2005031Skin · dentedC-2 DOOR HAS NUMEROUS DENTS, CUSTOMER REQUESTS DOOR TO BE RESKINNED. REF NR 23419 S/O 269001.SDR IXXA0500206SRepair · temporaryDURING ROUTINE C-CHECK, TO COMPLY WITH DTA REQUIREMENTS REMOVE EXISTING FASTENERS AND EXISTING FUSELAGE DOUBLER AT STATION 107 LONGERON 35 RIGHT. INSTALL REPAIR AT FUSELAGE SKIN SECTION FROM STATION 98.5 TO STATION 114.5 BETWEEN LONGERON 34 LEFT TO LONGERON 3SDR WLDA2004104Drain · corrodedDURING C2 CHECK INSPECTION FOUND CORROSION IN WASTE TANK DRAIN PAN AT STA 1970 BETWEEN L50L AND L50R. REMOVED WASTE TANK DRAIN PAN AND INSTALLED NEW PART PER MD11 SRM 51-33-01 VOL II REV 36. APPLIED PROTECTION COATING.SDR ASAA0470028Support Angle · corrodedPAE: DURING C-CHECK FOUND CORROSION FWD CARGO BAY AFT CTR BULKHEAD SUPPORT ANGLE UPPER SIDE AT BS 500 D. REPAIRED IAW SRM.(K)SDR IXXA060047SWeb · crackedDURING ROUTINE C-CHECK FOUND WEB CRACKED ST STATION 30 -X48. REMOVED DAMAGE. FABRICATED REPAIR DOUBLER, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED REPAIR DOUBLER AND FASTENERS AT STATION 30 TO 33.5 AT -X48. IAW SRM 53-2-0, 51-1-4, 51-1-5, AND 51-1-8SDR IXXA0500209SRepair · temporaryDURING ROUTINE C-CHECK TO COMPLY WITH DTA REQUIREMENTS REMOVED EXISTING EXTERNAL DOUBLER AT STATION 1702 LONGERON 26 LEFT. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED NEW REPAIR DOUBLER AT STATION 1690 TO 1713 LONGERON 24 LEFT TOSDR IXXA060003SDoubler · damagedDURING ROUTINE C CHECK REPLACE EXTERNAL FUSELAGE SKIN REPAIR AT STATION 1795 LONGERON 35 LT DUE TO DTA REQUIREMENTS. REMOVED FASTENERS NEEDED TO PERFORM REPAIR, AND EXISTING DOUBLER. FABRICATED REPAIR PARTS, LOCATED, DRILLED TREATED, PRIMED, INSTALLED REPAIR PSDR IXXA060002SDoubler · damagedDURING ROUTINE C-CHECK, REPLACE EXISTING FUSELAGE SKIN REPAIR LOCATED AT STATION 1686 LONGERON 35 RT DUE TO DTA REQUIREMENTS. REMOVED FASTENERS NEEDED TO PERFORM REPAIR. REMOVED EXISTING DOUBLER. REMOVED DAMAGE, FABRICATED REPAIR PARTS, LOCATED, DRILLED, TREATSDR IXXA0500228SRepair · temporaryDURING ROUTINE C-CHECK TO COMPLY WITH DTA REQUIREMENTS REMOVED EXISTING DOUBLER AT STATION 1544 LONGERON 35 RIGHT. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED NEW REPAIR PARTS AND FASTENERS AT STATION 1537 TO STATION 1551 BETWEENSDR IXXA0500207SRepair · temporaryDURING ROUTINE C-CHECK, TO COMPLY WITH DTA REQUIREMENT REMOVED EXISTING DOUBLER AT STATION 74 LONGERON 35 RIGHT. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TREATED, PRIMED, INSTALLED REPAIR PARTS, AND FASTENERS AT STATION 70 TO 78.5, LONGERONS 34 LEFT TO LONGSDR IXXA060101SRib · crackedDURING ROUTINE C-CHECK FOUND FORWARD ENTRY DOOR CUT OUT, AFT RIB CRACKED BETWEEN LONGERON 19 LT AND 20 LT. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED RIB. FABRICATED NEW RIB, LOCATED, DRILLED,TREATED, PRIMED, INSTALLED NEW RIB AND NEW FASTENERS. IAW SRM 53SDR 2004UALA00920Beam · unknownLT AND RT WHEEL WELL CANTED BEAMS. INSTALLED DOUBLER TO MLG CANTED BEAMS.SDR GAIA04150Seat Track · mismanufacturedDURING C-CHECK INSPECTION, FOUND CABIN SEAT TRACK BS 344-480, RBL45.5 NOT IN COMPLIANCE WITH DWG NR 2902. REF FASI NR REMOVED AND REPLACED SEAT TRACK IAW DWG NR 2902.SDR IXXA0500007SSkin · crackedDURING A ROUTINE C-CHECK INSPECTION, EXTERNAL FUSELAGE CRACKED .75 INCH FROM STA 1718.000 TO STA 1719.000. MAINTENANCE PERFORMED MAJOR REPAIR IAW DC8 DRM 53-2-1 FIG 7. REMOVED FASTENERS IAW DC8 SRM 51-1-21 PG 1. REMOVED CRACKED AREA IAW DC8 SRM 51-1-21 PG 1SDR A6WA200440108Skin · damagedFOUND DENT AND CREASE IN FUSELAGE SKIN AT FS 760 BETWEEN STRINGERS 8R AND 9R. REMOVED DAMAGE, FABRICATED EXTERNAL DOUBLER FROM 2024-T3 .050 INCH, AND INSTALLED EXTERNAL DOUBLER IAW BRAS EO 601R-53-5200B. (M)SDR VNAA0408005Structure · vibrationAT 28,000, THE CREW FELT A MODERATE VIBRATION AND SLOWED TO 290 AND THE VIBRATION LESSENED. AFTER SELECTING THE FLAPS TO 20, THE VIBRATION INCREASED THEN LESSENED AGAIN. THE MODERATE VIBRATION CONTINUED UNTIL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT IN ASDR USAA040359Channel · crackedPIT - FOUND CHANNEL CRACKED 2 INCHES AND 1.5 INCHES, BETWEEN BS 727D AND BS 727E. REPLACED PART NR 65-65710-34. (M)SDR ASAA0410355Skin · crackedPAE - FOUND FUSELAGE OUTER SKIN CRACKED. REPAIRED WINDOW POST. INSTALLED DOUBLER AFTER STOP DRILLING. (M)SDR A6WA200440071Floor Support · crackedFLOOR SUPPORT ANGLES CRACKED AT FS 280, WL 73.5 LBL 9 AND RBL 9, BOTH INBOARD ANGLES. REMOVED LEFT ANGLE, P/N 601R31113-57 AND RT ANGLE P/N 601R31113-58 AND INSTALLED NEW SAME P/N ANGLES LEFT AND RT AND TREATED AND PAINTED. ALL WORK PERFORMED IAW SRM 51-23-0SDR ASOA04297Doubler · crackedDURING AN A-CHECK IN BTR, THE LEFT DOUBLER AT FS 640, STRINGER 9 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT DOUBLER AT FS 640, STRINGER 9. (M)SDR ASAA0480331Floor Panel · crackedOKC - FOUND DURING C-CHECK, PASSENGER CABIN FLOOR PANEL HAS DISBONDED AND HAS CRACKED EDGE AT FS 160-180. REPLACED FLOOR PANEL PER SRM 53-05. (M)SDR CA040506007Bushing · failedON INSTALLATION OF THE BUSHING, WHILE IT WAS BEING PRESSED INTO THE LUG OF THE PYLON, THE TOP OF THE BUSHING SHEARED OF THE BODY. MARKS ON THE BUSHING SHOW A TWISTING ACTION AS THE BUSHING WAS BEING INSTALLED. AN INDEPENDENT COMPANY, DID AN INSPECTION (REPOR
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