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 CALA2022033100845Frame · noneDURING ROTO INSP OF "LH" FR35 STGR30 A CRACK INDICATION WAS NOTED ON HOLE #2LHS FR35 STGR30 "AFT SKIN". DIP CREATED PER STEP 41 OF ECRA 5321-02067 REACHES 44091TFC / 98342TFH WHICHEVER OCCURS FIRST PER PART 2.4 IN INTERVALS OF 8800FC / 17200FH WHICHEVER OCCURSSDR CALA2022033100843None · missingPDA 2 LAV SERVICE DOOR MISSING DOOR DID NOT DEPART AIRCRAFT, ALL HARDWARE REINSTALLED, REFERENCE LOG PAGE 8266793 FOR CORRECTIVE ACTION.SDR CALA2022033100833None · none(SUPPORT TASK) MAIN CABIN AFT DECK PRESSURE PLATE GOUGED BETWEEN STA 1681-1700 LBL24, TRANSCRIBED FROM HAECO GSO NRC 9283144SDR HNAA2022041300157None · noneE907791 - SSI 53-20-13 SERVICE DOOR CENTER SILL CORRODED AROUND NUT PLATES HOLES .... RAR SERVICE DOOR CENTER SILL IAW EMB 145 SRM 51-40-02.SDR 7C7A2022040100013None · noneSEVERAL CORROSION SPOTS ON SKIN BTW STA X 487-510 BTW STR 31S-31P (INTERNAL).SDR DALA2022033002116Structure · corrodedSHIP 3223 CORROSION FLOOR STRUCTURE Y1162.5 LOC BTW FR68 TO FR70 LH SIDE IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED FLOOR STRUCTURE PER A320 SRM 51-72-11 AND 51-42-11. (2175590)SDR CALA2022033100814Bracket · corrodedDURING INSPECTION OF THE BULK CARGO COMPARTMENT FOUND CORROSION IN FRAME 64 TO FRAME 65 STR 33 TO 25 REQ. EVALUATION AS NOTED ON LTPR NR# 5001118110-0020. INSPECTION PERFORMED ON AFT CRG COMPARTMENT, FOUND CORROSION ON CONSIDERED MAJOR AND PERMANENT CATEGORY ASDR 2022FA0000175None · chippedSLICK MAGNETO LOCKED UP AND CLIPPED A GEAR TOOTH AND METAL SHAVING. THIS WAS DURING A TRAINING FLIGHT AND OCCURRED JUST AS STUDENT WAS LANDING AS HE HEARD A LOUD NOISE EMITTING FROM THE ENGINE COMPARTMENT. ON TEAR DOWN. FOUND THAT THE MAGNETO WAS LOCKED, ANDSDR FDEA202203280719None · noneFLOOR PANEL REQ REWORK IAW FEDEX EA F-5310-T0367574 REWORKED FLOOR PANEL IAW FEDWX EA F-5310-T0367574 FUSELAGE - MAIN FRAME- DECK PLATE, STA 1708, BL 0, CORROSIONSDR VNAA202203269928Skin · gougedFUSELAGE EXTERNAL SKIN IS GOUGED UNDER TCAS DIRECTIONAL ANTENNA.SDR VNAA202203089928Skin · gougedFUSELAGE EXTERNAL SKIN IS GOUGED UNDER TCAS DIRECTIONAL ANTENNA.SDR DALA2022032802049None · noneSHIP 3269 FAA - AAI FINDING - DURING INSPECTION OF REPAIR PER ER/A 546005- 14AD FOUND THAT FASTENER SPACING / FASTENER COUNT DOES NOT MATCH THE FIGURE AND INSTRUCTIONS PER ER/A IN CENTER FUEL TANK. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTION ON TOP SKIN PASDR JJBA20220327047Floor Support · corrodedMIDDLE LATERAL FLOOR SUPPORT BETWEEN FRAMES 16-18 IN FWD WET AREA HAS SIGNS OF CORROSION. REMOVED AND REPLACED MIDDLE LATERAL FLOOR SUPPORT BETWEEN FRAMES 16-18 FWD WET AREA.SDR SWIA202265720None · corrodedTCAS DOUBLER CORRODED BETWEEN FS295.00 AND FS310.00. (C CHECK RO 5/23/22) EVALUATED DAMAGE OF TCAS DOUBLER AND FOUND IT TO BE OUT OF LIMITS REF. CRJ-900 SRM, 53-21-01-101-002-A02. REMOVED AND REPLACED TCAS DOUBLER BETWEEN FS295.00 TO FS310.00 REF. CRJ-90SDR R61A2022040700243None · corrodedCORRODED SHEAR CLIP FOUND AT FR 82 STRG 27R-28R. REMOVED AND REPLACED SHEAR CLIP AT FR 82 BETWEEN STGR 27R-28R. REF EMB SRM 51-40-08.SDR R61A2022040700242None · noneCORRODED SHEAR CLIP FOUND AT FR 76 STRG 27R-28R. REMOVED AND REPLACED SHEAR CLIP AT FR 76 STGR 27R-28R. REF EMB SRM 51-40-08.SDR IPXA2022032880593Insulation · contaminatedINSPECTION TYPE:N/ATHERE IS A EXTREMELY STOUT FUEL SMELL IN AIRCRAFTCONFIRMED SMELL WAS COMING FROM RESIDUAL FUEL SPILLED DURING INTIAL REPAIR. R/R INSULATION BLANKETS IAW AMM 25-00-00, IPC 25-55-03-01DSDR GTIA2022032836348Door Sill · corroded"FOUND COROSION @FR68, STR23RH
RAF01 2733457-2 OPENED
TC 534195-01-2-ACCOMPLISHED ON LOG PAGE 2766458-2."SDR GTIA2022032836346Not Reported · dented"FOUND DENT @ FR14+8' DOOR STOP 2-3LH
RAF01 2766457-1 OPENED
NR-00004 / LP 2855779-1-ACCOMPLISHED ON LOG PAGE 2766459-1."SDR DALA2022032802045None · corrodedSHIP 3269 CORROSION INTERNAL STRUCTURE WEB LOCATED BTW FR33 TO FR34 AT LEVEL STR 38R IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED INTERNAL WEB PER A320 SRM 51-72-11. (2171959)SDR FDEA202203260696Skin · corrodedWHILE REMOVING APU INLET DUCT TO F.O.M. THE AFT SIDE OF CUT STRAP WAS FOUND EXFOLIATED. ACCOMPLISHED REPAIR IAW SRM 53-80-15-2R DETAIL I SHEET 2 ON AFT CUT OUT OF APU INLET AT STA. 1825 BETWEEN STRINGERS 5 & 6 FOR CORROSION DAMAGE ON STRAP PART # 148N3141-SDR CALA2022032800799Cover · not reported(A3NB-53-4-6134) ADF 1 COVER PLATE HAS 2 EA SCREWS NEED REMOVED (REPAIR AS REQUIRED).SDR VNAA2022032799913Floorbeam · corrodedCORROSION ON FLOORBEAM FS 985.00 TO FS 1098 27LBL AFT BAGGAGE BAY. CORRECTIVE ACTION: SDR VNAA2022032799911Stringer · corrodedCORROSION ON SKIN SPLICE FS STA 281 BETWEEN STRINGERS 24L TO 24R AT MAIN AVIONICS COMPARTMENT. (E/E). CORRECTIVE ACTION: SDR VNAA202203269912Skin Panel · corrodedFUSELAGE EXTERNAL SKIN UNDER ANTENNA FOOT PRINT BETWEEN FS501 AND FS517 IS CORRODED.SDR VNAA202203269911Skin · corrodedEXTERNAL SKIN WITHIN FOOT PRINT OF ANTENNA AT STGR 27 FROM FS 409.00 TO FS 421.00 HAS CORROSION.SDR VNAA20220326993Bulkhead · crackedF.S. 202.75 BULKHEAD AT LBL 13.77 WEB FOUND AN INDICATION BETWEEN 3RD AND 6TH AND 6TH FASTNER FROM THE BOTTOM APPROX 1.75" LONG OVER 100% FSH FAILED NDT.SDR VNAA20220326992Bulkhead · crackedF.S. 202.75 BULKHEAD AT RBL 13.77 WEB FOUND AN INDICATION BETWEEN 3RD AND 6TH AND 6TH FASTNER FROM THE BOTTOM APPROX 1.75" LONG OVER 100% FSH FAILED NDT.SDR VNAA20220326991Frame · gougedCREW ESCAPE HATCH SURROUND STRUCTURE L/H FRAME IS GOUGEDSDR VNAA202203259993Angle · cracked(N0070) THE L/H DRAG ANGLE WHERE THE VERTICAL STAB, FUSELAGE, AND APU FIREWALL MEET IS CRACKED. ACCOMPLISHED REPAIR OF L/H DRAG ANGLE WHERE THE VERTICAL STAB, FUSELAGE AND APU FIREWALL MEET, BOTH FWD & AFT DRAG ANGLE IAW CRJ700 SRM 55-31-00-201-001-A01. TOP CSDR 2022FA0000170Web · crackedCRACKING IN NOSE WHEEL WELL STRUCTURE COMPONENTS: RH DOUBLER, P/N: 7413133-16, LH DOUBLER, P/N: 7413133-15, TOP WEB, P/N: 7413133-10, AND FRAME, P/N: 7413133-59SDR CALA2022032500790Hinge · cracked(SDR) DURING INSPECTION OF AFT CARGO DOOR HINGE, NDT FOUND DISCR EPANCY IN 3EA HOLES. HOLE WITH DISCREPANCY DRILLED TO OVERSIZE IAW SRM 51-44-11/001 T ABLE 16 FINAL DIAMETER AT HOLE A: 0.213", AND HOLES B&C: 0.197". HFEC C/W - NO CRACKS OR OTHER DAMAGE NOTED. SDR SWIA202265285None · crackedANGLE CRACKED FR.52 L/H AT WHEEL WELL BULKHEAD. (C CHECK RO 04/08/22) REMOVED AND REPLACED CRACKED ANGLE AT FR.52 L/H AT WHEEL WELL BULKHEAD REF SRM 51-40-08, 51-23-06, CPM 51-25-00-910-001-A SEE CONTINUE CARD FOR WORK ACCOMPLISHED.SDR SWIA202265281None · damagedLIGHTNING STRIKE DAMAGE ON FUSELAGE SKIN BETWEEN FR32-33 AND STGR 11R-12R AS MARKED. (C CHECK RO 04/08/22) REPAIRED LIGHTNING STRIKE BY PERFORMING CUTTING OUT DAMAGE AND INSTALLING FILLER AND DOUBLER REF ETD2022-170-011754-B (1).PDFSDR R61A2022040700250Shear Web · corrodedFWD FUSELAGE L/H FLOOR SHEAR WEB CORRODED BTW FR 19 TO FR 19A. R&R IAW EMB 175 SRM 51-41-02.SDR JJBA20220324054None · noneDENT LOCATED ON BAGGAGE DOOR AT 2.25 FROM UPPER EDGE AND 11.5 FROM AFT EDGE. DRESS BACK DENT LOCATED ON BAGGAGE DOOR AT 2.25 FROM UPPER EDGE AND 11.5 FROM AFT EDGE AND PERFORMED NDTSDR CALA2022032500780Floor Support · corrodedREF AMES NR 143879-0100-0067. UPPER CABIN FLOOR BEAM AT PREVIOUS REPAIR STA 365 LBL 6 CORRODED REMOVED AND REPLACED UPPER CABIN FLOOR BEAM @LBL 6 TO RBL 34 PER B757 SRM 53-00-51 REPAIR 1.SDR CALA2022032500779Keelbeam · not reportedWHILE ACCOMPLISHING INSPECTIONS PER FCD 5330-05575D, PRODUCTION REPORTED MULTIPLE DISCREPANT/OVERSIZED HOLES IN THE RH KEEL BEAM MLG ATTACHMENT STRUCTURE. ER ECRA 5330-06914. ACCOMPLISH A PERMANENT REPAIR PER LATEST REVISION OF EC/RA 5330-06914 ON OR BEFORE 24SDR CALA2022032500778Not Reported · not reportedWHILE ACCOMPLISHING INSPECTIONS PER FCD 5330-05575D, PRODUCTION REPORTED MULTIPLE DISCREPANT/OVERSIZED HOLES IN THE LH KEEL BEAM MLG ATTACHMENT STRUCTURE. ECRA 5330-06914. ACCOMPLISH A PERMANENT REPAIR PER LATEST REVISION OF EC/RA 5330-06914 ON OR BEFORE 24-FESDR IXXA2022032403Seat Track · wornFO'S AFT IB SEAT TRACK HOLES ARE WORNSDR IXXA2022032402Seal Depressor · damagedAFT LOWER CORNER SEAL DEPRESSORSDR IXXA2022032401Seal Depressor · damagedFWD LOWER SEAL DEPRESSOR DAMAGEDSDR SWIA202265347None · elongatedL/H AFT WINDSCREEN INBD UPPER MOUNT AT FRAME 84 ELONGATED (C-CHECK RO 4/11/2022) REMOVED AND REPLACED L/H AFT WINDSCREEN INBD UPPER MOUNT AT FRAME 84 REF SRM 51-40-08SDR JJBA20220323052Floor Support · corrodedLAV/CARGO LATERAL FLOOR SUPPORT FR 59-61+4 STR 17L CORROSION. REMOVED AND REPLACED LAV/CARGO LATERAL FLOOR SUPPORT FR 59 - 61+4 STR 17L. NO DEFECTS NOTED AT THIS TIMESDR IXXA2022032301Bracket · crackedP-33 PANEL BRACKET CRACKEDSDR CALA2022032300770Frame · cracked(AD2020-20-05) DURING ROTO INSPECTION OF THE RH FR16 DOUBLE JOGG LE HOLE #19. REJECTABLE DAMAGE INDICATION WAS NOTED DUE TO MECHA NICAL DAMAGE IN THE I/B LAYER (FRAME). REPAIR BEFORE NEXT FLIGHT REF VT MAE NR#0023205, REPAIRD RH FR16 DOUBLE JOGGLE HOLE #19 IAWSDR SWIA202265590None · dentedMULTIPLE DENTS (7) FOUND ON RHS OF FUSELAGE, AT APPROXIMATELY BETWEEN FS589 TO FS574, AFT & I/B OF GROUND AIR DOOR. (MARKED) / PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDARD ACFT PRACTICES. (C-CSDR MASA20220411177Tripler · wornWEAR ON TRIPLER SKIN SKIN (PREVIOUS REPAIR) LOCATED BTW FS969-985 FS969 & SGTR 26L-26R, REAR FUSELAGE (4 LOCATIONS). CORRECTIVE ACTION: TRIPLER SKIN SKIN (PREVIOUS REPAIR) LOCATED BTW FS969-985 FS969 & SGTR 26L-26R, REAR FUSELAGE
WERE REPAIRED PER REO 690-5SDR MASA20220411176None · corrodedPITTING CORROSION ON SLAT TRACKS: 1-1, 1-3, 3-1 AT UPPER SURFACE; SLAT TRACK 1-2 & 2-2 AT LOWER SURFACE; SLAT TRACK 2-1 & 3-2 AT UPPER/LOWER SURFACE FOR RH WING.| CORRECTIVE ACTION: SLAT TRACKS WAS PERFORMED PER EA 81-2022-038 REV IR.EA 81-2022-039 REV IR AND SDR MASA20220411175None · corrodedPITTING CORROSION ON SLAT TRACK: 1-1, 1-2, 1-3 & 2-3 AT UPPER/LOWER SURFACE; SLAT TRACK 2-3, 3-1 & 3-2 AT UPPER SURFACE, FOR LH WING |CORRECTIVE ACTION: SLAT TRACKS WAS PERFORMED PER EA 81-2022-040 REV IR, EA 81-2022-041 REV IR AND EA 81-2022-042 REV IR
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