JASC 5310
Service difficulty reports · 38,528
Reports filed under 5310 · Fuselage Main, Structure, 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 = '5310' 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 = '5310' 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 CALA2022011400145Fastener · cracked(REPAIR BEFORE NEXT FLIGHT) ROTO PROBE OF LH FR68 #1 DOOR STOP F ITTING FASTENER HOLES FOUND A CRACK AT #3 HOLE.() REPAIRED LH FR68 #1 DOOR STOP FITTING IAW EC/RA 5341-01294. FORM 44-0008 ATTACHED EMP# V935774 WORK ACCOMPLISHED AT ST ENGINEERI NG AEROSPACE OF SDR CALA2022011400134Intercostal · crackedROTO PROBE OF RH FR20 #7 DOOR STOP FITTING FOUND THAT THE BOTTOM IB HOLE HAS A CRACK INDICATION 001/002. WORK ACCOMPLISHED BY VTMAE EMP V935774 ACCOMPLISH EC/RA 5311-02712 ON OR BEFORE THE AIRCRAFT REACHES 40,251 TOTAL EXCEED 15,500 FLIGHT CYCLES THEREAFTER. ISDR CALA2022011400136Frame · crackedLH FR16 #1 DOOR STOP FITTING ROTO PROBE FOUND THAT THE BOTTOM IB HOLE HAS A CRACK INDICATION 001/002. WORK ACCOMPLISHED BY VTMAE EMP V935774 ACCOMPLISH EC/RA 5311-02712 ON OR BEFORE THE AIRCRAFT REACHES 40,251 TOTAL EXCEED 13,700 FLIGHT CYCLES THEREAFTER. INSPSDR CALA2022011400135Frame · crackedLH FR35 ROTO PROBE AT STGR 30 FASTENER HOLES FOUND THE BOTTOM AF T HOLE CRACKED ACCOMPLISHED BY VTMAE EMP V935774 ON OR BEFORE JUNE 20, OF ECRA5310-07963 2022, PERFORM AN INSPECTION PER PART 2 OF THE LATEST REVISION PERFORMED INTERIM REPAIR TO LH FR35 STGR 30 SDR K11A2022021700113Stringer · damagedFRAME DAMAGED AT STA 1070 RBL 21 STR 27SDR IPXA2022020978817Floor Panel · damagedINSPECTION TYPE:A300PNL 242KN BROKENFABBED IAW SREO A300-5320-40552-BSDR WX0A2022020473953Door Frame · crackedNRC 2000-0069: (141-13) L/H FWD PAX DOOR CUTOUT(L1) FR 16, CRACKS FOUND AT STOP FITTING #7 UPPER AND LOWER INBD. HOLES. / L/H FWD PAX DOOR CUTOUT (L1) FR 16, CRACK REPAIRED ON FRAME 16 AT STOP FITTING NO.07 UPPER INBD HOLES AS PER AIRBUS DOSSIER 81014852 AND SDR SWAA2022013161065Web · corrodedCORROSION ON AFT CARGO BAY THRESHOLD SUB WEB AT RBL 26 BS 787+13; BS 787+16; BS 787+19; BS 807+2; BS 827+1; BS 827+3; BS 827+6; BS 827+7. REMOVED CORROSION ON SUBTHRESHOLD WEB. FOUND OUT OF LIMITS IAW SRM 53-60-15-1A-1; PARAG. 4.G.(2) DETAIL G. COMPLETED SDR IPXA2022012678310Floor Panel · damagedINSPECTION TYPE:A300PNL 231NG DAMAGEDFABBED IAW SREO A300-5320-40552-BSDR IPXA2022012678308Floor Panel · damagedINSPECTION TYPE:A300PNL 242DN BROKENFABBED IAW SREO A300-5320-40552-BSDR FDEA202201120052Stringer · crackedLOWER BULK CARGO COMPARTMENT STATION 1979 RIGHT BUTT LINE 49.5 STRINGER FOUND WITH CRACK AS MARKED. LOWER BULK CARGO COMPARTMENT STATION 1979 RIGHT BUTT LINE 49.5 CRACK STRINGER REPAIRED AS PER B777 SRM 53-70-53-2R FIGURE 202 REPAIR 2 FROM STATION 1946 TO SDR FDEA202201120051Stringer · crackedLOWER BULK CARGO COMPARTMENT STATION 1937, RIGHT BUTT LINE 41.5 STRINGER FOUND WITH CRACK AS MARK. LOWER BULK CARGO COMPARTMENT STATION 1937 RIGHT BUTT LINE 41.5 CRACK STRINGER REPAIRED AS PER B777 SRM 53-70-53-2R FIGURE 202 REPAIR 2 FROM STATION 1924 TO SDR CALA2022011300123Frame · crackedTWO ADDTIONAL FASTENER HOLES WERE FOUND CRACKED AT FR36 PRESSURE PANEL O/B OF ALLOWABLE CUT-OUT AREA REPAIRED ADDITIONAL FASTENER HOLES FOUND CRACK AT FR36 PRESSURE PANEL IAW EC/RA 5330-01903. EMP: V935774 WC: 0018304 STA: ST ENG BFM SFR# 1027449SDR CALA2022011300122Intercostal · crackedRH FR16 #1 DOOR STOP FITTING ROTO PROBE FOUND THAT THE BOTTOM IB HOLE HAS A CRACK INDICATION REPAIRED RH FR16 #1 DOOR STOP FITTING AREA IAW EC/RA 5311-02712. EMP: V935774 WC: 0017897 STA: ST ENG BFM SFR# 0017897SDR CALA2022011300121Frame · crackedRH FR16 #7 DOOR STOP ROTO PROBE FOUND THAT THE TOP IB AND BOTTOM IB HOLES HAVE CRACK INDICATIONS REPAIRED RH FR16 #7 DOOR STOP FITTING AREA IAW EC/RA 5311-02712. EMP: V935774 WC: 0017896 STA: ST ENG BFM SFR# 1027447SDR CALA2022011200120Fastener · cracked(REPAIR BEFORE NEXT FLIGHT) ROTO PROBE OF RH FR68 #1 DOOR STOP F ITTING FASTENER HOLES FOUND A CRACK AT #3 HOLE.() REPAIRED RH FR68 #1 DOOR STOP FITTING IAW EC/RA 5341-01294. EMP# V934774 WORK ACCOMPLISHED AT ST ENGINEERING AREOSPACE OF MOBILE AT BFM ON NR# 00SDR CALA2022011200119Fastener · out of round(REPAIR BEFORE NEXT FLIGHT) VISUAL AND ROTO PROBE INSPECTION OF LH FR68 #7 DOOR STOP FITTING FASTENER HOLES FOUND #2 AND #4 HOLE S OUT OF ROUND.() REPAIRED LH FR68 #7 DOOR STOP IAW EC/RA 5341-01294 FORM 44-0008 ATTACHED. EMP# V935774 WORK ACCOMPLISHED AT ST ENSDR SWAA2022021460701Web · corrodedCORROSION FLOOR STRUCTURE WEB LOCATED BTW BS 767 TO BS 787 AT LEVEL STR 27R AND WL 149.50 AT AFT CARGO COMPARTMENT ; 2022-11378 / [01] TOOL USED: TEMPERATURE CHART: P/N: KT8P2; S/N: 19021963; DUE DATE: 14-MAY-22.; [02] REPLACED WEB AND FASTENERS LOCATED BTW BSSDR FDEA202201110212Splice · crackedMAIN DECK CARGO COMPARTMENT FLOOR BEAM - UPPER CAP AFT FLANGE CRACKED, AT STA580, LBL45.5 COMPLIED WITH FEDEX EA: F-5310-T0366559 PT1, EA TITLE: FUSELAGE - MAINFRAME - STA 580 FLOOR BEAM SPLICE SEGMENT UPPER AFT FLANGE CRACK REPAIR- REPAIR DOCUMENTATION SDR IPXA2022020478634None · crackedINSPECTION TYPE:3CL-3 DOOR JAMB INNER SKIN REPAIR DOUBLER IS CRACKED BETWEEN STA. 1250.75 & 1256.75.REPAIRED CRACKED L-3 DOOR JAMB INNER SKIN BETWEEN STA. 1250.75 & 1256.75 IAW VT-SAA EA 011-5310-01-A9471 REV. I/R AND UPS EO MD11-5310-82750-A. (MAJOR) REF. FAASDR ASAA2022011137312Floorbeam · corrodedAFT WET AREA FLOOR BEAM AT STA 947 CORRODED AT LBL 50. GROUNDED - YES. REMOVED CORRODED SECTION OF T-CAP AND REPLACED FROM LBL 8 TO LBL 50 IAW B737-800 SRM 53-70-51-2R-5W=2 O=.180 R=.090 L=1 D=.090. INFO CHANGE 2-1-22SDR ASAA2022011137274Floorbeam · corrodedAFT WET AREA FLOOR BEAM AT STA 947 CORRODED AT LBL 50. GROUNDED - YES. REMOVED CORRODED SECTION OF T-CAP AND REPLACED FROM LBL 8 TO LBL 50 IAW B737-800 SRM 53-70-51-2R-5W=2 O=.180 R=.090 L=1 D=.090.SDR FDEA202201110039Crossbeam · crackedMAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM CRACKED, AT FR64, BETWEEN -Y953 AND -Y1456 REPAIRED THE MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE CRACKED CROSSBEAM AT FR64 BETWEEN -Y953 AND -Y1456 PER A300-600F SRM53-10-15 FIGURE 211. THIS IS CSDR SWAA2022020359596Web · corrodedSUPPLEMENTAL INFORMATION: AFT CARGO DOOR CUT OUT LOWER WEB HAS NUMEROUS SPOTS OF CORROSION ; AFT CARGO DOOR CT OT LOWER WE HAS NMEROS SPOTS OF CORROSION / [01] LOCATED AND DRILLED NEW PART AT AFT CARGO DOOR CUT OUT LOWER WEB REF B-737-700-SRM 51-40-05-0G-0; [0SDR SWAA2022022159719Web · corrodedCORROSION WEB LOCATED BS1016; LBL 9 AND WL208.1 AT AFT GALLEY AREA 2022-15903 / [01] TOOL USED DIGITAL CALIPER P/N: 500-197-30 S/N: A18135101 DUE DATE: 06-AUG-22;[02] REPLACED WEB AND FASTENERS LOCATED BS1016; ; BL 0 AND BL 37 WL208.1 AT AFT GALLEY AREA IAW B7SDR SWAA2022021560370Web · crackedCRACK WEB LOCATED BTW BS277 TO BS294.5 AND BL 0 AT FWD GALLEY AREA ; 2022-12321 / [01] REPLACED WEB AND FASTENERS LOCATED BTW BS277 TO BS294.5 AND BL 0 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG: 141A5400; REV -. <BR>SEE INDIVIDUAL SIGN OFFS BELOW.; SDR F3LA2022012600093Floorbeam · corrodedDISCREPANCY: REF PEMCO N/R #11918.0285 FWD FUSELAGE UNDERNEATH FLOOR BOARDS, AT FR 16 DUMMY BEAM FWD SECTION ABOUT 6 INCHES AREA CORRODED.
CORRECTIVE ACTION: REMOVED AND REPLACED FWD FUSELAGE UNDRENEATH FLOOR BOARDS AT FR 16 DUMMY BEAM FWD SECTION IAW A320 SRSDR F3LA2022012600090Plate · corrodedDISCREPANCY: REF PEMCO N/R #11918.0293 AFT FUSELAGE R/H SIDE BETWEEN FR 69 AND FR 70 SHEAR PLATE WEB CORRODED AT SEVERAL ATTACHMENT HOLES.
CORRECTIVE ACTION: REMOVED AND REPLACED SHERE WEB PLATE BETWEEN FRO 69 AND FR70 FUSELAGE R/H IAW A320 SRM 51-42-11.SDR F3LA2022012600091Plate · corrodedDISCREPANCY: REFERENCE PEMCO N/R #11918.0288 AFT FUSELAGE L/H SIDE AT FR 70 SHEAR WEB CORRODED AT END NEXT TO RIVET ATTACHMENT.
CORRECTIVE ACTION: CORRODED SHERE WEB REMOVED AND REPLACED AND PAINTED, VOR CABLES DISPLACED AND REINSTALLED, OPS CHECK GOOD IAW A3SDR F3LA2022012600092Floorbeam · corrodedDISCREPANCY: REFERENCE PEMCO N/R# 11918.0289 AFT FUSELAGE L/H SIDE AT FR68, (Y765) FLOOR BEAM CORRODED
CORRECTIVE ACTION: REMOVED AND REPLACED FLOOR BEAM L/H FR68 (Y765) IAW A-320 SRM 51-42-11, SRM 51-74-00, SRM 53-00-14-283-002SDR ASAA2022011037191Frame · gougedFRAME STA. 227R-10 INCHES O/B FROM CL 0 -.375" LX.375'W IMPACT DAMAGE ON AFT FACE JUST ABOVE LOWER RADIUS OF FRAME. DOT. GROUNDED - YES. ACCOMPLISHED DOUBLER REPAIR OF FRAME IAW ALASKA EA# 900ER-53EA-24129 DATED 01-19-2022.REPAIR COMPLETED PER BOEING SR 3-524SDR ASAA2022011037185Intercostal · crackedFWD WET AREA, INTERCOSTAL AT RBL 36 STA. 312-328 CRACKED. GROUNDED - YES. REMOVED AND REPLACED INTERCOSTAL IAW 737-800 SRM 51-40-02-0G-0.SDR ASAA2022011037184Intercostal · crackedFWD WET AREA, INTERCOSTAL AT LBL 44 STA.312-328 CRACKED. GROUNDED - YES. REMOVED AND REPLACED INTERCOSTAL IAW 737-800 SRM 51-40-02-0G-0.SDR ASAA2022011037183Intercostal · crackedFWD WET AREA, INTERCOSTAL AT BL0 STA.278-294 CRACKED. GROUNDED - YES. REMOVED AND REPLACED INTERCOSTAL AT FS278-FS294 AT BL0 IAW B737-800 SRM 51-40-02-0G-0.SDR SWAA2022011860605Drain · crackedCUSTOMER REQUEST: BS 1016 CENTER FUSELAGE DRAIN CRACKED ; / [01] REMOVED DAMAGE DRAIN AT STA 1016 ( CENTER DRAIN ) PER B737 SRM 51-40-02-0G-0; [02] LOCATED AND DRILLED NEW DRAIN PER B737 SRM 51-40-05-0G-0; [03] VERIFIED STEPS 1 AND 2; [04] OK TO INSTALL DRAIN;SDR MASA20220110029None · none"MAINTENANCE DISCOVERED CORROSION ON THE AFT EQUIPMENT BAY SUPPORT PLATE. PERFORM PERMANENT REPAIR IAW CRJ7/9 STRUCTURAL REPAIR MANUAL (SRM)
5-62-55-001-001-A01, ITEM 100D 8CRJ700/900 (REV. 38 DATED JUL 9TH 2021.))"SDR CALA2022011200111None · crackedROTO PROBE OF LH FR68 #1 DOOR STOP FITTING FASTENER HOLES FOUND A CRACK AT #3 HOLE SEE LP#7790391 FOR SCEPTER SIGNOFF. ACCOMPLISHED BY EMP#V935774 AT BFM ST AEROSPACE MOBILE. NR#0018923SDR SWAA2022022159692Frame · crackedCRACK ON FRAME LOCATED ON BS312 AND BTW STR5L TO STR6L AT FWD GALLEY AREA 2022-15867 / [01] TOOL USED DIGITAL CALIPER P/N: 500-172-30 S/N: 15237811 DUE DATE: 11-MAY-22;[02] TOOL USED CALIPER PN:500-197-30; SN:A21146280; DUE DATE: 17-OCT-22;[03] RADIUS GAUGE P/SDR SWAA2022021559555Web · crackedCRACK WEB LOCATED BETWEEN BS 294.5 TO BS 303.9 AND STR 16L AT PASSENGER CABIN ; 2022-12255 / [01] TOOL USED P/N:NORTEC 600D S/N:2000053402 CAL DUE DATE:23-APR.-22; [02] TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 500D; S/N: N500X12101V022236 ; DUE DATE: 02-JUSDR SWAA2022021459617Web · corrodedCORROSION FLOOR STRUCTURE WEB BTW BS 344 TO BS 360 LBL 62 WL 208.1 AT PASSENGER CABIN ; 2022-11290 / [01] TOOL USED P/N:45MG S/N:130064101 CAL DUE DATE: 11-MAY-22; [02] REPAIRED WEB (CLIP) FLOOR STRUCTURE BTW BS 344 TO BS 360 LBL 62 WL 208.1 AT PASSENGER CABINSDR SWAA2022021459631Web · corrodedCORROSION FLOOR STRUCTURE WEB LOCATED STA 1016 BETWEEN BL 0 AND LBL 20 AT AFT GALLEY AREA ; 2022-11322 / [01] TOOL USED: TEMPERATURE CONTROLLER: P/N: 38615K71; S/N: AE-40585; DUE DATE: 07-JUL22.; [02] STEP 1 IN ERROR; CORRECTED STEP IS: TOOL USED: TEMPERATURE SDR REXA2022021000232Frame · crackedLH FRAME AT FS 235 CRACKED BETWEEN STGR 11L AND STGR 13L.
"REPAIRED LH F.S. 235 FRAME IAW MHIRJ REO 690-53-11-1391
REV+- DATED 2022-01-05.SDR HALA2022011000015Vent · corrodedSHIP 373 AREA AROUND AFT LAV VENT CORRODED. CORRECTIVE ACTION: BLENDED AND CHECKED LIMITS, LEVEL 1 CORROSION REMOVED AND WITHIN LIMITS, FINAL SKIN THICKNESS OF .076". APPLIED PRIMER AND PAINT REF. HAL A-330 SRM 53-41-11 FIG. 101. (2080133)SDR DALA2022011000199Profile · crackedSHIP 3267 CRACK EMERGENCY EXIT DOOR 843 LH LOAD TRANSMITTING PROFILE IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED PROFILE FITTING PER A320 SRM 51-72-11. (2080407)SDR CALA2022011000096None · crackedROTO PROBE OF RH FR68 #1 DOOR STOP FITTING FASTENER HOLES FOUND A CRACK AT #3 HOLESDR CALA2022011000087None · out of roundVISUAL AND ROTO PROBE INSPECTIN OF LH FR68 #7 DOOR STOP FITTING FASTENER HOLES FOUND #2 AND #4 HOLES OUT OF ROUNDSDR HNAA2022020700065Not Reported · not reportedE894714 - RH WING RIB 21 UPPER FLANGE CRACKED .... PERFORMED REPAIR TO RH WING RIB 21 IAW EO1-57-22-0005.SDR HNAA2022020700064Not Reported · not reportedE894713 - LH WING RIB 21 UPPER FLANGE CRACKED .... PERFORMED REPAIR TO LH WING RIB 21 IAW EO1-57-21-0376SDR FDEA202201080200Support · corrodedCTR CARGO COMPT: STA 1841 - AFT LOWER BULKHEAD FROM LONGERONS 49R-42R, UNDERSIDE OF SEVERAL NUTPLATES ON SUPPORT HAVE EXFOLIATION CORROSION.(ALL NUTPLATES MARKED) 0000662326 : SUN, KEVIN - 03-FEB-2022 00:07 REMOVED AND REPLACED SUPPORT P/N AGA 7170-19 ASDR FDEA202201080024Crossbeam · crackedMAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM CRACKED, AT FR64, BETWEEN -Y1456 AND -Y1959 REPAIRED THE MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE CRACKED CROSSBEAM AT FR64 BETWEEN -Y1456 AND -Y1959 PER A300-600F SRM53-10-15 FIGURE 211. THIS IS
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