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 IXXA2022060105Plate · corrodedFLC SILL PLATE CORRODED.SDR IXXA2022060101Seal Depressor · crackedSEAL DEPRESSOR CRACKEDSDR SWIA202266161None · crackedL/H FORWARD FUSELAGE SKIN IS CRACKED AT THE L/H TRU DOOR AFT LATCH CUTOUT IN THE FORWARD LOWER RADIUS OF THE LATCH CUTOUT. (C-CHECK RO 7/26/2022) REMOVED AND REPLACED L/H FWD FUSE SKIN IAW SRM 51-42-13, 51-42-06 AND REO 601R-53-11-3775 REV-- DATED:2022-SDR SWIA202265904None · crackedLH WINDSHIELD POST APPEARS CRACKED RADIATION FORWARD FROM UPPER BARREL NUT HOLE. (C-CHECK RO 6/6/2022) REMOVED L/H WINDSHIELD SIDE POST P/N: 601R33223-1 REF. CRJ-700 SRM 51-42-21-001-001-A01 AND INSTALLED THE NEW LH WINDSHIELD SIDE POST REF CRJ 700 SRM SDR GTIA2022060236460None · noneBOTH PILOTS AND ALL 3 FA'S SMELLED A DIRTY SOCK SMELL TURNING BASE TO FINAL IN FRONT TO BACK OF AIRCRAFT.-PERFORMED TROUBLESHOOTING PROCEDURES IAW TSM 05-50-00-810-831-A. VERIFIED THAT ODER WERENT DETECTED ON EITHER PACK WITH ENGINE AND OR APU BLEED RUNNING. ASDR JJBA20220531060None · noneLH CENTER FUSELAGE I HAS DENT FWD OF FRM 20 BELOW STGR 14. EVALUATED DENT DIM ARE L=1.20 W=.780 D=.030 NF-700 FOUND TO BE OUT OF LIMITS. RECONTOURED DENT LH FUSELAGE FR20 BELOW STR 14. REEVALUATED DENT L=.550 W=.40 D=.015 NF-800 AND DENT HAS SHARP EDGE FOUND TSDR JJBA20220531054None · noneSIGNS OF CORROSION ON FLOOR GUSSET AT FR59 TO FR60 APPROX LBL15. REMOVED AND REPLACED FLOOR GUSSET AT FR59 TO FR60 APPROX LBL 15SDR 2022F00250None · noneAIRCRAFT 9154 N3333U DEPARTED FOR A LOCAL FLIGHT FROM SIGNATURE RAMP / BOMBARDIER HANGAR 2 RAMP AROUND 10.00 AM| LT. AIRCRAFT DID NOT HAVE MEL, FLIGHT LOG THAT HAD OPEN ENTRIES ONBOARD NOR THE LIST CRS. ALSO NOT ONBOARD WAS CERTIFICATES FIELDER FOR INSURANCE, SDR SWIA202265924None · crackedDURING GVI AFTER A HIGH LOAD LANDING EVENT ( AMM 05-51-01) SUBTASK B., FOUND LH OVERWING WING TO FUSELAGE FAIRING PANEL 171CL TO HAVE A CRACK IN THE PANEL RUNNING THROUGH A RIVET HOLE OF THE LOWER AFT STIFFNER. (FILED CLOSED)REMOVED AND REPLACED LH OVERWING SDR GTIA2022060236459None · noneFUME EVENT DES 12,000FT PACK 1 TURNED OFF FUMES DISSIPATED -PERFOMRMED TSM FOR CABIN ODOR/FUMES REF 05-50-00-810-831-A. CREW ISOLATED ODOR TO PACK 1. VERIFIED PACK 2 FREE OF CONTAMINATION SEE NEXT ITEM FOR PACK 1 MEL.SDR GTIA2022053136455None · nonePUNGENS DIRTY SOCK SMELL ON AIRCRAFT SAFETY CONCERN-ACCOMPLISHED TSM 05-50-00-810-836 PERFORMED DECONTAMINATION OF THE ENVIRONMENTAL CONTROL SYST IAW AMM 21-00-00 NO SIGHT OF CONTAMINATION ISOLATED BOTH PACKS ON APU NO SIGNS OF SMELL PERFORMED ENG 1 & 2 RUN IASDR GTIA2022053136454None · noneFAS REPORT SMELLING "DIRTY SOCK" SMELL THROUGHOUT THE CABIN-PERFORMED TROUBLESHOOTING PROCEDURE IAW TSM 05-50-00-810-831-A. VERIFIED WITH AEROTRACER THAT NO ODORS WERE DETECTED ON EITHER PACK WITH ENGINES AND APU BLEED RUNNING. AC OK FOR CONTD SVC.SDR GTIA2022053136452None · noneDIRTY SOCK ODOR IN AFT CABIN-PERFORMED TSM 05-50-00-810-831-A INSPECTION OF THE A/C WAS PERFORMED AND ENGINES WERE INSPECTED NO EVIDENCE OF LEAKS. ENGINE RUN-UP PERFORMED. WE IDENTIFIED THE SOURCE OF THE ODOR. PLEASE SEE ITEM 1 ON LOG PAGE 2975560-1SDR GTIA2022053136448None · noneDIRTY SOCK SMELL IN AFT CABIN AFTER DECENDING THROUGH FL180-ACCOMPLISHED TSM 05-50-00-810-831 FOR CABIN ODOR. RAN BOTH PACK ON APU BLEED. ISOLATED PACKS, NO SIGN OF CONTAMINATION WITH AEROTRACER WALK THRU OF CABIN, RAN BOTH ENG BLEED, ISOLATED PACKS, NO SIGN OSDR CALA2022053001385Structure · corrodedE/E COMP ZONE 117 CORRODED INTERCSTAL BETWEEN FR STA 323.3- 312 BELOW LOWER SILL. REF TO PEMCO NR 12185.1141. REWORKED WEB AND REPLACED CHORD AT E/E COMPT ZONE 117 BETWEEN ST A 323 TO STA 312 S-23L BELOW LWR SILL PER B737-800 SRM 53-00-04 WORK PERFORMED BY V90SDR GTIA2022053136445None · noneL1 DOOR EMER ASSIST BOTTLE BELOW LIMITS-SERVICED L1 DOOR EMER ASSIST BOTTLE IAW AMM 52-10-00.SDR SWIA202265831None · damagedSTRUCK GEESE ON TAKEOFF AT 1200FT. RETURNED TO FIELD. DO NOT BELIEVE WE INGESTED ANY BIRDS INTO ENGINES. BELIEVE IT WAS TOP OF FUSELAGE ONLY. ( FLIGHT 3647 - FILED CLOSED) COMPLIED WITH COMPLETE BIRD STRIKE INSPECTION PER AMM 05-51-05, FOUND DAMAGE TO UPPSDR IXXA2022052805Lock · corrodedLOCK ASSY. CORRODEDSDR IXXA2022052804Seal Depressor · crackedSEAL DEPRESSOR CRACKEDSDR IXXA202205281003Stringer Fitting · corrodedSTRINGER CHANNEL FITTING CORRODEDSDR IXXA2022052802Frame · corrodedFRAME CHORD CORRODEDSDR IXXA202205281001Support · corrodedROLLER TRAY SUPPORT CORRODEDSDR JJBA20220527053None · noneAT REAR FUSE, CRACK FOUND ON RH TOP SKIN BTW FR 76 - FR 77 AT STR 2R. BUSHING REPAIR ON RH REAR FUSE 1 UPPER SKIN, BTW SKIN EDGE FR76 AND BTW STR 2R- 3RSDR JJBA20220527052None · noneCF 4 UNDERFLOOR FR 59 BTW STR 19L - 19R CORROSION ON TOP FLANGE. SPLICE REPAIR ON CENTER FUSE 4 FR 59, BTW STR 20L-21L & BTW STR 20R - 21RSDR JJBA20220527048None · noneAT REAR FUSE, CRACK FOUND ON LH TOP SKIN AT FR 75 BTW STR 2L-3L. REPAIR DOUBLER ON LH FUSE 1 UPPER SKIN AT FR 75 & BTW STR 1L-3SDR GTIA2022053136443None · noneCREW REPORTED AIR QUALITY EVENT -PERFORMED INSPECTION IAW TSM 05-50-00-810-831 FOUND GCU 2 DAMAGED. NO OTHER DEFECTS FOUND. SEE LOG PAGE 2812745-1.SDR UIEA2022052800552Doubler · crackedEO 4453A821-1 & 4 FUSELAGE SKIN NOSE WHEEL WELL FORWARD CORNER DOUBLER INSPECTION AND MODIFICATE (SB 747-53A2851) L/H FASTENERS & WASHERS DEVIATIONS DOUBLER S.E.M AND R/H FASTENERS WASHERS DEVIATIONS FASTENER HOLE CRACK (1EA), L/R DOUBLER INSTALLED AS PER BOSDR CALA2022053001366Buttstrap · corrodedDURING AFT CARGO INSPECTION CORROSION WAS FOUND ON THE BUTTSTRAPAT FR64, BTW STRG 44-43R AS NOTED ON LTPR NR#5001146904-0010. REWORKED CORROSION ON BUTTSTRAP FR64, STR 43-44R NDT HFEC ADDITIONAL REQUIREMENTS, REF LP 8685828 AND ROTO INSPECTED WITH NIL FINDINGSSDR CALA2022053001378Structure · crackedBS 2370 PIVOT BULKHEAD RH FORWARD OUTER CHORD CRACK FOUND AS MARKED. TRANSFER REF NR HX WO.728386 AND ORIGINATED BY EMP NO.V897425. EA 5380-01113 REV A OP 014 ACCOMPLISHED. WORK ACCOMPLISHED BY MECHANIC V893003 INSPECTED BY V897231. RII INSPECTED BY HX169517.SDR CALA2022053001377Structure · crackedLH BS2370 PIVOT BULKHEAD FORWARD CHORD FOUND 1EA CRACK APPROX 1.5" LONG AS MARKED. TRANSFER REF NR HX WO.727733 AND ORIGINATED BY EMP NO.V897425. EA 5380-01113 REV A OP 013 ACCOMPLISHED. WORK ACCOMPLISHED BY MECHANIC V893003 INSPECTED BY V897231. RII INSPECTEDSDR SWIA202266086None · corrodedMAIN AVIONICS BAY STR 21L BACK UP SILL ATTACH ANGLE (PN SH670-31828-1) COMMON TO FS349.00 FRAME CORRODED (C-CHECK RO 7/8/2022) EVALUATED ATTACH ANGLE AT STR21L COMMON TO FS349.00, EXFOLIATE CORROSION WAS FOUND OUT OF LIMITS. REMOVED AND INSTALLED NEW MASDR SWIA202266085None · corrodedMAIN AVIONICS BAY FS349.00 FRAME CORRODED BETWEEN STR 26L AND STR 26R (C-CHECK RO 7/8/2022) REMOVED AND INSTALLED NEW FS349.00 FRAME FROM STR 23L TO STR 24R REF. CRJ 700 SRM 51-42-06-001-001-A01 AND DWG:SH690-31350 REV M. COMPLIED WITH TASK CARD 51-900-SDR JJBA20220526051None · noneAT REAR FUSE, CRACK FOUND ON RH TOP SKIN AT FR 75 BTW STR 2R - 3 R. REPAIR DOUBLER ON RH FUSE 1 UPPER SKIN, AT FR 75 & BTW STR 2R - 3 RSDR JJBA20220526050None · noneAT REAR FUSE II EXT, SUSPECTED CRACKS (12X) FOUND ON LH SIDE SKIN BTW FR 77 - FR80 AND BTW STR 3R - 9 R. 8 BUSHING REPAIRS ON LH REAR FUSE 2 SKIN ON FR 77-78-79 AND BTW STR 3L-10L. REPAIR DOUBLERS ON LH FUSE SKIN. DOUBLER #1 ON FR 78 & BTW STR 5L-7L & DOUBLER SDR JJBA20220526049None · noneSUSPECTED CRACK ON LH BEAM AT FR33. REPAIR DOUBLER ON LH CENTER FUSE 2 OMEGA BEAM AT FRAME 33SDR JJBA20220526047None · noneLH WINDSHIELD HAS SIGNS OF CORROSION AT LOWER OUTBD FLANGE ON BACKSIDE. EVAL AREA AT LH WINDSHIELDS LOWER OUTBD FLANGE ON BACK SIDE, FWD ORIG THICKNESS .160" MAT LOSS .011" REMAINING MAT .149" ON AFT SIDE ORIG THICKNESS .160" MAT LOSS .018" REMAINING MAT .142 SDR JJBA20220526046None · noneANGLE SHAPE FOUND CRACKED ON INBD SIDE OF MAIN FLOOR BEAM Y - 479.0 BTW STA 4154.5 & 5633.0. REMOVED AND REPLACED ANGLE AS REQUIREDSDR CALA2022052701365Frame · crackedFR68 STR 22 LH FRAME HAS CRACK INDICATION IN RADIUS OF STR22 FLA NGE. GEN BY V892444 PER NR9294428/36428 9 FOR REF. ON HAECO LP 9294428 WITH NO DEVIATIONS ON THE FR68 ST EPAIR ON THE LH FR68 STR22LH FRAME INNER WEB PER PART 3 OF THE L R22LH FRAME INNER WEB/STISDR CALA2022052701361Skin · damagedREF AMES NR 0100-0224. DENT/GOUGE ON LEFT HAND SIDE FUSELAGE STA LINE 450 WATERLINE 167 REQUIRES REPAIR DUE TO OUT OF LIMITS. REPAIRED DAMAGED AREA AT WL 167 STA 457 L/H SIDE IAW AMES REA 47486REA03. ACCOMPLISHED BY V931857.SDR JR2R20220526233Web · crackedLH WHEEL WELL WEB AT FR52 CRACKEDSDR DALA2022052703713Strap · misrepairedSHIP 666 HOLE INCORRECTLY DRILLED (DISTANCE WITH ADJACENT RIVET) ON STABILIZATION STRAP AT PASSENGER FLOOR STRUCTURE (LOOKING UP FROM AFT CARGO), STA. 1520, RBL 24. CORRECTIVE ACTION: SUMMARY OF NRC 00248: STABILIZATION STRAP AT PASSENGER FLOOR STRUCTURE WAS RSDR UIEA2022051600482Fitting · crackedFUSE - CENTER SECTION - STA 1000 FRONT SPAR SHEAR TIE AND INTERCOSTAL LUG FTG INSPECTION FOUND CRACKED AT STA 1000 RBL 33.99. FUSE - CENTER SECTION - STA 1000 RBL 33.99" FRONT SPAR SHEAR TIE LUG FTG P/N 69B14267U9 REPLACED AND INSTALLED IAW ATLAS EO: 4453C024 SDR UIEA2022051600483Fitting · crackedFUSE - CENTER SECTION - STA 1000 FRONT SPAR SHEAR TIE AND INTERCOSTAL LUG FTG INSPECTION FOUND CRACKED AT STA 1000 LBL 57.5. FUSE - CENTER SECTION - STA 1000 LBL 57.5" FRONT SPAR SHEAR TIE LUG FTG P/N: 69B14267U7 REPLACED AND INSTALLED IAW ATLAS EO: 4453C024 PSDR UIEA2022051800487Cargo Track · crackedAFT CARGO STA 1860 AND STA 1880 LBL 24" CARGO TRACK FOUND CRACKED. AFT CARGO STA 1830.45 TO STA 1890.45 LBL 24.75 CARGO TRACK REPAIRED IAW RI-53-00-15595 REV.ASDR UIEA2022051800488Skin · crackedEO 4453A516 PART 1 AND PART 2 - FUSE SKIN NOSE WHEEL WELL AFT CORNER SKIN PANEL INSPECTION FOUND LH SKIN CRACKED. FUSE - STA 400 L/H AND R/H SKIN NOSE WHEEL WELL AFT CORNER SKIN PANEL MOD ACCOMPLISHED IAW EO 4453A516 PART 3 AND PART 4 AND RI-53-10-15613 REV.A<SDR FXGA202205252213Longeron Splice · corrodedCORRODED LONGERON AND SPLICES FROM F/STA 1211 TO 1259. TO REMOVE AND REPLACE A CORRODED LONGERON SECTION (29L) AND ITS TWO CORRODED SPLICES AT F/STA 1211 AND 1259. REMOVED CORRODED SPLICES AND STRINGER SECTION, REPLACE WITH NEW. PERFORM ALL WORK FROM DC-9/MD-SDR JJBA20220525044None · noneAGING AIRCRAFT FINDING: FLOOR PANEL 231JF AFT SUPPORT AT MAIN DOOR HAS SIGNS OF CORROSION. REMOVED AND REPLACED 1EA SHAPE U SUPPORT AFT AT MAIN DOORSDR JGVR20220525003Angle · corrodedFOUND THE EXISTING LH AND RH TAILCONE STINGER RUDDER FAIRING ATTACHMENT ANGLES CORRODED BEYOND REPAIR, REPLACED WITH NEW TEXTRON P/N 6912630-67 AND P/N 6912630-68 REFERENCING CESSNA 680A SRM 51-40-05 AND SRM 51-40-13.SDR JR2R20220525584Doubler · corrodedRH SHEAR PANEL IS CORRODED BETWEEN FR12 AND FR14SDR CALA2022052501339Intercostal · corrodedE/E COMP ZONE 117 CORRODED INTERCOSTAL BETWEEN FR STA 344-330.6 BELOW LOWER SILL. REF TO PEMCO NR 12185.1140. REMOVED AND REPLACED CHORD (ANGLE) L/H STRING 23 STA 260 TO STA 360. P/N 141A8240U37 IAW B737-800 SRM 51-40-02 AND 51-40-05 WORK PERFORMED BY V907635,
Back to JASC 5300