JASC 5312
Service difficulty reports · 20,047
Reports filed under 5312 · Fuselage Main, Bulkhead, 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 = '5312' 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 = '5312' 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 UPS04843255Pressure Blkhd · crackedINSPECTION TYPE: C3, F/S 1766 FWD SIDE OF AFT PRESSURE BULKHEAD IS CRACKED 65 INCHES ABOVE FLOOR AND LBL 35. REMOVED EXISTING REPAIR AND CUT OUT CRACKED AREA. NDT VERIFIED NO CRACKS NOTED AT CUT OUT. FABRICATED FILLER, FINGER DOUBLER, & DOUBLER INSTALLED IASDR UPS04843254Pressure Blkhd · crackedINSPECTION TYPE:C3 F/S 1766 FWD SIDE OF AFT PRESSURE BULKHEAD IS CRACKED 65 INCHES ABOVE FLOOR AND RBL 35. REMOVED EXISTING REPAIR DOUBLERS AND CUT OUT CRACKED AREA. NDT VERIFIED NO CRACKS NOTED AT CUTOUT. FABRICATED REPAIR DOUBLERS & FILLER AND INSTALLED ISDR IXXA060149SPanel · dentedDURING ROUTINE C CHECK, FOUND LEFT AFT WHEEL WELL PANEL 161X DENTED ON OUTER SKIN. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS, LOCATED, TRIMMED, TREATED, APPLIED ADHESIVE, CURED, AND PRIMED REPAIR PARTS IAW DC8 SRM 51-1-9A, 53-8-3, 51-1-15, AND 51-1-8.SDR CALA0400628Beam · corrodedINSPECTION FOUND BULKHEAD BEAM WEB CORRODED AT STA 110, S30L. THE BEAM WEB WAS REPAIRED IAW ECRA 5310-04387.SDR UPS04843308Bulkhead · corrodedINSPECTION TYPE: C3, FWD SIDE OF FS 70 BULKHEAD LOWER CHORD HAS INTERGRANULAR CORROSION AT LONGERON 32R. FOUND INTERGRANULAR CORROSION OUT OF LIMITS IAW DC-8 SRM 53-2-0 FIG 1F. REMOVED STA 70 LOWER FWD CHORD BETWEEN LONGERONS 32R & 33R. FABRICATE AND ONE -9SDR 2005FA0000267Bulkhead · crackedDURING COMPLIANCE OF NDT EDDY CURRENT INSP OF FS-793.75 BULKHEAD, CAP ANGLE WAS FOUND CRACKED. NEW CAP ANGLE WAS INSTALLED IAW DWG NR SE20000210, REV. D.SDR USAA040583Channel · corrodedPIT - FOUND RADIAL CHANNEL CORRODED 1 SQUARE INCH, AFT PRESSURE BULKHEAD. REMOVED CORROSION, MANUFACTURED AND INSTALLED RADIAL CHANNEL PER EO 5302V112. (M)SDR EIA2004073Pressure Panel · corrodedRT WING GEAR WW PRESSURE DECK HAS SURFACE CORROSION SEVERAL AREAS BETWEEN BS 1319-1337 10 INCH INBD OF FUSELAGE SKIN. REMOVED CORROSION PER B747 SRM 51-10-01 AND 53-10-07 FOUND OUT OF LIMITS, REMOVED DAMAGE , FABRICATED REPAIR PARTS AND INSTALLED PER B747SRM SDR SWIA200414423Angle · crackedAT 280 BULKHEAD, BL 9.00 & BR 9.00 2 ANGLES CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED THE NEW ANGLES AT FS 280 L & R BL 9 UNDER FLOORBEAMS IAW EO 601R-53-11-136.SDR DLM88040834Bulkhead · crackedCRACKED WEB IN FWD FACE OF AFT P-DOME AT X=0. REPLACED WEB IN UPPER FWD EDGE OF AFT P-DOME AT X=0.SDR DL73S040828Bulkhead · crackedINSPECTION OF THE FS 178 BULKHEAD PER AD 200-05-29 REVEALED A CRACK IN THE FLOOR WEB AT WL 207.5 AND RBL 28. THE CRACKED SECTION OF WEB WAS REMOVED AND REPLACED WITH A NEW PART PER ER/A 093110-14AD.SDR UPS04243196Bulkhead · crackedINSPECTION TYPE:C, BULGING CORROSION AND CRACKED SKIN FOUND ON BS 870 BULKHEAD RBL 43 APPROX HALF WAY DOWN ON BULKHEAD. DERIVETED REPAIR STRAP ON BULKHEAD IAW SRM 51-30-02. REPAIR FOUND OUT OF LIMITS. DAMAGED SECTION CUT OUT IAW SRM 53-10-09. HFEC CARRIED SDR SWAA042514Bulkhead · crackedDURING SCHEDULED SERVICE CHECK, FOUND BULKHEAD WEB AT BS 727, LBL 14, WL 175, CRACKED. REPAIRED BULKHEAD WEB PER EA.SDR SWAA042519Bulkhead · crackedDURING SPV, FOUND BULKHEAD WEB AT BS 178, RBL 10, WL, 234, CRACKED. REMOVED AND REPLACED WEB SECTION PER SRM.SDR SWAA042533Bulkhead · canningDURING SCHEDULED HC2-CHECK, FOUND AFT PRESSURE BULKHEAD ABS 1016, BETWEEN STR 11R AND STR 12L, OIL CANNING. REPAIRED BULKHEAD SECTION PER SRM.SDR COMA0460486Fitting · shearedLEFT AND RIGHT LOW PRESSURE AIR CONDITIONING DUCTS, BULKHEAD FITTINGS HAVE ALIGNMENT PINS MISSING. PERFORMED A MAJOR REPAIR AT FS 621.00 LT AND RT BY REMOVING DAMAGED BULKHEAD FITTINGS, AND INSTALLING NEW FITTINGS P/N 601R96151-7 AT BOTH LOCATIONS IAW CRJ SRMSDR F3LA200400091Pressure Panel · crackedFLIGHT CREW REPORTED ALTITUDE CABIN CLIMBED AT 150 FPM WITH BOTH PACKS IN AUTO AT CRUISE ALTITUDE. PRESSURIZED AIRCRAFT ON THE GROUND AND FOUND AN 8-INCH CRACK AT TOP OF RT WHEEL WELL, STA 664, RBL 37. REPAIRED PER SRM 53-60-51, FIGURE 203, DETAIL IV AND EA SDR UPS04843128Bulkhead · crackedINSPECTION TYPE: C2, THE AFT PRESSURE BULKHEAD WEB APPROXIMATE 2 INCH CRACK AT RBL 3 STA.1766 FROM INSIDE 60 H0LE. REPAIRED AFT PRESSURE BULKHEAD WEB 2 INCH CRACK AT STA.1766 RBL 3 IAW SAA SK708-993 DATED 8/26/04, UPS EO DC8-5320-20956 DATED 09/08/04 & 8110-3SDR F3LA200400086Bulkhead · crackedDURING C-2 CHECK, INSPECTION REPORTED CRACK ON OTBD SIDE OF LBL 5.7 BELOW WL 207 ON 178 BULKHEAD. REPAIRED CRACKS ON 178 BULKHEAD BELOW WL 207 PER EA B3-53R-10470 AND SRM 53-10-08 FIG 210.SDR F3LA200400085Bulkhead · crackedDURING C-2 CHECK, INSPECTION REPORTED CRACKS ON 178 BULKHEAD AT IB SIDE OF LBL 5.7 VERTICAL CORD AND BELOW WL 207. REPAIRED CRACKS ON 178 BULKHEAD BELOW WL 207 IAW EA B3-53R-10470 AND SRM 53-10-08, FIG. 210.SDR F3LA200400084Bulkhead · crackedDURING C-2 CHECK, INSPECTION REPORTED TWO CRACKS AT BL 0, ABOVE WL 184.5 AT 188.0, 178 BULKHEAD. REPAIRED CRACKS AT BL 0 ABOVE WL 184.5 IAW SRM 53-10-08, FIG. 211, DETAIL VIII AND EA B3-53R-10470.SDR F3LA200400083Bulkhead · crackedDURING C-2 CHECK, INSPECTION REPORTED CRACK ON BULKHEAD AT BS 178 AT IB SIDE OF LBL 5.7 VERTICAL CORD AND ABOVE WL 207. REMOVED DAMAGE FROM BULKHEAD AT BS 178 AT IB SIDE OF LBL 5.7. FABRICATED REPAIR DOUBLER AND INSTALLED IAW SRM 53-10-08.SDR F3LA200400082Bulkhead · crackedDURING C-2 CHECK, INSPECTION REPORTED CRACK ON 178 BULKHEAD, RBL 5.7, BELOW WL 207 IB OF RBL 5.7 AT LOWER RADAR ANTENNA MOUNT. PERFORMED REPAIR IAW EA B3-53R-10470 AND SRM 53-10-08, FIG. 210, DETAIL VII.SDR F3LA200400081Bulkhead · crackedDURING C-2 CHECK, INSPECTION REPORTED CRACK ON 178 BULKHEAD ON O/B SIDE OF RBL 5.7 ABOVE WL 207. REMOVED DAMAGE, FABRICATED REPAIR PARTS, TREATED, PRIMED AND INSTALLED PER EA B3-53R-10470 AND SRM 53-10-08, FIG 210, DETAIL 3.SDR F3LA200400080Bulkhead · scratchedDURING C-2 CHECK, INSPECTION REPORTED CRACK AT 178 BULKHEAD O/B OF RBL 5.7 AT WL 218. DETERMINED TO BE A SCRATCH, NOT A CRACK. FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE, FABRICATED DOUBLER, TREATED, PRIMED AND INSTALLED REPAIR PER EA B3-53R-10470 AND SRM 53SDR F3LA200400079Bulkhead · crackedDURING C-2 CHECK, INSPECTION REPORTED CRACKED WEB 178 BULKHEAD AT BL 19R, WL 195. REMOVED CRACKED WEB PER SRM 51-40-02. REMOVED DOUBLER PER SRM 51-40-02. PARTIALLY OPENED 178 BULKHEAD WEB TO GET ACCESS TO CRACKED WEB PER SRM 51-40-02. DRILLED NEW INTERCOSTSDR SWIA200413925Angle · crackedFS 625 OBLIQUE ANGLE IS CRACKED ON LT SIDE OF AFT PRESSURE BULKHEAD, APPROX .65 INCH LONG. (ITEM FOUND AT C-CHECK INSPECTION.) INSTALLED ANGLE PN 601R-35012-51 IAW CRJ 200 SRM 51-42-06.SDR DL76L040767Bulkhead · gougedTHE WEB OF THE CANTED BULKHEAD ON THE FWD SIDE OF THE NLG WHEEL WELL WAS FOUND GOUGED AT WL 175 AND LBL 22. THE GOUGE WAS REMOVED WITH A 1 X 2 INCH CUTOUT. THE CUTOUT WAS REPAIRED WITH AN ALUMINUM REPAIR DOUBLER PER ER/A 092714-14.SDR USAA040457Bulkhead · crackedPIT - FOUND FORWARD PRESSURE BULKHEAD CENTER CRACKED .5 INCH, STATION 178 FPBH RBL 6 WL 215. INSTALLED DOUBLER REPAIR PER EO 5300V153 REV A. (M)SDR SWAA042296Bulkhead · crackedDURING SCHEDULED C4 CHECK, FOUND BS 1016 AFT PRESS BULKHEAD WEB CRACKED AT STR 6L. REPAIRED WEB PER SWA EA.SDR USAA040421Bulkhead · crackedPIT - FOUND BULKHEAD SKIN CRACKED .5 INCH, BL 0, WL 186, STATION 178 BULKHEAD. CUT OUT DAMAGE, INSTALLED FILLER AND DOUBLER PER SRM 53-10-08, FIG 203. (M)SDR USAA040420Bulkhead · crackedPIT - FOUND BULKHEAD SKIN CRACKED .75 INCH, STATION 178 BULKHEAD LBL 5.7 ABOVE WL 184, INBOARD SIDE. REMOVED CRACK AND INSTALLED DOUBLER PER EO 5300V155. (M)SDR SWAA042284Bulkhead · crackedDURING SPV, FOUND BS 1016, BULKHEAD WEB AT STR 7R AND STR 8R, CRACKED. REPAIRED BULKHEAD WEB PER EA.SDR SWAA042276Gusset · crackedDURING SCHEDULED 1/4D CHECK, FOUND BS 178, BULKHEAD LOWER GUSSET AFT CORNER CRACKED. REMOVED AND REPLACED GUSSET PER BAC DRAWING.SDR QXEA200400622Bulkhead · crackedBULKHEAD CRACKED AT BATHTUB FITTING RT SIDE OF AFT PRESSURE BULKHEAD. REPAIRED IAW REO 670-53-61-034.SDR SWAA042245Beam · crackedDURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM AT BS 178, RBL 17.1, WL 226, CRACKED. REMOVED AND REPLACED VERTICAL BEAM PER SRM.SDR SWIA200413866Angle · crackedLT FS 625 OBLIQUE ANGLE IS CRACKED ON AFT SIDE OF AFT PRESSURE BULKHEAD IN ECS BAY. ( ITEM FOUND AT C-CHECK INSPECTION.) REMOVED AND REPLACED DAMAGED BRACKET IAW SRM 51-42-06. N 601R-35012-51.SDR MWEA040128Angle · crackedCABIN SIDE OF AFT PRESSURE BULKHEAD, A STIFFNER AT TWELVE O'CLOCK POSITION IS CRACKED ON OB END. FABRICATED AND INSTALLED ANGLE.SDR UPS04242965Panel · crackedINSPECTION TYPE: C, CRACK FOUND ON SKIN IN LT W/W I/B SKIN JUST BEHIND BRACKET FOR PLUMB BOB. HFEC CARRIED OUT ON ABOVE AREA IAW NDTM 51-00-00 PT 6 FIG 4, CRACK CONFIRMED, ENDS MARKED. CUTOUT DAMAGED SKIN & FABRICATED REPAIR DOUBLER IAW SRM 51-40-2. INSTALLSDR USAA040373Bulkhead · crackedPIT - FOUND BULKHEAD WEB CRACKED .5 INCH, FS 178 BULKHEAD WEB, B/L0, WL/L 186. INSTALLED DOUBLER, FILLER PER SRM 53-10-08 FIG 203. (M)SDR USAA040354Bulkhead · crackedPIT - FOUND FORWARD PRESSURE BULKHEAD CRACKED APPROX 1 INCH, STATION 178 FPBH, WL 218, LBL 10. REPAIRED UNDER EO 5300V153 UNDER INSPECTION PROGRAM. (M)SDR USAA040377Frame · crackedPIT - FOUND FRAME CRACKED .5 INCH, BELTFRAME STATION 767 AT STRINGER S14L. INSTALLED DOUBLER AND FILLERS PER SRM 53-00-07 PAGES 202-203. (M)SDR USAA040375Bulkhead · crackedPIT - FOUND SKIN CRACKED 1.25 INCH, THROUGH FASTENER STATION 1040 BL-0 AFT PRESSURE BULKHEAD, 9 FASTENERS ABOVE CENTER OF BULKHEAD. MANUFACTURED FILLER AND DOUBLER PER 53-80-08 FIG 201. (M)SDR USAA040353Bulkhead · crackedPIT - FOUND FORWARD PRESS BULKHEAD CRACKED 1 INCH, STATION 178 RBL 10. REPAIRED UNDER EO 5300V153 AND ON A INSPECTION PROGRAM. (M)SDR USAA040349Frame · corrodedPIT - FOUND PRESSURE FRAME CORRODED .25 INCH BY 8 INCH AREA, AFT PRESSURE BULKHEAD BS 1016 BETWEEN STRINGER 27L AND 26R. (M)SDR USAA040350Bulkhead · corrodedPIT - FOUND AFT WEB PRESSURE BULKHEAD CORRODED .5 INCH BY .5 INCH AREA, BS 1016 ABOVE AND BETWEEN. (M)SDR DL738040687Bulkhead · puncturedTHE FS 178 BULKHEAD ASSY WAS DAMAGED BY CONTACT WITH A JETWAY AT WL 230 NEAR RBL 30. THE RBL 17 BEAM, THE UPPER BULKHEAD AND RT SIDE CHORD WERE DAMAGED AND REPLACED. THE BULKHEAD WEB DAMAGE WAS REMOVED WITH A CUTOUT AND REPAIRED WITH TWO ALUMINUM REPAIR DOUBSDR EIA2004054Pressure Panel · corrodedFUSELAGE INTERIOR, STA 1420, LBL 10 TO RBL 10 CORROSION ON UPPER SURFACE OF WHEEL WELL PRESSURE DECK WEB. REMOVED DAMAGED AREA. FABRICATED REPAIR FILLER AND DOUBLERS. INSTALLED REPAIR DOUBLERS AND FILLERS PER B747 SRM 53-10-07 FIG 2.SDR USAA040369Bulkhead · crackedPIT - FOUND BULKHEAD SKIN CRACKED .25 INCH, AT RIVET OUTBOARD OF RBL 57 AT WL 234 STATION 178 BULKHEAD. INSTALLED DOUBLER PER EO 5300V153. (M)SDR UPS04242775Bracket · crackedINSPECTION TYPE: C, ON REMOVAL OF SECTION OF BULKHEAD AT BS 178, SUPPORT BRACKET FOR PNEUMATIC BOTTLE FOUND CRACKED. REMOVED SUPPORT BRACKET FOR PNEUMATIC BRAKE BOTTLE IAW SRM 51-30-2. FABRICATED SUPPORT BRACKET IAW DRW60-6962 AND SRM 51-20-1 FIG 7, INSTALLE
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