JASC 5312
Service difficulty reports · 20,045
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 SWAA2016071853922Pressure Panel · crackedMAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS 663, LBL 35, CENTER WING BOX. REPAIRED WEB IAW SRM.SDR SWAA2016071353746Fitting · crackedAFT CARGO BAY BULKHEAD FITTING CRACKED AT BS 948, LBL 10. R & R THE FITTING IAW SRM.SDR REXA2016061701181Bulkhead · crackedAFT PRESSURE BULKHEAD IS CRACKED AT TOP OF CARGO DOOR AFT TRACK AT 621. REPAIRED AFT PRESSURE BULKHEAD CRACK WEB AT TOP OF CARGO DOOR AFT TRACK LBL 27.5, FS 621 IAW REO 601R-53-61-1541 AND REO 601R-53-61-5735.SDR SWAA2016062953342Pressure Panel · crackedLOWER FUSELAGE WEB CRACKED AT BS 663.75, RBL 12. REPAIRED WEB IAW SRM.SDR SWAA2016062753215Bulkhead · canningAFT PRESSURE BULKHEAD OIL CANNED AT BS 1016, STR 1L. REPAIRED BULKHEAD PER SRM AND EA.SDR SWAA2016062353155Bulkhead · crackedBULKHEAD CRACKED AT BS 663, LBL 33. R & R BULKHEAD IAW SRM AND DWG.SDR SWAA2016062153099Pressure Panel · crackedLOWER FUSELAGE WEB CRACKED AT BS 663.75, LBL 30. REPAIRED WEB IAW EA.SDR FQAR20160617027Doubler · crackedDURING A ROUTINE INSPECTION, A DOUBLER INSTALLED ON A BULKHEAD IN THE EMPENNAGE WAS FOUND TO BE CRACKED. THE CRACKED DOUBLER WAS MADE VISIBLE BY REMOVING THE FAIRING BETWEEN THE VERTICAL FIN AND AFT FUSELAGE AND LOOKING AFT AND UP WITH A MIRROR AND FLASHLIGHTSDR WVER2016061750503Stiffener · crackedFS 202.75, FWD SIDE OF BULKHEAD, LBL 30.0 STIFFENER HAS AN INDICATION .15" LONG AT THE UPPER EDGE OF FLANGE.SDR SWAA2016071853977Pressure Panel · crackedMAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS 663, RBL 42. REPAIRED WEB IAW EA.SDR K11A2016071472203Bulkhead Web · corrodedCORROSION AT FWD BULKHEAD UNDER RAY DOMESDR REXA2016061501178Bulkhead · gougedAFT PRESSURE BULKHEAD, FWD LT SIDE HAS SKIN GOUGED. REPAIRED 621 BULKHEAD LT FWD SIDE IAW REO 601R-53-61-2155, REO 601R-53-61-1285.SDR REXA2016061401220Bulkhead Web · gougedFWD FACE OF AFT BULKHEAD BS 621, RBL 36.20 IS GOUGED. CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLER IAW REO 601R-53-61-1285 REV D.SDR REXA2016061401176Bulkhead · cracked202.75 BULKHEAD AT BL 23.7 IS CRACKED AT BRAKE CABLE PASS THROUGH. REPAIRED STA 202.75, BULKHEAD AT LBL23.7 IAW REO 601R-53-11-563.SDR LR7A2016061400801Angle · crackedDURING SCHEDULED C-12 CHECK, UNDER JOB CARD HC5313, FOUND THE LT AFT FUSELAGE INTERIOR FS 836 BULKHEAD WEB ANGLE CRACKED AT WL190, WL185, LBL62. REPAIRED IAW SMP583 SRM FIG 51-140-19.SDR LR7A2016061400800Angle · crackedDURING SCHEDULED C-12, CHECK UNDER JOB CARD HC5313, FOUND THE RT AFT FUSELAGE INTERIOR FS836, BULKHEAD WEB ANGLE CRACKED AT WL190, WL185, RBL62. REPAIRED IAW SMP583, SRM FIG 51-140-19.SDR SWAA2016062953326Pressure Panel · crackedMAIN WHEEL HORIZONTAL PRESSURE DECK BEADED WEB CRACKED AT BS 665, RBL 39. REPAIRED WEB PER SRM.SDR FXGA201606141611Bulkhead · crackedAFT PRESSURE BULKHEAD CRACKED AT LBL 40, FRAME STA 996 LT. DURING INSPECTION A CRACK WAS DISCOVERED. AFT PRESSURE BULKHEAD CRACKED AT LBL 40, FRAME STA 996 LT. REMOVE CLIP FROM RADIAL TRIM OUT DAMAGE HAT SECTION. FABRICATED REPAIR ANGLES AND INSTALLED IAW SDR SWAA2016061552868Structure · looseRIGHT MLG FORWARD BULKHEAD WHEEL WELL AREA PATCH LOOSE. SECURED PATCH IAW EA.SDR SWAA2016061352791Pressure Panel · crackedRIGHT MLG WHEEL WELL FORWARD CENTER WING REAR SPAR VAPOR WEB CRACKED. REPAIRED WEB IAW SRM.SDR FDEA201606111949Stiffener · crackedRIGHT ACM COMPARTMENT, STA 595 BULKHEAD, HORIZONTAL STIFFENER, 3RD FROM BOTTOM, OTBD EDGE IS CRACKED. FABRICATED NEW STIFFENER NCA6044-58 IN REF TO DWG NCA6044.SDR WVER20160611003Bulkhead Web · corrodedLEFT AND RIGHT FS 280.00, LOWER BULKHEAD WEBS, FOUND TO BE CORRODED. REPAIRED LT & RT FS 280.00 LOWER BULKHEAD WEB'S IAW REO 670-53-11-594, REV-A, DATED 2015/06/26.SDR SWAA2016070653548Frame · crackedLOWER BULKHEAD FRAME CRACKED AT BS 540, STRINGER 22R. REPAIRED FRAME IAW EA.SDR REXA2016061001091Bulkhead · corrodedFOUND BULKHEAD LOWER WEB AT FS 280.0 LT SIDE & RT SIDE TO BE CORRODED AND TO BE OUT OF LIMITS. WEBS LT SIDE & RT SIDE REQUIRED R & R IAW REO 670-53-11-594. COMPLIED WITH REO: 670-53-11-594, REV A.SDR SWAA2016062953334Pressure Panel · crackedMAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS 663, BETWEEN LBL 25 TO LBL 25.5. REPAIRED WEB IAW ER & EA.SDR SWAA2016062853291Pressure Panel · crackedMAIN WHEEL WELL SPAR VERTICAL PRESSURE WEB CRACKED AT BS 663, BETWEEN RBL 33 TO RBL 34. REPAIRED WEB IAW SRM.SDR SWAA2016062353170Pressure Panel · crackedRT WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS 663, RBL 42. REPAIRED WEB IAW SRM.SDR AALA20160609002Pressure Panel · crackedAIRCRAFT WAS IN BASE MX. MLG WW FWD VERTICAL PRESS WEB AT FS 663.75 IS CRACKED, BETWEEN RBL 10 & RBL 46 & BETWEEN LBL 25 - 46. REPAIRED WEB IAW SRM 57-10-10-2R REPAIR 3 ALTERNATIVE 2 EA 260887 & EA 260941.SDR FDEA201606081893Cap · crackedRIGHT BS 595 BULKHEAD TEE CAP VERTICAL LEG UPPER FASTENER HOLE AT LONGERON 39R HAS A CRACK INDICATION.SDR FDEA201606081892Bulkhead · crackedRIGHT BS 595 BULKHEAD WEB LOWER FASTENER HOLE COMMON TO THE TEE CAP HAS A CRACK INDICATION.SDR SWAA2016061552877Pressure Panel · crackedLOWER COMPOSITE WEB CRACKED AT BS 663, BETWEEN RBL 30 TO RBL 33. REPAIRED WEB IAW EA.SDR REXA2016060701015Bulkhead · crackedINDICATION NOTED AT FS 621 REAR PRESSURE BULKHEAD FWD FACE AT TOP OF CARGO DOOR TRACK, LBL 27.50, WL 82, APPROXIMATELY .400 IN LENGTH AND 100 PERCENT FULL SCREEN HEIGHT. FAILED NDT. CONTINUATION CARD 8798615, OP 77. REPAIRED FS 621 BULKHEAD IAW REO 601R-53-SDR SWAA2016061352816Pressure Panel · crackedRIGHT MAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS 663, RBL 34. REPAIRED WEB IAW SRM.SDR FQAR20160607024Doubler · crackedDURING A ROUTINE INSPECTION, A DOUBLER INSTALLED ON A BULKHEAD IN THE EMPENNAGE WAS FOUND TO BE CRACKED. THE CRACKED DOUBLER WAS MADE VISIBLE BY REMOVING THE FAIRING BETWEEN THE VERTICAL FIN AND AFT FUSELAGE AND LOOKING AFT AND UP WITH A MIRROR AND FLASHLIGHTSDR SWAA2016071153644Bulkhead Web · crackedNOSE WHEEL WELL RT SIDE WEB CRACKED BETWEEN BS 247 - 248, RBL 16. REPAIRED THE WEB IAW SRM.SDR WVER2016060600007Bulkhead · crackedPOST AT LBL30 ON FWD SIDE OF BS 202 BULKHEAD HAS AN INDICATION NOTED AT TOP AFT I-BEAM INSPECTION .200" LONG, FAILED NDT.SDR SWAA2016062753225Pressure Deck · crackedINTERNAL UPPER HORIZONTAL MAIN WHEEL WELL PRESSURE DECK CRACKED AT BS 673, LBL 40. REPAIRED WEB IAW SRM AND EA.SDR WVER2016060401Stiffener · crackedFS 202.25 FORWARD SIDE OF BULKHEAD, RBL 30 AND LBL 30 STIFFENERS INDICATED CRACKS.SDR CALA2016060600347Bulkhead · crackedLEFT WW FWD BULKHEAD APPEARS TO BE CRACKED APPROX 6" FROM CEILING. REMOVED DAMAGED AREA & INSTALLED REPAIR IAW SRM 57-10-10 REPAIR 3 PARA 4B.SDR AALA20160603003Stiffener · crackedAIRCRAFT WAS IN BASE MX. VERTICAL STIFFENER ON FS 1338 BULKHEAD ABOVE VAULT DOOR IS CRACKED. R & R STIFFENER IAW AARD 51-00-05 & DWG 9915562.SDR FDEA201606031807Bulkhead · crackedRIGHT STATION 595 BULKHEAD, LONGERON 38R, T CAP AFT LEG HAS CRACK INDICATION FROM RADIUS TO END OF LEG SECTION. CRACK LOCATED 1.75" BELOW LONGERON 38R. R & R SECTION OF CRACKED TEE CAP FROM LONGERON 36R TO 44R AT STA 595, PN ACA7016-501 IN REF TO DWG SR10530SDR SWAA2016060952697Pressure Panel · crackedMAIN WW VERTICAL PRESS WEB CRACKED AT BS 663, LBL 34. REPAIRED WEB IAW SRM.SDR SWAA2016060952696Pressure Panel · crackedMAIN WW VERTICAL PRESS WEB CRACKED AT BS 663, RBL 34. REPAIRED WEB IAW SRM.SDR SWAA2016060952720Pressure Panel · crackedRIGHT MAIN WW SPAR VERTICAL WEB CRACKED AT BS 663, RBL 34. REPAIRED WEB IAW SRM.SDR SWAA2016061452859Pressure Panel · crackedMAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS 663, LBL 27. REPAIRED WEB IAW EA.SDR SI6R20160705002Door · failedREMOVED CONDITIONED AIR DUCT FROM AFT PRESSURE BULKHEAD TO EXPOSE PLASTIC DOORS THAT ARE HINGED TO CHECK VALVE. PRESSURIZED AIRCRAFT IN HANGAR IN ACCORDANCE WITH MAINTENANCE MANUAL TO 8.0 PSI. PUSHED ON CHECK VALVE HINGED DOORS WITH HANDLE OF PLIERS, WHEN RESDR SIMA20160531010Bulkhead · corrodedRIGHT COCKPIT BULKHEAD IS CORRODED ON THE AFT SIDE AT FLOORBEAM FS 280.00. REPAIRED RT COCKPIT BULKHEAD IAW EO CR-53MR-174.SDR SIMA20160531007Stiffener · crackedLEFT BULKHEAD STIFFENER AT FS 280.00, 2ND FROM INBD IS CRACKED. INSTALLED NEW LT BULKHEAD STIFFENER 2ND FROM INBD AT FS 280.00 IAW SRM 51-42-06.SDR SIMA20160531008Stiffener · crackedSECOND FROM INBD STIFFENER FOR FS 280 BULKHEAD WEB, IS CRACKED AT THE LOWER END, RT HAND. INSTALLED NEW RT BULKHEAD STIFFENER 2ND FROM INBD IAW SRM 51-42-13 & 51-42-06.SDR FQAR20160531023Doubler · crackedDURING A ROUTINE INSPECTION, A DOUBLER INSTALLED ON A BULKHEAD IN THE EMPENNAGE WAS FOUND TO BE CRACKED. THE CRACKED DOUBLER WAS MADE VISIBLE BY REMOVING THE FAIRING BETWEEN THE VERTICAL FIN AND AFT FUSELAGE AND LOOKING AFT AND UP WITH A MIRROR AND FLASHLIGHT
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