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 USAA920071104Bulkhead · crackedMCN - MAJOR REPAIR - C20 CHECK - CRACKED FORWARD PRESSURE BULKHEAD WEB, BS 178, LBL 17, WL 224. REPAIRED FORWARD PRESSURE BULKHEAD WEB, BS 178, LBL 17, WL 224 IAW B737 SRM 53-10-08-2R12.SDR USAA920071103Bulkhead · crackedMCN - MAJOR REPAIR - C20 CHECK - CRACKED FORWARD PRESSURE BULKHEAD WEB, BS 178, LBL 5.7, WL 178. REPAIRED FORWARD PRESSURE BULKHEAD WEB, BS 178, LBL 5.7, WL 178 IAW B737 SRM 53-10-08-2R12.SDR SWAA075302Bulkhead · crackedDURING SCHEDULED 14Y CHECK, FOUND AFT PRESSURE BULKHEAD CRACKED AT BS 1016, STR 6L. REPAIRED BULKHEAD PER SRM.SDR USAA920071102Bulkhead · crackedMCN - MAJOR REPAIR - C20 CHECK - CRACKED FORWARD PRESSURE BULKHEAD WEB, BS 178, LBL 12, WL 234. REPAIRED FORWARD PRESSURE BULKHEAD WEB, BS 178, LBL 12, WL 234 IAW B737 SRM 53-10-08-2R9.SDR FDEA200710224660Bulkhead · crackedAIR CONDITIONING COMPT LT SIDE ON VERTICAL BULKHEAD FOUND CRACK. REPAIRED AREA IAW SRM 53-40-00 FIG 34 VOL I.SDR DHL2007748001Bulkhead · crackedRIGHT WW BS 870 BELOW LEAD CONTROL VALVE, BULKHEAD HAS 2 INCH CRACK. CUT OUT DAMAGED AREA BELOW APU LEAD CONTROL, CUT OUT 2" BY .75". FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 53-10-9 FIGURE 5. HEAT TREATED TO 150-190 KSI PER SPEC PO NR 7307279. ALSDR MASA200700726Bulkhead · crackedPRESSURE BULKHEAD FS 202.75, BL 23.71 FOUND CRACKED DURING C-CHECK, REPAIRED.SDR HYIA1352471Bulkhead · corrodedBULKHEAD LOCATED ON THE RIGHT FUSELAGE WALL JUST AFT OF FIRST OFFICERS SIDE WINDOW AT FUSELAGE STATION 154.5 FOUND TO BE CORRODED BEYOND MANUFACTURERS LIMITS. REMOVED CORRODED AREA AND SPLICED IN NEW BULK HEAD.SDR 07FDEA04660Bulkhead · crackedAIR CONDITIONING COMPT LT SIDE ON VERTICAL BHD FOUND CRACK.SDR KCSA071484Stiffener · corrodedCORROSION ON STIFFENER ON BOTTOM OF PRESSURE DECK AT BS 1265, LBL 78 TO LBL 114, WL 190.SDR SWAA075076Bulkhead · crackedDURING SCHEDULED BRDG CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 23L. REPAIRED WEB PER SRM.SDR WRNA200700065Bulkhead · crackedDURING ACCOMPLISHMENT OF CPCP TASK C53-310-02-00 AT M96 CHECK, LEVEL II CORROSION WAS FOUND ON AFT PRESSURE BULKHEAD AT STR TIE END ANGLE FITTING AT 35R. FABRICATED FITTING FROM 7076 T6511 EXTRUSION IAW SRM 51-10-40. APPLIED PROTECTIVE COATINGS IAW SRM 51-40SDR HYIA12138Stiffener · corrodedAFT PRESSURE BULKHEAD STIFFENER, BETWEEN STRINGERS LEFT 21 AND RIGHT 21, CORRODED. CORROSION REMOVED AND FOUND TO BE BEYOND MANUFACTURERS LIMITS. REMOVED AND INSTALLED STIFFENER IN ACCORDANCE WITH SRM 51-25-01.SDR HYIA12137Stiffener · corrodedFORWARD PRESSURE BULKHEAD LEFTHAND OUT BOARD STIFFNER CORRODED. CORROSION REMOVED AND FOUND TO BE BEYOND MANUFACTURERS LIMITS. REMOVED AND INSTALLED STIFNER IN ACCORDANCE WITH SRM 5125-01 AND 51-25-04.SDR USAA920070924Bulkhead · crackedMCN - MAJOR REPAIR - C-18 CHECK - NR 6505193, AFT PRESSURE BULKHEAD WEB CRACKED, BS 1016, LBL 58, WL 270. REPAIRED AFT PRESSURE BULKHEAD WEB, BS 1016, LBL 58, WL 270 IAW B737-300 SRM 53-80-08-2R7, FIGURE 201.SDR KCSA071452Bulkhead · chafedAPU PNEUMATIC DUCT SUPPORT CLAMP IS CHAFING ON STA 2460 BULKHEAD INNER CHORD AT LBL 44.SDR SWAA074976Pressure Panel · crackedDURING SCHEDULED C1 CHECK, FOUND LNG W/W CEILING PANEL WEB CUTOUT CRACKED AT OUTBOARD END. REPAIRED WEB PER ACO.SDR SWAA075003Pressure Panel · crackedDURING SCHEDULED 20Y CHECK, FOUND LEFT NLG W/W CEILING PANEL CRACKED AT BS 250 RBL 7.5. REPAIRED CEILING PANEL PER SRM.SDR SWAA075002Pressure Panel · crackedDURING SCHEDULED 20Y CHECK, FOUND RIGHT NLG W/W CEILING PANEL CRACKED AT BS 250 RBL 7.5. REPAIRED CEILING PANEL PER SRM.SDR ABXR070394Bulkhead · crackedAFT PRESSURE BULKHEAD LEFT VENTRAL DOOR CORNER (FORWARD SIDE) WAS CRACKED IN THE RADIUS OF THE FORWARD MOST FORMED SECTION. REPAIRED CRACK IAW DC9 SSRM DWG K05159.SDR KCSA071438Angle · crackedAFT BILGE BULKHEAD SUPPORT ANGLE IS CRACKED .5 INCH AT STA 1700, BELOW FLOOR LINE, RBL 18.SDR UIEA200700444Bulkhead · crackedRIGHT SIDE NOSE WHEEL WELL BULKHEAD WEB CRACKED AT STATION 260, WL 182 RBL 38. WEB REPAIRED AS PER BOEING MESSAGE 1-636527780-4.SDR LR7A07112Bulkhead · crackedDURING SCHEDULED C-7 CHECK PER JOB CARD HC5313 FOUND AFT FUSELAGE INTERIOR BULKHEAD WEB CRACK AT HI-LOK PIN HOLE FS 880 WL 210 RBL 73. REPAIR ACCOMPLISHED IAW SMP583 FIG 51-140-17 USING 7075T6 .040".SDR A6WA200740552Bulkhead · corrodedPILOTS BULKHEAD FS 280 HAS CORROSION APPROX .010 INCH DEEP BETWEEN LBL 9.0 AND RBL 9.0 AT WL 73.10. (M) MAINTENANCE INSTALLED NEW ANGLE IAW CRJ SRM 51-42-06 AND 51-42-13. (M)SDR 07FDEA04409Bulkhead · damagedFOUND OLD REPAIR (MISDRILLED HOLE) AT FRAME 54 BULKHEAD LT WEB, WAS ACCEPTED FOR ONLY ONE FERRY FLIGHT. REPAIR RENEWED BY REMOVING THE EXISTING DOUBLER, CUT OUT ON WEB FOOT AND INSTALLING DOUBLER AND REPAIR ANGLE IAW EA 6-5315-81126 AND RAS/AS/0248/2004 ISS BSDR USAA920070912Bulkhead · crackedCLT - MAJOR REPAIR - FPBH INSPECTION, CRACKED BULKHEAD WEB, BS 178, LBL 5, WL 184. REPAIRED BULKHEAD WEB, BS 178, LBL 5, WL 184 IAW USAIRWAYS EA 98903.SDR SWAA074865Pressure Panel · crackedDURING SCHEDULED HC2 CHECK, FOUND NLG W/W CEILING PANEL CRACKED AT BS 259, RBL 7.75. REPAIRED CEILING PANEL PER ACO.SDR NWAA073406301Bulkhead · crackedDURING "M" CHECK, FOUND CRACKS IN PRESSURE DECK CANTED BULKHEAD AT BS 1238. REPAIRED PER EA 63-210685 SECTION I. SECTION II REQUIRES DVI INSPECTIONS TO BE ACCOMPLISHED EVERY 4000 CYCLES.SDR KCSA071434Pressure Panel · crackedNOSE WHEEL WELL LEFT SIDE WALL PANEL WEB IS CRACKED .75 INCH AT STA 268, WL 170 BONDED STRAP.SDR KCSA071433Pressure Panel · crackedNOSE WHEEL WELL LEFT SIDE WALL PANEL WEB IS CRACKED .75 INCH AT STA 290, WL 170 BONDED STRAP.SDR KCSA071432Pressure Panel · crackedNOSE WHEEL WELL LEFT SIDE WALL PANEL WEB IS CRACKED .75 INCH AT STA 310, WL 170 BONDED STRAP.SDR TRAX200701479Bulkhead · corrodedFWD PRESSURE BULKHEAD AT LBL 10 LWR AREA, FITTING CORROSION FOUND (0.125 INCH) ON WEB.SDR TRAX200701426Angle · crackedON REAR PRESSURE BULKHEAD AFT SIDE AT FS 621.00 LBL 46.00 WL 93.00 AND RBL 46.00 WL 93.00 ANGLES FOUND CRACKED. BOTH CRACKED ANGLES OF F/S 621.00 AFT SIDE REMOVED AS PER SRM 51-42-20. NEW ANGLES FABRICATED AS PER SRM 51-24-16 AND TREATED AS PER SRM 51-21-11 SDR TRAX200701425Bulkhead · crackedON REAR PRESSURE BULKHEAD AR FS 621.00 RBL 36 MOUNT ISOLATOR BRACKET FOUND CRACKED. REPLACE ON REAR PRESSURE BULKHEAD AT FS 621.00 RBL 36, MOUNT ISOLATOR BRACKET REMOVED AND REPLACED IAW SRM 51-2-13.SDR LR7A07101Pressure Panel · crackedDURING SCHEDULED B-3 CHECK, WHEN REPAIRING RT MLG BEAM INNER CAP, FOUND A CRACKED PRESSURE WEB AT FS 577, WL 250, RBL 61. REPAIR ACCOMPLISHED IAW LYNDEN AIR CARGO MEA 382-53-07-059.SDR LR7A07098Bulkhead · crackedDURING SCHEDULED B-3 CHECK FOUND PER JOB CARD HB3200 LT MLG BHD CRACKED AT FS 610, WL183, LBL 62. REPAIR ACCOMPLISHED IAW SMP583 FIG 53-40-10.SDR TRAX200701422Pressure Panel · corrodedCORROSION FOUND ON FWD PRESSURE WEB, LBL 10 TOP AREA. 10-9-07 CORROSION REMOVED IAW SRM 51-21-42 WEB OUT OF LIMITS IAW SRM 53-11-00 FIG 301. REPAIR CARRIED OUT IAW SRM 53-11-10 FIG 403 FABRICATION COVER ON W/C 2000-9 MATERIAL THICKNESS: 0.053 MATERSDR SWAA074838Web · crackedDURING SCHEDULED MV1 CHECK, FOUND NLG W/W RIGHT ACCESS PANEL CUTOUT WEB CRACKED AT BS 247. REPAIRED WEB PER SWA EA.SDR KCSA071406Strap · corrodedLEFT AND RIGHT BS 1241 BULKHEAD SPICE STRAPS CORRODED AT AFT BOLT HOLES BS 1241, STR 27L AND STR 27R.SDR SWAA074775Bulkhead · crackedDURING SCHEDULED SPV CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, LBL 4.75. REPAIRED WEB PER SWA EA.SDR 07FDEA04212Bulkhead · damagedFOUND DENTS AT PRESSURE BULKHEAD FLOOR STRUCTURE C 49-50 (WITH CRACK 2MM) AND C 50-51 AT TR 4-5 LT ; C 52-53 AT TR 2-3 LT, C 48-49 AT TR 4-5 RT. REPAIR PERFORMED BY INSTALLING A DOUBLER AT TR 4-5 LT, C49-50 AND LET THAT DENTS AT THE OTHER AREAS AS IT IAW EA 6SDR SWAA074761Pressure Panel · crackedDURING SCHEDULED SPV CHECK, FOUND NLG W/W CEILING PANEL CRACKED AT RBL 7.5. REPAIRED PANEL PER ACO.SDR 07FDEA03930Strap · corrodedCORROSION FOUND BEHIND AFT PRESSURE BULKHEAD C80 AT INNER STRAP. REPAIR PERFORMED BY RELACEMENT OF PART IAW SRM 51-72-10.SDR 07FDEA03928Bulkhead · corrodedCORROSION FOUND BEHIND AFT PRESSURE BULKHEAD C80 AT CIRCUMFERENTIAL STRAP AND FLANGE REPAIR PERFORMED IAW SRM 53-19-17 FIG 201 AND DRAWING R539-707100.SDR EIA2007166Pressure Panel · corrodedNOSE LANDING GEAR WHEEL WELL, RT UPPER AT APPROX STA 280 HAS CORROSION BELOW AND UNDER STANDOFF. REMOVED CORROSION UNDER LINES SUPPORT (WEB) STA 280 RT WL 190 FOUND TO BE OUT OF LIMITS PER B747 SRM 53-30-01 AND 51-10-01. CUT OUT CORRODED SECTION AND INSTALLESDR ABXA070333Bulkhead · crackedAFT PRESSURE BULKHEAD CUTOUT LOWER LEFT UNMODIFIED CORNER HAD CRACK OF UNKNOWN LENGTH IN LOWER INBOARD SKIN TAB PORTION OF SKIN. REPAIRED AFT PRESSURE BULKHEAD ON LEFT AND RIGHT LOWER CORNERS IAW DC9 SRM.SDR LR7A07094Bulkhead · crackedDURING SCHEDULED B-2 CHECK, PER JOBCARD HB5302 FOUND AFT FUSELAGE INTERIOR UPPER BHD WEB CRACKED AT FS 880, WL 260, RBL 62. REPAIR CARRIED OUT IAW SMP583 FIG 53-50-05. P/N:7075T6 .063".SDR SWAA074612Stiffener · crackedDURING SCHEDULED BRDG CHECK, FOUND AFT PRESSURE BULKHEAD LOWER STIFFENER CRACKED AT BS 1016, 5 O'CLOCK POSITION. REPAIRED STIFFENER PER SRM.SDR SWAA074613Bulkhead · crackedDURING SCHEDULED BRDG CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, BL 0. REPAIRED WEB PER SRM.SDR USAA920070826Bulkhead · crackedCLT - MAJOR REPAIR - FPBH, CRACKED BULKHEAD WEB, BS 178, RBL 9.6, WL 234. REPAIRED BULKHEAD WEB, BS 178, RBL 9.6, WL 234 IAW B737-400 SRM 53-10-08.
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