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 SWAA082600Bulkhead · corrodedDURING SCHEDULED BRDG CHECK, FOUND AFT PRESSURE BULKHEAD WEB CORRODED AT BS 1016, BL 0. REPAIRED WEB PER ACO.SDR SWIA200820132Bulkhead · crackedREAR PRESSURE BULKHEAD WEB HAS .5 INCH CRACK (C-CHECK). REPAIRED PER REO.
SDR SWIA200820131Bulkhead · crackedREAR PRESSURE BULKHEAD WEB AT LINTEL ATTACHMENT HAS .2 INCH CRACK (C-CHECK). REPAIRED PER REO.
SDR SWIA200820130Bulkhead · crackedREAR PRESSURE BULKHEAD WEB HAS .5 INCH CRACK (C-CHECK). REPAIRED PER REO.
SDR USAA920081116Bulkhead · crackedMCN - MAJOR REPAIR - C21 CHECK - CRACKED BULKHEAD WEB, BS 178, LBL 17, WL 225. REPAIRED BULKHEAD WEB, BS 178, LBL 17, WL 225 IAW B737 SRM 53-10-08 2R 12 FIGURE 201.SDR SWAA082507Bulkhead · canningDURING SCHEDULED MV2 CHECK, FOUND AFT PRESSURE BULKHEAD OIL CANNED AT BS 1016, BETWEEN STR 5L AND STR 6L. REPAIRED BULKHEAD PER SWA EA.SDR MALA080074Bulkhead · crackedRT UPPER AFT BULKHEAD AT STA 733 CRACK FOUND. RT UPPER AFT BULKHEAD AT STA 733 REPAIRED IAW EO S53561 LPI INSPECTION DONE PER EO S53561 AND NO DEFECTS FOUND YG 1132.SDR SWAA082405Pressure Panel · crackedDURING SCHEDULED MV1 CHECK, FOUND NLG W/W FWD LEFT PRESSURE WEB CRACKED AT BS 246, WL 170. REPAIRED WEB PER SWA EA.SDR SWAA082424Stiffener · crackedDURING SCHEDULED BRDG CHECK, FOUND RADIAL STIFFENER CRACKED AT AFT PRESSURE BULKHEAD BS 1016, 3 O'CLOCK POSITION. REMOVED AND REPLACED STIFFENER PER SRM.SDR QXEA200800555Bulkhead · corrodedRFD C4 CHECK RT FS 280 LOWER BULKHEAD CORRODED. BLENDED CORROSION. BLENDED .003 MATERIAL FROM LOWER BULKHEAD IAW CRJ 700 SRM 53-11-10. ETCHED ALODINE PRIMED IAW CRJ 700 SRM 51-21-11 AND 51-25-06. APPLIED TOP COAT IAW SRM 51-25-01.SDR QXEA200800554Bulkhead · corrodedRFD C4 CHECK LT FS 280 LOWER BULKHEAD CORRODED. BLENDED CORROSION, ALL BLENDS WITHIN LIMITS, BLENDED .003 FROM LOWER BULKHEAD IAW CRJ 700 SRM 53-11-10. ETCHED ALODINE PRIMED IAW CRJ 700 SRM 51-21-11 AND 51-25-06, APPLIED TOP COAT IAW SRM 51-25-01.SDR SWAA082372Bulkhead · crackedDURING SCHEDULED BRDG CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, RBL 5.7, WL 187. REPAIRED WEB PER SWA EA.SDR 08FDEA01718Support Angle · crackedUPPER INTERMEDIATE AFT FUSELAGE (ZONE 312); AFT PRESSURE BULKHEAD (STA 2007), AFT FACE UPPER CENTER SECTION. THE FUSELAGE SKIN SUPPORT ANGLE IS CRACKED. REMOVED AND REPLACED THE SUPPORT ANGLE IAW SRM 51-31-01 & 51-35-01; VOL II; PG 1. ALODINED & PRIMED SDR SWIA200820010Bulkhead · crackedCRACK INDICATION NOTED ON AFT PRESSURE BULKHEAD LBL 36.20 JUST ABOVE LOWER LINER ATTACH CLIP. FOUND AT C-CHECK. REPAIRED PER REO 601R-53-61-1285 SHEET 11.
SDR A6WA200840388Bulkhead · crackedCRACK EXISTS ON FS 202 AT LBL 23 PRESSURE BULKHEAD AROUND PARKING BRAKE CABLE. REPAIR PERFORMED ON FS 202.75 LBL 23.72 PRESSURE BULKHEAD AROUND PARKING BRAKE IAW REO 601R-53-11-563. (A)SDR A6WA200840394Bulkhead · crackedREAR PRESSURE BULKHEAD CRACK AT LINTEL ATTACHMENT POINT. AFT PRESSURE BULKHEAD IN LINTEL FITTING AREA REPAIRED IAW REO 601R-53-61-1230 REV D. (A)SDR AALA200801146Bulkhead · deformedTUL - AFT PRESSURE BULKHEAD WEB DEFORMED AT STATION 1338. AREA OF DISCREPANCY IS 45 INCHES BY 28.5 INCHES. REPAIRED BULKHEAD DOME PER SRM 53 03 FIGURE 33 VIEW C ON BOTH SIDES OF AIRCRAFT PER ESO 80559.SDR SWAA082262Pressure Panel · crackedDURING SCHEDULED 12Y CHECK, FOUND NLG W/W CEILING PANEL WEB CUTOUT CRACKED AT BS 252, RBL 8. REPAIRED WEB PER ACO.SDR SWAA082296Bulkhead · crackedDURING SCHEDULED BRDG CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, LBL 17, WL 225. REPAIRED WEB PER SRM.SDR GLBA20061092Bulkhead · crackedFWD PRESSURE BULKHEAD CRACKED AT FS 84.0 AT RT AVIONICS BAY AT INTERSECTION A OF ANGLE AT WL 92.0 AND STIFFNER AT RBL 15.75. MAINTENANCE REPAIRED CRACK IN FORWARD PRESSURE BULKHEAD IAW SERVICE BULLETIN STEPS 3 THROUGH 8 & STEPS 1- THROUGH 22 AT F.S. 84.0. REPASDR SWAA082237Bulkhead · crackedDURING SCHEDULED BRDG CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, RBL 10, WL 234. REPAIRED WEB PER SRM.SDR SWAA082171Bulkhead · crackedDURING SCHEDULED BRDG CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, LBL 7 TO RBL 4.5, WL 198 TO WL 206. REPAIRED WEB PER SRM.SDR 08FDEA01485Bulkhead · corrodedBS 178 BULKHEAD EXT SURFACE WL 187 - 193 LBL 19" TO 24" HAS CORROSION PITS. CHEMICALLY REMOVED CORROSION FROM BS 178 BULKHEAD EXT SURFACE WL 185-193 LBL 19" TO 24". THICKNESS OF MATERIAL IS .055, MATERIAL REMAINING IS .053 A LOSS OF .022 FOUND TO BE WITH-IN LSDR 2008FA0000300Bulkhead · crackedWHILE PERFORMING AN (A-B) INSPECTION FOUND RT AFT FUSELAGE BLEED AIR LINE ATTACH BRACKETS PULLED FROM AFT FUSELAGE BULKHEAD RESULTING IN CRACKS IN THE BULKHEADS AT FRAME STA 329.92. RECOMMEND INSPECTING AREA THOROUGHLY AT EACH INSPECTION. RECOMMEND CONTACTINSDR USAA920080936Bulkhead · crackedMCN - MAJOR REPAIR - C21 CHECK - CRACKED BULKHEAD WEB, BS 178, RBL 3, WL 207. REPAIRED BULKHEAD WEB, BS 178, RBL 3, WL 207 IAW B737 SRM 53-10-08 2R11.SDR USAA920080935Bulkhead · crackedMCN - MAJOR REPAIR - C21 CHECK - CRACKED BULKHEAD VERTICAL BEAM WEB, BS 178, RBL 17.1, WL 183. REPAIRED BULKHEAD VERTICAL BEAM WEB, BS 178, RBL 17.1, WL 183 IAW B737 SRM 53-10-08 2R12.SDR USAA920080934Bulkhead · crackedMCN - MAJOR REPAIR - C21 CHECK - CRACKED BULKHEAD VERTICAL BEAM WEB, BS 178, RBL 5.7, WL 180 - WL 184. REPAIRED BULKHEAD VERTICAL BEAM WEB, BS 178, RBL 5.7, WL 180 - WL 184 IAW B737 SRM 53-10-08 2R12.SDR USAA920080933Bulkhead · crackedMCN - MAJOR REPAIR - C21 CHECK - CRACKED BULKHEAD CHORD, BS 178, RBL 29, WL 206 - WL 208. REPLACED BULKHEAD CHORD, BS 178, RBL 29, WL 206 - WL 208 IAW B737 SRM 51-40-02.SDR USAA920080932Bulkhead · crackedMCN - MAJOR REPAIR - C21 CHECK - CRACKED BULKHEAD CHORD, BS 178, LBL 5.7, WL 184. REPAIRED BULKHEAD CHORD, BS 178, LBL 5.7, WL 184 IAW B737 SRM 53-10-08-2R5.SDR USAA920080931Gusset · crackedMCN - MAJOR REPAIR - C21 CHECK - CRACKED BULKHEAD GUSSET, BS 178, RBL 20, WL 207. REPLACED BULKHEAD GUSSET, BS 178, RBL 20, WL 207 IAW B737 SRM 51-40-02.SDR A6WA200840369Bulkhead · crackedREAR PRESSURE BULKHEAD CRACKED AROUND LINTER FITTING ATTACHMENT POINT. REPAIRED IAW CRJ 200 REO 601R-53-61-1230 REV D. (S)SDR TRAX200800567Bulkhead · crackedVERTICAL BEAMS AT FS 409.0+128 (WING BOX FWD BULKHEAD) CRACKED IN THE RADIUS ON THE BOTTOM OUTBOARD SIDE AT LBL-18 AND INBOARD SIDE AT LBL 27. JOB COMPLETE. REPAIRED VERTICAL BEAMS AT FS 409.0+128 AT LBL-18 AND AT LBL-27 AS PER REO 601R-53-41-056. CUT OUT DSDR A6WA200840358Bulkhead · crackedREAR PRESSURE BULKHEAD WEB CRACK FS 621 LBL 45 BTWN WL 106.17 AND WL (LINTEL ATTACHMENT FITTING). REAR PRESSURE BULKHEAD WEB FS 621 LBL 45 BTWN WL 106.17 AND WL 113.33 REPAIRED IAW REO 601R-53-61-1230 REV D.SDR A6WA200840352Bulkhead · dentedDENT EXIST ON FLIGHT COMPARTMENT BULKHEAD FS 280 RBL 9 WL 93.0 FLIGHT COMPARTMENT BULKHEAD REPAIRED IAW REO 601R-53-11-1376.SDR TRAX200800543Bulkhead · crackedAFT PRESSURE BULKHEAD CRACKED JUST ABOVE CARGO DOOR TRACK. REPAIRED PER REO 601R-53-61-1541 AND REO 601R-53-61-2599. REMOVED FASTENERS AS REQUIRED PER REO 601R-53-61-1541. CUT OUT DAMAGED AREA AS SHOWN PER REO 601R-53-61-1541. PERFORMED ET INSPECTION OF REWOSDR TRAX200800542Bulkhead · crackedAFT PRESSURE BULKHEAD CRACKED AT LINTEL FITTING. REPAIRS PERFORMED IN ACCORDANCE WITH REO 601R-53-61-1230.SDR SWAA082045Bulkhead · crackedDURING SCHEDULED BRDG CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, RBL 17.1. REPAIRED WEB PER SRM.SDR A6WA200840329Bulkhead · crackedCRACK EXIST ON FORWARD PRESSURE BULKHEAD F/S 202.75 BL 45, WL 69, 684 AROUND PARKING BRAKE (.250 LONG). (M) FWD PRESSURE BULKHEAD REPAIRED IAW REO 601R5311536. (P)SDR SWAA082011Pressure Panel · crackedDURING SCHEDULED BRDG CHECK, FOUND BEADED PRESSURE WEB CRACKED AT BS 663, RBL 39. REPAIRED WEB PER SRM.SDR A6WA200840357Bulkhead · crackedCRACK FOUND ON PRESSURE BULKHEAD FS 202.75 LBL 23.71 AROUND PARKING BRAKE. CRACK PRESSURE BULKHEAD REPAIRED IAW REO 601R-53-11-563.SDR USAA920080937Bulkhead · crackedMCN - MAJOR REPAIR - C21 CHECK - CRACKED BULKHEAD WEB, BS 178, LBL 10, WL 234. REPAIRED BULKHEAD WEB, BS 178, LBL 10, WL 234 IAW B737 SRM 53-10-08 2R9.SDR USAA920080889Bulkhead · crackedMCM - MAJOR REPAIR - C21 - NR 6046444, .5 INCH CRACK ON WEB AT BS 178, WL 230, RBL17.1. INSTALLED REPAIR IAW SRM 53-10-08-2R 12 FIG 201.SDR 2008UALA02099Pressure Panel · crackedCABIN WING BOX UPPER PRESS DECK IS CRACKED BS 664 LBL 31". FABRICATED & INSTALLED REPAIR DOUBLER ON UPPER SURFACE OF PRESSURE DECK REF MM53-21-98 PG 801 & SRM51-40-02 PG 1-3. AC OK FOR SERVICE.SDR A6WA200840285Pressure Panel · corrodedCORROSION ON PRESSURE FLOOR FS 409 PLUS 128 TO FS 559, RBL 45. (M) CORROSION REMOVED ON PRESSURE FLOOR IAW SRM 51-21-06 .SDR A6WA200840286Pressure Panel · corrodedCORROSION ON PRESSURE FLOOR FS 409 PLUS 128 TO FS 559, LBL 45. CORRSION REMOVED IAW SRM 51-21-06.SDR USAA920080830Bulkhead · crackedCLT - MAJOR REPAIR - C22 CHECK - A 1" CRACK ON WEB AT BS 178, WL 187, BL 0. INSTALLED DOUBLER REPAIR IAW SRM 53-10-08 REPAIR 2.SDR SWAA081809Pressure Panel · crackedDURING SCHEDULED BRDG CHECK, FOUND BEADED PRESSURE WEB CRACKED AT BS 663, LBL 31. REPAIRED WEB PER SRM.SDR DLM88080545Splice · corrodedDURING HMV, CORROSION WAS FOUND ON AFT P-DOME WEB SPLICE AT 6HRS POSITION. WEB SPLICE WAS REPLACED IAW DOUGLAS DWG 5910130.SDR A6WA200840306Bulkhead · crackedCRACK EXISTS ON PILOT BULKHEAD FS 280 LBL 9 WL 71. (M) PILOTS BULKHEAD REPAIRED IAW REO 601R-53-11-171 REV "D". (A)SDR USAA920080831Bulkhead · crackedCLT - MAJOR REPAIR - C22 CHECK - TWO EACH CRACKS (.25") ON WEB EXTENDING FROM FASTENER HOLES AT BS 178, WL 234, RBL 9.5. INSTALLED DOUBLER REPAIR IAW SRM 53-10-08 R2 FIG 201.
Back to JASC 5312