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 COMA2010030450053Bulkhead · crackedFORWARD PRESSURE BULKHEAD AT FS 202.75 CRACKED AT CUTOUT FOR PARKING BRAKE CABLE. REPAIRED FWD PRESSURE BULKHEAD AT FS 202.75 IAW REO 601R-53-11-563 AND EA 10-5311-02890.SDR SWAA101140Pressure Panel · crackedDURING SCHEDULED 14Y CHECK, FOUND PRESSURE DECK SKIN CRACKED AT BS 664, LBL 32. REMOVED AND REPLACED SKIN PER SRM.SDR SIMA201006003Bulkhead · dentedDURING MAINTENANCE BASE VISIT FOUND THE REAR PRESSURE BULKHEAD DENTED/CREASED BEYOND LIMITS. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED REAR PRESSURE BULKHEAD IAW EO EM-53MR-1438. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR ASOA201000332Bulkhead · crackedCOMPLIED WITH A SPECIAL DETAILED INSP OF FS559.0 PRESSURE BULKHEAD WEB AND CAP ANGLE LOCAL TO BL9.0 AND BL18.0 LT AND RT IAW NDT MANUAL, PART 6, 53-41-201. (3) CRACKS NOTED LBL18 APPROX .2500" IN THE FRAME RADIUS, RBL18 APPROX .5" IN THE FRAME RADIUS AND RBL1SDR DALA1045698972Stiffener · crackedDURING H-CHECK FOUND HORIZONTAL STIFFENERS CRACKED AT FWD SIDE OF APB, LT UPPER CORNER. REPAIRED ANGLES IAW SRM 53-10.SDR COMA2010030150050Pressure Panel · crackedFOUND CRACK AT FS 461.00 PRESSURE FLOOR SKIN BL 0.00 (UNDER A/C DUCT). REPAIRED PRESSURE FLOOR SKIN AT FS 461.00 BL 0.00 IAW REO 601R-53-41-103.SDR VNAA2010022800015Bulkhead · crackedDURING SCHEDULED MAINTENANCE A CRACK WAS FOUND IN PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL FITTING. MAINTENANCE REPAIRED USING AIRCRAFT MAINTENANCE MANUALS AND RELEASED THE AIRCRAFT FOR SERVICE.SDR VNAA2010022800016Bulkhead · crackedDURING SCHEDULED MAINTENANCE A CRACK WAS FOUND IN PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL FITTING. MAINTENANCE REPAIRED USING AIRCRAFT MAINTENANCE MANUALS AND RELEASED THE AIRCRAFT FOR SERVICE.SDR TRBACPCP2010016Pressure Blkhd · corrodedCORROSION WAS FOUND ON THE FWD PRESSURE BULKHEAD IN ONE AERA OF THE WEB. REMOVED CORROSION IAW ATR SRI DO/TS-1189/10-13104, REF NDT REPORT AMS 100226-19 FOR HFEC AND UT RESULTS, COMPLIED WITH ATR SARAS DO/TS-1189-10...5623, C/W EO E2-53MR-236. NO SUPPLIEMENTSDR AALA20100224TUL31Support Angle · crackedCRACK ON FORWARD SIDE OF AFT PRESSURE BULKHEAD VERTICAL SUPPORT ANGLE ABOVE VAULT DOOR JAMB CENTERLINE OF AIRCRAFT AT STATION 1338. INSTALLED NEW SUPPORT ANGLE ON FORWARD SIDE OF AFT PRESSURE BULKHEAD ABOVE VAULT DOOR JAMB PER SRM 51-30-05.SDR ASOA201000309Bulkhead · crackedFOUND REAR PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL ATTACHMENT FITTING HAS INDICATION NOTED APPROX .2" IN LENGTH 70 PERCENT FSH. FAILED NDT INSPECTION. REPAIR PER EC/TC REO 601R-53-61-1230 HAS BEEN COMPLETE AND THE REPAIR C/W THE REQUIREMENTS OF ECTC ASDR COMA2010022450046Bulkhead · crackedREAR PRESSURE BULKHEAD WEB CRACKED AT CARGO DOOR TRACK ATTACH, LBL 27, FS 621. CUT OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER IAW REO 601R-53-61-1541, REV B.SDR SWIA201024064Bulkhead · crackedFS 559 PRESSURE BULKHEAD CRACKED. (C CHECK) REPAIRED PER REO.SDR VNAA2010022800014Bulkhead · crackedDURING SCHEDULED MAINTENANCE AT FS 559 BULKHEAD WEB, RBL 18 WL 59.10, A CRACK WAS FOUND. MAINTENANCE REPAIRED USING AIRCRAFT MAINTENANCE MANUALS AND RELEASED THE AIRCRAFT FOR SERVICE.SDR SIMA201005305Bulkhead · corrodedDURING MAINTENANCE BASE VISIT THE RIGHT FRAME 280 BULKHEAD LOWER WEB WAS FOUND TO BE CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT FRAME 280 LOWER WEB IAW EO CR-53MR-174. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SWAA100952Bulkhead · crackedDURING SCHEDULED 26Y CHECK, FOUND RT AFT BULKHEAD WEB CRACKED AT BS 663, RBL 58. REPAIRED WEB PER ER.SDR SWAA100945Bulkhead · crackedDURING SCHEDULED 14Y CHECK, FOUND BULKHEAD VERTICAL BEAM WEB CRACKED BETWEEN BS 178 TO BS 184, LBL 17.0. REMOVED AND REPLACED WEB SECTION PER SRM.SDR SWAA100944Bulkhead · crackedDURING SCHEDULED 14Y CHECK, FOUND BULKHEAD VERTICAL BEAM WEB CRACKED BETWEEN BS 178 TO BS 184, RBL 17.0. REMOVED AND REPLACED WEB SECTION PER SRM.SDR DALA104029872Bulkhead · crackedDURING "H" CHECK FOUND CRACK IN LT WEB IN NOSE WHEEL WELL STA 83. REPAIRED IAW SRM 53-01-2.SDR COMA2010022250044Bulkhead · crackedFOUND CRACK AT FS 621.00 BULKHEAD ABOVE AFT CARGO DOOR TRACK. REPAIRED AFT PRESSURE BULKHEAD AT FS 621.00 ABOVE AFT CARGO DOOR TRACK IAW REO 601R-53-61-1541.SDR ASOA201000284Bulkhead · crackedFS 559.0 BULKHEAD WEB & CAP ANGLE HAS (5) HFEL INDICATIONS NOTED AS LISTED: (1) IN WEB 70 PERCENT FSH 0.5" LONG AT RBL 18.0 WL 59.10 (2) IN WEB 60% FSH0.5" LONG AT RBL 9.0 WL 54.10 (3) IN CAP ANGLE 60 PERCENT FSH 0.2" LONG BELOW RBL 18.0 POST (4) IN CAP ANGLE SDR AALA20100217TUL01Bulkhead · crackedFORWARD LOWER LEFT SIDE OF RADOME BULKHEAD HAS CRACK AT STOP PAD ALIGNMENT PIN. DOUBLER WAS INSTALLED PER AARD 53-10-00-19.SDR USAA2010021890398Pressure Panel · crackedCLT - MAJOR REPAIR - Q5 CHECK - LEFT WHEEL WELL PRESSURE WEB CRACKED AT BS 663, LBL 28. REPAIRED THE LEFT WHEEL WELL PRESSURE WEB AT BS 663, LBL 28 IAW B737 SRM 53-60-51 REPAIR 4.SDR 2010FA0000445Firewall · crackedCRACK AT STA 124, ENGINE FIREWALL, M/R TRANSMISSION OIL COOLER LINES AREA.SDR UIEA201000056Strap · crackedFUSELAGE - BS 1241, LT BULKHEAD - SPLICE STRAP AND FORGING CRACK - REPAIR 747-53-2283, REV 4.SDR A6WA201040133Rib · crackedRT MLG WW BATT RIB CRACKED. REPAIRED RT MLG BATT RIB IAW REO 601R-57-51-046.SDR AALA20100215TUL06Doubler · corrodedCORROSION OUT OF LIMITS ON DOUBLER AT CENTER OF 1138 BULKHEAD AT LONGERON 30. INSTALLED DELTA PLATE DOUBLER PER SRM 51-30-00.SDR A6WA201040128Bulkhead · crackedFS 202.75 PRESSURE BULKHEAD CRACKED AT BRAKE CABLE PASS THRU. REPAIRED PRESSURE BULKHEAD FS 202.75 IAW REO 601R-53-11-563.SDR A6WA201040119Bulkhead · crackedFS 202.75 PRESSURE BULKHEAD CRACKED AT BRAKE CABLE PASS THROUGH. REPAIRED FS 202.75 PRESSURE BULKHEAD IAW REO 601R53-11-563.SDR ASOA201000254Isolator · crackedFOUND REAR PRESSURE BULKHEAD ISOLATOR IS CRACKED LBL9.0, APPROX WL 90. REMOVED AND REPLACED CRACKED ISOLATOR IAW SRM 51-42-10 FIG 4 AND 51-42-13 STEP 8.SDR ASOA201000253Bulkhead · crackedFOUND REAR PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL ATTACHMENT FITTING HAS INDICATION NOTED APPROX .2" IN LENGTH 90 PERCENT FSH FAILED NDT INSPECTION. REPAIR IAW EC/TC REO 601R-53-61-1230 HAS BEEN COMPLETE & THE REPAIR C/W THE REQUIREMENTS OF EC/TC & SDR ASOA201000252Bulkhead · crackedFOUND FS 559 BULKHEAD WEB RT SIDE HAS INDICATIONS NOTED OTBD OF RBL 9.0 WL 58.70 APPROX .2" IN LENGTH 55 FS AND INBD OF RBL 18.0 WL54.0 APPROX .3" IN LENGTH 60 PERCENT FSH FAILED NDT INSPECTION. REPAIRED FS 559 BULKHEAD AND CAP ANGLES FROM LBL 27 TO RBL 27 IASDR QXEA2010021600090Bulkhead · corrodedC-CHECK - LT AND RT LOWER BULKHEAD AT FS 280, SHOWS EVIDENCE OF CORROSION. BLENDED LIGHT SURFACE CORROSION IAW SRM 53-11-10-201-003-A01. TREATED, PRIMED & PAINTED WORKED AREAS IAW SRM 51-21-06-001-001-A01, 51-21-11-001-001-A01, AND 51-25-16-001-001-A01.SDR A6WA201040135Bulkhead · damagedFS559 PRESSURE BULKHEAD REG`S REO 601R-53-41-260. REPAIRED FS559.00 IAW REO 601R-53-41-260.SDR ASOA201000223Bulkhead · corrodedFS280 LT BULKHEAD WEB IS CORRODED ON INBD BOTTOM CORNER. REMOVED CORROSION FROM FS280 LH BULKHEAD PER SRM 51-21-06-001-001-A01. REMOVED .002 TO .003 APPROX .038 TO .037 LEFT AFTER BLENDOUT WITHIN LIMITS PER SRM 53-11-10-201-003-A01. ALODINED, PRIMED AND TOPSDR SWIA201023767Bulkhead · crackedFS 621 BULKHEAD WEB CRACKED ABOVE CARGO DOOR TRACK FITTING. (C CHECK) REPAIRED PER REO.SDR COMA2010021550040Bulkhead · crackedDURING EDDY CURRENT FOUND CRACK IN AFT PRESSURE BULKHEAD FS 621.00 ABOVE CARGO DOOR TRACK. REPAIRED AFT PRESSURE BULKHEAD AT FS 621.00 IAW REO 601R-53-61-1541.SDR USAA2010021890395Bulkhead · corrodedCLT - MAJOR REPAIR - Q5 CHECK - LEVEL 2 EXFOLIATION CORROSION ON THE AFT PRESSURE BULKHEAD WEB AT BS 1016, LBL 4 - RBL 4. REPAIRED THE AFT PRESSURE BULKHEAD WEB AT BS 1016, LBL 4 - RBL 4 IAW TYPICAL REPAIR 53-83-01.SDR USAA2010021590381Stiffener · corrodedCLT - MAJOR REPAIR - Q5 CHECK - LEVEL 2 EXFOLIATION CORROSION ON AFT PRESSURE BULKHEAD STIFFENER ANGLES AT BS 1061, BL 0. REPAIRED AFT PRESSURE BULKHEAD STIFFENER ANGLES AT BS 1061, BL 0 IAW TYPICAL REPAIR 53-83-01.SDR USAA2010021190345Bulkhead · corrodedBFM - C2 - MAJOR REPAIR - MAIN LANDING GEAR WHEEL WELL PRESSURE BULKHEAD HAS CORROSION ON FAIL SAFE STRAP AT BS 955, S23L & S22L. ACCOMPLISHED PERMANENT REPAIR ON MAIN LANDING GEAR WHEEL WELL PRESSURE BULKHEAD FAIL SAFE STRAP AT BS 955, S22L & S23L IAW EA 134SDR USAA2010021190344Bulkhead · corrodedBFM - C2 - MAJOR REPAIR - RIGHT MAIN LANDING GEAR WHEEL WELL PRESSURE BULKHEAD HAS CORROSION ON FAIL SAFE STRAP AT BS 955, S23R. ACCOMPLISHED PERMANENT REPAIR ON RIGHT MAIN LANDING GEAR WHEEL WELL PRESSURE BULKHEAD FAIL SAFE STRAP AT BS 955, S23R IAW EA 13416SDR AALA20100209TUL03Stiffener · crackedCABIN AFT BULKHEAD CRACKED STIFFENER TOP FORWARD SIDE OF STATION 1338 BULKHEAD JUST AFT OF LONGERON 1. INSTALLED DOUBLER PER SRM 53-01-00 & AARD 53-10-00-15.SDR ASOA201000190Bulkhead · crackedFS 621.00 PRESSURE BULKHEAD HAS A 70 PERCENT FSH HFEC INDICATION NOTED APPROX 0.1" LONG IN THE WEB AT THE UPPER INBD CORNER OF THE LINTEL ATTACH FITTING. FAILS NDT INSP AT THIS TIME. REPAIR IAW EC/TC REO 601R-53-61-1230 HAS BEEN COMPLETED AND THE REPAIR C/W TSDR ASOA201000187Bulkhead · crackedFS 559.00 PRESSURE BULKHEAD WEB AND CAP ANGLE (LT) HAS 2 INDICATIONS NOTED AS LISTED: 60 PERCENT FSH, 0.2" LONG IN WEB APPROX 1.0" OTBD OF LBL 9.0 @ WL 51.70. 2) 50 PERCENT FSH, 0.2" LONG IN CAP ANGLE RADIUS BELOW LBL 9.0 POST. AREAS MARKED ON ACFT. FAILS NDTSDR ASOA201000186Bulkhead · crackedFS 559.00 PRESSURE BULKHEAD WEB (RHS) HAS 3 INDICATIONS NOTED AS LISTED: 60 PERCENT FSH, 0.5" LONG IN WEB AT RBL 18.0 WL 59.10. 60 PERCENT FSH, 0.2" LONG IN WEB 1" OTBD OF RBL 9.0 WL 58.70. 50 PERCENT FSH, 0.2" LONG IN WEB AT RBL 9.0 WL 54.10. AREAS MARKED SDR SWAA100754Bulkhead · crackedDURING SCHEDULED 14Y CHECK, FOUND BULKHEAD VERTICAL BEAM WEB CRACKED BETWEEN BS 178 TO BS 180, RBL 5.7. REPAIRED WEB PER ER.SDR SWIA201024025Bulkhead · crackedFS 621 PRESSURE BULKHEAD CRACKED AT LINTEL FITTING INTERFACE. (C CHECK) REPAIRED PER REO.SDR SWIA201024024Angle · crackedFS 559 PRESSURE BULKHEAD CAP ANGLE CRACKED. (C CHECK) REPAIRED PER REO.SDR SWIA201024023Bulkhead · crackedFS 621 BULKHEAD WEB CRACKED ABOVE UPPER CARGO DOOR TRACK FITTING. (C CHECK) REPAIRED PER REO.SDR SWIA201023761Bulkhead · crackedFS 559 BULKHEAD WEB AND CAP ANGLE RADIUS CRACKED. (C CHECK) REPAIRED PER REO.
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