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 AWXA200300740Bulkhead · crackedLCQ - MAJOR REPAIR - DURING C-13 CHECK A 1 INCH CRACK WAS FOUND AT FASTENER HOLE ON BS 178 BULKHEAD WEB, RBL 17.1, WL 230. MAINTENANCE CUT OUT CRACK AT RBL 17.1, WL 230; FABRICATED A REPAIR PLATE; INSTALLED REPAIR PART IAW B737-300 SRM 51-70-13 FIG 1 PG 1-5.SDR AWXA200300739Bulkhead · crackedLCQ - MAJOR REPAIR - DURING C-13 CHECK 3 EACH 1 INCH CRACKS WERE FOUND AT TWO FASTENER HOLES ON BS 178 BULKHEAD WEB, LBL 17.1, WL 230. MAINTENANCE CUT OUT CRACKS AT LBL 17.1, WL 230; FABRICATED A REPAIR PLATE; INSTALLED REPAIR PART IAW B737-300 SRM 51-70-13 FSDR SWAA031383Bulkhead · crackedDURING SCHEDULED RON, FOUND BS 1016 BULKHEAD WEB CRACKED (2 EA) BETWEEN STR 7L AND STR 8L. REPAIRED BULKHEAD WEB PER SWA EA.SDR UPS03440938Pressure Panel · corrodedINSPECTION TYPE:C RT BLG W/W PRESSURE DECK SKIN CORRODED AT FS 1391 - 1395 RBL 116-120 . FS 1385- FS 1395 PRESSURE DECK WEB REPAIRED IAW SRM 53-10-07 FIG 2.SDR UPS03440937Pressure Panel · corrodedINSPECTION TYPE:C RT BLG W/W PRESSURE DECK WEB CORRODED CRACK AT FS 1436-1438 RBL 112-114. PRESSURE WEB REPLACED IAW SRM 51-10-01 PG 8 DUE TO COR CRACK 1 INCH X 1 INCH AND THROUGH THE WHOLE THICKNESS EXCEEDED SRM 53-10-01 FIG 1 LIMITATION.SDR DL733030563Bulkhead · corrodedCORROSION WAS FOUND ON THE FWD SIDE OF THE AFT PRESSURE BULKHEAD. THE DAMAGE IS TO THE WEB AND STIFFENER AT THE BOTTOM OF THE BULKHEAD AT BL 0 AND STA 1016. DAL ER/A 385133-14AD PROVIDES INSTRUCTIONS TO REPAIR THE WEB AND STIFFENER PER BOEING SB 737-53A1075,SDR SWAA031380Pressure Panel · crackedDURING SCHEDULED 1/4D CHECK, FOUND BOTH LT AND RT NLG W/W WEBS CRACKED (2 EA) AT BS 246.0,WL 168.5. REPAIRED WEBS PER SWA EA.SDR AWXA200300745Bulkhead · crackedDURING C-13 CHECK 3 EACH 1 INCH CRACKS WERE FOUND ON BS 178 BULKHEAD WEB AT RBL 5, WL 197.75 - 198.75, WL 201 - 201.75, AND RBL 6.25, WL 200.75 - 201.5. MAINTENANCE STOP DRILLED CRACKS ON BS 178 BULKHEAD WEB AT RBL 5, WL 197.75 - 198.75, WL 201 - 201.75, AND RSDR AWXA200300738Bulkhead · crackedDURING C-13 CHECK 3 EACH 1 INCH CRACKS WERE FOUND ON BS 178 BULKHEAD WEB AT LBL 5, WL 200.5 - 201, WL 197.75 - 198.5, AND LBL 6.25, WL 200.3 - 201. MAINTENANCE STOP DRILLED CRACKS AT LBL 5, WL 200.5 - 201, WL 197.75 - 198.5, AND LBL 6.25, WL 200.3 - 201; PERFSDR USAA030122Pressure Panel · crackedFOUND TWO CRACKS IN WEB 1 INCH EACH, PRESSURE WEB AT STATION 665 RBL 40. DOUBLERS AND FILLERS INSTALLED AT CUTOUT OF WEB PER TYP REP 53-60-04. (M)SDR 2003FA0000660Bulkhead · crackedTHIS DEFECT WAS FOUND AS A RESULT OF INSPECTION REQUIRED BY AD. THIS PART WAS REPLACED AT THIS TIME JUNE 17, 2003. TT 5187.97. THIS REPORT REQUIRED BY AD PART (I).SDR SWAA031368Bulkhead · crackedDURING SCHEDULED C3 CHECK, FOUND BS 1016 BULKHEAD CRACKED AT STR 5L. REPAIRED BULKHEAD PER SRM.SDR USAA030113Bulkhead · corrodedFOUND WEB CORRODED, 12 INCHES BY 6 INCHES, AFT PRESS BULKHEAD STATION 1016 LBL 4 INCHES-RBL 4 INCHS. MODIFIED PART NR INSTALLED, KIT NR 65C28106-1 AND 65C28106-16 PER EO 5302V112, REV A. (M)SDR SWAA031343Bulkhead · crackedDURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED AT BS 178, WL 234 AND LBL 12.0. REPAIRED BULKHEAD WEB PER SRM.SDR EIA2003084Bulkhead · corrodedRIGHT WING GEAR W/W BS 1241 CANTED BULKHEAD WEB AND VERTICAL STIFFENER CORRODED RBL 55-75. REMOVED DAMAGE, NDT AREA, FABRICATED AND INSTALLED REPAIR PER ECRA478-53-143-2.SDR SWAA031331Pressure Panel · crackedDURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESSURE WEB CRACKED AT BS 665, RBL 36. REPAIRED PRESSURE WEB PER SRM.SDR SWAA031321Pressure Panel · crackedDURING SCHEDULED 1/4D CHECK, FOUND NLG W/W CRACKED (2 EA) AT RT UPPER WEB TIRE BRAKE ATTACH HOLES. REPAIRED UPPER WEB PER SWA EA.SDR DL73K030539Strap · buckledFS 1016 PRESSURE BULKHEAD / OUTER CIRCUMFERENTIAL TEAR STRAP / STR5L TO 7L - BUCKLING: THE SUBJECT STRAP WAS FOUND BUCKLED BETWEEN FASTENERS FROM THE BULKHEAD WEB SPLICE AT S-7L TO APPROXIMATELY S-6L. THERE IS NO BUCKLING OR OIL CANNING OF THE BULKHEAD WEB. SDR CALA0300310Pressure Panel · crackedINSPECTION FOUND A .5 INCH CRACK IN MAIN WHEEL WELL PRESSURE DECK AT STA 673, LBL 31. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-60-51, FIGURE 203.SDR AWXA200300718Frame · crackedMCN - MAJOR REPAIR - DURING C-14 CHECK A 2 INCH CRACK WAS FOUND ON BS 178 BULKHEAD LT SIDE FRAME AT AFT SIDE OF CENTER RADIUS WL 207. MAINTENANCE REMOVED LT SIDE FRAME AT BS 178, WL 207; FABRICATED A NEW REPLACEMENT SIDE FRAME, INSTALLED REPAIR PART IAW B737SDR SWAA031309Bulkhead · crackedDURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED AT BS 178, WL 234, LBL 13. REPAIRED BULKHEAD WEB PER SRM.SDR SWAA031299Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND UPPER CHORD CRACKED AT BS 178, WL 233, LBL 25. REMOVED AND REPLACED UPPER CHORD PER SRM.SDR AWXA200300749Web · crackedDURING C-14 CHECK 2 EACH CRACKS WERE FOUND LT WHEEL WELL PRESSURE WEB AT OUTBOARD SIDE OF FORMED CHANNEL BS 664, LBL 32. MAINTENANCE CUTOUT DAMAGE ON LT W/W PRESSURE WEB BS 664, LBL 32; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED SDR AWXA200300769Bulkhead · crackedMCN - MAJOR REPAIR - DURING C-04 CHECK A .1875 INCH CRACK WAS FOUND ON RT BULKHEAD WEB FR 35 AT LOWER MOST OUTBOARD HOLE. MAINTENANCE STOP DRILLED CRACK AND PERFORMED A HFEC INSPECTION TO VERIFY CRACK WAS CONTAINED; FABRICATED REPAIR DOUBLERS AND A BRACKET ASSDR SWAA031271Bulkhead · crackedDURING SCHEDULED C1 CHECK, FOUND BS 1016 BULKHEAD CRACKED AT STR 7L. REPAIRED BULKHEAD PER SRM.SDR QXEA200300693Bulkhead · crackedCKB - FOUND CRACKS IN AFT BULKHEAD WHILE PERFOMING HYDRAULIC FLEX INSTALL ON RIGHT HAND WEB. REPAIRED IAW HOEIZON AIR EO R-53-114.SDR QXEA200300692Bulkhead · crackedCKB - FOUND CRACKS IN AFT BULKHEAD WHILE PERFORMING HYDRAULIC FLEX INSTALL ON THE LEFT HAND WEB. REPAIRED IAW REO 670-53-61-034.SDR UIEA200300035Bulkhead · crackedDURING C-CHECK, FOUND CRACKS AT LT AND RT SIDES OF STATION 140, FORWARD PRESSURE BULKHEAD WEB, WL 205-227 AND WL 250-258. THE REPAIR TRIMS OUT THE CRACKS, HFEC INSPECTS THE TRIM. INSTALLED REPAIR DOUBLERS ON THE AFT SIDE PER REF AND MOD DOUBLERS ON THE FORWASDR SWAA031223Pressure Panel · crackedDURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESS PANEL CRACKED AT BS 664, LBL 36. REPAIRED PRESS WEB PER SWA EA.SDR CALA0300271Pressure Panel · crackedINSPECTION FOUND A 2 INCH CRACK IN PRESSURE DECK WEB AT STA 663.75 IN RT WHEEL WELL JUST O/B OF J-BOX. THE CRACKED AREA WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-60-51, PAGE 214-221.SDR 03FDEA00822Bulkhead · crackedCOMPLY WITH E.A.8-5310-70387. FUSELAGE-MAINFRAME-REPAIR OF STA 1987 BULKHEAD P/N AJC7066-1. CLOSING ACTION ON 05-27-03 ON N/R C00019. COMPLIED WITH E.A.8-5310-70387.SDR P5CA0300882Bulkhead · crackedCRACK FOUND ON 1480 LWR BULKHEAD RT SIDE. REPAIRED PER S/B 53-2390.SDR ARWA20030506Bulkhead · crackedDURING (C) CHECK INSPECTION THE FOLLOWING WAS FOUND; STATION 1766 AFT PRESSURE BULKHEAD, L-3R UUPER EAP WITH 2 INCH CRACK. TRIMMED OUT DAMAGED AREA AND FABRICATED REPAIR PART IAW REPAIR ORDER AROW-031RO-2, PAGE 1 TO 2, DATED 05/01/03 AND REPAIR DRAWING NUMBERSDR SWAA031169Bulkhead · crackedDURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 179.5, WL 177 AT LBL 5.7. REPAIRED VERTICAL BEAM WEB PER SRM.SDR SWAA031168Bulkhead · crackedDURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, WL 234 AT RBL 10.5. REPAIRED BULKHEAD WEB PER SRM.SDR QXEA200300659Bulkhead · crackedCKB - RIGHT HAND PRESSURE BULKHEAD WEB BBL34-41 STRINGER 8-9 CRACKED. REPAIRED IAW CRJ 700 AMM 21-31-00-910-801-401 AND REO 670-53-61-034.SDR QXEA200300658Bulkhead · crackedCKB - LEFT PRESSURE BULKHEAD WEB BL 34-41 STRINGER 8-9 CRACKED. REPAIRED IAW CRJ 700 AMM TASK 21-21-00-710-801 AND REO 670-53-61-034.SDR SWAA031167Bulkhead · crackedDURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CRACKED (2 EA) AT LBL 17.1, BS 179 AT WL 227 AND BS 183 AT WL 231. REPAIRED VERTICAL BEAM WEB PER SRM.SDR SWAA031155Web · crackedDURING SCHEDULED C1 CHECK, FOUND NLG W/W BOTH LT/RT UPPER WEB CRACKED AT ACCESS PANEL CUTOUT TIRE STOP. REPAIRED UPPER WEB PER SWA EA.SDR SWAA031166Pressure Panel · crackedDURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESS WEB CRACKED AT BS 672, RBL 36. REPAIRED PRESS WEB PER SRM.SDR CA030526003Pressure Panel · cracked(CAN) DURING COMPANY SPECIAL FLEET INSPECTION 13 INCH CRACK DISCOVERED IN THE WHEEL WELL UPPER PRESSURE SKIN ALONG AIRCRAFT CENTER LINE AT EDGE OF STRINGER BETWEEN FRAME 29 TO 32. MANUFACTURER CONTACTED. DAMAGE REPAIRED AS PER BAE REPAIR INSTRUCTION HC532H9018SDR SWAA031140Bulkhead · crackedDURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED AT BS 178, WL 213 AND RBL 6.5. REPAIRED BULKHEAD WEB PER SRM.SDR C2XA03TY071Firewall · crackedDURING A SCHEDULED INSPECTION THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE TOP RIGHT HAND MOUNT. MAINTENANCE ACCOMPLISHED A DOUBLER REPAIR IAW EC 5330-01250, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WAS RELEASED FOR SERVICE AT COMPLETION OF INSPECTION.SDR DL73S030476Bulkhead · crackedWHILE ACCOMPLISHING INSPECTIONS OF THE AFT PRESSURE BULKHEAD IAW AD 99-08-23, 2 CRACKS WERE FOUND EMANATING FROM FASTENER HOLES IN THE BULKHEAD AT THE ATTACH AREA. THE CRACKED AREA OF WEB WAS CUTOUT AND REPAIRED WITH AN ALUMINUM DOUBLER IAW SRM AND ER/A 38508SDR SWAA031122Bulkhead · crackedDURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD WEB CRACKED (2 EA) AT BS 178, WL 234, LBL 8.5 AND LBL 9.5. REPAIRED BULKHEAD WEB PER SRM.SDR AWXA200300660Bulkhead · crackedDURING C-17 CHECK A .5 INCH CRACK WAS FOUND ON BS 178 BULKHEAD WEB AT RBL 1.0, WL 192. MAINTENANCE CUT OUT CRACK ON BS 178 BULKHEAD WEB AT RBL 1.0, WL 192 AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR DOUBLER AND FILLER; INSTASDR AWXA200300651Bulkhead · crackedDURING C-17 CHECK A 1 INCH CRACK WAS FOUND ON BS 178 BULKHEAD WEB AT RBL 7, WL 198.5-199.5. MAINTENANCE STOP DRILLED CRACK AND PERFORMED A HFEC INSPECTION TO VERIFY CRACK WAS CONTAINED; FABRICATED A DOUBLER AND 2 EACH FILLERS; INSTALLED REPAIR PARTS IAW SRM 53SDR PCAA0305075Pressure Panel · crackedSYR-LGA FLIGHT 3994. CREW REPORTED GEAR WOULD NOT RETRACT NORMALLY. LT AND RT AMBER DOOR ADVISORY LIGHTS ILLUMINATED AND RED DOOR ADVISORY LIGHT ILLUMINATED WHEN GEAR SELECTED UP. AIRCRAFT DIVERTED TO BGM. MAINTENANCE INSPECTED AIRCRAFT AND FOUND STRUCTURAL DASDR AWXA200300661Bulkhead · crackedLCQ - MAJOR REPAIR - DURING C-17 CHECK A 1.5 INCH CRACK WAS FOUND ON BS 178 BULKHEAD WEB AT RBL 6.5, WL 222-233.5. MAINTENANCE CUT OUT CRACK ON BS 178 BULKHEAD WEB AT RBL 6.5, WL 222-233.5 AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED SDR AWXA200300659Bulkhead · crackedDURING C-17 CHECK A .5 INCH CRACK WAS FOUND ON BS 178 BULKHEAD WEB AT LBL 1.0, WL 192. MAINTENANCE CUT OUT CRACK ON BS 178 BULKHEAD WEB AT LBL 1.0, WL 192 AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR DOUBLER AND FILLER; INSTA
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