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 DL72E971878Blkhd Stiffener · crackedAN EXISTING REPAIR WAS FOUND ON THE FS 1183 BULKHEAD VERTICAL STIFFENER AT RBL 8. THIS REPAIR WAS REMOVED AND A 2.5 CRACK WAS DISCOVERED IN THE IB FLANGE-TO-WEB RADIUS. S/B 727-53-0175 WHICH IS REQUIRED BY AD 90-06-09, CONTAINS INSPECTION, MODIFICATION, AND SDR 9717289954Bulkhead · crackedDURING L-CHECK, FOUND CRACKS ON THE NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE PANEL AT THE INBAORD AND OUTBOARD VERTICAL SUPPORTS FS 108. REPAIRED PER EA 99-151672.SDR UPS97824446Bulkhead Angle · crackedINSPECTION TYPE-C, FOUND RT MLG W/W UPPER BULKHEAD ATTACH ANGLE CRACKED FS 861, BL 47 RT. REMOVED CRACKED ATTACH ANGLE, FABRICATED NEW ATTACH ANGLE, DRILLED, TREATED, PRIME AND INSTALLED IAW DC8 SRM 53-1-0, 51-1-21, 51-1-8, 51-1-20D.SDR 9718339936Jamb · crackedDURING M CHECK, FOUND CRACK ON THE 5910130-9 CHANNEL AT THE LEFT AFT PRESSURE BULKHEAD DOOR JAMB. REPAIRED PER EA 99-151653.SDR SWAA970804Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED AT LBL 8.75 TO 14.0, AT RBL 9.25 TO 14.0, AT LBL 6.7, AT LBL 12 TO 12.5, AND AT LBL 11.0 TO 13.0. REPAIRED PER BOEING SRM.SDR 97ZZZX4518Bulkhead · crackedNOSE WHEELWELL SUBSTRUCTURE - CRACKS, LOOSE AND SHEARED RIVETS WERE FOUND ON BOTH SIDES OF NOSE GEAR WHEELWELL SUBSTRUCTURE. BULKHEAD, P/N 5013020-14, HAD CRACKED BUTT END, RIVETS SHEARED WHERE T-ANGLES, P/N 5213028-6 AND P/N 5013022-5 ARE RIVETED GUSSETS, P/SDR 97FDEA00615Bulkhead Doubler · corrodedNR 0851 024 WHILE WORKING NR 0748, DISCOVERED CORROSION ON FWD SIDE OF WHEEL WELL BULKHEAD RT RING DOUBLER, AT BS 873, RBL 58, WL 183. REMOVED, FABRICATED AND REPLACED RT RING DOUBLER AT BS 870, RBL 58, WL 183 IAW FED-EX DRAWING 69-14467.SDR 97FDEA00614Bulkhead Web · corrodedCORROSION (C57-174-01) ON BS 870 BULKHEAD WEB, RBL 70 - LBL 70, WL 178 TO 138. *S/D* BLENDED, REMOVED CORROSION ON BS 870 BULKHEAD WEB, FOUND TO BE OUT OF LIMITS PER FED SRM 53-10-1. REMOVED AND REPLACED BS 870 BULKHEAD WEB PER FED SRM 51-10-1.SDR 97FDEA00613Bulkhead Doubler · corrodedNR 0847 026 WHILE WORKING NR 0748, DISCOVERED CORROSION ON FWD SIDE OF WHEEL WELL BULKHEAD, LEFT RING DOUBLER AT 873, LBL 58, WL 183. REMOVED, FABRICATED AND REPLACED LEFT RING DOUBLER AT BS 870, LBL 58, WL 183 IAW FED-EX DRAWING 69-14467.SDR SWAA970818Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKS AT LBL 7, LBL 6.7, AND RBL 4.7 AND 6.7. REPAIRED PER BOEING SRM.SDR DLL10971747Pressure Deck · crackedTHE FUSELAGE NOSE LANDING GEAR HORIZONTAL PRESSURE DECK AFT PANEL AT LBL 55 JUST FORWARD OF FS 445 WAS PREVIOUSLY REPAIRED FOR CRACKS PER THE SRM. UPON INSPECTION, ADDITIONAL CRACKS WERE FOUND EXTENDING FROM FS 430 TO 447 AT LBL 55. IN ADDITION, UPON REPAIR SDR TSAA9753214Bulkhead Web · corrodedDURING HEAVY MAINTENANCE VISIT, NOTED CORROSION AT BS 1088 BULKHEAD WEB APU INLET AREA. REPAIRED PER ECO 1980R9 OPTION VIII. AIRCRAFT RETURNED T SERVICE. (M)SDR P5CA9701459Bulkhead Chord · crackedFIVE CRACKS IN THE NOSE LANDING GEAR CANTED BULKHEAD OUTER CHORDS. PERFORMED PERMANENT REPAIR OF THE BULKHEAD CHORDS PER MAE ENGINEERING AUTHORIZATION 47-5316-15-A0292.SDR ABXA9701449Blkhd Fitting · crackedDURING C-CHECK, FOUND AFT PRESSURE BULKHEAD FITTING BETWEEN FIRST AND SECOND RADIAL CRACKED. *S/D* REPLACED FITTING IAW DC9 SRM 51-30-2 AND 51-30-5.SDR ABXA9701424Blkhead Angle · crackedDURING D-CHECK, FOUND THE AFT PRESSURE BULKHEAD HORIZONTAL BEAM ATTACH ANGLE IS CRACKED AT LONGERON 15L. *S/D* REPLACED ATTACH ANGLE IAW DC9 SB 53-166.SDR USAA970269Bulkhead · crackedINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 3 CRACKS 1.5 INCH, .75 INCH AND 1.5 INCH. THE 1.5 INCH CRACK RBL 4.75 WL 201, .75 INCH CRACK LBL 4.75 WL 98, 1.5 INCH CRACK RBL 4.75 WL 198 178 BULKHEAD. INSTALLED DOUBLER AND STOP DRILLED PER TR 53-10-11. (M)SDR P5CA9701444Blkhd Shroud · delaminatedAPU DUCT SHROUD AT BS 2360 AFT PRESS BULKHEAD IS DELAMINATED. REPAIRED PER BOEING SRM 51-40-09.SDR ABXA9701445Blkhd Stiffener · crackedDURING C-CHECK, FOUND CRACK IN P-DOME STIFFENER AT LONGERON 12R. *S/D* REPAIRED IAW SRM DWG KO5159.SDR ABXA9701444Blkhd Skin · corrodedDURING C-CHECK, FOUND BULGE IN P-DOME SKIN LONGERON 16R. *S/D* REPAIRED IAW DC9 SRM 53-01.SDR ABXA9701427Bulkhead Angle · crackedDURING D-CHECK, FOUND THE AFT PRESS BULKHEAD ATTACH ANGLE AT LONGERON 14R CRACKED. *S/D* REPLACED ATTACH ANGLE IAW DC9 SB 53-166.SDR ABXA9701426Blkhd Angle · crackedDURING D-CHECK, FOUND THE AFT PRESS BULKHEAD ATTACH ANGLE BETWEEN LONGERON 15R AND 16R CRACKED. *S/D* REPLACED ATTACH ANGLE IAW DC9 SB 53-166.SDR SWAA970773Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED AT LBL 0.7 AND RBL 0.5. REPAIRED PER TRAMCO EWO 97-0623.SDR SWAA970755Bulkhead · corrodedDURING SCHEDULED D-CHECK, FOUND PRESSURE BULKHEAD BS 1033 CORRODED AT ATTACH SUPPORT ANGLE AT RBL 11. REPLACED PER BOEING SRM.SDR ABXA9701423Blkhead Angle · crackedDURING D-CHECK, FOUND THE AFT PRESSURE BULKHEAD HORIZONTAL BEAM ATTACH ANGLE IS CRACKED AT LONGERON 14L. *S/D* REPLACED UPPER ATTACH ANGLE AND REPAIRED LOWER ANGLE IAW DC9 SB 53-166.SDR ABXA9701422Blkhead Angle · crackedDURING D-CHECK, FOUND THE AFT PRESSURE BULKHEAD HORIZONTAL BEAM ATTACH ANGLE IS CRACKED AT LONGERON 12L. *S/D* REPLACED ATTACH ANGLE IAW DC9 SB 53-166.SDR ABXA9701420Blkhd Shear Tie · crackedDURING D-CHECK, FOUND THE LT PYLON BULKHEAD STA 1042 SHEAR TIE CRACKED BELOW LONGERON 14L. *S/D* REPLACED SHEAR TIE IAW DC9 SRM 53-02.SDR ABXA9701413Blkhd Stiffener · crackedDURING C-CHECK, FOUND THE AFT PRESSURE BULKHEAD LT UPPER NR 1 RADIAL INBOARD CORNER CRACKED. REPLACED RADIAL STIFFENER IAW DC-9 SRM.SDR ABXA9701410Bulkhead Frame · crackedDURING C-CHECK, FOUND THE AFT PRESSURE BULKHEAD DOOR JAMB UPPER DOOR FRAME CRACKED IN TWO PLACES. REPLACED FRAME IAW DC-9 SRM 51-30-2 AND 51-30-5.SDR DL72S971686Blkhd Stiffener · crackedA CRACK WAS FOUND IN THE VERTICAL STIFFENERS AT BOTH RBL AND LBL 36.83 ON THE FORWARD SIDE OF THE 1183 BULKHEAD. THE CRACKS ARE APPROXIMATELY .5 LONG AND ARE LOCATED AT WL 240. THE BEAM WILL BE REPAIRED PER RELEVANT OPERATIONS OF EO 4-59821-3.SDR SWAA970737Bulkhead · crackedDURING D-CHECK, FOUND BS 178 BULKHEAD CRACKED AT RBL 8.7 TO 9.7. REPAIRED PER BOEING SRM.SDR AU971461Web · cracked(AUS) FORWARD PRESSURE BULKHEAD CRACKED IN TWO PLACES:- 1. WEB AT HORIZONTAL BEAM 7 LOCATED OUTBOARD OF VERTICAL BEAM BL325L 2. WEB AT HORIZONTAL BEAM 8 LOCATED OUTBOARD OF VERTICAL BEAM BL325L FOUND DURING VISUAL INSPECTION IAW ER F28-53-10-20G.SDR 97ZZZX3810Bulkhead · crackedINSPECTION FOUND TAIL CONE BULKHEAD AT BS 230.187 CRACKED. REPLACED WITH P/N 1212130-2.SDR QXEA9700705Bulkhead · dentedPDX - REAR PRESSURE BULKHEAD HAS A DENT WITH A PREVIOUS REPAIR. REPAIRED IAW SRM 53-02-18 FIGURE 3.SDR CKSA97482Bulkhead Web · crackedDURING ROUTINE CPCP CHECK INSPECTION, FOUND 0.5 CRACK AT FS 740 NR 2 FUEL TANK CENTER SECTION BULKHEAD WEB LOWER SECTION AT LBL 48. INSTALLED DOUBLER REPAIR IAW EA B2-57-008 DTD 12 AUG 97 AND IAW SKETCH NO AIA/E/2608 REV A DTD 11 AUG 97 IAW FAA FORM 8110-3 DTSDR SWAA970718Bulkhead Web · crackedDURING SCHEDULED D CHECK, FOUND BS 178 WEB CRACKED AT WL 212 TO 212.5, WL 201 TO 202, 197.5 TO 199, 209.75 TO 210.25, 211.75 TO 213, 200.25 TO 201.25, 198.75 TO 199.25. REPAIRED PER BOEING SRM.SDR IH971355008Bulkhead Web · corrodedFUSELAGE, GROUND LUG HAS EXFOLIATION CORROSION, CANTED BULKHEAD FS 1463 LONGERON 6L LBL 7.0. ACCOMPLISHED MODIFIED VERSION OF STANDARD WEB REPAIR PER DC-9 SRM 53-01 FIGURE 4 SHEET 3, BY TRIMMING OUT DAMAGED AREA, FABRICATION AND INSTALLATION OF .125 7075-T6 DSDR CA970822003Bulkhead · cracked(CAN) DURING 100 HOUR INSPECTION CRACKS WERE FOUND AT FUSELAGE STATION 228 ON THE BULKHEAD, ATTACHED TO THE VERTICAL STABILIZER SPAR. EMPENNAGE REMOVED AND BULKHEAD WAS REPLACED. TOTAL TIME ACCUMULATED SINCE LAST ANNUAL WAS 65 HOURS. NO REPORTS OF ROUGH WATER SDR ABXA9701402Bulkhead Skin · corrodedDURING C-CHECK, FOUND LEVEL 2 CORROSION AT PRESSURE BULKHEAD STA 604. SKIN BULGING AND RIVETS SHEARED. REMOVED CORROSION AND TREATED AREA IAW 51-10-3. REPLACED FOUR FINGER DOUBLERS P/N 5914865-9-11-17-18 IAW DWG 5914865 AND DC-9 SRM 51-30-2 AND 51-30-5.SDR CALA9701228Bulkhead · buckledINSPECTION FOUND TAIL CONE BULKHEAD AT FS 2163, STRINGER 51L BUCKLED. THE BUCKLED AREA WAS REMOVED AND A REPAIR WAS INSTALLED USING DOUBLER AND FILLER IAW SRM 53-00-1 FIGURE 4 SHEET 2.SDR TWAA9791001Bulkhead 'T' Cap · crackedSTL - PRESSURE BULKHEAD 'T' CAP CRACKED 2.5 INCHES AT STATION 1167 L-14. REPLACED 'T' CAP PER SRM 53-03. (M)SDR AALA971521Bulkhead Support · corrodedTUL - NR 2 GALLEY SUPPORT CORRODED AT AFT PRESSURE BULKHEAD T-ANGLE INTERFACE. REPAIRED NR 2 GALLEY SUPPORT PER ESO 41000, CHAPTER 53, THEN REINSTALLED ON AIRCRAFT. TST: 22,212.44 HOURS. CYCLES, 3,511. (X)SDR QXEA9700723Bulkhead Beam · crackedPDX- FORWARD PRESSURE BULKHEAD IS CRACKED AT THE HORIZONTAL BEAM 7 ON THE PILOTS SIDE. FABRICATED AND INSTALLED DOUBLER REPAIR IAW FOKKER SRM 53-02-18 FIG 14.SDR MWEA97723Former · damagedDURING D CHECK, FOUND UNACCEPT AFT PRESS BULK HORIZ FORMERS LT SIDE STA Z14,24,34,48 AND INBD ATTACH ANGLES.SDR MWEA97722Bulkhead · damagedDURING D CHECK, FOUND AFT PRESS BULKHEAD LT AND RT SIDE DAMAGED BEYOND REPAIR. MAINTENANCE REPLACED IAW DAC DWG J060088.SDR QXEA9700734Bulkhead Rib · crackedPDX- VERTICAL RIB ON AFT PRESSURE BULKHEAD BELOW THE FLOOR ON THE FORWARD SIDE HAS CRACKS AROUND THE LOWER RIVET HEADS. REMOVED VERTICAL RIB, FABRICATED NEW BRACKET AND INSTALLED IAW FOKKER SRM 51-31-01 AND 51-30-02.SDR QXEA9700733Blkhd Doubler · crackedPDX- REPAIR DOUBLER HAS A CRACK THROUGH THE HI- LOK ON THE NR 2 BEAM OF THE REAR PRESSURE BULKHEAD BETWEEN BL 425L AND BL 1050L AT STRINGER NR 10 CONNECTION ANGLE. REMOVED DOUBLER, FABRICATED AND INSTALLED NEW DOUBLER IAW FOKKER SRM 51-11-4 AND 51-31-01.SDR SWAA970691Bulkhead · crackedDURING D CHECK, FOUND BS 178 BULKHEAD CRACK INDICATION AT LBL7.7 TO LBL 8.7, WL 219. REPAIRED PER TRAMCO EWO 97-0486.SDR SWAA970690Bulkhead · crackedDURING D CHECK, FOUND BS 178 BULKHEAD CRACK INDICATION AT RBL6.7, WL 212.5-213. REPAIRED PER TRAMCO EWO 97-0486.SDR SWAA970689Bulkhead · crackedDURING D CHECK, FOUND BS 178 BULKHEAD CRACK INDICATION AT LBL4.7, WL 198-198.5. REPAIRED PER BOEING SRM.SDR SWAA970688Bulkhead · crackedDURING D CHECK, FOUND BS 178 BULKHEAD CRACK INDICATION AT RBL 1, WL 187.5-188.5. REPAIRED PER TRAMCO EWO 97-0487.
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