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.

SDR SWIA201126292Bulkhead · corrodedFS 280 BULKHEAD LOWER LEFT AND RIGHT WEBS HAVE CORROSION. (C-CHECK) REPAIRED PER REO.Apr 4, 2011 · N611SK · Cndair CL6002C10SDR ASAA1149635Attach Angle · corrodedBULKHEAD ATTACH ANGLE CORRODED AT BS 945 BETWEEN STR 25R AND 26R. REMOVED AND REPLACED ATTACH ANGLE IAW B737 400 SRM 51 40 02.Apr 4, 2011 · N791AS · Boeing 737490SDR ASAA1149579Attach Angle · corrodedBULKHEAD ATTACH ANGLE STA 945 BETWEEN STA 25L 26L CORRODED. REMOVED CORRODED ANGLE. RECEIVED LOCATED TREATED PRIMED TOPCOATED AND INSTALLED NEW ANGLE IAW B737 400 SRM 51 40 02.Apr 4, 2011 · N791AS · Boeing 737490SDR USAA2011040791350Pressure Panel · crackedCLT - C3 - CRACK IN PRESSURE DECK AT BS 663, RBL 39.32. REPAIRED PRESSURE DECK AT BS 663, RBL 39.32 IAW EA 102882.Apr 4, 2011 · N529AU · Boeing 7373B7SDR ASOA201100684Angle · cracked1 EA ANGLE FWD OF FS 280 LWR BULKHEAD RBL 25.00 CRACKED. R & R ANGLE IAW SRM 51-42-06, 51-42-21. MAJOR REPAIR.Apr 4, 2011 · N379CA · Cndair CL6002C10SDR ZZDA2011363Bulkhead · corrodedAFT CARGO FORWARD FACE AFT PRESSURE BULKHEAD, STA 1053, RBL 2, CORROSION. ACCOMPLISHED AFT PRESSURE BULKHEAD DOUBLER REPAIR PER B717 SRM 51-41-05.Apr 4, 2011 · N987AT · Boeing 717200SDR SWAA112434Bulkhead · corrodedDURING SCHEDULED 16Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CORRODED AT BS 1016, BL 0. REPAIRED WEB PER BAC DWG.Apr 4, 2011 · N609SW · Boeing 7373H4SDR 2011FA0000226Bulkhead · crackedDURING INSP IAW AD72-07-09, DATED 10/17/1974, AND SL SE72-3, THE AFT BULKHEAD WAS FOUND CRACKED IN BOTH RUDDER CABLE CUTOUTS. UPON REMOVAL OF AFT BULKHEAD THE LT AND RT STABILIZER ATTACH BRACKETS, PN 0712629-3 AND PN 0712629-4 WERE ALSO FOUND CRACKED.Apr 4, 2011 · N982SF · Cessna P206ESDR VNAA2011040500003Bulkhead · crackedDURING SCHEDULED MAINTENANCE A CRACK WAS FOUND ON THE FS 280 BULKHEAD WEB. REPAIRS WERE MADE USING THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.Apr 3, 2011 · N259PS · Cndair CL6002B19SDR GUUA93653040311ABulkhead · crackedDURING SCHEDULED ROUTINE OXYGEN INSP DISCOVERED A CRACK ON INBD LT PRESSURE BULKHEAD AT FS 84.00. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER AT LT PRESSURE BULKHEAD F/A 84.00.Apr 3, 2011 · N81536 · Beech 1900DSDR COMA2011040490004Bulkhead · corrodedFS 280 RT LOWER BULKHEAD WEB AT CABIN FLOOR LINE CORRODED. REMOVED LOWER SECTION OF FS 280 RT BULKHEAD WEB, FABRICATED AND INSTALLED NEW SECTION IAW SRM 53-11-10-201-003-A01.Apr 3, 2011 · N678CA · Cndair CL6002D24SDR COMA2011040490003Bulkhead · corrodedFS 280 LT LOWER BULKHEAD WEB AT CABIN FLOOR LINE CORRODED. REMOVED LOWER SECTION OF FS 280 LT BULKHEAD WEB, FABRICATED AND INSTALLED NEW SECTION IAW SRM 53-11-10-201-003-A01.Apr 3, 2011 · N678CA · Cndair CL6002D24SDR SWIA201126296Bulkhead · crackedFS 559.0 PRESSURE BULKHEAD CRACKED AT LEFT SIDE. (C-CHECK) REPAIRED PER REO.Apr 2, 2011 · N944SW · Cndair CL6002B19SDR REXA201100211Bulkhead · chafedINTERNAL CARGO COMPARTMENT AT FS 621 PRESSURE BULKHEAD AT WL 103.5 BETWEEN LBL 27 AND RBL 36, SKIN IS CHAFED AT NINE LOCATIONS APPROX 1.00"L X 0.100"W X 0.005"D. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.Apr 2, 2011 · N827AY · Cndair CL6002B19SDR REXA201100210Bulkhead · chafedINTERNAL CARGO COMPARTMENT AT FS 621 PRESSURE BULKHEAD AT WL 86.75 ON RBL 27, SKIN IS CHAFED APPROX 1.00"L X 0.100"W X 0.005"D. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.Apr 2, 2011 · N827AY · Cndair CL6002B19SDR REXA201100199Rivet · damagedINTERNAL CARGO COMPARTMENT AT FS 621 PRESSURE BULKHEAD AT WL 86.5 BETWEEN RBL 18 AND RBL 36 HAS TWO DAMAGED RIVETS. RIVETS REMOVED AND REPLACED IAW SRM 51-42-06.Apr 2, 2011 · N827AY · Cndair CL6002B19SDR REXA201100198Bulkhead · damagedINTERNAL CARGO COMPARTMENT AT FS 621 PRESSURE BULKHEAD AT WL 94.5 ON LBL 9 HAS BROKEN ISOLATOR NUT PLATE. REPAIRED IAW SRM 51-42-06.Apr 2, 2011 · N827AY · Cndair CL6002B19SDR REXA201100197Bulkhead · damagedINTERNAL CARGO COMPARTMENT AT FS 621 PRESSURE BULKHEAD AT WL 86.5 BETWEEN LBL 9 AND LBL 36 HAS FOUR DAMAGED RIVETS. RIVETS REMOVED AND REPLACED IAW SRM 51-42-06.Apr 2, 2011 · N827AY · Cndair CL6002B19SDR A6WA201140359Bulkhead · gougedREAR PRESSURE BULKHEAD FWD SIDE HAS SEVERAL GOUGES FROM FASTENER STRANDS. REPAIRED GOUGED AREAS ON FWD SIDE OF REAR PRESSURE BULKHEAD IAW REO 601R-53-61-2155.Apr 1, 2011 · N459AW · Cndair CL6002B19SDR ASAA1149505Bulkhead · corrodedWHILE CLEANING FORWARD SIDE OF AFT PRESSURE BULKHEAD FOR THE RESTORATION CARD FOUND CORROSION AROUND THE RIVETS JUST TO THE LEFT OF BL 0. REMOVED CORROSION, CUTOUT LOWER SKIN FOR WEB ACCESS REMOVED STRINGER END FITTING. FABRICATED SKIN DOUBLER AND WEB DOUBLEApr 1, 2011 · N709AS · Boeing 737490SDR DALA1127509858Fitting · crackedAFT SIDE OF BULKHEAD STA 69, RBL 15 TO WHEEL WELL PRESSURE PANEL VERTICAL FITTING CRACKED IN RADIUS AND LWR ATTACH BOLT HOLE TO EDGE OF FITTING, VIEWED THRU ACCESS 4201A FWD OF RUDDER PEDALS REMOVED IAW SRM 51-30-5, PG 29, FABRICATED NOSE GEAR BEAM ATTACH FITApr 1, 2011 · N767NC · Doug DC951SDR REXA201100195Bulkhead · crackedFOUND FS 559 SEMI PRESSURE BULKHEAD HAS INDICATION NOTED AT RT WEB RBL 18 AND LBL 18 CAP ANGLE, ALL GREATER THAN 50 PERCENT SCREEN HEIGHT, FAILED NDT INSPECTION. REPAIR IAW BOMBARIDER REO 601R-53-41-260 REV E, BOMBARDIER REO 601R-53-41-609 REV B DEVIATION E, Apr 1, 2011 · N8543F · Cndair CL6002B19SDR ASAA1149504Stiffener · corrodedCORROSION ON BL 0 STIFFENER AT BS 1016 (AFT PRESSURE BULKHEAD). REMOVED CORRODED STIFFENER AND INSTALLED REPAIR PARTS IAW ASA EA 400 53EA 5300.Mar 31, 2011 · N709AS · Boeing 737490SDR DALA1124280942Angle · corrodedDURING PSV CHECK IN MSP, NOTED CORROSION COMMON TO THE AFT PRESSURE BULKHEAD ANGLE LOCATED S-28L TO S-28R. REPAIRED PER ERA 491320-14.Mar 31, 2011 · N942DL · Doug MD88SDR SWIA201126555Bulkhead · crackedFS 621 BULKHEAD, FORWARD FACE CRACKED AT UPPER CARGO DOOR TRACK FITTING. (C-CHECK) REPAIRED PER REO.Mar 30, 2011 · N652BR · Cndair CL6002B19SDR A6WA201140275Pressure Blkhd · crackedFWD PRESSURE BULKHEAD IS CRACKED AROUND THE PARKING BRAKE CABLE. REPAIRED FS 202.75 BULKHEAD AT LBL 23.71, LW 69.684 IAW REO 601R-53-11-563.Mar 30, 2011 · N417AW · Cndair CL6002B19SDR DALA1123199878Bulkhead · crackedFUSELAGE STA 37 BLKHD LT CRACKED AT LOWER GUIDE PIN. FAB FILLER DOUBLER USING A2469 ZETEC PER NDT SPM 06-10-01 FOUND NO CRACKS NOTED HEAT TREATED NEW DOUBLER ON PEMCO TRAVELER 2451N01760 FAB TAPERED SHIMS IAW DC9 SRM 51-10-4 SHIM IAW DC9 RECEIVED SPLICE ON PEMar 30, 2011 · N787NC · Doug DC951SDR REXA201100212Bulkhead · crackedCRACK INDICATION AT LBL 18 CRACK IS 1.0625 INCH LONG. CRACK INDICATION AT RBL 18 CRACK IS .8125 INCH LONG. CRACK INDICATION AT RBL 9 OUTBOARD POST CRACK IS .5 INCH LONG. CRACK INDICATION AT RBL 9 INBOARD POST CRACK IS .625 INCH LONG. REPAIRED IAW BOMBARDIEMar 29, 2011 · N8541D · Cndair CL6002B19SDR ASOA201100657Bulkhead · crackedFS 559 BULKHEAD FAILS NDT WITH AN INDICATION IN WEB AT RBL 18 AND AN INDICATION IN CAP ANGLE UNDER RBL 9 POST, BOTH GREATER THAN 50 PERCENT SCREEN HEIGHT. C/W EC/TC REO 601R-53-41-260 AND REO 601R-53-41-260, REV E. C/W EC/TC REO 601R-53-41-609 02 AND MET ALLMar 29, 2011 · N914EV · Cndair CL6002B19SDR ASOA201100656Bulkhead · crackedFS 559, BULKHEAD FAILS NDT WITH AN INDICATION IN WEB AT RBL 18 AND AN INDICATION IN CAP ANGLE UNDER RBL 9 POST. BOTH GREATER THAN 50 PERCENT SCREEN HEIGHT. REMOVED & DISCARDED RBL 9 POST, RBL 18 POST AND DOUBLER 601R32026-183 IAW REO 601R-53-41-260, REV D, SHMar 29, 2011 · N914EV · Cndair CL6002B19SDR ASOA201100655Bulkhead · crackedFS 559 BULKHEAD FAILS NDT WITH AN INDICATION IN WEB AT RBL 18 AND AN INDICATION IN CLIP ANGLE UNDER RBL 9 POST. BOTH GREATER THAN 50 PERCENT SCREEN HEIGHT. INSTALLED LT CAP ANGLE AND SPLICE IAW REO 601R-53-41-260. INSTALLED REPAIR PARTS ON LT 559 IAW REO Mar 29, 2011 · N914EV · Cndair CL6002B19SDR SWIA201125924Bulkhead · crackedFS 559 BULKHEAD CRACKED AT RIGHT SIDE. (C-CHECK) REPAIR PER REO.Mar 28, 2011 · N945SW · Cndair CL6002B19SDR SWIA201125907Bulkhead · crackedFS 202 BULKHEAD CRACKED AT BRAKE CABLE HOLE. (C-CHECK) REPAIR PER REO.Mar 28, 2011 · N945SW · Cndair CL6002B19SDR SWAA112294Bulkhead · crackedDURING SCHEDULED OTS CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, RBL 5.7. REPAIRED WEB PER EA.Mar 28, 2011 · N502SW · Boeing 7375H4SDR SWAA112234Bulkhead · crackedDURING SCHEDULED 22Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, BL 0. REPAIRED WEB PER EA.Mar 27, 2011 · N347SW · Boeing 7373H4SDR SWAA112232Pressure Panel · crackedDURING SCHEDULED 6Y CHECK, FOUND VERTICAL PRESSURE WEB CRACKED AT BS 663, RBL 43. REPAIRED WEB PER EA.Mar 27, 2011 · N211WN · Boeing 7377H4SDR SWAA112220Bulkhead · crackedDURING SCHEDULED 16Y CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 183, RBL 5.7. REMOVED AND REPLACED WEB PER EA.Mar 27, 2011 · N612SW · Boeing 7373H4SDR SWAA112330Bulkhead · crackedDURING SCHEDULED 26Y CHECK, FOUND RT AFT BULKHEAD WEB CRACKED AT BS 663.75. REPAIRED WEB PER EA.Mar 26, 2011 · N694SW · Boeing 7373T5SDR SWIA201126295Bulkhead · crackedFS 621 BULKHEAD FORWARD SIDE CRACKED AT WEB NEAR AFT CARGO TRACK (UPPER). (C-CHECK) REPAIRED PER REO.Mar 25, 2011 · N945SW · Cndair CL6002B19SDR DALA1124769871Attach Angle · crackedMAIN CABIN STA 1167 APB RT BOTTOM STIFFENER O/B ATTACH ANGLE CRACKED. CPCP TASK 58-53310. REMOVED & REPLACED ATTACH ANGLE ON APB RT O/B BOTTOM STIFFENER IAW DC9 SRM 51-30-2 & 51-30-5 PN9915558U242 & RP DC9-A-53-10-25-801-663A-A.Mar 25, 2011 · N780NC · Doug DC951SDR DALA1237610942Frame · damagedAFT PRESSURE BULKHEAD LOWER FRAME DAMAGED REPAIRED IAW PER SRM 53-03 FIG 37 AND ER/A 09-086680-12 REV EOPN 0603.Mar 24, 2011 · N942DL · Doug MD88SDR KO0R2011FA000285Bulkhead · corrodedCORROSION ON AFT SIDE OF THE 1480 BULKHEAD WEB, AFT OF OTBD TRUNNION FITTING WL120.Mar 24, 2011 · N706BL · Boeing 747251BSDR DALA1124829871Fitting · crackedNRC 1B/13 RT NLG WHEEL WELL STA 69 LBL-30 PRESSURE DECK TO WEB O/B FITTING CRACKED. REMOVED IEA FITTING IAW DC9 SRM 51-30-1, 51-30-5. INSTALLED NEW FITTING AT PRESSURE DECK TO WEB STA 69 LBL-30 IAW DC9 SRM 51-10-4, 51-10-3, 51-30-1, 51-30-5.Mar 24, 2011 · N780NC · Doug DC951SDR DALA1124819871Fitting · crackedNRC 1B/14 RT NLG WHEEL WELL STA 69 LBL-30 PRESSURE WEB I/B FITTING CRACKED. REMOVED IEA FITTING IAW DC9 SRM 51-30-1, 51-30-5, INSTALLED NEW FITTING AT PRESSURE DECK TO WEB I/B STA 69 LBL-30 IAW DC9 SRM 51-10-4, 51-10-3, 51-30-1, 51-30-5.Mar 24, 2011 · N780NC · Doug DC951SDR KCSA111086Bulkhead · corrodedSTA 1480 BULKHEAD WEB HAS CORROSION AT THE O/B SIDE OF LT MAIN BODY LANDING GEAR TRUNNION ATTACH AREA WL 136, LBL 65.Mar 24, 2011 · N708CK · Boeing 747212BSDR DALA1125029871Support · crackedAFT CARGO STA 851 CENTER VERTICAL BULKHEAD SUPPORT CRACKED APPROX 4 INCHES ON BOTTOM. REMOVED SUPPORT ANGLE AND PLATE IAW DC9 SRM 51-30-2. STOP DRILL IAW DC9 SRM 53-01 NO CRACK NOTED IAW DC9 NDT SPM 06-10-01-00. A2700 RECEIVED MAT .025 7075-T6 FAB DOUBLER IAMar 23, 2011 · N780NC · Doug DC951SDR ASOA201100560Isolator · brokenISOLATOR BROKEN ON FWD FACE OF 621 BULKHEAD APPROX 20" ABOVE FLOOR AT LBL 9 AND RBL 9. R & R ISOLATOR FWD FACE 621 BULKHEAD LBL 9 AND RBL 9 IAW SRM 51-42-06. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW SOP 5702.Mar 23, 2011 · N881AS · Cndair CL6002B19SDR REXA201100193Bulkhead · crackedFS 559 SEMI-PRESSUE BULKHEAD FOUND CRACKED IN THREE AREAS: RT WEB RBL 18, LT WEB LBL 9 AND CAP ANGLE AT LBL 18. REPAIRED IAW BOMBARDIER REOS GREO 601R-53-41-260 REV E AND 601R-53-41-609 REV B AND BOMBARDIER SERVICE CORPORATION EO 601R-53-20973.Mar 23, 2011 · N8718E · Cndair CL6002B19SDR SWAA112184Bulkhead · crackedDURING SCHEDULED 22Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, BL 0. REPAIRED WEB PER EA.Mar 22, 2011 · N347SW · Boeing 7373H4SDR ASOA201100538Bulkhead · crackedFOUND REAR PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL ATTACHMENT FITTING HAS INDICATIONS NOTED APPROX .2" IN LENGTH 50 PERCENT FSH FAILED NDT INSPECTION. REPAIR IAW EC/TC REO 601R-53-61-1230 HAS BEEN COMPLETE AND THE REPAIR C/W THE REQUIREMENTS OF EC/TCMar 22, 2011 · N914EV · Cndair CL6002B19
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