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 SWAA070909Stiffener · crackedDURING SCHEDULED 20Y CHECK, FOUND BULKHEAD STIFFENER CRACKED AT BS 1016, RBL 17, WL 209. REPAIRED STIFFENER PER SRM.SDR CALA0700067Stiffener · corrodedINSPECTION FOUND TWO CHANNEL STIFFENERS CORRODED ON FORWARD FACE OF APB LOWER SECTION. THE STIFFENERS WERE REMOVED AND NEW SECTIONS WERE SPLICED IN IAW BOEING DRAWING 65C28106.SDR AWXA200700327Pressure Panel · crackedMCN - FOUND LEFT WHEEL WELL CEILING PRESSURE WEB CRACKED, BS 664 - BS 675, LBL 30 - LBL 35, WL 208. REPAIRED LEFT WHEEL WELL CEILING PRESSURE WEB, BS 664 - BS 675, LBL 30 - LBL 35, WL 208 IAW B737-300 SRM 53-60-51-2R4.SDR WRNA200700032Bulkhead · dentedDURING C-CHECK, A SMALL DENT WAS FOUND IN THE AFT PRESSURE BULKHEAD AT STA 2360 APPROX WL 200, LBL 30. REMOVED DAMAGED SECTION OF BULKHEAD WEB, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-10-04 FIG 9, SRM 51-10-01 AND AMM 51-21-00.SDR DHL2007802539Bulkhead · corrodedFWD ACCY COMPT FWD PRESSURE BULKHEAD CAP SHOWS CORROSION AT STA 8.000 L-29R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 01-30-07, DWG NR ACG2-53-110 REV IR DATED 01-26-07. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-1-20D. CUT OUT DAMAGEDSDR UPS07849211Bulkhead · crackedINSPECTION TYPE:C3 AFT PRESSURE BULKHEAD CRACKED AT STA 1766 LBL 24 L10L AREA. CUT OUT DAMAGED AREA AT AFT PRESSURE BULKHEAD STA 1766 LBL 24 L10L IAW SRM 53-2-5 FIG 14A. FABRICATED AND INSTALLED FINGER DOUBLER, FILLER AND REPAIR DOUBLER AT AFT PRESSURE BULKSDR SWAA070741Frame · corrodedDURING SCHEDULED OTS CHECK, FOUND BULKHEAD FRAME CORRODED AT BS 1016, BL 0. REPAIRED BULKHEAD FRAME PER SRM.SDR TRAX200700207Intercostal · crackedCRACK THRU 2 FASTENERS ON AFT PRESS BULKHEAD INTERCOSTAL AT FS 623.00 LBL 51.5 STR 13L VERT FANGE OF INTERCOSTAL REQ'S CRACK LENGTH VERIFICATION. SERVICE BULLETIN 601R-53-048, FUSELAGE GENERAL VISUAL INSPECTION OF THE INTERCOSTAL MEMBERS AT FS 621/FS625.3 INSDR DL757070557Bulkhead · gougedTHE AFT PRESSURE BULKHEAD WAS DAMAGED FROM A TAIL STRIKE. THE DAMAGED SECTION OF BULKHEAD CHORD WAS CUT AWAY AND A NEW SECTION WAS FABRICATED AND INSTALLED.SDR SWAA070592Stiffener · crackedDURING SCHEDULED 22Y CHECK, FOUND BULKHEAD VERTICAL STIFFENER CRACKED AT BS 178, LBL 5.7, WL 184. REPAIRED STIFFENER PER SRM.SDR 07FDEA00281Bulkhead · damagedTOOLING MARKS FOUND ON AFT PRESSURE BULKHEAD AT ME15, C80/82. REPAIR WAS PERFORMED IAW RAS/DAHAM/4021516/2006 ISS. A (BLEND OUT, FASTENER REPLACEMENT), APPROVED BY EA 6-5319-103386.SDR SWAA070550Bulkhead · crackedDURING SCHEDULED 22Y CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, RBL 9 TO RBL 13. REPAIRED BULKHEAD PER SRM.SDR TRAX200700143Bulkhead · crackedRIGHT & LEFT 280 BULKHEAD WEBS CRACKED. REMOVED AND REPLACED LT AND RT 280 BULKHEAD WEBS IAW IS 670531100026 AND SRM 51-40-11 AND REO 670-53-11-052.SDR TRAX200700142Bulkhead · crackedSTA 280 BULKHEAD WEB CRACKED AFT SIDE JUST OUTBOARD OF RBL 9 (MARKED).SDR SWAA070522Bulkhead · crackedDURING SCHEDULED 20Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, 5 O'CLOCK POSITION. REPAIRED WEB PER SRM.SDR SWAA070528Bulkhead · crackedDURING SCHEDULED 22Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, 2 O'CLOCK POSITION. REPAIRED WEB PER SRM.SDR SWAA070529Bulkhead · crackedDURING SCHEDULED 22Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, 4 O'CLOCK POSITION. REPAIRED WEB PER SRM.SDR TRAX200700133Bulkhead · crackedAFT PRESSURE BULKHEAD IS CRACKED ADJACENT TO THE CARGO COMPARTMENT DOOR LINTEL ATTACHMENT FITTING. COMPLIED WITH N/R-00001 AFT PRESSURE BULKHEAD REPAIR AT LINTED ATTACH FITTING, IAW REO 601R-53-61-1230. COMPLIED WITH EC/TC REO 601R-53-61-1230.SDR SWIA200717934Bulkhead · crackedCABIN 280 BULKHEAD BELOW THE FLOOR AT STRINGER 9L AND 9R EACH HAVE A CRACK, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED CLIPS AT RBL9 AND LBL9.SDR UIEA200700035Bulkhead · crackedFUSELAGE STA 260 BULKHEAD LT LBL60 CANTED BULKHEAD WEB FOUND CRACKED. BULKHEAD STA 260 WEB REPAIRED AS PER SRM 53-10-04 FIG 47.SDR KCSA071055Bulkhead · dentedBS 2360 PRESSURE BULKHEAD WEB DENTED AT RBL 72, WL 225.SDR KCSA071054Bulkhead · dentedBS 2360 PRESSURE BULKHEAD WEB DENTED AT LBL 32, WL 320.SDR DHL2007743503Bulkhead · crackedAFT CABIN, BS 1183 BULKHEAD SHOWS CRACK AT VERTICAL FLANGE APPROX BETWEEN RBL 36.8 AND WL 230. COMPLIED WITH REPAIR PROCEDURES PER B727 SB 727-53-0192, TO INCLUDE: TERMINATION OF CRACK END BY STOP DRILLING (.250" HOLE), AND INSTALLATION OF REPAIR PARTS FROM SDR DHL2007743504Bulkhead · crackedAFT CABIN, BS 1183 BULKHEAD SHOWS CRACK AT VERTICAL FLANGE ANGLE, APPROX BETWEEN BBL 36.8 AND WL 225. COMPLIED WITH REPAIR PROCEDURES PER B727 SB 727-53-0192, TO INCLUDE: TERMINATION OF CRACK END BY STOP DRILLING (.250" HOLE), AND INSTALLATION OF REPAIR PARTSSDR KNNA200700017Vertical Beam · crackedFOUND LBL 5.7 VERTICAL BEAM IS CRACKED BOTH FLANGES AT STA 178 BULKHEAD. PROVIDE INSTRUCTIONS ON REPAIR OF LBL 5.7 VERTICAL CHORD AT STA 178.SDR KNNA200700015Bulkhead · crackedFOUND STA 178 BULKHEAD IS CRACKED AT WL-234, LBL-8 TO LBL-9. PROVIDE INSTRUCTION ON REPAIR OF BULKHEAD AT STA 178 LBL 8 - LBL 9 AND LBL-10-LBL 12.SDR KNNA200700012Bulkhead · crackedFOUND STA 178 BULKHEAD IS CRACKED AT STA 178 W/L 213.5, RBL1, W/L 224, LBL-1-RBL1, W/L 227, RBL 1. PROVIDE INSTRUCTIONS ON REPAIR OF BULKHEAD AT STA 178 W/L 213.5, RBL 1,SDR KNNA200700010Bulkhead · crackedFOUND STA 178 BULKHEAD IS CRACKED AT W/L 234,RBL 9-RBL 10. FOUND PROVIDE INSTRUCTIONS ON REPAIR OF BULKHEAD AT STA 178 RBL 9-RBL 10 .SDR 07FDEA00626Bulkhead · crackedCOMPLY WITH FEDEX EA 7-5330-102012, FUSELAGE - BS 11 83 BULKHEAD WEB CRACK REPAIR AT WL 225, BL61. COMPLIED WITH EA 7-5330-102012, RII:575461.SDR SWAA070363Pressure Panel · crackedDURING SCHEDULED SERVICE CHECK, FOUND RT NOSE WHEEL WELL PRESSURE WEB CRACKED AT BS 259, WL 174. REPAIRED WEB PER SWA EA.SDR SWAA070362Pressure Panel · crackedDURING SCHEDULED SERVICE CHECK, FOUND LT NOSE WHEEL WELL PRESSURE WEB CRACKED AT BS 247, WL 168.6. REPAIRED WEB PER SWA EA.SDR AMTA200700025Bulkhead · corrodedRIGHT MLG WHEEL WELL FORWARD BULKHEAD AT FS 1212 RBL 105.07 AND WL174.315 SUSPECT CORROSION BENEATH FITTING 27, SRM 3-11-00 PAGE 50 FIG 14 SHEET 2. REPAIRED PER EER 12903 GAMCO WORKORDER 316063. (M)SDR CIEA200700001Pressure Panel · crackedDURING INSPECTION OF THE AIRCRAFT TO EVALUATE A PRESSURIZATION LEAK, THE PANEL BEHIND THE REAR SPAR WAS FOUND TO BE CRACKED IN THE LOWER RADIUS AREA. THERE WAS A CRACK APPROXIMATELY 4 INCHES LONG NEAR THE CENTER LINE OF THE AIRCRAFT. THE AIRCRAFT SKIN WAS NOSDR USAA070069Pressure Panel · crackedBS 665, LBL 30, MLG WHEEL WELL PRESSURE FLOOR HAS CRACK. CUT OUT DAMAGED AREA, FAB'D & INSTALLED REPAIR DOUBLER, FILLERS, SHIMS, ANGLE PER TR 53-60-04, DEFECT SIZE: 1 INCH.SDR SDR0701Angle · crackedDURING SCHEDULED 5000 LANDING FS793 BULKHEAD CAP ANGLE NDT INSPECTION, DETECTED A 1.25 INCH LONG CRACK IN RT BULKHEAD CAP ANGLE. MANUFACTURER HAS RECOMMENDED REPLACEMENT OF LT AND RT FS793 BULKHEAD CAP ANGLES.SDR ZZDA070123109Bulkhead · crackedAIRCRAFT LEFT TAXI WAY NOSE GEAR STUCK IN MUD. BULKHEAD AT STA 110 CRACKED AND BENT BEYOND REPAIR. REPAIRED BULKHEAD AT STA 110 PER MDC DRAWING 9911509 REV L DATED 5/13/02 AND PER BOEING ENGINEERING ROD/SKETCH NUMBER 06-12-10-003-002, 8100-9 APPROVED ON 01-0SDR FAA200723001Angle · crackedDURING SCHEDULED 5000 LANDING FS793 BULKHEAD CAP ANGLE NDT INSPECTION, DETECTED A 1/25 INCH LONG CRACK IN RT BULKHEAD CAP ANGLE. MANUFACTURER HAS RECOMMENDED REPLACEMENT OF THE LT AND RT, FS793 BULKHEAD CAP ANGLES.SDR 2007FA0000075Bulkhead · corrodedTHE BULKHEAD, BRACKETS, AND DOUBLERS AT STA. 228.3 WERE SEVERELY CORRODED. THIS BULKHEAD IS THE FRONT SUPPORT FOR THE VERTICAL STABILIZER/RUDDER ASSEMBLY. THE CORROSION COVERED AN AREA APPROXIMATE THE SIZE OF THE FRONT RUDDER ATTACHMENT BRACKET THAT IS PART OFSDR 2007FA0000074Bulkhead · corrodedTHE BULKHEAD, BRACKETS, AND DOUBLERS AT STA. 228.3 WERE SEVERELY CORRODED. THIS BULKHEAD IS THE FRONT SUPPORT FOR THE VERTICAL STABILIZER/RUDDER ASSEMBLY. THE CORROSION COVERED AN AREA APPROXIMATE THE SIZE OF THE FRONT RUDDER ATTACHMENT BRACKET THAT IS PART OFSDR SWAA070314Pressure Panel · crackedDURING SCHEDULED 10Y CHECK, FOUND BEADED PRESSURE WEB CRACKED AT BS 663.75, LBL 32. REPAIRED PRESSURE WEB PER SRM.SDR USAA070051Pressure Panel · crackedOVERHEAD PRESSURE WEB AT BS 665 AT LBL 30 CRACKED. REMOVED DAMAGE, FABRICATED & INSTALLED FILLER & DOUBLER PER T/R 53-60-04, DEFECT SIZE: .6 INCH.SDR SWIA200717691Bulkhead · corrodedLEFT FORWARD BULKHEAD IN FRONT OF 1ST SEAT LOWER ATTACH TRACK CORRODED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED LOWER ATTACH TRACK FOR LEFT FORWARD BULKHEAD WITH A SERVICEABLE UNIT.SDR USAA070039Bulkhead · crackedLOCK FASTENER O/B GLIDE SLOPE ANTENNA SUPPORT AT LBL 5.7 & WL 234, STA 178 BULKHEAD WEB CRACKED. CUT OUT CRACK, FAB'D DOUBLER & FILLER PER EA 98402, SRM 53-10-08 REP 9, DEFECT SIZE: 0.125 INCH.SDR SWAA070188Vertical Beam · crackedDURING SCHEDULED SPV CHECK, FOUND BULKHEAD VERTICAL BEAM CHORD CRACKED AT BS 178, LBL 5.7, WL 184. REMOVED AND REPLACED CHORD PER SRM.SDR CA070115017Stiffener · cracked(CAN) SPECIAL INSP NR53 WAS COMPLETED IAW MM 5-20-05, WHICH INVOLVES THE FOLLOWING: AFT FUSELAGE AREA AND REAR PRESSURE BULKHEAD. INSPECT THE ENTIRE FWD AND AFT SIDE OF THE REAR PRESSURE BULKHEAD FOR CRACKS AND LOOSE OR MISSING RIVETS. CHECKED OXYGEN BOTTLESDR MWEA070002Channel · puncturedSTATION 218 BULKHEAD WALL ZEE CHANNEL STATION 0.007" ABOVE FLOOR IS PUNCTURED. INSTALLED ZEE CHANNEL.SDR MWEA070001Bulkhead · puncturedFOUND STATION 218 BULKHEAD WEB AT STATION 0.007" ABOVE FLOOR HAS PUNCTURE APPROXIMATELY 1/2" DIAGRAM. FABRICATED AND INSTALLED REPAIR DOUBLER.SDR A6WA200740028Bulkhead · crackedFOUND LEFT SIDE FORWARD FACE OF FORWARD PRESSURE BULKHEAD FS 202.75 CRACKED APPROX .2 INCH LONG AT HYDRAULIC SYSTEM NR 3 RT INBOARD BRAKE FITTING. MAINTENANCE REPAIRED CRACKED AREA IAW BOMBARDIER SERVICES CORP EO 601R-53-10650. (M)SDR DL757070030Bulkhead · damagedDURING WALK AROUND, THE FLIGHT CREW FOUND DAMAGE TO THE TAIL AREA STA 1720 BY THE P-DOME FERRY A/C TO ATL. REPAIRED P-DOME LOWER WEB.SDR COEA0712903Bulkhead · crackedDURING HEAVY CHECK, FOUND CRACK ON FRAME 25 LT AND RT OUTBOARD LOWER SIDE OF HYDRAULIC LINE CUTOUT. MAINTENANCE FOUND SB ATR42-53-0120 HAD BEEN PREVIOUSLY COMPLIED WITH. COMPLIED WITH SB ATR42-53-0121 ON BOTH LT AND RT SIDES FOR FRAME 25 HYDRAULIC LINES CUT
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