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 UPS97824832Bulkhead · crackedINSPECTION TYPE-D, FOUND AFT PRESSURE BULKHEAD CRACKED FS 1766, BL 24 TO 28 LT, WL +66. REMOVED DAMAGED AREA, FABRICATED DOUBLER, FILLER, FINGER DOUBLER, DRILLED, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 53-2-5 FIG 14A, 51-1-8, 51-1-21, 51-1-20D.SDR 9720339946Bulkhead · corrodedDURING LINE CHECK, FOUND CORROSION ON AFT PRESSURE BULKHEAD AT RADIAL NR 9 APPROXIMATELY 12 INCHES FROM OUTBOARD END. REPAIRED PER EA 99-152220.SDR USAA970291Bulkhead · corrosionCLT - DURING A Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION AT ALL SCREW HOLES .50 INCH BY .50 INCH AT STA 294 ENTIRE LENGTH UPPER CHORD SECTION 41, BULKHEAD. CORROSION TASK NR C53-107-01. INSTALLED SPLICE PER REPAIR DOCUMENT SRM 51-10-51. (X)SDR AALA972155Bulkhead Casting · corrodedTUL - CASTING CORRODED STRIGNER 30 AT 1183 BULKHEAD. REPLACED CORRODED CASTING STRINGER 30 AT STATION 1183. (M)SDR 97FDEA00727Bulkhead Chord · corrodedNR 0415 011 - CORROSION (C53-132-02-1/2) ON BS 870 LOWER CHORD LBL 65 TO LBL 40.SDR 97FDEA00726Bulkhead Web · corrodedNR 0414 010 - CORROSION (C53-132-02-1/2) ON BS 870 BULKHEAD WEB, LBL 45 TO RBL 45.SDR ABXA9701672Blkhd Stiffener · crackedDURING C-CHECK, FOUND THE AFT PRESSURE BULKHEAD LT RADIAL STIFFENER, NR 2 CRACKED. REPAIRED RADIAL STIFFENER IAW ABX SUPP SRM DWG NR K05159.SDR ABXA9701671Blkhd Stiffener · crackedDURING C-CHECK, FOUND AFT PRESSURE BULKHEAD RT RADIAL STIFFENER 3RD UP FROM FRP CRACKED. REPAIRED RADIAL STIFFENER IAW ABX SUPP SRM DWG NR K05159.SDR ABXA9701670Bulkhead Fitting · crackedDURING C-CHECK, FOUND FITTING CRACKED AT AFT PRESSURE BULKHEAD DOOR JAMB RT SIDE BETWEEN 3RD AND 4TH RADIAL STIFFENER, UP FROM FRP. REPLACED FITTING IAW DC9 SRM 51-30-2 AND 51-30-5.SDR ABXA9701669Bulkhead Former · crackedDURING C-CHECK, FOUND AFT PRESSURE BULKHEAD FORMER CRACKED (1ST UP FROM FRP LT SIDE). REMOVED AND REPLACED FORMER IAW DC9 SRM 51-30-2 AND 51-30-5.SDR SWAA970899Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED AT LT CHORD WL 193. REPAIRED PER BOEING SRM.SDR DLL10972037Bulkhead Web · crackedTHE BULKHEAD STIFFENER PANEL AT FS 328, RBL 22 WAS FOUND CRACKED AT THE END OF THE FOURTH MILLED STIFFENER FROM THE BOTTOM. CRACK TRIMMED OUT WITH A 1 BY 0.5 TRIM OUT. REPAIRED PER ERA 330780-14.SDR DLL10972028Bulkhead Web · corrodedFS 328 BULKHEAD WEB AT LBL 90 WAS FOUND TO HAVE CORROSION. CORROSION WAS CUTOUT. WEB WAS REPAIRED PER ERA 330749-14.SDR DL72K972036Bulkhead Web · crackedSEVERAL CRACKS FOUND IN THE FS 178 BLKHD RBL 6, LBL 5 AND BL 0. REPAIRED PER ERA 330815-14.SDR TWAA9809601Bulkhead Support · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND SUPPORT BRACKET ON AFT PRESSURE BULKHEAD AFT OF 24 RL CRACKED AT STA 579. REPLACED CRACKED ANGLE PER SRM 51-00. TOTAL TIME: 72,580 HOURS. TOTAL CYCLES: 77,573. (X)SDR 97FDEA00706Bulkhead Web · crackedEVIDENCE OF A CRACK AT FASTENER FWD SIDE OF BS 178 PRESSURE BULKHEAD WL 236, RBL 10. *S/D* REPAIRED DAMAGED PRESSURE BULKHEAD BS 178, WL 236, RBL 10 PER FED-EX SRM 53-10-9.SDR IXXA9800009Bulkhead Doubler · corrodedDURING ROUTINE D-CHECK INSPECTION, CORROSION WAS FOUND ON THE PRESSURE BULKHEAD FINGER DOUBLER BETWEEN FUSELAGE STATION 188 AN 208. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF AN INTERNAL FILLER, ONE EXTERNAL REPAIR DOUBLER, ASDR DL72W971990Bulkhead · crackedA 2 INCH CRACK WAS FOUND IN THE 1183 BULKHEAD AT RBL 8.0 AND WL 180. THIS ER/A WILL GIVE INSTRUCTIONS TO ACCOMPLISH A REPAIR UNTIL THE FULL MODIFICATION REQUIRED BY AIRWORTHINESS DIRECTIVE 90-06-09 IS ACCOMPLISHED. THE REPAIR WILL BE INSTALLED ON THE FWD SIDSDR CA971010003Bulkhead · misinstalled(CAN) ON INSPECTION, FOUND THAT THE FIRST 12 INCHES AFT OF THE REAR PRESSURE BULKHEAD (STN 345.0) TO THE RIGHT OF CENTERLINE AT THE UPPER CENTER STRINGER, RIVETS WERE INSTALLED WITH INSUFFICIENT EDGE DISTANCE. AIRCRAFT TT: 2,277 HOURS.SDR 97FDEA00702Bulkhead Web · corrodedNR 0414 002 CORROSION (C53-132-02 1/2) ON BS 870 BULKHEAD WEB LBL 45 TO RBL 45.SDR AU971603Bulkhead · cracked(AUS) FORWARD PRESSURE BULKHEAD CRACKED IN THE FOLLOWING LOCATIONS:-1. THREE CRACKS IN THE BULKHEAD WEB BETWEEN LBL 5.7 AND RBL 5.7 LOCATED UNDER THE RADAR SCANNER MOUNTING BRACKETS - CRACK LENGTHS 24MM (0.944IN) - 14MM (0.551IN) - 13MM (0.511IN) 2. CRACK IN SDR EIAA97222Bulkhead · corrodedDURING C-CHECK INSPECTION, DISCOVERED CORROSION, GOUGES, AND MISDRILLED HOLES ON THE FUSELAGE AFT REAR SPAR BULKHEAD DOUBLER AND CAP AT STA 942 BETWEEN LONGERONS14L TO 16L AND 12R TO 16R. REPAIRED BY TRIMMING AWAY DAMAGE, INSTALLING REPAIR DOUBLERS, ANGLES, ASDR USAA970286Bulkhead Skin · crackINT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND .50 INCH CRACK BS 178 BULKHEAD SKIN RIGHT UPPER ANTENNA (RADAR) MOUNT. INSTALLED REPAIR, REPAIRED PER SRM 53-10-11, FIGURE 1. (X)SDR UPS97224693Blkhd Stiffener · damagedINSPECTION TYPE-C, HYD LINE RUBBING STIFFENER. STIFFNER FOUND TO BE DAMAGED NECESSITATING A REPAIR. REPAIR CARRIED OUT IAW SRS EO 97-24-008 UPS ENG FILE NUMBER 727-53-1 967.SDR 9718419857Bulkhead Skin · crackedDURING ROUTINE MAINTENANCE, FOUND A CRACK IN THE AFT PRESSURE BULKHEAD SKIN AT THE LOWER LEFT CORNER AT THE DOOR JAMB. REPAIRED PER EA 98-152271.SDR 9718359962Bulkhead · crackedDURING M CHECK, FOUND CRACK IN NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE PANEL AT FS 110, RIGHT INBOARD VERTICAL BEAM ATTACH POINT. REPAIRED PER EA 99-151652.SDR 9718449102Bulkhead · crackedDURING L CHECK, FOUND CRACKS IN THE NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE PANEL AT THE RIGHT OUTBOARD AND INBOARD FITTINGS FS 110. REPAIRED PER EA 91-151699.SDR SWAA970868Bulkhead · crackedDURING SCHEDULED C4 CHECK, FOUND AFT PRESSURE BULKHEAD AT BS 1016 OIL CANNING. REPAIRED PER BOEING SRM.SDR DLL10971923Web · corrosionTHE LBL 22 WEB JUST AFT OF THE FWD NLG DOOR HINGE CUTOUT WAS FOUND CORRODED. A SECTION OF THE WEB MEASURING 8 BY 12 WAS CUT OUT. THE WEB IS MADE FROM TWO BONDED SHEETS OF 7075-T6 CLAD MATERIAL, ONE MEASURING .071 THK AND THE OTHER .025 THK. INSTALLED DOUBLESDR CKSA97539Bulkhead Frame · corrodedDURING ROUTINE C-CHECK INSPECTION, FOUND AFT PRESSURE BULKHEAD FWD SIDE FROM L24RH TO L12L HAS AREAS OF SPOT CORROSION LOWER SIDE. REMOVED CORRODED FRAME SECTION IAW L1011 SRM 51-21-01. REPAIRED IAW LOCKHEED L1011 SRM 53-11-0 FIG 848. FRAME REPAIR AT S25 ANSDR ABXA9701692Bulkhead · crackedFUSELAGE STA 680 LBL 5 TO LBL 22 JUST BELOW THE CENTER WING LOWER FORWARD SPAR, THE PRESSURE BULKHEAD IS CRACKED IN TWO PLACES. REMOVED CRACKED SECTION OF DOME, FABRICATED AND INSTALLED FILLERS AND DOUBLERS IAW SRM 53-25, FIGURE 13.SDR 9718439102Bulkhead · crackedDURING L CHECK, FOUND CRACK IN NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE PANEL LIGHT OUTBOARD FITTING FS 110. REPAIRED PER EA 91-151699.SDR W8PA971487Blkhd Support · corrodedPAE - CORROOSION ON FLORR TO BULKHEAD SUPPORT ANGLE ALONG LOWER FLANGE AT BS 947.5, RBL 21, WL 165. REMOVED ANGLE, FABRICATED NEW AND INSTALLED.SDR ABXA9701512Blkhd Fitting · crackedDURING C-CHECK, FOUND THE AFT PRESSURE BULKHEAD DOOR JAMB FITTING AT THE LOWER RT STOP PAD ATTACH FASTENER HOLE CRACKED. REPLACED THE FITTING IAW DC9 SRM 51-30-5 AND 51-30-5.SDR CA971003010Doubler · broken(CAN) DURING ANNUAL INSPECTION, A CRACK AT A RIVET HOLE WAS FOUND IN THE ABOVE DOUBLER. AFTER REMOVING THE DOUBLER IT WAS FOUND TO BE CRACKED INTO TWO PIECES. THE BULKHEAD ASSEMBLY WAS FOUND TO HAVE A .50 INCH CRACK RUNNING FROM EACH SIDE OF THE RIVET HOLE. SDR AU971539Web · cracked(AUS) FORWARD PRESSURE BULKHEAD WEB CRACKED IN SEVEN PLACES:- A. AREA UNDER THE RADAR SCANNING MOUNTING BRACKETS CONTAINED FOUR CRACKS BETWEEN LBL 5.5 AND RBL 5.7 - CRACK LENGTHS 27MM (1.06IN), 13MM (0.5IN) AND TWO CRACKS OF 16MM (0.630IN)B. TWO CRACKS EITHERSDR DHL9774211CBulkhead · corrodedAT C-CHECK, FWD CARGO COMPT BS 740 BULKHEAD BEAM CORRODED AT LOWER CHORD BETWEEN STGRS 27 AND 28 RT. REMOVED CORROSION, WITHIN LIMITS, EXCEPT O/B AREA OF CHORD FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. INSTALLED NEW CHORD AT FWD CARGO COMPT PER SRM 51-30SDR CKSA97530Bulkhead · corrodedDURING ROUTINE B-CHECK INSPECTION, FOUND EVIDENCE OF CORROSION ON AFT SIDE OF STA 870 BULKHEAD APPROX RBL50. REMOVED CORROSION IAW B727 SRM 51-10-6. FOUND OUT OF LIMITS IAW B727 SRM 51-10-1. INSTALLED DOUBLER REPAIR IAW SKETCH AIA/E/2635 DTD 9/9/97. NON-ROSDR 97FDEA00675Bulkhead · crackedCRACK IN 1183 BULKHEAD LBL 10, WL 172. CUT OUT CRACK FINAL APPROX 1 BY 1.5 AND INSTALLED A .063202473 DOUBLER PER EA 7-5310-29205. DATED 9/3/97.SDR TWAA9711311Bulkhead Skin · crackedSTL - REPLACED PORTION OF PRESSURE BULKHEAD AT NR 3 HOLE DUE TO CRACK. (M)SDR TWAA9711310Bulkhead Skin · crackedSTL - REPLACED A PORTION OF PRESSURE BULKHEAD SKIN AT NR 2 HOLE DUE TO CRACK. (M)SDR TWAA9711309Bulkhead Skin · corrodedSTL - REPLACED LOWER AFT BULKHEAD SKIN AT LONGERON 25 RIGHT DUE TO CORROSION. (M)SDR TWAA9711303Bulkhead Skin · crackedSTL - REPLACED SECTION OF AFT PRESSURE BULKHEAD SKIN AT UPPER RIGHT CORNER OF DOOR OPENING DUE TO CRACK. (X)SDR ASAA9740059Bulkhead Seal · tornSEA - DURING STRUCTURAL INSPECTION THE PRESSURE BULKHEAD AT STA 1016, LOWER WEATHER SEAL WAS FOUND TORN. REPAIRED PER EA 5320-01318. TT: 16,604 HOURS. TC: 8,816. (X)SDR ARWA970918Bulkhead · corrodedDURING CPCP INITIAL INSPECTION, FOUND 'C' BELLY, AFT BULKHEAD WALL FRAME REPAIR BETWEEN LONGERON 35L AND LONGERON 35R IS CORRODED (REPAIR AT FRAME) FS 1320. REMOVED CORROSION ON 'C' BELLY AFT BULKHEAD WALL ON STR 35L TO 35R, FABRICATED DOUBLER AND SHIM FROM SSDR AWXA9700576Blkhd Stiffener · damagedDURING SCHEDULED C-11 INSPECTION, FOUND NR 4 RT ZEE STIFFENER DAMAGED ON BS 1016 AFT PRESSURE BULKHEAD FWD FACE RBL 40, WL 274. REPLACED ZEE STIFFENER PER SRM 51-40-02 AND 51-10-02.SDR DL72S971880Blkhd Stiffener · crackedTWO CRACKS WERE FOUND IN THE VERTICAL STIFFENER AT RBL 36.83 ON THE FORWARD SIDE OF THE BS 1183 BULKHEAD. THE CRACKS ARE APPROX 1.75 AND 1 LONG AND ARE LOCATED AT APPROX WL 237 IN THE IB AND OB RADIUS, RESPECTIVELY, OF THE AFT CHORD. THIS AREA IS ADDRESSED ISDR CALA9701465Bulkhead Web · cracked.5 INCH CRACK AT APU OAD CONTROL VALVE CUT OUT IN RIGHT WHEEL WELL AT FWD BULKHEAD. FABRICATED AND INSTALLED DOUBLER REPAIR PER EC/RA 5310-01544.SDR 9717449962Bulkhead Fitting · crackedDURING M-CHECK, FOUND CRACK IN KEEL BEAM TO BULKHEAD FITTING FS 756. REPLACED FITTING PER SRM 51-01.SDR 97ZZZX4261Bonding · crackedDURING A PRE-PURCHASE INSPECTION, A CRACK WAS NOTICED IN THE BONDING PASTE (THICKENED RESIN) ATTACHING THE AFT BULKHEAD TO THE TAIL CONE AT THE LOWER LEFT CORNER. THE CRACK IS 2.25 INCHES LONG. THE MANUFACTURER STATED THIS TYPE OF CRACK OCCURS FROM STRIKING
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