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 DHL98727001Bulkhead Frame · crackedAT AFT BULKHEAD AFT ENTRY DOOR FRAME CRACKED AT NR 7 STOP LEFT AND RIGHT HAND. REPAIRED PER 727 S/B 53-0055.SDR 97FDEA00906Bulkhead Tee · crackedFUSELAGE BULKHEAD TEE CAP, RT SIDE, STA Y1156, FWD OF LONGERON 39, CANTED VERTICAL LEG HAS HFEC CRACK INDICATIONS 2 PLACES AT INBOARD FASTENER LOWER ROW. ONE MOVES INB, SECOND MOVES INB AND DOWN TO RADIUS. SEEN FROM AFT SIDE. REF EO 8-5310-7-3327 PT 2.SDR AU971613Bulkhead · cracked(AUS) FUSELAGE FORWARD PRESSURE BULKHEAD CRACKED IN TEN SEPARATE POSITIONS.SDR QXEA9800161Bulkhead Beam · crackedFORWARD PRESSURE BULKHEAD BEAM NR 5 UPPER FLANGE IS CRACKED AT A PREVIOUS REPAIR AT THE CENTER OF THE BEAM. REPAIRED IAW FOKKER SRM 51-10-4, 51-31-01 AND 51-30-02.SDR DHL97701003Bulkhead · crackedAFT 1183 BULKHEAD DOOR FRAME ON RT SIDE NEAR 2ND FROM TOP STOP HAS POSSIBLE CRACK INDICATION. CRACK 1.45, VERIFIED WITH NDT METHODS. INSTALLED TEMPORARY REPAIR PER AVITAS ENGINEERING ORDER 97PMSI 184D-1 PAGES 1, 2 AND 3.SDR 9724929977Bulkhead Doubler · crackedDURING L-CHECK, FOUND A CRACK IN THE AFT PRESSURE BULKHEAD DOUBLER AT THE UPPER LEFT DOOR STOP. REPAIRED PER EA 99-114603.SDR QXEA9800226Bulkhead Frame · crackedTHREE CRACKS EXTENDING FROM RIVET HEADS. LOCATED IN RIGHT WHEEL BAY APPROXIMATELY 3 FORWARD OF BULKHEAD FRAME 13345 AND IN THE TOP, AFT, OUTBOARD CORNER. INSTALLED NEW DOUBLER IAW EA 4-53-317.SDR DL72L972681Blkhd Stiffener · crackedA 2 INCH CRACK WAS FOUND IN THE RBL 36.83 STIFFENER AND A 1 INCH CRACK WAS FOUND IN THE LBL 36.83 STIFFENER AT WL 238 ON THE FS 1183 BULKHEAD. THE STIFFENERS WERE REPAIRED PER BOEING S/B 727-53-0192 AS DOCUMENTED IN ER/A 363498-14.SDR AALA972390Bulkhead Web · corrodedTUL - BS 178 WL 195-197, CORROSION ON BULKHEAD WEB ABOVE HORIZONTAL ANGLE. INSTALLED DOUBLER PER SRM 53-10-9. (M)SDR 98ZZZX96Bulkhead · crackedINSPECTION REVEALED A CRACK IN THE LEFT HAND DOOR POST AFT SECTION AT THE LOWER DOOR HINGE LOCATION. CRACK STARTS AT THE AFT SCREW HOLE AND PROGRESSES IN BOTH DIRECTIONS. CRACK IS APPROXIMATELY 1.3750 INCHES LONG.SDR CALA9701774Door Pan · wornINSPECTION FOUND 15 EACH ELONGATED FASTENER HOLES ON APB UPPER DOOR PAN. THE HOLES WERE REAMED FOR SECOND OVERSIZE HILOCK IAW SRM 51-30-5.SDR AU971619Bulkhead · cracked(AUS) FUSELAGE FORWARD PRESSURE BULKHEAD CRACKED IN TWO POSITIONS.SDR CALA9701770Bulkhead Web · buckledINSPECTION FOUND THE LT ENGINE PYLON FRONT SPAR WEB(LAV BULKHEAD) BUCKLED AT BOTTOM WITH A 2 CRACK AT BOTTOM OUTBOARD CORNER. THE BULKHEAD WEB WAS REMOVED AND REPLACED IAW SRM 51-10-2.SDR CALA9701764Bulkhead Web · buckledINSPECTION FOUND RT AFT LAV BULKHEAD WEB BUCKLED AT BOTTOM. A WEB AND TEE SUPPORT WERE FABRICATED AND INSTALLED IAW SRM 53-03.SDR CALA9701763Bulkhead Web · crackedINSPECTION FOUND A 3 CRACK IN AFT PRESSURE BULKHEAD DOOR FRAME. THE CRACK WAS LOCATED AT INBOARD END AND TOP OF DOOR JAMB ON FORWARD SIDE OF APB. THE CRACKED FRAME SECTION WAS REMOVED AND A NEW UPPER FRAME SECTION WAS INSTALLED ON DOOR JAMB IAW SRM 51-30-2.SDR 98ZZZX81Bulkhead · crackedDURING ANNUAL INSPECTION, FOUND CRACKING IN TAIL AT FS 271.92 BULKHEAD. REPAIRED PER BEECHCRAFT SI 990. AREA VERY HARD TO INSPECT. SI 990 ALSO HAS INSPECTION CRITERIA. CRACKING FOUND ON 3 AIRCRAFT AT THIS STATION WHILE C/W SI 990. SUBMITTER SUGGESTED BULLSDR DLL14972602Bulkhead Web · corrodedCORROSION FOUND ON THE RT LWR OUTB'D CORNER OF THE 328 BLKHD WEB. REPAIRED PER ERA 331000-14AD.SDR CALA9701761Bulkhead Web · crackedINSPECTION, FOUND TWO 1.75 CRACKS IN LT AFT PRESSURE BULKHEAD DOOR CUTOUT UPPER CORNER BELOW RADIUS. REPAIRED IAW DOUGLAS DRAWING J060088.SDR TWAA9809603Bulkhead · crackedMCI - DUIRNG MAINTENANCE CHECK, FOUND LT BULKHEAD OTBD OF LT TRUNNION, 3 INCHES FORWARD, HAD 3 INCH CRACK. CUT OUT CRACK AND INSTALLED DOUBLER PER SRM 53-05, PAGE 85. TOTAL CYCLES: 45,640 HOURS. TOTAL CYCLES: 23,735. (X)SDR ABXA9701944Bulkhead Web · crackedDURING C-CHECK, FOUND THE AFT BULKHEAD WEB OF THE E/E COMPARTMENT CRACKED JUST INBD OF THE NR 3 VERTICAL SUPPORT ON THE LT SIDE APPROX 2 ABOVE THE FLOOR. REPAIRED THE WEB IAW ABX REA D953-21807.SDR ABXA9701943Bulkhead Web · crackedDURING C-CHECK, FOUND THE AFT BULKHEAD WEB OF THE E/E COMPARTMENT CRACKED JUST OUTBD OF THE NR 5 VERTICAL SUPPORT ON THE LT SIDE. REPAIRED THE WEB IAW AX REA D953-21990.SDR AALA972362Bulkhead Tee · crackedTUL - HFEC INDICATES CRACK AT 1 FASTENER HOLE IN BULKHEAD TEE CAP LEG, RT SIDE. INSTALLED ARROWHEAD DOUBLER AND STRAP PER ESO 7349, DATED 11/20/97. (M)SDR 9725009606Bulkhead · crackedDURING LINE CHECK, FOUND CRACK IN THE AFT PRESSURE BULKHEAD SKIN AT THE UPPER LEFT AND RIGHT DOOR STOPS. REPAIRED PER EA 96-153409.SDR 9722799950Bulkhead Fitting · corrodedDURING H-CHECK, FOUND CORROSION ON LONGERON 25R END FITTING AT FORWARD SIDE OF AFT PRESSURE BULKHEAD. REPLACED FITTING (P/N 3914590-501N) PER SRM 53-01.SDR 9722789950Bulkhead Fitting · corrodedDURING H-CHECK, FOUND CORROSION ON LONGERON 26R END FITTING AT FORWARD SIDE AT AFT PRESSURE BULKHEAD. REPLACED FITTING (P/N 3914590-501N) PER SRM 53-01.SDR 9722779950Bulkhead Fitting · corrodedDURING H-CHECK, FOUND CORROSION ON LONGERON 24R END FITTING AT AFT SIDE OF AFT PRESSURE BULKHEAD. REPLACED FITTING (P/N 3914590-1) PER SRM 53-01.SDR SWIA971064Bulkhead Strap · corrodedCORROSION ON BUTT STRAP ALONG LEFT BULK HEAD UNDER GALLEY. REPLACED LEFT BUTT STRAP SILL.SDR USAA970354Bulkhead · crackedDURING B-CHECK, FOUND APPROXIMATE 2.5 INCH CRACKS IN AFT PRESSURE BULKHEAD DASHES 3, 85, AND 87 SKIN DOUBLERS AT LOWER LT HAND CORNER OF DOOR APERTURE AFT PRESSURE BULKHEAD STA 996. DETECTED BY VISUAL AND X-RAY. MADE DOUBLER REPAIR PER J060088-515. (X)SDR DLL14972536Bulkhead Web · crackedCRACKS FOUND IN BULKHEAD WEB AND LWR CAP AT FS 1363 BULKHEAD. REPAIRED PER AMOC ERA 331016-14AD.SDR F3LA97166Bulkhead · crackedPAE - RIGHT BS 727 BULKHEAD LOWER CHORD DISCOVERED CRACKED DURING ACCOMPLISHMENT OF FRONTIER ENGINEERING ORDER NR 53-10-737-004. REMOVED AND REPLACED LOWER SECTION OF CHORD IAW EO NR 53-10-737-001. (M)SDR AU971621Bulkhead · cracked(AUS) FUSELAGE FORWARD PRESSURE BULKHEAD CRACKED IN EIGHT POSITIONS.SDR 98FDEA00425Bulkhead Fitting · crackedSTA-VCE: RT FRONT SPAR TO Y=1156 BULKHEAD TEE FITTING WAS FOUND CRACKED. CRACK IS .450. MAJOR REPAIR PERFORMED IAW EA 8-5314-34480 B. (29 JUNE 1998).SDR 9724871235Bulkhead T-Cap · corrodedDURING M-CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON FS 1156 PRESSURE BULKHEAD T-CAP FROM LONGERON 49L TO 49R. REPAIRED PER EA 12-151004.SDR 9724671235Bulkhead · corrodedDURING M-CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON CENTER ACCESSORY COMPARTMENT BULKHEAD AT FS 1156, LONGERON 51L. REPAIRED PER EA 12-151004.SDR RAAA97E8039Blkhd Stiffener · crackedDURING SCHEDULED NR 2 CHECK, FOUND FWD PRESSURE BULKHEAD LOWER RT ACCESS PANEL STIFFENER CRACKED APPROX 1.0 INCH. REPLACED ACCESS PANEL STIFFENER PER SRM 51-2-9, M-54 NR 73.SDR P2EA97083Bulkhead Chord · crackedSJO - FOUND OUTBOARD CHORD CRACK FUSELAGE BULKHEAD, BS 1156, LEFT OUTBOARD CHORD WL 74. DEFECT SIZE 2 INCHES. REPAIRED FUSELAGE LEFT OUTBOARD CHORD IAW SB 737-53-1086. (M)SDR 9724739610Bulkhead Skin · crackedDURING PERIODIC CHECK, FOUND CRACK IN AFT PRESSURE BULKHEAD SKIN AT LOWER RIGHT CORNER. REPAIRED PER EA 96-154147.SDR P2EA97078Bulkhead · corrodedSJO - DISCREPANCY FOUND DURING SCHEDULED MAINTENANCE C-CHECK, NO DOCUMENTATION ON FILE FOR REPAIR AT NOSE WHEELWELL FWD BULKHEAD WEB, BS 294.5 BETWEEN RBL 5 INCH AND RBL 12 INCH, WL 169 TO WL 190. REPAIRED PER BOEING FAX NR C00-SJO-97-0297TRR DATED 11/14/97, SDR CA971219015Bulkhead · corroded(CAN) WHEN GLUED ON INSULATION WAS REMOVED AT REAR SIDE OF AFT PRESSURE BULKHEAD BELOW OUTFLOW VALVES, CORROSION WAS FOUND. SUSPECT MOISTURE TRAPPED BENEATH INSULATION. AIRCRAFT TT: 10,593 HOURS.SDR 98ZZZX1209Bulkhead Frame · chafedTHERE IS AN L-SHAPED CHAFE MARK ON FRAME 32 PRESSURE BULKHEAD, NEAR CENTERLINE BEHIND RT MLG DOOR UPLOCK ASSY. NEEDS INVESTIGATION. BLENDED ABOVE AREA IAW BAE FAX JM/FJ0844-97. REPROTECTED, PRIMED AND PAINTED.SDR 9724729601Bulkhead Doubler · crackedDURING PERIODIC CHECK, FOUND CRACK IN AFT PRESSURE BULKHEAD WEB DOUBLER (P/N 5910130-13) AT THE UPPER LEFT AND RIGHT CORNERS. REPAIRED PER EA 96-154142.SDR GAIA9767Bulkhead · damagedDURING WALKAROUND, THE FLIGHT CREW FOUND THAT THE INTERNAL BULKHEAD AT STATION 786 HAD MOVED AFT 4 INCHES. FURTHER INVESTIGATION REVEALED THAT THE FLOOR RESTRAINTS IN THE SEAT TRACK HAD BROKEN LOOSE. THE VERTICLE BULKHEAD SUPPORTS WERE BROKEN AT THE FLOOR ATSDR IXXA9800024Bulkhead Panel · crackedDURING ROUTINE D-CHECK INSPECTION, A CRACK WAS FOUND ON THE PRESSURE BULKHEAD PANEL BETWEEN FUSELAGE STATIONS 133 AND 148. REPAIR ACCOMPLISHED BY REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF FILLER, NESTED ANGLE DOUBLERS AND FINGER DOUBLER IN ACCOSDR AU971623Bulkhead · cracked(AUS) FRONT BULKHEAD CRACKED THROUGH TWO BOLT HOLES. FOUND FOLLOWING REMOVAL OF THE UPPER NOSE LEG MOUNT PLATE DUE TO TOWING DAMAGE. DAMAGE CAUSED BY INCORRECT GROUND HANDLING.SDR AALA972191Bulkhead Web · crackedTUL - STATION 870 BULKHEAD CRACKED AT CUTOUT FOR APU LOAD CONTROL VALVE. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-10-2 PAGE 261 (C). (M)SDR DHL9780262CBulkhead · crackedAT C-CHECK, MAIN CARGO COMPT REAR PRESSURE BULKHEAD LT AT STA 1760 5 FT ABOVE FLOOR SUPPORT INTERCOSTAL NR 6 FROM BOTTOM TO TOP HAS CRACK APPROX 1 INCH LONG. REMOVED DAMAGED SECTION OF PRESSURE BULKHEAD BY CUTTING AND FABRICATED REPAIR DOUBLER 24 X 13 PER SRSDR DHL9780261CBulkhead Web · crackedAT C-CHECK, MAIN CARGO COMPT REAR PRESSURE BULKHEAD RT AT STA 1760, 5 FT ABOVE FLOOR SUPPORT INTERCOSTAL NR 6 FROM BOTTOM TO TOP OUTBD OF STIFFENER HAS 1 INCH LONG CRACK. REMOVED DAMAGED SECTION OF PRESSURE BULKHEAD WEB, FABRICATED REPAIR DOUBLER 24 X 13 AND SDR 97FDEA00838Bulkhead Strap · corrodedUPON REMOVAL OF 8.70 BULKHEAD WEB (NR0414) FOUND TENSION LOAD STRAP TO BE CORRODED RBL 50-LBL 50, WL 160. *S/D* REMOVED AND REPLACED TENSION LOAD STRAP RBL 65 - LBL 65, WL 160, BS 870 PER BOEING DWG 65-15978 AND ER NR 054. INSTALLED HILOCS PER FED SRM 51-30SDR TWAA9713301Bulkhead Tee · crackedSTL - REPLACED PRESSURE BULKHEAD TEE BETWEEN LONGERON 11R AND 12R DUE TO A CRACK. (M)SDR ABXA9701815Bulkhead Fitting · corrodedDURING C-CHECK, FOUND THE CENTER FITTING AT LONGERON 30 THAT ATTACHES TO THE AFT PRESSURE BULKHEAD T-CAP HEAVILY CORRODED. REPLACED FITTING IAW ABX NEA 53120035-006, ITEM 8.
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