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 CAL951072Bulkhead · crackedGSO - INSPECTION FOUND A 4.05 INCH CRACK IN WEB ON LEFT SIDE OF NOSE WHEEL WELL AFT BULKHEAD AT LBL 6.12 AND A 3.25 INCH CRACK ON RIGHT SIDE OF NOSE WHEEL WELL AFT BULKHEAD AT RBL 7.50. THE CRACKS WERE LOCATED AT STATION 294.5. THE CRACKS WERE STOP DRILLED. SDR ABXA9600276Stiffener · crackedDURING C-CHECK INSPECTION, FOUND AFT PRESSURE BULKHEAD STIFFENER CRACKED AT STA 1072 AT LONGERON 14L. REPAIRED IAW DC-9 SUPPLEMENTAL SRM K05159.SDR ABXA9600275Blkhd Stiffener · crackedDURING C-CHECK INSPECTION, FOUND AFT PRESSURE BULKHEAD STIFFENER CRACKED AT STA 1072 AT LONGERON 15L. REPAIRED IAW DC-9 SUPPLEMENTAL SRM K05159.SDR ABXA9600274Blkhd Stiffener · crackedDURING C-CHECK INSPECTION, FOUND AFT PRESSURED BULKHEAD STIFFENER CRACKED AT STA 1072 BETWEEN LONGERON 16L AND 17L. REPAIRED IAW DC-9 SUPPLEMENTAL SRM K05159.SDR 9519239880Bulkhead Angle · crackedDURING L-CHECK, FOUND A CRACK IN THE FS 37 BULKHEAD SUPPORT ANGLE. REPAIRED ANGLE (P/N 9911500-509), PER EA 99-102613.SDR UPS805091Blkhd J-Beam · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND 5TH J-BEAM ON AFT SIDE OF PRESSURE BULKHEAD FS 1766 CRACKED AT RADIUS RT CORNER. REPAIRED PER UPS EO DC8-5310-7630-A.SDR ABXA9600273Blkhd Stiffener · crackedDURING C-CHECK INSPECTION, FOUND AFT PRESSURE BULKHEAD STIFFENER CRACKED AT STA 1072 AT LONGERON 12L. REPAIRED IAW DC-9 SUPP SRM K05159.SDR MWEA95389Blkhd Clip · crackedDURING D-CHECK, MAINTENANCE FOUND THE LEFT HAND LAVATORY PRESSURE BULKHEAD CLIP AT Z34 CRACKED. MAINTENANCE FABRICATED AND INSTALLED A CLIP OF 0.032 INCH 2024-T3 ALUMINUM PER SRM 51-30-2. AIRCRAFT RETURNED TO SERVICE.SDR MWEA95388Blkhd Clip · crackedDURING D-CHECK, MAINTENANCE FOUND THE LEFT HAND LAVATORY PRESSURE BULKHEAD CLIP AT Z-24 CRACKED. MAINTENANCE FABRICATED AND INSTALLED A CLIP OF 0.032 INCH 2024-T3 ALUMINUM PER SRM 51-30-2. AIRCRAFT RETURNED TO SERVICE.SDR MWEA95387Blkhd Clip · crackedDURING D-CHECK, MAINTENANCE FOUND THE LEFT HAND LAVATORY PRESSURE BULKHEAD CLIP AT Z-14 CRACKED. FABRICATED AND INSTALLED A CLIP OF 0.032 INCH 2024-T3 ALUMINUM PER SRM 51-30-2. AIRCRAFT RETURNED TO SERVICE.SDR CAL951119Blkhd Angle · crackedHOU - INSPECTION FOUND A .50 INCH CRACK IN OUTBOARD AFT PRESSURE BULKHEAD FORMER ATTACH ANGLE AT TEE CAP. THE CRACK WAS STOP DRILLED. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-01, FIGURE 2. (X)SDR CAL951113Blkhd Stiffener · crackedHOU - INSPECTION FOUND A 1 INCH CRACK ON FORWARD BULKHEAD VERTICAL STIFFENER. THE CRACK WAS STOP DRILLED. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-01, FIGURE 2, SHEET 4. (X)SDR 96ZZZX107Bulkhead · crackedAFTER LOCATING AND DRILLING BULKHEAD, A CRACK AT THE WELD POINT WAS FOUND. (THERE IS NOT SUPPOSED TO BE A SHRINKAGE LINE ON PART.) CRACKED AT FORMING (SHRINKAGE) LINE. THESE PARTS HAVE PILOT HOLES, THEN FORMED AFTER, AS CAN BE SEEN ON PILOT HOLES ON LOWER FSDR 95FDEA01725Blkhd Angle · corrosionCORROSION (C53-111-01-2), ON BULKHEAD SUPPORT ANGLE AROUND NUTPLATE HOLES BS 720D LBL 28 WL 156. CORROSION WAS FOUND TO BE OUT LIMITS. REMOVED BULKHEAD SUPPORT AND INSTALLED NEW BULKHEAD SUPPORT ANGLE AT BS 720D LBL 28 WL 156.SDR 95FDEA01724Blkhd Angle · corrosionCORROSION ON BULKHEAD SUPPORT ANGLE AT BS 480 RBL 24 TO 39 WL 155. CORROSION OUT OF LIMIT ON BULKHEAD SUPPORT ANGLE AT BS 480 RBL 24 TO 39. ROBBED SERVICEABLE BULKHEAD SUPPORT FROM N489FE AND REMOVED AND REPLACED SERVICEABLE BULKHEAD SUPPORT.SDR 9518239608Blkhd Fitting · crackedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE AFT PRESSURE BULKHEAD T-CAP TO FLOORBEAM TIE FITTING FS 996, RIGHT SIDE. REPLACED CASTING PER SRM 51-30-5 AND DWG 5911546.SDR CA960212017Bulkhead · damaged(CAN)BULKHEAD ON LEFT AND RIGHT HAND SIDE FOUND BENT IN THE LOWER FUSELAGE STRUCTURE UNDER THE FLOOR. ALL BULKHEADS BETWEEN STA 319 AND 237 SHOWS SIGNS OF DAMAGE. THE SUBMITER REPORTS PROBLEMS OF A SIMILAR NATURE WITH FOUR OTHER AIRCRAFT IN ITS FLEET. CESSNA CSDR SWAA950715Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND FUSELAGE PRESSURE BULKHEAD GOUGED AT FLAP DRIVE UNIT ATTACH POINT. REPAIRED PER TRAMCO EWO 95-0658.SDR AALA951914Blkhd Skin · crackedTUL - RIGHT A/C COMP - SMALL CRACK ON AFT BULKHEAD SKIN INBOARD OF ADG ACTUATOR. INSTALLED 1032 TITANIUM REPAIR DOUBLER PER SRM 53-20-00-0, FIGURE 6, SHEET 14. TST 11,610. CYCLES, 1,576. (X)SDR 95ZZZX6574Bulkhead · crackedDURING 100-HOUR INSPECTION, CRACK WAS FOUND AT THE TOP CENTER FUSELAGE BULKHEAD IN BEND RADIUS AT FS 172.0 WHERE DORSAL FIN ATTACH FITTING IS RIVETED. AIRCRAFT WAS USED FOR SKYDIVING OPERATIONS AND ESTIMATE LONG, FULL POWER OPERATION AND PROPELLER VIBRATION CSDR DLL16954502Blkhd Cap · crackedTHE STA 449 BULKHEAD CAP WAS FOUND WITH A 7 INCH LONG CRACK IN ITS BEND RADIUS AT RBL 90.70. REPAIRED PER DL ERA 272084-14.SDR 9519139946Bulkhead Tee · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FS 756 T-CAP AT LONGERON 30. REPAIRED T-CAP (P/N 3915182-502), PER EA 99-103092.SDR 95ZZZX6431Bulkhead · crackedDURING AN ANNUAL INSPECTION, THE BULKHEAD WAS FOUND CRACKED. ACCORDING TO CESSNA' C.A.P. FOR 100 SERIES AIRCRAFT, THIS IS A CRUCIAL PART OF A GOOD INSPECTION. SUBMITTER STATED IT IS ALSO NOTEWORTHY THAT BECAUSE THE AD ON THE SUBJECT TALKS MORE SPECIFICALLY ASDR AWXA9500761Blkhd Bolt · loosePHX - DURING SCHEDULED C4 INSPECTION, FOUND SEVERAL AFT PRESSURE BULKHEAD TO STRINGER BOLTS SHOWING EVIDENCE OF MOVEMENT. RETORQUED PER ER 5-53-16-10A. (M)SDR DLL16954311Blkhd Frame · corrodedTHE AFT P-DOME FRAME SEGMENTS BETWEEN S-22 AND S-44 WERE FOUND WITH CRACKS IN THE LOWER FLANGE RADIUS. THE FRAME SEGMENTS ARE MADE FROM .050 THICK 7178-T6 AL SHEET. ALSO, THE FRAME WEB BETWEEN S-44 AND S-33 WAS FOUND BADLY CORRODED. THE WEB IS FABRICATED FRSDR 9519119946Bulkhead Tee · crackedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE FS 996 AFT PRESSURE BULKHEAD FLOOR TEE AT RBL 34. REPAIRED TEE (P/N 5910163-139), PER EA 99-102944.SDR 9517269972Blkhd Panel · crackedDURING L-CHECK, FOUND A 2.5 INCH CRACK IN THE FS 83 PRESSURE PANEL, LEFT SIDE. REPAIRED PER EO 5310-01134.SDR UPS504915Blkhd Web · damagedWHILE IN FOR C-CHECK, MAINTENANCE FOUND HOLE DAMAGE IN THE AFT BULKHEAD AT STATION 2160 AND LBL 45. MAINTENANCE REMOVED THE DAMAGED PART FROM THE WEB AND REPAIRED THE WEB ACCORDING TO SRM 51-40-02.SDR ABXA9600132Blkhd Tee Cap · defectiveDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE AFT PRESSURE BULKHEAD LOWER TEE CAP SECTION HAD TWO DRILL STARTS. REPLACED LOWER TEE CAP IAW DC-9 SRM 51-30-2 AND 51-30-5.SDR DLL10954309Bulkhead · oversized holeDURING ACCOMPLISHMENT OF THE FS 1363 BULKHEAD REPAIR PER SI 7-69959-12, TWO FASTENER HOLES WERE OVERSIZED DUE TO FASTENER REMOVAL. THE SUBJECT FASTENERS ARE LOCATED 2 ROWS BELOW S-23. THE FWD HOLE IS .328 MAX DIAMETER AND THE AFT HOLE IS .4364 MAX DIAMETER. SDR DL72S954397Blkhd Supports · wornFOUND AT HMV, LT VERTICAL BULKHEAD SUPPORTS WORN AT FLOATING MOUNT BOLTS TO CABIN FLOORBEAMS ABOVE STRINGER 26L AND 22L, FS 720D C1 BAG BIN. REPAIRED PER SRM 53-10-9 FIG 9.SDR DL72S954396Blkhd Supports · wornFOUND AT HMV, RT VERTICAL BULKHEAD SUPPORTS WORN AT FLOATING MOUNT BOLTS TO CABIN FLOORBEAM STRINGER 26R AND 22R, C-1 BIN FS 720D. REPAIRED PER SRM 53-10-9 FIG 9.SDR DL72S954226Bulkhead · crackedFOUND AT HMV, FS 870 BULKHEAD CRACKED AT APU BLEED AIR DUCT CUTOUT AT LWR O/B CORNER. REPAIRED PER SRM 53-10-9.SDR UPS804836Bulkhead · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND 6 INCH CRACK AT PRESSURE BULKHEAD, BS 683 LONGERON 31R. ALSO, A 1.5 INCH CRACK RUNNING AT LONGERON 29R. MAINTENANCE REPLACED THE BULKHEAD ASSY IAW SRM 51-1-20D.SDR UPS804833Blkhd Channel · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND A 1 INCH CRACK ON CHANNEL BS 683, BULKHEAD, LONGERON 28R. MAINTENANCE REPAIRED CHANNEL IAW SRM 53-2-0.SDR CAL951055Bulkhead · corrodedHOU - INSPECTION FOUND CORROSION NEAR T-CAP ON RIGHT SIDE OF AFT PRESSURE BULKHEAD. THE CORRODED SECTION WAS CUTOUT. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-03, FIGURE 22. (M)SDR 9522059601Blkhd Web · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE WHEEL WELL BULKHEAD KEEL WEB FS 756. REPAIRED WEB (P/N 9910164-3), PER EA 12-5310-9-C0614.SDR SWAA950665Blkhd Web · damagedDURING D-CHECK, FOUND PRESSURE BULKHEAD WEB CHAFE DAMAGE AT BS 727 BL 0 WL 185. REPAIRED PER EWO 95-0595 AND BOEING STRUCTURAL REPAIR MANUAL.SDR DLL10954162Blkhd Straps · cutDURING ACCOMPLISHMENT OF S.I. 7-69959-12AD, THE AFT WEB SPLICE STRAPS AT RBL 42.5 AND LBL 42.5 WERE CUT AT LOWER END TO FACILITATE INSTALLATION OF THE LOWER CAP. THEY WILL BE REPAIRED PER THE L-1011 SRM AND DL ERA 272060-14AD.SDR ABXA9600156Blkhd Web · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE APB WEB CORRODED JUST BELOW FLOOR LEVEL AT FS 996 AND BETWEEN LBL 10 AND LBL 20. REPAIRED WEB IAW ABX REA D953-13041-MR.SDR 95ZZZX6912Bulkhead · crackedDURING ANNUAL INSPECTION, IT WAS DETERMINED THAT BOTH UPPER AND LOWER BULKHEADS WERE CRACKED NEAR RUDDER BAR ATTACH POINTS. P/N 241001-3, 241001-4, 241001-5, AND 241001-6. BULKHEADS WERE REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. SUBMITTER SUGGESTS SDR 95ZZZX6168Bulkhead · crackedDURING ANNUAL INSPECTION, DETERMINED THAT UPPER AND LOWER BULKHEADS NEAR RUDDER BAR ATTACH POINTS WERE CRACKED. ALL BULKHEADS WERE REPLACED. SUBMITTER SUGGESTS CLOSE INSPECTION OF THIS AREA DURING INSPECTION, WITH POSSIBLE REINFORCEMENT ADDED.SDR 95ZZZX6167Bulkhead · crackedDURING ANNUAL INSPECTION, DETERMINED THAT UPPER AND LOWER BULKHEADS NEAR RUDDER BAR ATTACH POINTS WERE CRACKED. ALL BULKHEADS WERE REPLACED. SUBMITTER SUGGESTS CLOSE INSPECTION OF THIS AREA DURING INSPECTION, WITH POSSIBLE REINFORCEMENT ADDED.SDR 95ZZZX6166Bulkhead · crackedDURING ANNUAL INSPECTION, DETERMINED THAT UPPER AND LOWER BULKHEADS NEAR RUDDER BAR ATTACH POINTS WERE CRACKED. ALL BULKHEADS WERE REPLACED. SUBMITTER SUGGESTS CLOSE INSPECTION OF THIS AREA DURING INSPECTION, WITH POSSIBLE REINFORCEMENT ADDED.SDR 95ZZZX6165Bulkhead · crackedDURING ANNUAL INSPECTION, DETERMINED THAT UPPER AND LOWER BULKHEADS NEAR RUDDER BAR ATTACH POINTS WERE CRACKED. ALL BULKHEADS WERE REPLACED. SUBMITTER SUGGESTS CLOSE INSPECTION OF THIS AREA DURING INSPECTION, WITH POSSIBLE REINFORCEMENT ADDED.SDR ABXA9600130Blkhd Web · crackedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE BULKHEAD WEB AT FS 1038 CRACKED AT LONGERON 11R. REPAIRED IAW DC-9 SRM 53-01 FIGURE 2.SDR ABXA9600129Blkhd Web · crackedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE BULKHEAD WEB AT FS 1038 HAD A SMALL CRACK RADIATING FROM LIGHTENING HOLE BETWEEN LONGERON 12R AND 13R. REPAIRED CRACK IAW DC-9 SRM 53-01 FIGURE 2.SDR 9516299926Blkhd Fitting · crackedDURING H-CHECK, FOUND A CRACK IN THE LOWER RIGHT HORIZONTAL STIFFENER END FITTING AT THE FS 521 BULKHEAD. REPLACED FITTING PER SRM 51-30-2.SDR CAL951054Door Jamb · crackedHOU - INSPECTION FOUND A 2 INCH CRACK AT LEFT LOWER CORNER OF AFT PRESSURE BULKHEAD DOOR JAMB. THE DOOR JAMB WAS REPAIRED IAW ECRA 5310-03176 AND EA 653A006. (M)SDR 9517239949Blkhd Web · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE FS 1038 BULKHEAD WEB, BETWEEN LONGERONS 7L TO 12L. REPAIRED WEB (P/N 9912246-17), PER EA 99-102958.
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