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.

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. Nov 20, 1995 · N12231 · Boeing 737217SDR ABXA9600276Stiffener · crackedDURING C-CHECK INSPECTION, FOUND AFT PRESSURE BULKHEAD STIFFENER CRACKED AT STA 1072 AT LONGERON 14L. REPAIRED IAW DC-9 SUPPLEMENTAL SRM K05159.Nov 17, 1995 · N955AX · Doug DC941SDR 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.Nov 17, 1995 · N955AX · Doug DC941SDR 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.Nov 17, 1995 · N955AX · Doug DC941SDR 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.Nov 17, 1995 · N675MC · Doug DC951SDR 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.Nov 16, 1995 · N779UP · Doug DC871FSDR 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.Nov 16, 1995 · N955AX · Doug DC941SDR 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.Nov 15, 1995 · N401ME · Doug DC932SDR 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.Nov 15, 1995 · N401ME · Doug DC932SDR 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.Nov 15, 1995 · N401ME · Doug DC932SDR 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)Nov 14, 1995 · N17533 · Doug DC932SDR 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)Nov 14, 1995 · N17533 · Doug DC932SDR 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 FNov 14, 1995 · N2071C · Bell 412SDR 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.Nov 14, 1995 · N490FE · Boeing 727227SDR 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.Nov 14, 1995 · N490FE · Boeing 727227SDR 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.Nov 14, 1995 · N608NW · Doug DC932SDR 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 CNov 11, 1995 · Cessna 208BSDR SWAA950715Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND FUSELAGE PRESSURE BULKHEAD GOUGED AT FLAP DRIVE UNIT ATTACH POINT. REPAIRED PER TRAMCO EWO 95-0658.Nov 10, 1995 · N56SW · Boeing 7372H4SDR 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)Nov 9, 1995 · N1765B · Doug MD11SDR 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 CNov 7, 1995 · N2311C · Cessna 180SDR 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.Nov 4, 1995 · N762DA · Lkheed 10113853SDR 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.Nov 3, 1995 · N8926E · Doug DC931SDR 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 ANov 2, 1995 · N8572S · Cessna 182HSDR 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)Nov 1, 1995 · N903AW · Boeing 7572S7SDR 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 FROct 30, 1995 · N762DA · Lkheed 10113853SDR 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.Oct 30, 1995 · N8926E · Doug DC931SDR 9517269972Blkhd Panel · crackedDURING L-CHECK, FOUND A 2.5 INCH CRACK IN THE FS 83 PRESSURE PANEL, LEFT SIDE. REPAIRED PER EO 5310-01134.Oct 29, 1995 · N9336 · Doug DC931SDR 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.Oct 27, 1995 · N809UP · Doug DC873FSDR 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.Oct 25, 1995 · N989AX · Doug DC932SDR 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. Oct 24, 1995 · N735D · Lkheed 10113851SDR 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.Oct 24, 1995 · N490DA · Boeing 727232SDR 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.Oct 24, 1995 · N490DA · Boeing 727232SDR 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.Oct 24, 1995 · N490DA · Boeing 727232SDR 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.Oct 23, 1995 · N819UP · Doug DC873FSDR 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.Oct 23, 1995 · N819UP · Doug DC873FSDR 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)Oct 21, 1995 · N17535 · Doug DC932SDR 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.Oct 19, 1995 · N601NW · Doug DC932SDR 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.Oct 18, 1995 · N53SW · Boeing 7372H4SDR 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.Oct 18, 1995 · N717DA · Lkheed 10113851SDR 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.Oct 18, 1995 · N989AX · Doug DC932SDR 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 Oct 18, 1995 · N6280R · Cessna 172RGSDR 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.Oct 18, 1995 · N6105V · Cessna 172RGSDR 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.Oct 18, 1995 · N6105V · Cessna 172RGSDR 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.Oct 18, 1995 · N6105V · Cessna 172RGSDR 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.Oct 18, 1995 · N6105V · Cessna 172RGSDR 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.Oct 16, 1995 · N989AX · Doug DC932SDR 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.Oct 16, 1995 · N989AX · Doug DC932SDR 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.Oct 16, 1995 · N926NW · Doug DC932SDR 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)Oct 15, 1995 · N17535 · Doug DC932SDR 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.Oct 13, 1995 · N8928E · Doug DC931
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