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 97ZZZX554Bulkhead · crackedDURING A 100 HOUR INSPECTION A BULKHEAD CRACK WAS FOUND ON THE RIGHT SIDE OF THE LATERAL PITCH BELLCRANK. THE MOVEMENT OF THE CYCLIC LT AND RT WILL FLEX THE BULKHEAD THAT THE BELLCRANK SUPPORT IS ATTACHED. THE BELLCRANK NOW MOVES FROM SIDE TO SIDE WHILE FLEXSDR ABXA9700254Bulkhead Clip · crackedDURING C-CHECK, A CLIP WAS FOUND CRACKED AT THE AFT PRESSURE BULKHEAD LONGERON 17 RIGHT, NR BF-624. THE CLIP WAS REPAIRED IAW DC9 SRM.SDR CKSA96319Bulkhead Angle · corrodedDURING C-4 CHECK INSPECTION, FOUND FS 1766 AFT PRESSURE BULKHEAD RIGHT HAND HORIZONTAL SUPPORT ANGLE ATTACHING TRANSVERSE FLOORBEAM CORRODED. REMOVED AND REPLACED ANGLE IAW DC-8 SRM 51-1-0 AND INSTALLED FASTENERS IAW DC-8 SRM 51-1-21. CORROSION CARD NR 5600-SDR CKSA96238Bulkhead Fitting · corrodedDURING C-4 CHECK INSPECTION, FOUND LEFT HAND WHEEL WELL 857 BULKHEAD 69.5 UPPER FITTING CORRODED. REPAIRED IAW DOUGLAS DRAWING NR J060192. C-4 CHECK CARD NR 3010, NON-ROUTINE TASK CARD NR 88042.SDR DLL10962614Bulkhead · crackedBS 1212 BULKHEAD WAS FOUND CRACKED AT LBL 30 AND RBL 6. THE CRACKS MEASURED 1 AND 8 RESPECTIVELY. DURING REPAIR THE TEE STIFFENER AND THE UPPER CAP WERE MISDRILLED. THE HOLES ARE BUSHED TO FIRST OVERSIZE AND THE RBL 6 LOCATION REQUIRED A CHANGE TO THE DOUBLSDR ABXA9700255Bulkhead Clip · crackedDURING C-CHECK, A CLIP WAS FOUND CRACKED AT THE AFT PRESSURE BULKHEAD LONGERON 14 LEFT, NR BF-627. THE CLIP WAS REPAIRED IAW DC9 SRM.SDR ABXA9700253Bulkhead Clip · crackedDURING C-CHECK, A CLIP WAS FOUND CRACKED AT THE AFT PRESSURE BULKHEAD LONGERON 12 RIGHT, NR BF-625. THE CLIP WAS REPAIRED IAW DC9 SRM.SDR ABXA9700252Bulkhead Clip · crackedDURING C-CHECK, A CLIP WAS FOUND CRACKED AT THE AFT PRESSURE BULKHEAD LONGERON 15 LEFT, NR BF-626. THE CLIP WAS REPAIRED IAW DC9 SRM.SDR CA970311064Bulkhead · cracked(CAN) BULKHEAD FOUND CRACKED BEYOND REPAIRABLE LIMITS.SDR USAA960747Bulkhead · corrosionINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 2 INCH CORRODED AREA AT BULKHEAD BS 1023 RBL 1 INCH WL 195. INSTALLED EXT REPAIR, REPAIRED PER SRM 53-10-4/53-10-3. CORROSION TASK NR C53-202-01, CORROSION LEVEL 1. (M)SDR UPS96421732Bulkhead Chord · crackedINSPECTION TYPE: C. FWD CARGO COMPARTMENT: AFTER HFEC INSPECTION, FOUND BULKHEAD CHORD STA 1000 CRACKED BETWEEN STR 46/47 RT, CRACK LENGTH APPROX. 40MM. REPLACED LWR CHORD SEGMENT AT BS 1000 ACC. EO B747-5310-5301-E PER SALES ORDER NR 69494-20.SDR DL73K962609Bulkhead · crackedTHE STATION 178 BULKHEAD WAS FOUND CRACKED IN SEVERAL LOCATIONS. DAMAGE CUTOUTS ARE: 1 X 1.75 AT RBL 5.7, WL 198; 1 X 1 AT RBL 5.7, WL 201; 1 X 1 AT LBL 5.7, WL 198; 1 X 1 AT LBL 5.8, WL 201; 1 X 1.75 AT LBL 5.7, WL 201. THE BULKHEAD WEB IS FABRICATED FSDR DLL15962720Frame · corrodedTHE P-DOME ZEE FRAME BETWEEN S-29 AND S-37 WAS FOUND CORRODED AND IN NEED OF REPLACEMENT. A NEW SECTION WAS SPLICED IN.SDR 9624819996Bulkhead Fitting · crackedDURING H-CHECK, FOUND CRACKS IN FS 756 CENTER LINE BULKHEAD FITTINGS: SECOND, THIRD AND FOURTH FROM THE TOP. REPLACED ALL FITTINGS (P/N 9958212-37) PER SRM 51-30-5.SDR DLL12962616Bulkhead · crackedA CRACK WAS FOUND AT FS 1212 BULKHEAD RBL 42.5. THE CRACK WAS TRIMMED OUT, FILLED AND REINFORCED. REVISION A: CORRECTED FASTENER PATTERN ON FIGURE 1, CHANGED RESTRICITONS TO 12 MONTHS. REVISION B: ADDED FAA APPROVAL.SDR SWAA961268Bulkhead Web · crackedDURING SCHEDULED D-CHECK, FOUND BULKHEAD BS 178 PRESSURE WEB CRACKED AT RBL 4.7. REPAIRED PER BOEING SRM.SDR SCNA96429Bulkhead Tee · damagedDURING HEAVY MAINTENANCE, FOUND FORWARD PRESSURE BULKHEAD TEE SUPPORT FOR HINGES WITH TWO LIGHTNING STRIKES. REMOVED TEE, FABRICATED AND INSTALLED A NEW TEE IN ACCORDANCE WITH SRM 51-30-2 AND DRAWING NBA6054. CLOSED AREA AND LEAK CHECKED GOOD.SDR 97ZZZX1769Door Frame · corrodedDURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, AFT ENTRY DOOR HAS CORROSION ON BOTTOM FRAME. REMOVED CORRODED CHANNEL. INSTALLED NEW CHANNEL IAW DC9 SRM'S 51-30-5, 51-10-4, AND 51-10-3.SDR USAA960738Bulkhead Angle · crackedPIT - DURNIG Q-1 CHECK, FOUND TWO 3 INCH CRACKS IN ADDITION TWO NESTED ANGLES CRACKED .75 AFT CENTER PRESSURE BULKHEAD, CRACKS FOUND SUBJECT ANGLE ONE AT STRINGER NR 11 LHS AND ONE AT STRINGER NR 62RHS. INSTALLED DOUBLER REPAIR PER USAIR EA NR 33790. (M)SDR DL73S962528Bulkhead · crackedTHE STATION 178 BULKHEAD WAS FOUND CRACKED IN SEVERAL LOCATIONS. DAMAGE CUTOUTS ARE: 1 DIA AT RBL 5.7, WL 198; 1 BY 1.5 AT RBL 5.7, WL 201; 1 BY 1.5 AT LBL 5.7, WL 198; 1 BY 2 AT LBL 5.7, WL 201; AND 1 BY 1.5 AT BL 0, WL 188. THE BULKHEAD WEB IS FABRICATSDR DL72S962588Bulkhead Support · wornAT MID VISIT, THE VERT SUPPORT BEAMS FOR AFT C1 BIN BULKHEAD WERE FOUND TO BE WORN. THEY WERE REPAIRED PER SRM 53-10-9.SDR 9624589140Bulkhead Panel · crackedDURING H-CHECK, FOUND CRACKS IN THE NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE PANEL AT FS 105 AT THE LEFT INBOARD AND OUTBOARD VERTICAL BEAM FITTINGS AND AT THE RIGHT OUTBOARD VERTICAL BEAM FITTING. REPAIRED PANEL (P/N 9910073-313) PER EA 91-111773.SDR UPS96421781Bulkhead Clip · crackedINSPECTION TYPE-C, FOUND CRACK ON BULKHEAD ATTACH CLIP AT STA 340 RT (2) MARKED. CRACKED CLIPS REMOVED AND NEW CLIPS FABRICATED AS PER SRM 51-40-03 AND INSTALLED AS PER 51-30-02.SDR UPS96421780Bulkhead Clips · crackedINSPECTION TYPE-C, FOUND CRACK ON BULKHEAD ATTACH CLIPS AT STA 340 LT (3) MARKED ATTACHED TO NWW SIDE PANEL. CRACKED CLIPS REMOVED AND NEW CLIPS FABRICATED AS PER SRM 51-40-03 AND INSTALLED AS PER SRM 51-30-02, OBTAINED FROM STA STOCK.SDR DLL15962723Press Deck · crackedTHE FUSELAGE HORIZ PRESSURE DECK PANEL WAS FOUND WITH A 1 INCH LONG CRACK AT RBL 102, JUST AFT OF FS 378. THE CRACK WAS CUTOUT AND REINFORCED WITH DOUBLERS.SDR AWXA9600695Bulkhead · dentedPAE - FLT 7806 - DURING ROUTINE MAINTENANCE CHECK, FOUND BS 178 PRESSURE BULKHEAD DENTED, WL 187, RBL 12. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR PIECES, IAW ER 2-53-12-31, TCO-PAN-96-1636RR. (M)SDR SWAA961236Bulkhead · crackedDURING SCHEDULED 1/2 D-CHECK, FOUND AFT CARGO FWD PRESSURE BULKHEAD AT BS 727 COMPRESSION CHORD CRACKED IN RADIUS OF LOWER LEG. REPAIRED PER SWA RA 1-253-1555.SDR CALA9601653Bulkhead · crackedINSPECTION FOUND A 6 INCH CRACK IN BULKHEAD AT STA 178, RT SIDE. THE CRACKED AREA WAS CUT OUT, A REPAIR DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-10-11.SDR CALA9601652Bulkhead · crackedINSPECTION FOUND A 6 INCH CRACK IN BULKHEAD AT STA 178, LT SIDE. THE CRACKED AREA WAS CUT OUT, A REPAIR DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-10-11.SDR SWAA961238Bulkhead · crackedDURING SCHEDULED SERVICE VISIT CHECK, FOUND BS 727 BULKHEAD CRACKED. REPAIRED PER BOEING SRM.SDR AALA961630Bulkhead Angle · corrodedTUL - FOUND CORROSION ON PRESSURE BULKHEAD T-ANGLE AT GALLEY SUPPORT NR 4. REPAIRED PER ESO NR 41000, DATED 11/07/96. INSTALLED ANGLE REPAIR OVER DAMAGED AREA 2 FASTENERS BEYOND. (M)SDR AALA961628Bulkhead Angle · corrodedTUL - FOUND CORROSION ON PRESSURE BULKHEAD T-ANGLE AT GALLEY NR 1 SUPPORT. REPAIRED PER ESO 41000 DATED 11/07/96. INSTALLED ANGLE REPAIR OVER DAMAGE 2 FASTENERS BEYOND. (M)SDR AALA961626Bulkhead Angle · corrodedTUL - FOUND CORROSION ON PRESSURE BULKHEAD T-ANGLE AT NR 3 GALLEY SUPPORT. REPAIRED ANGLE PER ESO 41000 DATED 11-27-96. INSTALLED ANGLE REPAIR 2 FASTENERS BEYOND DAMAGE. (M)SDR DL73S962481Bulkhead · crackedSTATION 178 BULKHEAD WAS FOUND CRACKED IN SEVERAL LOCATIONS. DAMAGE CUTOUTS ARE: 1INCH BY 2.5 INCH FOR RBL 5, WL 194, AND 1INCH BY 2.0 INCH FOR LBL 5, WL 194. REPAIRED PER ERA 304373-14 REV A.SDR 9624549760Bulkhead Panel · crackedDURING H-CHECK, FOUND CRACKS IN THE NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE PANEL AT FS 108, LEFT AND RIGHT SIDES, AT BOTH THE INBOARD AND OUTBOARD VERTICAL BEAM ATTACH FITTINGS. REPAIRED PANEL (P/N 9910073-313) PER EA 97-111754.SDR ABXA9700323Bulkhead Web · damagedDURING C-CHECK, THE AFT PRESSURE BULKHEAD WEB WAS FOUND DAMAGED AT LONGERON 271LT. REPAIRED IAW REA D953-17185-MR.SDR ABXA9700320Bulkhead · crackedDURING C-CHECK, THE BULKHEAD AT STA 1041 WAS FOUND CRACKED ON THE RT SIDE AT ENGINE MOUNT SPAR. REPAIRED IAW DC-9 SRM 51-30-1, 51-30-2 AND 51-30-5.SDR ABXA9700319Bulkhead · crackedDURING C-CHECK, THE BULKHEAD AT STA 1072 WAS FOUND CRACKED ON THE RT SIDE OF THE DOOR JAMB 24 FROM FLOOR. REPAIRED IAW REA D953-17165MR.SDR ABXA9700318Bulkhead · crackedDURING C-CHECK, THE BULKHEAD AT STA 76 WAS FOUND CRACKED NEXT TO RT CUSP. REPAIRED IAW REA D953-17160.SDR ABXA9700311Blkhd Door Jamb · crackedDURING C-CHECK, THE AFT PRESSURE BULKHEAD LT VENTRAL DOOR JAMB CORNER WAS FOUND CRACKED BEYOND A PREVIOUS STOP DRILL. REPAIRED IAW REA D953-17172SB.SDR DL73S962471Bulkhead · crackedTWO CRACKS WERE DISCOVERED ON FWD FACE OF THE F.S.178 BLKHDWEB. TWO INDEPENDENT CUTOUTS WERE REQUIRED TO REMOVE THE CRACKS. FIRST CUTOUT, LOCATED INBD OF THE RBL 5.7 VERTICAL STRAP AT WL 200, MEASURES 4.0 INCH VERTICALLY BY 1.0 INCH INBD/OTBD. THE SECOND CUSDR 96FDEA01640Bulkhead Panel · corrodedSNRM N00944, CENTER GEAR WHEEL WELL, LT BULKHEAD ACCESS PANELS 146AN AND 146BN PANEL LAND CORRODED. *S/D* REWORKED PER EA WORK INSTRUCTIONS, EA NR 8-5310-31745, STEPS 1 TO 5 FOR AFT ACCESS PANEL 146 IN, AND STEPS 1 TO 3 FOR FWD ACCESS PANEL 146BN FWD ACCESSSDR TWAA9613507Bulkhead · crackedSTL - DURING OP-15, FOUND A FOUR INCH CRACK AT BOTTOM OUTBOARD CORNER OF FORWARD BULKHEAD OF RIGHT LAV, STA 1136. REPAIRED PER SRM 53-03, FIGURE 21, SHEETS 1 AND 2. AIRCRAFT TOTAL TIME: 46,296 HOURS; 43,121 CYCLES. (X)SDR EISA96274Blkhd Stiffener · crackedDURING A SCHEDULED D-CHECK, FOUND A VERTICAL STIFFENER CRACKED IN OUTBOARD FLANGE STATION 1183 LBL 45. REPAIRED PER SRM 51-40-4. (M)SDR EISA96273Blkhd Vert Beam · crackedDURING A SCHEDULED D-CHECK, FOUND THE 1183 BLKHEAD VERTICAL BEAM CRACKED RBL 35. REPAIRED PER SRM 51-30-2 AND 51-40-4. (M)SDR EISA96272Blkhd Vert Beam · crackedDURING A SCHEDULED D-CHECK, FOUND THE 1183 BLKHEAD VERTICAL BEAM CRACKED LBL 35. REPAIRED PER SRM 51-40-4 AND 51-30-2. (M)SDR CALA9601561Bulkhead Skin · crackedINSPECTION FOUND A 6 INCH AND 7 INCH CRACK IN SKIN AT B.S. 178 BULKHEAD. THE CRACKED AREA WAS CUT OUT. DOUBLER AND FILLERS WERE FABRICATED AND INSTALLED IAW SRM 51-30-2 AND SRM 53-10-11.SDR CALA9601554Bulkhead Skin · crackedINSPECTION FOUND A 6.5 INCH CRACK IN STA 178 BULKHEAD SKIN PANEL ALONG HORIZONTAL STIFFENER AT WL 218, ON LT SIDE. THE CRACKED AREA WAS CUT OUT. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-11 AND SRM 51-10-2.SDR CALA9601553Bulkhead Skin · crackedINSPECTION FOUND A .50 INCH CRACK IN STA 178 BULKHEAD SKIN AT WL 233.5 AND A 6 INCH CRACK WAS FOUND AT HORIZONTAL STIFFENER AT WL 218, RT SIDE. THE CRACKED AREAS WERE CUT OUT. FILLERS AND DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 53-10-11 AND SRM 51-10-2SDR USAA960719Bulkhead Skin · crackedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1. 5INCH CRACK BS 178 BULKHEAD SKIN LBBL 5 INCH WL 202. STOP DRILLED CRACK AND INSTALLED DOUBLER, REPAIRED PER T/R 53-10-11. (M)
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