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 AU981558Bulkhead · cracked(AUS) FORWARD FIN ATTACHMENT FITTING DOUBLER CRACKED. FOLLOWING REMOVAL OF THE DOUBLER, THE BULKHEAD P/N 62444-05 AT FS 228-30 WAS ALSO FOUND TO BE CRACKED.SDR ABXA9801148Bulkhead Web · corrodedDURING C-CHECK, FOUND LEFT PYLON BULKHEAD FORWARD LOWER SIDE CORRODED. REPLACED WEB ON PYLON BULKHEAD IAW DC9 SRM 51-30-2, 51-30-5, AND 51-30-1.SDR 98ZZZX4781Bulkhead · crackedDURING ROUTINE INSPECTION, THE FIREWALL WAS FOUND CRACKED AT THE UPPER PART OF THE LOWER FIREWALL JUST BEHIND THE COWL MOUNT AND AT THE COWL MOUNT JUST BELOW THE BATTERY BOX. THIS DEPARTMENT HAS NOTICED THE FIREWALL IS .016 INCH THICK WHICH IS THINNER THAN FISDR 98ZZZX4780Bulkhead · crackedDURING A ROUTINE INSPECTION, THE FIREWALL WAS FOUND CRACKED IN 3 PLACES. THE FIREWALL THICKNESS - .016 INCH WHICH IS THINNER THAN OLDER MODELS WHICH ARE BETWEEN .020 INCH AND .024 INCH. (IT IS DIFFICULT FOR AN ACCURATE MEASUREMENT TO BE TAKEN WITHOUT DISASSESDR CALA9802090Bulkhead Web · crackedINSPECTION FOUND A 6 INCH CRACK IN WEB SECTION AT TAIL COMPARTMENT CANTED BULKHEAD STA 1463. THE WEB SECTION WAS REMOVED AND REPLACED IAW SRM 51-30-2.SDR CKSA98671Bulkhead Ring · corrodedZONE 310, PRESSURE BLKHD STA 2360 WL 185 BL 0 TO RBL 6, THE AFT FACE OF RING SEGMENT 65B02634-328 HAS 4 SQUARE INCH AREA OF LEVEL 2 CORROSION. REPAIRED IAW ASA CKF-6XB-065 SUPP SHT 2, 3, 4. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, ANSDR ABXA9801086Bulkhead Fitting · crackedDURING C-CHECK, FOUND AFT PRESSURE BULKHEAD DOOR JAMB FITTING CRACKED JUST ABOVE DOOR WARNING SWITCH. REPLACED FITTING IAW DC9 SRM 51-30-5.SDR 9811429916Bulkhead Angle · crackedDURING M CHECK, FOUND T ANGLE CRACKED ON BULKHEAD FS 47 NEAR CENTER LINE. REPAIRED PER EA 99-159528.SDR SWAA982955Bulkhead Chord · crackedDURING SCHEDULED D CHECK, FOUND SIDE CHORDS CRACKED IN RADIUS OF CHORD AT BS 178, LBL 29 AND RBL 29, WL 207. REPLACED PER BOEING SRM.SDR SWAA982947Bulkhead · crackedDURING SCHEDULED 1/2 D CHECK, FOUND BS 178 BULKHEAD CRACKS AT WL 213, LBL 6.5. REPAIRED PER BOEING SRM.SDR SWAA982946Bulkhead · crackedDURING SCHEDULED 1/2 D CHECK, FOUND BS 178 BULKHEAD CRACKS AT WL 218, LBL 18-16. REPAIRED PER BOEING SRM.SDR AU981518Bulkhead · cracked(AUS) REAR BULKHEAD/FUSELAGE SHELL JOINT CRACKED. PART TC: 1,498.SDR 98FDEA00709Bulkhead Tee · crackedTEE CAP VERTICAL LEG BOTTOM ROW OF FASTENERS, DISCONTINUITY INDICATION LT SIDE. *S/D* REPAIRED 1156 BLKHD TEE CAP.SDR USAA980585Bulkhead · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND TWO CRACKS STATION 178 BULKHEAD APPROX 2 INCHES AT RBBL 5.7 WL 200 WEB ASSY. INSTALLED DOUBLER PER SRM 53-10-08 FIG 209. (M)SDR USAA980584Bulkhead · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND TWO CRACKS STATION 178 BULKHEAD APPROX 2 INCHES AT LOWER LEFT RADAR ANTENNA MOUNT WEB ASSY LBL 5.7 WL 200. INSTALLED DOUBLER PER SRM 53-10-08 FIG 209. (M)SDR SWAA982976Bulkhead · crackedDURING SCHEDULED D CHECK, FOUND BS 178 BULKHEAD CRACK AT WL 197-201, LBL 4.7, WL 210-212, LBL 6.7, WL 200-201, RBL 4.7. REPAIRED PER BOEING SRM.SDR ABXA9801169Bulkhead · crackedPRESSURE BULKHEAD FS 680, 16 INCHES FROM BOTTOM, TWO CRACKS, ONE RUNS HORIZONTALLY FROM CENTER TO THE RIGHT 18 INCHESLONG, AND SECOND RUNS FROM CENTER HORIZONTALLY TO THE LEFT 4.5 INCHES LONG. REPAIRED IAW DC8 SRM 53-2-5.SDR P2EA98285Web · crackedSJO - FUSELAGE BULKHEAD SKIN CRACKED AT BS 178, WL 219, RBL 15 INCH, DEFECT SIZE LENGTH 7 INCH. REPAIRED FUSELAGE WEB SECTION AT BS 178, FROM WL 210 TO WL 234, BETWEEN RBL 1.5 AND RBL 18 INCH PER SRM 53-10-11, FIG 1 SHEET 6, DETAIL III. (M)SDR MZZA98276Bulkhead Web · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, IG CORROSION WAS FOUND ON BS 1183 BULKHEAD FLOOR SHEAR WEB AT RBL 15. THE CORRODED WEB WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-2. (M)SDR MWEA981083Bulkhead Splice · crackedAFT CARGO COMPARTMENT AFB CORRODED, CRACKED, BULGED RIVETS BROKEN BELOW RT LAV L19R TO L27R. REMOVED AND REPLACED EXISTING FRAME REPAIR SPLICE RIGHT HAND STATION 817.SDR MWEA981082Bulkhead Angle · corrodedAFT CARGO COMPT APB CORRODED, CRACKED BULGED RIVETS BROKEN BELOW RT LAV L19R TO L27R. REMOVED AND REPLACED TEE FLOOR LEVEL SUPPORT ANGLE.SDR MWEA981081Blkhd Doubler · crackedAFT CARGO COMP AFT PRESSURE BULKHEAD IS CORRODED, CRACKED, BULGED RIVETS BROKEN BELOW RT LAV L19R TO L27R. REMOVED AND REPLACED FINGER DOUBLER AT STATION 817 AFT PRESSURE BULKHEAD RADIUS 16.SDR MWEA981080Blkhd Doubler · corrodedAFT CARGO COMPARTMENT APB CORRODED, CRACKED, GOUGED RIVETS BROKEN BELOW RT LAV L19R TO L27R. REMOVED AND REPLACED APB WEB DOUBLER AND TRIPLER AT RT STATION 817.SDR MWEA981079Bulkhead Tee · corrodedAFT CARGO COMPT APB CORRODED, CRACKED, BULGED RIVETS BROKEN BELOW RT LAV L19R TO L27R. REMOVED AND REPLACED TEE CHORD SECTION.SDR MZZA98266Bulkhead Plate · corrodedTNN - DUIRNG D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, TG CORROSION WAS FOUND ON BS 740 BULKHEAD LOWER WIRING ACCESS HOLE REINFORCEMENT PLATE. THE CORRODED WIRING ACCESS HOLE REINFORCEMENT PLATE P/N 69-64841-1 WAS REMOVED AND REPLACED WITH NEW REINFORCEMENTSDR 98FDEA00700Bulkhead Web · crackedWHILE WORKING NR 486 FOUND A CRACK IN 1183 BULKHEAD WEB AT RBL 12, WL 202. *S/D* REPAIRED BS 1183 BULKHEAD WEB PER SRM 53-10-9.SDR SWAA982894Bulkhead Angle · corrodedDURING SCHEDULED D-CHECK, FOUND CORRODED LT BULKHEAD SUPPORT ANGLE AT BS 520, LBL 26, WL 157. REMOVED AND REPLACED BULKHEAD SUPPORT ANGLE PER BOEING SRM.SDR SWAA982890Bulkhead Angle · corrodedDURING SCHEDULED D-CHECK, FOUND CORRODED ON RT BULKHEAD SUPPORT ANGLE AT BS 520, RBL 26, WL 157. REPAIRED PER BOEING SRM.SDR VJ9800646Bulkhead Angle · corrodedSCHEDULED INSPECTION, THE ANGLE ON THE PRESSURE BULKHEAD WAS FOUND CORRODED AT L30 FS966. GAINED ACCESS TO AREA, REMOVED AND REPLACED ANGLE. REINSTALLED ALL PARTS REMOVED FOR ACCESS IAW DC9 SRM 51-10-4, 51-30-2, 51-30-1, 51-10-3, AND SB53-147 PG 44.SDR DHL9980165CBulkhead · crackedAT C-CHECK, AFT FWD LOWER CARGO COMPT BULKHEAD ON STA 1320 SHOWS SEVERAL CRACK DAMAGES LT AND RT. STOP DRILLED CRACKS AND FABRICATED REPAIR DOUBLERS PER SRM 53-2-0.SDR AU981502Frame · cracked(AUS) FUSELAGE FRAME (BULKHEAD) ADJACENT TO THE HORIZONTAL STABILIZER FORWARD ATTACHMENT POINT CRACKED AT FRAME TO FUSELAGE SHELL JOINT. PART TC: 129.SDR ABXA9801132Bulkhead Bracket · crackedSTATION 640 BULKHEAD TO FUSELAGE ATTACH BRACKET CRACKED BETWEEN LONGERON -26L AND -27L FORWARD ACCESSORY COMPARTMENT. REPAIRED IAW DC8 SRM 53-2-0.SDR AU981445Bulkhead · cracked(AUS) FUSELAGE STRUCTURE CRACKED ON LT AND RT SIDES IN AREA ADJACENT TO THE FORWARD UPPER TAILPLANE ATTACHMENT AREA WHERE THE FUSELAGE SHELL JOINS THE BULKHEAD.SDR 98ZZZX4572Web · crackedDURING A ROUTINE INSPECTION, THE FIREWALL WAS FOUND CRACKED AT THE COWL MOUNT JUST BELOW THE BATTERY BOX. THE CRACK WAS APPROXIMATELY 4 INCHES IN LENGTH. SUBMITTER STATED POSSIBLE CAUSE AS USE OF A THINNER FIREWALL AND NO LOAD BEARING SURFACE FOR THE LORD MOSDR UPS98828151Rib · crackedINSPECTION TYPE:C LT WING L/E RIB CRACKED XFS 741.25. REPAIRED IAW SRM 57-2-0.SDR UPS98828146Rib · crackedINSPECTION TYPE-C, L/E RIB CRACKED LT XFS785 UPPER RIB LT WING. REPAIRED IAW SRM 57-2-0.SDR SWAA982747Bulkhead Strip · corrodedDURING SCHEDULED D-CHECK, FOUND CORRODED BULKHEAD SEAL RETAINING STRIP AT BS 1030, RBL 19, WL 209.5. REMOVED AND REPLACED PER BOEING SRM.SDR SWAA982746Bulkhead Strip · corrodedDURING SCHEDULED D-CHECK, FOUND CORRODED BULKHEAD SEAL RETAINING STRIP AT BS 1032, LBL 12, WL 209.5. REMOVED ADH REPLACED PER BOEING SRM.SDR UPS98228161Bulkhead Beam · crackedINSPECTION TYPE-C, CRACK FOUND ON VERTICAL BEAM AT RIGHT BUTTOCK LINE 26.83 AT BS 1183 BULKHEAD CRACK ON VERTICAL BEAM AT RBL 26.85, BS 1183 BULKHEAD REPAIRED IAW APPENDIX D OF B727-5311-0631.SDR UPS98228131Bulkhead · damagedINSPECTION TYPE-C, FWD PRESSURE BULKHEAD AND STIFFENERS FOUND DAMAGED BS 178 WL 200 RBL 5. REPAIRED IAW UPS EO B727-5310-4290 USING REPAIR KIT 65C36289-1.SDR DHL9872005DBulkhead · crackedAT D CHECK, RADOME HOLD OPEN RODS STOWAGE BRACKETS ARE CRACKED. NDT, FOUND CRACKS UNDER CLIPS. CUT OUT CRACKED ARES ON FWD BULKHEAD, INSTALLED FLAT PRESSURE WEB REPAIR PER SRM 53-10-3 AT RBL 11 WL 232, 4.5 BY 6. INSTALLED WEB REPAIR AT LB 11 WL 233, 5.5 BY SDR ABXA9800937Bulkhead Fitting · crackedDURING C-CHECK, FOUND THE VENTRAL DOOR LOWER, LEFT STOP SUPPORT FITTING CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-2 AND 51-30-5.SDR ABXA9800934Bulkhead Skin · crackedDURING C-CHECK, FOUND THE AFT SIDE OF THE AFT PRESSURE BULKHEAD SKIN CRACKED AT THE RIGHT SIDE OF VENTRAL DOOR CUTOUT APPROX 30 INCHES ABOVE FLOOR LINE. REPAIRED IAW DC9 SRM 53-05.SDR RRXA99986Bulkhead · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION, FUSELAGE, AFT PRESS BULKHEAD, AT STA= 1766. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIRED DOUBLER TO BULKHEAD WEB IAW FAA APPROVED TIMCOSDR VJ9800615Bulkhead · corrodedDURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL. THE 540 BULKHEAD WAS FOUND WITH CORROSION AT THE BOTTOM STRINGERS 26 AND 28R. REMOVED TWO EACH DOUBLERS, CUT OUT CORROSION. FABRICATED AND INSTALLED INNER DOUBLER AND TWO EACH DOUBLERS IAW B737 SSDR GAIA9894Bulkhead · damagedDURING HEAVY C-CHECK INSPECTION, FOUND A HOLE LOCATED AT FS 950, 10 INCHES ABOVE STRINGER 28 LEFT. THE HOLE WAS REPAIRED USING BOEING TELEX AOC-OKO-98-0080TR. THE AIRCRAFT WAS THEN RETURNED TO SERVICE. (M)SDR 99ZZZX436Bulkhead · crackedCRACKED BULKHEAD WEB AT FS 409. REF: SB 600-679. DATE SEPT 10, 1997. AD 97-24-02 AMEND 39-10209 EFFECT DATE 12-3-97. FS 409 REPAIRED ERGINEERING ORDER 600-53-175.SDR 9811399156Bulkhead · corrodedDURING M CHECK, FOUND CORROSION ON LOWER LEG OF BULKHEAD T CAP AT FS 642, STR 28R-29R, AROUND FASTENER. REPAIRED PER EA 91-159460.SDR SWAA982627Bulkhead · crackedDURING SCHEDULED SERVICE CHECK, FOUND AFT PRESSURE BULKHEAD CRACKED. REPAIRED PER BOEING SRM.SDR COMA9860332Bulkhead Angle · crackedBULKHEAD ANGLES AT FS 621 ARE CRACKED. REPLACED ANGLES.
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