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 DL73S030113Bulkhead · canningINSPECTION OF THE AFT P-DOME REVEALED A 10 X 8 X .25 INCH OIL CAN IN THE LOWER WEB AREA OF NEAR BL 0. THE OIL CAN WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN ALUMINUM REPAIR DOULBER PER BAC S/B 737-53A1075 AND ER/A 384318-14AD.SDR AALA20030120Bulkhead · crackedTUL - FOUND MID BULKHEAD OUTBOARD FORWARD HOLE CRACKED. REPAIRED MID BULKHEAD PER ECO 90309 DATED 1/27/2003. (M)SDR 2003UALA00110Bulkhead · crackedBS 178 BULKHEAD WEB CRACKED AT LOWER LT RADAR MOUNT. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.SDR 2003UALA00109Bulkhead · cracked178 BULKHEAD, FORWARD WEB, LOWER RADOME MOUNT RT, CRACKED AT UPPER INBOARD END. MAJOR REPAIR ACCOMPLISHED. INSTALLED FILLER AND DOUBLER.SDR 2003UALA00099Bulkhead · dentedSTATION 178 BULKHEAD FORWARD WEB HAS A DENT NEXT TO UPPER RADOME MOUNT ON OUTBOARD SIDE. MAJOR REPAIR ACCOMPLISHED. FILLER AND DOUBLER INSTALLED.SDR P5CA0300809Bulkhead · crackedFWD PRESSURE BULKHEAD FOUND CRACK ON F/S 1HR 12:30 O'CLOCK. DAMAGED AREA TRIMMED OUT, REINFORCED AREA WITH STRAP & DOUBLER PER SRM 51-40-03 FIG-2.SDR P5CA0300748Bulkhead · crackedCRACK FOUND FWD PRESSURE BULKHEAD OF F/S 140, 12:20 O'CLOCK. DAMAGED AREA TRIMMED OUT. REINFORCED AREA W/ STRAP & DOUBLER PER SRM 54-40-03, FIG. 2.SDR QXEA0300238Bulkhead · damagedPDX- AFT PRESSURE BULKHEAD FEED THROUGH ORIFICE FOR NR 2 HYDRAULIC EDP PRESSURE LINE IS ELONGATED. REPAIRED IAW REO 670-53-61-034 AND 670-53-51-034.SDR AWXA200300132Web · crackedYVR - MAJOR REPAIR - DURING C-14 CHECK 2 EACH 1/2" CRACKS WERE FOUND ON 178 BULKHEAD RADAR ANTENNA ATTACH BRACKET, R/H SIDE AT UPPER INBOARD AND OUTBOARD ATTACH POINTS. MAINTENANCE STOP DRILLED CRACKS ON 178 BULKHEAD RADAR ANTENNA ATTACH BRACKET, R/H SIDE AT SDR AWXA200300116Bulkhead · crackedYVR - MAJOR REPAIR - DURING C-14 CHECK 3 EACH .2500 INCH CRACKS WERE FOUND ON 178 FORWARD BULKHEAD, LEFT SIDE, WL 213, LBL 11. MAINTENANCE STOP DRILLED CRACKS, ENLARGED HOLES, AND PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED DOUBLERS AND FILSDR SWAA030182Bulkhead · crackedDURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED AT BS 178, WL 234. REPAIRED BULKHEAD WEB PER SRM.SDR 2004F00027Bulkhead · crackedMAINTENANCE DISCOVERED MULTIPLE CRACKS ON THE FORWARD PRESSURE BULKHEAD, LOWER RT CORNER OF P/N 114-410026-6 WEB ASSY, AT THE UPPER END OF STIFFENER P/N 114-410026-55 AND AT STATION 84. THIS CRACK WAS APPROX 2 INCHES LONG. ANTICIPATE FINDING THAT THERE WAS ASDR ILPA048FPressure Panel · crackedDURING ROUTINE INSPECTION OF THE RIVETS AT THE FORWARD PRESSURE BULKHEAD, TWO SEPERATE CRACKS WERE NOTED IN THE LT DISHPAN JUST FORWARD OF THE PILOTS RUDDER PEDALS. THE CRACKS WERE BETWEEN FASTENERS. THE PN S25-8FN323-1 WAS REMOVED & REPLACED IN ACCORDANCE WITSDR LR7A03004Skin · crackedDURING SCHEDULED B1 INSPECTION PER JOB CARD HB3202 FOUND RMLG BAY SIDEWALL SKIN CRACKED .25 IN. AT FS 478, RBL 61, WL 170.REPLACED SKIN PANEL FS 477 TO 517 AND WL 150 IAW SRM SMP 583 53-40-02 AND DWG 34203. NR 0096.SDR DLM88030083Bulkhead · gougedFUSELAGE / BULKHEAD / NLG WHEEL WELL / RH SIDEWALL / FS 94 :WEB REPAIR THE WEB OF THE RH NOSE LANDING GEAR WHEEL WELL BULKHEAD WAS GOUGED BY A GEAR STEARING ACTUTATOR DURING A GROUND TUG OPERATION. THE SDR 2003FA0000206Bulkhead · crackedSMALL CRACK IN AFT BULKHEAD AT STA 209. ORIGINATING FROM UNDER THE ATTACH POINT OF RIGHT HORIZONTAL STABILIZER, ATHE THE UPPER INBOARD CORNER.SDR 2003FA0000047Bulkhead · crackedSMALL CRACK IN AFT BULKHEAD AT STATION 209. ORIGINATING FROM UNDER THE ATTACH POINT OF RT HORIZONTAL STABILIZER, AT THE UPPER INBOARD CORNER.SDR 2003F00269Frame · crackedAT C-CHECK, FOUND NR 2 ENGINE BULKHEAD AT FUSELAGE STATION 1342, ENGINE COWL LIP SEAL CRACKED FROM 1 O'CLOCK TO 4 O'CLOCK POSITION. INSTALLED NEW COWL SEAL RETAINER NR 2 ENGINE AT FUSELAGE STATION 1342, STRINGER 6L TO STRINGER 6R. (M)SDR CA030220003Bulkhead · cracked(CAN) CREW REPORTED ON LAST LEG TO AIRPORT, LOW PRESSURIZATION OF 3.2 PSI. DURING TROUBLESHOOTING FOUND A CRACK FOUR INCHES LONG ON BULKHEAD. LOCATION - CENTER OF FUSELAGE AT STATION 227.125.SDR 2004F00011Bulkhead · crackedON OPERATIONAL CHECK FLIGHT FOR PRESSURIZATION CHECKOUT, AIRCRAFT FAILED TO MAINTAIN MAXIMUM CABIN PRESSURE ON SINGLE ENGINE BLEED AIR. MAINT DISCOVERED MULTIPLE CRACKS ON FORWARD PRESSURE BULKHEAD, LOWER RT CORNER OF P/N 114-410026-6, WEB ASSY AT UPPER END OFSDR QXEA0300139Bulkhead · crackedCKB- CRACK INDICATED ON PRESSURE BULKHEAD AT STATION 1098.20 ON RIGHT HAND SIDE. REPAIRED IAW CRJ SRM 51-20-06, 51-21-16, 51-23-00, 51-42-21 AND REO 670-53-61-034.SDR C2XA02SH180Firewall · crackedSHV-DURING C CHECK APU FIREWALL WAS FOUND TO HAVE A CRACK AT FAR RIGHT FASTENER HOLE OF 2ND HORIZONTAL REINFORCEMENT FROM TOP. MAINTENANCE STOP DRILLED CRACK AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5330-01202. THE AIRCRAFT WAS APPROVED TO RETSDR C2XA02SH178Firewall · crackedSHV-DURING C CHECK APU FIREWALL WAS FOUND TO HAVE A CRACK AT TOP 2 RIVETS OF R/H VERTICAL REINFORCEMENT. MAINTENANCE STOP DRILLED CRACK AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5330-01202. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR 2003UALA00065Pressure Panel · crackedNOSE LANDING GEAR WHEEL WELL UPPER WEB AND UPPER AFT CHORD ANGLE PUNCTURED AND CRACKED, RBL 24 STA 294. MAJOR REPAIR ACCOMPLISHED. REPLACED CHORD ANGLE. WEB REPAIRED BY INSTALLING DOUBLER.SDR TSAA0351029Pressure Panel · corrodedFABRICATED NEW PRESSURE WEB REPAIR DOUBLER. ALODINED AND PRIMED ALL BARE ALUMINUM. FAY SURFACE SEAL INSTALLED REPAIR DOUBLER WITH BMS 5-95 AND FASTENERS IDENTIFIED. APPLIED CORROSION INHIBITING COMPOUND TO THE INTERNAL SURFACES. REPAIR COMPLETED IAW ECO 33SDR UPS03240053Panel · crackedINSPECTION TYPE: C, SUSPECT CRACK IN NLG WHEEL WELL STA 245 LT SIDE PANEL. REPAIR CARRIED OUT IAW SRM 51-40-2.SDR 2003FA0000055Bulkhead · crackedSMALL CRACK IN AFT FUSELAGE BULKHEAD AT STATION 209. ORIGINATING FROM UNDER THE RT HORIZONTAL STABILIZER UPPER ATTACH POINT.SDR 2003FA0000054Bulkhead · crackedSMALL CRACK IN AFT FUSELAGE BULKHEAD AT STATION 209. ORIGINATING FROM UNDER THE RIGHT HORIZONTAL STABILIZER UPPER ATTACH POINT.SDR QXEA0300095Angle · crackedPDX- FORWARD PRESSURE BULKHEAD BOTTOM CONNECTION ANGLE HAS A THREE INCH LONG CRACK IN RADIUS, AFT SIDE OF BULKHEAD FS1550 THROUGH THREE INCHES LEFT OF BL0. REPAIRED IAW FOKKER SRM 53-02-18 AND HORIZON AIR EA 4-53-1578.SDR QXEA0300094Angle · crackedPDX- FORWARD PRESSURE BULKHEAD BOTTOM CONNECTION ANGLE HAS A THREE INCH LONG CRACK IN RADIUS, AFT SIDE OF BULKHEAD FS1550 THROUGH 3 INCHES LEFT OF BL0. REPAIRED IAW FOKKER SRM 53-02-18 AND HORIZON AIR EA 4-53-1578.SDR AWXA200300064Bulkhead · crackedDURING C-14 CHECK A 1/2 INCH CRACK WAS FOUND ON AFT SIDE OF BULKHEAD WEB BS 178, RBL 4.7, WL 198.5, CONFIRMED BY HFEC. MAINTENANCE CUTOUT DAMAGED AREA OF WEB AND PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR DOUBLER; INSTALSDR AWXA200300063Web · crackedDURING C-14 CHECK A 1/2 INCH CRACK WAS FOUND ON AFT SIDE OF BULKHEAD WEB BS 178, LBL 4.7, WL 201, CONFIRMED BY HFEC. MAINTENANCE CUTOUT DAMAGED AREA OF WEB AND PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR DOUBLER AND FILLESDR AWXA200300079Bulkhead · crackedDURING C-14 CHECK A 1 INCH CRACK WAS FOUND BS 178 BULKHEAD WEB, LBL 5.7, WL 212.5. MAINTENANCE REMOVED STIFFENER AND "L" ANGLE TO ACCESS DAMAGE; CUTOUT CRACKED AREA OF BS 178 BULKHEAD WEB, LBL 5.7, WL 212.5; PERFORMED A HFEC INSPECTION OF CUOUT TO VERIFY NO CRSDR 2003UALA00042Pressure Panel · crackedPRESSURE DECK ABOVE LEFT WING WEB WAS CRACKED AT STA 663 LBL 33. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.SDR DLM88030041Bulkhead · damagedDURING HMV-2, TOOLING DAMAGE WAS FOUND ON THE VERTICAL FLANGE OF PN 5910130387 AFT PRESSURE BULKHEAD TEE CAP AT STA 1338 BETWEEN L-29L TO L-29R, AND ON PN 5910130285 PRESSURE BULHHEAD WEB. THE TEE CAP WAS SPICED PER MD80 SRM 53-03, FIG 37. THE WEB WAS REPAIREDSDR 2003UALA00031Bulkhead · crackedSTATION 178 BULKHEAD WEB CRACKED AT RIGHT LOWER RADAR MOUNT INBOARD UPPER SIDE. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR.SDR 2003UALA00030Bulkhead · crackedSTATION 178 BULKHEAD WEB CRACKED AT RBL 1 IN WL 188. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR.SDR SWAA030038Web · crackedDURING SCHEDULED BC CHECK, FOUND NLG WHEEL WELL RT SIDE WEB CRACKED AT BS 259, WL 174. REPAIRED WEB PER SWA EA.SDR SWAA030039Pressure Panel · crackedDURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESS WEB CRACKED AT BS 663, RBL 39.5. REPAIRED WEB PER SWA EA.SDR DHL2003753502Pressure Panel · crackedDURING "C" CHECK, NOSE SECTION LOWER LOBE INTERIOR PRESSURE WEB AT BS 294. PREVIOUS CRACK REPAIR DO NOT MEET SRM. REMOVED PREVIOUS REPAIR AT NOSE SECTION LOWER LOBE INTERIOR PRESSURE WEB, BS 294 IAW B-727, SRM 51-30-2. CUT OUT DAMAGED IAW B727 SRM 51-40-2, RSDR CALA0300005Pressure Panel · crackedINSPECTION FOUND AN 8 INCH CRACK IN LT MAIN WHEEL WELL PRESSURE DECK WEB AT STA 664-675. THE AREA WAS REPAIRED IAW SRM 53-60-51.SDR CA030114007Bulkhead · cracked(CAN) DURING SHEDULED MAINTENANCE DISCOVERED FLEXING UNDER THE DOOR SNUBBER ATTACH BRACKET WHEN OPENING AND CLOSING THE CABIN DOOR. INSPECTION REVEALED CRACKING IN BULKHEAD AND SKIN AT FS 215 REPAIRS CARRIED OUT IAW REPAIR DESIGN CERTIFICATE C-RA02-425/D.SDR LR7A02127Splice Plate · crackedDURING SCHEDULED C3 INSPECTION PER JOB CARD HSP53224 FOUND LH FS 497 BULKHEAD FITTING DOUBLER CRACKED AT LBL 50, WL 267.REPLACED SPLICE PLATE IAW SRM SMP 583 51-70. NR 2064.SDR ASAA0280706Bulkhead · crackedOKC - FOUND DURING 30K CHECK, BULKHEAD SUPPORT CRACKED IN MID CARGO BAY AT FS 529. REPLACED BULKHEAD PER SRM 51-10-4 AND 51-30-2. (M)SDR 2002UALA01873Bulkhead · dentedAFT PRESSURE BULKHEAD, RIGHT FORWARD CIRCUMFERENTIAL STRAP BULKHEAD DENTED AT FASTENERS. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED AND INSTALLED DOUBLER REPAIR.SDR AWXA200300009Web · crackedMCN - MAJOR REPAIR - DURING C-16 CHECK HFEC INSPECTION INDICATED A 1/4" CRACK ON BS 178 BULKHEAD WEB, WL 234, RBL 9, AT BUTTON HEAD HILOC FASTENER HOLE. MAINTENANCE REMOVED FASTENER, AND CUTOUT CRACKED AREA OF BULKHEAD WEB AT BS 178, WL 234, RBL 9; PERFORMED ASDR AUS20021433Bulkhead · damaged(AUS) REAR PRESSURE BULKHEAD DAMAGED ON LT SIDE. A GOUGE WAS FOUND ON A LAP JOINT OF A WEB DOME CLOSE TO S-15L.SDR DL73K021447Bulkhead · corrodedFUSELAGE / AFT PRESSURE BULKHEAD / FS 1016 / BL 0 : CORROSION REPAIR THE AFT PRESSURE BULKHEAD WEB AND STIFFENER AT BL 0 WERE FOUND CORRODED. THE CORROSION IS TYPICAL OF BAC S/B 737-53A1075 AND AD 2002-10-SDR SWAA022925Bulkhead · crackedDURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED AT BS 178, WL 222 AND LBL 2 TO LBL 3. REPAIRED BULKHEAD WEB PER BFG ER.SDR CA030103007Bulkhead · cracked(CAN) WHILE CONDUCTING A STRUCTURAL INSPECTION, BULKHEAD AT STATION 236.5 WAS FOUND CRACKED WHERE IT JOINS WITH RT SIDE FRAME BETWEEN RT STRINGER NR 12 AND 13. FRAME/BULKHEAD REPAIR CARRIED OUT IN ACCORDANCE WITH RAYTHEON FIELD REPAIR FR-KA-00814.
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