JASC 5412
Service difficulty reports · 1,087
Reports filed under 5412 · Nacelle/Pylon, Bulkhead/Firewall, 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 = '5412' 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 = '5412' 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 CKSA97167Access Door · crackedDURING CPCP CHECK INSPECTION, FOUND NR 4 PYLON ACCESS DOOR 411 CRACKED AT SEVERAL FASTENER HOLES. REPAIRED IAW AIA SKETCH AIA/E/2505 SRM 51-1-8, 51-1-20D EA 97-013A. CORROSION TASK CARD NUMBER 84-1-0551. NON-ROUTINE TASK CARD NUMBER 93384.SDR 9716996642Bulkhead · crackedDURING M-CHECK AND PRIOR TO SERVICE, FOUND CRACKS EXTENDING FROM FASTENER HOLE AT RIGHT TOP OF REAR ENGINE MOUNT BULKHEAD FRAME NAC STA 222, NR 2 PYLON. REPAIRED PER EA 66-120348.SDR 97FDEA00157Bulkhead Plate · misinstalledVCE: N0151. NR 3 PYLON FRONT SPAR BULKHEAD LOWER PLUG PLATE P/N AUB7125-1 INCORRECTLY INSTALLED - BEVELED SIDE FACING FORWARD INSTEAD OF AFTWARD. *** S/D *** COMING.SDR 97FDEA00156Bulkhead Plate · misinstalledVCE: N0150. NR 1 PYLON FRONT SPAR BULKHEAD LOWER PLUG PLATE P/N AUB7125-1 INCORRECTLY INSTALLED - BEVELED SIDE FACING FORWARD INSTEAD OF AFTWARD. *** S/D *** COMING.SDR 97ZZZX2559Blkhd Frame Tie · crackedRIGHT SIDE FORWARD FACE OF PYLON BULKHEAD FRAME TIE AT STA 1116 STR 14 HAS ONE INCH CRACK. FABRICATED AND INSTALLED REPAIR PART PER SRM 53-03, FIG 6 AND SRM 51-30-2. TOTAL TIME: 29,567. TOTAL CYCLES: 73,626. REFERENCE: NR B021718N00346.SDR ABXA9700816Bulkhead Web · crackedDURING C-CHECK, THE LT ENGINE PYLON BULKHEAD WEB STA 965 WAS FOUND CRACKED. THE WEB WAS REPLACED IAW DC9 SRM 51-30-2.SDR DLM11970065Bulkhead Web · crackedON WALKAROUND INSPECTION, FOUND NR 3 PYLON CAP WRINKLED. FURTHER INSPECTION REVEALS INTERNAL WEB CRACKED AT PYLON STA YN 286 (P/N AVB7540) REF SRM 54-51-02 FIG 2 PAGE 5 VOL III ITEM 8.SDR 97FDEA00029Bulkhead Web · crackedNR 1 PYLON NAC STA 286.0 BULKHEAD AFTER REMOVAL OF OTBD PYLON SKIN, CRACKS WERE DISCOVERD ON BOTH FWD AND AFT BULKHEAD WEBS. ALSO, EXTENSIVE CORROSION DAMAGE AND SIGNIFICANT MATERIAL LOSS IN STEEL FRAME. *S/D* REMOVED DAMAGED MEMBERS AND FABRICATED NEW PARTSDR 97FDEA00028Bulkhead Web · crackedAT NR 3 PYLON NAC. STA 286.0 BULKHEAD, AFTER REMOVAL OF OUTBOARD PYLON SKIN FOR REPAIR, INSPECTION REVEALED A CRACK IN THE AFT WEB OF THE 286.0 BULKHEAD. REPAIRED CRACKED WEB OF STA 286 BULKHEAD I.A.W. FED-EX ERA B-54-10-78 DATED 01/23/97.SDR 9627736613Bulkhead Chord · crackedDURING CHECK, FOUND NR 4 STRUT AFT BULKHEAD VERTICAL T-CHORD CRACKED VERTICALLY TWO INCHES FROM TOP RIGHT SIDE. REPLACED VERTICAL T-CHORD PER EA 66-120269 AND EA 66-120281.SDR 96UAL900956Bulkhead Fitting · loose fastenersDURING ROUTINE ENGINE CHANGE ON NR 4 ENGINE FOUND 4 LOOSE FASTENERS ON THE PYLON FWD ENGINE MOUNT FITTING INBOARD SIDE COMMON TO THE BULKHEAD. INSTALLED NEW FASTENERS. ADJACENT FASTENERS WERE INSPECTED WITH NO DEFECTS NOTED. BOEING S/B 747-54A2069 WAS PREVISDR ABXA9700292Bulkhead Clip · crackedDURING C-CHECK, A CLIP ON THE LT PYLON BULKHEAD STA 965, WAS FOUND CRACKED. THE CLIP WAS REPLACED IAW DC SRM.SDR ABXA9700249Bulkhead Clip · crackedDURING C-CHECK, A CLIP WAS FOUND CRACKED AT THE PYLON BULKHEAD STATION 965 LONGERON 17 RT, NR BF-600. THE CLIP WAS REPLACED IAW DC9 SRM.SDR MALA965173Firewall Doubler · crackedDURING MAINTENANCE IN MSP, FOUND RIGHT FIREWALL DOUBLER CRACKED AT UPPER OUTBOARD SIDE ABOVE TOP ENGINE HARNESS CANNON PLUG CONNECTOR .375 INCH LONG. REPAIR COMPLETED PER EA 01-96110 DATED 10/27/96. (M)SDR CALA9700023Bulkhead Chord · crackedINSPECTION FOUND A .125 INCH CRACK AT FASTENER HOLE COMMON TO THE AFT BULKHEAD VERTICAL CHORD LT FITTING OF NR 2 PYLON. THE CHORD ASSEMBLY WAS REPLACED IAW BOEING DRAWING 65B90413 AND SRM 51-10-01.SDR CALA9700020Bulkhead · crackedINSPECTION FOUND A .125 INCH CRACK AT NR 3 PYLON FASTENER HOLE COMMON TO THE AFT BULKHEAD VERTICAL CHORD LT FITTING. THE NR 3 PYLON LT BULKHEAD ASSEMBLY WAS REPLACED IAW SRM 51-10-01 AND BOEING DRAWING 65B90413.SDR CALA9700019Bulkhead · crackedINSPECTION FOUND A 2 INCH CRACK AT UPPER POSITION OF NR 4 PYLON AFT BULKHEAD INBOARD CHORD. THE CHORD AND AFT BULKHEAD ASSEMBLY WERE REPLACED IAW SRM 57-10-01 AND SB 747-54A2159.SDR TWRA96338Bulkhead · crackedNR 3 ENGNIE PYLON REAR TORQUE BULKHEAD T-CHORD CRACKED THROUGH ON LEFT AND RIGHT SIDES APPROXIMATELY 60 TO 8 INCHES LONG IN RADIUS. REPLACED T-CHORD ASSEMBLY ON LEFT AND RIGHT SIDES, IAW SRM 51-10-01/51-30-02. (M)SDR 97ZZZM88Chord · crackedNR 3 ENGNIE PYLON REAR TORQUE BULKHEAD T-CHORD CRACKED THROUGH ON LEFT AND RIGHT SIDES APPROXIMATELY 60 TO 8 INCHES LONG IN RADIUS. REPLACED T-CHORD ASSEMBLY ON LEFT AND RIGHT SIDES, IAW SRM 51-10-01/51-30-02. REFERENCE TWRA96338.SDR 9621656613Bulkhead Fitting · crackedDURING P-CHECK, FOUND A CRACK IN THE NR 3 PYLON AFT ENGINE MOUNT BULKHEAD TO FRONT SPAR ATTACH FITTING AT NACELLE STA 221. REPLACED FITTING (P/N 65B91314-3).SDR 9621636613Bulkhead Web · crackedDURING P-CHECK, FOUND A 1.5 INCH CRACK IN THE NR 1 PYLON LOWER BULKHEAD WEB AT NACELLE STA 210. REPAIRED WEB PER EA 66-106410.SDR MALA965128Firewall · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND 0.500 INCH TRANSVERSE CRACK IN RT FIREWALL. APPROXIMATE LOCATION IS BL 6.00 AND WL 91.00. STOP DRILLED CRACK, FABRICATED AND INSTALLED A 0.020 INCH STAINLESS REPAIR DOUBLER (3.50 INCH BY 1.20 INCH) IAW SDR UPS96221115Intercostal · crackedINSPECTION TYPE-SP, CRACK ACROSS 2 RIVET HOLES ON FLANGE OF HORIZONTAL INTERCOSTAL ON NR 2 ENG FIREWALL 4TH FWD FROM REAR ENG MT. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 54-10-3 FIG 2 AND 54-10-3 FIG 1.SDR 96ZZZX5754Firewall · crackedFIREWALL CRACKED.SDR 96ZZZX5753Firewall · crackedFIREWALL CRACKED.SDR 96ZZZX4703Web · crackedINSPECTION FOUND A CRACKED WEB AT BOTH ENGINE FIREWALLS AT ENGINE MOUNT AREA.SDR MWEA96323Firewall · crackedDURING D-CHECK, RT PYLON WAS FOUND TO HAVE SMALL CRACK IN LWR FWD CORNER OF ANGLED FIREWALL INBD OF AFT ENGINE ISOLATOR. FABRICATED A REPAIR AND INSTALLED IAW SRM 51-20-3 AND 54-01, FIG 2 SHEET 4.SDR UPS96420813Fire Wall · crackedINSPECTION TYPE: C. PYLON NR 3, FOUND VERTICAL FIRE WALL AT NAC STA 180 CRACKED AT LT TOP CORNER (CRACK IS 1.5 INCHES LONG). REPLACED FIRE WALL IAW SRM 51-30-02.SDR 96ZZZX4220Firewall · chafe/burnedWHILE PERFORMING SB A604-27-002, THE RT LOWER PYLON PANEL HEAT SHIELD HAD EVIDENCE OF ELECTRICAL SHORT DAMAGE. UPON FURTHER INVESTIGATION, RT ENGINE GENERATOR WIRE HARNESS WAS FOUND NEARLY SEVERED FROM CHAFING ON THE HEAT SHIELD. THE CLAMP SECURING THE WIRE SDR AU961090Firewall · damaged(AUS) VERTICAL FIREWALL LOWER DIAGONAL CENTRAL TUBE AND ATTACHING DOUBLERS SEPARATED FROM FIREWALL DURING HARD LANDINGSDR 96FDEA01237Bulkhead · crackedNR 2 ENGINE INTAKE FWD BULKHEAD STA 31.8 HAS SEVERAL CRACKS AT THE FOLLOWING POS; 5 O'CLOCK, 5:45, 6:15, 8:30 AND 9 O'CLOCK POSITION. REMOVED AND REPLACED LEFT AND LOWER WEB SECTIONS PER SRM 54-10-00.SDR 96FDEA01268Blkhd Stiffener · crackedDISCREPANCY: NR 2 ENGINE NOSE COWL BLKHD STIFFENER ON D-DUCT WEB CRACKED AT 10 O'CLOCK POSITION. REFERENCE: FCD 08-55-005 SNRM 4225. CORRECTIVE ACTION: REMOVED STIFFENER, WELDED CRACK, AND RE-INSTALLED STIFFENER PER SRM 57-00-00.SDR BTHA96001Firewall · crackedDURING INSPECTION FIREWALL WAS FOUND CRACKED BETWEEN LOWER RIGHT ENGINE MOUNT ATTACH POINT AND COWLING FLANGE. CRACK WAS 2.50 INCHES LONG AND RAN HORIZONTALLY. SUBMITTER SPECULATES CAUSE WAS AGE OF PART. RECOMMEND CLOSE AND DETAILED INSPECTION OF THIS AREA SDR 96ZZZX4186Fastener · failedDZUS FASTENER FOR ENGINE FIREWALL FAILED CAUSING FOD DAMAGE TO NR 2 ENGINE. ENGINE WAS SHUT DOWN IN-FLIGHT. AIRCRAFT LANDED SAFELY. REPLACED NR 2 ENGINE DUE TO DAMAGE TO COMPRESSOR AND TURBINE DAMAGE.SDR 96FDEA01000Blkhd Stiffener · crackedSNRM 4259. BULKHEAD STIFFENER CRACKED AT THE NR 2 ENGINE NOSE COWL L/E AS SEEN THROUGH ACCESS PANEL NR 361FL. S/D COMING.SDR CA960610001Firewall · corroded(CAN) DURING AN ENGINE CHANGE, FIREWALL WAS FOUND TO BE CORRODED EXCESSIVELY. FIREWALL WAS REPLACED AS PER MAINTENANCE MANUAL. SUBMITTER NOTES THAT THE MATERIAL OF THE FIREWALL IS GALVANIZED STEEL.SDR 96FDEA00951Bulkhead · loose boltsNR 1 ENG PYLON AFT BULKHEAD AFT FACE TWO ATTACH BOLTS ARE LOOSE AT UPPER AREA. REMOVED BOLTS FOR INSPECTION AND CLEANED BOLT HOLES. COMPLIED WITH HFEC INSPECTION ON 2 BOLT HOLES, NO DEFECTS NOTED. INSTALLED AND TORQUED BOLTS PER MM 20-50-02.SDR 96FDEA00950Bulkhead · loose screwsNR 1 ENG PYLON I/B SIDE AFT BULKHEAD AREA, THERE ARE 8 LOOSE TRI-WING SCREWS ON STA YN 417.212. REMOVED BOLTS FOR INSPECTION AND CLEARED BOLT HOLES. COMPLIED WITH HFEC INSPECTION ON 8 BOLTS HOLES, NO DEFECT NOTED. INSTALLED BOLTS AND TORQUED PER MM 20-50-02SDR 96ZZZX2235Firewall · crackedTHE LT AND RT ENGINE FIREWALLS FOUND TO HAVE CRACKS IN THE ALUMINUM PORTION OF FIREWALL AT THE AFT ENGINE MOUNT UPPER ATTACH FASTENERS DURING OTHER MAINTENANCE REQUIRING THE LOWER AFT NACELLES TO BE REMOVED. WITH THE NACELLES REMOVED, THE CRACKS ARE VISIBLE. SDR 96ZZZX1807Bulkhead · crackedTHE RT PYLON SUPPORT IS CRACKED 14.50 INCHES FROM THE FORWARD TRANSMISSION ISLAND AFT. THE CRACK WAS DISCOVERED DURING REPLACEMENT OF THE RT CYCLIC SERVO. THE FOLLOWING COMPONENTS OF THE PYLON STRUCTURE WERE CRACKED: BEAM (W.O. 65.00). PYLON SUPPORT ASSY, RSDR ABXA9600368Firewall · crackedDURING C-CHECK INSPECTION, DISCOVERED NR 1 PYLON LOWER FORWARD FIREWALL CRACKED. REPAIRED NR 1 PYLON LOWER SPAR WEB ON FORWARD FIREWALL THAT WAS CRACKED IAW ABX REA D854-13627MR.SDR AU960281Bulkhead · cracked(AUS) FIREWALL AND LH BULKHEAD CRACKED AT EXHAUST MOUNT ATTACHMENT - AIRCRAFT IS USED AS A FLOAT PLANESDR AU960280Bulkhead · cracked(AUS) FIREWALL AND RH BULKHEAD CRACKED IN AREA OF EXHAUST MOUNT ATTACHMENT - AIRCRAFT IS USED AS A FLOAT PLANESDR 96ZZZM791Blkhd Web · crackedDURING OP-15, FOUND A SIX INCH CRACK AT LOWER OUTBOARD CORNER OF RIGHT FORWARD ENGINE MOUNT BULKHEAD WEB, STATION 965. REPAIRED PER SRM 53-03, FIGURE 21.SDR 9604699853Bulkhead · crackedDURING LINE CHECK, FOUND A CRACK IN THE NR 2 ENGINE PYLON OUTER BULKHEAD. REPAIRED BULKHEAD (P/N 9958159-62) PER EA 98-099525.SDR UPS96805690Blkhd Lwr Cap · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED NR 3 PYLON I/B SUPPORT BULKHEAD FWD LOWER CAP HAS A 17 INCH LONG CRACK. REPAIRED PER UPS EO DC8-57-0647.SDR SWAA960075Blkhd Angle · crackedDURING SCHEDULED 1/2 D-CHECK, FOUND NUMBER 2 ENGINE PYLON, UPPER FWD BULKHEAD WEB TO SKIN ATTACH ANGLE CRACKED AT FWD FASTENER STA 222.7. REPAIRED PER SWA RA 1-257-030.SDR CAL960154Firewall · crackedIAH - INSPECTION FOUND THE NR 2 ENGINE PYLON FIREWALL PAN HAD A 2.5 INCH CRACK THROUGH FOUR FASTENERS AT NAC STATION 144. A DOUBLER WAS INSTALLED IAW ECRA 5450-01139. A DIP WAS ISSUED TO REINSPECT THE AREA AT LPV CHECKS AND PERMANENTLY REPAIR PAN AT NEXT 1/4SDR 96ZZZX833Gasket · wrong partINTERNAL GASKET, PN 2519216-17, WAS INSTALLED ON THE EXTERNAL SIDE OF THE LT PYLON FIREWALL. EXTERNAL GASKET, PN 2452012-1, SHOULD HAVE BEEN INSTALLED. DUE TO THIS INSTALLATION AND THE NATURAL DETERIORATION OF THESE GASKETS, SEVERE FIREWALL DAMAGE OCCURRED. SDR ABXA9600410Web · crackedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE PYLON BULKHEAD AT FS 965 CRACKED JUST ABOVE THE FLOOR LINE AT LBL 50. REPLACED PYLON BULKHEAD WEB IAW DC-9 SRM CHAPTERS 51-30-1, 51-30-2 AND 51-30-5.
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