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 QXEA0300155Firewall · crackedPDX- LEFT HAND FIREWALL HAS TWO CRACKS AT INBOARD SIDE NEAR THREE O'CLOCK POSITION NEAR ENGINE EXHAUST PIPE. REPAIRED IAW DHC-8 SRM 51-00-06 AND RD 8-54-806.SDR 2003F00270Frame · crackedAT C-CHECK, FOUND NR 2 ENGINE FORWARD BULKHEAD, ENGINE COWL LIP SEAL, CRACKED AT FUSELAGE STATION 1342, 6 O'CLOCK POSITION. INSTALLED NEW COWL SEAL RETAINER, NR 2 ENGINE, STRINGER 6L TO STRINGER 6R. (M)SDR P5CA0300730Support Angle · crackedCRACK APPROX. 2-3/4" FOUND #4 PYLON AFT ENG. BULKHEAD FRAME AT NAC STA 221.90 MID SPARE WEB LWR LATERAL SUPPORT ANGLE AT MID SECTION & JOINTING 3 FASTENERS. REPLACEMENT OF CRACKED LATERAL SUPPORT ANGLE CARRIED OUT PER SRM 51-10-01.SDR ALG2003F0218Channel · crackedDURING DAILY INSPECTION, 3 INCH CRACK IN RADIUS OF CHANNEL, WAS FOUND. CRACK STARTS BOTTOM OF CHANNEL AND GOES UP 3 INCHES JUST ABOVE RECEPTACLE DOUBLER. C/A: INSTALL STAINLESS STEEL DOUBLER.SDR HEEA083708Firewall · crackedENGINE BAY FIREWALL CRACKED.SDR AMTA200300189Bulkhead · gougedNR 1 PYLON STRUT STRUCTURE MID-BULKHEAD FITTING WEB GOUGED. REPAIRED WEB IAW ER/A 757-54R-5041. (M)SDR FFS2003F00006Seal · misalignedDURING INSPECTION OF THE RT FORWARD COWLING ASSEMBLY, IT WAS FOUND THAT THE AFT BULKHEAD HAD CRACKED AT THE LOWER MOUNT HOLES. WHEN THIS BULKHEAD IS BOLTED TO THE CORRESPONDING BULKHEAD FOR THE REAR COWLING ASSY, A SEAL INCORPORATED IN THE COWL ASSEMBLY. FSDR 0204236740Bulkhead · crackedDuring "L" check found crack on number 4 pylon torque bulkhead. Repaired per EA 67-193401.SDR QXEA0202241Heat Shield · crackedCKB - AFT HEAT SHIELD AFT NACELLE STATION 303.0 IS CRACKED. REPAIRED IAW RD 8/4-54-044SDR QXEA0202232Heat Shield · crackedCKB - LEFT HAND AFT HEAT SHIELD AT STATION 303.0 IS CRACKED. REPAIRED IAW RD 814-54-044.SDR QXEA0202092Firewall · crackedPDX - NR 1 NACELLE FIREWALL HAS A CRACK IN CLOSING ANGLE ON INBOARD SIDE OF FIREWALL APPROXIMATELY VERTICAL STATION 171.90. REPAIRED IAW DHC-8 200 RD 8-54-109.SDR 2002FA0001355Firewall · crackedDURING ROUTINE INSPECTION FOUND CRACK IN FIREWALL EXT POWER PLUG BEHIND AND RADIATING OUT TO COWL SHOCK MOUNT DOUBLER AND TOWARD UPPER LT. ALSO TOWARD LOWER RIGHT. THIS COULD BE FROM YEARS OF CONNECTING AND DISCONNECTING EXTERNAL POWER FIREWALL NEEDS TO BE CSDR 111202Bulkhead · crackedRT ENGINE NOSE COWLING BULKHEAD HAS 3 CRACKS, 2 CRACKS WERE WITHIN LIMITS, THE 3RD WAS OVER 3 INCHES WHICH IS OUT OF LIMITS.SDR QXEA0201898Firewall · crackedPDX - AFT ENGINE NACELLE FIREWALL IS CRACKED AT THE 2 O'CLOCK POSITION. REPAIRED IAW RD 8-54-611.SDR QXEA0201832Firewall · crackedPDX - LEFT HAND NACELLE AFT FIREWALL IS CRACKED AT APPROXIMATELY XN125.50, INBOARD SIDE AT SUPPORT BRACKET. REPAIRED IAW DHC-8 RD 8-54-109.SDR SWIA200211431Firewall · crackedLT PYLON LOWER FIRE BOX PANEL (412 DB) HAS A CRACK IN ITS FORWARD DIVIDER. FOUND DURING C CHECK INSPECTION. REPLACED DIVIDER IAW CRJ SRM 51-42-06.SDR AUS20021192Bulkhead · cracked(AUS) LH ENGINE NACELLE BULKHEAD CRACKED.SDR 2002UALA01460Bulkhead · crackedNR 2 PYLON WEB CRACKED, ACCESS THROUGH PYLON PANELS 446BL OR 446BR. MAJOR REPAIR ACCOMPLISHED. REPAIRED UPPER WEB WITH DOUBLER.SDR 2002UALA01459Bulkhead · crackedNR 2 PYLON AFT UPPER SPAR WEB, AFT INBOARD CORNER CRACKED FOR PNEUMATIC DUCT, ACCESS THROUGH RT WING PANEL 611PT. MAJOR REPAIR ACCOMPLISHED. REPAIRED UPPER WEB WITH DOUBLER.SDR 2002UALA01458Bulkhead · crackedNR 1 PYLON UPPER WEB CRACKED AT IDG CABLE CUTOUT. MAJOR REPAIR ACCOMPLISHED. REPAIRED UPPER WEB WITH DOUBLER.SDR 2002UALA01457Bulkhead · crackedNR 1 PYLON UPPER WEB CRACKED AT MAIN ENGINE WIRE HARNESS CUTOUT. MAJOR REPAIR ACCOMPLISHED. REPAIRED UPPER WEB WITH DOUBLER.SDR 2002UALA01456Bulkhead · crackedNR 1 PYLON PNEUMATIC DUCT CUTOUT, UPPER WEB CRACKED AT INBOARD AFT CORNER WHERE FIRE PROTECTION LINES ATTACHES. MAJOR REPAIR ACCOMPLISHED. REPAIRED UPPER WEB WITH DOUBLER.SDR 2002UALA01455Bulkhead · crackedNR 2 PYLON WIRE HARNESS CUTOUT AT UPPER WEB CRACKED ACCESS THROUGH INBOARD PANEL 442BL. MAJOR REPAIR ACCOMPLISHED. REPAIRED UPPER WEB WITH REPAIR DOUBLER.SDR 2002UALA01454Bulkhead · crackedNR 2 PYLON IDG WIRE HARNESS UPPER WEB CUTOUT HAS SEVERAL CRACKS. MAJOR REPAIR ACCOMPLISHED. REPAIRED UPPER PYLON WEB WITH REPAIR DOUBLER SPLICE L ANGLE AND STIFFENER.SDR QXEA0201297Firewall · crackedPDX - CRACK IN LEFT HAND NACELLE AFT FIREWALL APPROXIMATELY 2 O'CLOCK POSITION. REPAIRED IAW DHC-8-200 RD 8-54-611.SDR QXEA0201385Firewall · crackedPDX- CRACK IN FIREWALL JUST ABOVE MAIN LANDING GEAR RETRACT ACTUATOR ATTACH FITTING UPPER ACCESS HOLE ON NR 2 RIGHT HAND ENGINE. REPAIRED IAW DHC-8 RD 8-54-806.SDR UPS02439373Bulkhead · crackedINSPECTION TYPE:C CRACK FOUND ON NR 3 NACELLE STRUT REAR MOUNT BULKHEAD AFT O/B WEB APPROX .5 INCH LONG AND STOPPED AT FASTENER HOLE. NR 3 NACELLE STRUT REAR MOUNT BULKHEAD REPAIRED AS PER RS R54-53-34880 UPS EO NR 747-54-20029.SDR UPS02439318Bulkhead · crackedINSPECTION TYPE:C CRACKS FOUND ON NR 4 NACELLE STRUT REAR MOUNT FWD AND AFT WEBS. NR 4 NACELLE STRUT REAR MOUNT BULKHEAD REPAIRED AS PER RS R54-53-34881 & UPS ENGINEERING FILE NUMBER 747-54-20030.SDR AWXA200200856Attach Angle · crackedMCN - MAJOR REPAIR - DURING C-16 CHECK 2 EACH CRACKS WERE FOUND ON ATTACH ANGLES OF #1 PYLON, JUST AFT OF LOWER HEATSHIELD BLANKET. MAINTENANCE REMOVED CRACKED ATTACH ANGLES JUST AFT OF LOWER HEATSHIELD BLANKET, FABRICATED 2 EACH REPLACEMENT ATTACH ANGLES, ANSDR CA020801013Firewall · cracked(CAN) A CRACK WAS FOUND ON FIREWALL DURING MAINTENANCE OPERATION. LENGTH OF CRACK 3.75 PO. AN ENGINE AIR FILTER KIT HAS RECENTLY BEEN INSTALLED AS PER STC SH02-22 BASED ON FAA APPROVED STC: SR01049SE. A PART OF THIS MODIFICATION CONSIST OF INSTALLATION A DIFSDR UPS02438755Bulkhead · crackedINSPECTION TYPE:SPC NR 3 NACELLE STRUT REAR ENGINE MOUNT BULKHEAD CRACK REVEALED AT O/B FWD & AFT WEB AREA APPROX AT 5 O'CLOCK POSTION. NR 3 NACELLE STRUT REAR ENGINE MOUNT BULKHEAD CRACKED AREA REPAIRED PER HX RS R-54-53-34827 WITH REPAIR KIT INSTALLED PER RSDR F3LA200200170Firewall · damagedDURING C-3 CHECK, INSPECTION REPORTED HOLE IN FIREWALL UNDER SEALANT IN NR 2 ENGINE LT THRUST REVERSER COWL. REPAIRED DAMAGE PER EA 54T-737-037, REV A.SDR UPS02438663Bulkhead · crackedINSPECTION TYPE:SPC NR 2 PYLON REAR ENGINE MOUNT BULKHEAD CRACK FOUND AT AFT WEB DOUBLER APPROX .1875 INCH IN LENGTH. NR 2 PYLON REAR ENGINE MOUNT BULKHEAD REPAIRED AS PER R54-53-34828.SDR UPS02438661Bulkhead · crackedINSPECTION TYPE:SPC NR 1 PYLON REAR ENGINE MOUNT BULKHEAD CRACK FOUND AT AFT WEB DOUBLER APPROX .25 INCH IN LENGTH. NR 1 PYLON REAR ENGINE MOUNT BULKHEAD REPAIRED AS PER HX RS 54-53-34828.SDR UPS02438662Bulkhead · crackedINSPECTION TYPE:SPC CRACK REVEALED AT NR 4 PYLON REAR ENGINE MOUNT BULKHEAD FWD SIDE I/B DOUBLER, THE CRACK INITIATED FROM ONE FASTENER HOLE PROPAGATED UPWARD TO THE EDGE CRACK LENGTH .1875 INCH. NR 4 PYLON REAR MOUNT BULKHEAD REPAIRED AS PER HX RS R-54-53-34SDR AUS20020476Firewall · cracked(AUS) RT ENGINE FIREWALL STRUCTURE CRACKED IN THE INSIDE RADIUS OF THEVERTICAL FACE.SDR QXEA0200824Firewall · crackedPDX - NR 1 ENGINE AFT FIREWALL INBOARD UPPER ANGLE WEB HAS CRACK. REPAIRED IAW HORIZON AIR EA 2-54-141.SDR QXEA0200815Firewall · crackedPDX - NR 1 ENGINE INBOARD MID SPAN FIREWALL CRACKED WHERE IT IS ANGLED. REPAIRED IAW RD 8-54-806.SDR UPS02438254Bulkhead · crackedINSPECTION TYPE:C NR 2 PYLON REAR ENGINE MOUNT BULKHEAD CRACK FOUND AT AFT WEB APPROX 4 O'CLOCK (VIEW LOOKING FWD). NR 2 PYLON REAR ENGINE MOUNT BULKHEAD REPAIRED AS PER INSTRUCTION ON HAECO REPAIR SCHEME R-54-53-34787.SDR UPS02438255Bulkhead · crackedINSPECTION TYPE:C NR 2 PYLON REAR ENGINE MOUNT BULKHEAD CRACK FOUND AT FWD WEB APPROX 7 O'CLOCK (VIEW LOOKING FWD). NR 2 PYLON REAR ENGINE MOUNT BULKHEAD CRACKED AREA REPAIRED AS PER HAECO RS R-54-53-34787.SDR UPS02438074Firewall · crackedINSPECTION TYPE: NR 2 PYLON LOWER FIREWALL WEB O/B POSN CRACKED AT NAC 221.9 REAR ENGINE MOUNT BULKHEAD AREA. NR 2 PYLON LOWER FIREWALL WEB REPAIRED AS PER SRM 54-10-03 FIG 2.SDR QXEA0200665Firewall · crackedPDX- LT ENGINE FIREWALL INBOARD APPROXIMATELY MIDWAY DOWN HAS A ONE INCH CRACK. REPAIRED IAW DHC-8 RD 8-54-806.SDR MWEA020254Shear Tie · crackedRIGHT PYLON BULKHEAD STATION 1369 SHEAR TIE IS CRACKED LOCATED BETWEEN LONGERONS 13 RIGHT AND 14 RIGHT. -- FABRICATED AND INSTALLED SHEAR TIE REPAIR PARTS.SDR UPS02438014Bulkhead · crackedINSPECTION TYPE:C-2 NR 3 NACELLE STRUT REAR ENGINE MOUNT BULKHEAD FOUND CRACKED AT FWD & AFT FRAME WEB. BULKHEAD CHORD REPAIRED AS PER HX RS R54-53-34766 FOR DETAIL UPS EA B747-5410-16563-A.SDR UPS02438029Bulkhead · crackedINSPECTION TYPE:C NR 1 PYLON AFT TORQUE BULKHEAD FOUND 3 FASTENER HOLES CRACK AT CHORD AREA. REPAIR CARRIED OUT AS PER RS R-54-53-34764 INSTRUCTION.SDR UPS02438028Bulkhead · crackedINSPECTION TYPE:C NR 4 PYLON AFT TORQUE BULKHEAD FOUND 3 FASTENER HOLES CRACK AT CHORD AREA. REPAIR CARRIED OUT AS PER RS-54-53-34764 INSTRUCTIONS.SDR P5CA0200665Firewall · crackedCRACK ON CLOSURE BULKHEAD FIREWALL, NR 3 PYLON UNDER SLOT SEAL AREA. CRACK RUNS VERTICALLY APPROX 5 INCHES THEN SPLITS TO INBOARD SIDE. REPAIR CARRIED OUT REF SRM 54-10-03. CRACK STOP DRILLED PER SRM 51-10-01.SDR CA020312003Skin · cracked(CAN) - FIREWALL ASSEMBLY AFT LT.- STA 5896, WL 2830, BL 430 AND WL 2740, BL570.- FIREWALL IS MADE OF 0.016" TITANIUM THROUGH WHICH BOTH THE FIRE EXTINGUISHER AND AIR CONDITIONER TUBING ASSEMBLY FITTINGS PASS. - CRACKS FORM AROUND FITTING HOLES IN TITANIUM. - SDR 2002FA0000195Firewall · crackedDISCOVERED DURING AN ANNUAL INSPECTION THAT FIREWALL HAD A 2.75 INCH CRACK AT THE CENTER, LOWER COWL MOUNT DOUBLER. ALMOST IMPOSSIBLE TO VISUALLY DISCOVER WITHOUT KNOWLEDGE OF THE PROBLEM.SDR 2002FA0000194Firewall · crackedDISCOVERED DURING AN ANNUAL INSPECTION THAT THE FIREWALL HAD A 2.75 INCH CRACK AT THE CENTER, LOWER COWL MOUNT DOUBLER. ALMOST IMPOSSIBLE TO VISUALLY DISCOVER WITHOUT KNOWLEDGE OF THE PROBLEM.
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