JASC 5397
Service difficulty reports · 67
Reports filed under 5397 · Fuselage Main, Bulkhead Fuselage wiring, 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 = '5397' 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 = '5397' 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 2009FA0000255Wire · arcedTHIS IS ACTUALLY A G-36. THE ENGINE LOST POWER ON CLIMBOUT. TROUBLESHOOTING REVEALED THAT THE FUEL DELIVERY LINE 36-920001-13 HAD A HOLE ARCED IN IT FROM AN ELECTRICAL WIRE, P6 PIN 14 WIRE H21A20. THE WIRE BUNDLE HAD BEEN RUBBING AGAINST THE FUEL LINE AND HASDR CA080923003Wire · broken(CAN) ACFT OVERHAULED, CAME BACK TO BASE LAST WEEK OF AUGUST, NO SLING LOAD OPERATION HAS BEEN LOGGED. ELECTRICAL WIRE FOUND BROKEN AT HOOK CONNECTOR LOCATION. ELECTRICAL WIRE ATTACHED WITH CLAMPS (4X) ALONG THE SWING CABLE SUPPORT. THE ROUTING SEEMED TO BESDR 2008FA0000493Wire · fatiguedWIRES THAT CONNECT TO THE ALTERNATE AIR DOOR (WHICH ARE SOLDERED TO THE SWITCH) FOR THE TORNADO ALLEY TURBO SYSTEM ARE BECOMING FATIGUED AND SOLDER IS BREAKING AT SWITCH. IF THE ALTERNATE AIR WAS TO OPEN AND THESE WIRES WERE BROKEN, IT WOULD NOT GIVE THE PILOSDR QXEA200701458Seat Track · corrodedC5 PDX - CORROSION ON NR 9 SEAT TRACK AT STATION X597.5. REPAIRED IAW RD8-53-784.SDR 06FDEA03441Wire · burnedLEVEL-1 ALERT TANK 2L AFT PUMP LOW. TANK 2L LT AFT CB POPPED. REPLACED NR 2 L PUMP IAW MM 28-22-01-4 NO HELP. REMOVED ELC TERMINAL FROM R2-56 2X AND CB STAYED IN. REINSTALLED ORIGINAL NR 2 L PUMP IAW MM 28-22-01-4. FOUND ELECTRICAL WIRES BURNED UNDER SDR QXEA200602475Seat Track · corrodedC3 PDX-CORROSION IN RT OB SEAT TRACK AT X139.5. REPAIRED IAW RD-84-53-884 AND SRM 51-21-10.SDR MALA060113Seat Track · corrodedDURING N4K BRIDGE CHECK IN BNA, FOUND SEAT TRACK AT LBLK 18.3 IS CORRODED AND HAS BEEN REPAIRED BETWEEN FS 296 TO FS 319 IAW MESABA EO#S53342. REF: EAMS WORK ORDER 213551 TASK 1514.SDR QXEA200600353Wire · looseYYC - C3 FUSELAGE GENERATOR WIRING JUNCTION AT STATION 520, RIGHT BETWEEN STRINGER 2 AND 3 HAS ONE LOOSE TERMINAL AND ONE WIRE CONNECTOR HAS BURNED INSULATOR. REPAIRED IAW CRJ700 SRM 24-22-00-01-A01 AND AMM 24-22-01-710-801.SDR UIEA200500033Seat Track · damagedMAINTENANCE PICK UP DURING DAILY CHECK, FOUND MAIN DECK SEAT TRACK DAMAGED AT STATION 1730. CUT OUT DAMAGED AREA AND REPAIRED PER SRM 53-10-05 FIG 1A. (M)SDR 05FDEA00234Wire Harness · looseWIRE BUNDLE 9102/AFT RIDING ON FWD RELAY PANEL OUTBOURD FRAME TOP RIGHT CORNER ,REF DWG SP10240263 FRAME 4 OF 4,G-G (31) REPOSITIONED AND SECURED WIRE BUNDLE AS PER EA.8-2400-84061 ON FWD RELAY PANEL. (WIRE INSTALATION FWD&AFT RELAY PANEL HARNESS ADJUST.SDR 2005FA0000369Cable · burnedDEFECT WAS FOUND AT ENGINE REMOVAL AND FIREWALL CLEANING. THE ELECTRICAL CABLE BETWEEN AUX POWER RELAY AND STARTER RELAY WAS FOUND TO HAVE BURN MARKS AND OBVIOUS DAMAGE TO INSULATION. ADJACENT TO THE DAMAGED PORTION OF THE CABLE WAS A SHEET METAL SCREW IN THSDR CA041123003Wire · burnedFOUND WIRE BUNDLE INSIDE TOILET SHROUD BURNING AND SMOKING, C/B SYST 2 WATERLINE HEATER (LAV LIGHTS) POPPED IN AVIONICS BAY. FURTHER T/S ON WIRING BURNED, FOUND WIRES IDENTIFIED AS H75C20,H75A20, AND H75A20N (GRN) ALL BROKEN FROM SPLICES. ALSO, HEATER TAPE RSDR GTIA040813Cable · misinstalledONE TAILCONE CABLE NOT INSTALLED IN BLOCK. (TAILCONE LIGHT WAS ILLUMINATED). ROUTED AND INSTALLED CABLE IAW MM 53-53-02.SDR 2004UALA00167Wire · damagedWIRE DAMAGE AFT CARGO PIT STA 1230. THERE WAS NO CONCLUSIVE INDICATION OF WHAT INITIATED THE WIRE DAMAGE. THERE WAS NO APPARENT CHAFING. THERE WERE METAL CHIPS NOTED IN THE AREA, BUT NONE FOUND DIRECTLY ON OR BELOW THE WIRE BUNDLE. IT IS UNKNOWN, AS TO WHETHERSDR AUS20031205Wire Harness · worn(AUS) WIRING LOOM LOCATED AT BS 1000 BEHIND OVERHEAD LOCKERS CHAFED THROUGH INSULATION BLANKET AND CONTACTED FUSELAGE FRAME CAUSING BURNING OF WIRES AND DAMAGE TO THE INSULATION BLANKET AND FRAME. AREA OF DAMAGE TO FRAME WAS APPROXIMATELY 4.762MM BY 2.381MM(0.SDR ZES2003F00000Wire · shortedDURING ENGINE START, LT ENGINE WOULD MOTOR TO 20 PERCENT NR, THEN START CONTROL CIRCUIT BREAKER B4, 5 AMP WOULD TRIP. FOUND SHORTED WIRE IN THE IGNITION SYSTEM IN CABIN JUST FORWARD OF THE LEFT WHEEL WELL CONTACTING THE STRUCTURE WHERE IT PASSED THROUGH THE KSDR GTIA021376Seat Track · corrodedFTW - PASSENGER SEAT TRACK CORRODED AT FS 613-840, LEFT SIDE OUTBOARD TRACK. LEFT SIDE OUTBOARD TRACK FROM STATION 734-854 IS OUT OF LIMITS. REMOVED LEFT OUTBOARD SEAT TRACK. FABRICATED DRILLED AND LOCATED NEW TRACK SECTION AND SPLICES. INSTALLED NEW TRACK
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