JASC 5350
Service difficulty reports · 6,124
Reports filed under 5350 · Aerodynamic Fairings, 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 = '5350' 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 = '5350' 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 DALA13051440930Receptacle · wornMX DISCOVERED THAT BOTH THE LT AND RT UPPER RELEASE LATCH RECEPTACLES FOR THE TAILCONE WERE WORN OUT OF ALLOWABLE LIMITS. THE RECEPTACLES WERE REPLACED AND THE SYS WAS RIGGED TO SPECIFICATIONS. THE FUNCTIONAL CHECK WAS COMPLETED SATISFACTORILY.SDR DALA13051210930Release Cable · misroutedMX DISCOVERED THAT THE TAILCONE RELEASE CABLE WAS MISROUTED. THIS IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. THE CABLE ROUTING WAS CORRECTED PER THE MM.SDR DALA13050700997Cable · wornDURING SCHEDULED CHECK, TAILCONE TELEFLEX CABLE WAS NOTED TO BE WORN. SPIRAL WRAP WAS SHOWING WEAR & COMING OFF OF THE CABLE. REPLACED TELEFLEX CABLE IAW AMM 53-53-02-201-1.SDR DALA13050160908Sleeve · missingMX FOUND THE TAILCONE RELEASE CABLE SLEEVE WAS MISSING AND THE CABLE WAS OUT OF ALLOWABLE RIG LIMITS. THIS DISCREPANCY WAS LOCATED NEAR THE AFT ACCESSORY COMPARTMENT ON THE LEFT SIDE AT STA 1480 TO AFT ENTRY DOOR. THE CABLE WAS REPLACED, ADJUSTED, AND RIGGED SDR DALA13049440997Hook And Loop · missingDURING SCHEDULED CHECK, HOOK AND LOOP FOR THE RELEASE LANYARD NORMALLY LOCATED ON THE TOP OF THE TAILCONE SLIDE COVER WAS MISSING. TAILCONE SLIDE COVER WAS REPLACED IAW AMM 25-62-01 & WC 2500-4484. THE REQUIRED INSPECTION WAS ALSO COMPLETED.SDR DALA13049430997Pin · corrodedDURING SCHEDULED INSPECTION, THE TAILCONE TEE PIN AND BUSHINGS WERE FOUND TO BE RUSTED. THE TEE PIN BUSHINGS AND ASSOCIATED HARDWARE WERE REPLACED IAW AMM 53-53 AND THE REQUIRED FUNCTIONAL CHECKED AND INSPECTION WAS ACCOMPLISHED.SDR DALA13049420997Cable · wornDURING SCHEDULED CHECK, PLASTIC COATED TAILCONE RELEASE CABLE WAS FOUND TO BE WORN WHERE IT PASSES THROUGH THE CONDUIT CONNECTION TO THE TEE PIN. CABLE REPLACED IAW AMM 53-53 AND THE FUNCTIONAL CHECKED AND INSPECTION WAS COMPLETED.SDR DALA13049530908Release Mech · crackedMX DISCOVERED THAT THE TAILCONE RELEASE TRIGGER ASSY IN THE AFT CABIN WAS CRACKED. THE ASSY WAS REPLACED.SDR CALA2013100491728Seal · out of positionLT WING BODY AFT BODY FAIRING SEAL IS OUT OF PLACE. SEAL IS AFT LT HAND AFT ELEPHANT EAR FAIRING. INTERIM REPAIR WITH HIGH SPEED TAPE MADE.SDR DALA13048830908Cam · wornMX DISCOVERED THAT THE TAILCONE RELEASE MECHANISM CAM BASE WAS WORN OUT OF ALLOWABLE LIMITS. CAM BASE WAS REPLACED AND THE SYS WAS RIGGED TO SPECIFICATIONS.SDR CALA2013100391701Paint · blisteredRADOME HAS MULTIPLE PAINT BLISTERS. REPLACED RADOME IAW AMM.SDR DALA13047959219Spring · failedTAILCONE LATCH, LT UPPER, DOESN'T SPRING CLOSED. R & R SPRING IAW CMM. OPS CHECKED ON AMDS 1200-6647.SDR DALA13047949219Spring · failedTAILCONE LATCH, RT LOWER, IS SPRING LOADED TO OPEN. R & R SPRING IAW CMM. OPS CHECKED ON AMDS 1200-6647.SDR DALA13047939219Spring · failedTAILCONE LATCH, RT UPPER, DOESN'T SPRING CLOSED. R & R SPRING IAW CMM. OPS CHECKED ON AMDS 1200-6647.SDR DALA13047929219Spring · failedTAILCONE LATCH, LT LOWER, IS SPRING LOADED TO OPEN. R & R SPRING IAW CMM. OPERATIONS CHECKED ON AMDS 1200-6647.SDR DALA13047240995Cable · corrodedDURING SCHEDULED CHECK, THE TAIL CONE TEE PIN CABLE WAS NOTED TO BE RUSTY AT BOTH ENDS OF THE LT TAIL ACCESSORY COMPARTMENT. THE RUST WAS REMOVED AND THE CABLE WAS TREATED IAW WC 5350-01077-0101 AND THE REQUIRED INSPECTION WAS COMPLETED.SDR DALA13047230995Guide · corrodedDURING SCHEDULED MX CHECK, TAIL CONE RELEASE TEE PIN CABLE GUIDE BLOCK WAS FOUND TO BE CORRODED ON THE LT SIDE OF THE TAIL ACCESSORY COMPARTMENT. THE CORROSION WAS REMOVED FROM THE GUIDE BLOCK AND IT WAS TREATED AND REINSTALLED IAW AMM 53-53. THE REQUIRED INSSDR DALA13047220995Release Cable · frayedDURING SCHEDULED MX CHECK, THE TAIL CONE UPPER LATCH LEVER CABLE AT THE 11:00 POSITION WAS FOUND TO BE FRAYED. THE CABLE WAS REPLACED IAW AMM 53-53-00 AND THE REQUIRED INSPECTION WAS COMPLETED.SDR SWAA2013100921012Strap · corrodedLT WING TO BODY SUPPORT FAIRING CORRODED AT BS 851 LOWER SECTION. R & R STRAP IAW SRM & DRAWING.SDR SWAA2013100720927Strap · corrodedRT WING TO BODY LOWER SECTION OF SUPPORT FAIRING CORRODED AT BS 851. R & R STRAP IAW SRM.SDR DALA13046440997Release Mech · failedACFT FAILED INITIAL DROP CHECK OF THE TAILCONE RELEASE SYS. RELEASE MECHANISM CAM EXCEEDED 45 POUNDS ALLOWABLE PULL LIMIT. TEE PIN ADJUSTED IAW MANUAL AND THE SYSTEM RECHECKED. TAILCONE DROPPED AT 10 POUNDS OF MEASURED PULL FORCE. THE RII STEPS WERE COMPLETESDR SWAA2013121223243Web · corrodedRT WING TO BODY FILLET FAIRING HORN ASSEMBLY SUPPORT WEB CORRODED. R & R WEB IAW SRM.SDR DALA13046450956Release Cable · corrodedMX DISCOVERED THE TAILCONE EMERGENCY RELEASE CABLE WAS CORRODED BEYOND ALLOWABLE LIMITS. CABLE REPLACED AND THE SYS WAS RIGGED TO SPECIFICATIONS.SDR ASMF201310005Radome · deformedDURING TRANSIT CHECK, FOUND RADOME DEFORMED. FOUND OUT OF LIMITS IAW SRM 57-12-00. RADOME REPLACED IAW AMM 57-12-02.SDR DALA13045990995Cam · wornMX DISCOVERED THAT THE TAILCONE RELEASE MECHANISM CAM BASE WAS WORN OUT OF ALLOWABLE LIMITS. THE CAM BASE WAS REPLACED AND THE SYS WAS RIGGED TO SPECIFICATIONS. THE RII WAS SATISFACTORY.SDR SWAA2013100320731Support Angle · crackedWING TO BODY FAIRING SUPPORT ANGLE CRACKED AT BS 540 BETWEEN STRINGER 22R & STRINGER 23R. R & R ANGLE IAW SRM & DRAWING.SDR DALA13045490995Receptacle · wornMX DISCOVERED THAT ALL OF THE TAILCONE RELEASE SYSTEM GUIDE PIN RECEPTACLES WERE WORN BEYOND ALLOWABLE LIMITS. THE RECEPTACLES WERE REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS. THE FUNCTIONAL CHECK WAS COMPLETED SATISFACTORILY.SDR DALA13045480995Receptacle · wornMX DISCOVERED THAT THE LT UPPER RELEASE LATCH RECEPTACLE FOR THE TAILCONE WAS WORN, OUT OF ALLOWABLE LIMITS. THE RECEPTACLE WAS REPLACED AND THE SYS WAS RIGGED TO SPECIFICATIONS. THE FUNCTIONAL CHECK WAS COMPLETED SATISFACTORILY.SDR DALA13045470995Bracket · crackedMX DISCOVERED THAT THE TAILCONE RT UPPER LATCH, LOWER BRACKET HAD ELONGATED HOLE. THE BRACKET WAS REPLACED AND THE SYS WAS RIGGED TO SPECIFICATIONS. FUNCTIONAL CHECK WAS COMPLETED SATISFACTORILY.SDR DALA13045460995Bracket · crackedMX DISCOVERED THAT THE TAILCONE LT UPPER LATCH, LOWER BRACKET WAS CRACKED. THE BRACKET WAS REPLACED AND THE SYS WAS RIGGED TO SPECIFICATIONS. FUNCTIONAL CHECK WAS COMPLETED SATISFACTORILY.SDR DALA13045279223Release Cable · brokenDURING TAILCONE DROP, CABLE PRESSURE RELEASE PULL CABLE BROKE OFF. R & R PRESSURE RELEASE CABLE FOR ASSIST BOTTLE IAW AMM 53-52.SDR SWAA2013093020572Panel · crackedWING TO BODY FAIRING PANEL 3378L CRACKED FASTENER HOLE. REPAIRED PANEL IAW SRM.SDR DALA13044310989Cam · wornMX DISCOVERED THAT THE TAILCONE RELEASE MECHANISM CAM BASE WAS WORN OUT OF ALLOWABLE LIMITS. THE CAM BASE WAS REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS. THE RII WAS SATISFACTORY.SDR DALA13044200949Release Cable · frayedMX DISCOVERED THAT THE TAILCONE EMERGENCY RELEASE CABLE WAS FRAYED BEYOND ALLOWABLE LIMITS. THE CABLE WAS REPLACED AND THE SYS WAS RIGGED TO SPECIFICATIONS. THE RII STEPS WERE COMPLETED.SDR DALA13044109251Handle · damagedLEFT AFT FUSELAGE EXTERIOR TAILCONE JETTISON HANDLE MISSING 2 EACH STOW CLIPS. REPLACED MISSING TAILCONE JETTISON HANDLE CLIPS IAW SRM 51-30-08. PERFORMED OPS CHECK IAW W/C 5352-7116, STEP 5. (LP 1072756)SDR DALA13044020948Cable · wornMX FOUND THAT THE TAILCONE RELEASE CABLE INNER SHEATH WAS WORN OUT OF ALLOWABLE LIMITS. THE INTERIOR TELEFLEX CABLE WAS REPLACED, ADJUSTED, AND RIGGED BACK INTO SPECIFICATIONS. THE RII STEPS WERE COMPLETED AND THE FOLLOW-UP CHECK WAS SUCCESSFUL.SDR DALA13044010948Cable · wornMX FOUND THAT THE TAILCONE RELEASE CABLE SHEATH WAS WORN OUT OF ALLOWABLE LIMITS. THE CABLE WAS REPLACED, ADJUSTED, AND RIGGED BACK INTO SPECIFICATIONS. THE RII STEPS WERE COMPLETED AND THE FOLLOW-UP CHECK WAS SUCCESSFUL.SDR CALA2013090591023Screw · missingSCREW MISSING ON AFT BELLY FAIRING 197GB JUST FWD OF AFT BLADE ANTENNA. REPLACED SCREW.SDR VNAA2013090200001Skin · burnedCREW REPORTED LIGHTNING STRIKE ON LT NOSE OF ACFT. MX PERFORMED LIGHTNING STRIKE INSPECTION AND FOUND DAMAGE TO T/E OF VHF 2 ANTENNA, BURN MARKS ON TAIL CONE AND BURN MARK ON HORIZ STABILIZER TIP LOWER SIDE. MX R & R VHF NR 2 ANTENNA, R & R RT HORIZ STABILIZSDR DALA13042720953Release Cable · kinkedMX DISCOVERED THAT THE TAILCONE RELEASE CABLES WERE KINKED AND FRAYED BEYOND ALLOWABLE LIMITS. THE CABLES WERE REPLACED AND THE SYS WAS RIGGED TO SPECIFICATIONS. THE RII STEPS WERE COMPLETED.SDR DALA13042500923Pin · wornMX DISCOVERED THAT THE RELEASE LATCH "TEE PIN" FOR THE TAILCONE WAS WORN OUT OF ALLOWABLE LIMITS. THE T-PINS WERE REPLACED AND THE SYS WAS RIGGED TO SPECIFICATIONS. THE FUNCTIONAL CHECK WAS COMPLETED SATISFACTORILY.SDR DALA13042490923Release Cable · frayedMX DISCOVERED THAT THE TAILCONE KEVLAR RELEASE CABLE WAS FRAYED BEYOND ALLOWABLE LIMITS. THE CABLE WAS REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS. THE RII STEPS WERE COMPLETED.SDR SWAA2013092520494Strap · corrodedAFT FS BODY FAIRING ATTACH FRAME CORRODED AT BS 851 BETWEEN LONGERON 26L TO LONGERON 27L. R & R STRAP IAW SRM.SDR DALA13042730923Release Cable · brokenMX DISCOVERED THAT THE EMERGENCY ESCAPE PATH TAILCONE RELEASE CABLE WAS BROKEN. THIS IS CONSIDERED A DEFECT IN THE EMERGENCY ESCAPE SYS AND COULD HAVE AN ADVERSE AFFECT ON THE EVACUATION ROUTE IF IT PREVENTED PROPER DEPLOYMENT OF THE TAILCONE. THIS NOT IN COMPSDR DALA13042510923Arm · out of rigMX DISCOVERED THAT THE TAILCONE RELEASE ARM WAS OUT OF ALLOWABLE RIG LIMITS. THE AFT TAILCONE RELEASE ARM WAS ADJUSTED TO GET PIN CLEARANCE FROM THE DOOR STOP AND THE SYSTEM WAS RIGGED BACK INTO SPECIFICATIONS. THE RII STEPS WERE COMPLETED.SDR CALA2013082690717Nut Plate · damagedONE FASTENER WILL NOT SECURE ON WING TO BODY FAIRING 191BB, FASTENER IN TOP EDGE 5TH FROM LEADING EDGE. TAPED OVER FASTENER, TO BE REPAIRED WITHIN CYCLES, PTC IS 20387. REPLACED DAMAGED NUTPLATE.SDR DALA13041330875Pulley · damagedDURING AMDS 5350-01032-03, DROP CHECK, TAILCONE FAILED RELEASE CHECK. FOUND UPPER LT CABLE PULLEY DAMAGED. INSTALLED SERVICEABLE PULLEY IAW AMM 53-50. DROP CHECKED GOOD OK FOR SERVICE. REQUIRED INSPECTION COMPLETE.SDR DALA13041160977Bushing · wornTHE TAILCONE RELEASE CABLE T-PIN BUSHINGS WERE FOUND TO BE WORN IN THE RT AFT ACCESSORY COMPARTMENT. THE T-PIN BUSHINGS WERE REPLACED AND THE REQUIRED INSPECTION WAS COMPLETED ON WC 5350-01077-0101.SDR DALA13041019215Cable · frayedDURING SERVICE CHECK, TAILCONE JETTISON RELEASE CABLE FOUND FRAYED. R & R TAILCONE JETTISON RELEASE CABLE IAW IPC AND JIC.SDR CALA2013082690730Fastener · missingTWO EACH FASTENERS MISSING FROM RT WING TO BODY FAIRING. REPLACED FASTENER ON RT WING TO BODY PANEL LEADING EDGE. REMAINING MISSING FASTENER IS NOT IN LEADING EDGE OR CORNER OF PANEL. COVERED OPEN HOLE WITH ALUMINUM FOIL TAPE IAW SRM 51-10-05.
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