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 DALA13028460974Bushing · wornMX DISCOVERED THAT THE TEE PIN AND THE TEE PIN BUSHING WERE WORN BEYOND ALLOWABLE LIMITS AND REQUIRED REPLACEMENT.SDR DALA13028470974Receptacle · wornMX DISCOVERED THAT NUMEROUS TAILCONE GUIDE PIN RECEPTACLES WERE WORN OUT OF ALLOWABLE LIMITS. THE RECEPTACLES WERE REPLACED AND THE SYS WAS RIGGED TO SPECIFICATIONS. THE FUNCTIONAL CHECK WAS COMPLETED SATISFACTORILY.SDR AALA20130531008Pin · crackedCRACK AT STA 37, LOWER RT RADOME GUIDE PIN. CUT OUT CRACK AND INSTALLED DOUBLER AND FILLER IAW AARD 53-10-00-19.SDR SWAA2013061717157Attach Angle · crackedTAIL CONE INTERIOR JETTISON HANDLE STOWAGE ATTACH ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.SDR UALA2013052803688Seal · deterioratedAFT FUSELAGE FAIRING 198GB SEAL IS DETERIORATED. R & R THE TORN SEAL IAW ECRA 5335-01013.SDR DALA13024760926Bushing · wornDURING AN INSPECTION, MX DISCOVERED THAT THE TAILCONE JETTISON RELEASE PULL-CABLE BUSHINGS, PIN 11, LATCH RECEPTACLE, AND ALIGNMENT PIN RECEPTACLES WERE ALL WORN BEYOND ALLOWABLE LIMITS. THE SYS WAS REPAIRED BY BUSHING REPLACEMENTS IAW AMM 53-53-00/02, SRM 51-SDR DALA13024690952Cable · frayedDURING AN INSPECTION, MX DISCOVERED THAT THE TAILCONE JETTISON CABLES WERE DAMAGED BY FRAYING. THE SYSTEM WAS REPAIRED BY CABLE REPLACEMENT, ADJUSTMENT, AND RIGGING IAW AMM 20-10-17, 201.SDR DALA13024680952Cam · wornDURING AN INSPECTION, MX DISCOVERED THAT THE TAILCONE JETTISON RELEASE MECHANISM CAM BASE WAS WORN BEYOND ALLOWABLE LIMITS. THE SYS WAS REPAIRED BY CAM BASE REPLACEMENT IAW AMM 53-53-02.SDR UALA2013052403633Radome · damagedEXTERNAL SURFACE NOSE RADOME, SEGMENTED LIGHTNING DIVERTER STRIP AT 2 O"CLOCK, MISSING TOO MANY SEQUENTIAL METALLIC BUTTONS. R & R RADOME. ADJUSTED RADOME & BONDING CHECK GOOD AMM.SDR SWAA2013070117782Angle · crackedRT WING TO BODY FAIRING ANGLE CRACKED BETWEEN BS 685 + 10 TO BS 727, STRINGER 22R. R&R ANGLE IAW SRM.SDR UALA2013051503369Radome · faultyRADAR STILL DISPLAYS PHANTOM RETURN AT 7 MIGRTR, RETURN WITH HIGHER TILT. REPLACED RADOME.SDR DALA13022790950Structure · wornMX DISCOVERED THAT THE TAILCONE RELEASE CAM BASE WAS WORN AT AFT OF ACCESSORY COMPARTMENT AT 1100 POSITION. THE BASE WAS REPLACED.SDR UALA2013051403352Radome · damagedDENT IN NOSE CONE. FOUND RADOME PAINT CHIPPED. MADE INTERIM REPAIR. REPLACED RADOME REF MM.SDR DALA13022240998Lanyard · corrodedDURING SCHEDULED CHECK, THE TAIL CONE SLIDE TOGGLE PIN WAS NOTED TO HAVE SURFACE RUST. A NEW TAIL CONE SLIDE DEPLOYMENT LANYARD ASSY WAS INSTALLED IAW AMM 25-62-01-201 AND THE REQUIRED INSPECTION WAS COMPLETED.SDR DALA13021740969Pin · wornDURING SCHEDULED CHECK, THE TAIL CONE RELEASE T-PIN WAS NOTED TO BE WORN. THE TAIL CONE RELEASE T-PIN WAS REPLACED IAW AMM 53-53.SDR DALA13021730969Bracket · wornDURING SCHEDULED MX CHECK, THE UPPER TAIL CONE LANYARD SPRING BRACKET WAS NOTED TO BE WORN. THE UPPER TAIL CONE SPRING BRACKET WAS REPLACED IAW SRM 51-01.SDR DALA13021720969Receptacle · wornDURING SCHEDULED MX CHECK, THE UPPER RT TAIL CONE LATCH RELEASE RECEPTACLE WAS NOTED TO BE WORN. THE UPPER RT TAIL CONE RELEASE RECEPTACLE WAS REPLACED IAW AMM 53-53 .SDR DALA13021760969Receptacle · wornDURING SCHEDULED MX CHECK, NUMEROUS TAILCONE ALIGNMENT PIN RECEPTACLES WERE NOTED TO BE WORN (15EA). WORN RECEPTACLES WERE REPLACED IAW DWG-9911957.SDR DALA13021750969Clamp · wornDURING SCHEDULED CHECK, THE UPPER RT UPPER LATCH CLAMP SLOT FOR THE TAILCONE LATCH ATTACHMENT WAS NOTED TO BE WORN. MX REPLACED THE RT UPPER LATCH CLAMP IAW AMM 53-53.SDR UALA2013050803231Nut Plate · damagedONE FASTENER MISSING FROM LEADING EDGE OF LEFT SIDE WING TO BODY FAIRING 195PL. REPLACED DAMAGED NUTPLATE.SDR DALA13022029201Support · crackedWING TO BODY FILLET FAIRING SUPPORT, BS 977, LBL 7, CRACKED IN WEB OF SUPPORT. REMOVED FRAME FROM WHEEL WELL. DRILLED, SEALED AND INSTALLED IAW DWG 5930584 AND SRM 51-30-02.SDR UALA2013050903265Radome · erodedRADOME ERODED WITH POSSIBLE DELAMINATION. REPAIRED IAW SRM 53-10-72.SDR UALA2013050703213Radome · damagedDURING BIRD STRIKE INSPECTION FOUND 14 IN DIA. BY 4 IN DEPTH. DENT ON CENTER OF RADOME. REPLACED RADOME IAW AMM 53-15-11-000-001A.SDR REXA2013050300786Stiffener · crackedSTIFFENER FOR AFT WING TO BODY FAIRING CRACKED. REMOVED AND REPLACED WITH NEW STIFFENER FOR ALL TO BODY FAIRING IAW CRJ 900 SRM 51-42-15.SDR SWAA2013051416016Rub Strip · crackedFUSELAGE WING TO BODY FAIRING LOWER SIDE RIGHT RUB STRIP CRACKED AT STA 696. REMOVED AND REPLACED RUB STRIP IAW SRM.SDR SWAA2013052016263Fairing · delaminatedLEFT AFT WING TO BODY FAIRING PANEL 194GL, DELAMINATED. R & R PANEL IAW SRM.SDR QXEA2013043000868Fairing · crackedFINGERNAIL FAIRING 424AL CRACKED AT LOWER AFT CORNER. REMOVED CRACKED BRACKET IAW SRM 51-42-05-02-01, REV 12. MATCH DRILLED NEW BRACKET IAW SRM 51-40-07-02-01, REV 12. OK TO INSTALL NEW BRACKET. INSTALLED BRACKET IAW SRM 51-42-05-02-01, REV 12. REAPPLIED PSDR DALA13020060970Clamp · out of positionDURING SCHEDULED INSPECTION, CABLE CLAMP NR 18 WAS FOUND TO BE LOCATED LESS THAN .5" FROM THE CONDUIT IN THE AFT ACCESSORY COMPARTMENT AT THE FRAME AT 7 O'CLOCK POSITION. ADJUSTED CLAMP CLEARANCE IAW AMM 53-53-00-501 AND AMDS CARD 5350-01077-0101. REQUIRED ISDR Z5FA2013050354701Radome · damagedACFT WAS STRUCK BY LIGHTNING, MIDFLIGHT AT 13,000 FT WHILE EN-ROUTE. IMMEDIATELY AFTER THE STRIKE COCKPIT BEGAN TO ODOR OF ELECTRICAL SMOKE. CREW DONNED 02 MASKS AND DECLARED AN EMERGENCY. LANDING WAS UNEVENTFUL. MX ACCOMPLISHED A LIGHTNING STRIKE INSPECTION SDR DALA13019460920Bracket · wornMX DISCOVERED THAT THE TAILCONE RELEASE SYS AFT LT AND RT SPRING BRACKETS ARE WORN FROM THE SPRING. THE BRACKETS WERE REPLACED AND THE SYS WAS RIGGED TO SPECIFICATIONS. THE RII STEPS WERE COMPLETED AND THE FUNCTIONAL CHECK WAS COMPLETED SATISFACTORILY.SDR DALA13019450920Receptacle · wornMX DISCOVERED THAT THE TAILCONE RELEASE SYS LATCH RECEPTACLES WERE WORN BEYOND OF ALLOWABLE LIMITS. THE RECEPTACLES WERE REPLACED AND THE SYS WAS RIGGED TO SPECIFICATIONS. THE FUNCTIONAL CHECK WAS COMPLETED SATISFACTORILY.SDR DALA13019020970Conduit · looseDURING SCHEDULED INSPECTION, THE CABLE CONDUITS FOR THE TAILCONE RELEASE CABLE WERE FOUND TO BE LOOSE ON THE AFT ACCESSORY COMPARTMENT FRAME AT THE 7 O'CLOCK POSITION. RESECURED CABLE CONDUITS WITH NEW CLAMPS IAW AMM 53-53. REQUIRED INSPECTION COMPLETED.SDR DALA13019010970Release Cable · dirtyDURING SCHEDULED INSPECTION, THE TAILCONE RELEASE CABLES WERE FOUND TO BE GUMMED UP AND DIRTY AT THE CONDUITS ON THE AFT ACCESSORY AREA FRAME AT THE 7 O'CLOCK POSITION. THE CABLES AND CONDUITS WERE CLEANED IAW PS900-1-2-1, NR 01 AND THE REQUIRED INSPECTION WASDR DALA13019000970Release Cable · wornDURING SCHEDUED INSPECTION, THE TAILCONE RELEASE CABLE LOCATED IN THE TAILCONE INTERIOR WAS NOTED TO BE WORN & FRAYED. THE CABLE WAS REPLACED IAW AMM 53-53-00.SDR DALA13018990970Pin · wornDURING SCHEDULED INSPECTION, THE TAILCONE GUIDE RECEPTICLES WERE NOTED TO BE WORN. THE GUIDE PIN RECEPTICLES WERE REPLACED IAW SRM 51-01 AND THE REQUIRED INSPECTION WAS COMPLETED.SDR DALA13018980970Pin · looseDURING SCHEDULED INSPECTION, THE TAILCONE GUIDE PIN WAS DETERMINED TO BE LOOSE AT THE 12 O'CLOCK POSITION. THE GUIDE PIN WAS RESECURED IAW AMM 53-53-00 AND THE REQUIRED INSPECTION WAS COMPLETED.SDR DALA1316050683Fairing · puncturedFOUND PUNCTURE-DENT ON BODY FAIRING LT SIDE AFT OF ANTENNA BELOW L2 DOOR. CW PERMANENT REPAIR IAW SRM 51-70-05.SDR UALA2013042302835Fairing · gougedON WALK AROUND, FOUND GOUGE IN FUSELAGE BODY FAIRING 191DDL. DAMAGE PENETRATED OUTER SKIN OF PANEL LENGTH 4.25 INCHES. DEPTH 0.025 WIDTH 1 INCH. VISUAL CHECKED IAW EC-RA 5320-02141.SDR R61A201304210395Rib · crackedWHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE 192 CENTER FAIRING SUPPORT SPLICE CRACKED AT RIB 52. MAINTENANCE REMOVED AND REPLACED THE SPLICE RIB BRACKET AT RIB 52 IAW EMB 170 SRM 51-41-01. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.SDR DALA13018079010Release Mech · weakDURING SCHEDULED MX, THE TAILCONE EXTERNAL RELEASE HANDLE SPRING CLIPS WERE FOUND TO BE WEAK. THE SPRING CLIPS WERE REPLACED IAW AMM 53-53 AND OPS CHECKED GOOD. THE REQUIRED INSPECTION WAS COMPLETED.SDR DALA13018069010Cam · wornDURING SCHEDULED MX, THE TAILCONE RELEASE CAM ASSY WAS FOUND TO BE WORN AT THE UPPER LT POSITION AT STA 1510. THE UPPER LT TAILCONE RELEASE BASE WAS REPLACED IAW AMM 53-53-00 AND THE REQUIRED INSPECTION WAS COMPLETED.SDR DALA13017369010Clamp · damagedMX DISCOVERED THAT THE TAILCONE RELEASE SYS LOCKING CABLE CLAMP AND CONDUIT WAS OUT OF ALLOWABLE LIMITS. SOME CABLE BRACKETS WERE FOUND BROKEN AND REPLACED. ALSO, ALL OF THE TAILCONE RECEPTACLES IDENTIFIED AS WORN BEYOND LIMITS WERE REPLACED. THE CABLE WAS ASDR A6WA20130418897Attach Bracket · chafedFAIRING 193AB ATTACH BRACKETS ARE CHAFED (4 TOTAL). REMOVED AND REPLACED WITH SERVICEABLE PARTS P/N'S 601R31036-10, 601R31036-9, 478H0407-3. IAW CRJ 200 SRM 51-40-11 & 51-42-15.SDR DALA13016650918Cable · brokenMX DISCOVERED THAT THE TAILCONE RETRACT CABLE WAS BROKEN AT THE TURN-BUCKLE. THE CABLE WAS REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS.SDR SWIA201333243Fairing · looseFLT 4442. WHEN SELECTING FLAPS 20 DEGREES, AIRFRAME SHOOK AND BUFFETED. ONLY OCCURS ABOVE 195 KTS. SLOWING OR SELECTING FLAPS 30 DEGREES, WILL END THE BUFFETING. SECURED SCREWS ON FWD WING TO FUSELAGE FAIRING AND RESEALED. INSPECTED FLAPS, FLAPS HINGES ASDR DALA13017350930Cable · brokenMX DISCOVERED THAT THE TAILCONE CATWALK RT CABLE WAS BROKEN. THE CABLE WAS REPLACED AND THE SYS WAS RIGGED TO SPECIFICATIONS.SDR USAA2013041600034Support Frame · corrodedC4 CHECK - LEVEL 2 GALVANIC CORROSION ON FAIRING SUPPORT FRAME AT BS 800, S28L. REPAIRED FAIRING SUPPORT FRAME AT BS800, S28L IAW B757 SRM 51-10-02, 53-00-71-1A & 51-70-11.SDR USAA2013041600035Support Frame · corrodedC4 CHECK - LEVEL 2 GALVANIC CORROSION ON FAIRING SUPPORT FRAME AT BS 780, S27L. REPAIRED FAIRING SUPPORT FRAME AT BS780, S27L IAW B757 SRM 51-10-02, 53-00-71-1A, 51-20-01, 51-70-11.SDR UALA2013041002444Radome · damagedDURING LIGHTNING STRIKE INSPECTION, FOUND RADOME LOWER SECTION DAMAGED. REPAIRED 3EA DAMAGED AREA PER SRM REPAIR 6 PARAGRAPH 4.SDR AALA20130410003Radome · damagedORD - CREW REPORTED LIGHTNING STRIKE ON THE FIRST OFFICERS SIDE OF THE FUSELAGE. EMERGENCY DECLARED FLIGHT RETURNED ORD LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED THE RADOME AND FIVE PASSENGERS WINDOWS. SYSTEM GROUND CHECK NORMAL OPER
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