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 IPXA2015101194654Tail Cone · damagedINSPECTION TYPE:1C, RIGHT SIDE OF EXTENDED TAIL CONE HAS CHAFE DAMAGE AT BS 2165. ACCOMPLISHED PERMANENET REPAIR ON RT SIDE OF EXTENDED TAIL CONE AT BS 2165 IAW EA 011-5330-01-A5999, REV I/R AND EO 5350-58903-A.SDR SWAA2015092944390Tail Cone · delaminatedTAIL CONE DELAMINATED AT FWD LOWER SIDE AT DRAIN HOLE. R & R TAIL CONE IAW AMM.SDR DALA2015091705692Housing · wornMAINTENACE FOUND AFT ENTRANCE DOOR TAILCONE RELEASE PULL CABLE HOUSING WORN. THE TAIL CONE RELEASE CABLE WAS REPLACED.SDR CA151209008Radome · damaged(CAN) THE OPERATOR`S MAINTENANCE PROVIDER REPORTED THAT A PORTION OF THE RADOME COLLAPSED DURING A MAINTENANCE TEST FIGHT. THE ACFT WAS CLIMBING THROUGH FL170 WHEN THE CREW HEARD A LOUD THUD. THERE WERE NO MESSAGES ON THE ENGINE INDICATION AND CREW ALERTING SDR DALA2015082705255Block · out of rigTHE TAIL CONE UPPER RT BAYONET LOCK CABLE SLIDING BLOCK WAS FOUND OUT OF RIG, IT HAD A .7500" GAP ABOVE THE BAYONET LEVER PIN, WHERE ZERO GAP IS PERMITTED. MSP MAINTENANCE CHECKED AND ADJUSTED THE SLIDING BLOCK. IT IS WITHIN LIMITS NOW.SDR H44R2015082700001Fairing · failedCUSTOMER BROUGHT ACFT IN FOR ACCOMPLISHMENT OF REPETITIVE SB. DURING ACCOMPLISHMENT OF PRELIMINARY INSPECTION, NOTED ROTOR HUB FAIRING BROKEN OFF. PILOT RECALLED A SLIGHT BUFFET DURING FLIGHT BUT DID NOT THINK MUCH OF IT. PIECES AND HARDWARE FROM THE FAIRINSDR DALA2015081705030Latch Spade · wornUPPER LT TAILCONE LATCH SPADE WORN. R & R IAW AMM.SDR R61A201508130574Fairing · corrodedDURING HEAVY CHECK, FORWARD WING FUSELAGE TO FAIRING AFT BOTTOM FLANGE HAS 2 SCREWS DRILLED OUT AND IS CORRODED. MAINTENANCE R & R FORWARD WING FUSELAGE TO FAIRING AFT BOTTOM FLANGE IAW SRM 51-40-02, 51-40-01.SDR SIMA20150802003Fairing · crackedWHEEL BIN FAIRING IN FORWARD SECTION OF THE LEFT MAIN LANDING GEAR WHEEL WELL IS CRACKED 1 INCH. R & R FAIRING LOCATED IN THE LEFT MAIN LANDING GEAR WHEEL WELL IAW AMM 53-83-85.SDR SIMA20150802002Fairing · crackedWHEEL BIN FAIRING IN FORWARD SECTION OF RIGHT MAIN LANDING GEAR WHEEL WELL IS CRACKED 3/8 OF AN INCH & ATTACHING NUTPLATE IS LOOSE. R & R FAIRING IN THE RIGHT MAIN LANDING GEAR WHEEL WELL IAW AMM 53-83-85.SDR DALA2015080304786Handle · stiffDURING SCHEDULED CHECK OF THE TAILCONE DEPLOYMENT, IT WAS NOTED THAT THE FORCE REQUIRED TO PULL THE INTERNAL RELEASE HANDLE EXCEEDED TEST LIMITS. COMPLIED WITH REPAIR ON NON-ROUTINE WC OF WO 9554 07/31/15.SDR T6FA2015072901Skin · corrodedCORROSION FOUND ON LT SIDE MLG LEG FAIRING OUTER SKIN. REPAIRED IAW FIELD REPAIR.SDR CALA2015073094177Skin · dentedON WALK AROUND FOUND DENTS ON TAIL CONE LOWER SIDE AFT OF APU DOORS. SKIN DAMAGE OUT OF LIMITS. CUT OUT DAMAGED SKIN & HAD ALL NDTS ACCOMPLISHED. REPAIRED SKIN DAMAGE IAW SRM 53-151-11 FIG 203.SDR CALA2015072994170Skin · dentedON WALK AROUND FOUND DENTS ON TAIL CONE, LOWER SIDE AFT OF APU DOORS. SKIN DAMAGE OUT OF LIMITS, NEED TO REPAIR SKIN IAW SRM 53-51-11 FIG 203.SDR IPXA2015080992178Skin · damagedINSPECTION TYPE:1C, CHAFE DAMAGE TO EXTENDED TAILCONE FWD SKIN INNER SURFACE, RT SIDE REPAIRED TAIL CONE RT SKIN IAW EA 011-5330-01-A5916, REV IR AND EO MD11-5350-58296-A.SDR IPXA2015080992177Skin · damagedINSPECTION TYPE:1C, CHAFE DAMAGE TO EXTENDED TAILCONE FWD SKIN INNER SURFACE, LT SIDE REPAIRED TAILCONE LT SKIN IAW EA 011-5330-01-A5916, REV IR AND EO MD11-5350-58296-A.SDR DALA2015072904777Release Cable · frayedTAILCONE JETTISON CABLE FRAYED. R & R CABLE.SDR JJBA20150726007Tail Cone · nickedRIGHT SIDE TAIL CONE AT FS 762.409 & FS 780.252 HAS A NICK. REPAIRED NICK IAW RH 8-55-2867. CUT OUT DAMAGED AREA.SDR IPXA2015080992181Skin · damagedINSPECTION TYPE:1C, CHAFE DAMAGE TO EXTENDED TAILCONE FWD SKIN INNER SURFACE RT SIDE REPAIRED TAILCONE RT SKIN IAW EA 011-5330-01-A5910, REV IR AND EO MD11-5350-58273-A.SDR IPXA2015080992180Skin · damagedINSPECTION TYPE:3C, CHAFE DAMAGE TO EXTENDED TAILCONE FWD SKIN INNER SURFACE LT SIDE REPAIRED TAILCONE LT SKIN IAW EA 011-5330-01-A5910, REV. IR AND EO MD11-5350-58273-A.SDR DALA2015070904243Release Cable · frayedTAIL CONE RELEASE CABLE, DAMAGED AND FRAYED AFT OF BS 1485 AT 9 O`CLOCK POSITION. REPLACED THE RELEASE CABLE IAW AMM 53-53-02.SDR DALA2015071104304Pin · out of toleranceDURING TAILCONE RELEASE CHECK, FOUND DIMENSION AT LEVER TO PIN OUT OF TOLERANCE. FOUND EXCESSIVE PLAY IN AFT PAX ENTRY DOOR LOWER HINGE PLATES.SDR DALA2015070704215Cable · damagedCABLE DAMAGED AND FRAYED. REPLACED THE CABLE IAW AMM 53-53-02.SDR DALA2015070604181Release Cable · corrodedAFT PASSENGER DOOR EMERGENCY TAILCONE RELEASE CABLE IS FROZEN INTERNALLY, CORRODED. REPLACED EMERGENCY RELEASE CABLE IAW AMM 53-53-00-501.SDR DALA2015071004263Clamp · out of adjustCHECK FAILED STEP 21 OF THE TAILCONE RELEASE SYSTEM OPS CHECK. THE EXTERIOR RELEASE CABLE WAS OUT OF ALLOWABLE LIMITS AT THE CLAMP TO THE INTERNAL RELEASE CABLE. THE CLAMP ON THE CABLE WAS ADJUSTED AND THE SYSTEM WAS RIGGED BACK INTO SPECIFICATIONS. THE RIISDR DALA2015063004047Release Cable · frayedBROKEN STRANDS ON TAIL CONE RELEASE CABLE. RELEASE CABLE WAS REPLACED.SDR IPXA2015071391107Skin · chafedINSPECTION TYPE: 3C, RT EXTENDED TAIL CONE HAS CHAFE DAMAGE ON INNER STRUCTURE AT BS 2165. ACCOMPLISHED A PERMANENT REPAIR IAW EA 011-5330-01-A5872, REV I/R AND EO MD11-5350-58017-A.SDR IPXA2015071391106Skin · chafedINSPECTION TYPE: 3C, LT EXTENDED TAIL CONE HAS CHAFE DAMAGE ON INNER SKIN. ACCOMPLISHED PERMANENT DOUBLER IAW EA 011-5330-01-A5868, REV I/R AND EO MD11-5350-58014-A.SDR DALA2015062604009Bushing · wornTEE PIN BUSHING WORN. REPLACED BUSHING IAW AMM 53-53-00.SDR DALA2015062503975Release Cable · failedTAILCONE FAILED TO RELEASE DURING FUNCTIONAL CHECK. REPLACED TELEFLEX CABLE IAW AMDS 5352-7116.SDR SWAA2015071041735Support Frame · crackedLEFT WING TO BODY FAIRING STRUCTURE SUPPORT FRAME ANGLE CRACKED AT LEVEL OF BS 500D, WBL 76. R & R FRAME IAW SRM & DWG.SDR DALA2015062203898Release Cable · frayedMAINTENANCE DISCOVERED THAT THE TAILCONE EMERGENCY RELEASE CABLE WAS FRAYED BEYOND ALLOWABLE LIMITS. THE CABLE WAS REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS.SDR DALA2015062203899Release Cable · misriggedMAINTENANCE FOUND THAT THERE WAS EXCESSIVE TENSION IN THE RELEASE CABLE SYSTEM. SO MUCH TENSION THAT THE CONE RELEASED WITHOUT PULLING THE CABLE. ALSO, THE KEVLAR SLEEVE OVER THE RELEASE CABLE FOR THE TAILCONE WAS WORN OUT OF ALLOWABLE LIMITS. THE CABLE WASSDR CALA2015061593925Fastener · looseA VIBRATION WAS FELT FROM APPROX MID CABIN GOING AFT. THE RT ELEVATOR INDICATION ON THE LOWER EICAS PAGE WAS INDICATING A FLUTTERING OF ABOUT 1 INDICATOR WIDTH. NO VIBRATION WAS FELT IN THE COLUMN OR YOKE. THE CTR AP WAS ENGAGED & REMAINED ENGAGED. CHANGES SDR DALA2015071004246Release Cable · wornMAINTENANCE DISCOVERED THAT THE LT RELEASE LATCH CABLE FOR THE TAILCONE WAS WORN OUT OF ALLOWABLE LIMITS. THE CABLE WAS REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS. THE FUNCTIONAL CHECK WAS COMPLETED SATISFACTORILY.SDR REXA2015061000578Stiffener · crackedTASK CARD 900-53-900-106 AFT STIFFER CRACKED ON FUSELAGE FAIRING 195DL. R & R AFT STIFFENER ON FUSELAGE FAIRING PANEL 195DL YAW SUM 51-42-13.SDR DALA2015061003715Panel · crackedDURING A TAILCONE DROP, TAILCONE LOWER T/E PANEL WAS CRACKED AND DENTED. COMPLIED WITH ERA 463180-14MA PERMANENT REPAIR.SDR 7SSA2015102801Radome · cockedAIRCRAFT WAS ON ITS 2ND LEG OF THE DAY ENROUTE. THE LANDING GEAR DID NOT DEPLOY WHEN SELECTED GEAR DOWN. DURING INVESTIGATION IT WAS DETERMINED THE RADOME HAD MOVED AFT ALLOWING THE AFT PORTION TO COVER THE FRONT LIP OF THE NOSE LANDING GEAR DOORS PREVENTING TSDR DALA2015052703515Clevis · corrodedTHREE RUSTED CLEVIS`S, ON CABLE SUPPORT AT TAILCONE RELEASE SYSTEM. R & R AND ADJUSTED CLEVIS ON CABLE SUPPORT AT TAILCONE RELEASE IAW AMM. LP 1965257.SDR SWAA2015061640740Support · crackedWING TO BODY FAIRING SUPPORT CRACKED AT BS 670, RBL 10. R & R SUPPORT IAW SRM & DWG.SDR SWAA2015070841591Tail Cone · delaminatedTAIL CONE DELAMINATED. R & R TAIL CONE AMM.SDR V0XD20150523137Angle · corrodedAFT WING TO BODY FAIRINGS INTERNAL SUPPORT WEB HAS CORRODED SPLICE ANGLE. R & R ANGLE IAW SRM 51-42-06, WO 80289 & WC 1115.SDR SWAA2015052239953Support Bracket · crackedFORWARD LT UPPER WING TO BODY FAIRING SUPPORT BRACKET CRACKED. R & R BRACKET IAW SRM.SDR DALA2015051903419Cam · looseDURING CHECK, MAINTENANCE FOUND THE TAILCONE RELEASE CAM LEVER LOOSE ON THE SPLINES. MAINTENANCE REPLACED THE CAM LEVER ASSEMBLY AND THE FUNCTIONAL TEST WAS SATISFACTORY.SDR DALA2015051803418Clevis · improper partDURING CHECK, MAINTENANCE FOUND IMPROPER SAFETY ON 3 CLEVISES ON THE TAILCONE RELEASE CABLE. MAINTENANCE RESAFETIED THE CLEVIS AND THE FUNCTIONAL TEST WAS SATISFACTORY. LP 1951354.SDR DALA2015051803416Release Cable · out of adjustDURING CHECK, THE TAILCONE RELEASE CABLE FAILED GAP CLEARENCE DURING FUNCTIONAL TEST. THE TAILCONE RELEASE CABLE WAS ADJUSTED AND THE TEST WAS PERFORMED SATISFACTORILY. LP 1951349.SDR DALA2015051803414Release Cable · damagedDURING CHECK, MAINTENANCE FOUND THE KEVLAR ROPE ON THE TAILCONE RELEASE SYSTEM TO BE DAMAGED. MAINTENANCE REPLACED THE KEVLAR ROPE ON THE TAILCONE RELEASE SYSTEM. LP 1952047.SDR ASMF201506012Radome · out of limitsAIRCRAFT PERFORMED AN UNSCHEDULED LANDING DUE TO DURING CLIMB EICAS MSG WXR FAIL & BOTH WX RADARS DID NOT SHOW INDICATIONS CORRECT. PERFORMED A BIRD & HAIL STRIKE CONDITIONAL INSPECTION IAW MM 05-51-18, DETECTING FOD IN THE RADOME & IT WAS FOUND OUT OF LIMITSSDR SWAA2015051539741Latch · out of adjustAFT CABIN DOOR TAIL SLIDE, ARMING PAD BOTTOM LATCH OUT OF ADJUSTMENT. ADJUSTED LATCH IAW SRM.SDR CA150511011Tail Cone · damaged(CAN) LIGHTNING STRIKE ON NOSE CONE ON DEPARTURE. ALL NORMAL, CONTINUING TO STATION. FOUND MULTIPLE MELTED POINTS ON FUSELAGE TAIL CONE. TEMPORARY DISPOSITION ACCOMPLISHED IAW PP. PERMANENT DISPOSITION REQUIRED AT THE NEXT BC-06 CHECK.
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