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.

SDR DALA2014112406237Latch · wornMAINTENANCE DISCOVERED THAT THE LT LOWER RELEASE LATCH ASSEMBLY FOR THE TAILCONE WAS WORN OUT OF ALLOWABLE LIMITS. THE ASSEMBLY WAS REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS. THE FUNCTIONAL CHECK WAS COMPLETED SATISFACTORILY.Nov 23, 2014 · N926DL · Doug MD88SDR DALA2014112406239Bracket · wornMAINTENANCE DISCOVERED THAT THE TAILCONE LT AND RT SPRING BRACKETS ARE WORN FROM THE SPRING. THE BRACKETS WERE REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS. THE RII STEPS WERE COMPLETED AND THE FUNCTIONAL CHECK WAS COMPLETED SATISFACTORILY.Nov 22, 2014 · N926DL · Doug MD88SDR V0XD201411250245Angle · corrodedAFT WING TO BODY FAIRINGS SUPPORT WEB JOINT ANGLE AT FS 953 CORRODED. R & R ANGLE IAW SRM 51-42-06. WORK ORDER 80258 WORK CARD 1082.Nov 21, 2014 · N158GJ · Cndair CL6002C10SDR DALA2014111906178Receptacle · wornMAINTENANCE 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.Nov 18, 2014 · N926DL · Doug MD88SDR DALA2014111106048Release Cable · misroutedMAINTENANCE DISCOVERED THAT THE TAILCONE EXTERIOR RELEASE CABLE WAS MISROUTED. THIS IS NOT IN COMPLIANCE WITH 14 CFR, PART 121.703. THE CABLE ROUTING WAS CORRECTED IAW THE MM.Nov 10, 2014 · N915DL · Doug MD88SDR REXA2014110801128Support Channel · looseTASK CARD 900-53-900-106 MLG FAIRING LT VERTICAL SUPPORT CHANNEL IS LOOSE WHERE IT SECURES TO THE LOWER SUPPORT CHANNEL. SUSPECT VERTICAL SUPPORT CHANNEL FASTENER HOLE IS WORN PN CC670-85500-1 DWG CC670-85500. R & R LT MLG VERTICAL SUPPORT CHANNEL REATTACHEDNov 8, 2014 · N902XJ · Cndair CL6002D24SDR R61A201411061168Skin · damagedDURING HEAVY CHECK, TAIL CONE HAS TWO CREASES ON LT SIDE. MAINTENANCE FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 51-31-01 AND ETD 2014-170-093789. CUTOUT SIZES FWD 3.9" X 1", AFT 6" X .9 UNDER 17.6 DOUBLER REQUIRES DAMAGE TRACKER ISSUED 1 IAW GMM 5.1Nov 6, 2014 · N805MD · Emb ERJ170100SUSDR DALA2014110605998Pin · wornMAINTENANCE DISCOVERED THAT THE RELEASE LATCH TEE PIN FOR THE TAILCONE WAS FRAYED AND WORN OUT OF ALLOWABLE LIMITS. THE TEE PIN WAS REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS.Nov 3, 2014 · N952DL · Doug MD88SDR DALA2014110305881Release Cable · misroutedDURING LINE CHECK, MAINTENCE NOTED THE TAILCONE EXTERNAL RELEASE HANDLE CABLE WAS NOT ROUTED CORRECTLY. PROPERLY ROUTED IAW AMM 53-52-01.Nov 3, 2014 · N933AT · Boeing 717200SDR DALA2014103105873Release Cable · wornMAINTENANCE DISCOVERED THAT THE KEVLAR SLEEVE OVER THE RELEASE 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.Oct 30, 2014 · N905DL · Doug MD88SDR SWAA2014111134051Radome · crackedRADOME CRACKED 2.5 INCHES LONG 15 INCHES RT OF UPPER CTR BETWEEN 1ST & 2ND FASTENER HOLES. R & R RADOME IAW MM.Oct 29, 2014 · N409WN · Boeing 7377H4SDR DALA2014102905827Latch · wornLEFT UPPER TAILCONE LATCH WORN. R & R LATCH ASSEMBLY.Oct 28, 2014 · N957DN · Doug MD9030SDR SIMA20141026007Stiffener · crackedSTRAP & STIFFENER CRACKED BETWEEN PANELS 196DR & 196DL. R & R STRAP & STIFFENER FOR SPLICE BETWEEN PANELS 196DR & 195DL IAW AMM 51-42-13. PERFORMED ETN-CR-53-052 ON STIFFENER. APPLIED PROTECTIVE COATINGS TO ALL NEW PARTS IAW SRM 51-25-06 & 51-25-16.Oct 26, 2014 · N534AE · Cndair CL6002C10SDR DALA2014102405781Release Mech · out of rigAFT DOOR TAILCONE RELEASE TEST FAILED. FOUND OUT OF RIG. RIGGED AND TESTED IAW AMDS 5352-7116. OPS CHECK GOOD.Oct 24, 2014 · N954DN · Doug MD9030SDR CALA2014102392556Fairing · looseAIRFRAME VIBRATION ONCE AIRBORNE, EMER DECLARED, RETURNED. SECURED & APPLIED TAPE TO FILLET FAIRING ON LT SIDE OF FUSELAGE. COMPLETED INSPECTION OF FUSELAGE, NO DEFECTS FOUND.Oct 22, 2014 · N824UA · Airbus A319131SDR DALA2014102005636Cable · out of adjustDURING FUNCTIONAL TEST OF TAIL CONE RELEASE SYSTEM, FOUND LOCK CABLE TO BE OUT OF ADJUSTMENT AS REQUIRED IAW AMM 53-52-01-720, STEP F, E, 5 ADJUSTED IAW 53-52-01. COMPLETED FUNCTIONAL CHECK. OPS CKS GOOD. RII COMPLETE.Oct 19, 2014 · N899AT · Boeing 717200SDR DALA2014101905639Release Cable · misroutedDURING HYDRAUIC TROUBLESHOOTING IN THE TAIL CONE AREA, MAINTENANCE NOTICED THE TAIL CONE RELEASE CABLE MISROUTED AND RUBBING ON STRUCTURE. REROUTED CABLES IAW AMM 53-52-01, FIG'S 503 AND 504. LOCK CABLE AND PULL CABLE HAD NO TURNBUCKLES BROKEN OR TENSIONS DIOct 18, 2014 · N899AT · Boeing 717200SDR HYIA20141017054Fairing · out of alignmentREPAIR REQUIRED FOR THE MLG BELLY FAIRING PANEL 192FR PN S5247121200900. THE REPAIR IS NECESSARY DUE TO NUMEROUS AREAS OF GAPS & AERODYNAMIC MISMATCH WITH THE ADJACENT PANELS. IAW EO ATR-53-69-2014.Oct 17, 2014 · N14834 · Aerosp ATR42320SDR DALA2014102005715Slide Block · wornDURING CHECK, MAINTENANCE FOUND THE UPPER LT SLIDING BLOCK FOR THE TAIL CONE RELEASE CABLE WAS WORN. MAINTENANCE REPLACED BOTH THE UPPER LT AND RT CABLE BLOCKS AND A FUNCTIONAL TEST WAS PERFORMED.Oct 17, 2014 · N992DL · Doug MD88SDR DALA2014102005714Release Cable · corrodedDURING CHECK, MAINTENANCE FOUND THE TAIL CONE RELEASE CABLE CORRODED AND DAMAGED. MAINTENANCE REPLACED THE CABLE AND A FUNCTIONAL CHECK WAS PERFORMED.Oct 17, 2014 · N992DL · Doug MD88SDR HYIA20141017039Fairing · corrodedCORROSION DAMAGE ON LT MLG FAIRING AT FRAME 28A IAW FIGURES 2 & 3. THE CORROSION WAS CLEANED AWAY & BLENDING WAS PERFORMED AT THE LOCAL DAMAGED AREAS. NDT WAS THEN PERFORMED TO RECORD MATERIAL LOSS & DETERMINED THAT THE PART WAS FREE OF DEFECTS IAW EO ATR-53Oct 17, 2014 · N14834 · Aerosp ATR42320SDR HYIA20141017032Fairing · corrodedCORROSION FOUND ON FRAME 24A LT & RT SIDES IN MLG FAIRING. UPON REMOVAL OF PAINT CORROSION WAS FOUND IN AREAS SHOWN IN SECTION 2.0. CORROSION WAS CLEANED AWAY & BLENDING WAS PERFORMED AT THE LOCAL DAMAGED AREAS. NDT WAS THEN PERFORMED TO RECORD MATERIAL LOSOct 17, 2014 · N14834 · Aerosp ATR42320SDR HYIA20141017016Attach Angle · corrodedREPAIR REQUIRED FOR THE BELLY FAIRING UPPER ATTACH ANGLE ON FAIRING 192HR. UPON REMOVAL OF PAINT, CORROSION WAS FOUND. CORROSION WAS CLEANED AWAY & BLENDING WAS PERFORMED AT THE LOCAL DAMAGED AREAS. NDT WAS THEN PERFORMED TO RECORD MATERIAL LOSS & DETERMINEOct 17, 2014 · N14834 · Aerosp ATR42320SDR FDEA201410133146Angle · crackedRIGHT WING UPPER SURFACE APPROX 30 INCHES AFT OF R3 DOOR LOWER ANGLE AT SUPPORT FOR FAIRING PANEL 152DT IS CRACKED. FABRICATED & INSTALLED NEW ANGLE IAW DWG ANB7142.Oct 13, 2014 · N40061 · Doug MD1010FSDR DALA2014101405514Spring · brokenTAILCONE RELEASE INTERNAL HANDLE SPRING BROKEN. R & R SAME IAW AMM. OPS CHECKS GOOD.Oct 10, 2014 · N931DN · Doug MD9030SDR DALA2014101005527Attach Fitting · missingMAINTENANCE FOUND A MISSING CLIP ON THE INTERNAL RELEASE HANDLE OF THE TAILCONE. MAINTENANCE INSTALLED A CLIP.Oct 9, 2014 · N972DL · Doug MD88SDR SWIA201439576Panel · damagedVERTICAL STAB, TAIL CONE PANEL 326CT HAS TWO HOLES ON LT SIDE. C-CHECK, REMOVED AND INSTALLED AFT FRAME AND AFT FAIRING, 326CT ASSEMBLY IAW AMM 55. REPAIRED TAIL CONE PANEL 326CT REF STS EA.Oct 9, 2014 · N609SK · Cndair CL6002C10SDR DALA2014100905487Sleeve · wornMAINTENANCE DISCOVERED THAT THE KEVLAR SLEEVE OVER THE RELEASE 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.Oct 8, 2014 · N919DL · Doug MD88SDR DALA2014101405534Cam · wornMAINTENANCE FOUND A WORN TAILCONE CAM BASE. MAINTENANCE REPLACED THE TAILCONE CAM BASE AND THE RII STEPS WERE COMPLETED.Oct 7, 2014 · N975DL · Doug MD88SDR DALA2014100905486Release Cable · out of rigMAINTENANCE DISCOVERED THAT THE TAILCONE RELEASE CABLE WAS OUT OF ALLOWABLE RIG LIMITS AS IT DID NOT CLEAR THE CONDUIT BY THE SPECIFIED .2". THE CABLE CLAMPS WERE ADJUSTED AND THE SYS WAS RIGGED BACK INTO SPECIFICATIONS. THE RII STEPS WERE COMPLETED.Oct 7, 2014 · N945DL · Doug MD88SDR DALA2014100905485Cam · wornMAINTENANCE 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.Oct 7, 2014 · N945DL · Doug MD88SDR DALA2014100905484Conduit · wornMAINTENANCE DISCOVERED THAT THE LT AND RT SIDE CONDUIT FOR THE RELEASE CABLE OF THE TAILCONE WAS WORN OUT OF ALLOWABLE LIMITS. THE CONDUIT TUBE WAS REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS. THE FUNCTIONAL CHECK WAS COMPLETED SATISFACTORILY.Oct 7, 2014 · N945DL · Doug MD88SDR DALA2014100605426Panel · out of toleranceDURING TAILCONE RELEASE FUNCTIONAL CHECK, AFT ENTRANCE DOOR ROD FAILED TO PUNCTURE DECAL AND EXTEND. FOUND INTERFERENCE FROM DECORATIVE DOOR PANEL AROUND CAM ARM ASSY. TRIMMED DECORATIVE DOOR PANEL FOR CLEARANCE. OPS CHECKED GOOD IAW AMM 53-53-00-501 AND AMOct 6, 2014 · N945DL · Doug MD88SDR SIMA20141005001Support Bracket · crackedFAIRING SUPPORT BRACKET IN THE RT MAIN WW BELOW THE SIDE BRACE PINTLE PIN IS CRACKED. R & R WEB BRACKET IAW AMM 20-21-00.Oct 5, 2014 · N535EA · Cndair CL6002C10SDR FDEA201409302871Support · corrodedRIGHT AFT BODY FAIRING AFT SUPPORT SHOWING EXFOLIATION CORROSION. REPAIRED IAW EA 8-5320-T0311923.Sep 30, 2014 · N564FE · Doug MD1010FSDR REXA2014092901021Support Channel · looseMAIN LANDING GEAR FAIRING RT VERTICAL SUPPORT CHANNEL IS LOOSE WHERE IT SECURES TO THE LOWER SUPPORT CHANNEL DUE TO ATTACH SCREW PULLING THROUGH THE VERTICAL SUPPORT CHANNEL. REMOVED RT MLG VERTICAL SUPPORT CHANNEL. REPLACED, MATCH DRILLED & INSTALLED NEW RTSep 29, 2014 · N936XJ · Cndair CL6002D24SDR DALA2014093005357Latch · failedDURING THE TAILCONE RELEASE SYSTEM OPS CHECK, MAINTENANCE FOUND THAT THERE WAS EXCESSIVE TENSION IN THE RELEASE CABLE SYSTEM. THE TAILCONE UPPER RT LATCH PIN HUNG ON THE DROP. MAINTENANCE REPLACED THE LATCH AND CLEANED AND LUBED THE CABLE CONDUITS AND TAILCOSep 29, 2014 · N946DL · Doug MD88SDR REXA2014092701019Support Channel · looseMAIN LANDING GEAR FAIRING LT VERTICAL SUPPORT CHANNEL IS LOOSE WHERE IT SECURES TO THE LOWER SUPPORT CHANNEL. SUSPECT VERTICAL SUPPORT CHANNEL FASTENER HOLE IS WORN. PN CC670-85500-1 DWG CC 670-85500. REMOVED, DRILLED & INSTALLED NEW VERTICAL SUPPORT CHANNESep 27, 2014 · N936XJ · Cndair CL6002D24SDR SWAA2014093032468Attach Fitting · crackedLOWER RT WING TO BODY FAIRING ATTACH TEE CHORD CRACKED AT BS 727. R & R CHORD IAW DWG.Sep 21, 2014 · N604SW · Boeing 7373H4SDR DALA2014100705427Cam · wornWORN TAILCONE RELEASE CAM BS 1510 AT 10 O'CLOCK POSITION. TAIL ONE RELEASE CAM REPLACED IAW AMM 53-53-02.Sep 20, 2014 · N972DL · Doug MD88SDR DALA2014092205207Release 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. THE RII STEPS WERE COMPLETED.Sep 20, 2014 · N972DL · Doug MD88SDR SWAA2014093032446Skin Splice · crackedTAIL CONE, APU EXHAUST AFT MOUNTING RING AT 9 O'CLOCK POSITION INTERIOR SKIN SPLICE CRACKED. R & R SKIN SPLICE IAW SRM & DWG.Sep 19, 2014 · N355SW · Boeing 7373H4SDR SWAA2014093032445Skin Splice · crackedTAIL CONE, APU EXHAUST AFT MOUNTING RING AT 3 O'CLOCK POSITION INTERIOR SKIN SPLICE CRACKED. R & R SKIN SPLICE IAW SRM & DWG.Sep 19, 2014 · N355SW · Boeing 7373H4SDR CALA2014091892235Attach Fitting · corrodedFORWARD CARGO BILGE BELLY FAIRING ATTACH HAS CORROSION AROUND RIVETS ON SKIN FRAME 30 - 31 STRINGER 42L. CORROSION REMOVED IAW SRM 53-21-11DIAGRAM 105 PARA 4 E.Sep 13, 2014 · N854UA · Airbus A319131SDR DALA2014091605065Cable · frayedNITROGEN CYLINDER PULL CABLE HAS BROKEN STRANDS. R & R LANYARD.Sep 13, 2014 · N962DN · Doug MD9030SDR UHLA2014091100664Skin · damagedTAILCONE HAS DAMAGED AND CRACKED ON TOP, EIGHT INCHES AFT OF APU BULKHEAD, THREE INCHES LEFT OF CENTERLINE. CUTOUT DAMAGED AREA, FABRICATED REPAIR DOUBLER IAW ETD2014-170-077115.Sep 11, 2014 · N640RW · Emb ERJ170100SESDR SWAA2014100232516Angle · crackedTAIL CONE ANGLE CRACKED AT UPPER SURFACE FAIRING APU EXHAUST AREA. R & R ANGLE IAW SRM & DWG.Sep 9, 2014 · N352SW · Boeing 7373H4SDR NI6R201409110020Fairing · wrong partFOUND LT MLG FAIRING CHAFING FUSELAGE. DETERMINED THAT AFTERMARKET FAIRING PRODUCED BY UNDER PMA SA-1741005-239 TO BE MADE OF FIBERGLASS, AND AFTER APPROXIMATELY 800 FLIGHT HOURS, IT CHAFED THROUGH THE .051 SHEET METAL FUSELAGE SKIN IN SEVERAL CONTACTING AREASep 9, 2014 · N758HS · Cessna R172KSDR V0XD20140911179Angle · corrodedAFT BODY FAIRING SUPPORT WEB & ANGLE ARE CORRODED. REPAIRED SUPPORT STRUCTURE BY REMOVING LIGHT SURFACE CORROSION & TREATING IAW SRM 51-21-06 & 51-25-06. R & R ANGLE IAW SRM 51-42-06. WORK ORDER 80245 WC 1074.Sep 8, 2014 · N668CA · Cndair CL6002C10SDR DALA2014090904957Tail Cone · looseMAINTENANCE DISCOVERED THAT THE RT UPPER AND LOWER RELEASE SPADE RECEPTACLES FOR THE TAILCONE HAVE LOOSE AND MISSING HARDWARE. THE RECEPTACLE HARDWARE WAS REPLACED AND THE SYS WAS RIGGED TO SPECIFICATIONS. THE FUNCTIONAL CHECK WAS COMPLETED SATISFACTORILY.Sep 8, 2014 · N907DL · Doug MD88
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