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 DALA13041200977Slider · wornTHE TAILCONE RELEASE CABLE BLOCK/SLIDER AT UPPER LT SIDE IS WORN. REPLACED CABLE BLOCK/SLIDER AT UPPER LT SIDE IAW AMM 53-53.Aug 23, 2013 · N977DL · Doug MD88SDR DALA13041190977Slider · wornTHE TAILCONE RELEASE CABLE BLOCK/SLIDER AT UPPER RT SIDE WAS FOUND TO BE WORN. REPLACED CABLE BLOCK/SLIDER AT UPPER RT SIDE IAW AMM 53-53.Aug 23, 2013 · N977DL · Doug MD88SDR DALA13041180977Cable · chafedTHE TAILCONE RELEASE LOCK CABLE HAS CHAFED THRU THE PROTECTIVE SLEEVE. THE RELEASE CABLE WAS REPLACED AND THE REQUIRED INSPECTION WAS COMPLETED.Aug 23, 2013 · N977DL · Doug MD88SDR DALA13041170977Pin · wornTHE TAIL CONE RELEASE CABLE T-PIN WAS FOUND TO BE WORN. THE T-PIN WAS REPLACED AND THE REQUIRED INSPECTION WAS COMPLETED.Aug 23, 2013 · N977DL · Doug MD88SDR 2013FA0000493Tail Cone · corrodedCORROSION FOUND IN TAIL CONE INSPECTION, ON LOWER SKINS DUE TO NO WATER DRAINAGE AT LOW SPOTS.Aug 23, 2013 · N1DG · Bombdr BD7001A11SDR VNAA2013082100012Radome · damagedCREW REPORTED MULTIPLE BIRD STRIKE ON TAKEOFF. CREW ABORTED TAKEOFF AND RETURNED TO GATE. MX PERFORMED BIRD STRIKE INSPECTION, R & R DAMAGED RADOME AND RT RADOME LATCH AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.Aug 21, 2013 · N248PS · Cndair CL6002B19SDR CALA2013082190635Fairing · gougedON W-A FOUND GOUGE IN FUSELAGE. ON W-A FOUND GOUGE IN FUSELAGE BODY FAIRING 191DDL. DAMAGE PENETRATED OUTER SKIN OF PANEL LENGTH 4.25 INCHES. DEPTH 0.025 WIDTH 1 INCH. AS PER ECRA 5320-02141 ACP VISUAL CHECKED EVERY 500 HRS AND RPR PER PART 3 ON OR BEFORE Aug 21, 2013 · N120UA · Boeing 747422SDR DALA13039950925Receptacle · wornMX DISCOVERED THAT ALL OF THE TAILCONE RELEASE SYS GUIDE PIN RECEPTACLES WERE WORN BEYOND ALLOWABLE LIMITS. THE RECEPTACLES WERE REPLACED IAW SRM 51-30 AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS. THE FUNCTIONAL CHECK WAS COMPLETED SATISFACTORILY.Aug 19, 2013 · N925DL · Doug MD88SDR SWAA2013081919318Support Bracket · brokenWING TO BODY FAIRING RIB SUPPORT BRACKET BROKEN AT STATION 636, LONGERON 19R. R&R BRACKET IAW SRM.Aug 18, 2013 · N977AT · Boeing 717200SDR SWAA2013081919316Support Bracket · brokenWING TO BODY FAIRING RIB SUPPORT BRACKET BROKEN AT STATION 636, LONGERON 19L. R&R BRACKET IAW SRM.Aug 16, 2013 · N977AT · Boeing 717200SDR DALA13039690924Latch · unsecurePILOT DISCOVERED ONE TAILCONE RELEASE LATCH RECEPTACLE WAS POPPED AND ANOTHER WAS NOT FULLY LATCHED. THE RECEPTACLES WERE REATTACHED AND THE SYS CHECKED GOOD.Aug 16, 2013 · N924DL · Doug MD88SDR SWAA2013090519885Skin · delaminatedLT WING TO BODY FAIRING NR 3378 EXTERIOR SURFACE DELAMINATED NEAR THE LOWER EDGE AS MARKED. REPAIRED SURFACE IAW SRM.Aug 15, 2013 · N510SW · Boeing 7375H4SDR DALA13039620949Camshaft · corrodedMX DISCOVERED THAT THE EMERGENCY ESCAPE PATH TAILCONE RELEASE CABLE CAM SHAFT HAD CORRODED HARDWARE. THE NUTS WERE REPLACED AND THE SYSTEM WAS ADJUSTED.Aug 14, 2013 · N949DL · Doug MD88SDR DALA13039299020Cam · wornDURING SCHEDULED INSPECTION, THE TAILCONE RELEASE KEVLAR CABLE CAM BASE WAS FOUND TO BE WORN AT THE ROLLER GUIDES. THE CAM ASSY AND BASE WERE BOTH REPLACED IAW AMM 53-53 AND AMDS WC 5350-01077-0101. THE REQUIRED INSPECTIONS WERE COMPLETED.Aug 13, 2013 · N920DE · Doug MD88SDR DALA13039279020Slider · wornDURING SCHEDULED INSPECTION, THE TAILCONE RELEASE CABLE, CABLE CLAMP/SLIDER BLOCK WAS NOTED TO BE WORN AT THE UPPER RT LATCH. THE SLIDER BLOCK ASSEMBLY WAS REPLACED IAW AMM 53-53 AND THE RIG, FUNCTIONAL CHECK AND REQUIRED INSPECTIONS WERE COMPLETED.Aug 13, 2013 · N920DE · Doug MD88SDR DALA13039269020Pin · wornDURING SCHEDULED INSPECTION, THE TAIL CONE RELEASE TEE PIN CLEVIS AREA WAS NOTED TO BE WORN ON THE LT SIDE OF THE AFT ACCESSORY COMPARTMENT. THE TEE PIN WAS REPLACED IAW AMM 53-53 AND THE REQUIRED FUNCTIONAL CHECK AND REQUIRED INSPECTIONS WERE COMPLETED.Aug 13, 2013 · N920DE · Doug MD88SDR DALA13039259020Pulley · wornDURING SCHEDULED INSPECTION, THE TAILCONE RELEASE CABLE PULLEY WAS NOTED TO BE WORN AT THE 11 O'CLOCK POSITION AT STATION 1510 IN THE AFT ACCESSORY COMPARTMENT. THE PULLEY WAS REPLACED AND FUNCTIONAL CHECK AND REQUIRED INSPECTIONS WERE COMPLETED REF: AMDS WC Aug 13, 2013 · N920DE · Doug MD88SDR DALA13039229020Bushing · wornDURING SCHEDULED INSPECTION, TAILCONE RELEASE TEE PIN CLEVIS BUSHINGS WERE NOTED TO BE WORN ON THE LT SIDE OF THE AFT ACCESSORY COMPARTMENT. THE BUSHINGS WERE REPLACED IAW AMM 53-53 AND THE FUNCTIONAL CHECK AND REQUIRED INSPECTIONS WERE COMPLETED.Aug 13, 2013 · N920DE · Doug MD88SDR REXA2013081301583Sealant · missingLOUD POP AND AIRFRAME SHUDDER AT OR NEAR LEVEL OFF AT FL 250 FT SAME THING WHEN GEAR WAS EXTENDED JUST PRIOR TO DOWNLOCK GREEN GEAR. THIS ISSUE HAS HAPPENED THE LAST 4 LEGS AT TOP OF CLIMB. FOUND AERODYNAMIC SEALANT MISSING FROM LT & RT BELLY FAIRINGS L/E CAAug 13, 2013 · N831AY · Cndair CL6002B19SDR DALA13039280965Cam · wornDURING ROUTINE MX, THE LT TAILCONE RELEASE MECHANISM CAM WAS NOTED TO BE WORN IN TWO PLACES AT THE BASE. THE WORN CAM WAS REPLACED IAW AMM 53-53-2 AND THE REQUIRED INSPECTION WAS COMPLETED.Aug 11, 2013 · N965DL · Doug MD88SDR DALA13038850905Cable · out of rigDURING THE TAILCONE RELEASE SYSTEM FUNCTIONAL CHECK, MX FOUND THAT THERE WAS EXCESSIVE TENSION IN THE RELEASE CABLE SYSTEM. THE CABLE T-PIN CLIPS WERE RE-ADJUSTED AND THE SYSTEM WAS RE-RIGGED. THE RII STEPS WERE COMPLETED AND THE FOLLOW-UP CHECK WAS SUCCESSFUAug 9, 2013 · N905DL · Doug MD88SDR DALA13038840905Latch · wornDURING A CHECK OF TAILCONE RELEASE SYSTEM, MX FOUND THAT THE UPPER RT SIDE CABLE BLOCK FOR THE TAILCONE LATCH WAS WORN BEYOND ALLOWABLE LIMITS. MX REPLACED THE UPPER SLIDING BLOCKS FOR THE RT SIDE ONLY. THE TAILCONE WAS RIG CHECKED AFTER INSTALLATION AND FOUNAug 8, 2013 · N905DL · Doug MD88SDR DALA13038830905Arm · wornMX DISCOVERED THAT THE RT UPPER RELEASE LATCH LEVER FOR THE TAILCONE WAS WORN BEYOND ALLOWABLE LIMITS. THE LATCH LEVER ARM WAS REPLACED AND THE SYS WAS RIGGED TO SPECIFICATIONS. THE FUNCTIONAL CHECK WAS COMPLETED SATISFACTORILY.Aug 8, 2013 · N905DL · Doug MD88SDR C77A20130810012Panel · wornPANEL 192DL HAS SEVERAL FASTENER HOLES WORN AND ELONGATED IN THE COMPOSITE MATERIAL BETWEEN WHEEL WELL CUT OUTS, AFT EDGE. REPAIRED DAMAGED FASTENER HOLES IAW SRM II 51-72-06, 51-40-02 & 51-40-04.Aug 6, 2013 · N609CZ · Emb ERJ170200LRSDR CALA2013080790201Seal · failedVIBRATION IN BELLY, FAIRINGS & PASSENGER DOORS IAW TSM 05-50-00-810-801-A. VIBRATION INSPECTION PERFORMED IAW TSM. FOUND BAD SEAL ON PANELS 192 BT AND 192 DT.Aug 6, 2013 · N812UA · Airbus A319131SDR SWAA2013080918985Support · corrodedRT WING TO FS BODY FAIRING SUPPORT CORRODED AT STATION 832, BETWEEN STRINGER 30R TO STRINGER 24R. REPAIRED SUPPORT IAW SRM.Aug 5, 2013 · N978AT · Boeing 717200SDR SWAA2013083019736Angle · crackedLT WING TO BODY FAIRING TEE ANGLE CRACKED AT BS 727 BETWEEN STRINGER 21L & STRINGER 26L. R&R ANGLE IAW SRM & DRAWING.Aug 4, 2013 · N508SW · Boeing 7375H4SDR SWAA2013080918984Support · corrodedLT WING TO FS AFT BODY FAIRING SUPPORT CORRODED AT STATION 832, BETWEEN STRINGER 30L TO STRINGER 24L. REPAIRED SUPPORT IAW SRM.Aug 4, 2013 · N978AT · Boeing 717200SDR DALA13037470971Frame · bentDURING INSPECTION, TAILCONE L-FRAME WAS NOTED TO BE BENT AT THE 3:00 POSITION BETWEEN THE TAILCONE ALIGNMENT RECEPTICALS. NEW FRAME SECTION INSTALLED IAW SRM 51-01 AND DWG 9911957 AND THE REQUIRED INSPECTION WAS COMPLETED.Aug 4, 2013 · N971DL · Doug MD88SDR CALA2013080590122Radome · burnedRADOME HAS A BURN 11 O'CLOCK .25 DIA. DAMAGE AREA WITHIN LIMITS. REPLACED RADOME.Aug 3, 2013 · N447UA · Airbus A320232SDR SWAA2013081219024Angle · crackedFORWARD WING TO BODY FAIRING ANGLE CRACKED AT BS 540, STRINGER 24L. R&R ANGLE IAW SRM & DRAWING.Aug 2, 2013 · N508SW · Boeing 7375H4SDR SWAA2013080618874Plate · crackedWING TO BODY FAIRING ACCESS PANEL NR 3678R PLATE CRACKED. R&R PLATE IAW SRM.Aug 2, 2013 · N508SW · Boeing 7375H4SDR DALA13037540932Turnbuckle · brokenDURING INSPECTION, MX FOUND THAT THE TAILCONE CATWALK COUNTER BALANCE CABLE WAS BROKEN ON THE RT SIDE. THIS IS CONSIDERED A DEFECT IN THE EMERGENCY ESCAPE SYS AND COULD HAVE AN ADVERSE AFFECT ON THE EVACUATION ROUTE. THE MOVEABLE CATWALK COUNTER BALANCE CABLEAug 2, 2013 · N932DL · Doug MD88SDR USAA2013080200020Support Frame · cracked2S CHECK - CRACK IN FAIRING SUPPORT FRAME AT FR 56, S36L. REPAIRED SUPPORT FRAME IAW SRM 53-45-12, FIG. 214, 51-31-00, TABLE 4 & 51-75-12.Aug 1, 2013 · N765US · Airbus A319112SDR DALA13037130971Receptacle · wornDURING SCHEDULED INSPECTION, THE TAIL CONE ALIGNMENT PIN RECEPTICALS WERE FOUND TO BE WORN. THE RECEPTICALS WERE REPLACED IAW SRM 51-30 ON THE LT SIDE. THE RT RECEPTICALS WERE REPLACED ON A SEPARATE NON-ROUTINE CARD DUE TO A CORRESPONDING RT FRAME REPLACEMENTAug 1, 2013 · N971DL · Doug MD88SDR DALA13037120971Pin · wornDURING SCHEDULED INSPECTION IN MSP, THE TAIL CONE RELEASE CABLE T-PIN WAS NOTED TO BE WORN. THE T-PIN AND ASSOCIATED BUSHINGS WERE REPLACED IAW AMM 53-53, FIG 403 AND THE REQUIRED INSPECTION WAS COMPLETED.Aug 1, 2013 · N971DL · Doug MD88SDR DALA13037110971Bracket · wornDURING SCHEDULED INSPECTION IN MSP, THE TAIL CONE EVACUATION KEVLAR CABLE SPRING BRACKETS WERE FOUND TO BE WORN. NEW SPRING BRACKETS WERE INSTALLED AND THE REQUIRED INSPECTION WAS COMPLETED.Aug 1, 2013 · N971DL · Doug MD88SDR DALA13037100971Clamp · looseDURING SCHEDULED INSPECTION, THE TAIL CONE CABLE CONDUIT CLAMPS WERE FOUND TO BE LOOSE, WORN AND OUT OF POSITION. THE CABLE CONDUIT CLAMPS WERE REPLACED IN THE CORRECT POSITIONS AND THE REQUIRED INSPECTION WAS COMPLETED.Aug 1, 2013 · N971DL · Doug MD88SDR SWAA2013080618860Fairing · crackedRT OVERWING FAIRING NR 196CR CRACKED AT AFT LOWER CORNER. REPAIRED FAIRING IAW SRM.Jul 30, 2013 · N412WN · Boeing 7377H4SDR SWIA201334151Fairing · crackedWING TO FS FAIRING LT SIDE AFT HAS CRACK DAMAGE MEASURING 20" X 3 "ON THE LOWER AFT AREA. SERVICE REPAIR CRACKED DAMAGE ON WING TO FS FAIRING RT SIDE AFT IAW REO.Jul 29, 2013 · N790SK · Cndair CL6002C10SDR AALA20130729006Fairing · damagedPILOT REPORTED THERE WERE 3 FILLET FAIRING DAMAGED AFT OF THE WHEEL WELL. REPLACED LT SIDE PANELS 193CL, 194CL & BELLY PANEL 194DL.Jul 29, 2013 · N836NN · Boeing 737823SDR DALA13036799203Switch · inoperativeDURING TAILCONE RELEASE OPS CHECK, FOUND EXTERNAL TAILCONE RELEASE SWITCH INOPERATIVE, TAILCONE UNSAFE SWITCH. R & R SWITCH FOR EXTERNAL HANDLE RELEASE. OPS CHECKED GOOD IAW AMM. OK FOR SERVICE.Jul 29, 2013 · N903DA · Doug MD9030SDR CALA2013072990058Radome · damagedBS 1840 & 1900 GCS RADOME FASTENER HOLES MISDRILLED. REPAIRED IAW ECRA 5330-04636.Jul 28, 2013 · N179UA · Boeing 747422SDR DALA13036540972Bracket · wornDURING SCHEDULED INSPECTION, THE TAILCONE RELEASE SPRING BRACKETS WERE FOUND TO BE WORN ON THE LT & RT SIDES. REPLACED LT & RT SPRING BRACKETS IAW SRM 51-30. THE REQUIRED INSPECTION WAS COMPLETED.Jul 27, 2013 · N972DL · Doug MD88SDR DALA13036300972Bushing · wornDURING SCHEDULED INSPECTION, THE TAILCONE TEE PIN BUSHINGS WERE FOUND TO BE WORN. THE BUSHINGS WERE REPLACED IAW AMM 53-53 AND THE REQUIRED INSPECTION WAS COMPLETED.Jul 25, 2013 · N972DL · Doug MD88SDR DALA13036290972Cotter Pin · missingDURING SCHEDULED INSPECTION, THE TAILCONE CAM MECHANISM WAS NOTED TO HAVE MISSING COTTER PINS ON THE ROLLER BEARING BOLT NUTS. THE MISSING COTTER PINS WERE INSTALLED ON THE CAM MECHANISM IAW AMM 20-10-01 AND THE REQUIRED INSPECTION WAS COMPLETED.Jul 25, 2013 · N972DL · Doug MD88SDR DALA13036200972Bracket · damagedDURING SCHEDULED INSPECTION IN MSP, THE RT UPPER TAIL CONE LATCH BRACKET WAS NOTED TO HAVE A SHEARED FASTENER HEAD. THE FASTENER WAS REPLACED ON THE RT UPPER TAIL CONE LATCH BRACKET IAW SRM 51-30.Jul 25, 2013 · N972DL · Doug MD88SDR DALA13036190972Pin · rustedDURING SCHEDULED INSPECTION, THE LT & RT TAIL CONE SLIDER BLOCKS WERE FOUND TO HAVE RUSTED PINS. THE RUSTED PINS WERE REPLACED ON THE LT & RT SLIDER BLOCKS IAW AMM 20-10-01 AND THE REQUIRED INSPECTION WAS COMPLETED.Jul 25, 2013 · N972DL · Doug MD88SDR DALA13036839249Release Cable · corrodedTAILCONE RELEASE CABLE HAS CORROSION ON ALL CLEVIS COMMON TO YOKE, Y1567-895. R & R TAILCONE RELEASE CABLE NR 547 IAW AMM. RII COMPLIED WITH.Jul 24, 2013 · N949DN · Doug MD9030SDR DALA13036849249Release Cable · brokenDURING SERVICE CHECK, TAILCONE RELEASE CABLE ASSY RUN HAS A BROKEN WIRE. MX R & R TAILCONE CABLE ASSY RUN IAW MM. OPS CHECKED GOOD.Jul 23, 2013 · N949DN · Doug MD9030
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