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 V0XR201205080038Fairing · brokenPASSENGER DOOR FWD HINGE FAIRING BROKEN. REMOVED AND ATTEMPTED REPLACEMENT, MOUNT HOLES TRANSFERRED FROM ORIGINAL FAIRING TO NEW REPLACEMENT FAIRING, RESULTED UPON INSTALLATION OF NEW FAIRING THE TRANSFERED FAIRING MOUNT HOLES WERE MISALIGNED TO THE FUSELAGE May 10, 2012 · N390CA · Cndair CL6002C10SDR DALA1230260984Plate · wornWHILE DOING TAILCONE FUNCTIONAL CHECK, OPN 6908 AD, INSPECTION WROTE UP TAILCONE ALIGNMENT PIN RECEPTACLES 20 EA AS WORN/ELONGATED. REPLACED 20 RECEPTACLES.May 8, 2012 · N984DL · Doug MD88SDR DALA1229760990Tail Cone · wornDURING SERVICE CHECK, MAINTENANCE FOUND TAILCONE INTERIOR RELEASE T-PIN SLOTS WORN. INSTALLED NEW RELEASE T-PIN PER AMM. FUNCTIONAL CHECK PER 6808AD.May 6, 2012 · N990DL · Doug MD88SDR USAA2012050900006Support · corrodedC1 CHECK - LEVEL 2 GALVANIC CORROSION ON BELLY FAIRING SUPPORT BETWEEN FR40 TO FR44, -Y430. REPLACED BELLY FAIRING SUPPORT BETWEEN FR40 TO FR44, -Y430 IAW A330 SRM 51-72-11 & 51-42-11.May 5, 2012 · N270AY · Airbus A330323SDR USAA2012050700008Support · crackedC1 CHECK - CRACK ON BELLY FAIRING SUPPORT AT FR53.2, OUTBOARD OF S35L. REPAIRED BELLY FAIRING SUPPORT AT FR53.2, OUTBOARD OF S35L IAW A330 SRM 53-35-14, FIG. 202.May 4, 2012 · N270AY · Airbus A330323SDR VNAA2012050300004Radome · damagedCREW REPORTED TOP STATIC WICK ON LEFT WINGLET MISSING, WITH SOME BURN DAMAGE VISIBLE. CREW ALSO REPORTED POSSIBLE LIGHTNING STRIKE DAMAGE TO TAIL CONE. MAINTENANCE PERFORMED LIGHTNING STRIKE INSPECTION, REMOVED AND REPLACED RADOME AND LEFT WINGLET TIP FAIRINMay 3, 2012 · N244PS · Cndair CL6002B19SDR ALGA2012050202Skin · corrodedLOWER SKIN CORRODED BEYOND LIMITS AT STA 69.00.May 2, 2012 · Bell 412EPSDR FDEA201204291668Frame · crackedTAIL CONE ASSY DOOR 317AL HOLD OPEN ROD BRACKET SUPPORT WEB HAS 4 EA FASTENERS PULLING THRU SKIN. REMOVED HOLD OPEN ROD FOR FOM IAW SRM 51-40-21. REMOVED INTERNAL CLOSE OUT SKIN IAW SRM 51-40-21. UPON REMOVAL OF CLOSE OUT SKIN 3" CRACK WAS FOUND ON FR 103A BEApr 29, 2012 · N656FE · Airbus A300F4605RSDR DALA1228680945Release Cable · out of rigPERFORMED TAILCONE RELEASE SYSTEM OPERATIONAL CHECK 6908 AND FOUND THAT THERE WAS EXCESSIVE SLACK IN THE LOWER TAILCONE RELEASE CABLE. THE CABLE SYSTEM WAS RE-RIGGED AND THE LATCH LEVER CLAMP E WAS ADJUSTED. THE RII STEPS WERE COMPLETED AND THE FOLLOW-UP CHEApr 28, 2012 · N945DL · Doug MD88SDR DALA1227889940Cam · wornCOMPLIED WITH FUNCTIONAL CHECK OF TAILCONE RELEASE SYSTEM. FOUND RELEASE CAM BASE WORN IN 2 SPOTS. FAILED TORQUE CHECK REPLACED BASE.Apr 28, 2012 · N3322L · Doug DC932SDR DALA1227200912Bushing · wornDURING PSV "P" IN MSP WHILE PERFORMING OPN 6908 FOR THE TAIL CONE FUNCTIONAL CHECK AFT PASSENGER DOOR PULL TEST FAILED. PULL TEST SHOWED 28 LBS VERSUS THE REQUIRED 10 TO 20 LBS. THE "T" PIN AND BUSHINGS WERE REPLACED ON N/R #137, TAIL CONE FUNCTIONAL RE-PERFApr 26, 2012 · N912DL · Doug MD88SDR DALA1226559013Cam · wornDURING OPERATION 6908 FUNCTIONAL CHECK OF TAIL CONE RELEASE SYSTEM, MAINTENANCE FOUND TEE PIN 11 WORN WITH BUSHING AND BASE FOR RELEASE CAM WORN. REMOVED AND REPLACED TEE PIN 11 AND CAM ASSEMBLY PER AMM. RII COMPLETED FUNCTIONAL CHECK GOOD.Apr 25, 2012 · N913DE · Doug MD88SDR DALA1228730909Tail Cone · out of limitsDURING FUNCTIONAL CHECK OF TAILCONE RELEASE SYSTEM, MAINTENANCE FOUND THE GAP BETWEEN PIN AND ROD WAS BEYOND ALLOWABLE LIMITS. THE PIN WAS ADJUSTED AND BROUGHT WITHIN LIMITS AND THE RII COMPLETED.Apr 22, 2012 · N909DL · Doug MD88SDR DALA1228720909Release Cable · out of limitsPERFORMED TAILCONE RELEASE SYSTEM OPERATIONAL CHECK (6908) AND FOUND THE TAILCONE EXTERIOR RELEASE CABLE WAS OUT OF ALLOWABLE LIMITS. THIS DISCREPANCY WAS LOCATED AT THE CLAMP TO THE INTERIOR RELEASE CABLE SYSTEM. THE CABLE WAS ADJUSTED AND RIGGED BACK INTO Apr 22, 2012 · N909DL · Doug MD88SDR DALA1228710939Release Cable · misriggedMAINTENANCE DISCOVERED THAT THE TAILCONE EXTERNAL RELEASE HANDLE CABLE WAS ROUTED IN THE WRONG DIRECTION. THIS IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. THE CABLE ROUTING WAS CORRECTED PER THE MAINTENANCE MANUAL.Apr 22, 2012 · N939DL · Doug MD88SDR DALA1228700961Bushing · wornDURING FUNCTIONAL CHECK OF TAILCONE RELEASE SYSTEM, MAINTENANCE FOUND THE TEE PIN, BUSHING, AND UPPER RIGHT CLAMP BLOCK WORN BEYOND LIMITS. THE TEE PIN BUSHINGS AND CLAMP BLOCK WERE BOTH REPLACED AND THE RII COMPLETED. FOLLOWUP FUNCTIONAL WAS CHECK GOOD.Apr 22, 2012 · N961DL · Doug MD88SDR DALA1228760929Mechanism · out of limitsAIRCRAFT FAILED STEP 7 OF THE TAILCONE RELEASE SYSTEM OPERATIONAL CHECK. THE RELEASE MECHANISM CAM EXCEEDED THE ALLOWABLE TORQUE LIMIT. THE SYSTEM WAS CLEANED, LUBRICATED, AND THE SPRING TENSION ADJUSTED PER MANUAL. THE RII STEPS WERE COMPLETED AND SIGNED OApr 21, 2012 · N929DL · Doug MD88SDR DALA1228750929Release Cable · wornCHECK FAILED STEP 21 OF THE TAILCONE RELEASE SYSTEM OPERATIONAL 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. Apr 21, 2012 · N929DL · Doug MD88SDR DALA1228740929Tail Cone · out of limitsAIRCRAFT FAILED THE FUNCTIONAL CHECK OF TAILCONE RELEASE SYSTEM, DUE TO THE GAP BETWEEN PIN AND ROD WAS BEYOND ALLOWABLE LIMITS. THE PIN WAS ADJUSTED AND BROUGHT WITHIN LIMITS AND THE RII COMPLETED.Apr 21, 2012 · N929DL · Doug MD88SDR DALA1225589001Rod · out of rigDURING TAIL CONE FUNCTIONAL CHECK A/C JIC CARD OPN 6908AD THE AFT ENTRANCE DOOR EXTEND ROD WAS FOUND OUT OF RIG. THE ROD WAS ADJUSTED PER OPN 6908AD AND THE MD -88 AMM 53-53-00 AND THE OPS CHECK WAS GOOD.Apr 21, 2012 · N901DE · Doug MD88SDR CIEA2012042600001Fairing · detached(FLIGHT DISCREPANCY) - THE LT AFT WING TO FUSELAGE FAIRING, BECAME PARTIALLY DETACHED IN FLIGHT. FAIRING DID NOT COMPLETELY DETACH FROM AIRPLANE.Apr 20, 2012 · N113Y · Lear 55LEARSDR UALA2012042002371Radome · damagedON WALKAROUND FOUND DAMAGE TO NOSE RADOME. DAMAGE IS LOCATED ON LOWER LEFT RADOME APPROXIMATELY 11 INCHES BELOW CENTER LINE AND STARTS APPROXIMATELY IN LINE WITH FWD EDGE OF LIGHTENING DIVERTER. DAMAGE CONSISTS OF A DENT THAT MEASURE S 5" LONG BY 3.5" WIDE AApr 19, 2012 · N226UA · Boeing 777222SDR UIEA2012050700195Support · corrodedCORROSION ON LWR CHORD OF WING TO BODY FAIRING SUPPORT STRUCTURE BS 987.35 FROM LBL 14 TO RBL 14. REPLACED WITH NEW LWR CHORD IAW SRM 51-40-02 REV 20.Apr 18, 2012 · N747BC · Boeing 7474J6SDR DXTA2012082105100Skin · crackedTAILCONE SKIN CRACK DAMAGED AT APU HEAT SHIELD ATTACHMENTS. COMPLETED MFG REPAIR DEFINITION ATA53/03RD.Apr 11, 2012 · N655QS · Cessna 560XLSDR AALA20120410013Radome · puncturedINFLIGHT, CREW REPORTED POSSIBLE LIGHTNING STRIKE DAMAGE. FLIGHT DIVERTED & LANDED WITHOUT INCIDENT. DISCOVERED A PUNCTURE IN UPPER RADOME. REPLACED RADOME. SYSTEM GROUND CHECKED NORMAL.Apr 10, 2012 · N699AN · Boeing 757223SDR DALA1221349219Cable · brokenDURING SCHEDULED SLIDE DEPLOYMENT, CABLE BROKE ON TAIL CONE NITROGEN ASSIST BOTTLE. INSTALLED NEW NITROGEN ASSIST BOTTLE PER MM AND ALUMINUM WASHERS PER REPAIR ORDER 842417.Apr 9, 2012 · N919DN · Doug MD9030SDR VNAA2012040500003Radome · damagedCREW REPORTED POSSIBLE LIGHTNING STRIKE IN FLIGHT. MAINTENANCE PERFORMED LIGHTNING STRIKE INSPECTION, REMOVED AND REPLACED RADOME DUE TO BURN ON LOWER RIGHT HAND LIGHTNING STRIP AND REPAIRED BURN MARK DAMAGE ON RIGHT NOSE LANDING GEAR DOOR, LOWER FORWARD FUSEApr 5, 2012 · N718PS · Cndair CL6002C10SDR GLBA2012040202Fairing · damagedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A HOLE IN THE FUSELAGE FARING, RT SIDE UNDER AFT WING, AFT OF FS 363.250, 2.25 INCHES JUST ABOVE STRINGER 1R, .687 BY .25. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-53-01Apr 2, 2012 · N210GL · Beech 1900DSDR USAA2012033000001Frame · corrodedC1 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLANGE (BELLY FAIRING FRAME) AT FR39, Y1095. REPLACED FLANGE (BELLY FAIRING FRAME) AT FR39, Y1095 IAW A330 SRM 53-35-14 FIG 104 & 51-42-11.Mar 28, 2012 · N274AY · Airbus A330323SDR DALA1217049008Release Cable · sticksDURING INSPECTION THE TAIL CONE RELEASE CABLE WAS FOUND TO BE STICKING. MAINTENANCE REPLACED THE TAIL CONE RELEASE CABLE AND THE FUNCTIONAL CHECK WAS GOOD.Mar 17, 2012 · N908DE · Doug MD88SDR IXXA20120306006SRadome · damagedNOSE RADOME DAMAGED. R & R NOSE RADOME IAW MM 53-50-1.Mar 5, 2012 · N603AL · Doug DC873FSDR DALA1212560989Release System · out of adjustTHE TAIL CONE FAILED TO DROP. CABIN INTERIOR PULL TEST DID NOT FUNCTION. NO CORRECTIVE ACTION IDENTIFIED PER TO NRC 122. MRR 121256. MAINTENANCE FOUND THE INTERIOR LOCK CABLE TO BE BINDING IN THE SUPPORT FITTING. THE SYSTEM WAS RE-RIGGED AND ADJUSTED PER MMar 4, 2012 · N989DL · Doug MD88SDR DALA1212570959Tail Cone · failedTHE TAIL CONE RELEASE FUNCTIONAL CHECK FAILED THE PULL TEST. AMOUNT THAT SCALE EXCEEDED ALLOWABLE LIMITS WAS NOT SPECIFIED. NO CORRECTIVE ACTION IDENTIFIED PER TO NEC 139. MRR 121257. (2012-D0233) LP #DL0004253.Mar 4, 2012 · N959DL · Doug MD88SDR HNAA2012030200634Radome · damagedPOSSIBLE LIGHTNING STRIKE OR STATIC DISCHARGE ON APPROACH. NO VISIBLE STORMS IN THE AREA. NO LOSS OF INSTRUMENTS. MX FOUND NOSE CONE AND TAIL CONE DAMAGE FROM LIGHTNING STRIKE. ACFT STILL IN MX.Mar 2, 2012 · N807EX · Dhav DHC8102SDR COEA2012022101821Panel · separatedAIRCRAFT SUFFERED AN INFLIGHT SEPARATION OF THE STARBOARD CENTER LATERAL PANEL OF THE WING TO FUSELAGE FAIRING. THE SEPARATION OCCURRED EN ROUTE AND HAD JUST BEEN GIVEN DISCRETION FROM FL 190 TO 10,000 FEET. JUST AFTER THE TOP OF THE DESCENT THE CREW HEARD AFeb 21, 2012 · N821FX · Aerosp ATR72212SDR WX0A2012021671116Radome · damagedPOSSIBLE DAMAGE DUE TO BIRD STRIKE IN RADOME, COMPLIED WITH INSPECTION IAW AMM 05-51-08 & TASK CARD 10900513, FOUND RADOME DAMAGE. REMOVED AND REPLACED RADOME IAW AMM 53-51-00. AIRCRAFT RETURNED TO SERVICE.Feb 16, 2012 · N418NV · Doug MD83SDR ZZDA2012189Release Mech · failedTAIL CONE CAM RELEASE MECHANISM, FAILED DURING DEPLOYMENT. ACCOMPLISHED CAM RELEASE MECHANISM ADJUSTMENT PER B717 MM 53-52-03 AND 53-52-01. SEE NR 25139.Feb 14, 2012 · N939AT · Boeing 717200SDR DALA1209139208Release Cable · frayedTAIL CONE JETTISON BOTTLE CABLE FRAYED. REMOVED AND REPLACED CABLE. INSTALLED ON AIRCRAFT SIDE. CONNECTION TO TAIL CONE ACCOMPLISHED.Feb 11, 2012 · N908DA · Doug MD9030SDR DALA1209129208Screw · looseTAIL CONE JETTISON NOZZLE, MISSING SCREW AND OTHER OTHER SCREWS LOOSE. INSTALLED NEW SCREW AND TIGHTENED REMAINING 3 LOOSE SCREWS.Feb 11, 2012 · N908DA · Doug MD9030SDR DALA1209119208Release Cable · misinstalledTAIL CONE JETTISON BOTTLE ACTUATION CABLE IMPROPERLY INSTALLED, WRAPPED AROUND BOTTLE. REMOVED AND REPLACED CABLE.Feb 11, 2012 · N908DA · Doug MD9030SDR DALA1207420974Release Cable · misroutedTAIL CONE RELEASE MECHANISM INSTALLATION FAILED ROUTINE INSPECTION IN LGA. THE LANYARD WAS FOUND TO BE INCORRECTLY INSTALLED. MAINTENANCE DID CORRECT THE ROUTING PER AMM 53-53-00-401 FIG 402 VIEW A.Feb 10, 2012 · N974DL · Doug MD88SDR USAA2012041300013Support · corrodedS2 CHECK - LEVEL 2 GALVANIC CORROSION ON LOWER FUSELAGE FAIRING SUPPORT AT FR40 BETWEEN -Y450 & Y450. REPLACED LOWER FUSELAGE FAIRING SUPPORT AT FR40 BETWEEN -Y450 & Y450 IAW A330 SRM 51-74-00, 53-35-14 PB 122 FIG 104 & 51-42-11.Feb 2, 2012 · N276AY · Airbus A330323SDR UALA2012020200658Panel · damagedFOUND DAMAGE UPON ARRIVAL ON PANEL 198WR, RT AFT WING TO BODY FAIRING .22 INCH LONG. WIDTH 1 INCH PAINT CRACKED, DEPTH 0.05. ACCOMPLISHED PERMANENT REPAIR.Feb 2, 2012 · N777UA · Boeing 777222SDR DALA1205629018Fastener · corrodedEXCESSIVE CORROSION WAS FOUND ON THE TAIL CONE RELEASE MECHANISM PULLEY PINS, BOLTS, AND NUTS AT STA 1510 CANT. THIS CORROSION WAS BEYOND ALLOWABLE LIMITS SO THE AFFECTED HARDWARE WAS REPLACED.Feb 2, 2012 · N918DE · Doug MD88SDR DALA1205619018Clamp · wornA CLAMP FOR THE TAIL CONE RELEASE MECHANISM CABLE WAS FOUND WORN AT STA 1510 CANT. THIS WEAR WAS BEYOND ALLOWABLE LIMITS SO THE CLAMP WAS REPLACED. FOUND DURING HMV.Feb 2, 2012 · N918DE · Doug MD88SDR DALA1205609018Conduit · wornTHE CONDUIT FOR THE TAIL CONE RELEASE MECHANISM CABLE WAS FOUND WORN AT STA 1510 & 5:00 POSITION. THIS WEAR WAS BEYOND ALLOWABLE LIMITS SO THE CONDUIT WAS REPLACED. FOUND DURING HMV.Feb 2, 2012 · N918DE · Doug MD88SDR ASOA201200400Fairing · erodedLEFT WING ROOT FAIRING 191BB, ERODED AT L/E AROUND SCREW HOLES. FOUND SCREW HOLES TO HAVE PAINT DELAMINATION WITH MINOR EROSION TO L/E, REPAIRED IAW SRM 51-14-06-00.Feb 1, 2012 · N825AS · Cndair CL6002B19SDR HNAA2012012700507Stiffener · crackedBOTH VERTICAL STIFFNERS UNDER RADOME CRACKED AT TOP RIVET. TRIM DAMAGED AREA OUT ON BOTH STIFFNERS IAW RD8-53-7275. COMPLIED WITH HFEC INSPECTION. NO DEFECTS NOTED. COMPLETED REPAIRS AS REQUIRED IAW RD8-53-7275.Jan 27, 2012 · N911HA · Dhav DHC8102SDR DALA1203600958Release Cable · misroutedMAINTENANCE DISCOVERED THAT THE TAIL CONE EXTERNAL RELEASE HANDLE CABLE WAS MISROUTED THROUGH THE PULLEY BRACKET. THIS COULD HAVE AN ADVERSE AFFECT ON THE OPERATION OF THE RELEASE SYSTEM AND IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. THE CABLE ROUTING WAJan 24, 2012 · N958DL · Doug MD88SDR QXEA2012012600093Bracket · crackedRT WING TO FUSELAGE FAIRING MOUNT BRACKET FOR PANEL 264AR IS CRACKED IN THE UPPER AFT CORNER. ACFT IS DOWN FOR C-CHECK. CUT OUT AFFECTED AREA IAW RD 8/4-53-2089. CONFIRMED CUTOUT CRACK FREE REF NTM 51-00-06-910-801 PT 1. APPLIED ALODINE AND PRIMED REPAIR IJan 23, 2012 · N400QX · Bombdr DHC8402
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