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 MWEA060040Radome · bird strikeBIRDSTRIKE ON RADOME. REMOVED AND REPLACED RADOME.Apr 4, 2006 · N925ME · Boeing 717200SDR 2006UALA00608Radome · bird strikeBIRD STRIKE AFTER TAKEOFF. IMPACT BELOW NOSE. RADAR ANTENNA MAKES GRINDING NOISE DURING SWEEP. RADOME DAMAGED.Mar 28, 2006 · N448UA · Airbus A320232SDR DHL2006747002Fairing · damagedMX RELEASE FOR DROP IN VISIT FOR DAMAGE TO LT AFT BODY FAIRING AND FAIRING SUPPORT. MX RELEASE DONE ON 3-13-06 UNDER WORK ORDER 5001328.Mar 13, 2006 · N747DH · Boeing 727224SDR QXEA200600735Fairing · damagedYYC - C4 FUSELAGE EXTERIOR, RIGHT HAND WING ROOT FAIRING, BOTTOM EDGE AT STATION X384 HAS THREE LOOSE RIVETS. REPLACED IAW DHC-8-200 SRM 51-40-11, PAGES 1-4.Mar 8, 2006 · N350PH · Dhav DHC8202SDR QXEA200600734Fairing · damagedYYC - C4 FUSELAGE EXTERIOR LEFT HAND WING ROOT FAIRING AT STATION X427 NEAR BOTTOM EDGE HAS FOUR LOOSE RIVETS. REPLACED IAW DHC-8-200 SRM 51-40-00, PAGES 1-5 AND 51-40-11, PAGES 1-4.Mar 6, 2006 · N350PH · Dhav DHC8202SDR QXEA200600636Panel · corrodedPDX - C4 CHECK, ROOT FAIRING PANEL 262PT HAS CORRODED FASTENERS. REPAIRED IAW SRM 53-50-01.Mar 2, 2006 · N349PH · Dhav DHC8202SDR 2006UALA00337Structure · damagedDAMAGE TO THE HORIZONTAL STABILIZER AND TAIL CONE. MAJOR REPAIR ACCOMPLISHED. REPAIR DOUBLERS INSTALLED WITH AIRBUS RAS APPROVALS.Feb 21, 2006 · N854UA · Airbus A319131SDR USAA060264Support · corrodedSTA 780 - 800, BL 0, WEB FAIRING SUPPORT; CORROSION TASK C5319101. REMOVED & FAB'D NEW WEB SUPPORT & INSTALLED PER SRM 51-40-02, 51-40-03, 51-21-10, 53-00-71, DEFECT SIZE: 3"L X 1.3"W X .035"D.Feb 15, 2006 · N620AU · Boeing 7572B7SDR MWEA060014Cable · disengagedTAIL CONE ANNUNCIATOR CAME ON. FOUND TAIL CONE LOCK CABLE (INTERIOR HANDLE) DISENGAGED, RE-INSTALLED SAME CABLE.Feb 13, 2006 · N809ME · Doug DC982SDR USAA060180Support Angle · corrodedBELLY FAIRING SUPPORT ANGLE AFTER 44 BOTH SIDES OF CL CORRODED. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-72-11, 51-42-11, DEFECT SIZE: .125 INCH - 5 PLACES.Feb 1, 2006 · N677UW · Airbus A330323SDR CA060125004Cam · brokenHEARD A BANG DURING APPROACH, FOUND RT UPPER FWD COWL INNER PORTION HAD LIFTED FROM NORM POSITION. FOUND CAM BOLT FAILED THAT PROVIDES TENSION TO LWR COWL ASSY. OVER CTR COWL FASTENERS ON THESE A/C (4) INSTILL CONSIDERABLE FORCE AND HAVE A HISTORY ON ALL SIMJan 24, 2006 · Beech 1900CSDR FE5F200600001Clip · looseAFTER T/O, WHILE ALTITUDE 7000 FEET, THE PILOT FOUND TAILCONE UNSAFE LIGHT IS COMING ON, THEN AIRTURN BACK HOME BASE. DURING GROUND INSP FOUND LOCK CABLE IN INTERNAL WARNING SWITCH LOOSEN, IAW AMM 53-53-00 REPLACED CLIP AND REINSTALL LOCK CABLE OK, AND CHECK Jan 23, 2006 · N28007 · Doug MD83SDR MJYA0601018Fairing · crackedFUSELAGE WING TO BODY FAIRING FORMER REPAIRED DUE TO CRACK.Jan 6, 2006 · N767TW · Boeing 737230CSDR 06FDEA00029Radome · delaminatedRADOME, DELAMINATED/SWELLING ON INTERNAL SKIN FS 239. REMOVED AND REPLACED RADOME IAW MD10-10 MM 53-51-00-2 AND 20-50-02-2. SNRM N00335 OF WORK ORDER NR 0031297.Jan 5, 2006 · N359FE · Doug MD1010FSDR CA051229001Control Cable · misriggedDURING A SEVEN DAY CHECK OF AIRCRAFT C-FCGF, THE NOSE WHEEL STEERING CABLE WAS FOUND TO BE ROUTED AROUND AN AFT ATTACHMENT BOLT FOR THE NOSE WHEEL METERING VALVE ASSEMBLY. THE CABLE HAD BEEN RIGGED AND TENSIONED IN THAT POSITION. THE CABLE WAS DISENGAGED FRODec 24, 2005 · Boeing 737522SDR USAA051569Fairing · corrodedFOUND CORROSION FS 40.2 - 44 RT AT Y-430. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-42-00 AND 51-72-11, DEFECT SIZE: .50" BY .250" BY .048".Dec 19, 2005 · N675US · Airbus A330323SDR USAA051570Fairing · corrodedFOUND SEVERAL SPOTS OF CORROSION, FS 39.1-40.2 AT Y-430. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-42-00 AND 51-72-11, DEFECT SIZE: .25" BY 1".Dec 19, 2005 · N675US · Airbus A330323SDR USAA051567Fairing · corrodedFOUND CORROSION FRAME 40. REPLACED SUPPORT FLANGE PER SRM 51-42-00, 51-72-11, DEFECT SIZE: .025" BY 1".Dec 19, 2005 · N675US · Airbus A330323SDR USAA051562Support · corrodedFOUND CORROSION ON RECEPTACLES, FRAME 39.1 CENTER. REPLACED SUPPORT FLANGE PER SRM 51-42-00 AND SRM 51-72-11, DEFECT SIZE: .25" BY 1".Dec 19, 2005 · N675US · Airbus A330323SDR USAA051568Support · corrodedSEVERAL SPOTS OF CORROSION FOUND ON RECEPTACLES, FS 40.2, CENTER, DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-42-00 AND 51-72-11, DEFECT SIZE: .25" X 1".Dec 19, 2005 · N675US · Airbus A330323SDR AU510001924Fairing · bird strike(AUS) RT WING ROOT FAIRING SUFFERED A FRUIT BAT STRIKE DURING LANDING. THE BAT CAUSED A HOLE IN THE KEVLAR FAIRING BUT DID NOT PENETRATE. THE HOLE SIZE WAS APPROXIMATELY 180MM (7.08IN). (OTHER CAUSE: BIRDSTRIKE ) (CASA NR 510001924)Dec 12, 2005 · Dhav DHC8315SDR A6WA200540328Radome · noneREQUEST BIRD STRIKE INSPECTION. REMOVED AND REPLACED RADOME DUE TO BIRD STRIKE IAW AMM 53-81-01. PERFORMED BIRDSTRIKE AMM 05-51-25. NO FURTHER DAMAGE AND NO ENGINE INGESTION FOUND. (K)Nov 14, 2005 · N408AW · Cndair CL6002B19SDR QXEA200501657Seat Track · corrodedYYC - DURING C3 CHECK, RIGHT SIDE OF SEAT RAIL AT STATION 930-939 CORRODED. MAINTENANCE REPAIRED CORROSION IAW REO 670-53-0013.Oct 31, 2005 · N603QX · Cndair CL6002C10SDR 05FDEA03119Radome · delaminatedRADOME HAS DAMAGE AREA AT 1 O`CLOCK POSITION, DELAM AREA.Sep 26, 2005 · N425FE · Airbus A310203SDR 05FDEA02981Fairing · corrodedRIGHT WING TO BODY FAIRING NR 3437 HAS CORROSION (EXFOLIATED). REMOVED ANGLE IAW B727 SRM 51-30-2. FABRICATED ANGLE IAW BAC DRAWING 65-25582. ALODINED AND PRIMED ANGLE IAW B727 SRM 51-10-2. INSTALLED ANGLE IAW B727 SRM 51-30-2. REMOVED TEE CHORD IAW B727 Sep 17, 2005 · N464FE · Boeing 727225SDR IXXA05RNG053STail Cone · dentedDURING INSPECTION CHECK, FOUND SOME DENTS ON LT FUSELAGE TAIL CONE STA`S 1746, 1745 AND 1754. SKIN DENTS WILL BE REPAIRED IAW EWO ATI-53-013 AND FAA FORM 8110-3 MUST BE ISSUED APPROVING THIS REPAIR.Sep 7, 2005 · N721CX · Doug DC872SDR COMA0560486Sealant · vibrationFLIGHT 5564 - UNUSUAL VIBRATION DURING CLIMB. REPLACED THE AERODYNAMIC SEALANT ON BELLY FAIRING.Sep 3, 2005 · N489CA · Cndair CL6002B19SDR UPS05245313Clip · crackedRT BODY FAIRING 3427 HAS SMALL CRACK AT FWD ATTACHING END CLIP. ATTACHING END CLIP REPLACED IAW SRM 51-20-04.Aug 29, 2005 · N930UP · Boeing 72722CSDR UPS05245312Frame · corrodedBODY FAIRING 3608 AFT FRAME AT ATTACHING ANGLE IS CORRODED AT BS 1010 ADJACENT TO STR 26R. FRAME REPLACED IAW SRM 51-20-1 FIG 7.Aug 29, 2005 · N930UP · Boeing 72722CSDR VNAA0508016Radome · bird strikeAFTER LANDING INSPECTION REVEALED DAMAGE TO THE RADOME FROM A BIRD STRIKE. AFTER INSPECTION THE AIRCRAFT WAS FERRIED TO DAY WHERE MAINTENANCE REPLACED THE RADOME WITH A SERVICEABLE UNIT IAW CRJ200 AMM 53-81-01-000(400)-801. NO FURTHER DAMAGE WAS NOTED. THE Aug 24, 2005 · N226JS · Cndair CL6002B19SDR 2005UALA00849Radome · bird strikeCREW REPORT STRIKING TWO LARGE BIRDS ON CLIMB-OUT FROM ORD. STRUCK THE LOWER NOSE OR BELLY OF THE AIRCRAFT PASSING THROUGH 4800 FT. DAMAGE TO FUSELAGE SKIN AND FWD STRUCTURE REPAIRED PER MAJOR REPAIR EVA'S 50522A AND 50523A. RADOME REPLACED.Aug 8, 2005 · N121UA · Boeing 747422SDR DLM88050444Tail Cone · deployedEMS SERVICES BLEW TAIL CONE AT PHL. REPLACED TAIL CONE.Aug 8, 2005 · N948DL · Doug MD88SDR 2005UALA00776Skin · bird strikeCREW REPORT STRIKING TWO LARGE BIRDS ON CLIMB-OUT FROM ORD. STRUCK THE LOWER NOSE OR BELLY OF THE AIRCRAFT PASSING THROUGH 4800 FT. BIRD IMPACT DAMAGE TO RADOME AND SKIN FLANGE STRUCTURE FWD OF FWD PRESSURE BHD. RADOME REPLACED; STRUCTURE REPAIRED PER UA EVAug 8, 2005 · N121UA · Boeing 747422SDR VNAA0508008Radome · lightning strikeTHE CREW REPORTED A LIGHTNING STRIKE TO THE RADOME. MAINTENANCE COMPLIED WITH EN ROUTE & DETAILED LIGHTNING STRIKE INSPECTIONS IAW CRJ700 AMM 05-51-07-210-801-A01 & AMM 05-51-07-220-801-A01. MINOR BURN DAMAGE TO BOTH WINGLET TIPS WAS REPAIRED IAW BOMBARDIER Aug 5, 2005 · N709PS · Cndair CL6002C10SDR ASMF200507021Cable · damagedDURING TRANSIT SERVICE, THE TAILCONE WAS LOOSED. DURING OVERNIGHT CHECK, THE TAILCONE KEVLAR CABLE WAS REPLACED AND THE TAILCONE RELEASE MECHANISM CAM WAS ADJUSTED IAW MM 53-53-02 PAGE 203, BEING ALL CORRECT.Jul 25, 2005 · N753RA · Doug DC987SDR UPS05445126Support · corrodedINSPECTION TYPE:C AIR CONDITIONING BAY BODY FAIRING SUPPORT FOUND CORRODED AT BS 1155 LBL 65. CORROSION BLEND OUT 0.043" X 1" X 1.5" EXCEED SRM 53-50-01 FIG 5 LIMITS, SUPPORT REPAIRED AT LBL 65" AS PER SRM 51-40-04 FIG 1.Jul 21, 2005 · N683UP · Boeing 747121SDR ASO2005F00006Fairing · damagedDURING TAKEOFF, TOWER INFORMED CREW THAT TIRE DEBRIS WAS NOTICED ON RUNWAY AFTER DEPARTURE. THERE WERE NO INDICATIONS OF ENGINE DAMAGE AND AC CONTINUED. EMERGENCY WAS DECLARED AND EMERGENCY VEHICLES WERE REQUESTED TO BE ON STANDBY AS PRECAUTION. AC LANDED SJul 13, 2005 · N902EV · Cndair CL6002B19SDR BB05048Radome · collapsedDURING DESCENT, THE CREW HEARD A POP SOUND. AT THE SAME TIME, THE WEATHER RADAR WENT OUT OF SERVICE. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RADOME WHICH HAD COLLAPSED AND OPERATIONALLY CHECKED THE WEATHER RADAR SYSTEM. OPERATIONALJun 28, 2005 · N603AU · Boeing 757225SDR COMA0560315Fairing · looseFLIGHT 5112 LOUD THUMPING NOISE AFTER TAKEOFF. FOUND AERODYNAMIC BELLY FAIRING LOOSE WITH SEALANT MISSING. TIGHTENED LOOSE SCREWS AND APPLIED SEALANT.May 23, 2005 · N912CA · Cndair CL6002B19SDR WX0500045Skin · lightning strikeEVIDENCE OF 3 LIGHTNING EXIT POINTS ON TAILCONE AT DRAIN PORT AFT OF FUSELAGE, DRAIN PORT IN TAIL ACCESS PANEL AND AT 8 O’CLOCK POSITION ABOVE ACCESS. MAINTENANCE PERFORMED LIGHTNING STRIKE INSPECTION IAW MM 05-53-00. AIRCRAFT INSPECTED AND RELEASED FOR FERRMay 19, 2005 · N891GA · Doug DC983SDR QXEA200500996Channel · brokenAFT BELLY FAIRING 195DL JOINT STRAP, AFT CHANNEL HAS A BROKEN FLANGE AT AFT END OF CHANNEL. REPAIRED IAW HORIZON AIR EA R-53-333.May 16, 2005 · N616QX · Cndair CL6002C10SDR 05FDEA01251Fairing · crackedUPON INSPECTION OF REMOVED PARTS ON TC 44C0204 FOUND STATOR VANE SPACER IS CRACKED AT TIP (OFF AIRCRAFT PART). REPLACED STATOR VANE SPACER TO BE INSTALLED ON N00682 IAW A310-200 AMM 72-23-00.May 12, 2005 · N403FE · Airbus A310203SDR MWEA050043Skin · lightning strikeLIGHTNING STRIKE DAMAGE TO TAILCONE BOTTOM RIGHT EDGE. NO OTHER INFORMATION AT THIS TIME WAITING FOR FIX.May 12, 2005 · N910ME · Boeing 717200SDR 05FDEA01216Fairing · corrodedLEFT NR 1 AIR COND BAY BILGE AREA, FAIRING ASSY FOUND WITH CORROSION AS MARKED. CORROSION REMOVED AS PER SRM 51-21-01 VOL II ,MATERIAL ORIGINAL THICKNESS:0.04 REMOVED MATERIAL THICKNESS: 0.006, L:24, W:6, REMAIN THICKNESS: 0.034 AND FOUND WITHIN LIMIT AS PERMay 6, 2005 · N576FE · Doug MD11SDR LR7A05045Skin · delaminatedDURING SCHEDULED C-6 CHECK PER JOB CARD HC3212 RIGHT MWW SKIN (HONEYCOMB PANEL) FOUND DELAMINATED FROM FS 610-617 WL 189-200. RIGHT PANEL REPLACED IAW LAC MEA 382-53-05-024 R1 & DWG I05-005-02 FS 595-617 WL 180-200.Apr 28, 2005 · N402LC · Lkheed 382GSDR C8GA20050011Radome · lightning strikeFLT 716 FROM TOL TO MEM, DURING CRUISE OPERATION, AIRCRAFT FLEW THROUGH HEAVY WEATHER. DIVERTED TO BNA AND LANDED WITHOUT INCIDENT. ON POST FLIGHT FOUND LARGE HOLE IN RADOME APPROXIMATELY ONE FOOT IN DIAMETER. AFTER INSPECTION, DETERMINED TO BE LIGHTNING STApr 22, 2005 · N286SC · Boeing 7272A1SDR QXEA200500751Strap · brokenYYC - LOWER FUSELAGE AFT WING TO BODY FAIRING HAS STRAP BROKEN. REPAIRED IAW CRJ700 SRM 53-82-83-400-803-A01 AND HORIZON AIR EA R-53-307.Apr 12, 2005 · N614QX · Cndair CL6002C10SDR QXEA200500750Channel · wornYYC - LOWER FUSELAGE AFT WING TO BODY FAIRING HAS CENTRAL C-CHANNEL WORN. REPAIRED IAW HORIZON AIR EA R-53-307.Apr 12, 2005 · N614QX · Cndair CL6002C10SDR 05FDEA00878Rib · crackedEMPENNAGE, EXTENDED TAIL CONE AFT INTERIOR RIB FRAME FOUND CRACKED. REMOVED PER SRM 51-35-01 VOLUME II. NEW RIB AND SPLICES FABRICATED PER DWG AKC7605 AND PART MARKED PER GMM 7-0-1001. NEW RIB AND SPLICES INSTALLED PER SRM 51-35-01 VOLUME II.Apr 6, 2005 · N583FE · Doug MD11SDR QXEA200500634Stiffener · damagedYYC - CENTER FUSELAGE, LOWER FAIRING PANEL, PANEL STIFFENER REQUIRES REWORK DUE TO CONTACT WITH FUSELAGE SKIN. REPAIRED IAW HORIZON AIR EA R-53-287 AND MOD SUM 1S67053820021, REV A-1.Mar 25, 2005 · N612QX · Cndair CL6002C10
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