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 MWEA060040Radome · bird strikeBIRDSTRIKE ON RADOME. REMOVED AND REPLACED RADOME.SDR 2006UALA00608Radome · bird strikeBIRD STRIKE AFTER TAKEOFF. IMPACT BELOW NOSE. RADAR ANTENNA MAKES GRINDING NOISE DURING SWEEP. RADOME DAMAGED.SDR 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.SDR 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.SDR 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.SDR QXEA200600636Panel · corrodedPDX - C4 CHECK, ROOT FAIRING PANEL 262PT HAS CORRODED FASTENERS. REPAIRED IAW SRM 53-50-01.SDR 2006UALA00337Structure · damagedDAMAGE TO THE HORIZONTAL STABILIZER AND TAIL CONE. MAJOR REPAIR ACCOMPLISHED. REPAIR DOUBLERS INSTALLED WITH AIRBUS RAS APPROVALS.SDR 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.SDR MWEA060014Cable · disengagedTAIL CONE ANNUNCIATOR CAME ON. FOUND TAIL CONE LOCK CABLE (INTERIOR HANDLE) DISENGAGED, RE-INSTALLED SAME CABLE.SDR 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.SDR 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 SIMSDR 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 SDR MJYA0601018Fairing · crackedFUSELAGE WING TO BODY FAIRING FORMER REPAIRED DUE TO CRACK.SDR 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.SDR 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 FROSDR 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".SDR 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".SDR USAA051567Fairing · corrodedFOUND CORROSION FRAME 40. REPLACED SUPPORT FLANGE PER SRM 51-42-00, 51-72-11, DEFECT SIZE: .025" BY 1".SDR 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".SDR 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".SDR 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)SDR 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)SDR QXEA200501657Seat Track · corrodedYYC - DURING C3 CHECK, RIGHT SIDE OF SEAT RAIL AT STATION 930-939 CORRODED. MAINTENANCE REPAIRED CORROSION IAW REO 670-53-0013.SDR 05FDEA03119Radome · delaminatedRADOME HAS DAMAGE AREA AT 1 O`CLOCK POSITION, DELAM AREA.SDR 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 SDR 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.SDR COMA0560486Sealant · vibrationFLIGHT 5564 - UNUSUAL VIBRATION DURING CLIMB. REPLACED THE AERODYNAMIC SEALANT ON BELLY FAIRING.SDR UPS05245313Clip · crackedRT BODY FAIRING 3427 HAS SMALL CRACK AT FWD ATTACHING END CLIP. ATTACHING END CLIP REPLACED IAW SRM 51-20-04.SDR 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.SDR 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 SDR 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.SDR DLM88050444Tail Cone · deployedEMS SERVICES BLEW TAIL CONE AT PHL. REPLACED TAIL CONE.SDR 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 EVSDR 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 SDR 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.SDR 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.SDR 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 SSDR 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. OPERATIONALSDR COMA0560315Fairing · looseFLIGHT 5112 LOUD THUMPING NOISE AFTER TAKEOFF. FOUND AERODYNAMIC BELLY FAIRING LOOSE WITH SEALANT MISSING. TIGHTENED LOOSE SCREWS AND APPLIED SEALANT.SDR 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 FERRSDR 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.SDR 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.SDR MWEA050043Skin · lightning strikeLIGHTNING STRIKE DAMAGE TO TAILCONE BOTTOM RIGHT EDGE. NO OTHER INFORMATION AT THIS TIME WAITING FOR FIX.SDR 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 PERSDR 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.SDR 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 STSDR 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.SDR QXEA200500750Channel · wornYYC - LOWER FUSELAGE AFT WING TO BODY FAIRING HAS CENTRAL C-CHANNEL WORN. REPAIRED IAW HORIZON AIR EA R-53-307.SDR 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.SDR 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.
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