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 WTAA980009Radome · delaminatedFAT - EN ROUTE FAT TO MRY, WEATHER RADAR REPORTED PAINTING FALSE RETURNS. WEATHER CONDITIONS EN ROUTE REQUIRED AIRCRAFT TO RETURN TO STATION. MAINTENANCE REPLACED RADOME ASSEMBLY. WEATHER RADAR OPERATIONAL CHECK NORMAL ON GROUND. AIRCRAFT RETURNED TO SERVISDR QXEA9800217Fairing · dentedDENT 2.5 BY 2.0 AND .092 DEEP ADJACENT TO FRAME 10775 AND RIB BL13456 ON LOWER FAIRING DENT HAS CREASE IN THE BOTTOM. FABRICATED AND INSTALLED REPAIR IAW FOKKER SRM 53-02-17 FIGURE 1, PAGE 3.SDR 9800889301Clips · out of adjustDURING TAIL CONE FUNCTIONAL CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO RELEASE INTERIOR HANDLE FROM CLIPS. ADJUSTED CLIPS, FUNCTIONAL CHECK OK.SDR 9800879982Clips · out of adjustDURING TAILCONE FUNCTIONAL CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE INTERIOR RELEASE HANDLE FROM CLIP AND TO DEPLOY TAIL CONE. ADJUSTED HANDLE CLIPS AND RIGGED TAIL CONE DEPLOYMENT SYSTEM, FUNCTIONAL CHECK OK.SDR CALA9800013Cables · out of adjustPULL FROM THE TAIL CONE INTERIOR RELEASE HANDLE WAS EXCESSIVE AT 40 POUNDS. THE LATCH CABLES WERE RIGGED IAW MM 53-53-00.SDR 9800469903Clips · sprungDURING TAIL CONE FUNCTIONAL CHECK, FOUND THAT INSUFFICIENT FORCE WAS REQUIRED TO REMOVE INTERIOR HANDLE. REPLACED HANDLE CLIPS, FUNCTIONAL CHECK OK.SDR DHL9871756CTail Cone · delaminatedAT C CHECK, TAILCONE DELAMINATED. INSTALLED FIBERGLASS REPAIR PER SRM 51-40-8, N/R 4023.SDR DHL9871755CTail Cone · damagedAT C CHECK, HOLE IN TAILCONE, RT SIDE OF ATTACH POINT 4 ABOVE CENTERLINE. INSTALLED FIBERGLASS OVERLAY PER SRM 51-40-8, N/R 4016.SDR DHL9871754CTail Cone · gougedAT C CHECK, 2 EACH GOUGES LEFT TAILCONE 4'6 AFT OF ATTACH POINT AND 16 ABOVE CENTERLINE. INSTALLED OVERLAY REPAIR AT TAILCONE PER SRM 51-40-8, N/R 4015.SDR DHL9871753CTail Cone · gougedAT C CHECK, GOUGE IN TAIL CONE LEFT SIDE. INSTALLED FIBERGLASS REPAIR PER SRM 51-40-8, N/R 4014.SDR ASAA9780294Release · lack of lubeSEA - DURING TAILCONE EMERGENCY RELEASE CHECK FROM THE AFT CABIN ENTRY DOOR POSITION, THE TAILCONE FAILED TO RELEASE. LUBRICATED TAILCONE RELEASE MECHANISM AND TAILCONE RELEASED NORMALLY. (M)SDR CALA9701789Cable · wornTHE LT TAILCONE RELEASE CABLE WAS FOUND WORN AND FRAYED WHERE IT PASSES OVER UPPER MOST PULLEY. THE CABLE WAS REPLACED AND THE TAILCONE WAS RIGGED IAW MM 53-53-00.SDR CALA9701788Cables · out of adjustTHE TAILCONE PULL CHECK WAS HIGH. THE CABLES RELEASED AT 50 POUNDS AND THE CONE DID NOT DROP. MAINTENANCE FOUND AFT RT LOWER TAILCONE LATCH MECHANISM BINDING. THE TAILCONE RELEASE SYSTEM CABLES WERE RIGGED IAW CARD 08-5350-1-0007 AND OPERATION CHECKED GOOD.SDR WTAA970229Radome · bird strikeSMF - BIRD STRIKE ON LEFT NOSE AREA REPORTED. MAINTENANCE INSPECTED AREA FOR DAMAGE. NO DAMAGE NOTED. AIRCRAFT RETURNED TO SERVICE. (X)SDR CALA9701765Cables · out of adjustTHE FORCE REQUIRED TO DROP TAILCONE USING THE INTERIOR RELEASE HANDLE AND THE AFT PASSENGER ENTRANCE DOOR HANDLE WAS EXCESSIVE. MAINTENANCE RIGGED THE TAILCONE IAW MM 53-53-00 AND OPERATION CHECKED GOOD. IN ADDITION, ONE LOCK LATCH PIN WAS REPLACED DUE TO WESDR MWEA97862Tail Cone · out of adjustDURING C CHECK, TAILCONE DID NOT RELEASE DURING TEST. MAINTENANCE ADJUSTED TAILCONE IAW DAC MM 53-50-3. OPS CHECK GOOD RETURNED AC TO SERVICE.SDR K3HA9700129Radome · bird strikeBIRD STRIKE IN FLIGHT DAMAGED RADOME. REMOVED AND REPLACED NOSE DOME DUE TO DAMGE. PULLED BIRD STRIKE CONDITON INSPECTION MM 5-51-41. FOUND NO OTHER DAMAGE, INSTALLED NEW NOSE CONE MM 53-19-0.SDR C2XA97IA351Angle · crackedIAH - DURING C-CHECK INSPECTION, FOUND RIGHT SIDE WING TO FUSELAGE FAIRING FRAME 24 LOWER ATTACHMENT ANGLE CRACKED AT DEFLECTOR PLATE. MAINTENANCE REMOVED AND REPLACED THE ATTACHMENT ANGLE IAW ATR-72 SRM 51-25-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVSDR C2XA97IA350Angle · crackedIAH - DURING C-CHECK INSPECTION, FOUND LEFT WING TO FUSELAGE FAIRING FRAME 24 LOWER ATTACHMENT ANGLE CRACKED AT DEFLECTOR PLATE. MAINTENANCE REMOVED AND REPLACED THE ANGLE IAW ATR 72 SRM 51-25-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA97IA349Angle · crackedIAH - DURING C-CHECK INSPECTION, FOUND RIGHT SIDE FRAME SUPPORT FOR WING TO FUSELAGE PANEL 291AL, FORWARD END CRACKED. MAINTENANCE REMOVED AND REPLACED THE ATTACHMENT ANGLE IAW ATR-72 SRM 51-25-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR CALA9701641Cable · out of adjTHE TAIL CONE DROP TEST USING EXTERIOR RELEASE HANDLE WAS BELOW 25 MINIMUM PULL. THE TAIL CONE RELEASE SYSTEM WAS ADJUSTED IAW MM 53-53-00. THE TAIL CONE RELEASE CABLE PIN SHAFT WAS REPLACED DUE TO SHARP INDENTATIONS FOUND.SDR MWEA97837Clips · out of adjustDURING C-CHECK, FOUND TAIL CONE DID NOT PASS PULL TEST PULLED BELOW MINIMUM POUND FORCE REQUIRED AT VENTRAL STAIR LOCATION. MTC ADJUSTED PULL SYSTEM HANDLE CLIPS IAW MM 53-53-00, OPS CHECK GOOD.SDR WTAA970209Radome · bird strikeSMF - BIRD STRIKE ON RADOME ON APPROACH TO SMF. AIRCRAFT FERRIED TO FAT FOR REPAIRS. MAINTENANCE REPLACED RADOME. INSPECTED AREA, FOUND TO BE FREE OF CRACKS. REPLACED PULLED RIVETS. AIRCRAFT RETURNED TO SERVICE. (M)SDR C2XA97IA331Angle · crackedIAH - DURING C-CHECK INSPECTION, FOUND LOWER FUSELAGE FAIRING LEFT SIDE FRAME 27, UPPER INTERCOSTAL ATTACHMENT ANGLE CRACKED. MAINTENANCE REMOVED AND REPLACED THE ATTACHMENT ANGLE IAW ATR-72 SRM 51-25-04. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR MWEA97828Latch Mechanism · lack of lubeDURING C-CHK, TAIL CONE DID NOT PASS DROP TEST. MTC CLEANED AND LUBED LATCHING MECHANISM, OPS CHECK GOOD.SDR CALA9701600Cable · frayedINSPECTION FOUND TAIL CONE RELEASE CABLE FRAYED. THE CABLE WAS REMOVED AND REPLACED AND PULL CHECKED IAW MM 53-53-00.SDR 97ZZZX4794Fairing · deformedUPON INSPECTION OF AIRCRAFT, NOTED LT WING INBOARD FAIRING DENTED AND DEFORMED. WING HAD JUST BEEN REMOVED AND REINSTALLED FOR A STRUCTURAL INSPECTION 7.5 HOURS PRIOR.SDR DHL9780256CFillet · disbondedAT C-CHECK, FILLET PANEL 261K LOWER CORNER HAS SKIN SEPARATING. CLEANED AND REBONDED PER SRM 51-1-9.SDR DHL9780257CFillet · disbondedAT C-CHECK, R/H FILLET PANEL 262K HAS SKIN SEPARATION AT CORNER AND CORROSION ON INTERIOR. CLEANED AND REBONDED PER SRM 51-1-9. REMOVED LEVEL 1 CORROSION PER SRM 51-1-8.SDR ASAA9710104Tailcone · delaminatedSEA - DURING C-CHECK, THE TAILCONE WAS FOUND TO HAVE A SOFT SPOT DELAMINATED. REPAIRED PER EA 5350-01050 AND BOEING TELEX ASA-SEA-97-0431RR. (M)SDR CALA9701507Cable · frayedTHE FORCE REQUIRED TO DROP TAIL CONE USING THE INTERIOR RELEASE HANDLE EXCEEDED 40 POUNDS. THE TAIL CONE FAILED TO DISENGAGE USING THE PASSENGER AFT ENTRANCE DOOR RELEASE MECHANISM. INSPECTION FOUND LT UPPER SECTION OF TAIL CONE RELEASE CABLE WORN AND FRAYEDSDR P5CA9701801Tail Cone · delaminatedDELAMINATION, TAIL CONE - UPPER SURFACE, ABOVE APU TAILPIPE. REPAIRED PER SRM 53-30-03.SDR P5CA9701767Radome · delaminatedDELAMINATED RADOME FWD TIP. REPAIRED PER SRM 53-58-03.SDR MWEA97808Tail Cone · failedDURING C-CHECK, THE TAIL CONE FAILED DROP TEST AND WOULD NOT RELEASE AT 65 LBS INSIDE RELEASED AT 50 LB OUTSIDE. MTC ADJUSTED AND LUBRICATED IAW DMM 53-50-3.SDR WTAA970201Radome · bird strikeLAX - BIRD STRIKE TO NOSE CONE REPORTED. MAINTENANCE INSPECTED AREA FOR DAMAGE. NO DAMAGE NOTED. AIRCRAFT RETURNED TO SERVICE. (M)SDR P5CA9701747Fairing · damagedDAMAGED RT WING TO BODY FAIRING NR 292AR. REPAIR PER SRM 51-40-15, SRM 51-24-11.SDR P5CA9701694Radome · errodedERROSION ON RADOME. REPAIRED PER BOEING SRM 51-40-115 AND 53-52-01.SDR P5CA9701640Fillet · crackedCRACK ON FILLET AT STATION 1416, LBL 11. REPLACED FILLET PER BOEING SERVICE BULLETIN 53-2227.SDR GTIA9700377Fairing · looseACY - FLT 177 - JUST PASSED DOWNWING WITH FLAPS 25 AND GEAR DOWN NOTICED A PRONOUNCED LOW FREQUENCY VIBRATION. PASSENGERS IN AFT ALSO NOTICED THIS VIBRATION UPON DEPARTING THE AIRCRAFT. FOUND INBOARD TRAILING EDGE FLAP TO FUSELAGE FAIRING ON LEFT FLAP VERY LSDR DHL9780770CFairing · crackedUPON REMOVAL OF RT UPPER FUS AFT H/S FAIRING INNER SKIN FWD END HAS A 3 INCH CRACK. CUT OUT DAMAGED AREA OF SKIN AND FABRICATED REPAIR DOUBLER IAW DWGD 85350-3. TREATED AND PRIMED IAW SRM 51-1-8. INSTALLED REPAIR DOUBLER IAW DWG MMCD 85350-3.SDR PLGA970923ARadome · birdstrikeALB - FLT 4264 - AFTER TAKEOFF, CREW EXPERIENCED A BIRD STRIKE IN THE RADOME. AIRCRAFT RETURNED TO ALB AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AREA AND FOUND NO DAMAGE. AIRCRAFT RETURNED TO SERVICE. (M)SDR ASAA9780211Cable · disconnectedPDX - DURING MAINTENANCE CHECK, THE TAILCONE RELEASE CABLE WAS FOUND DISCONNECTED FROM THE CAM MECHANISM. RECONNECTED THE TAILCONE RELEASE CABLE TO THE CAM MECHANISM. (M)SDR DHL9780767CFairing · crackedAFT EXT FUS H/S AREA UPPER FIX FAIRING MID SECT HAS A CRACK, FS 1834. CUT OUT DAMAGED AREA OF SKIN AND FABRICATED REPAIR DOUBLER FROM 2024 T3 .32 IAW DWG NR MMCD 85350-3. TREATED AND PRIMED IAW SRM 51-1-8. INSTALLED REPAIR DOUBLER IAW DWG MMCD 85350-3. REPSDR DHL9780766CFairing · crackedAFT EXT FUS H/S AREA LWR FIX FAIRING AFT END IS CRACKED, FS 1890 DOT 314. CUT OUT DAMAGED AREA OF SKIN AND FABRICATED REPAIR DOUBLER FROM 032 301 1/2H 55 IAW DWG NR MMC D85350-3. TREATED AND PRIMED IAW SRM 51-1-8. INSTALLED REPAIR DOUBLER IAW DWG NR MMC D85SDR DHL9780765CFairing · crackedAFT EXT FUS H/S AREA UPPER FIX FAIRING, FWD SECT HAS WORKING FASTENERS AND CRACKED SKIN, FS 1800. CUT OUT DAMAGED AREA OF SKIN AND FABRICATED REPAIR DOUBLER FROM .032 301 1/2H. TREATED AND PRIMED IAW SRM 51-1-8. INSTALLED REPAIR DOUBLER IAW DWG NR MMC D8535SDR MWEA97770Lanyard · frayedDURING C-CHK, FOUND TAIL CONE LOWER DROP CABLE FROZEN AND TAIL CONE EMERGENCY EVAC LANYARD FRAYING. MTC REMOVED AND REPLACED TAIL CONE RELEASE CABLE AND CONDUIL IAW MM 53-50-3 AND INSTALLED SERVICEABLE LANYARD IAW 25-62-1.SDR P5CA9701548Fairing · crackedCRACKED RIGHT FUSELAGE WING TO BODY FAIRING AFT OF BODY GEAR. FIBERGLASS REPAIR APPLIED PER BAC SRM 51-40-09.SDR CALA9701352Clips · out of adjustTHE TAILCONE INTERIOR AND EXTERIOR RELEASE HANDLES PULLED FROM RETAINING CLIPS LOW AT 15-20 POUNDS. THE RETAINING CLIPS WERE ADJUSTED IAW MM 53-53-00.SDR P5CA9701547Fairing · crackedDELAMINATED AND CRACKED LEFT FUSELAGE BODY TO WING FAIRING FORWARD OF WING GEAR. REPAIRED FAIRING WITH FIBERGLASS OVERLAYS PER BAC SRM 51-40-15.SDR P5CA9701545Fairing · crackedCRACK ON LEFT FUSELAGE BODY FAIRING ABOVE BODY GEAR. REMOVED CRACK AND APPLIED FIBERGLASS FILLERS AND DOUBLERS PER BAC SRM 51-40-15.
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