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 CALA990022Recepticle · wornTAIL CONE TOP FIVE ALIGNMENT PIN RECEPTICLES WORN. REPLACED TOP FIVE ALIGNMENT PIN RECEPTICLES.SDR QXEA9900166Support · crackedPDX - 91J FAIRING SUPPORT ON FUSELAGE HAS APPROXIMATELY 10 INCH CRACK AT FORWARD CURVED SECTION JUST FORWARD OF NUT PLATES. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 51-31-03.SDR DHL9971223CFairing · corrodedAT C-CHECK, CORROSION ON BODY FAIRING PANEL NR 3334 AT FWD SECTION OF LT HEAT EXCHANGER AIR INLET DOOR. REMOVED FORMER AT FAIRING PANEL AND INSTALLED NEW PER SRM 51-30-2.SDR UPS99828680Fillet · corrodedINSPECTION TYPE:D, FILLET PNL 191AA HAS CORROSION AND BARE METAL A-708 RACK NR 25. FAB -3 PANEL, -5 AND -7 FILLERS IAW DAC DWG 5701940. ALODINED AND PRIMED PANEL L AND FILLER IAW DC8 SRM 51-1-8. INSTALLED FILLERS IAW DC8 SRM 51-1- 21 AND DC8 SRM 71-2-2.SDR MWEA990004Latch · out of adjustMKE - FOUND TAILCONE DEPLOY TENSION LOW. MAINTENANCE LUBRICATED AND ADJUSTED LATCHES. (X)SDR CALA9900006Cables · out of adjustTHE TAIL CONE RELEASE PULL WAS BELOW LIMITS WHEN USING INTERIOR OR EXTERIOR TAIL CONE HANDLE. THE CABLES, LATCHES AND CLIPS WERE ADJUSTED IAW MM 53-53-00.SDR QXEA9900161Support · loosePDX - LEFT-HAND WING ROOT FAIRING SUPPORT FOR 91G LOWER AFT END HAS 15 LOOSE RIVETS AND CHANNEL IS CHAFED. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 51-31-02.SDR COEA9801856Radome · fracturedPILOT REPORTED THAT HE HAD A BIRD STRIKE ON THE RADOME. UPON INSPECTION OF THE RADOME, THE MOST FORWARD PART OF THE RADOME WAS INDENTED APPROXIMATELY 2 INCHES DEEP BY 4 INCHES ACROSS. REMOVED AND REPLACED RADOME. AIRCRAFT RETURNED TO SERVICE. (X)SDR 98FDEA00752Tail Cone · crackedSNRM 413 TAIL CONE STRUCTURE OF RT HINGE FAIL DURING OPER: AREA DAMAGED DURING EXTEND OPER. REMOVED AND REPLACED TAIL CONE RT HINGE STRUCTURE DAMAGE LWR SKIN, INTERCOSTAL, RIBS, FRAME, PNL AND DOUBLERS PER DWG AKC 7504 AND OPER CK MM 53-52-01-2 FND SAT.SDR AALA982172Skin · gougedTUL - TWO GOUGES IN SKIN INSIDE, BETWEEN STATION 1148-1166 RIGHT SIDE ABOVE STRINGER 27R. INSTALLED REPAIRED DOUBLER IAW SRM 53-30-3 PAGE 151 FIG 24. (M)SDR MWEA981147Latch · out of adjustTAIL CONE DID NOT DROP DURING FUNCTIONAL CHECK. MTC ADJUSTED LATCH LEVER CABLE.SDR CALA9802140Frame · crackedINSPECTION FOUND A 2 INCH CRACK IN TAIL CONE FRAME UNDER ACTUATOR LINK AREA. THE CRACKED AREA WAS TRIMMED OUT. THE AREA WAS REINFORCED WITH FRAME AND SPLICE IAW SRM 53-30-00, FIGURE 3, 51-31-01 AND 51-21-01.SDR P5CA9801614Fairing · delaminatedNR 8 FIXED FAIRING TAIL CONE LOWER SKIN FOUND DELAMINATED. SANDED DOWN DELAMINATION AREA AND REPARIED PER SRM 51-40-09.SDR CALA9802131Cable · frayedTHE TAIL CONE DID NOT COMPLETELY RELEASE FROM AIRCRAFT WHEN OPERATED FROM AFT VENTRAL DOOR. THE FRAYED CABLE WAS REPLACED AND RIGGED IAW MM 53-53-0.SDR 99ZZZX56Radome · contaminatedVERY LOW RADAR TRANSMISSION THROUGH RADOME (27.7 PERCENT IN NOSE). MINIMUM SPEC IS 82 PERCENT. RADAR RANGE WILL BE DIMINISHED.SDR CALA9802096Cables · out of adjmtTHE FORCE REQUIRED TO RELEASE TAIL CONE USING EXTERIOR HANDLE WAS LOW. THE TAIL CONE CABLES WERE ADJUSTED IAW MM 53-53-00.SDR CALA9802095Clips · out of adjmtTHE FORCE REQUIRED TO PULL BOTH THE EXTERIOR AND INTERIOR TAIL CONE RELEASE HANDLES FROM CLIPS WAS LOW. THE EXTERIOR AND INTERIOR HANDLE CLIPS WERE ADJUSTED IAW MM 53-53-00.SDR QXEA9801881Nose Cowl · chafedDEEP CHAFE AT THE 6 O'CLOCK POSITION ON THE AFT FACE OF THE NOSE COWLING. REPAIRED IAW HORIZON AIR EA 4-72-32.SDR CKSA98675Channel · corrodedSTA 840, WL 91, RBL 21, THE AFT I/B FLANGE OF THE 69B01835-1 BODY FAIRING CHANNEL HAS AN AREA APPROX 1.50 SQ INCH WITH MODERATE CORROSION. REPAIRED IAW BOEING ASA CKF-EXB-239 SUPP SHT 1 AND 2. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK,SDR DHL9980122CFairing · delaminatedAT C-CHECK, FAIRING PANEL 162K IS DELAMINATED. REMOVED AND REPAIRED PANEL PER SRM 51-3-0.SDR DHL9872051DFairing · delaminatedAT D CHECK, WING TO BODY FAIRING NR 3347 DELAMINATED. INSTALLED REPAIR PER SRM 51-40-8, 6 BY 5, N/R 3638.SDR CALA9802048Channel · crackedINSPECTION FOUND A 1 INCH CRACK IN HORIZONTAL CHANNEL OF OUTBOARD AFT FAIRING AT RT MLG WHEEL WELL. THE CRACKED TEE WAS REMOVED AND A NEW TEE WAS INSTALLED IAW SRM 53-53-01, FIGURE 4, 51-21-01, AND 51-31-01.SDR CALA9802044Handle · out of adjustTHE FORCE REQUIRED TO RELEASE TAIL CONE USING THE EXTERIOR, INTERIOR, AND AFT ENTRY DOOR HANDLES WAS OUT OF LIMITS. THE HANDLES WERE ADJUSTED AND TESTED IAW MM 53-53-00.SDR CA981207017Nose Cone · damaged(CAN) ON APPROACH, AIRCRAFT ENCOUNTERED BIRD STRIKES. FIVE STRIKES ON AIRCRAFT WERE NOTED, BOTH LANDING LIGHT LENSES BROKEN, RIGHT ENGINE NOSE COWL DENTED, BOTH LANDING GEARS NO DAMAGE, AND RIGHT FLAP TRAILING EDGE DENT. NOSE COWL REPLACED, LIGHT LENSES REPLSDR 99ZZZX21Fastener · crackedDURING COMPLIANCE OF SB-BR700-72-900062, FOUND NUMEROUS FASTENERS CRACKED.SDR 99ZZZX20Fastener · crackedDURING COMPLIANCE OF SB-BR700-72-900062, FOUND FASTENER MISSING AND NUMEROUS FASTENERS CRACKED.SDR UPS98228166Frame · corrodedINSPECTION TYPE-C, FUSELAGE SLIDING FAIRING NR 3601 HAS CORRODED FRAME AT LOWER FWD CORNER. REPAIRED IAW SRM 53-10-4 AND TYPICAL WEB REPAIRS IAW SRM 51-40-3.SDR SWAA982698Fairing · crackedDURING SCHEDULED TRANSITION CHECK, WHILE WORKING DELAMINATION ON BODY FAIRING JUST FWD OF THE RT WHEEL WELL, FOUND RT WING ROOT FAIRING JUST FWD OF RT MLG WHEEL WELL HAS SEVERAL CRACKS BETWEEN FASTENER HOLES ON T/E. REPAIRED CRACKS BETWEEN FASTENER HOLES ON RSDR HEEA0016326Radome · mismanufacturedRADOME MOUNT HOLES MISALIGNED.SDR UPS98828220Skin · corrosionINSPECTION TYPE-D, REMOVED FWD SKIN ON RIGHT SIDE OF TAIL CONE DUE TO CORROSION. FAB NEW SKIN IAW DAC DWG 5644500, ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-21.SDR DHL9980120CFairing · delaminatedAT C-CHECK, PANEL 261K SHOWS DELAMINATION. REMOVED AND REPAIRED PANEL PER SRM 51-3-0.SDR CALA9801968Cable · out of adjTHE AFT ENTRY DOOR TAILCONE RELEASE PULLED HIGH AT 25 POUNDS. THE CABLE AND CONDUIT WERE REPLACED AND AN ADJUSTMENT/TEST WAS PERFORMED IAW MM 53-53-00.SDR P2EA98240Fairing · delaminatedSJO - LEFT WING TO BODY FAIRING (LT A/C BAY DOOR) INNER SKIN DELAMINATED. REPAIRED LEFT WING TO BODY FAIRING PER COOPESA EO C00-3-53-587-98 DATED OCT 26, 1998. (M)SDR P2EA98239Fairing · delaminatedSJO - RIGHT WING TO BODY FAIRING (RT A/C BAY DOOR) INNER DOOR SKIN AND SEAL DELAMINATED. REPAIRED RT WING TO BODY FAIRING PER COOPESA EO C00-3-53-588-98 DATED OCT 26, 1998. (M)SDR CALA9801939Latch · out of adjustTAIL COMPARTMENT TAILCONE OUT OF RIG. OUTSIDE HANDLE PULL LOW, DELTA TRIANGLE NOT 90 DEGREES, CATCHES ON RIGHT SIDE LATCHES. ADJUSTED LATCH LEVER CABLES AND ADJUSTED LOWER RIGHT LATCH LEVER. PERFORMED ADJUSTMENT TEST PER MM 53-53-00.SDR HEEA0016100Fairing · crackedFAIRING CRACKED AT MOUNT HOLE.SDR CALA9801837Cable · out of adjTHE AFT FUSELAGE TAIL CONE EXTERIOR HANDLE PULLED LOW AT 15 POUNDS. THE TAIL CONE CABLES WERE ADJUSTED IAW MM 53-53-00.SDR CKSA98517Fillet · crackedDURING PREFLIGHT, FOUND CRACK 18.5 INCHES LONG IN COMPOSITE PANEL LOCATED IN THE LOWER REAR BODY GEAR/WING TRAILING EDGE FILLET. CRACK IS DIRECTLY BEHIND THE LOWER WATER DRAIN ACCESS HATCH, IN THE LEFT OF THE AIRCRAFT CENTERLINE, BEHIND THE LEFT BODY GEAR, NESDR CALA9801731Tail Cone · warpedTHE TAILCONE PULL TEST EXCEEDED LIMITS AND THE TAILCONE DID NOT DEPLOY USING EITHER THE INTERIOR OR AFT RELEASE HANDLES. THE TAILCONE WAS REMOVED AND REPLACED IAW MM 53-53-00.SDR DHL9880409CFairing · crackedAT C-CHECK, RIGHT WING, WING TO BODY FAIRING AT BS 680 SUPPORT STRUCTURE HAS METAL LINES CRACKED. REMOVED SUPPORT AND FABRICATED AND INSTALLED PER MM 51-1-8. N/R 403SDR ARWA981015Fairing · corrodedCORROSION ON AFTER BODY FAIRING ABOVE LT UPPER HORIZ STAB AIRGATE FAIRING. CORROSION REMOVED, BLEND OUT ACCOMPLISHED PER BWIA BW-L15-53-A/4505, AREA TREATED IAW SRM 51-21-01/02, AREA PRIMED AND PAINTED. CONCESSION 113/98 W/O 24000 CCF 3156 L/P 10465. 8110-3SDR DHL9880417CFairing · delaminatedAT C-CHECK, RIGHT WING FAIRING PANEL 162K2 DELAMINATED. REMOVED PANEL, REPAIRED AND REINSTALLED PER SRM 51-3-0. N/R 720SDR DHL9880401CFairing · delaminatedAT C-CHECK, R/W FAIRING PANEL EDGE IS DELAMINATED NR 262K. CLEANED AND REPAIRED PER SRM 51-1-19. N/R 730SDR AU981136Fairing · missing(AUS) NR 20 BULLNOSE FAIRING MISSING. CAMBER LINK AND OTHER LINKS BROKEN AND ARM CRACKED.SDR DHL9880407CFairing · delaminatedAT C-CHECK, LEFT WING FAIRING PANEL NR 161V HAS DELAMINATION. REPAIRED DAMAGED PANEL AND REINSTALLED PER SRM 51-18 AND 51-1-21. N/R 250SDR VNAA9809001Nose Cone · bird strikeTHE CREW REPORTED THAT THEY MAY HAVE TAKEN A BIRD STRIKE ON THE NOSE CONE, DURING SHORT FINAL APPROACH. THE AIRCRAFT CONTINUED THE APPROACH AND LANDED WITHOUT INCIDENT. OUTSTATION MAINTENANCE WAS CALLED AND INSPECTED THE AIRCRAFT, IN ACCORDANCE WITH DORNIER SDR CALA9801606Fairing · crackedINSPECTION FOUND A 1 INCH CRACK AT NUT PLATE HOLE OF LT BODY FAIRING PANEL NR 3337. THE CRACKED SECTION WAS REMOVED. A REPAIR WAS INSTALLED IAW SRM 53-40-3, FIGURE 1, 51-10-2, 51-30-2, AND MM 51-20-12.SDR DHL9880434CRadome · delaminatedAT C-CHECK, RADOME HAS DELAMINATED AREAS PEELING AND SEVERAL NICKS. REMOVED AND REINSTALLED REPAIRED RADOME PER MM 53-50-1. N/R 0040SDR CALA9801597Clips · bentTHE FORCE REQUIRED TO PULL TAILCONE EXTERIOR RELEASE HANDLE FROM CLIPS WAS UNDER 25 POUNDS. THE CLIPS AND SUPPORTS WERE REPLACED AND OPERATION CHECKED GOOD IAW MM 53-53-00.SDR CALA9801568Clips · out of adjustTHE FORCE REQUIRED TO RELEASE TAILCONE EXTERIOR HANDLE FROM CLIPS WAS LOW AT 15 POUNDS. THE CLIPS WERE REPLACED AND ADJUSTED IAW MM 53-50-3.
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