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 DALA12010660984Cable · out of limitsPERFORMED TAILCONE RELEASE SYS OPS CHECK AND FOUND THE TAILCONE EXTERIOR RELEASE CABLE WAS OUT OF ALLOWABLE LIMITS. THE LOCKING CABLE CLAMPS DID NOT CLEAR THE LOWER END OF THE CONDUITS BY AT LEAST .5" WITH LATCHES IN THE FULL OPEN POSITION. THE CABLE CONDUITSDR TRBA20121020001Channel · corrodedDURING MX INSPECTION, FOUND THE TAIL CONE NUTPLATE GANG LT AND RT CHANNELS TO HAVE CORROSION BEYOND LIMITS. THE ACFT WAS REMOVED FROM SERVICE. REPLACED DAMAGED SECTIONS OF LT AND RT TAIL CONE NUTPLATE GANG CHANNELS IAW MM 53-91-30, SRM 53-91-24 AND EO E2-530SDR TRBA20121018001Channel · corrodedDURING B INSPECTION, FOUND THE TAIL CONE INTERNAL LT HORIZONTAL GANG CHANNEL HAS EXFOLIATING CORROSION ABOUT 20" FROM TAIL CONE LENS ASSY. THE ACFT WAS REMOVED FROM SERVICE. INSTALLED TAIL CONE IAW JIC 53-91-24. OPS CHECKED GOOD. ACFT RETURNED TO SERVICESDR 2012FA0000710Control Cable · frayedWHILE TROUBLESHOOTING, AN AUTO PILOT PORPOISE DISCREPANCY, THE TECH PULLED ON A PRIMARY RUDDER CABLE IN THE TAIL CONE AND IT SNAPPED. THE CABLE HAS BEEN BROKEN EXCEPT FOR A FEW STRANDS. IT APPEARS THE CABLE WAS NOT RIDING IN A PULLEY AND WAS CHAFING ON THE USDR SWAA2012111509363Support Angle · cracked70.5 WING FWD FAIRING CLOSE OUT SUPPORT ANGLE CRACKED AT BS 540. REMOVED DAMAGED SEAL ANGLE, FORMED NEW ANGLE AND HEAT TREATED PER BAC SPEC. LOCATED AND DRILLED FINISHED ANGLE AND INSTALLED IAW BOEING DWG 69-61951 84840U 10-16-2012.SDR UALA2012100805705Seal · displacedUPPER RIGHT WING TO BODY FAIRING FWD OF WING A PANELS 192BT AND 192AT HAS A 1 INCH SECTION OF SEAL MISSING. FLIGHT CREW FOUND ON PRE FLIGHT WALK AROUND. ACCOMPLISHED VISUAL INSPECTION OF PANEL AND SEAL. NO DAMAGE FOUND APPLIED 2 LAYERS OF SPEED TAPE PER EC-SDR DALA12009170981Cable · out of rigMX DISCOVERED THAT THE TAILCONE RELEASE LATCH CABLES WERE OUT OF ALLOWABLE RIG LIMITS. THE CABLES WERE ADJUSTED AND THE SYS WAS RIGGED BACK INTO SPECIFICATIONS. THE RII STEPS WERE COMPLETED.SDR UALA2012092905487Radome · damagedRADOME DAMAGED BY BIRD STRIKE. REPLACED NOSE RADOME AS PER AMM 53-12-01 PAGE SERIE 400. RADOME P/N 284T0052-39P S/N 0976 BORROWED.SDR E07A201209280001Skin · bentAFTER LANDING, CREW NOTICED ON POSTFLIGHT INSPECTION THE LT LOWER WING SKIN/WHEEL WELL FAIRING WAS PEELED BACK.SDR UALA2012092405395Skin · damagedFAB ANT REPAIR DOUBLER AT STA 1393. FAB REPAIR DOUBLER AT STA 1393 PER ECRA5361-01024. THE FUSELAGE SKIN REPAIR INSTALLED BETWEEN BS 1385-1401 & STR 28L-29L.SDR DALA1249249205Bottle · emptyWHILE PERFORMING TAILCONE FUNCTIONAL CHECK, FOUND THE TAILCONE ASSIST BOTTLE READING ZERO PSI. SERVICED AND LEAK CHECKED BOTTLE IAW AMM 12-18-01. CHECKED GOOD.SDR VNAA2012091800016Radome · damagedCREW REPORTED LIGHTNING STRIKE AND DAMAGE NOTED ON NOSE CONE. MAINTENANCE PERFORMED LIGHTNING STRIKE INSPECTION AND FOUND PUNCTURE IN RADOME AND TWO (2) DAMAGED RIVETS ON RIGHT WINGLET. MAINTENANCE ALSO NOTED NUMBER ONE COM ANTENNA WAS CRACKED. MAINTENANCE SDR DALA12007990915Conduit · damagedMX DISCOVERED THAT THE TAILCONE RELEASE SYS LATCH CABLE FORK END WAS BENT OUT OF ALLOWABLE LIMITS AND FOUND THAT THE CABLE CONDUIT WAS WORN AS WELL. THE CONDUIT WAS REPAIRED AND INSTALLED. TSDR UALA2012091705247Fairing · dentedDENT IN FORWARD MOST END OF MAIN BODY FAIRING ON LEFT SIDE OF ACFT. DAMAGE IS 2 IN BY 1 IN AND 0.03125 IN DEEP. DENT IS 15 INCHES FROM TOP OF FAIRING AND 1 INCH 3 INCHES FROM TRAILING EDGE. REF ECRA5325-01001 NO UNDERLYING CRACKS OR LOOSE FASTENERS AND EXTERSDR DALA1248369226Cable · frayedWHILE PERFORMING TAIL CONE FUNCTIONAL CHECK, FOUND NITROGEN JETTISON BOTTLE ACTIVATION CABLE FRAYED. MAINTENANCE REMOVED AND REPLACED TAIL CONE NITROGEN JETTISON BOTTLE PULL CABLE PER AMM.SDR SWIA201231806Bulkhead · scratchedSKIN ON NOSE RADOME BULKHEAD AT THE 3 POSITION IS SCRATCHED AND GOUGED. (C-CHECK) REPAIRED TO FS 169 RADOME BULKHEAD SKIN STRAP AS PER CRJ 200 SRM.SDR SIMA20120818006Frame · crackedDURING MAINTENANCE INSPECTION FOUND THE APU COWLING FORWARD FRAME CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. FABRICATED AND INSTALLED FILLER, DOUBLER AND SHIM. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR UALA2012090705053Seal · damagedCREW REPORT: DURING CLIMB THROUGH FL260 M.81 EXPERIENCED RHYTHMIC FLUTTER THROUGHOUT ENTIRE JET. FOUND DAMAGED SEAL ON FUSE FRNG 197BB AND REPAIRED, FOUND BULB SEAL DAMAGED ON LEFT LOWER SURFACE AT STRUT CUTOUT. REPLACED FRNG 192AT, ACP RUD INTEGRITY CHECK SDR V0XR20120906J0084Diaphragm · crackedCRACK IN LT WING TO FUSELAGE DIAPHRAGM AT BS 909.0. REPAIRED IAW REO 670-53-82-436, AN EDDY CURRENT INSPECTION WAS COMPLIED WITH AND NO REJECTABLE INDICATIONS IAW NDTM 51-20-06, REO 670-52-35-127, SRM 51-21-11,51-22-00, AND 51-42-06.SDR DALA12006060936Structure · bindingTHE FIRST OFFICER DISCOVERED THAT THE TAILCONE CATWALK OVER THE VENTRAL STAIRWAY WAS BINDING DURING OPERATION. THIS IS CONSIDERED A DEFECT IN THE EMERGENCY ESCAPE SYSTEM AND COULD HAVE AN ADVERSE AFFECT ON THE EVACUATION ROUTE. THE MOVEABLE CEILING (CATWALK)SDR SWAA2012082706984Door · looseTAIL CONE DOOR HANDLE IN AFT ACCESSORY COMPARTMENT LOOSE. SECURED DOOR IAW AMM.SDR UALA2012082304737Radome · damagedRADOME DAMAGED DUE TO BIRD STRIKE. INNER F ACE OF RADOME HAS DISBONDING-DELAMINATION ABOUT THE SIZE OF A FOOTBALL. REMOVED AND REPLACED NOSE RADOME AS PER MM. S-N OFF NT1944 S-N ON 026SDR IPXA12M75098Rib · crackedINSPECTION TYPE: 4C, WING-TO-BODY PANEL SUPPORT RIB CRACKED ON LT SIDE OF FUSELAGE EXTERIOR AT STA 1341. REMOVED FABRICATED AND INSTALLED REPLACEMENT RIB AT LT SIDE STA 1341 IAW DWG ANB 7142 AND SRM 51-35-01.SDR UALA2012072504050Radome · delaminatedRADOME HAS DELAMINATED OR PAINT CHIPS DOWN TO BRIGHT GREEN SURFACE. RADOME REPLACED.SDR UALA2012072504031Paint · peelingRADOME PEELING PAINT IS NOT WITHIN LIMITS. ACCOMPLISHED PAINT PER MM 51-75-11.SDR U2RA201207180009Fairing · crackedBODY FAIRING PANEL NR 294AR INTERIOR SURFACE FOUND CRACKED.SDR DALA12006219237Bottle · dischargedTAILCONE DISCHARGE BOTTLE PRESSURE LOW. SERVICED TAILCONE DISCHARGE BOTTLE PER AMM. CHECKED GOOD.SDR KCSA201207111113Panel Support · corrodedFAIRING SUPPORT BETWEEN WING GEAR DOORS AT APPROX BS 1345 RBL 8 TO LBL 8 FOUND EVIDENCE OF CORROSION.SDR IPXA12174557Fairing · gougedINSPECTION TYPE: 1C, APU EXHAUST FAIRING FR103A BELOW STR 7L IS GOUGED. ACCOMPLISHED REPAIR ON APU EXHAUST FAIRING AT FR103A BELOW ST 7L IAW EO A300-5240-47936-A, PARA 6A.SDR DALA1237330940Cable · misroutedAT ROTATION, THE CREW NOTED A "TAILCONE UNSAFE" MESSAGE ON THE OVERHEAD ANNUNCIATOR PANEL. ON LANDING, MAINTENANCE DISCOVERED THAT THE TAILCONE INTERNAL RELEASE HANDLE WAS OUT OF POSITION AT THE INTERNAL SWITCH. CABLE WAS REPOSITIONED TO THE CORRECT ROUTSDR UALA2012061203233Support · gougedFR 86 SUPPORT FOR TAILCONE IS GOUGED. REPLACED LOWER FRAME SUPPORT. MAJOR REPAIRSDR UALA2012060803120Radome · delaminatedCENTER OF RADOME DELAMINATED AT ONE SPOT MEASURING 2.5 INCH. REPLACED RADOME.SDR V0XR20120604J0050Fairing · damagedRAM AIR INLET DUCT DAMAGED BEYOND SERVICEABLE LIMITS. REPAIRED.SDR UALA2012060103041Radome · damagedLIGHTNING STRIKE ON ARRIVAL, LEFT SIDE. NO SYSTEMS EFFECTED. ACCOMPLISHED LIGHTNING STRIKE INSPECTION PER AMM. RADOME HAS 1-4 INCH HOLE NEAR CTR COMPLETELY THROUGH. REPLACED PER AMM.SDR DALA1235570944Link · damagedMAINTENANCE DISCOVERED THAT THE TAIL CONE CATWALK OVER THE VENTRAL STAIRWAY WAS STUCK IN THE DOWN POSITION. THE LINK ATTACHING THE CATWALK TO THE STAIRS TORQUE TUBE WAS MISSING HARDWARE AND WAS DAMAGED. THIS COULD HAVE AN ADVERSE AFFECT ON THE OPERATION OF TSDR DALA12000490870Fastener · looseDURING LINE CHECK, MAINTENANCE FOUND THE LOCK FASTENER LOOSE ON THE TAIL CONE DOOR HATCH. MAINTENANCE REPLACED THE RECEPTICAL, SECURED THE FASTENER AND RETURNED THE AIRCRAFT TO SERVICE.SDR UALA2012052502923Seal · wornAIRFRAME VIBRATION, FL200 UP TO FL340, MORE NOTICEABLE IN CLIMB THAN LEVEL FLT. ACCOMPLISHED TSM CHART 05-50-00 PB201 AND INFORMATION FROM VIBRATION SURVEY SUGGESTS BELLY FAIRING SOURCE OF VIBRATION. TAPED BELLY FAIRING SEALS REF MT53-004. FOUND SEAL WORN ONSDR UALA2012052702946Filler · looseFASTENER POPPED ON NOSE RADOME. FOUND CENTER OF LEFT SIDE ALLEN HEAD SPRING LOADED HOLE FILLER LOOSE. SECURED.SDR UALA2012052702945Radome · damagedSTATIC DISCHARGE NEAR RIGHT SIDE OF RADOME. INSPECTED RADOME FOR PINHOLES, PUNCTURES, ETC AND WXR ANTENNA AND WAVE GUIDE FOR DAMAGE. NO DAMAGE FOUND EXCEPT FOR DIVERTER STRIPS. REFERENCE CF 314 FOR DIVETER REPLACEMENT. OK FOR SERVICE PER MM 05-51-19.SDR KCSA201205231085Skin · corrodedCORROSION ON TAIL CONE EXTERNAL SKIN AT BS 2752 BOTTOM SIDE.SDR SWAA2013091220107Drag Angle · crackedRT FORWARD WING TO BODY FAIRING UPPER DRAG ANGLE CRACKED AT BS 540, STRINGER 21L. REPAIRED ANGLE IAW SRM.SDR DALA1233670925Pin · wornDURING FUNCTIONAL CHECK OF TAILCONE RELEASE SYSTEM OPS 6908, MAINTENANCE FOUND THE TEE PIN, BUSHING, AND CABLE WORN BEYOND THE TEE PIN 11, CAM ASSEMBLY, AND CABLE WERE ALL REPLACED AND THE RII COMPLETED.SDR VNAA2012051700016Radome · damagedCREW REPORTED LIGHTNING STRIKE ON RADOME IN FLIGHT. CREW LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED LIGHTNING STRIKE INSPECTION AND REMOVED AND REPLACED THE FOLLOWING COMPONENTS DUE TO LIGHTNING STRIKE DAMAGE: NOSE RADOME, WEATHER RADAR AND ONE SDR VNAA2012051500015Radome · damagedDURING PREFLIGHT WALK-AROUND, CREW FOUND POSSIBLE EVIDENCE OF LIGHTNING STRIKE ON RADOME. MAINTENANCE PERFORMED LIGHTNING STRIKE INSPECTION AND FOUND FIVE (5) BURN MARKS AT FRONT OF RADOME UNDER EROSION BOOT. BURN MARKS DETERMINED TO BE PAINT DAMAGE ONLY. NSDR DALA1231619009Pin · wornDURING FUNCTIONAL CHECK OF TAILCONE RELEASE SYSTEM FOUND EXCESSIVE WEAR ON PIN ASSEMBLY FITTING. REMOVED AND REPLACED PIN PER AMM. OPERATION CHECKS GOOD. OKAY FOR SERVICE.SDR DALA1231609009Release Cable · out of limitsWHILE PERFORMING INTERNAL RELEASE OF TAILCONE, PULL FORCE WAS LOW, 17LBS. ADJUSTED TAILCONE LATCHES PER AMM. PULL FORCE WITHIN LIMITS, 31 LBS. OPERATION CHECKS GOOD. OKAY FOR SERVICE.SDR R61A201205120293Drain · corrodedWHILE AIRCRAFT WAS IN FOR HEAVY CHECK, LEVEL 2 CORROSION WAS FOUND ON THE REAR FUSELAGE DRAIN, MID 2 DRAIN AND MID 1 DRAIN FAIRING (SHOWED EVIDENCE OF CORROSION BUILD UP). MAINTENANCE REPAIRED CORROSION BUILD UP TO REAR FUSELAGE MID 1 & 2 DRAIN FAIRINGS IAW ESDR DALA1231009214Cable · misroutedTAILCONE EMERGENCY EXIT EXTERIOR HANDLE LOCKING CABLE MISROUTEED PER DWG 59133350 SHEET 2 VIEW J-J. ALSO EXTERNAL HANDLE IS SEALED WITH PAINT AND UNABLE TO MOVE. FREED EXTERNAL HANDLE. REROUTED LOCKING CABLE IAW AMM 53-52-01-0830-801 PG 4 FIGURES 503 AND 50SDR DALA1230910966Bushing · damagedDURING FUNCTIONAL CHECK OF TAILCONE RELEASE SYSTEM, MAINTENANCE FOUND THE TEE PIN BUSHING, AS WELL AS THE LOWER CABLE CONDUIT DAMAGED, BEYOND ALLOWABLE LIMITS.SDR V0XR201205080039Fairing · brokenPASSENGER DOOR AFT HINGE FAIRING BROKEN. REMOVED AND ATTEMPTED REPLACEMENT, MOUNT HOLES TRANSFERRED FROM ORIGINAL AFT FAIRING TO NEW REPLACEMENT FAIRING, RESULTED UPON INSTALLATION OF NEW FAIRING THE TRANSFEREED FAIRING MOUNT HOLES WERE MISALIGNED TO THE FUSE
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