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 P5CA9801431Fairing · delaminatedLEFT FUSELAGE BODY FAIRING AT STA 900 IS DELAMINATED. REPAIRED PANEL PER SRM 51-40-07.SDR P5CA9801430Fairing · delaminatedLEFT FUSELAGE BODY FAIRING AT STA 850 IS DELAMINATED. REPAIRED PANEL PER SRM 51-40-07.SDR P5CA9801429Fairing · delaminatedLEFT HAND UNDERWING ROOT PANEL DELAMINATED. REMOVED PANEL AND REPAIRED PANEL AND INSTALLED PER SRM 51-40-09.SDR TWAA9813502Stops · out of positionTAIL CONE UNSAFE LIGHT CAME ON DURING DEPARTURE OUT OF BWI. MADE UNSCHEDULED LANDING AT DCA. FOUND CABLE BALL STOPS HAD BECOME UNSEATED. REINSTALLED CABLE BALL STOPS AT UNSAFE LIGHT SWITCH. CHECK-C 10-29-97 LAX.SDR CALA9801447Sliding Blocks · inoperativeTHE TAILCONE HUNG UP DURING RELEASE CHECK, HANDLE PULL WAS GOOD. BOTH UPPER SLIDING BLOCKS WERE REPLACED. A TAILCONE DROP/FUNCTIONAL CHECK WAS PERFORMED IAW MM 53-53-01 AND OPERATION CHECKED GOOD.SDR AU980985Panel · separated(AUS) LT AND RT WING TO FUSELAGE PANELS SEPARATED FROM THE AIRCRAFT. PART TC: 33,163.SDR DHL9880321CFairing · crackedAT C CHECK, RT WING TO BODY FAIRING NR 262G CRACKED AT INTERNAL FWD CORNER. FABRICATED REAPAIR DOUBLER, 3 BY 2 PER SRM 53-2-0, N/R 874.SDR CALA9801415Cables · out of adjustTHE FORCE REQUIRED TO DROP TAILCONE USING INTERIOR HANDLE WAS EXCESSIVE AT 45 POUNDS. THE FORCE REQUIRED USING EXTERIOR HANDLE WAS LOW AT 15 POUNDS. THE TAILCONE CABLES WERE ADJUSTED IAW MM 53-50-3.SDR CALA9801383Clips · out of adjustTHE PULL FROM CLIPS AT INTERIOR TAIL CONE RELEASE HANDLE WAS HIGH AT 50 POUNDS. THE TAIL CONE HANDLE CLIPS WERE ADJUSTED IAW MM 53-53-00.SDR HEEA0015459Radome · mismanufacturedHOLE FOR RADOME MISMANUFACTURED.SDR TWAA9812301Tail Cone · deformedDURING C-CHECK, THE TAIL CONE FAILED TO RELEASE DURING ROUTINE CHECK. FOUND THE UPPER SECTION OF THE TAIL CONE WAS DISTORTED SO THAT THE FOUR ATTACH POINTS DID NOT ALIGN WITH THE ATTACHMENT PINS. WAS NECESSARY TO CUT BACK THE TOP OF THE TAIL CONE, DRAW THE PSDR 98ZZZX3094Hinge · wornDURING ROUTINE INSPECTION, FOUND T/R GEARBOX FAIRING HINGE WORN, FILLER DOOR MISSING. THE FILLER DOOR HAD CONTACTED ONE TAIL ROTOR BLADE. THIS BLADE WAS FOUND UNSERVICEABLE. TAIL ROTOR HUB BLADE ASSY WAS REPLACED. AIRCRAFT WAS VISUALLY INSPECTED AND RETURNSDR CALA9801347Tail Cone · warpedTHE FORCE REQUIRED TO RELEASE TAIL CONE DURING FUNCTIONAL CHECK WAS EXCESSIVE. THE TAIL CONE HUNG UP ON RIGHT SIDE LATCH PINS. A SERVICEABLE TAIL CONE WAS INSTALLED AND ADJUSTED IAW MM 53-53-00.SDR DL72W981509Skin · cracked.25 INCH CRACK DORSAL FIN SKIN LEFT SIDE BELOW PANEL 9523. REPAIRED PER M/M 54-30-0 PG 804.SDR CA980827020Radome · bird strike(CAN) MULTIPLE BIRD STRIKES ON RADOME. MAINTENANCE CONFIRMED EVIDENCE OF MULTIPLE BIRD STRIKES ON RADOME. AIRCRAFT CHECKED FOR OTHER DAMAGE AND NONE FOUND. AIRCRAFT DECLARED SERVICEABLE.SDR CA980814012Radome · bird strike(CAN) MUTIPLE BIRD STRIKES ON RADOME. MAINTENANCE INSPECTION OF RADOME CONFIRMED BIRD STRIKES, NO DAMAGE TO RADOME, ENGINES/VANES OR PITOT STATIC SYSTEM.SDR CALA9801242Latch Levers · out of adjustTHE PULL FROM INTERIOR, EXTERIOR, AND AFT CABIN DOOR TAIL CONE RELEASE HANDLES WAS LOW. THE TAIL CONE LATCH LEVERS WERE ADJUSTED IAW MM 53-53-02.SDR SWIA971218Radome · bird strikeHIT A BIRD ON CLIMBOUT AND RETURNED FOR LANDING. PERFORMED BIRD STRIKE INSPECTION, FOUND NOSE RADOME RIGHT LOWER CORNER DAMAGED. REPLACED RADOME.SDR CALA9801212Pins · wornTHE FORCE REQUIRED TO RELEASE TAILCONE USING EXTERIOR HANDLE WAS BELOW LIMITS. WORN ALIGNMENT PINS AND RECEPTACLES WERE REPLACED AND LATCHES WERE ADJUSTED IAW MM 53-50-00.SDR CA980908039Fairing · missing(CAN) ON TURNAROUND INSPECTION, FOUND HALF OF C-2 CARGO DOOR FAIRING MISSING. RIGHT STABILIZER LEADING EDGE BENT, POSSIBLY HIT BY FAIRING. LEADING EDGE REPLACED AND FAIRING INSTALLED.SDR 98UAL900294Fairng · not sealedVIBRATION AND HUM ADJACENT TO ROW 9. THE REPORTED VIBRATION THAT WAS HEARD FROM ROW 9 (LEFT) WAS A RESULT OF DETERIORATED SEALANT ON THE UPPER WING TO BODY FAIRING AT THAT SAME LOCATION. THE FAIRING WAS RESEALED AT THE IMC AND THE AIRCRAFT RELEASED.SDR P5CA9801060Fairing · corrodedLEVEL 1 CORROSION FOUND ON BODY FAIRING PANEL 191 BBL ANTENNA CUTOUT AREA. CORROSION REMOVED AND REPROTECTED PER SRM 51-10-01 AND 51-10-02.SDR P5CA9801031Skin · corrodedTAIL CONE AREA CORROSION REVEALED AT FORWARD AREA OF APU BATTERY ACCESS DOOR STA 2600. CORROSION AREA REMOVED AND REPROTECTED PER SRM 51-10-01 AND 51-10-02.SDR CALA9801156Clips · out of adjustTHE TAIL CONE RELEASE HANDLE INSIDE TAIL COMPARTMENT PULLED HIGH FROM CLIPS AT 45 POUNDS. THE CLIPS WERE ADJUSTED AND FUNCTIONALLY CHECKED GOOD IAW MM 53-50-00.SDR HEEA0014884Radome · mismanufacturedHOLES ON RADOME WILL NOT LINE UP.SDR CALA9801155Cables · out of adjustTHE TAIL CONE PULL FROM INTERIOR RELEASE HANDLE, EXTERIOR RELEASE HANDLE, AND AFT ENTRY DOOR WAS LOW. THE TAIL CONE CABLES WERE RIGGED AND FUNCTIONALLY CHECKED GOOD IAW MM 53-53-00.SDR AU980822Radome · mismanufactured(AUS) RADOME FAILED TO MEET THE REQUIREMENTS OF RTCA/00-213 FOR A CLASS B RADOME. (TRANSMISSION EFFICIENCY).SDR CALA9801114Fairing · crackedINSPECTION FOUND AFT INBOARD SIDE OF LT WHEEL WELL FORWARD FAIRING CRACKED. THE CRACK WAS STOP DRILLED, REPAIR ANGLES WERE FABRICATED AND INSTALLED IAW SRM 53-01, FIGURE 2.SDR DHL9870937CTail Cone · disbondedAT C CHECK, VERTICAL STAB TAIL CONE HAS METAL DOUBLER DISBONDING AT UPPER SURFACE. INSTALLED BONDED REPAIR PER SRM 51-20-3, N/R 4557.SDR ARWA980715Tail Cone · misrepairedTAIL CONE, IMPROPER REPAIR AT FS 1995. REMOVED IMPROPER REPAIR. CUT DAMAGED AREA. FABRICATED REPAIR PARTS IAW DC-8 SRM 53-2-0, 53-5-3, 51-1-4. TREATED, PRIMED AND INSTALLED REPAIR PARTS IAW DC-8 SRM 51-1-8, 51-1-11, 51-1-21. REF CF WORK ORDER 020663 NR COSDR ARWA980714Tail Cone · misrepairedTAIL CONE IMPROPER REPAIR AT FS 1985. REMOVED IMPROPER REPAIR. CUT DAMAGED AREA. FABRICATED REPAIR PARTS IAW DC -8 SRM 53-2-0, 53-5-3, 51-1-4. TREATED, PRIMED AND INSTALLED REPAIR PARTS IAW DC-8 SRM 51-1-8, 51-1-11 AND 51-1-21. REF CF WORK ORDER 020663 NRSDR CALA9800971Fillet · corrodedINSPECTION FOUND LT FUSELAGE FILLET PANEL MATING SURFACE CORRODED AT STA 756 TO 832. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-01, FIGURE 4, 51-10-4, 51-10-3, AND 51-30-2.SDR CALA9800956Bracket · crackedINSPECTION FOUND A 2 INCH CRACK IN FORWARD WING TO FUSELAGE FAIRING ATTACH BRACKET AT STA 579. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-2, 51-10-3, AND 51-30-5.SDR DL757981171Fillet · damagedINBOUND DAMAGE TO FUESLAGE FILLET PANELS AND LT WING INBOARD FLAP DUE TO OVERWING SLIDE DOOR OPENED AND SLIDE FELL OUT INTO AIR STREAM. REPAIRED DAMAGE AND REPLACED SLIDE.SDR CALA9800938Cables · out of adjmtTHE TAIL CONE RELEASE PULLED HIGH FROM EXTERIOR HANDLE. THE LATCH LEVERS, LEVER CABLES, AND EXTERNAL RELEASE CABLE SYSTEM WERE ADJUSTED IAW MM 53-53-00, PARAGRAPH A.SDR SWAA981047Web · wornDURING SCHEDULED 1/4 D-CHECK, FOUND WEB FOR SLIPPER FAIRING I/B OF NR 3 SLAT WORN. REMOVED AND REPLACED PER BOEING SRM.SDR CALA9800883Cables · out of adjustEXCESSIVE FORCE WAS REQUIRED TO RELEASE TAILCONE USING AFT CABIN DOOR AND THE INTERIOR RELEASE HANDLE. THE CABLES AND LATCHES WERE ADJUSTED IAW MM 53-53-00.SDR 9809319760Clips · out of adjustDURING TAILCONE FUNCTIONAL CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO REMOVE BOTH THE INTERIOR AND EXTERIOR RELEASE HANDLES FROM THE RETENTION CLIPS. ADJUSTED CLIPS. FUNCTIONAL CHECK OK.SDR 9808869944Clips · out of adjustDURING TAIL CONE FUNCTIONAL CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO REMOVE THE EXTERIOR DEPLOYMENT HANDLE FROM THE CLIPS. ADJUSTED CLIPS, FUNCTIONAL CHECK OK.SDR CALA9800793Rigging · out of rigFORCE REQUIRED TO PULL INTERIOR TAIL CONE RELEASE HANDLE IS TO LOW. RIGGED HANDLE PER MM 53-53-00.SDR CALA9800792Cable · frayedFORCE REQUIRED TO RELEASE TAIL CONE TO HIGH. REPLACED CABLE, RIGGED TAIL CONE PER MM 53-53-00 AND FUNCTIONAL CHECKED.SDR CALA9800779Fairing · corrodedLOWER SKIN FAIRING AT STA 950 IS CORRODED BEYOND LIMITS. FABRICATED, TREATED, PRIMED, AND INSTALLED NEW LOWER SKIN FAIRING PER SRM 51-40-2, 51-10-2 AND MM 51-20-11.SDR 9808459929Clips · out of adjustDURING TAIL CONE FUNCTIONAL CHECK, FOUND THAT INADEQUATE FORCE WAS REQUIRED TO REMOVE BOTH THE INTERIOR AND EXTERIOR TAIL CONE RELEASE HANDLES FROM THE RETAINING CLIPS. ADJUSTED CLIPS, FUNCTIONAL CHECK OK.SDR WTAA9880075Radome · bird strikeFAT - BIRD STRIKE TO NOSE CONE AREA. AIRCRAFT REMAINS IN MAINTENANCE FOR REPAIRS. (M)SDR 9808299933Release Mech · out of adjustDURING TAIL CONE FUNCTION CHECK, FOUND THAT INADEQUATE FORCE WAS REQUIRED TO DEPLOY TAIL CONE USING THE INTERIOR HANDLE. RIGGED TAIL CONE DEPLOYMENT SYSTEM, FUNCTIONAL CHECK OK.SDR CALA9800714Cables · out of adjustTHE TAILCONE HUNG UP ON AFT UPPER LATCH WHEN DEPLOYED AND THE TAILCONE RELEASE EXTERIOR HANDLE HUNG UP ON LOWER EDGE OF OPENING. THE TAILCONE CABLES WERE ADJUSTED IAW MM 53-53-00. IN ADDITION, THE SIDE CLIP ON FORWARD SIDE WAS STRAIGHTENED.SDR P5CA9800965Fairing · brokenRT STABILIZER ROOT UPPER FAIRING FWD EDGE BROKEN. FIBERGLASS REPAIRED PER SRM 51-40-15 AND 51-24-11.SDR P5CA9800979Fairing · brokenEMPENNAGE LEFT STABILIZER ROOT UPPER FAIRING FORWARD EDGE BROKEN. REPAIRED AS PER SRM 51-40-15.SDR ARWA980457Fairing · damagedDURING D-CHECK, FOUND FUSELAGE RIGHT SIDE FORWARD OF WING, FAIRING SUPPORT HOLE IS ELONGATED. REAMED HOLE TO .375 DIAMETER AND FABRICATED REPAIR DOUBLER AND INSTALLED IN ACCORDANCE WITH INTERNATIONAL AVIATION ADVISORS, CONSULTANTS, AND PARTS, EO 98012104. WOSDR DL72W980972Fairing · crackedANGLE OUT AT STA 957 LT SIDE OF FUSELAGE OVER STA 18A. FAIRING ATTACH WEB CRACKED REF EO 4-60175-3. STARTED FABRICATING REPAIR AS PER M/M 53-12-0 FIG 1. FABRICATED REPAIR PER M/M 53-12-0. HEAT TREATED REPAIR PORTS PER PS 900-4-1 NR 1. OK TO INST SPLICE ANG
Back to JASC 5350