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 CALA9601681Lock Pin · wornTHE TAILCONE HUNG UP ON UPPER RIGHT LATCH DURING DROP TEST. MAINTENANCE FOUND UPPER RIGHT BAYONET LOCK PIN WORN. THE LOCK PIN WAS REPLACED AND THE TAILCONE WAS ADJUSTED IAW MM 53-53-00.SDR WRLA96046Tailcone · damagedDURING C-CHECK, (UPON COMPLETION OF UNRELATED REPAIRS), TAILCONE WAS BEING RAISED TO 'STOWED' POSITION WHEN A LOUD 'BANG' WAS HEARD. MAINTENANCE PERSONNEL LOWERED TAIL CONE TO INVESTIGATE. INVESTIGATION FOUND FAILURE OF TAILCONE ACTUATOR ATTACH SUPPORT TO ATSDR P5CA9600834Fairing · crackedCRACK ABOVE THE ACCORDIAN SEAL STRIKE PLATE ON RIGHT FUSELAGE BODY FAIRING. REPAIRED PER BAC SRM 51-40-09.SDR CALA9601526Tailcone · deployedWHEN OPERATIONS ARRIVED AT AIRCRAFT THE TAILCONE WAS FOUND DEPLOYED WITH THE EMERGENCY SLIDE UNRAVELED, BUT NOT INFLATED. MAINTENANCE FOUND THE TAILCONE CRACKED AND THE EVACUATION SLIDE DEPLOYMENT LANYARD CLEVIS END BROKEN. A NEW LANYARD WAS INSTALLED IAW MMSDR 9622609884Release Mech · inoperativeDURING LINE CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO RELEASE THE TAILCONE. FOUND THE LOWER CABLE INNER SLEEVE LODGED IN THE CONDUIT. REMOVED THE SLEEVE, CHECKED OK.SDR REXA96048Nose Cone · bird strikeABORTED TAKEOFF DUE TO BIRD STRIKE, RETURNED TO GATE FOR INSPECTION. INSPECTED NOSE AND NOSE CONE, NO VISUAL DAMAGE NOTED. AIRCRAFT OK FOR SERVICE. (M)SDR CALA9601650Clips · out of adjustTHE EXTERIOR TAILCONE RELEASE HANDLE PULLED FROM CLIPS AT 20 POUNDS. THE CLIPS WERE ADJUSTED IAW MM 53-53-00.SDR CALA9601649Clips · out of adjustTHE INTERIOR TAILCONE RELEASE HANDLE PULLED FROM CLIPS AT 50 POUNDS. THE CLIPS WERE ADJUSTED IAW MM 53-53-00.SDR RRXA96117Fillet Panel · damagedDURING PREFLIGHT FOUND 17 BY 24 HOLE ON RING WING FILLET PANEL (P/N 5658351-2), PANEL NUMBER 261H, AT Y=718. REPAIRED RING WING FILLET PANEL BY FABRICATING EXTERNAL DOUBLER AND INSTALLED IAW PER DRAWING B36-RO1, TEMPORARY REPAIR. PANEL NUMBER 261H WAS REMOVESDR CALA9601318Fairing · damagedTHE LT WING INBOARD SLAT TO FUSELAGE FAIRING WAS FOUND DAMAGED ON ARRIVAL. ICE DAMAGE WAS SUSPECT DUE TO THE NR 2 WATER SYSTEM WAS FOUND LEAKING FROM OVERFLOW AT SERVICING PANEL. THE NR 2 WATER SYSTEM WAS EMPTY ON ARRIVAL. THE NR 2 WATER SYSTEM WAS PLACARDESDR CALA9601334Clips · out of adjustTHE TAILCONE INTERIOR RELEASE HANDLE PULL FROM CLIPS WAS LOW. THE CLIPS WERE ADJUSTED IAW MM 53-53-00.SDR CALA9601333Latches · out of adjustTHE TAILCONE RELEASE AT EXTERIOR HANDLE AND AFT ENTRY DOOR WAS LOW. THE TAILCONE LATCHES WERE ADJUSTED IAW MM 53-53-00.SDR P5CA9600716Fairing · brokenBROKEN DRAIN HOLE FAIRING AT BODY FAIRING STATION 920. REPAIRED BODY FAIRING DRAIN HOLE FAIRING PER BAC 53-30-03.SDR P5CA9600712Radome · damagedTHREE HOLES IN A/C RADOME. MADE FIBERGLASS REPAIR PER BAC SRM 53-30-03, 53-50-03 AND 51-24-11.SDR CALA9601267Latches · bindingTHE TAILCONE FAILED DROP CHECK AT 50+ POUNDS WHEN USING THE EXTERIOR RELEASE HANDLE. THE TAILCONE LATCHES WERE LUBRICATED AND OPERATION CHECKED GOOD.SDR GTIA96NK189Release Mech · out of adjustLOG PAGE 027001. TAIL CONE FAILED TO RELEASE DURING TAIL CONE RELEASE SYSTEM CHECK. ADJUSTED TAIL CONE RELEASE SYSTEM MECHANISM IAW DC-9 MM 53-50-0. OPS CHECKS GOOD. (X)SDR CALA9601301Cables · out of adjustTHE TAILCONE WOULD NOT DROP WHEN RELEASE HANDLE WAS PULLED. THE TAILCONE CABLES WERE RIGGED IAW MM 53-53-00.SDR CALA9601300Clips · out of adjustTHE TAILCONE EXTERIOR RELEASE HANDLE PULLED TOO LIGHT OUT OF CLIPS. THE EXTERIOR HANDLE CLIPS WERE ADJUSTED PER MM 53-53-00.SDR CALA9601153Cables · out of adjustTAILCONE RELEASE USING INTERIOR HANDLE PULLED LOW AT 15 POUNDS. THE TAILCONE CABLES WERE ADJUSTED IAW MM 53-50-00.SDR 97ZZZX594Seal Strip · debondedWING TO FUSELAGE RUBBER SEALING STRIPS BEGAN TO UNBOND AND PULL AWAY. STRIPS WERE INSTALLED 5-7-96. PILOT REPORTED THEY ARE A POST-FLIGHT ITEM AND WERE SECURE AT LAST PREVIOUS POST-FLIGHT. SUSPECTED CAUSE OF FAILURE TO BE IMPROPER BONDING OF RUBBER TO WING SDR UPS96820831Tail Cone · crackedINSPECTION TYPE DLY, 6 TO 8 INCH CRACK IN TAIL CONE BEHIND LEFT ELEVATOR. REPAIRED CRACK IN TAIL CONE PER EO DC-8-5350-7876-A.SDR RRXA96153Fillet · delaminatedDURING A MAINTENANCE VISIT, FOUND CENTER WING FILLET PANEL DELAMINATED, DAMAGE PAST LIMITATION IAW DC-8 SRM, AT PANEL NR 162R. REPAIRED BY FABRICATING NEW FILLET PANEL AND INSTALLING IAW REO-02134 REV IR AND DOUGLAS DRAWING 566752 APPENDIX A, TREATED AREA IAWSDR RRXA96155Fillet · delaminatedDURING A MAINTENANCE VISIT, FOUND FILLET PANEL NR 162-W DELAMINATED, DAMAGE PAST LIMITATIONS IAW DC-8, AT Y=1058 TO Y=1078 LEFT SIDE. REPAIRED BY FABRICATING NEW FILLET PANEL IAW REO-02133 REV IR AND DOUGLAS DRAWING 5656352, TREATED AREA IAW DC-8 SRM 51-1-8.SDR CALA9601186Clips · out of adjustMORE THAN 30 POUNDS OF FORCE WAS REQUIRED TO PULL THE INTERIOR TAILCONE RELEASE HANDLE FROM CLIPS. THE RETAINING CLIPS WERE ADJUSTED TO SPECIFICATIONS PER MM 53-53-00.SDR CA960801004Radome · hail damage(CAN) HAIL DAMAGE TO RADOME AND LH AND RH LEADING EDGE DEVICES.SDR CA960801003Radome · hail damage(CAN) BIRD STRIKE AND HAIL DAMAGE TO RADOME, WINDSHIELD REPLACED TEMPORARY REPAIR TO RADOME.SDR 96ZZZM1283Upper Pulley Pin · missingDURING MAINTENANCE, FOUND TAILCONE RELEASE CABLE RUN 310A FS 1168.895 OFF THE NR 2 UPPER PULLEY. ALSO, THE GUIDE PIN WAS MISSING FROM THE 2ND UPPER PULLEY FROM BOTTOM (CABLE RUN 301A). REROUTED CABLE ON PULLEY AND INSTALLED GUIDE PIN.SDR CALA9601102Clips · out of adjustTHE FORCE REQUIRED TO PULL INTERIOR AND EXTERIOR TAILCONE RELEASE HANDLES OUT OF CLIPS WAS EXCESSIVE. THE CLIPS WERE ADJUSTED IAW MM 53-53-00.SDR GLBA96159Fillet · puncturedDVL - REPAIRED HOLE ON FUSELAGE ON RIGHT WING FILLET IAW SRM 51-70-00. (M)SDR CALA9601115Clips · out of adjustTHE TAILCONE EXTERIOR RELEASE HANDLE HAD EXCESSIVE PULL OUT OF CLIPS. THE TAILCONE EXTERIOR RELEASE HANDLE CLIPS WERE ADJUSTED IAW MM 53-53-00.SDR P5CA9600340Fairing · delaminatedDELAMINATED BODY FAIRING PANEL LOCATED BETWEEN LEADING EDGE OF MAIN LANDING GEAR CENTER DOORS. REPLACED PANEL PER BOEING SRM 51-30-02 AND 51-24-11.SDR CALA9601101Latches · out of adjustTHE FORCE REQUIRED TO DROP TAILCONE USING THE INTERIOR RELEASE HANDLE AND AFT ENTRANCE DOOR RELEASE HANDLE WAS EXCESSIVE. THE TAILCONE LATCHES WERE ADJUSTED IAW MM 53-53-00.SDR P5CA9600317Fairing · missingRIGHT HAND PACK LOUVER DOOR ACCESS PANEL SECTION OF FAIRING MISSING AT FORWARD INBOARD END OF DOOR. INSTALLED NEW FAIRING IAW SRM 51-30-02.SDR DL767961571Fairing · missingON ARRIVAL, FOUND FAIRING PANEL 195CL MISSING AND PANEL 195DL LEFT WING DAMAGED. INSPECTED AIRCRAFT FOR ADDITIONAL DAMAGE. REPLACED PANELS PER ERA 359898-14. REPAIRED FUSLAGE DAMAGE BETWEEN FS 1219 AND FS 1241 AND ABOVE S-22 AND S-23 PER SRM.SDR CALA9600955Latches · out of adjustTHE PULL REQUIRED TO RELEASE TAILCONE USING THE EXTERIOR HANDLE WAS LOW. THE TAILCONE LATCHES WERE ADJUSTED IAW MM 53-53-10.SDR CALA9600954Clips · out of adjustEXCESSIVE PULL WAS REQUIRED TO RELEASE TAILCONE EXTERIOR HANDLE FROM CLIPS. THE EXTERIOR HANDLE CLIPS WERE ADJUSTED IAW MM 53-53-00.SDR CALA9601062Latch · out of rigTHE TAILCONE EXTERIOR RELEASE HANDLE PULLED LOW AT 20 POUNDS. TAILCONE LATCH ADJUSTMENT WAS PERFORMED AND PULL WAS WITHIN SPECIFICATIONS PER MM 53-50-3.SDR CALA9601036Latch · out of adjustTHE TAILCONE EXTERIOR RELEASE HANDLE PULLED LOW AT 20 POUNDS. TAILCONE LATCH WAS ADJUSTED AND THE EXTERIOR RELEASE HANDLE PULL TESTED WITHIN SPECIFICATIONS AT 34 POUNDS PER MM 53-50-3.SDR CALA9600862Cable · twistedINSPECTION FOUND TAILCONE RELEASE CABLE ON LEFT HAND SIDE AT TIMING BLOCK DAMAGED AND TWISTED. THE CABLE WAS REMOVED AND REPLACED.SDR CALA9600861Clips · wornTHE TAILCONE INTERIOR RELEASE HANDLE CLIPS WERE FOUND WORN AND THE HANDLE PULLED FROM CLIPS AT 5 POUNDS. THE CLIPS WERE REMOVED AND REPLACED.SDR ARWA9606033Tail Cone · crackedTAIL CONE HAS CRACKS OF .5 AND 1.5 AT LONGERONS 7L AND 11L. REPAIRED CRACKS PER DC-8 SRM 53-2-0, FIG 1B, SHEET 3 AND 53-5-3, FIG 4, SHEETS 1 AND 2. CLEANED AND TREATED AREA PER DC-8 SRM 51-1-8.SDR TSAA965740Fairing Seal · missingFLT 257 - HNL-LIH - RECURRING VIBRATION, LOUD HIGH FREQUENCY VIBRATIONS FROM RIGHT SIDE WING ROOT AREA. STARTED AT 11,000 FEET DURING CLIMB AND STOPPED AT 9,000 FEET. DURING DESCENT, VIBRATION FELT IN NR 2 THRUST LEVER AND CABIN FLOOR. VIBRATION NOTICED WITSDR VNAA9606005Radome · bird strikeSHORTLY AFTER T/O, THE CREW REPORTED STRIKING A BIRD IN THE VICINITY OF THE AIRCRAFT RADOME. CREW CONTINUED ON WITH THE FLIGHT AND LANDED IN PIT WITHOUT FURTHER INCIDENT. PIT MX INSPECTED THE AIRCRAFT AND DISCOVERED THAT THE RADOME HAD BEEN DAMAGED. THEY RESDR P5CA9600286Panel · crackedFOUND LEFT WING UPPER FIXED FAIRING PANEL JUST AFT OF R/S FORWARD OF MLG BEAM ASSEMBLY CRACKED. CRACK APPROXIMATELY 12 INCHES LONG. REPAIRED WITH FIBERGLASS OVERLAYS IAW SRM 51-40-09.SDR CALA9600766Cables · out of adjustTHE TAILCONE INTERIOR AND EXTERIOR HANDLES PULLED AT 50 POUNDS TO OPEN LATCHES. THE TAILCONE CABLE PULL TENSION WAS ADJUSTED IAW MM 53-53-00.SDR P5CA9600291Fairing · delaminatedFOUND AFT WING-TO-BODY FAIRING 194BR DELAMINATED. REPAIRED FAIRING IAW SRM 51-40-14.SDR DLL10961600Fairing Support · crackedLOWER FUSELAGE FAIRING ATTACH ANGLE WAS REPLACED DUE TO A 20 INCH CRACK FROM LBL 14 TO RBL 15 AT FS STA 983.SDR SWAA960375Radome · damagedON TAKEOFF, AIRCRAFT HAD LIGHTNING STRIKE TO RADOME AREA. ALL SYSTEMS FUNCTIONING NORMALLY. AIRCRAFT RETURNED TO MDW AND MADE AN UNEVENTFUL LANDING. PERFORMED LIGHTNING STRIKE INSPECTION AND REPLACED RADOME PER BOEING M/M.SDR 9610622703Radome · water contamDURING CRUISE FLIGHT, WEATHER RADAR BECAME UNRELIABLE. AIRCRAFT DIVERTED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED RADOME AND SEAL DUE RADOME FULL OF WATER ON LEFT SIDE. RADAR OPERATIONALLY CHECKED OK.SDR CALA9600683Clips · out of adjustTHE TAIL CONE INTERIOR HANDLE PULL FROM CLIPS WAS 10 POUNDS. THE CLIPS WERE ADJUSTED IAW MM 53-53-00.
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