JASC 5610
Service difficulty reports · 9,652
Reports filed under 5610 · Flight Compartment Windows, 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 = '5610' 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 = '5610' 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 95ZZZX2146Slat Assy · mismfgTHE NEW STYLE CANOPY SLAT (ALUMINUM) REPLACES THE FIBERGLASS SLATS. THE ALUMINUM SLAT APPEARS TO BE MANUFACTURED TOO WIDE TO FIT PROPERLY ON THE CANOPY. THIS RESULTS IN THE SLAT BEING BOWED AT THE CENTER WHEN INSTALLED. THE CENTER SLAT SUPPORT PULLED AWAY FSDR 95ZZZX2402Support · crackedTHIS CANOPY SLAT IS A NEW DESIGN FROM SCHWEIZER. IT IS OF ALL ALUMINUM CONSTRUCTION AND REPLACES THE OLDER FIBERGLASS SLAT. THIS NEW TYPE SLAT APPEARS TO BE SLIGHTLY WIDER THAN THE PREVIOUS TYPE. WHEN IT'S BOLTED TO THE CABIN, IT BOWS SLIGHTLY AT THE CENTERSDR 9505642275Seal · looseDURING CLIMB, CAPTAIN'S WINDSHIELD EMITTING LOUD NOISE. MAINTAINED FL 160 AND DIVERTED TOWARDS ATL. DUMPED 11,000 POUNDS OF FUEL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND WEATHER SEAL TORN LOOSE ON TOP HALF OF WINDSHIELD. REMOVED SEAL AND REAPSDR VTZA95128Seal · ungluedIAD/ROC - FLT 6326 - DURING CLIMBOUT AT 125 HRS ON 4-10-95, RETURNED TO IAD DUE TO THE FO'S DV WINDOW SEAL LEAKING. AIRCRAFT WOULD NOT PRESSURIZE. AIRCRAFT RETURNED TO IAD WITH NO FURTHER INCIDENTS. MAINTENANCE RE-GLUED THE DV WINDOW SEAL AND PRESSURIZED THSDR HEEA954708Windshield · defectiveWINDHSIELD IS SHORT ON EDGE DISTANCE ON THE UPPER OUTBOARD CORNER.SDR ABXA9500310Hinge Pins · lack of lubeTHE FIRST OFFICER'S SLIDING WINDOW VERY DIFFICULT TO OPEN. CLEANED AND LUBED HINGE PINS AND LATCHING MECHANISM. WINDOW OPS CHECKED GOOD IAW DC-8 MM CHAPTER 56.SDR 95ZZZX2386Windhsield · mismanufacturedDURING PRE-PURCHASE INSPECTION, BOTH WINDSHIELDS WERE MEASURED UNDER MINIMUM THICKNESS SPECIFIED BY CESSNA AIRCRAFT. THESE ARE ORIGINAL UNITS AND MAINTENANCE RECORDS REFLECT NO REPAIRS SINCE NEW. IT IS SUSPECTED UNDER SPEC UNITS WERE INSTALLED NEW AT FACTORYSDR 95ZZZX2385Windshield · mismanufacturedDURING PRE-PURCHASE INSPECTION, WINDSHIELDS MEASURED UNDER MINIMUM THICKNESS SPECIFICED BY CESSNA AIRCRAFT. THESE ARE ORIGINAL EQUIPMENT AND MAINTENANCE RECORDS REFLECT NO REPAIRS. ITS IS SUSPECTED UNDER SPEC UNITS WERE INSTALLED NEW AT FACTORY. THIS AIRCRASDR C2XA95CL053Windshield · bird strikeFLT NR 3719 - PWM-EWR - CAPTIAN WINDSHIELD CRACKED BY BIRD STRIKE. EWR MAINTENANCE INSPECTED THE WINDSHIELD FOR THE PURPOSE OF A FERRY FLIGHT FROM EWR TO BTV FOR REPLACEMENT. BTV MAINTENANCE REMOVED AND REPLACED THE CAPTIANS WINDSHIELD IAW ATR-42 MAINTENANCESDR SCNA95045L-2 Window · not closedON INITIAL ACCELERATION AT HUX, L-2 WINDOW CAME OPEN. ABORTED TAKEOFF, RESHUT WINDOW, AND ALL INDICATION WERE NORMAL ON SECOND TAKEOFF (PACKS OFF TAKE-OFF). OPENED L-2 WINDOW AND INSPECTED TRACK AND LOCKING MECHANISM, CYCLED WINDOW SEVERAL TIMES AND FOUND ITSDR HEEA954627Windshield · distortedDISTORTED IN LOWER QUARTER AND L/H UPPER QUARTER (CAUSES SERIOUS VISUAL PROBLEMS DURING APPROACHES OFFSHORE).SDR HEEA954626Windshield · mis mfgFOUND WINDSHIELD TO HAVE IMPROPER FORM AND FIBERGLASS EDGING TOO THICK TO ALLOW PROPER FIT ON AIRFRAME. THIS CAUSED WINDSHIELD TO CRACK AT UPPER INBOARD CORNER. THE CRACK APPEARED THE FOLLOWING DAY AFTER THE INSTALLATION OF WINDOW WAS COMPLETED.SDR HEEA954625Windshield · mis mfgDURING INITIAL FIT OF WINDSHIELD ON AIRFRAME, FOUND WINDOW TO HAVE IMPROPER FORM AND FIBERGLASS EDGING TOO THICK TO ALLOW PROPER FIT ON AIRFRAME.SDR HEEA954624Windshield · mis mfgWINDSHIELD CRACKED DURING INSTALLATION AT UPPER INBOARD CORNER. FOUND WINDOW TO HAVE IMPROPER FORM AND FIBERGLASS EDGING TOO THICK TO ALLOW PROPER FIT ON AIRFRAME.SDR HEEA954623Windshield · mis mfgWINDSHIELD LAMINATED TO THICK AND CONTOUR OF WINDOW DOES NOT MATCH AIRFRAME.SDR HEEA954622Windshield · mis mfgWINDSHIELD LAMINATED TO THICK AND CONTOUR OF WINDOW DOES NOT MATCH AIRFRAME.SDR 95ZZZX3539Windshield · crackedNUC - UPON TAXIING ONTO RAMP IN AN UNPRESSURIZED CONDITION, THE FIRST OFFICER'S WINDSHIELD (OUTER PANE) CRACKED IN THE LOWER RIGHT CORNER. MAINTENANCE FOUND A CRACK IN THE OUTER GLASS RUNNING FROM THE OUTBOARD EDGE IN AN ARC APPROXIMATELY 10.50 INCHES IN LENGSDR 95FDEA00314Sliding Window · came openON ROTATION L/H SLIDING WINDOW CAME OPEN. TESTED CAPTS L2 WINDOW (SLIDING WINDOW) PER 727 MM 56-12-11 PG 505 PARA A, NO DEFECT NOTED. INSPECTED ENGINE INLETS AND EXHAUSTS, NO DEFECTS NOTED.SDR COM60442Windshield · shatteredPILOTS FRONT WINDSHIELD SHATTERED. REPLACED WINDSHIELD.SDR COM60441Window · leakingLT COCKPIT WINDOW LEAKED PRESSURIZATION AT 15,000 FEET CAUSING LOUD WIND NOISE. RESEALED THE LT SIDE COCKPIT WINDOW IAW M/M PROCEDURES AND AIRCRAFT RETURNED TO SERVICE.SDR DL73S951091Windshield · failedDURING CRUISE, HEARD BURNING NOISE AND HAS ACRID SMELL IN FLT DECK, THEN HAD SMOKE AT R-1 WINDOW TERMINAL BLOCK, LANDED BNA, FOUND R-1 WINDOW TERMINAL BURNED. RELACED R-1 WINDOW, CONTROLLER AND CIRCUIT BREAKER. OPERATION NORMAL.SDR 95ZZZX1586Windshield · crackedCOPILOT'S WINDSHIELD, OUTER PANEL SHATTERED AT FL 450. NO EMERGENCY ACTION WAS REQUIRED. DIVERTED TO DALLAS LOVE FIELD, AVIALL, FOR WINDSHIELD CHANGE. PART 91 OPERATION C/W FLIGHT MANUAL REQUIREMENTS ADDRESSING OUTER PANEL CRACKING.SDR SCNA95035L-1 Window · faultyWINDOW HEAT CONDUCTOR, UPPER LEFT L-1 WINDOW, ARCHING AND SMOKE NOTED. TURNED OFF L-1 AND L-2 WINDOW HEAT, CONDITION STOPPED. REPLACED L-1 WINDOW PER MM 56-11-11, PRESSURIZED WINDOW AS PER MM 36-00, OPS CHECKED WINDOW HEAT AS PER MM 30-45-02. NO LEAKS NOTEDSDR AWXA9500128Windshield · crackedORD- LAS - FLT 777 - DURING CRUISE, CREW NOTICED A BURNING SMELL FROM THE FO'S WINDOW. A SHORT TIME LATER THE WINDOW OUTER PANE SHATTERED. ACFT DIVERTED TO DSM AND LANDED WITHOUT INCIDENT. CONTRACT MX INSPECTED WINDOW AND VERIFIED ONLY OUTER PANE CRACKED. SDR 95ZZZX1275Windshield · screws corrodedWHEN REMOVING PILOT'S WINDSHIELD FOR REPLACEMENT, ALL ATTACH SCREWS WERE FOUND SEVERELY CORRODED TO THE POINT THE SCREWS BROKE WHEN REMOVAL WAS ATTEMPTED. BEECH RECOMMENDS REPLACEMENT AT 12,000 HOURS.SDR 9503456730Window · crackedEN ROUTE SFO-ANC, FLIGHT DIVERTED TO SEA DUE TO WINDOW 1R CRACKED. MAINTENANCE REPLACED THE WINDOW AND THE AIRCRAFT RETURNED TO SERVICE.SDR 9503289857Window Seal · looseDURING CLIMB JAX-MEM THE FLIGHT CREW HEARD A LOUD FLAPPING NOISE NEAR THE CAPTAIN'S EYEBROW WINDOW. MAINTENANCE CONTROL WAS NOTIFIED AND THE AIRCRAFT RETURNED TO JAX WITHOUT FURTHER INCIDENT. FOUND LOOSE SEALANT AT THE AFT SIDE OF THE CAPTAIN'S EYEBROW WINDOSDR ABXA9500121Retainer · crackedDURING D-CHECK ACCEPTANCE INSPECTION WHILE COMPLYING WITH AD 90-18-03; SB 56-11 REV 3, FOUND THE RIGHT CLEARVIEW WINDOW FRAME CRACKED IN THE UPPER AFT CORNER. REPLACED DOUBLER IAW DC-9 SRM 56-01 AND ABX REA D956-13036-SB.SDR 95UALA32011Window · looseCABIN DEPRESSURIZED DURING LANDING. FIRST OFFICERS WINDOW WAS THE SOURCE OF AIR LOSS. WINDOW IS LOOSE. WINDOW STARTED LEAKING ON DESCENT AND MOVED INWARD RELEASING CABIN PRESSURE ON TOUCH DOWN.SDR 96ZZZX4712Windshield · crackedWINDSHIELD CRACKED THROUGH OUTER PLY JUST ABOVE DEFOG NOZZLE OUTLET. DISCREPANCY NOTED ON POST-FLIGHT INSPECTION. BOTH WINDSHIELDS ON THIS AIRCRAFT HAVE BEEN REWORKED I N THIS AREA TO REMOVE CRAZING CAUSED BY WINDSHIELD HEAT. WINDSHIELD MET MINIMUM THICKNESSDR COM60429Windshield · crackedCO-PILOTS WINDSHIELD CRACKED. REPLACED WINDSHIELD.SDR DLM88950792Windshield · crackedDURING CRUISE, CAPTAIN'S L-1 WINDSHIELD OVERHEATED AND CRACKED. LANDED BOS. REPLACED WINDSHIELD AND CONTROLLER OPERATION NORMAL.SDR 95FDEA00152Window · crackedDURING CLIMB-OUT, R-1 WINDOW BEGAN ARCING FOLLOWED BY CRACKING OF THE OUTER PANE OF THE R-1 WINDOW. REMOVED R-1 WINDOW AND TAGGED PARTS, INSTALLED R-1 WINDOW PER MM 56-11-11. CHECK FOR CORRECT R-1 TERMINAL AND R-1 WINDOW CONTROL TO BE REPLACED. TERMINAL CK SDR 95ZZZX976Windshield · crackedPBI - STA 5681 - EN ROUTE FROM JAX TO MIA AT CRUISE FLIGHT, THE CAPTAIN'S FWD WINDSHIELD HEAT SHORTED INTERNALLY AND ARCED. SOON AFTER, THE OUTER PANE CRACKED RESEMBLING A SPIDER WEB. CAPTAIN'S VISIBILITY WAS NEAR ZERO. AN EMERGENCY WAS DECLARED AND THE AIRSDR 95ZZZZ126Windscreen · heating inopPILOT REPORTED THE RIGHT WINDSHIELD HEAT IS INOP. THE SYSTEM WAS TROUBLESHOT AND THE RIGHT WINDSCREEN WAS DETERMINED TO BE THE PROBLEM. THE RIGHT WINDSCREEN WAS REPLACED AND A FUNCTIONAL CHECK OF THE SYSTEM PERFORMED WITH ALL INDICATIONS NORMAL. (Z)SDR USAA950096Windshield · crackedBWI - FLT EN ROUTE DCA TO CMH WHEN CAPTAINS OUTER WINDSHIELD PANE CRACKED. FLIGHT DIVERTED TO BWI WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENACNE REPLACED CAPTAINS L1 WINDSHIELD. (Z)SDR PCAA9500193Windshield · failedSMOKE EMANATING FROM CAPT'S WINDSHIELD. REMOVED AND REPLACED CAPT'S WINDSHIELD DUE TO ARCING OF TERMINAL LEADS. ACFT RETURNED TO SERVICE. (W)SDR 95ZZZX1023Windshield · crackedPILOT'S WINDSHIELD OUTER LAYER CRACKED WHILE TAXIING TO RAMP AFTER LANDING.SDR 95ZZZX1027Window · chippedDURING CLEANING OF THE COPILOT'S SIDE WINDOW, A DEFECT WAS FOUND IN THE UPPER FORWARD CORNER. INVESTIGATION FOUND IT WAS A CHIP CAUSED BY THE WINDOW FRAME COMING IN CONTACT WITH THE WINDOW AND CAUSING A CHIP. THIS WAS A FACTORY INSTALLED WINDOW. CHECK CLEARSDR ABXA9500056Window · out of adjustDURING PREFLIGHT, BOTH CAPTAIN'S AND FIRST OFFICER'S SLIDING WINDOWS LOCKING MECHANISM LOCATED ON THE TOP FORWARD PART OF THE WINDOW, INTERMITTENTLY WILL NOT RELEASE. THIS RESULTING IN THE WINDOW NOT OPENING. ADJUSTED CAPTAIN'S AND FIRST OFFICER'S SLIDING WINSDR ABXA9500055Window · out of adjustDURING PREFLIGHT, BOTH CAPTAIN'S AND FIRST OFFICER'S SLIDING WINDOWS LOCKING MECHANISM LOCATED ON THE TOP FORWARD PART OF THE WINDOW, INTERMITTENTLY WILL NOT RELEASE. THIS RESULTING IN THE WINDOW NOT OPENING. ADJUSTED CAPTAIN'S AND FIRST OFFICER'S SLIDING WISDR USAA950037Windshield · crackedDCA - FLT 545 - DURING CLIMB-OUT, THE FIRST OFFICER'S WINDSHIELD HAD AN ELECTRICAL ARCING WHICH IMMEDIATELY CAUSED APPROXIMATELY TWENTY CRACKS IN THE OUTSIDE WINDOW. THE CAPTAIN DECLARED AN EMERGENCY AND RETURNED TO DCA. MAINTENANCE REPLACED THE WINDSHIELD. SDR 95ZZZX625Windshield · shatteredAIRCRAFT ARRIVED 1-8-95 WITH PILOT'S WINDSHIELD SHATTERED. REMOVED WINDSHIELD AND REPLACED WITH NEW, SN 94199H9537. NEW RETAINERS WERE FIT AND INSTALLED.SDR 9501161150Window · not latchedDURING TAKEOFF, THE FIRST OFFICER'S WINDOW CAME OPEN, ABORTED TAKEOFF. RESEATED AND LOCKED WINDOW. OPERATIONAL CHECK AND SECURITY CHECK OK.SDR HERA9502Windshield · crackedBET - FLT 1495 - EN ROUTE AT FL220, THE OUTSIDE LAYER OF THE RT FORWARD WINDSHIELD CRACKED. THE OUTSIDE AIR TEMPERATURE WAS MINUS 34 DEGREES CELSIUS AND THE WINDSHIELD HEAT WAS ON AT THE TIME. THE AIRCRAFT CONTINUED ON TO BET AND A LANDING WAS MADE WITHOUT ISDR ABXA9500181Retainer · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND CORROSION ON THE CAPTAIN'S CLEARVIEW WINDOW RETAINER. REPAIRED RETAINER IAW ABX REA D953-10757-MR.SDR 95ZZZW463Windshield · failedAIRCRAFT DEPARTED FIELD AT CRUISE ALTITUDE CAPTAINS WINDSHIELD SHATTERED. AIRCRAFT DIVERTED TO ALTERNATE AIRPORT AFTER DECLARING AND EMERGENCY, CALLED MX. WINDSHIELD ASSEMBLY REPLACED. AIRCRAFT RETURNED TO SERVICE. (W)SDR 95FDEA00014Window · crackedRIGHT FRONT WINDOW CRACKED, (FIRST OFFICER'S) OUTER PANE CRACKED. REMOVED AND REPLACED FIRST OFFICER WINDOW PER MM 56-11-11 UP TO 3 (8). COMPLETED INSTALLATION PER 56-11-11 PG 420 THROUGH STEP E. SEALANT APPLIED AT OPS CHECKED GOOD.SDR HEEA954173Windshield · separatedWINDSHIELD SEPARATED. RECEIVED WITH AIRCRAFT ON 12-26-94.SDR WTAA950039Seal · looseSFO - UNIDENTIFIED NOISE REPORTED IN COCKPIT DURING CLIMB. ACFT RETURNED TO STA WITHOUT INCIDENT. MAINTENANCE INSPECTED ACFT TO LOCATE SOURCE OF NOISE. FOUND 6 INCH PORTION OF 'PRC' SEAL LOOSE AT TOP OF CAPTAIN'S WINDSHIELD. REMOVED EXCESS MATERIAL. ACFT
Back to JASC 5610