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 ASOA201001849Windshield · crackedRT WINDSHIELD HEAT ARCED AND CAUSED THE WINDSHIELD TO CRACK IN FLIGHT (ENROUTE ACFT DIVERTED DUE TO MX -- EMERGENCY DECLARED AS A PRECAUTION) R & R RT WINDSHIELD IAW AMM 56-11-01. LEAK CK GOOD IAW AMM 21-32-00, WINDSHIELD HEAT OP CK GOOD IAW AMM 30-41-01. (SDR HNAA2010120300263Windscreen · smokePOPPING SOUND AND LIGHT SMOKE FROM LOWER PORTION OF CAPTAIN'S WINDSCREEN FOLLOWED BY BURNING RUBBER AND ELECTRICAL ODOR. R & R F/O'S RT WINDSCREEN IAW WC 56-00-00R.SDR SWAA107179Window · arcedR1 COCKPIT WINDOW ARCED. REMOVED AND REPLACED R1 WINDOW PER MM.SDR CA101201001Window · crackedREF DEFECT-953421 LP-540409 CAPT SIDE WINDOW CRACKING. PIREP- "WHILE ON DECENT INTO THE YVR TERMINAL AREA THE CAPTAIN`S SIDE WINDOW DEVELOPED A CRACK FROM THE FRONT TO BACK SIDES OF THE WINDOW. IN UNDER A FEW MINUTES TWO ADDITIONAL CRACKS DEVELOPED OF SIMILASDR CA101130008Window · failedWHILE IN CRUISE, THE CREW OBSERVED A SPARK/FLASH OF LIGHT THEN THE F/O`S FRONT WINDSCREEN SHATTERED. CREW OPTED TO DIVERT TO YLW AS IT WAS CLOSER AND THEY DECLARED AN EMERGENCY. FLIGHT LANDED SAFELY. PASSENGERS WERE SENT TO YKA VIA GROUND TRANSPORT. CREW WSDR VNAA2010120200019Window · crackedCREW REPORTED A CRACKED COCKPIT RIGHT WINDOW. FLIGHT DIVERTED TO BNA AND LANDED WITHOUT INCIDENT. MAINTENANCE USING AIRCRAFT MAINTENANCE MANUALS REMOVED AND REPLACED THE RIGHT COCKPIT WINDOW. AIRCRAFT WAS RELEASED FOR SERVICE.SDR AALA20101127MIA02Cable · brokenMIA - CAPTAINS SLIDING WINDOW OPENED DURING TAKEOFF ROLL. EMERGENCY DECLARED FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND WINDOW LOCKING CABLE BROKEN. REPLACED CAPTAINS SLIDING WINDOW. SYSTEM GROUND CHECK NORMAL OPERATSDR MASA2010113001354Windshield · crackedAT 280 MILES WEST OF DESTINATION (DSM) THE CREW RECEIVED A WINDSHIELD HEAT WARNING. THE CAUSE SEEMED TO BE A 5 INCH CRACK THAT TRACED THROUGH THE WINDSHIELD HEATING ELEMENT. CREW REDUCED ALTITUDE AND CABIN PRESSURE. ON DESCENT THE CAPTAIN'S WINDOW SHATTEREDSDR IPXA0563697Window · out of alignmentF/O COCKPIT WINDOW - UNABLE TO CLOSE AND LOCK. PERFORMED R2 WINDOW ADJ/TEST IAW AMM 56-11-02-5. WINDOW OPS NORMAL.SDR IPXA0563684Handle · stuckCAPTAIN'S WINDOW WILL NOT OPEN. RELEASE HANDLE IS STUCK AND WILL NOT MOVE BACK TO UNLOCK WINDOW. R & R CAPT L2 WINDOW LINK ARM IAW MM 56-11-02-4 ADJUSTED IAW MM 56-11-02-5. OPS NORMAL.SDR HNAA2010120300259Windshield · crackedF/O'S FRONT WINDSHIELD IS CRACKED. (CRACKED IN FLIGHT AT APPROX 3000 FT, WINDSHIELD HEAT IN WARMUP). R & R F/O'S WINDSHIELD IAW WC 56-00-00R, OPS CHECKED GOOD, OK FOR SERVICE.SDR C2XA10IA312Seal · out of positionIAH - FLIGHT 2568, DURING CLIMB, THE CREW REPORTED THAT THE F/O'S DV WINDOW SEAL POPPED OUT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE DV WINDOW PROFILE SEAL, LEAK CHECKED WITH NO DEFECTS, AND THE AIRSDR DXTA2010112402421Windshield · failedRT WINDSHIELD STARTED ARCHING AT 43,000 FT. COMPLETED THE EMERGRNCY CHECKLIST AND DESCENDED TO 10,000 FT. AROUND 20,000 FT THE WINDSHEILD SHATTERED.SDR CA101202004Windshield · crackedIN CRUISE THE CREW HEARD A LOUD BANG AND IMMEDIATELY NOTICED THE LEFT WINDSHIELD OUTER PANE HAD COMPLETELY CRACKED. THEY REQUESTED DESCENT, SLOWED THE AIRSPEED AND BEGAN TO DIAL UP THE CABIN TO REDUCE THE PRESSURE ON THE GLASS. THEY THEN REQUESTED A DIVERSIONSDR FDEA201011174401Window · crackedL-1 WINDOW CRACKED AND ARCED AT FL 210 DURRING CLIMB OUT. NO WEATHER AS AN ISSUE. SMOOTH AIR AND CLEAR SKIES. 3-4 CRACKS ALL ON OUTER PANE. REMOVED AND REPLACED L-1 WINDOW IAW AMM 56-11-011-4. WINDOW HEAT TEST CHECKED NORMAL IAW 30-41-033-4 RII 236332 R/C ASDR AALA20101116NRT01Window · crackedLEFT NUMBER 3 WINDOW HAS CRACKS IN ALL CORNERS. REPLACED LEFT NUMBER 3 WINDOW PER AMM 56-11-21-4. OPS CHECK NORMAL.SDR CA101121001Window · failedTHE CAPTAINS WINDSHIELD SHATTERED IN FLIGHT AT 30,000 FT. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS WINDSHIELD I/A/W AMM CH 56-11-01.SDR CA101115015Windshield · cracked(CAN) DURING CRUISE, THE FLIGHT CREW ENCOUNTERED A CRACKED OUTER WINDSHIELD. THE FLIGHT CREW DIVERTED THE AIRCRAFT. EMERGENCY VEHICLES WERE CALLED OUT LOCALLY AS A PRECAUTION. THE FLIGHT CREW DID NOT DECLARE AN EMERGENCY.SDR UALA2010111604244Seal · leakingFIRST OFFICERS WINDOW 2R CONTINUES HIGH PITCHED SQUEAL. HALF WAY UP AFT VERTICAL POST. FOUND SEALANT MISSING FROM SEAL RETAINER AT LOWER WINDOW FRAME. APPLIED SEALANT PER MM. CHECKED WITH DEF PRESS 3.0, NO LEAK FOUND PER MM. REPLACED RIGHT NR 2 SLIDING WSDR SWAA107182Window · arcedDIVERSION - R1 COCKPIT WINDOW ARCED DURING FLIGHT. REMOVED AND REPLACED R1 WINDOW SHIELD AND HEAT CONTROLLER PER MM.SDR IPXA0563605Window · failedF/O WINDOW UNABLE TO CLOSE WITHOUT USING 2 PEOPLE. REQUIRES FORCE TO CLOSE WINDOW EXTREMELY HIGH. ABLE TO CLOSE WINDOW AFTER 8 ATTEMPTS. ACCOMPLISHED ADJUSTMENT OF INBD/OTBD OF NR2 WINDOW IAW AMM 56-11-02-5 PARA (3). OPS CK NORMAL. OK FOR CONTINUED SERVICE.SDR REXA201000255Seal · missingDURING ARRIVAL IN MILWAUKEE, WI (MKE), THE FLIGHT CREW REPORTED AN AIR NOISE IN THE FLIGHT DECK AREA. A CABIN PRESSURE FLUCUATION WAS ALSO REPORTED BUT NOT ABLE TO BE QUANTIFIED. UPON FURTHER INSPECTION, A 1.5 INCH PORTION OF THE SEAL BETWEEN THE MAIN WINDSHSDR CA101108003Windshield · cracked(CAN) EN ROUTE IN THE CRUISE PHASE, THE FIRST OFFICERS WINDOW BEGAN TO ARC. THE CIRCUIT BREAKER WAS PULLED BUT THE WINDOW EVENTUALLY CRACKED. THE QRH WAS FOLLOWED AND THE FLIGHT DIVERTED. NO EMERGENCY WAS DECLARED.SDR UALA2010110504115Window · out of adjustFOUND CAPTAINS SLIDING WINDOW DIFFICULT TO OPEN THE FIRST TIME AFTER THE AIRCRAFT IS PRESSURIZED. AFTER THAT IT OPENS EASILY, ADJUSTED LOWER LINK ARM. PRESSURIZED ACFT TO 1.5 PSI AND WINDOW WAS DIFFICULT TO OPEN AND NEEDED MORE THEN THE 7LBS MAXIMUM ALLOWED PESDR UALA2010110304086Windshield · faultyLEFT WINDSHIELD DISPLAYED ON UPPER ECAM SCREEN. ANTI ICE. WINDSHIELD FOUND FAULTY. WINDSHIELD REPLACED. OKAY FOR SERVICE.SDR RMXA2010F00217Windscreen · crackedRT FWD WINDSHIELD CRACKED DURING FLIGHT. ACFT RETURNED TO AIRPORT WITHOUT INCIDENT.SDR IPXA10563485Window · bindsF/O'S SLIDING WINDOW DIFFICULT TO OPEN, BINDS IN TRACK, FOUND LINK ARM BUSHING WORN. R & R LINK ARM ASSY LUBED TRACKS & SECURED C-SCREW SHAFT IAW 56-11-02 F/O'S NR 2 SLIDING WINDOW. OPS CK'S GOOD.SDR WWQA110110Windshield · crackedWHILE IN CRUISE, THE RT WINDSHIELD OUTER PLY CRACKED. THE CREW LANDED THE ACFT AT TO VERIFY IT WAS ONLY THE OUTER PLY. THE CREW THEN WROTE A DISCREPANCY AND DEFERRED IT USING THE CDL FROM THE FLIGHT MANUAL CDL 56-1 AND CONTINUED ITS FLIGHT WHERE THE WINDSHIELSDR USAA2010110292465Windshield · crackedFLT 1822 - CLT- BOS - EMERGENCY LANDING - CAPTAIN'S FRONT WINDSHIELD CRACKED IN FLIGHT. DECLARED EMERGENCY. REPLACED CAPTAIN'S WINDSHIELD PER J/C 26L21056001. REMOVED AND REPLACED LEFT WINDOW HEAT COMPUTER PER AMM 30-42-34. OPERATIONAL CHECK WAS GOOD.SDR 2010F00230Windshield · crackedWHILE IN CRUZ THE RT WINDSHIELD OUTTER PLY CRACKED. THE CREW LANDED THE ACFT TO VERIFY IT WAS ONLY THE OUTER PLY. THE CREW THEN WROTE A DISCREPANCY AND DEFERED IT USING THE CDL FROM THE FLIGHT MANUAL 56-1 AND CONTIUED IT FLIGHT, WHERE THE WINDSHIELD WAS CHANGESDR SWAA106752Window · arcedL2 COCKPIT WINDOW ARCED. REMOVED AND REPLACED WINDOW AND CONTROLLER PER MM.SDR IPXA10563464Link · inoperativeCAPT SLIDING WINDOW DIFFICULT TO OPEN, UNABLE TO CLOSE. R & R ARM LINK TO L2 WINDOW. ADJUSTED ARM LINK AND UPPER CTR ROLLER. WINDOW OPENS AND CLOSES NORMALLY.SDR UALA2010110104025Windshield · crackedRT WINDSHIELD OUTER PANE CRACKED. WINDOW HEAT WAS WORKING PRIOR TO CRACKING. EICAS MSG AFTER CRACKED. R1 WINDSHIELD REPLACED IAW AMM AND CHECKS SATISFACTORY.SDR UALA2010102803996Window · delaminatedF/O RT REAR WINDOW DELAMINATED ON LWR EDG-APPEARS MILKY LIKE AN ELEC ARC MARK. REPLACED F/O RT REAR WINDOW.SDR DXTA2010102504269Window · crackedINNER MOST PANE OF DIRECT VISION CRACKED IN FLIGHT. CRACK IS ABOUT 20 INCHES LONG. REMOVED WINDOW AND INSTALLED NEW WINDOW. OPS CHECKED WINDOW HEAT SYS WITH NO DEFECTS. PRESSURIZED ACFT TO 4PSI AND LEAK CHECKED WINDOW WITH NO DEFECTS. ALL WORK ACCOMPLISHESDR CA101020005Windshield · crackedDEFECT 945435 CAPT OUTER PANE WINDSCREEN SHATTERED AT FL340. CREW REPORT THAT THEY HEARD A POP AND SAW A FLASH AND 2 SECONDS LATER THE WINDOW SHATTERED. PILOTS WINDSHIELD REPLACED IAW AMM 56-11-01 FUNCTION CHECKS & LEAK CHECKS COMPLETED & FOUND SERVICEABLE. SDR DALA1028291610Windshield · crackedPILOT RECEIVED AN EICAS WARNING THAT THE LEFT FORWARD WINDSHIELD HEAT WAS INOPERATIVE. CAPTAIN THEN NOTICED THAT THE WINDOW WAS CRACKED BUT NO SIGN OF LEAKAGE WAS IDENTIFIED. THE FLIGHT LANDED WITHOUT INCIDENT AND MAINTENANCE REPLACED THE NR 1 WINDSHIELD PERSDR CA101026006Windshield · crackedAT FL390, CAPTAIN`S WINDSHIELD CRACKED, DIVERTED. RAR CAPT`S WINDSHIELD IAW 56-11-01. (SEE ALSO SDR 2010103001627/SIMA201029301)SDR UALA2010101803851Windshield · damagedLOUD CONTINUOUS WHISTLE RT SIDE COCKPIT. REPLACED RT WINDSHIELD. NOISE INTERFERED WITH RADIO COMMUNICATION. STARTED REMOVAL OF RIGHT WINDSHIELD. CB'S PULLED. REMOVED OLD WINDSHIELD, CLEANED BOLTS AND FRAMES. REPLACED RIGHT WINDSHIELD.SDR SWAA106465Window · arcedL1 COCKPIT WINDOW ARCED IN UPPER RT CORNER. REMOVED AND REPLACED WINDOW PER MM.SDR SIMA201029301Windshield · crackedON FLIGHT 3767 DURING CRUISE AT FLIGHT LEVEL 390 THE CREW REPORTED THE CAPTAIN’S WINDSHIELD CRACKED. THE CAPTAIN ELECTED TO DIVERT TO DENVER. THE AIRCRAFT LANDED WITHOUT IINCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S WSDR SWAA106398Window · arcedR2 COCKPIT WINDOW ARCED AND DELAMINATED. REMOVED AND REPLACED WINDOW PER MM.SDR CA101012001Windshield · crackedCREW RETURNED TO DEPARTURE, DUE TO THEIR RT WINDSHIELD HEAT ELEMENT BURNED OUT. CREW REPORT WAS NO FIRE OR SMOKE SMELL, JUST A SMALL GLOW AND THEN A HAIRLINE CRACK IN THE WINDSHIELD. INCIDENT REPORT ON JAZZ SAFETY IRREGULARITY REPORT 101011/08. DEFECT 94385SDR Y9PA N617WA 10.12Windshield · crackedDEPARTED WITHOUT INCIDENT AND CLIMBED TO A CRUISING ALTITUDE OF 41,000 FT , APPROX 45 MINUTES INTO FLIGHT HEARD A VERY LOUD EXPLOSIVE SOUND, NOTICED THE LT SIDE WINDSHIELD WAS SEVERELY DAMAGED, CONFIRMED CABIN ALTITUDE AND DIFFERENTIAL REMAINED NORMAL, IMMEDISDR MASA2010101201115Windshield · smokeLT WINDSHIELD HEAT SMOKED IN FLT. MX R2 CAPTAINS WINDSHIELD, OPS CHECK GOOD.SDR ASOA201001509Windshield · crackedDURING CLIMB, CAPT SIDE WINDSHIELD CRACKED RETURN TO DEPARTURE, ACFT DID NOT EXCEED STRUCTURAL LANDING WEIGHT. (ACFT RETURNED TO DEPARTURE AFTER T/O -- SPARKS OBSERVED) R & R WINDSHIELD IAW AMM 56-11-01. OP'S AND PRESSURIZATION CHECKS STILL NEEDED, NO FURTHESDR IPXA10562981Latch · bindingR2 WINDOW LATCH MECHANISM JAMMING. R & R R2 WINDOW TO STEP 4C9 OF MM 56-11-02-4. COMPLETED REMAINING STEPS 4C10 THROUGH 4C21, AMM 56-11-02-4. OPS CK GOOD RII WINDOW HEAT POWER TERMINALS IAW GMM 04-02-MM 56-11-02-4.SDR SWAA105913Window · crackedR2 COCKPIT WINDOW ARCED AND CRACKED. REMOVED AND REPLACED WINDOW PER MM.SDR UALA2010100403650Window · delaminatedWINDOW (FLIGHT DECK) - SHOWS SIGNS OF DAMAGE. DELAMINATED MORE THAN 2 INCHES. F/O NR1 RT DELAMINATION IS MORE THAN 3.5 INCHES, MEASUREMENT IS 3.75 INCHES. VISIBILITY IS ONLY PARTIALLY AFFECTED. REPLACED F/O NR1 WINDOW ASSY IAW MM.SDR ASAA1058317Sliding Window · overheatedWINDOW HEAT R OVERHEAT SIDE ILLUMINATED. REMAINED ILLUMINATED AFTER COMPLETION OF QRH PROCEDURE FAULT CODE 304 020 42. REPLACED NR 2 RT SLIDER WINDOW PER MM 56 12 11 000 AND 56 12 11 400. OPS CHECK GOOD.
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