JASC 5600
Service difficulty reports · 237
Reports filed under 5600 · Window/Windshield System, 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 = '5600' 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 = '5600' 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 IPXA2026073030927Window · arcedFO FWD WINDOW STARTED ARCING WE SHUT OF FWD WINDOW HEAT OUTER WINDOW SHATTERED RAN QRH PROCEDURE AND CONTINUED FLIGHT NO SIGNS OF LEAK OR WINDOW BEING DEFORMED.SDR 2025F00149Windshield · crackedWHILE AT CRUISE AT FL 450 THE CREW HEARD A LOUD BANG AND REALIZED LEFT WINDSHIELD HAD CRACKED. CREW FOLLOWED ALL CHECKLISTS AND PROCEDURES AND WAS ABLE TO LAND AT DESTINATION DUE TO HOW CLOSE WE WERE.SDR 2025FA0000109Window · failedAFTER DEPARTING KSAV, LEVELING OFF AT FL400 THE PILOT'S SIDE FRONT WINDOW OUTER PLY SHATTERED. CREW FOLLOWED THE CHECKLIST AND RETURNED TO KSAV.SDR IPXA2024112636647Window · arcedR FWD WINDOW STARTED TO ARC. CHECK LIST SAID TO CONTINUE. WINDOW WAS NOT DEFORMED, AIR LEAK NOT OBSERVED. FL370. REMOVED AND REPLACED R1 WINDSHIELD REF MM 56-11-00-424-015. FINAL TORQUES COMPLETED. OPS CHECKS, INCLUDING WINDOW HEAT & WIPERS, PASSED, REF AMM 56SDR IPXA2024103198309Controller · not seatedRH WINDOW LAT FAULT LIGHT ON TROUBLESHOT DUE TO ISSUE MOVING TO OTHER WINDOW PER THE CREW AND FOUND THE CONTROLLER NOT PROPERLY SEATED. RESEATED CONTROLLER AND OPS CK NORMAL FOR 1 HOUR. THIS CLEARS DEFERRAL AND PLACARD REMOVED. REF AMM 30-42-00SDR CALA2024110102772Window Frame · crackedRH NO.1 WINDOW,WINDOW FRAME,UPPER AFTER CORNER HAS CRACK INDIATI ON SIGNAL(THE ENDS OF THE CRACK WAS MARKED).(REF AAR NR 10000203 87)SDR SWAA2024070206806Handle · brokenFO ASSIST HANDLE BROKEN.<[01] REMOVED AND REPLACED FO ASSIST HANDLE PER SIP. OPS CHECK GOOD.SDR SIMA20230911001Unknown · unknownPOTENTIAL BIRD STRIKE 30K FT SHATTERED FO WINDOW DECLARED EMERGENCY.-C/A-C/W BIRD STRIKE INSPECTION WORK CARD FOUND FO WINDSHIELD OUTER PAIN SHATTERED. NO FURTHER DEFFECTS NOTED SEE ITEM 3 OF THIS LOGPAGE FOR NEW DISCREPANCY IAW WC 05-50-02-200-801 AND SRM 56-SDR CALA2023091102759Unknown · missingSPEEETAPE DEPAPARTED AT ABOUT 5000FT INCREASE NOISE AND ACCOMPLISHED RE- TORQUE OF CAPTAINS NO.1 WINDOW PER AMM 56-11-01-00A-720A-A . RE TAPED WINDOW PER 56-DIP. PRESSURERIZED CABIN NO LEAKS NOTED . AIRCRAFT RETURNED TO SERVICE. ADD EMP:U291296. WINDOW TORQUESDR 2023FA0000397Windshield · separationEN ROUTE TEB-PBI AT FL300, CAPTAIN'S SIDE WINDSCREEN SHATTERED. WHILE CABIN PRESSURE REMAINED NORMAL, AN IMMEDIATE DESCENT WAS REQUESTED FROM ATLANTA CENTER AS A PRECAUTION WITH CLEARANCE FOR AN IMMEDIATE DESCENT TO FL180. AFTER SWITCHING RADIO FREQUENCIES, FUSDR R61A2023070100096Unknown · unknownSPRAY PATTERN ON WINDSHIELD SUGGESTS BIRD STRIKE JUST LEFT OF CENTERLINE OF RADOME/SUPPORT STRUCTURE. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. PERFORMED BIRD STRIKE INSPECTION, NO DAMAGE FOUND.SDR CALA2023070302157Tape · loosePLASTIC BANGING CAPT LEFT WINDOW 10000FT.LEFT AND RIGHT WINDSHIELD INSPECTION PERFORMED IAW AMM 56-11-00-00A-280B-A NO DAMAGE FOUND , FOUND ONLY HI SPEED TAPE LOOSE ON LH AND RH WINDSHIELD AND ANOTHER SEGMENT OF HUMP SEAL DETACHED ON LH WINDSHIELD . FROM UP OSDR IXXA20230627039Unknown · unknownPRE-DEPARTURE CREW CALL BACK, R2 WINDOW FAILS TO CLOSE.AIRCRAFT GROUNDED FOR UNSCHEDULED MAINTENANCE. SYSTEM INSPECTION IAW B767 AMM 56-11-04 ISOLATED FAULT TO DAMAGES IN WINDOW SHEAR. REMOVED AND REPLACED #2 WINDOW MECHANISM SCREW ASSEMBLY. #2 WINDOW RIG, OPESDR TSAA20230606056Unknown · unknownCA 1464/140 CORROSION AT RH WINDOWS CUTOUT EDGE, BETWEEN STA 887 AND STA 907, (L:0.7",W:0.3"). ALL CORROSION REMOVED AT RH WINDOWS CUTOUT EDGE BETWEEN STA 887 AND STA 907 (L: 0.7", W:0.3"). REMOVED 0.003" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND PROTECTIVESDR TSAA20230606055Unknown · unknownCA 1464/139 CORROSION AT RH WINDOWS CUTOUT EDGE, BETWEEN STA 867 AND STA 887, (L:0.7",W:0.3"). ALL CORROSION REMOVED AT RH WINDOWS CUTOUT EDGE BETWEEN STA 867 AND STA 887. REMOVED 0.006" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND PROTECTIVE IAW B737-300 SRM SDR TSAA20230606043Unknown · unknownCA 1464/99 CORROSION AT RH WINDOWS CUTOUT EDGE, BETWEEN STA 685 AND STA 706, 2 AREA (L:3.2",W:0.2")(L:0.5",W:0.3"). ALL CORROSION REMOVED AT RH WINDOWS CUTOUT EDGE BETWEEN STA 685 AND STA 706 (L:3.2", W:0.2") (L:0.5", W:0.3"). REMOVED 0.003", 0.004" IS WITHISDR TSAA20230606042Unknown · unknownCA 1464/98 CORROSION AT RH WINDOWS CUTOUT EDGE, BETWEEN STA 663.75 AND STA 685 (L:4",W:0.3"). ALL CORROSION REMOVED AT RH WINDOWS CUTOUT EDGE BETWEEN STA 663.75 AND STA 685 (L:4", W:0.3"). REMOVED 0.003" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND PROTECTIVE SDR TSAA20230606041Unknown · unknownCA 1464/97 CORROSION AT RH WINDOWS CUTOUT EDGE, BETWEEN STA 597 AND STA 616 (L:0.4",W:0.4"). ALL CORROSION REMOVED AT RH WINDOWS CUTOUT EDGE BETWEEN STA 597 AND STA 616 (L:0.4", W:0.4"). REMOVED 0.009" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND PROTECTIVE IASDR TSAA20230606040Unknown · unknownCA 1464/96 CORROSION AT RH WINDOWS CUTOUT EDGE, BETWEEN STA 559 AND STA 578 (L:0.4",W:0.4"). ALL CORROSION REMOVED AT RH WINDOWS CUTOUT EDGE BETWEEN STA 559 AND STA 578 (L:0.4", W:0.4"). REMOVED 0.009" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND PROTECTIVE IASDR TSAA20230606039Unknown · unknownCA 1464/95 CORROSION AT RH WINDOWS CUTOUT EDGE, BETWEEN STA 540 AND STA 559, 2 AREA (L:0.7",W:0.5")(L:0.6",W:0.2"). ALL CORROSION REMOVED AT RH WINDOWS CUTOUT EDGE BETWEEN STA 540 AND STA 559 (L:0.7", W:0.5") (L:0.6", W:0.2"). REMOVED 0.006", 0.005" IS WITHISDR TSAA20230606038Unknown · unknownCA 1464/94 CORROSION AT RH WINDOWS CUTOUT EDGE, BETWEEN STA 520 AND STA 540, 3 AREA (L:2",W:0.5")(L:0.5",W:0.5)(L:0.5",W:0.5").
ALL CORROSION REMOVED AT RH WINDOWS CUTOUT EDGE BETWEEN STA 520 AND STA E540 (L:2",W:0.5") (L:0.5",W:0.5") (L:0.5",W:0.5"). REMOSDR TSAA20230606037Unknown · unknownCA 1464/93 CORROSION AT RH WINDOWS CUTOUT EDGE, BETWEEN STA 500B AND STA 500C (L:0.6",W:0.5"). ALL CORROSION REMOVED AT RH WINDOWS CUTOUT EDGE BETWEEN STA 500B AND STA 500C. REMOVED 0.006" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND PROTECTIVE IAW B737-300 SRSDR TSAA20230606036Unknown · unknownCA 1464/92 CORROSION AT RH WINDOWS CUTOUT EDGE, BETWEEN STA 500A AND STA 500B (L:0.5",W:0.4"). ALL CORROSION REMOVED AT RH WINDOWS CUTOUT EDGE BETWEEN STA 500A AND STA 500B (L:0.5",W:0.4"). REMOVED 0.004" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND PROTECTIVESDR TSAA20230606035Unknown · unknownCA 1464/91 CORROSION AT RH WINDOWS CUTOUT EDGE, BETWEEN STA 400 AND STA 420 (L:0.5",W:0.3"). ALL CORROSION REMOVED AT RH WINDOWS CUTOUT EDGE BETWEEN STA 400 AND STA 420 (L:0.5",W:0.3"). REMOVED 0.005" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND PROTECTIVE IAWSDR TSAA20230606028Unknown · unknownCA 1464/61 CORROSION AT LH WINDOWS CUTOUT EDGE, BETWEEN STA 907 AND STA 927, 6 AREA (L:1.3",W:0.5")(L:0.7",W:0.5")(L:0.8",W:0.5")(L:1",W:0.5")(L:0.3",W:0.3")(L:0.6",W:0.2"). ALL CORROSION REMOVED AT LH WINDOWS CUTOUT EDGE BETWEEN STA 907 AND STA 927 (L:1.3",WSDR TSAA20230606027Unknown · unknownCA 1464/60 CORROSION AT LH WINDOWS CUTOUT EDGE, BETWEEN STA 887 AND STA 907, 3 AREA (L:0.8", W:0.4")(L:0.3", W:0.3")(L:7.5", W:0.6"). ALL CORROSION REMOVED AT LH WINDOWS CUTOUT EDGE BETWEEN STA 887 AND STA 907 (L:0.8, W:0.4")(L:0.3", W:0.3")(L:7.5", W:0.6"). SDR TSAA20230606026Unknown · unknownCA 1464/59 CORROSION AT LH WINDOWS CUTOUT EDGE, BETWEEN STA 867 AND STA 887, 8 AREA (L:1.9", W:0.4")(L:1.6", W:0.5")(L:1.7", W:0.5")(L:1.9", W:0.5")(L:2.9", W:0.5")(L:0.4", W:0.3")(L:0.5, W:0.3")(L:0.5", W:0.4"). ALL CORROSION REMOVED AT LH WINDOWS CUTOUT EDGSDR TSAA20230606025Unknown · unknownCA 1464/58 CORROSION AT LH WINDOWS CUTOUT EDGE, BETWEEN STA 847 AND STA 867, 8 AREA (L:5.5", W:0.5")(L:1.7", W:0.5")(L:0.6", W:0.3")(L:0.5", W:0.3")(L:1.1", W:0.6")(L:0.5", W:0.4")(L:0.9", W:0.5")(L:1.6", W:0.5"). ALL CORROSION REMOVED LH WINDOWS CUTOUT EDGE,SDR TSAA20230606024Unknown · unknownCA 1464/57 CORROSION AT LH WINDOWS CUTOUT EDGE, BETWEEN STA 827 AND STA 847, 3 AREA (L:1", W:0,3")(L:2,7", W:0.5")(L:1.4", W:0.5"). ALL CORROSION REMOVED AT LH WINDOWS CUTOUT EDGE, BETWEEN STA 827 AND STA 847 (L:1", W:0.3")(L:2.7", W:0.5")(L:1.4", W:0.5"). RSDR TSAA20230606023Unknown · unknownCA 1464/56 CORROSION AT LH WINDOWS CUTOUT EDGE, BETWEEN STA 807 AND STA 827, 5 AREA (L:1", W:0.5")(L:0.4", W:0.3")(L:0.5", W:0.5")(L:0.6", W:0.4")(L:0.5", W:0.4"). ALL CORROSION REMOVED AT LH WINDOWS CUTOUT EDGE BETWEEN STA 807 AND STA 827 (L:1", W:0.5")(L:0.SDR TSAA20230606022Unknown · unknownCA 1464/55 CORROSION AT LH WINDOWS CUTOUT EDGE, BETWEEN STA 787 AND STA 807, 2 AREA (L:0.4", W:0.2")(L:1.1", W:0.5"). ALL CORROSION REMOVED AT LH WINDOWS CUTOUT EDGE, BETWEEN STA 787 AND STA 807 (L:0.4", W:0.2")(L:1.1", W:0.5"). REMOVED 0.002", 0.004" MATERISDR TSAA20230606021Unknown · unknownCA 1464/54 CORROSION AT LH WINDOWS CUTOUT EDGE, BETWEEN STA 767 AND STA 787, 2 AREA (L:0.9",W:0.3")(L:1.2", W:0.3"). ALL CORROSION REMOVED AT LH WINDOWS CUTOUT EDGE, BETWEEN STA 767 & STA 787, 2 AREA (L:0.9",W:0.3")(L:1.2", W:0.3"). REMOVED 0.003" MATERIAL ISDR TSAA20230606020Unknown · unknownCA 1464/53 CORROSION AT LH WINDOWS CUTOUT EDGE, BETWEEN STA 747 AND STA 767 (L:4.6", W:0.5"). ALL CORROSION REMOVED AT LH WINDOWS CUTOUT EDGE BETWEEN STA 747 & STA 767 (L:4.6", W:0.5"). REMOVED 0.006" MATERIAL IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND PROTESDR TSAA20230606019Unknown · unknownCA 1464/52 CORROSION AT LH WINDOWS CUTOUT EDGE, BETWEEN STA 727E AND STA 747 (L:0.7", W:0.5"). ALL CORROSION REMOVED AT LH WINDOWS CUTOUT EDGE BETWEEN STA 727E AND STA 747 (L:0.7", W:0.5"). REMOVED 0.0078" MATERIAL IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND SDR KKVA20230515001Unknown · unknownCREW REPORTED ACRID SMELL IDENTIFIED DURING THE FLIGHT. ADDITIONAL COMMUNICATIONS BETWEEN MX AND CREW MEMBERS IDENTIFIED A BURNING / BURNING RUBBER SMELL. THIS WAS IDENTIFIED DURING CLIMB ROUGHLY ONE HOUR INTO FLIGHT. ADDITIONAL CONVERSATIONS WITH MX MANAGESDR A6WA202305068591Unknown · unknownRH WINDOW SHATTERED IN FLIGHT AT FL280 PRESSURIZATION IS NORMAL CW CRH REQ INSP **********AIRCRAFT REMOVED FROM SERVICE********* IN WORKSDR 2023F00124Windshield · crackedWINDOW L1 CRACK. CORRECTIVE ACTION: WINDOW L1 REMOVED AND REPLACEDSDR CALA2023042401233Frame · crackedAFTER HFEC INSPECTION AT THE RH WINDOW FRAME AT THE UPPER AFT CORNER AND INNER CORNER RADIUS FOUND TO BE CRACK PER EA 5310-04554 REV B STEP 9.1 STEP 9.2.SDR QMLA2023041820030Sliding Window · unknownWE (PILOT, NURSE, MEDIC) WERE RETURNING FROM OUR FUELING POINT AFTER COMPLETING AN INTER-FACILITY TRANSFER.
APPROXIMATELY FOUR MINUTES INTO A SIX-MINUTE FLIGHT, THE PARAMEDIC SITTING IN THE COPILOT SEAT (WITHOUT CONTROLS) , ASKED IF HE COULD OPEN THE SLIDING SDR FDEA202304150654Unknown · crackedCOCKPIT RH 2# WINDOW UPPER RAIL 1EA HOLE CRACKED. PERFORMED THE REPAIR ON THE CRACKED HOLE AT ENTABLATURE AND UPPER RAIL OF RH 2# WINDSHIELD STRUCTURE AS PER FEDEX EA#: 6-5310-T0373929 P1, MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA202304150653Unknown · crackedCOCKPIT LH 2# WINDOW UPPER RAIL 1EA HOLE CRACKED PERFORMED THE REPAIR ON THE CRACKED HOLE AT ENTABLATURE AND UPPER RAIL OF LH 2# WINDSHIELD STRUCTURE AS PER FEDEX EA#: 6-5310-T0373930 P1, THIS REPAIR CATEGORY B. MAJOR REPAIR IAW GMM 6-2-100.SDR AALA202304114063Seal · damagedAIRCRAFT WAS GROUNDED: AFTER TAKE OFF FIRST OFFICER WINDSCREEN SOUNDS LIKE HEAVY RAIN AFTER FL 370 TRANSITION TO BOTH FIRST OFFICER AND CAPTAIN WINDOWS LOUDER IN CLIMB AND SPEED RELATED. FOUND HUMP SEAL DAMAGE AT LEFT UPPER CORNER FIRST OFFICER WINDSHIELD. ACCSDR 2023FA0000202Windscreen · crackedAT APPROXIMATELY 1640 EST, N829DL WHILE REPOSITIONING FROM OPF TO PDK (ATLANTA) AT FLIGHT LEVEL 330, THE LEFT, FOREWORD WINDSCREEN BEGAN TO DELAMINATE AND EVENTUALLY CRACK. THIS WINDSCREEN IS CERTIFIED TO MAINTAIN CABIN PRESSURE WHILE WITHSTANDING AERODYNAMIC SDR U5QA202304060114Unknown · unknownIN CRUISE AT FL390, AMBER “WINDSHIELD HEAT” CAS DISPLAYED, ONE MINUTE LATER AFTER CYCLING WINDSHIELD HEAT THE LH WINDSHIELD CRACKED. MX C/A: ACFT STILL AOG IN KFAR, SETUP WITH BOMBARDIER MRT TO R&R CONTROLLER AND WINDSHIELD, AWAIT PARTS DELIVERY AT THIS TIME.SDR CVGA20230329001Windshield · crackedRIGHT WINDSHIELD SHATTERED.SDR CALA2023031500768Window · openREJECTED TAKEOFF APPROX 100 KIAS DUE TO FO WINDOW OPENING. GROSS WEIGHT 153.6 INSPECTED AND OPS CHECKED WINDOW REF AMM 56-12-11. PERFORMED HIGH ENERGY STOP REF AMM 05-51-07. FELL IN COOLING RECOMMENDED RANGE. AIRCRAFT ON THE GROUND PAST RECOMMENDED RANGE. OK TSDR CALA2023031300721Window Frame · crackedSUSPECT CRACK IN R3 WINDOW FRAME ON FWD. SIDE 2ND FASTENER FROM BOTTOM PERFORMED HFEC SURFACE INSPECTION OF L3 WINDOW FRAME AT SECOND FASTENER HOLE FROM THE BOTTOM OF FWD FRAME EDGE AND VERIFIED CRACK EMINATING AFT .200 FROM FASTENER EDGE. REF 737 NTM PART 6-5SDR CALA2023031300720Window Frame · crackedSUSPECT CRACK IN L3 WINDOW FRAME ON FWD. EDGE 2ND FASTENER FROM THE BOTTOM PERFORMED HFEC SURFACE INSPECTION OF L3 WINDOW FRAME AT SECOND FASTENER HOLE FROM THE BOTTOM OF FWD FRAME EDGE AND VERIFIED CRACK ACROSS FASTENER HOLE TO EDGES.REF 737 NTM PART 6-51-00-SDR ASAA2023031042312Bolt · unknownFO SIDE FLIGHT DECK EMERGENCY ESCAPE WINDOW IS VERY DIFFICULT TO OPEN. GROUNDED - YES. STARTED FO WINDOW ADJUSTMENT PER B737-800 AMM 56-12-11-820-801(12) REPLACED FWD BOTTOM SPECIAL BOLT THREADS RUINED. NEEDS TO BE RETHREADED. REPLACED FWD LOWER ROLLER AND BOLSDR M17F2023/023Windshield · crackedWINDOW CRACKED NO 1 LEFT 56101041
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