JASC 5620
Service difficulty reports · 603
Reports filed under 5620 · Passenger 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 = '5620' 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 = '5620' 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 IXXA20170817305Window Frame · corrodedAIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. UPPER CARGO WINDOW FRAME R-20 HAS PITTED CORROSION ON LOWER SURFACE AREA. REMOVED AND REPLACED UPPER CARGO WINDOW FRAME NEW P/N 144N3250Y4 IN ACCORDANCE WITH STRUCTURAL REPAIR MANUAL 51-40-02 PARAGRAPH 7 AND DRAWING 144SDR IXXA20170817299Window Frame · corrodedUPPER CARGO R4 WINDOW FRAME LOWER AREA CORRODED. FOUND OUT OF LIMITS IAW SRM 56-20-02-1A-1.SDR IXXA20170816314Window Frame · corrodedAIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. UPPER CARGO WINDOW FRAME L-12 HAS PITTED CORROSION ON LOWER SURFACE AREA. REMOVED AND REPLACED UPPER CARGO WINDOW FRAME L12 IN ACCORDANCE WITH STRUCTURAL REPAIR MANUAL 56-20-02 FIGURE 201 1, AND STRUCTURAL REPAIR MANUALSDR IXXA20170815308Window Frame · corrodedAIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. UPPER CARGO WINDOW FRAME R-24 HAS PITTED CORROSION ON LOWER SURFACE AREA. REMOVED AND REPLACED CARGO WINDOW FRAME NEW P/N 144N3250Y4 IN ACCORDANCE WITH STRUCTURAL REPAIR MANUAL 51-40-02 PARAGRAPH 7 AND DRAWING 144N3200.SDR IXXA20170815307Window Frame · corrodedAIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. UPPER CARGO WINDOW FRAME R-23 HAS PITTED CORROSION ON LOWER SURFACE AREA. REMOVED AND REPLACED CARGO WINDOW FRAME NEW P/N 144N3250Y4 IN ACCORDANCE WITH STRUCTURAL REPAIR MANUAL 51-40-02 PARAGRAPH 7 AND DRAWING 144N3200.SDR IXXA20170815306Window Frame · corrodedAIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. UPPER CARGO WINDOW FRAME R-21 HAS PITTED CORROSION ON LOWER SURFACE AREA. REMOVED AND REPLACED CARGO WINDOW FRAME NEW P/N 144N3250Y4 IN ACCORDANCE WITH STRUCTURAL REPAIR MANUAL 51-40-02 PARAGRAPH 7 AND DRAWING 144N3200.SDR AALA201708029035Window · cloudyAIRCRAFT IN BASE MAINTENANCE. PASSENGER WINDOW 1 LEFT IS CLOUDY. REPLACED WINDOW PER AMM 21-31-00 AND ACCOMPLISHED A SATISFACTORY LEAK CHECK.SDR DALA2017070105111Pan · crackedCRACK ON RT RING PAN (FWD UPPER CORNER) STA Y=756 AT PAX CABIN (CPAX). RING PAN WAS REPAIRED PER SRM 56-20-02-2R-1 REPAIR 1.SDR DALA2017062905051Pan · crackedCRACKED LT UPPER RING PAN STA 926 AT PASSENGER CABIN AREA. LT UPPER RING PAN STA 926 AT PASSENGER CABIN AREA WAS REPAIRED PER SRM 56-20-02 REPAIR1 FIG 201.SDR DALA2017062905050Pan · crackedCRACKED LT LWR RING PAN STA 928 AT PASSENGER CABIN AREA. LT LWR RING PAN STA 928 AT PASSENGER CABIN AREA WAS REPAIRED PER SRM 56-20-02 REPAIR 1 FIG 201.SDR DALA2017062905049Pan · crackedCRACKED LT LWR RING PAN STA 890 AT PASSENGER CABIN AREA. LT LWR RING PAN STA 890 AT PASSENGER CABIN AREA WAS REPAIRED PER SRM 56-20-02 REPAIR 1 FIG 201.SDR DALA2017062905048Pan · crackedCRACKED LT UPPER RING PANS STA 869 AT PASSENGER CABIN AREA. LT UPPER RING PANS STA 869 AT PASSENGER CABIN AREA WAS REPAIRED PER SRM 56-20-02 REPAIR 1 FIG 201.SDR DALA2017062905047Pan · crackedCRACKED LT LWR/UPPER RING PANS STA 831 AT PASSENGER CABIN AREA. LT LWR/UPPER RING PANS STA 831 AT PASSENGER CABIN AREA WAS REPAIRED PER SRM 56-20-02 REP 1 FIG 201.SDR DALA2017062905046Pan · crackedCRACKED LT LWR RING PAN STA 637 AT PASSENGER CABIN AREA. LT LWR RING PAN STA 637 AT PASSENGER CABIN AREA WAS REPAIRED PER SRM 56-20-02 REP 1 FIG 201.SDR DALA2017062004838Pan · crackedCRACKED RING PAN ON STA Y=832 AND Y=870 AFT UPPER CORNER ALSO ON STA Y=579 LOWER FWD CORNER AT PAX CABIN LT SIDE. RING PAN WERE REPAIRED PER SRM 56-20-02-2R FIG 202 TYPE B.SDR DALA2017062004835Pan · crackedCRACKED RING PAN ON STA Y=908 AFT LOWER CORNER AT PAX CABIN RT SIDE. RING PAN WERE REPAIRED PER SRM 56-20-02-2R FIG 202 TYPE B.SDR AALA201706199064Controller · inoperativeAIRCRAFT WAS NOT GROUNDED. L1 AND R1 DOOR-MOUNTED ELECTRICALLY DIMMABLE WINDOW CONTROLLERS ARE INOPERATIVE. ACCOMPLISHED RESET IAW AMM DMC-B787-A-56-21-03. OPERATIONAL CHECK GOOD.SDR AALA201706129050Window · crazedCRAZED LEFT NR 1 WINDOW BETWEEN FRAMES 23 AND 24. REPLACED THE WINDOW IAW AMM 56-20-00.SDR VNAA2017051000004Window · unknownLOUD POP FROM CABIN WINDOW.SDR 3HDR2017022000003Window · migratedDURING A PRELIMINARY INSPECTION OF THE FUSELAGE EXTERNAL AREAS A GASKET TYPE MATERIAL WAS FOUND MIGRATING OUT BETWEEN THE FORWARD RT PASSENGER CABIN WINDOW AND THE FUSELAGE SKIN. APPROXIMATELY 1.0 INCHES IN LENGTH AND 1/4 INCHES HIGH OF MATERIAL WAS NOTED STICSDR DALA2017021101137Pan · crackedCRACK ON LT RING PAN AT STA Y= 909 LWR SIDE (C PAX). DAMAGE AREA WAS CUT OUT PER SRM 56-20-02 REP 1 FIG 202. HFEC INSPECTION WAS PERFORMED ON TRIMMED AREAS NO CRACKS WERE FOUND ON EDGES PER NDTSPM 06-10-01.001. ANGLE AND WASHER REPAIR WERE FABRICATED PER SRM 5SDR DALA2017021101136Pan · crackedCRACK ON LT RING PAN AT STA Y= 877 UPPER SIDE (C PAX). DAMAGE AREA WAS CUT OUT PER SRM 56-20-02 REP 1 FIG 202. HFEC INSPECTION WAS PERFORMED ON TRIMMED AREAS NO CRACKS WERE FOUND ON EDGES PER NDTSPM 06-10-01.001. ANGLE AND WASHER REPAIR WERE FABRICATED PER SRMSDR DALA2017021101135Pan · crackedCRACK ON LT RING PAN AT STA Y= 831 UPPER SIDE (C PAX). DAMAGE AREA WAS CUT OUT PER SRM 56-20-02 REP 1 FIG 202. HFEC INSPECTION WAS PERFORMED ON TRIMMED AREAS NO CRACKS WERE FOUND ON EDGES PER NDTSPM 06-10-01.001. ANGLE AND WASHER REPAIR WERE FABRICATED PER SRMSDR DALA2017021101134Pan · crackedCRACK ON LT RING PAN AT STA Y= 637 UPPER SIDE (C PAX). DAMAGE AREA WAS CUT OUT PER SRM 56-20-02 REP 1 FIG 202. HFEC INSPECTION WAS PERFORMED ON TRIMMED AREAS NO CRACKS WERE FOUND ON EDGES PER NDTSPM 06-10-01.001. ANGLE AND WASHER REPAIR WERE FABRICATED PER SRMSDR DALA2017021101133Pan · crackedCRACK ON RT RING PAN AT STA Y= 889 LWR SIDE (C PAX). DAMAGE AREA WAS CUT OUT PER SRM 56-20-02 REP 1 FIG 202. HFEC INSPECTION WAS ACCOMPLISHED AND NO CRACKS WERE FOUND AFTER THE TRIM-OUT PER NDT SPM 06-10-01.001. ANGLE AND WASHER REPAIR WERE FABRICATED PER SRM SDR DALA2016120909722Pan · crackedCRACK ON LOWER FWD CORNER AT RING PAN WINDOW LT SIDE BTW STA Y 598-617. CRACKED RING PAN LOWER FWR CORNER BTW STA Y=598-617 LT, WAS REPAIRED PER SRM 56-20-02 FIG 202.SDR AALA201612129004Window · crazedCRAZED PASSENGER WINDOW BETWEEN FRAMES 60-61 AND STRINGERS 9 AND 12 LEFT. REPLACED WINDOW IAW AMM 56-20-00.SDR DALA2016113009392Pan · crackedCRACKED RT RING PAN LOWER/FWD CORNER STA Y=927 INTERNAL STRUCTURE (FUS). DAMAGE AREA WAS REPAIRED PER SRM 56-20-02, REPAIR 1, FIG 202.SDR DALA2016113009391Pan · crackedCRACKED LT RING PAN LOWER/AFT CORNER STA Y=636 INTERNAL STRUCTURE (FUS). RING PAN WAS REPAIR PER B717 SRM 56-20-02 FIG 202.SDR AALA201611159009Window · crazedCRAZED LEFT MAIN CABIN WINDOW AT STRINGER 8L TO 11L BETWEEN FRAMES 23 AND 24. REPLACED THE WINDOW IAW AMM 56-20-00 AND AMM 21-31-00.SDR ASMF20161216007Window · crackedAIRCRAFT RETURNED FROM FLIGHT DUE TO DURING CRUISE THE PASSENGER WINDOW 1A GOT CRACKED. AIRCRAFT WAS SENT TO THE HANGAR AND MAINTENANCE PERSONNEL REPLACED THE PASSENGER WINDOW 1A IAW AMM 56-21-00, TESTED CORRECT. THE GROUND HANDLING EQUIPMENT HITS AIRPLANE OR SDR DALA2016110708315Window · crackedCRACKED UPPER FWD CORNER WINDOW BETWEEN BS 427 AND 446. REPAIRED IAW SRM 56-20-02 REPAIR 1 TYPE C FIG 203. HFEC INSPECTION WAS ACCOMPLISHED AND NO CRACKS WERE FOUND AFTER TRIM OUT IAW NDT SPM 06-10-01. 001. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 56-2SDR DALA2016110208205Window Frame · burnedBURN DAMAGE TO WINDOW FRAME 3 SPOTS BETWEEN STATION 615 AND 645 RT SIDE. INSPECTED DAMAGE AREA AND BLENDED AREAS AND TREATED PER SRM 56-20-02.SDR AALA201609279006Window · crazedAIRCRAFT IN BASE MAINTENANCE. LEFT HAND CABIN WINDOW NR 1 CRAZED. REPLACED CABIN WINDOW NR 1 PER AMM 56-20-00.SDR AALA201608109017Window · crazedL1 PASSENGER CABIN WINDOW BETWEEN FRAMES 23 AND 24 AND STRINGER 8 - 11L HAS CRAZING. REPLACED THE WINDOW IAW AMM 56-20-00.SDR DALA2016080405760Pan · crackedCRACK FORWARD LOWER RING PAN STA Y=579 RT SIDE AT PASSENGER CABIN STRUCTURE. SM, CARD 3, ZONE 100. RING PAN WAS REPAIRED IAW SRM 56-20-02, FIG 202, TYPE B. CRACK LENGTH: 0.159" AND NO CRACKS WERE FOUND AFTER REMOVED DAMAGE IAW HFEC INSPECTION.SDR DALA2016080405759Pan · crackedCRACKED AFT LOWER RING PAN STA Y=851 LT SIDE AT PASSENGER CABIN STRUCTURE, CARD 4, ZONE 100. RING PAN WAS REPAIRED IAW SRM 56-20-02, FIG 202, TYPE B. CRACK LENGTH 0.132" AND NO CRACKS WERE FOUND AFTER REMOVE DAMAGE IAW HFEC INSPECTION.SDR DALA2016080405758Pan · crackedCRACKED AFT UPPER RING PAN STA Y=832, LT SIDE AT PASSENGER CABIN STRUCTURE, CARD 5, ZONE 100. RING PAN WAS REPAIRED IAW SRM 56-20-02, FIG 202, TYPE B. CRACK LENGTH 0.109" AND NO CRACKS WERE FOUND AFTER REMOVED DAMAGE IAW HFEC INSPECTION.SDR DALA2016080405757Pan · crackedCRACKED AFT LOWER RING PAN STA Y=636 LT SIDE AT PASSENGER CABIN STRUCTURE, CARD 6, ZONE 100. RING PAN WAS REPAIRED IAW SRM 56-20-02, FIG 202, TYPE B. CRACK LENGTH 0.140" AND NO CRACKS WERE FOUND AFTER REMOVE DAMAGE IAW HFEC INSPECTION.SDR DALA2016080405756Pan · crackedCRACKED AFT LOWER RING PAN, STA Y=617 LT SIDE AT PASSENGER CABIN STRUCTURE. SM, CARD 7, ZONE 100. RING PAN WAS REPAIRED IAW SRM 56-20-02, FIG 202, TYPE B. CRACK LENGTH: 0.125" AND NO CRACKS WERE FOUND AFTER REMOVE DAMAGE IAW HFEC INSPECTION.SDR DALA2016080405755Pan · crackedCRACKED AFT LOWER RING PAN STA Y=560 LT SIDE AT PASSENGER CABIN STRUCTURE. SM, CARD 8 ZONE 100. RING PAN WAS REPAIRED IAW SRM 56-20-02, FIG 202, TYPE B. CRACK LENGTH=0.158" AND NO CRACKS WERE FOUND AFTER REMOVE DAMAGE IAW HFEC INSPECTION.SDR VGCA20160725002Plug · corrodedCORROSION ON WINDOW PLUG FRAME BS 375 - 465. REPAIRED THE WINDOW PLUG IAW DWG R508-053-004-001.SDR AALA201607189038Window · crazedPASSENGER CABIN WINDOW NR 1 LEFT OUTER PANE OUTER SURFACE CRAZED. REPLACED WINDOW OUTER PANE IAW AMM 56-20-00.SDR VGCA20160708001Window Frame · corrodedCORROSION FOUND ON RIGHT WINDOW FRAME. REMOVED CORROSION, TREATED AND REPAIRED PER DWG R278-053-010-001.SDR JJBA20160622010Seal · out of positionINNER WINDOW SEAL POPPED OUT AT 4AB INFLIGHT. SECURED WINDOW PANE, NO OTHER DEFECTS.SDR AALA201606229003Window · crazedAIRCRAFT IN BASE MAINTENANCE: LT SIDE NR 1 PASSENGER CABIN WINDOW OUTER PANE IS CLOUDY, CRAZED. REPLACED WINDOW IAW AMM 56-20-00.SDR UIEA2016031500163Seal · leakingSEAT LOCATED 2L WINDOW SEAL LEAKING. R & R WINDOW SEAL LOCATED AT 2L SEAT POSITION IAW AMM 56-21-01.SDR COEA2016031412911Window Frame · corrodedHEAVY CHECK COE & MINOR REPAIR. LT CARGO COMPARTMENT WINDOW FRAME, BETWEEN FRAMES 23 & 24 HAS LEVEL 2 CORROSION. REPLACED WINDOW FRAME WITH OEM PART.SDR COEA2016031411911Window Frame · damagedHEAVY CHECK COE & MAJOR REPAIR. FRETTING DAMAGE ON LOWER INBD SURFACE OF WINDOW FRAME, FRAME 32 - 33, LEVEL 2. REPAIRED IAW SRAS CE 1526 16 10124 DATED 4 8 2016.SDR DALA2015112007086Pan · crackedCRACKED PAN ON MAIN ENTRANCE DOOR BETWEEN BEAMS 7 AND 8, BS 160. CRACK PAN ON MAIN ENTRANCE DOOR BETWEEN BEAM 7 AND 80 BS Y=160 WAS REPAIR IAW SRM 52-05D FIG 41 AND ER/A 539945-14, REV ORIG RII COMPLETED.
Back to JASC 5620