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 DALA2019022001070Pan · crackedCRACK RING PAN IN STA Y=908 AND L=14L, Y=870 AND L=12L, Y=851 AND L=12L. ALSO Y=832 AND L=12L AT CPAX. RING PAN REPAIRED PER SRM 56-20-02-2R PROCEDURE 1, REPAIR 1, FIG 202. TYPE B. (ET)HFEC INSPECTION WAS ACCOMPLISHED ON RING PAN IN STA Y=908 AND L=14L, Y=870 SDR AALA201901289001Window · crackedAIRCRAFT WAS NOT GROUNDED: PASSENGER REPORTS CRACK IN WINDOW AT SEAT ROW 14A. REPLACED ELECTRICALLY DIMMABLE WINDOW PER AMM 56-21-03.SDR AALA201901229033Window · delaminatedWINDOW PANE AT SEAT ROW 1F WAS DELAMINATED. REPLACED THE WINDOW.SDR AALA201901199001Window · crackedAIRCRAFT WAS NOT GROUNDED: PASSENGER WINDOW INNER PANE SCRATCHED OR CRACKED SEAT 12A. REPLACED WINDOW PER AMM 56-21-03.SDR AALA201901229032Window · delaminatedWINDOW PANE AT SEAT 27F WAS DELAMINATED. REPLACED THE WINDOW.SDR AALA201901179017Window · delaminatedWINDOW PANE DELAMINATED AT SEAT 9F. REPLACED THE WINDOW PANE.SDR AALA201901179016Window · delaminatedWINDOW PANE DELAMINATED AT SEAT 10F. REPLACED THE WINDOW PANE.SDR AALA201901179015Window · delaminatedWINDOW PANE DELAMINATED AT SEAT 11A. REPLACED THE WINDOW PANE.SDR AALA201901179014Window · delaminatedWINDOW PANE DELAMINATED AT SEAT 12A. REPLACED THE WINDOW PANE.SDR AALA201812209010Window · crazedL1 WINDOW WAS CRAZED BETWEEN FRAMES 23 - 24. REPLACED THE WINDOW IAW AMM 56-20-00, AND AMM 21-31-00.SDR CA190617005Window · debonded(CAN) RIGHT PASSENGER WINDOW - A PORTION OF THE REAR EDGE OF THE WINDOW SEPARATED FROM THE FRAME.SDR AALA2018111209006Window · crackedINNER WINDOW PANE WAS FOUND CRACKED AT SEAT 37A. REPLACED THE WINDOW PANE IAW AMM 56-21-02.SDR AALA201809209005Window · crackedCRACK IN THE DIMMABLE WINDOW AT SEAT ROW 12L. REPLACED THE WINDOW IAW AMM 56-21-03SDR DALA2018082875305Window · failedWINDOW AT 16A CRACKED IN FLIGHT, APPEARS TO BE OUTER PANE THAT DELAMINATED. OUTER PART OF WINDOW SEPARATED FROM AIRCRAFT IN FLIGHT. PERFORMED INSPECTION ON LT ENGINE WITH NO DEFECTS IAW AMM 05-51-19. REMOVED AND REPLACED PASSENGER COMPARTMENT WINDOW ASSY IAW SDR CALA2018070301544Window · scratchedWINDOW AT 37A HAS LARGE SCRATCH. REMOVED AND REPLACED CABIN WINDOW REF AMM 56-21-13.SDR 2018FA0000190Switch · inoperativeTHREE (3) OF THE PASSENGER CONTROL SWITCHES FOR THE CABIN WINDOW ELECTRONIC WINDOW SHADES HAVE FAILED INTERNALLY. THE LEFT SIDE FORWARD AND CENTER CONTROLS AND THE RIGHT SIDE CENTER CONTROL. BOTH LEFT SIDE SWITCHES ARE COMPLETELY INOP. THEY WILL NOT DARKEN, LISDR 2018FA0000189Window Shade · cloudyLEFT CENTER CABIN WINDOW WITH ELECTRONIC SHADING STUCK IN PRIVACY MODE. MAKING APPEAR AS IF YOU ARE LOOKING OUT THE WINDOW INTO SOLID CLOUDS. NO PASSENGER COMMANDS WORK TO CLEAR IT ARE CONTROL THE DARKENING. TESTED WINDOW IN A KNOWN GOOD POSITION, NO CHANGE TOSDR K11A2018072650808Window Frame · corrodedCORROSION ON EXTERIOR FUSELAGE PLUG WINDOW FRAME RTSIDE ACFT STA 610.SDR K11A2018072650807Window Frame · corrodedCORROSION ON EXTERIOR FUSELAGE PLUG WINDOW FRAME RT SIDE ACFT STA 590.SDR K11A2018050872605Window Frame · corrodedCORROSION ON EXTERIOR FUSELAGE PLUG WINDOW FRAME LT SIDE ACFT STA 1080.SDR K11A2018050872604Window Frame · corrodedCORROSION ON EXTERIOR FUSELAGE PLUG WINDOW FRAME RT SIDE ACFT STA 880.SDR K11A2018050872603Window Frame · corrodedCORROSION ON EXTERIOR FUSELAGE PLUG WINDOW FRAME RT SIDE ACFT STA 740.SDR K11A2018050872602Window Frame · corrodedCORROSION ON EXTERIOR FUSELAGE PLUG WINDOW FRAME RT SIDE ACFT STA 570-610.SDR K11A2018050872601Window Frame · corrodedCORROSION ON EXTERIOR FUSELAGE PLUG WINDOW FRAME RT SIDE ACFT STA 510-530.SDR PG9A2018040400151Window · inflt separationSHORTLY AFTER TAKE OFF, THE RT FORWARD PASSENGER WINDOW DEPARTED THE ROTORCRAFT, THE PILOT INITIATED A RETURN TO DEPARTURE FOR INSPECTION AND WINDOW REPLACEMENT.SDR DALA2018022601146Pan · crackedCRACKED RINGPANS (2EA) ON LT/RT WINDOW UPPER AFT CORNER OF STA 1003. (CRACK LONG 0.400") AREA WAS REPAIRED PER VOL I SRM 56-20-02 FIG 3.SDR DALA2018022601145Pan · crackedCRACK ON RINGPAN LOWER CORNER FWD STA 1156 RT SIDE. (CRACK LONG 0.385") AREA WAS REPAIRED PER VOL I SRM 56-20-02 FIG 3.SDR DALA2018022601144Pan · crackedCRACK ON RINGPAN OF WINDOW UPPER CORNER AFT STA 1135 AND LOWER CORNER FWD STA 1154 LT SIDE. (CRACK LONG 0.380") AREA WAS REPAIRED PER VOL I SRM 56-20-02 FIG 3.SDR DALA2018022601143Pan · crackedCRACK ON RINGPAN OF WINDOW UPPER CORNER AFT STA 1078 LT SIDE. (CRACK LONG 0.0405") AREA WAS REPAIRED PER VOL I SRM 56-20-02 FIG 3.SDR DALA2018022601142Pan · crackedCRACK ON RINGPAN OF WINDOW UPPER CORNER AFT STA 1116 LT SIDE. (CRACK LONG 0.380") AREA WAS REPAIRED PER VOL I SRM 56-20-02 FIG 3.SDR DALA2018022601141Pan · crackedCRACK ON RING PAN AFT UPPER CORNER STA Y=1155 RT. (CRACK LONG 0.0380") AREA WAS REPAIRED PER VOL I SRM 56-20-02 FIG 3.SDR DALA2018022601140Pan · crackedCRACK ON RING PAN FWD UPPER CORNER STA Y= 1002 AND FWD LWR STA Y= 1136 RT. (CRACK LONG 0.400") AREA WAS REPAIRED PER VOL I SRM 56-20-02 FIG 3.SDR DALA2018022601136Pan · crackedCRACK ON RING PAN FWD UPPER CORNER STA Y= 522 AND AFT LWR STA Y=943 RT. (CRACK LONG 0.380") AREA WAS REPAIRED PER VOL I SRM 56-20-02 FIG 3.SDR DALA2018022601135Pan · crackedCRACK ON RINGPAN OF WINDOW UPPER CORNER AFT STA 1097 AND LOWER CORNER FWD STA 1079 LT SIDE. AREA WAS REPAIRED PER VOL I SRM 56-20-02 FIG 3.SDR DALA2018022601134Pan · crackedCRACK ON RINGPAN UPPER CORNER AFT STA 1154 AND LOWER CORNER FWD STA 1137 LT SIDE. AREA WAS REPAIRED PER VOL I SRM 56-20-02 FIG 3.SDR AALA201802229009Window · crazedLEFT MAIN CABIN PASSENGER NR 1 WINDOW IS CRAZED. REPLACED THE WINDOW IAW AMM 56-20-00.SDR YBB2018F00000Window · crackedPILOT REPORTED THAT DURING FLIGHT, HEARD A NOISE FROM AFT OF THE ACFT. NOTICE AFT PAX NR 1 LT CABIN WINDOW CRACKED, DIVERTED NEAREST AIRPORT. UPON LANDING FOUND NR 1 LT PAX WINDOW CRACKED. SUSPECTED THAT FATIGUE, STRESS CRAZE WERE CONTRIBUTING FACTORS IN SDR AALA201801099033Window · crazedL1 CABIN WINDOW IS CRAZED. FRAMES 23-24. REPLACED THE WINDOW IAW E190 AMM 56-20-00.SDR AALA201712059021Window · scratchedAIRCRAFT IN BASE MAINTENANCE. LEFT HAND WINDOW 1 IS HAZY AND SCRATCHED. REPLACED WINDOW AND SEAL PER AMM 56-20-00.SDR AALA201711149024Window · contaminatedEXCESSIVE MOISTURE IN THE WINDOW ROW 13 RIGHT, FORWARD OVERWING EXIT. REMOVED AND REPLACED THE WINDOW IAW AMM 56-21-00. OPS CHECKED GOOD.SDR VNAA2017101199901Window · gougedRIGHT EMERGENCY EXIT WINDOW IS GOUGED OUT OF LIMITS. REMOVED AND REPLACED THE WINDOW IAW AMM 56-21-01-000-801, AND AMM 56-21-01-400-801.SDR AALA201710099048Window · damagedCRAZING & SCRATCHES ON L1 PASSENGER WINDOW BETWEEN STRINGER 9 AND 10, FRAMES 23 AND 24. REPLACED THE WINDOW IAW AMM 56-20-00. ACCOMPLISHED SATISFACTORY LEAK CHECK.SDR IXXA20170927304Window Frame · corrodedAIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. UPPER CARGO WINDOW FRAME R-19 HAS PITTED CORROSION ON LOWER SURFACE AREA. WINDOW FRAME WE REPAIRED IN ACCORDANCE WITH REA 47285REA04.SDR IXXA20170927303Window Frame · corrodedUPPER CARGO WINDOW FRAME R15 HAD CORROSION ON THE LOWER SURFACE AREA. THE WINDOW FRAME WAS REPAIRED IAW REA 47285REA04.SDR IXXA20170927300Window Frame · corrodedAIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. UPPER CARGO WINDOW FRAME R-6 HAS PITTED CORROSION ON LOWER SURFACE AREA.SDR IXXA20170921313Window Frame · corrodedAIRCRAFT GROUNDED FOR HAVY MAINTENANCE. UPPER CARGO WINDOW FRAME L-9 HAS PITTED CORROSION ON LOWER SURFACE AREA. REMOVED AND REPLACED LEFT HAND 9 CABIN WINDOW FRAME P/N 144N3250Y4 IN ACCORDANCE WITH STRUCTURAL REPAIR MANUAL 51-40-025 PARAGRAPH 7 AND DRAWING 14SDR DALA2017083006441Pan · crackedCRACKS ON RING PAN AT CAB PAX LT WINDOWS LWR CORNERS AT STA Y=656, Y= 831, Y=852 (CPAX). REPAIR WAS ACCOMPLISHED PER SRM 56-20-02-2R PROCEDURE 1.SDR DALA2017083006440Pan · crackedCRACKS ON RING PAN AT CAB PAX RT WINDOWS LWR CORNERS AT STA Y=833, Y= 581 (CPAX). REPAIR WAS ACCOMPLISHED PER SRM 56-20-02-2R PROCEDURE 1.SDR IXXA20170821302Window Frame · corrodedUPPER CARGO WINDOW FRAME R14 HAD CORROSION ON THE LOWER SURFACE AREA. REMOVED AND REPLACED THE CARGO WINDOW FRAME IAW SRM 56-20-02, TABLE 1, SRM 56-20-02, STEP 1, AND SRM 51-40-02, PARAGRAPH 4.SDR IXXA20170927301Window Frame · corrodedAIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. UPPER CARGO WINDOW FRAME R-12 HAS PITTED CORROSION ON LOWER SURFACE AREA.
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