N856AS
Service difficulty reports · 339
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. 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 n_number = 'N856AS' AND registry_match = 'registration' 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 n_number = 'N856AS' AND registry_match = 'registration' 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 SWIA202162590Bracket · crackedRH AND LH UPPER OBLEAK ANGLES ON FS.621.00 BULKHEAD AT STR. 14L AND 14R ARE CRACKED. (C-CHECK- RO 11/11/21) REMOVED AND REPLACED RH AND LH UPPER OBLEAK ANGLES ON FS.621.00 BULKHEAD AT STR. 14L AND 14R IAW CRJ 200 SRM 51-42-21-00SDR SWIA202162560None · dentedEXTERNAL FUSELAGE SKIN HAS SEVERAL DENTS/PRTRUDING DENTS FROM FS 574 TO FS 621, BETWEEN STR 27 AND STR 21L. (C-CHECK- RO 11/11/21) REPAIRED DAMAGE AT FS 574- FS 621 STR 27- STR 21L IAW REO 601R-53-61-7711 REV -- DATED 2021-10-08, REO 601R-53-61-7712 REV L SDR SWIA202162559None · corrodedLEFT FLOOR SILL FROM FS409+128 TO FS559 IS CORRODED IN NUMEROUS AREAS. (C-CHECK- RO 11/11/21) REMOVED LH FLOOR SILL CORROSION FROM FS 409+128 - FS 559 IAW REO 601R-53-41-666 REV C DATED 2012-11-06, REO 601R-53-41-2963 REV -- DATED 2021-10-06. COMPLETED TASDR SWIA202162558None · corrodedRIGHT FLOOR SILL ANGLE FROM FS409+128 TO FS559 IS CORRODED IN NUMEROUS AREAS. (C-CHECK- RO 11/11/21) REMOVED DAMAGE FROM RH FLOOR SILL ANGLE FROM FS 409+128 - FS 559 IAW REO 601R-53-41-666 REV C DATED 2012-11-06, REO 601R-53-41-2959 REV -- DATED 2021-10-07SDR SWIA202162557None · corrodedLEFT FLOOR SILL FROM FS409+128 TO FS559 IS CORRODED IN NUMEROUS AREAS. (C-CHECK- RO 11/11/21) DISCREPANCY SHOULD READ RH FLOOR SILL FROM FS 409+128 TO FS 559 IS CORRODED. REMOVED CORROSION FROM RH FLOOR SILL AT FS 409+128 - FS 559 IAW REO 601R-53-41-666 RESDR SWIA202162556None · corrodedLEFT FLOOR SILL ANGLE FROM FS409+128 TO FS559 IS CORRODED IN NUMEROUS AREAS. (C-CHECK- RO 11/11/21) REMOVED DAMAGE FROM LH FLOOR SILL ANGLE FROM FS 409+128 - FS 559 AND REOAIRED IAW REO 601R-53-41-2963 REV A DATED 2021-10-07 AND REO 601R-53-41-666 REV C DASDR SWIA202162555None · corrodedFWD SIDE OF RIB AT FS.310.00 IS CORRODED BETWEEN STR. 25L AND 25R. (C-CHECK- RO 11/11/21) UPON FURTHER INVESTIGATION FOUND CORROSION TO BE AT FS 319. REMOVED AND REPLACED FRAME SEGMENT AT FS 319 AT STR 25L AND 25R IAW CRJ 200 SRM 51-42-06 AND 51-42-21. COSDR SWIA202162651None · corrodedL/H FLAP OUTBD. BPSU (4 EA.MOUNT BOLTS) RUSTED (C-CHECK- RO 11/11/21) REPLACED AND INSTALLED NEW HARDWARE ON LH FLAP O/B PBSU IAW CRJ 200 AMM 27-51-10-400-801 STEPS 3.B.(4), (6)-(7). REPLACED ONE AT A TIME AND NO ELECTRICAL CONNECTIONS WERE DISCONNECTEDSDR SWIA202162626None · corrodedR/H FLIGHT SPOILER OTBD HINGE NUT AND RETAINING PLATE BOLTS, AND INBD AND OTBD BONDING JUMPER HARDWARE IS CORRODED. (C-CHECK- RO 11/11/21) REMOVED AND REPLACED CORRODED HARDWARE IAW CRJ 200 AMM 27-64-05-000/400-801SDR SWIA202162625None · corrodedR/H SPOILERON INBD HINGE NUT AND RETAINING PLATE BOLTS ARE CORRODED (C-CHECK- RO 11/11/21) REMOVED AND REPLACED RH SPOILERON IB HINGE NUT AND RETAINING PLATE HARDWARE IAW CRJ-200 AMM 27-64-01-000/400-801. REF ATTACHED CONTINUATION FOR WORK PERFORMED.SDR SWIA202162624None · corrodedR/H SPOILERON OTBD CENTER HINGE NUT, ALL LOWER ATTACH HARDWARE FOR INBD AND OTBD ACUATORS, INBD AND OTBD CENTER HINGE RETAINER PLATE SCREWS, AND ATTACHING SCREWS FOR BONDING JUMPERS ARE CORRODED. (C-CHECK- RO 11/11/21) REMOVED AND REPLACED R/H SPOILERON OTSDR SWIA202162623None · corroded#4 R/H FLAP ACTUATOR FWD ATTACH NUT IS CORRODED (C-CHECK- RO 11/11/21) RECIEVED IN A SERVICEABLE FWD ATTACHMENT NUT REFERENCE MX TRANS# 21955104 WVAC JOB 97404125 OP 5527 FOR REMOVAL AND REPLACEMENT.SDR SWIA202162622None · corrodedR/H FLAP BPSU MOUNTING BOLTS ARE CORRODED (C-CHECK- RO 11/11/21) REPLACED AND INSTALLED NEW HARDWARE ON RH FLAP BPSU IAW CRJ 200 AMM 27-51-10-400-801 STEPS 3.B.(4), (6)-(7). REPLACED ONE AT A TIME AND NO ELECTRICAL CONNECTORS WERE DISCONNECTED.SDR SWIA202162621None · corrodedR/H AILERON INBOARD AFT PCU LINK ATTACH NUT, INBOARD CENTER HINGE NUT, AND ATTACHING HARWARE FOR BOTH BONDING JUMPERS ARE CORRODED (C-CHECK- RO 11/11/21) R/H AILERON INBOARD AFT PCU LINK ATTACH NUT, INBOARD CENTER HINGE NUT, AND ATTACHING HARWARE FOR BOTSDR SWIA202162589None · chafedL/H AILERON UPPER L/E SKIN SHROUD DEEPLY CHAFFED ACROSS ENTIRE LENGTH (C-CHECK- RO 11/11/21) REMOVED, LOCATED, DRILLED, AND INSTALLED NEW L/H AILERON LEADING EDGE SHROUD IAW CRJ 200 SRM 51-42-06 AND 51-40-11SDR SWIA202162554None · corrodedCORROSION ON LOWER FUSELAGE SKIN AROUND DRAIN HOLES AND FASTENERS FS 559+94 TO FS 559+112 AT STR 27. (C-CHECK- RO 11/11/21) REPAIRED LOWER FUSELAGE SKIN AT STGR27 BETWEEN FS559+94 AND FS559+112 IAW MHIRJ REO 601R-53-51-600 REV-- DATED 2021-09-03. COMPLETESDR SWIA202162553None · corrodedCORROSION ON LOWER FUSELAGE SKIN FS 559+80 BETWEEN STR 26L AND 26R (C-CHECK- RO 11/11/21) REPAIRED LOWER FUSELAGE SKIN AT FS559+80 BETWEEN STGR26L & 26R IAW MHIRJ REO 601R-53-51-600 REV-- DATED 2021-09-03. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED SDR SWIA202162552None · corrodedCORROSION ON SKIN PANEL AND AROUND FASTENER HEADS AROUND LAV SERVICING POINT FS 559+80 TO FS 559+112 BETWEEN STR 21R AND 24R. (C-CHECK- RO 11/11/21) REMOVED CORROSION FROM SKIN AT FS 559+80 - FS 559+112 AT STR 21R - STR 24R IAW REO 601R-53-61-597 REV -- DASDR SWIA202162650None · corrodedBOTH INBD. AND OUTBD. L/H ELEV. FLUTTER DAMPERS , ROD END HARDWARE (2 EA. NUTS AND WASHERS RUSTED) (C-CHECK- RO 11/11/21) REMOVED AND REPLACED LH IB OB FLUTTER DAMPER AFT HARDWARE IAW CRJ200 AMM 27-34-05-400-801 REFERENCE MX TRANS FOR INSTALL AND OPS TESTSDR SWIA202162620None · corrodedHORIZONTAL STAB.TOP CANTED RIB ( FWD. STEADY FITTING) L/H LOWER HARDWAREWARE NUTS CORRODED IN THE MILLED POCKET (C-CHECK- RO 11/11/21) REMOVED AND REPLACED CORRODED HARDWARE IAW CRJ 200 AMM 20-21-00-910-801SDR SWIA202162619None · corrodedHORIZONTAL STAB. BATHTUB FITTINGS (16 TOTAL JOLL BOLTS CORRODED) (C-CHECK- RO 11/11/21) REMOVED AND REPLACED CORRODED JO-BOLTS IN BATHTUB FITTINGS IAW CRJ 200 SRM 51-42-22SDR SWIA202162551Stiffener · damagedFUSELAGE FS409+128 LBL18 INBD VERTICAL POST HAS AN INDICATION .2" LONG BY 50% FSH IN THE AFT RADIUS AT WL69. FAILED NDT INSPECTION. (C-CHECK- RO 11/11/21) REMOVED AND REPLACED VERTICAL POST ASSY AT FS 409+128 LBL 18 WITH NEW IAW CRJ 200 SRM 51-42-02, 51-SDR SWIA202162550None · damagedR/H I/B FLAP PANEL 684CB HAS DRILL DAMAGE AROUND FASTENER HOLE, AND STRUCTURE UNDER PANEL ON I/B FLAP. (C-CHECK- RO 11/11/21) COMPLIED WITH REO 601R-27-52-2435 REV -- DATED 2021-09-10 REPAIRED R/H I/B FLAP PANEL 684CB AND UNDERLYING STRUCTURE ON I/B FLAP.SDR SWIA202162588None · wornPILOTS FLIGHT COMPARTMENT FLOOR SEAT RAILS HAVE EXCESSIVE WEAR (C-CHECK- RO 11/11/21) REMOVED AND REPLACED PILOT SEAT TRACKS IAW CRJ 200 AMM 53-01-05-400-801SDR SWIA202162587None · chafedR/H I/B FLAP VANE CHAFFED AT W/S 139.924 (C-CHECK- RO 11/11/21) FOUND DAMAGE TO BE OUT OF LIMITS OF REO 601R-57-52-004 REV D, DATED 2012-12-19 AND REQUIRES REPLACEMENT. REMOVED AND REPLACED R/H I/B FLAP VANE L/E SKIN AND END CAP RIB AT WS 139.924 AND WS 1SDR SWIA202162586None · chafedR/H I/B FLAP VANE CHAFFED AT W/S 56.30 (C-CHECK- RO 11/11/21) REMOVED AND REPLACED WITH NEW R/H INBRD L/E FLAP VANE SKIN IAW CRJ 200 SRM 51-40-11 AND 51-42-13SDR SWIA202162585None · chafedL/H I/B FLAP VANE CHAFFED AT W/S 139.924 (C-CHECK- RO 11/11/21) REPLACED CHAFED CAP LH I/B FLAP VANE AT W/S 139.924 IAW CRJ 200 SRM 51-42-13SDR SWIA202162584None · chafedL/H I/B FLAP VANE CHAFFED AT W/S 104.099 (C-CHECK- RO 11/11/21) REPLACED CHAFED CAP AT LH I/B FLAP VANE AT W/S 104.099 IAW CRJ 200 SRM 51-42-13SDR SWIA202162583None · damagedL/H I/B FLAP VANE CHAFFED AT W/S 56.30 (C-CHECK- RO 11/11/21) REPLACED CHAFED CAP ON THE LH I/B FLAP VANE AT W/S 56.30 IAW CRJ 200 SRM 51-42-13SDR SWIA202162549None · chafedR/H I/B FLAP VANE CHAFFED AT W/S 104.099 (C-CHECK- RO 11/11/21) REMOVED AND REPLACED WITH NEW R/H INBOARD FLAP VANE CAP AT WS 104.099 IAW CRJ 200 SRM 51-40-11,51-42-13, & SKYCARD 51-900-1003-SKY NO WEIGHT CHANGE, FORM 337 IS ATTACHED, REF ATTACHED CONTINUSDR SWIA202162548None · dentedSMALL DENT JUST FWD OF PAX DOOR JUST BELOW GOLD STRIPE (C-CHECK- RO 11/11/21) REPAIRED DENT AT FS 280 BETWEEN STR 18L AND 17L IAW REO 601R-53-21-3498 REV -- DATED 9/12/21. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANSDR SWIA202157106Windshield · crackedCA SIDE WINDSHIELD CRACKED IN FLIGHT (FLIGHT 5106 . THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 22550210 WITH THE FOLLOWING CORRECTIVE ACTION: "REMOVED AND REPLACED CAPTAIN SIDE WINSHIELD PER TASK CARD 56-220-1000-SKY."SDR SWIA202155935Windshield · crackedON DECENT OUT OF FL250 FIRST OFFICER SIDE WINDSCREEN STARTED TO CRACK AND PROPAGATE. LARGE CRACK ALMOST FULL LENGTH OF WINDSCREEN. FLIGHT 1365 - FILED CLOSED REMOVED AND REPLACED THE RH WINDSHIELD IAW CRJ 200 AMM 56-11-01 AND TASK CARD 56-220-1000-SKY CSDR SWIA202062547None · damagedCOMPLY WITH REO 601R-53-41-1116 REPAIR & REINFORCEMENT FOR FS 559.00 LWR CAP ANGLES BL 9.00 & 18.00 LHS & RHS (C-CHECK- RO 11/11/21) COMPLIED WITH REO 601R-53-41-1116 REV. C DATED 2017-03-09 REPAIR & REINFORCEMENT FOR FS 559.00 LWR CAP ANGLES BL 9.00 & 18.SDR SWIA202062546Bushing · damagedREMOVE AND REPLACE BUSHINGS AND HARDWARE ON RH AILERON WING AFT SPAR REF CRJ 200 AMM 20-26-00-910-804 (C-CHECK- RO 11/11/21) REMOVED AND REPLACED BUSHINGS AND HARDWARE ON RH AILERON WING AFT SPAR IAW CRJ-200 AMM 20-26-00-910-803 AND REO 601R-57-51-015 REV SDR SWIA202062545Bushing · damagedREMOVE AND REPLACE BUSHINGS AND HARDWARE ON LH AILERON WING AFT SPAR REF CRJ 200 AMM 20-26-00-910-804 (C-CHECK- RO 11/11/21) REMOVED AND REPLACED BUSHINGS AND HARDWARE ON LH AILERON WING AFT SPAR IAW CRJ-200 AMM 20-26-00-910-803 AND REO 601R-57-51-015 REV SDR SWIA2020070751288Track · damagedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA - CARGO DOOR AFT TRACK DAMAGED WHERE LOWER ROLLER RIDES WHEN DOOR IS OPEN. C/W TEMPORARY REPAIR PER REO. PERMANENT REPAIR DUE WITHIN 600 FH BY 41542.9 TAT., THIS HAS BEEN DETERMINED TO BE A MAJOR REPAIR, A PERMANENSDR SWIA201844229Skin · corrodedWING PLANK HOLE IS CORRODED. REPAIRED WING PLANK IAW REO.SDR SWIA201844228Floor Skin · damagedPRESSURE FLOOR SKIN DAMAGED. REPAIRED PRESSURE FLOOR SKIN IAW REO.SDR SWIA201844235Skin · damagedFUSELAGE SKIN DAMAGED. REPAIRED DAMAGE IAW REO.SDR SWIA201844215Frame · corrodedFRAME IS CORRODED. R & R THE FRAME IAW SRM.SDR SWIA201844239Skin · damagedFUSELAGE SKIN DAMAGED. REPAIRED FUSELAGE SKIN IAW REO.SDR SWIA201844238Skin · damagedFUSELAGE SKIN DAMAGED. REPAIRED FUSELAGE SKIN IAW REO.SDR SWIA201844231Angle · damagedCAP ANGLE DAMAGED. REPAIRED CAP ANGLE IAW REO.SDR SWIA201844227Bulkhead · crackedPRESSURE BULKHEAD HAS MULTIPLE CRACK INDICATIONS. THE REPAIRED BULKHEAD IAW REO.SDR SWIA201844226Bulkhead · crackedPRESSURE BULKHEAD CRACKED. REPAIRED BULKHEAD IAW REO.SDR SWIA201844225Intercostal · corrodedPAX DOOR INTERCOSTAL CORRODED. REPAIRED THE INTERCOSTAL IAW SRM.SDR SWIA201844224Intercostal · corrodedPAX DOOR INTERCOSTAL CORRODED. REPAIRED THE INTERCOSTAL IAW SRM.SDR SWIA201844223Door Frame · crackedPAX DOOR FRAME CRACKED. . REPAIRED THE DOOR FRAME IAW REO.SDR SWIA201844222Door Frame · crackedPAX DOOR FRAME CRACKED. REPAIRED THE DOOR FRAME IAW REO.
Back to N856AS