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.

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 51-42-21-00Aug 16, 2021 · N856AS · Cndair CL6002B19 · Fuselage Structure (General)SDR 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 Aug 16, 2021 · N856AS · Cndair CL6002B19 · Fuselage Structure (General)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 TAAug 16, 2021 · N856AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR 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 2021-10-07Aug 16, 2021 · N856AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR 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 REAug 16, 2021 · N856AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR 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 DAAug 16, 2021 · N856AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR 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. COAug 15, 2021 · N856AS · Cndair CL6002B19 · Fuselage Main, KeelSDR 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 DISCONNECTEDAug 14, 2021 · N856AS · Cndair CL6002B19 · Aileron TabsSDR 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 27-64-05-000/400-801Aug 14, 2021 · N856AS · Cndair CL6002B19 · Wing StructureSDR 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.Aug 14, 2021 · N856AS · Cndair CL6002B19 · Wing StructureSDR 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 OTAug 14, 2021 · N856AS · Cndair CL6002B19 · Wing StructureSDR 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.Aug 14, 2021 · N856AS · Cndair CL6002B19 · AileronsSDR 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.Aug 14, 2021 · N856AS · Cndair CL6002B19 · AileronsSDR 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 BOTAug 14, 2021 · N856AS · Cndair CL6002B19 · Wing StructureSDR 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 51-40-11Aug 14, 2021 · N856AS · Cndair CL6002B19 · Aileron TabsSDR 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. COMPLETEAug 14, 2021 · N856AS · Cndair CL6002B19 · Fuselage Structure (General)SDR 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 Aug 14, 2021 · N856AS · Cndair CL6002B19 · Fuselage Structure (General)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 -- DAAug 14, 2021 · N856AS · Cndair CL6002B19 · Fuselage Structure (General)SDR 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 TESTAug 13, 2021 · N856AS · Cndair CL6002B19 · Flight Control SystemSDR 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 20-21-00-910-801Aug 13, 2021 · N856AS · Cndair CL6002B19 · Horizontal Stabilizer, Spar/RibSDR 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 51-42-22Aug 13, 2021 · N856AS · Cndair CL6002B19 · Horizontal Stabilizer, Plate/SkinSDR 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-Aug 11, 2021 · N856AS · Cndair CL6002B19 · Fuselage Main, KeelSDR 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.Aug 10, 2021 · N856AS · Cndair CL6002B19 · AileronsSDR 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 53-01-05-400-801Aug 9, 2021 · N856AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR 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 1Aug 9, 2021 · N856AS · Cndair CL6002B19 · AileronsSDR 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 51-42-13Aug 9, 2021 · N856AS · Cndair CL6002B19 · AileronsSDR 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 51-42-13Aug 9, 2021 · N856AS · Cndair CL6002B19 · AileronsSDR 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 51-42-13Aug 9, 2021 · N856AS · Cndair CL6002B19 · AileronsSDR 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 51-42-13Aug 9, 2021 · N856AS · Cndair CL6002B19 · AileronsSDR 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 CONTINUAug 9, 2021 · N856AS · Cndair CL6002B19 · Aileron TabsSDR 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 CHANAug 6, 2021 · N856AS · Cndair CL6002B19 · Fuselage Structure (General)SDR 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."Mar 30, 2021 · N856AS · Cndair CL6002B19 · Fuselage Main, StructureSDR 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 CFeb 2, 2021 · N856AS · Cndair CL6002B19 · Flight Compartment WindowsSDR 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.Dec 14, 2020 · N856AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR 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 Dec 8, 2020 · N856AS · Cndair CL6002B19 · Wing StructureSDR 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 Dec 8, 2020 · N856AS · Cndair CL6002B19 · Wing StructureSDR 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 PERMANENJul 5, 2020 · N856AS · Cndair CL6002B19 · Cargo/Baggage DoorsSDR SWIA201844229Skin · corrodedWING PLANK HOLE IS CORRODED. REPAIRED WING PLANK IAW REO.Jan 27, 2018 · N856AS · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA201844228Floor Skin · damagedPRESSURE FLOOR SKIN DAMAGED. REPAIRED PRESSURE FLOOR SKIN IAW REO.Jan 25, 2018 · N856AS · Cndair CL6002B19 · Fuselage Floor PanelSDR SWIA201844235Skin · damagedFUSELAGE SKIN DAMAGED. REPAIRED DAMAGE IAW REO.Jan 23, 2018 · N856AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA201844215Frame · corrodedFRAME IS CORRODED. R & R THE FRAME IAW SRM.Jan 23, 2018 · N856AS · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA201844239Skin · damagedFUSELAGE SKIN DAMAGED. REPAIRED FUSELAGE SKIN IAW REO.Jan 16, 2018 · N856AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA201844238Skin · damagedFUSELAGE SKIN DAMAGED. REPAIRED FUSELAGE SKIN IAW REO.Jan 16, 2018 · N856AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA201844231Angle · damagedCAP ANGLE DAMAGED. REPAIRED CAP ANGLE IAW REO.Jan 13, 2018 · N856AS · Cndair CL6002B19 · Fuselage Structure (General)SDR SWIA201844227Bulkhead · crackedPRESSURE BULKHEAD HAS MULTIPLE CRACK INDICATIONS. THE REPAIRED BULKHEAD IAW REO.Jan 13, 2018 · N856AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA201844226Bulkhead · crackedPRESSURE BULKHEAD CRACKED. REPAIRED BULKHEAD IAW REO.Jan 13, 2018 · N856AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA201844225Intercostal · corrodedPAX DOOR INTERCOSTAL CORRODED. REPAIRED THE INTERCOSTAL IAW SRM.Jan 11, 2018 · N856AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA201844224Intercostal · corrodedPAX DOOR INTERCOSTAL CORRODED. REPAIRED THE INTERCOSTAL IAW SRM.Jan 11, 2018 · N856AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA201844223Door Frame · crackedPAX DOOR FRAME CRACKED. . REPAIRED THE DOOR FRAME IAW REO.Jan 11, 2018 · N856AS · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA201844222Door Frame · crackedPAX DOOR FRAME CRACKED. REPAIRED THE DOOR FRAME IAW REO.Jan 11, 2018 · N856AS · Cndair CL6002B19 · Fuselage Main, Structure
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