N877AS

Service difficulty reports · 292

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 = 'N877AS' 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 SWIA202264854None · corrodedRH PRESSURE FLOOR SILL PANEL FROM FS 484.00 TO FS 529.00 IS CORRODED IN MULTIPLE LOCATIONS. (C CHECK RO 3/11/2022) REPAIRED R/H PRESSURE FLOOR SILL I.A.W. BOMBARDIER REO 601R-53-41-666 REV.C, DATED 2012-11-06, MHIRJ REO 601R-53-41-3008 REV.--, DATED 2022-Jan 4, 2022 · N877AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202264853None · corrodedRH PRESSURE FLOOR SILL PANEL FROM FS 449.00 TO FS 484.00 IS CORRODED IN MULTIPLE LOCATIONS. (C CHECK RO 3/11/2022) REPAIRED R/H PRESSURE FLOOR SILL I.A.W. BOMBARDIER REO 601R-53-41-666 REV.C, DATED 2012-11-06, MHIRJ REO 601R-53-41-3016 EV.--, DATED 2022-0Jan 4, 2022 · N877AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202264851None · corrodedRH PRESSURE FLOOR SILL PANEL FROM FS 409.00+112 TO FS 449.00 IS CORRODED IN MULTIPLE LOCATIONS. (C CHECK RO 3/11/2022) REPAIRED R/H PRESSURE FLOOR SILL I.A.W. BOMBARDIER REO 601R-53-41-666 REV.C, DATED 2012-11-06 AND MHIRJ REO 601R-53-41-3016 REV.--, DATEJan 4, 2022 · N877AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202264850None · corrodedRH PRESSURE FLOOR SILL ANGLE FROM FS 529.00 TO FS 559.00 IS CORRODED IN MULTIPLE LOCATIONS. (C CHECK RO 3/11/2022) REPAIRED CORROSION ON THE RH PRESSURE FLOOR SILL ANGLE FROM FS 529.00 TO FS 559.00 IAW BOMBARDIER REO 601R-53-41-666 REV.C, DATED 2012-11-0Jan 4, 2022 · N877AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202264849None · corrodedRH PRESSURE FLOOR SILL ANGLE FROM FS 484.00 TO FS 529.00 IS CORRODED IN MULTIPLE LOCATIONS. (C CHECK RO 3/11/2022) REPAIRED DAMAGED RH FLOOR SILL ANGLE BETWEEN FS 499-513, FS 524 AND FS 529 IAW REO 601R-53-41-666 REV C DATED 2012-11-06 AND INSTALLED ALTERJan 4, 2022 · N877AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202264847None · corrodedRH PRESSURE FLOOR SILL ANGLE FROM FS 449.85 TO FS 484.00 IS CORRODED IN MULTIPLE LOCATIONS. (C CHECK RO 3/11/2022) REPAIRED CORROSION DAMAGE AT FS 449,461 AND 473 IAW REO 601R-53-41-666 REV C DATED 2012-11-06 AND INSTALLED ALTERNATE FASTENERS AT INACCESSAJan 4, 2022 · N877AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202264845None · corrodedLH PRESSURE FLOOR SILL PANEL FROM FS 529.00 TO FS 559.00 IS CORRODED IN MULTIPLE LOCATIONS. (C CHECK RO 3/11/2022) REPAIRED L/H PRESSURE FLOOR SILL I.A..W. BOMBARDIER REO 601R-53-41-666 REV.C, DATED 2012/11/06 AND MHIRJ REO 601R-53-41-3012 REV.--, DATED 20Jan 4, 2022 · N877AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202264843None · corrodedRH PRESSURE FLOOR SILL ANGLE FROM FS 409.00+112 TO FS449.85 IS CORRODED IN MULTIPLE LOCATIONS. (C CHECK RO 3/11/2022) REPAIRED R/H PRESSURE FLOOR SILL ANGLE IAW BOMBARDIER REO 601R-53-41-666, REV -C DATED2012-11-06 AND MHIRJ REO 601R-53-41-3016, REV -- DAJan 4, 2022 · N877AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202264841None · corrodedLH PRESSURE FLOOR SILL PANEL FROM FS 449.85 TO FS 484.00 IS CORRODED IN MULTIPLE LOCATIONS. (C CHECK RO 3/11/2022) REPAIRED CORROSION ON LH PRESSURE FLOOR SILL PANEL FROM F.S. 449.85 - 484.00 IAW REO 601R-53-41-666 REV C DATED 2012-11-06 AND REO 601R-53-41Jan 4, 2022 · N877AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202264839None · corrodedLH PRESSURE FLOOR SILL PANEL FROM FS 409.00+112 TO FS 449.85 IS CORRODED IN MULTIPLE LOCATIONS. (C CHECK RO 3/11/2022) REPAIRED L/H PRESSURE FLOOR SILL I.A.W. BOMBARDIER REO 601R-53-41-666 REV.C, DATED 2012-11-06, MHIRJ REO 601R-53-41-3010 REV.--, DATED 20Jan 4, 2022 · N877AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202164933None · corrodedLH SIDE SEAT TRACK FROM FS 544.00 TO FS 559.00+80 IS CORRODED. (C CHECK RO 3/11/2022) REMOVED AND REPLACED LH SIDE SEAT TRACK F.S. 544 - 559+80 IAW CRJ-200 AMM 53-01-11-000/400-802. REF ATTACHED CONTINUATION FOR WORK PEFORMED.Dec 31, 2021 · N877AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202164932None · corrodedLH SIDE SEAT TRACK FROM FS 499.00 TO FS 544.00 IS CORRODED. (C CHECK RO 3/11/2022) REMOVED AND REPLACED LH SIDE SEAT TRACK F.S. 499.00 - 544.00 IAW CRJ-200 AMM 53-01-11-00/400-802. REF ATTACHED CONTINUATION FOR WORK PERFORMED.Dec 31, 2021 · N877AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202164931None · corrodedLH SIDE SEAT TRACK FROM FS 449.85 TO FS499.00 IS CORRODED. (C CHECK RO 3/11/2022) REMOVED DAMAGED SIDE SEAT TRACK AT FS 449.85 TO 499.00 AND INSTALLED A NEW SEAT TRACK IAW CRJ 200AMM 53-01-11-000/400-802Dec 31, 2021 · N877AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202164930None · corrodedLH SIDE SEAT TRACK FROM FS 409.00+112 TO FS 449.85 IS CORRODED. (C CHECK RO 3/11/2022) LH SIDE SEAT TRACK FROM FS 409.00+112 TO FS 449.85 WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW CRJ 200 AMM 53-01-11-000/400-802Dec 31, 2021 · N877AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202164928None · corrodedLH SIDE SEAT TRACK FROM FS 409.00+16 TO FS 409.00+112 IS CORRODED. (C CHECK RO 3/11/2022) REMOVED DAMAGED SEATTRACK AND INSTALLED A NEW SERVICABLE SEAT TRACK IAW CRJ 200 AMM 53-01-11-400-802Dec 31, 2021 · N877AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202164923None · corrodedLH SIDE SEAT TRACK FROM FS 364.00 TO FS 409.00+16 IS CORRODED. (C CHECK RO 3/11/2022) REMOVED AND REPLACED WITH SERVICEABLE LH SIDE SEAT TRACK RAIL FROM FS 364.00 TO FS 409.00+16 IAW CRJ 200 AMM 53-01-11-000-802 AND 53-01-11-400-802Dec 31, 2021 · N877AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202164922None · corrodedRH SIDE TRACK FROM FS 544.00 TO FS 559.00+80 IS CORRODED (C CHECK RO 3/11/2022) REMOVED AND REPLACED WITH SERVICEABLE RH SIDE SEAT TRACK RAIL FROM FS 544.00 TO FS 559.00+80 IAW CRJ 200 AMM 53-01-11-000-802, 53-01-11-400-802 AND SRM 51-40-11Dec 31, 2021 · N877AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202164921None · corrodedRH SIDE TRACK FROM FS 499.00 TO FS 544.00 IS CORRODED (C CHECK RO 3/11/2022) REMOVED AND REPLACED RH SIDE TRACK FROM FS 499.00 TO FS 544.00 IAW CRJ 200 AMM 53-01-11-000-802, 53-01-11-400-802 AND SRM 51-40-11Dec 31, 2021 · N877AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202164920None · corrodedRH SIDE TRACK FROM FS 449.85 TO499.00 IS CORRODED (C CHECK RO 3/11/2022) REMOVED AND REPLACED R/H SIDE SEAT RAIL F.S. 449.85 TO 499 IAW CRJ200 AMM 53-01-11-000--802 AND 53-01-11-400-802Dec 31, 2021 · N877AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202164911None · corrodedRH SIDE TRACK FROM FS 409.00+122 TO FS 449.85 IS CORRODED (C CHECK RO 3/11/2022) REMOVED AND REPLACED R/H SIDE SEAT RAIL AT F.S. 409+122 TO 449.85 IAW CRJ200 AMM 53-01-11-000-802 AND 53-01-11-400-802Dec 31, 2021 · N877AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202164910None · corrodedRH SIDE TRACK FROM FS 409.00+16 TO 409.00+112 IS CORRODED (C CHECK RO 3/11/2022) REMOVED AND INSTALLED SERVICEABLE SEAT TRACK RAIL IAW CRJ 200 AMM 53-01-11-000-802 AND53-01-11-400-802Dec 31, 2021 · N877AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202164909None · corrodedRH SIDE TRACK FROM FS 364.00 TO 409.00+16 IS CORRODED (C CHECK RO 3/11/2022) REMOVED AND REPLACED RH SIDE SEAT TRACK F.S. 364.00 - 409+16 IAW CRJ-200 AMM 53-01-11-000/400-802. REF ATTACHED CONTINUATION FOR WORK PERFORMED.Dec 31, 2021 · N877AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202164838None · corrodedFRAME CORRODED AT FS 333.00 BETWEEN STGR 25L AND STGR 25R. (C CHECK RO 3/11/2022) REMOVED AND REPLACED FS 333.00 BETWEEN STRINGER 23L AND 23R IAW CRJ700 SRM 51-42-06 AND 51-42-21. MAJOR REPAIR TASK CARD 51-900-1003-SKY AND FORM 337 COMPLETED AND ATTACHED.Dec 21, 2021 · N877AS · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202164836None · corrodedFRAME CORRODED AT FS 319.70 BETWEEN STGR 24L AND STGR 24R. (C CHECK RO 3/11/2022) REMOVED AND REPLACED FRAME SEGMENT AT F.S. 319.70 BETWEEN STRINGER 24L AND STRINGER 24R I.A.W. BOMBARDIER CRJ200 SRM 51-42-06 AND 51-42-21 REV.38B, DATED 11/25/2020. SKYWEST Dec 21, 2021 · N877AS · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202164975None · dentedRH EMERGENCY EXIT CUTTOUT FRAME HAS 6 DENTED STOP FITTING PADS. (C CHECK RO 3/11/2022) REMOVED AND REPLACED RH EMERGENCY EXIT DOOR STOP PADS IAW CRJ-200 AMM 52-21-00-000/400-803. REF ATTACHED CONTINUATION FOR WORK PERFORMED.Dec 19, 2021 · N877AS · Cndair CL6002B19 · DoorsSDR SWIA202164974None · dentedLH EMERGENCY EXIT CUTTOUT FRAME HAS 6 DENTED STOP FITTING PADS. (C CHECK RO 3/11/2022) REMOVED AND REPLACED LH EMERGENCY EXIT DOOR STOP PADS IAW CRJ-200 AMM 52-21-00-000/400-803. REF ATTACHED CONTINUATION FOR WORK PERFORMED.Dec 19, 2021 · N877AS · Cndair CL6002B19 · DoorsSDR SWIA202164965None · corrodedJ ANGLE FLOOR BOARD ATTACHING PLATE ON FRAM AT FS. 409.00 IS CORRODED (C CHECK RO 3/11/2022) REMOVED AND REPLACED AVIONICS BAY FLOOR BOARD SUPPORT J-ANGLE AT F.S. 409.00 IAW CRJ-200 SRM 51-42-21 AND 51-42-06. REF ATTACHED CONTINUATION FOR WORK PERFORMED.Dec 18, 2021 · N877AS · Cndair CL6002B19 · Fuselage Structure (General)SDR SWIA202164964None · corrodedR/H FLOOR SILL CORRODED ON LOWER SIDE AROUND RIVET BUCKTAIL AT FS 620.00 (C CHECK RO 3/11/2022) REMOVED AND INSTALLED R/H FLOOR SILL FROM FS 563 - 621 IAW GENERIC REO 601R-53-61-5376, REV-A, DATED 2018-10-25 AND DEVIATION REO'S 601R-53-61-7798, REV --, DADec 18, 2021 · N877AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202164963None · corrodedSTRAP SECURING DIAPHRAGM AT FS 621.00 BULKHEAD BETWEEN LBL 9.0 AND RBL 9.0 IS CORRODED. (C CHECK RO 3/11/2022) REMOVED AND REPLACED STRAP SECURING DIAPHRAGM AT FS 621.00 BULKHEAD BETWEEN LBL 9.0 AND RBL 9.0 WITH NEW SERVICABLE PART IAW CRJ 200 AMM 53-61-17Dec 18, 2021 · N877AS · Cndair CL6002B19 · Fuselage, Door HingeSDR SWIA202164908None · corrodedBOTH GUSSET PLATES CONNECTING FWD INTERCOSTALS TO MAIN AVIONICS BAY DOOR SURROUND STRUCTURE ARE CORRODED (C CHECK RO 3/11/2022) REMOVED AND REPLACED TWO (2) GUSSET PLATES (P/NS: 601R31049-55) FWD OF AVIONIC BAY DOOR IAW CRJ-200 SRM 51-42-21Dec 18, 2021 · N877AS · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA202164907None · corrodedCARGO SEAT TRACK SEGMENT RBL 9.0 FS 559+110 TO FS 574.00 IS CORRODED (C CHECK RO 3/11/2022) REMOVED DAMAGED SEAT TRACK AND INSTALLED A NEW SEAT TRACK IAW CRJ 200 AMM 53-00-49-000/400-801Dec 18, 2021 · N877AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202164906None · corrodedCARGO SEAT TRACK SEGMENT RBL 9.0 FS 559+80 TO 559+96 IS CORRODED (C CHECK RO 3/11/2022) REMOVED AND REPLACED CARGO SEAT TRACK RBL 9 F.S. 559+80 - 559+96 IAW CRJ-200 AMM 53-01-11-000/400-802.Dec 18, 2021 · N877AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202164905None · corrodedCARGO SEAT TRACK SEGMENT FS 617.00 TO FS 612.00 LBL 9.0 IS CORRODED (C CHECK RO 3/11/2022) REMOVED AND REPLACED CARGO SEAT TRACK SEGMENT F.S. 617.00 - 612.00 LBL 9 IAW CRJ-200 AMM 53-00-49-000/400-801. REF ATTACHED CONTINUATION WOR WORK PERFORMED.Dec 18, 2021 · N877AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202164834None · corrodedTWO CENTER INTERCOSTALS AFT OF MAIN AVIONICS BAY DOOR SURROUND FRAME FS.394.00 ARE CORRODED. (C CHECK RO 3/11/2022) REMOVED AND REPLACED TWO CENTER INTERCOSTALS AFT OF MAIN AVIONICS BAY DOOR SURROUND FRAME FS.394.00 IAW CRJ 200 SRM 51-42-21, SRM 51-42-06, Dec 18, 2021 · N877AS · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA202164832None · corroded3 INTERCOSTALS BETWEEN FS. 349.0 AND MAIN AVIONICS DOOR STRUCTURE ARE CORRODED. (C CHECK RO 3/11/2022) REMOVED AND REPLACED 3 INTERCOSTALS BETWEEN FS. 349.0 AND MAIN AVIONICS DOOR STRUCTURE IAW CRJ 200 SRM 51-42-06, 51-42-01 REV 38B DATE 11/25/2020, SKYCARDec 18, 2021 · N877AS · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA202164831None · corrodedFRAME SECTOR FS 589.00 CORRODED BETWEEN STR 16R AND 20R (C CHECK RO 3/11/2022) REMOVED AND REPLACED FRAME SECTOR AT F.S. 589.00 I.A.W. MHIRJ REO 601R-53-61-7787, REV--, DATED 2022-01-19. COMPLETED SKYWEST TASK CARD 51-900-1003-SKY FOR MAJOR REPAIR. NO CHANDec 18, 2021 · N877AS · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202164962None · crackedLH WING BATT RIB AT WS 48.30 CRACKED IN TWO LOCATIONS. (C CHECK RO 3/11/2022) REMOVED AND REPLACED L/H WING BATT RIB AT WS 48.30 IAW CRJ 200 SRM 51-40--11 AND 51-42-21. REF CONTINUATION CARD FOR WORK PERFORMED.Dec 14, 2021 · N877AS · Cndair CL6002B19 · Wing, Rib/BulkheadSDR SWIA202164830None · crackedLH WING BATT RIB AT WS 53.60 CRACKED. (C CHECK RO 3/11/2022) REPAIRD L/H WING BATT RIB AT WS 53.60 IAW BOMBARDIER REO 601R-57-51-046 REV B DATED 2002-02-28. REFCONTINUATION CARD FOR WORK PERFORMED.Dec 14, 2021 · N877AS · Cndair CL6002B19 · Wing, Rib/BulkheadSDR SWIA202164829None · cracked2 EA CRACKS FOUND ON RH BATT RIB WS 48.30 (C CHECK RO 3/11/2022) REMOVED AND REPLACED RIB AT RH WS 48.30 IAW CRJ-200 SRM 51-40-11 AND 51-42-21. REF ATTACHED CONTINUATION FOR WORK PERFORMED.Dec 13, 2021 · N877AS · Cndair CL6002B19 · Wing, Rib/BulkheadSDR SWIA202164828None · damagedFS409+129 VERTICAL POST AT BL0 HAS AN INDICATION .2" BY 80% FSH ON THE RIGHT SIDE VERTICAL FLANGE AFT RADIUS AT WL69. FAILED NDT INSPECTION. (C CHECK RO 3/11/2022) REMOVED AND REPLACED VERTICAL POST AT BL0 AND FS 409.+128 IAW REO 601R-53-41-889 REV D. DADec 12, 2021 · N877AS · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202164827None · corrodedL/H AND R/H FUSELAGE SKIN IS CORRODED AROUND SCREW HOLES FOR PANELS 191BB AND 192BB (FWD WING TO FUSELAGE FAIRINGS). (C CHECK RO 3/11/2022) REPAIRED CORROSION AT L/H AND R/H FUSELAGE SKIN AROUND SCREW HOLES FOR PANELS 191BB AND 192BB IAW MHIRJ REO 601R-53Dec 10, 2021 · N877AS · Cndair CL6002B19 · Fuselage Structure (General)SDR SWIA202164826None · crackedL/H SIDE FWD AVI BAY FLOOR AT F.S. 193.0 IS CRACKED. (C CHECK RO 3/11/2022) REPAIRED LH SIDE FWD AVI BAY FLOOR CRACK AT F.S. 193 IAW BOMBARDIER REO 601R-53-11-081 REV NC DATED 03-07-97. REF ATTACHED CONTINUATION FOR WORK PERFORMED. COMPLETED TASK CARD 51Dec 10, 2021 · N877AS · Cndair CL6002B19 · Fuselage Structure (General)SDR SWIA202164961None · corrodedLH WING SPOILERON HINGE HARDWARE AND KEEPER HARDWARE IS CORRODED. (C CHECK RO 3/11/2022) REMOVED AND REPLACED LH SPOILERON HINGE AND KEEPER HARDWARE AS NEEDED IAW CRJ-200 AMM 27-64-01-000/400-801. REF ATTACHED CONTINUATION FOR WORK PERFORMED.Dec 6, 2021 · N877AS · Cndair CL6002B19 · Wing StructureSDR SWIA202164960None · corrodedLH WING FLIGHT SPOILER HINGE HARDWARE AND KEEPER HARDWARE IS CORRODED. (C CHECK RO 3/11/2022) REMOVED AND REPLACED LH FLIGHT SPOILER HINGE AND KEEPER HARDWARE AS NEEDED IAW CRJ-200 AMM 27-64-05-000/400-801. REF ATTACHED CONTINUATION FOR WORK PERFORMED.Dec 6, 2021 · N877AS · Cndair CL6002B19 · Wing StructureSDR SWIA202164958None · corrodedLH WING IB GROUND SPOILER HINGE HARDWARE AND KEEPER HARDWARE IS CORRODED. (C CHECK RO 3/11/2022) INSTALLED NEW HARDWARE ON LH WING IB GROUND SPOILER IAW CRJ 200 AMM 27-65-01-400-801Dec 6, 2021 · N877AS · Cndair CL6002B19 · Wing StructureSDR SWIA202164956None · corrodedLH WING OB GROUND SPOILER HINGE HARDWARE AND KEEPER HARDWARE IS CORRODED. (C CHECK RO 3/11/2022) REMOVED AND REPLACED LH OB GROUND SPOILER HINGE AND KEEPER HARDWARE IAW CRJ-200 AMM 27-65-01-000/400-801. REF ATTACHED CONTINUATION FOR WORK PERFORMED.Dec 6, 2021 · N877AS · Cndair CL6002B19 · Wing StructureSDR SWIA202164955None · corrodedRH WING IB GROUND SPOILER HINGE HARDWARE AND KEEPER HARDWARE IS CORRODED. (C CHECK RO 3/11/2022) REMOVED AND REPLACED RH IB GROUND SPOILER HINGE AND KEEPER HARDWARE IAW CRJ-200 AMM 27-65-01-000/400-801. REF ATTACHED CONTINUATION FOR WORK PERFORMED.Dec 6, 2021 · N877AS · Cndair CL6002B19 · Wing StructureSDR SWIA202164954None · corrodedRH WING OB GROUND SPOILER HINGE HARDWARE AND KEEPER HARDWARE IS CORRODED. (C CHECK RO 3/11/2022) INSTALLED SERVICEABLE HARDWARE IAW CRJ 27-65-01-400-801. REFERENCE CAMP #23963983 FOR OPS CHECKS.Dec 6, 2021 · N877AS · Cndair CL6002B19 · Wing StructureSDR SWIA202164953None · corrodedRH WING FLIGHT SPOILER HINGE HARDWARE AND KEEPER HARDWARE IS CORRODED. (C CHECK RO 3/11/2022) REMOVED AND REPLACED RH FLIGHT SPOILER HINGE AND KEEPER HARDWARE IAW CRJ-200 AMM 27-64-05-000/400-801. REF ATTACHED CONTINUATION FOR WORK PERFORMED.Dec 6, 2021 · N877AS · Cndair CL6002B19 · Wing StructureSDR SWIA202164951None · corrodedRH WING SPOILERON HINGE HARDWARE AND KEEPER PLATE HARDWARE IS CORRODED. (C CHECK RO 3/11/2022) REMOVE AND REPLACED CORRODED HARDWARE ON RH SPOILERON HINGE AND KEEPER PLATE IAW CRJ-200 AMM 27-64-01-00/400-801.Dec 6, 2021 · N877AS · Cndair CL6002B19 · Wing Structure
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