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 SWIA202162615None · corrodedLBL27 FLOOR SEAT TRACK FS559+78 - FS559+96 SEGMENT IS CORRODED. (C-CHECK- RO 11/11/21) INSTALLED NEW SERVICABLE FLOOR TRACK IAW CRJ200 AMM 53-01-11-400-802Aug 20, 2021 · N856AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202162614None · corrodedRBL9 FLOOR SEAT TRACK FS559+86 - FS559+96 SEGMENT IS CORRODED. (C-CHECK- RO 11/11/21) INSTALLED NEW SERVICABLE FLOOR TRACK IAW CRJ200 AMM 53-01-11-400-802Aug 20, 2021 · N856AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202162613None · corrodedLBL9 FLOOR SEAT TRACK FS559+86 - FS559+96 SEGMENT IS CORRODED. (C-CHECK- RO 11/11/21) REMOVED AND REPLACED LBL9 SEAT TRACK FROM FS559+86 - FS559+96 IAW CRJ 200 AMM 53-01-11-000/400-802 REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMEDAug 20, 2021 · N856AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202162612Seat Track · corrodedRBL9 FLOOR SEAT TRACK FS559+5 - FS559+86 SEGMENT IS CORRODED. (C-CHECK- RO 11/11/21) REMOVED AND REPLACED RBL9 SEAT TRACK FS559+5 - FS559+86 SEAT TRACK SEGMENT IAW CRJ 200 AMM 53-01-11-000/400-802 REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMEAug 20, 2021 · N856AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202162611None · corrodedLBL9 FLOOR SEAT TRACK FS559+5 -- 559+86 SEGMENT IS CORRODED. (C-CHECK- RO 11/11/21) REMOVED AND REPLACED SEAT TRACK SEGMENT AT LBL 9 FS 559+5 - FS 559+86 IAW CRJ 200 AMM 53-01-11-400-802Aug 20, 2021 · N856AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202162572None · corrodedSERVICE DOOR SILL ANGLE IS CORRODED FS 319.00 TO FS 349.00 (C-CHECK- RO 11/11/21) REMOVED AND REPLACED SVC DOOR SILL ANGLE IAW CRJ 200 SRM 51-42-06 AND 51-42-21. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE NOTEDAug 20, 2021 · N856AS · Cndair CL6002B19 · DoorsSDR SWIA2021111562571Cup · corrodedPAX DOOR HANDRAIL CUPS ARE CORRODED (C-CHECK- RO 11/11/21) REMOVED AND REPLACED PAX DOOR HAND RAIL CUPS IAW CRJ 200 SRM 51-42-06. COMPLETED MAJOR REPAIR TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE NOTED.Aug 20, 2021 · N856AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA202162570None · corrodedPAX DOOR SILL ANGLE CORRODED (C-CHECK- RO 11/11/21) REMOVED AND REPLACE CORRODED ANGLE (LOWER SILL ANGLE) IAW CRJ-200-SRM 51-42-06, 51-42-13, 51-42-21, 51-40-11, 51-25-00. PERFORMED OP TEST OF DOOR WARNING SYSTEM JIAW CRJ-200-AMM 52-70-04-710-801, OP TESTAug 20, 2021 · N856AS · Cndair CL6002B19 · DoorsSDR SWIA202162569None · corrodedSERVICE DOOR LOWER FWD PAN AND SPLICE PLATE ARE CORRODED (C-CHECK- RO 11/11/21) REMOVED AND REPLACED SVC DOOR LOWER FWD AND SPLICE PLATE IAW CRJ 200 SRM 51-42-06, 51-42-21, AND SNIEO 601R38304 S06. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETEAug 20, 2021 · N856AS · Cndair CL6002B19 · Galley DoorsSDR SWIA202162568Seal · corrodedL/H EMERGENCY EXIT DOOR FWD AND AFT LOWER INTERNAL CORNERS OF DOOR STRUCTURE IS CORRODED (C-CHECK- RO 11/11/21) REMOVED AND REPLACED L/H EMERGENCY EXIT FORWARD AND AFT LOWER INTERNAL BRACKETS I.A.W. BOMBARDIER CRJ 200 SRM 51-42-11 AND 51-42-21. COMPLETED TAug 20, 2021 · N856AS · Cndair CL6002B19 · Fuselage Structure (General)SDR SWIA202162640None · corrodedLH SPOILERON HAS CORRODED HARDWARE ON ALL FOUR HINGES. (C-CHECK- RO 11/11/21) REPLACED L'H SPOILERON CORRODED HARDWARE AT ALL 4 HINGES WITH SERVICEABLE HARDWARE IAW CRJ 200 AMM 27-64-01- 400-801 STEP2B (1) THRU (4). OPA TEST OF FLIGHT SPOILER GOOD IAW CAug 19, 2021 · N856AS · Cndair CL6002B19 · Wing StructureSDR SWIA202162639None · corrodedALL LH SPOILERON HINGE BOLT KEEPERS HAVE CORRODED HARDWARE. (C-CHECK- RO 11/11/21) REPLACED AND INSTALLED NEW HARDWARE ON LH SPOILERON HINGE BOLT KEEPERS IAW CRJ 200 AMM 27-64-01-400-801 STEP 2.C(1)-(3)Aug 19, 2021 · N856AS · Cndair CL6002B19 · Wing StructureSDR SWIA202162638None · corrodedLH SPOILERON OB PCU WING ATTACH POINT NUTS ARE CORRODED. (C-CHECK- RO 11/11/21) REPLACED LH SPOILERON OB PCU WING ATTACH NUTS AND IB PCU LOWER MOUNT BOLT ANTI ROTATION PLATE BOLTS AND TEFLON WASHER IAW CRJ-200 AMM 27-62-01-000/400-801 AND 27-64-01-000/400Aug 19, 2021 · N856AS · Cndair CL6002B19 · Wing StructureSDR SWIA202162637None · corrodedLH SPOILERON IB PCU WING ATTACH POINT NUTS ARE CORRODED. (C-CHECK- RO 11/11/21) INSTALLED NEW HARDWARE ON L/H SPOILERON I/B PCU TO WING ATTACHING POINT IAW CRJ 200 AMM 27-62-01-400-801 STEP 2.B(4)-(7). REPLACED CORRODED SPOILERON HINGE NUT BEHIND IB PCU Aug 19, 2021 · N856AS · Cndair CL6002B19 · Wing StructureSDR SWIA202162636None · corrodedLH FLIGHT SPOILER IB PCU IB WING ATTACHING HARDWARE IS CORRODED (C-CHECK- RO 11/11/21) REPLACED L/H FLIGHT SPOILER I/B PCU HARDWARE AND WING ATTACH HARDWARE AS REQUIRED IAW CRJ 200 AMM 27-62-01-400-801. FUNCTIONAL TEST OF SECU'S GOOD IAW CRJ 200 AMM 27-64Aug 19, 2021 · N856AS · Cndair CL6002B19 · Wing StructureSDR SWIA202162635None · corrodedALL LH FLIGHT SPOILER HINGE NUTS ARE CORRODED. (C-CHECK- RO 11/11/21) REMOVED AND REPLACED ALL LH FLIGHT SPOILER HINGE NUTS IAW CRJ-200 AMM 27-64-05-000/400-801. OPS TEST OF FLIGHT SPOILER GOOD IAW CRJ 200 AMM 27-64-00-710-801. REFERENCE ATTACHED CONTINUEAug 19, 2021 · N856AS · Cndair CL6002B19 · Wing StructureSDR SWIA202162634None · corrodedALL LH FLIGHT SPOILER HINGE BOLT KEEPERS HAVE CORRODED HARDWARE. (C-CHECK- RO 11/11/21) REPLACED LH FLIGHT SPOILER BOLT RETENTION ANGLE HARDWARE IAW CRJ 200 AMM 27-64-05-400-801Aug 19, 2021 · N856AS · Cndair CL6002B19 · Wing StructureSDR SWIA202162633None · corrodedLH IB GRND SPOILER HAS CORRODED HARDWARE AT ALL HINGE POINTS. (C-CHECK- RO 11/11/21) REMOVED AND REPLACED LH GROUND SPOILER HINGE HARDWARE IAW CRJ-200 AMM 27-65-01-000/400-801.Aug 19, 2021 · N856AS · Cndair CL6002B19 · Wing StructureSDR SWIA202162632None · corrodedLH OB GRND SPOILER PCU LINK HARDWARE IS CORRODED. (C-CHECK- RO 11/11/21) REMOVED OLD LH OB GROUND SPOILER PCU LINK HARDWARE IAW CRJ-200 AMM 27-65-01-000-801 AND INSTALLED NEW HARDWARE IAW CRJ-200 AMM 27-65-01-400-801.Aug 19, 2021 · N856AS · Cndair CL6002B19 · Wing StructureSDR SWIA202162631None · corrodedLH OB GRND SPOILER PCU WING ATTACHING HARDWARE IS CORRODED. (C-CHECK- RO 11/11/21) REMOVED OLD HARDWARE ON LH OB GROUND SPOILER PCU WING HINGE IAW CRJ-200 AMM 27-65-01-000-801 AND INSTALLED NEW HARDWARE IAW CRJ-200 AMM 27-65-01-400-801.Aug 19, 2021 · N856AS · Cndair CL6002B19 · Wing StructureSDR SWIA202162630None · corrodedRH FLOOR SILL FS409+73 -- FS409+128 SEGMENT IS CORRODED. (C-CHECK- RO 11/11/21) REMOVED AND REPLACED R/H FLOOR SILL AT F.S 409+73 TO F.S 409+128 IAW REO 601R-53-31-1203 REV -- DATED 2021-09-20 AND SRM 51-42-06 AND 51-42-21.Aug 19, 2021 · N856AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202162629None · corrodedLH IB GRND SPOILER PCU LINK UPPER NUT IS CORRODED. (C-CHECK- RO 11/11/21) REMOVED AND REPLACED LH INBOARD GROUND SPOILER PCU LINK UPPER NUT WITH NEW SERVICEABLE HARDWARE IAW CRJ-200 AMM 27-65-01-000/400-801.Aug 19, 2021 · N856AS · Cndair CL6002B19 · Wing StructureSDR SWIA202162610None · corrodedLH FLOOR SILL IS CORRODED BETWEEN FS559 AND FS621. (C-CHECK- RO 11/11/21) UPON FURTHER INVESTIGATION FOUND CORROSION TO BE BETWEEN FS 559 AND FS 559+86. REMOVED AND REPLACED LH FLOOR SILL FROM FS 559 TO FS 559+86 IAW CRJ 200 SRM 51-42-06 AND 51-42-21.Aug 19, 2021 · N856AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202162609None · crackedINTERCOSTAL CLIP ANGLE AT FS484 ON OB SIDE OF LBL9 FLOOR BEAM IS CRACKED. (C-CHECK- RO 11/11/21) REMOVED AND REPLACED INTERCOSTAL CLIP ANGLE PN: 601R31171-27 AT FS484 ON OB SIDE OF LBL9 IAW CRJ-200 SRM 51-42-06 AND 51-42-21Aug 19, 2021 · N856AS · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA202162608None · crackedINTERCOSTAL CLIP ANGLE AT FS484 ON OB SIDE OF LBL27 FLOOR BEAM IS CRACKED. (C-CHECK- RO 11/11/21) REMOVED AND REPLACED CRACKED INTERCOSTAL CLIP ANGLE WITH NEW AT FS 484 ON OB SIDE OF LBL FLOOR BEAM IAW CRJ 200 BOMBARDIER REO 601R-53-41-059 REV -C DATED 202Aug 19, 2021 · N856AS · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA202162606None · corrodedRBL9 FS399 --FS409+128 FLOOR SEAT TRACK SEGMENT IS CORRODED. (C-CHECK- RO 11/11/21) REPLACED FLOOR SEAT TRACK AT RBL9 BETWEEN FS399 AND FS409+128 IAW CRJ200 AMM 53-01-11-000/400-802.Aug 19, 2021 · N856AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202162604None · corrodedLBL9 FS399 -- FS409+128 FLOOR SEAT TRACK SEGMENT IS CORRODED. (C-CHECK- RO 11/11/21) REMOVED AND REPLACED SEAT TRACK SEGMENT AT LBL 9 FS 399 - FS 409+128 IAW CRJ 200 AMM 53-01-11-400-802Aug 19, 2021 · N856AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202162567None · corrodedRH FLOOR SILL FS409+5 -- FS409+73 SEGMENT IS CORRODED. (C-CHECK- RO 11/11/21) REPAIRED RH FLOOR SILL BETWEEN F.S. 409+5 - 409+73 IAW MHIRJ REO 601R-53-31-1206 REV - - DATED 2021-10-06. COMPLETED TASK CARD 51-900-1003-SKY AND FORM M-337. NO WEIGHT CHANGE NAug 19, 2021 · N856AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA2021111562566Door Sill · corrodedRH FLOOR SILL IS CORRODED BETWEEN FS409 AND FS409+5. (C-CHECK- RO 11/11/21) REMOVED AND REPLACED RH FLOOR SILL IAW CRJ 200 SRM 51-42-06, 51-42-21, REO 601R-53-21-3500 REV -- DATED 2021-9-14 AND REO 601R-53-21-3501 REV -- DATED 2021-09-24. COMPLETED MAJOR RAug 19, 2021 · N856AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202162565None · corrodedRBL9 FLOORBEAM IS CORRODED BETWEEN FS409+5 AND FS409+119. (C-CHECK- RO 11/11/21) REMOVED RBL 9 FLOOR BEAM CAP BETWEEN F.S. 409.00 + 5 - F.S. 409.00 + 119 AND INSTALLED NEW SERVICEABLE BEAM CAP IAW CRJ-200 SRM 51-42-06, 51-42-21 AND MHIRJ REO 601R-53-51-5Aug 19, 2021 · N856AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202162564None · corrodedLBL9 FLOORBEAM IS CORRODED BETWEEN FS409+5 AND FS409+119 (C-CHECK- RO 11/11/21) REMOVED CORRODED LBL9 FLOORBEAM BETWEEN FS409+5 AND FS409+119 , FABRICATED AND INSTALLED NEW BEAM FROM EXTRUSION P/N N126-1707 IAW REO 601R-53-31-1210 REV - - DATED 2021-10-2Aug 19, 2021 · N856AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202162563None · corrodedLH FLOOR SILL FS409+73 -- FS409+128 SEGMENT IS CORRODED. (C-CHECK- RO 11/11/21) REMOVED AND REPLACED LH FLOOR SILL FS409+73- FS409+128 IAW CRJ200 SRM 51-42-06 ANF 51-42-21, COMPLIED WITH MHIRJ REO 601R-53-31-1204 REV - - DATED 2021-09-21. REF ATTACHED CONAug 19, 2021 · N856AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202162605None · corrodedSEAT TRACK SEGMENT RBL 9 IS CORRODED BETWEEN F.S.409+128 TO F.S.559 (C-CHECK- RO 11/11/21) REMOVED AND REPLACED SEAT TRACK SEGMENT FS 409+128 TO FS 559 IAW CRJ 200 AMM 53-01-11-400-802.Aug 18, 2021 · N856AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202162603None · corrodedSTRAP IS CORRODED BETWEEN FLOOR BEAM BL0 TO RBL9 AT F.S.559 (C-CHECK- RO 11/11/21) REMOVED CORROSION ON STRAP AT FS 559 BETWEEN BL0 TO RBL9 ORIGINAL MAT'L THK .050 REMAINING MAT'L THK .047 MAT'L LOSS .003 IS IN LIMITS IAW CRJ 200 SRM 51-21-06, AND 53-00-0Aug 18, 2021 · N856AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202162602None · corrodedSEAT TRACK SEGMENT IS CORRODED AT LBL 9 BETWEEN F.S.409+128 TO F.S.559 (C-CHECK- RO 11/11/21) REMOVED AND REPLACED SEAT TRACK SEGMENT AT LBL 9 FS 409+128 - FS 559 IAW CRJ 200 AMM 53-01-11-400-802Aug 18, 2021 · N856AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202162562None · corrodedFLOOR BEAM RBL 9 UPPER CAP IS CORRODED AT MULTIPLE LOCATIONS BETWEEN F.S.409+128 TO F.S.559 (C-CHECK- RO 11/11/21) REMOVED AND REPLACED FLOOR BEAM CAP AT FS 409+128 - FS 559 AT RBL 9 IAW REO 601R-53-41-2953 REV -- DATED 2021-08-24 & REO 601R-53-00-027 REV Aug 18, 2021 · N856AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202162561None · corrodedFLOOR BEAM LBL9 UPPER CAP IS CORRODED BETWEEN F.S. 409+128 TO F.S. 559 (C-CHECK- RO 11/11/21) REMOVED AND REPLACED FLOOR BEAM CAP AT LBL 9 FS 409+128 - FS 599 IAW REO 601R-53-41-2952 REV -- DATED 8/24/21, REO 601R-53-00-005 REV B DATED 2011-01-06, 601R-53Aug 18, 2021 · N856AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202162628None · corrodedL/H SIDE SEAT TRACK IS CORRODED BETWEEN F.S. 409.0+112 TO F.S. 461.0 (C-CHECK- RO 11/11/21) REMOVED L/H SIDE SEAT TRACK IS CORRODED BETWEEN F.S. 409.0+112 TO F.S.449.85 . INSTALLED NEW FABRICATED SEAT TRACK IAW CRJ 200 AMM 53-01-11-400-802. REFERENCE CAMP Aug 17, 2021 · N856AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202162601None · corrodedLBL9 FLOOR SEAT TRACK IS CORRODED BETWEEN F.S. 364 TO F.S. 394 (C-CHECK- RO 11/11/21) INSTALLED NEW SERVICABLE FLOOR TRACK IAW CRJ200 AMM 53-01-11-400-802Aug 17, 2021 · N856AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202162600None · corrodedF.S. 280 ANGLE IS CORRODED BETWEEN LBL9 AND RBL9. (C-CHECK- RO 11/11/21) REMOVED CORROSION ON FS 280 ANGLE BETWEEN LBL9 AND RBL 9 IAW CRJ 200 SRM 51-21-06.Aug 17, 2021 · N856AS · Cndair CL6002B19 · Fuselage Structure (General)SDR SWIA202162599None · crackedF.S. 280 RBL 9 INBOARD AND OUTBOARD CLIPS ARE CRACKED. (C-CHECK- RO 11/11/21) REMOVED DAMAGED CLIPS ON I/B AND O/B SIDE OF RBL9 AT FS 280 AND FABRICATED, AND INSTALLED NEW SERVICEABLE CLIPS FROM MATERIAL S6144-14 REFERENCED FROM RE0# 601R-53-11-171, REV DAug 17, 2021 · N856AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202162598None · corrodedF.S. 280 J ANGLE IS CORRODED. (C-CHECK- RO 11/11/21) REMOVED AND TREATED CORROSION ON FS 280 J ANGLE IAW: CRJ200-SRM-51-21-06, AND FOUND TO BE WITHIN LIMITS IAW: CRJ200-SRM-53-00-00. REF CONTINUE CARD FOR DETAILS OF WORK PERFORMED.Aug 17, 2021 · N856AS · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA202162597None · corrodedR/H SIDE SEAT TRACK IS CORRODED BETWEEN F.S. 484 TO F.S. 544. (C-CHECK- RO 11/11/21) REMOVED AND REPLACED RH SIDE SEAT TRACK BETWEEN FS 484 TO FS 554 IAW CRJ 200 AMM 53-01-11-000/400-802 REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMEDAug 17, 2021 · N856AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202162596None · corrodedL/H SIDE SEAT TRACK IS CORRODED AT F.S. 473. (C-CHECK- RO 11/11/21) REMOVED CORRODED SIDE SEAT TRACK AT F.S. 449.85 - F.S. 500.00 AND INSTALLED NEW SERVICEABLE SIDE SET TRACK IAW CRJ-200 SRM CRJ-200 AMM 53-01-11-000/400-802. REF ATTACHED CONTINUATION FOR AAug 17, 2021 · N856AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202162595None · corrodedL/H SIDE SEAT TRACK IS CORRODED BETWEEN F.S. 499 TO F.S. 544. (C-CHECK- RO 11/11/21) REMOVED AND REPLACED DAMAGED SEAT TRACK IAW CRJ200 AMM 53-01-11-000/400-802Aug 17, 2021 · N856AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202162594None · corrodedL/H SIDE SEAT TRACK IS CORRODED BETWEEN F.S. 544 TO F.S. 559.0+80. (C-CHECK- RO 11/11/21) REMOVED AND REPLACED DAMAGED SEAT TRACK IAW CRJ200 AMM 53-01-11-000/400-802Aug 17, 2021 · N856AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202162593None · corrodedR/H SIDE SEAT TRACK IS CORRODED BETWEEN F.S. 409.0+112 TO F.S. 449.85. (C-CHECK- RO 11/11/21) REMOVED AND REPLACED R/H SIDE SEAT TRACK IS CORRODED BETWEEN F.S. 409.0+112 TO F.S. 449.85, IAW CRJ-200 AMM 53-01-11-000/400-802, SEE CONTINUATION CARD FOR DETAILAug 17, 2021 · N856AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202162592Rail · gougedR/H SIDE SEAT TRACK IS GOUGED BETWEEN F.S. 409.0+16 TO F.S. 409.0+31. (C-CHECK- RO 11/11/21) REMOVED CORRODED SIDE SEAT TRACK F.S. 409.00+16 - F.S. 409.00+112 AND INSTALLED NEW SERVICEABLE SIDE SEAT TRACK IAW CRJ-200 AMM 53-01-11-000/400-802.Aug 17, 2021 · N856AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202162591None · corrodedR/H SIDE SEAT TRACK IS CORRODED BETWEEN F.S. 364 TO F.S. 409.0+16. (C-CHECK- RO 11/11/21) REMOVED CORRODED CABIN SIDE SET TRACK F.S. 364.00 - 409.00+16 AND INSTALLED NEW SERVICEABLE TRACK IAW CRJ-200 AMM 53-01-11-000/400-802.Aug 17, 2021 · N856AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202162627None · corrodedFLOOR TENSION STRAP CORRODED AT FS559 BETWEEN LBL45 AND LBL27. (C-CHECK- RO 11/11/21) REMOVED AND REPLACED CORRODED TENSION STRAP IAW CRJ200 SRM 51-42-06Aug 16, 2021 · N856AS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
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