N875AS

Service difficulty reports · 256

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 = 'N875AS' 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 SWIA202265441None · overheatedWING OVHT WARNING MESSAGE IN CLIMB, FOLLOW QRH, MESSAGE DIDN€™T CLEAR. / FA REPORTS CABIN SMELLS LIKE RUBBER BURNING. (FLIGHT 5735 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 24708232 WITH THE FOLLOWING CORRECTIVE ACTION: "FOR RUBBER Apr 22, 2022 · N875AS · Cndair CL6002B19 · Ice/Rain Protection SystemSDR SWIA202265201None · crackedRH BEAM INTERCOSTAL FOUND CRACKED ON RBL9 AND BETWEEN FS559.00+64 - FS559.00+80. (C-CHECK RO 3-25-22) REMOVED AND REPLACED RH BEAM INTERCOSTAL P/N 601R31117-35 AT RBL9 AND BETWEEN FS559.00+64-FS559.00+80 WITH A NEW IDENTICAL UNIT IAW CRJ200 SRM 51-42-06 AFeb 10, 2022 · N875AS · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA202265200None · nicked* FOUND TWO NICKS ON THE LH TRUNNION OF THE HSTA ATTACH FITTINGS.(AREA MARKED) (C-CHECK RO 3-25-22) BLENDED DAMAGES ON LH TRUNNION OF THE HSTA ATTACH FITTINGS REF CRJ200 SRM 51-12-00. WITHIN LIMITS, RECEIVED AND COMPLIED WITH ALL STEPS OF REO 601R-55-31-3Feb 8, 2022 · N875AS · Cndair CL6002B19 · Stabilizer Position IndicatingSDR SWIA202265211None · damagedCANN FLIGHT OBSERVERS LOWER SEAT RAIL P/N: 15981-1 FOR USE ON N929SW / SN: 7703. (C-CHECK RO 3-25-22) REMOVED AND REPLACED FLIGHT OBSERVER LOWER SEAT RAIL P/N 15981-1 REF CRJ 200 AMM 25-12-01-400-801Feb 2, 2022 · N875AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202265199None · corrodedCORROSION FOUND UNDERNEATH GIRT BAR FITTINGS AT SERVICE DOOR LOWER THRESHOLD FS319.70 TO FS349.00 STR17R (C-CHECK RO 3-25-22) REMOVED LOWER THESHOLD ANGLE REF CRJ 200 SRM 51-42-06 AND 51-42-36, INSTALLED LOWER THESHOLD ANGLE REF CRJ 200 SRM 51-42-06, REF Feb 1, 2022 · N875AS · Cndair CL6002B19 · Fuselage Internal StairsSDR SWIA202265198None · corrodedR/H ELEVATOR FITTING LOCATED @ BL15.25 NEEDS TO BE REPLACED DUE TO CORROSION IN THE BEARING BORE. (C-CHECK RO 3-25-22) REMOVED AND REPLACED R/H ELAVATOR FITTING ASSY( BEARING INCLUDED ) @ ES 15-25 P/N 600-24043-1 REF CRJ 200 SRM 51-42-06 AND CRJ 200 DWGJan 31, 2022 · N875AS · Cndair CL6002B19 · Elevator Tab, Attach FittingsSDR SWIA202265197None · damagedDEFECTS NOTED IN THE RH LWR WING PLANK FWD & AFT ATTACHMENT HOLES FOR THE RH WING DRAIN LOCATED BETWEEN WS0.00 + THE RH BOOST PUMP AND BETWEEN STR5 - STR7. (C-CHECK RO 3-25-22) REPAIRED DEFECTS IN THE RH LWR WING PLANK FWD & AFT ATTACHMENT HOLES FOR THE RJan 30, 2022 · N875AS · Cndair CL6002B19 · Wing, Center BoxSDR SWIA202265196None · damagedDEFECTS NOTED IN THE LH LWR WING PLANK FWD & AFT ATTACHMENT HOLES FOR THE LH WING DRAIN LOCATED BETWEEN WS0.00 + THE LH BOOST PUMP AND BETWEEN STR5 - STR7. (C-CHECK RO 3-25-22) REPAIRED DEFECTS IN THE LH LWR WING PLANK FWD & AFT ATTACHMENT HOLES FOR THE LJan 30, 2022 · N875AS · Cndair CL6002B19 · Wing, Center BoxSDR SWIA202265195None · corrodedBRACKET COMMON TO PAX DOOR INTERCOSTAL DD6 FOUND CORRODED. (C-CHECK RO 3-25-22) REMOVED AND REPLACED PAX DOOR BRACKET P/N 601R8084-2 WITH A SERVICEABLE UNIT IAW CRJ200 SRM 51-42-06 REVISION 38: JUL 10/2019 AND BOMBARDIER DRAWING 601R31702 REV. -N. COMPLIEJan 26, 2022 · N875AS · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA202265194None · gouged* THE RH WING AILERON HINGE FITTING WING SIDE #4 HINGE KEEPER BOLT HOLE ON OUTBD SIDE IS GOUGED. (MARKED) (C-CHECK RO 3-25-22) REMOVED DAMAGE ON RH WING AILERON HINGE FITTING WING SIDE #4 HINGE REF CRJ200 SRM 51-12-00. FOUND OUT OF LIMITS. RECEIVED AND CJan 22, 2022 · N875AS · Cndair CL6002B19 · Wing StructureSDR SWIA202265193None · chafed* THE RH WING AILERON HINGE FITTING WING SIDE #3 HINGE IS CHAFFED IN 2EA LOCATIONS. (MARKED) (C-CHECK RO 3-25-22) REMOVED DAMAGES ON RH WING AILERON HINGE FITTING WING SIDE #3 HINGE REF CRJ200 SRM 51-12-00. FOUND TO BE OUT OF LIMITS. RECEIVED AND COMPLIEJan 22, 2022 · N875AS · Cndair CL6002B19 · Wing StructureSDR SWIA202265192None · gouged* THE LH WING AILERON HINGE FITTING WING SIDE #3 HINGE INBD LUG IS GOUGED. (MARKED) (C-CHECK RO 3-25-22) REMOVED DAMAGE ON LH WING AILERON HINGE FITTING WING SIDE #3 HINGE REF CRJ200 SRM 51-12-00. FOUND TO BE WITHIN LIMITS. REF REO 601R-57-51-989 REV--,Jan 22, 2022 · N875AS · Cndair CL6002B19 · Wing StructureSDR SWIA202265232None · corroded*THE RH INBD GROUND HINGES HAS CORRODED HARDWARE. (C-CHECK RO 3-25-22) REMOVED AND REPLACED CORRODED CASTLE NUTS, WASHERS AND COTTER PINS ON R/H INBOARD GROUND SPOILER HINGE ATTACHMENT OUTBOARD AND INBOARD HINGE IAW CRJ200 27-65-01-400-801 STEPS 2.B.(9)Jan 21, 2022 · N875AS · Cndair CL6002B19 · Wing StructureSDR SWIA202265231None · corroded*THE RH INBD GROUND PCU HAS CORRODED HARDWARE. (C-CHECK RO 3-25-22) REMOVED AND REPLACED R/H INBOARD GROUND SPOILER PCU ATTACHMENT HARDWARE AND REPLACED WITH NEW IAW CRJ200 AMM 27-63-01-400-801 STEPS 2.B.(2)Jan 21, 2022 · N875AS · Cndair CL6002B19 · Wing StructureSDR SWIA202265230None · corroded*THE RH OUTBD GROUND HINGES HAS CORRODED HARDWARE. (C-CHECK RO 3-25-22) R/H OUTBOARD GROUND SPOILER HINGE ATTACHMENT CASTLE NUT, WASHER AND COTTER PIN REMOVED FROM INBOARD AND OUTBOARD HINGE AND REPLACED WITH NEW IAW CRJ200 AMM 27-65-01-400-801 STEPS 2.BJan 21, 2022 · N875AS · Cndair CL6002B19 · Wing StructureSDR SWIA202265229None · corroded*THE RH FLIGHT SPOILER HINGES HAS CORRODED HARDWARE. (C-CHECK RO 3-25-22) R/H FLIGHT SPOILER HARDWARE FOR HINGE ATTACHMENT REMOVED AND REPLACED WITH NEW IAW CRJ200 AMM 27-64-05-400-801 STEPS 2.B. / CAL TOOLS USED: TUC5658 DUE 6/30/22, TUC4822 DUE 6/30/22Jan 21, 2022 · N875AS · Cndair CL6002B19 · Flight Control SystemSDR SWIA202265228None · corroded*THE RH FLIGHT SPOILER PCU'S HAS CORRODED HARDWARE. (C-CHECK RO 3-25-22) R/H FLIGHT SPOILER PCU LOWER ATTACHMENT HARDWARE REMOVED AND REPLACED WITH NEW IAW CRJ200 AMM 27-62-01-400-801 STEPS 2. A THROUGH B / CAL TOOLS USED: TUC5658 DUE 6/30/22, TUC4822 DUJan 21, 2022 · N875AS · Cndair CL6002B19 · Flight Control SystemSDR SWIA202265227None · corrodedTHE RH SPOILERON HINGES'S HAS CORRODED HARDWARE. (C-CHECK RO 3-25-22) R/H SPOILERON HINGE ATTACHMENT HARDWARE REMOVED AND REPLACED WITH NEW IAW CRJ200 AMM 27-64-01-400-801 STEPS 2.B. AND C. / CAL TOOLS USED: TUC5658 DUE 6/30/22, TUC4822 DUE 6/30/22Jan 21, 2022 · N875AS · Cndair CL6002B19 · Wing StructureSDR SWIA202265226None · corroded* THE RH SPOILERON PCU'S HAS CORRODED HARDWARE. (C-CHECK RO 3-25-22) R/H SPOILERON PCU LOWER ATTACHMENT HARDWARE REMOVED AND REPLACED WITH NEW IAW CRJ200 AMM 27-62-01-400-801 STEPS 2. A. THROUGH B. / CAL TOOLS USED: TUC5658 DUE 6/30/22, TUC4822 DUE 6/30/Jan 21, 2022 · N875AS · Cndair CL6002B19 · Flight Control SystemSDR SWIA202265225None · corroded* THE LH SPOILERON HINGES HAS CORRODED HARDWARE. (C-CHECK RO 3-25-22) REMOVED AND REPLACED WITH NEW HARDWARE ON L/H SPOILERON, REF. CRJ-200 AMM 27-64-01-400-801. SEE CONTINUATION FOR WORK PERFORMED.Jan 21, 2022 · N875AS · Cndair CL6002B19 · Flight Control SystemSDR SWIA202265224None · corroded* THE LH SPOILERON PCU'S HAS CORRODED HARDWARE. (C-CHECK RO 3-25-22) REMOVED SURFACE CORROSION FROM L/H SPOILERON HARDWARE, REF. CRJ-200 SRM 51-21-06 STEPS 7. A. [1] (A)-(B).Jan 21, 2022 · N875AS · Cndair CL6002B19 · Flight Control SystemSDR SWIA202265223None · corroded* THE LH FLIGHT SPOILER HINGES HAS CORRODED HARDWARE. (C-CHECK RO 3-25-22) REMOVED CORRODED HARDWARE FROM THE LH FLIGHT SPOILER HINGES REF CRJ200 AMM 27-64-05-000-801 PGS 401-407. INSTALLED NEW HARDWARE FOR THE LH FLIGHT SPOILER HINGES REF CRJ200 AMM 27-6Jan 21, 2022 · N875AS · Cndair CL6002B19 · Wing StructureSDR SWIA202265222None · corroded* THE LH FLIGHT SPOILER PCU'S HAS CORRODED HARDWARE. (C-CHECK RO 3-25-22) REPLACED LH FLIGHT SPOILER PCU'S CORRODED HARDWARE REF CRJ200 AMM 27-64-05-000-801 AND AMM 27-64-05-400-801. REPLACED 2 SCREWS,1 SPLIT WASHER, 1 NUT, 3 WASHERS.Jan 21, 2022 · N875AS · Cndair CL6002B19 · Wing StructureSDR SWIA202265221None · corroded* THE LH OUTBD GROUND SPOILER BONDING JUMPER HAS CORRODED HARDWARE. (C-CHECK RO 3-25-22) REMOVED CORRODED L/H OUTBOARD GROUND SPOILER BONDING JUMPER ATTACHMENT HARDWARE AND REPLACED WITH NEW HARDWARE TO INCLUDE 2 EA NUTS AND 2 EA SCREWS. IAW CRJ200 AMM 27Jan 21, 2022 · N875AS · Cndair CL6002B19 · Wing StructureSDR SWIA202265220None · corroded* THE LH OUTBD GROUND SPOILER HINGES HAS CORRODED HARDWARE. (C-CHECK RO 3-25-22) REMOVED CORRODED L/H OUTBOARD GROUND SPOILER HINGE ATTACHMENT HARDWARE TO INCLUDE 3 EA NUTS AND COTTER PINS. ONLY REPALCED ONE NUT AT A TIME IAW CRJ200 AMM 27-65-01-400-801 PJan 21, 2022 · N875AS · Cndair CL6002B19 · Wing StructureSDR SWIA202265219None · corroded* THE LH OUTBD GROUND SPOILER PCU HAS CORRODED HARDWARE. (C-CHECK RO 3-25-22) REMOVED CORRODED L/H OUTBOARD GROUND SPOILER PCU ATTACHMENT HARDWARE AND REPLACED WITH NEW HARDWARE TO INCLUDE 3 EA NUTS, 1 EA BOLT, 2 EA WASHERS AND COTTER PINS. ONLY REPALCED Jan 21, 2022 · N875AS · Cndair CL6002B19 · Wing StructureSDR SWIA202265218None · corroded* THE LH INBD GROUND SPOILER HINGES HAS CORRODED HARDWARE. (C-CHECK RO 3-25-22) REMOVED CORRODED L/H INBOARD GROUND SPOILER HINGE ATTACHMENT HARDWARE AND REPLACED WITH NEW HARDWARE TO INCLUDE 3 EA NUTS AND COTTER PINS. ONLY REPALCED ONE NUT AT A TIME. IAWJan 21, 2022 · N875AS · Cndair CL6002B19 · Wing StructureSDR SWIA202265217None · corroded* THE LH INBD GROUND SPOILER PCU HAS CORRODED HARDWARE. (C-CHECK RO 3-25-22) L/H INBOARD GROUND SPOILER PCU ATTACHMENT HARDWARE REMOVED AND REPLACED WITH NEW IAW CRJ200 AMM 27-63-01-400-801 STEPS 2.B.(2)Jan 21, 2022 · N875AS · Cndair CL6002B19 · Wing StructureSDR SWIA202265214None · corroded* THE LH INBD FLAP OUTBD HINGE ARM SIDE PLATE ON OUTBD SIDE IS CORRODED AROUND NUTPLATE HOLES. (MARKED) (C-CHECK RO 3-25-22) REMOVED DAMAGE AT LH INBD FLAP OUTBD HINGE ARM SIDE PLATE ON OUTBD SIDE REF. CRJ-200 SRM 51-21-06. FOUND TO BE OUT OF LIMITS. RECJan 21, 2022 · N875AS · Cndair CL6002B19 · AileronsSDR SWIA202265210None · chafed* THE LH INBD FLAP OUTBD HINGE ARM SIDE PLATE ON OUTBD SIDE IS CHAFFED. (MARKED) (C-CHECK RO 3-25-22) BLENDED CHAFFING ON LH INBD FLAP OUTBD HINGE ARM SIDE PLATE ON OUTBD SIDE REF CRJ200 SRM 51-12-00. FOUND TO BE OUT OF LIMITS. RECEIVED AND COMPLIED WITHJan 21, 2022 · N875AS · Cndair CL6002B19 · AileronsSDR SWIA202265234None · corrodedPAX DOOR. UPPER STOP BOLT FITTING CORRODED. (C-CHECK RO 3-25-22) REMOVED AND REPLACED BRACKET ASSY P/N 601R38921-13 WITH A NEW SERVICEABLE UNIT IAW CRJ200 SRM 51-42-14.Jan 20, 2022 · N875AS · Cndair CL6002B19 · DoorsSDR SWIA202265233None · crackedPAX DOOR. AFT DRAG ANGLE SUSPECTED CRACK BY THE MOTOR ASSIST PULLEY. (C-CHECK RO 3-25-22) REMOVED AND REPLACED PAX DOOR AFT DRAG ANGLE P/N 601R31772-6 WITH A NEW UNIT IAW CRJ200 SRM 51-42-06 AND CRJ200 SRM 51-42-14.Jan 20, 2022 · N875AS · Cndair CL6002B19 · DoorsSDR SWIA202265191None · corroded*IN MAIN CABIN, ON PRESSURE FLOOR SUPPORT BEAM, FROM APPROXIMATELY 409+128 TO FS559, AND RBL9, HAS CORROSION ON MULTIPLE AREAS OF UPPER SURFACE. (MARKED) (C-CHECK RO 3-25-22) PERFORMED REPAIR ON FLOOR SUPPORT BEAM, FROM APPROXIMATELY 409+128 TO FS559.00Jan 20, 2022 · N875AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202265190None · gougedPAX DOOR CUT-OUT FRAME AFT ROLLER ATTACHMENT GOUGED. (C-CHECK RO 3-25-22) REMOVED AND REPLACED THE PAX DOOR AFT ROLLER BRACKET REF AMM 53-21-23-400-801 REV 64 SEP 10/2021 AND DWG 600-31469 REV A. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. CHECKS GJan 20, 2022 · N875AS · Cndair CL6002B19 · DoorsSDR SWIA202265189None · corroded*IN MAIN CABIN, ON PRESSURE FLOOR SUPPORT BEAM, FROM APPROXIMATELY 409+128 TO FS559, AND LBL9, HAS CORROSION ON MULTIPLE AREAS OF UPPER SURFACE. (MARKED) (C-CHECK RO 3-25-22) PERFORMED REPAIR ON FLOOR SUPPORT BEAM, FROM APPROXIMATELY 409+128 TO FS559.00Jan 20, 2022 · N875AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202265188None · gougedPAX. DOOR. CUT-OUT FRAME FS310.00 GOUGED JUST BELOW UPPER PIN STOP. (C-CHECK RO 3-25-22) PERFORMED REPAIR TO PAX DOOR SEAL STRIKER I.A.W. ALL STEPS OF REO 601R-53-22-033 REV-D DATE 2014/02/17 REPAIR TYPE IV. COMPLIED WITH TASK CARD 51-900-1003-SKY. OPS CHJan 20, 2022 · N875AS · Cndair CL6002B19 · Fuselage Structure (General)SDR SWIA202265187None · corroded*IN MAIN CABIN, L/H PRESSURE FLOOR SILL MEMBER, FROM APPROXIMATELY 409+128 TO FS559, NEAR STR17L, HAS MULTIPLE AREAS OF CORROSION. (MARKED) (C-CHECK RO 3-25-22) REMOVED CORROSION FROM L/H PRESSURE FLOOR SILL FS 409+128-FS 559 STR 17L PER CRJ 200 SRM 51-2Jan 20, 2022 · N875AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202265186None · corrodedPAX DOOR, INTERCOSTAL DD6 AFT END CORRODED. DISCREPANCY VIEWED THRU ACCESS HOLE 832GR. (C-CHECK RO 3-25-22) REMOVED AND REPLACED PAX DOOR DD6 INTERCOSTAL P/N 601R31902-323 WITH A SERVICEABLE UNIT IAW CRJ200 SRM 51-42-06 REVISION 38: JUL 10/2019 AND BOMBARJan 20, 2022 · N875AS · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA202265185None · corroded*IN MAIN CABIN, AT APPROXIMATELY FS409+30 TO FS409+128, AND NEAR LBL6-LBL8, FLOOR BEAM HAS MULTIPLE AREAS OF CORROSION. (MARKED) (C-CHECK RO 3-25-22) REMOVED AND REPLACED MAIN CABIN FLOOR BEAM CAP AT APPROXIMATELY FS409+30 TO FS409+128, AND NEAR LBL6-LBLJan 20, 2022 · N875AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202265184None · corroded*IN MAIN CABIN, ON FLOOR BEAM AT APPROXIMATELY FS409+16 TO FS409+128, AND BETWEEN RBL6 TO RBL8, FLOOR BEAM HAS MULTIPLE AREAS OF CORROSION. (MARKED) (C-CHECK RO 3-25-22) REMOVED AND REPLACED FLOOR BEAM CAP AT FS409+16 TO FS409+128, AND BETWEEN RBL6 TJan 20, 2022 · N875AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202265209None · corroded* THE RH SIDE SEAT TRACK FROM APPROX FS409+16 TO FS409+112 HAS MULTIPLE LOCATIONS OF CORROSION (MARKED) (C-CHECK RO 3-25-22) REMOVED AND REPLACED RH SIDE SEAT TRACK AT FS409+16 TO FS409+112 REF CRJ200 AMM 53-01-11-000-802 AND AMM 53-01-11-400-802.Jan 19, 2022 · N875AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202265208None · corroded* THE RH SIDE SEAT TRACK FROM APPROX FS364 TO FS409+16 HAS MULTIPLE LOCATIONS OF CORROSION (MARKED) (C-CHECK RO 3-25-22) REMOVED AND REPLACED RH SIDE SEAT TRACK FROM FS364 TO FS409+16 REF CRJ200 AMM 53-01-11-000-802 STEPS 1-3.A AND AMM 53-01-11-400-802 SJan 19, 2022 · N875AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202265207None · corroded* THE LH SIDE SEAT TRACK FROM APPROX FS409+16 TO FS409+112 HAS MULTIPLE LOCATIONS OF CORROSION.(MARKED) (C-CHECK RO 3-25-22) REMOVED AND REPLACED LH SIDE SEAT TRACK FROM FS409+16 TO 409+112 REF CRJ200 AMM 53-01-11-000-802 STEPS 1-3.A AND AMM 53-01-11-40Jan 19, 2022 · N875AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202265206None · corroded* THE LH SIDE SEAT TRACK FROM APPROX FS364 TO FS409+16 HAS MULTIPLE LOCATIONS OF CORROSION.(MARKED) (C-CHECK RO 3-25-22) REMOVED AND REPLACED LH SIDE SEAT TRACK FROM FS364 TO FS409+16 REF CRJ200 AMM 53-01-11-000-802 AND AMM 53-01-11-400-802 TORQUE SCREWDJan 19, 2022 · N875AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202265205None · corroded* THE LH SIDE SEAT RAIL RETAINER TRIM FROM APPROX FS364 TO FS409.00+16 HAS MULTIPLE LOCATIONS OF CORROSION.(MARKED) (C-CHECK RO 3-25-22) REMOVED AND REPLACED LEFT SEAT RAIL RETAINER AND SEAT RAIL FROM APPROX FS364 TO FS409+16 IAW CRJ200 AMM 53-01-11-00/4Jan 19, 2022 · N875AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202265183None · corroded*GUSSET COMMON TO FS409 FRAME AND INTERCOSTAL AT STR25R HAS CORROSION (MARKED). (C-CHECK RO 3-25-22) REPLACED GUSSET REF DRAWING #601R31049 REV:-F, CRJ200 SRM 51-42-21-00 REV: 38B DATED: 25 NOV 2020. FOR ALL WORK ACCOMPLISHED SEE CONTINUE CARD. COMPLIED Jan 19, 2022 · N875AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202265182None · damaged*FRAME AT FS394 HAS GOUGE DAMAGE ON TOPSIDE RADIUS OF THE UPPER FLANGE AT STR27 (MARKED). (C-CHECK RO 3-25-22) BLENDED FRAME AT FS394 UPPER FLANGE AT STR27 PER REF: CRJ-200 SRM 51-12-00, FOUND TO BE WITH IN LIMITS REF CRJ 200 SRM 53-00-00. RESTORED FINISHJan 19, 2022 · N875AS · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202265181None · corroded*CORROSION ON FLOOR SILL ATTACHING ANGLE RBL 45 BETWEEN FS 605.00 €“ 621.00 (C-CHECK RO 3-25-22) REMOVED CORROSION FROM FLOOR SILL ATTACHING ANGLE RBL45 F.S.605-621.00 IAW REO 601R-53-61-4690 REV.-- DATED 2012-10-24 FOUND TO BE WITHIN LIMITS.Jan 19, 2022 · N875AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202265180None · corroded*CORROSION ON FLOOR SUPPORT BEAM AT FS 589.00 BETWEEN RBL 27 €“ RBL 36 (C-CHECK RO 3-25-22) REMOVED AND REPLACED WITH NEW FLOOR SUPPORT AT FS 589.00 BETWEEN RBL 27 €“ RBL 36 REF CRJ200 SRM 51-42-06 REV 38 JUL 10/2019 AND BOMBARDIER DWG 601R35031 REV -Jan 19, 2022 · N875AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202265179None · corroded*CORROSION ON FLOOR SUPPORT STRAP AT FS 559.00 BETWEEN RBL 9 €“ RBL 18 (C-CHECK RO 3-25-22) REMOVED CORROSION ON FLOOR SUPPORT STRAP AT FS 559.00 BETWEEN RBL 9 €“ RBL 18 IAW CRJ200 SRM 51-21-06. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED NEW FLOOR Jan 19, 2022 · N875AS · Cndair CL6002B19 · Fuselage Internal Mounting Structure
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