N876AS

Service difficulty reports · 267

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 = 'N876AS' 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 SWIA202156210Stringer · crackedWHILE REMOVING R/H FLOOR SILL AT FS559.14 FOUND CRACK ON STRINGER 17R. (C-CHECK) RO 2/9/2021 REPLACED R/H STRINGER 17R BETWEEN FS559.00 & FS559.00+16. REF REO 601R-53-51-551 REV -- DATED 2021-01-30, CRJ200 SRM 51-42-06, & CRJ200 SRM 51-42-21. LEAK CHECK GOJan 18, 2021 · N876AS · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA202156209Floor Support · corrodedRBL9 FS409.00+118 TO FS559.00+10 FLOOR BEAM CAP HAS MULTIPLE SPOTS OF CORROSION (PITTING) ON I/B FLANGE (C-CHECK) RO 2/9/2021 FABRICATED AND INSTALL NEW RBL9 FLOOR BEAM CAP BETWEEN FS409.00+118 AND FS559.00+10. REF REO 601R-53-41-2854 REV -- DATED 2021-01-Jan 16, 2021 · N876AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202156208Floor Support · corrodedLBL9 FLOOR BEAM FROM APPROX. FS409.00+118 TO FS559.00+10 HAS CORROSION AND LOW SPOTS. REQUIRES EVALUATION. (C-CHECK) RO 2/9/2021 PERFORMED MAJOR REPAIR TO LBL 9 FLOOR BEAM CAP FROM FS 409+118 TO FS559+10, IAW MHIRJ REO 601R-53-41-2854 REV -- DATE 2021-01-Jan 15, 2021 · N876AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202156240Frame · corrodedCORROSION ON INBD FLANGE OF LBL9 BETWEEN FS409.00 +128 AND FS424.00 (C-CHECK) RO 2/9/2021 BLENDED CORROSION ON THE LBL9 FS409+128 - FS424 FLOORBEAM SECTION "OUT OF LIMITS." REF CRJ200 SRM 53-41-43, DRAWING 601R31118 REV L. SEE JOB 2757661 OP/430, MX TRANSJan 11, 2021 · N876AS · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202156207Floor Support · damagedDAMAGE TO UNDERLYING STRUCTURE DURING REMOVAL OF FLOOR BEAM CAP RBL9 AT APPROX. FS.409.00+16 TO APPROX. FS.409.00+128 (C-CHECK) RO 2/9/2021 REPLACED 12 RBL-9 FLOOR BEAMS APPROX BETWEEN FS409.00+16 AND FS 409.00+128. REF DWG 601R31117 REV E, CRJ200 SRM 51-4Jan 11, 2021 · N876AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202156206Intercostal · crackedPAX DOOR MID DD4 INTERCOSTAL IS CRACK (C-CHECK) RO 2/9/2021 REMOVED CRACKED PAX DOOR MID DD4 INTERCOSTAL, AND INSTALLED NEW INTERCOSTAL. REF. CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-21, BOMBARDIER DWG. 601R31702 REV. N. RESTORED FINISH. PRESSURE CHECK GOOD. Jan 6, 2021 · N876AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA202056205Angle · crackedLH BATT RIB @ APPROX. WS.48.30 FWD CAP ANGLE CRACKED (C-CHECK) RO 2/9/2021 REMOVED AND REPLACED LH BATT RIB ASSY AT WS48.30. REF REO 601R-57-21-3403 REV-- DATED 2021-01-15, DWG 601R10204 REV-J, CRJ-200 SRM 51-42-21. COMPLIED WITH SKY CARD 51-900-1003-SKY.Dec 30, 2020 · N876AS · Cndair CL6002B19 · Wing Miscellaneous StructureSDR SWIA202056204Rib · crackedLH BATT RIB CHANNEL CRACKED AT WS.53.60 (MARKED) (C-CHECK) RO 2/9/2021 REMOVED AND REPLACED WITH NEW ANGLE P/N 601R-57-51-046-5 IAW BOMBARDIER REO 601R-57-51-046 REV B DATED 2002-02-28 (ALL STEPS), BOMBARDIER DRAWING 601R10203 REV-G. COMPLIED WITH TDec 30, 2020 · N876AS · Cndair CL6002B19 · Wing, Rib/BulkheadSDR SWIA202056203Angle · misalignedEXISTING ANGEL (601R32004-75) AT FS333 BL0 DOES NOT ALINE WITH NEW FS333 FRAME SECTOR, TOP (601R32004-5) (C-CHECK) RO 2/9/2021 REMOVED AND REPLACED WITH NEW ANGLE. REF CRJ200 51-42-06, 51-42-21 AND BOMBARDIER DRAWING 601R32004 REV K. COMPLIED WITH 51-900Dec 30, 2020 · N876AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202056202Rib · crackedRH BATT RIBB AT WS.53.60 REPAIR ANGLE DOUBLER CRACKED (C-CHECK) RO 2/9/2021 REMOVED AND DISCARDED OLD REPAIR ANGLE P/N 601R-57-51-046-6. INSTALLED NEW ANGLE P/N 601R57-51-046-6 REF REO 601R-57-51-046 REV -B DATED 2002-02-28 & DWG 601R10203 REV-G. COMPLIEDDec 29, 2020 · N876AS · Cndair CL6002B19 · Wing, Rib/BulkheadSDR SWIA202056215Plate · crackedAFT PAX DOOR CENTERING PLATE IS CRACK (C-CHECK) RO 2/9/2021 REMOVED AND INSTALLED NEW PAX DOOR AFT CENTERING PLATE IAW CRJ 200 SRM 51-42-06 AND SRM 51-42-21.Dec 23, 2020 · N876AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA202056201Floorbeam · damagedFLOOR BEAM BLEND LOCATED AT FS561 LBL 27 REQUIRES REPAIR (100% MATERIAL LOSS) (C-CHECK) RO 2/9/2021 REMOVED FLOOR BEAM SECTION FROM FS559.00+90 TO FS569.00 LBL27 AND INSTALLED NEW SECTION REF CRJ200 SRM 53-00-43 AND REO 601R-53-51-547 REV-- DATED 2021-01-0Dec 20, 2020 · N876AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA202056200Former · crackedPAX DOOR AFT FORMER IS CRACK (C-CHECK) RO 2/9/2021 REMOVED CRACKED PAX DOOR AFT FORMER, AND INSTALLED NEW FORMER. REF. BOMBARDIER DWG 601R31702 REV. N., REF. CRJ200 SRM 51-40-11. COMPLIED WITH TASK CARD 51-900-1003-SKY. RESTORED FINISH. PRESSURE CHECK GOODec 18, 2020 · N876AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA202056239Bushing · corroded* BOTH VERTICAL STABILIZER PIVOT FITTING BUSHINGS ARE CORRODED/PITTING (C-CHECK) RO 2/9/2021 REMOVED AND INSTALLED NEW LH AND RH BUSHINGS IN THE VERTICAL STABILIZER PIVOT FITTING. REF- RIL #6370, REV NC, DATED 9-FEB-2019 AND SB 601R-55-007, REV D, DATED MDec 15, 2020 · N876AS · Cndair CL6002B19 · Vertical StabilizerSDR SWIA202056199Fitting · nicked*NICKS ON L/H INBD LUG FITTING AT WS178.00 (MARKED) (C-CHECK) RO 2/9/2021 REMOVED DAMAGE ON THE LH INBD LUG FITTING AT WS178.00 "WITHIN LIMITS" MHI REO 601R-57-21-3389 REV-- DATED 2020-12-24. COMPLIED WITH ST 51-900-1003-SKY. ROTO PEENED AND RESTORED FIDec 15, 2020 · N876AS · Cndair CL6002B19 · Wing Main, Frame StructureSDR SWIA202056198Fitting · chafed*R/H INBD LUG FITTING AT WS178.00 HAS EVIDENCE OF CHAFFING (MARKED) (C-CHECK) RO 2/9/2021 BLENDED R/H INBD LUG FITTING AT WS178.00 CHAFFE DAMAGE TO A SMOOTH CONTOUR AND RESTORED FINISH. FOUND TO BE WITHIN LIMITS. REF REO 601R-57-21-3390 REV -- DATED 2020-1Dec 15, 2020 · N876AS · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA202056197Plate · corroded* PAX DOOR SURROUND, GUSSET PLATE AT APPROXIMATELY FS349 STGR12L IS CORRODED (C-CHECK) RO 2/9/2021 REMOVED AND REPLACED GUSSET PLATE AT APPROXIMATELY FS349.00 ON STRINGER 12L. REF BOMBARDIER DWG 601R31098 REV -C AND CRJ200 SRM 51-42-06. COMPLIED WITH TASKDec 15, 2020 · N876AS · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA202056196Plate · corroded* PAX DOOR SURROUND, GUSSET PLATE AT APPROXIMATELY FS349 STGR9L IS CORRODED (C-CHECK) RO 2/9/2021 REMOVED AND REPLACED PAX DOOR GUSSET PLATE AT APPROXIMATELY FS349.00 AND STRINGER 9L REF DWG# 601R31098 REV. NC , AND CRJ200 SRM 51-42-06. COMPLIED WITH SKYDec 15, 2020 · N876AS · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA202056195Plate · corroded* PAX DOOR SURROUND, GUSSET PLATE AT APPROXIMATELY FS349 STGR7L IS CORRODED (C-CHECK) RO 2/9/2021 REMOVED AND REPLACED GUSSET PLATE AT FS349 STRINGER 7L IAW BOMBARDIER DWG 601R31096 REV D AND CRJ200 SRM 51-42-06. COMPLIED WITH SKYCARD 51-900-1003-SKY.Dec 15, 2020 · N876AS · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA202056193Frame · cracked* FS333 FRAME CRACKED AT APPROXIMATELY STGR1R (C-CHECK) RO 2/9/2021 REMOVED AND REPLACED FS333.00 FRAME BETWEEN BL0 AND STR 5R. REF DWG# 601R31522 REV -Y, CRJ200 SRM 51-42-06, & CRJ200 SRM 51-42-21. COMPLIED WITH TASK CARD 51-900-1003-SKY. LEAK CHECK GOOD.Dec 15, 2020 · N876AS · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202056238Nut · corrodedRH WING FLIGHT SPOILER INBOARD AND OUTBOARD ATTACH HINGES HAVE CORRODED HARDWARE (C-CHECK) RO 2/9/2021 REMOVED CORRODED NUTS (2 EA.) AND RETENTION ANGLE BOLTS (4 EA.) FROM RH WING FLIGHT SPOILER INBOARD AND OUTBOARD ATTACH HINGES. REF CRJ200 AMM 27-64-05-Dec 14, 2020 · N876AS · Cndair CL6002B19 · SpoilersSDR SWIA202056237Bolt · corrodedLH WING FLIGHT SPOILER ATTACH HINGES HAVE CORRODED HARDWARE (C-CHECK) RO 2/9/2021 REMOVED AND INSTALLED 4 EA NUTS, RETENTION ANGLE, 4 EA BOLTS, AND 8 EA SCREWS FROM LH WING FLIGHT SPOILER ATTACH HINGES IN FOUR LOCATIONS. REF CRJ200 AMM 27-64-05-000-801 & CDec 14, 2020 · N876AS · Cndair CL6002B19 · SpoilersSDR SWIA202056236Bolt · corrodedLH WING SPOILERON ATTACH HINGES AND PCU'S TO SPOILERON MOUNTINING HARDWARE IS CORRODED (C-CHECK) RO 2/9/2021 REPLACED L/H WING SPOILERON ATTACHMENT HINGES AND PCU TO SPOILERON HARDWARE IAW CRJ 200 AMM 27-64-01-400-801Dec 14, 2020 · N876AS · Cndair CL6002B19 · SpoilersSDR SWIA202056235Nut · corrodedRH WING INBOARD GROUND SPOILER PCU LINK AND OUTBOARD HINGE MOUNTING HARDWARE NUTS ARE CORRODED. (C-CHECK) RO 2/9/2021 REMOVED AND INSTALLED 1 EACH NEW NUT AND NEW COTTER PIN ON RH INBD GROUND SPOILER UPPER PCU LINK. REF - CRJ 200 AMM 27-65-01-000-801 STEP Dec 14, 2020 · N876AS · Cndair CL6002B19 · SpoilersSDR SWIA202056214Hinge Fitting · cracked* LEFT AILERON CENTER HINGE FITTING RIBLET CRACKED. (MARKED) (C-CHECK) RO 2/9/2021 REMOVED AND REPLACED WITH NEW CENTER HINGE FITTING FOR LH AILERON REF CRJ200 SRM 51-42-10Dec 14, 2020 · N876AS · Cndair CL6002B19 · AileronsSDR SWIA202056213Door Frame · crackedAVIONICS COMPARTMENT DOOR SURROUND. THE RH / FWD AND AFT DOOR GUIDES ARE CRACKED. FLAGGED (C-CHECK) RO 2/9/2021 INSTALLED NEW SERVICEABLE AVIONICS COMPARTMENT DOOR SURROUND RH FWD AND AFT DOOR GUIDES (FRAME GUIDE FITTINGS), REF. CRJ200 SRM 51-41-02 AND CRDec 14, 2020 · N876AS · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA202056192Skin · corroded*THE LH WING LOWER PLANK ACCESS HOLE UNDER PANEL 550BB HAS MULTIPLE LOCATIONS OF CORROSION. (MARKED) (C-CHECK) RO 2/9/2021 BLENDED CORROSION ON LH LOWER WING PLANK ACCESS HOLE FOR PANEL 550BB TO A SMOOTH CONTOUR, REMAINING THICKNESS OF 0.168" IS WITHIN LIDec 14, 2020 · N876AS · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA202056191Bulkhead Web · crackedAFT PRESSURE BULKHEAD F/S 621.0 STIFFENER IS CRACK (C-CHECK) RO 2/9/2021 REMOVED AND INSTALLED NEW BULKHEAD STIFFENER REF: CRJ 200 SRM 51-42-06, CRJ 200 SRM 51-40-11, CRJ 200 SRM 51-25-16, SRM 51-21-11 AND BOMBARDIER DWG 601R36008 REV. BC. COMPLIED WITH TADec 13, 2020 · N876AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA202056190Skin · bentH-STAB TIP LEADING EDGE FLANGE FOR PANEL 333AL IS BENT AND DE-FORMED (C-CHECK) RO 2/9/2021 REPLACED LEADING EDGE FLANGE SPLICE IAW REO 601R-55-11-680 REV-- DATE 2021-01-04 AND CRJ 200SRM 51-42-02 BOMBARDIER DRAWING # 600-23037 REV-L DATED 2016-03-14. COMPLDec 12, 2020 · N876AS · Cndair CL6002B19 · Horizontal Stabilizer, Plate/SkinSDR SWIA202056189Skin · bentH-STAB TIP LEADING EDGE FLANGE FOR PANEL 343AR IS BENT AND DE-FORMED (C-CHECK) RO 2/9/2021 REPLACED LEADING EDGE FLANGE SPLICE IAW REO 601R-55-11-680 REV-- DATE 2021-01-04 AND CRJ 200SRM 51-42-13 BOMBARDIER DRAWING # 600-23060 REV-V DATED 2016-03-14 COMPDec 12, 2020 · N876AS · Cndair CL6002B19 · Horizontal Stabilizer, Plate/SkinSDR SWIA202056188Skin · corroded* EXTERIOR FUSELAGE SKIN HAS CORROSION ON AND AROUND MULTIPLE RIVETS BETWEEN APPROX. FS 559.00 + 80 TO 559.00 + 112, AT LOWER CENTER FUSELAGE AREA. ( STGR 25L TO STGR 25R ). (C-CHECK) RO 2/9/2021 BLENDED ALL FOUR AREAS TO A SMOOTH CONTOUR AND RESTORED FINIDec 11, 2020 · N876AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA202056187Hinge Fitting · chafed*CHAFFING NOTED ONL/H INBD FLAP HINGE LUG PLATE AT WS80.50 (C-CHECK) RO 2/9/2021 BLENDED L/H INBD FLAP HINGE LUG PLATE AT WS80.50 CHAFFE DAMAGE TO A SMOOTH CONTOUR AND RESTORED FINISH. REMAINING MATERIAL WITHIN LIMITS. REF REO 601R-57-21-3392 REV -- DATEDDec 11, 2020 · N876AS · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA202056234Seat Track · corroded*MULITIPLE SPOTS OF CORROSION ON SIDE SEAT RAIL FWD OF FS409.0+128 TO FS364.00 FOR L/H SIDE (MARKED). (C-CHECK) RO 2/9/2021 INSTALLED NEW SIDE SEAT RAILS P/N 601R38312-31, 601R38312-29, AND 601R38312-119 IAW CRJ 200 AMM 53-01-11, TORQURED TO 50 IN / LBS WDec 10, 2020 · N876AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202056233Seat Track · corroded*MULITIPLE SPOTS OF CORROSION ON SIDE SEAT RAIL FWD OF FS409.0+128 TO FS364.00 FOR R/H SIDE (MARKED). (C-CHECK) RO 2/9/2021 REMOVED MULTIPLE SPOTS OF CORROSION ON THE RH SIDE SEAT RAIL AT APPROX FS.364 TO FS.409+128 REF CRJ 200 SRM 51-21-06. FOUND TO BE ODec 10, 2020 · N876AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202056232Seat Track · corroded*MULITIPLE SPOTS OF CORROSION ON SIDE SEAT RAIL AFT OF THE FS409.0+128 TO FS559.00+64 FOR L/H SIDE (MARKED). (C-CHECK) RO 2/9/2021 FOUND TO BE CORRODED BEYOND REPAIR, INSTALLED NEW SIDE SEAT TRACKS FROM F.S.409+128 TO F.S.559+80 IAW CRJ200 AMM 53-01-11-4Dec 10, 2020 · N876AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202056231Seat Track · corroded*MULITIPLE SPOTS OF CORROSION ON SIDE SEAT RAIL AFT OF THE FS409.0+128 TO FS559.00+64 FOR R/H SIDE (MARKED). (C-CHECK) RO 2/9/2021 FOUND THE RH SIDE SEAT RAILS AFT OF THE FS.409+128 TO FS.559+64 TO BE OUT OF LIMITS REF CRJ 200 SRM 53-21-49 FABRICATED AND Dec 10, 2020 · N876AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202056186Door Sill · corroded*CORROSION AT SERVICE DOOR LOWER SILL (C-CHECK) RO 2/9/2021 REMOVED CORRODED SILL AND INSTALLED NEW SERVICE DOOR LOWER SILL PN 601R38303-253 REF CRJ200 SRM 51-42-21, SRM 51-42-13, SRM 51-42-36, SRM 51-42-06 BOMBARDIER DWG 601R38303 REV AR. COMPLIED WITH 51Dec 10, 2020 · N876AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202056185Floor Support · corrodedCORROSION AT R/H FOOR SILL AT APPROX. FS559.00+14 (C-CHECK) RO 2/9/2021 REPLACED R/H FLOOR SILL BETWEEN FS559.00 & FS559.00+16. REF CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-21, & DWG 601R31133 REV J. COMPLIED WITH TASK CARD 51-900-1003-SKY.Dec 10, 2020 · N876AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202056184Intercostal · corroded*PAX DOOR, INTERCOSTAL AT DD6 BETWEEN APPROX FS320.10 AND FS338.90 HAS CORROSION.(MARKED) (C-CHECK) RO 2/9/2021 EVALUATED PAX DOOR, INTERCOSTAL AT DD6 AT FS320.10 AND FS338.90 CORROSION AS OUT-OF-LIMITS. REF. CRJ200 SRM 52-00-00. REMOVED PAX DOOR MID DD6 IDec 10, 2020 · N876AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA202056183Floor Support · corroded*CORROSION ON FLOOR BEAM OTBD FLANGE RBL 27, BETWEEN FS 589.00 - 621.00 (C-CHECK) RO 2/9/2021 BLENDED OUT CORROSION ON FLOOR BEAM OTBD FLANGE RBL 27, BETWEEN FS 589.00 - 621.00 TO A SMOOTH CONTOUR. REWORKED AREAS WITHIN LIMITS. SEE CONT CARD FOR FURTHER DEDec 10, 2020 · N876AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202056182Floor Support · corroded*CORROSION ON RH FLOOR SILL FS559.00+80-605.00 (C-CHECK) RO 2/9/2021 REMOVED AND REPLACED THE RH FLOOR SILL. COMPLIED WITH ALL STEPS OF RREO 601R-53-61-5376, REV-A, DATED 2018-10-25, DRAWING 601R35012 REV-T, & CRJ200 SRM 51-42-06,. COMPLIED WITH 51-900-10Dec 10, 2020 · N876AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202056181Floor Support · corroded*CORROSION ON FLOOR BEAM BETWEEN RBL9 OTBD FLANGE BETWEEN FS 559.00+112 - 559.00+80 (C-CHECK) RO 2/9/2021 CORROSION REMOVED FROM RBL9 OTBD FLANGE BETWEEN FS 559.00+80 - 559.00+112,. / NDT COMPLETED IAW CRJ 200 NDT 51-20-04 / REMOVED AND REPLACED TWO NUT PLDec 10, 2020 · N876AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202056180Intercostal · corroded*PAX DOOR, AFT INTERCOSTAL AT DD4 HAS CORROSION (APPROX FS338 TO FS347.25) (C-CHECK) RO 2/9/2021 REMOVED CORROSION ON PAX DOOR, AFT INTERCOSTAL AT DD4, AND EVALUATED AS OUT-OF-LIMITS. REF. CRJ200 SRM 52-00-00. REMOVED AND INSTALLED NEW AFT DD4 INTERCOSTAL.Dec 10, 2020 · N876AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA202056179Floor Support · corroded*CORROSION ON FLOOR BEAM TOP OTBD FLANGE LBL 27 BETWEEN FS 559.00+112 - 621.00. MULTIPLE AREAS MARKED. (C-CHECK) RO 2/9/2021 COMPLIED WITH REO 601R-53-00-005 REV B DATED 2011/01/06 AND REO 601R-53-61-7523 REV -- DATED 2020-12-30 "WITHIN LIMITS," FOR REPAIRDec 10, 2020 · N876AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202056178Floorbeam · corroded*CORROSION ON FLOOR SUPPORT BEAM TOP SURFACE AT FS 559.00, LBL 27-36 (C-CHECK) RO 2/9/2021 REMOVED AND REPLACED STRAP BETWEEN LBL27 & 3BL36 @ FS559.00. REF DWG 601R31025 REV N & CRJ200 SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1003-SKY. LEAK CHECK GOOD.Dec 10, 2020 · N876AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA202056177Floor Support · corroded*MULTIPLE SPOTS OF CORROSION ON THE R/H PRESSURE FLOOR SILL FROM FS409.0-128 TO FS559.00 (MARKED) (C-CHECK) RO 2/9/2021 BLENDED MULTIPLE SPOTS OF CORROSION ON THE RH PRESSURE FLOOR SILL FROM FS.409+128 TO FS.559 REF REO 601R-53-41-666 REV-C DATED 2012-11-0Dec 10, 2020 · N876AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202056176Floor Support · corroded*MULTIPLE SPOTS OF CORROSION ON THE L/H PRESSURE FLOOR SILL FROM FS409.0-128 TO FS559.00 (MARKED) (C-CHECK) RO 2/9/2021 BLENDED CORROSION TO A SMOOTH CONTOUR AND RESTORED FINISH TO REWORKED AREAS. REMAINING MATERIAL IS WITHIN LIMITS. REF REO 601R-53-41-666Dec 10, 2020 · N876AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202056230Seat Track · corroded*LEFT BL9 FLOOR SEAT RAIL FROM APPROX. AFT OF FS394.00 TO APPROX FS409.00+128 HAS CORROSION ALONG ITS LENGTH AROUND FASTENER HOLE AND ON MULTIPLE ELEMENTS. (MARKED) (C-CHECK) RO 2/9/2021 LBL9 FLOOR SEAT RAIL FROM APPROX. AFT OF FS.394 TO APPROX. FS.409+12Dec 9, 2020 · N876AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202056229Seat Track · corroded*RIGHT BL9 FLOOR SEAT RAIL FROM APPROX. AFT OF FS394.00 TO APPROX FS409.00+128 HAS CORROSION ALONG ITS LENGTH AROUND FASTENER HOLE AND NON MULTIPLE ELEMENTS. (MARKED) (C-CHECK) RO 2/9/2021 INSTALLED NEW SEAT RAIL AT RBL9 FROM F.S.394.00 TO F.S.409+128 IAWDec 9, 2020 · N876AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202056228Seat Track · corroded* MOST FWD LEFT BL9 SEAT RAIL FROM JUST AFT OF APPROX. FS409.00 GOING FORWARD IS CORRODED ON MULTIPLE ELEMENTS AND AROUND FASTENER HOLES IN NUMEROUS LOCATIONS ALONG ITS ENTIRE LENGTH. (MARKED) (C-CHECK) RO 2/9/2021 REMOVED AND REPLACED LBL9 SEAT RAIL FROM Dec 9, 2020 · N876AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
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