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 SWIA202265178None · corroded*CORROSION ON FLOOR BEAM RBL 9 BETWEEN FS 559.00 €“ 559.00+96 (C-CHECK RO 3-25-22) REMOVED AND REPLACED WITH NEW FABRICATED RBL9 FLOOR BEAM CAP BETWEEN FS 559.00 AND FS 574 .00 REF CRJ200 SRM 51-42-21, CRJ200 SRM 51-42-22, REO 601R-53-51-615 REV -- DATEDJan 19, 2022 · N875AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202265177None · corroded* THE FLOOR BEAM CAP AT RBL27 BETWEEN FS605 AND FS621 APROX HAS MULTIPLE LOCATIONS OF CORROSION. (MARKED) (C-CHECK RO 3-25-22) REPLACED FLOOR BEAM CAP AT RBL27 BETWEEN FS605 AND FS621 REF REO 601R-53-61-3778 REV -B DATE 2016-12-19 AND DRAWING 601R35031 Jan 19, 2022 · N875AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202265176None · corroded* THE FLOOR BEAM CAP AT RBL9 BETWEEN FS605 AND FS621 APROX HAS MULTIPLE LOCATIONS OF CORROSION. (MARKED) (C-CHECK RO 3-25-22) REMOVED AND REPLACED CORRODED FLOOR BEAM CAP AT RBL9 BETWEEN APPROX. FS605 AND FS621 WITH A SERVICEABLE UNIT REF CRJ 200 SRM 51-4Jan 19, 2022 · N875AS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202265175None · corroded*IN MAIN CABIN, ON SUPPORT TIE AT APPROXIMATELY FS319 AND STR 17R, CORROSION ON SUPPORT TIE. (MARKED) (C-CHECK RO 3-25-22) : REMOVED CORROSION OF SUPPORT TIE AT APPROX FS319 AND STGR 17R REF CRJ200 SRM 51-21-06. FOUND TO BE OUT OF LIMITS. REMOVED AND INSJan 19, 2022 · N875AS · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA202265212None · damaged*SERVICE DOOR HAS SEVERAL AREAS OF CHAFF DAMAGE ON EXTERIOR SKIN AROUND DOOR HANDLE (MARKED) (C-CHECK RO 3-25-22) REMOVED DAMAGE AT SERVICE DOOR ON EXTERIOR SKIN AROUND DOOR HANDLE PER REF CRJ200 SRM 51-12-00. FOUND OUT OF LIMITS. RECEIVED AND COMPLIED WJan 18, 2022 · N875AS · Cndair CL6002B19 · Fuselage Structure (General)SDR SWIA202265204None · chafedR/H STAB CENTER ELEVATOR HINGE FITTING HAS CHAFE AREA @ LWR OTBD MOUNT AREA (C-CHECK RO 3-25-22) BLENDED R/H STAB CENTER ELEVATOR HINGE FITTING AT LWR OTBD MOUNT AREA REF CRJ200 SRM 51-12-00. FOUND TO BE OUT OF LIMITS. RECEIVED AND COMPLIED WITH ALL STEPSJan 18, 2022 · N875AS · Cndair CL6002B19 · Elevator Tab, Attach FittingsSDR SWIA202265203None · chafedR/H STAB OTBD ELEVATOR HINGE FITTING HAS CHAFE AREA LWR SUPPORT (C-CHECK RO 3-25-22) BLENDED R/H STAB OTBD ELEVATOR HINGE FITTING LOWER SUPPORT IAW CRJ200 SRM 51-12-00. FOUND TO BE OUT OF LIMITS. RECEIVED AND COMPLIED WITH ALL STEPS OF REO 601R-55-11-713 Jan 18, 2022 · N875AS · Cndair CL6002B19 · Elevator Tab, Attach FittingsSDR SWIA202265174None · corroded*IN MAIN CABIN, FLOOR BEAM FRAME TIE AT APPROXIMATELY FS310 & STR 17L, FRAME TIE HAS MULTIPLE AREAS OF CORROSION. (MARKED) (C-CHECK RO 3-25-22) REMOVED CORROSION AT MAIN CABIN FLOOR BEAM FRAME TIE APPROX. FS 310.00 AND STGR. 17L. AS REQUIRED REF: CRJ-200Jan 18, 2022 · N875AS · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202265173None · corroded*RH MLG TRUNNION STRAP HAS CORROSION AROUND SEVERAL OF THE FASTENER HEADS (MARKED) (C-CHECK RO 3-25-22) CORROSION BLENDED ON RH MLG TRUNNION STRAP HAS CORROSION AROUND FASTENER HEADS REF CRJ200 SRM 51-21-06. FOUND OUT OF LIMITS. RECEIVED AND COMPLIED WITJan 17, 2022 · N875AS · Cndair CL6002B19 · Landing Gear SystemSDR SWIA202265172None · corroded*LH MLG TRUNNION STRAP HAS CORROSION AROUND SEVERAL OF THE FASTENER HEADS (MARKED) (C-CHECK RO 3-25-22) CORROSION BLENDED ON LH MLG TRUNNION STRAP HAS CORROSION AROUND FASTENER HEADS, WITH DIMENSIONS: L=11.00", W=1.5", THICKNESS REMAINING 0.200" +/- 0.01Jan 17, 2022 · N875AS · Cndair CL6002B19 · Landing Gear SystemSDR SWIA202265238None · failedRH ELEVATOR INBD PCU FAILED BEARING BACKLASH CHECK (C-CHECK RO 3-25-22) REMOVE AND INSTALLED NEW HARDWARE TO INCLUDE: QTY1 SPHERICAL BALL, QTY1 BOLT, QTY2 WASHER, QTY1 BUSHING, QTY1 NUT AT RH INBOARD PCU REF. CRJ-200 AMM 27-33-01-400-803. COMPLIED WITH TAJan 13, 2022 · N875AS · Cndair CL6002B19 · Flight Control SystemSDR SWIA202265237None · failedRH ELEVATOR MIDDLE PCU FAILED BEARING BACKLASH CHECK (C-CHECK RO 3-25-22) REMOVE AND INSTALLED NEW HARDWARE TO INCLUDE: QTY1 SPHERICAL BALL, QTY1 BOLT, QTY2 WASHER, QTY1 BUSHING, QTY1 NUT. AT R/H MIDDLE PCU REF. CRJ-200 AMM 27-33-01-400-803. BACKLASH CHECJan 13, 2022 · N875AS · Cndair CL6002B19 · Flight Control SystemSDR SWIA202265236None · failedLH ELEVATOR MIDDLE PCU FAILED BEARING BACKLASH CHECK (C-CHECK RO 3-25-22) REMOVE AND INSTALLED NEW HARDWAER 1EA BALL SPHERICAL, 1EA BOLT, 2 WASHERS, 1EA BUSHING NUT AND COTTER PIN AT L/H MIDDLE PCU REF,CRJ200 AMM 27-33-01-400-803. BACKLASH CHECK GOOD. COJan 13, 2022 · N875AS · Cndair CL6002B19 · Flight Control SystemSDR SWIA202265235None · failedLH ELEVATOR OTBD PCU FAILED BEARING BACKLASH CHECK (C-CHECK RO 3-25-22) REMOVED AND REPLACED L/H OTBD PCU WITH NEW HARDWAER 1EA BALL SPHERICAL, 1EA BOLT, 2 WASHERS, 1EA BUSHING NUT AND COTTER PIN REF,CRJ200 AMM 27-33-01-400-803 TUC 7832 CAL DUE DATE 02/28Jan 13, 2022 · N875AS · Cndair CL6002B19 · Flight Control SystemSDR SWIA202265202None · crackedUPPER PIONO HINGE ON TOP STEP #832ET HAS ELONGATED HOLES FOR ATTATCHMENT HARDWARE AND LOWER PIANO HINGE CRACKED AND DAMAGED. (C-CHECK RO 3-25-22) REMOVED AND REPLACED WITH NEW UPPER AND LOWER PIANO HINGE ON STEP PANEL # 832ET REF CRJ200 SRM 51-42-06Jan 10, 2022 · N875AS · Cndair CL6002B19 · Fuselage, Equipment Attach FittingsSDR SWIA202163105None · failedRIGHT ENGINE FAIL (N1 /N2 DROP) APPROXIMATELY 600 AGL, HIGH ITT, LOUD LOW FREQUENCY VIBRATION. FO SIDE PFD AND MFD MULTIPLE DROP OFFS STOPPED AFTER INFLIGHT SHUTDOWN. NORMAL SINGLE ENGINE LANDING. (FILED CLOSED - FLIGHT 5092) PLEASE REFERENCE AML 80687Dec 16, 2021 · N875AS · Cndair CL6002B19 · Fuselage Structure (General)SDR SWIA202165216None · wornREMOVE AND REPLACE BUSHINGS AND HARDWARE ON RH AILERON WING AFT SPAR REF CRJ 200 AMM 20-26-00-910-804 (C-CHECK RO 3-25-22) REMOVED AND REPLACED WITH NEW 8EA BUSHINGS FROM THE RH AILERON REAR SPAR HINGE POINTS REF CRJ 200 AMM 20-26-00-910-802 , CRJ200 ANov 18, 2021 · N875AS · Cndair CL6002B19 · Wing StructureSDR SWIA202165215None · wornREMOVE AND REPLACE BUSHINGS AND HARDWARE ON LH AILERON WING AFT SPAR REF CRJ 200 AMM 20-26-00-910-804 (C-CHECK RO 3-25-22) REMOVED AND REPLACED BUSHINGS ON L/H AILERON WING AFT SPAR, REF. CRJ-200 AMM 20-26-00-910-804. SEE CONTINUATION FOR WORK PERFORMED.Nov 18, 2021 · N875AS · Cndair CL6002B19 · Wing StructureSDR SWIA202162259None · faultyD:GEAR UP DISAGREE COMPLIED WITH QRH 13-3 DIVERTED TO LAX. MAIN GEAR INDICATED UNSAFE UNTIL COMPLETION OF 13-3. LANDING UNEVENTFUL. DEFERRED LANDING GEAR RETRACTION SYSTEM IN ACCORDANCE WITH MEL 32-30-1. COMPLIED WITH MAINTENANCE ACTIONS. INSTALLED AND SAFETYOct 29, 2021 · N875AS · Cndair CL6002B19 · Landing Gear Door ActuatorSDR SWIA202159593Pump · failedRTF- GEAR DISAGREE WARNING FOR NOSEGEAR NOT RETRACTING. IT MADE NO MOTION, BUT MAIN GEAR BOTH CAME UP. HYD 3 CAUTION MESSAGE POSSIBLY ASSOCIATED AFTER RUNNING QRH WITH BOTH HYDRAULIC SYSTEM 3 PUMPS ON (FLIGHT 5507 - FILED CLOSED) THIS DISCREPANCY WAS TRAJul 17, 2021 · N875AS · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), MainSDR SWIA2020010947562Floorbeam · crackedFLOOR MEMBER FS 280.00 HAS A CRACK IN LOWER SIDE AT LBL 9 COMMON TO FLOOR POST. (C-CHECK) RO 01/07/2020 PERFORMED PERMANENT REPAIR TO F.S.280 WEB BETWEEN LBL20.75 AND RBL20.75 IN REF REO. ALL STEPS COMPLETED AT THIS TIME, STRUCTURAL MAJOR REPAIR COMPLETE. SEEDec 3, 2019 · N875AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA2020061851085Fitting · damagedHORIZONTAL STABILIZER STEADY FITTING BOLT NUMBER 2 RHS AS REFERENCED IN REO LOOSE. COMPLETED REPAIR FOR ELONGATED HOLES IN V-STAB STEADY FITTING REF REO. PERFORMED GAP CHECK BETWEN V-SATB STEADY FITTING AND SLIDER BLOCK REF REO, GAP CHECK GOOD. GAP CHECK GOODNov 26, 2019 · N875AS · Cndair CL6002B19 · Horizontal Stabilizer Miscellaneous StructureSDR SWIA2020010947599Stringer · corrodedSTRINGER 27 CORRODED BETWEEN FS 349.00 AND 333.00 (C-CHECK) RO 01/07/2020 PERFORMED STRINGER REPAIR ON STGR27 BETWEEN FS280 - FS364 REF BOMBARDIER DWG, CRJ-200 SRM. COMPLIED WITH TASK CARD.Nov 26, 2019 · N875AS · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA2020010947598Stringer · corrodedSTRINGER 26 LH CORRODED BETWEEN FS 295.00 TO FS 310.00 (C-CHECK) RO 01/07/2020 REOMVED AND REPLACED STRINGER 26 LH. REF CRJ200 SRM BOMBARDIER DWG. NO LEAKS NOTED.Nov 26, 2019 · N875AS · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA2020010947597Stringer · corrodedSTRINGER 25 LH CORRODED BETWEEN FS 294.00 TO FS 310.00 (C-CHECK) RO 01/07/2020 PERFORMED STRINGER SPLICE REPAIR TO STGR25 LH FROM FS280-FS240, REF BOMBARDIER REO AND PER BOMBARIDER DWG. COMPLIED WITH TASK CARDNov 26, 2019 · N875AS · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA2020010947596Doubler · corrodedTCAS ANTENNA DOUBLER PLATE BETWEEN FS295.00 - FS310.00 AND BETWEEN STGR27 - STGR26R CORRODED, MARKED, (INSIDE FUSELAGE) (C-CHECK) RO 01/07/2020 EVALUATED ANTENNA DOUBLER PLATE BETWEEN FS 295.00 TO FS 310.00 AND STR 27 TO STR 26 RH FOUND TO BE OUT OF LIMITS MANov 26, 2019 · N875AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA2020010947602Hinge · chafed* PASSENGER DOOR HINGE HALF ON THE FUSELAGE HAS ALL LUG LANDS CHAFED DUE TO CONTACT WITH DOOR SIDE HINGE HALF LUGS. ALL LUGS ALSO HAVE ELONGATED HOLES. (C-CHECK) RO 01/07/2020 REMOVED PAX DOOR FUSELAGE HINGE REF. CRJ 200 SRM. INSTALLED THE NEW PAX DOOR FUSELNov 20, 2019 · N875AS · Cndair CL6002B19 · Fuselage, Door HingeSDR SWIA2020010947595Intercostal · corrodedINTERCOSTAL BETWEEN FRAMES FS364.00 AND FS349.00 AND BETWEEN STRGRS. 27 TO 26L COMMON TO SKIN HAS CORROSION. (C-CHECK) RO 01/07/2020 REMOVED CORROSION FROM INTERCOSTAL BETWEEN FRAMES FS364.00 AND FS349.00 AND BETWEEN STRGRS. 27 AND 26L AND COMMON TO LOWER SKNov 20, 2019 · N875AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020010947594Bolt · corroded* L/H FLIGHT SPOILER OBD PCU LOWER ATTACHMENT BOLT HAS CORRODED NUT AND IS MISSING COTTER PIN. (C-CHECK) RO 01/07/2020 REMOVED AND INSTALLED NEW LH WING ATTACHING HARDWARE @ FLIGHT SPOILER OTBD PCU TO REAR SPAR REF CRJ200 AMM. PERFORMED OPERATIONAL TEST OF FLNov 20, 2019 · N875AS · Cndair CL6002B19 · SpoilersSDR SWIA2020010947593Fitting · corrodedL/H AND R/H FITTINGS P/N 601R38343-2,-3 COMMON TO FRAME FWD. SIDE FS. 364.00 STRGR.26L AND 26R HAVE CORROSION (C-CHECK) RO 01/07/2020 REMOVED CORROSION FROM LH & RH FITTINGS P/N 601R38343-2, -3 COMMON TO FRAME FWD SIDE SIDE FS354.00 STGR 26L AND 26R REF CRJ Nov 20, 2019 · N875AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA2020010947561Frame · crackedSUSPECT CRACK FOUND ON LOWER FRAME FLANGE AT FS605.00 AND O/B OF STGR 24L. (MARKED) (C-CHECK) RO 01/07/2020 REMOVED AND REPLACED FRAME AT FS605.00 P/N 601R36026-27R. PER BOMBARDIER DWG 601R36026 REV AF AND REF CRJ200 SRM. NO LEAKS NOTED. COMPLIED WITH SKYWESNov 20, 2019 · N875AS · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2020010947592Strap · corrodedFLOOR BEAM STRAP AT FS589.00 BETWEEN LBL9 AND LBL27 CORRODED, MARKED (C-CHECK) RO 01/07/2020 REMOVED CORROSION IN REF CRJ 200 SRM 51-21-06. FOUND TO BE OUT OF LIMITS REF CRJ 200 SRM. MEASURED THICKNESS .088" ORIGINAL THICKNESS .100". MATERAL LOSS .012" MAX ALNov 19, 2019 · N875AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020010947591Strap · corrodedRH FLOOR STRAP AT FS559.00 AFT OF PRESSURE FLOOR SILL CORRODED, MARKED (C-CHECK) RO 01/07/2020 REMOVED CORROSION FROM RH FLOOR STRAP AT FS559.00 AFT OF PRESSURE FLOOR SILL REF CRJ200 SRM. ORIGINAL MATERIAL THICKNESS RH OUTBOARD FLOOR SUPPORT STRAP AT FS559 .Nov 19, 2019 · N875AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020010947590Seat Track · corrodedFLOOR SEAT RAIL, RBL9 AT FS559.00 - FS559+80 HAS MULTIPLE AREAS OF CORROSION (C-CHECK) RO 01/07/2020 REMOVED CORROSION ON CARGO SEAT TRACK AT RBL9 FS559.00 - FS559.00+80 REF CRJ200 SRM. FOUND TO BE OUT OF LIMITS REF CRJ200 SRM AND BSM.TOOL #7498 CAL DUE 31-DENov 19, 2019 · N875AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020010947589Seat Track · corrodedFLOOR SEAT RAIL, LBL9 AT FS559.00 - FS559+80 HAS MULTIPLE AREAS OF CORROSION (C-CHECK) RO 01/07/2020 REMOVED CORROSION FLOOR SEAT RAIL SECTION LBL9 FS559 TO FS599+80, REFERENCE CRJ200 SRM. CORROISON REMOVAL NOT WITHIN LIMITS, REFERENCE CRJ200 SRM. REMOVED ANNov 19, 2019 · N875AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020010947588Seat Track · corrodedCARGO SEAT TRACK AT RBL9, FS559+112 - FS570.00 HAS CORROSION (C-CHECK) RO 01/07/2020 REMOVED CORROSION ON CARGO SEAT TRACK AT RBL9 FS559+112 - FS570.00 REF CRJ200 SRM. ORIGINAL THICKNESS IS 0.110", REMAINING THICKNESS IS 0.87" MATERIAL LOSS IS 0.023" MAXIMUM Nov 19, 2019 · N875AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020010947587Seat Track · corrodedCARGO SEAT TRACK AT LBL9, FS559+112 - FS570.00 HAS CORROSION (C-CHECK) RO 01/07/2020 CARGO SEAT TRACK AT LBL9, FS559+112 - FS570.00 FOUND TO BE OUT OF LIMITS REF CRJ200 SRM. INSTALLED NEW SEAT TRACK PER BOMBARDIER REO. ALL STEPS COMPLIED WITH. SEE CONTINUE CANov 19, 2019 · N875AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020010947586Frame · corrodedAVIONICS BAY FS310.00 FWD AND AFT SIDE FRAME CORRODED BETWEEN STGR25L - STGR25R, MARKED (C-CHECK) RO 01/07/2020 BLENDED CORROSION. FOUND TO BE OUT OF LIMITS. INSTALLED NEW LOWER FRAME SECTOR FS310.00 REF CRJ-200 SRM AND BOMBARDIER. COMPLIED WITH TASK CARD.Nov 19, 2019 · N875AS · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2020010947585Frame · corrodedAVIONICS BAY FS333.00 FWD AND AFT SIDE FRAME CORRODED BETWEEN STGR26L - STGR26R, MARKED (C-CHECK) RO 01/07/2020 BLENDED CORROSION. OUT OF LIMITS. REPLACED FS333 FRAME SECTOR WITH NEW FRAME REF CRJ-200 SRM AND BOMBARDIER DWG. COMPLIED WITH TASK CARDNov 19, 2019 · N875AS · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2020010947584Frame · corrodedAVIONICS BAY FS349.00 FWD AND AFT SIDE FRAME CORRODED BETWEEN STGR26L - STGR25R, MARKED (C-CHECK) RO 01/07/2020 REPLACED FS349 FRAME SECTOR WITH NEW FRAME SECTORE REF CRJ-200 SRM AND DWG. COMPLIED WITH TASK CARDNov 19, 2019 · N875AS · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2020010947604Skin · dentedFUSELAGE DENT LOCATED NEAR UPPER FLANGE OF STGR24L AT 3.50" AFT OF FS 202.75 CANNOT BE DRESSED-BACK TO ORIGINAL COUNTOUR REFERENCING REO AS IT GOES INTO NON-MILLED SKIN UNDER, OR COMMON TO, STGR24L. (C-CHECK) RO 01/07/2020 PERFORMED PATCH REPAIR TO FUSELAGE DNov 18, 2019 · N875AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA2020010947583Floorbeam · corrodedTOP OTBD CORNER OF FLOOR BEAM NEXT TO RH SIDE SILL AT FS349.00 CORRODED, MARKED (C-CHECK) RO 01/07/2020 REMOVED CORROSION ON TOP OUTBOARD CORNER OF FLOOR BEAM RH AT FS 349.00 AND FOUND TO BE OUT OF LIMITS. REPAIRED PER REO. COMPLIED WITH TASK CARD. SEE CONTINNov 18, 2019 · N875AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA2020010947582Floor Support · corrodedRIGHT SIDE FLOOR SILL ANGLE AT FS319.00 HAS CORROSION, MARKED (C-CHECK) RO 01/07/2020 REMOVED CORROSION OH RH SIDE FLOOR SILL ANGLE AT FS319.00 REF CRJ 200 SRM. EVALUATED AND FOUND FLOOR SILL OUT OF LIMITS, REF CRJ 200 SRM. REPLACED RH SIDE FLOOR SILL ANGLE WNov 18, 2019 · N875AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020010947581Intercostal · corrodedTOP OF INTERCOSTAL CORRODED AT STGR21L BEWTEEN FS333.00 AND FS349.00, MARKED (C-CHECK) RO 01/07/2020 REMOVED CORROSION FROM TOP OF INTERCOSTAL AT STR 21 LH BETWEEN FS 333.00-349.00 REF CRJ 200 SRM. ORIGINAL MATERIAL THICKNESS IS 0.063" REF BOMBARDIER DWG. MINNov 18, 2019 · N875AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020010947580Floorbeam · corrodedAFT COCKPIT FLOOR SUPPORT ANGLE CORRODED AT FS280.00 (C-CHECK) RO 01/07/2020 REMOVED CORROSION FROM AFT FLOOR SUPPORT ANGLE AT F.S.280.00 IN REF CRJ200 SRM. MEASURED DEPTH OF BLEND OUT AT .028" WITH MICROMETER: TUC3939, DUE: 30-APR-20. ORIGINAL MATERIAL THICNov 18, 2019 · N875AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA2020010947579Floorbeam · corrodedFS280.00 BEAM BETWEEN RBL9 AND LBL9 CORRODED ACROSS THE TOP, MARKED (C-CHECK) RO 01/07/2020 REMOVED CORROSION ON TOP OF FS280.00 BEAM (FLOOR ANGLE) BETWEEN RBL9 AND LBL9, FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED NEW F.S.280.00 BEAM FILLER ANGLE P/N 60Nov 18, 2019 · N875AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA2020010947578Seat Track · corrodedRIGHT FLOOR SEAT RAIL FROM FS364.00 TO FS401.00 CORRODED MULTIPLE AREAS (C-CHECK) RO 01/07/2020 REMOVED CORROSION FROM FLOOR SEAT RAIL FROM RH SIDE FS364.00 TO FS401.00 REF CRJ200. FOUND TO BE OUT OF LIMITS REF CRJ200 SRM AND BSM. FABRICATED NEW SEAT TRACK RNov 18, 2019 · N875AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020010947577Seat Track · corrodedLEFT FLOOR SEAT RAIL FROM FS364.00 TO FS401.00 CORRODED MULTIPLE AREAS (C-CHECK) RO 01/07/2020 REMOVED CORROSION FROM FLOOR SEAT RAIL FROM FS364.00 TO FS401.00 ON L/H SIDE REF CRJ 200 SRM FOUND TO BE OUT OF LIMITS. FABRICATED NEW SEAT TRACK USING N126-2075,Nov 18, 2019 · N875AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020010947576Seat Track · corrodedRIGHT FLOOR SEAT RAIL FROM FS401.00 TO FS409+128 CORROSION IN MULTIPLE AREAS (C-CHECK) RO 01/07/2020 REMOVED CORROSION ON CARGO SEAT TRACK AT RBL9 FS559+112 - FS570.00 REF CRJ200 SRM. FOUND TO BE OUT OF LIMITS REF CRJ200 SRM (TOOL #8544 CAL DUE 30-SEP-20). RENov 18, 2019 · N875AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020010947575Floor Panel · corroded* R/H PRESSURE FLOOR SILL PANEL HAS MULTIPLE AREAS OF CORROSION BETWEEN FS 409.00 + 128 AND FS 559.00. (C-CHECK) RO 01/07/2020 REPAIRED THE R/H PRESSURE FLOOR SILL PANEL BETWEEN FS 409.00 + 128 AND FS 559.00. REF BOMBARDIER REO.Nov 18, 2019 · N875AS · Cndair CL6002B19 · Fuselage Floor Panel
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