N936EV

Service difficulty reports · 201

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 = 'N936EV' 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 SWIA202162974None · corroded*EVIDENCE OF CORROSION EXIST ON FLOOR SILL @STRG 17R BTW FS 589.00 AND FS 605.00. (C-CHECK RO 12-4-2021) BLENDED OUT CORROSION ON R/H FLOOR SILL BETWEEN FS589.00 AND FS605.00. REF. REO 601R-53-00-526 REV.-- DATED 05/22/2013 .FOUND TO BE IN LIMITS REF REOOct 14, 2021 · N936EV · Cndair CL6002B19 · DoorsSDR SWIA202162973None · corroded*EVIDENCE OF CORROSION EXIST ON FLOOR SILL @STRG 17R BTW FS 559.00 +64 AND FS 559.00 +112. (C-CHECK RO 12-4-2021) BLENDED OUT CORROSION ON R/H FLOOR SILL BETWEEN FS559.00+64 AND FS559.00+112. REF. REO 601R-53-00-526 REV.-- DATED 05/22/2013. FOUND TO BE OOct 14, 2021 · N936EV · Cndair CL6002B19 · DoorsSDR SWIA202162972None · corroded*EVIDENCE OF CORROSION EXIST IN MULTIPLE AREA @FS574.00 BTW STRG 24R AND 24L. (C-CHECK RO 12-4-2021) REMOVED AND REPLACED FS574 FRAME SECTION BETWEEN STR 25R TO STR 20L WITH A SPLICE REPAIR. REF REO 601R-53-61-7733 REV -- DATED 2021-10-28 & CRJ200 SRM 51Oct 14, 2021 · N936EV · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202163004None · damagedFABRICATE SEAT RAIL P/N 601R38312-25 TO BE INSTALLED ON JOB 2803881 OP.251 CAMP # 23640869 (C-CHECK RO 12-4-2021) FABRICATED AND INSTALLED SIDE SEAT RAIL P/N 601R38312-25 FROM EXTRUSION P/N 20276-288-0-0A, PO# T-59810. REF. REPAIR B OF REO 601R-53-00-05Oct 13, 2021 · N936EV · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202163003None · damagedFABRICATE SEAT RAIL P/N 601R38312-115 FOR INSTALLATION ON JOB 2803881 OP. 249 CAMP #23640844. (C-CHECK RO 12-4-2021) FABRICATED AND INSTALLED SIDE SEAT RAIL P/N 601R38312-115 FROM EXTRUSION P/N 20276-288-0-0A, PO# T-59810. REF. REPAIR B OF REO 601R-53-0Oct 13, 2021 · N936EV · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202162971None · corrodedINTERCOSTAL CORRODED BTWN FS'S 349/364 AND STGRS 27/26R (C-CHECK RO 12-4-2021) REMOVED AND REPLACED INTERCOSTAL WITH NEW SERVICABLE P/N 601R31049-10 REF CRJ-200 SRM 51-42-21, SRM 51-42-06 AND DWG. 601R31049 REV NC / COMPLIED WITH TASK CARD 51-900-1003-SKOct 13, 2021 · N936EV · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA202163002None · damaged* R/H SIDE SEAT RAIL MOUNTING CHANNEL SECTION AT APPROX FS 559.00 + 28 TO FS 559.00 + 80 HAS CLIP-NUT HOLE BROKEN OUT AT LOWER EDGE OF CHANNEL. (C-CHECK RO 12-4-2021) REMOVED AND REPLACED R/H SIDE SEAT RAIL MOUNTING CHANNEL SECTION AT APPROX FS 559.00 + Oct 12, 2021 · N936EV · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202163001None · damaged* R/H SIDE SEAT RAIL MOUNTING CHANNEL SECTION AT APPROX FS 495.00 TO FS 535.00 HAS CLIP-NUT HOLE BROKEN OUT AT LOWER EDGE OF CHANNEL. (C-CHECK RO 12-4-2021) ORDERED AND RECEIVED 1EA NEW RETAINER P/N: 601R38828-2 / REMOVED DAMAGED R/H SIDE SEAT RAIL RETAIOct 12, 2021 · N936EV · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202163000None · damaged* R/H SIDE SEAT RAIL MOUNTING CHANNEL SECTION AT APPROX. FS 443.00 TO FS 495.00 HAS CLIP-NUT HOLE BROKEN OUT AT LOWER EDGE OF CHANNEL. (C-CHECK RO 12-4-2021) REMOVED AND REPLACED RH SIDE SEAT RAIL MOUNTING CHANNEL SECTION FROM APPROX FS 443 TO FS 495 PEROct 12, 2021 · N936EV · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202162999None · corroded* R/H SIDE SEAT RAIL SECTION AT APPROX. FS 499.00 TO FS 548.00 HAS CORROSION SEVERAL PLACES. (C-CHECK RO 12-4-2021) REMOVED AND REPLACED R/H SIDE SEAT RAIL SECTION AT APPROX. FS 499.00 TO FS 548.00 REF: CRJ-200 AMM 53-01-11-000-802 & CRJ200 AMM 53-01-Oct 12, 2021 · N936EV · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202162998None · corroded* R/H SIDE SEAT RAIL SECTION AT APPROX. FS 449.85 TO FS 499.00 HAS CORROSION SEVERAL PLACES. (C-CHECK RO 12-4-2021) REMOVED CORROSION FOR RH SIDE SEAT RAIL PER REFENCE CRJ 200 SRM 51-21-06. FOUND SEAT RAIL TO BE OUT OF LIMITS. REMOVED AND INSTALLED NOct 12, 2021 · N936EV · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202162997None · corroded* R/H SIDE SEAT RAIL SECTION AT APPROX. FS 409.00 + 112 TO FS 449.95 HAS CORROSION SEVERAL PLACES. (C-CHECK RO 12-4-2021) REMOVED AND REPLACED R/H SIDE SEAT RAIL SECTION AT APPROX. FS 409.00+112 TO FS 449.95 REF: CRJ-200 AMM 53-01-11-000-802 & CRJ200 Oct 12, 2021 · N936EV · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202162996None · corroded* R/H SIDE SEAT RAIL SECTION AT APPROX. FS 409.00 + 16 TO FS 409.00 + 112 HAS CORROSION SEVERAL PLACES. (C-CHECK RO 12-4-2021) BLENDED OUT CORROSION ON R/H SIDE SEAT RAIL SECTION AT APPROX. FS 409.00 + 16 TO FS 409.00 + 112 IAW CRJ-200 SRM 51-21-06. /Oct 12, 2021 · N936EV · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202162995None · corroded* R/H SIDE SEAT RAIL MOUNTING CHANNEL SECTION AT APPROX. FS 364.00 TO FS 409.00 + 16 HAS CORROSION SEVERAL PLACES. (C-CHECK RO 12-4-2021) BLENDED OUT CORROSION ON RH SIDE SEAT RAIL RETAINER FROM FS 364 TO 409+16 AS MARKED REF CRJ 200 SRM 51-21-06 AND FOUOct 12, 2021 · N936EV · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202162994None · corroded* L/H SIDE SEAT RAIL MOUNTING CHANNEL SECTION AT APPROX. FS 443.00 TO FS 495.00 HAS CLIP-NUT HOLE BROKEN OUT AT LOWER EDGE OF CHANNEL. (C-CHECK RO 12-4-2021) REMOVED AND REPLACED DAMAGED SIDE SEAT RAIL MOUNTING CHANNEL AND INSTALLED NEW LH SIDE SEAT RAIOct 12, 2021 · N936EV · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202162993None · corroded* L/H SIDE SEAT RAIL SECTION AT APPROX. FS 548.00 TO FS 559.00 + 80 HAS CORROSION SEVERAL PLACES. (C-CHECK RO 12-4-2021) REMOVED LH SIDE SEAT RAIL FROM APPROX. FS 548.00 TO FS 559.00+80. REF: CRJ-200 AMM 53-01-11-000-802 AND INSTALLED NEW L/H SIDE SEAT ROct 12, 2021 · N936EV · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202162992None · corroded* L/H SIDE SEAT RAIL SECTION AT APPROX. FS 499.00 TO FS 548.00 HAS CORROSION SEVERAL PLACES. (C-CHECK RO 12-4-2021) BLENDED OUT CORROSION ON LH SIDE SEAT RAIL AS MARKED FS499.00 TO FS 548.00 REF CRJ 200 SRM 51-21-06.NO ALLOWABLE LIMITS GIVEN FOR SIDE SEOct 12, 2021 · N936EV · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202162991None · corroded* L/H SIDE SEAT RAIL SECTION AT APPROX. FS 449.95 TO FS 499.00 HAS CORROSION SEVERAL PLACES. (C-CHECK RO 12-4-2021) REMOVED AND REPLACED LH SIDE SEAT RAIL FROM APPROX. FS 449.95 TO FS 499.00 REF: CRJ-200 AMM 53-01-11-400-802. SEE CONTINUATION CARD FOR DEOct 12, 2021 · N936EV · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202162990None · corroded* L/H SIDE SEAT RAIL SECTION AT APPROX. FS 409.00 + 16 TO FS 409.00 + 112 HAS CORROSION SEVERAL PLACES. (C-CHECK RO 12-4-2021) BLENDED OUT CORROSION ON LH SIDE SEAT RAIL AS MARKED FS 409+16 TO FS 409+112 REF CRJ 200 SRM 51-21-06.NO ALLOWABLE LIMITS GIVENOct 12, 2021 · N936EV · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202162989None · corroded* L/H SIDE SEAT RAIL SECTION AT APPROX. FS 364.00 TO FS 409.00 + 16 HAS CORROSION SEVERAL PLACES. (C-CHECK RO 12-4-2021) BLENDED OUT CORROSION ON LH SIDE SEAT RAIL AS MARKED FS 364 TO 409+16 REF CRJ 200 SRM 51-21-06.NO ALLOWABLE LIMITS GIVEN FOR SIDE SEOct 12, 2021 · N936EV · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202162988None · corroded* L/H SIDE SEAT RAIL SECTION AT APPROX. FS 409.00 + 112 TO FS 449.95 HAS CORROSION SEVERAL PLACES. (C-CHECK RO 12-4-2021) BLENDED L/H SIDE SEAT RAIL SECTION AT APPROX. FS 409+112 TO FS 449.95 CRJ 200 SRM 51-21-06.FOUND TO BE OUT OF LIMITS REF CRJ-200 SROct 12, 2021 · N936EV · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202162987None · wornR/H INBD FLAP #3 (OTBD) FLAP VANE ACTUATOR HAS ABRASION DAMAGE ON THE BOTH GUIDE TRACKS AND TWO WORN CARRIAGE BEAM BUSHINGS. (C-CHECK RO 12-4-2021) BLENDED R/H INBD FLAP #3 (OTBD) FLAP VANE ACTUATOR HAS ABRASION DAMAGE ON THE BOTH GUIDE TRACKS AND TWO WOOct 12, 2021 · N936EV · Cndair CL6002B19 · Aileron TabsSDR SWIA202162986None · wornR/H INBD FLAP #2 (MID) FLAP VANE ACTUATOR HAS ABRASION DAMAGE ON THE BOTH GUIDE TRACKS AND TWO WORN CARRIAGE BEAM BUSHINGS. (C-CHECK RO 12-4-2021) / BLENDED R/H INBD FLAP #2 (MID) FLAP VANE ACTUATOR HAS ABRASION DAMAGE ON BOTH GUIDE TRACKS AND TWO WORN Oct 12, 2021 · N936EV · Cndair CL6002B19 · AileronsSDR SWIA202162985None · wornR/H INBD FLAP #1 (INBD) FLAP VANE ACTUATOR HAS ABRASION DAMAGE ON THE BOTH GUIDE TRACKS, TWO WORN CARRIAGE BEAM BUSHINGS, AS WELL AS A CORRODED INBD SPRING AND HARDWARE. (C-CHECK RO 12-4-2021) BLENDED R/H INBD FLAP #1 (INBD) FLAP VANE ACTUATOR HAS ABRAOct 12, 2021 · N936EV · Cndair CL6002B19 · AileronsSDR SWIA202162970None · cracked* L/H WHEEL WELL HAS WS48.30 CAP ANGLE ATTACHED TO LOWER SIDE OF UPPER WING SKIN CRACKED. (C-CHECK RO 12-4-2021) REMOVED AND REPLACED WITH NEW CAP ANGLE AT LH SIDE WS48.30 PN:600-10389-1 REF CRJ200 SRM 51-42-21 AND DWG:600-10212, REV -D. COMPLIED WITH 5Oct 12, 2021 · N936EV · Cndair CL6002B19 · Fuselage Structure (General)SDR SWIA202162969None · cracked* CARGO NET SUPPORT BEAM AFT LOWER ATTACHMENT BRACKET AT FS 621.00 BULKHEAD CRACKED. (C-CHECK RO 12-4-2021) INSTALLED NEW BRACKET AT FS 621.00 BULKHEAD CARGO NET SUPPORT BEAM AFT LOWER ATTACHMENT. REF CRJ-200 SRM 51-42-21 AND DWG 601R35050 REV Y. COMPLIEOct 12, 2021 · N936EV · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202162968None · cracked* CLIP CRACKED ON INTERCOSTAL AT FS 484.00 LBL 36. (C-CHECK RO 12-4-2021) REMOVED AND REPLACED LBL36 INTERCOSTAL CLIP @ FS484. REF REO 601R-53-41-059 REV -C DATED 2020-03-11. COMPLIED WITH TASK CARD 51-900-1003-SKY.Oct 12, 2021 · N936EV · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA202162967None · cracked* CLIP CRACKED ON INTERCOSTAL AT FS 484.00 LBL 27. (C-CHECK RO 12-4-2021) RE MOVED AND REPLACED CLIP ON INTERCOSTAL AT FS 484.00 LBL 27 PART NUMBER .601R31171-17 REF. PREVIOUSLY INCORPERATED REO 601R-53-41-059 REV-C DATE 2020-03-11. COMPLIED WITH 51-900-Oct 12, 2021 · N936EV · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA202163021None · corrodedRH OUTB FLAP, OUTB HINGE ARM ASSY HAS EVIDENCE OF CORRODED HARDWARE AT FWD ATTACH BOLT STOP PLATES, LEFT AND RIGHT SIDES. (FLAGGED) (C-CHECK RO 12-4-2021) REMOVED 4 EA. CORRODED BOLTS ON OUTBOARD FLAP HINGE ARM ATTACH POINT LH & RH STOP PLATES AND REPLAOct 11, 2021 · N936EV · Cndair CL6002B19 · Aileron TabsSDR SWIA202163020None · corroded#1 RH OUTB FLAP HINGE BOX 3 EA ATTACHING HARDWARE TO AIRFRAME HAS EVIDENCE OF CORROSION. (FLAGGED) (C-CHECK RO 12-4-2021) REMOVED 3 EA. CORRODED NUTS AND WASHERS AT MOUNT BOLTS ON OUTBOARD FLAP HINGE BOX ASSEMBLY AT WS178.00 AND REPLACED WITH NEW HARDWAROct 11, 2021 · N936EV · Cndair CL6002B19 · AileronsSDR SWIA202163019None · corroded#1 RH OUTB FLAP HINGE BOX SPRING HAS EVIDENCE OF CORROSION. (C-CHECK RO 12-4-2021) REMOVED BUTE DOOR ACTUATOR ON HINGE BOX AT WS178.00 TO FOM. REF. CRJ200 AMM 27-54-25-000-801 AND REINSTALLED BUTE DOOR ACTUATOR ON HINGE BOX AT WS178.00. REF. CRJ200 AMM 2Oct 11, 2021 · N936EV · Cndair CL6002B19 · Aileron TabsSDR SWIA202163018None · corroded#2 RH INB FLAP HINGE ARM HAS ALL 4 EA CASTLE NUTS SHOWING EVIDENCE OF CORROSION. (FLAGGED) (C-CHECK RO 12-4-2021) REMOVED CORRODED CASTLE NUTS AND INSTALLED NEW CASTLE NUTS RIGHT INBOARD FLAP HINGE ARM WS127.25 REF CRJ 200 AMM 57-52-08-400-802. TORQUE WROct 10, 2021 · N936EV · Cndair CL6002B19 · AileronsSDR SWIA202163017None · corroded#1 LEFT INB FLAP HINGE, FWD LUG CASTLE NUT SHOWING SIGNS OF CORROSION. (FLAGGED) (C-CHECK RO 12-4-2021) REMOVED AND REPLACED LH INBOARD #1 FLAP HINGE FWD HARDWARE (NUT AND COTTER PIN) REF: CRJ200 SRM 51-41-02. TUC1260 DUE: 31-AUG-22Oct 10, 2021 · N936EV · Cndair CL6002B19 · AileronsSDR SWIA202163016None · corroded#2 LEFT INB FLAP HINGE, FWD LUG CASTLE NUT SHOWING SIGNS OF CORROSION. (FLAGGED) (C-CHECK RO 12-4-2021) REMOVED AND REPLACED LH INBOARD #2 FLAP HINGE FWD HARDWARE (NUT AND COTTER PIN) REF: CRJ200 SRM 51-41-02. TUC1260 DUE: 31-AUG-22Oct 10, 2021 · N936EV · Cndair CL6002B19 · AileronsSDR SWIA202163015None · corroded#1 LEFT OUTBOARD FLAP HINGE BOX SPRING, FORWARD ATTACH HARDWARE HAS CASTLE NUT SHOWING EVIDENCE OF CORROSION. (C-CHECK RO 12-4-2021) REMOVED CORRODED CASTLE NUT AND INSTALLED NEW CASTLE NUT LEFT OUTBOARD FLAP HINGE BOX SPRING/ACTUATOR ASSEMBLY WS178.00 ROct 10, 2021 · N936EV · Cndair CL6002B19 · AileronsSDR SWIA202163014None · corroded#1 LH OUTBOARD FLAP HINGE BOX, AFT MOUNT CASTLE NUTS SHOWING EVIDENCE OF CORROSIN. (FLAGGED) (C-CHECK RO 12-4-2021) REMOVED 2 EA. CORRODED NUTS AT AFT MOUNT BOLTS ON LH OUTBOARD FLAP HINGE BOX ASSEMBLY AT WS178.00 AND REPLACED WITH NEW HARDWARE (2 EA. NUOct 10, 2021 · N936EV · Cndair CL6002B19 · Aileron TabsSDR SWIA202163013None · corroded* L/H AND R/H, INB AND OBD ELEVATOR FLUTTER DAMPERS HAVE CORRODED ATTACHMENT HARDWARE NUTS AT ROD END. (C-CHECK RO 12-4-2021) REPLACED CORRODED NUTS (4 EA.) AT LH AND RH INBD AND OTBD ELEVATOR FLUTTER DAMPER RODENDS WITH NEW NUTS. (4 EA.). REF. CRJ200 AMOct 10, 2021 · N936EV · Cndair CL6002B19 · Elevator Tab, Attach FittingsSDR SWIA202163012None · corroded#1 LEFT OUTBOARD FLAP HINGE BOX SPRING SHOWING EVIDENCE OF CORROSION. (C-CHECK RO 12-4-2021) REMOVED L/H BUTE DOOR ACTUATOR ON HINGE BOX ASSEMBLY AT WS178.00 TO FOM. REF. CRJ 200 AMM 27-54-25-000-801.AND REINSTALLED L/H BUTE DOOR ACTUATOR ON HINGE BOX AOct 10, 2021 · N936EV · Cndair CL6002B19 · Aileron TabsSDR SWIA202163011None · corroded#2 LEFT OUTBOARD FLAP HINGE BOX AFT, OUTBOARD, ATTACHED CASTLE NUT HARDWARE SHOWING EVIDENCE OF CORROSION. (FLAGGED) (C-CHECK RO 12-4-2021) REMOVED CORRODED AFT OUTBOARD CASTLE NUT LEFT FLAP HINGE BOX WS220.00 AND INSTALLED NEW CASTLE NUT REF CRJ 200 AMOct 10, 2021 · N936EV · Cndair CL6002B19 · Aileron TabsSDR SWIA202162966None · dentedL/H INBD FLAP (P/N: 601R14002-1 S/N: SBRJ1075) LWR SKIN IS DENTED IN 5 LOCATIONS IN ADDITION TO A PREVIOUS REPAIR. REPAIR L/H INBD FLAP LWR SKIN DAMAGE. (C-CHECK RO 12-4-2021) REMOVED & REPLACED LOWER I/B SKIN P/N 601R14008-45S & LOWER O/B SKIN P/N 601R1Oct 10, 2021 · N936EV · Cndair CL6002B19 · AileronsSDR SWIA202163010None · corrodedLH SPOILERON PCUS HAS RUSTED HARDWARE AT MOUNTING POINTS (C-CHECK RO 12-4-2021) REPLACED RUSTED HARDWARE WITH NEW HARDWARE LEFT SPOILERON PCU MOUNT POINTS REF CRJ 200 AMM 27-62-01-400-801 STEPS 2. B. (6) THRU (7) TORQUE WRENCH TUC5659 CAL DUE 28 FEB 20Oct 9, 2021 · N936EV · Cndair CL6002B19 · Wing StructureSDR SWIA202163009None · corrodedLH FLIGHT SPOILER PCUS HAS RUSTED HARDWARE AT MOUNTING POINTS (C-CHECK RO 12-4-2021) REPLACED RUSTY HARDWARE WITH NEW HARDWARE LEFT FLIGHT SPOILER PCU MOUNT POINTS REF CRJ 200 AMM 27-62-01-400-801 STEP 2. B. (6) THRU (7). TORQUE WRENCH TUC5689 CAL DUE 28Oct 9, 2021 · N936EV · Cndair CL6002B19 · Wing StructureSDR SWIA202163008None · corrodedLH OUTBOARD GROUND SPOILER PCU HAVE RUSTED HARDWARE FOR MOUNTING AND HINGE POINTS (C-CHECK RO 12-4-2021) REPLACED RUSTED HARDWARE WITH NEW HARDWARE LEFT OUTBOARD GROUNG SPOILER PCU FORK END AND HINGE LINK REF CRJ 200 AMM 27-63-01-400-801 STEP 2. B. (3)Oct 9, 2021 · N936EV · Cndair CL6002B19 · Wing StructureSDR SWIA202163007None · corrodedLH INBOARD GROUND SPOILER PCU HAVE RUSTED HARDWARE FOR MOUNTING AND HINGE POINTS (C-CHECK RO 12-4-2021) REPLACED RUSTY HARDWARE WITH NEW HARDWARE LEFT INBOARD GROUND SPOILER PCU FORK END AND HINGE LINK REF CRJ 200 AMM 27-63-01-400-801 STEP 2. B. (3) THOct 9, 2021 · N936EV · Cndair CL6002B19 · Wing StructureSDR SWIA202162965None · chafedRH AILERON UPPER AND LOWER FIXED LEADING-EDGE SKIN IS CHAFED IN NUMEROUS LOCATIONS AS MARKED. (C-CHECK RO 12-4-2021) REMOVED AND INSTALLED NEW RH AILERON UPPER FIXED LEADING-EDGE SKIN. REF: CRJ200 SRM 51-42-22, CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-21 AOct 9, 2021 · N936EV · Cndair CL6002B19 · Aileron TabsSDR SWIA202163006None · corrodedL/H AILERON INBD AND OTBD PCU ATTACH POINT HDWR HAS CORRODED COTTER PINS (C-CHECK RO 12-4-2021) REMOVED 2 EACH RUSTED COTTER PINS AND INSTALLED 2 EACH NEW COTTER PINS AT THE LH AILERON INBD/OTBD PCU ATTACH POINT HARDWARE. REF - CRJ 200 AMM 20-24-00-910-8Oct 8, 2021 · N936EV · Cndair CL6002B19 · Wing StructureSDR SWIA202162964None · damagedLEFT OVERWING EMER EXIT DOOR - FWD AND AFT HINGE FITTINGS AND ADJACENT LOWER DOOR SKIN EDGES DAMAGED (C-CHECK RO 12-4-2021) REPAIRED L/H OVERWING EMER EXIT DOOR - FWD AND AFT HINGE FITTINGS AND ADJACENT LOWER DOOR SKIN EDGES REF REO 601R-52-21-128 REV --Oct 7, 2021 · N936EV · Cndair CL6002B19 · Fuselage Structure (General)SDR SWIA202162963None · dented*RH INBD FLAP LOWER SKIN HAS 3EA DENTS (MARKED) (C-CHECK RO 12-4-2021) FOUND THE DENT ON RH INBD FLAP LOWER SKIN HAS 3EA DENTS OUT OF LIMITS REF CRJ 200 SRM57-52-00 . REPAIR RIGHT I/B FLAP REF: REO 601R-57-52-678 REV-C DATE 2012/10/19 . COMPLIED WITH ALOct 4, 2021 · N936EV · Cndair CL6002B19 · AileronsSDR SWIA202162962None · corroded* GALLEY SERVICE DOOR LOWER AFT PAN CORRODED ON LOWER SIDE. (C-CHECK RO 12-4-2021) REMOVED AND REPLACED THE GALLEY SERVICE DOOR LOWER AFT PAN REF CRJ 200 SRM 51-42-06, CRJ 200 SRM 51-42-21,CRJ 200 SRM 51-42-13, & DWG 601R38304 REV BM. COMPLIED WITH SKYWOct 3, 2021 · N936EV · Cndair CL6002B19 · Galley DoorsSDR SWIA202162961None · corroded* GALLEY SERVICE DOOR LOWER FWD PAN CORRODED ON LOWER SIDE. (C-CHECK RO 12-4-2021) REMOVED AND REPLACED THE GALLEY SERVICE DOOR LOWER FWD PAN REF CRJ 200 SRM 51-42-06, CRJ 200 SRM 51-42-21,CRJ 200 SRM 51-42-13, & DWG 601R38304 REV BM. COMPLIED WITH SKYWOct 3, 2021 · N936EV · Cndair CL6002B19 · Galley Doors
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