N868AS

Part: TRACK — GOUGED · airframe 42,000 hrs · 39,319 cycles

CARGO DOOR AFT TRACK HAS A GOUGE ON UPPER PORTION ABOUT 1/2 INCH LONG. DUE TO CARGO DOOR TRACK ATTACH POINT (AFT BULKHEAD). THIS HAS BEEN DETERMINED TO BE A MAJOR REPAIR. FORM M-337 WILL BE REQUIRED. (FILED CLOSED) REMOVED AND REPLACED AFT TRACK P/N 601R35066-5 ON AFT CARGO DOOR REF CRJ200 SRM 51-42-06 AND 51--77-00. COMPLIED WITH STRUCTURAL MAJOR REPAIR RII 51-900-1003-SKY AND FORM M-337. SEE CAMP 23629182 FOR LEAK CHECK.

Part: HANDLE — OUT OF ADJUST (PAX DOOR) · airframe 41,686 hrs · 39,038 cycles

PASSENGER DOOR WARNING ON CLIMB OUT. ON LANDING DOOR HANDLE WAS NOT FULLY STOWED. (FLIGHT 4643 - FILED CLOSED) FOUND THE LOCK/UNLOCK INDICATOR PUSH-ROD NOT ADJUSTED CORRECTLY PUTTING A PRELOAD ON THE OUTER HANDLE. ADJUSTED THE LOCK/UNLOCK INDICATOR PUSH-ROD IN REF TO AMM 52-11-21. OPS CHECK GOOD. ALL DOOR INDICATIONS NORMAL.

Part: SEAT TRACK — BROKEN (ZONE 200) · airframe 40,854 hrs · 38,316 cycles

SEAT TRACK FLOOR FITTING PART NUMBER CDSP1900-17 FOR CENTER 9G BULKHEAD ASSEMBLY IS BUSTED. C-CHECK RO 1/16/2021. ORDERED AND RECEIVED NEW SEAT TRACK FLOOR FITTING PART CDSP1900-17 FOR CENTER 9G BULKHEAD ASSEMBLY. INSTALLATION OF NEW FITTING INSTALLED ON JOB 2747460 OP 509 MX TRANS 21824491.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 40,854 hrs · 38,316 cycles

CORROSION FOUND ON SEAT TRACK LBL 9, APPROXIMATELY FS 559.+112. C-CHECK RO 1/16/2021. REMOVED AND REPLACED SEAT TRACK, REF CRJ 200 AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 40,854 hrs · 38,316 cycles

CORROSION FOUND ON SEAT TRACK, LBL 9 APPROXIAMTELY FS 559+4. C-CHECK RO 1/16/2021. REMOVED AND REPLACED SEAT TRACK, REF CRJ 200, AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 40,854 hrs · 38,316 cycles

CORROSION FOUND ON SEAT TRACK, RBL 9, FS 559.112. C-CHECK RO 1/16/2021. REMOVED DAMAGED SEAT TRACK AT RBL 9, FS 559.112, REF CRJ 200, AMM 53-01-11-000-802. INSTALLED NEW SEAT TRACK P/N 601R38779-49 AT RBL 9, FS 559.112, REF CRJ 200, AMM 53- 01-11-400-802, TOOL USED TUC6038, CAL DUE DATE: 31- MAY-21.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 40,854 hrs · 38,316 cycles

CORROSION FOUND SEAT TRACK RBL 9, FS 559.+96. C-CHECK RO 1/16/2021. REMOVED DAMAGED SEAT TRACK AT RBL 9, FS 559 +96, REF CRJ 200, AMM 53-01-11-000-802. INSTALLED NEW SEAT TRACK P/N 601R38779-13 AT RBL 9, FS 559. +96, REF CRJ 200, AMM 53- 01-11-400-802, TOOL USED TUC6038, CAL DUE DATE: 31- MAY-21.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 40,854 hrs · 38,316 cycles

PASSENGER SEAT TRACK P/N 601R31032-21 CORRODED AT RBL 9.0 FROM FS 409.00 TO FS 409.00+118, MARKED. C-CHECK RO 1/16/2021. REPLACED RBL 9 FLOOR SEAT TRACK FROM FS 409.00 TO FS 409.00+118 USING TOOL TUC 5657 CAL DUE 31-MAR-21, REF CRJ-200-AMM 53-01-11-400-802. SEE CONTINUATION CARD FOR DETAILS.

Part: FLOOR SUPPORT — BROKEN (ZONE 200) · airframe 40,854 hrs · 38,316 cycles

FLOOR BEAM HAS BROKEN AT LBL 9, FS 559.00+48-FS 559.00+64. C-CHECK RO 1/16/2021. REMOVED AND REPLACED NEW FLOOR BEAM WEB P/N 601R31119-61 AT LBL 9 FS 559.00+48-FS 559.00 +64, REF CRJ200 SRM 51-42-06 AND DWG 601R31119 REV-H. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: HINGE BOX — GOUGED (RT WING) · airframe 40,854 hrs · 38,316 cycles

RT WING INBD FLAP, HINGE BOX AT WS 80.50, AFT OUTBOARD ATTACH LUG ON THE WING IS GOUGED, MARKED. C-CHECK RO 1/16/2021. REPAIRED RT WING INBD FLAP, HINGE BOX AT WS 80.50, AFT OUTBOARD ATTACH LUG, REF REO 601R-57-21-3401, REV-, DATE 2021-01-11. SEE CONTINUATION CARD FOR DETAILS.

Part: STRINGER CLIP — CRACKED (ZONE 200) · airframe 40,854 hrs · 38,316 cycles

CLIP ATTACHING STRINGER 3L TO FS 280 BULKHEAD IS CRACKED. C-CHECK RO 1/16/2021. REMOVED AND REPLACED CLIP AT FS 280.00 AT STRINGER 3L, IAW CRJ 200 SRM 51-42-06 DRAWING 600-34017 REV AD. COMPLIED WITH 51-900-1003-SKY.

Part: POST — DAMAGED (FUSELAGE) · airframe 40,854 hrs · 38,316 cycles

FS 409+128 BL 0 RT VERTICAL POST FWD RADIUS DEFECT NOTED. C-CHECK RO 1/16/2021. REMOVED AND INSTALLED NEW POST ASSEMBLY (LT & RT), AND NEW (LT & RT) SUPPORT ANGLES AT FS 409 +128 BL 0, REF CRJ 200 SRM 51-42-06 AND REO 601R-53-41-889 REV B DATED 2017-03-06, CRJ-200-SRM 51-42-06, AND DWG 601R32208 REV H. COMPLIED WITH 51-900-1003-SKY. SEE CONTINUATION CARD FOR DETAILS.

Part: SUPPORT BEAM — CRACKED (CARGO DOOR TRACK) · airframe 40,854 hrs · 38,316 cycles

CARGO DOOR SURROUND TRACK SUPPORT BEAM BRACKET AT FS 574 CRACKED. C-CHECK RO 1/16/2021. REMOVED AND REPLACED NEW BRACKET PART NUMBER 601R35050-121, IAW CRJ200 SRM 51-42-21.

Part: SUPPORT BEAM — CHAFED (CARGO DOOR TRACK) · airframe 40,854 hrs · 38,316 cycles

CARGO DOOR SURROUND TRACK SUPPORT BEAM FORWARD OF FS 621 CHAFED FROM CABLE. C-CHECK RO 1/16/2021. REMOVED AND REPLACED NEW CARGO DOOR SURROUND-TRACK SUPPORT BEAM FORWARD OF FS 621.00, CRJ 200 SRM 51-40-11, SRM 51-42-21. SEE ATTACHED CONTINUATION CARD FOR DETAILS.

Part: SKIN — CRACKED (LT TRU BAY) · airframe 40,854 hrs · 38,316 cycles

LT TRU BAY DOOR AFT LATCH CUT-OUT ON FUSELAGE HAS A CRACK. C-CHECK RO 1/16/2021. INSTALLED NEW LT TRU LANDING SKIN PANEL P/N 600-33052-145, REF BOMBARDIER ENG DWG 600-33052 REV Y AND CRJ 200 SRM 51-42-06. COMPLIED WITH 51-900-1003-SKY.

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 40,854 hrs · 38,316 cycles

INTERCOSTAL BETWEEN FS 621 AND FS 625 AT STR 14L IS CRACKED. C-CHECK RO 1/16/2021. REMOVED AND INSTALLED NEW INTERCOSTAL AT STR 14L BETWEEN FS 621 AND FS 625 WITH NO FILLERS, REF CRJ-200-SRM 51-42-21, REO 601R-53-61-422 REV NC, DATED 2001-08-23, AND REO 601R-53-61-100 REV A, DATED 2008-01-23. COMPLIED WITH 51-900-1003-SKY. SEE CONTINUATION CARD FOR DETAILS.

Part: HINGE FITTING — DAMAGED (RT ELEVATOR) · airframe 40,854 hrs · 38,316 cycles

UPON REMOVAL OF RT ELEVATOR HINGE FITTING BEARING BORE WAS FOUND TO BE PITTED AND REQUIRES REPLACEMENT. HINGE FITTING PN IS 600-24043-1. C-CHECK RO 1/16/2021. REMOVED AND REPLACED RT ELEVATOR HINGE FITTING P/N 600-24043-1, REF BOMBARDIER DWG. 601R24025, REV (G) CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-21. COMPLIED WITH SKYCARD 51-900-1003-SKY.

Part: HINGE BOX — CORRODED (RT WING) · airframe 40,854 hrs · 38,316 cycles

RT OUTBOARD FLAP HINGE BOX, FORWARD ATTACH FITTING ON WS 220.00, INBOARD AND OUTBOARD FORWARD ATTACH BOLTS ARE CORRODED. C-CHECK RO 1/16/2021. REMOVED AND REPLACED WITH NEW 2 EA BOLTS AND 2 EA WASHERS AT RT OUTBOARD FLAP HINGE BOX, FORWARD ATTACH FITTING ON WS 220.00, INBOARD AND OUTBOARD FORWARD ATTACH BOLTS, REF CRJ 200 AMM 57-21-37-000-802 AND CRJ-200-AMM 57-21-37-400-802 TUC4822 DUE 30-APR-21. LEAK CHECK GOOD AND SEE CONTINUATION CARD FOR DETAILS.

Part: VANE — DAMAGED (RT WING TE FLAP) · airframe 40,854 hrs · 38,316 cycles

REPLACE RT WING INBOARD FLAP VANE INBOARD LEADING EDGE. C-CHECK RO 1/16/2021. REPLACED RT WING INBOARD FLAP VANE INBOARD LEADING EDGE WITH A SERVICEABLE UNIT, REF CRJ-200 SRM 51-42-13, CRJ-200 SRM 51-40-11, AND DWG 601R14303 REV J. COMPLIED WITH TASK CARD 51-900-1003-SKY, SEE CONTINUATION CARD FOR DETAILS.

Part: VANE — DAMAGED (RT WING TE FLAP) · airframe 40,854 hrs · 38,316 cycles

REPLACE RT WING INBOARD FLAP VANE CENTER OUTBOARD LEADING EDGE. C-CHECK RO 1/16/2021. REMOVED AND REPLACED RIGHTHAND WING INBOARD FLAP VANE CENTER SKIN OUTBOARD LEADING EDGE, IAW CRJ200 SRM 51-42-13 AND DRAWING 601R14303 REV J. SEE CONTINUATION FOR FUTHER DETAILS. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY.

Part: HINGE BOX — CORRODED (RT WING) · airframe 40,854 hrs · 38,316 cycles

RT OUTBOARD FLAP HINGE BOX, FORWARD ATTACH FITTING ON WS 264.00, OUTBOARD FORWARD ATTACH BOLT IS CORRODED. C-CHECK RO 1/16/2021. REMOVED AND REPLACED 1 EA BOLT AND 1 EA WASHER AT RT OUTBOARD FLAP HINGE BOX, FORWARD ATTACH FITTING ON WS 264.00, OUTBOARD FORWARD ATTACH BOLT, REF CRJ 200 AMM 57-21-37-000-803 AND CRJ-200-AMM 57-21-37-400-803 TUC4822 DUE 30-APR-21. LEAK CHECK GOOD AND SEE CONTINUATION CARD FOR DETAIL.

Part: VANE — DAMAGED (RT WING TE FLAP) · airframe 40,854 hrs · 38,316 cycles

REPLACE RT WING INBOARD FLAP VANE OUTBOARD LEADING EDGE. C-CHECK RO 1/16/2021. REPLACED RT WING INBOARD FLAP VANE ONBOARD LEADING EDGE WITH A SERVICEABLE UNIT, REF CRJ-200 SRM 51-42-13, CRJ-200-SRM 51-40-11, AND DWG 601R14303 REV J. COMPLIED WITH TASK CARD 51-900-1003-SKY. SEE CONTINUATION CARD FOR DETAILS.

Part: FLOOR SUPPORT — CORRODED (PRESSURE DECK) · airframe 40,854 hrs · 38,316 cycles

MULTIPLE AREAS OF CORROSION ON LT PRESSURE FLOOR SILL PANEL. C-CHECK RO 1/16/2021. REPAIRED LT PRESSURE FLOOR SILL PANEL, REF REO 601R-53-41-666 REV C DATED 2012-11-06, REO 601R-53-41-2825 REV- DATED 2021-01-05 AND CRJ-200-SRM 51-21-06. COMPLIED WITH 51-900-1003-SKY. SEE CONTINUATION CARD FOR DETAILS. PRESSURE CHECK GOOD.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 40,854 hrs · 38,316 cycles

RT SEAT RAIL STRUCTURE FROM FS 349.0 TO FS 559+80 HAS SEVERAL AREAS OF CORROSION. C-CHECK RO 1/16/2021. BLENDED CORROSION AT RT SEAT RAIL STRUCTURE FROM FS 349.0 TO FS 559.0+80, IAW CRJ200 SRM 51-25-16. CORROSION AREA BETWEEN FS 548 TO FS 559+40 OUT OF LIMITS. REPLACED SEAT TRACK SECTION FOR FS 548 TO FS 559+40, REF REO 601R-53-00-055 REV C DATED 2017-03-21 REPAIR B STEP 2 AND CRJ-200-AMM 53-01-11-400-802. SEE CONTINUATION CARD FOR DETAILS.

Part: FLOOR SUPPORT — CORRODED (PRESSURE DECK) · airframe 40,854 hrs · 38,316 cycles

MULTIPLE AREAS OF CORROSION ON RT PRESSURE FLOOR SILL PANEL. C-CHECK RO 1/16/2021. REPAIRED RT PRESSURE FLOOR SILL PANEL, REF REO 601R-53-41-666 REV C DATED 2012-11-06 AND REO 601R-53-41-2825 REV - DATED 2021-01-05. PRESSURE CHECK GOOD. COMPLIED WITH 51-900-1003-SKY. SEE CONTINUATION CARD FOR DETAIL.

Part: FRAME — CRACKED (ZONE 100) · airframe 40,854 hrs · 38,316 cycles

CLIP CRACKED ON TOP FLANGE OF FRAME AT FS 589 BETWEEN STGR 26R AND STGR 25R. C-CHECK RO 1/16/2021. REMOVED AND REPLACED CLIP ON TOP FLANGE OF FRAME AT FS 589 BETWEEN STGR 26R AND STGR 25R, REF CRJ 200 SRM 51-42-06.

Part: PLATE — CORRODED (PAX DOOR FRAME) · airframe 40,854 hrs · 38,316 cycles

PLATE ON FRAME AT FS 310 HAS CORROSION ABOVE SERRATED PLATE FOR PASSENGER DOOR FORWARD ANCHOR FITTING. C-CHECK RO 1/16/2021. REMOVED AND INSTALLED NEW FABRICATED GUSSET PLATE P/N 601R31109-97 AT FS 310, REF CRJ-200 SRM 51-42-06 AND DRAWING 601R31109 REV F. COMPLIED WITH 51-900-1003-SKY. SEE CONTINUATION CARD FOR DETAILS.

Part: DOUBLER — CORRODED (ZONE 200) · airframe 40,854 hrs · 38,316 cycles

SERVICE DOOR SURROUND LOWER DOUBLER HAS CORROSION AT FS 319. C-CHECK RO 1/16/2021. REMOVED CORROSION FROM SERVICE DOOR SURROUND LOWER DOUBLER. STRUCTURALLY ACCEPTABLE, REF REO601R-53-21-3368 REV- 2020-12-05 AND CRJ200 SRM 51-21-06. COMPLIED WITH 51-900-1003-SKY. SEE CONTINUATION CARD FOR DETAILS.

Part: SKIN — CORRODED (ZONE 100) · airframe 40,854 hrs · 38,316 cycles

CORROSION ON EXTERNAL SKIN AT BETWEEN FS 559+80 AND FS 559+112 AND BETWEEN STR 26L AND STR 26R, AREA MARKED. C-CHECK RO 1/16/2021. REMOVED CORROSION ON EXTERNAL SKIN AT BETWEEN FS 559+80 AND FS 559+112 AND BETWEEN STR 26L AND STR 26R, REF CRJ-200-SRM 51-21-06. BLENDED AREA FOUND TO BE OUT OF LIMITS, REF CRJ 200 SRM 53-00-31. REPAIRED EXTERNAL SKIN AT BETWEEN FS 559+80 AND FS 559+112 AND BETWEEN STR 26L AND STR 26R, REF REO-601R-53-51-538 REV- 2020-12-07. SEE CONTINUATION CARD FOR DETAILS.

Part: SKIN — CORRODED (ZONE 100) · airframe 40,854 hrs · 38,316 cycles

CORROSION ON EXTERNAL SKIN AT BETWEEN FS 559+32 AND FS 559+48 AND BETWEEN STR 26L AND STR 26R, LOCATIONS MARKED. C-CHECK RO 1/16/2021. REPAIRED DAMAGE ON EXTERNAL SKIN AT BETWEEN FS 559+32 AND FS 559+48 AND BETWEEN STR 26L AND STR 26R, IAW REO 601R-53-51-538 REV- DATE 2020-12-07.

Part: SKIN — CORRODED (ZONE 100) · airframe 40,854 hrs · 38,316 cycles

CORROSION ON EXTERNAL SKIN AT APPROXIMATELY FS 559+16 AND BETWEEN STR 26L AND STR 26R, MARKED. C-CHECK RO 1/16/2021. REPAIRED CORROSION ON EXTERNAL SKIN AT FS 559+16 AND BETWEEN STR 26L AND STR 26R, REF REO 601R-53-51-538 REV- DATED 2020-12-07. COMPLIED WITH ALL STEPS OF REO 601R-53-51-538 REV- DATED 2020-12-07. PRESSURIZATION LEAK CHECK GOOD. SEE CONTINUATION CARD FOR DETAILS.

Part: ATTACH BRACKET — CORRODED (R DOOR FRAME) · airframe 40,854 hrs · 38,316 cycles

SERVICE DOOR SURROUND BRACKET ATTACHING TO ANGLE AT FS 319 (LOWER SILL AREA) HAS CORROSION. C-CHECK RO 1/16/2021. REMOVED CORRODED ANGLE AND REPLACED WITH NEW ANGLE, PER CRJ 200 DWG 601R38303 REV AR & CRJ 200 SRM 51-42-21 & 51-42-06. C/W SKY CARD 51-900-1003-SKY.

Part: ANCHOR FITTING — CORRODED (PAX DOOR) · airframe 40,854 hrs · 38,316 cycles

SERRATED PLATE FOR PASSENGER DOOR FORWARD ANCHOR FITTING HAS CORROSION ABOVE AND BELOW ANCHOR FITTING. C-CHECK RO 1/16/2021. REMOVED AND REPLACED WITH NEW SERRATED PLATE FOR PASSENGER DOOR FORWARD ANCHOR FITTING, REF CRJ 200 AMM 52-11-17-400-804.

Part: SUPPORT BEAM — CRACKED (CARGO DOOR TRACK) · airframe 40,854 hrs · 38,316 cycles

CARGO DOOR SURROUND TRACK SUPPORT BEAM AT FS 621 LOWER BRACKET CRACKED. C-CHECK RO 1/16/2021. REMOVED AND INSTALLED CARGO DOOR LOWER TRACK SUPPORT BRACKET, REF CRJ-200-SRM 51-24-21 AND BOMBARDIER DRAWING 601R35050 REV AC. COMPLIED WITH 51-900-1003-SKY. SEE CONTINUATION CARD FOR DETAILS.

Part: SPLICE ANGLE — CRACKED (ZONE 200) · airframe 40,854 hrs · 38,316 cycles

CRACK ON INBOARD SPLICE ANGLE AT STR 3L JUST AFT OF FS 280. C-CHECK RO 1/16/2021. REPLACED SPLICE ANGLE AT STR 3L AT FS 280, REF CRJ-200-SRM 51-42-06 AND DWG PL 600-31057 REV P. COMPLIED WITH 51-900-1003-SKY. SEE CONTINUATION CARD FOR DETAILS.

Part: HINGE FITTING — OUT OF TOLERANCE (LT ELEVATOR) · airframe 40,854 hrs · 38,316 cycles

UPON REMOVAL OF LT ELEVATOR HINGE FITTING BEARING BORE WAS FOUND TO BE OUT OF TOLERANCE, REPLACE HINGE FITTING ASSEMBLY. P/N 600-24043-1. C-CHECK RO 1/16/2021. INSTALLED NEW HINGE FITTING ASSEMBLY P/N 600-24043-1 ON LT ELEVATOR, REF CRJ200 SRM 51-42-06, SRM 51-42-21, AND BOMBARDIER DRAWING 601R24025 REV -G. COMPLIED WITH 51-900-1003-SKY.

Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 40,854 hrs · 38,316 cycles

CORROSION FOUND ON AVIONICS BAY CUTOUT INTERCOSTAL LOWER FLANGE BETWEEN 26 L AND 27 L FROM FS 394.00 TO FS 409.00. C-CHECK RO 1/16/2021. BLENDED CORROSION FROM AVIONICS BAY CUTOUT INTERCOSTAL LOWER FLANGE BETWEEN 26 L AND 27 L FROM FS 394.00 TO FS 409.00, REF CRJ 200 SRM 51-21-06. STRUCTURALLY ACCEPTABLE AND COMPLIED WITH ALL STEPS OF REPAIR OF CORRODED AREA, REF REO 601R-53-21-3371 REV - DATE 2020-12-07. PERFORMED PRESSURE CHECK NO DEFECTS NOTED.

Part: SKIN — DENTED (ZONE 100) · airframe 40,854 hrs · 38,316 cycles

DENT ON EXTERNAL SKIN BETWEEN FS 349.00-333.00 AT STGR 26R. C-CHECK RO 1/16/2021. REPAIRED FUSELAGE EXTERNAL SKIN BETWEEN FS 349.00-333.00, AT STGR 26R, REF REO 601R-53-21-3373 REV- DATED 2020-12-14 AND REO 601R-51-00-309 REV -A DATED 2017-08-23. LEAK CHECK GOOD AND SEE CONTINUATION CARD FOR DETAILS.

Part: SKIN — DENTED (ZONE 100) · airframe 40,854 hrs · 38,316 cycles

DENT ON EXTERNAL SKIN BETWEEN FS 310.00-310.00, STGR 25R-24R. C-CHECK RO 1/16/2021. REPAIRED EXTERNAL SKIN BETWEEN FS 310.00-310.00, STGR 25R-24R, REF REO 601R-53-21-3367 REV - DATED 2020-12-10. COMPLIED WITH 51-900-1003-SKY. SEE CONTIUATION CARD FOR DETAILS.

Part: SKIN — SCRATCHED (ZONE 200) · airframe 40,854 hrs · 38,316 cycles

SCRATCH ON EXTERNAL SKIN BELOW FWD POTABLE WATER SERVICING PORT CUTOUT BETWEEN FS 349.00-364.00, 20R-19R. C-CHECK RO 1/16/2021. BLENDED SCRATCH ON EXTERNAL SKIN BELOW FWD POTABLE WATER SERVICING PORT CUTOUT BETWEEN FS 349.00-364.0 12R-19R, REF CRJ-200-SRM 51-12-00. BLENDED AREA FOUND TO BE OUT OF LIMTS REF CRJ 200 SRM 53-00-31. REPAIRED SCRATCH ON EXTERNAL SKIN BELOW FWD POTABLE WATER SERVICING PORT CUTOUT BETWEEN FS 349.00-364.0 12R-19R, REF REO 601R-53-21-3372 REV - DATED 2020-12-09. SEE CONTINUATION CARD FOR DETAILS.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 40,854 hrs · 38,316 cycles

FLOOR SUPPORT ANGLE ON THE AFT SIDE OF FS 280.00 BEAM BETWEEN LBL 9 & RBL 9 IS CORRODED AT MULTIPLE AREAS, MARKED. C-CHECK RO 1/16/2021. REMOVED AND REPLACED FS 280 LBL 9 RBL 9 AFT ANGLE, REF CRJ 200 SRM 51-42-06-00, CRJ200 SRM 51-42-21-00, AND PREVIOUSLY INCORPORATED GREO 601R-53-11-136, REV A, 2007/11/01. COMPLIED WITH 51-900-1003-SKY.

Part: RETAINER — WORN (FAIRING) · airframe 40,854 hrs · 38,316 cycles

3 EA FAIRING 193AB RETAINERS ARE WORN BEYOND PERMISSIBLE DIMENSIONS, RETAINERS ARE ATTACHED TO FUSELAGE SIDE, FLAGGED. C-CHECK RO 1/16/2021. REMOVED WORN RETAINERS AND INSTALLED 3 EA NEW RETAINERS WITH NEW NUTPLATES (P/N: 601R31036-10, 601R31036-11, 601R31036-12) FOR FAIRING 193AB WHERE FLAGGED, REF CRJ200 SRM 51-41-02, 51-40-11, 51-42-06.

Part: STRAP — CORRODED (FLOORBEAM) · airframe 40,854 hrs · 38,316 cycles

FLOOR STRAP CORRODED, LBL 29-LBL 43 FS 559.00, MARKED. C-CHECK RO 1/16/2021. BLENDED CORROSION FROM FLOOR STRAP LOCATED AT FS 559.00 BETWEEN LBL 29 AND LBL 43, REF CRJ 200, SRM 51-21-06. EVALUATED AND FOUND TO BE OUT OF LIMITS. INSTALLED 1 EA NEW FLOOR STRAP, REF CRJ 200, DRW 601R31025, REV K 14 EA SOLID RIVETS, 4 EA NUT PLATES, 8 EA BLIND NUT PLATE RIVETS, REF CRJ 200, SRM 51-42-15, SRM 51-42-06, SRM 51-45-00. COMPLIED WITH 51-900-1003-SKY AND SEE CONTINUATION CARD.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 40,854 hrs · 38,316 cycles

SEAT TRACK HAS CORROSION AT FORWARD END, LBL 9 FS 364.00-FS 398.00, MARKED. C-CHECK RO 1/16/2021. REMOVED OUT OF LIMITS SEAT TRACK, FABRICATE NEW LBL SEAT RAIL P/N 601R31032 FROM FS 364.00 TO FS 398.00 USING EXTRUSION 20276-288-0-0A, PO T55899, REF REO 601R-53-00-485, REV D, DATED 2018-01-29. INSTALLED, REF CRJ-200 AMM 53-01-11-400-802, TOOL TUC7824 DUE 30-JUN-21. SEE ATTACHED CONTINUE CARD FOR DETAILS.

Part: STRAP — CORRODED (FLOORBEAM) · airframe 40,854 hrs · 38,316 cycles

FLOOR STRAP CORRODED RBL 29-RBL 43 FS 559.00, MARKED. C-CHECK RO 1/16/2021. REMOVED CORROSION ON 3 EA AREAS STRAP FLOOR RBL 29-RBL 43, FS 559.00, REF CRJ200 SRM 51-21-06 ORIGINAL MATERIAL THICKNESS IS .050", LOWEST REMAINING THICKNESS IS .043", MATERIAL REMOVED IS .007", MAX ALLOWABLE IS .005" OR 10% OF THE THICKNESS. FOUND TO BE OUT OF LIMITS, REF CRJ 200 SRM 53-00-00 PGS 101-106 AND CRJ 200 SRM 53-41-43 PGS 1-10. INSTALLED NEW STRAP PART NUMBER 601R31025-29, IAW CRJ200 SRM 51-42-10.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 40,854 hrs · 38,316 cycles

SEAT RAIL HAS MULTIPLE AREAS OF CORROSION FS 409.00+4-FS 409.00+126 LBL 9, MARKED. C-CHECK RO 1/16/2021. REMOVED AND REPLACED SEAT RAIL FS 409.00+4-FS 409.00+126 LBL 9, REF CRJ-200 AMM 53-01-11-400-802 AND REO 601R-53-00-485 REV D DATED 2018-01-29 AND CRJ-200 SRM 51-41-02. SEE CONTINUATION CARD FOR DETAILS.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 40,854 hrs · 38,316 cycles

FLOOR BEAM CAP HAS CORROSION AT MULTIPLE AREAS ON THE INBOARD FLANGE RBL 9, FS 559.00+11-FS 569.00, MARKED. C-CHECK RO 1/16/2021. REMOVED CORROSION ON FLOOR BEAM CAP IN MULTIPLE AREAS ON INBOARD FLANGE RBL 9 FS 559.00+11-FS 569.00, REF CRJ200 SRM 51-21-06. EVALUATED AND FOUND TO HAVE 100% MATERIAL LOSS. FLOOR BEAM CAP AT RBL 9 LOCATED BETWEEN FS 559.00+11-FS 569 WILL BE REPLACED ON JOB: 2747461 OP: 255 MX TRANS 21886169.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 40,854 hrs · 38,316 cycles

SEAT TRACK HAS CORROSION AT MULTIPLE AREAS, RBL 9 FS 364.00-FS 398.00, MARKED. C-CHECK RO 1/16/2021. REMOVED AND REPLACED CORRODED SEAT RAIL WITH NEW SEAT RAIL AT RBL 9, BETWEEN FS 364.00 TO FS 398.00, REF CRJ-200 SRM 51-21-06, CRJ-200 SRM 53-21-19, REO 601R-53-00-485 REV-D, DATED 2018-01-29 AND CRJ-200 AMM 53-01-11-400-802. SEE CONTINUATION FOR DETAILS.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 40,854 hrs · 38,316 cycles

FLOOR BEAM CAP HAS MULTIPLE AREAS OF CORROSION ON THE INBOARD & OUTBOARD FLANGE RBL 9 FS 409.00+5-FS 409.00+118, MARKED. C-CHECK RO 1/16/2021. INSTALLED NEW FLOOR BEAM CAP AT RBL 9 BETWEEN FS 409.00+5 AND FS 409.00+118, REF DWG 601R31117 REV -E AND REO 601R-53-31-1159 REV- DATED 2020-12-05. COMPLIED WITH 51-900-1003-SKY. SEE CONTINUATION CARD FOR DETAILS.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 40,854 hrs · 38,316 cycles

FLOOR BEAM CAP HAS CORROSION AT MULTIPLE AREAS ON THE INBOARD FLANGE LBL 9, FS 559.00+11-FS 569.00, MARKED. C-CHECK RO 1/16/2021. REMOVED AND REPLACED FLOOR BEAM AT FS 559+11 TO FS 569 AT LBL 9, REF REO 601R-53-51-540 REV - DATED 2020-12-18, DWG 601R31032 REV NC, CRJ-200-SRM 51-42-21, CRJ-200-SRM 51-42-34, CRJ-200-SRM 51-42-22, CRJ-200-SRM 51-42-00, AND CRJ-200-SRM 51-42-15. SEE ATTACHED TASK 51-900-1003-SKY. SEE CONTINUE CARD FOR DETAILS.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 40,854 hrs · 38,316 cycles

FLOOR BEAM CAP HAS MULTIPLE AREAS OF CORROSION ON THE INBOARD FLANGE LBL 9 FS 409.00+5-FS 409.00+118, MARKED. C-CHECK RO 1/16/2021. REMOVED OUT OF LIMITS FLOOR BEAM CAP AND REPLACED, INSTALLED WITH NEW FABRICATED FLOOR BEAM CAP P/N 601R31117-17 AT FS 409.00+5 TO FS 409.00+118, REF DWG 601R31117 REV-E AND REO 601R-53-31-1159, REV- DATED 2020-12-05 STEPS 1 TO 8 COMPLIED WITH 51-900-1003-SKY. SEE CONTINUATION CARD FOR DETAILS.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 40,854 hrs · 38,316 cycles

RIGHT FLOOR SILL HAS MULTIPLE AREAS OF CORROSION FS 409.00+72-FS 409.00+128, MARKED. C-CHECK RO 1/16/2021. REMOVED HEAVY COROSION FROM MULTIPLE AREAS OF RT FLOOR SILL PANEL BETWEEN FS 409+72 & FS 409+128, REF CRJ200 SRM 51-21-06. EVALUATED AND FOUND BLENDED OUT WITHIN LIMITS, NDT NO DEFECTS NOTED, REF REO 601R-53-31-1161, REV-, 2020-12-13, RT FLOOR SILL FS 409+72 TO FS 409+128.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 40,854 hrs · 38,316 cycles

FLOOR SUPPORT ANGLE ON THE FORWARD SIDE OF FS 280.00 BEAM BETWEEN LBL 9 & RBL 9 IS CORRODED AT MULTIPLE AREAS, MARKED. C-CHECK RO 1/16/2021. REMOVED AND REPLACED FS 280 LBL 9 RBL 9 FWD ANGLE, REF CRJ 200 SRM 51-42-06 AND CRJ 200 SRM 51-42-21 AND DWG 600-34017 REV AB. COMPLIED WITH 51-900-1003-SKY AND SEE CONTINUATION CARD FOR DETAILS.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 40,854 hrs · 38,316 cycles

LEFT FLOOR SILL FROM FS 357-FS 409.00+04 HAS MULTIPLE AREAS OF CORROSION, MARKED. C-CHECK RO 1/16/2021. REPAIRED LT FLOOR SILL FROM FS 357 TO FS 409.00+04, REF CRJ 200 SRM 51-42-06, DWG 601R31148 REV W AND REO 601R-53-21-3364, REV- DATED 2020-12-04. COMPLIED WITH 51-900-1003-SKY. SEE CONTINUATION CARD FOR DETAILS.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 40,854 hrs · 38,316 cycles

RIGHT FLOOR SILL FROM FS 357-FS 409.00+04 HAS MULTIPLE AREAS OF CORROSION, MARKED. C-CHECK RO 1/16/2021. REMOVED NOTED CORROSION AND REPLACED DAMAGED SPLICE ANGLE WITH NEW SPLICE ANGLE ON RIGHT FLOOR SILL FROM FS 349-FS 409.00+04, NDT INSPECTED NO DEFECTS NOTED. APPLIED FINISHES, REF MHIRJ REO 601R-53-21-3384 REV - DATED 2021-01-11. FOR COMPLETE DETAILS OF WORK PERFORMED SEE CONTINUE CARD. COMPLETED SKYWEST TASK CARD 51-900-1003-SKY.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 40,854 hrs · 38,316 cycles

FLOOR BEAM CAP HAS CORROSION AT MULTIPLE AREAS ON THE OUTBOARD FLANGE RBL 9, FS 559.00+32-FS 559.00+112, MARKED. C-CHECK RO 1/16/2021. REMOVED AND INSTALLED NEW FLOOR BEAM CAP AT RBL 9, FS 559.00+32-FS 559.00+112, REF CRJ-200-SRM 51-42-34,CRJ-200 SRM 51-42-21, CRJ-200 SRM 51-42-22, DWG 601R31119 REV-E AND DWG 601R31026 REV-F, AND REO 601R-53-51-540 REV - DATED 2020-12-18. COMPLIED WITH 51-900-1003-SKY. SEE CONTINUATION CARD FOR DETAILS.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 40,854 hrs · 38,316 cycles

RIGHT FLOOR SILL CORRODED AT MULTIPLE LOCATIONS, FS 559.00+85-FS 559.00+116, MARKED. C-CHECK RO 1/16/2021. REMOVED AND REPLACED RT FLOOR SILL P/N 601R31133-102S, REF CRJ-200 SRM 51-42-06, CRJ-200 SRM 51-42-21, AND DRAWING 601R31026 REV F. COMPLIED WITH 51-900-1003-SKY. SEE CONTINUATION CARD FOR DETAILS.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 40,854 hrs · 38,316 cycles

THE LBL 27 FOOR BEAM CAP HAS CORROSION AND CHAFES ON ITS INBOARD AND OUTBOARD FLANGES BETWEEN APPROXIMATELY FS 605 AND APPROXIMATELY FS 621 (MARKED WITH RED GREASE PENCIL). C-CHECK RO 1/16/2021. INSTALLED NEW FLOOR BEAM CAP AT LBL 27, FS 605-FS 621, REF CRJ 200, BOMBARDIER REO 601R-53-61-3778, REV -B, DATE: 2016-12-19, BOMBARDIER DWG601R35031, REV Y, SRM 51-42-21, SRM 51-42-22. COMPLIED WITH 51-900-1003-SKY AND SEE CONTINUATION CARD FOR DETAILS.

Part: INTERCOSTAL — CRACKED (484) · airframe 40,854 hrs · 38,316 cycles

THE RT INTERCOSTAL AT FS 484, BETWEEN RBL 27 AND RBL 36, HAS A CRACKED INBOARD CLIP. C-CHECK RO 1/16/2021. REMOVED CRACKED CLIP AND INSTALLED NEW CLIP P/N: 601R1171-9 AT FS 484 RBL27 (INBOARD), REF CRJ200 SRM 51-42-06 AND SRM 51-42-21 AND REFERENCE ONLY BOMBARDIER REO 601R-53-41-059 REV -B DATED 2009-09-16. RESTORED FINISH AND APPLIED CIC / TASK CARD 51-900-1003-SKY COMPLIED WITH.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 40,854 hrs · 38,316 cycles

THE RBL 27 FLOOR BEAM CAP HAS CORROSION AND CHAFES ON ITS OUTBOARD FLANGE BETWEEN APPROXIMATELY FS 605 AND APPROXIMATELY FS 621 (MARKED WITH RED GREASE PENCIL). C-CHECK RO 1/16/2021. REMOVED & REPLACED RBL 27 FLOOR BEAM CAP AT APPROXIMATELY FS 605 TO FS 621.0, AS PER REO 601R-53-61-3778 REV-B DATED 2016-12-19, DRAWING 601R35031 REV-Y, CRJ 200 SRM 51-42-21, CRJ 200 SRM 51-42-22. REPLACED FASTENERS, BLIND NUTS & NUT PLATES AS REQUIRED. PRESSURE CHECK GOOD. COMPLIED WITH 51-900-1003-SKY.

Part: BULKHEAD WEB — CHAFED (AFT) · airframe 40,854 hrs · 38,316 cycles

THE FS 621 PRESSURE BULKHEADS FWD FACE "PICKET FENCE" STRAPS HAVE 22 LOCATIONS OF CHAFES: LBL 36.20 HAS 2 AREAS, LBL 27.50 HAS 2 AREAS, LBL 18.00 HAS 2 AREAS, LBL 9.50 HAS 4 AREAS, RBL 9.50 HAS 4 AREAS, RBL 18.00 HAS 2 AREAS, RBL 27.50 HAS 3 AREAS, RBL 36.20 HAS 3 AREAS (MARKED WITH RED GREASE PENCIL). C-CHECK RO 1/16/2021. REPAIRED FS 621 PRESSURE BULKHEAD FWD FACE "PICKET FENCE" STRAPS AT 22 LOCATION, REF REO 601R-53-61-7502 REV - DATED 2020-12-09. LEAK CHECK GOOD AND SEE CONTINUATION CARD FOR DETAILS.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 40,854 hrs · 38,316 cycles

THE LBL 9.0 FLOOR-SUPPORT BEAM'S CAP HAS CORROSION ALONG ITS ENTIRE LENGTH, FROM APPROXIMATELY FS 409+128 TO APPROXIMATELY FS 559, THE CORROSION IS ON BOTH THE INBOARD AND OUTBOARD FLANGES, AND EXTENDS UNDER THE FLOOR BEAM SEAT RAILS (MARKED WITH RED GREASE PENCIL). C-CHECK RO 1/16/2021. INSTALLED NEW LBL 9.0 FLOOR SUPPORT BEAM CAP FROM FS 409+128 TO FS 559, REF REO 601R-53-41-2824 REV- DATED 2020-12-06 AND REO 601R-53-00-027 REV D DATED 26-NOV-2009. COMPLIED WITH 51-900-1003-SKY AND SEE CONTINUATION CARD FOR DETAILS.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 40,854 hrs · 38,316 cycles

THE RBL 9.0 FLOOR-SUPPORT BEAMS CAP HAS CORROSION ALONG ITS ENTIRE LENGTH, FROM APPROXIMATELY FS 409+128 TO APPROXIMATELY FS 559, THE CORROSION IS ON BOTH THE INBOARD AND OUTBOARD FLANGES, AND EXTENDS UNDER THE FLOOR BEAM SEAT RAILS (MARKED WITH RED GREASE PENCIL). C-CHECK RO 1/16/2021. CUT OUT DAMAGED FLOOR BEAM AND BEAM FLANGES AT RBL 9, APPROXIMATELY FS 409128 TO FS 559.0. FABRICATED & INSTALLED NEW FLOOR BEAM SECTION, SPLICE PARTS & C- CHANNELS, AS PER REO 601R-53-41-2824 REV -, DATED 2020-12-06, DRAWING 601R31025 REV F AND CRJ 200 SRM'S 51-42-06, 51-42-21. INSTALLED USING NEW NUT CLIPS , DOME NUTS & FASTENERS. PRESSURE LEACK CHECKS GOOD. SEE CONTINUE CARDS FOR DETAILS. COMPLIED WITH 51-900-1003-SKY.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 40,854 hrs · 38,316 cycles

THE RBL 9 FOOR BEAM CAP HAS CORROSION AND CHAFES ON ITS INBOARD AND OUTBOARD FLANGES BETWEEN APPROXIMATELY FS 605 AND APPROXIMATELY FS 621(MARKED WITH RED GREASE PENCIL). C-CHECK RO 1/16/2021. REMOVED CORROSION ON FLOOR BEAM AT RBL 9 BETWEEN APPROX FS 605-FS 621, REF CRJ 200 SRM 51-21-06. FLOOR BEAM WAS FOUND TO BE OUT OF LIMITS, PER REF CRJ 200 SRM 53-00-00. REMOVED AND REPLACED FLOOR BEAM WITH NEW (P/N: 601R35031-3), REF CRJ 200 SRM 51-42-21 REF CRJ 200 SRM 51-42-22, BOMBARDIER DWG 601R35031, REV Y, BOMBARDIER REO 601R-53-61-3780, REV -A, DATE 2011-07-15. COMPLIED WITH 51-900-1003-SKY.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 40,854 hrs · 38,316 cycles

THE LBL 9 FOOR BEAM CAP HAS CORROSION AND CHAFES ON ITS INBOARD AND OUTBOARD FLANGES BETWEEN APPROXIMATELY FS 605 AND APPROXIMATELY FS 621(MARKED WITH RED GREASE PENCIL). C-CHECK RO 1/16/2021. REMOVED AND REPLACED THE LBL 9 FLOOR BEAM CAP AT APPROXIMATELY FS 605 THRU FS 621, REF CRJ 200 SRM 51-42-21 & REO 601R-53-61-3780 REV -A DATED 2011-07-15. REPLACED FASTENERS AND NUT PLATE AS REQUIRED. PRESSURE LEAK CHECKS GOOD. COMPLIED WITH 51-900-1003-SKY.

Part: SKIN — DENTED (RUDDER LE) · airframe 40,854 hrs · 38,316 cycles

RUDDER RT LEADING EDGE SKIN BETWEEN BOTTOM AND CENTER HINGES IS DENTED AND GOUGED, MARKED. C-CHECK RO 1/16/2021. BLENDED GOUGE FROM RUDDER RT LEADING EDGE SKIN BETWEEN BOTTOM AND CENTER HINGES, REF CRJ 200 SRM 51-12-00. DURING DRESS BACK OF DENT, SKIN FOUND TO BE CRACKED AND BLENDED ALMOST ALL THE WAY THROUGH AND THEREFORE OUT OF LIMITS OF CRJ 200 REO 601R-51-00-309 REV A 2017-08-23. FABRICATED AND INSTALL NEW LEADING EDGE SKIN PANEL, REF EO 600-22000 NIEO S07 DATED 2020-12-28. COMPLIED WITH 51-900-1003-SKY AND SEE CONTINUATION CARD FOR DETAILS.

Part: STOP FITTING — CORRODED (PAX DOOR) · airframe 40,854 hrs · 38,316 cycles

PASSENGER DOOR STOP ATTACHED TO THE LOWER TORQUE TUBE HAS CORROSION, MARKED. C-CHECK RO 1/16/2021. REMOVED CORROSION FROM PAX DOOR LATCH MECH UPPER STOP FITTING FOOT, REF CRJ200 SRM 51-21-06. EVALUATED AND FOUND UPPER STOP FITTING P/N 601R38923-3 IS OUT OF LIMIT, REF CRJ200 SRM 52-00-27. REMOVED DISCREPANT UPPER STOP FITTING AND WITH FASTENERS HOLES. LOCATED & DRILLED, PER CRJ200 SRM 51-40-06 REF BOMBARD. DWG 601R38923 REV -C. INSTALLED AND ADJUSTED NEW REPLACEMENT UPPER STOP FITTING P/N 601R38923-3 AT PAX DOOR LATCH MECH, PER CRJ200 SRM 51-41-02 AND CRJ200 AMM TASK 52-11-25-830-801 FIG 502.

Part: BEARING — EXCESS PLAY (L ELEVATOR HINGE) · airframe 40,854 hrs · 38,316 cycles

ALL 4 RT ELEVATOR HINGE POINT BEARINGS HAVE PLAY. C-CHECK RO 1/16/2021. REMOVED AND INSTALLED NEW 4 RT ELEVATOR HINGE POINT BEARINGS, REF CRJ-200-AMM 20-26-00-910-807 AND CRJ 200 AMM 20-26-00-910-808. BONDING CHECK GOOD AND SEE CONTINUATION CARD FOR DETAILS.

Part: STRUCTURE — DENTED (PAX DOOR) · airframe 40,854 hrs · 38,316 cycles

PASSENGER DOOR FORWARD AND AFT END CAPS DENTED AND DAMAGED FASTENERS. C-CHECK RO 1/16/2021. MEASURED DENT DAMAGE AND FOUND TO BE OUT OF ALLOWABLE LIMIT OF W/D < 25, REF CRJ200 SRM 52-00-31 FIG 102 SHEET 3. REMOVED AND REPLACED THE PAX DOOR UPPER FWD & AFT COVERS P/N 600-31902-287/ -288 WITH NEW PARTS, REF CRJ-200 SRM 51-40-06 & CRJ-200 SRM 51-42-13.

Part: STRUCTURE — CORRODED (PAX DOOR) · airframe 40,854 hrs · 38,316 cycles

PASSENGER DOOR DD6 HAS CORROSION SEVERAL AREAS. C-CHECK RO 1/16/2021. INSTALLED NEW REPLACEMENT INTERCOSTAL DD6 P/N 601R318057-1 WITH NEW FASTENERS AT PAX DOOR INNER STRUCTURE BETWEEN FS 320 & FS 338, PER CRJ200 SRM 51-42-06 & SRM 51-42-21 & BOMBARD DWG 601R31702 REV N. PRESSURE CHECK GOOD AND COMPLIED WITH 51-900-1003-SKY. SEE CONTINUATION CARD FOR DETAILS.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 40,854 hrs · 38,316 cycles

PASSENGER DOOR CLIP COMMON TO DD6 AND FS 329.76 FORMER HAS CORROSION. C-CHECK RO 1/16/2021. EVALUATED PAX DOOR INNER STRUCTURE CLIP COMMON TO INTERCOSTAL DD6 WITH HEAVY CORROSION OVERLAPING BOTH ELEMENTS AND WITH 50% OF SURFACE DAMAGED IS OUT OF ALLOWABLE DAMAGE LIMIT OF 30% AND ONE ELEMENT IN CROSS-SECTION, REF CRJ200 SRM 52-00-00 FIG 102 SHEET 2. REMOVED AND REPLACED THE CLIP AT PAX DOOR INNER STRUCTURE DD6 INTERCOSTAL AT FS 329.75 WITH NEW PART, PER CRJ200 SRM 51-42-06 REF BOMBARD DWG 601R31902 REV Y. COMPLIED WITH 51-900-1003-SKY.

Part: BEARING — EXCESS PLAY (ELEVATOR HINGE) · airframe 40,854 hrs · 38,316 cycles

ALL 4 LT ELEVATOR HINGE POINT BEARINGS HAVE PLAY. C-CHECK RO 1/16/2021. REMOVED AND INSTALLED NEW 4 LT ELEVATOR HINGE POINT BEARINGS, REF CRJ-200-AMM 20-26-00-910-807 AND CRJ 200 AMM 20-26-00-910-808. BONDING CHECK GOOD AND SEE CONTINUATION CARD FOR DETAILS.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 40,854 hrs · 38,316 cycles

LT WING INBOARD FLAP (CENTER OUTBOARD) VANE IS CHAFED. C-CHECK RO 1/16/2021. REMOVED AND REPLACED LT WING INBOARD FLAP (CENTER OUTBOARD) VANE, REF CRJ-200 SRM 51-42-13 AND DWG 601R14302 REV E. SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 40,854 hrs · 38,316 cycles

LT WING INBOARD FLAP (INBOARD) VANE IS CHAFED. C-CHECK RO 1/16/2021. INSTALLED NEW PANEL PN 601R14303-53, REF CRJ200 SRM 51-42-13 AND DWG 601R14303 REV J. COMPLIED WITH 51-900-1003-SKY. SEE CONTINUATION CARD FOR DETAILS.

Part: VANE — WORN (RT WING TE FLAP) · airframe 40,854 hrs · 38,316 cycles

RT WING INBOARD FLAP VANE HAS 3 EA WEAR MARKS ALONG LEADING EDGE, AREAS MARKED. C-CHECK RO 1/16/2021. REMOVED 3 EA WEAR MARKS ON RT WING INBOARD FLAP VANE LEADING EDGE, REF REO 601R-57-52-004, REV -D, DATED 2012-12-19. ALL 3 EA LOCATIONS ARE OUT OF LIMITS, PER REF CRJ 200 SRM 57-52-00. SEE JOB 2747461, OP 327, MX 21914352, JOB 2747461, OP 326, MX 21914353, & JOB 2747461, OP 283, MX 21914390 FOR CORRECTIVE ATIONS.

Part: VANE — WORN (LT WING TE FLAP) · airframe 40,854 hrs · 38,316 cycles

LT WING INBOARD FLAP VANE HAS 3 EA WEAR MARKS ALONG LEADING EDGE, AREA MARKED. C-CHECK RO 1/16/2021. INSTALLED LT WING INBOARD FLAP (OUTBOARD) VANE, REF CRJ200 SRM 51-42-13 AND DWG 601R14303 REV J. COMPLIED WITH 51-900-1003-SKY AND SEE CONTINUATION CARD FOR DETAILS.

Part: BOLT — CORRODED (RT SPOILER) · airframe 40,854 hrs · 38,316 cycles

RT FLIGHT SPOILER, BOTH PCU LINKS HAVE CORRODED HARDWARE. C-CHECK RO 1/16/2021. REMOVED AND REPLACED HARDWARE ON RT FLIGHT SPOILER, BOTH PCU LINKS WITH SERVICEABLE PARTS FROM SUPPLY. OPERATIONAL TEST OF THE FLIGHT SPOILER/SPOILERON, CHECKS GOOD, REF CRJ200 AMM TASK 27-64-00-710-801.

Part: BOLT — CORRODED (RT SPOILERON) · airframe 40,854 hrs · 38,316 cycles

RT SPOILERON, ALL 4 HINGES HAVE CORRODED HARDWARE. C-CHECK RO 1/16/2021. REMOVED AND REPLACED RT SPOILERON HARDWARE AT ALL 4 HINGES USING SERVICEABLE PARTS FROM SUPPLY. OPERATIONAL TEST OF THE FLIGHT SPOILER/SPOILERON CHECKS GOOD, REF CRJ200 AMM TASK 27-64-00-710-801.

Part: BOLT — CORRODED (LT SPOILER) · airframe 40,854 hrs · 38,316 cycles

LT FLIGHT SPOILER, ALL 4 HINGES HAVE CORRODED HARDWARE. C-CHECK RO 1/16/2021. REMOVED AND REPLACED HARDWARE AT ALL 4 HINGES ON LT FLIGHT SPOILER. PERFORMED OPERATIONAL TEST OF THE FLIGHT SPOILER/SPOILERON, CHECKS GOOD, REF CRJ 200 AMM 27-64-00-710-801.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 40,854 hrs · 38,316 cycles

LT OUTBOARD FLAP, LOWER SKIN HAS A DENT, INBOARD OF THE CENTER HINGE ARM, MARKED. C-CHECK RO 1/16/2021. DENT ON LT OUTBOARD FLAP, LOWER SKIN MEASURES 1.30" X 1.30" WITH A DEPTH OF .036". DENT IS IN CLOSE PROXIMITY TO FASTENERS AND CHEM MILL. DENTED AREA IS FOUND TO BE OUT OF LIMITS, REF CRJ 200 SRM57-53-00. ORDERED AND RECIEVED NEW FLAP.

Part: BOLT — CORRODED (RT SPOILER) · airframe 40,854 hrs · 38,316 cycles

RT FLIGHT SPOILER, ALL 4 HINGES HAVE CORRODED HARDWARE. C-CHECK RO 1/16/2021. REMOVED AND REPLACED HARDWARE AT ALL 4 HINGES OF RT FLIGHT SPOILER USING SERVICEABLE PARTS FROM SUPPLY. OPERATIONAL CHECK IS GOOD, REF CRJ200 AMM 27-64-00-710-801.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 40,854 hrs · 38,316 cycles

HORIZONAL STAB STEADY FITTING HAS CORROSION ON THE ATTACH HARDWARE. C-CHECK RO 1/16/2021. REMOVED AND REPLACED 5 EA BOLTS, 5 EA NUTS AND 5 EA WASHERS ON HORIZONAL STAB STEADY FITTING, REF CRJ 200 AMM 20-21-00-910-801. TUC5657 DUE 31-MAR-21.

Part: BOLT — CORRODED (RT SPOILER) · airframe 40,854 hrs · 38,316 cycles

RT OUTBOARD GROUND SPOILER, ALL 3 HINGES HAVE CORRODED HARDWARE. C-CHECK RO 1/16/2021. REMOVED AND REPLACED HARDWARE AT ALL THREE HINGES ON RT OUTBOARD GROUND SPOILER. OPERATIONAL TEST OF THE FLIGHT SPOILER/SPOILERON CHECKS GOOD, REF CRJ200 AMM 27-64-00-710-801.

Part: BOLT — CORRODED (LT SPOILERON) · airframe 40,854 hrs · 38,316 cycles

LT SPOILERON, ALL 4 HINGES HAVE CORRODED HARDWARE. C-CHECK RO 1/16/2021. REMOVED AND REPLACED HARDWARE AT ALL 4 HINGES ON LT SPOILERON. PERFORMED OPERATIONAL TEST OF THE FLIGHT SPOILER/SPOILERON, CHECKS GOOD, REF CRJ 200 AMM 27-64-00-710-801.

Part: SKIN — DENTED (FUSELAGE) · airframe 40,854 hrs · 38,316 cycles

FS 169.0 EXTERNAL SKIN ON UPPER LEFT SIDE HAS SEVERAL DENTS. C-CHECK RO 1/16/2021. INSTALLED NEW LT NOSE SKIN P/N 600-33052-113, REF CRJ 200 SRM 51-42-06, CRJ200 SRM 51-42-13, DWG 600-33052 REV -W. COMPLIED WITH 51-900-1003-SKY.

Part: SKIN — CHAFED (CARGO DOOR) · airframe 40,854 hrs · 38,316 cycles

CARGO DOOR EXTERNAL SKIN CHAFED AROUND OTTER HANDLE. C-CHECK RO 1/16/2021. REMOVED & REPLACED THE CARGO DOOR HANDLE & HOUSING ASSEMBLY, REF CRJ 200 SRM 51-42-21 & DRAWING 601R35027 REV AY. REPLACED PROX SWITCH, HARDWARE & BUSHINGS AS REQUIRED. OPERATIONS & PRESSURE CHECKS GOOD. COMPLIED WITH 51-900-1003-SKY.

Part: SKIN — DENTED (FUSELAGE) · airframe 40,854 hrs · 38,316 cycles

COMPLY WITH SCHEDULED MAINTENANCE CODE: RA59039-601R-53-00-743 N868ASMXCODEID51889-PR. THERE ARE TWO DENTS IN THE FUSELAGE, ONE LOCATED BETWEEN FS 295.0-FS 310.0 AT STR 21L AND THE OTHER LOCATED BETWEEN FS 409.00 AND FS 409.00+16 AND STR 16L-17L, PER REO 601R-53-00-743 REV A DATED 2020-04-27. CONDITION IS ACCEPTABLE FOR 5700 FLIGHT HOURS DUE BY 41494.7 TAT, PART NUMBER: -, SERIAL NUMBER: 7474, POSITION. C-CHECK RO 1/16/2021. DRESSED BACK DENTS FOUND TO BE WITH IN LIMITS, REF MHIRJ REO 601R-53-21-3379 REV- DATED 2020-12-24 AND MHIRJ REO 601R-53-31-1164 REV-- DATED 2020-12-24. SEE CONTINUATION CARD FOR WORK PERFORMED. COMPLIED WITH SKYWEST SKY CARD 51-900-1003-SKY.

Part: STRUT — DISCHARGED (NLG) · airframe 39,369 hrs · 36,956 cycles

ON DEPARTURE SELECTING GEAR UP WE RECEIVED GEAR DISAGREE WARNING MSG AND GEAR INDICATOR SHOWED NOSE GEAR DISAGREE. RAN QRH PROCEDURE AND GEAR DISAGREE WARNING MSG WENT AWAY AND HAD DOWN AND 3 GREEN. RETURNED TO BIS AND NORMAL LANDING. DECLARED EMERGENCY. FLIGHT 5495 CLOSEDINTERIGATED PSEU, FOUND NLG NO MOVEMENT. NOTED THERE WAS VERY LITTLE FLUID IN NLG STRUT. SERVICED WITH NITRO AND FLUID, IAW AMM. SWUNG NLG, NO DEFECTS NOTED. NLG EXTENSION CHECK TO BE DONE AFTER 24 HRS.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 35,793 hrs · 33,347 cycles

SMELLED ELECTRICAL SMOKE IN COCKPIT, DIVERTED. ODOR WAS AROUND FOR A COUPLE MINUTES. REWIRED THE RT NAVIGATION LIGHT ASSEMBLIES IAW AMM. REMOVED AND REPLACED TRANSFORMER T4LK IAW AMM. REMOVED AND REPLACED CIRCUIT BREAKER C13 ON CIRCUIT BREAKER PANEL 1 IAW ESPM. ALL OPS CHECKED GOOD

Part: BULKHEAD — CRACKED (BS 621) · airframe 35,138 hrs · 32,627 cycles

AFT BS 621 PRESSURE BULKHEAD FOUND CRACKED IN MULTIPLE AREAS. CUT OUT CRACKED AREAS OF THE BULKHEAD AND INSTALLED REPAIRS IAW REO 601R-53-61-1240 REV D AND REO 601R-53-61-5897 REV --.

Part: ANGLE — CRACKED (BS 621 BULKHEAD) · airframe 35,138 hrs · 32,627 cycles

THE LOWER SECTION OF ZEE ANGLE CRACKED ON THE AFT SIDE OF FS 621 AFT PRESSURE BULKHEAD AT RBL 36.2 WL 73. REMOVED AND REPLACED THE SECTION OF THE ZEE ANGLE IAW REO 601R-53-61-5897 REV --.

Part: CONNECTOR — FAILED (EMERGENCY LIGHTS) · airframe 35,094 hrs · 32,583 cycles

EMERGENCY EXIT LIGHT ON FWD WARDROBE INOPERATIVE. REMOVED AND REPLACED QUICK DISCONNECT CONNECTOR IAW ESPM 20-17-00. OPS CHECKED GOOD.

Part: SIGN — BROKEN (EMERGENCY LIGHTS) · airframe 34,029 hrs · 31,378 cycles

SERVICE DOOR LIGHTED EXIT SIGN IS BROKEN, UNSECURE. R & R SERVICE DOOR LIGHTED EXIT SIGN IAW AMM 33-51-13. OPS CHECKS GOOD.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 31,083 hrs · 28,304 cycles

CORROSION FOUND ON THE BS 349 FLOORBEAM RBL 32. REPAIRED IAW EA 12-2014-284.

Part: SKIN — CRACKED (RT WING) · airframe 31,083 hrs · 28,304 cycles

NR 2 RT WING LOWER SKIN CRACKED AT WS 148.019. REPAIRED IAW REO 601R-57-21-130 01 AND REO 601R-57-21-130, REV K. MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (BS 424-559) · airframe 31,083 hrs · 28,304 cycles

LEFT SIDE PRESSURE FLOOR SUPPORT HAS CORROSION BETWEEN BS 424-559. REPAIRED IAW REO 601R-53-41-666 AND REO 601R-53-41-666, REV C. MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (BS 424-559) · airframe 31,083 hrs · 28,304 cycles

RT SIDE PRESSURE FLOOR SUPPORT HAS CORROSION BETWEEN FS 424-559. REPAIRED IAW REO 601R-53-41-666 AND REO 601R-53-41-666, REV C. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 31,083 hrs · 28,304 cycles

CORROSION FOUND ON AFT ANGLE OF BS 349 FLOORBEAM. R & R THE FLOORBEAM ANGLE IAW SRM 51-42-06 AND 51-42-21.

Part: SEAT TRACK — CORRODED (NR 4) · airframe 31,083 hrs · 28,304 cycles

RIGHT NR 4 SEAT TRACK FOUND CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-41-02 AND AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (NR 1) · airframe 31,083 hrs · 28,304 cycles

RIGHT NR 1 SEAT TRACK IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED IAW AMM 53-01-11-000-802 AND AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (NR 1) · airframe 31,083 hrs · 28,304 cycles

NR 1 SEAT TRACK IS CORRODED BEYOND LIMITS. R & R THE SEAT TRACK IAW AMM 53-01-11-000-802 AND 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (NR 2) · airframe 31,083 hrs · 28,304 cycles

NR 2 SEAT TRACK IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802, AMM 53-01-11-400-802, AND SRM 51-41-02.

Part: SEAT TRACK — CORRODED (NR 3) · airframe 31,083 hrs · 28,304 cycles

NR 3 SEAT TRACK CORRODED. REMOVED THE CORROSION AND FOUND THE SEAT TRACK TO BE OUT OF LIMITS IAW SRM 53-21-49. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-11, AMM 53-01-11-00-802, AND AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (NR 2) · airframe 31,083 hrs · 28,304 cycles

LEFT NR 2 SEAT TRACK IS CORRODED BEYOND LIMITS. BLENDED IAW SRM. FOUND TO BE OUT OF LIMITS IAW 53-21-49. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 200 53-01-11 AND AMM 53-01-11-400-802.

Part: BRACKET — CRACKED (BS 461) · airframe 31,083 hrs · 28,304 cycles

FRAME TO PRESSURE FLOOR SUPPORT HAS A CRACKED BRACKET AT BS 461. R & R THE BRACKET IAW SRM 51-40-11.

Part: SEAT TRACK — CORRODED (NR 3) · airframe 31,083 hrs · 28,304 cycles

NR 3 FLOOR SEAT TRACK CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802, SRM 51-41-02, AND AMM 53-01-11-400-802.

Part: BRACKET — CRACKED (BS 449.85) · airframe 31,083 hrs · 28,304 cycles

FRAME TO PRESSURE FLOOR SUPPORT HAS A CRACKED BRACKET AT BS 449.85. R & R THE BRACKET IAW SRM 51-42-06, PG 11 & PG 18 & SRM 51-42-13, PG 1.

Part: ANGLE — CRACKED (BS 424) · airframe 31,083 hrs · 28,304 cycles

ANGLE CRACKED AT FS 424 NEXT TO RT FWD WING TO FUSELAGE ATTACH FITTING. REMOVED THE ANGLE IAW SRM 51-42-06 AND 51-42-21. INSTALLED REPAIRED ANGLE IAW SRM 51-42-06 & 51-42-21.

Part: SEAT TRACK — CORRODED (BS 439-473) · airframe 31,083 hrs · 28,304 cycles

RT SIDE SEAT TRACK SEGMENT FROM BS 439 - 473.15 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802 AND AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 31,083 hrs · 28,304 cycles

LT SIDE SEAT TRACK SEGMENT FROM BS 364 - 409+16 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW 53-01-11-000-802, SRM 51-40-11 AND AMM 53-01-420-001.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 31,083 hrs · 28,304 cycles

RT SIDE SEAT TRACK SEGMENT FROM BS 559+16 - 559+112 CORRODED. REPAIRED IAW REO 601R-53-00-055 AND REO 601-R53-00-055, REV A.

Part: STRUCTURE — CORRODED (PAX DOOR RAIL) · airframe 31,083 hrs · 28,304 cycles

PAX DOOR HANDRAIL CUPS FWD & AFT ARE CORRODED. CORROSION REMOVED IAW SRM 51-21-06-00. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED IAW SRM 51-42-10-00, SRM 51-42-06-00, SRM 51-40-11-00, SRM 51-40-11-42-06 AND DWG 601R31527.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 31,083 hrs · 28,304 cycles

FLOORBEAM AT FS 349 IS CORRODED. REMOVED CORROSION IAW SRM 51-26-06. R & R THE FLOORBEAM ANGLE IAW SRM 51-42-06 AND 51-42-21.

Part: FLOOR SUPPORT — CORRODED (BS 349-394) · airframe 31,083 hrs · 28,304 cycles

THE RIGHT FLOOR SUPPORT FROM BS 349-394 IS CORRODED. REPAIRED IAW REO'S 601R53-00-530, 601R-53-21-2579, REO 601R-53-00-530 AND 601R-53-21-2579.

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 31,083 hrs · 28,304 cycles

RT SIDE SEAT TRACK SEGMENT FROM BS 364 - 409+16 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802, SRM 51-40-11, AND AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 473-559) · airframe 31,081 hrs · 28,303 cycles

LT SIDE SEAT TRACK FROM BS 473.15 - 559.80 HAS CORROSION. REMOVED DRILLED AND INSTALLED NEW SERVICEABLE SEAT TRACK IAW AMM 53-01-11-000-802 & 53-01-111-400-802 & SRM 51-40-11.

Part: ANGLE — CRACKED (BS 484) · airframe 31,081 hrs · 28,303 cycles

BS 484 ANGLE IS CRACKED AT RBL 36. REMOVED ANGLE IAW SRM 51-42-06 AND 51-42-21. REPAIRED IAW REO 601R-53-41-059.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 31,081 hrs · 28,303 cycles

LEFT FLOOR SUPPORT HAS CORROSION FROM BS 559+112 - 559+80. BLENDED CORROSION IAW SRM 51-12-00-00. COMPLIED WITH REO 601R-53-00-526.

Part: ANGLE — CORRODED (BS 574-589) · airframe 31,081 hrs · 28,303 cycles

CORROSION ON ANGLE LBL 27 FROM BS 574 - 589. AROUND SCREW HOLES. BLENDED CORROSION IAW SRM 51-12-00-00.

Part: HINGE — GOUGED (PAX DOOR) · airframe 31,081 hrs · 28,303 cycles

ASD PIANO HINGE ASD HALF HAS GOUGES AT NR 4, 11, 22, 23, 24 & 25 LUGS COUNTING FROM THE FWD END. COMPLIED WITH REO 601R-52-11-1347.

Part: FLOOR SUPPORT — CORRODED (BS 559-574) · airframe 31,081 hrs · 28,303 cycles

LEFT FLOOR SUPPORT HAS CORROSION FROM BS 559+112 - 574. REMOVED CORROSION IAW SRM 51-12-00-00. COMPLIED WITH REO 601R-53-00-526.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 31,081 hrs · 28,303 cycles

CORROSION ON LT FLOOR SUPPORT FROM BS 559 - 559+80. BLENDED CORROSION IAW SRM 51-12-00-00. COMPLIED WITH REO 601R-53-00-526.

Part: ANGLE — CRACKED (BS 484) · airframe 31,081 hrs · 28,303 cycles

BS 484 ANGLE CRACKED . REMOVED CRACKED ANGLE IAW SRM 51-42-06 AND 51-42-21. REPAIRED IAW REO 601R-53-41-059.

Part: ISOLATOR — BROKEN (PRESSURE BLKHD) · airframe 31,081 hrs · 28,303 cycles

ISOLATOR BROKEN ON AFT PRESSURE BULKHEAD. REMOVED BROKEN ISOLATOR AND REPLACED ONE IAW SRM 51-42-13.

Part: ACCESS PANEL — LOOSE (RUDDER) · airframe 31,083 hrs · 28,304 cycles

INSPECTION COVERS ON BOTTOM SURFACE OF RUDDER APPEAR TO BE LOOSE AND CONTACTING FUSELAGE TAILCONE. COMPLIED WITH REO 601R-55-41-018 AND REO 601R-55-41-018 01.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 31,083 hrs · 28,304 cycles

SMALL CRACK AT PAX DOOR AFT DRAG ANGLE BY DOOR ASSIST ACTUATOR PULLEY BRACKET. COMPLIED WITH REO 601R-52-11-513. REMOVED PULLEY FITTING ASSY 601R-31706-1, REF IAW SRM 51-42-06-00. COMPLIED WITH REO 601R-52-11-513, REV A. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702.

Part: DOOR — LACK OF LUBE (EMERGENCY EXIT) · airframe 31,081 hrs · 28,303 cycles

LEFT OVERWING EMERGENCY EXIT FAILED THE FUNCTIONAL TEST. PERFORMED LUBRICATION OF LT OVERWING EMERGENCY EXIT IAW AMM 72-20-52-640-802. COMPLIED WITH FUNCTIONAL TEST OF LT EMERGENCY EXIT IAW AMM 52-21-00-720-801 FUNCTIONAL TEST GOOD.

Part: STRAP — CRACKED (RT WING) · airframe 31,083 hrs · 28,304 cycles

RT WING LOWER SURFACE CRACK AT WS 148.019. R & R JOINT STRAP IAW SRM 51-42-21 AND 51-42-06. REMOVED JOINT STRAP AND WAS FOUND CRACKED REPLACED JOINT STRAP IAW SRM 51-42-21 51-42-06.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 30,435 hrs · 27,676 cycles

FWD EMERGENCY LIGHTS INOPERATIVE. R & R THE BATTERY PACK IAW AMM 33-51-04. OPS CHECKED GOOD.

Part: SKIN — CRACKED (RT WING) · airframe 30,354 hrs · 27,602 cycles

CRACK FOUND ON RT WING LOWER WING PLANK FWD SPLICE JOINT RWS 65.75. COMPLIED WITH REO 601R-57-21-2188. MAJOR REPAIR.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 30,093 hrs · 27,350 cycles

SMALL CRACK AT PAX DOOR AFT DRAG ANGLE.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 30,074 hrs · 27,329 cycles

SMALL CRACK AT PAX DOOR AFT DRAG ANGLE BY DOOR ASSIST ACTUATOR PULLET BRACKET. REPAIRED IAW REO 601R-52-11-1360, REV. B.

Part: SPRING ASSY — BROKEN (PAX DOOR) · airframe 29,667 hrs · 26,929 cycles

PAX DOOR WILL NOT OPEN. R & R BROKEN SPRING ROD ASSEMBLY ON PRESSURE VENT FLAP IAW AMM 52-11-15. OPS CHECK GOOD, AC OK FOR SERVICE.

Part: SKIN — CRACKED (RT WING) · airframe 29,646 hrs · 26,906 cycles

RT WING, LOWER SURFACE, CRACKED AT WS 149. COMPLIED WITH GREO 601R-57-21-138 REV A.

Part: LIGHT — UNSERVICEABLE (EXTERIOR) · airframe 29,244 hrs · 26,500 cycles

EXTERIOR EMERGENCY LIGHT UNSERVICEABLE. R & R EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21.

Part: BULKHEAD — CRACKED (BS 954) · airframe 27,430 hrs · 24,625 cycles

FS 621, BULKHEAD FAILS NDT AT UPPER CARGO TRACK LBL 27.50 WL 130 WITH AN INDICATION FULL SCREEN HEIGHT. C/W REO 601R-53-61-1541, REV D DATED 10/31/2011. FOUND TO BE SATISFACTORY.

Part: ANGLE — CRACKED (BS 280) · airframe 27,427 hrs · 24,621 cycles

WHILE PERFORMING INSPECTION OF PASSENGER DOOR UPPER AND LOWER SILLS IAW 53-21-126 PART 9, FOUND ANGLES ON INBD AND OTBD SIDE OF STR 3L JUST AFT OF FS 280 TO SPLIT THROUGH THE WIDTH OF FLANGE APPROX .750 INCHES LONG. REMOVED DAMAGED ANGLES 2 EA AFT OF FS 280 STR 3 IAW SRM 51-42-06. LOCATED FASTENER HOLES ONTO NEW SERVICEABLE ANGLES IAW SRM 51-40-11 AND FINISHED IAW SRM 51-25-00. INSTALLED NEW SERVICEABLE ANGLE IAW SRM 51-42-06.

Part: SUPPORT CHANNEL — CRACKED (CARGO DOOR) · airframe 27,427 hrs · 24,621 cycles

CARGO DOOR FWD LOWER SUPPORT CHANNEL CRACKED. R & R CARGO DOOR FWD LOWER SUPPORT CHANNEL PN IAW SRM 51-42-06.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,189 hrs · 23,262 cycles

EMERGENCY "EXIT" LIGHT INOPERATIVE AT FWD CABIN PAX ENTRY. REMOVED AND INSTALLED A NEW EXIT SIGN IAW AMM 33-51-10. OPS CHECKED GOOD.

Part: LIGHT — MISSING (CABIN) · airframe 26,155 hrs · 23,221 cycles

EXIT SIGN AT FWD ENTRANCE DOOR MISSING. REPLACED FLOOR LEVEL EMERGENCY FLOOD LIGHT AT PAX DOOR ENTRANCE IAW AMM 33-51-19. OPS TESTED GOOD.

Part: PROXIMITY SENSOR — OUT OF ADJUST (MLG) · airframe 25,860 hrs · 22,907 cycles

ON TAKEOFF, RECIEVED REO "GEAR DISAGREE" AND "NOSE DOOR OPEN" WARNING MESSAGES. COMPLIED W/ QRH CONFERED W/ DISPATCH AND MX AND CONTINUED AT 250 KTS AND GEAR DOWN. (EMERGENCY DECLARED AS A PRECAUTION) PERFORMED ADJUSTMENT OF NLG STEERING CENTERED, OLEO EXTENDED PROX SENSOR IAW AMM 32-61-05. OPS TEST GOOD . EXTENSION /RETRACTION CHECKS PERFORMED IAW AMM 32-33-00. RII COMPLIED IAW GMM 3-3, NO DEFECTS NOTED. (SDR CLOSED)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 24,883 hrs · 21,842 cycles

NR5 & NR6 EXTERIOR AND NR3 INTERIOR CEILING EMERGENCY LIGHTS INOP. R & R NR3 BATTERY PACK IAW AMM 33-51-04. OPS CHECK GOOD. R & R NR3 BATTERY PACK IAW AMM 33-51-04. OPS CHECK GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 24,302 hrs · 21,185 cycles

NR 8 EXTERIOR EMERGENCY LIGHT (RT AFT) INOP. RELAMPED NR 8 EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21. RELAMPED NR 8 EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21. (CLOSED)

Part: ACTUATOR — FAILED (RUDDER) · airframe 24,188 hrs · 21,060 cycles

UNCOMMANDED LARGE RUDDER DEFLECTION CAUSING LARGE YAWING MOMENT IN CRUISE AND ON APPROACH. AP ENGAGEMENT MADE NO DIFFERENCE. (ENROUTE, ACFT DIVERTED TO DUE TO MX -- EMERGENCY DECLARED) R & R LT AND RT YAW DAMPERS IAW AMM CH 22-22-01-000-801. PERFROMED OPS TEST IAW AMM CH 22-22-01-710-802. OPS CHECKED GOOD AT THIS TIME. PERFORMED AN OPS TEST OF RUDDER CONTROL SYS IAW AMM 27-21-00. NO DEFECTS NOTED. (CLOSED)

Part: PLACARD — UNKNOWN (EMERGENCY EXIT) · airframe 23,546 hrs · 20,325 cycles

BOTH EMERGENCY EXITS (OVERWING) PLACARDS ARE NOT IN COMPLIANCE WITH AD 2010-09-10. R & R LT AND RT OVERWING EXIT OPERATING INSTRUCTIONS PLACARDS IN THE PROPER LOCATIONS IAW AMM 11-30-00-000-801 AND 11-30-00-400-801.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 23,546 hrs · 20,325 cycles

FLOORBEAM CAP AT LBL 9 FS 605 IS CORRODED. RESOLVED ON W/O: 179116 TASKCARD: N/R-00834 ). DUE TO AVAILABILITY FASTENER LISTED IS STEP 6 OF MWC 414, CANNOT BE INSTALLED AT THIS TIME. FASTENER IS INSTALLED UNDER STEP 7 OF MWC 414 IAW REO 601R-53-61-3874 (PLT114-8), STEPS 1, 2, 3. ECTC SIGN OFF STEP 10 OF MWC 414. C/W EC/TC REO 601R-53-61-3780 AND BOMBARDIER REO 601R-53-61-3780 REV-- DATED 8/21/2010 AS WRITTEN. RII FOUND TO BE SATISFACTORY/ASA RII C/W 5300002".

Part: FLOORBEAM — CORRODED (BS 605) · airframe 23,546 hrs · 20,325 cycles

FLOORBEAM CAP AT LBL 9 FS 605 IS CORRODED. REPAIRED FLOORBEAM.

Part: ANGLE — CRACKED (BS 625) · airframe 23,546 hrs · 20,325 cycles

LT SIDE OBLIQUE ANGLE FROM FS 625 IS CRACKED. REMOVED ANGLE IAW SRM 51-42-21. INSTALLED NEW ANGLE IAW REO 601R-53-61-100 & SRM 51-42-21.

Part: POST — FAILED (BS 409) · airframe 23,546 hrs · 20,325 cycles

FS 409+128, LBL 18, VERT POST FAILS NDT WITH AN INDICATION ON OTBD POST AFT RADIUS (UPPER) GREATER THAN 50 PERCENT SCREEN HEIGHT APPROX .3" LONG. COMPLIED WITH EC/TC REO 601R-53-11-926 IAW REO 601R-53-11-926 REV B.

Part: WEB — CORRODED (BS 280) · airframe 23,546 hrs · 20,325 cycles

FS 280 WEB HAS SEVERAL AREAS OF CORROSION. COMPLIED WITH EC/TC REO 601R-53-11-926 IAW REO 601R-53-11-926 REV B.

Part: CHANNEL — CORRODED (BS 280) · airframe 23,546 hrs · 20,325 cycles

FWD J-CHANNEL AT FS 280 IS CORRODED BEYOND LIMITS. REMOVED FWD "J" CHANNEL IAW SRM 51-42-06. INSTALLED FWD "J" ANGLE IAW SRM 51-42-06.

Part: POST — CRACKED (BS 409) · airframe 23,546 hrs · 20,325 cycles

FS 409+128 RBL 18 VERT POST FAILS NDT WITH AN INDICATION ON BOTH INBD AND OTBD POST IN AFT RADIUS (UPPER) BOTH GREATER THAN 50 PERCENT SCREEN HEIGHT APPROX .3 LONG. REMOVED POST IAW SRM 51-42-06. LOCATED, DRILLED AND INSTALLED POST IAW REO 601R-53-41-889, 51-40-11 AND 51-42-06. COMPLIED WITH EC/TC REO 601R-53-41-889 AND MEET ALL THE REQUIREMENTS OF REO 601R-53-41-889 REV A.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 23,546 hrs · 20,325 cycles

PAX DOOR AFT DRAG ANGLE IS CRACKED. REMOVED DAMAGED AND INSTALLED A NEW DRAG ANGLE 601R31772-5S IAW SRM 51-42-06.

Part: ANGLE — CORRODED (SILL) · airframe 23,546 hrs · 20,325 cycles

SERVICE DOOR SILL ANGLE CORRODED IN SEVERAL AREAS. FOUND CORROSION TO BE APPROX .002" DEEP AND WITHIN ALLOWABLE LIMITS IAW SRM 51-21-23 AND 53-00-00. REMOVED THE LIGHT CORROSION IAW SRM 51-21-06.

Part: FLOOR SUPPORT — CORRODED (BS 559-621) · airframe 23,546 hrs · 20,325 cycles

FLOOR SUPPORT OTBD OF RBL 36 IS CORRODED FROM FS 621 TO 559+80. BLENDED CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00, FIG 102. REMOVED FLOOR SUPPORT. LOCATED NEW . INSTALLED IAW SRM 51-42-06 AND 51-42-21.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 23,546 hrs · 20,325 cycles

FS 280, LBL 9, INBD FLOOR SUPPORT CLIP CRACKED. FLOOR SUPPORT CLIP REPLACED ON MWC 8747421 OP 356.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 23,546 hrs · 20,325 cycles

FS 280, LBL 9, OTBD FLOOR SUPPORT CLIP CRACKED. FLOOR SUPPORT CLIP REPLACED ON MWC 8747421 OP 356.

Part: INTERCOSTAL — CORRODED (BS 589) · airframe 23,546 hrs · 20,325 cycles

INTERCOSTAL CAP AT FS 589 BETWEEN LBL 18 & 27 IS CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 51-21-06 AND 253-00-00. INTERCOSTAL CAP REQUIRES REPLACEMENT. REMOVED INTERCOSTAL CAP IAW SRM 51-42-06 AND 51-42-21. INTERCOSTAL CAP REQUIRES DRILL, LOCATE AND INSTALL. LOCATED, DRILLED AND INSTALLED IAW SRM 51-42-06, SRM 51-42-15 AND SRM 51-42-21. (CLOSED)

Part: FITTING — CRACKED (BS 460) · airframe 23,546 hrs · 20,325 cycles

RBL 9, FS 460 OTBD FITTING CRACKED. REMOVED CRACKED FITTING AND ALL THE RIVETS AND LOCK FASTENERS AT RBL 9, FS 460 OTBD AND LOCATED, DRILLED AND FITTED THE NEW PART IAW SRM 51-42-06. REMOVED LOCK FASTERNERS IAW SRM 51-42-23 AND SRM 51-40-11. INSTALLED FITTING AT RBL 9, FS 460 IAW SRM 51-42-21, 51-42-60, 51-25-01 AND 51-21-11.

Part: FLOORBEAM — CORRODED (BS 605) · airframe 23,546 hrs · 20,325 cycles

FLOORBEAM CAP AT LBL 9, FS 605 IS CORRODED. REMOVED CORROSION FROM FLOORBEAM CAP. DEEPEST MATERIAL LOSS AT 0.012 DEEP X 0.75" W X 0.50" L AND FOUND TO BE OUT OF LIMITS IAW SRM 51-21-06, 53-00-00, 53-61-43. REMOVED FLOORBEAM CAP BETWEEN FS 570 AND FS 621 IAW SRM 51-42-06 AND SRM 51-42-21. DRILLED NEW SERVICEABLE FLOORBEAM CAP IAW SRM 51-40-11 AND INSTALLED.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 23,546 hrs · 20,325 cycles

PLATE ASSY, PN 601R38957-119, SHOWS HEAVY CORROSION. AFTER PAINT REMOVAL FOUND TO BE LIGHT CORROSION. REMOVED CORROSION IAW SRM 51-21-06. ALODINED, PRIMED, AND TREATED AREA IAW SRM 51-32-00 AND 51-25-00. REMOVED OLD CORROSION NUTPLATE AND INSTALLED NEW ONE IAW SRM 51-45-00. (CLOSED)

Part: SILL — CORRODED (BS 349) · airframe 23,546 hrs · 20,325 cycles

RT FLOOR SUPPORT SILL CORRODED AT AFT OF FS 349.00. REMOVED CORROSION ON SILL IAW SRM 51-21-06. FOUND WITHIN LIMITS IAW SRM 53-00-00.

Part: RIB — CRACKED (LT WING LE) · airframe 23,546 hrs · 20,325 cycles

LT INBD L/E HAS A CRACKED RIB UNDER PANEL 520CZ. REMOVED DAMAGED RIB IAW SRM 51-42-06 AND 51-42-13. LOCATED HOLES IN NEW RIB IAW SRM 51-40-11. INSTALLED NEW RIB IAW SRM 51-42-06 AND 51-42-13.

Part: ANGLE — CORRODED (BS 280) · airframe 23,546 hrs · 20,325 cycles

FS 280, J-ANGLE PREVIOUS REPAIR BETWEEN LBL 9 AND RBL 9 CORRODED. REPLACED FS 280 J-ANGLE ON MWC 8747421 OP 356.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · airframe 23,546 hrs · 20,325 cycles

FLOORBEAM CAP AT LBL 27 FROM FS 621 TO 574 IS CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 51-21-06 AND 53-00-00. LOCATED AND DRILLED IAW SRM 51-42-06, 51-42-21 AND REO 601R-53-61-3778.

Part: FLOOR SUPPORT — CORRODED (BS 319.7) · airframe 23,546 hrs · 20,325 cycles

FLOOR SUPPORT ANGLE AT FS 319.70 JUST INBD OF FWD SERVICE DOOR LWR CORNER CORRODED. REMOVED CORROSION IAW SRM 51-21-06, FOUND WITHIN LIMITS IAW SRM 53-00-00.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 23,546 hrs · 20,325 cycles

FS 280, RBL 9, OTBD FLOOR SUPPORT ANGLE CRACKED. FLOOR ANGLE REPLACED ON MWC 8747421.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 23,546 hrs · 20,325 cycles

FS 280, RBL 9 INBD FLOOR SUPPORT CLIP CRACKED. REPLACED ON MWC 8747421 OP 356.

Part: SKIN — CRACKED (FUSELAGE) · airframe 23,546 hrs · 20,325 cycles

FUSELAGE SKIN ON RT SIDE FOR NLG SPADE DOOR IS CRACKED IN CORNER. COMPLIED WITH EC/TC REO 601R-53-11-0048 IAW REO 601R-53-11-0048, REV FOUND TO BE SATISFACTORY.

Part: BRACKET — CRACKED (INLET COWL) · airframe 23,546 hrs · 20,325 cycles

RT ENGINE INLET COWL HAS A CRACKED BRACKET ON AFT SIDE OF BULKHEAD AT 5 O'CLOCK POSITION. C/W REO 601R-71-61-3415 REV NC.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 23,219 hrs · 19,955 cycles

LT EXTERIOR NR3 EMERGENCY LIGHT INOP. REPLAMPED LT EXTERIOR NR3 EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECK GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 23,219 hrs · 19,955 cycles

RT EXTERIOR NR 8 EMERGENCY LIGHT INOP. RELAMPED RT EXTERIOR NR 8 EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECK GOOD.

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 21,711 hrs · 18,186 cycles

FLAPS FAIL AT 30 DEG, EMERGENCY DECLARED, EQUIPMENT ON STANDBY AS A PRECAUTION.

Part: WARNING LIGHT — MULTIPLE FAIL · airframe 21,606 hrs · 18,068 cycles

PRIOR TO V1, RECEIVED EFIS COMP MON. APPROX V1 NOTICED AMBER IAS FLAG CONTINUED. AFTER T/O , LOST F/O SIDE AIR DATA. [EMERGENCY DECLARED -- AIRCRAFT RETURNED TO DEPARTURE AFTER T/O].

Part: FLAP — MALFUNCTIONED (WING) · airframe 19,978 hrs · 16,504 cycles

FLAPS FAIL CAUTION WHEN RETRACTING FLAPS FROM 8 DEGREES TO 0 DEGREES ON DEPARTURE. ACFT RETURNED TO DEPARTURE AFTER T/O, EMERGENCY DECLARED.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 19,885 hrs · 16,429 cycles

THE 281ELW IS CRACKED ALONG VERTICAL CORNERS. REMOVED COMPOSITE DAMAGE ALONG VERTICAL CORNER, FABBED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER USING RTV106 AND CR3523-4-4 FASTENERS PO 100782 IAW BOMBARDIER REO 601R-25-53-005.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 19,885 hrs · 16,429 cycles

FS 484 ANGLE RBL 27 IS CRACKED IN RADIUS. REMOVED CLIP AND RIVETS AND INSTALLED NEW CLIP AND RIVETS IAW CRJ 200 SRM 51-42-06, 51-42-20, AND REO 601R-53-41-059. REQUIRES PAINT AND DYNATROL. PAINTED REPAIRED AREAS AT FS 484 ANGLE RBL 27 IAW CRJ SRM 51-25-01. ALSO APPLIED DYNATROL TO REPAIRED AREAS IAW CRJ SRM 51-21-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,885 hrs · 16,429 cycles

CARGO SEAT TRACK AT RBL 27 FS 559+80 IS CORRODED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,885 hrs · 16,429 cycles

CARGO SEAT TRACK AT LBL 9 FS 559+80 IS CORRODED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 19,885 hrs · 16,429 cycles

FS 484 ANGLE LBL 27 IS CRACKED IN RADIUS. REMOVED CLIP AND RIVETS AND INSTALLED NEW CLIP AND RIVETS IAW CRJ 200 SRM 51-42-06, 51-42-20, AND REO 601R-53-41-059. REQUIRES PAINT AND DYNATROL. PAINTED REPAIR AREA IAW CRJ SRM 51-25-01 AND APPLIED DINITROL IAW CRJ SRM 51-21-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,885 hrs · 16,429 cycles

CARGO SEAT TRACK AT LBL 27 AT FS 559+80 IS CORRODED.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 19,885 hrs · 16,429 cycles

LIGHT SURFACE CORROSION UNDER 281LLF AT CARGO DOOR ENTRANCE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,885 hrs · 16,429 cycles

CARGO SEAT TRACK AT RBL 9 FS 559 + 80 IS CORRODED.

Part: POST — CRACKED (FUSELAGE) · airframe 19,885 hrs · 16,429 cycles

FS 409+128 LBL 18 LT INBOARD POST WL 69 HAS INDICATION NOTED APPROX .3 INCH LENGTH. FAILS NDT. WORK DONE IAW CRJ 200 SRM 51-42-06, CRJ 200 SRM 51-24-21 AND BOBARDIER DWG 601R32208, CRJ 200 NDTM PT 1 51-20-08, ASA CRJ 200 SRM 51-25-00, ASA CRJ 200 SRM 51-42-22.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 19,885 hrs · 16,429 cycles

CARGO DOOR SUPPORT BEAM LOWER ANGLE IS CRACKED APPROX .2 INCHES IN LENGTH.

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 19,885 hrs · 16,429 cycles

RT FS 484 RBL 36.0 INTERCOSTAL CRACKED PREVIOUS REPAIR. REMOVED OUTBOARD PULLEY AND BRACKET AND SLID FWD. REMOVED CRACKED ANGLE. FABRICATED NEW ANGLE BRACKET. ANGLE BRACKET REQUIRES HOLE TRANSFERS AND FURTHER SHAPING. AFTER REPAIR OUTBOARD CONTROL CABLE PULLEY AND BRACKET ON FS 484 REQUIRES INSTALLATION. REPLACED RT FS 484 RBL 360 INTERCOSTAL CLIP IAW SRM 51-41-02 AND REO 610R-53-41-059. INSTALLED OUTBOARD CONTROL CABLE PULLEY BRACKET IAW SRM 51-41-02. C/W EC/TC REO 601R-53-41-059.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 19,885 hrs · 16,429 cycles

PAX DOOR AFT DRAG ANGLE IS CRACKED AT DOOR ASSIST CABLE PULLEY BRACKET APPROX 1 INCH LONG. REPAIRED PAX DOOR AFT DRAG ANGLE IAW CRJ 200 PER REO 601R-52-11-513 ASA RII C/W: 5300014.

Part: ANGLE — CRACKED (BS 625) · airframe 19,885 hrs · 16,429 cycles

RT FS 625.0 ANGLE IS CRACKED. REMOVED AND REPLACED RT FS 625.00 ANGLE IAW SRM 51-42-06.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,885 hrs · 16,429 cycles

CARGO SEAT TRACK AT LBL 9 FS 559+96 IS CORRODED. REMOVED CORRODED CARGO SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-01-11-400-802. DRILLED HOLES IAW SRM 51-41-02. COUNTERSUNK HOLES IAW SRM 51-40-11.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 19,885 hrs · 16,429 cycles

CARGO SEAT TRACK AT RBL 9 FS 559+96 IS CORRODED. REMOVED CORRODED CARGO SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-01-11-400-802. LOCATED AND DRILLED HOLES IAW SRM 51-41-02. COUNTERSUNK HOLES IAW SRM 51-40-11.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 19,885 hrs · 16,429 cycles

CARGO SEAT TRACK AT LBL 9 FS 621 IS CORRODED. REMOVED CARGO BAY SEAT TRACK AY FS 621 LBL 9 AND INSTALLED SERVICEABLE SEAT TRACK IAW SRM 51-41-04.

Part: ANCHOR — CORRODED (CARGO BAY) · airframe 19,885 hrs · 16,429 cycles

FIVE CARGO BAY PLATE ANCHORS ARE CORRODED. REMOVED AND REPLACED 5 EACH CARGO DOOR ANCHOR PLATES IAW SRM 51-41-04.

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 19,885 hrs · 16,429 cycles

LBL 36.0 FS 484 INTERCOSTAL CRACKED. REMOVED OUTBOARD PULLEY AND BRACKET AND SLID FWD. REMOVED CRACKED ANGLE. FABRICATED NEW ANGLE BRACKET. ANGLE BRACKET REQUIRES HOLE TRANSFERS AND FURTHER SHAPING. AFTER REPAIR OUTBOARD CONTROL CABLE PULLEY AND BRACKET ON FS 484 REQUIRES INSTALLATION. REPLACED LBL 360 FS 484 INTERCOSTAL CLIP IAW REO 601R-53-41-069. INSTALLED OUTBOARD CONTROL CABLE PULLEY BRACKET IAW SRM 51-41-02. C/W EC/TC REO 601R-53-41-059.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 19,885 hrs · 16,429 cycles

FS 559 BULKHEAD WEB AND CAP ANGLE HAS INDICATIONS NOTED. RT WEB WL 58.70 HAS INDICATION NOTED APPROX .2 INCH IN LENGTH 70 PERCENT FSH AND LT CAD ANGLE AT LBL 18 HAS INDICATION NOTED APPROX .3 INCH IN LENGTH 70 PERCENT FSH, FAILED NDT INSPECTION. COMPLIED WITH EC/TC REO 601R-53-41-260 IAW BOMBARDIER REO 601R-53-41-260, REV C. C/W EC/TC REO 601R-53-41-827 & MET ALL THE REQUIREMENTS OF REO 601R-53-41-827.

Part: RIB — CRACKED (LLT WING) · airframe 19,885 hrs · 16,429 cycles

LT WING BATT RIB ASSY AT WS 53.60 IS CRACKED .800 INCH LONG JUST AFT OF TOP AFT FASTENER BEFORE THE RADIUS. COMPLIED WITH REPAIR TO LT BATT RIB AT WS 53.60 REPAIR IAW BOMBARDIER REO 601R-57-51-046.

Part: DOOR — BINDING (PAX DOOR) · airframe 19,723 hrs · 16,274 cycles

FLIGHT ATTENDANT REPORTS DIFFICULTY CLOSING MAIN CABIN DOOR. FLT 4941 DEL 23 MINS.

Part: DOOR — BINDING (PAX DOOR) · airframe 19,718 hrs · 16,269 cycles

FLIGHT ATTENDANT REPORTS DIFFICULTY CLOSING MAIN CABIN DOOR. FLT 4941 DEL 23 MINS.

Part: CONNECTOR — LOOSE (NLG) · airframe 19,415 hrs · 15,991 cycles

NOSE DOOR OPEN RED MSG AFTER TAKE OFF. ACFT RETURNED TO BNA AFTER T/O, EMERGENCY DECLARED. FLT 4992 DEL 75 MINS. NC. FLT 4992 CX. FOUND CANNON PLUG LOOSE ON NLG DOOR SELECTOR VALVE. RESECURED IAW CRJ200 AMM 32-22-20. DOORS OPS CHECK NORMAL. ON GROUND WITH MTC SWITCH.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

LT WING EMERGENCY MID LIGHT INOP. RELAMPED LT WING EMERGENCY MID LIGHT IAW 33-51-21. (A)

Part: STEP — BROKEN · airframe 18,426 hrs · 15,104 cycles

TOP THRESHOLD STEP BROKEN.

Part: HANDLE — STIFF (PAX DOOR) · airframe 17,645 hrs · 14,445 cycles

PAX DOOR HANDLE DIFFICULT TO OPERATE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 16,664 hrs · 13,658 cycles

AFT EMERGENCY LIGHT IS INOP ON RIGHT OF FUSELAGE.

Part: DOOR — STUCK (SERVICE DOOR) · airframe 16,317 hrs · 13,396 cycles

SERVICE DOOR WON'T OPEN.

Part: SKIN — CRACKED (PAX DOOR) · airframe 16,039 hrs · 13,189 cycles

CRACK FOUND ON PAX DOOR INNER SKIN AT FS 329.50 NEAR HANDLE PIVOT SHAFT.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 16,002 hrs · 13,165 cycles

PAX DOOR HANDLE IS CRACKED. PAX DOOR STEP NR 2 REMOVED IAW AMM 20-21-00. HANDLE REMOVED IAW AMM 52-11-03. HANDLE INSTALLED IAW AMM 52-11-03. PAX DOOR STEP NR 2 INSTALLED IAW AMM 20-21-00. PAX DOOR FUNCTIONAL TEST C/OUT IAW AMM 52-11-03. PAX DOOR OPS TEST C/OUT IAW AMM 52-11-03.

Part: FRAME — CRACKED (BS 640) · airframe 16,002 hrs · 13,165 cycles

SUSPECT CRACK ON LEFT DOUBLER AT FRAME 640. PERFORMED EDDY CURRENT INSPECTION OF SUSPECT AREA PER MTC REQUEST IAW CRJ 200 NDTM PART 1, 51-20-06. LEFT FS 640 IS CRACKED. REMOVED DAMAGE ON LT DOUBLER FRAME 640. AND PERFORMED EO 600-53-059 PART B ESB MOD. ALL WORK ACCOMPLISHED ON N/R 13,14,15 AND DEVIATION TO EO 059 PART B.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 16,002 hrs · 13,165 cycles

ASD (PAX DOOR) OUTER HANDLE CRACKED. PAX DOOR OUTER HANDLE REMOVED AND REPLACED.

Part: FRAME — CRACKED (BS 640) · airframe 16,003 hrs · 13,165 cycles

SUSPECT CRACK ON LEFT DOUBLER AT FRAME 640. PERFORMED EDDY CURRENT INSPECTION OF SUSPECT AREA PER MTC REQUEST. LEFT FS 640 DOUBLER IS CRACKED.

Part: HANDLE — CRACKED (AIRSTAIR DOOR) · airframe 16,003 hrs · 13,165 cycles

ASD OUTER HANDLE CRACKED.

Part: PLATE — CORRODED · airframe 15,082 hrs · 12,479 cycles

ASD - HINGE HORIZONTAL PLATE CORRODED UNDER AND AROUND DOOR HANDRAIL PIVOT FITTINGS - FS 310 TO 349 - BL 44 TO 47 LEFT. REMOVED FWD AND AFT HANDRAIL PIVOT FITTINGS ON STRINGER FS 310 TO 349 BL44 TO 47 LT. REMOVED ASD PROX SWITH AND GROUNDING POINT. ALL WORK DONE PER CRJ200 SRM 51-41-02 CM20420 AFTER FURTHER INSPECTION OF STRINGER AT STA 310 THRU 349 , LH BL 44 TO LH 47,DETERMINED STRINGER TO BE "OUT - OF LIMITS ". REMOVED STRINGER , AND ATTACHED PARTS ( 2 EA BRACKETS AT STATIONS 315 AND 341 , AND 3 EA UPPER ATTACH ANGLES , STATION 310 THRU 349 ). REMOVED ALL PARTS IAW CRJ 200 SRM 51-42-06 ,AND 51-42-13.

Part: ANCHOR FITTING — CRACKED (PAX DOOR) · airframe 15,082 hrs · 12,479 cycles

PAX DOOR CABLE FWD ANCHOR FITTING CRACKED (MARKED).

Part: ATTACH ANGLE — CRACKED (BS 280) · airframe 15,082 hrs · 12,479 cycles

FOUND LBL -9 OUTBD AFT ATTACH CLIP CRACKED AT FS 280. REMOVED AND REPLACED IAW SRM 51-42-21. (CLOSED)

Part: HANDLE — CRACKED (E&E BAY DOOR) · airframe 15,082 hrs · 12,479 cycles

AVIONIC DOOR EXTERIOR HANDLE CRACKED BASE.

Part: HANDLE — MALFUNCTIONED (SERVICE DOOR) · airframe 15,082 hrs · 12,479 cycles

SERVICE DOOR EXTERIOR HANDLE WILL NOT DELOPY OPEN. HANDLE WILL NEED TO BE INSPECTED ONCE OPEN FOR CORROSION. INSPECTED SERVICE DOOR HANDLE NO CORROSION NOTICED LUBED HANDLE IAW MM 12-00 OPS CK GOOD ( SUPPLEMENTAL - SDR CLOSED)

Part: WEB — CRACKED (BS 280) · airframe 15,082 hrs · 12,479 cycles

THE 280 WEB CRACKED FROM BOTTOM 2 RIVET JUST O/B OF RBL 9.0. ALL WORK COMPLETED IAW SRM. (CLOSED)

Part: FLOOR SUPPORT — CORRODED (BS 280) · airframe 15,082 hrs · 12,479 cycles

FWD FLOOR SUPPORT ANGLE, FWD SIDE OF FS 280 HAS CORROSION AROUNG RECEPTICLE'S. REMOVED FWD FLOOR SUPPORT ANGLE AND REMOVED LIGHT CORROSION ON FWD FLOOR SUPPORT ANGLE, FWD SIDE OF FS 280 PER CRJ 200 SRM 51-21-06 FOUND TO BE WITHIN LIMITS PER CRJ 200 SRM 53-11-00 PG BLOCK 101- 199 JP21771 APPLIED SURFACE FINISH TO FWD FLOOR SUPPORT ANGLE PER CRJ 200 SRM 51-25-00. JP21771 REINSTALL. REINSTALLED FWD FLOOR SUPPORT PER SRM 51-42-06. (CLOSED)

Part: BULKHEAD — CORRODED (BS 280) · airframe 15,082 hrs · 12,479 cycles

AFT TOP ANGLE OF THE 280 BULKHEAD HAS CORROSION AT SEVERAL LOCATION BETWEEN LRL 9.0 AND RBL 9.0. ALL WORK COMPLETED IAW ALL SRM`S AND MM`S (CLOSED)

Part: WEB — CORRODED (BS 280) · airframe 15,082 hrs · 12,479 cycles

THE 280 WEB HAS CORROSION ON TOP EDGE BETWEEN FWD AND AFT ANGLES. REMOVED CORROSION FROM FS 280 WEB PER CRJ 200 SRM 51 21 06 FOUND TO BE WITHIN LIMITS PER CRJ 200 SRM 53 11 00. (CLOSED)

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 14,797 hrs · 12,265 cycles

FOUND FS 202.00 BULKHEAD CRACKED AT PARKING BRAKE CABLE HOLE.

Part: DOOR — UNSECURE (AIRSTAIR) · airframe 14,690 hrs · 12,184 cycles

ASD WILL NOT SECURE CLOSED, FLT 4376 DEL 26 MINS.

Part: HANDLE — STICKS (PAX DOOR) · airframe 14,529 hrs · 12,057 cycles

PAX DOOR RED HANDLE STICKING WHEN CLOSING DOOR.

Part: DOOR — UNKNOWN (MAIN PAX)

DURING A GROUND INSPECTION, THE PASSENGER DOOR WAS FOUND VERY HARD TO CLOSE AND EXTREMELY LOUD. MAINTENANCE OPENED AND CLOSED THE PASSENGER DOOR 6 TIMES WITH NO DEFECTS NOTED. MAINTENANCE ALSO CLEANED, RESEALED THE DOOR STRIKERS, AND LUBRICATED THE SEAL ON THE PASSENGER DOOR FOR PREVENTATIVE MAINTENANCE. AC OK FOR SERVICE. (K)

Part: DOOR — NONE (CABIN)

DURING A GROUND INSPECTION, THE PASSENGER DOOR WAS FOUND TO BE DIFFICULT TO CLOSE. MAINTENANCE REMOVED DEBRIS AND CYCLED PASSENGER DOOR WITH NO DEFECTS NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: DOOR — INOPERATIVE (FUSELAGE)

DURING A GROUND INSPECTION IN MCO, THE PASSENGER DOOR WOULD NOT CLOSE. MAINTENANCE REINSTALLED THE PASSENGER DOOR CABLE ONTO THE PULLEY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STEP — BROKEN (PAX DOOR)

DURING A GROUND INSPECTION IN CVG, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND TO BE BROKEN AT THE ATTACH POINT. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — MALFUNCTIONED (GALLEY)

FLT 4916 - DURING CRUISE FROM ATL-BUF, THE CAPTAIN NOTICED AN ELECTRICAL BURNING SMELL IN THE COCKPIT. SHORTLY AFTER, THE FLIGHT ATTENDANT REPORTED AN ELECTRICAL BURNING SMELL IN THE CABIN. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO TYS, WHERE IT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE GALLEY FLOOR LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: HANDLE — BINDING (PAX DOOR)

DURING A GROUND INSPECTION, THE PASSENGER DOOR WAS FOUND HARD TO OPEN FROM THE OUTSIDE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR OUTER HANDLE. OPS CHECK GOOD. AIRCRAFT OF FOR SERVICE. (K)

Part: FRAME — CRACKED (FUSELAGE)

DURING AN A-CHECK IN BTR, THE RIGHT SIDE FRAME AND DOUBLER AT FS 640, STRINGER 10R WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE RIGHT SIDE FRAME AND DOUBELR AT FS 640, STRINER 10R IAW SRM 51-40-00. (M)

Part: ANCHOR FITTING — CRACKED (PASSENGER DOOR)

DURING AN A-CHECK, THE FORWARD ANCHOR FITTING ON THE PASSENGER DOOR WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE FORWARD ANCHOR FITTING ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.

Part: LENS — CRACKED (CABIN)

DURING A C-CHECK IN MCN, THE EMERGENCY EXIT LIGHT LENS COVER BY THE SERVICE DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY BY THE SERVICE DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — DAMAGED (CABIN)

DURING A C-CHECK IN MCN, THE EMERGENCY EXIT FLOOR LIGHT AND COVER FORWARD OF THE PASSENGER DOOR WAS FOUND DAMAGED AND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT FOOL FLIGHT ASSEMBLY FORWARD OF THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: SEAL PLATE — CRACKED (CARGO DOOR)

DURING A C-CHECK IN MCN, THE CARGO DOOR SEAL PLATE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE CARGO DORO SEAL PLATE IAW ASA EO 600-53-0117. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE LT AND RT FLOOR SUPPORT ANGLE AT FS 621 IN THE CARGO COMPARTMENT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT AND RIGHT FLOOR SUPPORT ANGLE AT FS 621 IN THE CARGO COMPARTMENT IAW ASA EO 600-53-0105. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE INTERCOSTALS AT FS 484 INBOARD SIDE OF LBL 36 AND RBL 36 AND OUTBOARD OF LBL 27 AND RBL 27 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE INTERCOSTALS AT FS 484 INBOARD SIDE OF LBL 36 AND RBL 36 AND OUTBOARD OF LBL 27 AND RBL 27 IAW ASA EO 600-53-0111. (M)

Part: BRACKET — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE BRACKETS AT FS 280, LBL 9 AND RBL 9 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE BRACKETS AT FS 280, LBL 9 AND RBL 9 IAW SRM 51-00. (M)

Part: STRINGER — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE FS 718 BETWEEN STRINGERS 10-12 ON THE RIGHT SIDE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FS 718 BETWEEN STRINGERS 10-12 ON THE RIGHT SIDE IAW ASA EO 600-53-0067A. (M)

Part: SUPPORT BEAM — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE LEFT AND RIGHT ENGINE SUPPORT BEAM AT BL 36.20 WAS FOUND TO BE CRAKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT AND RIGHT ENGINE SUPPORT BEAM AT BL 36.20 IAW ASA EO 600-53-0070. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DURING GROUND INSPECTION IN DFW, A CABIN CEILING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BURNED OUT CEILING EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)