N445SW

Part: WARNING MESSAGE — ILLUMINATED (ZONE 700) · airframe 43,650 hrs · 39,790 cycles

GEAR DISAGREE WARNING ON DEPARTURE NOSE GEAR DOWN WHILE BOTH MAINS WERE UP. RAN QRH AND EXTENDED GEAR FOR LANDING SUCCESSFULLY. (FLIGHT 5442 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 31401093 WITH THE FOLLOWING CORRECTIVE ACTION: "SEE CP 31401375 FOR REPLACEMENT OF THE NLG OLEO EXTENDED SENSOR BRACKET. SEE CP 31401413 AND CP 31402598 FOR TROUBLESHOOTING AND MAINTENANCE PERFORMED FOR THE NLG SHOCK STRUT REPACK. COMPLIED WITH NLG SHOCK STRUT SERVICING TASK CARD 12-710-003. PERFORMED EXTENSION/RETRACTION OF THE NLG IN REFERENCE TO AMM 32-33-00. OPS CHECK GOOD AT THIS TIME. SEE CAMP CP 31405652 FOR EXTENSION CHECK AFTER 24 HOURS OF THE AIRCRAFTS MOVEMENT."

Part: WARNING MESSAGE — ACTIVATED · airframe 43,214 hrs · 39,294 cycles

FLAPS FAIL CAUTION MESSAGE IN CRUISE. RAN QRH, LANDED NORMALLY. DESCENT RATE AT TOUCHDOWN 300FPM. (FLIGHT 4728 - FILED CLOSED)RESET AND OPERATED FLAPS 5 FULL CYCLES AND COMPLETED AD 2009-06-12/10 COMPLIANCE FORM OK TO CONTINUE IN SERVICE FOR 10 FLIGHT CYCLES COMPLIED WITH IN ACCORDANCE WITH FIM FMRP CHAPTER 27 RESET PROCEDURE AND AD 2009-06-12 TRACKING CREATED FOR FULL AD COMPLIANCE MCI CREATED FOR 10 FLIGHT CYCLE EVENT

Part: KEEPER — DAMAGED (PCU BOLT) · airframe 42,104 hrs · 38,224 cycles

TRANSFER FROM EAML 615 : TRANSFERRED FROM CAMP 35722. UPON REMOVAL OF LT WING FLIGHT SPOILER OB PCU BOLT TO REPLACE DAMAGED ANTI ROTATION KEEPER WC5152 FOUND GOUGED SPOILER HINGE ON T/E OF WING, EVAL (C-CHECK RO 1/3/2024) REMOVED AND INSTALLED NEW SPOILER FITTING ASSEMBLY P/N 601R10086-S0101 REF EO 601R10033 SNIEO S04 DATED 24-NOV-2023, BOMBARDIER DWG 601R10226 REV -Y, AND BOMBARDIER DWG 601R10006 REV -N.. COMPLIED WITH 51-900-1003-SKY AND FUEL LEAK CHECK GOOD . SEE CONTINUATION CARD FOR DETAILS

Part: KEEPER — DAMAGED (LT SPOILER PCU) · airframe 42,104 hrs · 38,224 cycles

TRANSFER FROM EAML 615 : TRANSFERRED FROM CAMP 35722. UPON REMOVAL OF LT WING FLIGHT SPOILER OB PCU BOLT TO REPLACE DAMAGED ANTI ROTATION KEEPER WC5152 FOUND GOUGED SPOILER HINGE ON T/E OF WING, EVAL (C-CHECK RO 1/3/2024) REMOVED AND INSTALLED NEW SPOILER FITTING ASSEMBLY P/N 601R10086-S0101 REF EO 601R10033 SNIEO S04 DATED 24-NOV-2023, BOMBARDIER DWG 601R10226 REV -Y, AND BOMBARDIER DWG 601R10006 REV -N.. COMPLIED WITH 51-900-1003-SKY AND FUEL LEAK CHECK GOOD . SEE CONTINUATION CARD FOR DETAILS

Part: FLOOR PANEL — CRACKED (E/E BAY) · airframe 42,104 hrs · 38,224 cycles

LH FWD EQUIPMENT COMP THE FLOOR PANEL IS CRACKED AT FR193 (C-CHECK RO 11/16/2023) PERFORMED DOUBLER REPAIR AT LH FWD EQUIPMENT COMP. FLOOR PANEL FR 193 . PERFORMED NDT INSPECTION ON CUTOUT BY BARON NDT LLC FAA CRS#5NDR545D REPORT #S101923-1 WITH NO DEFECTS NOTED IAW REO 601R-53-11-3897.

Part: FLOOR PANEL — CRACKED (BS 193) · airframe 42,104 hrs · 38,224 cycles

LH FWD EQUIPMENT COMP THE FLOOR PANEL IS CRACKED AT FR193 (C-CHECK RO 11/16/2023) PERFORMED DOUBLER REPAIR AT LH FWD EQUIPMENT COMP. FLOOR PANEL FR 193 . PERFORMED NDT INSPECTION ON CUTOUT BY BARON NDT LLC FAA CRS#5NDR545D REPORT #S101923-1 WITH NO DEFECTS NOTED IAW REO 601R-53-11-3897.

Part: CASE — GOUGED (RT ENGINE FAN) · airframe 42,104 hrs · 38,224 cycles

EVAL GOUGED RT ENG FAN CASE AT 12 OCLOCK POSITION JUST FWD OF FAN CASE BOLTS (C-CHECK RO 11/16/2023) PERFORMED REPAIR OF GOUGED RT ENG. FAN CASE AT 12 OCLOCK POSITION IAW CRJ-200 REO 601R-71-61-4364. REV. -- DATE: 2023-10-12. PERFORMED NDT ET/UT INSPECTION BY BARON NDT, LLC. FAA, CRS#5NDR545D, REPORT #S101723-1. TOOLS USED: FLAPPER PEENING KIT ID: FSA0045-A. DUE DATE: 14-FEB-24, FLAPPER PENNING KIT ID: FSA0045-B. DUE DATE: 14-FEB-24. AJ180 ID: AV-6059. DUE DATE: JAN-24.

Part: FRAME — CORRODED (BS 349 S25-26R) · airframe 42,104 hrs · 38,224 cycles

AVIONICS BAY FR 349 AFT FACE BETWEEN STGR 26L AND 25R SIGNS OF CORROSION (C-CHECK RO 11/16/2023) BLENDED OUT CORROSION AT AVIONICS BAY FR349 AFT FACE BETWEEN STGR26L AND STGR25R. NDT PERFORMED BY BARON NDT LLC FAA CRS #5NDR545D REPORT #$101223-2. ORIGINAL THICKNESS 0.063", MATERIAL LOSS 0.002", REAMAINING MATERIAL IS 0.061". FOUND TO BE WITHIN LIMITS IAW CRJ 200 SRM 53-00-00

Part: INTERCOSTAL — CORRODED (BS 394-409) · airframe 42,104 hrs · 38,224 cycles

AVIONICS BAY L/H INBOARD INTERCOSTAL BETWEEN FR 394 AND 409 SIGNS OF CORROSION (C-CHECK RO 11/16/2023) BLENDED OUT AREA ON AVIONICS BAY L/H O/B INTERCOSTAL. NDT PERFORMED BY BARON NDT LLC FAA CRS #5NDR545D REPORT #S092723-1. ORIGINAL THICKNESS 0.080" MATERIAL LOSS 0.006", REMAINING MATERIAL 0.074" FOUND TO BE WITHIN LIMITS IAW CRJ 200 SRM 53-00-00

Part: INTERCOSTAL — CORRODED (BS 409 S25R) · airframe 42,104 hrs · 38,224 cycles

AVIONICS BAY AT STGR 25R INTERCOASTAL BETWEEN FR 409 AND 409 + 16, SIGNS OF CORROSION (C-CHECK RO 11/16/2023) REMOVED CORROSION AT AVIONICS BAY ON STR 25R INTERCOSTAL BETWEEN FR 409 AND FR409+16,PERFORMED NDT INSPECTION BY BARON NDT,LLC FAA CRS# 5NDR545D REPORT #S092523-2 EVALUATED BLENDED AREA,ORIGINAL THICKNESS .063" MATERIAL LOSS .003" REMAINING THICKNESS .060" FOUND TO BE WITH IN LIMITS IAW CRJ 200 SRM 53-00-00

Part: FRAME — CORRODED (BS 349) · airframe 42,104 hrs · 38,224 cycles

AVIONICS BAY FR 349 FWD FACE BETWEEN STGR 25R AND 24R SIGNS OF CORROSION (C-CHECK RO 11/16/2023) BLENDED AREA AT AVIONICS BAY ON FR 349 FWD FACE BETWEEN STGR 25R AND STGR 24R, PERFORMED NDT ET/UT INSPECTION BY BARON NDT,LLC FAA CRS# 5NDR545D REPORT# S092823-4. ORIGINAL THICKNESS :0.063", LOSS MATERIAL: 0.001", REMAINING MATERIAL: 0.062" FOUND TO BE IN LIMITS IAW CRJ 200 SRM 53-00-00.

Part: CASE — GOUGED (RT ENGINE FAN) · airframe 42,104 hrs · 38,224 cycles

EVAL GOUGED RT ENG FAN CASE AT 12 OCLOCK POSITION JUST FWD OF FAN CASE BOLTS (C-CHECK RO 11/16/2023) PERFORMED REPAIR OF GOUGED RT ENG. FAN CASE AT 12 OCLOCK POSITION IAW CRJ-200 REO 601R-71-61-4364. REV. -- DATE: 2023-10-12. PERFORMED NDT ET/UT INSPECTION BY BARON NDT, LLC. FAA, CRS#5NDR545D, REPORT #S101723-1. TOOLS USED: FLAPPER PEENING KIT ID: FSA0045-A. DUE DATE: 14-FEB-24, FLAPPER PENNING KIT ID: FSA0045-B. DUE DATE: 14-FEB-24. AJ180 ID: AV-6059. DUE DATE: JAN-24.

Part: INTERCOSTAL — CORRODED (BS 409) · airframe 42,104 hrs · 38,224 cycles

AVIONICS BAY AT STGR 25R INTERCOASTAL BETWEEN FR 409 AND 409 + 16, SIGNS OF CORROSION (C-CHECK RO 11/16/2023) REMOVED CORROSION AT AVIONICS BAY ON STR 25R INTERCOSTAL BETWEEN FR 409 AND FR409+16,PERFORMED NDT INSPECTION BY BARON NDT,LLC FAA CRS# 5NDR545D REPORT #S092523-2 EVALUATED BLENDED AREA,ORIGINAL THICKNESS .063" MATERIAL LOSS .003" REMAINING THICKNESS .060" FOUND TO BE WITH IN LIMITS IAW CRJ 200 SRM 53-00-00

Part: SUPPORT BRACKET — CORRODED (BS 409 S25-26R) · airframe 42,104 hrs · 38,224 cycles

AVIONICS BAY FR 409 AFT SUPPORT BRACKETS BETWEEN STGR 26R AND 25R SIGNS OF CORROSION (C-CHECK RO 11/16/2023) BLENDED OUT CORROSION IN AVIONICS BAY FR 409 AFT SUPPORT BRACKET BTW STGR 26R AND 25R I.A.W. CRJ200 SRM 53-00-00. NDT PERFORMED BY BARON NDT LLC, FAA CRS# 5NDR545D, PERFORMED ET/UT DETAILED INSPECTION, NO DEFECTS NOTED AT TIME OF INSPECTION, SEE REPORT # S100523-3 P.O. NUMBER 169463 DATE 04OCT2023.

Part: INTERCOSTAL — CORRODED (BS 394-409) · airframe 42,104 hrs · 38,224 cycles

AVIONICS BAY R/H O/B INTERCOSTAL BETWEEN FR 394 AND FR 409 SIGNS OF CORROSION (C-CHECK RO 11/16/2023) REMOVED CORROSION AND PERFORMED NDT ET/UT INSPECTION NDT LLC FAA CRS#5NDR545D REPORT #S092723-2 EVALUATED BLENDED AREA AT AVIONICS BAY ON RH O/B INTERCOSTAL BETWEEN FR 394 AND FR 409, ORIGINAL THICKNESS: 0.050", MATERIAL LOSS: 0.001" REMAINING MATERIAL: 0.049" FOUND TO BE WITH IN LIMITS IAW CRJ 200 SRM 53-00-00

Part: FRAME — CORRODED (BS 409) · airframe 42,104 hrs · 38,224 cycles

AVIONICS BAY FR 409 AFT SUPPORT BRACKETS BETWEEN STGR 26R AND 25R SIGNS OF CORROSION (C-CHECK RO 11/16/2023) BLENDED OUT CORROSION IN AVIONICS BAY FR 409 AFT SUPPORT BRACKET BTW STGR 26R AND 25R I.A.W. CRJ200 SRM 53-00-00. NDT PERFORMED BY BARON NDT LLC, FAA CRS# 5NDR545D, PERFORMED ET/UT DETAILED INSPECTION, NO DEFECTS NOTED AT TIME OF INSPECTION, SEE REPORT # S100523-3 P.O. NUMBER 169463 DATE 04OCT2023.

Part: FRAME — CORRODED (BS 349) · airframe 42,104 hrs · 38,224 cycles

AVIONICS BAY FR 349 AFT FACE BETWEEN STGR 26L AND 25R SIGNS OF CORROSION (C-CHECK RO 11/16/2023) BLENDED OUT CORROSION AT AVIONICS BAY FR349 AFT FACE BETWEEN STGR26L AND STGR25R. NDT PERFORMED BY BARON NDT LLC FAA CRS #5NDR545D REPORT #$101223-2. ORIGINAL THICKNESS 0.063", MATERIAL LOSS 0.002", REAMAINING MATERIAL IS 0.061". FOUND TO BE WITHIN LIMITS IAW CRJ 200 SRM 53-00-00

Part: INTERCOSTAL — CORRODED (BS 394-409) · airframe 42,104 hrs · 38,224 cycles

AVIONICS BAY R/H O/B INTER-COASTAL BETWEEN FR 394 AND FR 409 SIGNS OF CORROSION (C-CHECK RO 11/16/2023) REMOVED CORROSION AND PERFORMED NDT ET/UT INSPECTION BY BARON NDT LLC FAA CRS#5NDR545D REPORT #S092723-2 EVALUATED BLENDED AREA AT AVIONICS BAY ON RH O/B INTERCOSTAL BETWEEN FR 394 AND FR 409, ORIGINAL THICKNESS: 0.050", MATERIAL LOSS: 0.001" REMAINING MATERIAL: 0.049" FOUND TO BE WITH IN LIMITS IAW CRJ 200 SRM 53-00-00

Part: SHEAR TIE — CORRODED (BS 409 S26L/R) · airframe 42,104 hrs · 38,224 cycles

AVIONICS BAY, AFT FACE FR 409, FOOT SPLICE HAS SIGNS OF CORROSION BETWEEN STGR 26L AND 26R (C-CHECK RO 11/16/2023) BLENDED OUT CORROSION AT AFT FACE FR409 FOOT SPLICE BETWEEN STGR26R AND 26L. NDT PERFORMED BY NDT UT/ET BY BARON NDT FAA CRS #5NDR545D, REPORT # $100223-24.ORIGINAL THICKNESS 0.063", MATERIAL LOSS 0.004", REMAINING MATERIAL 0.059" FOUND TO BE WITHIN LIMITS IAW CRJ 200 SRM 53-00-00

Part: FRAME — CORRODED (BS 364) · airframe 42,104 hrs · 38,224 cycles

AVIONICS BAY FR 364 FWD FACE HAS SIGNS OF CORROSION BETWEEN STGR 27 AND 25R (C-CHECK RO 11/16/2023) REMOVED CORROSION AT AVIONICS BAY FR364 FWD FACE BETWEEN STGR 27R AND 25R. NDT PERFORMED BY BARON NDT LLC FAA CRS #5NDR545D REPORT # $092723-4. ORIGINAL THICKNESS 0.080",MATERIAL LOSS 0.002", REMAINING MATERIAL 0.078", FOUND TO BE WITHIN LIMITS IAW CRJ 200 SRM 53-00-00

Part: FRAME — CORRODED (BS 349 S24-25R) · airframe 42,104 hrs · 38,224 cycles

AVIONICS BAY FR 349 FWD FACE BETWEEN STGR 25R AND 24R SIGNS OF CORROSION (C-CHECK RO 11/16/2023) BLENDED AREA AT AVIONICS BAY ON FR 349 FWD FACE BETWEEN STGR 25R AND STGR 24R, PERFORMED NDT ET/UT INSPECTION BY BARON NDT,LLC FAA CRS# 5NDR545D REPORT# S092823-4. ORIGINAL THICKNESS :0.063", LOSS MATERIAL: 0.001", REMAINING MATERIAL: 0.062" FOUND TO BE IN LIMITS IAW CRJ 200 SRM 53-00-00.

Part: INTERCOSTAL — CORRODED (BS 394-409) · airframe 42,104 hrs · 38,224 cycles

AVIONICS BAY L/H INBOARD INTER-COASTAL BETWEEN FR 394 AND 409 SIGNS OF CORROSION (C-CHECK RO 11/16/2023) BLENDED OUT AREA ON AVIONICS BAY L/H O/B INTERCOSTAL. NDT PERFORMED BY BARON NDT LLC FAA CRS #5NDR545D REPORT #S092723-1. ORIGINAL THICKNESS 0.080" MATERIAL LOSS 0.006", REMAINING MATERIAL 0.074" FOUND TO BE WITHIN LIMITS IAW CRJ 200 SRM 53-00-00

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 42,104 hrs · 38,224 cycles

AVIONICS BAY L/H INBOARD INTER-COASTAL BETWEEN FR 364 AND FR 349 SIGNS OF CORROSION (C-CHECK RO 11/16/2023) REMOVED CORROSION ON AVIONICS BAY L/H INBOARD INTERCOSTAL BETWEEN FR 364 AND FR349, PERFORMED NDT UT/ET INSPECTION BY BARON NDT FAA CRS#5NDR545D, REPORT # S092723-3 AND EVALUATED BLENDED AREA AS FOLLOW: ORIGINAL THICKNESS 0.080". REMOVED MATERIAL 0.003". RAMAINING THICKNESS 0.077". THEREFORE IT IS WITHIN OF LIMITS IAW CRJ-200 SRM 53-00-00.

Part: STRUCTURE — CORRODED (BS 364 S25-27R) · airframe 42,104 hrs · 38,224 cycles

AVIONICS BAY FR 364 FWD FACE HAS SIGNS OF CORROSION BETWEEN STGR 27 AND 25R (C-CHECK RO 11/16/2023) REMOVED CORROSION AT AVIONICS BAY FR364 FWD FACE BETWEEN STGR 27R AND 25R. NDT PERFORMED BY BARON NDT LLC FAA CRS #5NDR545D REPORT # $092723-4. ORIGINAL THICKNESS 0.080",MATERIAL LOSS 0.002", REMAINING MATERIAL 0.078", FOUND TO BE WITHIN LIMITS IAW CRJ 200 SRM 53-00-00

Part: HINGE FITTING — CORRODED (LT WIND FLAP) · airframe 42,104 hrs · 38,224 cycles

SIGNS OF CORROSION ON LH IB FLAP HINGE FWD ATTACHMENT HOLE AT WS80.50 (C-CHECK RO 11/16/2023) REMOVED CORROSION FROM LH INBD FWD WS 80.50.NDT PERFORMED BY BARON NDT ,LLC FAA CRS # 4NDR545D, PERFORMED ET/UT REPORT #S100423-14.PERFORMED LPI REPORT #S101923-3. ORIGINAL THICKESS 0.250", MATERIAL LOSS 0.006", REMAINING MATERIAL 0.244".FOUND TO BE IN LIMITS IAW CRJ 200 REO 601R-57-21-3797

Part: HINGE — CORRODED (LT TE FLAP) · airframe 42,104 hrs · 38,224 cycles

SIGNS OF CORROSION ON LH IB FLAP HINGE FWD ATTACHMENT HOLE AT WS80.50 (C-CHECK RO 11/16/2023) REMOVED CORROSION FROM LH INBD FWD WS 80.50.NDT PERFORMED BY BARON NDT ,LLC FAA CRS # 4NDR545D, PERFORMED ET/UT REPORT #S100423-14.PERFORMED LPI REPORT #S101923-3. ORIGINAL THICKESS 0.250", MATERIAL LOSS 0.006", REMAINING MATERIAL 0.244".FOUND TO BE IN LIMITS IAW CRJ 200 REO 601R-57-21-3797

Part: BRACKET — CRACKED (DOOR TRACK) · airframe 38,875 hrs · 34,465 cycles

LOWER CHANNEL ON FWD SIDE OF CARGO DOOR TRACK IS CRACKED. C-CHECK RO 9/1/2020. REMOVED AND REPLACED LOWER CHANNEL BRACKET ON FWD SIDE OF THE CARGO DOOR TRACK WITH NEW PART REFERENCE CRJ200 SRM & BOMBARDIER DWG. SEE CONTINUATION CARD FOR DETAILS.

Part: DOUBLER — CORRODED · airframe 38,875 hrs · 34,465 cycles

DOUBLER PN.601R10203-32 ATTACHED TO THE OUTBOARD OF RT BATTERY RIB AT APROXIMATELY WS53.6 IS CORRODED. C-CHECK RO 9/1/2020. BLENDED CORROSION FROM DOUBLER PN.601R10203-32 ATTACHED TO THE OUTBOARD OF RT BATTERY RIB AT APROXIMATELY WS53.6 REF CRJ 200 SRM. EVALUATED AND FOUND TO BE OUT OF LIMITS, REF CRJ-200-SRM. RECEIVED FROM ENGINEERING REO ALL STEPS COMPLIED WITH.

Part: STIFFENER — CRACKED (BS 621 BULKHEAD) · airframe 38,875 hrs · 34,465 cycles

FS 621 AFT BULKHEAD LT LOWER STIFFENER OUTBOARD FOR LBL36 AT STGR 16 IS CRACKED. REMOVED AND INSTALLED NEW STIFFENER (601R36008-51) ON FS621 AFT BULKHEAD AT LBL36, STGR16, REF CRJ 200 SRM, & DWG.

Part: FORMER — CORRODED (PAX DOOR) · airframe 38,875 hrs · 34,465 cycles

PASSENGER DOOR AFT FORMER SUPPORT ANGLE UNDER SEAL RETAINER @ FS.347 IS CORRODED. C-CHECK RO 9/1/2020. REMOVED AND INSTALLED NEW PASSENGER DOOR AFT FORMER SUPPORT ANGLE AT FS.347 REF CRJ 200 SRM AND DWG.

Part: BULKHEAD WEB — CHAFED (BS 621) · airframe 38,875 hrs · 34,465 cycles

FS 621 BULKHEAD HAS 3 CHAFE MARKS 3"? ABOVE FLOOR AT APPROXIMATELY LBL 23, RBL 31, AND RBL 41. C-CHECK RO 9/1/2020. REMOVED DAMAGE AT PRESSURE BULKHEAD F/S 621 APPROX 3" ABOVE FLOOR AT LBL 23, AT RBL 31, AND RBL 41 IAW CRJ 200 SRM. BLENDED AREAS AT RBL41 AND LBL 23 FOUND TO BE OUT OF LIMITS, AND RBL31 WAS FOUND TO BE WITHIN LIMITS, REF REO. REPAIRED FS 621 BULKHEAD, REF REO.

Part: SKIN — DENTED (FWD FUSELAGE) · airframe 38,875 hrs · 34,465 cycles

EVALUATE DENT JUST AFT OF PITOT- STATIC BELOW CO-PILOT SIDE WINDOW. REPAIRED FUSELAGE SKIN JUST AFT OF PITOT STATIC BELOW CO-PILOT SIDE WINDOW, REF REO. PRESSURE CHECK GOOD.

Part: ANGLE — CORRODED (BS 338) · airframe 38,875 hrs · 34,465 cycles

CLIP AT FS.338 NEAR PASSENGER DOOR HINGE IS CORRODED. REMOVED CLIP AT FS.338 AND FOUND TO BE OUT OF LIMITS. INSTALLED NEW CLIP AT FS.338 NEAR THE PASSENGER DOOR HINGE, REF MHIRJ DWG. AND CRJ 200 SRM. COMPLIED WITH TASK CARD.

Part: FRAME — CORRODED (BS 313) · airframe 38,875 hrs · 34,465 cycles

FRAME AF FS.313 BETWEEN DD4-DD5 IS CORRODED. REMOVED AND INSTALLED NEW FRAME AT FS313 BETWEEN DD4 AND DD5. REF DWG AND CRJ 200 SRM. DETAILS.

Part: FORMER — CORRODED (PAX DOOR) · airframe 38,875 hrs · 34,465 cycles

PASSENGER DOOR AFT FORMER @ FS.347 IS CORRODED. REMOVED AND INSTALLED NEW PASSENGER DOOR AFT FORMER AT FS.347, REF CRJ 200 SRM AND DWG.

Part: INTERCOSTAL — CORRODED (BS 320-328) · airframe 38,875 hrs · 34,465 cycles

INTERCOSTAL AT DD7 BETWEEN FS.320-328 IS CORRODED. REMOVED AND INSTALLED A NEW PASSENGER DOOR INTERCOSTAL AT DD7 BETWEEN FS320-FS328. REF DWG AND SRM. DETAILS.

Part: INTERCOSTAL — CORRODED (BS 323-335) · airframe 38,875 hrs · 34,465 cycles

INTERCOSTAL AT DD1 BETWEEN FS.323-335 IS CORRODED. REMOVED AND INSTALLED A NEW INTERCOSTAL AT DD1 BETWEEN FS323-FS335. REF DWG, CRJ 200 SRM.

Part: INTERCOSTAL — CORRODED (BS 320-338) · airframe 38,875 hrs · 34,465 cycles

INTERCOSTAL AT DD3 BETWEEN FS.320-338 IS CORRODED. REMOVED AND INSTALLED NEW INTERCOSTAL AT DD3 BETWEEN FS.320-338 REF CRJ 200 SRM AND DWG.

Part: INTERCOSTAL — CORRODED (DOOR) · airframe 38,875 hrs · 34,465 cycles

INTERCOSTAL AT DD5 BETWEEN FS.311-320 IS CORRODED. REMOVED AND INSTALLED A NEW INTERCOSTAL AT DD5 BETWEEN FS311-FS320. REF DWG AND SRM.

Part: ANGLE — CORRODED (RT WING) · airframe 38,875 hrs · 34,465 cycles

RIGHT BATTERY RIB AT WS53.60 HAS CORROSION ON FORWARD CHANNEL, ANGLES AND DOUBLE. REPLACED AND INSTALLED REPLACEMENT ANGLE P/N 601R10203-25 PO: T54192 AT RT BATTERY RIB AT WS53.60. REF. CRJ 200 SRM AND DWG COMPLIED WITH SKYWEST TASK CARD.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 38,875 hrs · 34,465 cycles

THE PASSENGER DOOR INTERCOSTAL BETWEEN FS329.50 AND FS338.00 AT DD6 HAS CORROSION. REMOVED AND INSTALLED A NEW INTERCOSTAL AND CLEAT AT DD6 FROM FS320-FS338. REF DWG, AND SRM.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 38,875 hrs · 34,465 cycles

THE PASSENGER DOOR INTERCOSTAL BETWEEN FS320.10 AND FS329.50 AT DD4 HAS CORROSION. (MARKED). C-CHECK RO 9/1/2020. REMOVED AND INSTALLED INTERCOSTAL AT DD4 BETWEEN FS.320.10-329.5 REF CRJ 200 SRM AND DWG.

Part: DOOR FRAME — CORRODED (PAX DOORWAY) · airframe 38,875 hrs · 34,465 cycles

THE PASSENGER DOOR FORMER AT FS311.75 AT DD5 HAS CORROSION. REMOVED AND INSTALLED NEW PASSENGER DOOR FWD FORMER AT FS311.75 IAW SRM AND DWG.

Part: ANGLE — CORRODED (LT WING) · airframe 38,875 hrs · 34,465 cycles

LEFT BATTERY RIB AT WS53.60 HAS CORROSION ON THE INBOARD SIDE OF THE UPPER ANGLE AT RADIUS (MARKED). C-CHECK RO 9/1/2020. REMOVED CORROSION ON LT BATTERY RIB AT WS53.60, REF. CRJ200 SRM. REMOVED UPPER REINFORCEMENT ANGLE AND HI LITES TO FOM, REF. CRJ200 SRM. & INSTALLED UPPER REINFORCEMENT ANGLE REF MHIRJ REO.

Part: ACCESS PANEL — GOUGED (LT WING) · airframe 38,875 hrs · 34,465 cycles

LT WING AUX SPAR ACCESS PANEL 540AT RECESSED AREA FOR CLOSEOUT PANEL HAS SCRAPES AND GOUGES INTO BASE METAL AS MARKED. C-CHECK RO 9/1/2020. BLENDED DAMAGE TO A SMOOTH FINISH ON LT WING AUX SPAR AT ACCESS PANEL 540AT, NDT INSPECTED NO DEFECTS NOTED, ROTO PEENED REWORKED AREAS, RESTORED FINISH TO REWORKED AREAS, REF MHIRJ, BOMBARDIER ENG. DWG, COMPLIED WITH SKY CARD.

Part: DOOR SILL — CORRODED (EMERGENCY EXIT) · airframe 38,875 hrs · 34,465 cycles

RT EMERGENCY DOOR CUTOUT LOWER SILL CLEVIS PINS CORRODED. C-CHECK RO 9/1/2020. REMOVED AND REPLACED RT EMERGENCY DOOR CUTOUT LOWER SILL CLEVIS PIN REF CRJ 200 AMM.

Part: PIN — CORRODED (EMERGENCY EXIT) · airframe 38,875 hrs · 34,465 cycles

LT EMERGENCY DOOR CUTOUT LOWER SILL CLEVIS PINS CORRODED. C-CHECK RO 9/1/2020. REMOVED AND REPLACED LT EMERGENCY DOOR CUTOUT LOWER SILL CLEVIS PIN, REF CRJ 200 AMM.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 38,875 hrs · 34,465 cycles

THE PASSENGER DOOR INTERCOSTAL BETWEEN FS338.00 AND FS347.50 AT DD6 HAS CORROSION (MARKED). C-CHECK RO 9/1/2020. REMOVED AND INSTALLED NEW PASSENGER DOOR INTERCOSTAL, NEW CLEAT, AND NEW BRACKET AT DD6 BETWEEN FS338-FS347.25. REF DWG AND CRJ 200 SRM. SEE CONTINUATION CARD FOR DETAILS.

Part: ANGLE — CRACKED (BS 621-625) · airframe 38,875 hrs · 34,465 cycles

CLIP AT APPROXIMATELY STR 13R, BETWEEN FS621 AND FS625, IS CRACKED. REMOVED AND INSTALLED CLIP IAW DWG AND SRM.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 38,875 hrs · 34,465 cycles

THE PASSENGER DOOR INTERCOSTAL BETWEEN FS338.00 AND FS347.25 AT DD5 HAS CORROSION (MARKED). C-CHECK RO 9/1/2020. REMOVED AND INSTALLED NEW INTERCOSTAL AT DD5 BETWEEN FS338.00-FS347.25. REF DWG AND CRJ 200 SRM. SEE CONTINUATION CARDS FOR DETAILS.

Part: ANGLE — CRACKED (BS 621-625) · airframe 38,875 hrs · 34,465 cycles

CLIP AT APPROX STR 13L, BEWEEN FS621 AND FS625, IS CRACKED. C-CHECK RO 9/1/2020. REMOVED AND REPLACED CLIP AT APPROXIMATELY STGR 13L, BETWEEN FS621 & FS625, REF CRJ 200 SRM. & DWG.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 38,875 hrs · 34,465 cycles

THE SEAT TRACK AT LBL27.00 FROM FS559.00+96 TO FS559.00+112 HAS MULTIPLE LOCATIONS OF CORROSION. REMOVED CORROSION ON SEAT TRACK AT LBL27.00 FROM FS559.00+96 TO FS559.00+112 REF. CRJ 200 SRM. ORIGINAL MATERIAL THICKNESS OF LOCATION T=0.110 REF. STANDARD MANUAL, REMAINING THICKNESS AFTER BLENDED OUT IS 0.082? MATERIAL LOSS IS 0.028 MAXIMUM ALLOWABLE LOSS IS 0.020? FOUND TO BE OUT OF LIMITS, REF. CRJ 200 SRM. REMOVED & REPLACED SEAT TRACK AT LBL27.00 FROM FS 559.00+96 TO FS 559.00+112 REF. CRJ 200 AMM.

Part: STOP FITTING — CHAFED (PAX DOOR) · airframe 38,875 hrs · 34,465 cycles

THE PASSENGER DOOR SUPPORT WHEEL STOP FITTING ON DOOR SIDE IS CHAFFE. REMOVED AND REPLACED PASSENGER DOOR SUPPORT WHEEL STOP FITTING P/N 601R317093-5, REF CRJ 200 SRM.

Part: BEAM — CORRODED (BS 589-621) · airframe 38,875 hrs · 34,465 cycles

THE BEAM CAP AT LBL9.00 BETWEEN APPROX FS589.00 AND FS621.00 HAS MULTIPLE LOCATIONS OF CORROSION (MARKED). C-CHECK RO 9/1/2020. THE BEAM CAP AT LBL9.00 BETWEEN APPROX FS589.00 AND FS621.00 REPLACED REF REO AND DRAWING. SEE CONTINUATION CARD FOR DETAILS.

Part: FLOORBEAM — CORRODED (BS 621) · airframe 38,875 hrs · 34,465 cycles

THE FLOOR BEAM ATTACHMENT AT FS621.00 AT LBL27.00 HAS CORROSION AND CHAFFED (MARKED). C-CHECK RO 9/1/2020. REMOVED CHAFE AND NOTED CORROSION FROM FLOOR BEAM ATTACHMENT AT FS621.00 AND LBL27.00 REF CRJ-200 SRM. EVALUATED AND FOUND TO BE OUT OF LIMITS. SUBMITTED TO ENGINEERING. RECEIVED AND COMPLIED WITH MHIRJ REO, ENG. DW, FOUND TO BE STRUCTURALLY ACCEPTABLE FOR DETAILS SEE ATTACHED CONTINUATION CARD

Part: FLOORBEAM — CHAFED (BS 621) · airframe 38,875 hrs · 34,465 cycles

THE FLOOR BEAM ATTACHMENT AT FS621.00 AT LBL9.00 IS CHAFFED (MARKED). C-CHECK RO 9/1/2020. REMOVED CHAFE FROM FLOOR BEAM ATTACHMENT AT FS621.00 AND LBL9.00 REF CRJ-200 SRM 51-12-00. EVALUATED AND FOUND TO BE OUT OF LIMITS. SUBMITTED TO ENGINEERING. RECEIVED AND COMPLIED WITH MHIRJ REO, ENG.DWG, FOUND TO BE STRUCTURALLY ACCEPTABLE FOR DETAILS SEE ATTACHED CONTINUATION CARD.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 38,875 hrs · 34,465 cycles

THE RT FLOOR SILL FROM APPROXIMATELY FS559.00+16 TO FS559.00+48 HAS MULTIPLE LOCATIONS OF CORROSION. REMOVED CORROSION FROM RT FLOOR SILL AT APPROXIMATELY FS559.00+16 - FS559.00+48 IAW SRM. EVALUATED AND FOUND TO BE OUT OF LIMITS, IAW REO. RECEIVED AND COMPLETED ALL STEPS OF REO. RT FLOOR SILL AT APPROXIMATELY FS559.00+16 - FS559.00+48 IS CONSIDERED STRUCTURALLY ACCEPTABLE.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 38,875 hrs · 34,465 cycles

THE SEAT TRACK AT LBL27.00 FROM FS559.00+80 TO FS559.00+96 HAS CORROSION. REMOVED CORROSION ON SEAT TRACK AT LBL27.00 FROM FS559.00+80 TO FS559.00+96 REF. CRJ 200 SRM. ORIGINAL MATERIAL THICKNESS OF LOCATION T=0.110 REF. STANDARD MANUAL REMAINING THICKNESS AFTER BLENDED OUT IS 0.080? MATERIAL LOSS IS 0.030 MAXIMUM ALLOWABLE LOSS IS 0.020? FOUND TO OUT OF LIMITS REF. CRJ 200 SRM. . REMOVED & REPLACED SEAT TRACK AT LBL27.00 FROM FS559.00+80 TO FS559.00+96. REF. CRJ 200 AMM & CRJ 200 AMM.

Part: SKIN — CORRODED (SERVICE DOOR) · airframe 38,875 hrs · 34,465 cycles

SERVICE DOOR HAS CORROSION ON ITS AFT FACE (MARKED). C-CHECK RO 9/1/2020. REMOVED CORROSION FROM THE SERVICE DOOR AFT PAN, REF. CRJ200 SRM AND FOUND TO BE OUT OF LIMITS. RECEIVED AND COMPLIED WITH MHIRJ REO. PERFORMED PRESSURE CHECK REF CRJ 200 AMM, CHECK GOOD. COMPLIED WITH TASK CARD. SEE CONTINUATION FOR FURTHER DETAILS.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 38,875 hrs · 34,465 cycles

THE SEAT TRACK AT LBL9.00 FROM APPROXIMATELY FS559.00+96 TO FS559.00+112 HAS MULTIPLE LOCATIONS OF CORROSION. REMOVED CORROSION ON SEAT TRACK AT LBL 9.00 FROM FS559.00+96 TO FS559.00+112, REF. CRJ 200 SRM. ORIGINAL MATERIAL THICKNESS OF LOCATION T=0.110,? REF STANDARD MANUAL, REMAINING THICKNESS AFTER BLENDED OUT IS 0.080? MATERIAL LOSS IS 0.030? MAXIMUM ALLOWABLE LOSS IS 0.020? FOUND TO BE OUT OF LIMITS, REF. CRJ 200 SRM. REMOVED & REPLACED SEAT TRACK AT LBL9 FROM FS 559.00+96 TO FS 559.00+112, REF CRJ 200 AMM.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 38,875 hrs · 34,465 cycles

THE SEAT TRACK AT RBL27.00 FROM APPROXIMATELY FS559.00+80 TO FS559.00+96 HAS MULTIPLE LOCATIONS OF CORROSION. SEAT TRACK SECTION LOCATED AT RBL-27 BETWEEN FS559.00+80 TO FS559.00+96 IS OUT OF LIMITS DUE TO SEVERE PITTING AND INTERGRANULAR CORROSION FOUND ON OVER 40% OF SEAT TRACK FASTENER HOLES REPLACE TRACK. REPLACED THE SEAT TRACK.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 38,875 hrs · 34,465 cycles

THE SEAT TRACK AT RBL27.00 FROM APPROXIMATELY FS559.00+96 TO FS559.00+112 HAS MULTIPLE LOCATIONS OF CORROSION. SEAT TRACK SECTION LOCATED AT RBL-27 BETWEEN FS559.00+96 TO FS559.00+112 IS OUT OF LIMITS DUE TO SEVERE PITTING AND INTERGRANULAR CORROSION FOUND ON OVER 40% OF SEAT TRACK FASTENER HOLES REPLACE PART. REPLACED SEAT TRACK PN 601R38669-9, RBL 27.00, FS 559.00+96 TO FS 559.00+112 REF CRJ 200 AMM.

Part: SEAT TRACK — CORRODED (BS 559-621) · airframe 38,875 hrs · 34,465 cycles

THE SEAT TRACK AT RBL27.00 FROM APPROXIMATELY FS559.00+112 TO FS621.00 HAS MULTIPLE LOCATIONS OF CORROSION. SEAT TRACK SECTION LOCATED AT RBL-27 BETWEEN FS559.00+112 TO FS621.00 IS OUT OF LIMITS DUE TO SEVERE PITING AND INTERGRANULAR CORROSION FOUND ON OVER 40% OF SEAT TRACK FASTENER HOLES REPLACE PART. REPLACED SEAT TRACK PN 601R386631-3, RBL 27.00, FS 559.00+112 TO FS 621.00 REF CRJ 200 AMM.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 38,875 hrs · 34,465 cycles

THE SEAT TRACK AT LBL9.00 JUST AFT AT APPROXIMATELY FS559.00 TO FS559.00+80 HAS MULTIPLE LOCATIONS OF CORROSION. REMOVED CORROSION ON SEAT TRACK AT LBL 9.00 FROM FS559.00 TO FS559.00+80, REF. CRJ 200 SRM. ORIGINAL MATERIAL THICKNESS OF LOCATION T=0.110,? REF STANDARD MANUAL, REMAINING THICKNESS AFTER BLENDED OUT IS 0.080? MATERIAL LOSS IS 0.030? MAXIMUM ALLOWABLE LOSS IS 0.020? FOUND TO BE OUT OF LIMITS, REF. CRJ 200 SRM. REMOVED & REPLACED SEAT TRACK AT LBL9 FROM FS 559.00 TO FS 559.00+80, REF. CRJ 200 AMM.

Part: SKIN — CORRODED (BS 559) · airframe 38,875 hrs · 34,465 cycles

EXTERIOR FS'S 559+80/559+112 - STGR'S 26L/26R - MULTITUDE OF RIVETS/SKIN SHOWING CORROSION. REMOVED CORROSION AT FS.559+80-FS.559+112 BETWEEN STRG 26L/26R, REF CRJ 200 SRM AND FOUND TO BE OUT OF LIMITS, REF CRJ 200 SRM. RECEIVED AND COMPLIED WITH ALL STEPS OF REO.

Part: WEB — CORRODED (PAX DOOR) · airframe 38,875 hrs · 34,465 cycles

THE PASSENGER DOOR AFT WEB HAS MULTIPLE LOCATIONS OF CORROSION (MARKED). C-CHECK RO 9/1/2020. REMOVED AND REPLACED THE PASSENGER DOOR AFT WEB WITH NEW WEB REF CRJ 200 SRM.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 38,875 hrs · 34,465 cycles

THE SEAT TRACK AT RBL9.00 FROM APPROXIMATELY FS559.00+96 TO FS559.00+112 HAS MULTIPLE LOCATIONS OF CORROSION. SEAT TRACK LOCATED AT RBL-9 BETWEEN FS559.00+96 - FS559.00+112 IS OUT OF LIMITS DUE TO SEVERE PITING AND INTERGRANULAR CORROSION FOUND ON 50% OF SEAT TRACK, REPLACED PART. REPLACED SEAT TRACK PN 601R386631-9, RBL 9.00, FS 559.00+96 - FS 559.00+112 REF CRJ 200 AMM.

Part: FRAME — CORRODED (BS 574) · airframe 38,875 hrs · 34,465 cycles

FRAME AT FS 574.0 IN THE AREA OF RBL 26 TO LBL 26 HAS CORROSION. C-CHECK RO 9/1/2020. REMOVED CORROSION AT FRAME FS574.00 IN THE AREA OF STGR 26L TO STGR 26R REF CRJ-200 SRM. BLENDED AREA FOUND TO BE OUT OF LIMITS CRJ200 SRM. REPAIRED FRAME AT FS 574.0 REF REO. SEE CONTINUATION CARD FOR DETAILS.

Part: FLOORBEAM — CHAFED (BS 621) · airframe 38,875 hrs · 34,465 cycles

THE FLOOR BEAM ATTACHMENT AT FS621.00 AT RBL9.00 IS CHAFFED (MARKED). C-CHECK RO 9/1/2020. REMOVED CHAFE FROM FLOOR BEAM ATTACHMENT FITTING AT FS621.00 AND RBL9.00 REF CRJ-200 SRM. EVALUATED AND FOUND TO BE OUT OF LIMITS. SUBMITTED TO ENGINEERING. RECEIVED AND COMPLIED WITH MHIRJ REO, ENG.DWG. FOUND TO BE STRUCTURALLY ACCEPTABLE FOR DETAILS SEE ATTACHED CONTINUATION CARD .

Part: SKIN — CORRODED (BS 559) · airframe 38,875 hrs · 34,465 cycles

EXTERIOR FS 559+96 SKIN CORRODED FROM STGR 23R TO 24R. C-CHECK RO 9/1/2020. REMOVED CORROSION AT FS 559+96 BETWEEN STRG 23R AND 24R REF REO. BLENDED AREA FOUND TO BE WITHIN LIMITS. SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH SKYWEST TASK CARD. PRESSURE LEAK CHECK GOOD.

Part: FRAME — CORRODED (BS 559) · airframe 38,875 hrs · 34,465 cycles

FRAME AT FS 559.0+112 IN THE AREA OF RBL 26 TO LBL 26 HAS CORROSION. C-CHECK RO 9/1/2020. EVALUATED AND FOUND FRAME AT FS.559+112 IN AREA OF RBL26 TO LBL26 TO BE OUT OF LIMITS. INSTALLED A NEW FRAME SPLICE ANGLE REF CRJ 200 SRM AND BOMBARDIER DWG. COMPLIED WITH TASK CARD. SEE CONTINUATION FOR FURTHER DETAILS.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 38,875 hrs · 34,465 cycles

THE SEAT TRACK AT LBL9.00 FROM APPROXIMATELY FS559.00+80 TO FS559.00+96 HAS MULTIPLE LOCATIONS OF CORROSION. REMOVED CORROSION ON SEAT TRACK AT LBL 9.00 FROM FS559.00+80 TO FS559.00+96, REF. CRJ 200 SRM. ORIGINAL MATERIAL THICKNESS OF LOCATION T=0.110,? REF. STANDARD MANUAL, REMAINING THICKNESS AFTER BLENDED OUT IS 0.079? MATERIAL LOSS IS 0.031 MAXIMUM ALLOWABLE LOSS IS 0.020? FOUND TO OUT OF LIMITS, REF. CRJ 200 SRM. 101. REMOVED & REPLACED SEAT TRACK AT LBL9 FROM FS 559.00+80 TO FS 559.00+96, REF. CRJ 200 AMM.

Part: FLOORBEAM — CHAFED (BS 621) · airframe 38,875 hrs · 34,465 cycles

THE FLOOR BEAM ATTACHMENT AT FS621.00 AT RBL27.00 IS CHAFFED (MARKED). C-CHECK RO 9/1/2020. REMOVED CHAFE FROM FLOOR BEAM ATTACHMENT FITTING AT FS621.00 AND RBL 27.00 REF CRJ-200 SRM. EVALUATED AND FOUND TO BE OUT OF LIMITS. SUBMITTED TO ENGINEERING. RECEIVED AND COMPLIED WITH MHIRJ REO, ENG.DWG, FOUND TO BE STRUCTURALLY ACCEPTABLE FOR DETAILS SEE ATTACHED CONTINUATION CARD.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 38,875 hrs · 34,465 cycles

THE RT FLOOR SILL JUST AFT OF FS559.00+80 TO JUST AFT OF FS559.00+112 HAS MULTIPLE LOCATIONS OF CORROSION (MARKED). C-CHECK RO 9/1/2020. REMOVED CORROSION ON RT FLOOR SILL JUST AFT OF FS559.00+80 TO JUST AFT FS559.00+112, REF CRJ 200 SRM, FLOOR SILL WAS OUT OF LIMITS PER BOMBARDIER REO. REMOVED AND REPLACED FLOOR SILL (WITH NEW) REF MHIRJ REO, & BOMBARDIER DWG. SEE CONTINUATION CARD FOR DETAILS.

Part: SKIN — CORRODED (BS 559) · airframe 38,875 hrs · 34,465 cycles

EXTERIOR STGR 23R JUST FWD OF FS 559+112 SILVER DOLLAR SIZE AREA CORRODED AS MARKED. C-CHECK RO 9/1/2020. REMOVED CORROSION ON EXTERIOR STRG 23R JUST FWD OF FS.559+112. FOUND TO BE OUT OF LIMITS. RECEIVED AND COMPLIED WITH ALL STEPS OF MHIRJ REO. COMPLIED WITH TASK CARD. SEE CONTINUATION FOR FURTHER DETAILS.

Part: FRAME — CRACKED (BS 333) · airframe 38,875 hrs · 34,465 cycles

SUSPECT CRACK IN THE FUSELAGE FORMER/FRAME AT APPROX. FS333 AT A TOOLING HOLE AT APPROX. STGR1L (MARKED ON AFT SIDE). C-CHECK RO 9/1/2020. REMOVED AND INSTALLED NEW FUSELAGE FORMER/FRAME PN 601R32004-41 AT APPROX. FS333 AT STGR1L TO STGR4L WITH SEALANT, SOLID FASTENERS AND HI-LITE FASTENERS. REF: ENG. DWG. AND CRJ-200 SRM. SEE CONTINUATION CARD FOR DETAILS. PRESSURE CHECK GOOD.

Part: SEAT TRACK — CORRODED (BS 559-621) · airframe 38,875 hrs · 34,465 cycles

THE SEAT TRACK AT LBL27.00 FROM APPROXIMATELY FS559.00+112 TO FS621.00 HAS MULTIPLE LOCATIONS OF CORROSION. REMOVED CORROSION ON SEAT TRACK AT LBL27.00 FROM FS559.00+112 TO FS621.00 REF. CRJ 200 SRM. ORIGINAL MATERIAL THICKNESS OF LOCATION T=0.110 REF. STANDARD MANUAL, REMAINING THICKNESS AFTER BLENDED OUT IS 0.080? MATERIAL LOSS IS 0.030? MAXIMUM ALLOWABLE LOSS IS 0.020? FOUND TO OUT OF LIMITS, REF. CRJ 200 SRM. REMOVED & REPLACED SEAT TRACK AT LBL27.00 FROM FS559.00+112 TO FS 621.00, REF. CRJ 200 AMM.

Part: SEAT TRACK — CORRODED (BS 559-621) · airframe 38,875 hrs · 34,465 cycles

THE SEAT TRACK AT LBL9.00 FROM APPROXIMATELY FS559.00+112 TO FS621.00 HAS MULTIPLE LOCATIONS OF CORROSION. REMOVED CORROSION ON SEAT TRACK AT LBL 9.00 FROM FS559.00+112 TO FS621.00 REF. CRJ 200 SRM. ORIGINAL MATERIAL THICKNESS OF LOCATION T=0.110,? REF STANDARD MANUAL, REMAINING THICKNESS AFTER BLENDED OUT IS 0.080? MATERIAL LOSS IS 0.030? MAXIMUM ALLOWABLE LOSS IS 0.020? FOUND TO BE OUT OF LIMITS, REF. CRJ 200 SRM. REMOVED & REPLACED SEAT TRACK AT LBL9 FROM FS 559.00+112 TO FS 621.00 REF CRJ 200 AMM.

Part: SEAT TRACK — CORRODED (BS 559-621) · airframe 38,875 hrs · 34,465 cycles

THE SEAT TRACK AT RBL9.00 FROM APPROXIMATELY FS559.00+112 TO FS621.00 HAS MULTIPLE LOCATIONS OF CORROSION. SEAT TRACK SECTION LOCATED AT RBL-9 BETWEEN FS559.00+112 - FS621.00 IS OUT OF LIMITS DUE TO SEVERE PITING AND INTERGRANULAR CORROSION FOUND ON OVER 50% OF SEAT TRACK FASTENER HOLES REPLACE PART. REPLACED SEAT TRACK PN 601R386631-3, RBL 9.00, FS 559.00+112 TO FS 621.00 REF CRJ 200 AMM.

Part: SKIN — CORRODED (BS 559) · airframe 38,875 hrs · 34,465 cycles

EXTERIOR FS'S 559/559+32 ADJACENT TO STGR 27 SEVERAL AREAS SHOWING CORROSION AS MARKED. C-CHECK RO 9/1/2020. REMOVED CORROSION ON FUSELAGE SKIN EXTERIOR FS'S 559/559+32 ADJACENT TO STGR 27 CRJ 200 SRM. BLENDED AREA FOUND TO BE WITHIN LIMITS REF REO. COMPLIED WITH TASK CARD. SEE CONTINUATION FOR FURTHER DETAILS.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 38,875 hrs · 34,465 cycles

THE SEAT TRACK AT RBL9.00 FROM APPROXIMATELY FS559.00+80 TO FS559.00+96 HAS MULTIPLE LOCATIONS OF CORROSION. SEAT TRACK LOCATED AT RBL 9 BETWEEN FS559.00+80 - FS559.00+96 IS OUT OF LIMITS DUE TO SEVERE PITING AND INTERGRANULAR CORROSION FOUND ON 50% OF SEAT TRACK; REPLACED PART. REPLACED SEAT TRACK PN 601R38779-13, RBL 9.00, FS 559.00+80-FS 559.00+96 REF CRJ 200 AMM.

Part: SEAT TRACK — CORRODED (BS 364-399) · airframe 38,875 hrs · 34,465 cycles

FLOOR SUPPORT STRUCTURE SEAT RAIL LBL9 FROM APPROXIMATELY FS364 TO FS399 HAS CORROSION AROUND FASTENER HOLES AND OTHER MARKED ELEMENTS. C-CHECK RO 9/1/2020. REMOVED AND REPLACED SEAT TRACK AT LBL 9 FROM FS 364 TO FS 399 WITH A SERVICABLE UNIT REF CRJ200 AMM. SEE CONTINUATION FOR DETAILS.

Part: STRAP — CORRODED (BS 559) · airframe 38,875 hrs · 34,465 cycles

TOP STRAP @ FS 559.0 LBL 27 TO SILL HAS CORROSION. C-CHECK RO 9/1/2020. REPLACED 559 LBL27 TOP STRAP, REF. CRJ200 SRM AND BOMBARDIER DRAWING. NO LEAKS DETECTED ON PRESSURE LEAK CHECK. COMPLIED WITH SKYWEST TASK CARD.

Part: FLOOR SUPPORT — CORRODED (BS 319) · airframe 38,875 hrs · 34,465 cycles

FLOOR SUPPORT STRUCTURE BRACKET AT THE FWD SERVICE DOOR FRAME FS319 HAS CORROSION. C-CHECK RO 9/1/2020. REMOVED CORROSION ON FWD SIDE OF LOWER FRAME BRACKET AT FS 319 & RBL 40, REF CRJ 200 SRM. BLENDED AREA FOUND TO BE OUT OF LIMITS REF CRJ200 SRM. INSTALLED BRACKET AT THE FWD SERVICE DOOR FRAME FS319 & RBL40 REF CRJ200 SRM AND BOMBARDIER DRAWING. SEE CONTINUATION CARD FOR DETAILS.

Part: DOOR FRAME — CORRODED (BS 364) · airframe 38,875 hrs · 34,465 cycles

MAIN AVIONICS COMPARTMENT DOOR CUTOUT INTERIOR SURROUND STRUCTURE FS364 GUSSET AT APPROX. STGR26R HAS CORROSION. C-CHECK RO 9/1/2020. BLENDED CORROSION, REFERENCE CRJ200 SRM. BEYOND ALLOWABLE LIMITS REF. CRJ200 SRM. REMOVED AND REPLACED GUSSET P/N: 601R31049-55 PER REF CRJ-200 SRM & BOMBARDIER DWG.

Part: FLOOR SUPPORT — CORRODED (BS 310-319) · airframe 38,875 hrs · 34,465 cycles

FLOOR SUPPORT STRUCTURE GALLEY MOUNT STRUCTURE BETWEEN FS310 TO FS319 AND APPROX. RBL6 (MARKED). C-CHECK RO 9/1/2020. BLENDED CORROSION ON GALLEY MOUNT FLOOR SUPPORT STRUCTURE BETWEEN FS310 TO FS319 AT APPROX RBL6 REF CRJ 200 SRM. PART WAS OUT OF LIMITS PER REF CRJ 200 SRM. REPLACED REF DWG. SEE CONTINUATION CARD FOR MORE DETAILS.

Part: FLOOR SUPPORT — CORRODED (BS 319) · airframe 38,875 hrs · 34,465 cycles

FLOOR SUPPORT STRUCTURE RT FLOOR SILL AROUND FS319 HAS CORROSION (MARKED). C-CHECK RO 9/1/2020. REMOVED CORROSION ON FLOOR SUPPORT STRUCTURE RT FLOOR SILL AROUND FS319 REF CRJ-200-SRM. BLENDED AREA FOUND TO BE OUT OF LIMITS DUE TO 100% MATERIAL LOSS. REMOVED CORRODED SILL AND INSTALLED NEW RT FLOOR SILL P/N 601R31148-79 AT FS319 REF CRJ200 SRM DRAWING. SEE CONTINUATION CARD FOR DETAILS.

Part: PRESSURE PANEL — CORRODED · airframe 38,875 hrs · 34,465 cycles

LT PRESSURE FS PANEL HAS SEVERAL AREAS OF CORROSION. C-CHECK RO 9/1/2020. REMOVED CORROSION FROM LT PRESSURE FS PANEL REF CRJ 200 SRM. BLENDED AREA FOUND TO BE WITHIN LIMITS REF REO. SEE CONTINUATION CARD FOR DETAILS.

Part: SEAT TRACK — CORRODED (BS 399-409) · airframe 38,875 hrs · 34,465 cycles

FLOOR SUPPORT STRUCTURE SEAT RAIL LBL9 FROM APPROXIMATELY FS399 TO FS409+128 HAS CORROSION AROUND FASTENER HOLES AND OTHER MARKED ELEMENTS. C-CHECK RO 9/1/2020. REMOVED AND REPLACED SEAT TRACK AT LBL 9 FROM FS 399 TO FS 409+128 WITH A SERVICABLE UNIT REF CRJ200 AMM. SEE CONTINUATION FOR DETAILS.

Part: FLOOR SUPPORT — CORRODED (BS 409) · airframe 38,875 hrs · 34,465 cycles

FLOOR SUPPORT STRUCTURE FLOOR BEAM, RBL9 FROM APPROX. FS409+4 TO FS409+120 HAS CORROSION (MARKED). C-CHECK RO 9/1/2020. REPLACED FLOOR BEAM AT RBL9 FROM APPROXIMATELY FS409+4 TO FS409+120 REF CRJ 200 SRM, DWG AND REO. SEE CONTINUATION CARD FOR DETAILS.

Part: SEAT TRACK — CORRODED (BS 399-409) · airframe 38,875 hrs · 34,465 cycles

FLOOR SUPPORT STRUCTURE SEAT RAIL RBL9 FROM APPROXIMATELY FS399 TO FS409+120 HAS CORROSION AROUND FASTENER HOLES AND OTHER MARKED ELEMENTS. C-CHECK RO 9/1/2020. REMOVED SEAT RAIL TO FOM FROM FS399 TO FS409+112 RBL9, REF CRJ200 AMM & INSTALLED NEW SEAT TRACK RBL 9 FROM FS399 TO FS409+120 REF CRJ200 AMM TOOL USED TUC 7826, CAL DUE 28-FEB-21.

Part: FRAME — CORRODED (BS 333) · airframe 38,875 hrs · 34,465 cycles

FS333 FRAME HAS CORROSION BETWEEN STGR 25R AND STGR 25L. C-CHECK RO 9/1/2020. REMOVED CORROSION AND FOUND FRAME AT FS.333 TO BE OUT OF LIMITS REF CRJ 200 SRM. INSTALLED A NEW FRAME AT FS.333 REF CRJ 200 SRM AND DRAWING. COMPLIED WITH TASK CARD. SEE CONTINUATION FOR FURTHER DETAILS.

Part: FRAME — CORRODED (BS 280) · airframe 38,875 hrs · 34,465 cycles

FS280 CIRCUMFERENTIAL JOINT HAS CORROSION ON MULTIPLE LOCATIONS ON THE STRAP BETWEEN STGR 25R AND STGR 25L (MARKED). C-CHECK RO 9/1/2020. REPAIRED *FS280 CIRCUMFERENTIAL JOINT REF REO. SEE CONTINUATION CARD FOR DETAILS.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 38,875 hrs · 34,465 cycles

SEAT TRACK LBL 9 FS 409+128 TO FS 559.0 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK AT LBL 9 FROM FS 409+128 TO FS 559.0 WITH A SERVICABLE UNIT REF CRJ200 AMM.

Part: ANGLE — CORRODED (BS 364) · airframe 38,875 hrs · 34,465 cycles

MAIN AVIONICS COMPARTMENT DOOR CUTOUT INTERIOR SURROUND STRUCTURE FS364 REINFORCING ANGLE BETWEEN APPROXIMATELY STGR 25R TO STGR 25L FOR THE FRAME IS CORRODED (MARKED). C-CHECK RO 9/1/2020. REMOVED CORROSION AND EVALUATED. CORROSION OF REINFORCING ANGLE FOUND TO BE OUT OF LIMITS PER CRJ200 SRM. REMOVED AND REPLACED ANGLE REF. BOMBARDIER DRAWING. COMPLIED WITH SKYWEST TASK CARD. SEE CONTNIUE CARD FOR ALL DETAILS.

Part: ANGLE — CRACKED (BS 484) · airframe 38,875 hrs · 34,465 cycles

RT FS 484.0 CLIP RBL 36 CLIP CRACKED. C-CHECK RO 9/1/2020. REMOVED AND INSTALLED A NEW RT CLIP AT FS.484 RBL 36 REF REO. COMPLIED WITH ALL APPLICABLE STEPS OF REO. COMPLIED WITH TASK CARD. SEE CONTINUATION FOR FURTHER DETAILS.

Part: FLOOR SUPPORT — CORRODED (BS 409) · airframe 38,875 hrs · 34,465 cycles

FLOOR SUPPORT STRUCTURE FLOOR BEAM, LBL9 FROM APPROXIMATELY FS409+4 TO FS409+96 HAS CORROSION (MARKED). C-CHECK RO 9/1/2020. REPAIRED FLOOR BEAM, LBL9 FROM APPROXIMATELY FS409+4 TO FS409+96 REF CRJ-200-SRM AND REO. SEE CONTINUATION CARD FOR DETAILS.

Part: STRAP — CORRODED (BS 559) · airframe 38,875 hrs · 34,465 cycles

TOP CAP @ FS 559.0 RBL 27 TO SILL HAS CORROSION. C-CHECK RO 9/1/2020. REPLACED FLOOR STRAP AT RBL 27 & FS.559.00, FLOOR STRAP P/N 601R31025-29 WITH NEW FASTENERS PER CRJ200 SRM REF. BOMBARD. DRAWING. COMPLIED WITH SKYWEST TASK CARD, LEAK CHECK GOOD NO DEFECTS NOTED. SEE CONTINUATION FOR DETAILS OF WORK PERFORMED.

Part: ANGLE — CRACKED (BS 484) · airframe 38,875 hrs · 34,465 cycles

LT FS 484.0 CLIP LBL 27 CLIP CRACKED. C-CHECK RO 9/1/2020. REMOVED AND INSTALLED NEW FS 484 CLIPS AT LBL 27.0, REF CRJ-200-SRM AND PREVIOUSLY INCORPORATED REO FOR FASTENER CALLOUT ONLY. SEE CONTINUATION CARD FOR DETAILS.

Part: INTERCOSTAL — CORRODED (BS 310-319) · airframe 38,875 hrs · 34,465 cycles

INTERCOSTAL AT STGR 20R BETWEEN FS310 AND FS319 HAS CORROSION. C-CHECK RO 9/1/2020. REMOVED CORROSION AND EVALUATED INTERCOSTAL REF. CRJ200 SRM. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW INTERCOASTAL REF. BOMBARDIER DRAWING. NO LEAKS FOUND AFTER PRESSURE LEAK CHECK. COMPLIED WITH SKYWEST TASK CARD.

Part: FLOOR SUPPORT — CORRODED (BS) · airframe 38,875 hrs · 34,465 cycles

FLOOR SUPPORT STRUCTURE LOWER FLOOR SUPPORT ANGLE AT THE BOTTOM OF THE SERVICE DOOR CUT-OUT HAS CORROSION (MARKED). C-CHECK RO 9/1/2020. REMOVED CORROSION ON THE FLOOR SUPPORT STRUCTURE LOWER FLOOR SUPPORT ANGLE AT THE BOTTOM OF THE SERVICE DOOR CUT-OUT, REF: CRJ-200 SRM. EVALUATED AND FOUND TO BE IS OUT OF LIMITS REF. CRJ200 SRM. INSTALLED NEW SERVICE DOOR FLOOR SUPPORT ANGLE PART#601R38303-253 PER BOMBARDIER DWG CRJ 200 SRM.

Part: INTERCOSTAL — CORRODED (EMERGENCY EXIT) · airframe 38,875 hrs · 34,465 cycles

LT OVERWING EMERGENCY EXIT DOOR INTERCOSTAL BELOW THE LATCH HANDLE HAS 11 RUSTY NUT PLATES AND CORROSION ON THE FLANGE. LT OVERWING EMERGENCY EXIT DOOR INTERCOSTAL BELOW THE LATCH HANDLE REPLACED 11 NUT PLATES REF CRJ 200 SRM.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 38,875 hrs · 34,465 cycles

RT INBOARD FLAP UPPER SKIN HAS DENTS AT WS 73 10" FROM TRAILING EDGE AND WS 76 14" FROM TRAILING EDGE. EVALUATE AND REMOVE DAMAGE, OR FILL AND PAINT. C-CHECK RO 9/1/2020. REPAIRED RT INBOARD FLAP UPPER SKIN, REF CRJ-200-SRM. SEE CONTINUATION CARD FOR DETAILS.

Part: ANGLE — BENT (LT WING TE FLAP) · airframe 38,875 hrs · 34,465 cycles

LT INBOARD FLAP FWD RIB, BOTTOM RIB ANGLE BENT UP AND NOT SECURED. RIB IS ON THE INBOARD SIDE OF THE OUTER HINGE ARM. REMOVED AND INSTALLED SERVICEABLE LT INBOARD FLAP, REF CRJ 200 AMM. PERFORMED OPERATIONAL TEST OF THE FLAPS IAW CRJ 200 AMM, TEST GOOD.

Part: BULKHEAD WEB — DENTED (BS 621) · airframe 38,875 hrs · 34,465 cycles

FS621 BULKHEAD HAS A DENT AND CHAFE MARK 3" ABOVE FLOOR AT APPROXIMATELY LBL32. C-CHECK RO 9/1/2020. REPAIRED FS621 BULKHEAD 3" ABOVE FLOOR AT APPROXIMATELY. LBL32, REF REO. SEE CONTINUATION CARD FOR DETAILS COMPLIED WITH SKYWEST TASK CARD.

Part: BULKHEAD — SCRATCHED (BS 621) · airframe 38,875 hrs · 34,465 cycles

FS 621 BULKHEAD HAS A 9? SCRATCH AT APPROXIMATELY LBL 24. BLENDED DAMAGE ON FS 621 BULKHEAD AT APPROXIMATELY LBL 24, REF CRJ-200-SRM. BLENDED AREA WAS FOUND TO BE OUT OF LIMITS, REF REO. REPAIRED FS 621 BULKHEAD AT APPROXIMATELY LBL 24, REF REO.

Part: SKIN — CHAFED (RT AILERON) · airframe 38,875 hrs · 34,465 cycles

RT AILERON EXTERIOR SKIN CHAFFED ON BOTTOM INBOARD AND OUTBOARD LEADING EDGES (MARKED). C-CHECK RO 9/1/2020. REMOVED CHAFE DAMAGE FROM THE RT AILERON OUTBOARD LEADING EDGE SKIN, EVALUATED AND FOUND TO BE WITHIN LIMITS, REF.CRJ200 SRM. REMOVED RT AILERON LOWER INBOARD SKIN PANEL, P/N 601R13031-148, REF CRJ200 SRM. REPALCED RT AILERON LOWER INBOARD SKIN PANEL, PN 601R13031-148, PER BOMBARDIER DWG AND CRJ 200 SRM.

Part: SKIN — CHAFED (RT WING) · airframe 38,875 hrs · 34,465 cycles

RIGHT WING LOWER PLANK CHAFE FROM FAIRING AT RBL 45. C-CHECK RO 9/1/2020. REPAIRED RIGHT WING LOWER PLANK AT RBL 45, REF REO. SEE CONTINUATION CARD FOR DETAILS.

Part: ATTACH BRACKET — CRACKED (BS 461) · airframe 38,875 hrs · 34,465 cycles

FS461.00 AND UNDER OVERWING PANEL 162EL THE PANEL ATTACH BRACKET ANGLE IS CRACKED (MARKED). C-CHECK RO 9/1/2020. INSTALLED NEW OVER WING PANEL 162EL ATTACH BRACKET P/N, REF CRJ200 SRM.

Part: ATTACH BRACKET — CRACKED (BS 473) · airframe 38,875 hrs · 34,465 cycles

AFT OF FS473.15 AND UNDER OVERWING PANEL 162EL THE PANEL ATTACH BRACKET ANGLE IS CRACKED (MARKED). C-CHECK RO 9/1/2020. REMOVED AND INSTALLED ANGLE AT FS473.15, REF CRJ-200-SRM. SEE CONTINUATION CARD FOR DETAILS.

Part: ATTACH BRACKET — CRACKED (BS 473) · airframe 38,875 hrs · 34,465 cycles

AFT OF FS473.15 AND UNDER OVERWING PANEL 161EL THE PANEL ATTACH BRACKET ANGLE IS CRACKED (MARKED). C-CHECK RO 9/1/2020. REMOVED AND REPLACED BRACKET ANGLE, P/N 601R31037-33, AT AFT OF FS473.15 AND UNDER OVERWING PANEL 161EL, REF CRJ200 SRM AND DWG. C/W ATTACHED TASK.

Part: ATTACH BRACKET — CRACKED (BS 473) · airframe 38,875 hrs · 34,465 cycles

FWD OF FS473.15 AND UNDER OVERWING PANEL 161EL THE PANEL ATTACH BRACKET ANGLE IS CRACKED. REMOVED AND INSTALLED NEW ATTACH BRACKET FWD OF FS473.15 AND UNDER OVERWING PANEL 161EL, REF CRJ-200-SRM.

Part: ATTACH FITTING — GOUGED (TE FLAP HINGE) · airframe 38,875 hrs · 34,465 cycles

RT OUTBOARD FLAP AFT HINGE BOX ATTACH FITTING, OUTBOARD ATTACH POINT INBOARD LUG GOUGED. C-CHECK RO 9/1/2020. BLENDED RT OUTBOARD FLAP, AFT HINGE BOX, OUTBOARD ATTACH POINT, INBOARD LUG REF CRJ-200 SRM. SUBMITTED TO ENGINEERING. RECEIVED AND COMPLIED WITH MHIRJ REO. FOUND TO BE STRUCTURALLY ACCEPTABLE. FOR DETAILS SEE ATTACHED CONTINUATION CARD.

Part: ATTACH BRACKET — CRACKED (BS 449) · airframe 38,875 hrs · 34,465 cycles

FS449.85 AND UNDER OVERWING PANEL 162EL THE PANEL ATTACH BRACKET ANGLE IS CRACKED. REMOVED AND REPLACED PANEL 162EL ATTACH BRACKET WITH NEW P/N 601R31037-48 AT FS 449.85, REF CRJ200 SRM.

Part: ATTACH BRACKET — CRACKED (BS 473) · airframe 38,875 hrs · 34,465 cycles

FWD OF FS473.15 AND UNDER OVERWING PANEL 162EL THE PANEL ATTACH BRACKET ANGLE IS CRACKED. REMOVED AND REPLACED OVER WING PANEL ATTACH BRAKET FWD OF FS473.15, REF CRJ200 SRM.

Part: LINKAGE — CORRODED (RUDDER XMITTER) · airframe 38,875 hrs · 34,465 cycles

RUDDER POSITION TRANSMITTER LINKAGE HAS CORRODED HARDWARE. C-CHECK RO 9/1/2020. REMOVED AND REPLACED CORRODED HARDWARES ON THE RUDDER TRANSMITTER LINKAGE PER REF CRJ 200 AMM AND CRJ 200 AMM.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 38,875 hrs · 34,465 cycles

RT INBOARD FLAP VANE SKIN CHAFED AT THE CENTER OF THE LEADING EDGE. C-CHECK RO 9/1/2020. REMOVED AND REPLACED WITH NEW RT INBOARD FLAP CENTER VANE SKIN, REF CRJ 200 SRM AND BOMBARIDER DWG. COMPLIED WITH SKYWEST TASK CARD.

Part: HINGE FITTING — GOUGED (RT ELEVATOR) · airframe 38,875 hrs · 34,465 cycles

RT ELEVATOR HINGE FITTING ON THE HORIZONTAL STABILIZER, CENTER POSITION, HAS A GOUGE (MARKED). C-CHECK RO 9/1/2020. BLENDED GOUGE FROM RT ELEVATOR HINGE FITTING ON THE HORIZONTAL STABILIZER, CENTER POSITION, REF CRJ 200 SRM. EVALUATED AND FOUND TO BE OUT OF LIMITS. SUBMITTED TO ENGINEERING AND RECEIVED MHIRJ REO. ALL STEPS COMPLIED WITH. COMPLIED WITH TASK CARD.

Part: SUPPORT — GOUGED (DOOR TRACK) · airframe 38,875 hrs · 34,465 cycles

CARGO DOOR TACK SUPPORT STRUCTURE OUTBOARD BEAM MEMBER IS GOUGED AT THE FWD END BELOW THE CABLE PULLEY (MARKED). C-CHECK RO 9/1/2020. REPLACED AND INSTALLED NEW OUTBOARD BEAM MEMBER, P/N 601R35050-64 PO:T000055969/1, AT CARGO TRACK SUPPORT STRUCTURE FS574.00 - FS621.00 REF CRJ200 SRM AND DWG. SEE CONTINUATION CARDS FOR DETAILS,

Part: WINDOW POST — CRACKED (RT COCKPIT) · airframe 38,875 hrs · 34,465 cycles

RT WINDSHIELD SIDE POST LOWER OUTBOARD CLIP CRACKED. C-CHECK RO 9/1/2020. REMOVED RT WINDSHIELD SIDE POST LOWER OUTBOARD CLIP (FITTING), REF CRJ200 SRM & INSTALLED NEW CLIP (FITTING) AT RT WINDSHIELD SIDE POST LOWER OUTBOARD, REF CRJ200 SRM AND BOMBARDIER DWG.

Part: LINK — CORRODED (RT SPOILER PCU) · airframe 38,875 hrs · 34,465 cycles

RT INBOARD GROUND SPOILER PCU LINK HARDWARE IS CORRODED. INSTALLED NEW HARDWARE ON RT INBOARD GROUND SPOILER PCU LINK, REF CRJ 200 AMM. OPERATIONS CHECK GOOD.

Part: SUPPORT — CRACKED (DOOR TRACK) · airframe 38,875 hrs · 34,465 cycles

CARGO DOOR TACK SUPPORT STRUCTURE CLIP ANGLE AT THE FORWARD END OF THE BEAM IS CRACKED.(FLAGGED). C-CHECK RO 9/1/2020. REPLACED CLIP ANGLE, PN 601R35050-121, WITH NEW PART PER CRJ 200 SRM & BOMBARDIER DWG. SEE CONTINUE CARD FOR DETAILS.

Part: LINK — CORRODED (RT SPOILER PCU) · airframe 38,875 hrs · 34,465 cycles

RT OUTBOARD GROUND SPOILER PCU LINK HARDWARE IS CORRODED. C-CHECK RO 9/1/2020. INSTALLED NEW HARDWARE ON RT OUTBOARD GROUND SPOILER PCU LINK, REF CRJ 200 AMM.

Part: SKIN — CHAFED (RT AILERON) · airframe 38,875 hrs · 34,465 cycles

RT AILERON UPPER LEADING EDGE OUTBOARD SKIN IS CHAFFED. C-CHECK RO 9/1/2020. REMOVED AND INSTALLED NEW RT AILERON UPPER LEADING EDGE SKIN, PART # CC670-13052-4 REF CRJ-200-SRM, AND BOMBARDIER DRAWING. SEE CONTINUATION CARD FOR DETAILS.

Part: CAM — CHAFED (PAX DOOR) · airframe 38,875 hrs · 34,465 cycles

PASSENGER DOOR SURROUND AFT CAM CHAFED THROUGH PROTECTIVE COATING. REPLACED CHAFED AFT DOOR CAM? AND SHIM WITH NEW DOOR CAM AND SHIM P/N 600-31688-18 AND 600-31900-83, REF CRJ 200 SRM.

Part: HOUSING — CHAFED (CRGO DOOR HANDLE) · airframe 38,875 hrs · 34,465 cycles

CARGO DOOR OUTER HANDLE HOUSING CHAFED (MARKED). C-CHECK RO 9/1/2020. REMOVED AND INSTALLED NEW CARGO DOOR HANDLE HOUSING, REF CRJ 200 SRM AND BOMBARIDER DWG 601R35027 REV-AY. COMPLIED WITH SKYWEST TASK CARD. ALL OPERATIONS CHECKS AND LEAK CHECK GOOD.

Part: VANE — CRACKED (RT WING TE FLAP) · airframe 38,875 hrs · 34,465 cycles

CRACK ON OUTBOARD MOVEABLE FLAP VANE AT APPROXIMATELY WS 226.51 TRAILING EGDE. REMOVED AND REPLACED RT OUTBOARD FLAP, REF CRJ200 AMM. ALL ASSOCIATED OPERATIONS CHECKS GOOD.

Part: CAM — CHAFED (PAX DOOR) · airframe 38,875 hrs · 34,465 cycles

PASSENGER DOOR SURROUND FORWARD CAM CHAFED THROUGH PROTECTIVE COATING. REPLACED CHAFED FWD DOOR CAM? AND SHIM WITH NEW DOOR CAM AND SHIM P/N 600-31688-17 AND 600-31900-83, REF CRJ 200 SRM.

Part: STOP FITTING — CHAFED (E/E BAY DOOR) · airframe 38,875 hrs · 34,465 cycles

LEFT AFT AVIONICS BAY DOOR STOP FITTING ON THE FUSELAGE CHAFED. INSTALLED NEW PART LEFT AFT AVIONICS BAY DOOR STOP FITTING ON THE FUSELAGE, PER CRJ 200 SRM.

Part: STOP FITTING — CHAFED (E/E BAY DOOR) · airframe 38,875 hrs · 34,465 cycles

LEFT FORWARD AVIONICS BAY DOOR STOP FITTING ON THE FUSELAGE CHAFED. REMOVED DAMAGED FWD LT AVIONICS BAY DOOR STOP FITTING, AND INSTALLED NEW P/N 601R38343-1, PER CRJ 200 SRM 51-41-02 AND AMM TASK.

Part: STOP FITTING — CHAFED (E/E BAY DOOR) · airframe 38,875 hrs · 34,465 cycles

RIGHT FORWARD AVIONICS BAY DOOR STOP FITTING ON THE FUSELAGE CHAFED. REMOVED DAMAGED FWD RT AVIONICS BAY DOOR STOP FITTING, AND INSTALLED NEW P/N 601R38343-1, PER CRJ 200 SRM AND AMM TASK.

Part: PAN — CORRODED (SERVICE DOOR) · airframe 38,875 hrs · 34,465 cycles

SERVICE DOOR LOWER FORWARD PAN HAS CORROSION (MARKED). C-CHECK RO 9/1/2020. REMOVED SERVICE DOOR CORROSION FROM LOWER FORWARD PAN, REF CRJ-200 AMM. BLENDED AREA FOUND TO BE OUT OF LIMITS, REF CRJ200 SRM. REPAIRED SERVICE DOOR LOWER FORWARD PAN, REF REO. SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH TASK CARD.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 38,875 hrs · 34,465 cycles

PASSENGER DOOR AFT DRAG ANGLE CRACKED NEAR PULLEY BRACKET. REMOVED AND INSTALLED NEW PASSENGER DOOR AFT DRAG ANGLE, REF CRJ 200 SRM.

Part: HOUSING — CHAFED (DOOR HANDLE) · airframe 38,875 hrs · 34,465 cycles

SERVICE DOOR CHAFED 3 PLACES AROUND OUTER HANDLE CUTOUT (MARKED). C-CHECK RO 9/1/2020. BLENDED SERVICE DOOR CHAFES AT 3 PLACES AROUND OUTER HANDLE CUTOUT (MARKED), REF CRJ-200 REO. EVALUATED AND FOUND TO BE OUT OF LIMITS. SUBMITTED TO ENGINEERING. RECIEVED MHI REO. ALL STEPS COMPLIED WITH, SEE CONTINUATION CARD FOR DETAILS.

Part: SKIN — DENTED (SERVICE DOOR) · airframe 38,875 hrs · 34,465 cycles

DENT ON THE SERVICE DOOR BETWEEN THE 'C' AND 'T' LETTERING. EVALUATE AND REPAIR OR FILL AND PAINT AS NEEDED. C-CHECK RO 9/1/2020. REPAIRED DENT ON THE SERVICE DOOR BETWEEN THE 'C' AND 'T' LETTERING, REF MHIRJ REO. SEE CONTINUATION CARD FOR DETAILS.

Part: BRACKET — CRACKED (EXTERNAL POWER) · airframe 38,875 hrs · 34,465 cycles

D: EXTERNAL POWER SERVICE PANEL LOWER MOUNTING BRACKET HAS A 2" CRACK IN THE RADIUS OF THE BEND. REPAIR AT NEXT C CHECK C: MCI. C-CHECK RO 9/1/2020. REMOVED AND INSTALLED NEW EXTERNAL POWER SERVICE PANEL, REF CRJ-200 SRM, ENG. DWG. AND MHIRJ REO. SEE CONTINUATION CARD FOR DETAILS.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 38,875 hrs · 34,465 cycles

COMPLY WITH SCHEDULED MAINTENANCE CODE: AD-COMPLIED WITH PARAGRAPH (J) OF AD BY: (J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FWD FACE OF THE FUSELAGE STATION (FS) 621 PRESSURE BULKHEAD, IAW AWL OF BOMBARDIER TR. (J)(2) MODIFYING THE RPB AND DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FS 621 PRESSURE BULKHEAD WEB, IAW BOMBARDIER REPAIR ENGINEERING ORDER (REO) AND MARKING THIS CAMP AS "STRUCTURAL REPAIR," WHICH WILL GENERATE AN RA FOR TRACKING THE SDIR FOR THIS REO ON THIS AIRPLANE, PART NUMBER: -, SERIAL NUMBER: 7651, POSITION. C-CHECK RO 9/1/2020. COMPLIED WITH SKY CARD.

Part: BUSHING — WORN (LT AILERON) · airframe 38,875 hrs · 34,465 cycles

REMOVE AND REPLACED BUSHINGS AND HARDWARE ON LT AILERON WING AFT SPAR, REF CRJ 200 AMM 20-26-00-910-804. REMOVED AND REPLACED BUSHINGS AND HARDWARE ON LT AILERON WING AFT SPAR, REF CRJ 200 AMM AND CRJ 200 AMM.

Part: UNKNOWN — FIRE (ENGINE) · airframe 37,524 hrs · 32,913 cycles

DURING SECOND ENGINE START WE HAD A HOT START. GROUND CREW INDICATED ENGINE FIRE. AFTER MOTORING THE ENGINE, THE GROUND CREW STILL INDICATED ENGINE FIRE. WE ELECTED TO RUN THE EXPEDITED DEPLANING CHECKLIST WHICH INCLUDING ACTIVATING THE FIRE BOTTLES. FIRE CREWS ARRIVED AND FOUND NO SIGNS OF EXTERNAL DAMAGE OR SMOKE. ENGINE EXTERNAL TEMPS READ UNDER 100F. (FLT#3986) CLOSED VERIFIED FIRE BOTTLES WERE NOT BLOWN, VERIFIED FIRE BOTTLE PRESSURES ARE GOOD IAW AMM. PERFORMED OPS TEST OF THE ENGINE FIRE / OVERHEAT DETECTION SYSTEM IAW AMM. C/W ENGINE RUNS WITH FLT CREW. COULD NOT DUPLICATE HOT START. NO FIRE DAMAGE NOTED.

Part: ROD — FAILED (PAX DOOR) · airframe 36,618 hrs · 31,898 cycles

PASSENGER DOOR WARNING MESSAGE ON APPROACH. EMERGENCY DESCENT. DEPLOYED PAX O2 MASK. (FLT#3502) CLOSED REMOVED AND REPLACED PAX DOOR ROD. ALSO REPACKED OXYGEN GENERATORS. 6L AND 11R AND LAV FOUND NOT USED IAW AMM. REMOVED AND REPLACED REST OF OXYGEN GENERATORS IAW AMM. COMPLIED WITH EMERGENCY DEPLOYMENT OF PASSENGER OXYGEN SYSTEM OPS CHECK GOOD IAW AMM. PERFORMED PRESSURIZATION CHECK OF A/C NO LEAKS NOTED IAW AMM.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 35,766 hrs · 30,917 cycles

CORROSION FOUND ON FLOOR SUPPORT CROSS BEAM UNDER NYLON PAD AT FS 349.0 AT LBL 39.0. (C-CHECK) RO: 07/03/2018 REMOVED AND INSTALLED NEW ANGLE IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 35,766 hrs · 30,917 cycles

FS 280 FLOORBEAM CRACKED AT RBL 9 ON FS 280 FLOORBEAM. (C-CHECK) RO: 07/03/2018 COMPLIED WITH PERMANENT REPAIR FS 280 FLOORBEAM BULKHEAD IAW REO.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 35,766 hrs · 30,917 cycles

PAX DOOR INTERCOSTAL DD1 (P/N:601R31902-318) CRACKED ON UPPER FLANGE. (C-CHECK) RO: 07/03/2018 REMOVED AND REPLACED PAX DOOR INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 35,766 hrs · 30,917 cycles

PAX DOOR INTERCOSTAL DD7 (P/N:601R318825-1) CRACKED ON UPPER FLANGE. (C-CHECK) RO: 07/03/2018 REMOVED AND REPLACED PAX DOOR INTERCOSTAL IAW SRM.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 35,766 hrs · 30,917 cycles

AFT CARGO DOOR LOWER SILL HAS EVIDENCE OF CORROSION AROUND FASTENER HOLES FROM FS 574.00 TO FS 621.00. (C-CHECK) RO: 07/03/2018 REMOVED AND REPLACED AFT CARGO DOOR LOWER SILL IAW REO. LEAK CHECK GOOD AT THIS TIME.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 35,766 hrs · 30,917 cycles

AFT CARGO SEAT TRACK CAP AT LBL 27.00 HAS EVIDENCE OF CORROSION AROUND FASTENER HOLES BETWEEN FS 559.00+112 TO FS 574.00. (C-CHECK) RO: 07/03/2018 REMOVED AND REPLACE CARGO FLOOR BEAM CAP FROM FS559+112 TO 574 IAW REO AND SRM.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 35,766 hrs · 30,917 cycles

RT PRESSURE FLOOR SILL, FLOOR PANEL HAS AREAS OF CORROSION FROM FS 409+128 - FS559. (C-CHECK) RO: 07/03/2018 REMOVED CORROSION FROM RT PRESSURE FLOOR SILL FLOOR PANEL IAW REO. PRESSURE CHECK GOOD AT THIS TIME.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 35,766 hrs · 30,917 cycles

LT PRESSURE FLOOR SILL, FLOOR PANEL HAS AREAS OF CORROSION FROM FS 409+128 - FS 559. (C-CHECK) RO: 07/03/2018 REMOVED CORROSION FROM LT PRESSURE FLOOR SILL, FLOOR PANEL IAW REO. PRESSURE CHECK GOOD AT THIS TIME.

Part: RIB — CORRODED (LT WING) · airframe 35,766 hrs · 30,917 cycles

DOUBLER AND BATT RIB IN L/H WHEEL WELL HAVE CORROSION AT WS 53.60. (C-CHECK) RO: 07/03/2018 REMOVED AND INSTALLED NEW BATT RIB AND DOUBLER AT LT WHEEL WELL AT WS 53.60 IAW SRM.

Part: ANGLE — CORRODED (LT WING) · airframe 35,766 hrs · 30,917 cycles

CLIP (ANGLE) ON FWD LWR AREA OF BATT RIB LOCATED AT WS 58.88 IS CORRODED. (C-CHECK) RO: 07/03/2018 REMOVED AND REPLACED WITH NEW CLIP P/N 601R10205-7 IAW SRM.

Part: ANGLE — CORRODED · airframe 32,203 hrs · 26,997 cycles

PAX DOOR LOWER SILL ANGLE HAS CORROSION AT SEVERAL LOCATIONS. INSTALLED NEW PAX DOOR LOWER SILL ANGLE IAW SRM. OPS CHECK GOOD AT THIS TIME.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 32,203 hrs · 26,997 cycles

RT INBD FLAP, OTBD FLAP VANE L/E CHAFED. R & R THE RT INBD FLAP, OTBD L/E VANE CAP IAW SRM.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 32,203 hrs · 26,997 cycles

LT INBD FLAP, INBOARD FLAP VANE LEADING EDGE CHAFED. R & R THE LT INBD FLAP, INBD FLAP LEADING EDGE VANE CAP, PN 601R14303-53 IAW SRM.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 32,203 hrs · 26,997 cycles

RT INBD FLAP, INBD FLAP VANE LE CHAFED. R & R THE RT INBD FLAP, INBD L/E VANE CAP IAW SRM.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 32,203 hrs · 26,997 cycles

LEFT INBD FLAP, OTBD FLAP VANE L/E CHAFED. R & R THE LT INBD FLAP,OTBD L/E VANE CAP IAW SRM.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 32,203 hrs · 26,997 cycles

LEFT INBD FLAP, CENTER FLAP VANE L/E, WS 104, CHAFED. R & R THE LT INBD FLAP, CENTER L/E VANE CAP IAW SRM.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 32,203 hrs · 26,997 cycles

RT INBD FLAP, CENTER L/E VANE CAP, WS108 CHAFED. R & R THE RT INBD FLAP, CENTER L/E VANE IAW SRM.

Part: STRAP — CORRODED (BS 559) · airframe 32,203 hrs · 26,997 cycles

EVIDENCE OF CORROSION ON RT SIDE FLOOR STRAP AT APPROXIMATELY BS 559, RBL 36 - 42 IN 3 LOCATIONS. R & R RT FLOOR STRAP IAW SRM.

Part: STRAP — CORRODED (BS 559) · airframe 32,203 hrs · 26,997 cycles

EVIDENCE OF CORROSION AT FS 559.00 ON STRAP AT APPROXIMATELY LBL 42.00. INSTALLED NEW STRAP AT FS 559.00 LBL 42.00 IAW SRM. LEAK CHECK GOOD AT THIS TIME.

Part: PLATE — CORRODED (SERVICE DOOR) · airframe 32,203 hrs · 26,997 cycles

SERVICE DOOR FLOOR PROTECTOR HAS CORROSION. R & R NEW SERVICE DOOR FLOOR PROTECTOR PLATE IAW SRM.

Part: INLET — ERODED (LT ENGINE) · airframe 29,146 hrs · 23,892 cycles

LEFT ENGINE INLET HAS EROSION FROM 6 O`CLOCK POSTITION TO 8 O`CLOCK POSTION. COMPLIED WITH TEMPORARY REPAIR OF EROSION ON OUTER SKIN L/E OF LT ENGINE INLET COWL FROM 6 O`CLOCK POSITION TO 8 O`CLOCK POSITION IN REFERENCE TO REO.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHT) · airframe 28,635 hrs · 23,400 cycles

LT SIDE WINDSCREEN EXIT LIGHT HAS BROKEN CONNECTOR. C-CHECK, INSTALLED CONNECTOR AND CONTACT TO EXIT LIGHT WIRE IAW ESPM AND AMM.

Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · airframe 28,635 hrs · 23,400 cycles

CARGO FLOOR SUPPORT CORRODED. C-CHECK, REMOVED CORROSION IAW REO.

Part: FLOOR SUPPORT — CHAFED (CARGO BAY) · airframe 28,635 hrs · 23,400 cycles

CARGO FLOOR SUPPORT HAS SEVERAL CHAFING MARKS NEAR NUTPLATES. C-CHECK, REPAIRED CARGO FLOOR SUPPORT, BLENDED CHAFES SMOOTH AND RESTORED FINISH TO REPAIR IAW REO.

Part: SEAT TRACK — CORRODED (BS 444-495) · airframe 28,635 hrs · 23,400 cycles

LT SIDE SEAT TRACK FROM BS 444.02 - 495.98 CORRODED. C-CHECK, R & R SEAT TRACK IAW AMM AND SRM.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 28,635 hrs · 23,400 cycles

CHAFE ON LT INBD FLAP VANE L/E. C-CHECK, BLENDED LT INBD FLAP VANE L/E IAW SRM AND REO.

Part: FLOOR SUPPORT — CORRODED (BS 516-559) · airframe 28,635 hrs · 23,400 cycles

LEFT PRESSURE FLOOR SUPPORT UPPER SURFACE ANGLE, BS 516-559 HAS THREE LOCATIONS OF CORROSION ALONG LBL 43. REMOVED CORROSION IAW REO AND EA.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 28,635 hrs · 23,400 cycles

CHAFE ON RT INBD FLAP VANE L/E. C-CHECK BLENDED RT INBD FLAP VANE L/E IAW SRM AND REO.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 28,635 hrs · 23,400 cycles

CHAFE ON RT INBD FLAP VANE L/E. C-CHECK, BLENDED RT INBD FLAP VANE L/E IAW SRM AND REO.

Part: FLOOR SUPPORT — CORRODED (BS 409-473) · airframe 28,635 hrs · 23,400 cycles

LEFT PRESSURE FLOOR SUPPORT UPPER SURFACE DOUBLER BS 409-473 HAS FOUR LOCATIONS OF CORROSION ALONG LBL 43. C-CHECK, REMOVED CORROSION IAW REO.

Part: FRAME — CORRODED (BS 513) · airframe 28,635 hrs · 23,400 cycles

FRAME AT BS 513 HAS CORROSION ON AFT EDGE. C-CHECK, BLENDED CORROSION IAW SRM AND REO.

Part: FLOOR SUPPORT — CORRODED (BS 474-513) · airframe 28,635 hrs · 23,400 cycles

RIGHT PRESSURE FLOOR SUPPORT UPPER SURFACE ANGLE, BS 474-513, HAS THREE LOCATIONS OF CORROSION ALONG RBL 43. C-CHECK, REMOVED CORROSION IAW REO AND STS EA.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 28,635 hrs · 23,400 cycles

CHAFE ON LT INBD FLAP VANE L/E. C-CHECK, BLENDED LT INBD FLAP VANE L/E IAW SRM.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 28,635 hrs · 23,400 cycles

CHAFE ON RT INBD FLAP VANE L/E. C-CHECK, BLENDED RT INBD FLAP VANE L/E IAW SRM AND REO.

Part: FLOOR SUPPORT — CORRODED (BS 409-473) · airframe 28,635 hrs · 23,400 cycles

RIGHT PRESSURE FLOOR SUPPORT UPPER SURFACE DOUBLER, BS 409-473 HAS THREE LOCATIONS OF CORROSION ALONG RBL 43. C-CHECK, REMOVED CORROSION IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 474-513) · airframe 28,635 hrs · 23,400 cycles

LEFT PRESSURE FLOOR SUPPORT UPPER SURFACE DOUBLER, BS 474-513 HAS TWO LOCATIONS OF CORROSION ALONG LBL 43. C-CHECK, REMOVED CORROSION IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 516) · airframe 28,635 hrs · 23,400 cycles

RIGHT PRESSURE FLOOR SUPPORT UPPER SURFACE HAS CORROSION AT BS 516, RBL 43. C-CHECK, REMOVED CORROSION IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 28,635 hrs · 23,400 cycles

RT PRESSURE FLOOR SUPPORT UPPER SURFACE NUT PLATE STRIP HAS CORROSION BS 559, RBL 38. C-CHECK, REMOVED CORROSION IAW SRM AND EA.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 28,635 hrs · 23,400 cycles

CHAFE ON LT INBD FLAP VANE L/E. C-CHECK, BLENDED LT INBD FLAP VANE L/E IAW SRM.

Part: SEAT TRACK — CORRODED (BS 400) · airframe 28,635 hrs · 23,400 cycles

RIGHT CABIN FLOOR SEAT TRACK CORRODED AT BS 400 RBL 9. C-CHECK, R & R SEAT TRACK IAW AMM.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 28,635 hrs · 23,400 cycles

PAX DOOR AFT DRAG ANGLE CRACKED AT PULLEY MOUNT FOR ASSIST MOTOR. C-CHECK, REPAIRED PAX DOOR AFT DRAG ANGLE NEAR PULLEY MOUNT IAW REO.

Part: STIFFENER — CRACKED (BS 409) · airframe 28,635 hrs · 23,400 cycles

VERTICAL POST AT FS 409+128, RBL 27 INBD SIDE IS CRACKED ON LOWER RADIUS. C-CHECK REPLACED POST IAW SRM AND EA.

Part: STIFFENER — CRACKED (BS 409) · airframe 28,635 hrs · 23,400 cycles

VERTICAL POST AT BS 409+128, LBL 18 OTBD SIDE IS CRACKED ON LOWER RADIUS. C-CHECK, REPLACED POST IAW SRM AND REO.

Part: STIFFENER — CRACKED (BS 409) · airframe 28,635 hrs · 23,400 cycles

VERTICAL POST AT BS 409+128, RBL 18 OTBD SIDE IS CRACKED IN LOWER RADIUS. C-CHECK, REPLACED POST IAW SRM AND REO.

Part: BULKHEAD — CRACKED (BS 202) · airframe 28,635 hrs · 23,400 cycles

PARKING BRAKE CABLE PASS THRU HOLE ON BULKHEAD CRACKED AT BS 202. C-CHECK, REPAIRED PRESSURE BULKHEAD IAW REO.

Part: STIFFENER — CRACKED (BS 409) · airframe 28,635 hrs · 23,400 cycles

VERTICAL POST AT BS 409+128 AND LBL 27 INBD SIDE IS CRACKED IN LOWER RADIUS. C-CHECK, REPLACED POST IAW SRM AND EA.

Part: SKIN — CHAFED (RT MLG DOOR) · airframe 28,635 hrs · 23,400 cycles

RIGHT MLG DOOR CHAFED AT AFT LOWER CORNER, INTERNAL SKIN. C-CHECK, RT MLG DOOR REPAIRED BY BLENDING IAW REO.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 28,539 hrs · 23,302 cycles

EXTERNAL EMERGENCY LIGHT, NR 5 IS BURNED OUT. REPLACED LAMP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,853 hrs · 22,611 cycles

NR 2 EMERGENCY OVERHEAD LIGHT IS BURNED OUT. FLT 7369 RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,578 hrs · 20,409 cycles

NR 4 OVERHEAD EMERGENCY LIGHT DOES NOT ILLUMINATE. (FLT 4520) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 25,437 hrs · 20,268 cycles

NR 3 EXTERIOR EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 25,156 hrs · 20,008 cycles

RIGHT WING AFT OVERWING EMERGENCY LIGHT IS OUT. (SERVICE) LIGHT WORKED AFTER EMERGENCY LIGHT BATTERY PACK WAS CHARGED.

Part: SKIN — DENTED (TE FLAP) · airframe 25,062 hrs · 19,924 cycles

LEFT INBOARD FLAP LOWER SKIN IS DENTED. (C-CHECK) REPAIRED LEFT INBOARD FLAP LOWER SKIN AS PER CRJ 200 SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,942 hrs · 19,815 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4813) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,873 hrs · 19,747 cycles

THE 4TH OVERHEAD EMERGENCY LIGHT FROM THE FRONT IS OUT. (FLT 4605) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,754 hrs · 19,642 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 2 IS OUT. (FLT 4722) RELAMPED EMERGENCY LIGHT.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 24,684 hrs · 19,582 cycles

FLT 4609, NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,407 hrs · 19,348 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4472) RELAMPED EMERGENCY LIGHT.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 24,369 hrs · 19,313 cycles

FLT 4451, NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 24,306 hrs · 19,246 cycles

NR 8 EXTERIOR EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,306 hrs · 19,246 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4718) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,015 hrs · 18,965 cycles

FORWARD CEILING EMERGENCY FLOOD LIGHT IS OUT. (FLT 4688) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 23,689 hrs · 18,658 cycles

FORWARD AND AFT RIGHT EXTERIOR EMERGENCY LIGHTS ARE OUT. (FLT 4743) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,615 hrs · 18,583 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4550) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 23,615 hrs · 18,583 cycles

FORWARD EXTERIOR EMERGENCY EXIT LIGHTS OUT OVER LEFT AND RIGHT WINGS. (FLT 4481) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 23,588 hrs · 18,562 cycles

NR 2 AND NR 8 EXTERIOR EMERGENCY LIGHTS ARE OUT. (SERVICE) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,466 hrs · 18,452 cycles

NR 3 OVERHEAD EMERGENCY LIGHT BURNED OUT. (FLT 4473) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 23,466 hrs · 18,452 cycles

LEFT MIDDLE EXTERIOR EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,402 hrs · 18,400 cycles

SECOND TO LAST OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4692) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,317 hrs · 18,323 cycles

AFT 2 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 4511) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 23,276 hrs · 18,281 cycles

FORWARD AND AFT LEFT EXTERIOR EMERGENCY LIGHTS ARE OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 23,177 hrs · 18,187 cycles

RIGHT MIDDLE AND AFT FUELAGE EXTERIOR OVERWING EMEGENCY LIGHTS ARE OUT. (SERVICE) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,843 hrs · 17,891 cycles

NR 2 AND 3 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 4553) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 22,182 hrs · 17,314 cycles

THE 1ST AND 3RD EMERGENCY EXIT LIGHTS (EXTERIOR) ON LEFT SIDE OVERWING ARE BURNED OUT. (FLT 4615) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,847 hrs · 17,037 cycles

AFT OVERHEAD EMERGENCY LIGHT OUT. (FLT 4604) RELAMPED EMERGENCY LIGHT.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,769 hrs · 16,974 cycles

FS 559.0 PRESSURE BULKHEAD CRACKED AT RIGHT SIDE. (C-CHECK) REPAIR PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,909 hrs · 17,088 cycles

FS 621.0 BULKHEAD AT AFT CARGO DOOR UPPER TRACK CRACKED AT WEB. (C-CHECK) REPAIRED PER REO.

Part: MOUNT — CORRODED (LT ENGINE) · airframe 21,544 hrs · 16,772 cycles

FORWARD MOUNT BOLTS ON LEFT ENGINE HAVE SMALL AREA PITTED AND SHANK DIAMETER ON AREA 2 OUT OF LIMITS PER AMM. (ENGINE CHANGE) REPLACED LEFT ENGINE FORWARD MOUNT PINS.

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 21,544 hrs · 16,772 cycles

VIB CAUTION MESSAGE ON N2 OF LEFT ENGINE FOLLOWED BY HOT ITT FOLLOWED BY OIL PRESSURE LOSS. (FLT 4719) REPLACED LEFT ENGINE ASSEMBLY WITH A SERVICEABLE UNIT PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,356 hrs · 16,613 cycles

FIRST CEILING LEVEL EMERGENCY FLOOD LIGHT INOPERATIVE. (FLT4779) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,843 hrs · 16,175 cycles

AFT EMERGENCY CEILING LIGHT INOP. (FLT 4560) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,414 hrs · 15,797 cycles

OVERHEAD EMERGENCY LIGHT INOP. (FLT 4763) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,284 hrs · 14,812 cycles

AFT CEILING LEVEL EMERGENCY FLOODLIGHT INOP. (FLT 4562) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,004 hrs · 14,589 cycles

EMERGENCY LIGHT AT AFT END OF CABIN INOP. (FLT 4879) RELAMPED EMERGENCY LIGHT.

Part: SELECTOR VALVE — MALFUNCTIONED (NLG) · airframe 17,606 hrs · 13,519 cycles

FLT 4543 - ON GEAR EXTENSION, RECEIVED A NLG GEAR DISAGREE WARNING MESSAGE. REPLACED NLG SELECTOR VALVE ASSEMBLY PN ON 750006000, PN OFF 601R75146-1, SN ON 1063, SN OFF 1928.

Part: FITTING — CRACKED (BULKHEAD) · airframe 17,578 hrs · 13,498 cycles

AFT PRESSURE BULKHEAD FORWARD FACET CRACKED AT LINTEL FITTING (C-CHECK). REPAIRED PER REO.

Part: LINK — CORRODED (AILERON) · airframe 17,578 hrs · 13,498 cycles

C-CHECK, LEFT FLUTTER DAMPER SHEAR LINK ASSEMBLY CORRODED. REPLACED PER AMM.

Part: FITTING — CORRODED (LT ENGINE MOUNT) · airframe 17,578 hrs · 13,498 cycles

C-CHECK, LEFT AFT ENGINE MOUNT THRUST FITTING CORRODED. REPLACED PER AMM.

Part: FITTING — CORRODED (RT ENGINE MOUNT) · airframe 17,578 hrs · 13,498 cycles

RIGHT AFT ENGINE MOUNT THRUST FITTING CORRODED (C-CHECK). REPLACED PER AMM.

Part: ACM — OVERHEATED (RIGHT) · airframe 16,538 hrs · 12,721 cycles

FLT 3743 - RIGHT PACK WAS SMOKING IN AUTO MODE. REPLACED RIGHT ACM IAW AMM 21-51-10. OPS CHECK GOOD, P/N 782790-15, S/N OFF 200110263.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 12,595 hrs · 9,753 cycles

AFT CENTER CEILING LEVEL EMERGENCY FLOOD LIGHT IS INOP. RELAMPED AFT CENTER CEILING EMERGENCY LIGHT.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 12,537 hrs · 9,707 cycles

RT INBD FS484 CLIP CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CLIP P/N 601R-31171-9 AT STN 484, RBL 27.0 IAW CRJ 200 REO 601R-53-41-059, REV A.

Part: SUPPORT BEAM — CRACKED (ENGINE) · airframe 12,537 hrs · 9,707 cycles

ENG SUPPORT BEAM LT LWR ACCESS PNL CUTOUT IS CRACKED AT FWD INBD CORNER, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS TO ENGINE SUPPORT BEAM LT LOWER WEB PER CRJ200 SRM 51-42-06 P11 AND 51-42-20 PG 23.

Part: FRAME — CRACKED (BS 280) · airframe 12,537 hrs · 9,707 cycles

FS 280 RBL9 LWR FRAME CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR ANGLE PER BOMBARDIER REO 601R 53-11-171 AND 601R 53-11-102 P/N 86144A33.

Part: STEP — CRACKED (PAX DOOR) · airframe 12,537 hrs · 9,707 cycles

PAX DOOR 4TH STEP CRACK IN FWD AND AFT RADIUS, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR ON FWD 4TH STEP ON PAX DOOR IAW CRJ200 REO 601R-52-11-702 REV A.

Part: FRAME — CRACKED (BS 280) · airframe 12,537 hrs · 9,707 cycles

FS 280 LBL9 UPPER FRAME CRACKED MARKED RBL 9 UPPER FRAME CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS PER REO 601R-53-11-136.

Part: SUPPORT — CRACKED (BS 461) · airframe 12,537 hrs · 9,707 cycles

CRACKED SUPPORT FS 461 RBL10 WL70, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW SUPPORT AT FS 461 RBL10 WL70 P/N 600-31068-19 PER CRJF200 SRM 51-42-21 PG 1, 2, 3, AND 4.

Part: STRINGER CLIP — CRACKED (BS 625) · airframe 12,537 hrs · 9,707 cycles

CRACK AT STR 12 FS 625 LT SIDE, DISCOVERED DURING C-CHECK INSPECTION. FS 625 LT SIDE ATTACH CLIP AT STR 12 REPLACED WITH NEW PART IAW CRJ 200 SRM 51-42-21 PG 13-19.

Part: WEB — CRACKED (PAX DOOR) · airframe 12,537 hrs · 9,707 cycles

PAX DOOR AFT WEB CRACKED UNDER HAND RAIL STOP AND GAS SPRING SUPPORT, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED DOUBLER, ANGLES AND SHIMS AS PER REO 601R-52-11-702.

Part: HINGE — CRACKED (ESCAPE HATCH) · airframe 12,537 hrs · 9,707 cycles

LT HINGE ARM ON CREW ESCAPE HATCH IS CRACKED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED BROKEN HINGE ARM ON CREW ESCAPE HATCH PER CRJ200 SRM 51-41-04 PG 1-11.

Part: ENGINE — VIBRATION (LT ENGINE) · airframe 11,933 hrs · 9,268 cycles

LT N2 CORE VIB AT 26,500 IN ICING CONDITION. SHUTDOWN LT ENGINE, DIVERTED TO BOI. RAN ENGINES IAW 72-00-00 AND VIBES STAYED NEAR .2 TO .3 MILS. WITHIN LIMITS OF MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 9,775 hrs · 7,686 cycles

NR 1 AFT CEILING LEVEL EMERGENCY FLOOD LIGHT INOP. REPLACED AFT CEILING LEVEL EMERGENCY FLOODLIGHT IAW MM 33-51-16. OPERATIONAL CHECK GOOD.

Part: PCU — MALFUNCTIONED (SPOILERS) · airframe 9,393 hrs · 7,384 cycles

FLT SPOILERS FAULT STATUS MSG. REPLACED LT OB PCU ON LT FLIGHT SPOILER. OPERATIONAL CHECK GOOD IAW MM 27-61-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 9,366 hrs · 7,363 cycles

THE 1ST OVERHEAD EMERGENCY LIGHT IN THE CABIN IS INOP. REPLACED CABIN CEILING EMERGENCY LIGHT IAW MM 33-51-16. OPERATIONAL CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (HORIZONTAL STAB) · airframe 8,932 hrs · 7,019 cycles

IN FLIGHT AT 31,000 FT RECEIVED STAB TRIM AND MACH TRIM CAUTION MSG. REPLACED HSTCU AND MOTOR CONTROL UNIT IAW 27-23-01 AND RII 27-415. P/N 7062-3, S/N OFF 319.

Part: BPSU — MALFUNCTIONED (TE FLAPS) · airframe 8,169 hrs · 6,396 cycles

CLIMBING THRU FLT LEVEL 280, RECEIVED AMBER FLAPS FAIL CAUTION MSG. REPLACED RT BPSU IAW MM 27-51-10 AND FECU IAW MM 27-51-05. OPS CHECK GOOD, PN: 860D100-18 SN OFF: 1104.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 8,127 hrs · 6,362 cycles

CEILING LEVEL EMERGENCY FLOODLIGHT A BEAM ROW 10 IS INOPERATIVE. RELAMPED IAW CRJ 200 AMM 33-51-16.

Part: CONTACT — DIRTY (EMERGENCY LIGHT) · airframe 8,127 hrs · 6,362 cycles

EMERGENCY FLOOR LIGHTING STRIP AFT SECTIONS WILL NOT ILLUMINATE. CLEANED CONTACTS AT SEGMENTS. OPERATIONAL CHECK GOOD.

Part: CLIP — CRACKED (BS 280) · airframe 9,232 hrs · 7,254 cycles

FS 280 RBL 9 (2 EA) CLIPS CRACKED I/B & O/B. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED RIGHT O/B CLIP PER CRJ200 SRM 51-42-06 & 51-40-20. INSTALLED RIGHT I/B CLIP PER CRJ200 SRM 51-42-06.

Part: FLOORBEAM — CRACKED (BS 621) · airframe 9,232 hrs · 7,254 cycles

RIGHT FLOORBEAM ANGLE AT FS 621.00 BETWEEN RBL 27 AND RBL 45. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED REPAIR PARTS PER REO 601R-53-61-117 AND CRJ200 SRM 51-42-06 AND SRM 51-42-21.

Part: FLOORBEAM — CRACKED (BS 621) · airframe 9,232 hrs · 7,254 cycles

LEFT FLOORBEAM ANGLE AT FS 621 BETWEEN LBL 27 AND LBL 45. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED REPAIR PARTS PER REO 601R-53-61-117 AND CRJ200 SRM 51-42-06 AND 51-42-21.

Part: CLIP — CRACKED (BS 280) · airframe 9,232 hrs · 7,254 cycles

FS 280 LBL 9, 2 EA CLIPS CRACKED I/B & O/B. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED CLIPS IAW ENG DWG 601R31113 AND CRJ200 SRM CG 51-42-06 & 51-42-20.

Part: OXYGEN MASK — DEPLOYED (CABIN) · airframe 7,562 hrs · 5,895 cycles

AFTER OPENING MAIN CABIN DOOR, ALL O2 MASKS DEPLOYED. RE-PACKED PASSENGER O2 MASKS IAW AMM 35-21-09.

Part: PCU — INOPERATIVE (FLT SPOILER) · airframe 6,914 hrs · 5,382 cycles

RIGHT SPOILERON NR 3 PCU INOPERATIVE. REMOVED AND REPLACED RIGHT OUTBOARD SPOILER ON PCU WITH SERVICEABLE UNIT IAW MM 27-62-01. REPLACED RIGHT SECU WITH SERVICEABLE UNIT, MM 27-60-00. OPERATIONAL CHECK GOOD. P/N 49-164-06, S/N OFF: 01624.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILER) · airframe 6,760 hrs · 5,267 cycles

INBOARD GROUND SPOILERS STATUS ON AFTER 2ND ENGINE START. REMOVED AND REPLACED NR 1 SECU IAW MM CH 27-61-05, OPERATIONAL CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 6,646 hrs · 5,174 cycles

FIRST GREEN SECTION OF THE EMERGENCY FLOOR PATH LIGHTS IS OUT. REPLACED FORWARD GREEN EMERGENCY FLOOR LIGHTING STRIP IAW CRJ MM 33-51-01, OPERATIONAL CHECK GOOD.

Part: SWITCH — DIRTY (STAB TRIM) · airframe 6,271 hrs · 4,872 cycles

MACH TRIM AND STAB TRIM CAUTION MESSAGES INFLIGHT AT CRUISE ALTITUDE. CLEANED PILOTS SIDE SWITCH. PERFORMED TEST OF HSTCU, OPERATIONAL CHECK GOOD.

Part: PCU — MALFUNCTIONED (FLIGHT SPOILER) · airframe 5,253 hrs · 4,088 cycles

SPOILERON FAULT MESSAGE. REPLACED HYDRAULIC NR 1 PRESSURE SWITCH, LEFT SPOILERON PCU AND NR 2 SECU. OPS CHECK GOOD IAW MM CH 27-62-01. P/N 49-164-06, S/N OFF 01598.

Part: ACTUATOR — MALFUNCTIONED (HORIZONTAL STAB) · airframe 4,984 hrs · 3,874 cycles

NR 2 STAB TRIM WOULD NOT ENGAGE. REMOVED AND REPLACED HSTA IAW MM 27-42-05, 27-42-01 & 27-40-00. REPLACED MCU P/N: 7062-3, S/N OFF: 904. REPLACED STAB ENGAGE PANEL. P/N: 601R51706-3. OPS CHECK GOOD.

Part: PCU — MALFUNCTIONED (SPOILERS) · airframe 4,443 hrs · 3,468 cycles

ON TAXI OUT, SPOILERONS FAULT STATUS MESSAGE. REMOVED AND REPLACED RIGHT SPOILERON OUTBOARD PCU AND SECU NR 1. OPS CHECK SATISFACTORY. LEAK CHECK SATISFACTORY IAW MM 27-60-03. PCU P/N: 49-164-06, S/N OFF: 01389.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILER) · airframe 4,221 hrs · 3,304 cycles

CREW REPORTS GROUND SPOILER FAULTS. REMOVED & REPLACED NR 1 SECU, REF MM 27-61-05. OPS CHECKS GOOD.

Part: FLOORBEAM — CRACKED (FUSLAGE) · airframe 4,055 hrs · 3,167 cycles

FS 280 RT FLOORBEAM RBL 9.0 INBOARD AND OUTBOARD ATTACH ANGLES CRACKED. DISCOVERED DURING C-CHECK INSPECTION. ANGLES REPLACED IAW CRJ SRM 51-40-11 AND RII 53-401.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 4,055 hrs · 3,167 cycles

FS 625 RIGHT INTERCOSTAL ANGLE STR 14R CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11. P/N: 601-35012-52

Part: ANGLE — CRACKED (FUSELAGE) · airframe 4,055 hrs · 3,167 cycles

FS 625 LT INTERCOSTAL ANGLE STR 14L CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11. P/N: 601-35012-51

Part: HANDLE — CRACKED (PAX DOOR) · airframe 4,055 hrs · 3,167 cycles

PAX DOOR OUTER HANDLE CRACKED. DISCOVERED DURING C-CHECK INSPECTION. PAX DOOR OUTER HANDLE INSTALLED IAW CRJ MM 52-11-03-400-802.

Part: CLIP — CRACKED (FUSELAGE) · airframe 4,055 hrs · 3,167 cycles

FS 484 RT INTERCOSTAL I/B CLIP RBL 27 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. CLIP REPLACED IAW REO 601R-53-41-059 REV ''A''.

Part: ECU — MALFUNCTIONED (TE FLAPS) · airframe 3,423 hrs · 2,652 cycles

''FLAPS FAIL'' CAUTION DURING CRUISE FLIGHT. NO FLAP LANDING IAW QRH. REMOVED AND REPLACED FECU IAW CL 600 MM 27-51-05. OPS CHECKS GOOD.

Part: WIRE — BROKEN (CONNECTOR) · airframe 3,373 hrs · 2,612 cycles

(STALL FAIL) MESSAGE WHILE ENROUTE COMPLIED WITH THE APPROPRIATE QRH PROCEDURE. REPAIRED BROKEN WIRE AT CONNECTOR FOR CAPT STICK SHAKER.

Part: BPSU — MALFUNCTIONED (TE FLAPS) · airframe 2,868 hrs · 2,242 cycles

FLAP FAIL CAUTION MESSAGE APPEARED 20 MIN AFTER DEPARTURE. REMOVED AND REPLACED LT BPSU. RIGGED LEFT AND RIGHT BPSU IAW MM 27-51-10. FOUND FECU POTENTIOMETER OUTSIDE LIMIT. ADJUSTED FECU POTENTIOMETERS. REMOVED AND REPLACED FLAP CONTROL LEVER PER CRJ MM 27-51-00. OPS CHECK OF FLAP CONTROL LEVER GOOD. FLAP OPS CHECK GOOD. P/N: 7-45500-1 S/N OFF: 0470.

Part: CONTROL UNIT — MALFUNCTIONED (LT SPOILERS) · airframe 2,540 hrs · 1,964 cycles

FLT SPOILER AND O/B GROUND SPOILER STATUS MESSAGES ILLUMINATED. REMOVED AND REPLACED LEFT SECU. MESSAGES NO LONGER DISPLAYED. OPS CHECK GOOD AT THIS TIME. S/N OFF 01600.

Part: STRUCTURE — BURNED (LT TE FLAPS) · airframe 2,181 hrs · 1,687 cycles

LEFT OUTBOARD FLAP TRAILING EDGE HAS SEVERAL BURNED AREAS AS A RESULT OF A LIGHTNING STRIKE. INSTALLED SERVICEABLE FLAP ON LEFT OUTBOARD POSITION IAW 27-54-01 AND 27-54-05. S/N OFF: SB/RJ/731.

Part: WIRE — SHORTED (FLAP CANNON PLUG) · airframe 252 hrs · 199 cycles

AT ROTATION, WINDSHEAR FAIL STATUS MESSAGE AND STICK SHAKER ACTUATION UP TO 180 KNTS. RETURNED FOR LANDING AT SLC. FOUND WIRE CG51C22 SHORTING AT FLAP POSITION TRANSMITTER CANNON PLUG P1CF. REMOVED DAMAGED WIRE LENGTH AND REPLACED SOCKETS ON ALL WIRES TO CONNECTORS. FLAP OPERATIONS CHECKS GOOD.

Part: WIRE — SHORTED (FLAP POSITION IN) · airframe 195 hrs · 157 cycles

UPON ROTATION IN OKC, THROUGH 10 DEGREE PITCH UP, STICK SHAKER ACTIVATED. WINDSHEAR FAIL STATUS MESSAGE AND CONTINUOUS IGNITION, AIRSPEED WAS ROUGHLY 165 KTS. THEN ON FINAL IN SLC, GEAR WAS COMING DOWN, WINDSHEAR FAIL MESSGE APPEARED AGAIN, CONTINUOUS IGNITION LIGHT CAME ON MOMENTARILY. NO STICK SHAKER ACTIVATION. REPLACED #2 ADSHC. GROUND FUNCTIONAL CHECK GOOD. UPDATE 7/17/02: FOUND WIRE CG51C22 SHORTING AT FLAP POSITION TRANSMITTER CANNON PLUG. REMOVED DAMAGED WIRE LENGTH AND REPLACED SOCKETS ON ALL WIRES TO CONNECTOR. FLAP OPERATION CHECKS GOOD. FAULT CODES CLEARED.