N905EV

Part: UNKNOWN — CRACKED · airframe 43,215 hrs · 39,781 cycles

RIGHT M/L/G WHEEL WELL. BRAKE PRESSURE TRANSDUCER BRACKET CRACKED. (C-CHECK RO 4/26/2023) REMOVED CRACKED AND INSTALLED NEW BRAKE PRESSURE TRANSDUCER MOUNT BRACKET IN RH MLG WHEEL WELL - REF REO 601R-53-42-007, REV A, DATE 31-JAN-2006. OPERATIONAL AND LEAK CHECKS PASSED. COMPLIED WITH TASK CARD 51-900-1003-SKY AND MAJOR REPAIR (M-337).

Part: UNKNOWN — CORRODED · airframe 43,215 hrs · 39,781 cycles

MULTIPLE SPOTS OF CORROSION NOTED ON RH FLOOR SILL FS473.15.00 TO FS499.00 (AREA MARKED) (C-CHECK RO 4/26/2023) REMOVED CORROSION ON RH FLOOR SILL BETWEEN FS473.15.00 TO FS499.00 REF CRJ200 SRM 51-21-06FOUND TO BE WITHIN LIMITS/RESTORED FINISH REF REO 601R-53-41-666, REV -C, DATED. 2012-11-06 DISPOSITION 1.2. SEE CONTINUATION CARD FOR DETAILS.COMPLIED WITH 51-900-1003-SKY. COMPLIED WITH ALL STEP OF REO 601R-53-41-666, REV -C, DATED. 2012-11-06 DISPOSTION 1.2.

Part: UNKNOWN — DENTED · airframe 43,215 hrs · 39,781 cycles

CREASED/DENT DAMAGE FOUND ON UPPER FUSELAGE SKIN 3.5" AFT OF 31.875% BETWEEN STR 4R-5R (C-CHECK RO 4/26/2023) COMPLIED WITH REPAIR ON UPPER FUSELAGE SKIN 3.5" AFT OF 31.875% BET. STR 4R-5R REF REO 601R-53-71-222 REV A DATED 2023-04-08, COMPLIED WITH SKYWEST TASKCARD 51-900-1003-SKY.

Part: UNKNOWN — CRACKED · airframe 43,215 hrs · 39,781 cycles

LEFT SIDE. FLOOR BEAM OUTBOARD CLIP AT FS 484.0 IS CRACKED. (C-CHECK RO 4/26/2023) REMOVED AND REPLACED LEFT SIDE FLOOR BEAM OUTBOARD CLIP AT FS484.0. REF. REO 601R-53-41-059 REV. -C DATED 2020-03-11.COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY (CL600-2B19) STRUCTURAL MAJOR REPAIR (**RII**)

Part: UNKNOWN — CRACKED · airframe 43,215 hrs · 39,781 cycles

RH FLOOR BEAM FS484.00 RBL 27 CLIP IS CRACKED (INBD CLIP) (C-CHECK RO 4/26/2023) REMOVED AND REPLACED FLOOR BEAM CLIP AT FS 484.0, RBL 27. REF. REO 601R-53-41-059 REV. -C DATED 2020-03-11. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY (CL600-2B19) STRUCTURAL MAJOR REPAIR (**RII**)

Part: UNKNOWN — UNKNOWN · airframe 43,215 hrs · 39,781 cycles

UPON REMOVAL ON THE RIGHT STAB TIP FOUND HOLE THE FLANGE UPPER SIDE WHERE THE NUTPLATE WAS. (C-CHECK RO 4/26/2023) REMOVED AND INSTALLED NEW SPLICE P/N 600-23037-22. REF: DWG 600-23037, REV: L, DWG 600-23026, REV: T, CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-13. COMPLIED WITH 51-900-1003-SKY. SEE CONTINUATION CARD FOR WORK PERFORMED

Part: UNKNOWN — GOUGED · airframe 43,215 hrs · 39,781 cycles

EXISTING DOUBLER AT AFT SIDE FS.280 BULKHEAD RBL12 WL93.50 IS GOUGED AND DENTED. (C-CHECK RO 4/26/2023) REMOVED AND REPLACED DOUBLER AT AFT SIDE FS.280 BULKHEAD RBL12 WL93.50 WITH NEW REF. CRJ 200 SRM 51-42-06. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKYCOMPLIED WITH ALL STEPS OF REO 601R-53-11-1524 REV.-A, DATED 10-NOV-2008

Part: UNKNOWN — PUNCTURED · airframe 43,215 hrs · 39,781 cycles

FS.280 BULKHEAD HAS A PUNCTURE AT RBL14 WL87.50. (C-CHECK RO 4/26/2023) PERFORMED DOUBLER REPAIR AT FS280 BULKHEAD AT RBL14 WL87.50 REF REO 601R-53-11-3850 REV-- DATED 2023-04-03. COMPLIED WITH TASK 51-900-1003-SKY. SEE CONTINUE CARD FOR DETAILS ON WORK PERFORMED.

Part: UNKNOWN — CORRODED · airframe 43,215 hrs · 39,781 cycles

* FUEL CELL ACCESS PANEL LANDING AT 540BB HAS CORROSION 2 PLCS, MARKED. (C-CHECK RO 4/26/2023) REMOVED CORROSION ON FUEL CELL ACCESS PANEL LANDING AT 540BB REF CRJ 200 SRM 51-21-06. FOUND TO BE WITH IN LIMITS. COMPLIED WITH ALL STEPS OF REO 601R-57-21-030 REV-L, DATED 2014-02-05 AND REO 601R-57-21-3722, REV --, DATED 2023-03-28. NO LEAKS NOTED. COMPLIED WITH 51-900-1003-SKY. SEE CONTINUATION CARD DETAILS OF WORK PERFORMED.

Part: UNKNOWN — CORRODED · airframe 43,215 hrs · 39,781 cycles

PASSENGER DOOR. FWD DOOR STAIRS HANDLE ARM CUT-OUT CORRODED ON THE FLOOR SUPPORT ANGLE. (C-CHECK RO 4/26/2023) REMOVED AND INSTALLED NEW PAX FWD CUT STAIR HANDLE ARM CUT OUT IAW CRJ 200 SRM 51-42-06 AND DWG 601R31527 REV. AM. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY.

Part: UNKNOWN — CORRODED · airframe 43,215 hrs · 39,781 cycles

FUSELAGE DOOR SURROUND ANGLE IS CORRODED. (C-CHECK RO 4/26/2023) REMOVED AND REPLACED FUSELAGE PAX DOOR ANGLE REF CRJ 200 SRM 51-42-06, SRM 51-42-13, SRM 51-42-21 AND DWG 601R31527 REV AM. REMOVED AND INSTALLED FWD AND NEW AFT HANDRAIL FITTING IAW CRJ 200 SRM 51-41-02. ADJUSTMENT OF THE PAX DOOR PS9MB PROXIMITY SENSOR ON THE FLOOR STRUCTURE CHECKS GOOD PER CRJ200 AMM 52-70-04-820-803, STEP 3F. OPS CHECK IS GOOD. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY.

Part: UNKNOWN — CORRODED · airframe 43,215 hrs · 39,781 cycles

PASSENGER DOOR. AFT DOOR STAIRS HANDLE ARM CUT-OUT CORRODED ON THE FLOOR SUPPORT ANGLE. (C-CHECK RO 4/26/2023) REMOVED AND INSTALLED NEW AFT DOOR STAIR CUP IAW CRJ 200 SRM 51-42-06 AND DWG 601R31527 REV. AM. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY.

Part: UNKNOWN — CORRODED · airframe 43,215 hrs · 39,781 cycles

R/H SIDE SEAT RAIL FROM APPROXIMATELY FS449.85 TO FS499.00 HAS NUMEROUS SPOTS OF CORROSION AND CHAFING, MARKED. (C-CHECK RO 4/26/2023) REMOVED AND REPLACED R/H SIDE SEAT RAIL FROM APPROXIMATELY FS449.85 TO FS499.00. REF. CRJ200 AMM 53-01-11-400-802

Part: UNKNOWN — CORRODED · airframe 43,215 hrs · 39,781 cycles

R/H SIDE SEAT RAIL FROM FS409.00+16 TO FS409+112 HAS NUMEROUS SPOTS OF CORROSION AND CHAFING, MARKED. (C-CHECK RO 4/26/2023) REMOVED AND REPLACED R/H SIDE SEAT RAIL FROM FS409.00+16 TO FS409+112. REF. CRJ200 AMM 53-01-11-400-802

Part: UNKNOWN — CORRODED · airframe 43,215 hrs · 39,781 cycles

RIGHT HAND FLOOR SUPPORT BEAM CAP RBL9R, HAS NUMEROUS SPOTS OF CORROSIION AND WEAR, FROM FS409.0 TO FS409.0+112. (CORROSION SPOTS MARKED WITHIN RED GREASE PENCIL). (C-CHECK RO 4/26/2023) BLENDED OUT CORROSION ON RBL 9 FLOOR BEAM CAP FROM FS 409 TO 409+112 AS MARKED REF CRJ 200 SRM 51-21-06. COMPLIED WITH ALL STEPS OF REO 601R-53-31-1273 REV -- DATED 2023-04-10. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. SEE CONTINUATION CARDS FOR DETAILS

Part: UNKNOWN — CORRODED · airframe 43,215 hrs · 39,781 cycles

R/H PRESSURE FLOOR SILL. ONE (1) SPOT OF CORRORION AT FS518.0 (C-CHECK RO 4/26/2023) REMOVED CORROSION FROM RH PRESSURE FLOOR SILL AT FS518.00 REF. CRJ 200 SRM 51-21-06. FOUND TO BE OUT OF LIMITS. PERFORMED REPAIR IAW ALL STEPS OF REO 601R-53-41-3143 REV-- DATED 2023-04-06. COMPLIED WITH TASK CARD 51-900-1003-SKY. SEE CONTINUATION CARD FOR DETAILS.

Part: UNKNOWN — CHAFED · airframe 43,215 hrs · 39,781 cycles

*R/H WING INBOARD FLAP VANE SKIN LEADING EDGE IS CHAFED AT THE INBOARD. (C-CHECK RO 4/26/2023) REMOVED DAMAGED RH IB FLAP VANE INBOARD LEADING EDGE SKIN AND INSTALLED A NEW VANE SKIN 601R14303-54 REF CRJ 200 SRM 51-42-13 AND DRAWING 601R14302 REV E. COMPLIED WITH SKYCARD 51-900-1003 STRUCTURAL MAJOR REPAIR

Part: UNKNOWN — DENTED · airframe 43,215 hrs · 39,781 cycles

*DENTS IN BOTTOM DOUBLER BELOW AND AFT OF GROUND AIR CONDITIONING CONNECTION PNL 172BR (MARKED) (C-CHECK RO 4/26/2023) REPAIRED DAMAGED AREA COMMON TO LOWER FUSELAGE SKIN APPROXIMATELY BETWEEN FS574 & FS621 AND STRG26L TO STRG20R IAW REO 601R-53-61-7991 REV -- DATED 2023-04-12. COMPLIED WITH 51-900-1003-SKY. COMPLIED WITH ALL STEPS OF REO 601R-53-61-7991 REV -- DATED 2023-04-12.SEE CONTINUATION CARD FOR DETAILS

Part: UNKNOWN — GOUGED · airframe 43,215 hrs · 39,781 cycles

*CARGO DOOR INTERIOR SURROUND AFT TRACK ASSY GOUGED/WORN OUTBOARD TRACK UPPER AND INBOARD TRACK UPPER SIDE (MARKED) (C-CHECK RO 4/26/2023) REMOVED DAMAGED AND INSTALLED NEW AFT CARGO DOOR AFT TRACK IAW CRJ200 SRM 51-42-06 REV. 39 ISSUED 03/10/21, SRM 51-42-21 REV. 39 ISSUED 03/10/21, DWG# 601R35207 REV. -W AND PREVIOUSLY INCORPERATED BOMBARDIER REO 601R-53-61-1541 REV. -F DATED 2014/11/12. COMPLIED WITH 51-900-1003-SKY. SEE CONTINUATION CARD FOR DETAILS

Part: UNKNOWN — CHAFED (UNKNOWN) · airframe 43,215 hrs · 39,781 cycles

* L/H AILERON UPPER LEADING EDGE SKIN IS CHAFED, MARKED. (C-CHECK RO 4/26/2023) BLENDED DAMAGE ON LH AILERON UPPER LEADING EDGE REF REO 601R-57-60-013, REV -A, DATED 2013-08-05.FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED WITH NEW LH AILERON UPPER LEADING EDGE SKIN REF CRJ200 SRM 51-42-06 AND 51-42-21 AND DWG:CC670-13000, REV D. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: TRANSMITTER — FAILED (TE FLAP SYSTEM) · airframe 41,853 hrs · 38,533 cycles

UNCOMMANDED FLAP EXTENSION IN FLIGHT WITH ASSOCIATED FLAPS DEGRADED STATUS MESSAGE. FLAPS EVENTUALLY STOWED AT 0 DEGREES OF EXTENSION. COMPLIED WITH FLAP TWIST QRH PROCEDURE. PERIODIC HYD 2B AND HYB 3B CAUTION MESSAGES. MESSAGES CLEARED WITH QRH PROCEDURE. (FLIGHT 5758) AFTER TROUBLE SHOOTING FOUND LH FLAP POSITION TRANSMITTER SIGNAL DRIFTING. REMOVED AND REPLACED LH FLAP POSITION TRANSMITTER IN REF TO AMM 27-55-01. OPS CHECK GOOD AT THIS TIME. AIRCRAFT OK FOR CONTINUED SERVICE. PLEASE REFERENCE AML 785039

Part: BRACKET — BROKEN (SERVICE DOOR) · airframe 39,265 hrs · 36,176 cycles

SERVICE DOOR AFT SURROUND PANEL 232EZ LOWER BRACKET IS BROKEN WHERE MARKED. (C CHECK) RO 3/7/2020 REMOVED AND REPLACED AFT LOWER BRACKET COMMON TO SERVICE DOOR SURROUND PANEL 232EZ AND FS349 FRAME, PN 601R40170-25 PO 7632-00009/155, REFERENCE CRJ200 SRM.

Part: MOUNT BRACKET — CRACKED (ZONE 100) · airframe 39,265 hrs · 36,176 cycles

RH STUB FAIRING FWD MOUNTING BRACKET CRACKED. (C CHECK) RO 3/7/2020 REMOVED AND REPLACED WITH NEW RH STUB FAIRING FWD MOUNTING BRACKET REF CRJ200 SRM.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 39,265 hrs · 36,176 cycles

BEAM CAP AT LBL9 FS409.00 TO 409.00+48 FOUND TO BE OUT OF LIMITS ON CAMP # 20320140. PERFORM A SPLICE REPAIR. (C CHECK) RO 3/7/2020 PERFORMED FLOOR BEAM CAP SPLICE REPAIR FROM FS409.00 TO 409.00+48 LBL9. REF CRJ-200 SRM, REPAIR NO. 2 AND BOMBARDIER REO. COMPLIED WITH SKYWEST TASK CARD. SEE CONTINUE CARD FOR DETAILS.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 39,265 hrs · 36,176 cycles

BEAM CAP AT LBL9 FS409.00+96 TO 409.00+112 FOUND TO BE OUT OF LIMITS ON CAMP # 20320140. PERFORM A SPLICE REPAIR. (C CHECK) RO 3/7/2020 PERFORMED FLOOR BEAM CAP SPLICE REPAIR FROM FS409.00+96 TO 409.00+112 LBL9 . REF CRJ-200 SRM REPAIR NO. 2 AND BOMBARDIER REO. COMPLIED WITH SKYWEST TASK CARD. SEE CONTINUE CARD FOR DETAILS.

Part: PLATE — CORRODED (PAX DOOR) · airframe 39,265 hrs · 36,176 cycles

PAX DOOR AFT ANCHOR FITTING SERRATED PLATE, AIRCRAFT SIDE THAT ATTACHES TO FS349 FRAME, CORRODED. (C CHECK) RO 3/7/2020 REMOVED AND REPLACED WITH NEW PAX DOOR AFT ANCHOR FITTING SERRATED PLATE, AIRCRAFT SIDE THAT ATTACHES TO FS349 FRAME, PN 600-38061-6, REFERENCE CRJ200 SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 39,265 hrs · 36,176 cycles

F.S. 280, RBL 9 O/B ANGLE CRACKED IN RADIUS AT TOP OF ANGLE. (C CHECK) RO 3/7/2020 REMOVED CRACKED ANGLE AT FS 280.0 RBL 9.0 O/B SIDE AND INSTALLED NEW ANGLE,REF BOMBARDIER REO.

Part: SKIN — GOUGED (RUDDER) · airframe 39,265 hrs · 36,176 cycles

*RUDDER HAS GOUGE ON LH SKIN BETWEEN LOWER AND MIDDLE HINGE. ( MARKED ) (C CHECK) RO 3/7/2020 CUT AWAY DAMAGE ON RUDDER LH SKIN AND INSTALLED REPAIR TO LHS RUDDER SKIN BETWEEN R.S. 85.07 AND R.S. 90.32 IN REF REO. COMPLIED WITH SKYWEST TASK CARD. SEE CONTINUE CARD FOR DETAILS.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 39,265 hrs · 36,176 cycles

F.S. 280, LBL 9 O/B ANGLE CRACKED IN RADIUS AT TOP OF ANGLE. (C CHECK) RO 3/7/2020 REMOVED CRACKED ANGLE FROM FS 280.0 LBL 9.0 AND INSTALLED NEW ANGLE,REF BOMBARDIER REO.

Part: SKIN PANEL — BROKEN (VERTICAL STAB) · airframe 39,265 hrs · 36,176 cycles

WHILE INSPECTING PANEL 326BL FOR DISBONDED TEFLON STIPS FOR JOB 2763291 OP 82 MX TRANS. 20282016 FOUND PANEL TO BE UNSERVICABLE DUE TO BROKEN OFF SECTION OF PANEL (C CHECK) RO 3/7/2020 REMOVED AND REPLACED PANEL 326BL OUTER SKIN P/N:600-21134-45 REF. SRM.

Part: SKIN — CRACKED (WING) · airframe 39,265 hrs · 36,176 cycles

COMPLY WITH SB 601R-57-037 REV E DATED 3/5/2009 ( WINGS - LOWER WING PLANK - MODIFICATION OF THE LEFT AND RIGHT WINGS IN AREA OF THE REAR SPAR AT WS148.019 ) PART'S A AND B (C CHECK) RO 3/7/2020 SERVICE BULLETIN, WINGS --- LOWER WING PLANK --- MODIFICATION OF THE LEFT AND RIGHT WINGS IN THE AREA OF THE REAR SPAR AT WS148.019, PART A, INCORPORATED.

Part: WINDOW — CRACKED (CABIN) · airframe 39,265 hrs · 36,176 cycles

R/H WINDOW #4 (4CD) IS CRACKED AND CHIPPED ON THE OUTER WINDOW PANE, FWD LEADING EDGE. REQUIRES REPLACEMENT (C CHECK) RO 3/7/2020 REMOVED AND REPLACED THE PASSENGER WINDOW #4 @ (4CD). REF CRJ200 AMM. PRESSURE CHECKS GOOD.

Part: BRACKET — CRACKED (RT WING) · airframe 39,265 hrs · 36,176 cycles

CONNECTING BRACKET/BRIDGE FOR CANOE PANEL 697AB IS CRACKED. (C CHECK) RO 3/7/2020 INSTALLED NEW CONNECTING BRACKET TO CANOE PANEL # 697AB AS REQUIRED PER REF: CRJ200 SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 39,265 hrs · 36,176 cycles

SEAT TRACK AT LBL9.00 FROM FS409.00 TO FS409.00+112HAS MULTIPLE LOCATIONS OF PITTED CORROSION (C CHECK) RO 3/7/2020 BLENDED OUT CORROSION ON SEAT TRACK LBL9.0 AT FS409.00 TO FS409.00+112. REF. CRJ200 SRM. EVALUATED BLEND AS OUT-OF-LIMITS. REMOVED SEAT TRACK, AND INSTALLED SERVICEABLE SEAT TRACK. REF. CRJ200 A.M.M.

Part: FRAME — CORRODED (FUSELAGE) · airframe 39,265 hrs · 36,176 cycles

*FRAME 513.00 HAS HEAVY CORROSION PITTING FROM APPROXIMATELY STGR 4RH €“ STGR 7RH (MARKED) (C CHECK) RO 3/7/2020 BLENDED OUT CRROSION ON FS 513 FRAME RH AT STRINGER 4R TO 7R AND FOUND ACCEPTABLE TO ENGINEERING REF REO.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 39,265 hrs · 36,176 cycles

*FWD CABIN - APPROX. FS. 333.00 RIGHT HAND STGR 1 THE FRAME IS CRACKED (MARKED) (C CHECK) RO 3/7/2020 REMOVED FS 333.00 FRAME TO FOM REF CRJ200 SRM. INSTALLED NEW FS 333.0 FRAME REF CRJ200 SRM AND DRW. PRESSURE CHECKS GOOD. SEE CONTINUATION CARD FOR DETAILS

Part: STRINGER — CORRODED (FUSELAGE) · airframe 39,265 hrs · 36,176 cycles

*BETWEEN FS333.00 AND FS349.00 / STGR. 27 REPAIR IS CORRODED. FLAGGED (C CHECK) RO 3/7/2020 NO ALLOWABLE DAMAGE ALLOWED ON REPAIR PARTS FS333.00 AND FS349.00 / STGR. 27 REPAIR REF CRJ200 SRM. REMOVED BAD REPAIR PARTS FS333.00 AND FS349.00 / STGR. 27 REF CRJ200 SRM. INSTALLED REPAIR SPLICES REF CRJ200 SRM STRINGER REPAIR PROCEDURE STEPS 14-17. AND BOMBARDIER DRW. PRESSURE LEAK CHECKS GOOD.

Part: DAMPER — CORRODED (RT ELEVATOR) · airframe 39,265 hrs · 36,176 cycles

*RH ELEV CENTER HINGE INBD FLUTTER DAMPER CORRODED HARDWARE AT ELEV ATTACH POINT (MARKED) (C CHECK) RO 3/7/2020 REMOVED AND REPLACED RH ELEVATOR INBD AND OTBD FLUTTER DAMPER CORRODED HARDWARE REF. CRJ-200 AMM. PERFORMED OPERATIONAL TEST OF THE ELEVATOR CONTROL SYSTEM REF. CRJ-200 AMM. OPS CHECKED GOOD. SEE ATTACHED CONTINUATION CARD FOR WORK PERFORMED

Part: CLEAT — CRACKED (FUSELAGE) · airframe 39,265 hrs · 36,176 cycles

*FWD CABIN - FS. 280 BULKHEAD LEFT HAND STGR 3 - STRINGER TO FRAME CLEAT HAS SIGNS OF A CRACK (MARKED). (C CHECK) RO 3/7/2020 REMOVED AND REPLACED CRACKED CLEAT AT FS. 280 BULKHEAD LEFT HAND STGR 3 WITH NEW REF. CRJ 200 SRM AND BOMBARDIER DWG.

Part: GUIDE — BROKEN (E&E DOOR) · airframe 39,265 hrs · 36,176 cycles

*ALL 4 OF THE AVIONICS BAY DOOR GUIDES ON THE SURROUND (2EA FWD AND 2EA AFT) ARE BROKEN (MARKED) (C CHECK) RO 3/7/2020 REMOVED AND INSTALLED ALL FOUR (2EA. FWD AND 2EA. AFT) NEW AVIONICS BAY DOOR GUIDES REF BOMBARDIER CRJ-200 CMM. SEE CONTINUATION CARD FOR DETAILS..

Part: ATTACH FITTING — CRACKED (COCKPIT) · airframe 39,265 hrs · 36,176 cycles

WINDSHIELD CENTER POST LOWER LH & RH ATTACH FITTINGS CRACKED IN RADIUS. MARKED IN RED. (C CHECK) RO 3/7/2020 REMOVED CRACKED ATTACH FITTINGS AND INSTALLED NEW ATTACH FITTINGS 2EA. IN THE WINDSHIELD CENTER POST REF BOMBARDIER DWG AND CRJ 200 SRM. SEE CONTINUATION CARD FOR DETAILS.

Part: SUPPORT — DAMAGED (FUSELAGE) · airframe 39,265 hrs · 36,176 cycles

ANGLE SUPPORT AT FS349.00 COMMON TO CROSSBEAM FRAME SUPPORT BETWEEN LBL 27 AND L/H FLOOR SILL IS EXFOLIATED. (C CHECK) RO 3/7/2020 REMOVED AND REPLACED ANGLE SUPPORT LOCATED BETWEEN LBL27 AND LH FLOOR SILL ON FS349 CROSSBEAM, REFERENCE CRJ200 SRM AND BOMBARDIER DRAWING.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 39,265 hrs · 36,176 cycles

*PRESSURE FLOOR BEAM CHANNEL CORROSION FS409.00+128 €“ 559.00 RBL 9(L) (MARKED) (C CHECK) RO 3/7/2020 REMOVED CORROSION FROM PRESSURE FLOOR BEAM CHANNEL BETWEEN FS409.00+128 AND FS559.00 RBL9 REF CRJ 200 SRM. EVALUATED AND FOUND TO BE OUT OF LIMITS, REF BOMBARDIER DWG AND BOMBARDIER REO. REMOVED AND REPLACED RH FLOOR BEAM CAP AT RBL9 FROM FS 409.00+128 TO FS 559.00 REF BOMBARDIER REO. SEE CONTINUATION CARD FOR DETAILS.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 39,265 hrs · 36,176 cycles

*LH PRESSURE FLOOR SILL HAS CORROSION FROM FS409.00+128 TO FS559.00 (MARKED) (C CHECK) RO 3/7/2020 REPAIRED LH FLOOR PRESSURE SILL. ALL STEPS COMPLIED WITH. SEE CONTINUATION CARD FOR DETAILS. NO WEIGHT CHANGE AS THESE WERE MINIMAL BLENDS. PRESSURE CHECKS GOOD.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 39,265 hrs · 36,176 cycles

*RH PRESSURE FLOOR SILL HAS CORROSION FROM FS409.00+128 TO FS559.00 (MARKED). (C CHECK) RO 3/7/2020 REPAIRED RH FLOOR PRESSURE SILL REF REO. ALL STEPS COMPLIED WITH. SEE CONTINUATION CARD FOR DETAILS. NO WEIGHT CHANGE AS THESE WERE MINIMAL BLENDS.

Part: ANGLE — DAMAGED (FUSELAGE) · airframe 39,265 hrs · 36,176 cycles

F.S 409.0+128 BL 0.0 RH AFT VERTICAL POST RADIUS DEFECT NOTED. (C CHECK) RO 3/7/2020 REMOVED AND INSTALLED NEW LH AND RH ANGLE AT FS 409+128 BL 0 VERTICAL POST. REF CRJ-200 SRM, BOMBARDIER REO AND BOMBARDIER DWG. COMPLIED WITH SKYWEST TASK CARD. ALL ASSOCIATED CHECKS GOOD. SEE CONTINUE CARD FOR DETAILS.

Part: FRAME — CORRODED (FUSELAGE) · airframe 39,265 hrs · 36,176 cycles

*FS605.00 FRAME IS CORRODED FROM LH STGR25 TO RH STGR24. FAGGED & CIRCLED WITH GREASE PENCIL. (C CHECK) RO 3/7/2020 BLENDED OUT CORROSION ON FS 605 LOWER FRAME AS MARKED BETWEEN STRINGER 25L TO 24R REF CRJ 200 SRM. ORIGINAL THICKNESS OF FS 605 LOWER FRAME SECTOR IS .050", AMOUNT REMAINING IS .045" REF NDT, MAX ALLOWABLE IS 10% OR .005" AND WITHIN LIMITS FOR MATERIAL LOSS, HOWEVER CORROSION WAS FOUND ON TWO ELEMENTS AND JUST OVER 30% LENGTH OF FRAME THEREFORE OUT OF LIMITS REF CRJ 200 SRM. RECEIVED AND COMPLIED WITH BOMBARDIER REO. PRESSURE LEAK CHECKS GOOD. SEE CONTINUATION CARD FOR DETAILS

Part: ANGLE — CORRODED (FUSELAGE) · airframe 39,265 hrs · 36,176 cycles

*AFT PRESSURE BULKHEAD (FS621) LOWER FLOOR ANGLE IS CHAFED AND CORRODED AROUND SCREW HOLES FROM LH TO RH MARKED WITH GREASE PENCIL & FLAGGED (C CHECK) RO 3/7/2020 REMOVED CORROSION AND CHAFFING ON AFT PRESSURE BULKHEAD (FS621.00) LOWER FLANGE ANGLE REF CRJ200 SRM. FOUND TO BE OUT OF LIMITS. RECEIVED REO. COMPLIED WITH ALL STEPS OF REO. SEE CONTINUE CARD FOR DETAILS.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 39,265 hrs · 36,176 cycles

*RH PRESSURE FLOOR SILL ANGLE HAS CORROSION FROM FS409.00+128 TO FS559.00 (MARKED) (C CHECK) RO 3/7/2020 REPAIRED RH FLOOR PRESSURE SILL ANGLE REF REO. ALL STEPS COMPLIED WITH. SEE CONTINUATION CARD FOR DETAILS. WEIGHT CHANGE NEGLIGIBLE DUE TO BLENDS ONLY PERFORMED.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 39,265 hrs · 36,176 cycles

* LBL 9.0 AT FS 559.0 TO FS 559.0+80 UPPER CAP HAS AREAS OF CORROSION. (C CHECK) RO 3/7/2020 BLENDED CORROSION FROM FLOOR SUPPORT BEAM CAP AT FS559.00 - FS559.00+80 REF CRJ 200 SRM. ELAUATED AND FOUNF TO BE OUT OF LIMITS. PERFORMED SPLICE REPAIR ON FLOOR SUPPORT BEAM CAP AT FS559.00 - FS559.00+80 REF CRJ 200 SRM. REPAIR #2 AND BOMBARDIER REO. SEE CONTINUATION CARD FOR DETAILS.

Part: STRAP — CORRODED (FUSELAGE) · airframe 39,265 hrs · 36,176 cycles

*PRESSURE FLOOR BEAM STRAP CORROSION FS424.00 RBL 0 €“ RBL 9 (MARKED) (C CHECK) RO 3/7/2020 REMOVED CORROSION FROM PRESSURE FLOOR BEAM STRAP AT FS424.00 RBL 0 -RBL 9 REF CRJ 200 SRM. EVALUATED AND FOUND TO BE OUT OF LIMITS, REMOVED AND INSTALLED NEW FLOOR BEAM STRAP REF BOMBARDIER AND CRJ 200 SRM. SEE CONTINUATION CARD FOR DETAILS.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 39,265 hrs · 36,176 cycles

*PRESSURE FLOOR BEAM CHANNEL CORROSION FS409.00+128 €“ 559.00 LBL 9(R) (MARKED) (C CHECK) RO 3/7/2020 REMOVED CORROSION ON PRESSURE FLOOR BEAM CHANNEL FS409.00+128 THRU FS559.00 LBL 9(R). REF. CRJ200 SRM. ORIGINAL MATERIAL THICKNESS IN AREA IS .050" REF. DWG, REMAINING MATERIAL THICKNESS IN AREA IS .028" REF. NDT REPORT, MATERIAL LOSS IN AREA IS .022". AREA AT FLOOR BEAM FS 409.00+128 - 559.00 LBL 9(R) IS OUT OF LIMITS OF ALLOWABLE DAMAGE LIMITS OF 10 PERCENT REF. CRJ-200 SRM. COMPLETED PRESSURE FLOOR BEAM CHANNEL REPAIR REF BOMBARDIER REO. SEE CONTINUATION CARD FOR DETAILS.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 39,265 hrs · 36,176 cycles

*THE WARDROBE FLOOR SUPPORT FITTIING HAS CORROSION BETWEEN FS295.00 AND FS310.00 BETWEEN LBL27.00 AND LBL9.00. (MARKED) (C CHECK) RO 3/7/2020 REMOVED AND REPLACED THE WARDROBE FLOOR SUPPORT FITTIING PLATE BETWEEN FS295.00 AND FS310.00 BETWEEN LBL27.00 AND LBL9.00. REF: CRJ-200 SRM AND BOMBARDIER DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 39,265 hrs · 36,176 cycles

*THE SEAT TRACK AT LBL9.00 FROM FS364.00 TO FS394.00 HAS MULTIPLE LOCATIONS OF PITTED CORROSION. (MARKED) (C CHECK) RO 3/7/2020 BLENDED SEAT TRACK CORROSION AT LBL9.0 FROM FS364.00 TO FS394.00. EVALUATED AS OUT-OF-LIMITS. REPLACED SEAT TRACK WITH NEW SEAT TRACK. REF. CRJ200 A.M.M.

Part: STRAP — CORRODED (FUSELAGE) · airframe 39,265 hrs · 36,176 cycles

*PRESSURE FLOOR BEAM STRAP CORROSION FS559.00 RBL 27 AND OUTBD (MARKED) (C CHECK) RO 3/7/2020 REMOVED CORROSION FROM PRESSURE FLOOR BEAM STRAP FS559.00 RBL 27 AND OUTBD. IAW CRJ 200 SRM. STRAP ORIGINAL MATERIAL THICKNESS =.050 IN., MATERIAL LEFT AFTER BLENDING = .030 IN., MATERIAL TAKEN = .020 IN., MAX ALLOWABLE DAMAGE 10% OF THICKNESS = .005 IN. PER REF: CRJ200 SRM STRAP IS FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED PRESSURE FLOOR BEAM STRAP REF CRJ200 SRM AND BOMBARDIER DWG PRESSURE LEAK CHECKS GOOD.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,265 hrs · 36,176 cycles

*FLOORBEAM UPPER CAP LONGITUDIAL BL9 LH FS409.00 TRU FS409.0+128 HAS MULTIBLE AREAS OF CORROSION. MARKED (C CHECK) RO 3/7/2020 BLENDED CORROSION ON FLOORBEAM UPPER CAP BL9 LH AT FS409.0 - FS409.0+128 REF CRJ 200 SRM EVALUATED AND FOUND TO BE OUT OF LIMITS IN THE FWD AND AFT CRITICAL AREAS, REF BOMBARDIER REO. SPLICE REPAIRS COMPLETED ON CAMP#'S 20508542, 20508554 TO CAPTURE RII MAJOR REPAIR SKY CARD. SEE CONTINUATION CARD FOR DETAILS

Part: STRAP — CORRODED (FUSELAGE) · airframe 39,265 hrs · 36,176 cycles

*PRESSURE FLOOR BEAM STRAP CORROSION FS424.00 RBL 27 AND OUTBD (MARKED) (C CHECK) RO 3/7/2020 REMOVED CORROSION FROM PRESSURE FLOOR BEAM STRAP FS424.00 RBL27 AND OUTBD. CRJ200 SRM. STRAP ORIGINAL MATERIAL THICKNESS = 0.050", MATERIAL LEFT AFTER BLENDING = 0.044", MATERIAL LOSS = 0.006" MAX ALLOWABLE LOSS IS 10% OR THICKNESS OR 0.005" REF: CRJ200 SRM, FOUND STRAP TO BE OUT OF LIMITS. REPLACED FLOOR BEAM STRAP, REF CRJ200 SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 39,265 hrs · 36,176 cycles

*LH SEAT FLOOR TRACK (LBL 9), CORROSION AROUND NUMEROUS FASTENERS FS409.00+128 €“ 559.00 (MARKED) (C CHECK) RO 3/7/2020 REMOVED CORROSION ON RH SEAT TRACK LBL 9 BETWEEN FS409.00+12 TO FS559.00 REF CRJ 200 SRM. EVALUATED AND FOUND TO BE OUT OF LIMITS REF BOMBARDIER STANDARDS MANUAL AND CRJ 200 SRM. REMOVED AND INSTALLED NEW LH SEAT TRACK LBL 9 BETWEEN FS409.00+12 TO FS559.00 REF CRJ 200 AMM. SEE CONTINUATION CARD FOR DETAILS.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 39,265 hrs · 36,176 cycles

* THE RH FLOOR SILL AT FS 319.00 HAS CORROSION. (MARKED) (C CHECK) RO 3/7/2020 REMOVED CORROSION TO THE R/H FLOOR SILL AT FS 319.00 PER REF: CRJ200 SRM. GALLEY SUPPORT ANGLE ORIGINAL THICKNESS IS .090", AMOUNT REMAINING IS .087" REF NDT, REMOVED .003" AND MAX ALLOWABLE IS .009" AND THEREFORE THE ANGLE/ DOUBLER IS IN LIMITS OF CRJ 200 SRM 53-00-00. ORIGINAL THICKNESS OF THE RH FLOOR SILL IS .063" AMOUNT REMAINING IS .027" REF NDT, REMOVED .036" AND MAX ALLOWABLE IS .0063" THEREFORE THE SILL IS OUT OF LIMITS REF CRJ 200 SRM. REMOVED AND REPLACED THE SILL IAW CRJ 200 SRM. PRESSURE LEAK CHECKS GOOD.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 39,265 hrs · 36,176 cycles

*RH SEAT FLOOR TRACK (RBL 9), CORROSION AROUND NUMEROUS FASTENERS FS409.00+128 €“ 559.00 (MARKED (C CHECK) RO 3/7/2020 REMOVED CORROSION ON RH SEAT TRACK RBL 9 BETWEEN FS409.00+12 TO FS559.00 REF CRJ 200 SRM. EVALUATED AND FOUND TO BE OUT OF LIMITS REF CRJ 200 SRM. REMOVED AND INSTALLED NEW RH SEAT TRACK RBL 9 BETWEEN FS409.00+12 TO FS559.00 REF CRJ 200 AMM AND CRJ 200 SRM. SEE CONTINUATION CARD FOR DETAILS.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 39,265 hrs · 36,176 cycles

* THE FLOOR SUPPORT CROSSBEAM AT FS349.00 AT THE LH FLOOR SILL HAS CORROSION. (MARKED) (C CHECK) RO 3/7/2020 REMOVED CORROSION FROM FLOOR SUPPORT CROSSBEAM REF CRJ 200 SRM. EVALUATED AND FOUND TO BE OUT OF LIMITS. FFLOOR SUPPORT CROSSBEAM AT FS349.00 AT THE LH FLOOR SILL IS STRUCTURALLY ACCEPTABLE REF BOMBARDIER REO. ALL STEPS OF BOMBARDIER REO HAVE BEEN COMPLIED WITH.

Part: STRAP — CORRODED (FUSELAGE) · airframe 39,265 hrs · 36,176 cycles

*PRESSURE FLOOR BEAM STRAP CORROSION FS559.00 LBL 27 AND OUTBD (MARKED) (C CHECK) RO 3/7/2020 REMOVED AND INSTALLED NEW PRESSURE FLOOR BEAM STRAP AT FS 559.00 & LBL 27.00. REF. BOMBARDIER CRJ200 SRM AND DWG. PRESSURE LEAK CHECKS GOOD.

Part: STRAP — CORRODED (FUSELAGE) · airframe 39,265 hrs · 36,176 cycles

*PRESSURE FLOOR BEAM STRAP CORROSION FS424.00 LBL 0 €“ LBL 9 (MARKED) (C CHECK) RO 3/7/2020 REMOVED AND REPLACED PRESSURE FLOOR BEAM STRAP FS424.00 LBL 0 €“ LBL 9. REF: CRJ-200 AND BOMBARDIER. SEE CONTINUATION CARD FOR DETAILS.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 39,265 hrs · 36,176 cycles

*THE WARDROBE FLOOR SUPPORT FITTING HAS CORROSION BETWEEN FS295.00 AND FS310.00 BETWEEN LBL27.00 AND THE LH FLOOR SILL. (MARKED) (C CHECK) RO 3/7/2020 REMOVED AND REPLACED THE WARDROBE FLOOR SUPPORT FITTIING PLATE BETWEEN FS295.00 AND FS310.00 BETWEEN LBL27.00 AND LH FLOOR SILL. REF: CRJ-200 SRM AND BOMBARDIER DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 39,265 hrs · 36,176 cycles

* RBL 9.0 FS 559.0 TO FS 559.0+80 UPPER CAP FLOOR SUPPORT HAS AREAS OF CORROSION.(MARKED) (C CHECK) RO 3/7/2020 REMOVED CORROSION FORM RBL 9.0 FS559.0+80 UPPER FLOOR CAP. NDTD FOR THICKNESS, AND EVALUATED AS OUT-OF-LIMITS. INSTALLED NEW UPPER FLOOR SUPPORT CAP. REF. BOMBARDIER REO. COMPLIED WITH TASK CARD.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 39,265 hrs · 36,176 cycles

*BETWEEN FS364.00 AND FS349.00 THE LH INTER-COSTAL IS CORRODED (C CHECK) RO 3/7/2020 LH INTER-COSTAL BETWEEN FS364.00 AND FS349.00 HAS CORROSION ON MORE THAN 2 ELEMENTS AND OVER FASTENER HOLES. INTERCOSTAL IS OUT OF LIMITS REF CRJ200 SRM. REMOVED INTERCOSTAL LH STGR 27 FS349 TO FS364 REF CRJ200 SRM. INSTALLED NEW INTERCOSTAL REF CRJ200 SRM AND REF DRW. PRESSURE LEAK CHECKS GOOD.

Part: ANCHOR FITTING — CRACKED (PAX DOOR) · airframe 39,265 hrs · 36,176 cycles

*PAX DOOR AFT ANCHOR IS CRACKED. FLAGGED (C CHECK) RO 3/7/2020 ORDERED AND RECEIVED NEW SERVICEABLE PAX DOOR AFT ANCHOR FITTING P/N 601R38074-7 QTY.1 AND HAS BEEN INSTALLED WITH NEW ATTACHING HARDWARE REF CRJ 200 AMM AND CRJ 200 SRM. PAX DOOR COUNTER BALANCE ADJUSTMENT CHECK IS GOOD.

Part: RIB — CRACKED (RT WING) · airframe 39,265 hrs · 36,176 cycles

*RH WING BATT RIB AT APPROXIMATELY WS48.00 IN GEAR WELL AREA IS CRACKED (MARKED) (C CHECK) RO 3/7/2020 REMOVED AND REPLACED RH WING BATT RIB AT APPOXIMATELY WS48.00 IN GEAR WELL AREA. REF: CRJ200 SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,265 hrs · 36,176 cycles

*THE EXTERNAL FUSELAGE ON THE LOWER RH SIDE JUST AFT OF AFT NOSE LANDING GEAR DOOR IS CRACKED. (MARKED). (C CHECK) RO 3/7/2020 REPAIRED THE EXTERNAL FUSELAGE ON THE LOWER RH SIDE JUST AFT OF AFT NOSE LANDING GEAR DOOR. REF BOMBARDIER REO. PRESSURE CHECKS AND OPS CHECKS GOOD. SEE CONTINUATION CARD FOR DETAILS.

Part: PLATE — CORRODED (PAX DOOR) · airframe 39,265 hrs · 36,176 cycles

*PAX DOOR FWD ANCHOR SERATED PLATE IS CORRODED (C CHECK) RO 3/7/2020 REMOVED AND REPLACED PAX DOOR FWD ANCHOR FITTING SERRATED PLATE, REF CRJ200 SRM AND CRJ200 AMM. PAX DOOR COUNTER BALANCE ADJUSTMENT CHECK IS GOOD.

Part: RIB — CRACKED (LT WING) · airframe 39,265 hrs · 36,176 cycles

*LH WING BATT RIB AT APPOXIMATELY WS48.00 IN GEAR WELL AREA IS CRACKED (MARKED) (C CHECK) RO 3/7/2020 REMOVED AND REPLACED LH WING BATT RIB AT APPOXIMATELY WS48.00 IN GEAR WELL AREA. REF: CRJ200 SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 39,265 hrs · 36,176 cycles

* THE INTERCOSTAL ADJACENT TO STRINGER 14R, THAT SPANS BETWEEN FS 621 AND FS 625, IS CRACKED. (C CHECK) RO 3/7/2020 REMOVED AND REPLACED CLIP P/N: 601-35012-52 BETWEEN FS 621 AND FS 625, STRINGER 14R REF. CRJ-200 SRM AND BOMBARDIER. COMPLIED WITH SKYWEST TASK CARD.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 39,265 hrs · 36,176 cycles

* THE INTERCOSTAL BETWEEN FS 621 AND FS 625, AT STRINGER LOCATION 14L, HAS A SUSPECTED CRACK ON ITS OUTBOARD FLANGE THAT ATTACHES TO THE FUSELAGE SKIN. (C CHECK) RO 3/7/2020 VERIFIED THE CRACK. REMOVED THE CRACKED INTERCOSTAL / BRACKET AT STRINGER 14L BETWEEN FS 621 AND 625 REF CRJ 200 SRM. INSTALLED A NEW INTERCOSTAL/ BRACKET AT STRINGER 14 L BETWEEN FS 621 AND FS 625 REF CRJ 200 SRM. PRESSURE LEAK CHECKS GOOD. REFERENCE THE CONTINUE CARD FOR DETAILS.

Part: FASTENER — CORRODED (LT SPOILER) · airframe 39,265 hrs · 36,176 cycles

*LH INBD GROUND SPOILER CORROSION ON BOTH HINGE ATTACH HARDWARE (C CHECK) RO 3/7/2020 REPLACED LH INBD GROUND SPOILER BOTH HINGE ATTACHING HARDWARE REF CRJ200 AMM. OPS CHECK GOOD.

Part: ATTACH ANGLE — CHAFED (VERTICAL STAB) · airframe 39,265 hrs · 36,176 cycles

*THE VERITCAL STABILIZER LEADING EDGE PANEL LOWER FAIRING SUPPORT RIB'S RH UPPER ATTACH ANGLE IS CHAFED. (C CHECK) RO 3/7/2020 REMOVED AND INSTALLED A NEW ANGLE, ON THE VERTICAL STABILIZER LEADING EDGE, THE LOWER FAIRING SUPPORT RIB R-H UPPER ATTACH ANGLE REF. CRJ200 SRM.

Part: ATTACH ANGLE — CHAFED (VERTICAL STAB) · airframe 39,265 hrs · 36,176 cycles

*THE VERITCAL STABILIZER LEADING EDGE PANEL LOWER FAIRING SUPPORT RIB'S LH UPPER ATTACH ANGLE IS CHAFED. (C CHECK) RO 3/7/2020 REMOVED AND INSTALLED A NEW ANGLE, ON THE VERTICAL STABILIZER LEADING EDGE, THE LOWER FAIRING SUPPORT RIB L-H UPPER ATTACH ANGLE REF. CRJ200 SRM.

Part: FASTENER — CORRODED (RT SPOILER) · airframe 39,265 hrs · 36,176 cycles

*RH OUTBD GROUND SPOILER, CORROSION ON BOTH HINGE ATTACH HARDWARE (C CHECK) RO 3/7/2020 REPLACED RH OUTBD GROUND SPOILER BOTH HINGE ATTACHING HARDWARE REF CRJ200 AMM. OPS CHECK GOOD.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,265 hrs · 36,176 cycles

*FRAME BELOW THE LEFT WINDSHIELD SIDE POST SUPPORT IS CRACKED. (C CHECK) RO 3/7/2020 REMOVED FRAME BELOW LEFT WINDSHIELD SIDE POST SUPPORT REF CRJ 200 SRM. INSTALLED NEW FRAME BELOW LEFT WINDSHIELD SIDE POST SUPPORT WITH NEW REF CRJ 200 SRM. PRESSURE LEAK CHECKS GOOD, OPERATIONAL CHECKS GOOD. REFERENCE THE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 39,265 hrs · 36,176 cycles

* THE INTERCOSTAL ADJACENT TO STRINGER 14L, THAT SPANS BETWEEN FS 621 AND FS 625, IS CRACKED. (C CHECK) RO 3/7/2020 REMOVED AND REPLACED CLIP P/N: 601-35012-51 BETWEEN FS 621 AND FS 625, STRINGER 14L REF. CRJ-200 SRM AND BOMBARDIER. COMPLIED WITH SKYWEST TASK CARD.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 39,265 hrs · 36,176 cycles

* THE INTERCOSTAL BETWEEN FS 621 AND FS 625, AT STRINGER LOCATION 15R, HAS A SUSPECTED CRACK ON ITS OUTBOARD FLANGE THAT ATTACHES TO THE FUSELAGE SKIN. (C CHECK) RO 3/7/2020 REMOVED CRACKED INTERCOSTAL CLIP REF. CRJ200 SRM. LOCATED AND DRILLED FULL SIZE ALL HOLES COMMON TO REPLACEMENT CLIP REF. CRJ200 SRM AND INSTALLED REPLACEMENT CLIP REF CRJ200 SRM.

Part: FASTENER — CORRODED (LT SPOILERON) · airframe 39,265 hrs · 36,176 cycles

*LH SPOILERON, CORROSION ON THE INBD HINGE ATTACH HARDWARE (C CHECK) RO 3/7/2020 REPLACED LH SPOILERON INBD HINGE ATTACHING HARDWARE REF CRJ200 AMM. CHECKS GOOD.

Part: BRACKET — CHAFED (PAX DOOR) · airframe 39,265 hrs · 36,176 cycles

*PASSENGER DOOR UPPER AFT ROLLER BRACKET ON SURROUND, CHAFFED (MARKED) (C CHECK) RO 3/7/2020 REMOVED AND REPLACED PAX DOOR UPPER AFT ROLLER BRACKET ON DOOR SURROUND, PN 600-31471-9 PO T-51948, REFERENCE CRJ200 SRM.

Part: LATCH — BROKEN (AC DOOR) · airframe 39,265 hrs · 36,176 cycles

*GROUND A/C DOOR 172BR AFT LATCH BULLNOSE BROKEN (MARKED) (C CHECK) RO 3/7/2020 REMOVED AND INSTALLED NEW LATCH AND RIVETS IN PANEL 172BR, AFT GROUND A/C DOOR, REF CRJ200, SRM.

Part: MOUNT BRACKET — CRACKED (PAX DOOR) · airframe 39,265 hrs · 36,176 cycles

*PAX DOOR ASSIST MOTOR MOUNT BRACKET IS CRACKED. (C CHECK) RO 3/7/2020 REMOVED DISCREPANT CRACKED MOTOR MOUNT BRACKET REF. CRJ200 SRM. LOCATED AND DRILLED FULL SIZE ALL HOLES COMMON TO REPLACEMENT PAX DOOR MOTOR MOUNT BRACKET, REF. CRJ200 SRM. INSTALLED REPLACEMENT MOTOR MOUNT BRACKET REF. CRJ200 SRM. RESTORED FINISH REF. CRJ200 SRM AND APPLIED CORROSION INHIBITING COMPOUND REF. CRJ200 SRM.

Part: NUT PLATE — CORRODED (EMERGENCY EXIT) · airframe 39,265 hrs · 36,176 cycles

*NUT PLATES ATTACHING HINGE FITTINGS IN BOTTOM OF R/H EMERGANCY-EXIT HAVE CORROSION. (C CHECK) RO 3/7/2020 REMOVED ATTACHING HINGE IN ORDER TO REMOVE NUTPLATES, REMOVED CORRODIED NUTPLATES AND RIVETS, INSTALLED NEW NUTPLATES AND RIVETS, INSTALLED ATTACHING HINGE, REF CRJ 200 AMM AND SRM. ADJUSTMENT, FITS AND CLEARANCES ARE GOOD.

Part: GUIDE — CHAFED (TE FLAP) · airframe 39,265 hrs · 36,176 cycles

CHAFFING ON THE GUIDES ON RIGHT HAND WING FLAP HINGE FAIRING 692BB. (C CHECK) RO 3/7/2020 REMOVED AND REPLACED GUIDES ON RIGHT HAND WING FLAP HINGE FAIRING 692BB REF CRJ-200 SRM.

Part: PANEL — CHAFED (RT AILERON) · airframe 39,265 hrs · 36,176 cycles

CHAFFING ON THE RIGHT HAND WING AILERON PANEL 699BB. (C CHECK) RO 3/7/2020 ORDERED AND RECIEVED NEW RH AILERON PANEL 699BB. DRILLED AND COUNTERSUNK FASTENER HOLES ON NEW PANEL REF SRM.

Part: SKIN — DENTED (FUSELAGE) · airframe 39,265 hrs · 36,176 cycles

ADM#3845 - DENT FOUND ON RH SIDE OF FUSELAGE SKIN PANEL APPROXIMATELY FS 275.8 BETWEEN STGR 22R AND 23R. (C CHECK) RO 3/7/2020 HAND DRESSED TO REFORM TO ORIGINAL CONTOUR TO DISCREPANT SKIN, ENSURED NO OIL CANNING OCCURRED POST REWORK COMPLIED WITH REO. SEE CONTINUATION FOR DETAILS.

Part: SKIN — DENTED (RT WING) · airframe 39,265 hrs · 36,176 cycles

ADM#3861 - R/H WING TRAILING EDGE WS 220.00 HAS 6 DENTS ON UPPER SKIN. (MARKED (C CHECK) RO 3/7/2020 DENT AT APPROXIMATELY WS219.40 MEASURES .560" LONG BY .463" AND .004" DEEP WITH A W/D RATIO OF 115. DENT AT APPROXIMATELY WS221.80 MEASURES .450 LONG BY .443" AND .003" DEEP WITH A W/D RATIO OF 147. REPAIRED REF BOMBARDIER REO.

Part: SKIN — DENTED (RT SPOILER) · airframe 39,265 hrs · 36,176 cycles

ADM#3863 - TOTAL OF 9 DENTS WERE FOUND ON THE R/H FLIGHT SPOILER UPPER SKIN(MARKED) (C CHECK) RO 3/7/2020 REMOVED AND INSTALLED NEW RH FLIGHT SPOILER REF. CRJ200 AMM RIG AND OP CHECKS GOOD.

Part: SKIN — DENTED (LT WING) · airframe 39,265 hrs · 36,176 cycles

ADM#3858 - L/H WING TRAILING EDGE WS 220.00 HAS 11 DENTS ON THE UPPER SKIN. (MARKED) (C CHECK) RO 3/7/2020 REMOVED AND REPLACED L/H WING TRAILING EDGE PANEL P/N 601R10226+5 PER REF: DWG, AD AND CRJ200 SRM. SEE CONTINUATION FOR DETAILS

Part: SKIN — DENTED (RT SPOILER) · airframe 39,265 hrs · 36,176 cycles

ADM#3864 - TWO DENTS WERE FOUND ON THE R/H INBOARD GROUND SPOILER UPPER SKIN.(MARKED) (C CHECK) RO 3/7/2020 REMOVED AND INSTALLED NEW RH IB GROUND SPOILER REF. CRJ200 AMM. RIG AND OP CHECKS GOOD.

Part: SKIN — DENTED (LT SPOILER) · airframe 39,265 hrs · 36,176 cycles

ADM#3866 - TOTAL OF 11 DENTS WERE FOUND ON THE L/H FLIGHT SPOILER. (MARKED) (C CHECK) RO 3/7/2020 REMOVED AND INSTALLED NEW LH FLIGHT SPOILER REF. CRJ200 AMM. RIG AND OP CHECKS GOOD.

Part: SKIN — DENTED (LT SPOILER) · airframe 39,265 hrs · 36,176 cycles

ADM#3862 - L/H OUTBOARD GROUND SPOILER UPPER SKIN HAS 9 DENTS. (MARKED) (C CHECK) RO 3/7/2020 REMOVED AND REPLACED LH OTBD GROUND SPOILER WITH NEW HARDWARE REF CRJ 200 AMM. BLEED HYDRAULICS CHECK GOOD, CLEARANCE, RIGGING AND OPS CHECK ARE GOOD.

Part: ANGLE — WEAK (FUSELAGE) · airframe 39,265 hrs · 36,176 cycles

COMPLY WITH REO REPAIR & REINFORCEMENT FOR FS 559.00 LWR CAP ANGLES BL 9.00 & 18.00 LHS & RHS (C CHECK) RO 3/7/2020 COMPLIED WITH REO REPAIR & REINFORCEMENT FOR FS 559.00 LWR CAP ANGLES BL 9.00 & 18.00 LHS & RHS. SEE CONTINUATION CARD FOR DETAILS.

Part: SKIN — DENTED (FUSELAGE) · airframe 36,907 hrs · 34,108 cycles

FUSELAGE SKIN HAS A DENT WITH A CREASE APPROX 1.5 INCHES LONG AT FS 610 BETWEEN STRINGERS 20L AND 19L. REPAIRED DENT IN FUSELAGE SKIN AT FS 610 IAW REO'S 601R-51-00-309, 601R-53-61-6702 AND EC/TC'S REO 601R-51-00-309 AND REO 601R-53-61-6702.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 36,907 hrs · 34,108 cycles

EVALUATE OR REPAIR RT 9G BULKHEAD AFT SIDE DAMAGE AT INSERT / RIVNUT LOCATIONS. C/W ECTC EO CL-600-2B19-53-L05837.

Part: SKIN — DENTED (TE FLAP) · airframe 36,907 hrs · 34,108 cycles

SEVERAL DENT FOUND ON THE LT OUTBOARD FLAP UPPER SKIN. PERFORMED A MAJOR REPAIR TO LT OUTBOARD FLAP UPPER SKIN IAW EC/TC SNIEO 601R14535 S02.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 36,907 hrs · 34,108 cycles

EVALUATE OR REPAIR CENTER 9G BULKHEAD AFT SIDE DAMAGE AT INSERT/RIVNUT LOCATIONS. C/W ECTC EO CL-600-2B19-53-L05836.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 36,907 hrs · 34,108 cycles

COMPLY WITH REO 601R-53-61-1240REV D DATED 10-31-16 AT FS 621 AFT PRESSURE BULKHEAD DUE TO CRACKS AT RBL9.5, BL 0.0 (2LOCATIONS), LBL 9.5 AND LBL 18. REPAIRED AFT PRESSURE BULKHEAD IAW EC/TC REO 601R-53-61-1240 REV E AND REO 601R-53-1240 REV D DATED 10-31-16.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 36,907 hrs · 34,108 cycles

INDICATION NOTED AT FS621 REAR PRESSURE BULKHEAD FWD FACE AT LBL 18.0 WL75.7-WL77.1 1.4" LONG AND 80% FSH FAILING NDT. COMPLIED WITH ECTC REO 601R-53-61-6705.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 36,907 hrs · 34,108 cycles

INDICATION NOTED AT FS621 REAR PRESSURE BULKHEAD FWD FACE AT RBL 9.5 WL78.6-WL79.8 1.2" LONG AND 100% FSH FAILING NDT. COMPLIED WITH ECTC REO 601R-53-61-6705.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 36,907 hrs · 34,108 cycles

LEFT HAND FLOORBEAM LBL 27 UPPER O/B FLANGE IS CORRODED AROUND MULTIPLE FASTENER HOLES BETWEEN FS 559+110 TO FS 559+118. COMPLIED WITH ECTC REO 601R-53-51-353.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 36,907 hrs · 34,108 cycles

LEFT HAND FLOORBEAM LBL 27 UPPER O/B FLANGE IS CORRODED AROUND MULTIPLE FASTENER HOLES BETWEEN FS 621 TO FS 559+110. COMPLIED WITH ECTC REO 601R-53-61-3778.

Part: HINGE — GOUGED (FUSELAGE) · airframe 36,908 hrs · 34,108 cycles

PAX DOOR HINGE (FUSELAGE SIDE) IS GOUGED ON LANDS FULL LENGTH OF HINGE. REPAIRED PAX DOOR HINGE (FUSELAGE SIDE) IAW REO 601R-53-21-814 REV C, TYPE IV REPAIR, DATED 2017-08-02 AND EC/TC REO 601R-53-21-814.

Part: SKIN — DENTED (TE FLAP) · airframe 36,908 hrs · 34,108 cycles

RIGHT INBOARD FLAP LOWER SKIN AT LOCATION K WAS DENTED APPROX .739 INCHES BY .070 INCHES DEEP. PERFORMED A MAJOR REPAIR TO RIGHT INBOARD FLAP LOWER SKIN IAW SRM 57-52-00.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 36,908 hrs · 34,108 cycles

CARGO DOOR FLOOR SILL HAS CORROSION AROUND MULTIPLE NUTPLATE HOLES BETWEEN FS 574 TO FS 621. REPAIRED CARGO DOOR FLOOR SILL IAW REO 601R-53-61-1574 AND ECTC REO 601R-53-61-1574.

Part: DOUBLER — CHAFED (FUSELAGE) · airframe 36,908 hrs · 34,108 cycles

AFT SIDE OF FS 280 BULKHEAD AT RBL12 APPROXIMATELY 24 INCHES ABOVE FLOOR HAS TWO CHAFED AREAS AT A PREVIOUS REPAIR. REPAIRED CHAFE DAMAGE IAW REO 601R-53-11-3318 REV-, DATED 2018-08-31 AND EC/TC REO 601R-53-11-3318 REV 0.

Part: HINGE — CHAFED (PAX DOOR) · airframe 36,908 hrs · 34,108 cycles

PAX DOOR HINGE (DOOR SIDE) HAS CHAFE/GOUGE DAMAGE ON THE 15TH AND 16TH LANDS FROM FWD SIDE OF DOOR. REPAIRED PAX DOOR HINGE (DOOR SIDE) IAW REO 601R-52-11-1347 REV -C, TYPE IV REPAIR, DATED 2017-08-02 AND EC/TC REO 601R-52-11-1347.

Part: FLOOR SUPPORT — DAMAGED (BS 564-559) · corrosion level 2 · airframe 33,414 hrs · 30,707 cycles

DURING A C-CHECK INSPECTION, THREE HOLES WERE FOUND TO BE OBLONG ON A U-CHANNEL SPLICE DURING A REPAIR OF BEAM CAP AT RBL 9 AT BS 564-559+8, MAINTENANCE COMPLIED WITH SNIEO601R31005 S01, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (BS 559) · corrosion level 2 · airframe 33,414 hrs · 30,707 cycles

DURING C-CHECK INSPECTION, A CORRODED FLOOR SUPPORT WAS FOUND BETWEEN BS 559.48 - 559.80 RBL 9. MAINTENANCE COMPLIED WITH REO601R-53-51-288 AND EC/TC601R-53-51-288 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — DENTED (BS 586-605) · corrosion level 2 · airframe 33,414 hrs · 30,707 cycles

DURING A C-CHECK INSPECTION, DAMAGE TO THE FUSELAGE SKIN WAS FOUND AFT OF THE GROUND AIR DOOR BETWEEN BS 574-605 AND STRINGERS 21-26R. THE SKIN WAS REPAIRED IAW REO 601R-53-61-5820 AND EC/TCREO 601R-53-61-5820, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SEAT TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 33,414 hrs · 30,707 cycles

DURING C-CHECK INSPECTION, A SEAT TRACK SEGMENT BETWEEN BS 559.8 TO 559.112 LBL 9 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED, FABRICATED AND INSTALLED A NEW SEAT TRACK SEGMENT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SEAT TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 33,414 hrs · 30,707 cycles

DURING C-CHECK INSPECTION, SEAT TRACK WAS FOUIND TO BE CORRODED FROM BS 559 - 559.80 AT LBL 9. REMOVED, FABRICATED AND REPLACED THE AFFECTED SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — DENTED (BS 589) · corrosion level 2 · airframe 33,414 hrs · 30,707 cycles

DURING C-CHECK INSPECTION, A DENT WAS FOUND. REPAIRED BELOW THE CARGO DOOR IAW EC/TC EA38-2015-068 AND EA38-2015-068 REV B AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SEAT TRACK — CORRODED (BS 424-559) · airframe 33,414 hrs · 30,707 cycles

DURING C-CHECK INSPECTION, THE SEAT TRACK BETWEEN BS 424 - 559, RBL 9 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SEAT TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 33,414 hrs · 30,707 cycles

DURING C-CHECK INSPECTION, A SEAT TRACK BETWEEN BS 559.80 TO 559.112 AT RBL 27 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED, FABRICATED AND INSTALLED A NEW SEAT TRACK SEGMENT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SEAT TRACK — CORRODED (BS 394-409) · corrosion level 2 · airframe 33,414 hrs · 30,707 cycles

DURING A C-CHECK INSPECTION, A SEAT TRACK SEGMENT BETWEEN BS 394 TO 409+112 RBL 9 WAS FOUND TO HAVE NUMEROUS SCREW HOLES WITH CORROSION. MAINTENANCE REMOVED, FABRICATED AND INSTALLED A NEW SEAT TRACK SEGMENT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CLEAT — DENTED (FUSELAGE) · airframe 33,414 hrs · 30,707 cycles

MCN - DURING C-CK INSPECTION, A DENT IN THE FWD FUSELAGE LEFT SIDE AT FS 250.00 STR 23R WAS REPAIRED IAW EA/ECTC 12-2016-129 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE ON 09/25/16.

Part: FLOOR SUPPORT — CORRODED (BS 559) · corrosion level 2 · airframe 33,414 hrs · 30,707 cycles

DURING C-CHECK INSPECTION, THE LEFT FLOOR SUPPORT WAS FOUND TO BE CORRODED BETWEEN BS 559.48 - 559.80. MAINTENANCE COMPLIED WITH ECTC/REO 601R-53-00-526 AND GENERIC REO 601R-53-00-526 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SEAT TRACK — CORRODED (BS 559-574) · corrosion level 2 · airframe 33,414 hrs · 30,707 cycles

DURING C-CHECK INSPECTION, A SEAT TRACK SEGMENT BETWEEN BS 559.112 TO 574. RBL 9 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED, FABRICATED AND INSTALLED A NEW SEAT TRACK SEGMENT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SEAT TRACK — CORRODED (BS 364-394) · corrosion level 2 · airframe 33,414 hrs · 30,707 cycles

DURING C-CHECK INSPECTION, A SEAT TRACK SEGMENT BETWEEN RBL 9 WAS FOUND TO BE CORRODED AT BS 364. MAINTENANCE REMOVED, FABRICATED AND INSTALLED A NEW SEAT TRACK SEGMENT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,414 hrs · 30,707 cycles

MCN - DURING C-CK INSPECTION A SEAT TRACK SEGMENT BETWEEN FS559.80 TO 559.96 AT LBL 9 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED, FABRICATED AND INSTALLED A NEW SEAT TRACK SEGMENT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE ON 09/25/2016.

Part: SEAT TRACK — CORRODED (BS 559-574) · corrosion level 2 · airframe 33,414 hrs · 30,707 cycles

DURING C-CHECK INSPECTION, A SEAT TRACK SEGMENT BETWEEN BS 559.112 TO 574 LBL 9 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED, FABRICATED AND INSTALLED A NEW SEAT TRACK SEGMENT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SEAT TRACK — CORRODED (BS 364-394) · corrosion level 2 · airframe 33,414 hrs · 30,707 cycles

DURING A C-CHECK INSPECTION, A SEAT TRACK SEGMENT BETWEEN BS 364 TO 394 LBL 9 WAS FOUND TO BE CORRODED AT FS364. MAINTENANCE REMOVED, FABRICATED AND INSTALLED A NEW SEAT TRACK SEGMENT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SEAT TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 33,414 hrs · 30,707 cycles

DURING A C-CHECK INSPECTION, A SEAT TRACK SEGMENT BETWEEN BS 559.8 TO 559.96 LBL 27 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED, FABRICATED AND INSTALLED A NEW SEAT TRACK SEGMENT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SEAT TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 33,414 hrs · 30,707 cycles

DURING C-CHECK INSPECTION, A CORRODED SEAT TRACK WAS FOUND BETWEEN BS 559 - 559.80 LBL 9. MAINTENANCE REMOVED, FABRICATED AND INSTALLED A NEW SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (BS 559) · corrosion level 2 · airframe 33,414 hrs · 30,707 cycles

DURING C-CHECK INSPECTION, CORROSION WAS FOUND ALONG THE RIGHT FLOOR SUPPORT BETWEEN BS 559 - 559.96. MAINTENANCE REPAIRED THE FLOOR SUPPORT IAW REO 601R-53-00-576-01 AND EC/TC REO 601R-53-00-576, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DRAG ANGLE — CRACKED (DOOR) · corrosion level 2 · airframe 33,414 hrs · 30,707 cycles

MCN - DURING C-CK INSPECTION, THE ASD DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE RECEIVED AND COMPLIED WITH EC/TC REO601R-52-11-2352 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE ON 09/25/2016.

Part: SEAT TRACK — CORRODED (BS 424-559) · airframe 33,414 hrs · 30,707 cycles

DURING C-CHECK INSPECTION, THE SEAT TRACK BETWEEN BS 424 - 559, LBL 9 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK WITH A FABRICATED UNIT AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 33,414 hrs · 30,707 cycles

MCN - DURING C-CK INSPECTION, THE FLOOR SUPPORT ANGLE AT FS280 RBL 9 WAS FOUND TO BE CRACKED UNDERSIDE OF FLOORBEAM. MAINTENANCE COMPLIED WITH REO 601R-53-11-926-01, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE ON 09/25/16.

Part: SHIM — MIGRATED (RT MLG WW) · airframe 33,414 hrs · 30,707 cycles

MCN - DURING C-CK INSPECTION, SHIMS WERE FOUND TO BE MIGRATING FROM UNDER THE ATTACHMENT FITTING FROM THE PRESSURE BOX CROSSBEAM TO THE SIDE STAY ACTUATOR FITTING RT WHEEL WELL. MAINTENANCE COMPLIED WITH EC/TC REO 601R53-41-101 01 AS WRITTEN, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE ON 09/25/16.

Part: SHIM — MIGRATED (LT MLG WW) · airframe 33,414 hrs · 30,707 cycles

MCN - DURING C-CK INSPECTION, SHIMS WERE FOUND TO BE MIGRATING FROM UNDER THE ATTACHMENT FITTING FROM THE PRESSURE BOX CROSSBEAM TO THE SIDE STAY ACTUATOR FITTING LT WHEEL WELL. MAINTENANCE COMPLIED WITH EC/TC REO 601R53-41-101 01 AS WRITTEN, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE ON 09/25/16.

Part: SKIN — DAMAGED (BS 397) · airframe 28,800 hrs · 26,454 cycles

LIGHTNING DAMAGE FOUND AT BS 397.5, TWO INCHES LEFT OF STRINGER 27. PERFORMED A MAJOR REPAIR BY INCORPORATING REO 601R-53-00-115, REV "E", AND EC/TC REO 601R-53-00-115.

Part: SKIN — DAMAGED (BS 405) · airframe 28,800 hrs · 26,454 cycles

LIGHTNING DAMAGE FOUND AT BS 405, STR 27. PERFORMED A MAJOR REPAIR BY INCORPORATING REO 601R-53-00-115, REV "E", AND EC/TC REO 601R-53-00-115.

Part: SKIN — DAMAGED (BS 362-363) · airframe 28,800 hrs · 26,454 cycles

LIGHTNING STRIKE DAMAGE FOUND BS 362 AND 363 AT S24R. PERFORMED A MAJOR REPAIR BY INCORPORATING REO 601R-53-00-115, REV "E", AND EC/TC REO 601R-53-00-115.

Part: SKIN — DAMAGED (BS 400) · airframe 28,800 hrs · 26,454 cycles

LIGHTNING DAMAGE FOUND AT BS 400, TWO INCHES RIGHT OF STRINGER 27. PERFORMED A MAJOR REPAIR BY INCORPORATING REO 601R-53-00-115, REV "E", AND EC/TC REO 601R-53-00-115.

Part: SKIN — DAMAGED (BS 358) · airframe 28,800 hrs · 26,454 cycles

LIGHTNING DAMAGE FOUND AT BS 358.5, TWO INCHES LEFT OF STRINGER 27. PERFORMED A MAJOR REPAIR BY INCORPORATING REO 601R-53-00-115, REV "E", AND EC/TC REO 601R-53-00-115.

Part: SKIN — DAMAGED (BS 402) · airframe 28,800 hrs · 26,454 cycles

LIGHTNING DAMAGE FOUND AT BS 402.5 TWO AND A HALF INCHES INBD OF STRINGER 26L. PERFORMED A MAJOR REPAIR BY INCORPORATING REO 601R-53-00-115, REV "E", AND EC/TC REO 601R-53-00-115 UNDER WO 345216.

Part: SKIN — DAMAGED (BS 346) · airframe 28,800 hrs · 26,454 cycles

LIGHTNING DAMAGE FOUND AT BS 346 BETWEEN S26 AND 27L. PERFORMED A MAJOR REPAIR BY INCORPORATING REO 601R-53-00-115, REV "E" AND REO 601R-53-00-115.

Part: SKIN — DAMAGED (BS 409) · airframe 28,800 hrs · 26,454 cycles

LIGHTNING DAMAGE FOUND AT BS 409, ONE, TWO INCHES INBD OF STRINGER 26R AND ONE, THREE INCHES OTBD OF STRINGER 26R. PERFORMED A MAJOR REPAIR BY INCORPORATING REO 601R-53-00-115, REV"E", AND EC/TC REO 601R-53-00-115.

Part: SKIN — DAMAGED (BS 344-347) · airframe 28,800 hrs · 26,454 cycles

LIGHTNING STRIKE DAMAGE FOUND BS 344 AND 347.5, STRINGER 24R. PERFORMED A MAJOR REPAIR BY INCORPORATING REO 601R-53-00-115, REV "E", AND EC/TC REO 601R-53-00-115.

Part: SKIN — DAMAGED (BS 280) · airframe 28,799 hrs · 26,453 cycles

LIGHTNING STRIKE DAMAGE FOUND AT BS 250 BETWEEN S26 - 27L. BLENDED DAMAGE IAW STEP 2A2 OF REO 601R-53-00-115, REV E. REPAIRED IAW ECTC REO 601R-53-00-115.

Part: SKIN — DAMAGED (BS 332) · airframe 28,800 hrs · 26,454 cycles

LIGHTNING STRIKE DAMAGE, FOUND AT BS 332 BETWEEN S26 AND 27L. PERFORMED A MAJOR REPAIR BY INCORPORATING REO 601R-53-00-115, REV "E", AND EC/TC REO 601R-53-00-115.

Part: SKIN — DAMAGED (BS 318-320) · airframe 28,800 hrs · 26,454 cycles

LIGHTNING STRIKE DAMAGE FOUND BS 318 AND 320.5, S25 - 26L. PERFORMED A MAJOR REPAIR BY INCORPORATING REO 601R-53-00-115, REV "E", AND EC/TC REO 601R-53-00-115.

Part: SKIN — DAMAGED (BS 311) · airframe 28,800 hrs · 26,454 cycles

LIGHTNING STRIKE DAMAGE FOUND AT BS 311, STRINGER 25R. PERFORMED A MAJOR REPAIR BY INCORPORATING REO 601R-53-00-115, REV "E", AND EC/TC REO 601R-53-00-115.

Part: SKIN — DAMAGED (BS 330) · airframe 28,800 hrs · 26,454 cycles

LIGHTNING STRIKE DAMAGE FOUND AT BS 330, S24R. PERFORMED A MAJOR REPAIR BY INCORPORATING REO 601R-53-00-115, REV "E", AND EC/TC REO 601R-53-00-115.

Part: SKIN — BURNED (BS 316-614) · airframe 28,800 hrs · 26,454 cycles

LIGHTNING STRIKE DAMAGE FOUND AT BS 614.5 AND 316 S26R. PERFORMED A MAJOR REPAIR BY INCORPORATING REO 601R-53-00-115, REV "E", AND EC/TC REO 601R-53-00-115.

Part: SKIN — DAMAGED (BS 268-271) · airframe 28,800 hrs · 26,454 cycles

LIGHTNING STRIKE DAMAGE FOUND BS 268 - 271.5 S27. PERFORMED A MAJOR REPAIR BY INCORPORATING REO 601R-53-00-115, REV "E", AND EC/TC REO 601R-53-00-115.

Part: SKIN — DAMAGED (BS 301) · airframe 28,800 hrs · 26,454 cycles

LIGHTNING STRIKE DAMAGE FOUND AT BS 301, S26R. PERFORMED A MAJOR REPAIR BY INCORPORATING REO 601R-53-00-115, REV "E", AND EC/TC REO 601R-53-00-115.

Part: SKIN — DAMAGED (BS 303) · airframe 28,800 hrs · 26,454 cycles

LIGHTNING STRIKE DAMAGE FOUND AT BS 303, S24R. PERFORMED A MAJOR REPAIR BY INCORPORATING REO 601R-53-00-115, REV"E", AND EC/TC REO 601R-53-00-115.

Part: SKIN — DAMAGED (BS 310) · airframe 28,800 hrs · 26,454 cycles

LIGHTNING STRIKE DAMAGE FOUND AT BS 310 BETWEEN S26 & 27R. PERFORMED A MAJOR REPAIR BY INCORPORATING REO 601R-53-00-115, REV"E", AND EC/TC REO 601R-53-00-115.

Part: SKIN — DAMAGED (BS 273) · airframe 28,800 hrs · 26,454 cycles

LIGHTNING STRIKE DAMAGE FOUND AT BS 273.5. INBD OF S26L. PERFORMED A MAJOR REPAIR BY INCORPORATING REO 601R-53-00-115, REV "E", AND EC/TC REO 601R-53-00-115.

Part: SKIN — DAMAGED (BS 243) · airframe 28,799 hrs · 26,453 cycles

LIGHTNING STRIKE DAMAGE, FOUND AT FS 243, BETWEEN STGR 26 - 27L. DRILLED OUT DAMAGE IAW STEP B3A OF REO 601R-53-00-115, REV E. REPAIRED IAW ECTC REO 601R-53-00-115.

Part: SKIN — DAMAGED (BS 259-264) · airframe 28,799 hrs · 26,453 cycles

LIGHTNING STRIKE DAMAGE BS 259 - 264 S27. REPAIRED BY INCORPORATING REO 601R-53-00-115, REV "E", AND EC/TC REO 601R-53-00-115.

Part: SKIN — DAMAGED (BS 312-313) · airframe 28,800 hrs · 26,454 cycles

LIGHTNING STRIKE DAMAGE FOUND BS 312 AND 313.5 AT S27. PERFORMED A MAJOR REPAIR BY INCORPORATING REO 601R-53-00-115, REV "E", AND EC/TC REO 601R-53-00-115.

Part: STRINGER — CORRODED (BS 333-349) · airframe 28,799 hrs · 26,453 cycles

STRINGER 27, REPAIR AT BS 333-349 IS CORRODED. REMOVED AND REPLACED IAW SRM 51-42-06 AND SRM 53-00-03.

Part: SKIN — CRACKED (RT WING) · airframe 28,799 hrs · 26,453 cycles

FOUND RT SIDE LOWER WING PLANK DRAIN HOLE WS 85.50 HAS INDICATION NOTED AT AFT SIDE OF DRAIN HOLE APPROX .300, LONGERON 90 PERCENT FSH FAILED NDT INSPECTION. COMPLETED WITH REO:601R-57-21-2227 P1.

Part: ANGLE — BROKEN (BS 625 BULKHEAD) · airframe 28,799 hrs · 26,453 cycles

REAR PRESSURE BULKHEAD WEB AFT SIDE HAS A BROKEN ANGLE ON LT SIDE APPROXIMATELY STR 14L. R & R ANGLE ON STR 14L, BS 625 IAW SRM 51-42-21.

Part: ATTACH ANGLE — CRACKED (BS 484) · airframe 28,799 hrs · 26,453 cycles

BS 484, RBL 27. INTERCOSTAL ATTACH ANGLE IS CRACKED. REMOVED CRACKED ATTACH ANGLE IAW SRM 51-42-21 AND 51-42-06. INSTALLED NEW ATTACH ANGLE IAW SRM 51-40-06, 51-40-11, 51-42-06 AND 51-42-21.

Part: STRAP — CORRODED (BS 559) · airframe 28,799 hrs · 26,453 cycles

BS 559, RBL 36, FLOORBOARD ATTACH STRAP IS CORRODED. BLENDED AREA IAW SRM 51-21-06. FOUND TO BE OUT OF LIMITS IAW SRM TR 53-30. COMPLIED WITH PERMANENT REPAIR IAW EA 32-2014-086.

Part: STRAP — CORRODED (BS 559) · airframe 28,799 hrs · 26,452 cycles

BS 559, LBL 36, THE FLOORBOARD ATTACHMENT STRAP IS CORRODED. BLENDED CORRODED AREA IAW SRM 51-21-06, AND FOUND TO BE OUT OF LIMITS IAW SRM TR 53-30. COMPLIED WITH EA 32-2014-086.

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 28,799 hrs · 26,452 cycles

FLOOR SUPPORT BS 409+128 - 559, LBL 45 CORRODED. BLENDED OUT CORROSION IAW REO 601R-53-41-666, REV C, 2012-11-06. REPAIRED IAW REO 601R-53-41-666.

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 28,799 hrs · 26,453 cycles

BS 409+128 - 559. RBL 45, FLOOR SUPPORT CORRODED. BLENDED OUT CORROSION IAW REO 601R-53-41-666, REV C 2012-11-06. REPAIRED IAW ECTC REO 601R-53-41-666 AND REO 601R-53-41-666, REV C.

Part: FRAME — CORRODED (BS 333) · airframe 28,799 hrs · 26,452 cycles

FRAME BS 333 IS CORRODED BETWEEN STRINGERS 26L - 26R. FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 53-00-00 .

Part: FRAME — CORRODED (BS 349) · airframe 28,799 hrs · 26,452 cycles

FRAME AT FS 349 STRINGER 27 IS CORRODED. FOUND CORROSION TO BE OUT OF LIMITS OF SRM 53-00-00. REMOVED FRAME IAW SRM 51-42-06 AND 51-42-21. LOCATED AND DRILLED NEW FRAME IAW SRM 51-40-11. INSTALLED NEW FRAME IAW SNIEO 601R32005 S01.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 28,799 hrs · 26,452 cycles

FLOORBEAM INBD AND OTBD ANGLES ARE CRACKED AT BS 280.0 LBL 9. REMOVED CRACKED ANGLES IAW SRM 51-42-21. INSTALLED FABRICATED ANGLES IAW SRM 51-42-21 AND AMM TASK 20-21-00-910-801. AND INSTALLED IAW SRM 51-25-16- AND 51-40-11. COMPLIED WITH EC/TC IAW BSC REO 601R-53-11-926, REV B, DATED 5/10/06.

Part: PANEL — DAMAGED (WING) · airframe 28,799 hrs · 26,452 cycles

PANEL 598JT HAS ONE ELONGATED HOLE DUE TO SCREW REMOVAL. REPAIRED PANEL IAW EA 05-2014-048, SECTION I STEPS 1, 2A, B, C AND D.

Part: WEB — CORRODED (BS 470-476) · airframe 28,799 hrs · 26,453 cycles

BS 470 - 476, BETWEEN RBL 36 - 45, THE FLOOR SUPPORT FINGER WEB IS CORRODED. BLENDED OUT CORROSION IAW REO 601R-53-41-666, REV C 2012-11-06,. COMPLIED WITH ECTC REO 601R-53-41-666 AND REO 601R-53-41-666.

Part: WEB — CORRODED (BS 470-476) · airframe 28,799 hrs · 26,452 cycles

BS 470 - 476, BETWEEN LBL 36 - 45, FLOOR SUPPORT FINGER WEB IS CORRODED. LPERFORMED A MAJOR REPAIR BY INCORPORATING REO 601R-53-41-66, REV"C" AND EC/TC 601R-53-41-666 .

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 28,799 hrs · 26,452 cycles

MID CABIN OVERHEAD EXIT LIGHTS BURNED OUT. R & R LAMPS . OPS TESTED EXIT LIGHTS IAW AMM 33-51-00-710-801. OPS TESTED GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 28,799 hrs · 26,452 cycles

FLOOR LEVEL EXIT SIGN AT PAX DOOR DOES NOT COME ON WHEN EMERGENCY LIGHTS BATTERY PACK NR 1 IS TESTED. R & R DIODE ASSY IAW ESPM 20-18-10. R & R NR 1 BATTERY CHARGER ASSY FOR EMERGENCY LIGHTS IAW AMM 33-51-05-400-801. PERFORMED SELF TEST OF THE CHARGER ASSY IAW AMM 33-51-04-740-801. OPS CHECK GOOD.

Part: BEARING — FAILED (RT ELEVATOR) · airframe 28,799 hrs · 26,452 cycles

RT ELEVATOR A FAILED BEARING. R & R PCU BUSHING IAW AMM 20-26-00-910-802 & 20-26-00-910-804, REV 49 . R & R RT ELEVATOR SYS 1, 2 & 3 BEARINGS IAW AMM 20-26-00-910-807 AND 20-26-00-910-808 REV 49. RT ELEVATOR BEARING BACKLASH CHECKS WITH SYS 3 GOOD IAW AMM 27-31-00-220-804.

Part: BEARING — FAILED (LT ELEVATOR) · airframe 28,799 hrs · 26,452 cycles

LT ELEVATOR FAILED BEARING BACKLASHED ON SYS NR 3. R & R THE PCU BUSHINGS IAW AMM 20-26-00-910-802 AND 20-26-00-910-804. R & R THE LT ELEV SYS 1, 2 & 3 BEARINGS IAW AMM 20-26-00-910-807 AND 20-26-00-910-808, REV 49.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 27,725 hrs · 25,383 cycles

CABIN AFTMOST CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP IAW AMM 33-51-16. OPS CHECKED GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 25,973 hrs · 23,726 cycles

RT WING FWD EMERGENCY LIGHT OUT. REPLACED LAMP IAW AMM 33-51-21.

Part: LOCK — BINDING (SERVICE DOOR) · airframe 24,969 hrs · 22,743 cycles

SERVICE DOOR LOCK RELEASE HANDLE INOPERATIVE. INSTALLED PIN IN SERVICE DOOR RELEASE LOCK HANDLE IAW AMM 200 52-41-03. OPS CHECKED GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 24,614 hrs · 22,383 cycles

EXTERIOR EMERGENCY LIGHT NR 3 IS OUT. RELAMPED THE EXTERIOR NR 3 EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: INTERCOSTAL — CRACKED (BS 621-625.3) · airframe 24,350 hrs · 22,120 cycles

DURING GVI OF INTERCOSTALS AT FS 621- 625.3. FOUND INTERCOSTAL TO BE CRACKED AT AFT RADIOUS, APPROX .500' LONG. OPEN.

Part: INTERCOSTAL — CRACKED (BS 621-625.3) · airframe 24,350 hrs · 22,120 cycles

WHILE PERFORMING GENERAL VISUAL INSPECTION OF THE INTERCOSTAL AT FS 621- 625.3 IAW SB 601R-53-048, REV C FOUND INTERCOSTAL TO BE CRACKED AT AFT RADIUS APPROX .500" LONG. REO 601R-53-61-4686 HAS BEEN ACCOMPLISHED.

Part: INTERCOSTAL — CRACKED (BS 621-625.3) · airframe 24,350 hrs · 22,120 cycles

WHILE PERFORMING GENERAL VISUAL INSPECTION OF THE INTERCOSTAL MEMBERS AT FS 621- 625.3 IAW SB 601R-53-048, REV "C" FOUND INTERCOSTAL TO BE CRACKED AT AFT RADIUS APPROX .500" LONG. COMPLIED WITH REO 601R-53-61-4686. SDR CLOSED.

Part: FLOOR SUPPORT — CORRODED (BS 349-364) · airframe 24,350 hrs · 22,120 cycles

CORROSION AROUND NUTPLATES RT FLOOR SUPPORT FS 349 - 364. COMPLIED WITH REO 601R-53-21-2357. LOCATED HOLES IN NEW SERVICEABLE FLOOR SUPPORT IAW SRM 51-40-11.

Part: FLOORBEAM — CORRODED (BS 409) · airframe 24,350 hrs · 22,120 cycles

NUTPLATE HOLE ON FLOORBEAM CAP INBD SIDE AT FS 409+129 IS CORRODED AT RBL 9. FOUND CORROSION AT NUTPLATE HOLE TO BE OUT OF LIMITS IAW REO 601R-53-00-005, REV B. REPAIRED AREA IAW NDTM 51-20-06. REPAIRED IAW REO 601R-53-41-1631.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 24,337 hrs · 22,106 cycles

FOUND CARGO DOOR SUPPORT BEAM AFT LOWER ANGLE IS CRACKED APPROX .5 INCHES IN LENGTH. REMOVED CRACKED AFT LOWER ANGLE FROM CARGO DOOR SUPPORT BEAM AND REPLACED WITH NEW PARTS IAW SRM 51-40-11 AND 51-42-21,

Part: SEAT TRACK — CORRODED (BS 394-409) · airframe 24,350 hrs · 22,120 cycles

LBL 9 & RBL 9 FS 394.00 - FS 409.00+128 SEAT TRACKS CORRODED & GOUGED IN NUMEROUS LOCATIONS. REMOVED DAMAGED SEAT RAIL SEGMENT FROM FS 399.50 - 409+126 IAW AMM 53-01-11-000-802 AT RBL AND LBL 9. INSTALLED NEW SERVICEABLE SEAT RAIL AT RBL 9 & LBL 9 FS 394.00 - FS 409.00+128 IAW REO 601R-53-00-485 STEP 7. FABRICATED SEAT RAILS IAW GREO 601R-53-00-485.

Part: BULKHEAD WEB — CRACKED (AFT) · airframe 24,350 hrs · 22,120 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS INDICATION NOTED AT LBL 27.50 WL 130 APPROX .3" IN LENGTH 100 PERCENT FSH. FAILED NDT INSPECTION. COMPLIED WITH AND MET ALL THE REQUIREMENTS OF REO 601R-53-61-1541, REV D DATED 10/31/2011. SDR CLOSED.

Part: FLOOR SUPPORT — CORRODED (BS 409) · airframe 24,350 hrs · 22,120 cycles

RBL 9, FS 409 - 409.00+128 CORRODED AROUND NUMEROUS NUTPLATES ON FLOOR SUPPORT CAP INBD SIDE. REMOVED FLOOR SUPPORT CAP AT RBL 9 FS 409.00 - FS 409+128 IAW SRM 51-42-06 AND SRM 51-42-21. INSTALLED NEW FLOORBEAM UPPER CAP AT RBL 9.0 FROM FS 409+5 TO FS 409+118 IAW REO 601R-53-31-767, REV A, STEPS 1 THRU 3. FABRICATED AND LOCATED HOLES FOR NEW FLOOR SUPPORT CAP FROM N126-1577 STOCK, PO W000012498 AND BOMBARDIER REO 601R-53-31-765 STEPS 1-8. REO 601R-53-21-765 HAS BEEN ACCOMPISHED.

Part: FLOOR SUPPORT — CORRODED (BS 559-621) · airframe 24,337 hrs · 22,106 cycles

CARGO FLOOR SUPPORT CAP CORRODED, LBL 27 FS 559+112 - 621 AROUND NUTPLATES. INSTALLED NEW FLOOR SUPPORT CAP IAW SRM 51-42-06, 51-42-21, AND 51-42-22 AND REO 601R-53-61-3778, REV A.

Part: SILL — CORRODED (BS 559-621) · airframe 24,350 hrs · 22,120 cycles

CARGO DOOR SILL CORRODED, AROUND NUTPLATES FS 559+112 - FS 621. REMOVED CORRODED CARGO DOOR SILL IAW SRM 51-42-06-00 AND 51-42-21-00. INSTALLED NEW CARGO DOOR SILL IAW SRM 51-42-06, 51-42-21 AND REO 601R-53-61-690.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 24,350 hrs · 22,120 cycles

CORROSION ON OTBD END OF FLOORBEAM RT SIDE FS 349.00. REMOVED A CORRODED WINDSCREEN MOUNT FLOORBEAM ANGLE AT FS 349 AND RBL 27 TO RBL 40 IAW SRM 51-42-06 /51-42-21 /51-42-13. DRILLED AND LOCATED A NEW SERVICEABLE WINDSCREEN MOUNT FLOOR ANGLE AT FS 349, RBL 27 TO RBL 40 IAW IAW SRM 51-42-06/51-42-21/51-42-13. INSTALLED NEW SERVICEABLE SUPPORT ANGLE AT FS 349 RBL 27 TO RBL 40 IAW SRM TASK 51-42-06, 51-42-13 & 514221.

Part: SEAT TRACK — CORRODED (BS 409-563) · airframe 24,350 hrs · 22,120 cycles

FS 409+126 - FS 563 SEAT TRACK CORRODED AND GOUGED IN NUMEROUS LOCATIONS. SEAT TRACK REMOVED IAW AMM 53-01-11-002-002. INSTALLED NEW SERVICEBLE SEAT TRACK IAW REO 601R-53-00-485, STEP 7. FABRICATED SEAT TRACK IAW GREO 601R-53-00-485. COMPLIED WITH REO 601R-53-00-485.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 24,337 hrs · 22,106 cycles

SEAT TRACK CORRODED & GOUGED IN NUMEROUS PLACES. REMOVED DAMAGED SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED NEW SERVICEABLE SEAT TRACK IAW AMM 53-01-11-400-802.

Part: FLOOR SUPPORT — CORRODED (BS 409) · airframe 24,350 hrs · 22,120 cycles

RBL 9, FS 409.00 - FS 409.00+128 CORRODED AROUND NUMEROUS NUTPLATES ON FLOOR SUPPORT CAP INBB SIDE. REMOVED FLOOR SUPPORT CAP FROM LBL 9 IAW SRM 51-42-06. INSTALLED NEW FLOOR SUPPORT CAP AT LBL 9, FS 409 - FS 409.112 BY COMPLING WITH STEPS 1, 2, 4 & 8 OF REO 601R-53-31-765 AT REO 601R-53-31-767, REV A. LOCATED AND DRILLED FASTENER ATTACHMENT HOLES IN NEW FLOOR SUPPORT CAP AT LBL 9, FS 409.50 - FS 409.00+118 IAW REO 601R-53-31-765, STEP 3.

Part: FLOOR SUPPORT — CORRODED (BS 349-364) · airframe 24,350 hrs · 22,120 cycles

CORROSION AROUND NUTPLATES RT FLOOR SUPPORT FS 349.00 -FS 364.00. COMPLIED WITH REO 601R-53-21-2357. LOCATED HOLES IN NEW SERVICEABLE FLOOR FLOOR SUPPORT IAW SRM 51-40-11.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 24,337 hrs · 22,106 cycles

PAX DOOR FRAME STRUCTURE IS CRACKED AFT OF PRESSURE VENT FLAP ASSY. REMOVED CRACKED ANGLE IAW SRM 51-42-06. INSTALLED NEW SERVICEABLE ANGLE IAW SRM 51-42-06. SDR CLOSED.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 24,337 hrs · 22,106 cycles

SEAT TRACK HAS MULTIPLE AREAS OF CORROSION. LOCATED & DRILLED SEAT TRACK IAW SRM 51-40-11.

Part: RELAY — UNSERVICEABLE · airframe 24,246 hrs · 22,013 cycles

DURING CLIMBOUT, RECEIVED AN AC ESSENTIAL CAUTION MESSAGE INTERMITTENT RAN QRH AND SWITCHED TO AC ESSTENTIAL TRANSFER, IT MADE NO DIFFERENCE-RETURNED TO DEPARTURE. ACFT RETURNED TO DEPARTURE AFTER TAKE OFF. EMERGENCY DECLARED. R & R ESSTENTIAL BUSS RELAY. OPS CHECK TEST GOOD IAW AMM 24-51-27. IPC 24-01-06 ITEM 55A.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 23,196 hrs · 20,862 cycles

OVER WING MIDDLE EMERGENCY LIGHT INOPERATIVE. RELAMPED LT OVER WING MIDDLE EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 23,196 hrs · 20,862 cycles

RT WING AFT EMERGENCY LIGHT INOPERATIVE. RELAMPED RT WING AFT EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,186 hrs · 20,850 cycles

EMERGENCY CEILING LIGHTS INOPERATIVE. R & R EMERGENCY LIGHT BATTERY PACK NR 4 IAW AMM 33-51-04. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 23,166 hrs · 20,825 cycles

NR 7 AND NR 8 EXTERIOR EMERGENCY LIGHTS INOPERATIVE. R & R EMERGENCY LIGHT BATTERY PACK NR 4 IAW AMM 33-51-04. OPS CHECKED GOOD

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,166 hrs · 20,825 cycles

PAX AND SERVICE DOOR GREEN AND BOTH MIDDLE OVERWING EMERGENCY LIGHTS. BATTERY PACKS WERE SWAPPED AND NOW LT/RT AFT OVERWING EMERGENCY LIGHTS AND NR 2 & 4 CEILING EMERGENCY LIGHTS ARE INOPERATIVE. R & R EMERGENCY LIGHT BATTERY PACK NR 4 IAW AMM 33-51-04. OPS CHECK GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 22,112 hrs · 19,675 cycles

EMERGENCY LIGHT INOPERATIVE. RELAMPED LT MIDDLE EMERGENCY LIGHT IAW AMM 33-51-04. OPS CHECKED GOOD.

Part: WIRE HARNESS — ARCED (C/B PANEL) · airframe 22,126 hrs · 19,691 cycles

WHILE COMPLYING WITH REO 601R-24-60-002 , FOUND ON MAIN WIRE BUNDLE TO CB PANEL WIRE DAMAGED BY ARCING AND BURNING. R & R WIRES IAW AMM 24-31-01. OPS CHECKED IAW AMM 24-31-01.

Part: UPLOCK — FAILED (MLG) · airframe 21,833 hrs · 19,366 cycles

AT FL200 "GEAR DISAGREE" MASTER WARNING. GEAR SHOWED LT & RT MAINS UP AND NOSE GEAR SHOWS RED. (EMERGENCY DECLARED) REPLACED NLG UPLOCK ASSY IAW AMM 32-33-05. OPS AND LEAKS CHECK GOOD AT THIS TIME.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 21,382 hrs · 18,851 cycles

NR 2 CEILING EMERGENCY LIGHT INOP. RELAMPED NR 2 CEILING EMERGENCY LIGHT IAW AMM 33-51-16. RELAMPED NR 2 CEILING EMERGENCY LIGHT IAW AMM 33-51-16.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,995 hrs · 18,395 cycles

LT SIDE FUSELAGE AFT MOST EMERGENCY LIGHT IS INOP. R & R LT SIDE FUSELAGE AFT MOST EMERGENCY LIGHT IAW AMM 33-51-21. OPS CK GOOD. R & R LT SIDE FUSELAGE AFT MOST EMERGENCY LIGHT IAW AMM 33-51-21. OPS CK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,585 hrs · 17,920 cycles

THE WARDROBE FLOOR LEVEL EMERGENCY FLOODLIGHT IS INOP. REMOVED THE WARDROBE FLOOR LEVEL EMERGENCY FLOOD LIGHT IAW AMM 33-51-19-000-801. THE WARDROBE FLOOR LEVEL EMER FLOOD LIGHT REINSTALLATION AND EMERGENCY LIGHT OPS CHECK IS DUE. INSTALLED A NEW FLOOR LEVEL EMERGENCY FLOODLIGHT IAW AMM TASK 33-51-19-400-801. OPS TEST OF THE WARDROBE FLOOR LEVEL EMERGENCY FLOODLIGHT IS GOOD IAW AMM TASK 33-51-00-710-801. (CLOSED)

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 20,585 hrs · 17,920 cycles

PAX DOOR AFT DRAG ANGLE IS CRACKED 1" LONG IN THE RADIUS AT POWER ASSIST MOTOR PULLEY BRACKET LOCATION. REMOVED DAMAGED SECTION OF DRAG ANGLE AND REPAIRED IAW REO 601R-52-11-513. COMPLETED AND COMPLIED WITH EC/TC CARD REO 601R-52-11-513.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 20,585 hrs · 17,920 cycles

PAX DOOR SILL IS CORRODED ADJACENT TO CONNECTOR J1MB, FLANGES ON HANDRAIL SUPPORT STOW CUPS AND AROUND NUT CLIPS. REMOVED PAX DOOR SILL CTR CAP ANGLE IAW SRM 51-42-12. REMOVED SILL ANGLE PN 601R31527-221 IAW SRM 51-41-02, 51-42-06, 51-42-13, AND 51-42-21. LOCATED ANGLE AND DRILLED FASTENER HOLES IAW SRM 51-41-02, 51-42-06, 51-42-13, AND 51-42-21. INSTALLED CTR ANGLE, SILL ANGLE, FWD/AFT ANGLE, AND FWD/AFT CLEATS IAW SRM 51-41-02, 51-42-06, 51-42-16, AND 51-42-21. SEALED AND PAINTED PAX DOOR SILL IAW SRM 51-23-00, 51-25-16, AND 51-25-06.

Part: POST — CRACKED (BS 409) · airframe 20,585 hrs · 17,920 cycles

INDICATION NOTED AT FS 409+128 VERTICAL POST RBL 18, WL 69.00 OTBD CHANNEL 90 PERCENT FULL SCREEN HEIGHT APPROX .25IN LENGTH VERTICALLY. AREA MARKED ON ACFT. REMOVED POST ASSY IAW SRM 51-42-06. INSTALLED POST IAW REO 601R-53-41-889 ITEM 3.

Part: POST — CRACKED (BS 409) · airframe 20,585 hrs · 17,920 cycles

INDICATION NOTED AT FS 409+128 VERTICAL POST IN RADIUS OF THE OTBD CHANNEL 95 PERCENT FULL SCREEN HEIGHT APPROX .25IN LENGTH VERTICALLY (LBL 18 WL 69.00). AREA MARKED ON ACFT. REMOVED FS 409+128, LBL 18, POST ASSY & SEPARATED HALVES OF CHANNEL IAW SRM 51-42-06. INSTALLED LBL 18, FS 409+128 POST ASSY IAW REO 601R-53-41-889, REV A & SRM 51-42-06.

Part: POST — CRACKED (BS 409) · airframe 20,585 hrs · 17,920 cycles

INDICATION NOTED AT FS 409+128 VERTICAL POST BL 0.00 WL 69.00 RT CHANNEL 50 PERCENT FULL SCREEN HEIGHT APPROX .20 IN LENGTH VERTICALLY. AREA MARKED ON ACFT. REMOVED POST ASSY IAW SRM 51-42-06. INSTALLED FS 409+128 BL 0 POST ASSY IAW REO 601R-53-41-889.

Part: ISOLATOR — CRACKED (BS 621 BULKHEAD) · airframe 20,585 hrs · 17,920 cycles

FS 621 FWD SIDE OF AFT BULKHEAD 6 ISOLATORS CRACKED. R & R ISOLATORS ON FWD SIDE OF AFT BULKHEAD IAW SRM 51-42-06.

Part: ROLLER — WORN (PAX DOOR) · airframe 20,585 hrs · 17,920 cycles

PASSENGER DOOR FAILS FUNCTIONAL TEST. DOOR REQUIRES MODERATE EFFORT TO OPEN AND FORCE REQUIRED TO COMPLETE FULL UNLATCH CYCLE IS 20 LBS. (MAX ALLOWED IS 16 LBS). FOUND ROLLER LOCATED IN PAX DOOR LATCH BOX ASSY THAT CONTROLS DOOR PRESS VALVE LEVER WORN. REF 8763231, OP 341 FOR ROLLER REPLACEMENT. PAX DOOR FUNCTION TEST DUE. FUNC CHECK OF PAX DOOR GOOD IAW MM 52-11-00-720-802.

Part: FLOOR SUPPORT — CRACKED (BS 484) · airframe 20,585 hrs · 17,920 cycles

FS 484, RBL 27 FLOOR SUPPORT ANGLE CRACKED. R & R FS 484, RBL 27, FLOOR SUPPORT CLIP PN 601R31171-9 IAW SRM 51-42-06 AND 51-42-21.

Part: ANGLE — CRACKED (BS 484) · airframe 20,585 hrs · 17,920 cycles

FS 484, RBL 36 PREVIOUS REPAIR ANGLE CRACKED. REPAIR TO THE INTERCOSTALS AT FS 484, BETWEEN BL 27.00 AND BL 36.00 IS COMPLETED IAW REO 601R-53-41-059.

Part: FLOOR SUPPORT — CRACKED (BS 280) · airframe 20,585 hrs · 17,920 cycles

FS 280, RBL 9 OTBD FLOOR SUPPORT CLIP CRACKED. REMOVED CLIP & EXISTING SHIM. FABRICATED A NEW CLIP, TREATED, PIRMED AND PAINTED, SEALED AND INSTALLED THE SAME SERVICEABLE SHIM AND NEW CLIP. PRIMED AND PAINTED AFTER INSTALLATION. ALL WORK PERFORMED IAW ASA REO 601R-53-11-926 IAW REO 601R-53-11-926, REV B. COMPLIED WITH EC/TC REO 601R-53-11-926 IAW REO 601R-53-11926, REV B.

Part: FLOOR SUPPORT — CRACKED (BS 280) · airframe 20,585 hrs · 17,920 cycles

FS 280 LBL 9 INBD FLOOR SUPPORT CLIP CRACKED. REMOVED CLIP AT FS 280, FABRICATED A NEW CLIP. REMOVED AND RETAINED ORIGINAL SHIM. LOCATED NEW CLIP, TREATED, PRIMED AND PAINTED. INSTALLED SAME SERVICEABLE SHIM AND NEW CLIP, PRIMED AND PAINTED. ALL WORK PERFORMED IAW REO 601R-53-11-926. COMPLIED WITH EC/TC REO 601R-53-11-926 IAW REO 601R-53-11-926 REV B.

Part: ANGLE — CRACKED (BS 621-625) · airframe 20,585 hrs · 17,920 cycles

LT 621-625 OBLIQUE ANGLE IS CRACKED. REMOVED AND INSTALLED NEW ANGLE IAW SRM 51-42-21. PAINTED ANGLE IAW SRM 51-25-16.

Part: PLACARD — DETERIORATED (PAX DOORWAY) · airframe 20,433 hrs · 17,747 cycles

PAX DOOR EXIT AND TO OPEN PLACARD DETERIORATED. R & R PAX DOOR EXIT AND TO OPEN PLACARDS IAW AMM 11-30-02. R & R PAX DOOR EXIT AND TO OPEN PLACARDS IAW AMM 11-30-02.

Part: FLAP — FAILED (WING) · airframe 17,429 hrs · 14,524 cycles

FLAP FAIL AFTER TAKEOFF. FLAPS AT 0 POSITION.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 16,874 hrs · 14,035 cycles

NR 4 EMERGENCY BATTERY FAILED OPS CHECK.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 16,874 hrs · 14,035 cycles

FS 621-625 UPPER RT OBLIQUE ANGLE CRACKED IN RADIUS.

Part: ANGLE — CRACKED (BS 484) · airframe 16,874 hrs · 14,035 cycles

LEFT FS 484 FLOOR SUPPORT INTERCOSTAL ANGLE CRACKED AT LBL 27.0. REPLACED FLOOR SUPPORT INTERCOSTAL ANGLE IAW REO 601R-53-41-059 STEPS 8-13.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 16,874 hrs · 14,035 cycles

RIGHT FS 280 FLOOR SUPPORT ANGLE CRACKED .3 INCH LONG I/B RBL 9.0.

Part: RIB — CRACKED (RT WING) · airframe 16,874 hrs · 14,035 cycles

RT WING BAT WEB AT FS 53.6 CRACKED BETWEEN 2 FASTENERS. REPAIRED RT WING BAT WEB AT WS 53.6 IAW REO 601R-57-51-0046. C/W ASA ECTC REO 601R-57-51-046. SUPPLEMENTAL-SDR CLOSED 11/17/2008.

Part: RIB — CRACKED (LT WING) · airframe 16,874 hrs · 14,035 cycles

LT BATTERY RIB ASSY AT WS 53.60 IS CRACKED AROUND A FASTENER. TRIMMED AWAY DAMAGE FROM LT BATTERY RIB. REMOVED NUT PLATES AND FABRICATED ALL REPAIR PARTS. ALL WORK PERFORMED IAW BOMBARDIER AEROSPACE REO 601R-57-51-046 STEPS 1-4 REPAIR 2. REPAIR ITEMS REQUIRE INSTALL. INSTALLED ALL REPAIR PARTS & NUT PLATES IAW BOMBARDIER AEROSPACE REO 601R-57-51-046 STEPS 5-8. C/W ASA ECTC REO 601R-57-51-046. SUPPLEMENTAL-SDR CLOSED 11/17/2008.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 16,874 hrs · 14,036 cycles

WHILE PERFORMING FS 559 BULKHEAD INSPECTION, AN INDICATION WAS NOTED APPROX .500 INCH OTBD OF RBL 9, WL 58.70 APPROX .250 IN LENGTH VERTICALLY.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 16,874 hrs · 14,035 cycles

RIGHT FS 460 FLOOR SUPPORT FITTING P/N 600-31068-19 CRACKED 1 INCH LONG OUTBOARD SIDE RBL 9. REMOVED RT FS 460 FLOOR SUPPORT FITTING IAW CRJ 200 SRM 51-42-06 AND 51-42-21. LOCATED FASTENER HOLES IN NEW SERVICEABLE FITTING IAW CRJ 200 SRM 51-40-11. FITTING REQUIRES INSTALL. INSTALLED RT FS 460 FLOOR SUPPORT FITTING IAW CRJ 200 SRM 51-42-06 AND 51-42-21. SUPPLEMENTAL-SDR CLOSED 11/17/2008.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 16,874 hrs · 14,035 cycles

PAX DOOR AFT DRAG ANGLE IS CRACKED.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 16,874 hrs · 14,035 cycles

RIGHT FS 484 FLOOR SUPPORT INTERCOSTAL ANGLE CRACKED AT RBL 9.0. REPLACED ANGLE AT RT FS 484 FLOOR SUPPORT RBL 9.0 IAW SRM 51-42-06 AND 51-40-11. SUPPLEMENTAL-SDR CLOSED 11/17/2008.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 16,874 hrs · 14,035 cycles

FS 621-625 UPPER LT OBLIQUE ANGLE CRACKED IN RADIUS.

Part: BEAM — CORRODED (FUSELAGE) · airframe 16,874 hrs · 14,035 cycles

LEFT FS 409.0+128 VERTICAL BEAM CRACKED .1 INCH LONG O/B SIDE LBL 18 AT BOTTOM OF BEAM. REPAIRED LT FS 409.0+128 VERTICAL BEAM LBL 18 O/B IAW BOMBARDIER REO 601R-53-41-056. REQUIRES ECTC. COMPLIED W/ECTC REO 601R-53-41-056 IAW REO 601R-53-41-056 REV E. SUPPLEMENTAL-SDR CLOSED 11/17/2008.

Part: BEAM — CRACKED (FUSELAGE) · airframe 16,874 hrs · 14,035 cycles

LEFT FS 409.0+128 VERTICAL BEAM CRACKED .1 INCH LONG O/B SIDE LBL 9 AT BOTTOM OF BEAM. ACCOMPLISHED REPAIR TO FS 409+128 VERTICAL BEAM O/B SIDE OF LBL 9 IAW BOMBARDIER REO 601R-53-41-237. ASA ECTC REQUIRES COMPLIANCE. COMPLIED WITH ECTC REO 601R-53-41-237 IAW BOMBARDIER REO 601R-53-41-237 REV A. ASA RII COMPLIED WITH: 5300194. SUPPLEMENTAL-SDR CLOSED 11/17/2008.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 16,874 hrs · 14,035 cycles

LEFT FS 484 FLOOR SUPPORT INTERCOSTAL PREVIOUS REPAIR ANGLE AT LBL 36.0 CRACKED. REPLACED ANGLE AT LT FS 484 FLOOR SUPPORT LBL 36.0 IAW REO 610R-53-41-059, STEPS 5-12 AND 14. PRESSURE LEAK CHECK DUE. PRESSURIZATION CHECKS GOOD IAW AMM 21-32-00-863-801. C/W EC/TC REO 601R-53-41-059.

Part: FLOOR SUPPORT — CRACKED (BS 484) · airframe 16,874 hrs · 14,035 cycles

LEFT FS 484 FLOOR SUPPORT ANGLE CRACKED AT LBL 9.0. REMOVED ANGLE IAW SRM 51-42-06. FABRICATED REPAIR ANGLE IAW 51-40-11 AND 51-42-06 SRM. REPLACED ANGLE ON FLOOR SUPPORT IAW SRM 51-24-36 AND 51-31-59.

Part: PANEL — CRACKED (FUSELAGE) · airframe 16,874 hrs · 14,035 cycles

OPERATION 76/PNL 444BT HAS A CRACK ABOUT 1 INCH LONG IN IT.

Part: PRIORITY VALVE — MALFUNCTIONED (MLG) · airframe 16,287 hrs · 13,493 cycles

AFTER T/O "GEAR DISAGREE WARNING MESSAGE. AIRCRAFT RETURNED TO CLE AFTER T/O. EMERGENCY DECLARED. REMOVED AND REPLACED NOSE LANDING GEAR PRIORITY VALVE IAW CRJ 200 AMM 32-30-01, OPS CHECK AND LEAK CHECK GOOD, DEFERRED CLEAR OK FOR SERVICE. (B)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 16,180 hrs · 13,403 cycles

2ND FROM THE FRONT EMERGENCY CEILING LIGHT INOP. REMOVED AND REPLACED LAMP IAW AMM 33-51-16 OPS CHECK GOOD. (B)

Part: PRIORITY VALVE — MALFUNCTIONED (NLG) · airframe 15,927 hrs · 13,180 cycles

AFTER T/O IN ATL - GEAR DISAGREE WARNING NOSE GEAR DID NOT RETRACT. RAN QRH, NOSE GEAR (AND MAINS) CAME DOWN AND LOCKED. AIRCRAFT RETURNED TO ATL AFTER T/O. EMERGENCY DECLARED. FLT 4785 DEL 137 MINS. REMOVED AND REPLACED NLG PRIORITY VALVE, LK AND OPS CHECKD GOOD. REMOVED AND REPLACED NLG SELECTOR VALVE, LEAK AND OPS CHECKED. REF CRJ MM 32-33-10. (B)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,889 hrs · 13,148 cycles

WHITE EMERGENCY EXIT LIGHT BY PAX DOOR HAS SEVERAL BULBS INOP. REMOVED AND REPLACED WHITE EMERGENCY EXIT LIGHT BULBS IAW CRJ 200 AMM 33-51-19. OPS CHECK GOOD. SDR CLOSED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,961 hrs · 12,396 cycles

DURING OPS TEST OF EMERG LIGHTING SYSTEM, THE FLOOR LEVEL EXIT LIGHTS AT THE LT/RT OVERING EXITS, FWD OF THE SERVICE DOOR, AND ON THE AFT FACE OF THE GALLEY ARE INOP, 4 LIGHTS TOTAL.

Part: SUPPORT BEAM — CRACKED (FUSELAGE) · airframe 14,949 hrs · 12,387 cycles

CARGO DOOR SUPPORT BEAM ANGLE THAT ATTACHES TO REAR PRESSURE BULKHEAD IS CRACKED APPROX .2 INCH IN LENGTH.

Part: UNKNOWN — UNKNOWN (NLG) · airframe 13,292 hrs · 11,100 cycles

NOSE GEAR DISAGREE W/N RETRACT AFTER T/O. A/C RETURNED TO ATL AFTER T/O. TOWER DECLARED EMERGENCY.

Part: UNKNOWN — UNKNOWN (NLG) · airframe 13,187 hrs · 11,029 cycles

AFTER T/O NOSE GEAR DISAGREE, NOSE GEAR SLOW TO RETRACT. A/C RETURNED TO ATL AFTER T/O. EMERGENCY DECLARED. FLTS 4278, 4648 CX.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,046 hrs · 10,915 cycles

AFT RIGHT EMERGENCY LIGHT INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,585 hrs · 10,573 cycles

FWD HALF OF CABIN LIGHTING INOP. (CABIN INTERIOR LIGHTS WITHOUT PHOTOLUMINESCENT FLOOR PROXIMITY EMERGENCY ESCAPE PATH MARKING SYSTEM STRIP/TAPE).

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,574 hrs · 10,565 cycles

LEFT SIDE FUSELAGE FWD EMERGENCY LIGHT INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,009 hrs · 10,141 cycles

EMERGENCY LIGHT ABOVE ROW 2 INOP.

Part: SKIN — CORRODED (BS 333) · airframe 11,933 hrs · 10,075 cycles

CORROSION FOUND BETWEEN STRINGER 26L AND STRINGER 26R AT FS 333.00 UNDER AVIONICS FLOORBOARD.

Part: ARM — CRACKED (TE FLAP) · airframe 11,933 hrs · 10,075 cycles

POSSIBLE CRACK ON RT OB FLAP NR 4 HINGE ARM FWD ATTACH POINT. LPI OR EDDY CURRENT INSPECTION REQUIRED FOR VERIFICATION. CRACKED AREA MARKED. (MTC) REMOVED AND REPLACED RIGHT OUTBOARD FLAP IAW CRJ200 AMM 27-54-05/JC7020945 (CLOSED)

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 11,933 hrs · 10,075 cycles

RT SIDE F.S. 484 INTERCOSTAL CRACKED (MTC)

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 11,933 hrs · 10,075 cycles

LT SIDE FS 484 INTERCOSTAL IS CRACKED (MTC)

Part: FLOOR SUPPORT — CORRODED (BS 280) · airframe 11,933 hrs · 10,075 cycles

FWD ANGLE AT FS 280 IS CORRODED. REMOVED FWD FLOOR SUPPORT ANGLE AT F/S 280 AND ORDERED/RECEIVED NEW ANGLE PN:600-34017-351 REF: CRJ200 SRM 51-42-06 PSP19749 12SEP06 (SUPPLEMENTAL-SDR CLOSED 9/20/06)

Part: FLOORBEAM — CRACKED (BS 280) · airframe 11,933 hrs · 10,075 cycles

IB FLOORBEAM TO FS 280 WEB CRACKED IB OF LBL 9 (MARKED). ALL WORK DONE IAW BOMBARDIER REO601R-53-11-926 CM20420. (CLOSED)

Part: ATTACH FITTING — CRACKED (BS 280) · airframe 11,933 hrs · 10,075 cycles

LT OB 280 CLIP IS CRACKED. ALL WORK DONE IAW BOMBARDIER REO 601R-53-11-926 JP21771) (CLOSED)

Part: ANGLE — CRACKED (BS 280) · airframe 11,933 hrs · 10,075 cycles

CRACK IN AFT ANGLE OF FS 280 OB OF LBL 9. ALL WORK DONE IAW BOMBARDIER REO601R-53- 11-926 CM20420 (CLOSED)

Part: ANGLE — CRACKED (BS 280) · airframe 11,933 hrs · 10,075 cycles

CRACK IN LWR ANGLE OF FS 280 CTR WEB OB OF RBL 9. ALL WORK DONE IAW BOMBARDIER REO601R-53-11-926 CM20420 (CLOSED)

Part: FLOORBEAM — CRACKED (BS 280) · airframe 11,933 hrs · 10,075 cycles

IB FLOORBEAM TO FS 280 ANGLE CRACKED IB OF RBL 9. ALL WORK DONE IAW BOMBARDIER REO601R-53-11-926 JP21771) (CLOSED/06)

Part: DOOR — NOT CLOSED (PAX DOOR) · airframe 11,505 hrs · 9,748 cycles

PAX DOOR WILL NOT FULLY CLOSE WHEN PASSENGERS ARE ON BOARD...FLT 4681 CX

Part: DOOR — MALFUNCTIONED (MAIN PAX) · airframe 11,479 hrs · 9,724 cycles

MAIN CABIN DOOR WILL NOT SHUT.

Part: DOOR — INOPERATIVE (MAIN PAX) · airframe 11,475 hrs · 9,721 cycles

FOUND MAIN CABIN DOOR WILL NOT SHUT.

Part: DOOR — MALFUNCTIONED (MAIN PAX) · airframe 11,454 hrs · 9,705 cycles

FOUND MAIN CABIN DOOR DOES NOT CLOSE PROPERLY. DOOR IS HARD TO PULL CLOSE AND SECURE, FLTS 4238 + 4828.

Part: DOOR — MALFUNCTIONED (MAIN PAX) · airframe 11,441 hrs · 9,694 cycles

MAIN PASSENGER DOOR WOULD NOT CLOSE PROPERLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,393 hrs · 9,658 cycles

EMERGENCY LIGHTS WILL NOT ARM AND WILL NOT ILLUMINATE DURING TEST NOR DOES THE STATUS MSG APPEAR ON THE EICAS WHEN SELECTED ON. FLT 4084 CX

Part: DOOR — UNKNOWN (PAX DOOR) · airframe 11,246 hrs · 9,538 cycles

PASSENGER DOOR DIFFICULT TO CLOSE FROM INSIDE AIRCRAFT AND VENT DOOR DOES NOT ALWAYS SEAT.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 11,246 hrs · 9,538 cycles

PILOT'S WINDSHIELD SHATTERED. (EMERGENCY VEHICLES DISPATCHED)

Part: DOOR — MALFUNCTIONED (CABIN) · airframe 11,189 hrs · 9,494 cycles

DIFFICULTY CLOSING MAIN CABIN DOOR, FLT 4610 DEL 60 MINS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,096 hrs · 9,425 cycles

FOUND EMERGENCY LIGHT ABOVE ROW 4 INOP.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

DURING A GROUND INSPECTION IN VPS, THE EMERGENCY CEILING LIGHT AT ROW 10 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY CEILING LIGHT AT ROW 10. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

DURING AN A-CHECK, THE RT FWD EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE RT FWD EXTERIOR EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE FS 280 LT CLIPS INBOARD AND OUTBOARD AT LBL 9 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE FS 280 LT CLIPS INBOARD AND OUTBOARD AT LBL 9. (M)

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE FS 280 RIGHT CLIPS INBOARD AND OUTBOARD AT RBL 9 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE FS 280 RT CLIPS INBOARD AND OUTBOARD AT RBL. (M)

Part: SUPPORT ANGLE — CRACKED (FUSELAGE)

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

Part: SUPPORT BEAM — CRACKED (FUSELAGE)

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

Part: PLATE — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE CARGO FLOOR LANDING PLATE AT FS 589 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO FLOOR LANDING PLATE AT FS 589 IAW ASA EO 600-53-0117. (M)

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE FS 625 LT/RT CLIPS WERE FOUND TO BE CRAKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE FS 625 LT/RT CLIPS. (M)

Part: SUPPORT BEAM — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 WAS FOUND TO CRACKED UNDER THE FIRE LOOP CLIP BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 IAW ASA EO 600-53-0072B. (M)

Part: SUPPORT BEAM — CRACKED (FUSELAGE)

DURING AN A-CHECK IN MCN, THE ENGINE SUPPORT BEAM AT BL 36.20 LEFT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE PERFORMED A TEMPORARY REPAIR TO THE ENGINE SUPPORT BEAM AT BL 36.20 LEFT IAW ASA EO 600-53-0071. (M)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

DURING HANGAR MAINTENANCE, THE LT EXTERIOR SECOND FROM THE FROM EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LT EXTERIOR SECOND FROM THE FRONT EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: BUSHING — MIGRATED (WING-FUSELAGE) · airframe 6,760 hrs

DURING DESCENT, AT APPROX 24,000 FT THE CREW HEARD A LOUD (BANG) FROM UNDER THE RT WING ROOT. ALL INDICATIONS WERE NORMAL INCLUDING THE FLIGHT CONTROLS AND DOORS. AN EMERGENCY WAS DECLARED WITH A NORMAL APPROACH AND LANDING ACCOMPLISHED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED AN INSPECTION OF THE RT MLG. NO DEFECTS WERE NOTED. MAINT ALSO INSPECTED THE RT WING ROOT FOR POSSIBLE MIGRATION OF THE WING TO FUSELAGE FITTING BUSHINGS IAW REO601R-57-21-407. THE REO ALLOWS FOR BUSHING MIGRATION, WHICH IS TENTATIVELY SCHEDULED FOR FEB 2005. THIS MRR WILL REMAIN OPEN PENDING PERFORMANCE OF THAT INSPECTION.

Part: STEP — CRACKED (FUSELAGE)

DURING A HANGAR INSPECTION IN MCN, THE LOWER STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE LOWER STEP ON THE PASSENGER DOOR. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: FITTING — CRACKED (FUSELAGE)

DURING A HANGAR INSPECTION, THE FORWARD PASSENGER DOOR CABLE ANCHOR FITTING WAS FOUND TO BE CRACKED. MAINTENANCE WILL MONITOR THE CRACK AND REPLACE DOOR CABLE ANCHOR FITTING WITHIN 100 FLIGHT HOURS IAW REO 601R-52-11-272. (M)