N933EV

Part: UNKNOWN — SMOKE · airframe 33,642 hrs · 32,193 cycles

SELECTOR PANEL BELOW FLIGHT ATTENDANT INTERPHONE PUSHED IN BEYOND THE HOUSING, FLIGHT ATTENDANT NOTICED MOMENTARY MINOR SMOKE WHICH SHORTLY THEREAFTER DISSIPATED. (FLT 5787, FILED CLOSED)REMOVED AND REPLACED ATTENDANT INTERPHONE HANDSET IN REF WITH CRJ200 AMM 23-31-10. OPS CHECK GOOD AT THIS TIME. A/C OK FOR CONTINUED SERVICE.

Part: UNKNOWN — DAMAGED (UNKNOWN) · airframe 33,604 hrs · 32,145 cycles

COMPLY WITH REPAIR AUTHORIZATION: RA81748-601R-53-11-3816 N933EV,MXCODEID65355-PR - DAMAGED SCREW HOLE TO ACCESS DOOR SURROUND STRUCTURE FOR ACCESS PANEL 131AL INSTALLATION. COMPLIED WITH TEMPORARY DISPOSITION IAW REO 601R-53-11-3816 DATED: 2022-12-18 REV -- "THE SUBJECT CONDITION IS STRUCTURALLY ACCEPTABLE FOR 600 FLIGHT HOURS FROM THE TIME OF INCORPORATION OF THIS REO AT REV --" PERFORM PERMENANT REPAIR OF ACCESS PANEL 131AL SURROUND STRUCTURE, PART NUMBER: , SERIAL NUMBER: , POSITION: THIS PERMANENT REPAIR HAS BEEN DETERMINED TO BE A MAJOR REPAIR PER GMM 3-26 "FATIGUE CRITICAL BASELINE STRUCTURE". M-337 FORM REQUIRED. (FILED CLOSED)COMPLIED WITH PERMANENT REPAIR INSTALLATION OF FREEZE PLUG TO FUSELAGE ACCES PANEL 131AL CUTOUT @3'OCLOCK POSITION REF REO 601R-53-11-162 REV D DATE 2019-02-05. COMPLIED WITH STRUCTURAL MAJOR REPAIR RII 51-90-1003-SKY.

Part: NONE — WARNING MESSAGE · airframe 33,226 hrs · 31,791 cycles

ON THE MISSED APPROACH, AFTER SELECTING GEAR UP, GOT A GEAR DISAGREE WARNING & NLG INDICATOR RED. RAN QRH PROCEDURE. GEAR SELECTED DOWN IAW CHECKLIST, GOT 3 GREEN INDICATORS. NO LIMITATIONS EXCEEDED. AIRCRAFT IS DOWNGRADED FROM CAT II STATUS. FOUND ASSOCIATED B1 CODES TO BE 007451, 007416 & 007437. TROUBLESHOT FIM 32-21-00 AND 32-61-05. FOUND NLG DOWN SNSR PX21 GAP OUT OF ADJUST AT 0.021. INSPECTED BRACKET & FOUND NO DEFECTS. ADJUSTED PX21 GAP TO CORRECT GAP (0.045). FOUND NG UP SNSR PX22 GAP OUT OF ADJUST AT 0.024. INPSECTED BRACKET & FOUND NO DEFECTS. ADJUSTED SENSOR PX22 TO PROPER GAP. PERFORMED OPS TEST OF MLG EXTENSION/RETRACTION SYS IAW AMM 32-30-00. OP TESTED GOOD.

Part: NONE — CRACKED · airframe 32,259 hrs · 30,909 cycles

BATT RIB CHANNEL CRACKED AT LHS WS 53.60. (C-CHECK RO 6/1/2022) REPAIRED BATT RIB CHANNEL CRACK AT LHS WS 53.60.REF REO 601R-57-51-046 REV B DATED 2002-02-28.C/W 51-900-1003-SKY

Part: NONE — CRACKED · airframe 32,259 hrs · 30,909 cycles

BATT RIB FWD ANGLE CRACKED AT LHS WS48.30. (C-CHECK RO 6/1/2022) REMOVED AND REPLACED DAMAGED ANGLE P/N 600-10204-27 REF CRJ200 SRM 51-42-21, 51-42-06, BOMBARDIER ENG DWG 600-10204 REV M COMPLIED WITH 51-900-1003 SKY

Part: NONE — SHIFTED · airframe 32,259 hrs · 30,909 cycles

LH MLG TRUNNION AFT FORCE MATE BUSHING IS MIGRATED .010 THE PN FOR LH MLG TRUNNION IS 601R10068-1 (C-CHECK RO 6/1/2022) REPLACE LH MLG TRUNNION AFT BUSHING PER REO 601R-57-21-3588 REV --, DATED 2022-05-10. SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: NONE — CRACKED · airframe 32,259 hrs · 30,909 cycles

FRAME AT FS333 STRINGER 1L CRACKED. (C-CHECK RO 6/1/2022) REMOVED AND REPLACED FRAME SECTOR AT FS333 STRINGER 1L REF DWG 601R31016 REV C, DWG 601R31522 REV AC, DWG 601R32004 REV N. CRJ 200 SRM 51-42-06 & CRJ 200 SRM 51-42-21. COMPLIED WITH SKYWEST TASK CAD 51-900-1003-SKY.PRESSURE LEAK CHECK GOOD AT THIS TIME.

Part: NONE — CORRODED · airframe 32,259 hrs · 30,909 cycles

CORROSION FOUND AT FS 349.00 CROSSBEAM TOP CAP BETWEEN LBL27-LBL36. (C-CHECK RO 6/1/2022) REPAIRED CORROSION FOUND AT FS 349.00 CROSSBEAM TOP CAP BETWEEN LBL27-LBL36. REF DWG 601R38673 REV D, CRJ200 SRM 51-42-21, CRJ200 SRM 51-42-06, AND CRJ200 SRM 51-42-13. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: NONE — CRACKED · airframe 32,259 hrs · 30,909 cycles

LH WINDSHIELD LOWER SIDE POST SUPPORT AT FS236.75, WL103.90 IS CRACKED. (MARKED) (C-CHECK RO 6/1/2022) REPLACED LH WINDSHIELD LOWER SIDE POST SUPPORT AT FS236.75, WL 103.90 PER CRJ200 SRM 51-42-06 & DRAWING 601R34032 REV P. CHECKS GOOD. SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: NONE — CRACKED · airframe 32,259 hrs · 30,909 cycles

RH WINDSHIELD LOWER SIDE POST SUPPORT AT FS236.75, WL103.90 IS CRACKED. (MARKED) (C-CHECK RO 6/1/2022) REMOVED AND INSTALLED NEW SUPPORT ANGLE AT R/H WINDSHIELD POST AT FS236.75 AND WL103.90 REF CRJ200 SRM 51-42-06 AND DWG 601R34032 REV P. COMPLIED WITH TASK CARD 51-900-1003-SKY. LEAK CHECK GOOD. SEE CONTINUE CARD FOR DETAILS.

Part: NONE — OUT OF TOLERANCE · airframe 32,259 hrs · 30,909 cycles

WHILE COMPLYING WITH SB 601R-57-046 REV C PART E (LH) AND PART F (RH) O/S FASTENERS WERE FOUND AT HOLE #14 BOTH LH AND RH SIDE. (FASTENER TYPE IS HST411AG-10), (HOLE DIA. IS .3400") WITH NO DEFECTS NOTED. (C-CHECK RO 6/1/2022) REPAIRED HOLE #14 BOTH LHS AND RHS PER REO 601R-57-21-3584 REV -- DATE 2022-04-14 (LHS) AND REO 601R-57-21-3585 REV -- DATE 2022-04-14 (RHS) C/W 51-900-1003-SKY

Part: NONE — CRACKED · airframe 32,259 hrs · 30,909 cycles

PAX DOOR HAS CRACK AT UPPER INTERCOSTAL INSIDE ACCESS PANEL LOCATION 832BR. (C-CHECK RO 6/1/2022) INSTALLED REPLACEMENT INTERCOSTAL P/N 601R31902-318 AT PAX DOOR INNER STRUCTURE BETWEEN FS.338 & FS.349 REF. CRJ200 SRM 51-42-06 & BOMBARD. DWG. 601R31702 REV. -N. COMPLIED WITH TASK CARD 51-900-1003-SKY. SEE CONTINUATION CARD FOR MAINTENANCE PERFORMED.

Part: NONE — CRACKED · airframe 32,259 hrs · 30,909 cycles

FS 280 RBL 9.0 INBOARD CLIP IS CRACKED. (C-CHECK RO 6/1/2022) REMOVED AND REPLACED 1EA. CLIP AT FS 280.00 RBL 9 IAW CRJ 200 SRM 51-42-21. REVISION 38, DATED JUL10/2019, REO 601R-53-11-926 REV-B DATED 2006-05-10. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY.

Part: NONE — CORRODED · airframe 32,259 hrs · 30,909 cycles

INTERNAL FUSELAGE FS 310.0 JUST AFT OF RBL 7.0 GALLEY MOUNT HAS CORROSION. (C-CHECK RO 6/1/2022) REMOVED AND INSTALLED NEW MOUNT PLATE PN# 601R38669-121 REF DWG 601R38669 REV-N AND CRJ200 SRM 51-42-06. RESTORED FINISH. COMPLIED WITH TASK CARD 51-900-1003-SKY. SEE CONTINUE CARD FOR DETAILS.

Part: NONE — CRACKED · airframe 32,259 hrs · 30,909 cycles

FS 280 RBL 9.0 OUT BOARD CLIP IS CRACKED (C-CHECK RO 6/1/2022) REMOVED AND REPLACED 1EA. CLIP AT FS 280.00 RBL 9 IAW CRJ 200 SRM 51-42-21. REVISION 38, DATED JUL10/2019. CRJ200 SRM 51-40-11 REVISION 38, DATED JUL10/2019, REO 601R-53-11-926 REV-B DATED 2006-05-10. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY.

Part: NONE — CORRODED · airframe 32,259 hrs · 30,909 cycles

INTERNAL FUSELAGE FS 310.0 JUST FWD AND INB OF LBL 27 WARDROBE MOUNT HAS CORROSION. (C-CHECK RO 6/1/2022) REMOVED INSTALLED NEW WARDROBE MOUNT PLATE P/N 601R38670-31 WITH NEW HARDWARE. FS310.00 FWD AND IN/BD OF LBL27 REF DWG 601R38670 REV T AND CRJ200 SRM 51-42-10. COMPLIED WITH TASK CARD 51-900-1003-SKY

Part: NONE — CRACKED · airframe 32,259 hrs · 30,909 cycles

AFT EQUIPTMENT BAY L/H SIDE FS 625 CLIP AT STR 14 IS CRACKED. (C-CHECK RO 6/1/2022) REMOVED AND INSTALLED NEW FS625 STGR14L CLIP REF DWG 601-35012 REV-B AND CRJ 200 SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1003-SKY. SEE CONTINUE CARD FOR DETAILS.

Part: NONE — CRACKED · airframe 32,259 hrs · 30,909 cycles

FS 280.0 LBL9.0 INBOARD CLIP IS CRACKED. (C-CHECK RO 6/1/2022) REMOVED, FABRICATED, LOCATED, DRILLED, AND INSTALLED NEW FS280 LBL9 INBD CLIP REF PREVIOUSLY INCORPERATED REO 601R-53-11-171, REV -D, DATED 13-FEB-07. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: NONE — CRACKED · airframe 32,259 hrs · 30,909 cycles

L/H SIDE LBL 27.0 AT FS 484.0 INBOARD CLIP IS CRACKED. (C-CHECK RO 6/1/2022) REMOVED THE CLIP AT LBL 27, FS484.00 AND REPLACED WITH NEW IAW CRJ200 51-42-06, AND CRJ200 SRM 51-42-21 AND DWG 601R31171 REV-B. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: NONE — CRACKED · airframe 32,259 hrs · 30,909 cycles

AFT EQUIPTMENT BAY R/H SIDE FS 625 CLIP AT STR 14R IS CRACKED. (C-CHECK RO 6/1/2022) REMOVED AND INSTALLED NEW FS625 STGR14R CLIP REF DWG 601-35012 REV-B AND CRJ 200 SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1003-SKY. SEE CONTINUE CARD FOR DETAILS.

Part: NONE — CRACKED · airframe 32,259 hrs · 30,909 cycles

FS 280 LBL 9.0 OUT BOARD CLIP IS CRACKED. (C-CHECK RO 6/1/2022) REMOVED, FABRICATED, LOCATED, DRILLED, AND INSTALLED NEW FS280 LBL9 OTBD CLIP REF PREVIOUSLY INCORPERATED REO 601R-53-11-171, REV -D, DATED 13-FEB-07. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: NONE — CORRODED · airframe 32,259 hrs · 30,909 cycles

RH PRESSURE FLOOR SILL PANEL HAS SPOTS OF CORROSION AT FS.409.00. + 128 TO FS.559.00. (MARKED) (C-CHECK RO 6/1/2022) REMOVED CORROSION ON RH PRESSURE FLOOR SILL PANEL HAS 8 SPOTS AT. FS. 409.00+128 TO FS559.00 REF. REO #601R-53-41-666 REV.-C DATED 2012-11-06. COMPLIED WITH TASK CARD 51-900-1003-SKY. SEE CONTINUATION CARD FOR MAINTENANCE PERFORMED.

Part: NONE — CRACKED · airframe 32,259 hrs · 30,909 cycles

L/H SIDE FS 625 CLIP IS CRACKED AT STR 15L (C-CHECK RO 6/1/2022) REMOVED AND INSTALLED NEW FS625 STGR15L CLIP REF DWG 601-35012 REV-B, CRJ200 SRM 51-42-21 AND CRJ 200 SRM 51-42-06. RESTORED FINISH. COMPLIED WITH TASK CARD 51-900-1003-SKY. SEE CONTINUE CARD FOR DETAILS.

Part: NONE — CORRODED · airframe 32,259 hrs · 30,909 cycles

* LH PRESSURE FLOOR SILL HAS SPOTS OF CORROSION AT LBL36 AND APPOX. FS. 484.00 (MARKED). (C-CHECK RO 6/1/2022) REMOVED CORROSION ON LH PRESSURE FLOOR SILL FROM 2 SPOTS AT LBL36 AND APPOX. FS. 484.00 REF CRJ200 SRM 51-21-06. EVALUATED AND FOUND TO BE WITH LIMITS REF REO 601R-53-41-3030 REV -- DATED 2022-04-19 (ALL STEPS COMPLIED WITH) AND REO 601R-53-41-666 REV C DATED 2012-11-06. RESTORED FINISH. COMPLIED WITH TASK CARD 51-900-1003-SKY. SEE CONTINUE CARD FOR DETAILS.

Part: NONE — CORRODED · airframe 32,259 hrs · 30,909 cycles

* FLOOR BOARD SUPPORT ANGLE AT FS.621.00 BETWEEN RBL9 AND RBL27 HAS A SPOTS OF CORRSIOIN (MARKED). (C-CHECK RO 6/1/2022) INSTALLED NEW FLOOR BOARD SUPPORT ANGLE AT FS.621.00 BETWEEN RBL9 AND RBL27.REF REO 601R-53-61-3780 REV -A DATE 2011-07-15, REO 601R-53-61-3778 REV B DATED 2016-12-19, DWG. 601R35031 REV AG, CRJ 200 SRM 51-42-06 & 51-42-21. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: NONE — CORRODED · airframe 32,259 hrs · 30,909 cycles

* THE RH WING LOWER SKIN'S EXTERNAL SURFACE HAS A SMALL SPOT OF SURFACE CORROSION AT RBL 45, WHERE ACCESS PANEL 193AB MEETS THE WING'S TRAILING EDGE. (C-CHECK RO 6/1/2022) REMOVED THE CORROSION WHERE PANEL 193AB MEETS THE R/H WING TRAILING EDGE AT RBL 45, BLENDED TO A SMOOTH CONTOUR, EVALUATED AND FOUND TO BE WITH-IN LIMITS, RESTORED THE FINISH, AND RESTORED THE SELF CONTOURING SEALANT PAD REF BOMBARDIER REO 601R-57-21-880 REV D DATED 2017/03/06 ( STEPS 1-10 COMPLIED WITH). COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: NONE — CRACKED · airframe 32,259 hrs · 30,909 cycles

* R/H WINDSHIELD SIDE POST SUPPORT CRACKED. (C-CHECK RO 6/1/2022) REMOVED AND REPLACED CRACKED R/H WINDSHIELD SIDE POST SUPPORT FITTING WITH NEW REF. CRJ 200 SRM 51-42-21 AND DWG #601R33007 REV -U. COMPLIED SKYWEST CARD 51-900-1003-SKY AND FORM M-337.

Part: NONE — CRACKED · airframe 32,259 hrs · 30,909 cycles

* L/H WINDSHIELD SIDE POST SUPPORT CRACKED. (C-CHECK RO 6/1/2022) REMOVED AND REPLACED L/H WINDSHIELD SIDE POST SUPPORT REF. CRJ200 SRM 51-42-21 AND DWG 601R33007 REV -U. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: NONE — GOUGED · airframe 32,259 hrs · 30,909 cycles

L/H WING - FWD FACE OF FWD SPAR HAS A GOUGE TO BARE METAL - WS 389L (C-CHECK RO 6/1/2022) REPAIRED L/H WING - FWD FACE OF FWD SPAR REF REO 601R-57-21-3586 REV -- DATED 2022-04-15. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY.

Part: NONE — CHAFED · airframe 32,259 hrs · 30,909 cycles

*LH AILERON ASSY UPPER LEADING-EDGE SKIN CHAFFED MULTIPLE AREAS ALONG ENTIRE WIDTH (MARKED) (C-CHECK RO 6/1/2022) REMOVED AND REPLACED LH AILERON ASSY UPPER LEADING-EDGE SKIN REF DWG CC670-13000 REV-D, CRJ200 SRM 51-42-21, CRJ200 SRM 51-42-22, AND CRJ200 SRM 51-42-06. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY.

Part: NONE — GOUGED · airframe 32,259 hrs · 30,909 cycles

* THE MAIN AVIONICS COMPARTMENT DOOR'S HANDLE HOUSING HAS GOUGES FROM CONTACT WITH THE HANDLE ASSY, AND SURFACE CORROSION NEAR ITS MID POINT ON THE RH SIDE OF THE HANDLE CUTOUT. (C-CHECK RO 6/1/2022) INSTALLED NEW AVNX COMPARTMENT DOOR HANDLE ASSY REF CRJ200 SRM 51-42-06, CRJ 200 AMM 52-42-03 AND DWG 601R31050 REV AD, ALL CHECKS GOOD. COMPLIED WITH TASK CARD 51-900-1003-SKY. SEE CONTINUATION CARD FOR MAINTENANCE PERFORMED.

Part: NONE — GOUGED · airframe 32,259 hrs · 30,909 cycles

* THE CARGO DOOR'S EXTERNAL HANDLE HOUSING HAS SMALL GOUGES FROM CONTACT WITH THE HANDLE ASSY. (C-CHECK RO 6/1/2022) REMOVED AND INSTALLED NEW CARGO DOOR HANDLE HOUSING REF CRJ200 SRM 51-42-21 AND DWG 601R35027 REV-AY. COMPLIED WITH TASK CARD 51-900-1003-SKY. LEAK CHECK GOOD. SEE CONTINUE CARD FOR DETAILS.

Part: NONE — CHAFED · airframe 32,259 hrs · 30,909 cycles

* THE CARGO DOOR'S EXTERNAL SKIN HAS CHAFES AND SCRATCHES ALONG THE TOP EDGE NEAR IT'S CENTERLINE. (C-CHECK RO 6/1/2022) REPAIRED THE CARGO DOOR'S EXTERNAL SKIN CHAFES AND SCRATCHES ALONG THE TOP EDGE NEAR IT'S CENTERLINE REF REO 601R-52-31-396 REV -- DATED 2022-04-26 LEAK CHECK GOOD C/W 51-900-1003-SKY

Part: NONE — CRACKED · airframe 32,259 hrs · 30,909 cycles

COMPLY WITH SCHEDULED MAINTENANCE CODE: AD 2019-08-04/02 40000 FC - COMPLY WITH PARAGRAPH (J) OF AD 2019-08-04 BY: (J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION (FS) 621 PRESSURE BULKHEAD, IN ACCORDANCE WITH AWL 53-61-153 OF BOMBARDIER TR 2B-2187, DATED JUNE 22, 2011, TO APPENDIX B€“AIRWORTHINESS LIMITATIONS, OF PART 2 OF THE BOMBARDIER CL-600-2B19 MRM. (J)(2) MODIFYING THE RPB AND DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FS 621 PRESSURE BULKHEAD WEB, IN ACCORDANCE WITH BOMBARDIER REPAIR ENGINEERING ORDER (REO) 601R-53-61-1240, REVISION D, DATED OCTOBER 31, 2016. 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: 8022, POSITION: (C-CHECK RO 6/1/2022) COMPLIED WITH PARAGRAPH (J) OF AD 2019-08-04 BY: / (J)(2) MODIFYING THE RPB AND DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FS 621 PRESSURE BULKHEAD WEB, IN ACCORDANCE WITH BOMBARDIER REPAIR ENGINEERING ORDER (REO) 601R-53-61-1240, REVISION D, DATED OCTOBER 31, 2016. / AND; / MARKING THIS CAMP AS "STRUCTURAL REPAIR," WHICH WILL GENERATE AN RA FOR TRACKING THE SDIR FOR THIS REO ON THIS AIRPLANE. / COMPLIED WITH SERIAL NUMBER 8022. / C/W TASK CARD 51-900-1003-SKY

Part: NONE — DAMAGED · airframe 32,259 hrs · 30,909 cycles

COMPLY WITH REO 601R-53-41-1116 REPAIR & REINFORCEMENT FOR FS 559.00 LWR CAP ANGLES BL 9.00 & 18.00 LHS & RHS (C-CHECK RO 6/1/2022) COMPLIED WITH REPAIR & REINFORCEMENT FOR FS 559.00 LWR CAP ANGLES BL 9.00 & 18.00 LHS & RHS REF REO 601R-53-41-1116 REV C DATED 2017/03/09. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: SELECTOR VALVE — FAILED (MLG) · airframe 31,459 hrs · 30,215 cycles

RECEIVED GEAR DISAGREE WARNING MESSAGE AFTER SELECTING GEAR DOWN FOR LANDING. RAN QRH, LANDING GEAR EXTENDED WITH MANUAL RELEASE. (FLIGHT 5325 - FILED CLOSED) TROUBLESHOT GEAR DISAGREE WARNING MESSAGE PER CRJ200 FIM 32-60-00. REMOVED AND REPLACED MLG SELECTOR VALVE IN REFERENCE TO CRJ200 AMM 32-32-10. OPS CHECK AND LEAK CHECK GOOD. AC OKAY FOR RETURN TO SERVICE.

Part: WINDSHIELD — CRACKED (COCKPIT RT) · airframe 31,012 hrs · 29,823 cycles

TRANSFER FROM EAML 667907 : RIGHT WINDSHIELD CRACKED UPON PARKING AT GATE (FLIGHT 5076 - FILED CLOSED) REMOVED AND REPLACED RH WINDSHIELD IAW AMM 56-11-01 AND COMPLIED WITH TASK CARD 56-220-1000-SKY. OPS AND LEAK CHECK GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (MULTIPLE) · airframe 27,146 hrs · 26,355 cycles

HIT SEVERE TURBULENCE. RECEIVED R/L ENG OIL WARNING MESSAGES AND AP PITCH TRIM, STAB TRIM, MACH TRIM CAUTION MESSAGES. (FLT#5975) PER AMM FOR SEVERE TURBULENCE EVENT PERFORMED FDR DOWNLOAD REFERENCE. DATA ANALYSIS SHOWED AN AIRCRAFT INSPECTION REQUIRED. COMPLIED WITH INSPECTION. OPS CHECKS OF AP PTCH TRIM, MACH TRIM, AND STAB TRIM. R/L ENG OIL WARNINGS ARE DUE TO THE RESULT OF LUBE SYSTEM STACK UP CONDITION ENCOUNTERED DURING SEVERE TURBULENCE EVENT.

Part: FRAME — CORRODED (FUSELAGE) · airframe 26,721 hrs · 25,976 cycles

FS 559.00 + 96 FRAME CORRODED ON FWD SIDE NEAR STR 27. (C-CHECK) RO: 02/12/2019 PERFORMED REPAIR AT FS559.00+96 FRAME IAW SRM. PERFORMED LEAK CHECK IAW AMM, NO LEAKS NOTED.

Part: SKIN — CORRODED (LT WING) · airframe 26,721 hrs · 25,976 cycles

LANDING AT LT WING PLANK CUTOUT FOR ACCESS PANEL 550HB HAS PITTING CORROSION. (C-CHECK) RO: 02/12/2019 COMPLIED WITH PERMANENT REPAIR LT WING PLANK CUTOUT FOR ACCESS PANEL 550HB IAW REO. ALL CHECKS OKAY.

Part: STRAP — CORRODED (FUSELAGE) · airframe 26,721 hrs · 25,976 cycles

RT FLOOR SUPPORT STRAP AT FS 559.00 BETWEEN RBL 27.0 AND RBL 42.0 CORRODED. (C-CHECK) RO: 02/12/2019 REMOVED AND REPLACED FLOOR STRAP AT FS559 RBL27-42, REF SRM. ALL CHECKS OKAY.

Part: FRAME — CORRODED (FUSELAGE) · airframe 26,721 hrs · 25,976 cycles

FS 605.00 FRAME CORRODED FWD SIDE BETWEEN STR 27 AND 21L.(C-CHECK) RO: 02/12/2019 REMOVED AND INSTALLED NEW FRAME SEGMENT AT FS 605 FROM STRINGER 20 L TO 20R IAW SRM AND REO.

Part: PANEL — CORRODED (FUSELAGE) · airframe 26,721 hrs · 25,976 cycles

R/H PRESSURE FLOOR SILL PANEL HAS CORROSION AT MULTIPLE PLACES BETWEEN FS 409.00 + 128 AND FS 559.00. (C-CHECK) RO: 02/12/2019 REMOVED CORROSION ON MULTIPLE AREAS OF RT PRESSURE FLOOR SILL PANEL IAW SRM. COMPLIED WITH ALL STEPS IAW REO. PRESSURE CHECK GOOD.

Part: DOOR SILL — GOUGED (FUSELAGE) · airframe 26,721 hrs · 25,976 cycles

CARGO DOOR LOWER SILL HAS SEVERAL GOUGES BETWEEN FS 574.00 AND FS 621.00. (C-CHECK) RO: 02/12/2019 REMOVED AND REPLACED CARGO SILL IAW SRM AND REO.

Part: STRAP — CORRODED (FUSELAGE) · airframe 26,721 hrs · 25,976 cycles

LT FLOOR SUPPORT STRAP AT FS 559.00 BETWEEN LBL 27.0 AND LBL 42.0 CORRODED. (C-CHECK) RO: 02/12/2019 REMOVED AND REPLACED DAMAGED LT FLOOR SUPPORT STRAP P/N 601R31025-29 AT FS 559.00 BETWEEN LBL 27.0 AND LBL 42.0 IAW REO.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 26,721 hrs · 25,976 cycles

FORWARD FACE 621 BULKHEAD HAS MULTIPLE CHAFES AT LBL 9 18 27 35 AND RBL 9 18 27 35. (C-CHECK) RO: 02/12/2019 COMPLIED WITH PERMANENT REPAIR 621 CHAFES IAW REO.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 26,721 hrs · 25,976 cycles

FORWARD FACE 621 BULKHEAD SEVERAL CHAFES ON Z ANGLE AT LBL 18 AND RBL 18, 27. (C-CHECK) RO: 02/12/2019 COMPLIED WITH PERMANENT REPAIR 621 Z ANGLE, IAW REO.

Part: ATTACH FITTING — CHAFED (FUSELAGE) · airframe 26,721 hrs · 25,976 cycles

THE FLOORBEAM ATTACHMENT TO THE REAR PRESSURE BULKHEAD FOR RBL 9.0 HAS A CHAFED SPOT ON ITS UPPER OUTBOARD FLANGE AT APPROX FS 619. (C-CHECK) RO: 02/12/2019 COMPLIED WITH REO.

Part: SKIN — DENTED (FUSELAGE) · airframe 26,721 hrs · 25,976 cycles

DENT IN FUSELAGE SKIN BETWEEN STGR23L & STGR24L JUST FORWARD OF FRAME FS265.00. (C-CHECK) RO: 02/12/2019 COMPLIED WITH ALL STEPS OF REPAIR IAW REO.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 26,721 hrs · 25,976 cycles

FLOOR FRAME, FS349.00, AT THE SERVICE DOOR LOWER SILL IS CORRODED. (C-CHECK) RO: 02/12/2019 REPAIRED CORRODED FLOOR FRAME AT SERVICE DOOR, FS349.00 IAW REO.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 26,721 hrs · 25,976 cycles

SUPPORT ANGLE AT FS349 FOR WINDSCREEN SUPPORT STRUCTURE FOUND CORRODED. (C-CHECK) RO: 02/12/2019. REMOVED AND INSTALLED NEW ANGLE P/N 601R38783-13, IAW SRM.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 25,570 hrs · 24,928 cycles

RECEIVED A GEAR DISAGREE WARNING MESSAGE WHEN WE LOWERED GEAR AT 210 KNOTS WITH FLAPS UP. IT CLEARED ON ITS OWN WHILE THE GEAR WAS COMING DOWN. (FLT 5073) CLOSED PERFORMED A DETAILED INSPECTION OF THE LANDING GEAR HARNESSES. NO DEFECTS NOTED AT THIS TIME. PERFORMED NUMEROUS LANDING GEAR EXTENSIONS/RETRACTION IAW AMM. NO FAULTS AT THIS TIME.

Part: FLOORBEAM — GOUGED (BS 618) · airframe 25,342 hrs · 24,721 cycles

TWO GOUGES ON THE FLOORBEAM AT LBL 27 AND BS 618 ON INBD AND OTBD FLANGES. PERFORMED A TEMPORARY REPAIR IAW REO.

Part: STRUT — DISCHARGED (NLG) · airframe 24,419 hrs · 23,890 cycles

GEAR DISAGREE AFTER TAKE OFF. NLG DID NOT COME UP. SERVICED THE NOSE LANDING GEAR STRUT AND REPLACED THE SCHRADER VALVE IAW AMM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 24,315 hrs · 23,795 cycles

LOWER ANGLE OF CARGO DOOR SUPPORT BEAM THAT ATTACHES TO REAR PRESSURE BULKHEAD IS CRACKED APPROX .500 LONG. (C-CHECK) REMOVED AND REPLACED ANGLE IAW SRM.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 24,315 hrs · 23,795 cycles

REAR PRESSURE BULKHEAD WEB FWD FACE HAS 7 CHAFED AREAS .200 LONG BY .200 WIDE APPROX .003 DEEP WL105 AT LBL27.50, LBL18, I/B OF LBL9.50, I/B OF RBL9.50 RBL18, RBL27.50 & RBL36.20. (C-CHECK) REPAIRED DAMAGE IAW REO.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 23,089 hrs · 22,400 cycles

PAX CALL INDICATOR LIGHT ON CABIN OVERHEAD EXIT SIGN INOPERATIVE. REMOVED AND REPLACED THE EXIT SIGN INDICATION LIGHTS IAW AMM 33-51-14. OPS CHECKED GOOD.

Part: SKIN — CRACKED (PAX DOOR) · airframe 22,360 hrs · 21,568 cycles

PAX DOOR SKIN IS CRACKED BEHIND AFT COUNTER BALANCE PULLY MOUNT. COMPLIED WITH EC/TC REO 601R-52-11-702 AND MET ALL REQUIREMENTS OF REO 601R-52-11-702, REV C, MCO CLEARED. COMPLIED WITH ECTC REO 601R-52-11-702 AND NOT ALL THE REQUIREMENTS OF REO 601R-52-11-702 REV C.

Part: INTERCOSTAL — CRACKED (BS 621-625) · airframe 22,360 hrs · 21,568 cycles

INTERCOSTAL AT STRINGER 15L AND BS 621-625 IS CRACKED. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-42-21, 51-42-22, AND DWG 601R-350121.

Part: INTERCOSTAL — CRACKED (BS 623) · airframe 22,360 hrs · 21,568 cycles

INTERCOSTAL CRACKED AT FS 623, STRINGER 14L, LBL 51. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-42-21 & 51-42-22.

Part: STIFFENER — CRACKED (BS 185) · airframe 22,360 hrs · 21,568 cycles

CRACK WAS DISCOVERED IN STIFFENER AT BS 185, RBL 13.7. WHEN DAMAGE SKIN PANEL WAS REMOVED. REMOVED 2 STIFFENER AT FS 185, RBL 13.7, I ORDERED NEW STIFFENER IAW SRM 51-42-06, SRM 51-42-21. DRILLED AND INSTALL NEW 2-STIFFNER AT FS 185, RBL 13.7 IAW SRM 51-42-06 AND 51-42-21.

Part: INTERCOSTAL — CRACKED (BS 623) · airframe 22,360 hrs · 21,568 cycles

INTERCOSTAL CRACKED AT BS 623, STRINGER 15L, LBL51. INSTALLED A NEW INTERCOSTAL IAW SRM 51-42-21, 51-42-22, AND DWG 601R350121.

Part: ANGLE — CORRODED (BS 623) · airframe 22,360 hrs · 21,568 cycles

ANGLE CRACKED AT BS 623, STRINGER 15R, RBL 51. R & R THE ANGLE IAW SRM 51-42-06.

Part: ANGLE — CRACKED (BS 625) · airframe 22,360 hrs · 21,568 cycles

ANGLE CRACKED AT BS 625.30, STRINGER 14R, RBL 45. R & R THE ANGLE IAW SRM 51-42-06, AND DWG -601-35012.

Part: SEAT TRACK — CORRODED (BS 449-499) · airframe 22,360 hrs · 21,568 cycles

LEFT SIDE SEAT TRACK FROM BS 449-499 HAS CORROSION. R & R SEAT TRACK AT FS449-499 IAW AMM 53-01-11-000-802 AND 53-01-11-400-802. C

Part: SEAT TRACK — CORRODED (BS 499-544) · airframe 22,360 hrs · 21,568 cycles

RIGHT SIDE SEAT RAIL FROM FS 499-544 HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802, AND AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 559-574) · airframe 22,360 hrs · 21,568 cycles

RIGHT SEAT TRACK FROM FS 559+112-574, RBL 18 HAS CORROSION. EVALUATED SEAT TRACK RT FLOOR FROM FS 559+112-574, RBL18 OUT OF LIMITS IAW SRM 53-61-49. REMOVED IAW SRM 53-00-49. INSTALLED NEW FABRICATED SEAT TRACK RT FLOOR FS 559+112-574, RBL18 IAW AMM 53-00-49-400-801. COMPLIED WITH EC/TC ROE 601R-53-00-485.

Part: SEAT TRACK — CORRODED (BS 544-559) · airframe 22,360 hrs · 21,568 cycles

RT SIDE SEAT TRACK FROM BS 544-559+112 HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802, AND AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 22,360 hrs · 21,568 cycles

LEFT FLOOR SEAT TRACK FROM FS 409+112-559 HAS CORROSION. COMPLIED WITH ECTC REO 601R-53-00485. FABRCATED SEAT TRACKS IAW GREO 601R-53-00-485, REV A. REMOVED SEAT TRACK AT FS 409-408+112-559 IAW AMM 53-01-11-000-802. INSTALLED NEW FABRICATED SEAT TRACK IAW AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 544-559) · airframe 22,360 hrs · 21,568 cycles

LEFT SIDE SEAT TRACK CORRODED FROM BS 544-559+112 CORRODED. R & R THE SEAT TRACK IAW AMM 53-01-11-000-802, AND AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 364-394) · airframe 22,360 hrs · 21,568 cycles

LT FLOOR SEAT TRACK FROM FS 364-394 HAS CORROSION. COMPLIED WITH ECTC REO 601R-53-00-485, FABRICATED SEAT RAILS IAW GREO 601R-53-00-485, REV A. REMOVED SEAT RAILS IAW AMM 53-01-11-000-802. REPLACED SEAT RAIL IAW AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 394-409) · airframe 22,360 hrs · 21,568 cycles

LT FLOOR SEAT TRACK FROM FS 394-409 HAS CORROSION. COMPLIED WITH ECTC REO 601R-53-00-485, FABRICATED SEAT RAILS IAW GREO 601R-53-00-485, REV A. REMOVED SEAT RAILS IAW AMM 53-01-11-000-802. REPLACED SEAT RAIL IAW AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 22,360 hrs · 21,568 cycles

LEFT SEAT TRACK FROM FS 559+80-559+96, LBL 9 HAS CORROSION. COMPLIED WITH ECTC REO 601R-53-00-485. FABRICATED SEAT RAILS IAW GREO 601R-53-00-485, REV A. REMOVED SEAT RAIL AT FS 559+80-559+96, LBL 0 IAW AMM 53-01-11-000-802. INSTALLED NEW FABRICATED SEAT RAIL IAW AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 22,360 hrs · 21,568 cycles

RIGHT SEAT TRACK FROM 559+80-559+96, RBL 9 HAS CORROSION. COMPLIED WITH ECTC ROE 601R-53-00-485. FABRICATED SEAT RAILS IAW GREO 601R-53-00-485, REV A. REMOVED SEAT RAIL AT FS 559+80-559+96, RBL9 IAW AMM 53-01-11-000-802. INSTALLED NEW FABRICATED SEAT RAIL IAW AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 499-544) · airframe 22,360 hrs · 21,568 cycles

LEFT SIDE SEAT TRACK FROM BS 499-544 HAS CORROSION. R & R THE SEAT IAW AMM 53-01-11-000-802, 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 22,360 hrs · 21,568 cycles

RIGHT SEAT TRACK FROM BS 559-559+96 HAS CORROSION. COMPLIED WITH ECTC RO 601R-53-00-485. FABRICATED SEAT RAILS IAW GREO 601R-53-00-485, REV A. REMOVED SEAT RAIL AT FS 559-559+96 RT IAW AMM 53-01-11-000-802. INSTALLED NEW FABRICATED SEAT TRACK IAW AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 449-499) · airframe 22,360 hrs · 21,568 cycles

RT SIDE SEAT TRACK AT BS 449-499 HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802 AND 53-01-11-000-802.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 22,360 hrs · 21,568 cycles

LEFT FLOOR SEAT TRACKS FROM FS 559-559+96 HAS CORROSION. COMPLIED WITH ECTC REO 601R-53-00-485. FABRICATED SEAT RAILS IAW GREO 601R-53-00-485 REV A. REMOVED SEAT RAIL AT FS 559-559+96 IAW AMM 53-01-11-00-802. INSTALLED FABRICATED SEAT TRACK IAW AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 22,360 hrs · 21,568 cycles

LT FLOOR SEAT TRACK FROM FS 409-409+112 HAS CORROSION. COMPLIED WITH ECTC REO 601R-53-00485. FABCRATED SEAT RAILS IAW GREO 601R-53-00-485, REV A. REMOVED SEAT RAIL AT FS 409-408+112 IAW AMM 53-01-11-000-802. INSTALLED NEW FABRICATED SEAT RAIL IAW AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 22,360 hrs · 21,568 cycles

RT FLOOR SEAT TRACK FROM FS 409+112-559 HAS CORROSION. EVALUATED SEAT RAIL RT FLOOR SEAT TRACK FS 409+112-559 IAW 53-21-49 FOUND TO BE OUT OF LIMITS. COMPLIED WITH EC/TC REO 601R-53-00-485, REV A. REMOVED SEAT TRACK AT FS 409+112-559 IAW AMM 53-01-11-000-802. INSTALLED NEW FABRICATED RT SEAT TRACK FROM FS 409+112-559 IAW AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 409-449) · airframe 22,360 hrs · 21,568 cycles

LT SIDE SEAT TRACK SECTION 449.85-409.00+112 HAS CORROSION IN SEVERAL AREA OUT OF LIMITS. COMPLIED WITH REO 601R-53-00-625 REV DATE 2016-04-20. R & R LT SIDE SEAT TRACK 449.85-409.00+112 IAW AMM 53-01-11-400-802. RECEIVED AND COMPLIED WITH ECTC REO 601R-53-00-625.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 22,360 hrs · 21,568 cycles

LT SIDE SEAT TRACK SECTION 409.00+112-409.00+16 HAS CORROSION IN SEVERAL AREA OUT OF LIMITS. COMPLIED WITH REO 601R-53-00-625. REMOVED LT SIDE SEAT TRACK AT FS 409.00 + 112-409 + 16 IAW AMM 53-01-11-000-802. INSTALLED NEW SERIVCABLE LT SIDE SEAT TRACK AT FS 409+12-409.00+16 IAW AMM 53-01-11-400-802. RECEIVED AND COMPLIED WITH ECTC REO 601R-53-00-625.

Part: SEAT TRACK — CORRODED (BS 409-449) · airframe 22,360 hrs · 21,568 cycles

RT SIDE SEAT TRACK SECTION 449.85-409.00+112 HAS CORROSION IN SEVERAL AREAS OUT OF LIMITS. COMPLIED WITH REO 601R-53-00-625, REV DATE 2016-04-20. REMOVED RT SIDE SEAT TRACK 449.85-409.00+112 IAW AMM 53-01-11, 946-000-802. REPLACED RT SIDE SEAT TRACK 449.85-409.00+112 IAW AMM 53-01-11-400-802. RECEIVED AND COMPLEID WITH ECTC REO 601R-53-00-625.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 22,360 hrs · 21,568 cycles

LT SIDE SPOT TRACK SECTION BS 409.00 & 16-364 HAS CORROSION IN SEVERAL GEARS OUT OF LIMITS. COMPLIED WITH REO 601R-53-00-625, RECEIVED AND COMPLIED WITH ECTC REO 601R-53-00-625. REMOVED LT SIDE SEAT TRACK FS 409.00+16-364 IAW AMM 53-01-11-000-802. INSTALLED NEW SERVICEABLE LT SIDE SEAT TRACK 44FS409+16-364 IAW AMM 53-01-11-400-802.

Part: PLATE — CONTAMINATED (ESCAPE HATCH) · airframe 22,360 hrs · 21,568 cycles

CREW ESCAPE HATCH MECHANISM DETAIL INSPECTION COULD NOT BE COMPLIED WITH DUE TO MALFUNCTIONING TRIGGER PLATE ON OUTER HANDLE. CLEANED EXCESS GRUDGE & DIRT ACCUMULATION FROM UNDERNEATH OUTER HANDLE OF CREW ESCAPE HATCH USING BRISTLE BRUSH AND A RAG TRIGGER PLATE ON ENTER HANDLE IS NOW OPERATING CORRECTLY IAW AMM 52-22-00-710-801.

Part: DOOR FRAME — BENT (CARGO DOORWAY) · airframe 22,360 hrs · 21,568 cycles

AFT CARGO DOOR FWD FRAME BENT AT TRACK. COMPLIED WITH ECTC EA 32-2016-056 PERMANENT REPAIR. RECEIVED AND COMPLIED WITH EA 32-2016-056. RECEIVED AND COMPLIED WITH ECTC EA 32-2016-056.

Part: SKIN — DENTED (BS 185-193) · airframe 22,360 hrs · 21,567 cycles

FUSELAGE SKIN BELOW ADG DOOR HAS SEVERAL DENTS. COMPLIED WITH ECTC REO 601R-53-11-2892 PERMANENT REPAIR. REMOVED SKIN BELOW ADG DOOR IAW SRM 51-42-01. DRILLED & INSTALLED NEW SKIN UNDER ADG DOOR EXCEPT FOR 6 FASTENERS THAT WILL BE SUBMITTED TO ENGINE IAW SRM 51-42-06, DWG NR 601R33010, REV A. AFTER SKIN WAS REMOVED FOUND MEMBER DAMAGED, PN 600-33252-79, R & R MEMBER. REMOVED MEMBER, PN 600-33252-79 IAW SRM 51-42-06. INSTALLED NEW MEMBER IAW SRM 51-42-06. COMPLIED WITH DISPOSITION FOR ALTERNATE FASTENERS ON RT SKIN BETWEEN FS 185.00 & FS 193.00 REO 601R-53-11-2892, DATED 2016-04-22. RECEIVED AND COMPLIED WITH EC/TC REO 601R-53-11-2892.

Part: DOOR — BINDING (MAIN PAX) · airframe 21,352 hrs · 20,520 cycles

MAIN PASSENGER DOOR WILL NOT OPEN. WAS ABLE TO OPEN MAIN PASSENGER DOOR USED A LITTLE MORE FORCE TO OPEN DOOR LATCH CYCLED SEVERAL TIMES. OPS CHECKED GOOD IAW 52-11-00.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 21,314 hrs · 20,481 cycles

EXIT SIGN AT ROW 8 ON CEILING IS MISSING. FOUND LENS IN OTBD BIN. REINSTALLED EXIT SIGN IAW AMM 33-50-01. ACFT OK FOR SERVICE.

Part: BULKHEAD — CRACKED (BS 621) · airframe 21,158 hrs · 20,321 cycles

FOUND CRACK ON THE AFT PRESSURE BULKHEAD. CRACK RUNS VERTICAL ON THE INBD SIDE OF THE FITTING OUTLINE.

Part: BULKHEAD — CRACKED (BS 621) · airframe 21,158 hrs · 20,321 cycles

FOUND A CRACK ON THE AFT PRESSURE BULKHEAD. CRACK IS LOCATED JUST ABOVE THE AFT CARGO DOOR TRACK AT LBL 27.50 ABOVE WL 121.93 AND AT THE ZEE MEMBER HEEL LINE LOCATION. CRACK MEASURES APPROX .75 IN VERTICAL.

Part: WARNING MESSAGE — FALSE ACTIVATION (MLG) · airframe 21,060 hrs · 20,228 cycles

ON GO AROUND, RECEIVED GEAR DISAGREE AND NOSE DOOR OPEN , RAN QRH, MESSAGE CLEARED. PULLED EMERGENCY GEAR HANDLE. INTERROGATED PSEU AND MDC FOR FAULTS NOT LOGGED. PERFORMED AN OPS CHECK OF LANDING GEAR SYSTEM IAW AMM32-30-00 AND 32-34-00, OPS CHECKED GOOD. VERIFIED PROXIMITY SENSOR GAPS, ALL GOOD AT THIS TIME. ACFT OK FOR SERVICE.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 19,006 hrs · 18,175 cycles

LEFT FWD EXTERNAL EMERGENCY LIGHT IS INOPERATIVE. R & R BULB IAW AMM 33-51-21. OP'S CHECKED GOOD.

Part: WINDOW FRAME — DAMAGED (COCKPIT) · airframe 18,495 hrs · 17,637 cycles

CAPTAIN`S WINDSHEILD FRAME LOWER SILL DAMAGE 9.0" FROM AFT SIDE. BLENDED OUT DAMAGE TO WINDSHIELD FRAME LOWER SILL, FOUND TO BE WITH IN LIMITS IAW SRM 53-11-35. MAJOR REPAIR IAW GMM 5-3.

Part: SKIN — SCRATCHED (BS 193-202.75) · airframe 18,495 hrs · 17,637 cycles

ONE MINOR SCRATCH 7.8 INCHES LONG BETWEEN BS 202.75 - 193.00. 2 INCHES ABOVE S13L. BLENDED OUT DAMAGE, FOUND TO BE WITHIN LIMITS IAW SRMTR-53-00-31. MAJOR REPAIR IAW GMM 5-3.

Part: SKIN — SCRATCHED (BS 193-202.75) · airframe 18,495 hrs · 17,637 cycles

TWO MINOR SCRATCHES BETWEEN FS 202.75 - 193, 1.9 INCHES ABOVE S13L. BLENDED OUT DAMAGE, FOUND TO BE WITH-IN LIMITS IAW SRM TR-53-00-31. MAJOR REPAIR IAW GMM 5-3.

Part: SKIN — SCRATCHED (BS 210-220) · airframe 18,495 hrs · 17,637 cycles

TWO MINOR SCRATCHES BETWEEN BS 220 & 210 , ONE FIVE INCHES ABOVE S12L AND ONE NINE INCHES ABOVE S12L. BLENDED OUT DAMAGE, FOUND TO BE WITHIN LIMITS IAW SRM TR- 53-00-31. MAJOR REPAIR IAW GMM 5-3.

Part: SKIN — SCRATCHED (BS 202-210) · airframe 18,495 hrs · 17,637 cycles

2 MINOR SCRATCHES BETWEEN FS 210-202.75. 1.5 INCHES ABOVE S12L. BLENDED OUT DAMAGE, FOUND TO BE WITHIN LIMITS IAW SRM TR-53-00-31. MAJOR REPAIR IAW GMM 5-3.

Part: SUPPORT BRACKET — CRACKED (CARGO DOOR) · airframe 17,784 hrs · 16,944 cycles

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

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 17,784 hrs · 16,944 cycles

FOUND FWD CHANNEL CRACKED APPROX .25 INCH LONG. REMOVED DAMAGED CHANNEL IAW SRM 51-42-06 & SRM 51-42-21. LOCATED & DRILLED NEW CHANNEL IAW SRM 51-40-11 AND INSTALLED IAW SRM 51-42-06 & 51-42-21.

Part: BULKHEAD — CRACKED (BS 559) · airframe 17,784 hrs · 16,944 cycles

FOUND FS 559, BULKHEAD WEB HAS CRACK INDICATIONS. REPAIRED IAW ECC/TC REO 601R-53-41-260, REO 601R-53-41-260, REV E.

Part: ANGLE — CRACKED (BS 484 INTERCOST) · airframe 17,784 hrs · 16,944 cycles

BS 484 INTERCOSTAL ANGLE CRACKED AT LBL 27. REMOVED INTERCOSTAL ANGLE IAW 51-42-06. LOCATED NEW ANGLE IAW SRM 51-40-11 AND INSTALLED IAW REO 601R-53-41-059.

Part: ANGLE — CRACKED (BS 484) · airframe 17,778 hrs · 16,938 cycles

BS 484 INTERCOSTAL ANGLE CRACKED AT LBL 36 POST REO 601R-53-41-059. REMOVED INTERCOSTAL ANGLE AND INSTALLED NEW ANGLE IAW REO 601R-53-41-059.

Part: SKIN — CORRODED (BS 559) · airframe 17,779 hrs · 16,939 cycles

FUSELAGE EXTERIOR SKIN PANEL HAS CORROSION AROUND DRAINS AT FS 559+94, STR 27. NO DAMAGE ALLOWED IN THIS AREA. REPAIRED IAW CL600-2B19-53-I00159.

Part: SKIN — CORRODED (BS 559) · airframe 17,783 hrs · 16,943 cycles

FUSELAGE EXTERIOR SKIN PANEL HAS CORROSION AROUND SEVERAL FASTENERS AND TWO DRAINS BETWEEN FS 559+32 AND 559+48 S26L & 26R. NO DAMAGE ALLOWED IN THIS AREA. REPAIRED IAW CL600-2B19-53-I00159.

Part: WEB — CRACKED (BS 280) · airframe 17,779 hrs · 16,939 cycles

FS 280, LOWER WEB IS CRACKED. REPAIRED IAW REO 601R-53-11-926 IAW REO 601R-53-11-926 REV B.

Part: FLOOR SUPPORT — CRACKED (BS 280) · airframe 17,778 hrs · 16,938 cycles

BS 280, FLOOR SUPPORT ANGLE AT LBL 9.00+3 IS CRACKED APPROX 1.5 INCH LONG. REPAIRED IAW REO 601R-53-11-926, REV B.

Part: SKIN — CORRODED (BS 559) · airframe 17,783 hrs · 16,943 cycles

FUSELAGE EXTERIOR SKIN PANEL HAS CORROSION AROUND DRAINS AT FS 559+12 S26L & 26R. NO DAMAGE ALLOWED IN THIS AREA. REPAIRED IAW CL600-2B19-53-I00159.

Part: BEAM — CRACKED (BS 621) · airframe 17,770 hrs · 16,932 cycles

CARGO DOOR SUPPORT BEAM LOWER CLIP IS CRACKED AT FS 621. REMOVED CARGO DOOR SUPPORT BEAM LOWER CLIP AND REPLACED WITH NEW PARTS IAW SRM 51-40-11 AND 5-42-21, PN 601R35050-109, PO W19731.

Part: FLOOR SUPPORT — CORRODED (BS 589-620) · airframe 17,778 hrs · 16,938 cycles

LEFT CARGO FLOOR SUPPORT HAS LIGHT SURFACE CORROSION BETWEEN FS 589.00 AND 620. REMOVED FLOOR SUPPORT IAW SRM 51-42-06 & 51-42-21. INSTALLED NEW FLOOR SUPPORT IAW SRM 51-42-06 & 51-42-21 AND REO 601R-53-61-1574.

Part: ISOLATOR — BROKEN (BS 621 BULKHEAD) · airframe 17,770 hrs · 16,932 cycles

BS 621 BULKHEAD HAS BROKEN ISOLATOR ON LBL 27. R & R BROKEN ISOLATOR IAW SRM 51-42-06.

Part: ANGLE — CRACKED (BS 625) · airframe 17,770 hrs · 16,932 cycles

LT UPPER FS 625 OBLIQUE ANGLE IS CRACKED. REMOVED LT UPPER OBLIQUE ANGLE AT FS 625 IAW SRM 51-42-06. LOCATED AND DRILLED NEW OBLIQUE ANGLE IAW SRM 51-40-11. INSTALLED NEW OBLIQUE ANGLE IAW SRM 51-42-06.

Part: FLOOR SUPPORT — CORRODED (BS 589-619) · airframe 17,778 hrs · 16,938 cycles

FLOOR SUPPORT AT LBL 27 HAS CORROSION AROUND SEVERAL NUTPLATES BETWEEN FS 589.00 AND FS 619.00. REMOVED FLOOR SUPPORT IAW SRM 51-42-06. DRILLED AND INSTALLED NEW FLOOR SUPPORT IAW REO 601R-53-61-3778 AND SRM 51-40-11.

Part: SEAT TRACK — CORRODED (BS 364) · airframe 17,778 hrs · 16,938 cycles

DEFECT DESCRIPTION: PASSENGER SEAT TRACK AT FUSELAGE STATION 364 RBL 9 HAS CORROSION AROUND FASTENER HOLE. R & R FLOOR SEAT RAIL AT RBL 9 BETWEEN FS 364 AND 394, IAW AMM 53-01-11-000-802 AND AMM 53-01-11-400-802.

Part: UNKNOWN — ODOR (CABIN) · airframe 15,663 hrs · 14,626 cycles

DURING FLIGHT, F/A AND PASSENGERS DETECTED AN ODOR OF SOMETHING BURNING. ODOR DESCRIBED AS BURNING PAPER, ODOR WAS IN THE CABIN ONLY AND WAS NOT EVIDENT IN THE COCKPIT. ODOR DISSIPATED AFTER A COUPLE OF MINUTES. PERFORMED OPS CHECK IAW AMM 21-50-00. NO DEFECTS NOTED.

Part: PLACARD — MISSING (CABIN) · airframe 15,193 hrs · 14,092 cycles

F/A REPORTS "BOARDING DOOR EXIT PLACARD IS MISSING". REPLACED BOARDING. BOARDING DOOR EXIT PLACARD IAW AMM 11-30-00.

Part: LENS — BROKEN (EMERGENCY LIGHTS) · airframe 13,437 hrs · 12,134 cycles

LENS COVER BROKE AT BOARDING DOOR. R & R LENS COVER AT BOARDING DOOR IAW AMM 33-51-19. DEFER CLEARED. (CLOSED)

Part: PLATE — CORRODED (SERVICE DOOR) · airframe 13,291 hrs · 11,960 cycles

SERVICE DOOR PLATE ASSY CORRODED BEYOND LIMITS. LOCATED AND DRILLED HOLES IN NEW SERVICE DOOR PLATE ASSY IAW SRM 51-40-11. INSTALLED SERVICE DOOR PLATE ASSY IAW SRM 51-40-00. MINOR REPAIR.

Part: STRUCTURE — CORRODED (PAX DOOR) · airframe 13,291 hrs · 11,960 cycles

CORROSION DAMAGE PAX DOOR AFT CONER FS 345 TO FS 349.00. REMOVED CORROSION IAW SRM 51-21-06. PERFORMED UT THICKNESS INSP OF BLEND AREA ON STRAP IAW MAC NDT INSP PROCEDURE UT-3 MINIMUM MATERIAL REMAINING IS .099". FOUND TO BE WITHIN LIMITS IAW SRM 53-00-00.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 13,291 hrs · 11,960 cycles

ASO AFT DRAG ANGLE CRACKED AT CABLE FOR MOTOR, BD161723 11/15/10 (KF), RESOLVED ON W/O: 181807 TASKCARD: N/R-00234. REMOVED AND REPLACED AFT DRAG ANGLE ON PAX DOOR IAW CRJ 200 SRM 51-42-06 LS5500124 11/18/10 THIS IS A MINOR REPAIR SM161739 11/18/10 (AJ 11/18/10).

Part: FITTING — CRACKED (FUSELAGE) · airframe 13,291 hrs · 11,960 cycles

FS 280 CLIP CRACKED AT LBL 9.0 FLOORBEAM INBD SIDE. RESOLVED ON W/O: 181807 TASKCARD: N/R-00192. REMOVED CLIP THEN INSTALLED NEW CLIP PER CRJ 200 SRM 51-42-21 HILITE, SRM 51-42-06 SOLID RIVETS, SRM 51-23-00 WET INSTALL JR161745 11/16/10 2. CLIP NEEDS FINISH CODE CRJ 200 SRM 51-21-16 A032 JR161745 11/16/10 PAINTED CLIP PER CRJ 200 SRM 51-21-16 FINISH CODE A032 JR161745 11/17/10 (AJ 11/17/10).

Part: FITTING — CRACKED (FUSELAGE) · airframe 13,291 hrs · 11,960 cycles

FS 280 CLIP CRACKED AT RBL 9.0 FLOORBEAM INBD SIDE. REMOVED CLIP THEN INSTALLED NEW CLIP IAW SRM 51-42-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 13,291 hrs · 11,960 cycles

FS 280 CLIP CRACKED AT LBL 9.0 FLOORBEAM OUTBD SIDE. RESOLVED ON W/O: 181807 TASKCARD: N/R-00191. REMOVED CLIP PER CRJ 200 SRM 51-42-21 HILITE, SRM 51-42-06 SOLID RIVETS JR161745 11/16/10 2. NEW CLIP NEEDS TO BE INSTALLED JR161745. INSTALLED NEW CLIP PER CRJ 200 SRM 51-42-21 HILITE, SRM 51-23-00 WET INSTALL, SRM 51-21-16 FINISH CODE A032 JR161745 11/17/10 (AJ 11/17/10).

Part: TRACK — DAMAGED (CABIN) · airframe 13,291 hrs · 11,960 cycles

LIGHT FLOOR, TRACK AFT DAMAGED (5 PIECES). REPLACED DAMAGED SECTIONS WITH NEW PARTS.

Part: FITTING — CRACKED (FUSELAGE) · airframe 13,291 hrs · 11,960 cycles

FS 280 CLIP CRACKED AT RBL 9.0 FLOORBEAM OUTBD SIDE. REMOVED CLIP THEN INSTALLED NEW CLIP IAW SRM 51-42-21.

Part: COMPUTER — FAILED (ALTIMETER) · airframe 12,406 hrs · 10,924 cycles

DURING FLIGHT THE FOLLOWING EICAS MSG'S POSTED: RAD ALT FLAG, TCAS FAIL, GPWS FAIL, WINDSHEAR FAIL STATUS MSG'S, AND SPOILERONS, FLT SPOILERS INBD GRND SPOILERS AND OTBS GRND SPOILERS CAUTIONS MSG'S. ACOMPLISHED FLAPS 20 LANDING IAW QRH. (EMERGENCY DECLARED) R & R RAD ALT COMPUTER (TRANCEIVER) IAW AMM 34-44-01, OPS CHECK GOOD. (CLOSED)

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 10,626 hrs · 8,963 cycles

CLIMBING THROUGH FL 260, GOT A "CARGO BTL LO" MSG, DIVERTED TO NEAREST SUITABLE AIRPORT PER QRH. DESCENDING THROUGH 8,000FT THE MSG EXTINGUISHED. NO EVIDENCE OF SMOKE OR HALON IN CARGO BAY. EMERGENCY DECLARED. EN ROUTE TO ILM, A/C DIVERTED TO CAE DUE TO MTC.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,363 hrs · 8,683 cycles

FWD CEILING EMERGENCY LIGHT INOP.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 9,154 hrs · 7,509 cycles

FS 484.0 LBL 36 INTERCOSTAL FLANGE CRACKED IN RADIUS. NOT PREVIOUSLY REPAIRED.

Part: BEAM — CRACKED (FUSELAGE) · airframe 9,154 hrs · 7,509 cycles

CARGO DOOR SUPPORT BEAM LOWER ANGLE IS CRACKED .3 INCH IN LENGTH.

Part: ANCHOR FITTING — CRACKED (PAX DOOR) · airframe 9,154 hrs · 7,509 cycles

FWD/AFT PAX DOOR ANCHOR FITTING ARE CRACKED AND HAVE CORRODED HARDWARE. REMOVED LT WINDSCREEN IAW AMM 25-24-04-000-801. REMOVED AND REPLACED FWD AND AFT PAX DOOR ANCHOR FITTINGS ASSY AND CORRODED HARDWARE WITH SERVICEABLE PARTS IAW EO 600-52-66 C/W. INSTALLED LT WINDSCREEN IAW AMM 25-24-04-400-801.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 9,154 hrs · 7,509 cycles

CARGO BAY FLOORBEAM FLOOR PANEL ATTACH FLANGE IS CORRODED AT LBL 27 OUTBOARD FLANGE FS 589. CORROSION APPEARS MINOR AND ISOLATED.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 9,154 hrs · 7,509 cycles

FS 484.0 RBL 27.0 WL 73.0 INTERCOSTAL ATTACH ANGLE CRACKED IN RADIUS.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 9,154 hrs · 7,509 cycles

LT AND RT FS 621.00 TO 625.00 OBLIQUE ANGLES IN AFT EQUIPMENT COMPARTMENT ARE CRACKED 2 INCHES LONG ON AFT RADIUS.

Part: STRUCTURE — MISSING (FUSELAGE) · airframe 9,154 hrs · 7,509 cycles

LT EMER EXIT DOOR CUTOUT 6 O'CLOCK POSITION, DOOR LANDING MISSING A 7 INCH LONG SECTION OF MATERIAL THAT IS BONDED TO FUSELAGE SKIN THAT MAKES DOOR LANDING. REPAIRED LT EMERGENCY EXIT LANDING IAW BOMBARDIER AEROSPACE PROCESS SPECIFICATION 157-028. PRESSURE LEAK CHECK OF LT OVERWING EMERGENCY EXIT GOOD IAW CRJ 200 AMM 21-32-00-863-801. SUPPLEMENTAL-SDR CLOSED 11/17/2008.

Part: STRIP — CRACKED (CABIN) · airframe 9,154 hrs · 7,509 cycles

FOUR EACH EMER PHOTOLUMINESCENT FLOODLIGHT STRIPS ARE CRACKED.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 9,154 hrs · 7,509 cycles

LT SIDE FLOOR SUPPORT IS CRACKED 1.0 INCH AT FS 621, WL 73, LBL 40. REPAIRED THE LT FS 621 FLOOR ANGLE IAW BOMBARDIER REO 601R-53-61-117, REV C ASA EC/TC 601R-53-61-117, INCORPORATED. SUPPLEMENTAL-SDR CLOSED 11/17/2008.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 9,154 hrs · 7,509 cycles

FS 484.0 RBL 36 WL 73.0 INTERCOSTAL FLANGE CRACKED IN RADIUS.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 8,517 hrs · 6,927 cycles

RT FWD EXTERIOR EMERGENCY LIGHT BURNED OUT REPLACED RT FWD EXTERIOR EMERGENCY LIGHT BULB IAW CRJ 200 AMM 33-51-21. OPS CK GOOD. --[SDR CLOSED](B)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,845 hrs · 6,340 cycles

FWD FACING EXIT LIGHT ON AISLE OVERWING EMERGENCY LIGHTS INOP. FLT 4898 DEL 166 MINS.

Part: FLAP — FAILED (WING) · airframe 7,659 hrs · 6,193 cycles

FLAPS FAIL CAUTION MSG ON APPROACH. FLAPS FAILED AT ZERO WHEN SELECTING EIGHT DEGREES. FLT 4503 DEL 390 MINS.

Part: FLAP — MALFUNCTIONED (WING) · airframe 7,511 hrs · 6,068 cycles

ON APPROACH AT 2500 FT FLAPS FAIL MESSAGE WHEN MOVED TO 8 DEGREES. EMERGENCY VEHICLES ROLLED AS A PRECAUTION.

Part: FLAP — MALFUNCTIONED (WING) · airframe 7,491 hrs · 6,048 cycles

DURING APPROACH TO (KBOS) REC'D "FLAPS FAIL" CAUTION MESSAGE WHEN SELECTING FLAPS TO "8" DEGREES, FLAP INDICATIONS ARE "0" DEGREES. EMERGENCY VEHICLES WERE REQUESTED TO BE ON STANDBY AS A PRECAUTION.

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 7,491 hrs · 6,048 cycles

DURING APPROACH TO (KBOS) REC'D "FLAPS FAIL" CAUTION MESSAGE WHEN SELECTING FLAPS TO "8" DEGREES, FLAP INDICATIONS ARE "0" DEGREES. EMERGENCY VEHICLES WERE REQUESTED TO BE ON STANDBY AS A PRECAUTION.

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 7,485 hrs · 6,046 cycles

FLAP FAIL AT ZERO ON APPROACH FIRE TRUCKS REQUESTED TO BE ON STANDBY AS A PRECAUTION. FLTS 4336, 4455 CX.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,396 hrs · 5,970 cycles

RIGHT FWD OVERWING EMERGENCY LIGHT INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,348 hrs · 5,929 cycles

RT 2ND FROM FRONT EXTERNAL EMERGENCY LIGHT INOP.

Part: WARNING LIGHT — ILLUMINATED (THRUST REVERSER) · airframe 7,299 hrs · 5,888 cycles

FLT 4501 DEL 133 MINS, R THRUST REVERSER UNLOCKED CAUTION MSG INFLIGHT, A/C RETURNED TO ATL AFTER T/O. EMERGENCY DECLARED.

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 7,096 hrs · 5,725 cycles

RIGHT WING FWD OVERWING FORWARD EMERGENCY LIGHT INOP.

Part: LIGHT — INOPERATIVE (WINGS) · airframe 7,096 hrs · 5,725 cycles

LT AND RT WING LEADING EDGE EMERGENCY LIGHTS INOP.

Part: COWLING — DEPARTED (NR 2 NACELLE) · airframe 5,845 hrs · 4,705 cycles

NR 2 ENG FAILURE AT 32,000 FT, LOUD BAM WAS HEARD NR 2 THRUST LEVER SLAMMED TO IDLE. A/C YAWED TO THE LT, SEVER VIBRATION BEGAN IMMEDIATELY, UNABLE TO SECURE ENGINE, EMERGENCY DECLARED. EN ROUTE TO ATL A/C DIVERTED TO TRI DUE TO MTC. UPON GROUND INSPECTION BOTH UPPER AND LOWER ENGINE COWLINGS WERE FOUND TO HAVE DEPARTED THE AIRCRAFT. FLT 4344 CX. [07-23-07] REMOVED AND REPLACED NR 2 ENGINE IN ACCORDANCE WITH CRJ 200 AMM 71-0-00. OPERATIONAL AND LEAK CHECK COMPLIED WITH. ALL PARAMETERS WITHIN SERVICABLE LIMITS IAW CRJ 200 AMM 71-00-00. OK FOR SERVICE.

Part: UNKNOWN — UNKNOWN (NLG STEERING) · airframe 5,069 hrs · 4,112 cycles

NWS INOP MESSAGE. EMERGENCY DECLARED.

Part: ANCHOR FITTING — CORRODED (PAX DOOR) · airframe 4,319 hrs · 3,525 cycles

PAX DOOR AFT CABLE ANCHOR FITTING SERRATED MOUNTING PLATE CORRODED (MARKED).

Part: FLOORBEAM — CRACKED (BS 621) · airframe 4,319 hrs · 3,525 cycles

RIGHT 621 FLOOR ATTACH ANGLE CRACKED IN CARGO BAY.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 4,319 hrs · 3,525 cycles

EMERGENCY EXIT LIGHT COVER ABOVE SERVICE DOOR OPENING CRACKED (MARKED).

Part: LIGHT — BROKEN (CABIN) · airframe 2,808 hrs · 2,336 cycles

EMERGENCY LIGHT JUST INSIDE OF PAX DOOR ON FWD WALL BROKEN.

Part: GUARD — OPEN (PX DOOR)

DURING A GROUND INSPECTION, THE FORWARD PASSENGER DOOR WAS DIFFICULT TO OPEN AFTER PARKING. MAINTENANCE FOUND THE PASSENGER DOOR ASSIST GUARD NOT FULLY CLOSED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: SIGN — INOPERATIVE (CABIN)

DURING A GROUND INSPECTION IN CAE, THE EMERGENCY EXIT SIGN, NEAR THE PASSENGER DOOR, WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT SIGN, NEAR THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)