N746SK

Part: DOOR FRAME — CORRODED (BS 1000-1051) · airframe 47,954 hrs · 31,466 cycles

CORROSION NOTED ON 3EA CHORD INNER REINFORCEMENTS AT AFT CARGO DOOR SURROUND STRUCTURE BETWEEN FS 1000.00 - FS 1051.00 #27497074 (C-CHECK RO 1/30/2024) INSTALLED 3EA NEW CHORD INNER REINFORCEMENTS AT AFT CARGO DOOR SURROUND STRUCTURE BETWEEN FS 1000.00 - FS 1051.00 REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG MM670-35085 REV -L. COMPLIED WITH TASK CARD 51-900-1002-SKY. SEE CONTINUATION FOR FURTHER DETAILS.

Part: ANGLE — CRACKED (BS 280 RBL 12) · airframe 47,954 hrs · 31,466 cycles

ANGLE CC670-33199-4 THAT ATTACHES TO COCKPIT CENTER FLOOR BEAM AT RBL12.00 & SUPPORTS FLIGHT COMPARTMENT FLOOR PANEL 221ALF IS CRACKED. (C-CHECK RO 1/30/2024) INSTALLED NEW ANGLE CC670-33199-4S ASSEMBLY IAW CRJ700 SRM 53-11-43-201-003-A01 SEE CONTINUATION FOR WORK PERFORMED,COMPLIED WITH 51-900-1002-SKY

Part: SKIN — CHAFED (RT AILERON) · airframe 47,954 hrs · 31,466 cycles

RH AILERON UPPER SKIN IS CHAFED ON THE LOWER SIDE OF THE TRAILING EDGE BETWEEN AILS343.35 & AILS337.03 (C-CHECK RO 1/30/2024) INSTALLED NEW LEADING EDGE SKIN ON RH AILERON PER REF CRJ 700 SRM 51-42-21-001-001-A01 AND CRJ 700 SRM 51-42-27-001-001-A01 AND DWG CC670-13000, REV -D. SEE CONTINUATION FOR WORK PERFORMED C/W TASK CARD 51-900-1002-SKY

Part: WEB — CRACKED (BS 280 RBL 12) · airframe 47,954 hrs · 31,466 cycles

FOUND WEB OF THE RH CENTER COCKPIT FLOOR BEAM AT BL12.00 CRACKED FROM FS280.00 & WL72.10 (C-CHECK RO 1/30/2024) PERFORMED REPAIR AS PER GENERIC REPAIR TYPE 4 OF CRJ700 SRM 53-11-43-201-003-A01 TO WEB OF THE RH CENTER COCKPIT FLOOR BEAM AT BL12.00 CRACKED FROM FS280.00 & WL72.10.COMPLIED WITH 51-900-1002-SKY

Part: ANGLE — CRACKED (BS 280 RBL 26) · airframe 47,954 hrs · 31,466 cycles

STIFFENER ANGLE AT RBL26.00 FWD SIDE OF THE FS280.00 IS CRACKED, (C-CHECK RO 1/30/2024) REMOVED AND REPLACED STIFFENER ANGLE AT RBL26.00 FWD SIDE OF THE FS280.00 IRT DWG CC670-34010 REV-K, CRJ700 SRM 51-42-06-001-001-A01 & CRJ700 SRM 51-42-13-001-001-A01, COMPLIED WITH 51-900-1002-SKY

Part: GUSSET — CRACKED (BS 280 RBL 12) · airframe 47,954 hrs · 31,466 cycles

FLOOR SUPPORT GUSSET AT RBL12 FS280 IS CRACKED (C-CHECK RO 1/30/2024) INSTALLED NEW FLOOR SUPPORT GUSSET AT RBL12 FS280 IAW CRJ700 SRM 51-42-06-001-001-A01 AND DRAWING CC670-33052 REV -G SEE CONTINUATION FOR WORK PERFORMED, COMPLIED WIRTH 51-900-1002-SKY

Part: BRACKET — CRACKED (THRUST REVERSER) · airframe 47,954 hrs · 31,466 cycles

R/H LWR TRANSCOWL FLANGE ON STANDOFF BRACKET COMMON TO AFT LATCH FAIRING IS CRACKED. (C-CHECK RO 1/30/2024) REPLACED STAND-OFF BRACKET P/N CN624-2039-203 ON R/H LOWER TRANS COWL, REF. CRJ700 SRM 51-42-13-001-001-A01 & TRANS COWL ASSEMBLY DWG. CN624-2001, REV. W.COMPLIED WITH 51-900-1002-SKY.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 47,954 hrs · 31,466 cycles

R/H 280 FLOOR BEAM IS CORRODED ON THE FWD SIDE BETWEEN BL0 AND RBL9 (C-CHECK RO 1/30/2024) REMOVED AND REPLACED R/H FS280 FLOOR BEAM. REF: CRJ700 SRM 51-42-06-001-001-A01 , CRJ700 SRM 51-42-21-001-001-A01, CRJ700 SRM 51-42-13-001-001-A01, CRJ700 SRM 51-42-22-001-001-A01, AND DWG CC670-34010 REV -K, COMPLIED WITH 51-900-1002-SKY

Part: FLOORBEAM — CORRODED (BS 280) · airframe 47,954 hrs · 31,466 cycles

L/H 280 FLOOR BEAM IS CORRODED ON THE FWD SIDE BETWEEN BL0 AND LBL9 (C-CHECK RO 1/30/2024) REMOVED AND REPLACED L/H FS280 FLOOR BEAM. REF: CRJ700 SRM 51-42-06-001-001-A01 , CRJ700 SRM 51-42-21-001-001-A01, CRJ700 SRM 51-42-13-001-001-A01, CRJ700 SRM 51-42-22-001-001-A01, AND DWG CC670-34010 REV -K, COMPLIED WITH 51-900-1002-SKY

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 47,954 hrs · 31,466 cycles

PAX DOOR AFT DD2 INTERCOSTAL IS CORRODED (C-CHECK RO 1/30/2024) REMOVED AND INSTALLED NEW PAX DOOR AFT DD2 INTERCOSTAL REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV. N ,NO LEAKS NOTED COMPLIED WITH SKY WEST SKYCARD 51-900-1002-SKY LEAK CHECK GOOD

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 47,954 hrs · 31,466 cycles

PAX DOOR AFT DD3 INTERCOSTAL IS CORRODED (C-CHECK RO 1/30/2024) REMOVED AFT DD3 INTERCOSTAL REF CRJ700 SRM 51-42-06-001-001-A01 AND INSTALLED NEW AFT DD3 INTERCOSTAL TO PAX DOOR REF DWG 601R31702 REV. N AND CRJ 700 SRM 51-42-06-001-001-A01, COMPLIED WITH 51-900-1002-SKY. LEAK CHECK GOOD

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 47,954 hrs · 31,466 cycles

PAX DOOR FWD DD2 INTERCOSTAL IS CORRODED (C-CHECK RO 1/30/2024) REMOVED PAX DOOR FWD DD2 INTERCOSTAL REF CRJ700 SRM 51-42-06-001-001-A01 AND INSTALLED NEW PAX DOOR FWD DD2 INTERCOSTAL REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV. N,M COMPLIED WITH 51-900-1002-SKY. LEAK CHECK GOOD

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 47,954 hrs · 31,466 cycles

PAX DOOR AFT DD5 INTERCOSTAL IS CORRODED (C-CHECK RO 1/30/2024) REMOVED PAX DOOR AFT DD5 INTERCOSTAL REF CRJ700 SRM 51-42-06-001-001-A01 AND INSTALLED NEW AFT DD5 INTERCOSTAL TO PAX DOOR REF DWG 601R31702 REV. N AND CRJ 700 SRM 51-42-06-001-001-A01, COMPLIED WITH 51-900-1002-SKY, LEAK CHECK GOOD

Part: INTERCOSTAL — CORRODED (DOOR DD4) · airframe 47,954 hrs · 31,466 cycles

PAX DOOR FWD DD4 INTERCOSTAL IS CORRODED (C-CHECK RO 1/30/2024) REMOVED PAX DOOR FWD DD4 INTERCOSTAL REF CRJ700 SRM 51-42-06-001-001-A01 AND INSTALLED NEW PAX DOOR FWD DD4 INTERCOSTAL REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV. N, COMPLIED WITH 51-900-1002-SKY , LEAK CHECK GOOD

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 47,954 hrs · 31,466 cycles

PAX DOOR AFT DD4 INTERCOSTAL IS CORRODED (C-CHECK RO 1/30/2024) REMOVED PAX DOOR AFT DD4 INTERCOSTAL REF CRJ700 SRM 51-42-06-001-001-A01 AND INSTALLED NEW AFT DD4 INTERCOSTAL TO PAX DOOR REF DWG 601R31702 REV. N AND CRJ 700 SRM 51-42-06-001-001-A01, COMPLIED WITH 51-900-1002-SKY, LEAK CHECK GOOD

Part: INTERCOSTAL — CORRODED (FWD PAX DOOR) · airframe 47,954 hrs · 31,466 cycles

PAX DOOR FWD DD5 INTERCOSTAL IS CORRODED (C-CHECK RO 1/30/2024) REMOVED PAX DOOR FWD DD5 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND INSTALLED PAX DOOR FWD DD5 REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV. N, COMPLIED WITH 51-900-1002-SKY, LEAK CHECK GOOD

Part: INTERCOSTAL — CORRODED (MID PAX DOOR) · airframe 47,954 hrs · 31,466 cycles

PAX DOOR MID DD6 INTERCOSTAL IS CORRODED (C-CHECK RO 1/30/2024) REMOVED PAX DOOR MID DD6 INTERCOSTAL IAW CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-21-001-001-A01 AND INSTALLED PAX DOOR MID DD6 REF CRJ700 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 AND DWG 601R31702 REV. N,COMPLIED WITH 51-900-1002-SKY. LEAK CHECK GOOD. PART FOR PART, NO WEIGHT CHANGE

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 47,954 hrs · 31,466 cycles

PAX DOOR FWD DD3 INTERCOSTAL IS CORRODED (C-CHECK RO 1/30/2024) REMOVED PAX DOOR FWD DD3 INTERCOSTAL REF CRJ700 SRM 51-42-06-001-001-A01 AND INSTALLED NEW PAX DOOR FWD DD3 INTERCOSTAL REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV. N,, COMPLIED WITH 51-900-1002-SKY, LEAK CHECK GOOD

Part: FLOOR SUPPORT — CORRODED (BS 1004-1047) · airframe 47,954 hrs · 31,466 cycles

EXFOLIATED CORROSION FOUND ON FLOOR BEAM CAP AT FS1004-FS1047 LBL 9 (C-CHECK RO 1/30/2024) INSTALLED ALL REPAIRED PARTS FOR FLOOR BEAM CAP AT FS1004-FS1047 LBL9 IAW CRJ 700 SRM 53-00-41-201-001-A01 AND REO 670-53-61-2204 REV. -- DATED 2023-11-20. SEE CONTINUATION FOR WORK PERFORMED AND COMPLIED WITH TASK CARD 51-900-1002-SKY

Part: GUIDE — CHAFED (AFT CRGO DOOR) · airframe 47,954 hrs · 31,466 cycles

AFT CARGO DOOR, UPPER, FORWARD ROLLER GUIDE (ITEM 43 SRM 53-61-58) HAS CHAFE DAMAGE (C-CHECK RO 1/30/2024) .REMOVED AND REPLACED AFT CARGO DOOR, UPPER, FORWARD ROLLER GUIDE PER DWG# MM670-35060 REV V IAW CRJ700 SRM 51-42-06-001-001-A01 AND 51-42-10-001-001-A01, COMPLIED WITH TASK CARD 51-900-1002-SKY

Part: BRACKET — CRACKED (RT WING) · airframe 47,954 hrs · 31,466 cycles

RIGHT WING MAIN FUEL TANK, SLAT TRACK CANISTER 1-3 BRACKET HAS SUSPECTED CRACK. (C-CHECK RO 1/30/2024) REPLACED RIGHT WING MAIN FUEL TANK, SLAT TRACK CANISTER 1-3 BY COMPLYING WITH ALL STEPS OF REO 670-57-42-577 REV-- DATED: 2016-12-02 . SEE CONTINUE CARD FOR WORK PERFORMED. ALL CHECKS GOOD.COMPLIED WITH SKYWEST SKY CARD 51-900-1002-SKY

Part: FLOOR SUPPORT — CORRODED (BS 1004-1047) · airframe 47,954 hrs · 31,466 cycles

EXFOLIATED CORROSION FOUND ON FLOOR BEAM CAP AT FS1004-FS1047 LBL 27 REQIURES REPLACEMENT (C-CHECK RO 1/30/2024) REPAIRED FLOOR BEAM CAP CUTOUT DAMAGED SECTION FROM FS977 - FS1065 LBL27, FABRICATED AND INSTALLED ALL REPAIR PARTS IAW CRJ 700 SRM 53-00-41-201-.001-A01. COMPLIED WITH 51-900-1002-SKY.

Part: FLOOR SUPPORT — CORRODED (BS 1004-1047) · airframe 47,954 hrs · 31,466 cycles

SUSPECTED CORROSION FOUND ON FLOOR BEAM CAP AT FS1004-FS1047 RBL 9 (C-CHECK RO 1/30/2024) REPAIRED FLOOR BEAM CAP CAP SECTION FROM F/S 977 TO F/S 1074, FABRICATED REPAIR BEAM CAP SECTION AND QTY 2 SPLICE ANGLE, INSTALLED ALL REPAIR PARTS IAW CRJ 700 SRM 53-00-41-201-001-A01 AND REO 670-53-61-2204 REV. -- DATED 2023-11-20.COMPLIED WITH SKYCARD 51-900-1002-SKY

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 47,954 hrs · 31,466 cycles

PAX DOOR DD1 (AFT) INTERCOSTAL IS CRACKED. (MARKED) (C-CHECK RO 1/30/2024) REMOVED CRACKED DD1 (AFT) INTERCOSTAL FROM PAX DOOR REF CRJ700 SRM 51-42-06-001-001-A01 AND INSTALLED NEW AFT DD1 INTERCOSTAL TO PAX DOOR REF DWG 601R31702 REV. N AND CRJ 700 SRM 51-42-06-001-001-A01, COMPLIED WITH 51-900-1002-SKY, LEAK CHECK GOOD

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 47,954 hrs · 31,466 cycles

PAX DOOR INTERCOSTAL DD7A IS CORRODED. (C-CHECK RO 1/30/2024) REMOVED PAX DOOR FWD DD7A INTERCOSTAL REF CRJ700 SRM 51-42-06-001-001-A01 AND INSTALLED PAX DOOR FWD DD7A INTERCOSTAL REF DWG 601R31702 REV. N AND CRJ700 SRM 51-42-06-001-001-A01, COMPLIED WITH 51-900-1002-SKY , LEAK CHECK GOOD

Part: ANGLE — CORRODED (PAX DOOR HANDLE) · airframe 47,954 hrs · 31,466 cycles

PAX DOOR OUTER HANDLE ANGLE IS CORRODED.. (C-CHECK RO 1/30/2024) REMOVED AND INSTALLED PAX DOOR OUTER HANDLE ANGLE REF CRJ700 SRM 51-42-21-001-001-A01 AND DWG 601R317040 REV. C NO LEAKS NOTED COMPLIED WITH SKYWEST SKY CARD 51-900-1002-SKY,NO LEAKS NOTED

Part: DOOR FRAME — DAMAGED (BS 347) · airframe 47,954 hrs · 31,466 cycles

PAX DOOR FS347.25 AFT FORMER HAS OVERSIZED HOLES DUE TO OLD PREVIOUS REPAIR. REQUIRES REPLACEMENT (C-CHECK RO 1/30/2024) REMOVED PAX DOOR AFT ANGLE SUPPORT TO FOM IAW CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-21-001-001-A01 AND INSTALLED AFT ANGLE SUPPORT TO NEW PAX DOOR AFT FORMER FS347.25 REF DWG 601R31702 REV. N AND CRJ 700 SRM 51-42-06-001-001-A01, COMPLIED WITH 51-900-1002-SKY , LEAK CHECK GOOD. PART FOR PART, NO WEIGHT CHANGE.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 47,954 hrs · 31,466 cycles

PAX DOOR DD1 INTERCOSTAL (MID) IS CORRODED (C-CHECK RO 1/30/2024) REMOVED PAX DOOR MID DD1 INTERCOSTAL IAW CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-21-001-001-A01 AND INSTALLED PAX DOOR MID DD1 INTERCOSTAL REF CRJ700 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 AND DWG 601R31702 REV. N. COMPLIED WITH 51-900-1002-SKY, LEAK CHECK GOOD

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 47,954 hrs · 31,466 cycles

PAX DOOR DD3 INTERCOSTAL (MID) IS CORRODED (C-CHECK RO 1/30/2024) REMOVED PAX DOOR MID DD3 REF CRJ700 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 CORRECTIVE ACTION: INSTALLED PAX DOOR MID DD3 REF CRJ700 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 AND DWG 601R31702 REV. N, COMPLIED WITH 51-900-1002-SKY, LEAK CHECK GOOD

Part: FLOOR SUPPORT — CORRODED (BS 280-310) · airframe 47,954 hrs · 31,466 cycles

L/H FLOOR SILL BETWEEN FS280.00 TO FS310.00 HAS CORROSION (MARKED) (C-CHECK RO 1/30/2024) REMOVED AND INSTALLED NEW FLOOR SILL AND NEW SPLICE ANGLE AT LBL 41 BETWEEN FS 280 TO FS 310 PER DWG SH670-32170, REV V, REF CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-21-001-001-A01, COMPLIED WITH 51-900-1002-SKY, LEAK CHECK GOOD

Part: DOOR SILL — CORRODED (AFT CARGO) · airframe 47,954 hrs · 31,466 cycles

* AFT CARGO DOOR LOWER SILL HAS MULTIPLE SPOTS OF CORROSION (MARKED). (C-CHECK RO 1/30/2024) REMOVED AND INSTALLED NEW AFT CARGO DOOR LOWER SILL P/N MM670-35655-003 REF CRJ700 SRM 51-42-06-001-001-A01 AND CRJ700 SRM 51-42-21-001-001-A01, CRJ700 SRM 51-42-13-001-001-A01ANS SWG MM670-35085 REV -L, PERFORMED THE LEAK CHECK AFT CARGO DOOR CHECKS GOOD, NO LEAKS NOTED.

Part: STRINGER — DAMAGED (BS 1144-1162 S7R) · airframe 47,954 hrs · 31,466 cycles

STGR7R IS DAMAGED. FS1144.00 - 1162.00. (FLAGGED) (C-CHECK RO 1/30/2024) REPAIRED STGR7R FROM FS1144.00 - 1162.00 BY COMPLYING WITH ALL STEPS (1-14) OF REO 670-53-61-2200, REV --, DATED 2023-12-18.

Part: FLOOR SUPPORT — CORRODED (BS 587-684 LBL9) · airframe 47,954 hrs · 31,466 cycles

*MULTIPLE SPOTS OF CORROSION NOTED ON FLOOR BEAM CAP AT LBL9 BETWEEN FS587-FS684(MARKED) (C-CHECK RO 1/30/2024) COMPLIED WITH FLOOR BEAM SPLICE REPAIR AT LBL9 BETWEEN FS587 - FS684 REF CRJ700 SRM 53-00-41-201-001-A01, REO 670-53-31-830 REV -- DATE 2023-12-25 AND REO 670-53-31-835 REV -- DATE 2023-12-18, COMPLIED 51-900-1002-SKY ,

Part: CUP — CORRODED (HANDRAIL) · airframe 47,954 hrs · 31,466 cycles

* PAX DOOR FWD BELOW FLOOR HAND RAIL CUP CORRODED IN MULTIPLE SPOTS (MARKED). (C-CHECK RO 1/30/2024) CORROSION FOUND TO BE OUT OF LIMITS PER REF. CRJ700 SRM 53-21-23-101-001-A01. REMOVED AND INSTALLED NEW FWD HAND RAIL CUP FITTING P/N SH670-31840-3 ON PASSENGER DOOR SURROUND. REF MHIRJ DWG SH670-31840 REV-A REF: CRJ700 SRM 51-42-06-001-001-A01 AND CRJ700 SRM 51-42-21-001-001A01,COMPLIED WITH 51-900-1002-SKY

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 47,954 hrs · 31,466 cycles

*CORROSION NOTED ON FLOOR BEAM CAP AT RBL9 AT APPROX. FS549 (MARKED), (C-CHECK RO 1/30/2024) REMOVED CORROSION, NO ALLOWABLE DAMAGE ON BEAM CAP REF CRJ 700 SRM 53-31-43-001-001-A02. CUT AND REPLACED RBL 9 FLOOR BEAM SECTION FROM FS 543.00 TO FS 573.00 REF. CRJ 700 SRM 53-00-41-201-001-A01. 51-42-06-001-001-A01 SRM 51-42-21-001-001-A01 & DRWG SH670-33400 REV. J, , RECEIVED MATERIAL DEVIATION FOR NEW FLOOR BEAM CLEATS MHIRJ REO 670-53-31-833 REV -- DATED:2023-12-18 . COMPLIED WITH 51-900-1002-SKY

Part: STRINGER — CORRODED (BS 1015-1031) · airframe 47,954 hrs · 31,466 cycles

*CORROSION NOTED ON STRG26R BETWEEN FS1015-1031 (MARKED), (C-CHECK RO 1/30/2024) REMOVED CORROSION ON STRG26R BETWEEN FS1015-1031 FOUND WITHIN LIMITS IAW REO670-53-61-2208 REV -- DATE 2023-12-01 AND CRJ-700 SRM 51-42-06-001-001-A01. SEE CONTINUE CARD FOR MORE DETAILS AND COMPLIED WITH ALLTHE STEPS OF THE REO 670-53-61-2208 REV -- DATE 2023-12-01,COMPLIED WITH SKYWEST SKYCARD 51-900-1002-SKY,NO LEAKS NOTED

Part: STRINGER — DAMAGED (BS 1144-1162 S7L) · airframe 47,954 hrs · 31,466 cycles

STGR7L IS DAMAGED. FS1144.00 - 1162.00. (FLAGGED) (C-CHECK RO 1/30/2024) REPAIRED STGR7L FROM FS1144.00 - 1162.00 BY COMPLYING WITH ALL STEPS (1-14) OF REO 670-53-61-2199, REV. --, 2023-12-18. COMPLIED WITH 51-900-1002-SKY

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 47,954 hrs · 31,466 cycles

*MULTIPLE SPOTS OF CORROSION NOTED ON FLOOR BEAM CAP AT RBL9 BETWEEN FS645-FS629 (MARKED), (C-CHECK RO 1/30/2024) REPAIRED FLOOR BEAM CAP AT RBL9 BETWEEN FS645-FS629 ( CORROSION OUT OF LIMIT) PER REO #670-53-31-840 REV (--) 2023-12-26 AND CRJ 700 SRM 53-00-41-201-001-A01. COMPLIED WITH SKY CARD 51-900-1002-SKY STRUCTURAL MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 47,954 hrs · 31,466 cycles

*CORROSION NOTED FLOOR BEAM CAP AT LBL9 AT APPROX FS549 (MARKED), (C-CHECK RO 1/30/2024) REMOVED CORROSION, NO ALLOWABLE DAMAGE ON BEAM CAP REF CRJ700 SRM 53-31-43-001-001-A02. CUT AND REPLACED LBL 9 FLOOR BEAM SECTION FROM FS545 TO FS570 REF CRJ700 SRM 53-00-41-201-001-A01. RECEIVED MATERIAL DEVIATION FOR NEW FLOOR BEAM CLEATS MHIRJ REO 670-53-31-836 REV -- DATED:2023-12-19. SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH 51-900-1002-SKY

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 47,954 hrs · 31,466 cycles

*CORROSION NOTED AT CROSSBEAM AT FS549 BETWEEN RBL9-LBL9 (MARKED) (C-CHECK RO 1/30/2024) REMOVED CORROSION FROM CROSSBEAM AT FS549 BETWEEN RBL9-LBL9 REF. CRJ 700 SRM 51-21-06-001-001-A01. THERE IS NO DAMAGE ALLOWED TO FLOOR SUPPORT STRUCTURE REF. CRJ 700 SRM 53-31-43-101-001-A02. REPAIRED CROSSBEAM AT FS549 BETWEEN RBL9 AND LBL9 REF REO 670-53-31-824 REV -- DATED 2023-12-08. SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH 51-900-1002-SKY.

Part: DOOR SILL — CORRODED (PAX DOORWAY) · airframe 47,954 hrs · 31,466 cycles

* PAX DOOR LOWER SILL CORRODED IN MULTIPLE SPOTS (MARKED). (C-CHECK RO 1/30/2024) PAX DOOR LOWER SILL ANGLE IS REMOVED AND REPLACED BY NEW PART IAW CRJ700 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01 AND DWG SH670-31810 REV Y.COMPLIED WITH 51-900-1002-SKY, LEAK CHECK GOOD

Part: FRAME — CORRODED (ZONE 100) · airframe 47,954 hrs · 31,466 cycles

*CORROSION NOTED ON FRAME 517 BETWEEN STRG25L-27 (MARKED), (C-CHECK RO 1/30/2024) REMOVED AND INSTALLED NEW FLANGE P/N SH670-33260-3 AT FRAME F/S 517 BETWEEN STGR 25L-26L IAW CRJ700 SRM 51-42-06-001-001-A01 AND CRJ700 SRM 51-42-21-001-001-A01 AND REO 670-53-31-827, REV --, 2023-12-14. COMPLIED WITH SKYWEST SKY CARD 51-900-1002-SKY NO LEAKS NOTED

Part: FLOORBEAM — CORRODED (BS 280) · airframe 47,954 hrs · 31,466 cycles

* FLOOR BEAM AT FS.280.00 FLOOR PANEL SUPPORT ANGLE HAS SPOTS OF CORROSION (MARKED). (C-CHECK RO 1/30/2024) REMOVED AND REPLACED FWD FLOOR SUPPORT P/N CC670-34095-1S ON FS280 FLOOR BEAM. REF: CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01, DWG CC670-34010 REV -K, COMPLIED WITH 51-900-1002-SKY

Part: BRACKET — CRACKED (THRUST REVERSER) · airframe 47,954 hrs · 31,466 cycles

L/H LWR TRANSCOWL OTBD A BRACKET IS CRACKED (C-CHECK RO 1/30/2024) INSTALLED 1 EA. NEW STANDOFF P/N CN 624-2082-201. ON L/H LOWER TRANS COWL, REF. REO670-54-21-971, REV. A, DATED 2017/05/11.

Part: SKIN — PUNCTURED (THRUST REVERSER) · airframe 47,954 hrs · 31,466 cycles

L/H LWR TRANSCOWL INNER PERFORATED SKIN IS PUNCTURED. (C-CHECK RO 1/30/2024) REPAIRED L/H LOWER TRANSCOWL REF MHIRJ REO 670-54-21-1599 REV -- 2023-12-08. COMPLIED WITH TASK CARD 51-900-1003 SKY

Part: SKIN — DAMAGED (AFT) · airframe 47,954 hrs · 31,466 cycles

UNDER PANEL 321AT FWD DORSAL STARK, TOOLING DAMAGE IN SEVERAL AREAS TO THE EXTERIOR FUSELAGE SKIN (MARKED) 27394743 (C-CHECK RO 1/30/2024) BLENDED OUT TOOLING DAMAGE IN SEVERAL AREAS TO THE EXTERIOR FUSELAGE SKIN UNDER PANEL 321AT. REF: CRJ-700 SRM 51-12-00-001-001-A01 AND COMPLIED WITH ALL STEPS OF REO 670-53-51-272 REV-- DATED 2023-11-29. SEE CONTINUE CARD FOR WORK PERFORMED.COMPLIED WITH THE TASKCARD 51-900-1002-SKY. BLEND ONLY NO WEIGHT CHANGE

Part: BRACKET — CRACKED (THRUST REVERSER) · airframe 47,954 hrs · 31,466 cycles

L/H LWR TRANSCOWL INBD A BRACKET IS CRACKED (C-CHECK RO 1/30/2024) INSTALLED 1 EA. NEW A BRACKET P/N CN 624-2082-201 ON L/H LOWER TRANS COWL. REF. REO 670-54-21-971, REV. A, DATED 2017/05/11. COMPLIED WITH STEPS 1-3.

Part: BRACKET — CRACKED (THRUST REVERSER) · airframe 47,954 hrs · 31,466 cycles

R/H LOWER TRANSCOWL INBD "A" BRACKET IS CRACKED (C-CHECK RO 1/30/2024) REPLACED I/B STAND-OFF ANGLE P/N CN624-2082-201 ON R/H LOWER TRANS COWL, REF. REO 670-54-21-971, REV. A, 2017-05-11. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY

Part: HINGE — SCRATCHED (PAX DOOR) · airframe 47,954 hrs · 31,466 cycles

PAX DOOR HINGE MULTIPLE LUGS ARE SCRATCHED AND PITTED. (C-CHECK RO 1/30/2024) REPAIRED PAX DOOR PIANO HINGE IAW CRJ.700 SRM 52-11-01-201-007-A01 TYPE I AND IV STEPS 1,2,3,4 AND DWG 601R318073 REV. E. COMPLIED WITH SKY CARD 51-900-1002-SKY

Part: BRACKET — CRACKED (THRUST REVERSER) · airframe 47,954 hrs · 31,466 cycles

R/H UPPER TRANSCOWL OTBD A BRACKET CRACKED (C-CHECK RO 1/30/2024) REMOVED AND REPLACED R/H UPPER TRANSCOWL OUTBD "A" BRACKET (STANDOFF) WITH NEW STANDOFF P/N CN624-2082-201 REF. REO 670-54-21-971 REV. A, 2017/05/11. COMPLIED WITH SKYCARD 51-900-1002-SKY.

Part: BRACKET — CRACKED (THRUST REVERSER) · airframe 47,954 hrs · 31,466 cycles

R/H UPPER TRANSCOWL INBD A BRACKET IS CRACKED (C-CHECK RO 1/30/2024) REMOVED AND REPLACED R/H UPPER TRANSCOWL INBD "A" BRACKET (STANDOFF) WITH NEW STANDOFF P/N CN624-2082-201 REF. REO 670-54-21-971 REV. A, 2017/05/11. COMPLIED WITH SKYCARD 51-900-1002-SKY.

Part: BRACKET — CRACKED (THRUST REVERSER) · airframe 47,954 hrs · 31,466 cycles

R/H LWR TRANSCOWL OTBD "A" BRACKET IS CRACKED (C-CHECK RO 1/30/2024) REPLACED O/B STAND-OFF ANGLE P/N CN624-2082-201 ON R/H LOWER TRANS COWL, REF. REO 670-54-21-971, REV. A, 2017-05-11. COMPLIED WITH TASK CARD 51-900-1002-SKY

Part: COAMING — CHAFED (THRUST REVERSER) · airframe 47,954 hrs · 31,466 cycles

R/H LWR TRANSCOWL INNER COAMING IS CHAFED @ SPIGOT RECEPTACLE (C-CHECK RO 1/30/2024) REPLACED COAMING P/N CN624-2060-209 ON R/H LOWER TRANS COWL, REF. CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-13-001-001-A01 & TRANS COWL STAGE THREE BUILD DWG. CN624-2003, REV. AG. COMPLIED WITH TASK CARD 51-900-1002-SKY

Part: VANE — CHAFED (LT TE FLAP) · airframe 47,954 hrs · 31,466 cycles

LEFT INBOARD FLAP VANE, CENTER INBOARD LEADING EDGE CAP HAS A CHAFE. (C-CHECK RO 1/30/2024) REMOVED LEFT INBOARD FLAP VANE, CENTER INBOARD LEADING EDGE (PN CC670-14012-5) COMPLETE PER CRJ700 SRM 51-42-10-001-001-A01 AND INSTALLED NEW PART # CC670-14012-5 LEFT INBOARD FLAP VANE, CENTER INBOARD LEADING EDGE CAP REF. CRJ-700 SRM 51-42-13-001-001-A01 REV. 38 JULY 25,2020 AND DRAWING CC670-14010 REV F . COMPLIED WITH SKYWEST SKYCARD 51-900-1002-SKY

Part: WINDOW POST — CRACKED (LT WINDSHIELD) · airframe 47,954 hrs · 31,466 cycles

LEFT WINDSHIELD SIDE POST IS CRACKED AT THE UPPER BARREL NUT. (C-CHECK RO 1/30/2024) REMOVED LEFT WINDSHIELD SIDE POST PN 601R33223-1 REF, CRJ700 SRM 51-42-21-001-001-A01. CORRECTIVE ACTION: INSTALLED NEW LEFT WINDSHIELD SIDE POST PN 601R33223-1 . REF: CRJ700 SRM 51-42-21-001-001-A01 AND DWG. CC670-33055 REV -F, COMPLIED WITH 56-220-1000-SKY AND 51-900-1002-SKY' LEAK CHECK WAS GOOD NO LEAK NOTED AT THIS TIME

Part: SKIN — DENTED (BS 1031 S25-27) · airframe 47,954 hrs · 31,466 cycles

DURING AUDIT OF 1C TASK CARD 53-900-304 (EXTERNAL ZONAL INSPECTION OF THE REAR FUSELAGE - FS977.00 TO FS1098.20 BELOW WL72.50) FOUND SEVERAL DENTS ON FUSELAGE SKIN AT FS1031.00 BETWEEN STR27 AN STR25 FWD OF DRAIN MAST. (C-CHECK RO 1/30/2024) REMOVED PAINT AND REPAIRED SEVERAL DENTS ON FUSELAGE SKIN AT FS1031.00 BETWEEN STR27 AN STR25 FWD OF DRAIN MAST REF CRJ-700 SRM 51-26-01-001-001-A01 AND COMPLIED WITH ALL THE STEPS REO 670-53-61-2203 REV -- DATED 2023-11-21,COMPLIED 51-900-1002-SKY

Part: BULKHEAD — BENT (BS 280) · airframe 47,954 hrs · 31,466 cycles

ANGLE ON AFT SIDE OF THE FS280.00 BULKHEAD FLANGE IS BENT. WL97.80 BL11L. (FLAGGED) (C-CHECK RO 1/30/2024) REPAIRED ANGLE AFT SIDE OF THE FS280 BULKHEAD FLANGE IS BENT CUT DAMAGE ANGLE SECTION AWAY AND REMOVED ALL BURRS AND SHARP EDGE REF COMPLIED WITH REO 670-53-11-1906 REV -- DATED 2023-12-25 AND REO #670-53-11-1904 REV-- DATED 2023-11-28, COMPLIED WITH 51-900-1002-SKY

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 47,954 hrs · 31,466 cycles

*FWD VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE IS CRACKED AT L/H SIDE (MARKED) (C-CHECK RO 1/30/2024) REMOVED FWD VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE AND INSTALLED NEWLY FABRICATED FWD DRAG ANGLE, FILLER, AND DOUBLER ON LH SIDE REF CRJ700 SRM 55-31-00-201-001-A01 AND COMPLIED WITH THE MHIRJ REO 670-55-31-168 REV -- DATE 2023-11-29.COMPLIED WITH 51-900-1002-SKY

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 47,954 hrs · 31,466 cycles

*AFT VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE IS CRACKED AT L/H SIDE (MARKED) (C-CHECK RO 1/30/2024) REMOVED AFT VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE REF CRJ 700 SRM 51-42-10-001-001-A01 AND SRM 51-42-21-001-001-A01 AND INSTALLED NEW AFT VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE REF CRJ 700 SRM 51-42-13-001-001-A01, SRM 51-42-21-001-001-A01, AND SRM 51-42-22-001-001-A01 AND DWG IFBA670-35002 REV-C. COMPLIED WITH 51-900-1002-SKY

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 47,954 hrs · 31,466 cycles

*SUSPECTED CRACK AT R/H VERTICAL TO FUSELAGE AFT DRAG ANGLE (MARKED), (C-CHECK RO 1/30/2024) REPAIRED R/H VERTICAL TO FUSELAGE AFT DRAG ANGLE REF CRJ-700-SRM 55-31-00-201-001-A01. COMPLIED WITH 51-900-1002-SKY AND SEE CONTINUATION CARD FOR DETAILS

Part: HOUSING — GOUGED (CRGO DOOR HANDLE) · airframe 47,954 hrs · 31,466 cycles

*AFT CARGO DOOR EXTERNAL HANDLE HOUSING IS GOUGED(MARKED) (C-CHECK RO 1/30/2024) INSTALLED NEW AFT CARGO BAY DOOR HANDLE HOUSING PN 119992-5 REF CRJ 700 SRM 51-42-21-001-001-A01 AND DWG 601R35027 REV AY.LEAK CHECK GOOD, COMPLIED WITH 51-900-1002-SKY

Part: ACCESS DOOR — CRACKED (GROUND POWER) · airframe 47,954 hrs · 31,466 cycles

CAMP# 27347459: LP GROUND CONNECTION ACCESS DOOR 182BR UPPER LAND (FUSELAGE INTERNAL DOUBLER) IS CRACKED. (C-CHECK RO 1/30/2024) REMOVED THE CRACKED FUSELAGE INTERNAL DOUBLER FOR THE L P GROUND CONNECTION ACCESS DOOR 182BR UPPER LAND AND REPAIRED INTERNAL DOUBLER (LANDING) OF LP GROUND CONNECTION ACCESS DOOR 182BR ,REF CRJ 700 SRM 51-42-21-001-001-A01 REV. 38 DATED JUL 25/2020 AND REO 670-53-61-2196, REV --, DATED ON 2023-11-30 (NO INTERNAL DOUBLER REPLACEMENT WAS NECESSARY) COMPLIED WITH 51-900-1002-SKY, LEAK CHECK GOOD

Part: COWL DOOR — DENTED (LT NACELLE) · airframe 47,954 hrs · 31,466 cycles

ADM # N746SK-8199 SMOOTH DENT LENGTH 3.25 WIDTH 2.5 INCH DEPTH .060, PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDARD ACFT PRACTICES. (C-CHECK RO 1/30/2024) REPAIRED L/H LOWER FAN COWL DOOR OUTER SKIN FINAL IAW REO 670-54-14-1277 REV. -- DATED 2023-12-07 ALL STEPS COMPLIED WITH STEPS 1 THROUGH 16.COMPLIED WITH SKYCARD 51-900-1002-SKY ,COMPLIED WITH M-337.

Part: HINGE — WORN (PAX DOOR) · airframe 47,954 hrs · 31,466 cycles

COMPLY WITH SCHEDULED MAINTENANCE CODE: RA68347-670-53-21-1994 746S MXCODEID55678-PR - PAX DOOR PIANO HINGE ON FUSELAGE WORN. COMPLIED WITH TEMPORARY REPAIR PER REO 670-53-21-1994. PERMANENT REPAIR DUE WITHIN 6100 FLT HRS BY 49363.5 TAT, PART NUMBER: - , SERIAL NUMBER: 10202, POSITION: (C-CHECK RO 1/30/2024) COMPLIED WITH SCHEDULED MAINTENANCE CODE: RA68347-670-53-21-1994 746SK CODEID55678-PR - PAX DOOR PIANO HINGE ON FUSELAGE WORN. REMOVED AND REPLACED PAX DOOR HINGE ASSY (FUSELAGE SIDE) REF. CRJ 700 SRM 53-21-23-201-007-A01 AND DWG. SH670-31810 REV. AE. AND REO 670-53-21-1994 REV -- DATE 2021-04-04COMPLIED WITH 51-900-1002-SKY

Part: UNKNOWN — SMOKE · airframe 46,975 hrs · 30,609 cycles

D: WHITE SMOKE IN ENTIRE AIRCRAFT AFTER PACKS TURNED ON AT THE GATEC: MEL 21-51-1FCAT C DUE 04/13/2023 (FLIGHT 3029 FILED CLOSED)APR 04, 2023 STATION: DFW--LEFT PACK IS DEFERRED PER CRJ 700 MEL 21-51-1F NO MAINT ACTION REQUIRED MCC NOTIFIED PLACARD INSTALLED APR 05, 2023 STATION: DFW -- R&R LH ACM IN REFERENCE TO APPLICABLE STEPS IN AMM 21-51-08OPS CHECK GOOD AT THIS TIME.PLACARDS REMOVED.DMI CLEARED.LEAK CHECK GOODAT THIS TIME.

Part: NONE — CRACKED · airframe 45,956 hrs · 29,777 cycles

HSTA UPPER FITTING CROSS TIE BRACKET FOUND CRACKED AND REQUIRES REPLACEMENT. (FILED CLOSED) REMOVED AND REPLACED HASTA UPPER TIE ROD PER AMM 27-42-01

Part: NONE — GOUGED · airframe 45,956 hrs · 29,777 cycles

GOUGE DAMAGE FOUND TO THE HSTA LOWER FITTING P/N AV670-21125-007, ON THE LH SIDE INBOARD FLANGE FACE. DAMAGE MEASURES 0.375"L X 0.92"W X 0.0295" D, AND IS OUT OF THE ALLOWABLE DAMAGE LIMITATIONS OF SRM 55-31-27. (FILED CLOSED) GOUGE DAMAGE FOUND TO THE HSTA LOWER FITTING P/N AV670-21125-007, ON THE LH SIDE INBOARD FLANGE FACE. DAMAGE MEASURES 0.375"L X 0.92"W X 0.0295" D, AND IS OUT OF THE ALLOWABLE DAMAGE LIMITATIONS OF SRM 55-31-27. DAMAGE REQUIRES DETERMINATION OF MAJOR/MINOR REPAIR. SEE CP 25339152 FOR DETERMINATION.

Part: NONE — CRACKED · airframe 44,814 hrs · 28,941 cycles

MX REQUEST REMOVAL AND REPLACEMENT TO BE PERFORMED OF CAPT WINDSHEILD DUE TO CRACK. (FLIGHT 3726 - FILED CLOSED) REMOVED AND REPLACED CAPTAIN'S WINDSHIELD WITH A SERVICEABLE UNIT IAW AMM 56-11-01 AND TASK CARD 56-220-1000-SKY. OPS AND LEAK CHECK GOOD.

Part: NONE — UNRELIABLE · airframe 44,500 hrs · 28,716 cycles

COMPLY WITH: 670BA-53-036 - FUSELAGE - CENTER FUSELAGE, FS669.40 TO FS855.40 - REPLACEMENT OF THE BEAMS AF LBL36 AND RBL36, AND THE FLOOR ASSEMBLY BETWEEN FS693.00 AND FS847.00 WITH BEAMS INSTALLED AT BL0, LBL9, LBL18, LBL27, RBL9, RBL18 AND RBL27 REV D PART(S) 0 (FILED CLOSED) COMPLIED WITH: 670BA-53-036 - FUSELAGE - CENTER FUSELAGE, FS669.40 TO FS855.40 - REPLACEMENT OF THE BEAMS AF LBL36 AND RBL36, AND THE FLOOR ASSEMBLY BETWEEN FS693.00 AND FS847.00 WITH BEAMS INSTALLED AT BL0, LBL9, LBL18, LBL27, RBL9, RBL18 AND RBL27 REV D. FOLLOW ON LEAK AND OPS CHECKS GOOD.

Part: DOOR FRAME — DAMAGED (BS 347) · airframe 43,279 hrs · 27,802 cycles

PAX DOOR FORMER AT FS 347.25 IS DAMAGED AT DATUM 4 WHERE PAX DOOR ASSIST PULLEY BRACKET MOUNTS. THIS DAMAGE HAS BEEN DETERMINED TO BE A MAJOR REPAIR. MAINTENANCE FORM M-337 REQUIRED. (FILED CLOSED) REPLACED PAX DOOR FORMER AT F.S. 347.25 AND PULLEY MOUNT BRACKET AT DATUM 4 IN REFERENCE TO CRJ 700 SRM 51-77-00 AND ST CARD 51-900-1002. ALSO COMPLETED FORM M-337

Part: SKIN — DAMAGED (PAX DOOR) · airframe 43,279 hrs · 27,802 cycles

TRANSFER FROM EAML 603636 : CREATED FROM FORWARD DISCREPANCY. PLEASE REFERENCE AML 603545 / DAMAGE DETERMINED TO BE OUT OF LMITS PER CRJ700 SRM TASK 52-11-01 / DAMAGE TO INNER SKIN MEASUREMENTS OUT OF LIMITS. DAMAGE IS 5 INCHES IN LENGTH AND 2 1/4 INCHES WIDE. DAMAGE LOCATED ON FS347.00 PER GMM 3-26 THIS REPAIR HAS BEEN DETERMINED TO BE A MAJOR REPAIR FORM M-337 / REQUIRED. (FLIGHT 3240 - FILED CLOSED) REPAIRED DAMAGE TO PAX DOOR INNER SKIN, AT FS 347.25 AND DATUM 4 PER REO 670-52-11-1216 REV --, DATED 2021-04-01

Part: WINDOW — CRACKED (COCKPIT) · airframe 42,893 hrs · 27,544 cycles

SEE CP 22129454-1 FOR ORIGINAL DISCREPANCY, FOUND CRACK ON RH WINDOW BOTTOM AFT CORNER. REMOVED RT FLIGHT COMPARTMENT WINDOW, IN REFERENCE TO AMM 56-12-01. REFERENCE ML 22129454-1 FOR INSTALLATION OF RT FLIGHT COMPARTMENT WINDOW.

Part: HINGE — CRACKED (PAX DOOR) · airframe 41,359 hrs · 26,444 cycles

THE LWR HINGE ON THE PAX DOOR STOW PANEL IS CRACKED AT MULTIPLE LOCATIONS (MARKED). (C-CHECK) RO 2/07/2020 REMOVED AND REPLACED HINGE AND SOLID FASTENERS, REF CRJ700 SRM. LOCATED AND DRILLED, DEBURRED NEW HINGE. REF CRJ700 SRM

Part: FLOOR SUPPORT — CORRODED (COCKPIT) · airframe 41,359 hrs · 26,444 cycles

LH COCKPIT FLOOR SUPPORT ANGLE, COMMON TO LBL 12 BEAM HAS MULTIPLE SPOTS OF CORROSION. INSTALLED "NEW' SUPPORT ANGLE P/N CC670-33199-3 REF CRJ 700 SRM TASK. HI-LITE FASTENERS.

Part: STRINGER CLIP — DAMAGED (BS 394) · airframe 41,359 hrs · 26,444 cycles

CLEAT ON STRINGER 19R AT FS 394 REQUIRES REPLACEMENT (C-CHECK) RO 2/07/2020 CLEAT ON STRINGER 19R AT FS 394 REPLACED WITH NEW FABRICATED CLEAT. / REF: CRJ 700 SRM AND DRWG.

Part: FLOORBEAM — GOUGED (BS 280) · airframe 41,359 hrs · 26,444 cycles

DOUBLER FS 280 FLOOR SILL RHL 36 PN SH670-314524-1 GOUGED (C-CHECK) RO 2/07/2020 REMOVED AND REPLACED DOUBLER ON FLOOR SILL REF. CRJ-700 SRM.

Part: FAIRING — CRACKED (PAX DOOR HINGE) · airframe 41,359 hrs · 26,444 cycles

BOTH FWD (141AL) AND AFT (141BL) PAX DOOR HINGE FAIRS ARE CRACKED (C-CHECK) RO 2/07/2020 REPLACED BOTH FWD AND AFT (PANELS 141AL AND 141BL) PAX DOOR HINGE FAIRINGS WITH NEW ONES P/N- 601R31895-11 AND 601R31895-12 REF: CRJ-700 S.R.M.

Part: WEB — DAMAGED (NOT REPORTED) · airframe 41,359 hrs · 26,444 cycles

FABRICATE RH LWR WEB SECTION PN CC670-34170 IAW REO (C-CHECK) RO 2/07/2020 NEW R/H LOWER WEB SECTION P/N CC670-34170 FABRICATED FROM .040" 7075-T6 PO#T000042476 REF BOMBARDIER REO.

Part: FASTENER — CORRODED (RT WING TE FLAP) · airframe 41,359 hrs · 26,444 cycles

INBOARD AND OUTBOARD FLAP PANEL SCREWS CORROATED. (C-CHECK) RO 2/07/2020 REPLACED 7 FASTENERS PART# AVL200-4-41R AND REPLACED CORROATED BOLTS WITH NEW ONES. PER CRJ-700 SRM.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 41,359 hrs · 26,444 cycles

CORROSION FOUND ON RH F.S. 280.0 AFT WEB AT FLOOR LEVEL AROUND RBL 9.0. (C-CHECK) RO 2/07/2020 REMOVED AND REPLACED RH 280 BULKHEAD LWR WEB SECTION, REF BOMBARDIER REO. COMPLIED WITH SWA M-337 FOR MAJOR REPAIR.

Part: TORQUE TUBE — CHAFED (LT WING TE FLAPS) · airframe 41,359 hrs · 26,444 cycles

*LH WING FLAP TORQUE TUBE HAS CHAFE FROM CONTACT WITH NYLON FLAP TUBE RETAINER AT APPROX STATION WS 252.00 . NYLON RETAINER IS MISSING. (C-CHECK) RO 2/07/2020 REPLACED LH WING FLAP TORQUE TUBE AND NYLON RETAINER WITH NEW. COMPLIED WITH TASK.

Part: SEAT TRACK — CORRODED (BS 557) · airframe 41,359 hrs · 26,444 cycles

*RH PAX SEAT RAIL MOUNT CHANNEL HAS EVIDENCE OF CORROSION AT FS 557.00 . (C-CHECK) RO 2/07/2020 REPAIRED RH SEAT RAIL CHANNEL PER SRM.

Part: PAN — CRACKED (CAPTAIN'S SEAT) · airframe 41,359 hrs · 26,444 cycles

*CAPTAIN'S SEAT PAN HAS EVIDENCE OF CRACK AT FWD INBOARD (RH) MOUNT BOLT. (C-CHECK) RO 2/07/2020 REMOVED AND REPLACED CAPTAIN'S SEAT PAN SHROUDS (RH AND BACK) WITH NEW, REF CRJ 700 CMM.

Part: PAN — CRACKED (COPILOT'S SEAT) · airframe 41,359 hrs · 26,444 cycles

*COPILOT'S SEAT PAN HAS EVIDENCE OF CRACK AT FWD INBOARD AND OUTBOARD MOUNT BOLTS. (C-CHECK) RO 2/07/2020 REMOVED AND REPLACED COPILOT'S SEAT PAN SIDE SHROUDS, REF CRJ 700 SRM.

Part: CABLE — CORRODED (RT AILERONS) · airframe 41,359 hrs · 26,444 cycles

*RH WING UPPER AND LOWER AILERON CABLES HAVE EVIDENCE OF CORROSION AT WS130.00 . (C-CHECK) RO 2/07/2020 REPLACED RH WING UPPER AND LWR AILERON CABLES WITH NEW REF. CRJ-700 AMM.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 41,359 hrs · 26,444 cycles

FS 280 RH BEAM TOP FLANGE RADIUS CORRODED (C-CHECK) RO 2/07/2020 REMOVED AND REPLACED RH 280.0 BEAM, REF CRJ 700 SRM AND BOMBARDIER DWG. COMPLIED WITH SKYWEST TASK FOR A STRUCTURAL MAJOR REPAIR. COMPLIED WITH SWA M-337.

Part: DOUBLER — CORRODED (BS 533) · airframe 41,359 hrs · 26,444 cycles

* CORROSION DETECTED IN FWD BAG BAY,ON "BOW-TIE" DOUBLER ATTACHED TO F.S. 533.00 (MARKED). (C-CHECK) RO 2/07/2020 REPLACED FORWARD BAGGAGE BAY JOINT STRAP AT FS533 PER SRM.

Part: STRINGER — CORRODED (BS 394) · airframe 41,359 hrs · 26,444 cycles

* CORROSION DETECTED (ON) STGR 19R, APROX 3" AFT OF F.S. 394.00, AT CANNON PLUG (J380) ATTACHING CLIP(MARKED). (C-CHECK) RO 2/07/2020 INSTALLED REPAIR OF STGR 19R REF CRJ 700 SRM. LEAK CHECK GOOD. COMPLIED WITH TASK. COMPLIED WITH FORM 337

Part: STRINGER — CORRODED (BS 295-310) · airframe 41,359 hrs · 26,444 cycles

* CORROSION DETECTED ON STGR 26R, BETWEEN F.S. 295.00 & F.S. 310.00, ON "FLANGE" AROUND SEVERAL FASTENER BUCKTAILS (MARKED). (C-CHECK) RO 2/07/2020 REMOVED AND REPLACED STRINGER 26R BETWEEN FS 295.00 AND FS 310.00 REF CRJ 700 SRM. NO LEAKS FOUND. COMPLIED WITH MAJOR REPAIR FORM M-337 AND TASK CARD. NO WEIGHT CHANGE.

Part: STRINGER — CORRODED (BS 295-310) · airframe 41,359 hrs · 26,444 cycles

* CORROSION DETECTED ON STGR 26L, BETWEEN F.S. 295.00 & F.S. 310.00, ON "FLANGE" AROUND SEVERAL FASTENER BUCKTAILS (MARKED). (C-CHECK) RO 2/07/2020 INSTALLED NEW STRINGER REF CRJ 700 SRM. LEAK CHECK GOOD. COMPLIED WITH MAJOR REPAIR -337 AND TASK CARD.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 41,359 hrs · 26,444 cycles

FLIGHT DECK BL12 LH FLOOR BEAM HAS EVIDENCE OF CRACK IN RADIUS AT FS280 FLOOR POST ATTACHMENT. (C-CHECK) RO 2/07/2020 REMOVED AND INSTALLED FABRICATED FLIGHT DECH BL12 LH FLOOR BEAM REF. CRJ-700 SRM. COMPLIED WITH MAJOR REPAIR M-337 AND TASK CARD.

Part: FITTING — CORRODED (FUSELAGE) · airframe 41,359 hrs · 26,444 cycles

* CORROSION DETECTED ON (L/H) SIDE OF FWD NOSE JACK FITTING (UNDER FLOOR) ON "FLANGE" OF SUPPORT FITTING AROUND SEVERAL FASTENER BUCKTAILS COMMON TO BELLY SKIN (MARKED). (C-CHECK) RO 2/07/2020 REPLACED NLG JACK FITTING SUPPORT REF DWG AND SRM. NO LEAKS FOUND / COMPLIED WITH M-337. COMPLIED WITH TASK CARD.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 41,359 hrs · 26,444 cycles

* CORROSION DETECTED ON AFT SIDE OF F.S. 280.00 ON CRAWL BOARD SUPPORT "ANGLE" (MARKED). (C-CHECK) RO 2/07/2020 REMOVED AND REPLACED CRAWL AWAY FLOOR SUPPORT ANGLE AT F.S. 280.0, REF CRJ 700 SRM.

Part: CARGO TRACK — CORRODED (BS 581) · airframe 41,359 hrs · 26,444 cycles

* CORROSION DETECTED IN FWD BAG BAY, ON (L/H / AFT) CARGO TIE DOWN "FITTING" JUST AFT OF F.S. 581.00 (MARKED). (C-CHECK) RO 2/07/2020 INSTALLED NEW (L/H AFT) FWD CARGO TIE DOWN FITTING PN: SH670-33390-2 IAW BOMBARDIER DRAWING, CRJ700 SRM.

Part: DOUBLER — CORRODED (BS 581) · airframe 41,359 hrs · 26,444 cycles

* CORROSION DETECTED IN FWD BAG BAY, ON "BOW-TIE" DOUBLER ATTACHED TO F.S. 581.00 (MARKED). (C-CHECK) RO 2/07/2020 REPAIRED FWD BAGGAGE BAY JOINT STRAP AT FS 581 PER SRM. SEE CONTINUATION SHEET FOR DETAILS.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 41,359 hrs · 26,444 cycles

CORROSION NOTED ON TOP OF FLOORBEAM AT FS280.00 (C-CHECK) RO 2/07/2020 REMOVED AND REPLACED CROSS BEAM TOP CAP COMMON TO LH/RH 280.0 BEAMS, REF CRJ 700 SRM.

Part: INTERCOSTAL — CORRODED (BS 310-319) · airframe 41,359 hrs · 26,444 cycles

INTERCOSTAL IS CORRODED BETWEEN F.S 310.00 AND F.S 319.00 AT STRG. 19 R/H. (C-CHECK) RO 2/07/2020 REPLACED INTERCOSTAL AT STRINGER 19R, BETWEEN FS310.00 & 319.00 PER SRM.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 41,359 hrs · 26,444 cycles

*FS 280 BEAM BL12RH SHEAR BOX "L" ANGLE HAS EVIDENCE OF CRACK IN RADIUS. (C-CHECK) RO 2/07/2020 REMOVAED AND REPLACED SHEAR BOX ANGLE AT BL12 RH OF 280.O BULKHEAD, REF CRJ 700 SRM.

Part: FLOOR SUPPORT — CORRODED (BS 280-295) · airframe 41,359 hrs · 26,444 cycles

R/H FLOOR SILL IS CORRODED BETWEEN F.S 280.00 AND F.S 295.00 AT FWD CORNER. (C-CHECK) RO 2/07/2020 REPLACED RH FLOOR SILL REF CRJ 700 SRM. NO LEAKS FOUND. COMPLIED WITH TASK. COMPLIED WITH FORM 337

Part: FLOORBEAM — CORRODED (BS 280) · airframe 41,359 hrs · 26,444 cycles

*COCKPIT FLOOR PANEL 221ALF AFT SUPPORT ANGLE ON FWD SIDE OF FS 280 BEAM HAS EVIDENCE OF CORROSION ON TOP SIDE. (C-CHECK) RO 2/07/2020 REMOVED AND REPLACED COCKPIT AFT FLOOR SUPPORT ANGLE FOR FLOOR PANEL 221ALF COMMON TO THE 280.0 BEAMS, REF CRJ 700 SRM.

Part: SKIN — CRACKED (LT NAC DOOR) · airframe 41,359 hrs · 26,444 cycles

*LH ENGINE UPPER TRANSCOWL HAS CRACK FWD OF FWD LATCH ASSY AND FASTENERS PULLED THROUGH STIFFENER AFT OF FWD LATCH ASSY. (C-CHECK) RO 2/07/2020 ORDERED AND RECEIVED SERVICEABLE LH/UPPER TRANSCOWL ASSEMBLY. SEE TRANS # 20073058, JOB 710202100, OPERATION 527 FOR INSTALLATION.

Part: SKIN — CHAFED (BS 969) · airframe 41,359 hrs · 26,444 cycles

*LOWER FUSELAGE SKIN CHAFED EXTERNALLY FROM CONTACT WITH FAIRING FASTENER AT APPROX FS969.5 STRINGER 27. (C-CHECK) RO 2/07/2020 REPAIRED LOWER SKIN PANEL AT FS969.5 PER REO.

Part: STOP — CORRODED (TORQUE SHAFT) · airframe 41,359 hrs · 26,444 cycles

*PAX DOOR LATCH MECHANISM UPPER (DOOR CLOSED) TORQUE SHAFT STOP HAS EXFOLIATION CORROSION. (C-CHECK) RO 2/07/2020 REPLACED PAX DOOR UPPER LATCH MECHANISM STOP FITTING PER AMM. CHECKS GOOD.

Part: PANEL — CORRODED (PAX DOOR) · airframe 41,359 hrs · 26,444 cycles

PAX DOOR STAIR PANEL 832EL IS CORRODED. (C-CHECK) RO 2/07/2020 REMOVED CORROSION FROM PANEL 832EL, NOMINAL THICKNESS .050'' REMAINING MATERIAL THICKNESS AFTER BLENDING .046'', MATERIAL LOSS .004'' OF 8% OF NOMINAL THICKNESS, ALLOWABLE LOSS 50% OF NOMINAL THICKNESS, BLEND IS WITHIN LIMITS REF CRJ 700 SRM.

Part: SUPPORT ANGLE — CRACKED (WNG-BDY FAIRING) · airframe 41,359 hrs · 26,444 cycles

WING TO BODY FAIRING 195DL HAS CRACKED SUPPORT ANGLE (C-CHECK) RO 2/07/2020 REPLACED SUPPORT ANGLE ON BELLY FAIRING 195DL PER SRM AND INCORPORATED MODSUM.

Part: LEVER — BROKEN (CARGO DOOR LOCK) · airframe 41,359 hrs · 26,444 cycles

*FWD CARGO DOOR AFT LOCK LEVER BROKEN OFF (C-CHECK) RO 2/07/2020 REPLACED FWD CAGO DOOR AFT LOCK LEVER REF. CRJ-700 CMM. OP'S TEST PASSED.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 41,359 hrs · 26,444 cycles

*PAX DOOR INNER HANDLE CRACKED AT SHAFT. (C-CHECK) RO 2/07/2020 REMOVED AND INSTALLED NEW FROM STOCK PAX DOOR INNER HANDLE REF CRJ700 AMM.

Part: BAND — DETERIORATED (THRUST REVERSER) · airframe 41,359 hrs · 26,444 cycles

*LH PYLON THRUST REVERSER FLOATING TIE BAR INBOARD UPPER AND LOWER ELASTIC BUSHINGS AT K-FRAME ATTACHMENT ARE DETERIORATED AND DISBONDED. (C-CHECK) RO 2/07/2020 REPLACED BUSHINGS UPPER AND LOWER IN THE FLOATING TIE-BAR ENG LH PER CRJ 700 AMM TASK.

Part: LINER — CHAFED (RT NACELLE) · airframe 41,359 hrs · 26,444 cycles

*RH ENGINE FWD CORE COWL INTERNAL LINER CHAFED THROUGH AT FWD SIDE OF DRAIN PAN FROM CONTACT WITH ENGINE HARNESS. (C-CHECK) RO 2/07/2020 REMOVED AND REPLACED R/H ENG INTERNAL FWD CORE COWL DRAIN PANS IAW CRJ700 SRM AND AMM.

Part: BAR — DETERIORATED (THRUST REVERSER) · airframe 41,359 hrs · 26,444 cycles

*RH PYLON THRUST REVERSER FLOATING TIE BAR INBOARD UPPER AND LOWER ELASTIC BUSHINGS AT K-FRAME ATTACHMENT ARE DETERIORATED AND DISBONDED. (C-CHECK) RO 2/07/2020 REPLACED BUSHINGS UPPER AND LOWER IN THE FLOATING TIE-BAR ENGINE RH PER CRJ 700 AMM TASK. INSTALLED FLOATING TIE BAR IAW CRJ 700 AMM. OPS CHECK GOOD.

Part: LINER — DAMAGED (CARGO DOOR) · airframe 41,359 hrs · 26,444 cycles

FWD CARGO LINER 151 FLW HAS IMPACT DAMAGE/HOLE. (C-CHECK) RO 2/07/2020 REPAIRED CRACK ON CARGO PANEL # 151 FLW COMPLIED WITH C&D ZODIAC CMM.

Part: THRESHOLD — CRACKED (COCKPIT) · airframe 41,359 hrs · 26,444 cycles

COCKPIT/FWD GALLEY FLOOR THRESHOLD STRIP CRACKED. (C-CHECK) RO 2/07/2020 ORDERED AND RECEIVED NEW TRESHHOLD STRIP BETWEEN THE GALLEY AREA AND FLIGHT COMPATMENT. INSTALLED NEW TRESHOLD BETWEEN COCKPIT/FWD GALLEY FLOOR AREA. REF. CRJ-700 AMM.

Part: SKIN — CHAFED (LT NACELLE) · airframe 41,359 hrs · 26,444 cycles

*LH ENGINE UPPER FAN COWL HAS CHAFE IN FORMER FROM CONTACT WITH INBOARD TR FEEDBACK ACTUATOR LVDT HARNESS. (C-CHECK) RO 2/07/2020 COMPLIED WITH REPAIR SRS742 PER SRM.

Part: BRACKET — CRACKED (ZONE 200) · airframe 41,359 hrs · 26,444 cycles

FWD UPPER BRACKET ON THE ENTRANCE STORAGE COMPARTMENT IS CRACKED (MARKED). (C-CHECK) RO 2/07/2020 REMOVED AND REPLACED FWD UPPER BRACKET ON ENTRANCE STORAGE COMPARTMENT WITH NEW FROM STOCK REF C&D ZODIA CMM.

Part: STRINGER FITTING — CORRODED (FUSELAGE) · airframe 33,843 hrs · 20,411 cycles

STR JOINT PIECE AT FS 333 COMMON TO STR 25R HAS CORROSION. REMOVED OUT OF LIMITS STR JOINT PIECE AND REPLACED WITH NEW SERVICEABLE PART IAW SRM. LEAK CHECK GOOD AT THIS TIME.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 33,843 hrs · 20,411 cycles

PASSENGER DOOR INTERCOSTAL DD6, PN 601R318057-1 HAS CORROSION. INSTALLED NEW INTERCOSTAL DD6 IAW SRM. PRESSURIZATION LEAK CHECK GOOD, NO LEAKS FOUND.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 33,843 hrs · 20,411 cycles

CORROSION ON RT FLOOR SILL FS 349.0 AT RBL 42. COMPLIED WITH PERMANENT REPAIR ON RT FLOOR SILL AT FS 349.0, LBL42 IAW STS EA. LEAK CHECK GOOD.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 33,843 hrs · 20,411 cycles

FLOOR SUPPORT ANGLE ATTACHED TO PASSENGER DOOR SILL FS 310 TO FS 349 IS CORRODED. R & R PASSENGER DOOR FLOOR SUPPORT ANGLE IAW SRM. OPS CHECK GOOD AT THIS TIME.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 33,843 hrs · 20,411 cycles

INTERCOSTAL FS 319 TO FS 333, STR 20R IS CORRODED. REMOVED AND INSTALLED INTERCOSTAL BETWEEN FS 319.7 AND FS 349.00, STR 20R IAW SRM. PRESSURE CHECK AND LEAK CHECK GOOD AT THIS TIME.

Part: ACCESS PANEL — CHAFED (TE FLAP) · airframe 33,843 hrs · 20,411 cycles

LEFT INBD FLAP PANEL 584JB IS CHAFED. REPLACED LT INBD FLAP ACCESS PANEL 584JB, PN CC670-14178-1 IAW SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 33,843 hrs · 20,411 cycles

LEFT INTERCOSTAL BETWEEN FS 349.00 AND FS 364.00 COMMON TO STR 27 HAS CORROSION. REMOVED LT INTERCOSTAL BETWEEN FS 349.00 AND FS 364.00 COMMON TO STR 27 AND INSTALLED NEW SERVICEABLE LT INTERCOSTAL BETWEEN FS 349.00 AND FS 364.00 COMMON TO STR 27 IAW SRM. LEAK CHECK GOOD AT THIS TIME.

Part: PAN — CRACKED (FUSELAGE) · airframe 33,843 hrs · 20,411 cycles

FORWARD EQUIPMENT BAY FLOOR PAN HAS A CRACK AT APPROXIMATELY FS 195.0. ACCOMPLISHED PERMANENT REPAIR FORWARD EQUIPMENT BAY FLOOR PAN CRACKED AT APPROXIMATELY FS 195.00 LT SIDE BY ACCUMULATOR GAUGES IAW REO AND STS EA.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 33,843 hrs · 20,411 cycles

RIGHT LONGERON BETWEEN FS 333.00 AND FS 364.00 HAS CORROSION. R & R RT LONGERON BETWEEN FS 333 TO FS 364 COMMON TO STR 25R IAW SRM. LEAK CHECK GOOD.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 33,843 hrs · 20,411 cycles

STR 26R BETWEEN FS 333.00 AND FS 364.00 HAS CORROSION. INSTALLED NEW SERVICEABLE STRINGER, STR 26R BETWEEN FS 333-FS 364 IAW SRM. PRESSURIZATION LEAK CHECK ACCOMPLISHED. CHECKED GOOD AT THIS TIME IAW AMM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 33,843 hrs · 20,411 cycles

FRAME AT FS 295.00 HAS CORROSION BETWEEN STR 26L AND STR 26R. REPAIR OF FS 295.00 FRAME IAW REO. LEAK CHECK GOOD.

Part: FRAME — CORRODED (FUSELAGE) · airframe 33,843 hrs · 20,411 cycles

FRAME AT FS 333.00 HAS CORROSION BETWEEN STR 26L AND STR 26R. C/W REPAIR OF FS 333.00 FRAME IAW REO. LEAK CHECK GOOD.

Part: PLATE — CORRODED (FUSELAGE) · airframe 33,843 hrs · 20,411 cycles

RIGHT DOOR STOP BACKING PLATE BETWEEN STR 27 AND STR 26R AT FS 364.00 FRAME HAS CORROSION UNDER NUTPLATES. INSTALLED NEW FABRICATED REPAIR PART, RT DOOR STOP FITTING BACKING PLATE AT FS 364.00 FRAME BETWEEN STR 27 AND STR 26R IAW AMM..

Part: FRAME — CORRODED (FUSELAGE) · airframe 33,843 hrs · 20,411 cycles

FRAME AT FS 310.00 HAS CORROSION BETWEEN STR 25L AND STR 26R. REPAIR OF FS 310.00 FRAME IAW REO. LEAK CHECK GOOD.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 33,843 hrs · 20,411 cycles

ATTACHMENT ANGLE ON STR 26L BETWEEN FS 349.00 AND FS 364.00 HAS CORROSION. REPLACED WITH NEW SERVICEABLE ATTACHMENT ANGLE ON STR 26L BETWEEN FS 349-FS 364 IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 33,843 hrs · 20,411 cycles

STR 25R HAS CORROSION BETWEEN FS 319.7 AND FS 333.00. INSTALLED NEW SERVICEABLE STR 25R BETWEEN FS 280.00 AND FS 333.00 IAW SRM. PRESSURIZATION LEAK CHECK ACCOMPLISHED. CHECKED GOOD AT THIS TIME IAW AMM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 33,843 hrs · 20,411 cycles

RIGHT INTERCOSTAL BETWEEN FS 349.00 AND FS 364.00 COMMON TO STR 27 HAS CORROSION. REMOVED AND INSTALLED NEW SERVICEABLE RT INTERCOSTAL BETWEEN FS 349.00 AND FS 364.00 COMMON TO STR 27 IAW SRM. LEAK CHECK GOOD AT THIS TIME.

Part: FRAME — CORRODED (FUSELAGE) · airframe 33,843 hrs · 20,411 cycles

FRAME AT FS 319.7 HAS CORROSION BETWEEN STR 25L AND STR 26R. COMPLIED WITH REO REPAIR OF FS 319.7 FRAME, LEAK CHECK GOOD.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 33,843 hrs · 20,411 cycles

PASSENGER DOOR, CORROSION ON INTERCOSTAL DD2. INSTALLED INTERCOSTAL DD2 IAW SRM. PRESSURIZATION LEAK CHECK ACCOMPLISHED. CHECKED GOOD AT THIS TIME IAW AMM.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 33,843 hrs · 20,411 cycles

PASSENGER DOOR, CORROSION ON INTERCOSTAL DD4. INSTALLED INTERCOSTAL DD4 IAW SRM. PRESSURIZATION LEAK CHECK ACCOMPLISHED. CHECKED GOOD AT THIS TIME IAW AMM.

Part: PLENUM — WORN (LT ACM) · airframe 28,880 hrs · 17,397 cycles

LEFT AIR CONDITIONING PLENUM WORN. C-CHECK, R & R LT PLENUM IAW EA.

Part: HINGE — GOUGED (PAX DOOR) · airframe 28,880 hrs · 17,397 cycles

PASSENGER DOOR PIANO HINGE ON FUSELAGE HAS A GOUGE ON THE AFT MOST LAND. C-CHECK, REPAIRED PASSENGER DOOR PIANO HINGE GOUGE ON FUSELAGE IAW SRM AND REO.

Part: SKIN — DENTED (PAX DOOR) · airframe 28,880 hrs · 17,397 cycles

PASSENGER DOOR-FWD/UPPER SECTION WITH A DENT ON THE SKIN. AS MARKED. C-CHECK, R & R NEW PAX DOOR FWD UPPER CORNER COVER IAW SRM.

Part: BEARING — WORN (PAX DOOR) · airframe 28,880 hrs · 17,397 cycles

PASSENGER DOOR FWD PULL-IN LEVER WITH THE BEARING ASSY WORN. C-CHECK, BLENDED OUT CHAFE ON PASSENGER DOOR FWD PULL-IN-LEVER IAW REO.

Part: STOP FITTING — CHAFED (PAX DOOR) · airframe 28,880 hrs · 17,397 cycles

PASSENGER DOOR SURROUND STRUCTURE FWD UPPER FITTING STOP CHAFED. C-CHECK, BLENDED WEAR DAMAGE ON PAX DOOR UPPER FWD STOP FITTING IAW STS EA.

Part: WEB — CRACKED (BS 195) · airframe 28,880 hrs · 17,397 cycles

AT FS 195, SLOT IN LOWER DECK, WHERE FRAME PASSES THRU CRACKED AND EXTENDING UNDER ADG PUMP MOUNTING PLATE. REPAIRED CRACK IN ELECTRICAL BAY FLOOR WEB AT APPROXIMATELY FS 195, RT SIDE UNDER ADG PUMP IAW REO.

Part: SKIN — DENTED (NACELLE DOOR) · airframe 28,880 hrs · 17,397 cycles

LT ENGINE LOWER FAN COWL DOOR HAS SEVERAL DENTS AT 6 O'CLOCK POSITION. REPAIRED LT ENGINE LOWER FAN COWL DOOR DENTS IAW REO.

Part: LEAD — CHAFED (LT IDG) · airframe 28,880 hrs · 17,397 cycles

LT ENGINE IDG POWER LEADS CHAFING LOWER COWLING, 6:00 POSITION. C-CHECK, REPAIRED LT ENGINE IDG POWER CABLE IAW REO.

Part: SKIN — DENTED (PAX DOOR) · airframe 28,880 hrs · 17,397 cycles

PASSENGER DOOR-AFT/UPPER SECTION WITH A DENT ON THE SKIN. C-CHECK, COMPLIED WITH PERMANENT REPAIR IAW REO.

Part: DOOR — CORRODED (E/E BAY) · airframe 28,880 hrs · 17,397 cycles

MAIN AVIONICS COMPARTMENT DOOR-THE EXTERNAL SURROUND STRUCTURE INSIDE ACCESS ENTRY WITH MARKS OF CORROSION. C-CHECK, BLENDED OUT CORROSION FROM INNER SKIN OF MAIN AVIONICS DOOR CUTOUT SURROUND IAW REO.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 28,880 hrs · 17,397 cycles

FS 280 FLOORBEAM IS CORRODED. C-CHECK, R & R IAW REO. PERFORMED E/T INSP ON FS 280 BEAM IAW REO. NO DEFECTS NOTED. NDT REPORT ATTACHED.

Part: SKIN — DENTED (LT NACELLE) · airframe 28,880 hrs · 17,397 cycles

SEVERAL DENTS ON LT ENGINE LOWER NOSE COWL AND FAN COWL DOORS AT 6 O'CLOCK POSITION. COMPLIED WITH THE REPAIR OF SEVERAL DENTS ON THE LT ENGINE LOWER NOSE COWL AND FAN COWL DOORS AT THE 6 O'CLOCK POSITION IAW EA.

Part: LEAD — CHAFED (RT IDG) · airframe 28,880 hrs · 17,397 cycles

RIGHT ENGINE IDG ELECTRIC POWER LEAD CHAFING HYD PUMP LINE, 8:00 POSITION, JUST AFT OF HYD PUMP. C-CHECK, REPAIRED RT ENGINE IDG POWER CABLE IAW REO.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 26,987 hrs · 16,327 cycles

FOUND 5 ELONGATED HOLES IN LT SEAT TRACK AT FS 485 STRINGER 15L. C CHECK REPAIRED IAW REO.

Part: ENGINE — FAILED (NR 2) · airframe 26,598 hrs · 16,113 cycles

PERFORMED A REJECTED TAKE OFF AT APPROXIMATELY 105 KNOTS DUE TO LOSS OF DIRECTIONAL CONTROL & APPARENT LOSS OF POWER FROM THE NR 2 ENG. FLT 1301 REPLACED ENG ON CP 10385995.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,395 hrs · 15,428 cycles

EMERGENCY LIGHTS BURNED OUT. FLT#5538 RELAMPED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,033 hrs · 15,230 cycles

LT FLOOR SEAT TRACK AT FS 683.0 - 836.0 REQUIRES REPLACEMENT. C-CHECK REPLACE LT FLOOR SEAT TRACK AT FS 683.0 - 836.0 IAW AMM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,033 hrs · 15,230 cycles

RT FLOOR SEAT TRACK AT FS 581.0 - 683.0 REQUIRES REPLACEMENT. C-CHECK REPLACED RT FLOOR SEAT TRACK AT FS 581.0 - 683.0 IAW AMM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,033 hrs · 15,230 cycles

RT FLOOR SEAT TRACK AT FS 683.0 - 836.0 REQUIRES REPLACEMENT. C-CHECK REPLACED RT FLOOR SEAT TRACK AT FS 683.0 - 836.0 IAW AMM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,033 hrs · 15,230 cycles

RT FLOOR SEAT TRACK AT FS 350.0 - 485.0 REQUIRES REPLACEMENT. C-CHECK REPLACED RT FLOOR SEAT TRACK AT FS 350.0 - 485.0 IAW AMM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,033 hrs · 15,230 cycles

RT SIDE SEAT TRACK AT FS 379.0 - 477.4 REQUIRES REPLACEMENT. C-CHECK REPLACED RT SIDE SEAT TRACK AT FS 379.0 - 477.4 IAW AMM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,033 hrs · 15,230 cycles

LT FLOOR SEAT TRACK AT FS 485.0 - 581.0 REQUIRES REPLACEMENT. C-CHECK REPLACED LT FLOOR SEAT TRACK AT FS 485.0 TO 581.0 IAW AMM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,033 hrs · 15,230 cycles

LT SIDE SEAT TRACK AT FS 573.0 - 669.4 REQUIRES REPLACEMENT. C-CHECK REPLACED LT SIDE SEAT TRACK AT FS 573.0 - 669.4 IAW AMM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,033 hrs · 15,230 cycles

RT SIDE SEAT TRACK AT FS 785.15 - 861.0 REQUIRES REPLACEMENT. C-CHECK REPLACED RT SIDE SEAT TRACK AT FS 785.15 - 861.0 IAW AMM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,033 hrs · 15,230 cycles

LT FLOOR SEAT TRACK AT FS 581.0 - 683.0 REQUIRES REPLACEMENT. C-CHECK REPLACED LT FLOOR SEAT TRACK AT FS 581.0 - 683.0 IAW AMM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,033 hrs · 15,230 cycles

LT SIDE SEAT TRACK AT FS 785.15 - 861.0 REQUIRES REPLACEMENT. C-CHECK REPLACED LT SIDE SEAT TRACK AT FS 785.15 - 861.0 IAW AMM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,033 hrs · 15,230 cycles

RT SIDE SEAT TRACK AT FS 713.0 - 761.85 REQUIRES REPLACMENT. C-CHECK REPLACED RT SIDE SEAT TRACK AT FS 713.0 - 761.85 IAW AMM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,033 hrs · 15,230 cycles

LT SIDE SEAT TRACK AT FS 379.0 - 477.4 REQUIRES REPLACEMENT. C-CHECK REPLACED LT SIDE SEAT TRACK AT FS 379.0 - 477.4 IAW AMM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,033 hrs · 15,230 cycles

RT SIDE SEAT TRACK AT FS 669.4 - 713.0 REQUIRES REPLACEMENT. C-CHECK REPLACED RT SIDE SEAT TRACK AT FS669.4 - 713.0 IAW AMM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,033 hrs · 15,230 cycles

LT FLOOR SEAT TRACK AT FS 374.0 - 485.0 REQUIRES REPLACEMENT. C-CHECK REPLACED LT FLOOR SEAT TRACK FS 374.0 - 485.0 IAW AMM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,033 hrs · 15,230 cycles

LT SIDE SEAT TRACK AT FS 669.4 - 713.0 REQUIRES REPLACEMENT. C-CHECK REPLACED LT SIDE SEAT TRACK AT FS 669.4 - 713.0 IAW AMM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,033 hrs · 15,230 cycles

RT SIDE OF SEAT TRACK AT FS 573.0 - 699.4 REQUIRES REPLACEMENT. C-CHECK REPLACED RT SIDE SEAT TRACK AT FS 573.0 - 699 IAW AMM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,033 hrs · 15,230 cycles

LT SIDE SEAT TRACK AT FS477.4 - 573.0 REQUIRES REPLACEMENT. C-CHECK REPLACED LT SIDE SEAT TRACK AT FS 477.4 - 573.0 IAW AMM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,033 hrs · 15,230 cycles

RT SIDE SEAT TRACK AT FS 477.4 - 573.0 REQUIRES REPLACEMENT. C-CHECK REPLACED RT SIDE SEAT TRACK AT FS 477.4 - 573.0 IAW AMM.

Part: SKIN — CHAFED (BS 980) · airframe 25,033 hrs · 15,230 cycles

DURING C-CHECK, CHAFE ON LOWER SKIN AT FS 980. REPAIRED CHAFE ON LOWER SKIN AT FS 980 IAW REO.

Part: LEVER — CHAFED (PAX DOOR) · airframe 25,033 hrs · 15,230 cycles

C-CHECK, PAX DOOR FWD, PULL IN LEVER CHAFED. BLENDED DAMAGE ON PAX DOOR IAW REO.

Part: SKIN — CORRODED (FUSELAGE) · airframe 25,033 hrs · 15,230 cycles

MAIN AVIONICS COMPARTMENT DOOR CUT OUT SURROUND SKIN HAS FRETTING CORROSION ON INNER SKIN SURFACE. C-CHECK REPAIRED IAW REO.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 25,033 hrs · 15,230 cycles

FS 280 FLOORBEAM IS CORRODED BEYOND LIMITS REPLACEMENT REQUIRED. C-CHECK REPLACED FS 280.0 CROSSBEAM IAW REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,382 hrs · 14,846 cycles

NR 4 AND NR 5 OVERHEAD EMERGENCY LIGHTS ARE BURNED OUT. (FLT 5527) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,949 hrs · 14,590 cycles

NR 2 OVERHEAD EMERGENCY LIGHT DOES NOT ILLUMINATE. (FLT 6476) REPLACED NR 2 EMERGENCY POD LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,758 hrs · 14,488 cycles

EMERGENCY EXIT ROW LIGHT IN ROW 12 A AND B HAS A BULB OUT. (FLT 5159) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,226 hrs · 14,164 cycles

NR 2 OVERHEAD EMERGENCY LIGHT BURNED OUT. (FLT 5648) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,506 hrs · 13,179 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6239) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,474 hrs · 13,161 cycles

SECOND FROM LAST OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: SIGN — INOPERATIVE (CABIN) · airframe 21,341 hrs · 13,088 cycles

MID CABIN OVERHEAD FLIGHT ATTENDANT EMERGENCY EXIT SIGN LIGHTS ARE OUT. (FLT 5297) REPLACED OVERHEAD EMERGENCY EXIT SIGN ASSEMBLY MID CABIN IN REF TO AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,308 hrs · 13,070 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: CABLE — FAILED (PAX DOOR) · airframe 21,308 hrs · 13,070 cycles

PASSENGER DOOR IS HARD TO OPEN FROM EXTERIOR AND WILL NOT POP OUT FROM FUSELAGE CUTOUT. (SERVICE) REPLACED THE PASSENGER DOOR AFT GAS SPRING AFT CABLE. ADJUSTED GAS SPRING CABLE ANCHOR IN REF TO AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,066 hrs · 12,927 cycles

NR 5 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5428) RELAMPED EMERGENCY LIGHT.

Part: LATCH — OBSTRUCTED (JUMPSEAT) · airframe 20,912 hrs · 12,842 cycles

AFT FLIGHT ATTENDANT JUMPSEAT SEAT BELT BUCKLE LATCH IS STICKING. (FLT 6261) CLEANED DEBRIS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,670 hrs · 12,709 cycles

NR 5 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5192) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,626 hrs · 12,689 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6397) RELAMPED EMERGENCY LIGHT.

Part: SKIN — CHAFED (LT AILERON) · airframe 20,356 hrs · 12,523 cycles

LEFT AILERON UPPER LEADING EDGE CHAFED. (C-CHECK) REPLACE LEFT AILERON UPPER LEADING EDGE PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 20,326 hrs · 12,507 cycles

AFT 2 OVERHEAD EMERGENCY LIGHTS ARE OUT. (SERVICE) REPLACED NR 4 ELBP & BATTERY CHARGER. P/N:AD-2013-1A S/N OFF:75713

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,326 hrs · 12,507 cycles

NR 5 CEILING EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,303 hrs · 12,496 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5350) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,189 hrs · 12,434 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4248) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,121 hrs · 12,396 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5785) RELAMPED EMERGENCY LIGHT.

Part: RELAY — FAILED (EMERGENCY LIGHT) · airframe 19,574 hrs · 12,111 cycles

EMERGENCY EXIT LIGHTS CYCLE ON AND THEN OFF CONTINUOUSLY WHEN IN THE 'AUTO' POSITION. (FLT 2059) REPLACED RELAY K135 IN JB11.

Part: SENSOR — OUT OF ADJUST (NLG) · airframe 18,928 hrs · 11,757 cycles

GEAR DISAGREE WARNINGS. (FLT 6497) ADJUSTED LEFT NLG WEIGHT ON WHEELS SENSOR.

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 17,705 hrs · 11,069 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN. (FLT 6940) CLEANED AND LUBED MAIN CABIN DOOR ROLLERS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,401 hrs · 10,288 cycles

NR 2 OVERHEAD EMERGENCY LIGHT INOPERATIVE. (FLT 6093) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,892 hrs · 9,984 cycles

SECOND TO LAST EMERGENCY CEILING LIGHT INOP. (FLT 6115) RELAMPED EMERGENCY LIGHT.

Part: PRINTED CKT BOARD — DEFECTIVE (EMERGENCY LIGHT) · airframe 15,892 hrs · 9,984 cycles

EMERGENCY LIGHT ILLUMINATING INTERMITTENTLY. (FLT 6573) REPLACED PCB5 ON JB11 PER AMM.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 15,664 hrs · 9,848 cycles

FS 280 CROSSBEAM CORRODED AND CRACKED. (C CHECK) BEAM REPLACED PER REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,360 hrs · 9,661 cycles

NR 5 EMERGENCY EXIT LIGHT INOP. (FLT 5934) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,615 hrs · 9,204 cycles

CEILING EMERGENCY FLOODLIGHT ADJACENT TO ROW 14 INOP. (FLT 6644) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,562 hrs · 9,164 cycles

NR 2 CABIN CEILING EMERGENCY LIGHT INOP. (FLT 6572) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,947 hrs · 8,805 cycles

ROW 4 EMERGENCY OVERHEAD LIGHT INOP. (FLT 6942) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,814 hrs · 8,725 cycles

EMERGENCY CEILING LEVEL FLOODLIGHT OVER ROW 15 INOP. (FLT 6093) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,647 hrs · 8,627 cycles

SECOND TO LAST CEILING LEVEL EMERGENCY FLOODLIGHT INOP. (FLT 6100) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,444 hrs · 8,520 cycles

NR 2 EMERGENCY CEILING LIGHT INOP. (FLT 5818) RELAMPED EMERGENCY LIGHT.

Part: ADC — MALFUNCTIONED (NR 1) · airframe 13,298 hrs · 8,434 cycles

CAPTAINS AND FIRST OFFICERS ALTIMETER READINGS BEYOND LIMITS. (FLT 6097) REPLACED NR 1 ADC.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,117 hrs · 8,332 cycles

MAIN CABIN DOOR EMERGENCY LIGHT INOP. (FLT 6704) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,579 hrs · 7,997 cycles

EMERGENCY EXIT LIGHT INOP. (FLT 6547) RELAMPED EMERGENCY LIGHT.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 12,465 hrs · 7,930 cycles

FLT 5987 - OVERHEAD EMERGENCY FLOODLIGHT NR 6 INOP. RELAMPED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 12,304 hrs · 7,834 cycles

FLT 5952 - NR 4 EMERGENCY LIGHT INOP. RELAMPED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 12,260 hrs · 7,812 cycles

FLT 6644 - LOWER LEFT SIDE OVERWING EMERGENCY EXIT SIGN INOP. RELAMPED.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 12,203 hrs · 7,776 cycles

FLT 6543 - CAPTAINS WINDSHIELD CRACKED. REPLACED WINDSHIELD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 11,005 hrs · 7,029 cycles

CLT 6663 - CEILING EMERGENCY FLOOD LIGHT, AFT CABIN, INOP. RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,799 hrs · 6,904 cycles

NR 4 CEILING LEVEL EMERGENCY FLOODLIGHT INOP (FLT 5818). RELAMPED EMERGENCY LIGHT.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 10,737 hrs · 6,870 cycles

FLT 6564 - EMERGENCY EXIT SIGN LEFT SIDE INOP. REPLACED CHARGER AND BATTERY.

Part: STEERING SYS — MALFUNCTIONED (NLG) · airframe 10,337 hrs · 6,640 cycles

CAUTION STEERING INOP. MESSAGE UPON TOUCH DOWN (WOW) RUNWAY 120 IN SAT AIRCRAFT VEERED OFF THE RUNWAY. CLEARED NWS PLT HANDWHEEL FAULT CHECKED RIGGING OF NWS CONTROL BOX. PERFORMED TAXI CHECK.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 8,888 hrs · 5,786 cycles

FLT 6612 - EMERGENCY LIGHT IN FRONT OF CABIN IS INOP. REPLACED NR 1 ELBP AS REQUIRED. LIGHTS OPS CHECK GOOD.

Part: POWER SUPPLY — DISCHARGED (EMERGENCY LIGHTS) · airframe 8,023 hrs · 5,259 cycles

FLT 6710 - OVERHEAD EMERGENCY LIGHT POD IS INOP. REPLACED NR 4 ELBP IAW CRJ AMM 33-51-17. OPS CHECK GOOD.

Part: CONTROL CABLE — FRAYED (RUDDER) · airframe 8,300 hrs · 5,432 cycles

LEFT OUTBOARD RUDDER CABLE IS WORN, FOUND AT C-CHECK. REPLACED RUDDER CABLE IAW CRJ7/9 AMM 27-21-00-400-801-A02.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 5,363 hrs · 3,554 cycles

ON CLIMB-OUT ABOUT FL190, THE F/O WINDSHIELD CRACKED. REPLACED RIGHT WINDSHIELD PER AMM 56-12-01. OPS CHECK GOOD, P/N OFF: NP139321-003, S/N OFF: 04231H3790.

Part: SIGN — INOPERATIVE (CABIN) · airframe 5,313 hrs · 3,523 cycles

LIGHTED "EXIT" PLACARD ON GALLEY SERVICE DOOR FAILS TO LIGHT. SECURED CONNECTION AT GALLEY SERVICE DOOR TOP EXIT SIGN LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD.

Part: STEP — CRACKED (PAX DOOR) · airframe 4,160 hrs · 2,780 cycles

PAX DOOR HAS 2 CRACKS ON FWD AND AFT ENDS OF SECOND STAIR FROM THE TOP, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS PER BOMBARDIER PER REO 670-52-11-104 AND RII 52-900-1000.

Part: ACM — MALFUNCTIONED (A/C BAY) · airframe 3,903 hrs · 2,613 cycles

AFTER ENGINE START WITH BOTH PACKS ON, RECEIVED SIGNIFICANT AMOUNT OF SMOKE AND DIRT IN COCKPIT. LEFT PACK AUTO FAIL MESSAGE AND TEMP FAIL MESSAGE. REPLACED LEFT SIDE ACM IAW CRJ MM 21-51-08. OPERATIONAL CHECKS GOOD, SN OFF: 00911.

Part: CONTROL UNIT — MALFUNCTIONED (SLAT\FLAP SYSTEM) · airframe 2,775 hrs · 1,880 cycles

SLAT HALFSPEED STATUS MSG. REPLACED NR 2 SFECU IAW AMM 22-51-01. OPERATIONAL CHECK GOOD.

Part: DETECTOR — MALFUNCTIONED (TE FLAPS) · airframe 1,044 hrs · 741 cycles

FLAPS HALFSPEED STATUS MESSAGE AFTER DEPARTING ORD. REPLACED LEFT OB FLAP, OB SENSOR IAW MM 27-52-45. OPERATIONAL CHECK GOOD.