N738EV

Part: WINDOW — FAILED (ZONE 200) · airframe 39,148 hrs · 28,811 cycles

CAPTAIN SIDE WINDOW SHATTERED ON CLIMB OUT (FLIGHT 6335 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 29965758 WITH THE FOLLOWING CORRECTIVE ACTION: "REMOVED AND REPLACED CAPTAIN SIDE WINDOW PER CRJ700 MIP 56-220-1000-SKY"

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 38,962 hrs · 28,674 cycles

UPON REMOVAL OF FLOOR BOARD 251BLF BETWEEN FS677.00 - FS693.00 ON FLOOR BEAM LBL9 ON TOP OF INBOARD FLANGE AND JUST FWD OF END OF SEAT TRACK, FOUND CORROSION AND PREVIOUS BLEND OUT. CAMP# 29710999 (C-CHECK RO 3/14/2025) REMOVED CORROSION FROM I/B FLANGE OF FLOOR BEAM FS 677.0-693.0 LBL 9.0 JUST FWD. OF END OF SEAT TRACK IAW REO 670-53-31-1013 REV -- DATED: 2025-02-28. COMPLIED WITH SKYWEST TASK CARD: 51-900-1002-SKY

Part: RIB — CRACKED (ZONE 500) · airframe 38,962 hrs · 28,674 cycles

DURING REMOVAL OF LH FIXED L/E INBD SEAL, FOUND CRACK ON LH RIB SS57.16. (C-CHECK RO 3/14/2025) REPAIRED LH WING RIB AT SS 57.16 AS PER MHIRJ REO 670-57-41-598 REV -- DATED 2024-12-24. ALL STEPS OF REO COMPLIED WITH. COMPLIED WITH 337 AND SKYWEST TASK CARD 51-900-1002-SKY

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 38,962 hrs · 28,674 cycles

FLOOR BEAM RBL9 HAS MULTIPLE SPOTS OF CORROSION BETWEEN FS581-FS677 (C-CHECK RO 3/14/2025) BLENDS FOUND TO BE OUT OF LIMITS, INSTALLED FLOOR BEAM RBL9 IB FLANGE REPAIR AT APPROX FS592-FS602, FS608-FS624, & FS634-FS650 REF CRJ700 SRM 53-00-41-201-001-A01 FIGURE 53-00-41-991-829, CAPTURING ALL DAMAGE, COMPLIED WITH 51-900-1002-SKY

Part: CLEAT — CORRODED (ZONE 800) · airframe 38,962 hrs · 28,674 cycles

PASSENGER DOOR 2EA CLEATS (600-31902-269) COMMON TO INTERCOSTAL P/N 600-31902-257 CORRODED. CAMP 29263752. (C-CHECK RO 3/14/2025) REMOVED AND REPLACED PASSENGER DOOR 2EA CLEATS (600-31902-269) COMMON TO INTERCOSTAL P/N 600-31902-257 REF. DRWG 601R31702 REV. N AND CRJ 700 SRM 51-42-06-001-001-A01. COMPLIED WITH SKY WEST TC 51-900-1002-SKY.

Part: ANGLE — CORRODED (ZONE 800) · airframe 38,962 hrs · 28,674 cycles

PASSENGER DOOR DD7 FWD INTERCOSTAL CLIP P/N 601R318824-1 CORRODED. CAMP 29254117. (C-CHECK RO 3/14/2025) REMOVED AND REPLACED PASSENGER DOOR DD7 FWD INTERCOSTAL CLIP, REF. DRWG 601R31702 REV. N AND CRJ-700, SRM 51-42-06-001-001-A01. COMPLIED WITH SKY WEST TC 51-900-1002-SKY.

Part: SLAT TRACK — WORN (ZONE 600) · airframe 38,962 hrs · 28,674 cycles

R/H #1 SLAT, #3 TRACK HAS AREA OF WEAR (C-CHECK RO 3/14/2025) BLENDED OUT CHAFED ON R/H #1 SLAT #3 TRACK (2EA). REPAIRED RH #1 SLAT #3 TRACK FOUND TO BE STRUCTURALLY AND FUNCTIONALLY ACCEPTABLE PER REO 670-57-42-1875 REV -- DATED 2024-12-04. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. OP CHECK GOOD. RIG CHECK GOOD. SEE CONTINUATION CARD FOR DETAILS.

Part: SKIN — DENTED (ZONE 100) · airframe 38,962 hrs · 28,674 cycles

DENT AT FS 220.00 ON EXTERNAL AIRCRAFT SKIN BETWEEN STGR 23R - 24R. MARKED. (C-CHECK RO 3/14/2025) REPAIRED DENT AT FS 220.00 ON EXTERNAL AIRCRAFT SKIN BETWEEN STGR 23R - 24R PER REO 670-53-11-2067 REV -- DATER 2024-12-27. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. LEAK CHECK GOOD. SEE CONTINUATION CARD FOR DETAILS.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 38,962 hrs · 28,674 cycles

INNER CHORD UNDER AFT CARGO FLOOR SILL BETWEEN FS1031 AND FS1046 CORRODED AROUND NUTPLATE HOLES. (C-CHECK RO 3/14/2025) REMOVED AND REPLACED INNER CHORD UNDER AFT CARGO DOOR SILL BETWEEN FS1031 AND FS1046. REF. CRJ700 SRM 51-42-06-001-001-A01 AND DWG# MM670-35085 REV. L. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY (CL600-2C10) STRUCTURAL MAJOR REPAIR (**RII**)

Part: SLAT TRACK — CORRODED (ZONE 600) · airframe 38,962 hrs · 28,674 cycles

R/H #3 SLAT, #2 TRACK HAS LIGHT CORROSION AND WEAR AT UPPER INBD EDGE (C-CHECK RO 3/14/2025) REPAIRED THE RH 3-2 SLAT TRACK AS PER REO 670-57-42-1880 REV -- DATED 2024-12-05. OPS CHECKS GOOD SEE CONTINUE CARD FOR DETAILS. M-337 AND SKYWEST TASK CARD 51-900-1002-SKY COMPLIED WITH.

Part: CHANNEL — CORRODED (ZONE 100) · airframe 38,962 hrs · 28,674 cycles

DRAIN MAST CHANNEL ATTACHMENT CORRODED BETWEEN FS 1031.00 AND FS1051. STGR 27 #29227777 (C-CHECK RO 3/14/2025) INSTALLED NEW REPLACEMENT AFT DRAIN MAST CHANNEL (P/N MM670-43255-001) USING ALL NEW FASTENERS BETWEEN FS1031.00 AND FS1051.00 BETWEEN STGR 26R AND STGR27. REF BOMBARDIER DWG MM670-43200 REV -N AND CRJ700 SRM 51-42-06-001-001 A01. LEAK CHECKED GOOD. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.

Part: SLAT TRACK — CORRODED (ZONE 600) · airframe 38,962 hrs · 28,674 cycles

R/H #2 SLAT, #2 TRACK HAS TWO AREAS OF LIGHT PITTING CORROSION (C-CHECK RO 3/14/2025) PERFORMED A BLEND OUT REPAIR ON R/H #2 SLAT #2 TRACK AND FOUND TO BE STRUCTURALLY ACCEPTABLE PER REO 670-57-42-1874 REV -- DATE: 2024-12-04 COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. SEE CONTINUATION CARD FOR DETAILS.

Part: SKIN — DAMAGED (ZONE 200) · airframe 38,962 hrs · 28,674 cycles

MULTIPLE LIGHTNING STRIKES ALONG LH, LOWER EXTERNAL AIRCRAFT SKIN BETWEEN FS 202.00 - 581.00. MARKED AND NUMBERED (12EA) (C-CHECK RO 3/14/2025) REPAIRED DAMAGE ALONG LH, LOWER EXTERNAL AIRCRAFT SKIN BETWEEN FS 202.00 - 581.00 REF. MHIRJ REO 670-53-00-762 REV -A DATE 2025-01-02. COMPLIED WITH ALL STEPS OF TASK CARD 51-900-1002-SKY. REPAIRED 2EA LOCATION WITH A CUT OUT REPAIR PER MHIRJ REO 670-53-11-2070 REV--, DATED 2024-12-30, ALL STEPS COMPLIED WITH.

Part: SLAT TRACK — WORN (ZONE 600) · airframe 38,962 hrs · 28,674 cycles

R/H #3 SLAT #3 TRACK HAS AREA WITH WEAR MARKS (C-CHECK RO 3/14/2025) REPAIRED RH #3 SLAT #3 TRACK AS PER REO 670-57-42-1873 REV -- DATED 2024-12-04. M-337 AND SKYWEST TASK CARD 51-900-1002-SKY COMPLIED WITH.

Part: INTERCOSTAL — MECHANIC ERROR (ZONE 200) · airframe 38,962 hrs · 28,674 cycles

WHILE LOCATING AND DRILLING NEW DD2 MID INTERCOSTAL, LOCATED PART IN DIFFERENT AREA MAKING THE HOLES NOT LINE UP WITH EXISTING HOLES. (C-CHECK RO 3/14/2025) RELOCATED DD2 MID AND ADDRESSED ELONGATED HOLE REF. REO 670-52-11-1427 REV. -- DATED 2024-12-06 COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. LEAK CHECK GOOD. SEE CONTINUATION CARD FOR DETAILS.

Part: LUG — DAMAGED (ZONE 200) · airframe 38,962 hrs · 28,674 cycles

UPON REMOVAL OF PASSENGER DOOR FOUND AFT 7 LUG HOLES ELONGATED. CAMP 29210559. (C-CHECK RO 3/14/2025) REMOVED AND REPLACED PAX DOOR HINGE FUSELAGE SIDE WITH A NEW SERVICEABLE UNIT REF CRJ700 SRM TASK 53-21-23-201-007-A01 REV 38 DATED 25 JULY 2020 AND DWG. SH670-31810 REV. AE LEAK CHECK GOOD. SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH SKYWEST TASK CRD 51-900-1002-SKY.

Part: LANDING — CRACKED (ZONE 100) · airframe 38,962 hrs · 28,674 cycles

LEFT HAND TRU ACCESS DOOR LAND VISIBLE CRACK ON AFT LATCH CUT-OUT (C-CHECK RO 3/14/2025) REMOVED AND REPLACED CRACKED LEFT HAND TRU LANDING WITH NEW LANDING (P/N CC670-33151-3) USING ALL NEW FASTENERS, REF BOMBARDIER DWG# CC670-33040 REV G AND CRJ700 SRM 51-42-06-001-001 A01. SEE CONTINUATION STEPS FOR MORE DETAILS. SKYWEST TASK CARD 51-900-1002-SKY AND M-337 COMPLIED WITH.

Part: ANGLE — CORRODED (ZONE 800) · airframe 38,962 hrs · 28,674 cycles

PASSENGER DOOR ANGLE NEAR OUTER HANDLE BOX CORRODED. CAMP 29201029. (C-CHECK RO 3/14/2025) REMOVED AND REPLACE PASSENGER DOOR ANGLE NEAR OUTER HANDLE BOX, REF. DRW 601R31702, REV. N, CRJ-700, SRM 51-42-21-001-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY

Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 38,962 hrs · 28,674 cycles

PASSENGER DOOR DD1A MID INTERCOSTAL CORRODED. CAMP 29200915. (C-CHECK RO 3/14/2025) REMOVED AND INSTALLED PASSENGER DOOR DD1A MID INTERCOSTAL REF. DRW 601R31702, REV. N, CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-21-001-001-A01 COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. LEAK CHECK GOOD.

Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 38,962 hrs · 28,674 cycles

PASSENGER DOOR DD7A INTERCOSTAL CORRODED. CAMP 29200974. (C-CHECK RO 3/14/2025) REMOVED AND INSTALLED PASSENGER DOOR DD7A INTERCOSTAL, REF. DRW 601R31702, REV. N, CRJ-700, SRM 51-42-06-001-001-A01 AND CRJ-700, SRM 51-42-21-001-001-A01. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. SEE CONTINUATION CARD FOR DEDETAILS. LEAK CHECK GOOD.

Part: FORMER — CORRODED (ZONE 800) · airframe 38,962 hrs · 28,674 cycles

PASSENGER DOOR FS329.41 FORMER, BETWEEN DD5 AND DD6 CORRODED. CAMP 29202916. (C-CHECK RO 3/14/2025) REMOVED AND INSTALLED PASSENGER DOOR FS329.41 FORMER, BETWEEN DD5 AND DD6, REF. DRW 601R31702, REV. N, CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-21-001-001-A01. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. LEAK CHECK GOOD.

Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 38,962 hrs · 28,674 cycles

PASSENGER DOOR DD4 AFT INTERCOSTAL CORRODED. CAMP 29201169. (C-CHECK RO 3/14/2025) REMOVED AND INSTALLED NEW PASSENGER DOOR DD4 AFT INTERCOSTAL REF. DRWG 601R31702 REV. N AND CRJ 700 SRM 51-42-06-001-001-A01. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. LEAK CHECK GOOD. SEE CONTINUATION CARD FOR DETAILS.

Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 38,962 hrs · 28,674 cycles

PASSENGER DOOR DD6 MID INTERCOSTAL CORRODED. CAMP 29200953. (C-CHECK RO 3/14/2025) REMOVED AND INSTALLED PASSENGER DOOR DD6 MID INTERCOSTAL REF. DRW 601R31702, REV. N, CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-21-001-001-A01. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. LEAK CHECK GOOD. SEE CONTINUATION CARD FOR DETAILS.WHILE REPLACING INTERCOSTAL, FOUND CLEAT CRACKED. REPALCED WITH NEW P/N 600-31902-269.

Part: INTERCOSTAL — CORRODED (ZONE 200) · airframe 38,962 hrs · 28,674 cycles

PASSENGER DOOR DD2 MID INTERCOSTAL CORRODED. CAMP 2900904. (C-CHECK RO 3/14/2025) REMOVED AND INSTALLED PASSENGER DOOR DD2 MID INTERCOSTAL REF. DRWG 601R31702 REV. N AND CRJ 700 SRM 51-42-06-001-001-A01. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. LEAK CHECK GOOD. SEE CONTINUATION CARD FOR DETAILS.

Part: INTERCOSTAL — CORRODED (ZONE 200) · airframe 38,962 hrs · 28,674 cycles

PASSENGER DOOR DD1 MID INTERCOSTAL CORRODED. CAMP 29200795. (C-CHECK RO 3/14/2025) REMOVED AND INSTALLED PASSENGER DOOR DD1 MID INTERCOSTAL REF. DRW 601R31702, REV. N, CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-21-001-001-A01. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. LEAK CHECK GOOD.

Part: FORMER — CRACKED (ZONE 800) · airframe 38,962 hrs · 28,674 cycles

PASSENGER DOOR AFT FORMED CRACKED. CAMP 29200642. (C-CHECK RO 3/14/2025) REMOVED AND INSTALLED NEW PASSENGER DOOR AFT FORMER REF. DRWG 601R31702 REV. N, CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-21-001-001-A01. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. LEAK CHECK GOOD.

Part: INTERCOSTAL — CORRODED (ZONE 200) · airframe 38,962 hrs · 28,674 cycles

PASSENGER DOOR DD4 MID INTERCOSTAL CORRODED. CAMP 29200939. (C-CHECK RO 3/14/2025) REMOVED AND INSTALLED PASSENGER DOOR DD4 MID INTERCOSTAL REF. DRW 601R31702, REV. N, CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-21-001-001-A01. LEAK CHECK GOOD. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.

Part: INTERCOSTAL — BENT (ZONE 800) · airframe 38,962 hrs · 28,674 cycles

PASSENGER DOOR DD1 AFT INTERCOSTAL BENT. CAMP 29201100. (C-CHECK RO 3/14/2025) REMOVED AND INSTALLED NEW PASSENGER DOOR DD1 AFT INTERCOSTAL REF. DRWG 601R31702 REV. N AND CRJ 700 SRM 51-42-06-001-001-A01. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. LEAK CHECK GOOD.

Part: FORMER — CORRODED (ZONE 800) · airframe 38,962 hrs · 28,674 cycles

PASSENGER DOOR FWD FORMED CORRODED. CAMP 29200567. (C-CHECK RO 3/14/2025) REMOVED AND INSTALLED NEW PASSENGER DOOR FWD FORMER REF. DRWG 601R31702 REV. N, CRJ-700, SRM 51-42-06-001-001-A01 AND CRJ-700, SRM 51-42-21-001-001-A01. COMPLIED WITH SKYWEST TASK CARD. PRESSURE LEAK CHECK GOOD.

Part: DOUBLER — CRACKED (ZONE 200) · airframe 38,962 hrs · 28,674 cycles

PASSENGER DOOR AFT PULL IN CAM DOUBLER CRACKED. CAMP 29201392. (C-CHECK RO 3/14/2025) REMOVED AND REPLACED PASSENGER DOOR AFT PULL IN CAM DOUBLER REF. DRWG 601R31702 REV. N, CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-21-001-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY AND SKYWEST FORM M337.

Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 38,962 hrs · 28,674 cycles

PASSENGER DOOR DD5 AFT INTERCOSTAL CORRODED. CAMP 29201248. (C-CHECK RO 3/14/2025) REMOVED AND INSTALLED NEW PASSENGER DOOR DD5 AFT INTERCOSTAL REF. DRWG 601R31702 REV. N AND CRJ 700 SRM 51-42-06-001-001-A01. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. LEAK CHECK GOOD. SEE CONTINUATION CARD FOR DETAILS.

Part: INTERCOSTAL — CORRODED (ZONE 200) · airframe 38,962 hrs · 28,674 cycles

PASSENGER DOOR DD3 MID INTERCOSTAL CORRODED. CAMP 29200928. (C-CHECK RO 3/14/2025) REMOVED AND INSTALLED PASSENGER DOOR DD3 MID INTERCOSTAL REF. DRW 601R31702, REV. N, CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-21-001-001-A01. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. SEE CONTINUATION CARD FOR DETAILS. LEAK CHECK GOOD.

Part: INTERCOSTAL — CRACKED (ZONE 800) · airframe 38,962 hrs · 28,674 cycles

PASSENGER DOOR DD7 AFT INTERCOSTAL CRACKED. CAMP 29201333. (C-CHECK RO 3/14/2025) REOMVED AND INSTALLED NEW PASSENGER DOOR DD7 AFT INTERCOSTAL REF. DRWG 601R31702 REV. N AND CRJ 700 SRM 51-42-06-001-001-A01. LEAK CHECK GOOD. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.

Part: INTERCOSTAL — BENT (ZONE 800) · airframe 38,962 hrs · 28,674 cycles

PASSENGER DOOR FWD DD1 INTERCOSTAL BENT. CAMP 29200753. (C-CHECK RO 3/14/2025) REMOVED AND INSTALLED NEW PASSENGER DOOR DD1 FWD INTERCOSTAL REF. DRWG 601R31702 REV. N AND CRJ 700 SRM 51-42-06-001-001-A01. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. SEE CONTINUATION CARD FOR DETAILS. LEAK CHECK GOOD.WHILE RELACING INTERCOSTAL FOUND BRACKET CRACKED. REPALCED WITH NEW P/N 601R318084-2.

Part: FITTING — GROOVED (DOOR FRAME) · airframe 38,962 hrs · 28,674 cycles

PASSENGER DOOR SURROUND FS310 CAM FITTING GROOVED ON LOWER SURFACE (C-CHECK RO 3/14/2025) INSTALLED NEW REPLACEMENT CAM FITTING AT PAX DOOR SURROUND STRUCTURE FS.310 STGR 5L PER CRJ700 SRM TASK 51-42-21-001-001-A01 REF. BOMBARDIER DWG. SH670-31810 REV. AE. COMPLIED WITH TASK CARD 51-900-1002-SKY AND M337.

Part: STRIKER — GOUGED (ZONE 200) · airframe 38,962 hrs · 28,674 cycles

PASSENGER DOOR SURROUND LOWER SEAL STRIKER GOUGED NUMEROUS PLACES (C-CHECK RO 3/14/2025) REMOVED DISCREPANT PAX DOOR LOWER SILL STRIKER ANGLE FOR REPLACEMENT REF. CRJ700 SRM TASK 51-42-20-001-001-A01. WET INSTALLED NEW REPLACEMENT PAX DOOR SURROUND LOWER SILL STRIKER ANGLE AT DOOR THRESHOLD PER. CRJ700 SRM TASK 51-42-20-001-001-A01 REF. BOMBARDIER DWG. SH670-31810 REV. AE. COMPLIED WITH SKY WEST TC 51-900-1002-SKY.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 38,962 hrs · 28,674 cycles

CRACK NOTED ON LBL12 FLOORBEAM ATTACHED TO FWD SIDE OF 280 CROSSBEAM (C-CHECK RO 3/14/2025) REMOVED AND REPLACED LBL12 BEAM SECTION FROM PREVIOUS REPAIR. REF CRJ700 SRM 53-11-43-201-003-A01 REPAIR TYPE IV. REV. 38 ISSUED 07/25/2020, SRM 51-42-06-001-001-A01 REV 38 DATED 07/25/2020, SRM 51-42-21-001-001-A01 REV 38 DATED 07/25/2020. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY (CL600-2C10) STRUCTURAL MAJOR REPAIR (**RII**).

Part: SUPPORT — CRACKED (ZONE 100) · airframe 38,962 hrs · 28,674 cycles

AFT WING TO FUSELAGE FAIRING SUPPORT RH FS909 ANGLE CRACKED AT (RBL17.63) AFT DIAPHRAGM (C-CHECK RO 3/14/2025) REPAIRED AFT WING TO FUSELAGE FAIRING SUPPORT RH FS909 ANGLE AT (RBL17.63) AFT DIAPHRAGM REF REO 670-53-82-478 REV -A DATED 2014-11-12, COMPLIED WITH 51-900-1002-SKY

Part: STAND OFF — CRACKED (ZONE 400) · airframe 38,962 hrs · 28,674 cycles

R/H LWR TRANSCOWL OTBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 3/14/2025) REMOVED AND REPLACED O/B STAND-OFF ANGLE P/N CN624-2082-201 ON R/H LOWER TRANSCOWL, REF. REO 670-54-21-971, REV. B, 2023-11-28. COMPLIED WITH MAJOR REPAIR M-337 AND SKY CARD 51-900-1002-SKY.

Part: RIVET — SHEARED (ZONE 400) · airframe 38,962 hrs · 28,674 cycles

R/H LWR TRANSCOWL Z STIFFENER RIVETS ARE SHEARED (C-CHECK RO 3/14/2025) REPAIRED INNER PERFORATED SKIN AT SHEARED RIVETS COMMON TO ZED STIFFENER P/N CN624-2038-203 ON R/H LOWER TRANSCOWL, REF. REO 670-54-21-1688, REV. --, 2024-11-25. COMPLIED WITH MAJOR M-337 AND SKY CARD 51-900-1002-SKY.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 38,962 hrs · 28,674 cycles

CORROSION ON FLOORBEAM LBL9, TOP INBD FLANGE BETWEEN FS 581.00 - 677.00. AREAS MARKED (C-CHECK RO 3/14/2025) REPAIRED ALL MARKED AREAS ON LBL9 FLOOR BEAM, UPPER INBOARD FLANGE BETWEEN FS581 AND FS677. REF. REO 670-53-31-987 REV.-- ISSUED 2024-12-11 AND CRJ700 SRM 53-00-41-201-001-A01.COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY (CL600-2C10) STRUCTURAL MAJOR REPAIR (**RII**)

Part: STRIKER — CORRODED (ZONE 200) · airframe 38,962 hrs · 28,674 cycles

CORROSION NOTED ON LWR SRV DOOR SEAL STRIKER BETWEEN FS319-349 (MARKED) (C-CHECK RO 3/14/2025) REMOVED AND REPLACED CORRODED LWR SERVICE DOOR SEAL STRIKER WITH NEW STRIKER (P/N SH670-31412-7) PER DWG SH670-31950 REV Y AND CRJ 700 SRM 51-42-06-001-001-A01 REV 38 DATED 25 JULY 2020. COMPLIED WITH MHIRJ EO# SH670-31950, DATE: 2024.17.12 FOR SEAL STRIKER REPAIR PROR TO INSTALATION. M-337 AND SKYWEST TASK CARD 51-900-1002-SKY COMPLIED WITH. PERFORMED PRESSURE LEAK CHECK, NO LEAKS NOTED.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 38,962 hrs · 28,674 cycles

CORROSION ON FLOORBEAM LBL9, TOP INBD FLANGE AT FS 549.00. AREAS MARKED (C-CHECK RO 3/14/2025) CORROSION ON FLOORBEAM LBL9, TOP INBD FLANGE AT FS 549.00 FOUND TO BE OUT OF LIMITS, REPAIRED BY COMPLYING WITH REO 670-53-31-985 REV -- DATED 2024-12-05, CRJ700 SRM 53-00-41-201-001-A01 REV 38 JUL 25/2020, CRJ700 SRM 51-42-21-001-001-A01 REV 38 JUL 25/2020, & CRJ700 SRM 51-42-06-001-001-A01 REV 38 JUL 25/2020, COMPLIED 51-900-1002-SKY

Part: MOUNT — CORRODED (ZONE 200) · airframe 38,962 hrs · 28,674 cycles

CORROSION NOTED ON MOUNTING FITTINGS (2EA) FOR FWD MONUMENT AT APPROX. FS310 AND LBL 19 AND 36 (MARKED) (C-CHECK RO 3/14/2025) REMOVED FS.310 LBL19 & LBL36 FWD MONUMENT FITTINGS FOR REPLACEMENT REF. CRJ700 SRM TASK 51-42-21-001-001-A01. INSTALLED NEW INBD & OUTBD ATTACH FITTINGS FOR FWD MONUMENT ON FLOOR CROSS BEAM AT FS.310 BETWEEN LBL19 & LBL36 PER CRJ700 SRM TASK 51-42-20-001-001-A01 REF. BOMBARDIER DWG. SH670-32120 REV. D . COMPLIED WITH TASK CARD 51-900-1002-SKY.

Part: DOOR SILL — CORRODED (ZONE 200) · airframe 38,962 hrs · 28,674 cycles

AFT CARGO DOOR SILL HAS AREAS OF CORROSION. AREAS MARKED (C-CHECK RO 3/14/2025) REMOVED AND REPLACED AFT CARGO DOOR SILL. REF. CRJ700 SRM 51-42-06-001-001-A01, SRM 51-42-13-001-001-A01, SRM 51-42-21-001-001-A01 AND DWG# MM670-35085 REV. L. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY (CL600-2C10) STRUCTURAL MAJOR REPAIR (**RII**).

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 38,962 hrs · 28,674 cycles

CORROSION ON FLOORBEAM RBL9, TOP INBD FLANGE BETWEEN FS 501.00 - 565.00. AREAS MARKED (C-CHECK RO 3/14/2025) REPAIRED ALL DAMAGES ON RBL9 FLOOR BEAM UPPER INBD FLANGE BETWEEN FS 501.00 - 565.00. REF. REO 670-53-31-982 REV.-- ISSUED 2024-12-04 AND CRJ700 SRM 53-00-41-201-001-A01 FIGURE 53-00-41-991-828 AND FIGURE 53-00-41-991-829. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY (CL600-2C10) STRUCTURAL MAJOR REPAIR (**RII**)

Part: SKIN — CORRODED (ZONE 100) · airframe 38,962 hrs · 28,674 cycles

CORROSION NOTED ON INTERNAL SKIN AROUND AFT DRAIN MAST SUPPLY LINES BETWEEN FS1031-FS1051 (MARKED) (C-CHECK RO 3/14/2025) REPAIRED THE SKIN AROUND AFT DRAIN MAST SUPPLY LINES PER REO 670-53-61-2430 REV-- DATED 2024-12-26, ALL STEPS COMPLIED WITH. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. LEAK CHECK GOOD. SEE CONTINUATION CARD FOR DETAILS.

Part: STAND OFF — CRACKED (ZONE 400) · airframe 38,962 hrs · 28,674 cycles

R/H UPPER TRANSCOWL OTBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 3/14/2025) INSTALLED 1 EA. NEW A-BRACKET P/N CN624-2082-201 ON OTBD. SIDE OF R/H UPPER TRANSCOWL. REF. REO 670-54-21-971, REV. B, 2023-11-28. COMPLIED WITH STEPS 1-3 AND 51-900-1002-SKY.

Part: STAND OFF — CRACKED (ZONE 400) · airframe 38,962 hrs · 28,674 cycles

R/H UPPER TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 3/14/2025) INSTALLED 1 EA. NEW A-BRACKET P/N CN624-2082-201 ON INBD. SIDE OF R/H UPPER TRANSCOWL, REF. REO 670-54-21-971, REV. B, 2023-11-28. COMPLIED WITH STEPS 1-3. AND COMPLIED WITH 51-900-1002-SKY.

Part: STAND OFF — CRACKED (ZONE 400) · airframe 38,962 hrs · 28,674 cycles

R/H LWR TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 3/14/2025) REMOVED AND REPLACED I/B STAND-OFF ANGLE P/N CN624-2082-201 ON R/H LOWER TRANSCOWL, REF. REO 670-54-21-971, REV. B, 2023-11-28. COMPLIED WITH MAJOR REPAIR M-337 AND SKY CARD 51-900-1002-SKY.

Part: STRUCTURE — CRACKED (ZONE 100) · airframe 38,962 hrs · 28,674 cycles

FORWARD FUSELAGE JUST AFT OF FS 169.00 LEFT HAND TRU LATCH CUT OUT , SUSPECTED CRACKS ( 2 ). MARKEDMX # 29132843. (C-CHECK RO 3/14/2025) INSTALLED A NEW REPLACEMENT HYDRAULIC BAY SKIN ON THE FWD FUSELAGE USING ALL NEW FASTENERS, REF BOMBARDIER DWG# CC670-33040 REV G, REO 670-53-11-2060 REV-- DATED 2024-12-03 AND CRJ700 SRM'S 51-42-06-001-001 A01 AND 51-42-13-001-001 A01. SKYWEST TASK CARD 51-900-1002-SKY COMPLIED WITH.

Part: SKIN — GOUGED (ZONE 600 FLAP) · airframe 38,962 hrs · 28,674 cycles

R/H OTBD FLAP HAS GOUGE ON LWR SURFACE INBD OF CENTER FARING @ 41/2" FROM T/E (C-CHECK RO 3/14/2025) CUT OUT DAMAGE AND PERFORMED SKINS AND PLATINGS, METALLIC OUTBOARD FLAP REPAIR TYPE III. REF. CRJ700 SRM 57-53-01-201-001-A01 REPAIR TYPE III.COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY (CL600-2C10) STRUCTURAL MAJOR REPAIR (**RII**)

Part: WINDSHIELD — CRACKED · airframe 38,379 hrs · 28,131 cycles

TRANSFER FROM EAML 1131261 : LH WINDSHIELD INNER PANE CRACKED. (FILED CLOSED)REMOVED AND REPLACED THE PILOTS WINDSHIELD PER THE APPLICABLE STEPS OF AMM 56-11-01. OPS AND LEAK CHECK GOOD AT THIS TIME

Part: UNKNOWN — SMOKE (UNKNOWN) · airframe 38,359 hrs · 28,111 cycles

UPON TOUCHDOWN IN SAF, THE ENTIRE CABIN WAS FILLED WITH A SMOKE LIKE SCENT. WE NOTICED THE SMELL IN THE FLIGHT DECK AS WELL. (FLT 4989 FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS

Part: SEAT TRACK — CORRODED · airframe 38,359 hrs · 28,111 cycles

R/H SEAT TRACK AT RBL9 BETWEEN FS847.00 TO FS977.00 SEVERAL AREAS HAS CORROSION (MARKED) (C-CHECK RO 5/18/2023) REMOVED AND REPLACED RH SEAT TRACK RAIL AT RBL9.00 BETWEEN FS847.00 TO FS977.00 REF CRJ700 AMM 53-00-49-000-801-A03 & 53-00-49-400-801-A03

Part: WINDOW POST — CRACKED (COCKPIT WINDOW) · airframe 34,723 hrs · 25,254 cycles

TRANSFERRED FROM ML 22676393 CRACK FOUND ON THE RH SIDE POST TOP HOLE, CRACK APPEARS TO BE DOWN TO THE NUT PLATE. PER GMM 3-26 THIS HAS BEEN DETERMINED TO BE A MAJOR REPAIR AND FORM M-337 WILL BE REQUIRED (FILED CLOSED) REMOVED AND REPLACED DAMAGED RT SIDE WINDOW POST IN REFERENCE TO CRJ700 SRM 51-10-06, 51-42-20 51-77-00 AND TASK CARD 51-900-1002-SKY AND FORM M-337. SEE CP 22686075 FOR PRESSURIZATION CHECK.

Part: ATTACH BRACKET — CRACKED (LT SLAT) · 25,116 cycles

L/H SLAT CANNISTER 1-3 AFT ATTACH BRACKET IS CRACKED AT BOTTOM OF WELD. (C-CHECK) RO 3/8/2021 REPAIRED L/H SLAT CANNISTER 1-3 AFT ATTACH BRACKET, COMPLIED WITH ALL STEPS BOMBARDIER GENERIC REO 670-57-42-577 REV -- DATE 2016-12-02 AND COMPLIED WITH TASK CARD 51-900-1002-SKY (SEE CONTINUATION FOR DETAILS)

Part: ATTACH BRACKET — CRACKED (RT WING SLAT) · 25,116 cycles

R/H SLAT CANNISTER 1-3 AFT ATTACH BRACKET IS CRACKED AT BOTTOM OF WELD. (C-CHECK) RO 3/8/2021 REPAIRED R/H SLAT CANNISTER 1-3 AFT ATTACH BRACKET REF BOMBARDIER GENERIC REO 670-57-42-577 REV -- DATE 2016-12-02 AND CRJ700 SRM 51-42-21-001-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY (SEE CONTINUATION FOR DETAILS)

Part: ANGLE — CORRODED (ZONE 100) · 25,116 cycles

FOUND CORROSION ON REINFORCING ANGLE ON FS379.00 AT STGR 22R (C-CHECK) RO 3/8/2021 REMOVED AND REPLACED REINFORCEMENT ANGLE P/N SH670-32119-1 COMMON TO FRAME AT FS 379.00 REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG# SH670-32050 REV J DATE 2012/08/09. COMPLIED WITH 51-900-1002-SKY

Part: FRAME — CORRODED (ZONE 100) · 25,116 cycles

FS319.70 FRAME HAS EXISTING CORROSION ON AFT SIDE CUTOUT OF STGR 26L (C-CHECK) RO 3/8/2021 REMOVED AND REPLACED FRAME FS 319.00 FROM STGR 25L TO 24R REF CRJ700 SRM 53-00-06-201-006-A01 AND SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY.

Part: FRAME — CORRODED (ZONE 100) · 25,116 cycles

FOUND CORROSION ON R/H AFT SIDE OF FRAME AT F.S.379.00 AT STGR 21R (MARKED). (C-CHECK) RO 3/8/2021 REMOVED AND REPLACED FRAME AT FS 379.00 REF DWG SH670-32050 REV J AND REF CRJ700 SRM 51-42-06-001-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY. LEAK CHECK GOOD.

Part: SKIN — CRACKED (NACELLE) · 25,116 cycles

CRACK FOUND ON SKIN COMMUN TO ONE OF 6 ATTACH POINTS OF LATCH ASSY. REF. CAMP # 22107482 ( JOB 1, OP. 274) (C-CHECK) RO 3/8/2021 DAMAGE ON SKIN REPAIRED. REF. REO 670-54-21-1419 REV.-- DATED 2021-01-21

Part: COAMING — CHAFED (THRUST REVERSER) · 25,116 cycles

LH LWR TRANS COWL LATCH DOOR COAMING IS CHAFFED. (C-CHECK) RO 3/8/2021 INSTALLED NEW L/H LWR TRANS COWL DOOR COAMING. / ALL STEPS COMPLIED WITH IN BOMBARDIER REO 670-54-21-1207 REV A DATED 2015-08-27 / COMPLIED WITH 51-900-1002 SKY

Part: SKIN — CRACKED (LT NACELLE) · 25,116 cycles

LH UPPER TRANSCOWL, I/B STAND-OFF CRACKED AT FASTENER HOLE. (C-CHECK) RO 3/8/2021 INSTALLED NEW STANDOFF PN 624-2082-201. REF GREO 670-54-21-971. REV. A DATED 2017/05/11 / COMPLIED WITH TASK CARD 51-900-1002-SKY AND COMPLETED M-337

Part: FLOORBEAM — CORRODED (ZONE 200) · 25,116 cycles

FLOOR SILL, F.S. 280 TO SERVICE DOOR CUTOUT APPEARS CORRODED. (C-CHECK) RO 3/8/2021 REMOVED CORROSION AT FLOOR SILL AT FS 280 TO SERVICE DOOR CUTOUT REF CRJ 700 SRM 51-21-06-001-001-A01. 100% MATERIAL LOSS OUT OF LIMITS REF CRJ 700 SRM 53-00-45-201-001-A01. REPLACED FLOOR SILL AT FS 280 TO SERVICE DOOR CUTOUT REF CRJ 700 SRM 51-42-06-001-001-A01 SRM 51-42-21-001-001-A01 SRM 51-42-13-001-001-A01 AND DWG 670-32170 REV: V. AND COMPLIED WITH TASK CARD 51-900-1002-SKY. LEAK CHECK GOOD.

Part: LINTEL — CRACKED (ZONE 200) · 25,116 cycles

FS285 STRG3L LINTEL FOUND CRACKED. COMPLY WITH SB 670BA-53-040 REV: C DATED 09/20/2012 (C-CHECK) RO 3/8/2021 COMPLIED WITH PERMANENT REPAIR OF THE LINTEL STRIGER 3L IAW SB NO. 670BA-53-040 REV C DATED 09/20/2012 WITH THE INCORPORATION OF REO NO. 670-53-21-493 REV -D DATED 2015-07-10. SEE CONTINUE CARD NO. MX TRANS #22091942 JOB NO. 710146117 OP 1 FOR DETAILS. CONPLIED WITH 51-900-1002-SKY. / SERVICE BULLETIN 670BA-53-040, REVISION C, FUSELAGE - CENTER FUSELAGE, PRIMARY STRUCTURE FS280.00 TO FS295.00 - INSPECTION AND REINFOCEMENT OF LINTEL STRINGER 3 OF THE MAIN PASSENGER DOOR, PART B, INCORPORATED.

Part: FLOORBEAM — CRACKED (ZONE 200) · 25,116 cycles

SUSPECT CRACK IN THE RADIUS OF THE COCKPIT FLOORBEAM AT LBL12 ON THE FWD SIDE OF THE FS280 BULKHEAD (C-CHECK) RO 3/8/2021 REPAIREDCOCKPIT FLOORBEAM AT LBL 12 FWD OF FS 280 REF CRJ-700 SRM 53-11-43-201-003-A01 REV 38 DATED JUL 25/2020 & CRJ-700 SRM 51-42-21-001-001-A01 REV 38 DATED JUL 25/2020 / COMPLIED WITH TASK CARD 51-900-1002-SKY

Part: STRINGER — CORRODED (ZONE 100) · 25,116 cycles

CORROSION ON STRINGER 21R FS379 BUT ACTUALLY ON TIE IN CLIP (C-CHECK) RO 3/8/2021 REMOVED AND REPLACED TIE CLIP P/N SH670-32301-5 PER REF DWG BOMBARDIER INC, CANADAIR SH670-32280 REV H AND REF CRJ700 SRM 51-42-06-001-001-A01 COMPLIED WITH SKY CARD 51-900-1002-SKY

Part: SKIN — CORRODED (ZONE 100) · 25,116 cycles

UPON REMOVAL OF EXISTING DOUBLERS AT STA 977 STR 27 FOUND CORROSION AT AFT END OF DOUBLER FOOPRINT COMMON TO FAIRING ATTACHMENT AT STA 985 STR 26L-26R (C-CHECK) RO 3/8/2021 REPAIRED CORROSION DAMAGE IAW REO 670-53-61-1806 REV -- DATED 2021-01-14 COMPLIED WITH TASK CARD 51-900-1002-SKY, AND COMPLETED M-337

Part: ANCHOR FITTING — CORRODED (PAX DOOR) · 25,116 cycles

PASSENGER DOOR FORWARD AND AFT ANCHOR FITTINGS HAVE MISCELLANEOUS CORRODED HARDWARE, FS310.00 & FS349.00. (C-CHECK) RO 3/8/2021 REMOVED AND REPLACED CORRODED HARDWARE ON PASSENGER DOOR FORWARD AND AFT ANCHOR FITTINGS AS PER CRJ 700 AMM 52-11-17-400-804

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · 25,116 cycles

*FLOOR SUPPORT, FS1051.30 €“ RBL40.0, IS CORRODED. (MARKED) (C-CHECK) RO 3/8/2021 REPAIRED FS1051 FLOOR BEAM AT RBL40 IAW CRJ700 REO 670-53-61-1805 REV-- 2021-02-03, CRJ-700 SRM 51-42-06-001-001-A01, CRJ-700 SRM 51-42-21-001-001-A01, CRJ700SRM 51-23-00-001-001-A01. COMPLIED SKYWEST CARD NO 51-900-1002-SKY RESTORED FINISH.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · 25,116 cycles

*RIGHT HAND FLOOR SILL IS CORRODED AT THE FORWARD END FS969.00 €“ FS985.00. (MARKED) (C-CHECK) RO 3/8/2021 REMOVED AND INSTALLED NEW RH FLOOR SILL P/N SH670-31518-1 BETWEEN FS969.00 - FS985.00 REF CRJ700-SRM51-42-06-001-001-A01 AND DWG SH670-32170, REV V. PRESSURE CHECK GOOD AT THIS TIME. COMPLIED WITH TASK CARD 51-900-1002-SKY

Part: FLOOR SUPPORT — GOUGED (ZONE 200) · 25,116 cycles

*RBL9 FLOOR BEAM OUTBOARD FLANGE GOUGED, FS863.00 €“ FS953.00. (MARKED) (C-CHECK) RO 3/8/2021 REPAIRED DAMAGED FLOOR BEAM AT RBL9 FS 855-885 IAW CRJ700 SRM 53-00-41-201-001-A01 FIG 53-00-41-991-830. COMPLIED WITH 51-900-1002-SKY ( CL600-2C10), AND M-337.

Part: PLATE — CORRODED (ZONE 100) · 25,116 cycles

*FORWARD AND AFT LOWER JOINT PLATES FOR THE FORWARD BAGGAGE BAY SURROUND STRUCTURE HAVE CORROSION, FS536.00 & FS575.00, STGR25L (MARKED) (C-CHECK) RO 3/8/2021 REMOVED AND REPLACED FWD AND AFT LWR JOINT PLATE AT FS 536.00 AND FS 575.00 STGR 25L REF CRJ700 SRM 51-42-24-001-001-A01 AND DRAWING SH670-33750 REV AA. COMPLIED WITH TASK CARD 51-900-1002-SKY.

Part: PLATE — CORRODED (E/E BAY) · 25,116 cycles

*AVIONICS BAY DOOR SURROUND: JOINT PLATE ON THE FS364 FRAME AND STGR25L LONGERON IS CORRODED (MARKED). (C-CHECK) RO 3/8/2021 REPLACED A-BAY DOOR SURROUND JOINT PLATE WITH A NEW ONE. REF: CRJ-700 SRM 51-42-21-001-001-A01, REO-670-53-21-1934 REV -- DATE 2021-01-25 & DWG SH670-32070 REV. NC / COMPLIED WITH SKY WEST TASK CARD 51-900-1002-SKY. / SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: INTERCOSTAL — CORRODED (DOOR FRAME) · 25,116 cycles

*GALLEY SERVICE DOOR SURROUND STRUCTURE, INTERCOSTAL AT STGR20R, BETWEEN FS310 TO FS319 IS CORRODED. (MARKED) (C-CHECK) RO 3/8/2021 REMOVE AND REPLACED INTERCOSTAL AT STGR 20R BWTN FS 310.00 TO 319.00 REF DWG SH670-32047 REV NC AND REF CRJ700 SRM 51-42-21-001-001-A01 AND 51-42-06-001-001-A01 COMPLIED WITH 51-900-1002-SKY.

Part: STRINGER — CORRODED (ZONE 100) · 25,116 cycles

*STRINGER, STGR26R, HAS CORROSION BETWEEN FS280 AND FS310. (MARKED) (C-CHECK) RO 3/8/2021 REMOVED AND REPLACED STGR 26R FS 280.00 TO FS 333.00 REF CRJ700 SRM 51-42-06-001-001-A01 AND AND DWG# SH670-31630 REV J AND RESTORED FINISH REF CRJ700 SRM 51-21-06-001-001-A01 COMPLIED WITH SKYCARD 51-900-1002-SKY PRESSURE CHECK GOOD

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · 25,116 cycles

*PRESSURE FLOOR STRUCTURE €ŒFLOOR BEAM€? AT RBL9 BETWEEN APPROX. FS693 AND FS847 HAS CORROSION(MARKED). (C-CHECK) RO 3/8/2021 REMOVED CORROSION AND COMPLIED WITH REO 670-53-41-505 REV--, 2021-01-14 AND, / COMPLIED WITH TASK CARD 51-900-1002-SKY

Part: STRINGER — CORRODED (ZONE 100) · 25,116 cycles

*STRINGER, STGR21R, NOTED CORROSION BETWEEN FS364 AND FS379 (MARKED). (C-CHECK) RO 3/8/2021 REMOVED AND REPLACED STGR 21R, REF (DWG SH670-31383, REV NC, DATED 29-8-98) AND (CRJ700 SRM 51-42-06-001-001-A01). RESTORED FINISH REF CRJ700 SRM 51-25-01-001-001-A01. SEE CONTINUE CARD FOR DETAILS. C/W WITH SKYCARD 51-900-1002-SKY

Part: FLOORBEAM — CRACKED (ZONE 200) · 25,116 cycles

*SUSPECT CRACK IN THE RADIUS OF THE COCKPIT FLOORBEAM AT RBL12 ON THE FWD SIDE OF THE FS280 BULKHEAD/CROSSBEAMS (FLAGGED) (C-CHECK) RO 3/8/2021 REPAIRED COCKPIT FLOORBEAM AT RBL 12 FWD OF FS 280 REF CRJ-700 SRM 53-11-43-201-003-A01 REV 38 DATED JUL 25/2020 / COMPLIED WITH TASK CARD 51-900-1002-SKY

Part: PLATE — CORRODED (E/E BAY DOOR) · 25,116 cycles

*AVIONICS BAY DOOR SURROUND: JOINT PLATE ON THE FS364 AND STGR25R LONGERON IS CORRODED (MARKED). (C-CHECK) RO 3/8/2021 REPLACED AVIONICS BAY DOOR SURROUND: JOINT PLATE ON THE FS364 AND STGR25R LONGERON. REF. DWG SH670-32050 REV. D / COMPLIED WITH 51-900-1002-SKY

Part: DOOR SILL — CORRODED (PAX DOORWAY) · 25,116 cycles

*PASSENGER DOOR SURROUND, BACK-UP SILL AT STRG21L, BETWEEN FS310 AND FS333 IS CORRODED. (MARKED) (C-CHECK) RO 3/8/2021 REPLACED PASSENGER DOOR SURROUND, BACK UP SILL AT STGR 21L BETWEEN FS310-FS333 WITH NEW. REF CRJ-700 SRM 51-42-21-001-001-A01, CRJ-700 SRM 51-42-06-001-001-A01 AND DWG SH670-31822 REV NC. OPS CHECK GOOD. PRESSURE CHECK GOOD. COMPLIED WITH 51-900-1002-SKY

Part: STRINGER — CORRODED (ZONE 100) · 25,116 cycles

*STRINGER, STGR19R, HAS CORROSION BETWEEN FS280 AND FS295. (MARKED) (C-CHECK) RO 3/8/2021 CORROSION AT STRINGER 19R BETWEEN FS 280 TO FS 295. CORRODED ALL THE WAY THROUGH NO DAMAGE ALLOWED. REPLACED DAMAGED PORTION OF STRINGER REF CRJ 700 SRM 53-00-03--201-001-A01, AND REPAIR S6295 TYPE Z10. LEAK CHECK GOOD. OPS CHECK GOOD. COMPLIED WITH 51-900-1002-SKY

Part: STRINGER — CORRODED (ZONE 100) · 25,116 cycles

*STRINGER, STGR27, HAS CORROSION JUST AFT OF THE FS295 FRAME. (MARKED) (C-CHECK) RO 3/8/2021 REPLACED STGR27 FROM FS295 - FS280 P/N SH670-31642-1 REF. CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-20-001-001-A01 AND DWG SH670-31630 REV NC. LEAK CHECKED GOOD. COMPLIED WITH TASK CARD 51-900-1002-SKY.

Part: STRINGER SPLICE — CORRODED (ZONE 100) · 25,116 cycles

*FS333 JOINT, STRINGER SPLICE AT STGR25L HAS CORROSION (MARKED). (C-CHECK) RO 3/8/2021 CORROSION ON STRINGER SPLICE AT STRINGER 25L FS 333 ASSESSED. NO DAMAGE ALLOWED IN AREA. REF CRJ700 SRM 53-21-03-101-002-A01. REPLACED JOINT SPLICE STRIP WITH NEW PART P/N: SH670-32429-3 REF CRJ 700 SRM 51-42-06-001-001-A01 CRJ 700 SRM 51-42-21-001-001-A01, DWG SH670-32429 REV NC AND DWG SH670-32420 REV E. COMPLIED WITH 51-900-1002-SKY

Part: DOUBLER — CHAFED (FUSELAGE) · 25,116 cycles

*DOUBLER UNDER PNLS.195DR/DL CHAFED IN SEVERAL AREAS. (MARKED) (C-CHECK) RO 3/8/2021 REPAIRED DAMAGED DOUBLER IAW REO 670-53-00-290 REV F DATED 2019/04/26. PRESSURE LEAK CHECK GOOD. COMPLIED WITH TASK CARD 51-900-1002-SKY.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · 25,116 cycles

LEFT WING OUTBOARD FLAP - INBOARD AFT LOWER HINGE LUG FITTING HAS CORRODED HARDWARE. (C-CHECK) RO 3/8/2021 REMOVED LEFT WING OUTBOARD FLAP - INBOARD AFT LOWER HINGE LUG FITTING HARDWARE REF CRJ700 AMM 57-53-27-000-801(CONFIG A01) STEPS 4.A(2)(3)(4)(5)(6)(7). INSTALLED NEW HARDWARE FOR THE LEFT WING OUTBOARD FLAP - INBOARD AFT LOWER HINGE LUG FITTING REF CRJ700 AMM 57-53-27-400-801(CONFIG A01) STEPS 4.A(2)(3)(4).

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · 25,116 cycles

RIGHT WING OUTBOARD FLAP - OUTBOARD FORWARD HINGE BOX SUPPORT FITTING HAS CORRODED HARDWARE. (C-CHECK) RO 3/8/2021 REPLACED RH WING OUTBOARD FLAP, OUTBOARD FORWARD HINGE BOX SUPPORT FITTING CORRODED HARDWARE WITH NEW REF CRJ-700 AMM 57-54-02-400-808-A01, LEAK CHECK GOOD, SEE CONTINUATION CARD FOR DETAILS.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · 25,116 cycles

*LEFT WING OUTBOARD FLAP - OUTBOARD AFT LOWER HINGE LUG FITTING HAS CORRODED HARDWARE. (C-CHECK) RO 3/8/2021 REMOVED LEFT WING OUTBOARD FLAP - OUTBOARD AFT LOWER HINGE LUG FITTING HARDWARE REF CRJ700 AMM 57-53-27-000-803 (CONFIG A01) STEPS 4.A.(4)(5)(6). INSTALLED NEW LEFT WING OUTBOARD FLAP - OUTBOARD AFT LOWER HINGE LUG FITTING HARDWARE REF CRJ700 AMM 57-53-27-400-803 (CONFIG A01).

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,034 hrs · 24,709 cycles

SBN - FLIGHT 2986 MAINTENANCE INSPECTIOON DISCOVERED THE NR 1 INTERIOR OVERHEAD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB, OPERATIONALLY TESTED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: GROUND WIRE — UNSECURE (EMERGENCY LIGHTS) · airframe 31,708 hrs · 22,832 cycles

DURING MX INSPECTION, THE GALLEY FLOOR EMERGENCY EXIT SIGN WOULD NOT ILLUMINATE. MX SECURED GROUND WIRE FOR CONNECTOR P372 WITH OPERATIONAL CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: GROUND WIRE — UNSECURE (EMERGENCY LIGHTS) · airframe 31,707 hrs · 22,832 cycles

GALLEY FLOOR. NEXT TO SERVICE DOOR, EMERGENCY EXIT SIGN WILL NOT ILLUMINATE. SECURED THE GROUND WIRE FOR CONNECTOR P372 IAW AMM 20-23-00. EMEGENCY LIGHTS OPS CHECKED GOOD IAW AMM 33-51-00.

Part: RELAY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 22,290 hrs · 20,443 cycles

THE CREW REPORTED EMERGENCY LIGHTS ARE CYCLING ON AND OFF WITH GROUND POWER AND APU POWER. MAINTENANCE REPLACED THE RELAY KJ35 IAW ESPM 20-39-00. OPS CHECKED GOOD.

Part: RELAY — FAULTY (EMERGENCY LIGHTS) · airframe 30,988 hrs · 22,290 cycles

EMERGENCY LIGHTS CYCLING ON AND OFF WITH GROUND POWER AND APU POWER. CONTRACT MX REMOVED AND REPLACED RELAY K135 WITH OPERATIONAL CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,876 hrs · 22,205 cycles

FLOORBEAM CORRODED LBL9 FS 1031.00. REPAIRED FLOORBEAM IAW EC/TC REO 670-53-61-1331 AND REO 670-53-61-1331 AND EC/TC EO 700-53-10-00017, EO 700-53-10-00017.

Part: SEAT TRACK — CORRODED (BS 673-720) · airframe 30,876 hrs · 22,205 cycles

LEFT SEAT TRACK RETAINER BS 673 - 720 CORRODED. COMPLIED WITH EC/TC EA 25-2017-026 AND EA 25-2017-026.

Part: SEAT TRACK — CORRODED (BS 783-854) · airframe 30,876 hrs · 22,205 cycles

LEFT SEAT TRACK RETAINER BS 783 - 854 CORRODED. COMPLIED WITH EC/TC EA 25-2017-027 AND EA 25-2017-027.

Part: SKIN — DENTED (RUDDER) · airframe 30,876 hrs · 22,205 cycles

RUDDER SKIN DAMAGED. COMPLIED WITH REO 670-53-00-290 AND REO 670-53-00-492 AND EC/TC REO 670-53-00-492.

Part: FRAME — CORRODED (FUSELAGE) · airframe 30,876 hrs · 22,205 cycles

FRAME 1088.20 AFT SIDE CORRODED BTW STGR 25L-26R. REMOVED CORROSION FROM 1088.20 AFT SIDE IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS INSP IAW BSC NDT INSP PROCEDURE 4.3. MIN REMAINING MATERIAL IS 060". NO DAMAGE ALLOWED ON FRAME. COMPLIED WITH EC/TC EA 32-2017-043 PERFORMED PERMANENT REPAIR IAW EA 32-2017-043.

Part: CLEAT — CORRODED (FUSELAGE) · airframe 30,876 hrs · 22,205 cycles

CLIP AT STGR 27 FS 265 CORRODED. REMOVED CLEAT, BLENDED CORROSION AND INSTALLED SAME CLEAT IAW EA 25-2017-036 AND EC/TC EA 25-2017-036.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 30,876 hrs · 22,205 cycles

LT JACK FITTING SUPPORT AT FS 265-280 IS CORRODED. REMOVED CORRODED LT JACK FITTING SUPPORT AND INSTALLED NEW SUPPORT IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 AND DWG CC670-322050.

Part: STRIKER — CORRODED (SERVICE DOOR) · airframe 30,876 hrs · 22,205 cycles

DURING C CHECK, FOUND SERVICE DOOR LOWER PRESSURE SEAL STRIKER CORRODED. R & R SEAL STRIKER.

Part: RETAINER — CORRODED (E/E BAY DOOR) · airframe 30,876 hrs · 22,205 cycles

DURING C CHECK, FOUND AVIONICS BAY DOOR PRESSURE SEAL RETAINERS CORRODED. R & R THE SEAL RETAINERS.

Part: STRINGER — CORRODED (BS 280) · airframe 30,876 hrs · 22,205 cycles

DURING C CHECK, FOUND STRINGER 27 AFT SIDE OF BS 280 FRAME CORRODED. R & R THE STRINGER.

Part: FRAME — CORRODED (BS 319) · airframe 30,876 hrs · 22,205 cycles

DURING C CHECK, FOUND FWD SIDE OF FRAME BS 319.7 CORRODED BETWEEN STRINGERS 26 & 27L. BLENDED FRAME.

Part: SEAT TRACK — CORRODED (BS 679-714) · airframe 30,876 hrs · 22,205 cycles

DURING C CHECK, FOUND THE LEFT SEAT TRACK CORRODED. COMPLIED WITH EC/TC REO 670-53-00-343, REO 670-53-00-343, AND AMM 53-00-49-400-801-A03.

Part: SKIN — CORRODED (FUSELAGE) · airframe 30,876 hrs · 22,205 cycles

DURING C CHECK, FOUND AVIONICS BAY DOOR INTERNAL SKIN SURROUND CORRODED. BLENDED AREA, PERFORMED NDT.

Part: STRINGER — CORRODED (BS 319-333) · airframe 30,876 hrs · 22,205 cycles

DURING C CHECK, FOUND STRINGER 25R CORRODED. R & R THE STRINGER.

Part: FLOOR SUPPORT — CORRODED (BS 280-319) · airframe 30,876 hrs · 22,205 cycles

DURING C CHECK, FOUND THE RIGHT FLOOR SUPPORT CORRODED. R & R THE FLOOR SUPPORT.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 30,876 hrs · 22,205 cycles

DURING C CHECK, FOUND TCAS DOUBLER CORRODED. R & R TCAS DOUBLER.

Part: RISER — CORRODED (PAX DOOR) · airframe 30,876 hrs · 22,205 cycles

DURING C CHECK, FOUND FWD PAX DOOR RISER PANEL CORRODED. REPAIRED. PERFORMED NDT. INSTALLED NEW FASTENERS AND APPLIED TOP COAT.

Part: SEAT TRACK — CORRODED (BS 714-763) · airframe 30,876 hrs · 22,205 cycles

DURING C CHECK, FOUND THE LEFT SEAT TRACK CORRODED. COMPLIED WITH EC/TC REO 670-53-00-343, REO 670-53-00-343, AND AMM 53-00-49-400-801-A03.

Part: STRINGER — CORRODED (BS 310-319) · airframe 33,680 hrs · 24,847 cycles

DURING C CHECK, FOUND STRINGER 21R CORRODED. R & R THE STRINGER.

Part: SKIN — CORRODED (BS 280) · airframe 30,876 hrs · 22,205 cycles

DURING C CHECK, FOUND EXTERNAL SKIN CORRODED. COMPLIED WITH EC/TC EA 32-2017-027, EC/TC EA 32-2017-028, EA 32-2017-027 AND EA 32-2017-028.

Part: FLOORBEAM — CORRODED (BS 1031) · airframe 30,876 hrs · 22,205 cycles

DURING C CHECK, FOUND CARGO BAY FLOORBEAM CORRODED. COMPLIED WITH EC/TC EO 70053-10-00018 & EO 70053-10-00018.

Part: STRINGER CLIP — CORRODED (BS 310-319) · airframe 33,680 hrs · 24,847 cycles

DURING C CHECK, FOUND STRINGER CLIP CORRODED. R & R THE STRINGER CLIP.

Part: SUPPORT — CORRODED (BS 785-797) · airframe 30,876 hrs · 22,205 cycles

DURING C CHECK, FOUND THE SEAT TRACK TRIM SUPPORT CORRODED. COMPLIED WITH EC/TC EA 43-2017-016, & EA 43-2017-016.

Part: SKIN — CORRODED (BS 501-517) · airframe 30,876 hrs · 22,205 cycles

DURING C CHECK, FOUND FUSELAGE EXTERNAL SKIN CORRODED UNDER ADF ANTENNA WHILE ACCESSING FOR FRAME REPAIR AT BS 501. COMPLIED WITH EC/TC EA 43-2017-013, & EA 43-2017-013 ON FUSELAGE SKIN

Part: FRAME — CORRODED (BS 310) · airframe 30,876 hrs · 22,205 cycles

DURING C CHECK, FOUND FWD SIDE OF FRAME AT BS 310 CORRODED. COMPLIED WITH EC/TC EO 700-53-10-00019, & EO 700-53-10-00019.

Part: FRAME — CORRODED (BS 1047) · airframe 30,876 hrs · 22,205 cycles

DURING C CHECK, FOUND AFT CARGO FRAME CORRODED. COMPLIED WITH EC/TC EA 32-2017-026, & EA 32-2017-026.

Part: FRAME — CORRODED (BS 333) · airframe 30,876 hrs · 22,205 cycles

DURING C CHECK, FOUND THE FRAME AT BS 333 CORRODED AFT SIDE. COMPLIED WITH EC/TC EO 700-53-10-00020, & EO 700-53-10-00020.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 30,876 hrs · 22,205 cycles

DURING C CHECK, FOUND CORRODED INTERCOSTAL. R & R THE INTERCOSTAL.

Part: PAN — CRACKED (FUSELAGE) · airframe 30,876 hrs · 22,205 cycles

DURING C CHECK FOUND TRU FLOOR PAN CRACKED AT RT AFT LATCH. REPAIRED BY C/W EC/TC & REO CC -670-33040 S06.

Part: PANEL — CORRODED (PAX DOOR) · airframe 30,876 hrs · 22,205 cycles

DURING C CHECK FOUND CORROSION AROUND NUTPLATES FOR PANEL 832AB ON BOTTOM OF PAX DOOR. REMOVED CORROSION AND REPAIRED BY C/W EC/TC AND STS EA 30-2017-025 DATED 02/05/2017.

Part: LIGHT — WORN (CABIN) · airframe 30,876 hrs · 22,205 cycles

DURING C CHECK, FOUND EMERGENCY LIGHT WORN. R & R THE LIGHT.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,876 hrs · 22,205 cycles

DURING C CHECK FOUND LT SIDE SEAT RAIL SEGMENT CORRODED. REMOVED SEAT RAIL, C/W EC/TC AND REO FOR FABRICATING SEAT RAIL AND INSTALLED NEW SEAT RAIL.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,876 hrs · 22,205 cycles

DURING C CHECK FOUND SEAT RAIL SEGMENT CORRODED. REMOVED CORRODED SEAT RAIL IAW AMM 53-00-49-000-801-A03. FABRICATED AND INSTALLED NEW SEAT RAIL IAW EC/TC & REO 670-53-00-343 REV M AND AMM 53-00-49-400-801-A03.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 30,876 hrs · 22,205 cycles

DURING C CHECK FOUND SERVICE DOOR LOWER SILL ANGLE CORRODED. REMOVED LOWER SILL, DRILLED UP AND INSTALLED NEW SILL ANGLE.

Part: SEAT TRACK — CORRODED (BS 683-836) · airframe 30,876 hrs · 22,205 cycles

DURING C CHECK, FOUND RBL 9 SEAT TRACK CORRODED. REMOVED AND REPLACED THE SEAT TRACK.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,876 hrs · 22,205 cycles

RT SEAT RAIL SEGMENT FS 572-674 CORRODED. REPAIRED SEAT RAIL BY COMPLYING WITH EC/TC REO 670-53-00-013 AND REO 670-53-00-013 REV J DATED 10-22-2014.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,876 hrs · 22,205 cycles

AFT CARGO LT FLOOR SILL CORRODED AT FS 1052 LBL 42. REPAIRED SEAT RAIL BY COMPLYING WITH EC/TC REO 670-53-00-390 AND REO 670-53-00-390 REV -- DATED 01-22-2014

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,876 hrs · 22,205 cycles

AFT CARGO LT FLOOR SILL CORRODED AT FS 1079 LBL 36. REPAIRED SEAT RAIL BY COMPLYING WITH EC/TC REO 670-53-00-390 AND REO 670-53-00-390 REV -- DATED 01-22-2014.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 30,876 hrs · 22,205 cycles

AFT CARGO RT FLOOR SILL CORRODED AT FS 1051.30-1088.20. REPAIRED FLOOR SILL BY COMPLYING WITH EC/TC REO 670-53-00-390 AND REO 670-53-00-390 REV -- DATED 01-22-2014.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 30,876 hrs · 22,205 cycles

AFT CARGO LT FLOOR SILL CORRODED AT FS 1052 LBL 42. REPAIRED SILL BY COMPLYING WITH EC/TC REO 670-53-00-390 AND REO 670-53-00-390 REV- DATED 01-22-2014.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 30,876 hrs · 22,205 cycles

DURING C CHECK FOUND AFT CARGO RTFLOOR CORRODED. C/W EC/TC & REO 53-00-390 REV- AS WRITTEN. REMOVED CORROSION, PERFORMED NDT ON DISCREPANT AREA, AND RESTORED FINISH.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 30,876 hrs · 22,205 cycles

SERVICE DOOR LOWER SILL AREA, UPPER CAP ANGLE CORRODED. REMOVED SERVICE DOOR LOWER SILL UPPER CAP ANGLE, RECEIVED AND DRILLED UP NEW CAP ANGLE THEN INSTALLED IAW SRM 51-42-06-001-001 A01 AND 51-40-11-001-001 A01. CLASSIFIED AS MINOR REPAIR.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 30,876 hrs · 22,205 cycles

STR 26R HAS CORROSION BETWEEN FRAMES 280-295. CORROSION OUT OF LIMITS. REMOVED STR 26R ALONG WITH STR SPLICE AND 4 EA CLIPS, THEN INSTALLED NEW PARTS IAW SRM 51-42-06-001-001 A01,51-42-21-001-001-A01, AND DRAWING SH670-31634. THIS REPAIR IS CLASSIFIED AS MAJOR.

Part: ANGLE — CORRODED (DOOR SILL) · airframe 30,876 hrs · 22,205 cycles

PAX DOOR LOWER SILL UPPER CAP ANGLE CORRODED. REMOVED AND REPLACED THE DOOR SILL UPPER CAP ANGLE IAW SRM 51-41-02-001-001-A01, 51-42-11-001-001-A01 AND DRAWING SH670-31810 REV Y.

Part: FLOOR SUPPORT — CORRODED (BS 349-364) · airframe 30,876 hrs · 22,205 cycles

CORRODED FLOOR SUPPORT BETWEEN BS 349-364, RBL 2. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-11-001-001-A01, AND 51-42-20-001-001-A01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,876 hrs · 22,205 cycles

RT SEAT RAIL SEGMENT FS 713-759 CORRODED IN SEVERAL AREAS. REMOVED AND REPLACED SEAT RAIL AT FS 713-759 RT SIDE PER AMM 53-00-49-000-801-A17,53-00-49-400-801-A017 AND EC/TC REO 67053-00-343 AND REO 670-53-00-343.

Part: ANGLE — CORRODED (BS 349) · airframe 30,876 hrs · 22,205 cycles

CORRODED ANGLE BS 349 STRINGER 20R. REMOVED AND REPLACED THE ANGLE IAW SRM 51-42-06-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 482-572) · airframe 30,876 hrs · 22,205 cycles

SEAT TRACK ,BS 482-572 CORRODED AT SEVERAL AREAS. COMPLIED WITH EC/TC REO 670-53-00-343, REO 670-53-00-343, AND AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 836-977) · airframe 30,876 hrs · 22,205 cycles

RBL 9 SEAT TRACK BS 836 - 977 CORRODED AT SEVERAL AREAS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000/400-801-A17 AND COMPLIED WITH EC/TC REO 670-53-00-343, AND REO 670-53-00-343.

Part: FLOOR SUPPORT — CORRODED (BS 286) · airframe 30,876 hrs · 22,205 cycles

NR 1 GALLEY FLOOR SUPPORT MOUNT CORRODED BS 286, RBL 17. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-42-21-001-001-A01 AND DRAWING SH670-32120. REV D.

Part: ANGLE — CORRODED (PAX DOOR SILL) · airframe 30,876 hrs · 22,205 cycles

PAX DOOR LOWER SILL ANGLE CORRODED. -MTC- REMOVED AND REPLACED PAX. DOOR LOWER SILL ANGLE PER. CRJ 700 SRM 51-41-02-001-001-A01, 51-42-11-001-001-A01 AND DRAWING SH670-31810 REV Y.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,876 hrs · 22,205 cycles

RBL9 SEAT RAIL SEGMENT FS 989-1005 CORRODED SEVERAL AREAS. REMOVED AND REPLACED SEAT RAIL AT FS 989-1005 ON RBL9 IAW AMM 53-00-49-000/400-801-A17.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 30,876 hrs · 22,205 cycles

COCKPIT FLOOR PANEL 221ALF RT SUPPORT ANGLE CORRODED AFT. SECTION APPROX FS 277.00, RBL 12. REMOVED AND REPLACED RT SUPPORT ANGLE IAW SRM 51-42-00-001-001-A01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,876 hrs · 22,205 cycles

RBL27 SEAT RAIL SEGMENT FS 977-1005 CORRODED SEVERAL AREAS. REMOVED AND REPLACED SEAT RAIL AT FS 977-1005 ON RBL27 IAW AMM 53-00-49-000/400-801-A17.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,876 hrs · 22,205 cycles

LBL9 SEAT RAIL SEGMENT FS 989-1005 CORRODED SEVERAL AREAS. REMOVED AND REPLACED SEAT RAIL AT FS 989-1005 ON LBL9 IAW AMM 53-00-49-000/400-801-A17.

Part: ATTACH ANGLE — CORRODED (BS 349-364) · airframe 30,876 hrs · 22,205 cycles

STRINGER 27L INTERCOSTAL ATTACH FLANGE HAS CORROSION FROM BS 349-364. REMOVED AND REPLACED INTERCOSTAL ATTACH FLANGE IAW SRM 51-40-11-001-001-A01,51-42-20-001-001-A01, AND 51-42-06-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 977-1005) · airframe 30,876 hrs · 22,205 cycles

RBL 9 SEAT TRACK BS 581 - 683 CORRODED IN SEVERAL AREAS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000/400-801-A17.

Part: SEAT TRACK — CORRODED (BS 581-683) · airframe 30,876 hrs · 22,205 cycles

LBL 9 SEAT TRACK BS 581 - 683 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 A17, EC/TC REO 670-53-00-343, REO 670-53-00-343 REV. K, AND AMM 53-00-49-801 A17.

Part: SEAT TRACK — CORRODED (BS 374-485) · airframe 30,876 hrs · 22,205 cycles

LBL 9 SEAT TRACK BS 374 - 485 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 A03, EC/TC REO 670-53-00-343, REO 670-53-00-343 REV. M, AND AMM 53-00-49-801 A03.

Part: SEAT TRACK — CORRODED (BS 683-836) · airframe 30,876 hrs · 22,205 cycles

LBL 9 SEAT TRACK BS 683-836 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 A17, EC/TC REO 670-53-00-343, REO 670-53-00-343 REV. K, AND AMM 53-00-49-801 A17.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,876 hrs · 22,205 cycles

RBL9 SEAT RAIL SEGMENT FS 350-485 CORRODED. REMOVED SEAT RAIL IAW AMM 53-00-49-000-801 A03, COMPLIED WITH EC/TC REO 670-53-00-343 AND REO 670-53-00-343 REV M FOR FABRICATING NEW SEAT RAIL AND INSTALLED IAW AMM 53-00-49-801 A03.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,876 hrs · 22,205 cycles

RT SEAT RAIL SEGMENT FS 482-572 CORRODED. REMOVED SEAT RAIL IAW AMM 53-00-49-000-801 A03, COMPLIED WITH EC/TC REO 670-53-00-343 AND REO 670-53-00-343 REV M FOR FABRICATING NEW SEAT RAIL AND INSTALLED IAW AMM 53-00-49-801 A03.

Part: FITTING — CORRODED (FUSELAGE) · airframe 30,876 hrs · 22,205 cycles

OUTER STRAP FITTING CORRODED UNDER SERVICE DOOR AT FS 319.70 STR 18 RT. REMOVED AND REPLACED OUTER STRAP FITTING IAW SRM 51-42-21-001-001 A01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,876 hrs · 22,205 cycles

RT SEAT RAIL SEGMENT FS 674-713 CORRODED. REMOVED SEAT RAIL IAW AMM 53-00-49-000-801 A17, COMPLIED WITH EC/TC REO 670-53-00-343 AND REO 670-53-00-343 REV M FOR FABRICATING NEW SEAT RAIL AND INSTALLED IAW AMM 53-00-49-801 A17.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,876 hrs · 22,205 cycles

LT SEAT RAIL SEGMENT FS 860-968 CORRODED. REMOVED SEAT RAIL IAW AMM 53-00-49-000-801 A03, COMPLIED WITH EC/TC REO 670-53-00-343 AND REO 670-53-00-343 REV M FOR FABRICATING NEW SEAT RAIL AND INSTALLED IAW AMM 53-00-49-801 A03.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 30,876 hrs · 22,205 cycles

CORROSION ON AVIONICS BAY FLOOR SUPPORT ANGLE AFT FACE AT FS 280. REMOVED AND REPLACED FLOOR SUPPORT ANGLE ON FS 280 IAW SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01, 51-42-13-001-001-A01 AND 51-42-21-001-001-A01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 30,876 hrs · 22,205 cycles

COCKPIT FLOOR PANEL 221 ALF LT SUPPORT ANGLE CRACKED AFT SECTION, APPROX FS 277.00 LBL 12. REMOVED AND REPLACED FLOOR SUPPORT ANGLE ON FS 277.00 & LBL 12 IAW SRM 51-42-06-001-001-A01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 30,876 hrs · 22,205 cycles

COCKPIT FLOOR PANEL 221 ALF AFT. SUPPORT ANGLE CORRODED AT FS 280.00. REMOVED AND REPLACED FLOOR SUPPORT ANGLE ON FS 280.00 IAW SRM 51-42-06-001-001-A01.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 28,513 hrs · 20,282 cycles

GALLEY EMERGENCY LIGHT HAS A BURNED BULB. R & R BURNED LIGHT BULB IAW AMM 33-51-05, OPS CHECK GOOD.

Part: RETAINER — DAMAGED (CARGO DOOR SEAL) · airframe 28,165 hrs · 20,002 cycles

FWD CARGO DOOR SEAL RETAINER DAMAGED AT LOWER FWD AND AFT CORNERS. COMPLIED WITH EC/TC REO 670-52-35-127 01. THIS IS A PERMANENT REPAIR.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 27,464 hrs · 19,443 cycles

12 CD SIDEWALL LOWER EXIT SIGN HAD ONE LIGHT BULB BURNED OUT. R & R THE BULB IAW AMM 33-51-05. OPS CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 27,464 hrs · 19,443 cycles

MAIN ENTRANCE FWD UPPER EXIT SIGN HAVE ONE LIGHT BULB BURNED OUT. R & R THE BULB IAW AMM 33-51-05. OPS CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 27,464 hrs · 19,443 cycles

12AB SIDEWALL LOWER EXIT SIGN HAD ONE LIGHT BULB BURNED OUT. R & R THE BULB IAW AMM 33-51-05. OPS CHECKED GOOD.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 27,083 hrs · 19,140 cycles

F/A ADVISES OVERHEAD EMERGENCY LIGHT AT ROW 4 IS INOPERATIVE. REPINNED SOCKET AT ROW 4 FLOOD LIGHT IAW ESPM 20-16-00. OPS CHECK GOOD, DMIL CLEARED PLACARD, REMOVED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,425 hrs · 18,604 cycles

EMERGENCY LIGHT IN ARMED POSITION CYCLE ON TO OFF ON THEIR OWN. R & R EPSU BATTERY PACK BETWEEN BS 565 - 581 IAW AMM 33-51-17-01 PERFORMED OPS IAW AMM 33-51-17-710 AIPC 33-51-17-01, FIG 1, ITEM 6.

Part: UNKNOWN — ODOR (CABIN) · airframe 25,959 hrs · 18,244 cycles

FUEL ODOR IN CABIN DURING DESCENT. COMPLIED WITH -SL-21-028, NO DEFECTS NOTED.

Part: CIRCUIT BOARD — FAILED (EMERGENCY LIGHTS) · airframe 25,762 hrs · 18,096 cycles

EMERGENCY LIGHTS ON WHEN SWITCH IN ARM POSITION. R & R THE PRINTED CIRCUIT BOARD IAW AMM 24-06-11. OPS CHECKED GOOD AT THIS TIME. ACFT RETURNED TO SERVICE.

Part: HANDLE — UNSERVICEABLE (PAX DOOR) · airframe 24,955 hrs · 17,483 cycles

CANN THE PAX DOOR OUTER HANDLE ASSY. REMOVED PAX DOOR DETENT ASSY IAW AMM 52-11-03-000-802. INSTALLED SERVICEABLE DETENT ASST IAW AMM 52-11-03-400-802. OPS CHECK GOOD ON PLL TEST. REMOVED PAX DOOR OUTER HANDLE IAW AMM 52-11-03-000-801. INSTALLED NEW PAX DOOR OUTER HANDLE IAW AMM 52-11-03-400-801. FITTED AND DRILLED ALL PARTS OF OUTER HANDLE ASSY FOR INSTALLATION IAW SRM 51-40-11-001-001-A01 AND DWG: 601R31741 AND DWG R31704, SR543667.

Part: DOOR — LACK OF LUBE (SERVICED DOOR) · airframe 24,955 hrs · 17,483 cycles

SERVICE DOOR FAILED FUNCTION CHECK. LUBRICATED GALLEY SERVICE DOOR IAW AMM TASK 12-20-52-640-801 PERFORMED FUNCTIONAL CHECK IAW AMM TASK 52-41-00-720-801. COMPLIED WITH FUNC CHECK IAW TASK CONE 000-52-840-101 AND AMM 52-41-00-720-801, OPS CHECK GOOD. FOUND TOP 2 BOLTS FROZEN ON FWD CONTROL RODS REMOVED BOLTS IAW AMM 52-41-02-000-804, 807 CLEANED BOLTS AND BEARING REINSTALLED BOLTS IAW 52-41-02-400-804 807. COMPLIED WITH OPS CHECK IAW AMM 52-41-00-710-801, OPS CK GOOD.

Part: DOOR — LACK OF LUBE (EMERGENCY EXIT) · airframe 24,955 hrs · 17,483 cycles

RIGHT OVERWING EMERGENCY EXIT FAILED FUNCTIONAL CHECK EXCEEDS MAXIUM FORCE REQUIRED TO OPERATE HANDLE. LUBRICATED RT OVERWING EXIT DOOR IAW AMM 12-20-52-640-802, AND PERFORMED FUNCTIONAL TEST OF OVER WING DOOR IAW AMM 52-21-00-720-801 FUNCTIONAL TEST GOOD.

Part: DOOR — LACK OF LUBE (EMERGENCY EXIT) · airframe 24,955 hrs · 17,483 cycles

LEFT OVERWING EMERGENCY EXIT FAILED FUNCNIONAL TEST. EXCEEDS MAXIUM FIRCE TO OPERATE HANDLE. LUBRICATED LT OVERWING EXIT IAW AMM 12-20-52-640-802, AND PERFORMED FUNCTIONAL CHECK IAW AMM 52-21-00-720-801, FUNCTIONAL TEST GOOD.

Part: UNKNOWN — CORRODED (BS 661-645) · airframe 24,955 hrs · 17,483 cycles

CORROSION FOUND ON LBL 9 AT FS 661 & FS 645. BLENDED AND EVALUATED FOUND TO BE OUT OF LIMITS IAW SRM 53-31-43-101-001-A01 & 51-21-06-0014-001-A01. RECEIVED AND COMPLIED WITH REO 670-53-31-325, REV DATE 2014-06-05.

Part: STRAP — DAMAGED (RT WING) · airframe 24,955 hrs · 17,483 cycles

ONE HOLE ON RT WING STRAP OVERSIZED BEYOND SB670BA-57-020 LIMITS. COMPLIED WITH REO 670-57-21-704 P1. MAJOR REPAIR.

Part: UNKNOWN — CORRODED (BS 549) · airframe 24,955 hrs · 17,483 cycles

CORROSION FOUND ON LBL 9 AT BS 549.00. UPON SEAT TRACK REMOVAL. REMOVED 1 AREAS OF CORROSION AT FS549 LBL9, SRM TASK 53-31-43-101-001-A02. RECEIVED AND COMPLIED WITH REO 670-53-31-325.

Part: SEAT TRACK — CORRODED (BS 581-677) · airframe 24,955 hrs · 17,483 cycles

SEAT TRACK CORRODED AT BS 581 - 677, LBL 9, CORRODED. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-00-49-000-801-A03 AND AMM 53-00-49-400-801-A03.

Part: FLOOR SUPPORT — CORRODED (BS 310) · airframe 24,955 hrs · 17,483 cycles

CORROSION ON FLOOR FLOOR SUPPORT AT BS 310 +10, RBL 41. REMOVED RT FLOOR SUPPORT IAW SRM 51-41-02,51. IAW SOP 5702.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 24,955 hrs · 17,483 cycles

SEAT TRACK CORRODED BS 485 - 581, LBL 9. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-00-801, A03 AND AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 364-485) · airframe 24,955 hrs · 17,483 cycles

SEAT TRACK CORRODED AT BS 364 - 485, LBL 9. R & R SEAT TRACK IAW AMM 53-00-49-000-801-A03 AND 53-00-49-400-801-A03.

Part: FLOORBEAM — CORRODED (BS 333) · airframe 24,955 hrs · 17,483 cycles

CORROSION ON FLOORBEAM ANGLE AT BS 333 RBL 12. REMOVED CORROSION FROM FLOORBEAM ANGLE IAW SRM 51-21-6-001-001-A01.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 24,955 hrs · 17,483 cycles

RIGHT BS 280, BULKHEAD WEB CORRODED. BLENDED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-11-10-201-003-A01. COMPLIED WITH ECTC REO670-53-11-594 01 AND GREO 670-53-11-594, REV.

Part: FLOORBEAM — CORRODED (BS 310) · airframe 24,955 hrs · 17,483 cycles

CORROSION ON FLOORBEAM AT BS 310.0+10. LBL 41. REMOVED AND REPLACED ANGLES IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-06-001-001-A01. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 679-830) · airframe 24,955 hrs · 17,483 cycles

SEAT TRACK CORRODED AT BS 679 - 830.4 LBL 9. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03 AND AMM 53-00-49-400-801.

Part: FRAME — DAMAGED (BS 280) · airframe 24,952 hrs · 17,479 cycles

OBLONG HOLE WAS DISCOVERED IN THE BS 280 FRAME. REPAIRED IAW REO 670-53-11-947. MAJOR REPAIR.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 24,955 hrs · 17,483 cycles

LEFT BS 280 BULKHEAD WEB CORRODED. REMOVED CORROSION IAW SRM 53-11-10-201-003-A01. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 830-1000) · airframe 24,952 hrs · 17,479 cycles

SEAT TRACK CORRODED AT BS 830.4-1000, LBL 9. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-00-49-000-801-A03 AND AMM TASK 53-00-49-400-801. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 458-549) · airframe 24,952 hrs · 17,479 cycles

SEAT TRACK CORRODED AT BS 458-549, RBL 9. R & R SEAT TRACK IAW AMM 53-00-49-00-801-A03 AND 53-00-49-400-801-A03. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 581-677) · airframe 24,952 hrs · 17,479 cycles

LEFT SIDE WALL SEAT TRACK CORRODED AT BS 581-677. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-00-49-000-801 & AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 785-863) · airframe 24,952 hrs · 17,479 cycles

RT SIDE WALL SEAT TRACK CORRODED BS 785.15-863. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-801 & AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 677-708) · airframe 24,952 hrs · 17,479 cycles

LT SIDE WALL SEAT TRACK CORRODED AT BS 677-708. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 AND AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 24,952 hrs · 17,479 cycles

LT SIDE WALL SEAT TRACK CORRODED BS 485-581. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-801 & AMM 53-00-49-400-801.

Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · airframe 24,952 hrs · 17,479 cycles

CARGO FLOOR SUPPORT CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-61-23-101-001-A01. REPAIRED IAW REO 670-53-61-913, REV "A". MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 677-708) · airframe 24,952 hrs · 17,479 cycles

RIGHT SIDEWALL SEAT TRACK CORRODED AT BS 677-708. R & R SEAT TRACK IAW AMM 53-00-49-000-801 AND GREO 670-53-00-343, REV E.

Part: SEAT TRACK — CORRODED (BS 581-677) · airframe 24,952 hrs · 17,479 cycles

RT SIDE WALL SEAT TRACK CORRODED AT BS 581-677. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-00-801 AND AMM 53-00-49-400-801. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 708-761) · airframe 24,952 hrs · 17,479 cycles

RT SIDE WALL SEAT TRACK CORRODED BS 708-761.85. R & R SEAT TRACK IAW AMM 53-00-49-000-801 AND 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 877-969) · airframe 24,952 hrs · 17,479 cycles

RT SIDE WALL SEAT TRACK CORRODED AT BS 877-969, SURFACE CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-400-801 AND AMM 53-00-49-000-801.

Part: SEAT TRACK — CORRODED (BS 708-761) · airframe 24,952 hrs · 17,479 cycles

LEFT SIDE WALL SEAT TRACK CORRODED AT BS 708-761.85. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 & AMM, 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 677-830) · airframe 24,952 hrs · 17,479 cycles

SEAT TRACK CORRODED AT BS 677 - 830.4 RBL 9. R & R SEAT TRACK IAW AMM 53-00-49-00-801-A03 AND 53-00-49-400-801-A03. MAJOR REPAIR.

Part: VANE — GOUGED (RT WING TE FLAP) · airframe 24,952 hrs · 17,479 cycles

RT INBD FLAP INBD VANE ACTUATOR HAS SMALL GOUGE ON UPPER SKIN. BLENDED OUT GOUGE ON UPPER SKIN FOUND TO BE WITHIN LIMITS IAW 57-52-01. THIS REPAIR IS CLASSIFIED AS A REPAIR IAW SOP 5702.

Part: STRINGER — CORRODED (PAX DOOR) · airframe 24,952 hrs · 17,479 cycles

PAX DOOR STRINGER HAS CORROSION INSIDE ICE BREAKER DOOR. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 24,952 hrs · 17,479 cycles

FLIGHT DECK CENTER FLOORBEAM ANGLE IS CORRODED. R & R FLOORBEAM ANGLE FWD SIDE OF BS 280 IAW SB670BA-53-041.

Part: SUPPORT — CRACKED · airframe 24,952 hrs · 17,479 cycles

THERE IS A CRACK IN THE RT TRU SUPORT, OTBD OF THE HYD ACCUMULATOR PRESSURE GAGES. COMPLIED WITH EC/TC REO 670-53-11-509 AND GREO 670-53-11-509, REV.

Part: SUPPORT — CRACKED · airframe 24,952 hrs · 17,479 cycles

THERE IS A CRACK IN THE LT TRU SUPPORT OTBD OF THE ADG HYD PUMP. COMPLIED WITH EC/TC 670-53-11-509 AND GREO 670-53-11-509 REV-DATED: 07-06-2010.

Part: SEAT TRACK — CRACKED (COCKPIT) · airframe 24,955 hrs · 17,483 cycles

CAPTAIN`S INBD SEAT TRACK WEAR STRIP WAS FOUND TO HAVE A BROKEN SECTION APPROXIMATELY 3.8 INCHES LONG. REMOVED CAPTAIN'S INBD SEAT TRACK IAW SRM 51-42-21-001-01-A01 DWG 601R-41082. INSTALLED REPLACEMENT SEAT TRACKS IAW SRM 51-42-21-001-001-A01.

Part: SIGN — MISSING (CABIN) · airframe 24,903 hrs · 17,440 cycles

PAX DOOR EMERGENCY EXIT SIGN MISSING. FOUND EMERGENCY EXIT SIGN AND INSTALLED PANEL IAW AMM 33-51-05. ACFT OK FOR SERVICE.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 24,067 hrs · 16,837 cycles

FWD F/A FLASHLIGHT INOPERATIVE. INSTALLED NEW FLASHLIGHT IAW AMM 25-61-01. OK FOR SERVICE.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 22,962 hrs · 16,045 cycles

MEGAPHONE INOPERATIVE. R & R MEGAPHONE IAW AMM 25-61-14. OPS CHECKED GOOD.

Part: MEGAPHONE — UNKNOWN (CABIN) · airframe 22,190 hrs · 15,509 cycles

MEGAPHONE INOPERATIVE. OPS CHECK OF MEGAPHONE GOOD IAW AMM 23-31-01. ACFT GOOD FOR SERVICE.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 21,424 hrs · 14,971 cycles

FWD CABIN FLASHLIGHT IS INOPERATIVE. R & R BATTERIES IN FLASHLIGHT IAW AMM 25-61-00. OPS CHECKED GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: CONTROL ROD — UNSECURE (DOOR HANDLE) · airframe 21,405 hrs · 14,953 cycles

GALLEY SERVICE DOOR HANDLE DOES NOT SWING PAST THE 12:00 POSITION, UNABLE TO OPEN THE DOOR. INSPECTED HANDLE ASSY FOUND CONTROL ROD TO UPLOCK CRANK UNSECURE. RESECURED CONTROL ROD TO UPLOCK CRANK IAW AMM 52-41-03. OPS CHECK GOOD, DEFER CLEARED PLACARD REMOVED. SDR CLOSED.

Part: DOOR — LACK OF LUBE (SERVICE) · airframe 20,161 hrs · 14,012 cycles

SERVICE DOOR IS VERY DIFFICULT TO OPEN. LUBRICATED SERVICE DOOR & OPS CHECKED GOOD IAW AQMM 52-41-00. (SDR CLOSED)

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 19,951 hrs · 13,857 cycles

RT 280 BULKHEAD LOWER WEB CORRODED. REPAIR CLASSIFIED AS A MAJOR.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 19,951 hrs · 13,857 cycles

BS 280 BULKHEAD WEB CORRODED.

Part: POST — CRACKED (BS 280) · airframe 19,930 hrs · 13,843 cycles

FS 280, RBL 27.00 VERTICAL POST LOWER ATTACH POINT CRACKED. REMOVED POST IAW SRM 51-42-06-001-001-A01. LOCATED, DRILLED, AND INSTALLED NEW POST IAW SRM 51-42-06-001-001. REPAIR CLASSIFIED AS MINOR.

Part: SEAT TRACK — CORRODED (BS 836.5-977) · airframe 19,930 hrs · 13,843 cycles

RT SEAT TRACK AT RBL 9 FROM FS 836.5 TO 977 CORRODED. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-51-49-101-001-A01. REMOVED OLD SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 683-836.5) · airframe 19,930 hrs · 13,843 cycles

RT SEAT TRACK AT RBL 9 FROM FS 683 TO 836.5 CORRODED. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-51-49-101-001-A01. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-00-49-400-801-A03.

Part: FLOOR SUPPORT — CORRODED (E/E BAY) · airframe 19,930 hrs · 13,843 cycles

FLOOR SUPPORT FOR AVIONICS FLOORBOARD 141ALF CORRODED. R & R CORRODED FLOOR SUPPORT IAW SRM 51-42-06-001-001-A01.

Part: ANGLE — CRACKED (FUSLEAGE) · airframe 19,930 hrs · 13,843 cycles

PERFROMED EDDY CURRENT INSPECTION OF VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE IAW MAC NDT INSP PROCEDURE ET-2. ATTACH DRAG ANGLE IS VERIFIED CRACKED. PERFORMED CUTOUT OF DAMAGED AREA ON FWD DRAG ANGLE IAW REO 670-53-31-018. PERFORMED NDT OF AREA IAW REO 670-55-31-018. NO INDICATIONS NOTED.

Part: SEAT TRACK — CORRODED (BS 669.4-997) · airframe 19,930 hrs · 13,843 cycles

SEAT TRACK FS 669.4 TO 997 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-41-49-101-001-A01.

Part: SEAT TRACK — CORRODED (BS 349-349) · airframe 19,930 hrs · 13,843 cycles

CORROSION ON SEAT TRACK FROM FS 349 TO 379 APPROX RBL 9. R & R SEAT RAIL. EVALUATED SEAT TRACK DETERMINED THAT SEAT TRACK IS OUT OF ALLOWABLE LIMITS IAW SRM 53-21-49-101-001. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801-A03. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801-A03.

Part: HINGE BRACKET — CORRODED (PAX DOOR) · airframe 19,930 hrs · 13,843 cycles

CENTER HINGE BRACKET FOUND TO BE CORRODED AT THE TOP OF PAX DOOR. REPAIRED HINGE LOWER CHANNEL IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 581-683) · airframe 19,930 hrs · 13,843 cycles

RIGHT SEAT TRACK AT RBL 9, FS 581 TO 683 CORRODED. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-31-49-101-001-A01. R & R SEAT TRACK IAW AMM 53-00-49-400-801 AND AMM 53-00-49-000-801.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 19,930 hrs · 13,843 cycles

FOUR CORRODED "L" ANGLES FOUND TO BE CORRODED AT HINGE SIDE OF PAX DOOR. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESSS INSPECTION OF BLEND AREA IAW MAC NDT INSP PROCEDURE UT-3. NO INDICATIONS NOTED.

Part: SEAT TRACK — CORRODED (BS 370) · airframe 19,930 hrs · 13,843 cycles

CORROSION ON SEAT TRACK FROM BS 370, LBL 9. SEAT TRACK IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-21-49-101-001. REMOVED SEAT TRACK FROME FS 374-485 IAW AMM 53-00-49-000-801-A03. INSTALLED NEW SEAT TRACK AT IAW AMM 53-00-49-400-801-A03.

Part: STRUCTURE — CORRODED (PAX DOOR) · airframe 19,930 hrs · 13,843 cycles

TWO FWD & AFT BOTTOM CORNER ON PAX DOOR CORRODED. REMOVED FWD & AFT BOTTOM CORNER COVERS SRM 51-42-13-001-001-A01. INSTALLED FWD & AFT BOTTOM CORNER IAW SRM 51-42-06-001-001-A01.

Part: SILL — CORRODED (BS 319) · airframe 19,930 hrs · 13,843 cycles

FLOOR SILL HAS CORROSION FWD OF SERVICE DOOR FRAME AT FS 319. REMOVED AND REPLACED IAW SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01 AND 51-42-21-001-001-A01.

Part: CHANNEL — CORRODED (PAX DOORWAY) · airframe 19,947 hrs · 13,855 cycles

PAX DOOR THRESHOLD NUTPLATE CHANNEL CORRODED. FOUND CHANNEL TO BE OUT OF LIMITS IAW SRM 51-21-06-001-001-A01. REMOVED CHANNEL IAW SRM 51-02-001-001-A01. INSTALLED NEW CHANNEL IAW SRM 51-41-02-001-001-A01.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 19,930 hrs · 13,843 cycles

ANGLE FWD SIDE OF FS 280 FLOORBEAM IS CORRODED. R & R ANGLE IAW SRM 51-42-06-001-001, 51-42-21-001-001, AND DWG CC670-33052.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 19,930 hrs · 13,843 cycles

LEFT BS 280 BULKHEAD LOWER WEB CORRODED. REPAIRED IAW SRM 53-11-10-201-003-A01.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 19,930 hrs · 13,843 cycles

FS 280 FLOORBEAM CORRODED. REPAIRED IAW REO 670-53-11-047 AND REO 670-53-11-047, REV E.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 19,930 hrs · 13,843 cycles

VERTICAL STAB CRACKED ON LT SIDE LOWER DRAG ANGLE. R & R DRAG ANGLE IAW SRM 51-42-13-001-001-A01, 51-42-21-000-001-A01, 51-42-22-001-001-A01, AND DWG NR BA670-35002.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 19,930 hrs · 13,843 cycles

RT 280 BULKHEAD LOWER WEB CORRODED. REPAIRED IAW SRM 53-11-10-201-003-A01.

Part: PLACARD — DETERIORATED (CABIN) · airframe 19,930 hrs · 13,843 cycles

PAX DOOR TO OPEN AND EXIT PLACARD DETERIORATED. R & R PAX DOOR OPEN AND EXIT PLACARDS IAW AMM 20-60-04. R & R PLACARDS IAW AMM 20-60-04.

Part: LIGHT — MISSING (CABIN) · airframe 19,000 hrs · 13,208 cycles

RT EMERGENCY OVERWING DOOR MISSING FWD FLOOR TRACK LIGHTING STRIP. REPLACED RT EMERGENCY OVERWING DOOR FWD FLOOR TRACK LIGHTING STRIP IAW AMM 33-51-01.

Part: SIGN — MISSING (EMERGENCY LIGHT) · airframe 18,810 hrs · 13,079 cycles

EXIT SIGN BY GALLEY DOOR MISSING. REPLACED COVER OVER FLOOR LIGHT ASSY. ON GALLEY 2 IAW AMM 33-51-11. OP'S TESTED GOOD.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 18,079 hrs · 12,578 cycles

CREW REPORTS MEGHPHONE INOP. R & R MEGHPHONE IAW AMM 25-61. OPS CK GOOD. ACFT OK FOR SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 16,996 hrs · 11,843 cycles

FWD F/A FLASHLIGHT INOP. R & R FWD FLASHLIGHT IAW AMM 25-61-00. OPS CHECK GOOD. (CLOSED)

Part: FLASHLIGHT — INOPERATIVE (COCKPIT)

FWD FLASHLIGHT, INOPERATIVE. R & R FLASHLIGHT.

Part: WIRE HARNESS — UNSERVICEABLE (NLG STEERING) · airframe 16,689 hrs · 11,638 cycles

NOSE WHEEL STEERING CAUTION MSG AFTER TAKEOFF WHEN GEAR RETRACTED. LANDED WITHOUT NWS. NOT AN OVERWEIGHT LANDING. UNABLE TO RESET ON GROUND WITH MX (ACFT RETURNED TO DEPARTURE AFTER T/O -- EMERGENCY DECLARED) R & R NWS HARNESS, OPS CHECK GOOD IAW AMM 32-61-05. NWS INOP MSG REMAINS. (CLOSED)

Part: SEAT TRACK — CORRODED (BS 581-693) · airframe 15,991 hrs · 11,131 cycles

RIGHT SEAT TRACK CORRODED FROM FS 581.00 TO 693.00. SEAT TRACK CORROSION IS BEYOND ALLOWABLE BLEND OUT SEAT TRACK FOUND TO BE UNSERVICEABLE PER SRM 53-31-49-101-001-A01. REMOVED UNSERVICEABLE SEAT TRACK AND REPAIRED WITH SERVICEABLE NEW SEAT TRACK AND WORK DONE IAW AMM 53-00-49-000-801-A03 AND 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 797-813.7) · airframe 15,991 hrs · 11,131 cycles

RT SIDE WALL SEAT TRACK AT FS 797-813.70 CORRODED. REMOVED CORROSION FROM RT SIDE SEAT TRACK "WALL" BETWEEN FS 797.00 AND 813.70. ALL WORK DONE IAW SRM 51-12-00-101-001-A01. SEAT TRACK FOUND TO BE IN SERVICEABLE LIMITS PER SRM 53-41-49-101-001-A01. ALODINE IS REQUIRED ON REWORKED AREA. APPLIED ALODINE TO REWORKED AREA PER SRM 53-41-49-101-001-A01.

Part: SEAT TRACK — CORRODED (BS 581-645) · airframe 15,991 hrs · 11,131 cycles

CENTER FLOOR TRACK CORRODED AND PITTED FROM FS 581 TO 645. CLEANED CENTER FLOOR TRACK FROM FS 581 TO FS 645 IAW 51-12-00-001-001. SEAT TRACK FOUND TO BE OUT OF LIMITS AND IS UNSERVICEABLE PER SRM 53-31-49-101-001-A01. REMOVED LT CENTER SEAT TRACK IAW AMM 53-00-49-000-801 AND INSTALLED SERVICEABLE TRACK AT LT CENTER FS 581 TO 645 IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 797-813.7) · airframe 15,991 hrs · 11,131 cycles

LT SIDE WALL SEAT TRACK AT FS 797.00 TO 813.70 CORRODED. REMOVED CORROSION FROM SEAT TRACK BETWEEN FS 797.00 AND 813.70 ON LT SIDE WALL ALL WORK DONE IAW SRM 51-12-00-101-001-A01. SEAT TRACK FOUND TO BE IN SERVICEABLE LIMITS PER SRM 53-41-49-101-001-A01. ALODINE IS REQUIRED ON REWORKED AREA. APPLIED ALODINE TO REWORKED AREA PER SRM 53-41-49-101-001-A01.

Part: SEAT TRACK — CORRODED (BS 364) · airframe 15,991 hrs · 11,131 cycles

CTR FLOOR TRACK AT FS 364 NEAR 1ST SCREW PITTED. CLEANED CENTER FLOOR TRACK AT FS 364 NEAR 1ST SCREW IAW SRM 51-12-00-001-001. SEAT TRACK FOUND TO BE OUT OF LIMITS PER SRM 53-21-49-101-001-A01. REMOVED AND REPLACED SEAT/CENTER FLOOR TRACK AT FS 364 IAW AMM 53-00-49-000/(400)-801.

Part: STRAKE — CRACKED (VERTICAL STAB) · airframe 15,991 hrs · 11,131 cycles

AFT DORSAL STAKE FOUND WITH 1" CRACK DEFECT MARKED WITH RED TAPE. REPAIRED CRACK AT AFT DORSAL STRAKE IAW SRM 51-75-16-001-A01. REPAIR OF AFT DORSAL FULLY CURED IAW SRM 51-75-16-001-A01. PRIMED AND PAINTED IAW SRM 51-25-01-001-A01.

Part: UNKNOWN — ODOR (GALLEY) · airframe 15,569 hrs · 10,798 cycles

F/A REPORTED ELECTRIC SMOKE TYPE ODOR IN THE GALLEY AREA W/NO VISABLE INDICATIONS NOTED. CW GVI TO GALLEY OPERATED ALL GALLEY COMPONENTS/ LIGHTS NO DEFECTS NOTED IAW AMM 38-10-00, 33-26-00. (CLOSED)

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 15,107 hrs · 10,452 cycles

FLOOR SUPPORT FRAME CORRODED. REMOVED CORRODED FLOOR SUPPORT FRAME. NEW FRAME ON REQ. WORK DONE IAW SRM 51-42-02. PICKED UP FASTENER HOLES ,COUNTERSUNK, INSTALLED NUT PLATES AND INSTALLED NEW FRAME SUPPORT. SRM 51-42-06,51-41-02. APPLIED CHEMICAL CONVERSION COATING IAW SRM 51-21-11. ADJUSTED PROX SENSOR PX25 IAW AMM 52-70-04. PERFORMED RII OF PASSENGER DOOR PROX SENSOR PX25 IAW GMM 3.3.

Part: SEAT TRACK — CORRODED · airframe 15,107 hrs · 10,452 cycles

SEAT TRACK HAS CORROSION. R & R DAMAGED PORTION OF SEAT TRACK AT FS 349 & RBL 9.00 IAW EC/TC REO 670-53-00-074.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 15,107 hrs · 10,452 cycles

FS 280 FWD CTR FLOOR SUPPORT BETWEEN LT AND RT BL9 CORRODED. REMOVED AND REPLACED FLOORBEAM. IAW ALL APPROPRIATE SRM`S.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 13,884 hrs · 9,535 cycles

COCKPIT FLASHLIGHT INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,445 hrs · 8,421 cycles

EMERGENCY EXIT LIGHTS LOWER FWD AND AFT OF SERVICE DOOR HAVE SEVERAL BULBS BURNED OUT.

Part: SPHERICAL BEARIN — CRACKED (FUSELAGE) · airframe 11,026 hrs · 7,337 cycles

RT WING TO FUSELAGE PICK UP LINK AT FS 787.00 UPPER AND LOWER SPHERICAL BEARINGS CRACKED DUE PERMANENT REPAIR. THIS SDR WILL REMAIN OPEN PENDING MAINTENANCE DETERMINATION OF AN APPROPRIATE CORRECTIVE ACTION.

Part: SPHERICAL BEARIN — CRACKED (FUSELAGE) · airframe 11,026 hrs · 7,337 cycles

RT WING TO FUSELAGE PICK UP LINK AT FS 787.00 UPPER AND LOWER SPHERICAL BEARINGS CRACKED. REQUIRES REPEAT INSP EVERY 1000 FLT HRS.

Part: SUPPORT ANGLE — CORRODED (GALLEY DOOR) · airframe 11,026 hrs · 7,337 cycles

CORROSION FOUND ON THE SERVICE DOOR GALLEY SUPPORT ANGLE. (S)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PAX DOOR THRESHOLD FLOOR SUPPORT ANGLE HAS CORROSION DAMAGE (MARKED) (RESOLVED ON W/O: 97397 TASKCARD: N/R 00173) WORK COMPLETED IN ACCORDANCE WITH: ITEM 1 R&R FLOOR SUPPORT ANGLE IAW CRJ 700 SRM 51-40-00 AND SRM 51-40-11. DH 7025983 ITEM 2 ADJUSTED AND SAFETIED PROX SWITCH PX 25 IAW CRJ 700 AMM 52-70-04. MV7022816 08-16-08.

Part: INTERCOSTAL — CRACKED (ASD) · airframe 11,026 hrs · 7,337 cycles

ASD 318 INTERCOSTAL CRACKED. REMOVED AND REPLACED INTERCOSTAL 318 ON PASSENGER DOOR IAW SRM 51-42-06. (S)

Part: FLOORBEAM — CORRODED (BS 280)

THE 280 BEAM CORRODED AND CRACKED OUTBOARD OF LBL 9. REFER TO STEPS 2-15 ON ATTACHED M234 FOR WORK ACCOMPLISHED. INSTALLED LT DRIP TRAY IAW CRJ 700 SRM 51-42-13. (S)

Part: FLOORBEAM — CORRODED (BS 280)

FS 280 FWD ANGLE (FLIGHT STATION FWD FLOOR LAND) CORRODED. REMOVED FWD ANGLE AT FS 280. ALL WORK DONE IAW CRJ 700 SRM 51-42-06. DRILLED UP FWD ANGLE IAW SRM 51-42-06. (S)

Part: TRUNNION — CORRODED (MLG)

CORROSION ON RT MLG FWD TRUNNION. REFER TO N/R-00201 FOR DOCUMENTATION AS THE LANDING GEAR WAS REMOVED AND REPLACED FOR EO 700-32-023. LANDING GEAR WAS SENT TO THE GEAR SHOP. (S)

Part: TRUNNION — CORRODED (LT MLG)

CORROSION ON LT MLG FWD TRUNNION. THE LANDING GEAR WAS REMOVED AND REPLACED FOR EO 700-32-023. LANDING GEAR WAS SENT TO THE GEAR SHOP. (S)

Part: DRAG ANGLE — CRACKED (ASD)

ASD AFT DRAG ANGLE CRACKED. CUT AWAY SECTION OF AFT ASD DRAG ANGLE IAW REO 670-52-11-072. PERFORMED EDDY CURRENT INSPECTION OF CUT LINES ON AIRSTAIR DOOR AFT DRAG ANGLE IAW REO 670-52-11-072 PER CRJ700 NDTM 51-20-006. NO DEFECTS NOTED. (S)

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 10,322 hrs · 6,852 cycles

LEFT AFTMOST EXTERNAL EMERGENCY LIGHT INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 9,760 hrs · 6,463 cycles

EMERGENCY LIGHT IN CABIN INOP, SECOND LIGHT FROM FRONT.

Part: WARNING SYSTEM — MALFUNCTIONED (ANTI-SKID SYS) · airframe 9,560 hrs · 6,329 cycles

ANTI-SKID INBOARD CAUTION MSG ILLUMIMATED CYCLED ANTI-SKID CONTROL UNIT CIRCUIT BREAKERS. PERFORMED OPS CHK. MSG EXTINGUISHED. EMERGENCY DECLARED. EN ROUTE TO EYW A/C DIVERTED TO NQX DUE TO MTC. FLT 4465 DEL 52 MINS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 9,436 hrs · 6,253 cycles

FLT 4916 DEL 315 MINS, EMERGENCY LIGHTS WILL NOT COME ON.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 8,315 hrs · 5,470 cycles

FWD F/A FLASHLIGHT INOP.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 8,277 hrs · 5,447 cycles

MEGAPHONE INOP.

Part: SERVICE DOOR — STUCK · airframe 8,124 hrs · 5,332 cycles

F/A UNABLE TO OPEN SERVICE DOOR.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 7,750 hrs · 5,066 cycles

F/O'S FLASHLIGHT INOP.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 7,569 hrs · 4,940 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT HAS SEVERAL INOP BULBS.

Part: SILL — CORRODED (FUSELAGE) · airframe 7,206 hrs · 4,697 cycles

CORROSION ON LOWER LEG OF PAX DOOR SILL FS 330. REMOVED AND TREATED CORROSION AS REQUIRED. APPLIED AO23 FINISH AS REQUIRED. ALL WORK PERFORMED IAW CRJ 700 SRM 51-25-01. SM17032 SUPPLEMENTAL - SDR CLOSED 01/26/07.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 7,206 hrs · 4,697 cycles

RT VERTICAL STAB TO FUSELAGE ATTACH ANGLE IS CRACKED AT AFT END. REPAIR OF RT VERTICAL STAB TO FUSELAGE ANGLE IAW REO 670-55-31-017.

Part: SEAT TRACK — CORRODED (BS 581-687) · airframe 7,206 hrs · 4,697 cycles

FOUND LT SIDEWALL SEAT TRACK CORRODED, FS 581 TO 687, SEC 3.

Part: SEAT TRACK — CORRODED (BS 687-836) · airframe 7,206 hrs · 4,697 cycles

FOUND RT FLOOR SEAT TRACK HAS CORROSION, FS 687 TO 836 - SEC 4.

Part: SEAT TRACK — CORRODED (BS 836-985) · airframe 7,206 hrs · 4,697 cycles

FOUND RT FLOOR SEAT TRACK CORRODED, FS 836 TO 985 SEC 5.

Part: SEAT TRACK — CORRODED (BS 495-581) · airframe 7,206 hrs · 4,697 cycles

FOUND LT FLOOR SEAT TRACK CORROSION, FS 495 TO 581, SEC 2.

Part: SEAT TRACK — CORRODED (BS581-687) · airframe 7,206 hrs · 4,697 cycles

FOUND RT FLOOR SEAT TRACK CORROSION, FS 581 TO 687 - SEC 3.

Part: SEAT TRACK — CORRODED (BS 350-495) · airframe 7,206 hrs · 4,697 cycles

FOUND RT FLOOR SEAT TRACK CORRODED, FS 350 TO 495, SEC 1.

Part: SEAT TRACK — CORRODED (BS 581-687) · airframe 7,206 hrs · 4,697 cycles

FOUND LT FLOOR SEAT TRACK CORROSION, FS 581 TO 687, SEC 3.

Part: SEAT TRACK — CORRODED (BS 680-712) · airframe 7,206 hrs · 4,697 cycles

FOUND RT SIDEWALL SEAT TRACK CORRODED, FS 680 TO 712.

Part: SEAT TRACK — CORRODED (BS 485-576) · airframe 7,206 hrs · 4,697 cycles

FOUND LT SIDEWALL SEAT TRACK CORROSION, FS 485 TO 576, SEC 2.

Part: SEAT TRACK — CORRODED (BS 495-581) · airframe 7,206 hrs · 4,697 cycles

FOUND RT FLOOR SEAT TRACK CORRODED, FS 495 TO 581, SEC 2.

Part: SEAT TRACK — CORRODED (BS 350-495) · airframe 7,206 hrs · 4,697 cycles

FOUND RT SIDEWALL SEAT TRACK CORRODED, FS 350 TO 495, SEC 1.

Part: SEAT TRACK — CORRODED (BS 365-495) · airframe 7,206 hrs · 4,697 cycles

FOUND LT FLOOR SEAT TRACK CORROSION, FS 365 TO 495 - SEC 1.

Part: SEAT TRACK — CORRODED (BS 712-761) · airframe 7,206 hrs · 4,697 cycles

FOUND RT SIDEWALL SEAT TRACK CORRODED, FS 712 TO 761, SEC 5.

Part: SEAT TRACK — CORRODED (BS 836-985) · airframe 7,206 hrs · 4,697 cycles

FOUND LT SIDEWALL SEAT TRACK CORRODED, FS 836 TO 985, SEC 5.

Part: SEAT TRACK — CORRODED (BS 576-680) · airframe 7,206 hrs · 4,697 cycles

FOUND LT SIDEWALL SEAT TRACK CORRODED, FS 576-TO 680, SEC 4.

Part: SEAT TRACK — CORRODED (BS 785-863) · airframe 7,206 hrs · 4,697 cycles

FOUND LT SIDEWALL SEAT TRACK CORRODED, FS 785 TO 863, SEC 6.

Part: SEAT TRACK — CORRODED (BS 495-581) · airframe 7,206 hrs · 4,697 cycles

FOUND RT SIDEWALL SEAT TRACK CORRODED, FS 495 TO 581, SEC 2.

Part: SEAT TRACK — CORRODED (BS 687- 836) · airframe 7,206 hrs · 4,697 cycles

FOUND LT FLOOR SEAT TRACK CORROSION, FS 687 TO 836, SEC 4.

Part: SEAT TRACK — CORRODED (BS 785-863) · airframe 7,206 hrs · 4,697 cycles

FOUND RT SIDEWALL SEAT TRACK CORRODED, 785 TO 863, SEC 6.

Part: SEAT TRACK — CORRODED (BS 863-985) · airframe 7,206 hrs · 4,697 cycles

FOUND RT SIDEWALL SEAT TRACK CORRODED, FS 863 TO 985, SEC 7.

Part: SEAT TRACK — CORRODED (BS 350-485) · airframe 7,206 hrs · 4,697 cycles

FOUND LT SIDEWALL SEAT TRACK CORROSION, FS 350 TO 485, SEC 1.

Part: SEAT TRACK — CORRODED (BS 863-985) · airframe 7,206 hrs · 4,697 cycles

FOUND LT SIDEWALL SEAT TRACK CORRODED, FS 863 TO 985.

Part: SEAT TRACK — CORRODED (BS 836-985) · airframe 7,206 hrs · 4,697 cycles

FOUND LT FLOOR SEAT TRACK CORROSION, FS 836 TO 985, SEC 5.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 7,206 hrs · 4,697 cycles

FOUND FS 280 HAS CORROSION ON CROSS BEAM. WORK COMPLETED IN ACCORDANCE WITH: CRJ700 REO 670-53-11-046, REO 670-53-11-047, IS 67053110002, AND ASA SP 607 AND EO700-53-0061.

Part: WEB — CORRODED (BS 280) · airframe 7,206 hrs · 4,697 cycles

FOUND FS 280 LT WEB CORRODED. REPAIRED IAW REO 670-53-11-052. ITEM: 9 RII SATISFACTORY PER ASA SP 607 AND EO700-53-0062.

Part: WEB — CORRODED (BS 280) · airframe 7,206 hrs · 4,697 cycles

FOUND FS 280 HAS CORROSION ON RT WEB. REPAIRED IAW REO 670-53-11-052. SM 17032ITEM: 9 AND ALL SRMS. RII SATISFACTORY PER ASA SP 607 AND EO700-53-0062 01

Part: PLACARD — WORN (PAX DOOR) · airframe 7,206 hrs · 4,697 cycles

PAX DOOR 'EXIT' PLACARD WORN REMOVED AND REPLACED "EXIT" PLACARD IAW CRJ 700 AMM 11-20. NO DEFECTS NOTED AT THIS TIME.

Part: PLACARD — WORN (PAX DOOR) · airframe 7,206 hrs · 4,697 cycles

PAX DOOR 'OPEN' PLACARD WORN. REMOVED AND REPLACED "OPEN " PLACARD IAW CRJ AMM 11-20. NO DEFECTS NOTED AT THIS TIME.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 7,206 hrs · 4,697 cycles

PAX DOOR OUTER HANDLE CRACKED (MARKED) REMOVED RODS AND LOCKING DIVCE. REMOVED PAX DOOR OUTER HANDLE. DRILLED UP NEW PAX DOOR OUTER HANDLE AND INSTALLED IAW CRJ 700 AMM 52-11-03 PAGES 401-403. REINSTALLED LOCKING DIVICE , RODS, AND UPPER STEP IAW CRJ 700 AMM 52-11-03 JOB COMPLETE.

Part: PLACARD — WORN · airframe 7,206 hrs · 4,697 cycles

PAX DOOR ARROW PLACARD WORN. REMOVED AND REPLACED ARROW PLACARD IAW CRJ 700 AMM 11-20. NO DEFECTS NOTED AT THIS TIME.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 5,634 hrs · 3,728 cycles

EMERGENCY LIGHTS INOP

Part: WIRE — DAMAGED (EMERGENCY LIGHT)

DURING A GROUND INSPECTION IN SLC, THE EMERGENCY EXIT SIGN, DS158, WAS FOUND TO BE INOPERATIVE. MAINTENANCE FOUND AND REPAIRED DAMAGED WIRING AT CANNON PLUG P341. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LATCH — CONTAMINATED (PAX DOOR)

DURING A GROUND INSPECTION IN ATL, THE FORWARD PASSENGER DOOR WOULD NOT CLOSE. MAINTENANCE REMOVED DEBRIS FROM THE PASSENGER DOOR LATCH MECHANISM. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STEP — CRACKED (PAX DOOR)

DURING AN A-CHECK IN MCN, THE PASSENGER DOOR BOTTOM STEP WAS FOUND CRACKED AT THE ATTACH POINT. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. (M)

Part: STEP — CRACKED (PAX DOOR)

DURING A C-CHECK IN MCN, THE PASSENGER DOOR LOWER STEP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL REMOVE AND REPLACE THE PASSENGER DOOR LOWER STEP. (M)

Part: LIGHT — INOPERATIVE (EXTERIOR)

FLT 4744 - DURING A GROUND INSPECTION IN SLC, THE AFT EXTERIOR EMERGENCY LIGHT ON THE LEFT SIDE WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE AFT EXTERIOR EMERGENCY LIGHT ON THE LEFT SIDE. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)