N713EV

Part: SKIN — DAMAGED (ZONE 600 FLAP) · airframe 41,538 hrs · 30,106 cycles

RH OTBD FLAP UNDER WING SKIN HAS CREASING DUE TO BIRD STRIKE DAMAGE. REPAIRED RH OTBD FLAP UNDER WING SKIN IAW SRM 57-53-01 TYPE 3 REPAIR.

Part: SKIN — DAMAGED (ZONE 600 FLAP) · airframe 41,532 hrs · 30,098 cycles

RH OTBD FLAP UNDER WING SKIN HAS CREASING DUE TO BIRD STRIKE DAMAGE. (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS

Part: WINDSHIELD — DELAMINATED (COCKPIT RIGHT) · airframe 40,601 hrs · 29,301 cycles

RIGHT WINDSHIELD FOGGING ON EDGES ALL AROUND. (FLIGHT 3085 FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 27688183 WITH THE FOLLOWING CORRECTIVE ACTION: "FOUND RH WINDSHIELD TO HAVE DELAMINATION OUT OF LIMITS. REMOVED AND REPLACED RH WINDSHIELD IAW AMM 56-11-01. SEE CP 27688308 FOR WORK PERFORMED."

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 40,264 hrs · 29,021 cycles

CORROSION FOUND ON FWD SIDE OF FRAME AT FS517, STGR 17L - 18L. (C-CHECK RO 11/10/2023) FS517 FRAME FOUND TO BE OUT OF LIMITS. MATERIAL IS MORE THEN 80% EXFOLIATED. REF CRJ700 SRM 53-31-06-101-002-A01. RECEIVED REO AND PERFORMED REPAIR TO LH FS517 FRAME SEGMENT AT STR18L WITH ALL STEPS OF REO 670-53-31-820 REV-- DATED 2023-10-11 AND REO 670-53-31-822 REV -- DATED 2023-10-16. NO LEAKS NOTED. COMPLIED WITH TASK CARD 51-900-1002-SKY.

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 40,264 hrs · 29,021 cycles

FOUND CORROSION ON LH WEB AT FS 280.00 (C-CHECK RO 11/10/2023) REMOVED AND REPLACED WITH NEW LH LOWER WEB AT FS 280.00 REF. CRJ 700 SRM 53-11-10-201-003-A01. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. SEE CONTINUATION CARD FOR DETAILS.

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 40,264 hrs · 29,021 cycles

FOUND CORROSION ON LH WEB AT FS 280.00 (C-CHECK RO 11/10/2023) REMOVED AND REPLACED WITH NEW LH LOWER WEB AT FS 280.00 REF. CRJ 700 SRM 53-11-10-201-003-A01. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. SEE CONTINUATION CARD FOR DETAILS.

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 40,264 hrs · 29,021 cycles

CORROSION FOUND ON L/H CROSSBEAM AT F.S 280.0 BULKHEAD (C-CHECK RO 11/10/2023) REMOVED AND REPLACED LH FLOOR CROSS BEAM WITH NEW DUE TO OUT OF LIMIT CORROSION REF. CRJ 700 SRM 51-42-06-001-001-A01,CRJ700 SRM 51-42-13-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01,CRJ700 SRM 51-42-22-001-001-A01, AND DWG #CC670-34010 REV. K, SEE CONTINUATION CARD FOR WORK DETAILS, COMPLIED WITH SKYWEST M-337 FORM AND SKYWEST STRUCTURAL MAJOR REPAIR TASK CARD 51-900-1002-SKY.

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 40,264 hrs · 29,021 cycles

CORROSION FOUND ON R/H CROSSBEAM AT F.S 280.0 BULKHEAD (C-CHECK RO 11/10/2023) CORROSION AT R/H CROSSBEAM AT FS 280.0 IS OUT OF LIMITS. REMOVED AND INSTALLED NEW R/H CROSSBEAM AT FS 280.0 REF DWG CC670-34010 REV K, CRJ 700 SRM 51-42-13-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01, CRJ700 SRM 51-42-06-001-001-A01, AND CRJ700 SRM 51-41-00-001-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY.

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 40,264 hrs · 29,021 cycles

*CORROSION NOTED ON FRAME 549 BETWEEN STRG25R-26L(MARKED), MX#27166285 (C-CHECK RO 11/10/2023) BLENDED CORROSION ON FRAME AT FS 549 BETWEEN STGR 25R - STGR 26L REF CRJ700 SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMITS. RECEIVED REO AND PERFORMED REPAIR TO FRAME FS549.00 BETWEEN STR26L TO STR26R IAW ALL STEPS OF REO 670-53-31-818, REV--, DATED 2023-10-05. NO LEAKS NOTED. COMPLIED WITH TASK CARD 51-900-1002-SKY.

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 40,264 hrs · 29,021 cycles

GALLEY SERVICE DOOR I/B MOUNTING ANGLE HAS CORROSION AT THE FWD LATCH FITTING (C-CHECK RO 11/10/2023) REMOVED AND REPLACED GALLEY SERVICE DOOR I/B MOUNTING ANGLE WITH NEW REF. CRJ 700 SRM 51-42-06-001-001-A01 AND DWG #SH670-31950 REV.Y. COMPLIED WITH SKYWEST M-337 FORM AND SKYWEST CARD 51-900-1002-SKY.

Part: UNKNOWN — GOUGED (UNKNOWN) · airframe 40,264 hrs · 29,021 cycles

*FWD BAG BAY THRESHOLD DOUBLER ASSY. GOUGED AT FWD AND AFT HINGE POINTS (MARKED), MX#27166428 (C-CHECK RO 11/10/2023) REMOVED DAMAGE ON FWD BAG BAY THRESHOLD DOUBLER ASSY. (INNER CLOSING SKIN) AT FWD AND AFT HINGE POINTS. REF. CRJ700 SRM 51-12-00-001-001-A01. FOUND TO BE OUT OF LIMITS. REPAIRED AREA IAW ALL STEPS OF REO 670-53-21-814 REV--, DATED 2023-10-10. COMPLIED WITH TASK CARD 51-900-1002-SKY.

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 40,264 hrs · 29,021 cycles

R/H UPPER TRANSCOWL INBD "A" BRACKET STANDOFF CRACKED. (C-CHECK RO 11/10/2023) REMOVED CRACKED STANDOFF, AND INSTALLED 1 EA NEW INBD "A" BRACKET STANDOFF P/N CN624-2082-201 ON R/H UPPER TRANSCOWL REF REO #670-54-21-971 REV (A) 2017-05-11 STEPS 1-3, AND CRJ 700 SRM 51-42-28-001-001-A01. COMPLIED WITH 51-900-1002-SKY.

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 40,264 hrs · 29,021 cycles

*FWD BAG BAY FLOOR SUPPORT PLATE CORRODED BETWEEN STRG23L-22L AND AFT OF FRAME 581 (MARKED),MX#27166412 (C-CHECK RO 11/10/2023) BLENDED CORROSION ON FWD BAGGAGE BAY SUPPORT PLATE BETWEEN STGR 22L - STGR 23L AFT OF FRAME AT FS 581 REF CRJ700 SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMITS REF CRJ700 SRM 53-32-58-101-001-A01. REMOVED AND REPLACED FWD BAGGAGE BAY FLOOR SUPPORT PLATE @ STRG23L-22L FS581 WITH NEW UNIT REF REF CRJ700 SRM 51-42-21-001-001-A01 AND DWG SH670-33600 REV. AD. SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 40,264 hrs · 29,021 cycles

L/H LOWER TRANSCOWL OUTBD "A" BRACKET STANDOFF CRACKED. (C-CHECK RO 11/10/2023) REPLACED CRACKED O/B STAND-OFF ANGLE ("A" BRACKET) P/N CN624-2082-201 ON L/H LOWER TRANSCOWL, REF. REO 670-54-21-971, REV. A, 2017-05-11.C/W SKY CARD 51-900-1002-SKY

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 40,264 hrs · 29,021 cycles

ANGLE FLOOR PANEL SUPPORT AT FS. 280.00 CROSSBEAM HAS CORROSION BETWEEN LBL9 AND RBL9. (C-CHECK RO 11/10/2023) REMOVED AND REPLACED ANGLE FLOOR PANEL SUPPORT AT FS. 280.00 BETWEEN LBL9 AND RBL9 WITH NEW REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG CC670-34010 REV -K, COMPLIED WITH SKYWEST M-337 FOR AND SKYWEST TASK CARD 51-900-1002-SKY, SEE CONTINUATION CARD FOR WORK DETAILS.

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 40,264 hrs · 29,021 cycles

*CORROSION NOTED ON FRAME 565BETWEEN STRG26R-26L(MARKED), MX#27166289 (C-CHECK RO 11/10/2023) BLENDED CORROSION ON FRAME AT FS 565 BETWEEN STGR 26L - STGR 26R REF CRJ700 SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMITS. PERFORMED REPAIR AT LOWER FRAME SECTOR AT FS565 BETWEEN STR26L-STR26R IAW REO 670-53-31-816 REV--, DATED 2023-10-10. NO LEAKS NOTED. COMPLIED WITH TASK CARD 51-900-1002-SKY.

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 40,264 hrs · 29,021 cycles

*FWD BAG BAY SUPPORT PLATE CORRODED BETWEEN STRG22L-23L AND FWD OF FRAME 533 (MARKED), MX#27166390 (C-CHECK RO 11/10/2023) BLENDED CORROSION ON FWD BAGGAGE BAY SUPPORT PLATE BETWEEN STGR 22L - STGR 23L FWD OF FRAME AT FS 533 REF CRJ700 SRM 51-21-06-001-001-A01. FOUND REWORKED AREA IS OUT LIMITS IAW 53-32-58-101-001-A01. REMOVED AND REPLACED WITH NEW BRACKET (SUPPORT PLATE) AT FWD BAG BAY BETWEEN STRG22L-23L AND FWD OF FRAME 533 REF CRJ700 SRM 51-42-21-001-001-A01, CRJ700 SRM 51-45-00-001-001-A01 AND DWG SH670-33390 REV NC. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. SEE CONTINUATION CARD FOR DETAILS.

Part: UNKNOWN — BROKEN (UNKNOWN) · airframe 40,264 hrs · 29,021 cycles

L/H UPPER TRANSCOWL INBD "A" BRACKET STANDOFF BROKEN. (C-CHECK RO 11/10/2023) INSTALLED 1 EA. NEW STAND-OFF P/N 624-2082-201 ON L/H UPPER TRANS COWL REF. REO 670-54-21-971, REV. A, DATED 2017-05-11. COMPLIED WITH STEPS 1-3. COMPLIED WITH SKYCARD 51-900-1002-SKY.

Part: UNKNOWN — WORN (UNKNOWN) · airframe 40,264 hrs · 29,021 cycles

R/H SLAT TRACK 3-1 HAS ABNORMAL WEAR ON UPPER AND LOWER SURFACE (MARKED) (C-CHECK RO 11/10/2023) REMOVED PITTING AT AREAS REF CRJ-700 SRM 51-12-00-001-001-A01. WITHIN LIMITS, REF REO 670-57-42-1440 DATE: 2023-09-22 REV --. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.

Part: UNKNOWN — CHAFED (UNKNOWN) · airframe 40,264 hrs · 29,021 cycles

*R/H SLAT TRACK 1-1 IS CHAFFED AT LOWER/OTBD SIDE AT ATTACHMENT POINT (MARKED), MX#27140153 (C-CHECK RO 11/10/2023) COMPLIED WITH ALL THE STEP OF REO 670-57-42-1437 REV-- DATED 2023-09-18,ENSURED BLEND OUT HAS SMOOTH CONTOUR, ENSURED COMPLETE DAMAGE REMOVAL AND BLEND DEPTH IS NOT GREATER THAN REPORTED.ENSURED REWORKED AREA WAS CRACK FREE, APPLIED FINISH AND MARK SLAT TRACK WITH REO 670-57-42-1437. COMPLIED WITH SKYWEST 51-900-1002-SKY (CL600-2C10)

Part: UNKNOWN — WORN (UNKNOWN) · airframe 40,264 hrs · 29,021 cycles

*R/H SLAT TRACK 1-2 HAS ABNORMAL WEAR ON UPPER AND LOWER SURFACE, MX#27140154 (C-CHECK RO 11/10/2023) REMOVED PITTING AT AREAS REF CRJ-700 SRM 51-12-00-001-001-A01. COMPLIED WITH REO 670-57-42-1026 REV-A DATED 2023-09-22. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 40,264 hrs · 29,021 cycles

FORWARD EQUIPMENT COMPARTMENT RH DOOR LANDING POSSIBLE CRACK AT AFT LATCH CUT-OUT (C-CHECK RO 11/10/2023) REMOVED AND WET INSTALLED NEW RH DOOR LANDING FROM UPPER ELECTRIC BAY ACCESS DOOR FROM FS169 TO FS193 REF CRJ 700 SRM 51-42-06-001-001-A01, DWG NO CC670-33040 REV G AND REO 670-53-11-1885 REV -- DATED 2023-09-15. COMPLIED WITH TASK CARD 51-900-1002-SKY.

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 40,264 hrs · 29,021 cycles

FORWARD EQUIPMENT COMPARTMENT LH DOOR LANDING POSSIBLE CRACK AT AFT LATCH CUT-OUT (C-CHECK RO 11/10/2023) REMOVED L/H SIDE FWD EQUIPMENT COMPARTMENT DOOR LANDING REF CRJ 700 SRM 51-42-06-001-001-A01 AND WET INSTALLED NEW L/H SIDE FWD EQUIPMENT COMPARTMENT DOOR LANDING REF CRJ 700 SRM 51-42-06-001-001-A01, DWG NO CC670-33040 REV -G AND REO 670-53-11-1884 REV -- DATED 2023-09-15. SEE CONTINUATION CARD FOR DETAILS.COMPLIED WITH 51-900-1002-SKY

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 40,264 hrs · 29,021 cycles

VERTICAL STABILIZER TO FUSELAGE ATTACHMENT LH FORWARD DRAG ANGLE DOUBLER POSSIBLE CRACK (C-CHECK RO 11/10/2023) REMOVED, FABRICATED AND REPLACED WITH NEW LH FWD DRAG ANGLE AT FUSELAGE TO VERT STAB ATTACHMENT REF CRJ700 SRM 55-31-00-201-001-A01 AND ALL STEPS OF REO 670-55-31-018 REV -A DATED 2016-11-10. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 40,264 hrs · 29,021 cycles

VERTICAL STABILIZER TO FUSELAGE ATTACHMENT RH FORWARD DRAG ANGLE POSSIBLE CRACK (C-CHECK RO 11/10/2023) REMOVED, FABRICATED AND REPLACED WITH NEW RH FWD DRAG ANGLE AT FUSELAGE TO VERT STAB ATTACHMENT REF REO 670-55-31-018 REV -A DATED 2016-11-10. COMPLIED WITH ALL STEPS OF REO 670-55-31-018 REV -A DATED 2016-11-10. COMPLIED WITH 51-900-1002-SKY

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 40,264 hrs · 29,021 cycles

VERTICAL STABILIZER TO FUSELAGE ATTACHMENT RH AFT DRAG ANGLE POSSIBLE CRACK (C-CHECK RO 11/10/2023) REMOVED, FABRICATED AND REPLACED WITH NEW RH AFT DRAG ANGLE AT FUSELAGE TO VERT STAB ATTACHMENT REF REO 670-55-31-018 REV -A DATED 2016-11-10. COMPLIED WITH ALL STEPS OF REO 670-55-31-018 REV -A DATED 2016-11-10. COMPLIED WITH 51-900-1002-SKY.

Part: SKIN — DENTED (BS 501 S19-20L) · airframe 36,517 hrs · 26,177 cycles

FOUND DENT ON LH EXTERNAL SKIN AT FS501.00 BETWEEN STGR 19L AND STGR 20L. (C-CHECK RO 4/22/2021) COMPLIED WITH DENT REPAIR AT LH EXTERNAL SKIN FS501.00 BETWEEN STGR 19L AND STGR 20L REF-CRJ-700 REO 670-53-31-629 REV -- DATED 2021-04-08 & REO 670-51-00-085 REV A DATED 2017-08-23 LEAK CHECK GOOD. / COMPLIED WITH TASK 51-900-1002-SKY.

Part: DOUBLER — CHAFED (FUSELAGE) · airframe 36,517 hrs · 26,177 cycles

LH PYLON HYDRAULIC EDP PRESSURE LINE FIREWALL FITTING IS LOOSE AND CHAFING ON DOUBLER AND RIVETS. (C-CHECK RO 4/22/2021) REMOVED AND REPLACED WEB AND DOUBLER AT LH PYLON FIREWALL REF-CRJ-700 SRM 51-42-06-001-001 A01 AND DWG MM670-37001 REV AB. / COMPLIED WITH TASK 51-900-1002-SKY

Part: FRAME — CORRODED (BS 319.7 S18-21L) · airframe 36,517 hrs · 26,177 cycles

F.S.319.70 FRAME SECTION FROM STGR18LTO STGR21L IS CORRODED. (C-CHECK RO 4/22/2021) REMOVED AND INSTALLED NEW FRAME SECTION FS319.70 FROM STGR18L TO STGR21L REF-CRJ-700 SRM 51-42-06-001-001 A01, SRM 51-42-21-001-001 A01 AND DWG SH670-31810 REV Y. LEAK CHECK GOOD. / COMPLIED WITH TASK 51-900-1002-SKY

Part: FRAME — CORRODED (BS 856 RBL9) · airframe 36,517 hrs · 26,177 cycles

RBL 9 BETWEEN F.S. 856.00 (SECTION AFT OF JOINT) AND F.S. 879.00 IS CORRODED BEYOND LIMITS AND REQUIRES REPAIR. (C-CHECK RO 4/22/2021) COMPLIED WITH RBL9 FLOOR BEAM FLANGE REPAIR BETWEEN FS863.00-FS879.00 REF-CRJ-700 SRM 53-00-41-201-001 A01 AND COMPLIED WITH REO 670-53-51-209 REV -- DATED 2021-03-24 AT RBL9 FS856 APPROX WITH THE BLEND OUT AREA IS WITHIN LIMITS. / COMPLIED WITH TASK 51-900-1002-SKY

Part: STRIKER — DAMAGED (PAX DOOR) · airframe 36,517 hrs · 26,177 cycles

PAX DOOR LWR SEAL STRIKER'S FWD HOLE IS EXTREMELY ELONGATED. (C-CHECK RO 4/22/2021) REMOVED DAMAGED PAX DOOR LOWER SEAL STRIKER AND INSTALLED NEW PAX DOOR LOWER SEAL STRIKER P/N:SH670-31886-3S REF CRJ700 SRM 51-42-21-001-001-A01 AND DRAWING SH670-31810 REV Y COMPLIED WITH 51-900-1002-SKY

Part: STRINGER — DAMAGED (BS 1051 S19L) · airframe 36,517 hrs · 26,177 cycles

STGR 19L AT F.S. 1051 HAS A MISSDRILLED HOLE AT STGR CLIP LOCATION. (C-CHECK RO 4/22/2021) REMOVED AND REPLACED DAMAGED SECTION OF STRINGER 19L FROM FS977 TO FS1060 IAW CRJ700 SRM 53-00-03-201-001-A01 FIGURE 53-00-03-991-805 AND CRJ700 SRM 51-42-21-001-001-A01. STRINGER P/N MM670-35118-003S PO T59029. C/W TASK CARD 51-900-1002-SKY. COMPLIED WITH ALL STEPS OF REO 670-53-61-1861 REV-- DATED 2021-03-26. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.

Part: FORMER — CORRODED (BS 311.75) · airframe 36,517 hrs · 26,177 cycles

DURING OF REMOVAL OF INNER SKIN FOUND FWD FORMER FS 311.75 PN 601R318024-3 IS CORRODED AT UPPER TENSION ROD CUT OUT. (C-CHECK RO 4/22/2021) REMOVED AND INSTALLED NEW PAX DOOR FWD FORMER FS311.75 REF-CRJ-700 SRM 51-42-06-001-001 A01 AND DWG 601R318031 REV A,LEAK CHEK GOOD. / COMPLIED WITH TASK 51-900-1002-SKY

Part: STOP — WORN (CARGO DOOR TRACK) · airframe 36,517 hrs · 26,177 cycles

AFT BAGGAGE BAY DOOR TRACK STOPS WORN BEYOND LIMITS (C-CHECK RO 4/22/2021) ORDERED AND RECEIVED 4 NEW AFT BAGGAGE DOOR TRACK STOPS. INSTALLED ON JOB 71008165 OP 53 CAMP 22340237

Part: BEAM — CORRODED (BS 863-879) · airframe 36,517 hrs · 26,177 cycles

CORROSION FOUND ON LBL9 BEAM IN THE PAD UP AREA BETWEEN F.S. 863 AND F.S. 879. (C-CHECK RO 4/22/2021) REPAIRED DAMAGED LBL9 BEAM LOCATED BETWEEN FS863 & FS879 IAW CRJ 700 SRM 53-00-41-201-001-A01 & DWG SH670-37383 REV C, COMPLIED WITH TASK CARD 51-900-1002-SKY, COMPLIED WITH 337 FORM

Part: SLAT TRACK — CORRODED (RT WING SLAT) · airframe 36,517 hrs · 26,177 cycles

* RH SLAT TRACK 1-1 HAS WEAR MARKS AND IS CORRODED (C-CHECK RO 4/22/2021) AFTER BLENDED AREAS RH SLAT TRACK 1-1 ARE FOUND WITHIN TOLERANCE LIMITS REF-CRJ-700 REO 670-57-42-1025 REV -- DATED 2021-03-09, OPS/CHECK GOOD. SEE CONTINUATION CARD FOR DETAILS. / COMPLIED WITH TASK 51-900-1002-SKY.

Part: SLAT TRACK — CORRODED (LT WING SLAT) · airframe 36,517 hrs · 26,177 cycles

LH SLAT TRACK 3-2 CORRODED (C-CHECK RO 4/22/2021) COMPLIED WITH REO 670-57-42-1024REV-- DATED2021-03-08 AND CARD 51-900-1002-SKY OPS CHECK GOOD AT THIS TIME

Part: HINGE — GOUGED (PAX DOOR) · airframe 36,517 hrs · 26,177 cycles

THE PASSENGER DOOR HINGE HALF, DOOR SIDE, HAS CRATCHES/GOUGES ON ALL LUGS, AND AN ELONGATED SLOTTED TUBULAR SPRING PIN HOLE ON ITS AFT LUG. (C-CHECK RO 4/22/2021) REMOVED DAMAGE AS REQUIRED FROM THE OUTER SURFACE OF EACH LUG ON THE PASSENGER DOOR SIDE DOOR HINGE. REF CRJ-700 SRM 52-11-01-201-007-A01 TYPE 1 DISPOSITION AND REO 670-52-11-511 REV E DATED 2017-08-02 TYPE 1 DISPOSTION. WITHIN LIMITS. RESTORED FINISH. COMPLIED WITH 51-900-1002-SKY

Part: HINGE — GOUGED (PAX DOOR) · airframe 36,517 hrs · 26,177 cycles

THE PASSENGER DOOR HINGE HALF, FUSELAGE SIDE, HAS SCRATCHES/GOUGES ON ALL LUG LANDS, AND THE FWD 5 LUGS HAVE SCRATCHES/GOUGES. (C-CHECK RO 4/22/2021) REMOVED AND INSTALLED NEW PAX DOOR FUSELAGE HINGE REF-CRJ-700 SRM 53-21-23-201-007 A01 AND DWG SH670-31810 REV AE, LEAK CHECK GOOD. / COMPLIED WITH TASK 51-900-1002-SKY

Part: SLAT TRACK — CORRODED (RT WING SLAT) · airframe 36,517 hrs · 26,177 cycles

RH SLAT TRACK 2-2 CORRODED (C-CHECK RO 4/22/2021) REMOVED CORROSION ON RH SLAT TRACK 2-2 AND COMPLIED WITH THE TEMPORARY DISPOSITION OF REF REO 670-57-42-1031 REV -- DATED 2021-03-11 AND COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. / REINSPECTION REQUIRED OF REPAIR AREA AT INTERVALS NOT TO EXCEED 1000 FLIGHT HOURS.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 36,517 hrs · 26,177 cycles

* LH INBD FLAP LOWER SKIN HAS 2 DENTS (MARKED) (C-CHECK RO 4/22/2021) NDT DENTS DEFECT FREE. EVAL INBD DENT IS WITHIN LIMITS. EVAL OTBD DENT IS OUT OF LIMITS. RECEIVED ENGINEERING DISPOSITION TO REPAIR SKIN FOR LH I/B FLAP LWR SKIN. REPAIRED DAMAGE PER CRJ700 SRM 57-52-01-201-005-A01 AND DWG CC670-14050 REV-M. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED. / COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY (CL600-2C10) STUCTURAL MAJOR REPAIR (**RII**)

Part: SLAT TRACK — CORRODED (LT WING SLAT) · airframe 36,517 hrs · 26,177 cycles

LH SLAT TRACK 2-2 CORRODED (C-CHECK RO 4/22/2021) AFTER BLENDED AREAS LH SLAT TRACK 2-2 ARE FOUND WITHIN TOLERANCE LIMITS REF-CRJ-700 REO 670-57-42-1023 REV -- DATED 2021-03-08, OPS/CHECK GOOD. SEE CONTINUATION CARD FOR DETAILS. / COMPLIED WITH TASK 51-900-1002-SKY.

Part: SLAT TRACK — CORRODED (LT WING SLAT) · airframe 36,517 hrs · 26,177 cycles

LH SLAT TRACK 1-2 CORRODED (C-CHECK RO 4/22/2021) AFTER BLENDED AREAS LH SLAT TRACK 1-2 ARE FOUND WITHIN TOLERANCE LIMITS REF-CRJ-700 REO 670-57-42-1022 REV -- DATED 2021-03-08, OPS/CHECK GOOD. SEE CONTINUATION CARD FOR DETAILS. / COMPLIED WITH TASK 51-900-1002-SKY.

Part: SLAT TRACK — CORRODED (RT WING SLAT) · airframe 36,517 hrs · 26,177 cycles

RH SLAT TRACK 3-2 CORRODED (C-CHECK RO 4/22/2021) COMPLIED WITH REO 670-57-42-1028 REV -- DATED 2021-03-09 AND CARD 51-900-1002-SKY

Part: SLAT TRACK — CORRODED (RT WING SLAT) · airframe 36,517 hrs · 26,177 cycles

* RH SLAT TRACK 1-2 CORRODED (C-CHECK RO 4/22/2021) AFTER BLENDED AREAS RH SLAT TRACK 1-2 ARE FOUND WITHIN TOLERANCE LIMITS REF-CRJ-700 REO 670-57-42-1026 REV -- DATED 2021-03-09, OPS/CHECK GOOD. SEE CONTINUATION CARD FOR DETAILS. / COMPLIED WITH TASK 51-900-1002-SKY.

Part: SEAT TRACK — CORRODED (BS 579-677) · airframe 36,517 hrs · 26,177 cycles

* THE PASSENGER CABIN SEAT RAIL ON LBL 9 HAS MULTIPLE SPOTS OF CORROSION, CHAFES, SCRATCHES AND/OR GOUGES BETWEEN APPROX. FS 579 AND APPROX. FS 677. (C-CHECK RO 4/22/2021) REPLACED SEAT TRACK LOCATED AT LBL 9.0 FROM FS579-FS677 WITH FABRICATED REF CRJ-700 AMM 53-00-49-400-801-A17

Part: FLOOR SUPPORT — CORRODED (BS 280-319) · airframe 36,517 hrs · 26,177 cycles

* THE RH FLOOR SILL BETWEEN FS 280 AND FS 319 HAS CORROSION IN MULTIPLE SPOTS. (C-CHECK RO 4/22/2021) REPLACED RH FLOOR SILL FROM FS280.00-FS319.70 WITH NEW REF CRJ-700 SRM 51-42-06-001-001-A01, CRJ-700 SRM 51-42-21-001-001-A01 CRJ-700 SRM 51-42-13-001-001-A01 DRAWING SH670-32170 REV V COMPLIED WITH 51-900-1002-SKY. ALL CHECKS GOOD. SEE CONTINUE CARD FOR DETAILS.

Part: SEAT TRACK — CORRODED (BS 501-565 LBL9) · airframe 36,517 hrs · 26,177 cycles

THE PASSENGER CABIN SEAT RAIL ON LBL 9 HAS MULTIPLE SPOTS OF CORROSION, CHAFES, SCRATCHES AND/OR GOUGES BETWEEN APPROX. FS 501 AND APPROX. FS 565. (C-CHECK RO 4/22/2021) REPLACED FABRICATED NEW SEAT RAIL REF CRJ700 AMM TASK 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 694-469 LBL9) · airframe 36,517 hrs · 26,177 cycles

THE PASSENGER CABIN SEAT RAIL ON LBL 9 HAS MULTIPLE SPOTS OF CORROSION, CHAFES, SCRATCHES AND/OR GOUGES BETWEEN APPROX. FS 394 AND APPROX. FS 469. (C-CHECK RO 4/22/2021) FABRICATED AND INSTALLED NEW LBL9 SEAT TRACK P/N SH670-32249-1 FROM FS394 TO FS469 USING EXTRUSION 20276-288-0-0A, PO# T58082, REF CRJ-700 SRM 53-00-49-201-002-A01 AND CRJ-700 AMM 53-00-49-400-801-A04

Part: SEAT TRACK — CORRODED (BS 579-677) · airframe 36,517 hrs · 26,177 cycles

THE PASSENGER CABIN SEAT RAIL ON LBL 27 HAS MULTIPLE SPOTS OF CORROSION, CHAFES, SCRATCHES AND/OR GOUGES BETWEEN APPROX. FS 579 AND APPROX. FS 677. (C-CHECK RO 4/22/2021) REPLACED WITH FABRICATED. PASSENGER CABIN SEAT RAIL LOCATED AT LBL 27.0 FROM FS579-FS677. REF CRJ-700 AMM 53-00-49-400-801-A17.

Part: STRINGER — CORRODED (BS 295-310 S22L) · airframe 36,517 hrs · 26,177 cycles

IN THE AVIONICS BAY STRINGER 22L HAS CORROSION AROUND FASTENERS BETWEEN FS 295 AND FS 310. (C-CHECK RO 4/22/2021) REMOVED AND INSTALLED NEW STRINGER 22L IN THE AVIONICS BAY BETWEEN FS295 AND FS310 REF-CRJ-700 SRM 51-42-06-001-001 A01 AND SRM 51-42-21-001-001 A01 LEAK CHECK GOOD. SE CONTINUATION CARD FOR DETAILS. / COMPLIED WITH TASK 51-900-1002-SKY

Part: SEAT TRACK — CORRODED (BS 501-565 LBL27) · airframe 36,517 hrs · 26,177 cycles

* THE PASSENGER CABIN SEAT RAIL ON LBL 27 HAS MULTIPLE SPOTS OF CORROSION, CHAFES, SCRATCHES AND/OR GOUGES BETWEEN APPROX. FS 501 AND APPROX. FS 565. (C-CHECK RO 4/22/2021) INSTALLED NEW SEAT RAIL REF CRJ700 AMM 53-00-49-400-801 (CONFIG A03) SEE CONTINUATION CARD FOR MORE INFO.

Part: SEAT TRACK — CORRODED (BS 394-469 LBL27) · airframe 36,517 hrs · 26,177 cycles

THE PASSENGER CABIN SEAT RAIL ON LBL 27 HAS MULTIPLE SPOTS OF CORROSION, CHAFES, SCRATCHES AND/OR GOUGES BETWEEN APPROX. FS 394 AND APPROX. FS 469. (C-CHECK RO 4/22/2021) REPLACED SEAT TRACK FROM FS394-FS485 LBL 27 WITH NEW REF CRJ-700 AMM 53-00-49-400-801-A17.

Part: SEAT TRACK — CORRODED (BS 501-565) · airframe 36,517 hrs · 26,177 cycles

THE PASSENGER CABIN SEAT RAIL ON RBL 9 HAS MULTIPLE SPOTS OF CORROSION, CHAFES, SCRATCHES AND/OR GOUGES BETWEEN APPROX. FS 501 AND APPROX. FS 565. (C-CHECK RO 4/22/2021) FABRICATED AND INSTALLED NEW SEAT RAIL RBL9 P/N SH670-33426-1 USING EXTRUSION 20276-288-0-0A PO# T58082 FROM FS501 BETWEEN APPROX. FS 501 AND APPROX FS 565 REF CRJ-700 SRM 53-00-49-201-002-A01 AND CRJ-700 AMM 53-00-400-49-801-A03

Part: SEAT TRACK — CORRODED (BS 579-677) · airframe 36,517 hrs · 26,177 cycles

* THE PASSENGER CABIN SEAT RAIL ON RBL 9 HAS MULTIPLE SPOTS OF CORROSION, CHAFES, SCRATCHES AND/OR GOUGES BETWEEN APPROX. FS 579 AND APPROX. FS 677. (C-CHECK RO 4/22/2021) FABRICATED AND INSALLED NEW RBL9 SEAT RAIL, P/N SH670-33425-3, FROM FS579 TO 677 USING EXTRUSION 20276-288-0-0A, PO # T58082, REF CRJ-700 SRM 53-00-49-201-002-A01 AND CRJ-700 AMM 53-00-49-400-801-A03.

Part: FRAME — CORRODED (BS 319.7 S26-27L) · airframe 36,517 hrs · 26,177 cycles

FUSELAGE FRAME 319.70 HAS CORROSION ON ITS LOWER FLANGE BETWEEN STGR 26L AND 27 AND ADDITIONAL CORROSION NOTED AROUNS STGR 21L. (C-CHECK RO 4/22/2021) REMOVED AND REPLACED FUSELAGE FRAME FS319.70 REF- DWG SH670-31630 REV K, CRJ-700 SRM 51-42-06-001-001 A01 AND SRM 51-42-21-001-001 A01,SEE CONTINUATION CARD FOR DETAILS. LEAK CHECK GOOD. / COMPLIED WITH TASK 51-900-1002-SKY

Part: DOOR FRAME — CORRODED (PAX DOORWAY) · airframe 36,517 hrs · 26,177 cycles

THE PASSENGER DOOR SURROUND STRUCTURE'S SILL BACKUP, MOUNTED TO STRINGER 21L, BETWEEN FS 310 AND FS 333 HAS LARGE AMOUNTS OF CORROSION. (C-CHECK RO 4/22/2021) PAX DOOR SURROUND STRUCTURE BACKUP SILL PN: SH670-31822-1, COMMON TO STRG21L LOCATED BETWEEN FS310 & FS333 IS OUT OF LIMITS OF CRJ700 SRM 53-00-00-101-001-A01, REPLACED IAW CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42--21-001-001-A01, & DWG SH670-31810 REV Y, COMPLIED WITH TASK CARD 51-900-1002-SKY,

Part: STRINGER — CORRODED (BS 437-453 S19R) · airframe 36,517 hrs · 26,177 cycles

STRINGER 19R HAS MULTIPLE SPOTS OF CORROSION BETWEEN FS 437 AND FS 453. (C-CHECK RO 4/22/2021) REPAIRED STRINGER 19R REF-CRJ-700 SRM 53-00-03-201-001 A01 AND SRM 51-42-21-001-001 A01.LEAK CHECK GOOD. / COMPLIED WITH TASK 51-900-1002-SKY

Part: SEAT TRACK — CORRODED (BS 394-469 RBL9) · airframe 36,517 hrs · 26,177 cycles

* THE PASSENGER CABIN SEAT RAIL ON RBL 9 HAS MULTIPLE SPOTS OF CORROSION, CHAFES, SCRATCHES AND/OR GOUGES BETWEEN APPROX. FS 394 AND APPROX. FS 469. (C-CHECK RO 4/22/2021) INSTALLED NEW SEAT RAIL AT RBL 9.0 FROM FS394.00-FS469.00 P/N SH670-32159-1 REF CRJ-700 AMM 53-00-49-400-801-A03

Part: SEAT TRACK — CORRODED (BS 868.5-960.5) · airframe 36,517 hrs · 26,177 cycles

CORROSION DETECTED ON (L/H) SEAT TRACK SECTION THAT SPANS FROM F.S. 868.5 TO F.S 960.5, IN NUMEROUS LOCATIONS (MARKED). (C-CHECK RO 4/22/2021) INSTALLED NEW SEAT TRACK REF CRJ700 AMM 53-00-49-400-801 (CONFIG A03) SEE CONTINUATION CARD FOR MORE INFO.

Part: SEAT TRACK — CORRODED (BS 960-988) · airframe 36,517 hrs · 26,177 cycles

CORROSION DETECTED ON (L/H) SEAT SIDE TRACK , SMALL SECTION THAT SPANS FROM F.S. 960.5 TO F.S 988.5, IN NUMEROUS LOCATIONS (MARKED). (C-CHECK RO 4/22/2021) INSTALLED NEWLH SIDE SEAT TRACK FS960.5 TOFS988.5 REF CRJ700 AMM 53-00-49-400-801 (CONFIG A03) SEE CONTINUATION CARD FOR MORE INFO.

Part: SEAT TRACK — CORRODED (BS 868.5-960.5) · airframe 36,517 hrs · 26,177 cycles

CORROSION DETECTED ON (R/H) SEAT SIDE TRACK SECTION THAT SPANS FROM F.S.868.5 TO F.S. 960.5, IN NUMEROUS LOCATIONS (MARKED). (C-CHECK RO 4/22/2021) FABRICATED Y INSTALLED NEW RH SIDE SEAT TRACK P/N SH670-37543-3 FROM FS868.5 TO FS960.5 USING EXTRUCION 20276-288-0-0A, PO# T58082 REF CRJ-700 SRM 53-00-49-201-002-A01 AND 51-41-02-001-001-A01

Part: ATTACH ANGLE — CORRODED (BS 1051 S19L) · airframe 36,517 hrs · 26,177 cycles

CORROSION ON ANGLE ATTACHED TO STGR 19L AND FRAME FS 1051.00 (C-CHECK RO 4/22/2021) REMOVED AND REPLACED ANGLE, FS1051, STGR19L, ,REO 670-53-61-1861 REV--,2021-03-26 DWG MM670-36025 REV B,DWG MM670-36080 REV G,DWG MM670-36483 REV E, CRJ 700 SRM 51-42-21-001-001-A01, / COMPLIED WITH 51-900-1002-SKY

Part: MOUNT — CORRODED (WING TO BODY) · airframe 36,517 hrs · 26,177 cycles

EVIDENCE OF CORROSION FOUND AROUND NUTPLATE HOLES OF FWD WING TO FUSELAGE FAIRING MOUNTING JOINT STRAP (MARKED). (C-CHECK RO 4/22/2021) LOCATED, DRILLED AND INSTALLED NEW "T" SUPPORT PN: SH670-39063-1. REF CRJ 700 SRM 51-42-06-001-001-A01, 51-40-06-001-001-A01, 51-45-00-001-001-A01

Part: ATTACH FITTING — CORRODED (FAIRING) · airframe 36,517 hrs · 26,177 cycles

EVIDENCE OF CORROSION AROUND MULTIPLE NUTPLATE HOLES UNDER FAIRING 191AB ON PANEL ATTACH FRAME. (C-CHECK RO 4/22/2021) REMOVED CORROSION FROM FROM PLATE JOINT SPLICE ATTACHED TO FRAME PER CRJ 700 SRM 51-21-06-001-001-A01, FOUND TO BE OUT OF LIMITS PER CRJ 700 SRM 53-82-55-101-001-A01, REMOVED AND REPLACED PLACE SPLICE JOINT PN SH670-39054-3 PO# T-58783, PER CRJ 700 SRM 51-42-06-001-001-A01, SRM 51-42-10-001-001-A01 AND DWG SH670-39050 REV G , RESTORE FINISH PER TR51-0068 SRM 51-21-16-001-001-A01.

Part: SKIN — CORRODED (BS 939-977 S27) · airframe 36,517 hrs · 26,177 cycles

* SURFACE CORROSION DETECTED, LWR/EXTERNAL BELLY SKIN, AROUND FASTENER HEADS IN STGR (27) BETWEEN F.S. 939.00 AND F.S. 977.00 JOINT STRAP (APROX (20) FASTENERS) MARKED. (C-CHECK RO 4/22/2021) REMOVED SURFACE CORROSION ON LWR/EXTERNAL BELLY SKIN, AROUND FASTENER HEADS ON STGR 27 BETWEEN F.S. 939.00 AND F.S. 977.00 JOINT STRAP REF. CRJ 700 SRM 51-21-06-001-001-A01 AND COMPLIED WITH ALL STEPS OF REO 670-53-51-206 REV -- DATE: 2021-03-06. / COMPLIED WITH TASK 51-900-1002-SKY

Part: SKIN — CHAFED (BS 977) · airframe 36,517 hrs · 26,177 cycles

CHAFED AREA FOUND, LWR/EXTERNAL BELLY SKIN, (BEGINING) APROX 2" AFT OF F.S. 977.00 JOINT STRAP LINE, AND EXTENDING AFT FOR APROX 2.5", L/H SIDE OF STGR (27) ATTACHMENT FASTENERS (MARKED). (C-CHECK RO 4/22/2021) BLENDED DAMAGE ON LWR EXTERNAL BELLY SKIN AT APPROX FS 977.00. REF CRJ700 SRM 53-00-01-101-001-A01. NDT DEFECT FREE. EVAL OF DAMAGE IS OUT OF LIMITS. REF CRJ 700 SRM 53-61-01-001-003-A01 AND REO 670-53-00-290 REV-D DATED 2015-09-10. RECEIVED COMPLIED WITH ALL STEPS OF REPAIR REO 670-53-00-290 REV-F DATED 2019-04-26. LEAK CHECK GOOD. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED. / COMPLIED WITH SKY CARD 51-900-1002-SKY

Part: CARGO TRACK — CORRODED (BS 453-560) · airframe 36,517 hrs · 26,177 cycles

FWD CARGO R/H FWD #3 BAGGAGE RETRIEVAL FLOOR TRACK F/S 453-560 (APPROXIMATELY) HAS CORROSION PITTING. (C-CHECK RO 4/22/2021) FABRICATED NEW PART WITH P/N DSY7058-3 AND REPLACED AT FWD CARGO RH # 3 BAGGAGE RETRIEVAL FLOOR TRACK FS453-560 REF-CRJ-700 DWG DSY7058 REV --.

Part: CARGO TRACK — CORRODED (BS 453-560) · airframe 36,517 hrs · 26,177 cycles

FWD CARGO R/H #4 BAGGAGE RETRIEVAL FLOOR TRACK F/S 453-560 (APPROXIMATELY) HAS CORROSION PITTING. (C-CHECK RO 4/22/2021) FABRICATED NEW PART WITH P/N DSY7058-3 AND REPLACED AT FWD CARGO RH # 4 BAGGAGE RETRIEVAL FLOOR TRACK FS453-560 REF-CRJ-700 DWG DSY7058 REV --

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 34,377 hrs · 24,498 cycles

DURING MX CHECK, THE EPSU NR 2 FAILED AN OPS CHECK. MX REMOVED AND REPLACED THE NR 2 EPSU BATTERY, OPS CHECKED GOOD. ACFT APPROVED FOR RETURN TO SERVICE.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 33,990 hrs · 24,207 cycles

RBL 30 STIFFENER ON FORWARD SIDE OF FS 202 BULKHEAD HAS AN INDICATION NOTED AT THE TOP .200 INCHES LONG. FAILED NDT INSPECTION. REPAIRED RBL 30 STIFFENER IAW SRM 53-11-10-201-005.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 33,048 hrs · 23,485 cycles

RT FLOOR SILL CORRODED AT RBL 46 & FS 283.00. REMOVED AND REPLACED FLOORSILL AT FS 283.00 ON RBL 46 IAW SRM 51-42-06-001-001-A01, 51-42-10-001-001-A01 AND SH670-32170-S019.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 33,048 hrs · 23,485 cycles

INTERCOSTAL AT STR 27R BTW FS 280.00-268.00 CORRODED. COMPLIED WITH EC/TC EA 25-2016-338 AND EA 25-2016-338, REPAIR TO FORWARD JACK FITTING RT FS 268.00-280.00.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,048 hrs · 23,485 cycles

LBL9 FLOORBEAM CORRODED BETWEEN FS 578-680.5. FLOORBEAM LBL9 BETWEEN FS 571.50-685.50 REQUIRES REPLACEMENT, CORROSION BEYOND REPAIR. MULTIPLE HEAVY DEEP PITTING. REMOVED FLOORBEAM IAW SRM 53-31-43-101-001-A02 COMPLIED WITH EC/TC REO 670-53-00-486 REV A DATED 01/06/2017. COMPLIED WITH SNEO 670-34081-501. COMPLIED WITH SPECIFIC EO 700-53-0389.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,048 hrs · 23,485 cycles

LBL27 FLOORBEAM CORRODED BETWEEN FS 1015-1031. CUT LBL27 FLOORBEAM AT FS 1037 AND REMOVED UP TO FACTORY SPLICE AT 977.00 PER REO 670-83-00-029 & SUPPLEMENT 53-00-41. FABRICATED REPAIR PARTS AND PRIMED IAW SRM SUPPLEMENT 53-00-41. PERFORMED EDDY CURRENT INSPECTION OF FLOORBEAM CUT LINE IAW NDTM PT 1 51-20-06-250-A01. NO INDICATIONS NOTED AT THIS TIME. INSTALLED NEW SERVICEABLE FLOORBEAM FS 977.00-1037.00 IAW SRM 53-00-41-201-001-A01. REPAIRED FLOORBEAM IAW EC/TC EO 700-53-10-00004.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,048 hrs · 23,485 cycles

LBL9 FLOORBEAM CORRODED BETWEEN FS 1015-1031. CUT AND FABRICATED REPAIR PARTS IAW SRM SUPPLEMENT 53-00-41. PERFORMED EDDY CURRENT OF FLOORBEAM CUT EDGES IAW NDTM PT 1 51-20-06-250-A01. NO INDICATIONS NOTED AT THIS TIME. INSTALLED REPAIRED PARTS IAW SRM SUPPLEMENT 53-00-41 & REO 670-53-61-1317. APPLIED CIC TO FLOORBEAM AT LBL9 FS 977-1037 IAW SRM 51-21-11-001-001-A01. REPAIRED FLOORBEAM IAW EC/TC EO 700-53-10-00003.

Part: FLOOR SUPPORT — CORRODED (BS 485-571) · airframe 33,048 hrs · 23,485 cycles

LBL 9 FLOOR SUPPORT CORRODED BETWEEN BS 485 & 571. THE FLOOR SUPPORT IS BEYOND LIMITS IAW SRM 53-31-43-101-001-A02. REMOVED AND REPLACED THE FLOOR SUPPORT IAW EC/TC REO 670-53-00-486.

Part: MOUNT — CORRODED (BS 581) · airframe 20,410 hrs · 14,072 cycles

DURING C CHECK, FOUND CARGO NET ANCHOR MOUNTING PAD AT BS 581 & STRINGER 24 HAS CORROSION DAMAGE. REMOVED AND REPLACED CARGO NET ANCHOR PAD IAW SRM 51-42-21-001-001-A01, & 51-40-11-001-001-A01.

Part: HINGE BRACKET — BENT (CARGO DOOR) · airframe 20,410 hrs · 14,072 cycles

DURING C CHECK, FOUND FWD CARGO DOOR FWD HINGE PANEL ATTACHMENT BRACKET BENT. REPAIRED IAW EC/TC EA 26-2017-003, & EA 26-2017-003.

Part: FLOOR SUPPORT — CORRODED (BS 977-1037) · airframe 33,048 hrs · 23,485 cycles

DURING C CHECK, FOUND RBL 9 FLOOR SUPPORT HAS 3 SPOTS OF CORROSION AT BS 1015, 1020, 1033. REMOVED AND REPLACED THE FLOOR SUPPORT IAW EC/TC REO 670-53-61-1314, & EC/TC EO700-53-10-00001.

Part: SEAT TRACK — CORRODED (BS 830-1003) · airframe 20,410 hrs · 14,072 cycles

DURING C CHECK, FOUND THE SEAT TRACK CORRODED AT BS 830.4 - 1003, LBL 9. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A17 & 53-00-49-400-801-A17.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,048 hrs · 23,485 cycles

FLOORBEAM CORRODED AT FS 517.0 RBL9. INSPECTED AND FOUND NO DAMAGE ALLOWED ON THE FLOOR SUPPORT STRUCTURE. REMOVED AND REPLACED FLOORBEAM AT FS 517.0 RBL9, COMPLIED WITH GREO 670-53-00-029 REV A, REO 670-53-00-486 AND EC/TC EO 700-53-0391. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 33,048 hrs · 23,485 cycles

SEAT TRACK SEGMENT CORRODED BS 485-581, RBL 9. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A17, 53-00-49-400-801-A17, REO 670-53-00-343 REV M, AND EC/TC REO 670-53-00-343.

Part: SEAT TRACK — CORRODED (BS 684-830) · airframe 33,048 hrs · 23,485 cycles

CORROSION FOUND ON SEAT TRACK BS 684.0-830.4, RBL 9. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A17, 53-00-49-400-801-A17, REO 670-53-00-343 REV M AND EC/TC REO 670-53-00-343.

Part: SEAT TRACK — CORRODED (BS 830-973) · airframe 33,048 hrs · 23,485 cycles

SEAT TRACK CORRODED BS 830.40-973, RBL 9. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A17, 53-00-49-400-801-A17, REO 670-53-00-343 REV M, AND EC/TC REO 670-53-00-343.

Part: SEAT TRACK — CORRODED (BS 581-684) · airframe 33,048 hrs · 23,485 cycles

SEAT TRACK CORRODED BS 581-684, LBL 9. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A17, 53-00-49-400-801-A17, REO 670-53-00-343 REV M , AND EC/TC REO 670-53-00-343.

Part: SEAT TRACK — CORRODED (BS 581-684) · airframe 33,048 hrs · 23,485 cycles

SEAT TRACK CORRODED AT BS 581-684, RBL 9. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A17, 53-00-49-400-801-A17, REO 670-53-00-343 REV M, AND EC/TC REO 670-53-00-343.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 33,048 hrs · 23,485 cycles

SEAT TRACK SEGMENT CORRODED BS 485-581, LBL 9. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A17, 53-00-49-400-801-A17, REO 670-53-00-343 REV M, AND EC/TC REO 670-53-00-343.

Part: FLOOR SUPPORT — CORRODED (BS 549) · airframe 33,048 hrs · 23,485 cycles

LEFT FLOOR SUPPORT CORRODED BS 549 LBL 46. - REMOVED CORROSION, REPLACED RIVETS AND COMPLIED WITH NDT IAW EC/TC REO 670-53-00-390 AND REO 670-53-00-390 REV.

Part: SEAT TRACK — CORRODED (BS 683-836) · airframe 33,048 hrs · 23,485 cycles

SEAT TRACK CORRODED AT BS 683 - 836 LBL 9. REMOVED, FABRICATED AND INSTALLED A NEW SEAT TRACK IAW REO 670-53-00-343, EC/TC REO 670-53-00-343 AND AMM 53-49-00/400-801.

Part: SEAT TRACK — CORRODED (BS 677-708) · airframe 33,048 hrs · 23,485 cycles

RIGHT SIDE SEAT TRACK CORRODED AT BS 677 - 708. REMOVED, FABRICATED AND INSTALLED NEW SEAT TRACK IAW REO 670-53-00-343, EC/TC REO 670-53-00-343 AND AMM 53-49-00/400-801.

Part: SEAT TRACK — CORRODED (BS 785-863) · airframe 33,048 hrs · 23,485 cycles

LEFT SIDE SEAT TRACK CORRODED AT BS 785 - 863. REMOVED, FABRICATED AND INSTALLED A NEW SEAT TRACK IAW REO 670-53-00-343, EC/TC REO 670-53-00-343 AND AMM 53-49-00/400-801.

Part: SEAT TRACK — CORRODED (BS 581-677) · airframe 33,048 hrs · 23,485 cycles

RIGHT SIDE SEAT TRACK CORRODED AT BS 581-677. REMOVED, FABRICATED AND INSTALLED A NEW SEAT TRACK IAW REO 670-53-00-343, EC/TC REO 670-53-00-343 AND AMM 53-49-00/400-801.

Part: SEAT TRACK — CORRODED (BS 708-761) · airframe 33,048 hrs · 23,485 cycles

SIDE SEAT TRACK CORRODED BS 708 - 761. REMOVED, FABRICATED AND INSTALLED A NEW SEAT TRACK IAW REO 670-53-00-343, EC/TC REO 670-53-00-343 AND AMM 53-49-00/400-801.

Part: SEAT TRACK — CORRODED (BS 785-863) · airframe 33,048 hrs · 23,485 cycles

SIDE SEAT TRACK CORRODED AT BS 785.15 - 863. REMOVED, FABRICATED AND INSTALLED NEW SIDE SEAT RAIL IAW REO 670-53-00-343, EC/TC REO 670-53-00-343 AND AMM 53-00-49-000/400-801.

Part: BRACKET — CORRODED (BS 581) · airframe 33,048 hrs · 23,485 cycles

CARGO NET ANCHOR MOUNT PAD CORRODED AT BS 581 & STRINGER 27. REMOVED AND REPLACED CARGO NET ANCHOR MOUNT PAD IAW SRM 51-40-11-001-001-A01 AND 51-42-20-001-001-A01.

Part: MOUNT FITTING — CORRODED (CARGO BAY) · airframe 33,048 hrs · 23,485 cycles

CARGO NET ANCHOR MOUNTING PAD HAS CORROSION. REMOVED AND REPLACED CARGO NET ANCHOR MOUNTING PAD AT FS581.00 STR27 IAW SRM 51-40-11-001-001-A01 AND 51-42-20-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 33,048 hrs · 23,485 cycles

CORROSION FOUND ON SIDE SEAT TRACK, BS 485-581. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A17 & 53-00-49-400-801-A17.

Part: SEAT TRACK — CORRODED (BS 349-485) · airframe 33,048 hrs · 23,485 cycles

SEAT TRACK SEGMENT IS CORRODED OUT OF LIMITS AT BS 349 - 485, RBL9. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A17, 53-00-49-400-801-A17 AND REO 670-53-00-343.

Part: SEAT TRACK — CORRODED (BS 677-708) · airframe 33,048 hrs · 23,485 cycles

SIDE SEAT TRACK CORRODED BS 677 - 708. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A17, 53-00-49-400-801-A17 AND REO 670-53-00-343 REV K.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 33,048 hrs · 23,485 cycles

CORROSION FOUND ON RT SIDEWALL SEAT TRACK BS 485-581. REMOVED, FABRICATED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000/400-801-A17, REO 670-53-00-343 REV M AND EC/TC REO 670-53-00-343.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 33,048 hrs · 23,485 cycles

DURING C CHECK, FOUND ASD AFT RISER SUPPORT ANGLE CRACKED ON REPAIR ANGLE. REMOVED AND REPLACED THE CRACKED AFT DRAG ANGLE IAW REO 670-52-11-072, TYPE II AND EC/TC REO 670-52-11-072 REV E.

Part: SKIN — DAMAGED (NACELLE) · airframe 33,048 hrs · 23,485 cycles

DURING C CHECK, FOUND LOWER FORWARD CORE COWL INNER SKIN DAMAGED RIGHT ENGINE. COMPLIED WITH REPAIR IAW REO 670-54-23-959, & EC/TC REO 670-54-23-959

Part: STIFFENER — CRACKED (PAX DOOR) · airframe 33,048 hrs · 23,485 cycles

DURING C CHECK, FOUND ASD MOTOR LOWER SUPPORT ANGLE, LOWER CORNER CRACKED IN RADIUS. REMOVED AND REPLACED THE PAX DOOR MOTOR ASSIST STIFFENER IAW CRJ700 SRM 51-40-11-001-001-A01. THIS IS A MINOR REPAIR.

Part: PANEL — CORRODED · airframe 33,048 hrs · 23,485 cycles

MAC - DURING C CHECK, DISCOVERED CORROSION ON AFT SIDE PANEL LOWER CORNER. REMOVED CORROSION FROM AREA. BLENDED AND REPAIRED THE BLEND AREA IAW REO 670-52-11-104 REV E AND EC/TC REO 670-52-11-104.

Part: PANEL — CORRODED (ZONE 800) · airframe 33,048 hrs · 23,485 cycles

DURING C CHECK, FOUND FWD LOWER CORNER OF ASD FWD RISER CORRODED. REMOVED CORROSION. BLENDED AREA AND FOUND TO BE WITHIN REPAIRABLE LIMITS IAW REO 670-52-11-104. REPAIRED AREA IAW REO 670-52-11-104 & EC/TC REO 670-52-11-104.

Part: CONNECTOR — LOOSE (SMOKE DETECTOR) · airframe 33,033 hrs · 20,092 cycles

THE CREW REPORTED A SMOKE AFT LAV WARING MESSAGE DURING DESCENT. FA ADVISED THERE WAS NO SMOKE, FIRE OR FUMES. MAINTENANCE INSPECTED AND FOUND LOOSE CONNECTOR ON THE SMOKE DETECTOR. CONNECTED THE CONNECTOR AND OPS CHECKED GOOD.

Part: PANEL — DAMAGED (PAX DOOR) · airframe 32,131 hrs · 22,770 cycles

PASSENGER DOOR FWD SIDE PANEL DAMAGED. REPAIRED IAW GREO 670-52-11-848 REV, REO 670-52-11-897 & EC/TC REO 670-52-11-848 01.

Part: STRUT — DISCONNECTED (SERVICE DOOR) · airframe 31,963 hrs · 22,641 cycles

SERVICE DOOR WILL NOT OPEN FROM INSIDE/OUTSIDE HANDLES, DOORS AND OVERWING EMERGENCY EXITS. FOUND SERVICE DOOR UPLOCK STRUT DISCONNECTED. RECONNECTED STRUT IAW AMM 52-41-02. DEFER CLEARED, PLACARD REMOVED.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 30,266 hrs · 21,261 cycles

COCKPIT FLASHLIGHT INOPERATIVE. REPLACED FLASHLIGHT BATTERIES, OPS CKS GOOD IAW AMM 25-61-00. NO FURTHER DEFECTS NOTED.

Part: SKIN — GOUGED (FUSELAGE) · airframe 29,830 hrs · 20,924 cycles

AFT FUSELAGE HAS GOUGES AT LOW PRESSURE GROUND AIR CONNECTION. REMOVED PAINT AND BLENDED DAMAGES AT AFFECTED LOCATIONS IAW SRM 51-12-00/ TR51-0050 AND SRM 51-25-01. FOUND ADDITIONAL DAMAGES AND SUBMITTED TO ENGINEERING IAW SRM 51-13-01. THIS HAS BEEN CLASSIFIED AS A MAJOR, IAW GMM 5-3. COMPLIED WITH EA EJ-CRJ753-00023.

Part: RETAINER — DAMAGED (FWD CARGO DOOR) · airframe 28,952 hrs · 20,223 cycles

FWD CARGO DOOR SEAL RETAINER CORNERS ARE DAMAGED. REPAIRED IAW REO 670-52-35-127, REV C. MAJOR REPAIR.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 28,782 hrs · 20,095 cycles

MAIN CABIN EMERGENCY EXIT LOCATING SIGNS LIGHT INOPERATIVE. R & R 1 BATTERY PACK IAW AMM 33-51-17. OPS CHECKED GOOD.

Part: FITTING — CHAFED · airframe 28,699 hrs · 20,036 cycles

LEFT FUSELAGE AND WING FITTING FWD SIDE OF AFT FLANGE HAVE CONTACT MARKS FROM LINKS. REMOVED DAMAGED FROM FUSELAGE AND WING FITTINGS IAW SRM 51-12-00-001-A01, TR 51-0050.

Part: GATE — GOUGED (PAX DOOR) · airframe 28,699 hrs · 20,036 cycles

PAX DOOR PRESSURE VENT FLAP GOUGED BY ICE BREAKER CABLE. REPAIRED IAW REO 670-52-11-238, REV DATED 11/9/2006. MAJOR REPAIR.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 28,699 hrs · 20,036 cycles

PAX DOOR SILL CORRODED. BLENDED IAW SRM 51-21-06-001-001-A01 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-21-23-101-001-A01. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-42-21-001-001-A01 AND SRM 51-42-06-001-001-A01.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 28,699 hrs · 20,036 cycles

FLOORBEAM ANGLE CORRODED AT BS 280. ANGLE REPLACED DURING SB 670BA-53-041 REV D, PART A. MAJOR REPAIR.

Part: DOOR SILL — CORRODED · airframe 28,699 hrs · 20,036 cycles

SERVICE DOOR SILL CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-23-101-002-A01. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-42-06-001-001-A01, 51-41-001-001-A01.

Part: FLOOR SUPPORT — CORRODED (BS 283) · airframe 28,699 hrs · 20,036 cycles

FLOOR SUPPORT CORRODED AT BS 283, BLENDED THE FLOOR SUPPORT IAW SRM 51-21-06-001-001-A01.

Part: BULKHEAD — CORRODED (BS 280) · airframe 28,699 hrs · 20,036 cycles

AFT SIDE OF RT BULKHEAD WEB AT BS 280 IS CORRODED. REPAIRED IAW REO 670-53-11-594. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 28,699 hrs · 20,036 cycles

FLOORBEAM AT BS 280 IS CORRODED. REPAIRED IAW SB 670BA-53-041. MAJOR REPAIR.

Part: ANGLE — CORRODED (PAX DOORWAY) · airframe 28,699 hrs · 20,036 cycles

PAX DOOR UPPER CAP ANGLE CORRODED. BLENDED DAMAGE IAW SRM 51-21-06-001-001-A01, FOUND TO BE OUT OF LIMITS IAW SRM 53-21-23-101-001-A01. REMOVED THE MID UPPER CAP ANGLE IAW SRM 51-42-06-001-001-A01. LOCATED FASTENER HOLES IN NEW SERVICEABLE MID UPPER CAP ANGLE IN REF TO SRM 51-42-06-001-001-A01. INSTALLED MID UPPER CAP ANGLE IAW 51-42-06-001-001-A01 / 51-42-21-001-001-A01.

Part: STRIKER — CORRODED (DOOR SEAL) · airframe 28,699 hrs · 20,036 cycles

SERVICE DOOR LOWER, SEAL STRIKER CORRODED. BLENDED IAW SRM 51-21-06-001-001-A01 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-21-23-101-002-A01. REMOVED AND REPLACED THE SEAL STRIKER IAW SRM 51-42-06-001-001-A01, SH 670-31412-7, SRM 51-40-11-001-001-A01, AND DWG SH670-31412-7.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 28,699 hrs · 20,036 cycles

PAX DOOR BOTTOM ANGLE HAS CORROSION. REPAIRED IAW EA 25-2014-358, REV 0I.

Part: ANGLE — CORRODED (COCKPIT DOOR) · airframe 28,699 hrs · 20,036 cycles

LEFT COCKPIT DOOR LOWER POST, LOWER ANGLE CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00-101-001-A01. R & R THE ANGLE IAW SRM 51-42-10-001-001-A01, 51-42-13-001-001-A01 & 51-42-06-001-001-A01.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 28,699 hrs · 20,036 cycles

AFT SIDE OF BULKHEAD WEB AT BS 280 IS CORRODED. REPAIRED IAW REO 670-53-11-594. MAJOR REPAIR.

Part: ANGLE — CORRODED (COCKPIT DOOR) · airframe 28,699 hrs · 20,036 cycles

RT COCKPIT DOOR LOWER POST LOWER ANGLE CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00-101-001-A01. R & R THE ANGLE IAW SRM 51-42-10-001-001-A01, SRM 51-42-13-001-001-A01 & SRM 51-42-06-001-001-A01.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 28,699 hrs · 20,036 cycles

FLOORBEAM AT BS 280 IS CORRODED. REPAIRED IAW SB670BA-53-041. MAJOR REPAIR.

Part: CHANNEL — CORRODED · airframe 28,699 hrs · 20,036 cycles

TCAS ANTENNA DOUBLE CHANNEL CORRODED AT STR 27. EVALUATED TCAS ANTENNA DOUBLER CHANNEL AT STR 27, NO DAMAGE ALLOWED IAW SRM 53-21-01-101-002-A01. REMOVED ANTNNA & DOUBLER CHANNEL IAW AMM 34-43-07-000-801-A03 & 51-42-21-001-001-A01 AND 51-42-06-001-001-A01. INSTALLED TCAS CHANNEL ASSY IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01. LOCATED AND DRILLED TCAS DOUBLER CHANNEL IAW SRM 51-40-001-001-A01. REINSTALLED ORIGINAL TCAS BTM ANTENNA IAW AMM 34-43-07-400-801, A03.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 28,699 hrs · 20,036 cycles

CRAWLWAY FLOORBEAM ANGLE ON AFT SIDE OF BS 280 CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00-101-001-A01. REMOVED AND REPLACED IAW SRM 51-42-06-001-001-A01, 51-40-11-001-001-A1, AND 51-42-06-001-001-A01.

Part: STRINGER — CORRODED (BS 349-364) · airframe 28,699 hrs · 20,036 cycles

STRINGER 26R CORRODED BETWEEN BS 349 - 364. BLENDED IAW SRM 51-21-06-001-001-A01 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-21-03-101-006-A01. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-06-001-001-A01.

Part: SKIN — CORRODED (FUSELAGE) · airframe 28,699 hrs · 20,036 cycles

MAIN AVIONICS BAY DOOR CUTOUT HAS CORROSION AROUND SEAL LAND. BLENDED DAMAGE IAW SRM 51-12-00-001-001-A1. BLENDED AREA WELL WITHIN LIMITS REF REO 670-53-21-242, REV-B .

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 28,544 hrs · 19,919 cycles

DURING LINE CHECK, FOUND EMERGENCY FLOOD LIGHT AT ROW 6 INOPERATIVE. REPLACED THE ELECTRICAL CONNECTOR PIN IAW ESPM 20-26-03. OPS CHECKED GOOD IAW AMM 33-51-00.

Part: RETAINER — DAMAGED (CARGO DOOR SEAL) · airframe 27,749 hrs · 19,323 cycles

FWD CARGO DOOR SEAL RETAINER IS DAMAGED. COMPLIED WITH EC/TC REO 670-52-35-127 01. MAJOR REPAIR IAW GMM 5-3.

Part: MEGAPHONE — UNKNOWN · airframe 27,394 hrs · 19,057 cycles

MEGAPHONE IAW EO 700-25-0166. R & R MEGAPHONE IAW AMM 25-60-00.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 26,604 hrs · 18,477 cycles

EMERGENCY LIGHTS ON STATUS MESAGE IS ON WITH EMERGENCY LIGHTS ON IN CABIN WILL NOT EXTINGHUISH. CREW RESET SYSTEM, NOW WORKS NORMALLY IAW AMM 33-51-00. AC OK FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 26,372 hrs · 18,315 cycles

FLASHLIGHT DOES NOT WORK. REPLACED BATTERIES IAW AMM 25-60-00, OPS CHECKED GOOD, ACFT OK FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (ANTI ICE SYS) · airframe 26,408 hrs · 18,340 cycles

RECEIVED WING ANTI-ICE DUCT WARNING IN FLIGHT, FOLLOWED BY MULTIPLE LT WING AND MULTIPLE RT WING ANTI-ICE CAUTION MESSAGES. EMERGENCY DECLARED. PERFORMED LEAK TEST OF THE WING ANTIICE DUCTS IAW AMM 30-11-00, OPS TESTED WING ANTI ICE CONTROL AND INDICATING SYSTEMS IAW AMM 30-12-00. NO DEFECTS NOTED. FAULTS NOT PRESENT. ACFT GOOD FOR SERVICE.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 26,217 hrs · 18,207 cycles

LFT WING FWD EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP AND OPS CHECKED GOOD IAW CMM 33-52-07.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 25,332 hrs · 17,557 cycles

RIGHT EXTERIOR EMERGENCY LIGHT LENS AFT OF SERVICE DOOR BROKEN. R & R EMERGENCY LIGHT LENS IAW GMM 3-8.6

Part: GLOWSTRIP — MISSING (CABIN) · airframe 24,419 hrs · 16,925 cycles

PHOTOLUMINECSENT STRIP ON FLOOR IS MISSING IN FRONT OF WARDROBE CLOSET REPLACED MISSING PHOTOLUMINECSENT STRIP IAW AMM 33-51-01.

Part: LAMP — BURNED OUT (EMERGENCY LGIHT) · airframe 24,319 hrs · 16,855 cycles

CABIN, THIRD FROM FRONT CEILING EMERGENCY LIGHT, INOPERATIVE. REPLACED LAMP IAW AMM 33-51-09. OPS CHECKED GOOD.

Part: FRAME — DAMAGED (BS 349) · airframe 24,254 hrs · 16,808 cycles

WHILE REPLACING LONGERON AT STR25R LOWER FRAME SECTOR AT FS 349 TORE. NO REPAIR ALLOWED FOR THIS SECTOR REPLACEMENT IS REQUIRED. REMOVED FRAME, DRILLED UP NEW FRAME & INSTALLED FRAME ATTACH FLANGE SRM 51-42-06-001-001. REPAIRED IAW SRM 51-42-06-001-001 AND SRM 51-42-21-001-001.

Part: FLOOR SUPPORT — CORRODED (BS 280) · airframe 24,271 hrs · 16,821 cycles

COCKPIT FLOOR SUPPORT AT FS 280 CORRODED. REMOVED CORRODED FLOOR SUPPORT IAW SRM 51-42-06-001-001. LOCATED & DRILLED NEW ANGLE IAW SRM 51-40-06-001-001-A01 & 51-40-11-001-001. INSTALLED COCKPIT FLOOR SUPPORT IAW SRM 51-42-06-001-001-A01.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 24,254 hrs · 16,808 cycles

CEILING PANEL 231ALF EMERGENCY LIGHT LENS CRACKED. REMOVED CRACKED LENS FROM 243ALC IAW AMM 33-51-09-000-801 AND REPLACED WITH SERVICEABLE LENS IAW AMM 33-51-09-400-801.

Part: STRINGER — CORRODED (BS 333-349) · airframe 24,271 hrs · 16,821 cycles

STRINGER 25R CORRODED BETWEEN BS 333 AND 349. CORROSSION FOUND TO BE OUT OF LIMITS REF SRM 53-21-23-101-003. REMOVED LONGERON IAW SRM 51-42-06-001-001-A01. DRILLED NEW LONGERON IAW SRM 51-40-00-001-001.

Part: FLOOR SUPPORT — CORRODED (BS 1047-1051) · airframe 24,271 hrs · 16,821 cycles

FLOOR SUPPORT AT BS 1047-1051 LBL 30, CORRODED AROUND NUT PLATE. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. COMPLIED WITH REO 670-53-61-926.

Part: FRAME — CORRODED (BS 333) · airframe 24,271 hrs · 16,821 cycles

FRAME BS 333 CORRODED AT STRINGER 25R. BLENDED CORROSION IAW SRM 51-21-06-001-001. NO DAMAGE ALLOWED IAW SRM 53-21-06-101-002-A01. COMPLIED WITH REO 670-53-21-913.

Part: SEAT TRACK — CORRODED (BS 364) · airframe 24,271 hrs · 16,821 cycles

SEAT TRACK RBL 9 BS 364 CORRODED. REMOVED CORRODED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-00-49-400-801 (A01).

Part: FLOOR SUPPORT — CORRODED (BS 280-319.7) · airframe 24,269 hrs · 16,820 cycles

RIGHT FLOOR SUPPORT CORRODED FROM FS 280 TO 319.7. REMOVED CORRODED RT FLOOR SUPPORT. LOCATED, DRILLED AND INSTALLED NEW FLOOR SUPPORT IAW SRM 51-40-11-001-001, 51-92-10-001-001-A01 AND 51-40-11-001-001-A01. INSTALLED NEW RING DOUBLER, AND ACCOMPANYING PARTS TO NEW FLOOR SUPPORT IAW 51-42-10-001-001-A01 AND 51-40-11.

Part: FLOOR SUPPORT — CORRODED (BS 1047-1088.2) · airframe 24,269 hrs · 16,820 cycles

RIGHT FLOOR SUPPORT CORRODED FROM FS 1047 TO 1088.2. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. COMPLIED WITH REO 670-53-61-926.

Part: FLOOR SUPPORT — CORRODED (BS 969-985) · airframe 24,271 hrs · 16,821 cycles

LEFT FLOOR SUPPORT CORRODED FROM FS 969 TO 985. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. DAMAGE EXCEEDS ALLOWABLE DAMAGE LIMITS OF SRM 53-00-00-101-001-A01. COMPLIED WITH REO 670-53-00-377.

Part: FLOOR SUPPORT — CORRODED (BS 1047-1088.2) · airframe 24,269 hrs · 16,820 cycles

LEFT FLOOR SUPPORT CORRODED FROM FS 1047 TO 1088.2. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. COMPLIED WITH REO 670-53-61-926 IAW NDTM PART 1 51-20-006.

Part: SEAT TRACK — CORRODED (BS 364) · airframe 24,271 hrs · 16,821 cycles

SEAT TRACK AT RBL 9 BS 364 CORRODED. REMOVED CORRODED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED SERVICEABLE SEAT TRACK AT RBL 9.00 FS 364-485 IAW AMM 53-00-49-400-801.

Part: FLOOR SUPPORT — CORRODED (BS 349) · airframe 24,271 hrs · 16,821 cycles

RIGHT FLOOR SUPPORT CORRODED AT FS 349. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. COMPLIED WITH REO 670-53-21-911.

Part: ANGLE — CORRODED (DOOR HINGE) · airframe 24,254 hrs · 16,808 cycles

TWO LEFT ANGLES HINGE SIDE OF ASD FOUND TO BE CORRODED. R & R ANGLE IAW AMM 51-42-06-001-001-A01.

Part: STRINGER — CORRODED (BS 364 S26R) · airframe 24,254 hrs · 16,808 cycles

STRINGER 26R CORRODED AT FRAME BS 364. REMOVED STRINGER. S26R REF SRM 51-42-06-001-001 AND SRM 51-42-21-001-001. LOCATED & DRILLED NEW STRINGER 26RT FS 333-364 IAW SRM 51-40-11-001-001-A01. INSTALLED NEW STRINGER IAW SRM 51-42-21-001-001-A01 & 51-42-06-001-001-A01.

Part: FRAME — CORRODED (BS 310) · airframe 24,261 hrs · 16,815 cycles

FRAME 310.00 CORRODED AT STGR 27. REMOVED CORROSION IAW SRM 51-21-06-001-01-A01. DAMAGE NOT WITHIN LIMITS OF SRM 53-21-06-101-002-A01. COMPLIED WITH REO 670-53-21-914.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 24,269 hrs · 16,820 cycles

TCAS DOUBLER CORRODED LOCATED BETWEEN FRAMES 295 & 310 STRINGER 27. REMOVED TCAS DOUBLER IAW SRM 51-42-06-001-001. DRILLED NEW DOUBLER IAW SRM 51-40-11-001-001. INSTALLED NEW DOUBLER IAW SRM 51-42-06-001-001-A01.

Part: STRINGER — CORRODED (BS 295-310) · airframe 24,261 hrs · 16,815 cycles

STRINGER 25R CORRODED BETWEEN FRAMES 295.00 & 310.00. REMOVED STRINGER IAW SRM 51-42-06-001-001-A01. DRILLED AND INSTALLED NEW STRINGER IAW SRM 51-40-11-001-001.

Part: FLOOR SUPPORT — CORRODED (BS 280) · airframe 24,254 hrs · 16,808 cycles

CRAWLWAY FLOORBOARD FWD SUPPORT ANGLE CORRODED AT FRAME 280.00. R & R CRAWLWAY FLOORBOARD ANGLE AT FS280 IAW SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01.

Part: BULKHEAD — CORRODED (BS 280) · airframe 24,261 hrs · 16,815 cycles

BULKHEAD WEB AFT FACE CORRODED AT FS 280.00. INSTALLED LOWER WEB RT FS280 BULKHEAD IAW REO EC/TC 670-53-11-594. COMPLIED WITH EC/TC REO 670-53-11-594. COMPLIED WITH GREO 670-53-11-594, REV DATED 4/27/12.

Part: BULKHEAD — CORRODED (BS 280) · airframe 24,261 hrs · 16,815 cycles

LT LOWER BULKHEAD WEB AFT FACE CORRODED AT FS 280.00. REMOVED LT LOWER BULKHEAD WEB AT LOCATED AND DRILLED NEW BULKHEAD WEB IAW 51-40-11-001-001. INSTALLED LT LOWER LOWER WEB IAW SRM 51-42-06, 51-42-13. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 24,254 hrs · 16,808 cycles

BS 280.00, FLOORBEAM CORRODED. INSTALLED FLOORBEAM IAW REP 670-53-11-074. REPAIRED IAW REO 670-53-11-047 AND REO 670-53-11-040, REV E.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 24,179 hrs · 16,747 cycles

EMERGENCY EXIT LIGHT COVER MISSING AT SEAT 12D. INSTALLED EMERGENCY EXIT LIGHT COVER AMM 33-51-07.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 23,191 hrs · 15,994 cycles

PASSENGER DOOR HAS CRACK AT AFT DRAG ANGLE AT THE DOOR ASSIST PULLEY BRACKET. FOUND CRACK TO BE .650" LONG. FOUND CRACK TO BE WITHIN LIMITS IAW REO 670-52-11-287 REV A, ZONE 3.

Part: LINK — CRACKED (WNG TO BDY) · airframe 22,743 hrs · 15,674 cycles

WING TO FUSELGAE PICK UP LINKS AT FS 797 LT & RT SIDE CRACKED. REINSPECTED IAW REO 670-57-21-381, REV E. NO FURTHER DEFECTS NOTED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 22,417 hrs · 15,439 cycles

EMERGENCY CEILING LIGHT AT ROW 9 INOPERATIVE. RELAMPED EMERGENCY CEILING LIGHT AT ROW 9 IAW AMM 33-51-09, OPS CHECK GOOD.

Part: CONNECTOR — MISWIRED (EMERGENCY LIGHT) · airframe 20,556 hrs · 14,125 cycles

REFER TO DIML 611741-2 EMERGENCY CEILING LIGHT NR3 IS INOP. REPINNED CONNECTOR PL125P2 IAW ESPM 20-26-00, REF TO AFDL 611742-2 FOR OP'S CHECK. (CLOSED)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 20,542 hrs · 14,112 cycles

ROW 4, C/D EXIT SIGN INOP. R & R FWD CABIN EMERGENCY BATTERY PACK NR 1 IAW AMM 33-51-17, AND PACK NR 2 FUSES IAW CMM 33-21-70. OPS CHECK GOOD. (CLOSED)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 20,542 hrs · 14,112 cycles

CABIN NR 3 EMERGENCY CEILING LIGHT INOP. R & R BATTERY PACK NR 1 AND BATTERY PACK NR 2 FUSES IAW AMM 33-51-17 AND CMM 33-21-70. OPS CHECK GOOD. DEFER 611725-1 AND 611725-2 CLEARED. (CLOSED)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 20,487 hrs · 14,072 cycles

SERVICE DOOR AREA FLOOR LEVEL EMERGENCY FLOOD LIGHT INOPERATIVE. R & R BATTERY PACKS IAW AMM 33-51-17 AND CMM 33-21-70.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 20,487 hrs · 14,072 cycles

CABIN NR 3 CEILING EMERGENCY LIGHT INOPERATIVE. R & R BATTERY PACK IAW AMM 33-51-17 AND CMM 33-21-70.

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY LIGHT IN OVERHEAD AISLE IS INOPERATIVE. REMOVED AND INSTALLED SERVICABLE POWER SUPPLY UNIT IAW AMM 32-51-17-000-801 (A01) AND 33-51-17-400-801. OPS CHECKED GOOD.

Part: SUPPORT — CORRODED (BS 533) · airframe 19,994 hrs · 13,729 cycles

LT SEAT TRACK SUPPORT UNDER CTR FLOORBOARD AT FS 533 IS CORRODED. ACCOMPLISHED REPAIR LT SEAT TRACK SUPPORT IAW SRM 53-00-00 AND REO 670-53-31-189 AND EC/TC REO 670-53-31-189.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,994 hrs · 13,729 cycles

NR1 LT SIDEWALL SEAT RAIL HAS CORROSION. R & R SIDEWALL SEAT RAIL IAW SRM 51-41-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,994 hrs · 13,729 cycles

NR1 RT SIDEWALL SEAT RAIL HAS CORROSION. REMOVED SEAT RAIL IAW AMM 53-0-49 & INSTALLED REPLACEMENT SEAT RAIL IAW AMM 53-00-49,51-23-00 & SRM 51-21-01 53-00-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,994 hrs · 13,729 cycles

NR 2 LT SEAT TRACK HAS CORROSION, LBL9. R & R SEAT TRACK IAW SRM 51-41-02 AND AMM 53-00-49.

Part: SUPPORT — CORRODED (BS 485) · airframe 19,994 hrs · 13,729 cycles

LT SEAT TRACK SUPPORT UNDER CTR FLOORBOARD AT FS 485 IS CORRODED. BLENDED CORROSION IAW SRM 51-21-06. MATERIAL LOSS OF .005 NOTED, ORIGINAL MATERIAL THICKNESS OF .056, REMAINING MATERIAL THICKNESS OF .049 NOTED, FOUND TO BE WITHIN LIMITS IAW SRM 53-00-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,994 hrs · 13,729 cycles

NR2 RT SEAT TRACK HAS CORROSION. REMOVED RT NR 2 SEAT TRACK AND INSTALLED SERVICEABLE RT NR 2 SEAT TRACK IAW AMM 53-00-49-400-801, SRM 51-21-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,994 hrs · 13,729 cycles

NR1 LT AND RT SEAT TRACKS HAVE CORROSION AT LBL9 AND RBL9. REMOVED SEAT TRACK, FABRICATED, ALODINED AND INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801/ SRM 51-21-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,994 hrs · 13,729 cycles

NR3 LT SIDEWALL SEAT RAIL HAS CORROSION. R & R SIDEWALL SEAT RAIL IAW SRM 51-41-02 AND AMM 53-00-49.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,994 hrs · 13,729 cycles

CORROSION ON LT SIDE SEAT RAIL APPROX 3 FT BEHIND OVERWING EXIT DOOR. BLENDED AND FOUND OUT OF TOLERANCE, R & R SEAT TRACK IAW AMM 53-00-49

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,994 hrs · 13,729 cycles

NR3 LT SEAT TRACK HAS CORROSION, LBL9. R & R NR 3 LEFT SEAT TRACK LBL9 IAW SRM 51-41-02 AND AMM 53-00-49.

Part: SUPPORT — CORRODED (BS 517) · airframe 19,994 hrs · 13,729 cycles

LT SEAT TRACK SUPPORT UNDER CTR FLOORBOARD AT FS 517.0 IS CORRODED. ACCOMPLISHED REPAIR IAW SRM 53-00-00 AND REO 670-53-31-189.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,994 hrs · 13,729 cycles

NR 2 RT SIDEWALL SEAT RAIL HAS CORROSION. REMOVED UNSERVICEABLE SIDEWALL SEAT RAIL, LOCATED, DRILLED, ALODINED, PRIMED AND TOPCOATED SERVICEABLE SIDE WALL SEAT RAIL, INSTALLED SERVICEABLE SIDEWALL SEAT RAIL IAW SRM 51-41-02/ 51-40-11/ 51-21-11/ 51-25-04/ 51-25-16 16948 12-13-10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,994 hrs · 13,729 cycles

NR3 RT SEAT TRACK HAS CORROSION. R & R NR 3 RT SEAT TRACK IAW SRM 51-41-02 AND AMM 53-00-49.

Part: SUPPORT — CORRODED (BS 549) · airframe 19,994 hrs · 13,729 cycles

LT & RT SEAT TRACK SUPPORTS UNDER CTR FLOORBOARD AT FS 549 ARE CORRODED. (OPEN)

Part: SUPPORT — CORRODED (BS 645) · airframe 19,994 hrs · 13,729 cycles

LT SEAT TRACK SUPPORT UNDER CTR FLOORBOARD AT FS 645 IS CORRODED. REPAIRED CORROSION ON FLOORBEAM AT FS 549 LBL 8 AND RBL 8 IAW ASA EC/TC'S REO 670-53-31-189.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,994 hrs · 13,729 cycles

NR2 LT SIDEWALL SEAT RAIL HAS CORROSION. R & R SIDEWALL SEAT RAIL IAW SRM 51-41-02 AND AMM 53-00-49.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,994 hrs · 13,729 cycles

NR3 RT SIDEWALL SEAT RAIL HAS CORROSION. R & R NR3 RT SIDEWALL SEAT RAIL IAW SRM 51-41-02 AND AMM 53-00-49.

Part: SUPPORT FITTING — DAMAGED (SERVICE DOOR) · airframe 19,994 hrs · 13,729 cycles

UPPER SERVICE DOOR SUPPORT FITTING CRACKED. R & R UPPER SERVICE DOOR SUPPORT FITTING IAW SRM 51-41-02.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 19,994 hrs · 13,729 cycles

FS 280 CROSSBEAM SEVERLY CORRODED ACROSS UPPER SURFACE APPLY CIC AFTER REPAIRS ARE COMPLETE. REMOVED DAMAGED 280 CROSSBEAM ND REPLACED WITH NEW SERVICABLE BEAM PN CC670-34175-7 IAW SRM 51-42-06 AND 51-42-21.

Part: SKIN — CORRODED (SERVICE DOOR) · airframe 19,994 hrs · 13,729 cycles

SERVICE DOOR HAS INNER SKIN CORROSION AROUND BONDING JUMPER SCREW AND AT BOTTOM OF DOOR. LIGHTLY BLENDED CORROSION ON SERVICE DOOR LOWER DOUBLER. NO MEASURABLE MATERIAL LOSS NOTED, REMOVED CORROSION IAW SRM 51-21-06 AND RESTORED FINISH IAW SRM 51-25-06 & 51-25-16

Part: PLACARD — DAMAGED (CABIN) · airframe 19,994 hrs · 13,729 cycles

EMERGENCY ESCAPE HATCH OPEN PLACARD , CLOSED PLACARD, INSTRUCTION PLACARD, & ARROW INDICATING DIRECTION TO OPEN PLACARD UNSERVICEABLE 4 TOTAL 13262, PG 32. REPLACED EMERGENCY ESCAPE HATCH EXTERIOR PLACARDS, WITH NEW PLACARDS PN S1864, S1859, S1875, S1887 IAW AMM 20-60-11, 20-60-04.

Part: STOP — OUT OF ADJUST (LT OVERWING EXIT) · airframe 19,994 hrs · 13,729 cycles

LT OVERWING EMERGENCY EXIT FAILED FUNCTIONAL TEST. ADJUSTED STOPS IAW AMM 52-21-002-820-801. REQUIRED FUNCTIONAL TEST CARRIED OUT IAW AMM 52-21-00-720-801. FOUND TO BE SATISFACTORY.

Part: LIGHT — UNKNOWN · airframe 19,994 hrs · 13,729 cycles

CANNED 2 SECTIONS OF EMERGENCY LIGHT STRIPS. REPLACED 2 SECTIONS OF EMERGENCY LIGHT STRIPS WITH PN PL22-300LH00 LIGHT STRIPS IAW ASA SUPPLEMENT 33-51-01.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 19,633 hrs · 13,484 cycles

CAPTAINS FLASHLIGHT INOP. R & R THE BATTERIES IN THE CAPT'S FLASHLIGHT IAW AMM 25-61-00. OPS CK GOOD.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 18,868 hrs · 12,882 cycles

F/A REPORTS "EXIT" LENS MISSING ON LIGHT AT SERVICE DOOR ENTRANCE. REPLACED LENS IAW AMM 33-51-05

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 18,790 hrs · 12,825 cycles

F/A FLASHLIGHT DOES NOT WORK. R & R F/A FLASH LIGHT IAW AMM 25-61-00. (CLOSED)

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 18,721 hrs · 12,772 cycles

G2 GALLEY EMERGENCY FLOOD LIGHT LENS CRACKED. REMOVED AND REPLACED MAIN CABIN G-2 GALLEY, EMERGENCY FLOOD LIGHT LENS IAW MM 33-21-00.

Part: BULB — BLOWN (EMERGENCY LIGHTS) · airframe 18,721 hrs · 12,772 cycles

G2 GALLEY EMERGENCY FLOOD LIGHT HAS 3 BULBS BLOWN. RELAMPED G2 GALLEY, 3EA BULBS, OPS CHECKED GOOD IAW AMM CHAP. 33-51-00.

Part: LENS — BROKEN (EXIT SIGN) · airframe 18,721 hrs · 12,772 cycles

WARDROBE EXIT SIGN LENS BROKEN. REMOVED AND REPLACED LENS AT MAIN PASSENGER CABIN EXIT SIGN ON WARDROBE IAW 33-51-05.

Part: RELAY — INTERMITTENT (EMERGENCY LIGHT) · airframe 18,695 hrs · 12,753 cycles

FLT 5423 EMERGENCY LIGHT CYCLING ON/OFF ON GROUND AND APU POWER. REPLACED RELAY K135 PER AMM 20-42-00. OPS OK PER AMM 24-06-11.

Part: FLASHLIGHT — INTERMITTENT (COCKPIT) · airframe 17,937 hrs · 12,176 cycles

FO'S FLASHLIGHT INTERMITTENT.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 17,936 hrs · 12,176 cycles

REPLACED F/O FLASHLIGHT IAW AMM 25-61-01. (CLOSED)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,269 hrs · 10,888 cycles

FORWARD FLIGHT ATTENDANT WARDROBE EMERGENCY LIGHTS HAVE SEVERAL INOP BULBS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,910 hrs · 10,611 cycles

AFT NR 6 CEILING EMERGENCY FLOODLIGHT INOP.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 15,048 hrs · 9,950 cycles

EMERGENCY BATTERY NR 1 PACK WIRES PULLED OUT OF CR124. REMOVED AND REPLACED NR 1 BATTERY PACK DIODE PACK CR124. COMPLIED WITH OPS TEST OF EMERGENCY LIGHT SYSTEM IAW AMM 33-51-00-710-80, NO DEFECTS FOUND.

Part: FLOOR SUPPORT — CORRODED (BS 469-565) · airframe 15,048 hrs · 9,950 cycles

LBL 9 FLOORBEAM CORRODED AND HAS TOOLING DAMAGE AT FS 469.00 - 565.00. REWORKED AREA PER REO 670-53-31-119.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 15,048 hrs · 9,950 cycles

RT 280 FLOORBEAM CORRODED. R/R FLOORBEAM.

Part: WEB — CORRODED (BS 280)

LT BS 280 WEB HAS SURFACE CORROSION ON AFT LOWER WEB. REMOVED AND REPLACED BS 280 LT WEB REFER TO M-234 FORM FOR WORK ACCOMPLISHED.

Part: DRAG ANGLE — CRACKED (DOOR) · airframe 15,048 hrs · 9,950 cycles

THE AFT DRAG ANGLE ON THE ASD STEP RISER IS CRACKED LOCATION MARKED.

Part: SEAT TRACK — CORRODED (BS 708-761) · airframe 15,048 hrs · 9,950 cycles

RT SIDEWALL SEAT RAILS HAVE SCATTERED CORROSION BETWEEN FS 708.00 TO FS 761.00. BLENDED CORROSION IAW SRM 53-31-49. EXCEED ALLOWABLE LIMITS. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-00-49.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,048 hrs · 9,950 cycles

LT SIDEWALL SEAT RAILS HAVE SCATTERED CORROSION BETWEEN FS 394.00 TO FS 565.00.

Part: SEAT TRACK — CORRODED · airframe 15,048 hrs · 9,950 cycles

SEAT TRACK HAS SCATTERED CORROSION THROUGH OUT CABIN AT LBL9. REMOVED AND REPLACED LBL 9 FORWARD SEAT TRACK IAW SRM 51-41-06.

Part: SEAT TRACK — CORRODED (BS 581-613) · airframe 15,048 hrs · 9,950 cycles

RT SIDEWALL SEAT RAILS HAVE SCATTERED CORROSION BETWEEN FS 581.00 TO FS 613.00. EXCEED THE ALLOWABLE DAMAGE IAW SRM 53-31-49 MA 7026048. REMOVED AND REPLACED SEAT TRACK PER AMM 53-00-49.

Part: SEAT TRACK — CORRODED (BS 693-708) · airframe 15,048 hrs · 9,950 cycles

LT SIDEWALL SEAT RAILS HAVE SCATTERED CORROSION BETWEEN FS 693.00 TO FS 708.00.

Part: DOUBLER — CORRODED (BS 280) · airframe 15,048 hrs · 9,950 cycles

CORROSION DAMAGE INTERNAL BELLY DOUBLER JUST AFT OF FS 280.00, REMOVED FASTENERS TO ACCOMMODATE CORROSION REMOVAL, REMOVED ALL CORROSION IN MARKED AREAS ON INTERNAL BELLY DOUBLER JUST AFT OF FS 280. ALL WORK DONE IAW SRM 51-21-06. PERFORMED ET INSPECTION OF REWORKED AREA PER REO 670-53-21-407 IAW NDTM 51-20-006. NO DEFECTS NOTED.

Part: FLOOR SUPPORT — CORRODED (BS 280) · airframe 15,048 hrs · 9,950 cycles

CORROSION DAMAGE ON NUT PLATE SUPPORT ANGLE ATTACHED TO AFT SIDE OF FS 280.00 IN A/E/B (MARKED). REMOVED CORRODED NUT PLATE SUPPORT ANGLE FROM AFT SIDE OF F.S. 280.00 IN A/E/B CORRION ON RADIUS OF ANGLE, ANGLE FOUND TO BE NO GOOD. ALL WORK DONE IAW 51-42-06. PICKED UP EXISTING FASTENER HOLES AND INSTALLED ANGLE FOR FLOORBOARD IN AVIONICS BAY AFT OF FS 280 PER SRM 51-42-06.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,600 hrs · 9,634 cycles

LOWER EXIT LIGHT AFT OF SERVICE DOOR HAS SEVERAL INOP BULBS. (RESOLVED ON W/O 98983 TASKCARD: N/R 00010) RELAMPED LOWER EMERGENCY EXIT LIGHT ASSY IAW CRJ 700 AMM 33-51-05. OPS CHECK GOOD.

Part: SIGN — INOPERATIVE (CABIN) · airframe 12,489 hrs · 8,138 cycles

LEFT INTERIOR OVERWING LOWER EMERGENCY EXIT SIGN IS INOP.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 12,320 hrs · 8,022 cycles

CAPTAIN FLASHLIGHT NOT WORKING.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,812 hrs · 7,670 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 4 INOP. CABIN EMERGENCY LIGHTS - CEILING LEVEL FLOODLIGHTS.

Part: HANDLE — LOOSE (SERVICE DOOR) · airframe 11,698 hrs · 7,600 cycles

SERVICE DOOR RELEASE HANDLE LOOSE WN LET OPEN.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 11,421 hrs · 7,390 cycles

FS 296 TO FS 310 STRINGER 25R IS CORRODED. [06-08-07] CLEANED FS296 TO FS 310 STRINGER 25R FOUND NO DEFECTS. PER CRJ700 SRM 51-10-00.

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 11,421 hrs · 7,390 cycles

VERTICAL STABILIZER TO FUSELAGE ANGLE CRACKED ON LEFT T/E. [06-08-07] WORK ACCOMPLISHED ON EC/TC REO 670-55-31-018.

Part: HANDLE — CRACKED (AIRSTAIR DOOR) · airframe 11,421 hrs · 7,390 cycles

ASD OUTER HANDLE CRACKED. [06-08-07] REMOVED AND REPLACED ASD OUTER HANDLE IAW CRJ 700 MM 52-11-03.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 10,953 hrs · 7,064 cycles

F/O`S FLASHLIGHT INOP.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT)

DURING A GROUND INSPECTION, THE FIRST OFFICERS FLASHLIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS FLASHLIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING A C-CHECK, THE FORWARD FLOOR SUPPORT, AT FS 280, WAS FOUND TO BE CORRODED. THIS MRR WILL REMAIN OPEN PENDING MAINTENANCES DETERMINATION OF APPROPRIATE CORRECTIVE ACTION. (K)

Part: FLOOR SUPPORT — CORRODED (BS 310-349)

DURING A C-CHECK, THE PASSENGER DOOR SILL FLOOR SUPPORT ANGLE, AT FS310 TO FS349, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR SILL FLOOR SUPPORT ANGLE, AT FS310 TO FS349, IAW SRM 51-42-10. (K)

Part: HANDLE — CRACKED (E/E BAY DOOR)

DURING A C-CHECK, THE FORWARD AVIONICS BAY DOOR HANDLE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FORWARD AVIAONICS BAY DOOR HANDLE IAW SRM 51-42-06. (K)

Part: PULLEY — CRACKED (PAX DOOR)

DURING A C-CHECK, THE PASSENGER DOOR, ABOVE THE QASSIST CABLE PULLEY, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE PASSENGER DOOR, ABOVE THE ASSIST CABLE PULLEY, IAW REO. (K)

Part: UNKNOWN — CRACKED (BS 280)

DURING A C-CHECK, A SUSPECTED CRACK WAS FOUND AT FS 280, LBL9 AND RBL9. MAINTENANCE REPAIRED THE CRACK AT FS 280, LBL 9 AND RBL 9, IAW REO. (K)

Part: UNKNOWN — CORRODED (BS 280)

DURING C-CHECK, CORROSION WAS FOUND AT FS 280. MAINTENANCE REPAIRED THE CORRODION AT FS 280 BY INSTALLING NEW WEBS IAW SRM. (K)

Part: STRUCTURE — CRACKED (PAX DOOR)

DURING A C-CHECK IN MCN, THE AFT SIDE OF THE PASSENGER DOOR, BELOW THE TOP STEP, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE AFT SIDE OF THE PASSENGER DOOR, BELOW THE TOP STEP, IAW BOMBARDIER REO 670-52-11-154. (M)

Part: STRUCTURE — CRACKED (PAX DOOR)

DURING A C-CHECK IN MCN, THE FORWARD SIDE OF THE PASSENGER DOOR, BELOW THE TOP STEP, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE FORWARD SIDE OF THE PASSENGER DOOR, BELOW THE TOP STEP, IAW BOMBARDIER REO 670-52-11-154 AND 670-52-11-072. (M)

Part: CROSSBEAM — CORRODED (BS 280)

DURING A C-CHECK IN MCN, THE CROSSBEAM, AT FS 280, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED THE CROSSBEAM, AT FS 280, IAW ASA EO 700-53-0054A. (M)

Part: CROSSBEAM — CRACKED (BS 280)

DURING C-CHECK, THE FS 280, AT LBL 9 AND RBL 9, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FS 280 CROSSBEAM, AT LBL 9 AND RBL 9, IAW EO700-53-0061. (K)

Part: HANDLE — CRACKED (E/E BAY DOOR)

DURING A C-CHECK IN MCN, THE FORWARD AVIONICS BAY DOOR HANDLE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL REMOVE AND REPLACE THE FORWARD AVIONICS BAY DOOR HANDLE. (M)

Part: STRUCTURE — CRACKED (PAX DOOR)

DURING A C-CHECK, THE PASSENGER DOOR, BELOW THE TOP STEP ON THE FORWARD SIDE, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE PASSENGER DOOR, BLEOW THE TOP STEP ON THE FORWARD SIDE, IAW REO. (K)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

DURING A GROUND INSPECTION, THE EMERGENCY CEILING FLOODLIGHT AT ROW 17 WAS FOUND TO BE INOPERATIVE. MAINT REMOVED AND REPLACED THE LAMP IN THE EMERGENCY CEILING FLOODLIGHT AT ROW 17. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT)

DURING TAKEOFF, THE CREW RECEIVED A GEAR DISAGREE WARNING. THE QRH WAS COMPLIED WITH AND THE LANDING GEAR WAS RECYCLED. ALL INDICATIONS SHOWED GREEN (UP AND LOCKED). WITH ALL INDICATIONS SHOWING NORMAL, THE FLIGHT CONTINUED. AN EMERGENCY WAS DECLARED AS A PRECAUTION AND THE AIRCRAFT LANDED SAFELY. MAINTENANCE INTERROGATED THE PROXIMITY SENSOR ELECTRONIC UNIT THROUGH THE MAINTENANCE DIAGNOSTIC COMPUTER WITH NO FAULTS FOUND AND ALSO SWUNG THE LANDING GEAR NUMEROUS TIMES WITH NO FAULTS FOUND. AIRCRAFT OK FOR SERVICE. (K)

Part: WARNING LIGHT — ILLUMINATED (NLG STEERING)

DURING CLIMB OUT, THE CREW RECEIVED AN (NWS INOP MSSG) ON EICAS. THE NOSE WHEEL STEERING (NWS) FAULT SUBSEQUENTLY CLEARED AND THE AIRCRAFT CONTINUED. THE QRH WAS COMPLIED WITH AND THE CREW RESET THE NWS SYSTEM UPON LANDING IN IAH SAFELY. THE TOWER ROLLED EMERGENCY EQUIPMENT AS A PRECAUTION. MAINTENANCE RE RACKED THE NOSE WHEEL ELECTRONIC CONTROL UNIT AND NO FAULTS WERE FOUND. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: SWITCH — INOPERATIVE (NLG STEERING)

DURING CLIMB-OUT FROM BTR-ATL, THE CREW RECEIVED A NOSE WHEEL STEERING INOPERATIVE CAUTION MESSAGE. THE QRH WAS COMPLIED WITH AND THE NWS WAS TURNED OFF. THE CREW REQUESTED EMERGENCY VEHICLES BE PUT ON STANDBY AS A PRECAUTION. THE TOWER DECLARED AN EMERGENCY AND THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE NWS PRESSURE SWITCH. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: DUCT — CRACKED (WING)

DURING A GROUND INSPECTION IN DFW, THE RIGHT INBOARD LEADING EDGE SLAT DE-ICE TUBE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT INBOARD SLAT TELESCOPIC DUCT. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: SUPPORT BRACKET — CRACKED (FUSELAGE)

DURNG A HANGAR CHECK IN BTR, THE LEFT ANTI-ICE DUCT SUPPORT BRACKET AFT THE PRESSURE BULKHEAD AT FS 1098.2 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE ANTI-ICE DUCT SUPPORT BRACKETS AFT THE PRESSURE BULKHEAD AT FS 1098.2 IAW ASA EO 700-36-0003B. (M)