N761ND

Part: FITTING — CORRODED (ZONE 100) · airframe 38,252 hrs · 28,233 cycles

CORROSION ON NOSE JACK-FITTING RH ANGLE ON FWD SIDE OF FS280. (C-CHECK RO 8/11/2024) BLENDED CORROSION TO A SMOOTH CONTOUR REF CRJ 700 SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED NEW ANGLE P/N CC670-32154-2 REF CRJ 700 SRM 51-42-21-001-001-A01 AND DRAWING CC670-32050 REV NC. COMPLIED WITH TASK CARD 51-900-1002-SKY. CHECKS GOOD. SEE CONTINUATION FOR FURTHER DETAILS.

Part: SKIN — BENT (RT AILERON) · airframe 38,252 hrs · 28,233 cycles

DURING MOVEMENT OF RIGHT HAND AILERON, COTTER KEY HEAD CONTACTED AILERON LEADING EDGE CAUSING UPPER LEADING EDGE OF AILERON TO BEND AT HINGES # 2 AND # 3 (C-CHECK RO 8/11/2024) REMOVED UPPER AILERON SKIN REF CRJ700 SRM 51-42-21-001-001-A01 AND INSTALLED RH AILERON UPPER SKIN SHROUD REF DWG CC670-13000 REV D, CRJ700 SRM 51-42-21-001-001-A01, 51-42-22-001-001-A01, 51-42-06-001-001-A01. COMPLIED WITH 51-900-1002-SKY.

Part: FRAME — CORRODED (ZONE 100) · airframe 38,252 hrs · 28,233 cycles

PLATE AFT OF FS.280 FRAME UNDERFLOOR APPROX. STRG 25L-STRG 25R HAS CORROSION (MARKED) (C-CHECK RO 8/11/2024) REPAIRED PLATE AFT OF FS.280 FRAME UNDERFLOOR APPROX. STRG 25L-STRG 25R REF MHIRJ REO 670-53-11-1982 REV -- DATED 2024-07-09. COMPLIED WITH ALL STEPS OF THE REO. COMPLIED WITH TASK CARD 51-900-1002-SKY. SEE CONTINUATION FOR FURTHER DETAILS.

Part: SUPPORT BEAM — CHAFED (ZONE 100) · airframe 38,252 hrs · 28,233 cycles

SUPPORT BEAM FOR AFT BAGGAGE DOOR TRACK HAS CHAFING FROM BAGGAGE DOOR CABLES. (C-CHECK RO 8/11/2024) EVALUATED 2AE CHAFINGS ON SUPPORT BEAM (P/N: MM670-35502-010) FOR AFT BAGGAGE DOOR TRACK WITH LOCATIONS AT FS1000 AND FS1047 OUT OF LIMITS. COMPLIED WITH ALL STEPS OF REO 670-53-61-2321 REV -- DATED 2024-07-19. COMPLIED WITH TASK CARD 51-900-1002-SKY REPAIRING AFT BAGAGE BAY DOOR TRACK. SEE CONTINUE CARD FOR WORK PERFORMED.

Part: SPAR — CORRODED (ZONE 600) · airframe 38,252 hrs · 28,233 cycles

CENTER WING REAR SPAR R/H FWD ANGLE FOR THE TIRE BURST PANEL HAS CORROSION. (C-CHECK RO 8/11/2024) EVALUATED RH FWD ANGLE FOR TIRE BURST PANEL OUT OF LIMITS. ORDERED NEW PART, DRILLED AND LOCATED NEW PART. INSTALLED AND PERFORMED LEAK TEST OF AREA. NO LEAKS NOTED. REF CRJ700 AMM 28-11-00-790-801 (CONFIG A01), CRJ 700 SRM 51-42-21-001-001-A01 AND DWG # CC670-10338 REV -A AND DWG # CC670-10320 REV -F.COMPLIED WITH TASK CARD 51-900-1002-SKY

Part: TEE ANGLE — CORRODED (ZONE 100) · airframe 38,252 hrs · 28,233 cycles

CENTER FUSELAGE T CAP CORRODEDIN MULTIPLE LOCATIONS ON LBL9 BETWEEN APPROXIMATELY F841.00 AND FS853.00 AS MARKED (C-CHECK RO 8/11/2024) PERFORMED REPAIR PER REO 670-53-41-677 REV -- DATED 2024-07-08 CENTER FUSELAGE T CAP ON LBL9 BETWEEN APPROXIMATELY F841.00 AND FS853.00 COMPLIED WITH TASK CARD 51-900-1002-SKY "STRUCTURAL MAJOR REPAIR"

Part: PLATE — CORRODED (ZONE 100) · airframe 38,252 hrs · 28,233 cycles

FORWARD BAGGAGE BAY JOINT PLATE AT APPROXIMATELY FS581.00 BETWEEN STGR25L AND STGR26L CORRODED (C-CHECK RO 8/11/2024) REMOVED CORROSION FROM FORWARD BAGGAGE BAY JOINT PLATE AT APPROXIMATELY FS581.00 BETWEEN STGR25L AND STGR26L REF. CRJ-700 SRM 51-21-06-001-001-A01 FOUND TO BE OUT OF LIMITS REF CRJ-700 SRM 53-31-23-101-001-A01 REMOVED AND INSTALLED A NEW FWD BAGGAGE BAY JOINT PLATE CRJ 700 SRM 51-42-22-001-001-A01, REF CRJ 700 SRM 51-42-21-001-001-A01 AND DWG SH670-33750 REV-Y COMPLIED WITH TASK CARD 51-900-1002-SKY SEE CONTINUATION FOR FURTHER DETAILS.

Part: TIE DOWN — CORRODED (ZONE 100) · airframe 38,252 hrs · 28,233 cycles

FORWARD BAGGAGE BAY CARGO TIEDOWN PAD AT FS581.00 BETWEEN STGR23L AND STGR22L CORRODED AS MARKE (C-CHECK RO 8/11/2024) REMOVED FROM FORWARD BAGGAGE BAY CARGO TIEDOWN PAD ( BRACKET ) AT FS581.00 BETWEEN STGR23L AND STGR22L REF. CRJ-700 SRM 51-42-21-001-001-A01 AND INSTALLED NEW MACHINED BRACKET PN SH670-33390-2 REF. CRJ-700 SRM 51-42-21-001-001-A01 , CRJ-700 SRM 51-45-00-001-001-A01 AND DRAWING SH670-33600 REV. AD, COMPLIED W/51-900-1002-SKY

Part: TIE DOWN — CORRODED (ZONE 100) · airframe 38,252 hrs · 28,233 cycles

FORWARD CARGO BAY TIE DOWN PAD AT FS581.00 BETWEEN STGR27 AND STGR26L CORRODED AS MARKED (C-CHECK RO 8/11/2024) REMOVED FROM FORWARD CARGO BAY TIE DOWN PAD AT FS581.00 BETWEEN STGR27 AND STGR26L AND INSTALLED NEW BRACKET PN SH670-33389-2 AT FORWARD CARGO BAY FS581.00 BETWEEN STGR27 AND STGR26L REF. CRJ-700 SRM 51-42-21-001-001-A01 , REF. CRJ-700 SRM 51-42-06-001-001-A01 , REF. CRJ-700 SRM 51-42-15-001-001-A01 AND REF. DWG NO. SH670-33600 REV AD.COMPLIED WITH 51-900-1002-SKY

Part: TEE ANGLE — CORRODED (ZONE 100) · airframe 38,252 hrs · 28,233 cycles

CENTER FUSELAGE T CAP CORRODED ON RBL9 BETWEEN APPROXIMATELY FS685.00 AND FS697.00 AS MARKED (C-CHECK RO 8/11/2024) REMOVED CORROSION FROM CENTER FUSELAGE T CAP CORRODED ON RBL9 BETWEEN APPROXIMATELY FS685.00 AND FS697.0. PERFORMED ALL STEPS OF REO 670-53-41-673 REV-- DATED 2024-06-26.

Part: INTERCOSTAL — CHAFED (ZONE 200) · airframe 38,252 hrs · 28,233 cycles

INTECOSTAL IS CHAFED STGR9R BETWEEN FS1144.00 & FS1162.00. (FLAGGED) (C-CHECK RO 8/11/2024) BLENDED OUT CHAFE ON INTERCOSTAL LOCATED ON STGR9R BETWEEN FS1144.00 & FS1162.00. REF CRJ 700 SRM 51-12-00-001-001-A01REMOVED DAMAGED INTERCOSTAL BETWEEN FS 1144.00 TO FS 1162.00 STGR 9 RH REF CRJ700 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01..FABRICATED INTERCOSTAL P/N MM670-36537-020 FROM 7075-O .071" PO# T-58109 REF. BOMBARDIER DWG MM670-36537 REV. G. INSTALLED NEW INTERCOSTAL REF DRAWING MM670-36086 REV -M AND CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-21-001-001-A01. PERFORMED LEAK TEST OF THE AIR CONDITIONING DISTRIBUTION SYSTEM, REF. CRJ700 AMM 21-51-00-790-801, TEST GOOD, NO LEAKS FOUND AT THIS TIME.PERFORMED OPERATIONAL TEST OF THE AIR CONDITIONING DISTRIBUTION SYSTEM IAW CRJ 700 AMM 21-51-00-710-801-A01 OPS TEST GOODCOMPLIED WITH TASK CARD 51-900-1002

Part: DOOR SILL — GOUGED (ZONE 100) · airframe 38,252 hrs · 28,233 cycles

FORWARD BAGGAGE BAY SILL BETWEEN FS533.00 AND FS581.00 STGR26L CORRODED AND GOUGED IN MULTIPLE AREAS AS MARKED (C-CHECK RO 8/11/2024) REPAIRED CORROSION/GOUGE DAMAGE TO THE FWD BAGGAGE BAY DOOR SURROUND INNER CLOSING SKIN BETWEEN FS533.00-FS581.00 AND STR25L-STR26L PER REO 670-53-31-893 REV -- DATED 2024-06-25 COMPLIED WITH TASK CARD 51-900-1002-SKY. SEE CONTINUATION FOR FURTHER DETAILS.

Part: TEE ANGLE — CORRODED (ZONE 100) · airframe 38,252 hrs · 28,233 cycles

CENTER FUSELAGE T CAP CORRODEDIN MULTIPLE LOCATIONS ON LBL9 BETWEEN APPROXIMATELY F697.00 AND FS841.00 AS MARKED (C-CHECK RO 8/11/2024) BLENDED CORROSION FROM MULTIPLE LOCATIONS ON LBL9 T-CAP FLOOR STRUCTURE BETWEEN FS697 AND FS841. REPAIRED T-CAP REF REO 670-53-41-678 REV -A DATED 2024-07-22 AND CRJ-700 SRM 51-42-06-001-001-A01. RESTORED FINISH. COMPLIED WITH TASK CARD 51-900-1002-SKY AND MAJOR REPAIR(M-337 FORM) CHECKS GOOD. SEE CONTINUATION CARD FOR DETAILS.

Part: CAP — CORRODED (ZONE 100) · airframe 38,252 hrs · 28,233 cycles

CENTER FUSELAGE T CAP CORRODEDIN MULTIPLE LOCATIONS ON RBL9 BETWEEN APPROXIMATELY F697.00 AND FS841.00 AS MARKED (C-CHECK RO 8/11/2024) CUT OUT DAMAGED AREAS AND PERFROMED PERMANENT REPAIRS TO FS697.00 - FS841.00 RBL 9 BEAM T-CAP AS PER REO 670-53-41-670 REV -A DATED 2024-07-18, ALL STEPS HAVE BEEN COMPLIED WITH. SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH 51-900-1002-SKY

Part: FRAME — CORRODED (ZONE 100) · airframe 38,252 hrs · 28,233 cycles

CORROSION AT FS597.00 STGR19R AFT FACE AS MARKED (C-CHECK RO 8/11/2024) PERFORMED REPAIR TO FS597.00 STGR19R AFT FACE BY COMPLYING WILL ALL STEPS OF REO 670-53-31-894 REV -- DATE 2024-06-21. SEE CONTINUATION FOR WORK PERFORMED. COMPLIED WITH TASK CARD 51-900-1002

Part: STRINGER — CORRODED (ZONE 100) · airframe 38,252 hrs · 28,233 cycles

CORROSION ON STGR19R BETWEEN FS364.00 AND FS379.00 AS MARKED (C-CHECK RO 8/11/2024) BLENDED OUT CORROSION ON STGR19R BETWEEN FS364.00 AND FS379.00 REF CRJ-700 SRM 51-21-06-001-001-A01 COMPLIED WITH REO 670-53-21-2423 REV -B DATED 2024-07-27 REPAIR. COMPLIED WITH TASK CARD 51-900-1002-SKY. CHECKS GOOD. SEE CONTINUATION FOR FURTHER DETAILS.

Part: FRAME — CORRODED (ZONE 100) · airframe 38,252 hrs · 28,233 cycles

CORROSION AT FS597.00 BETWEEN STGR18L AND STGR19L AS MARKED (C-CHECK RO 8/11/2024) REMOVED CORROSION AT FS597.00 BETWEEN STGR18L AND STGR19L PER CRJ700 SRM 51-21-06-001-001-A01 FOUND OUT OF LIMITS. REMOVED AND INSTALLED A NEW STUB FRAME P/N SH670-33178-1 FOR FS.597 STGR 18L AND 19L REF CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01 AND DWG. SH670-33750 REV. AA AND DWG. SH670-33100 REV. K AND DWG SH670-33178 REV NC. COMPLIED WITH TASK CARD 51-900-1002-SKY CHECKS GOOD. SEE CONTINUATION FOR FURTHER DETAILS.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 38,252 hrs · 28,233 cycles

FLOOR SUPPORT BRACKET MOUNTED ON THE FS319.00 FRAME HAS INTERGRANULAR CORROSION. (MARKED) (C-CHECK RO 8/11/2024) INSTALLED NEW FLOOR SUPPORT BRACKET (FITTING) MOUNTED ON THE FS319.00 FRAME REF CRJ-700 SRM 51-42-21-001-001-A01 AND DWG#SH670-31950 REV-Y.COMPLIED W/ 51-900-1002-SKY

Part: STRINGER — CORRODED (ZONE 100) · airframe 38,252 hrs · 28,233 cycles

CORROSION BETWEEN FS319.70 AND FS333.00 STGR20L AS MARKED (C-CHECK RO 8/11/2024) REMOVED AND INSTALLED NEW REPLACEMENT STGR 20L PER CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-21-001-001-A01,DWG:SH670-31810 REV Y. COMPLIED WITH 51-900-1002-SKY. CHECKS GOOD. SEE CONTINUATION FOR FURTHER DETAILS.

Part: FRAME — CORRODED (ZONE 100) · airframe 38,252 hrs · 28,233 cycles

CORROSION AT FS265.00 AS MARKED BETWEEN STGR26L AND STGR26R (C-CHECK RO 8/11/2024) REMOVED CORROSION AT FS.265 FRAME ATTACH FLANGE BETWEEN STRG 26L AND 26R REF CRJ 700 SRM 51-42-06-001-001-A01 FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED A NEW REPLACEMENT FS.265 FRAME LOWER STIFFENING ANGLE REF CRJ 700 SRM 51-42-06-001-001-A01 AND DWG SH670-34020 REV -A. COMPLIED WITH TASK CARD 51-900-1002-SKY. ALL CHECKS GOOD. SEE CONTINUATION FOR FURTHER DETAILS.

Part: SLAT TRACK — CORRODED (ZONE 500) · airframe 38,252 hrs · 28,233 cycles

LH #2 LEADING EDGE SLAT TRACK 2-2 IS GROOVED, PITTED/CORRODED IN TWO AREAS. (C-CHECK RO 8/11/2024) LH #2 LEADING EDGE SLAT TRACK 2-2 REMOVED IAW CRJ700 AMM 27-81-41-000-802-A01 AND REPLACED AND INSTALLED WITH NEW SLAT TRACK IAW CRJ700 AMM 27-81-41-400-802-A01. SLATS AND SLAT TRACK RIGGING AND OPERATIONAL TEST, GOOD. SEE CONTINUATION CARD FOR MORE DETAILS

Part: SLAT TRACK — GROOVED (ZONE 500) · airframe 38,252 hrs · 28,233 cycles

LH #1 LEADING EDGE SLAT TRACK 1-1 IS GROOVED. (C-CHECK RO 8/11/2024) REPAIRED LH #1 LEADING EDGE SLAT TRACK 1-1, COMPLIED WITH REO 670-57-42-1586 REV: -- DATE 2024-06-24 - RIGGING CHECK GOOD PER CRJ700 AMM 27-81-00-820-801-A02. OPS TEST GOOD AT THIS TIME. COMPLIED W/ 51-900-1002-SKY

Part: SLAT TRACK — GROOVED (ZONE 500) · airframe 38,252 hrs · 28,233 cycles

LH #1 LEADING EDGE SLAT TRACK 1-3 IS GROOVED. (C-CHECK RO 8/11/2024) BLENDED OUT 2EA GROOVES ON LH SLAT TRACK 1-3 REF CRJ 700 SRM 51-12-00-001-001-A01 REPAIRED THE LH #1 LEADING EDGE SLAT TRACK 1-3 REF REO 670-57-42-1588 REV --, DATED 2024-06-24. COMPLIED WITH TASK CARD 51-900-1002-SKY. SEE CONTINUATION FOR FURTHER DETAILS.

Part: SLAT TRACK — GROOVED (ZONE 600) · airframe 38,252 hrs · 28,233 cycles

LH #2 LEADING EDGE SLAT TRACK 2-3 IS GROOVED. (C-CHECK RO 8/11/2024) REMOVED LH WING SLAT TRACK 2-3 AND INSTALLED NEW/SERVICEABLE SLAT TRACK 2-3 PER CRJ700 AMM 27-81-41-400-801-A01. OPS TEST GOOD AT THIS TIMETOOL USED: TORQUE WRENCH ID:TUC6231 CAL DATE DUE:31-JUL-24 TORQUE WRENCH ID:TUC4606 CAL DATE DUE:05-APR-24

Part: SLAT TRACK — CORRODED (ZONE 600) · airframe 38,252 hrs · 28,233 cycles

RH #2 LEADING EDGE SLAT TRACK 2-2 IS GROOVED, PITTED/CORRODED. (C-CHECK RO 8/11/2024) REMOVED RIGHT WING SLAT TRACK 2-2 (P/N: CC670-12051-9; S/N: M480) AND INSTALLED NEW/SERVICEABLE SLAT TRACK 2-2 (P/N: CC670-12051-9; S/N: M1830) PER CRJ700 AMM 27-81-41-400-802-A01. COMPLIED WITH SKYWEST TASK CARD 27-900-1009-SKY. RIGGING TEST PASSED AND OPS TEST GOOD AT THIS TIME.TOOL USED: TUC4236, CAL DUE 30/APR/2025

Part: SLAT TRACK — GROOVED (ZONE 500) · airframe 38,252 hrs · 28,233 cycles

LH #3 LEADING EDGE SLAT TRACK 3-3 IS GROOVED. (C-CHECK RO 8/11/2024) REMOVED LH WING DRIVEN SLAT TRACK 3-3 (P/N: CC670-12090-5 S/N: M410) AND INSTALLED NEW/SERVICEABLE SLAT TRACK 3-3 (P/N: CC670-12090-5, S/N M617) PER CRJ700 AMM 27-81-41-400-803-A01. GAPS AND MISMATCH GOOD & OPS TEST GOOD AT THIS TIME.TOOL USED TUC4236, CAL DUE 30/APR/2025

Part: SLAT TRACK — GROOVED (ZONE 600) · airframe 38,252 hrs · 28,233 cycles

RH #3 LEADING EDGE SLAT TRACK 3-1 IS GROOVED, PITTED/CORRODED. (C-CHECK RO 8/11/2024) REPAIRED RH #3 LEADING EDGE SLAT TRACK 3-1 PER REO 670-57-42-1585 REV --, DATE 2023-06-21 - RIGGING CHECK GOOD PER CRJ700 AMM 27-81-00-820-801-A02. OPS TEST GOOD AT THIS TIME. COMPLIED WITH 51-900-1002-SKY. SEE CONTINUE CARD FOR FURTHER DETAILS.

Part: SLAT TRACK — GROOVED (ZONE 600) · airframe 38,252 hrs · 28,233 cycles

RH #1 LEADING EDGE SLAT TRACK 1-1 IS GROOVED. (C-CHECK RO 8/11/2024) REPAIRED RH #1 LEADING EDGE SLAT TRACK 1-1 REF REO 670-57-42-1581 REV --, DATED 2024-06-21 - RIGGING CHECK GOOD PER CRJ700 AMM 27-81-00-820-801-A02. OPS TEST GOOD AT THIS TIME.COMPLIED WITH 51-900-1002-SKY.

Part: SLAT TRACK — CORRODED (ZONE 600) · airframe 38,252 hrs · 28,233 cycles

RH #1 LEADING EDGE SLAT TRACK 1-3 IS GROOVED, PITTED/CORRODED. (C-CHECK RO 8/11/2024) COMPLIED WITH REO 670-57-42-1583 REV-- DATED 2024-06-21 - RIGGING CHECK GOOD PER CRJ700 AMM 27-81-00-820-801-A02. OPS TEST GOOD AT THIS TIME.COMPLIED WITH 51-900-1002-SKY

Part: SLAT TRACK — CORRODED (ZONE 500) · airframe 38,252 hrs · 28,233 cycles

LH #1 LEADING EDGE SLAT TRACK 1-2 IS GROOVED, PITTED/CORRODED. (C-CHECK RO 8/11/2024) REMOVED LH WING NON DRIVEN SLAT TRACK 1-2 (PN: CC670-12021-9, S/N M496) AND INSTALLED NEW/SERVICEABLE SLAT TRACK 1-2 (PN: CC670-12021-9, S/N M1926) PER CRJ700 AMM TASK 27-81-41-400-802-A01. COMPLIED WITH SKYWEST TASK CARD 27-900-1009-SKY OPS TEST GOOD AT THIS TIME.TOOL USED: TORQUE WRENCH TUC 4236, DUE CAL 30/APR/2025.

Part: SLAT TRACK — GROOVED (ZONE 500) · airframe 38,252 hrs · 28,233 cycles

LH #3 LEADING EDGE SLAT TRACK 3-1 IS GROOVED. (C-CHECK RO 8/11/2024) REMOVED SLAT TRACK 3-1 ( SN: M481) AND INSTALLED NEW/SERVICEABLE SLAT TRACK 3-1 (SN: M1035) REF CRJ700 AMM 27-81-41-400-801-A01. COMPLIED WITH SKYWEST TASK CARDS 27-900-1009-SKY. GAPS AND MISMATCH GOOD AND OPS TEST GOOD AT THIS TIME.TORQUE WRENCH USED TUC4238 CALDUE:31-AUGUST-2024.

Part: SLAT TRACK — CORRODED (ZONE 600) · airframe 38,252 hrs · 28,233 cycles

RH #1 LEADING EDGE SLAT TRACK 1-2 IS GROOVED, PITTED/CORRODED. (C-CHECK RO 8/11/2024) REMOVED RIGHT WING SLAT TRACK 1-2 (P/N: CC670-12021-9; S/N: M495) AND INSTALLED NEW/SERVICEABLE SLAT TRACK 1-2 (P/N: CC670-12021-9; S/N: M1945) PER CRJ700 AMM 27-81-41-400-802-A01.COMPLIED WITH SKYWEST TASK CARD 27-900-1009-SKY. RIGGING TEST PASSED AND OPS TEST GOOD AT THIS TIME.TOOL USED: TUC4236, CAL DUE 30/APR/2025

Part: BRACKET — CRACKED (ZONE 400) · airframe 38,252 hrs · 28,233 cycles

L/H LWR TRANSCOWL HAS A CRACK @ THE END OF THE OMEGA SEAL ABOVE THE "A" BRACKET REPAIRED I/B EDGE OF SCOOP ON L/H LOWER TRANSCOWL, REF. REO 670-54-21-1650, REV. --, 2024-06-19. COMPLIED WITH M-337 AND SKY CARD 51-900-1002-SKY

Part: STAND OFF — CRACKED (ZONE 400) · airframe 38,252 hrs · 28,233 cycles

L/H LWR TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 8/11/2024) REPLACED I/B STAND-OFF ANGLE P/N CN624-2082-201 ON L/H LOWER TRANSCOWL, REF. REO 670-54-21-971, REV. B, 2023-11-28. COMPLIED WITH M-337 AND SKY CARD 51-900-1002-SKY.

Part: RIVET — SHEARED (THRUST REVERSER) · airframe 38,252 hrs · 28,233 cycles

L/H LWR TRANSCOWL HAS Z STIFFENER RIVETS SHEARED (C-CHECK RO 8/11/2024) REPAIRED L/H LOWER TRANSCOWL INNER SKIN COMMON TO ZED STIFFENER AT SHEARED FASTENER HOLES, REF. REO 670-54-21-1652, REV. --, 2024-07-04. COMPLIED WITH MAJOR REPAIR M-337 AND SKY CARD 51-900-1002-SKY.

Part: STAND OFF — CRACKED (ZONE 400) · airframe 38,252 hrs · 28,233 cycles

L/H UPPER TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 8/11/2024) INSTALLED 1 EA. NEW STANDOFF P/N CN624-2130-201 ON L/H UPPER TRANS COWL, REF. REO 670-54-21-971, REV. B, 2023-11-28, AND CRJ700 SRM 51-40-11-001-001-A01. COMPLIED WITH STEPS 1-3. MAJOR REPAIR (M-337), AND 51-900-1002 SKY.

Part: COAMING — CHAFED (ZONE 400) · airframe 38,252 hrs · 28,233 cycles

L/H LWR TRANSCOWL INNER COAMING IS CHAFED @ FWD LATCH (C-CHECK RO 8/11/2024) REPAIRED L/H LOWER TRANSCOWL INNER COAMING AT FWD. LATCH, REF. REO 670-54-21-1652, REV. --, 2024-07-04. COMPLIED WITH MAJOR REPAIR M-337 AND SKY CARD 51-900-1002-SKY.

Part: ANGLE — CRACKED (ZONE 200) · airframe 38,252 hrs · 28,233 cycles

RIGHT TORQUE BOX BL9R FS280.00 OUTBOARD ANGLE OUTBOARD SIDE OF THE TORQUE BOX AT FS280.00 IS CRACKED. (C-CHECK RO 8/11/2024) REMOVED DAMAGED OUTBD ANGLE AT FS280-00 RBL-9 OUT BOARD OF TORQUE BOX. REF CRJ-700 SRM 51-42-21-001-001-A01. INSTALLED 1 EA NEW O/B ANGLE PN CC670-34099-2SB AT FS280-00 RBL-9 OUT BOARD OF TORQUE BOX PER CRJ 700 SRM 51-42-21-001-001-A01 AND DRAWING CC670-34010 REV -K. COMPLIED WITH TASK CARD 51-900-1002-SKY. SEE CONTINUATION FOR FURTHER DETAILS.

Part: HINGE — CORRODED (ZONE 500) · airframe 38,252 hrs · 28,233 cycles

LH INBD FLAP THE INBD HINGE BOX HAS SIGNS OF CORROSION AT HINGE POINT (MARKED) (C-CHECK RO 8/11/2024) PERFORMED REPAIR OF L/H I/B FLAP HINGE BOX CORROSION AT HINGE POINT BY COMPLYING WITH ALL STEPS OF REO 670-57-54-062 REV -- DATE 2024-06-24 COMPLIED WITH TASK CARD 51-900-1002-SKY SEE CONTINUE CARD FOR WORK PERFORMED.

Part: SKIN — DENTED (ZONE 600 FLAP) · airframe 38,252 hrs · 28,233 cycles

RIGHT INBOARD FLAP LOWERE SKIN INBOARD OF THE INBOARD FLAP HINGE ARM HAS FOUR DENTS. (MARKED) (C-CHECK RO 8/11/2024) REPAIRED R/H I/B FLAP LOWER SKIN REF CRJ 700 SRM 57-52-01-201-005-A01, FIG. 57-52-01-995-803. SEE CONTINUATION SHEET FOR DETAILS. COMPLIED WITH TASK CARD 51-900-1002-SKY

Part: HANDLE — MISALIGNED (ZONE 800) · airframe 38,252 hrs · 28,233 cycles

MAIN AVIONICS COMPARTMENT DOOR HANDLE MISALIGNED / STICKS (C-CHECK RO 8/11/2024) INSTALLED NEW MAIN AVIONICS COMPARTMENT DOOR HANDLE HOUSING PER CRJ700 SRM 51-42-21-001-001-A01 AND DWG NO. CC670-38651 REV E. INSTALLED MAIN AVIONICS COMPARTMENT DOOR HANDLE REF. CRJ-700 AMM 52-42-03-400-801-A01. OPERATIONAL TEST/ LEAK TEST OF THE MAIN AVIONICS COMPARTMENT DOOR GOOD AT THIS TIME. COMPLIED WITH 51-900-1002-SKY. PERFORMED PRESSURE TEST OF AVIONICS DOOR REF CRJ700 AMM 52-00-00-790-801 (CONFIG A01). PRESSURE TEST GOOD

Part: STRIKER — GOUGED (CARGO DOOR FRAME) · airframe 36,594 hrs · 26,932 cycles

FWD CARGO DOOR SURROUND, FWD SEAL STRIKER AT F.S 535.64 GOUGED BEYOND REPAIR / REF SRM 53-31-23-991-801 ITEM # 102B PN SH670-31426-8 (FILED CLOSED) DRILLED OFF FWD CARGO DOOR SURROUND FWD SEAL STRIKER AT F.S 535.64 IAW SRM 51-42-06, / [PN SH670-31426-8 .POO SEE MR 1784104]

Part: SHAFT — OUT OF ADJUST (PAX DOOR HANDLE) · airframe 32,451 hrs · 23,731 cycles

RECEIVED A PASSENGER DOOR WARNING MESSAGE IN FLIGHT AFTER HEARING A LOUD NOISE DURING OUR INITIAL CLIMB. ALSO A PROX SYSTEM 1 FAULT STATUS MESSAGE. NO PRESSURIZATION PROBLEMS NOTED. RAN QRH DIVERTED. (FLT#2953) CLOSED FOUND INNER PAX DOOR HANDLE LOWER SHAFT ASSY NOT TOUCHING STOP HOUSING . REMOVED . CLEANED . LUBED . AND REINSTALLED INNER HANDLE LOWER SHAFT ASSY . OPS CHECK GOOD IAW AMM. PERFORMED OPS CHECK OF PAX DOOR OUTER HANDLE OPS CHECK GOOD IAW AMM. PRESSURIZED A/C HELD PRESSURE FOR SEVERAL MINUTES IAW AMM. NO PRESSURE DROP.

Part: SKIN — CHAFED (LT AILERON) · airframe 32,424 hrs · 23,707 cycles

LH AILERON LOWER LEADING EDGE CHAFE. (C-CHECK) RO: 06/01/2019 REMOVED AND REPLACED 2EA L/H AILERON LWR LEADING EDGE PANELS IAW SRM.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 32,424 hrs · 23,707 cycles

PAX DOOR INTERCOSTAL DD4 P/N 601R318081-1 IS CORRODED. (C-CHECK) RO: 06/01/2019 REPLACED PAX DOOR INTERCOSTAL DD4 P/N 601R318081-1 WITH NEW IAW SRM.

Part: SKIN — CHAFED (RT AILERON) · airframe 32,424 hrs · 23,707 cycles

RIGHT AILERON HAS CHAFE MARKS ON TOP LEADING EDGE. (C-CHECK) RO: 06/01/2019 INSTALLED NEW R/H AILERON UPPER LEADING EDGE SKIN IAW SRM.

Part: FRAME — CORRODED (BS 364) · airframe 32,424 hrs · 23,707 cycles

FS 364 FRAME HAS CORROSION AT STR 26R. REMOVED DAMAGE FRAME SECTOR AND INSTALLED A NEW FRAME SECTOR TO FS364 STGR 26R IAW SRM, LEAK CHECK GOOD.

Part: ANGLE — CORRODED (CARGO DOOR SILL) · airframe 32,424 hrs · 23,707 cycles

AFT BAGGAGE BAY DOOR SILL CORROSION, LOCATED IN THE CENTER. REMOVED AND INSTALLED NEW AFT BAG BAY DOOR LOWER SILL ANGLE IAW SRM.

Part: HOUSING — WORN (GALLEY DOOR) · airframe 32,424 hrs · 23,707 cycles

GALLEY SERVICE DOOR , EXTERNAL OUTER HANDLE ASSEMBLY HAS GROOVE WORN INTO HOUSING AND OUTER SKIN. (C-CHECK) RO: 06/01/2019 REMOVED AND REPLACED SERVICE DOOR HANDLE HOUSING WITH NEW IAW SRM AND REO.

Part: CONTROL ROD — OUT OF RIG (ELEVATORS) · airframe 32,023 hrs · 23,386 cycles

ON CLIMB WE RECEIVED ELEVATOR SPLIT CAUTION FOLLOWED SOON AFTER BY AP TRIM AND CAS MISCOMP. WE RAN THE QRH AND RETURNED TO THE FIELD. REMOVED HARDWARE FROM ALL LH AND RH MECHANICAL CONTROL PATH LOCATIONS FOR THE ELEVATOR. RE-RIGGED THE LH AND RH UPPER CONTROL RODS ON THE ELEVATOR QUADRANT AND THE LH LOAD LIMITER. ALL WORK PERFORMED IAW AMM. SAFETIED ALL FOREMENTIONED COMPONENTS IAW AMM. OPS CHECK GOOD AT THIS TIME. PASSED FUNCTIONAL FLIGHT.

Part: FRAME — CORRODED (BS 310) · corrosion level 2 · airframe 30,454 hrs · 22,100 cycles

BS 310 FRAME IS CORRODED BETWEEN STRINGERS 26L AND 25R ON FWD AND AFT SIDE OF WEB. REPAIRED THE FRAME IAW REO 670-53-21-799, REV A, AND EC/TC 670-53-21-799 01.

Part: PLATE — CORRODED (DOOR STEP) · corrosion level 2 · airframe 30,454 hrs · 22,100 cycles

SERVICE DOOR STEP PLATE IS CORRODED. REMOVED AND REPLACED THE SERVICE DOOR STEP PLATE IAW SRMS 51-40-11-001-001-A01, 51-42-02-001-001-A01, AND 51-42-06-001-001-A01.

Part: FITTING — WORN (NLG DOOR) · airframe 30,454 hrs · 22,100 cycles

NLG AFT DOOR HAS EXCESSIVE LATERAL AND LONGITUDINAL PLAY GREATER THAN 0.100. REMOVED AND REPLACED THE LT AND RT AFT NLG DOOR FITTINGS IAW EC/TCS EO 700-32-20-00006, AND EO 700-32-20-00007.

Part: DOUBLER — CORRODED (BS 295-310) · airframe 30,454 hrs · 22,100 cycles

ANTENNA DOUBLER BETWEEN BS 310 AND 295, STRINGER 27 IS CORRODED AROUND ANTENNA CONNECTION. REMOVED AND REPLACED THE DOUBLER IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-25-21-001-001-A01, AND 51-21-00-001-001-A01.

Part: HINGE — DAMAGED (PAX DOOR) · airframe 30,454 hrs · 22,100 cycles

PASSENGER DOOR HINGE RETAINING PIN HOLE ON DOOR SIDE IS DAMAGED. REPAIRED THE DOOR HINGE IAW REO 670-53-11-1000, REV A, AND EC/TC REP 670-52-11-1000.

Part: FRAME — CORRODED (BS 319) · corrosion level 2 · airframe 30,454 hrs · 22,100 cycles

BS 319 FRAME IS CORRODED AT STRINGER 26R. REPAIRED THE FRAME IAW REO 670-53-21-799, REV A, AND EC/TC REO 670-53-21-799 02.

Part: FRAME — CORRODED (BS 295) · airframe 30,454 hrs · 22,100 cycles

BS 295 FRAME IS CORRODED BETWEEN STRINGERS 25R AND 24L ON FWD AND AFT SIDE OF FRAME WEB. REPAIRED THE FRAME IAW REO 670-53-21-799, REV A, EC/TC 670-53-21-799, REO 670-53-21-1494, REV, AND EC/TC 670-53-21-1494.

Part: FRAME — CORRODED (BS 319) · corrosion level 2

FRAME SECTOR CORRODED AT BS 319.70, BETWEEN STRINGERS 18L AND 21L. REMOVED AND REPLACED THE FRAME SECTION IAW SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.

Part: DOOR SILL — CORRODED (PAX DOOR) · airframe 30,454 hrs · 22,100 cycles

PASSENGER DOOR BACK UP SILL FROM BS 310 - 349, STRINGER 21L IS CORRODED. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.

Part: HINGE — CHAFED (PAX DOOR) · airframe 30,454 hrs · 22,100 cycles

PASSENGER DOOR HINGE AFT LUG LANDING ON FUSELAGE SIDE IS CHAFED FROM RETAINING PIN. REPAIRED THE DOOR HINGE IAW REO 670-53-21-582, AND EC/TC REO 670-53-21-582.

Part: DOOR SILL — CORRODED (MAIN PAX) · airframe 30,454 hrs · 22,100 cycles

PASSENGER DOOR LOWER SILL IS CORRODED. REMOVED AND REPLACED THE DOOR SILL.

Part: TRU — SHORTED (NR 2) · airframe 29,839 hrs · 21,612 cycles

PILOT REPORTED A STRONG BURNED INSULATION ODOR FORWARD AREA OF AIRCRAFT. MX REMOVED AND REPLACED THE NR 2 TRU, OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,868 hrs · 20,886 cycles

DURING SCHEDULED MX THE EMERGENCY LIGHT AT THE EXIT ROW WAS FOUND INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK, AND OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 28,176 hrs · 20,361 cycles

CORROSION FOUND ON FLOORBEAM 27 LBL FS 1031. REPAIR ACCOMPLISHED PER EO 700-53-10-00008 REV 0 FLOORBEAM REPAIR FS 977-1037 LBL 27.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 28,176 hrs · 20,361 cycles

CORROSION FOUND ON FLOORBEAM LBL 9 FS 1031. REPAIR ACCOMPLISHED PER EO 700-53-10-00007 REV 0 FLOORBEAM REPAIR AT FS 1010-1037 LBL 9 KBA670-36100-S43 REV 0 BULKHEAD AND LAV ATTACHMENTS INSTL.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 28,176 hrs · 20,361 cycles

CRACKED FLOORBEAM AT FS 280 RT SIDE. REPAIR ACCOMPLISHED PER REO 670-53-11-1229 REV 0 REPAIR TO CROSSBEAM.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 26,152 hrs · 18,731 cycles

ROW 16 CEILING EXIT LIGHT INOPERATIVE. INSTALLED A LAMP IN ROW 16 CEILING EXIT IAW AMM 33-24-07, OPS CHECK GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 26,152 hrs · 18,731 cycles

12AB LOWER EXIT SIGN HAVE 1 LIGHT BULB BURNED. R & R 12AB LOWER EXIT SIGN BULB AS REQUIRED. OPS CHECK GOOD IAW AMM 33-51-00

Part: LIGHT — INOPERATIVE · airframe 25,619 hrs · 18,313 cycles

F/A EMERGENCY LIGHT WILL NOT TURN ON. SYS SELF RESET FAULT NO LONGER EXIST IAW NO FURTHER ACTION IS REQUIRED.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 25,587 hrs · 18,286 cycles

12AB LOWER EXIT SIGN 1 LIGHT BULB BURNED. REPLACED THE BULBS IAW AMM 33-51-11, OPS CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 25,587 hrs · 18,286 cycles

ROW 15 EMERGENCY CEILING LIGHT BULB BURNED. REPLACED THE BULB IAW AMM 33-51-09. OPS CHECKED GOOD.

Part: WARNING LIGHT — INTERMITTENT (COCKPIT) · airframe 24,679 hrs · 17,543 cycles

EMERGENCY LIGHTS ON STATUS INTERMITTENTLY IN FLIGHT. LIGHTS DID NOT ACTUALLY COME ON. COULD NOT DUPLICATE FAULT, OPS CHECKED GOOD. IAW AMM 33-51-00.

Part: FRAME — CORRODED (BS 280) · airframe 24,637 hrs · 17,510 cycles

FRAME BS 280 FOUND CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01.

Part: ACCESS PANEL — GOUGED (TE FLAP) · airframe 24,633 hrs · 17,506 cycles

ON THE L/E OF PANEL 584EB, THERE IS A 1" GOUGE. REMOVED DAMAGE TO PANEL 584EB IAW SRM 57-52-1-101-001-A01. BLENDED AREA IS OUT OF ALLOWABLE LIMITS IAW SRM 57-52-01-101-001-A01 PERFORMED EDDY CURRENT INSPECTION OF PANEL 584EB IAW NDTM PT 1 51-20-006-250-A01.

Part: ACCESS PANEL — GOUGED (TE FLAP) · airframe 24,633 hrs · 17,506 cycles

ON PANEL 584GB L/E THERE IS A ONE INCH GOUGE. REMOVED DAMAGE ON FLAP ACCESS PANEL 584GB IAW SRM 57-52-01-101-001-A01. BLENDED AREA IS OUT OF ALLOWABLE LIMITS IAW SRM 57-52-01-101-001-A01.

Part: INTERCOSTAL — CRACKED (RT WING) · airframe 24,633 hrs · 17,506 cycles

RT WING INBD FIXED L/E INTERCOSTAL CRACKED. RECEIVED AND COMPLIED WITH EA 25-2015-159 (P1). RECEIVED FINAL DISPOSITION OF STS EA 25-2015-159, DATED 5-22-15. COMPLIED WITH STS EA 25-2015-159, DATED 5-22-15. RECEIVED AND COMPLIED WITH ECTC EA 25-2015-159.

Part: SEAT TRACK — CORRODED (BS 380-480) · airframe 24,633 hrs · 17,506 cycles

LT SIDE SEAT TRACK BS 380-480 HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-401-000-801 AND AMM 53-00-49-400-801, A03.

Part: SEAT TRACK — CORRODED (BS 708-761) · airframe 24,633 hrs · 17,506 cycles

LT SIDE SEAT TRACK BS 708-761 HAS CORROSION. R & R THE SEAT TRACK IAW AMM 53-00-49-000-801-A03 AND 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 370-790) · airframe 24,633 hrs · 17,506 cycles

SEAT TRACK AT LBL 9, BS 370-490 HAS CORROSION. FOUND BEYOND LIMITS IAW REO 670-53-00-013. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 A03 AND 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 485-585) · airframe 24,633 hrs · 17,506 cycles

SEAT TRACK AT LBL9, BS 485-585 HAS CORROSION. CORRODED BEYOND LIMITS IAW REO 670-53-00-013. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 53-00-49-000-801-A03, ECTC REO 670-53-00-343, GREO 67-53-00-343, AND AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 480-565) · airframe 24,633 hrs · 17,506 cycles

RT SIDE SEAT TRACK BS 480-565 HAS CORROSION. R & R CORRODED BEYOND LIMITS IAW REO 670-53-00-013. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801, A03 AND 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 585-690) · airframe 24,633 hrs · 17,506 cycles

SEAT TRACK AT RBL 9, BS 585-690 HAS CORROSION. R & R THE SEAT TRACK IAW AMM 53-00-49-000-801 CONFIG A03, AND 53-00-49-400-801, CONFIG A03.

Part: SEAT TRACK — CORRODED (BS 830-1000) · airframe 24,633 hrs · 17,506 cycles

SEAT TRACK AT RBL 9, BS 830-1000 IS CORRODED. R & R SEAT TRACK IAW AMM 53-00-49-000-801-A03 AND 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 785-863) · airframe 24,633 hrs · 17,506 cycles

LT SIDE SEAT TRACK BS 785-863 IS CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03 AND AMM 53-00-49-400-801, CONFIG A03.

Part: SEAT TRACK — CORRODED (BS 485-585) · airframe 24,633 hrs · 17,506 cycles

SEAT TRACK AT LBL 27, BS 485 - 585 HAS CORROSION. FOUND CORRODED BEYOND LIMITS IAW REO 670-53-00-013. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 A03 AND 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 708-761) · airframe 24,633 hrs · 17,506 cycles

RT SIDE SEAT TRACK BS 708-761 HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 AND AMM 53-00-49-400-801A-03.

Part: SEAT TRACK — CORRODED (BS 677-847) · airframe 24,633 hrs · 17,506 cycles

SEAT TRACK AT RBL 9, BS 677-847 IS CORRODED. R & R THE SEAT TRACK IAW AMM 53-00-49-000-801-A03, AND 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 565-677) · airframe 24,633 hrs · 17,506 cycles

RT SIDE SEAT TRACK FS 565-677 HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03, AND AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 485-585) · airframe 24,633 hrs · 17,506 cycles

SEAT TRACK AT RBL9, BS 485-585 HAS CORROSION. R & R THE SEAT TRACK IAW AMM 53-00-49-000-801-A03, AND 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 379-480) · airframe 24,633 hrs · 17,506 cycles

RT SIDE SEAT TRACK BS 379-480 HAS CORROSION. FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013, REV J. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801, AND AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 480-575) · airframe 24,633 hrs · 17,506 cycles

LT SIDE SEAT TRACK BS 480-575 HAS CORROSION. FOUND CORRODED BEYOND LIMITS IAW REO 670-53-00-013. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 A03 AND 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 575-674) · airframe 24,633 hrs · 17,506 cycles

LT SIDE SEAT TRACK BS 575-674 HAS CORROSION. R & R THE SEAT TRACK IAW AMM 53-00-49-000-801 A03 AND AMM 53-00-49-400-801 A03.

Part: SEAT TRACK — CORRODED (BS 785-863) · airframe 24,633 hrs · 17,506 cycles

RT SIDE SEAT TRACK BS 785-863 IS CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 AND AMM 53-00-49-400-801-031.

Part: SEAT TRACK — CORRODED (BS 674-712) · airframe 24,633 hrs · 17,506 cycles

RT SIDE SEAT TRACK BS 674-712 HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03 AND AMM 53-00-49-401-801-A03.

Part: SEAT TRACK — CORRODED (BS 674-712) · airframe 24,633 hrs · 17,506 cycles

LT SIDE SEAT TRACK BS 674-712 HAS CORROSION. R & R THE SEAT TRACK IAW AMM 53-00-49-000-801-A03 AND 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 830-1000) · airframe 24,633 hrs · 17,506 cycles

LBL 9 SEAT TRACK BS 830-1000 IS CORRODED. R & R SEAT TRACK IAW AMM 53-00-49-400-801-A03, AND 53-00-49-000-801-A03.

Part: SEAT TRACK — CORRODED (BS 863-969) · airframe 24,633 hrs · 17,506 cycles

LT SIDE SEAT TRACK BS 863-969 IS CORRODED. R & R THE SEAT TRACK IAW AMM 53-00-49-000-801, CONFIG A03.

Part: SEAT TRACK — CORRODED (BS 677-847) · airframe 24,633 hrs · 17,506 cycles

SEAT TRACK LBL 9, BS 677-847 IS CORRODED. R & R THE SEAT TRACK IAW AMM 53-00-49-000-801-A03, 53-00-49-400-801-A03.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 24,633 hrs · 17,506 cycles

LOWER FLOORBOARD SUPPORT AT FS 280.00 HAS CORROSION DAMAGE THAT NEED TO BE EVALUATED. CORROSION OUT OF LIMITS, R & R SUPPORT ANGLE. REMOVED LOWER FLOORBOARD SUPPORT AT FS 280 IAW SRM 51-42-06-001-001-A01. LOCATED & DRILLED NEW FLOOR SUPPORT IAW SRM 51-40-11-001-001-A01. INSTALLED NEW FLOOR SUPPORT AT FS 280 IAW SRM 51-42-21-001-001-A01 & 51-42-15-001-001-A01.

Part: RIVET — DAMAGED (COCKPIT DOOR) · airframe 24,633 hrs · 17,506 cycles

BOTTOM OF LT COCKPIT DOOR POST IS CORRODED AND HAS RIVET HEAD MISSING BLENDED CORROSION ON BOTTOM LT COCKPIT DOOR POST IAW SRM 51-21-06-001-001-A01. REMOVED POST ANGLE BRACKET TO FOM IAW SRM 51-42-13-001-001-A01. INSTALLED NEW ANGLE BRACKET IAW EA 32-2015-203.

Part: FLOOR SUPPORT — CORRODED (BS 280-319) · airframe 24,633 hrs · 17,506 cycles

RT FLOOR SILL AT FS280-319 IS CORRODED. REMOVED RT FLOOR SILL AT FS280 -319 IAW SRM 51-42-06-001-001-A01. DRILLED & LOCATED NEW SERVICEABLE RT FLOOR SILL FS 280-319 IAW SRM 51-42-06-001-001-A01 & DWG SH670-32170. FINISHED INSTALLATION OF RT FLOOR SILL FS 280-319 IAW SRM 51-42-21-001-001 & DWG NR SH670-32170.

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 24,633 hrs · 17,506 cycles

SCRATCH ON FUSELAGE JUST FWD OF AFT CARGO DOOR. COMPLIED WITH EC/TC EA 32-2015-200 PERMANENT REPAIR. BLENDED AND REMOVED SCRATCH IAW SRM 51-12-00-001-001-A01.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 23,042 hrs · 16,297 cycles

EXTERIOR EMERGENCY LIGHT LENS AT AFT SERVICE DOOR IS BROKEN. REPLACED LENS IAW AMM 33-51-15.

Part: RETAINER — DAMAGED (CARGO DOOR SEAL) · airframe 21,724 hrs · 15,319 cycles

FWD CARGO DOOR SEAL RETAINER DAMAGED. COMPLIED WITH EC/TC REO 670-52-35-127. MAJOR REPAIR IAW GMM5-3.

Part: DOOR — UNKNOWN (PAX) · airframe 21,149 hrs · 14,908 cycles

MAIN ENTRANCE DOOR DIFFICULT TO OPEN FROM OUTSIDE. PERFORM OPS CHECK IAW AMM 52-11-00. OPS CHECKED GOOD. OK FOR SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 20,017 hrs · 14,076 cycles

FLOOR SUPPORT IS CORRODED. REMOVED FLOOR SUPPORT AT BS 280 IAW SRM 51-42-06-001-001-A01. LOCATED AND DRILLED FLOOR SUPPORT IAW SRM 51-40-11-001-001-A01. INSTALLED FLOOR SUPPORT IAW SRM 51-42-21-001-001-A01 AND 51-42-06-001-001-A01.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 20,015 hrs · 14,075 cycles

PAX DOOR AFT DRAG ANGLE CRACKED AT CABLE PULLEY BRACKET AREA. R & R DRAG ANGLE IAW SRM 51-42-06-001-001 & SRM 51-42-13-001-001. LOCATED FASTNER HOLES OF DRAG ANGLE IAW SRM 51-40-11-001-001-A01 AND DWG 601R31702.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 20,015 hrs · 14,075 cycles

CORROSION AROUND FASTENER HOLE AND ON INBD EDGE OF TOP SURFACE ON ASD LOWER SILL FWD CAP ANGLE LOCATED AND DRILLED FASTNER HOLES AND INSTALLED NUTPLATE IAW SRM 51-40-11-001-001-A01 AND 51-45-00-001-001-A01 AND 51-42-06-001-001-A01. INSTALLED IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. MAJOR REPAIR.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 20,015 hrs · 14,075 cycles

CORROSION AROUND FASTNER HOLE AND ON INBD & AFT EDGE OF TOP SURFACE ON ASD LOWER SILL AFT CAP ANGLE. REPLACED AFT CAP ANGLE IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 485-570) · airframe 20,015 hrs · 14,075 cycles

LEFT SIDE SEAT TRACK CORRODED FROM BS 485 TO 570. R & R SEAT TRACK IAW AMM 53-00-49-000-801 & 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 785-797) · airframe 20,015 hrs · 14,075 cycles

RT SIDE SEAT TRACK CORRODED FROM APPROX FS 785 TO 797. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED NEW SERVIEABLE SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 581-661) · airframe 20,015 hrs · 14,075 cycles

RT SIDE SEAT TRACK CORRODED FROM APPROX FS 581-661. R & R WITH SERVICABLE SEAT TRACK AT RT SIDE FS 581-661 IAW AMM 53-00-49-000-801 AND 53-00-49-400-801.

Part: FLOOR SUPPORT — CORRODED (BS 319) · airframe 20,015 hrs · 14,075 cycles

FLOOR SUPPORT CORRODED AT FS 319 AT RBL 45. REMOVED FLOOR SUPPORT AT RBL 45, FS 280-319 IAW SRM 51-42-06-001-001-A01 & 51-41-02-001-001-A01. LOCATED & DRILLED NEW FLOOR SUPPORT AT RBL 45 FS 280 - 319 IAW SRM 51-40-11-001-001-A01. INSTALLED FS 280-319 RT FLOOR SUPPORT AT RBL 45 IAW SRM 51-42-06-001-001.

Part: SEAT TRACK — CORRODED (BS 870-875) · airframe 20,015 hrs · 14,075 cycles

RT SIDE SEAT TRACK CORRODED FROM APPROX FS 870 TO 875. R & R WITH SERVICEABLE SEAT TRACK AT RT SIDE FS 870 TO 875 IAW AMM 53-00-49-000-801 & 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 570-675) · airframe 20,015 hrs · 14,075 cycles

LT SIDE SEAT TRACK CORRODED FROM APPROX FS 570 TO 675. REMOVED LT SEAT TRACK IAW AMM 53-00-49-000-801. REPLACED LT SIDE SEAT TRACK AT FS 573-661 IAW AMM 53-00-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 581-681) · airframe 20,015 hrs · 14,075 cycles

LBL 9 SEAT TRACK CORRODED FROM FS 581 TO 681. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 860-875) · airframe 20,015 hrs · 14,075 cycles

LT SIDE SEAT TRACK CORRODED FROM APPROX FS 875 TO 860. R & R SEAT TRACK IAW AMM 53-00-49-000-801 AND 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 675-712) · airframe 20,015 hrs · 14,075 cycles

LT SIDE SEAT TRACK CORRODED THREE SPOTS FROM APPROX FS 675 TO 712. SEAT TRACK IAW AMM 53-00-49-000-801 AND 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 490-555) · airframe 20,015 hrs · 14,075 cycles

RT SIDE SEAT TRACK CORRODED FROM FS 490 TO 555. R & R WITH SERVICEABLE SEAT TRACK IAW AMM 53-00-49-000-801 & 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 712-761) · airframe 20,015 hrs · 14,075 cycles

LT SIDE SEAT TRACK CORRODED FROM APPROX FS 712 TO 761. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 873-977) · airframe 20,015 hrs · 14,075 cycles

LT SIDE SEAT TRACK CORRODED FROM APPROX FS 873 TO 977. R & R WITH SERVICEABLE SEAT TRACK IAW AMM 53-00-49-000-801 & 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 724-761) · airframe 20,015 hrs · 14,075 cycles

RT SIDE SEAT TRACK CORRODED FROM APPROX FS 724-761. R & R RT SIDE SEAT TRACKAT FS 724 WITH SERVICABLE IAW AMM 53-00-49-000-801 AND 53-00-49-400-801.

Part: SKIN — CORRODED (BS 300) · airframe 20,015 hrs · 14,075 cycles

SKIN UNDER TCAS ANTENNA AT APPROX FS300 CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001, REO 670-53-21-952 AND REO 670-53-21-952.

Part: INTERCOSTAL — CORRODED (BS 364) · airframe 20,015 hrs · 14,075 cycles

INTERCOSTAL CORRODED AT S26R FS 364. REMOVED DAMAGED INTECOSTAL, LOCATED & DRILLED NEW INTERCOSTAL IAW SRM 51-42-06-001-001-A01. INSTALLED NEW INTERCOSTAL IAW SRM 51-42-06-001-001-A01. MAJOR REPAIR.

Part: DOUBLER — CORRODED (BS 295-310) · airframe 20,015 hrs · 14,075 cycles

ANTENNA DOUBLER BETWEEN FS 295 & 310 AT STR 27 CORRODED. REMOVED CORRODED DOUBLER IAW SRM 51-42-06-001-001 DRILLED NEW DOUBLER IAW SRM 51-40-11-001-001. INSTALLED ANTENNA DOUBLER AT FS 295-310 STGR 27 IAW SRM 51-42-06-001-001.

Part: FRAME — CORRODED (BS 310) · airframe 20,015 hrs · 14,075 cycles

CORROSION ON FRAME 310 FWD SIDE AT S27. REPAIRED IAW SRM 51-21-06-001-001-A01 AND REO 670-53-21-949.

Part: FRAME — CORRODED (BS 310) · airframe 20,015 hrs · 14,075 cycles

CORROSION ON FRAME BS 310 STR 27. REPAIRED IAW SRM 51-21-06-001-001-A01 AND REO 670-53-21-949.

Part: FITTING — CORRODED (FUSELAGE) · airframe 20,015 hrs · 14,075 cycles

NOSE JACK FITTING LEFT SUPPORT INTERCOSTAL CORRODED ON SKIN ATTACH FLANGE. REMOVED CORROSION ON NOSE JACK FITTING INTERCOSTAL IAW SRM 51-21-06-001-001-A01 AND REO 670-53-11-834.

Part: SILL — CORRODED (FUSELAGE) · airframe 20,015 hrs · 14,075 cycles

AFT CARGO DOOR SILL HAS CORROSION IN SEVERAL PLACES. REPAIRED IAW SRM 51-21-06-001-001-A01 AND GREO 670-53-61-913.

Part: RISER — CRACKED (STEP) · airframe 20,015 hrs · 14,075 cycles

STEP RISER CRACKED ON AFT SIDE OF ASD. REMOVED ASD AFT RISER PANEL RECEIVED & DRILLED UP NEW PANEL FOR STIFFNERS REF SRM 51-42-06-001-001 & SRM 51-40-11-001-001. INSTALLED THE RISER PNL IAW SRMS 51-42-13-001-A01 AND 51-42-03-001-001-A01. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW ASA SOP 5702.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 20,015 hrs · 14,075 cycles

FS 280 CROSSBEAM CORRODED CENTER SECTION. REMOVED, FABRICATED AND REPLACED LT/RT BEAM SECTIONS, BEAM SPLICE DOUBLERS BEAM BACK-UP ANGLES (LT/RT FWD OF FS 280 LT/RT TI DOUBLERS IAW SRM 51-42-06-001-001-A01, 51-42-10-001-001-A01, 51-42-21-0001-001-A01, 51-42-22-001-001-A01. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW ASA SOP 5702.

Part: FLOOR SUPPORT — CORRODED (BS 349) · airframe 20,015 hrs · 14,075 cycles

FLOOR SUPPORT CORRODED AT FS 349 RBL45. REPAIRED FLOOR SUPPORT IAW SRM 51-21-06-001-001-A01 AND REO 670-53-21-946 IAW NDTM PART 1, 51-20-006.

Part: FLOOR SUPPORT — CORRODED (BS 310-349) · airframe 20,015 hrs · 14,075 cycles

SERVICE DOOR ACCESS FLOOR SUPPORT ANGLE CORRODED AT FS 310-349. R & R LOWER SERVICE DOOR SUPPORT ANGLE AND SIX ATTACH BRACKETS IAW SRM 51-42-06-001-001-A01, 51-41-02-001-001-A01 AND 51-40-11-001-001-A01.

Part: FRAME — CORRODED (BS 295) · airframe 20,015 hrs · 14,075 cycles

CORROSION ON FRAME AT FS 295 AFT SIDE BETWEEN STR 26L & 25R. REPAIRED IAW SRM 51-21-06-001-001-A01 AND REO 670-53-21-950.

Part: INTERCOSTAL — CORRODED (BS 364) · airframe 20,015 hrs · 14,075 cycles

INTERCOSTAL AT FS 364, STR 27R CORRODED. REMOVED DAMAGED INTECOSTAL, LOCATED & DRILLED NEW INTERCOSTAL IAW SRM 51-42-06-001-001-A01. INSTALLED NEW INTERCOSTAL IAW SRM 51-42-06-001-001-A01. MAJOR REPAIR

Part: FRAME — CORRODED (BS 280) · airframe 20,015 hrs · 14,075 cycles

CIRCUMFERENTIAL JOINT AT FS 280 HAS CORROSION AT STR 27. REPAIRED IAW SRM 51-21-06-001-001-A01 AND REO 670-53-21-951.

Part: FRAME — CORRODED (BS 310) · airframe 20,015 hrs · 14,075 cycles

CORROSION ON FRAME 310 FWD SIDE AT STR 26R. REPAIRED IAW SRM 51-21-06-001-001-A01 AND REO 670-53-21-949.

Part: FRAME — CORRODED (BS 349) · airframe 20,015 hrs · 14,075 cycles

FRAME BS 349, CORROSION ON AFT SIDE FROM STR 26R-26L. R & R FRAME IAW SRM 51-42-06-001-001.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 20,014 hrs · 14,074 cycles

INTERCOSTAL CRACKED AT PANEL 832BR ON ASD. REMOVED INTERCOSTAL AND ATTACH BRACKETS IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. LOCATED, DRILLED AND DEBURRED NEW INTERCOSTAL IAW SRM 51-40-11-001-001-A01. INSTALLED OF THE INTERCOSTAL IAW SRM 51-42-06-001-001-A01.

Part: INTERCOSTAL — CORRODED (BS 364 S27L) · airframe 20,015 hrs · 14,075 cycles

INTERCOSTAL AT FS 364, STR 27L CORRODED. REMOVED DAMAGED INTERCOSTAL, LOCATED & DRILLED NEW INTERCOSTAL IAW SRM 51-42-06-001-001-A01. INSTALLED NEW INTERCOSTAL IAW SRM 51-42-06-001-001-A01.

Part: FRAME — CORRODED (BS 295) · airframe 20,015 hrs · 14,075 cycles

CORROSION ON FRAME 295 FWD SIDE BETWEEN STR 26 & 27L. REPAIRED IAW SRM 51-21-06-001-001-A01 AND REO 670-53-21-950.

Part: WEB — CORRODED (BS 280) · airframe 20,015 hrs · 14,075 cycles

FS 280 LT WEB CORRODED. R & R FS 280 LT WEB. REPAIRED IAW REO 670-53-11-594.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 20,015 hrs · 14,075 cycles

THREE SUPPORT ANGLES CORRODED ON SERVICE DOOR THRESHOLD BRACKETS. REMOVED ANGLES IAW SRM 51-42-06-001-001-A01. LOCATED DRILLED AND DEBURRED PARTS IAW RM 51-40-11-001-001-A01. INSTALLED SUPPORT ANGLES IAW SMR 51-42-06-001-001-A01.

Part: FRAME — CORRODED (BS 319 S26L) · airframe 20,015 hrs · 14,075 cycles

CORROSION ON FRAME 319.70 FWD SIDE STR 26L. REPAIRED IAW SRM 51-21-06-001-001-A01 AND REO 670-53-21-948.

Part: STIFFENER — CRACKED (PAX DOOR) · airframe 20,014 hrs · 14,074 cycles

ASD MOTOR SUPPORT STIFFENER IS CRACKED. REMOVED STIFFENER. RECEIVED AND DRILLED UP NEW STRIFFENER AND INSTALLED REF SRM 51-42-06-001-001 AND SRM 51-40-11-001-001. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW ASA SOP 5702.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 20,015 hrs · 14,075 cycles

FLOOR SUPPORT ANGLE AT FS 280 CORRODED. REMOVED CORRODED ANGLE. LOCATED AMD DRILLED ANGLE IAW SRM 51-40-11-001-001-A01. INSTALLED ANGLE IAW SRM 51-42-06-001-001-A01 AND DWG 670-34256.

Part: FLOOR SUPPORT — CORRODED (BS 280) · airframe 20,015 hrs · 14,075 cycles

FLOOR SUPPORT CORRODED AT FS 280, RBL 45. R & R CORRODED AND DAMAGED FLOOR SUPPORT IAW SRM 51-42-06-001-001 IAW SRM 51-42-06-001-001.

Part: FRAME — CRACKED (FUSELAGE) · airframe 20,014 hrs · 14,074 cycles

TRU FLOOR PAN CRACK RT SIDE AFT CORNER OF AFT FRAME OF TRU DOOR OPENING TO SCUPPER OF ADG PUMP. REPAIRED IAW EC/TC REO 670-53-11-509 AND GENERIC REO 670-53-11-509 REV.

Part: ANGLE — CORRODED (FUSLEAGE) · airframe 20,014 hrs · 14,074 cycles

ASD LOWER SILL ANGLE CORRODED AROUND SEVERAL NUTPLATES. REMOVED CORRODED MID CAP ANGLE IAW SRM 51-41-02-001-001. INSTALLED MID CAP ANGLE IAW SRM 51-41-02-001-001-A01.

Part: SILL — CORRODED · airframe 20,014 hrs · 14,074 cycles

ASD LOWER SILL CORRODED SEVERAL PLACES. R & R ANGLES IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 19,161 hrs · 13,493 cycles

EMERGENCY LIGHTS WOULD NOT STAY ON MORE THAN 3 SECONDS WHEN SELECTED ON. RE-CHARGED EMERGENCY LIGHTS IAW AMM 24-32-07. OPS CHECKED GOOD AT THIS TIME.

Part: LIGHT — MISSING (CABIN) · airframe 18,060 hrs · 12,649 cycles

EMERGENCY LIGHT AT 12AB MISSING. REPLACED EMERGENCY LIGHT IAW AMM 33-51-01.

Part: INSULATOR — DAMAGED (OVERHEAT LOOP) · airframe 17,969 hrs · 12,574 cycles

LEFT BLEED DUCT WARNING MESSAGE IN CLIMB. CONTINUED, PRESSURIZED, AND EMERGENCY DECLARED. MDC INDICATES LT BLEED LOOP A OPEN. REPAIRED LT BLEED LOOP A BY REMOVING AND REPLACING CERAMIC INSULATORS ON PLUGS MT139P1 AND MT141P1 OF LOOPS MT139 & MT141 IAW AMM 36-21-01. OPS TESTED GOOD NO DEFECTS NOTED.

Part: CONTROLLER — UNSERVICEABLE (ANTI ICE SYSTEM) · airframe 17,962 hrs · 12,568 cycles

LEFT BLEED DUCT WARNING MESSAGE IN FLIGHT. LOST CABIN PRESSURE. DECLARED AN EMERGENCY. ACFT RETURNED TO DEPARTURE. R & R ANTI-ICE CONTROLLER IAW 30-12-12 PERFORMED SUCCESSUL OPS CHECK. PERFORMED OPS CHECK OF THE LT PACK IAW AMM 21-51-00, REF 30-12-12 ITEM NR 5. NO FURTHER DEFECTS NOTED. ACFT OK FOR SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (LT BLEED) · airframe 17,693 hrs · 12,376 cycles

LEFT BLEED DUCT WARNING, FOLLOWED QRH PROCEDURES ACFT RETURNED TO DEPARTURE, EMERGENCY DECLARED. PERFORMED LEAK TEST, INSPECTION AND CONTINUITY CHECK OF LT BLEED AIR SYS AND LT BLEED LOOP B IAW FIM TASK 36-21-01 AND AMM 36-10-00. LEAK TESTED GOOD. OPS CHECKED GOOD. NO DEFECTS FOUND AT THIS TIME.

Part: CONTROLLER — INOPERATIVE (LT BLEED SYS) · airframe 17,470 hrs · 12,215 cycles

LEFT BLEED WARNING, ACFT RETURNED TO DEPARTURE AFTER T/O. EMERGENCY DECLARED. R & R AILC IAW AMM 30-12-12, OPS CHECKED GOOD.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 17,235 hrs · 12,053 cycles

F/A MEGAPHONE INOPERATIVE. REPLACE MEGAPHONE.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 17,235 hrs · 12,053 cycles

MEGAPHONE INOPERATIVE. REPLACED MEGAPHONE IAW AMM 25-61-05.

Part: UNKNOWN — ODOR (CABIN) · airframe 16,928 hrs · 11,845 cycles

STRONG ODOR OF EXHAUST FUMES IN CABIN IN FLIGHT AND ON GROUND. OPS CHECKED LT PACK IAW AMM 21-51-00-710-801. CHECKED GOOD. OK FOR SERVICE.

Part: LIGHT — SEPARATED (CABIN) · airframe 16,658 hrs · 11,652 cycles

EMERGENCY LIGHT SEPARATED AFT OF RT EMERGENCY EXIT. R & R FLOOR EMERGENCY LIGHT IAW AMM 33-51-01.

Part: PRECOOLER — FAILED (BLEED DUCT) · airframe 16,128 hrs · 11,275 cycles

LEFT BLEED DUCT WARNING MESSAGE IN FLIGHT., ACFT DIVERTED, EMERGENCY DECLARED. R & R LT PRE-COOLER ASSY IAW AMM 21-53-04. R & R T DUCT IAW AMM 21-61-12. ALL OPS AND LEAK CHECKED GOOD.

Part: CONTROLLER — FAILED (BLEED SYS) · airframe 15,955 hrs · 11,158 cycles

LEFT BLEED DUCK WARNING MESSAGE CAME COME ON DURING CLIMBOUT. LANDING RATE LESS THAN 200 FPM. (ACFT RETURNED AFTER T/O -- EMERGENCY DECLARED AS A PRECAUTION) R & R IAW AMM 30-12-12. RUN ENGS OPS CHECK GOOD. (CLOSED)

Part: DOOR — BINDING (MAIN PAX) · airframe 15,853 hrs · 11,085 cycles

PAX DOOR WILL NOT OPEN. PERFORMED OPS CHECK OK AT THIS TIME IAW AMM 52-11-00. ACFT OK FOR SERVICE.

Part: MEGAPHONE — WEAK (CABIN) · airframe 15,517 hrs · 10,853 cycles

F/A REPORTS MEGAPHONE IS WEAK. REPLACED MEGAPHONE BATTERY. OPS CHECKED GOOD IAW AMM 25-61-14.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,474 hrs · 10,820 cycles

RT NR 5 SIDEWALL SEAT TRACK CORRODED. BLENDED SEAT TRACK AND FOUND TO BE IN LIMITS IAW SRM 53-51-49.

Part: SEAT TRACK — GOUGED (CABIN) · airframe 15,474 hrs · 10,820 cycles

RT 7 SIDEWALL SEAT TRACK GOUGED. R & R RT NR 7 SIDEWALL SEAT TRACK IAW REO 670-53-00-314 AND 670-53-00-074 THIS IS CONSIDERED A MAJOR REPAIR RII FOUND TO BE SATISFACTORY.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,474 hrs · 10,820 cycles

RT NR 6 SIDEWALL SEAT TRACK HAS CORROSION DAMAGE. R & R SEAT TRACK IAW REO 670-53-00-314. MAJOR REPAIR.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 15,474 hrs · 10,820 cycles

PAX DOOR AFT INTERCOSTAL CLOSE TO DOOR HINGE IS CRACKED IN RADIUS. REMOVED INTERCOASTAL AND INSTALLED SERVICEABLE AFT INTERCOASTAL IAW SRM 51-42-06 AND SRM 51-42-21. MAJOR REPAIR.

Part: PLACARD — DETERIORATED (CABIN) · airframe 15,474 hrs · 10,820 cycles

PAX DOOR "EXIT" PLACARD ON 2ND STEP IS DETERIORATED. R & R PLACARD IAW AMM 20-60-04.

Part: STEP — CORRODED (PAX DOOR) · airframe 15,474 hrs · 10,820 cycles

CORROSION BY PAX DOOR UPPER STEP ON AFT STAIR WEB. REMOVED CORROSION IAW SRM 51-11-04. MINOR REPAIR.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,474 hrs · 10,820 cycles

LT NR 6 SIDEWALL SEAT TRACK HAS CORROSION DAMAGE. REMOVED CORROSION FROM SEAT TRACK AND FOUND TO BE WITHIN REPAIRABLE LIMITS IAW SRM 53-51-49.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,474 hrs · 10,820 cycles

RT NR 4 SIDEWALL SEAT TRACK HAS CORROSION DAMAGE. R & R SEAT TRACK IAW AMM 53-00-49 AND REO 670-53-314. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,474 hrs · 10,820 cycles

LT NR 5 SIDEWALL SEAT TRACK HAS CORROSION DAMAGE. R & R SEAT TRACK IAW REO 670-53-00-314 AND AMM 53-00-49. MAJOR REPAIR.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 15,474 hrs · 10,820 cycles

PAX DOOR AFT DRAG ANGLE CRACKED NEAR ASSIST MOTOR PULLEY. REPAIRED DAMAGED PAX DOOR AFT DRAG ANGLEIAW REO 670-52-11-072. A MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,474 hrs · 10,820 cycles

LT NR4 SIDEWALL SEAT TRACK HAS CORROSION DAMAGE. R & R SEAT TRACK IAW SRM 53-00-49 AND REO 670-53-00-314. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 15,474 hrs · 10,820 cycles

RT NR 1 FLOOR SEAT TRACK CORRODED NUMEROUS AREAS. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801 AND EC/TC REO 670-53-00-314.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 15,474 hrs · 10,820 cycles

LEFT NR 2 FLOOR SEAT TRACK HAS MINOR SURFACE CORROSION IN 2 EA PLACES. REMOVED AND REPLACED LT NR 2 FLOOR SEAT TRACK WITH NEW IAW REO 670-53-00-314. THIS IS A MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,474 hrs · 10,820 cycles

RT NR 3 FLOOR SEAT TRACK CORRODED. REMOVED SEAT TRACK AND REPLACED WITH SERVICABLE SEAT TRACK IAW REO 670-53-00-314 AND EC/TC REO 670-53-00-314. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 15,474 hrs · 10,820 cycles

LT NR 1 FLOOR SEAT TRACK CORRODED AT FWD END. REMOVED SEAT TRACK AND INSTALLED NEW IAW AMM 53-00-49-000-0801.

Part: PLACARD — TORN (ESCAPE HATCH) · airframe 15,474 hrs · 10,820 cycles

CREW ESCAPE HATCH EXTERIOR PLACARDS TORN AND FADED. REMOVED AND INSTALLED SERVICEABLE PLACARDS IAW AMM 20-60-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,474 hrs · 10,820 cycles

RT NR 2 FLOOR SEAT TRACK CORRODED NUMEROUS PLACES. R & R SEAT TRACK IAW AMM 53-00-49 AND REO 670-53-00-314. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 15,474 hrs · 10,820 cycles

LT FS 280 FLOORBEAM CORRODED AROUND FASTENER HOLES. R & R LT SIDE BEAM FS 280.00 WITH NEW IAW SRM 51-42-06, 51-42-13, AND 51-42-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,474 hrs · 10,820 cycles

LT NR 3 FLOOR SEAT TRACK CORRODED. BLENDED MINOR SURFACE CORROSION, REMAINING MATERIAL IS WITHIN SERVICABLE LIMITS IAW SRM 53-21-49.

Part: CIRCUIT BREAKER — TRIPPED (TE FLAPS) · airframe 13,893 hrs · 9,747 cycles

FLAPS FAIL 30 CAUTION, EMERGENCY DECLARED. FLAPS FAIL RESET RESET IAW AMM 05-51-51-970-801-A01 RESET PROCEDURES. AS PER MCC, NO FURTHER ACTION IS REQUIRED.

Part: SOCKET — BROKEN (EMERGENCY LIGHT) · airframe 12,991 hrs · 9,071 cycles

GALLEY 3 FLOOR LEVEL EMERGENCY FLOODLIGHT DS155 LAMP SOCKET IS BROKEN. R & R GALLEY 3 FLOOR LEVEL EMERGENCY FLOOD LIGHT DS155 IAW AMM 33-51-11 OPS GOOD DEFER CLEARED PLACARD REMOVED.

Part: SWITCH — LOOSE (PAX DOOR) · airframe 12,682 hrs · 8,829 cycles

PAX DOOR DIFFICULT TO OPEN. FOUND SWITCH (POWER ASSIST) LOOSE IN SWITCH RETAINER SECURED SWITCH OPS CK GOOD MM 20-41-00 52-11-08.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 12,484 hrs · 8,685 cycles

CAPT'S FLASHLIGHT INOP. REPLACED CAPT'S FLASH LIGHT, OPS CHECK GOOD IAW AMM 25-60-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,659 hrs · 8,066 cycles

AFT GALLEY LOWER EMERGENCY LIGHT INOP.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 11,167 hrs · 7,685 cycles

LOWER WEB ATTACH ANGLE (CC670-34117-6) AT FS 280, RBL 26, CRACKED.

Part: CROSSBEAM — CRACKED (FUSELAGE) · airframe 11,167 hrs · 7,685 cycles

RT 280 CROSSBEAM FOUND CRACKED. REMOVED AND REPLACED.

Part: WEB — CRACKED (FUSELAGE) · airframe 11,167 hrs · 7,685 cycles

LEFT 280 WEB FOUND CRACKED. CORROSION REMOVED PER BLENDING. BLEND WITHIN ALLOWABLE LIMITS. APPLIED A023 FINISH TO BLENDED AREA. ALL WORK ACCOMPLISHED PER SRM.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 11,167 hrs · 7,685 cycles

LT 280 CROSSBEAM CORRODED. REMOVED AND REPLACED.

Part: DRAG ANGLE — CRACKED (FUSELAGE) · airframe 11,167 hrs · 7,685 cycles

LEFT AFT DRAG ANGLE FOUND CRACKED. REMOVED AND REPLACED LT AFT DRAG ANGLE, APPLIED FAY SEAL AND A023 FINISH TO AREA IAW SRM 51-40-11 AND 51-41-02 AND DRAWING BA670-35002.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 11,167 hrs · 7,685 cycles

SEVERAL AREAS MARKED FOR CORROSION AND PAINT MISSING BETWEEN FS 1047 AND AFT EQUIPMENT BAY CUTOUT.

Part: HANDLE — STICKING (EMERGENCY EXIT) · airframe 11,167 hrs · 7,685 cycles

RIGHT OVERWING EMERGENCY EXIT RELEASE HANDLE STICKING.

Part: PLACARD — DAMAGED (ASD) · airframe 11,167 hrs · 7,685 cycles

ASD STEP "EXIT" PLACARD DAMAGED.

Part: LIGHT — FAILED (CABIN) · airframe 9,133 hrs · 6,145 cycles

WITH EMERGENCY LIGHTS SW IN ON POSITION LIGHTS COME ON THEN FADE WITHIN 15-20 SECONDS. FLT 5083 DEL 136 MINS. FLT 4926,4927 CX.

Part: LIGHT — UNKNOWN (CABIN) · airframe 9,133 hrs · 6,145 cycles

REFER TO AFDL 447034-3 EMERGENCY LIGHTS.

Part: LIGHT — UNKNOWN (CABIN) · airframe 9,133 hrs · 6,145 cycles

REFER TO AFDL 447034-3 EMERGENCY LIGHTS.

Part: FADEC — MALFUNCTIONED (RT ENGINE) · airframe 8,809 hrs · 5,894 cycles

DURING DESCENT FROM 22500 TO 12000 @ 300KIAS GOT R FADEC MSG RAN QRH & MONITORED ENGINE INDICATIONS. R ITT WENT TO 932 C. SHUTDOWN R ENGINE. RAN SINGLE ENGINE PROCEDURES CHECK AND LANDED WITH ALL CHECK LIST NO HOT ICON GAUGE TURNED RED. EMERGENCY DECLARED. R&R FUEL METERING UNIT AND FADEC IAW CRJ 700 AMM 733-21-07, 73-21-03 ALL OPS CHECK OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 6,646 hrs · 4,359 cycles

RT LWR EMERGENCY LIGHT AT RT EMERGENCY DOOR DOES NOT COME ON.

Part: TRACK — BROKEN (THRUST REVERSER) · airframe 6,633 hrs · 4,346 cycles

LEFT ENG UPPER INBOARD T/R SLIDER TRACK BROKEN. INSTALLED NEW LT ENG UPPER INBD T/R SLIDER TRACK IAW REO 670-78-34-0293.

Part: WEB — CORRODED (BS 280) · airframe 6,633 hrs · 4,346 cycles

LEFT LOWER FS 280 WEB IS CORRODED. BLENDED MINOR SURFACE CORROSION WITHIN LIMITS TO MAX DEPTH OF.004, TREATED, PRIMED AND PAINTED BLEND OUT IAW REO 670-53-11-052.

Part: WEB — CORRODED (BS 280) · airframe 6,633 hrs · 4,346 cycles

RIGHT LOWER FS 280 WEB IS CORRODED. REMOVED AND REPLACED RT LOWER 280 WEB IAW REO670-53-11-052 REFER TO M-234 MAINTENANCE CONTINUATION LOG STEPS 2-7 FOR WORK ACOMPLISHED.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 6,633 hrs · 4,346 cycles

FS 280 FLOORBEAM IS CRACKED AND CORRODED. WORK DONE IAW IS670-53-11-0026 REFER TO M-234 MAINTENANCE CONTINUATION LOG STEPS 2-26 FOR WORK ACOMPLISHED.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 5,143 hrs · 3,295 cycles

N/W/S INOP MESSAGE DURING FLT. EMERGENCY DECLARED.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 5,079 hrs · 3,251 cycles

AFTER T/O AND SELECTING GEAR RETRACTION GOT A NOSE WHEEL STEERING INOP MSG. EMERGENCY DECLARED.

Part: UNKNOWN — UNKNOWN · airframe 4,941 hrs · 3,157 cycles

UPON GEAR RETRACT -STEERING INOP- CAUTION MSG. MW STG OFF PER CHECK LIST, ON AGAIN IN FLIGHT. RESET UNSUCCESSFUL. UPON LANDING, CYCLES G-2 C/B'S ON P1 AND P2 AND RESET GOOD. EMERGENCY DECLARED. EMERGENCY EQUIPMENT ON STANDBY.

Part: UNKNOWN — INOPERATIVE (NLG STEERING) · airframe 4,827 hrs · 3,082 cycles

AFTER TAKEOFF, GOT NOSE STEERING INOP. FOLLOWED QRH, TURNED STEERING OFF. AFTER LANDING RESET NWS 1-G2, 2-G2. FURTHER OPERATIONS NORMAL. EMERGENCY DECLARED.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 4,056 hrs · 2,610 cycles

WHEN THE EMERGENCY LIGHTS ARE IN THE ARMED POSITION, THE LIGHTS CYCLE ON AND OFF BY THEMSELVES.

Part: CAUTION MESSAGE — ILLUMINATED (FADEC) · airframe 3,605 hrs · 2,290 cycles

RT FADEC FAULT CAUTION (EMERGENCY DECLARED) EN ROUTE TO SLC A/C DIVERTED TO GJT DUE TO MTC.

Part: LIGHT — DAMAGED (CABIN) · airframe 3,390 hrs · 2,161 cycles

FLOOR EMERGENCY LIGHT TRACK DAMAGED THROUGHOUT CABIN