N744EV

Part: NONE — OVERHEATED · airframe 41,219 hrs · 30,321 cycles

BRAKE OVER HEAT MASTER WARNING IN DECENT. COME ON SHOWED 12 ON RIGHT INBOARD THE WENT TO 0, WENT AWAY. CAME BACK ON AT 20. FLOWED QRH STAYED RED 0 ALL THE WAY TO THE GATE. (FLIGHT 3083 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 25769593 WITH THE FOLLOWING CORRECTIVE ACTION: "COULD NOT DUPLICATE FAULT ON GROUND. DUE TO FOUND HISTORY IN THE LAST 30 DAYS. REMOVED AND REPLACED #3 BTMS THERMOCOUPLE SENSOR IAW AMM 32-46-01. OPS CHECK GOOD."

Part: NONE — ODOR · airframe 40,954 hrs · 30,103 cycles

ON APPROACH CREW DETECTED BURNING ELECTRICAL SMELL. AFTER LANDING NOTICED RECIRC FAN FAULT STATUS MESSAGE AND BREAKER 1A5 WAS POPPED. (FLIGHT #3226 FILED CLOSED) COMPLIED WITH FDE SMOKE SMELL IN THE COCKPIT REF CRJ 709 FIM 21-21-00. PERFORMED INSPECTION FOR SMOKE AND FIRE DAMAGE. NONE NOTED. PERFORMED 30 DAY HISTORY SEARCH FOR SMOKE EVENT DISCREPANCIES. NONE NOTED. TROUBLESHOOTING DETERMINED BURNING SMELL CAUSED BY #1 RECIRCULATION FAN. PLEASE REFERENCE AML 959648 FOR RECIRC FAN DEFERRAL.

Part: BATTERY PACK — ODOR (EMERGENCY LIGHTS) · airframe 39,404 hrs · 28,899 cycles

ON APPROACH TO DFW FAS REPORTED FUMES AND A VAGUE ELECTRICAL SMELL FROM ROWS 15 THROUGH 17. ROUGHLY 1 MINUTE LATER THE SMELL DISSIPATED AND WAS NOT PRESENT FOR REMAINDER OF FLIGHT. NO INDICATIONS OF SMOKE IN COCKPIT (FLIGHT 3086 - FILED CLOSED) TROUBLE-SHOT PER FIM 21-22-00-810-806 AND FOUND AED AND #4 EMERGENCY BATTERY PACK AND CHARGER ASSEMBLY TO BE ONLY SOURCED OF FAINT SMELL. REMOVED AND REPLACED #4 EMERGENCY BATTERY PACK AND CHARGER ASSEMBLY IN REFERENCE TO AMM 33-51-17. OPS CHECK GOOD IN REFERENCE TO AMM 33-51-00. AIRCRAFT IS ACCEPTABLE FOR RETURN TO AND CONTINUED SERVICE. / PLEASE REFERENCE AML 748986

Part: SKIN — DAMAGED (LT WING TE FLAP) · airframe 39,083 hrs · 28,685 cycles

LH OB FLAP LOWER SKIN AND TRAILING EDGE DAMAGED BETWEEN FS 254.96 TO FS 262.76 (FILED CLOSED) REPAIRED L/H O/B FLAP LOWER SKIN AND T/E DAMAGE IAW CRJ-700 SRM 57-53-01-201-001-A01 TYPE IV REPAIR. COMPLETED AND ATTACHED SKYWEST STRUCTURAL MAJOR REPAIR TASK 51-900-1002-SKY AND 337. NO WEIGHT CHANGE. REFER TO CONTINUE CARD FOR ALL DETAILS OF REPAIR.

Part: SKIN — DENTED (LT WING) · airframe 39,083 hrs · 28,685 cycles

LH LOWER WING SURFACE PN CC670-10046-5 HAS DENT DAMAGE @ WS 255 BETWEEN STR 11 & 12 (FILED CLOSED) REPAIRED L/H WING LOWER SKIN IAW MHIRJ REO 670-57-21-919 REV. -- DATED 8/6/2021. COMPLETED AND ATTACHED SKYWEST STRUCTURAL MAJOR REPAIR TASK 51-900-1003-SKY AND 337. NO WEIGHT CHANGE. SEE CONTINUE CARD FOR DETAILS.

Part: FLOOR PANEL — CRACKED (COCKPIT) · airframe 37,418 hrs · 27,504 cycles

COCKPIT PANEL 221KLW IS CRACKED. C-CHECK RO 9/27/2020. REMOVED & INSTALLED THE COCKPIT PANEL 221KLW, REF CRJ 700 AMM.

Part: SUPPORT — CRACKED (LT MLG FAIRING) · airframe 37,418 hrs · 27,504 cycles

LT MLG FAIRING DIAPHRAGM ASSY SUPPORT STRUCTURE CRACKED, MARKED. C-CHECK RO 9/27/2020. THE CRACKED LT MLG FAIRING DIAPHRAGM ASSY SUPPORT (P/N CC670-39205-5) HAS BEEN REPLACED WITH NEW AND INSTALLED WITH NEW HARDWARE, REF CRJ700 SRM.

Part: STRINGER — CRACKED (BS 280) · airframe 37,418 hrs · 27,504 cycles

FWD CABIN AT APPROX FS 280.00 LEFT HAND STGR 3LH IS CRACKED, MARKED. C-CHECK RO 9/27/2020. REMOVED CRACKED STGR 3L AND INSTALLED REPAIR (PN: 670-53-21-493-1 REPAIR ANGLE, -2 STRUCTURAL SHIM AND -3 SHIM) TO PAX DOOR LINTEL (STGR 3) BETWEEN FS 280.00 AND FS 295.00, REF REO. COMPLIED WITH TASK CARD. PRESSURE CHECK GOOD. COMPLIED WITH SB FOR REPAIR/REINFORCEMENT TO PASSENGER DOOR STRINGER 3 LINTEL ACCOMPLISHED ON CAMP.

Part: SHAFT — WORN (E/E DOOR HANDLE) · airframe 37,418 hrs · 27,504 cycles

THE AVIONICS DOOR HANDLE'S SHAFT ASSEMBLY APPEARS TO HAVE EXCESSIVE PLAY FROM WORN COMPONENTS. C-CHECK RO 9/27/2020. REMOVED AND INSTALLED NEW AVIONICS DOOR HANDLE HOUSING, REF CRJ700 SRM AND DWG. NO LEAKS NOTED. COMPLIED WITH TASK CARD.

Part: STRINGER CLIP — CORRODED (BS 349) · airframe 37,418 hrs · 27,504 cycles

FS 349.00 AT STR 21L ATTACH CLIP ANGLE CORRODED. C-CHECK RO 9/27/2020. FABRICATED AND INSTALLED ATTATCH ANGLE CLIP AT FS 349.00 AT STR-21L, REF DWG AND CRJ700 SRM.

Part: STRINGER CLIP — CORRODED (BS 310) · airframe 37,418 hrs · 27,504 cycles

FS 310.00 STGR 21L CLIP ANGLE HAS CORROSION. C-CHECK RO 9/27/2020. FABRICATED AND INSTALLED CLIP ANGLE AT STGR 21L AT FS 310.00, REF DWG AND CRJ700 SRM.

Part: PANEL — DAMAGED (FWD CARGO) · airframe 37,418 hrs · 27,504 cycles

FWD CARGO PANEL 151FLW HAS COMPOSITE DAMAGE. C-CHECK RO 9/27/2020. REPAIRED FWD CARGO PANEL 151FLW, PER C&D ZODIAC CMM. GLASS CLOTH 7781 PO T-47401. COMPLIED WITH TASK CARD.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 37,418 hrs · 27,504 cycles

LT FS 280 FLOOR CROSS BEAM HAS CORROSION BETWEEN RBL 9 AND LBL 9. C-CHECK RO 9/27/2020. LT FS 280 FLOOR CROSS BEAM BETWEEN RBL 9 AND LBL 9 HAS CORROSION ON FWD FACE THAT IS PITTED AND EXFOLIATED 100% MATERIAL LOSS AND IS OUT OF LIMITS, REF CRJ 700 SRM. LT FS 280 FLOOR CROSS BEAM IS REMOVED AND REPLACED WITH NEW ON MX.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 37,418 hrs · 27,504 cycles

REMOVE AND REPLACE LT AND RT FS 280 FLOOR BEAMS WITH SERVICEABLE, DUE TO OUT OF LIMIT CORROSION. C-CHECK RO 9/27/2020. REMOVED AND REPLACED LT AND RT FS 280 FLOOR BEAMS WITH SERVICEABLE PARTS, REF DWG SRM. COMPLIED WITH TASK CARD. SEE CONTINUATION CARD FOR DETAILS.

Part: HINGE — CORRODED (PAX DOOR) · airframe 37,418 hrs · 27,504 cycles

REPLACE PAX DOOR HINGE FUSELAGE SIDE ALL LUGS INNER HOLES ARE OUT OF LIMITS SEE CAMP NR 21410382, JOB NR 710157105, OP NR 53. C-CHECK RO 9/27/2020. REMOVED & REPLACED WITH NEW PAX DOOR HINGE FUSELAGE SIDE, REF CRJ700 SRM AND DWG.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 37,418 hrs · 27,504 cycles

RT FS 280 FLOOR CROSS BEAM HAS CORROSION BETWEEN RBL 9 AND LBL 9. C-CHECK RO 9/27/2020. RT FS 280 FLOOR CROSS BEAM BETWEEN RBL 9 AND LBL 9 HAS CORROSION ON FWD FACE THAT IS PITTED AND EXFOLIATED 100% MATERIAL LOSS AND IS OUT OF LIMITS, REF CRJ 700 SRM. RT FS 280 FLOOR CROSS BEAM IS REMOVED AND REPLACED WITH NEW ON MX.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 37,418 hrs · 27,504 cycles

FABRICATE RT FLOOR SEAT TRACK AT FS 485-FS 581 FOR JOB 710157104 OP 35. C-CHECK RO 9/27/2020. FABRICATED NEW RT FLOOR SEAT TRACK FROM FS 485 TO FS 581 USING EXTRUSION 20276-288-0-0A, PO T55899, REF CRJ700 SRM.

Part: STRINGER — CORRODED (BS 349-379) · airframe 37,418 hrs · 27,504 cycles

FS 349.00-FS 379.00 STRG 21RH IS CORRODED IN SEVERAL AREAS, MARKED. C-CHECK RO 9/27/2020. FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED NEW STGR 21R BETWEEN FS 333 TO FS 379, REF CRJ700 SRM AND DWG. LEAK CHECK GOOD. COMPLIED WITH TASK CARD.

Part: INTERCOSTAL — CORRODED (BS 333-349) · airframe 37,418 hrs · 27,504 cycles

FS 333.00-FS 349.00 21LH INTERCOSTAL CORRODED, MARKED. C-CHECK RO 9/27/2020. REMOVED AND REPLACED FS 333-FS 349 STRG 21L INTERCOSTAL, REF CRJ 700 SRM & DRAWING. ACCESSED & RESTORED ACCESS AS REQUIRED. LEAKS & OPERATIONS CHECK GOOD AT THIS TIME. SEE CONTINUE CARD FOR DETAILS.

Part: SKIN — DENTED (BS 280) · airframe 37,418 hrs · 27,504 cycles

RT FUSELAGE EXTERIOR DENT FOUND JUST AFT OF FS 280, APPROX STGR 26, FLAGGED. C-CHECK RO 9/27/2020. REPAIRED RT FUSELAGE EXTERIOR DENT FOUND JUST AFT OF FS 280, APPROX STGR 2, REF BOMBARDIER MHIRJ REO.

Part: PANEL — CORRODED (CARGO BAY) · airframe 37,418 hrs · 27,504 cycles

FWD CARGO PANEL 151 HLW HAS HOLE WORN IN KNEECAP. C-CHECK RO 9/27/2020. REPAIRED FWD CARGO PANEL 151 HLW WORN AREA IN KNEECAP FOR CRJ700, REF. C&D CMM. COMPLIED WITH TASK CARD.

Part: FRAME — CORRODED (BS 280) · airframe 37,418 hrs · 27,504 cycles

FS 280.00 STRG 22RH-23RH BELOW FLOOR CIRCUMFERENTIAL JOINT STRAP CORRODED, MARKED. C-CHECK RO 9/27/2020. REPAIRED CORROSION FROM FS 280.00 STRG 22RH-23RH BELOW FLOOR CIRCUMFERENTIAL JOINT STRAP. FOUND TO BE WITHIN LIMITS, REF CRJ-700 SRM AND BOMBARDIER DWG. SEE CONTINUATION CARD FOR DETAILS. LEAK CHECK GOOD.

Part: STRINGER — CORRODED (BS 333-349) · airframe 37,418 hrs · 27,504 cycles

FS 333.00-FS 349.00 STRG 22RH IS CORRODED, MARKED. C-CHECK RO 9/27/2020. REMOVED CORROSION FROM STGR 22R AT FS 333.00-FS 349.00, EVALUATED AS OUT-OF-LIMITS. REPLACED STGR 22R WITH SERVICABLE STGR, REF BOMBARDIER DWG AND CRJ700 SRM.

Part: SEAT TRACK — CORRODED (BS 349-485) · airframe 37,418 hrs · 27,504 cycles

FABRICATE RT FLOOR SEAT TRACK AT FS 349-FS 485 FOR JOB 710157104 OP 32. C-CHECK RO 9/27/2020. FABRICATED NEW RT FLOOR SEAT TRACK FROM FS 349 TO FS 485 USING EXTRUSION 20276-288-0-0A, PO T55899, REF CRJ700 SRM.

Part: FRAME — CORRODED (BS 280) · airframe 37,418 hrs · 27,504 cycles

FS 280.00 STRG 21RH-22RH BELOW FLOOR CIRCUMFERENTIAL JOINT STRAP CORRODED, MARKED. C-CHECK RO 9/27/2020. REMOVED CORROSION FROM FS 280.00 STRG 21RH-22RH BELOW FLOOR CIRCUMFERENTIAL JOINT STRAP, REF CRJ-700 SRM. FOUND TO BE WITHIN LIMITS, REF CRJ-700 SRM AND BOMBARDIER DWG. RESTORED FINISH, REF CRJ-700 SRM. SEE CONTINUATION CARD FOR DETAILS. LEAK CHECK GOOD.

Part: STRINGER — CORRODED (BS 333-349) · airframe 37,418 hrs · 27,504 cycles

FS 333.00-FS 349.00 STRG 21RH AFT SUPPORT ANGLE CORRODED, MARKED. C-CHECK RO 9/27/2020. REMOVED CORROSION FROM FS 333.00-FS 349.00 STRG 21RH AFT SUPPORT ANGLE, REF CRJ-700 SRM. NDT AND EVALUATED, FOUND TO BE OUT OF LIMITS, REF CRJ-700 NDT AND CRJ-700 SRM. REMOVED AND INSTALLED NEW AFT SUPPORT ANGLE AT FS 333.00-FS 349.00 STRG 21RH, REF CRJ-700 SRM. COMPLIED WITH SKYWEST M-337 FORM AND SKYWEST CARD. SEE CONTINUATION CARD FOR DETAILS.

Part: ATTACH ANGLE — CORRODED (BS 333-349) · airframe 37,418 hrs · 27,504 cycles

FS 333.00-FS 349.00 STRG 20RH AFT INTERCOSTAL ATTACH ANGLE CORRODED, MARKED. C-CHECK RO 9/27/2020. REPLACED CORRODED ANGLE WITH NEW ANGLE, REF CRJ-700 SRM. SEE CONTINUE CARD FOR DETAILS.

Part: FRAME — CORRODED (BS 280) · airframe 37,418 hrs · 27,504 cycles

FS 280.00 STRG 20RH-21RH BELOW FLOOR CIRCUMFERENTIAL JOINT STRAP CORRODED, MARKED. C-CHECK RO 9/27/2020. REMOVED CORROSION FROM FS 280.00 STRG 20RH-21RH BELOW FLOOR CIRCUMFERENTIAL JOINT STRAP, REF CRJ-700 SRM. FOUND TO BE WITHIN LIMITS, REF CRJ-700 SRM AND BOMBARDIER DWG. RESTORED FINISH, REF CRJ-700 SRM. SEE CONTINUATION CARD FOR DETAILS. LEAK CHECK GOOD.

Part: SEAT TRACK — CORRODED (BS 677-830) · airframe 37,418 hrs · 27,504 cycles

FLOOR SEAT TRACK SEGMENT STARTING AFT OF FS 677.00 TO AFT OF FS 830.40 LBL 9 HEAVILY CORROSION PITTED IN INNER EDGE, TOP, AROUND FASTENERS AND GOUGED (MARKED). C-CHECK RO 9/27/2020. REPLACED NEW SEAT TRACK SEGMENT STARTING AFT OF FS 677.00-FS 830.40 LBL 9, REF CRJ700 AMM.

Part: STRINGER — CORRODED (FWD CARGO) · airframe 37,418 hrs · 27,504 cycles

FWD CARGO BAY STRINGER CORRODED, AS MARKED, FS 533-STGR 22L. C-CHECK RO 9/27/2020. REMOVED AND INSTALLED NEW STRINGER SECTION FWD CARGO BAY STRINGER FS 533-STGR 22L, REF CRJ-700 SRM AND DWG. SEE CONTINUE CARD FOR MORE DETAILS. ALL CHECK GOOD. COMPLIED WITH.

Part: FLOOR SUPPORT — CORRODED (BS 517-533) · airframe 37,418 hrs · 27,504 cycles

RBL 9 FLOOR BEAM HAS CORROSION ON UPPER FLANGE AT INBOARD SIDE OF SEAT RAIL BETWEEN FS 517.00 AND FS 533.00. C-CHECK RO 9/27/2020. CUT AWAY DAMAGE ON DAMAGED SECTION OF FLOOR BEAM. FABRICATED, LOCATED AND DRILLED REPAIR PARTS. INSTALLED REPAIR PARTS TO FLOOR BEAM AND RESTORED FINISH, REF CRJ700 SRM & BOMBARDIER DWG. COMPLIED WITH TASK CARD.

Part: FLOOR SUPPORT — CORRODED (BS 565) · airframe 37,418 hrs · 27,504 cycles

LT FLOOR SILL AT FS 565.00 HAS CORROSION. C-CHECK RO 9/27/2020. BLENDED OUT CORROSION AT FS 565 ON LT FLOOR SILL AND FOUND IN LIMITS, REF REO. ALL STEPS COMPLIED WITH.

Part: INTERCOSTAL — CORRODED (BS 310-333) · airframe 37,418 hrs · 27,504 cycles

INTERCOSTAL AT STGR 21L BETWEEN FS 310.00 AND FS 333.00 CORRODED. C-CHECK RO 9/27/2020. REMOVED AND INSTALLED NEW INTERCOSTAL (BACK-UP SILL) FS 310-FS 333 AT STGR 21L, REF CRJ700 SRM AND DWG. ALL CHECK GOOD. COMPLIED WITH.

Part: FRAME — CORRODED (BS 1031) · airframe 37,418 hrs · 27,504 cycles

FS 1031.00 FRAME FWD SIDE HAS CORROSION BETWEEN STGR 25L TO 25R. C-CHECK RO 9/27/2020. REPAIRED CORROSION ON FS 1031.00 FRAME FWD SIDE ON LOWER FLANGE AT STGR 25L TO 25R, REF CRJ 700 SRM AND COMPLIED WITH REO. SEE CONTINUATION CARD FOR DETAILS.

Part: NUT PLATE — CORRODED (BS 581) · airframe 37,418 hrs · 27,504 cycles

FWD CARGO BAY TIE DOWN NUTPLATE BRACKET CORRODED, AS MARKED, FS 581 BETWEEN STGRS 22L/23L. C-CHECK RO 9/27/2020. BLENDED OUT CORROSION ON TIE DOWN BRACKET AT FS 581 STGR 22L-23L, REF CRJ700 SRM. FOUND PART TO BE OUT OF LIMITS. REMOVED AND INSTALLED NEW TIE DOWN PLATE FITTING, REF CRJ700 SRM AND DWG. COMPLIED WITH TASK CARD.

Part: DOUBLER — CORRODED (BS 536) · airframe 37,418 hrs · 27,504 cycles

FWD CARGO BAY BUTTERFLY DOUBLER CORRODED, AS MARKED, FS 536-STGR 25L. C-CHECK RO 9/27/2020. BLENDED CORROSION ON THE FWD CARGO BAY BUTTERFLY DOUBLER CORRODED, AS MARKED, FS 536.00-STGR 25L FOUND ACCEPTABLE AT THIS TIME. ORIGINAL THICKNESS .080" LOWEST THICKNESS .076" MATERIAL LOSS .004" WITHIN LIMITS USING TUC 8414, CAL DUE 30-JUN-21, REF CRJ-700 SRM.

Part: INTERCOSTAL — CORRODED (BS 319-333) · airframe 37,418 hrs · 27,504 cycles

INTERCOSTAL AT STGR 20R BETWEEN FS 319.70 AND FS 333.00 CORRODED. C-CHECK RO 9/27/2020. BLENDED OUT CORROSION ON INTERCOSTAL ON OUTBOARD SIDE AROUND ALL OWER FASTENERS HOLES, REF CRJ-700 SRM. COMPLIED WITH REPAIR, REF MHIRJ REO. SEE CONTINUATION CARD FOR DETAILS.

Part: FLOOR SUPPORT — CORRODED (BS 863-879) · airframe 37,418 hrs · 27,504 cycles

FS 863.00 FS879.00 RT FLOOR SILL CORRODED IN SEVERAL AREAS, MARKED. C-CHECK RO 9/27/2020. BLENDED OUT CORROSION ON RT FLOOR SILL FS 863-879 AND FOUND IN LIMITS OF REO. ALL STEPS COMPLIED WITH.

Part: FRAME — CORRODED (BS 1047) · airframe 37,418 hrs · 27,504 cycles

FS 1047.00 FRAME FWD SIDE HAS CORROSION BETWEEN STGR 25L AND 26L. C-CHECK RO 9/27/2020. REMOVED CORROSION AT FS 1047.00 FRAME FWD SIDE HAS CORROSION BETWEEN STGR 25L AND 26L, REF CRJ-700 SRM, WITHIN LIMITS.

Part: SEAT TRACK — CORRODED (BS 677-860) · airframe 37,418 hrs · 27,504 cycles

FLOOR SEAT TRACK SEGMENT STARTING AFT OF FS 677.00 TO AFT OF FS 830.40 RBL 9 HEAVILY CORROSION PITTED IN INNER EDGE, TOP AROUND FASTENERS AND GOUGED (MARKED). C-CHECK RO 9/27/2020. REPLACED NEW SEAT TRACK SEGMENT STARTING AFT OF FS 677.00-FS 830.40 RBL 9, REF CRJ700 AMM.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 37,418 hrs · 27,504 cycles

FLOOR SUPPORT CORRODED AT MULTIPLE AREAS, FORWARD SIDE OF THE FS 280.00 BEAM BETWEEN BL 9L-BL 9R. C-CHECK RO 9/27/2020. FLOOR SUPPORT ANGLE AT FS 280 BETWEEN BL 9L-BL 9R IS CORRODED AND OUT LIMITS, REF CRJ-700 SRM. REMOVED AND INSTALLED NEW COCKPIT FLOOR SUPPORT ANGLE, REF DWG AND CRJ-700 SRM. COMPLIED WITH TASK CARD.

Part: SEAT TRACK — CORRODED (BS 863-985) · airframe 37,418 hrs · 27,504 cycles

FS 863.00 FS 985.00 RBL 9 FLOOR SEAT TRACK CORRODED IN SEVERAL AREAS, MARKED. C-CHECK RO 9/27/2020. BLENDED AND REMOVED CORROSION ON FLOOR SEAT TRACK AT APPROX FS 863.00-FS 985.00 RBL 9, REF CRJ700 SRM. FOUND TO BE WITHIN LIMITS AND RESTORED FININSH.

Part: FRAME — CORRODED (BS 1015) · airframe 37,418 hrs · 27,504 cycles

FS 1015.00 FRAME FWD SIDE HAS CORROSION BETWEEN STGR 26L TO 26R. C-CHECK RO 9/27/2020. REMOVED CORROSION ON FS 1015.00 FRAME FWD SIDE BETWEEN STGR 26L TO 26R, REF CRJ700 SRM. FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED NEW FRAME SECTION AT FS 1015.00, REF CRJ700 REO AND CRJ900 SRM. NO LEAKS NOTED. COMPLIED WITH TASK CARD.

Part: FRAME — CORRODED (BS 645) · airframe 37,418 hrs · 27,504 cycles

CORROSION ON FRAME FS 645.00 BETWEEN STGR 26L-STGR26R, MARKED. C-CHECK RO 9/27/2020. REMOVED CORROSION ON FRAME FS 645.00 BETWEEN STGR 26L-STGR26R, REF CRJ-700 SRM AND COMPLIED WITH MHIRJ REO. THE FRAME WITHIN LIMITS.

Part: FLOOR SUPPORT — CORRODED (BS 533) · airframe 37,418 hrs · 27,504 cycles

LT FLOOR SILL AT FS 533.00 HAS CORROSION. C-CHECK RO 9/27/2020. BLENDED OUT CORROSION ON LT FLOOR SILL FS 533 AND FOUND IN LIMITS, REF REO. ALL STEPS COMPLIED WITH.

Part: TIE DOWN — CORRODED (BS 533) · airframe 37,418 hrs · 27,504 cycles

FWD CARGO BAY TIEDOWN MOUNT PLATE CORRODED, AS MARKED, FS 533 BETWEEN STGRS 22L/23L. C-CHECK RO 9/27/2020. COMPLETED REO FOR FWD CARGO BAY TIE DOWN MOUNT PLATE BRACKET. SEE CONTINUATION CARD FOR WORK PERFORMED.

Part: FRAME — CORRODED (BS 517) · airframe 37,418 hrs · 27,504 cycles

FWD CARGO BAY FRAME CORRODED, AS MARKED, FS 517 BETWEEN STGRS 26L/26R. C-CHECK RO 9/27/2020. REPAIRED FWD CARGO BAY FRAME CORRODED, AS MARKED, FS 517 BETWEEN STGRS 26L/26R, REF CRJ-700 SRM. SEE CONTINUE CARD FOR MORE DETAILS. LEAK CHECK GOOD.

Part: DOOR SILL — CORRODED (FWD CARGO DOOR) · airframe 37,418 hrs · 27,504 cycles

FWD CARGO BAY DOOR SILL CLOSEOUT MOUNTING TAB CORRODED, AS MARKED, AROUND NUTPLATE HOLE FS 536 BETWEEN 24L/25L. C-CHECK RO 9/27/2020. CORRODED MOUNTING TAB, FWD CARGO BAY DOOR SILL CLOSEOUT AREA FS 536 STRG 24L/25L, FOUND TO BE OUT OF LIMITS, IAW CRJ700 SRM. TAB REMOVED AND REPLACED WITH LOCAL FABRICATION, REF CJ700 SRM. SEE CONTINUE CARD FOR WORK COMPLETED.

Part: DOOR SILL — CORRODED (FWD CARGO) · airframe 37,418 hrs · 27,504 cycles

FWD CARGO BAY DOOR SILL CORRODED MULTIPLE AREAS, AS MARKED. C-CHECK RO 9/27/2020. REPAIRED FWD CARGO BAY DOOR SILL, IAW REO NDT COMPLIED WITH. SEE CONTINUATION SHEET FOR MORE DETAILS. VISUALLY VERIFIED ALL DISPOSISTIONS ON REO ARE ACCOMPLISHED. COMPLIED WITH TASK CARD.

Part: SEAT TRACK — CORRODED (BS 985-1015) · airframe 37,418 hrs · 27,504 cycles

FS 985.00 FS 1015.00 RBL 27 FLOOR SEAT TRACK HEAVILY CORROSION PITTED, MARKED. C-CHECK RO 9/27/2020. REMOVED AND REPLACED WITH NEW FROM STOCK FS 985.00-FS 1015.00 RBL 27 FLOOR SEAT TRACK, REF CRJ700 AMM.

Part: FRAME — CORRODED (BS 1000) · airframe 37,418 hrs · 27,504 cycles

FS 1000.00 STRG 26L-25L FWD SIDE OF FRAME CORRODED, MARKED. C-CHECK RO 9/27/2020. REMOVED CORROSION AT FS 1000.00 STGR 26L-25L FWD SIDE OF THE FRAME FLANGED, REF CRJ700 SRM. OUT OF LIMITS. RECEIVED REO. COMPLIED WITH ALL STEPS OF REO. NO LEAKS NOTED. COMPLIED WITH TASK CARD

Part: SEAT TRACK — CORRODED (BS 830-969) · airframe 37,418 hrs · 27,504 cycles

FS 830.40 FS969.00 LBL 9 FLOOR SEAT TRACK CORRODED IN SEVERAL AREAS, MARKED. C-CHECK RO 9/27/2020. REMOVED AND REPLACED WITH NEW FROM STOCK FS 830.40-FS 969.00 LBL 9 FLOOR SEAT TRACK, REF CRJ700 AMM.

Part: FRAME — CORRODED (BS 295) · airframe 37,418 hrs · 27,504 cycles

FS 295.00 FRAME HAS CORROSION ON THE AFT SIDE STGR 25L STGR 24R, MARKED. C-CHECK RO 9/27/2020. REPAIRED FS 295.00 FRAME HAS CORROSION ON THE AFT SIDE STGR 25L-STGR 24R, REF CRJ-700 SRM. SEE CONTINUE CARD FOR MORE DETAILS.

Part: FLOORBEAM — CORRODED (BS 501) · airframe 37,418 hrs · 27,504 cycles

RBL 9 FLOOR BEAM HAS CORROSION AROUND FASTENER UPPER OUTBOARD SIDE AT FS 501.00. C-CHECK RO 9/27/2020. CUT AWAY DAMAGE ON DAMAGED SECTION OF FLOOR BEAMS, REF CRJ700 SRM. FABRICATED, LOCATED AND DRILLED REPAIR PARTS, REF CRJ700 SRM. INSTALLED REPAIR PARTS TO FLOOR BEAM AND RESTORED FINISH, REF CRJ700 SRM & BOMBARDIER DWG.

Part: FRAME — CORRODED (BS 1051) · airframe 37,418 hrs · 27,504 cycles

FS 1051.30 FRAME AFT SIDE HAS SUSPECTED CORROSION BETWEEN STGR 25L AND 25R. C-CHECK RO 9/27/2020. NO CORROSION FOUND AT FS 1051.30 FROM STGR 25L-26L OR STGR 25R-26R. REMOVED CORROSION ON FRAME FLANGE BETWEEN 26R AND 26L AT FS 1051.30, REF CRJ700 SRM. WITHIN LIMITS OF REO. COMPLIED WITH ALL STEPS OF REO.

Part: FRAME — CORRODED (BS 310) · airframe 37,418 hrs · 27,504 cycles

FS 310.00 FRAME HAS CORROSION ON THE FORWARD SIDE STGR 24L-STGR 24R, MARKED. C-CHECK RO 9/27/2020. REMOVED CORROSION FROM FS 310.00 FRAME ON THE FWD SIDE STGR 24L TO STGR 24R, REF CRJ700 SRM. RECEIVED REO, WITHIN LIMITS. COMPLIED WITH ALL STEPS OF REO.

Part: FRAME — CORRODED (BS 280) · airframe 37,418 hrs · 27,504 cycles

CORROSION ON CIRCUMFERENTIAL JOINT INTERFACE FS 280.00-FS 280.62 STGR 23L-STGR 24R. C-CHECK RO 9/27/2020. REMOVED CORROSION ON CIRCUMFERENTIAL JOINT INTERFACE FS 280.00-FS 280.62 STGR 26L-STGR 24R, REF CRJ700 SRM. OUT OF LIMITS. RECEIVED REO. COMPLIED WITH ALL STEPS OF REO. NO LEAKS NOTED.

Part: FLOOR SUPPORT — CORRODED (BS 661-677) · airframe 37,418 hrs · 27,504 cycles

LBL 9 FLOOR BEAM HAS CORROSION ON UPPER SIDE OF UPPER FLANGE INBOARD/OUTBOARD SIDE BETWEEN FS 661.00 AND FS 677.00. C-CHECK RO 9/27/2020. COMPLIED WITH FLOOR BEAM REPAIR ON UPPER SIDE OF UPPER FLANGE INBOARD/OUTBOARD SIDE BETWEEN FS 661-677, PER MHIRJ REO.

Part: INTERCOSTAL — CORRODED (BS 310-319) · airframe 37,418 hrs · 27,504 cycles

INTERCOSTAL AT STGR 20R BETWEEN FS 310.00 AND FS 319.70 CORRODED. C-CHECK RO 9/27/2020. REMOVED OUT OF LIMITS INTERCOSTAL AND INSTALLED NEW SERVICEABLE INTERCOSTAL AT STGR 20R FS310.00 TO FS319.70, REF CRJ700 SRM AND DWG. ALL CHECK GOOD COMPLIED WITH.

Part: SKIN — CORRODED (BS 939-969) · airframe 37,418 hrs · 27,504 cycles

FS 939.00 FS 969.00 STRG 21 LT 21 RT CORROSION ON EXTERIOR SKIN AROUND SEVERAL FASTENERS, MARKED. C-CHECK RO 9/27/2020. BLENDED-OUT CORROSION AT FS 939.00 FS 969.00 STRG 21 LT 21 RT CORROSION ON EXTERIOR SKIN AROUND SEVERAL FASTENER, REF CRJ-700 SRM, WITHIN LIMITS. COMPLIED WITH MHIRJ REO. ALL CHECK GOOD.

Part: SKIN — GOUGED (PAX DOOR) · airframe 37,418 hrs · 27,504 cycles

PAX DOOR OUTER SKIN UPPER FWD CORNER HAS NUMEROUS GOUGES AND SCRAPES. C-CHECK RO 9/27/2020. REPAIRED DAMAGE TO PAX DOOR OUTER SKIN UPPER FWD CORNER, REF CRJ700 SRM AND COMPLIED WITH ALL STEPS OF REO. NO DEFECTS NOTED. COMPLIED WITH TASK CARD.

Part: SEAT TRACK — CORRODED (BS 784-855) · airframe 37,418 hrs · 27,504 cycles

RT SIDE SEAT TRACK RAIL AT APPROX FS 784-FS 855 HAS CORROSION. C-CHECK RO 9/27/2020. RT SIDE SEAT TRACK RAIL FS 784-FS 855 CORROSION FOUND TO BE OUT OF LIMITS, IAW CRJ700 SRM. REMOVED AND REPLACED SEAT RAIL, IAW CRJ 700 SRM. SEE CONTINUATION CARD FOR WORK ACCOMPLISHED.

Part: SEAT TRACK — CORRODED (BS 713-763) · airframe 37,418 hrs · 27,504 cycles

RT SIDE SEAT TRACK RAIL AT APPROX FS 713-FS 763 HAS CORROSION. C-CHECK RO 9/27/2020. REPLACED RT SEAT TRACK RAIL APPROX FS 713.00-FS 763.00, REF CRJ 700 SRM. SEE CONTINUATION CARD FOR DETAILS.

Part: NUT PLATE — DAMAGED (CARGO DOOR) · airframe 37,418 hrs · 27,504 cycles

CARGO DOOR SURROUND STRUCTURE FS 1000 ABOVE SILL, NUTPLATE HAS BROKEN RIVET, AS MARKED. C-CHECK RO 9/27/2020. REMOVED AND REPLACED 1 EA NUTPLATE RIVET AT FS 1000 ABOVE SILL, REF CRJ700 SRM.

Part: SEAT TRACK — CORRODED (BS 379-485) · airframe 37,418 hrs · 27,504 cycles

LT FLOOR SEAT TRACK RAIL AT APPROX FS 379-FS 485 HAS CORROSION. C-CHECK RO 9/27/2020. REMOVED AND REPLACED LT FLOOR SEAT TRACK RAIL AT APPROX FS 379-485, REF CRJ700 AMM.

Part: SEAT TRACK — CORRODED (BS 349-485) · airframe 37,418 hrs · 27,504 cycles

RT FLOOR SEAT TRACK RAIL AT APPROX FS 349-FS 485 HAS CORROSION. C-CHECK RO 9/27/2020. REMOVED CORROSION ON RT FLOOR SEAT TRACK RAIL AT APPROX FS 349-FS 485, REF CRJ-700 SRM. MEASURED AND EVALUATED SEAT TRACK, FOUND TO BE OUT OF LIMITS, AND HAS MORE THAN ONE TYPE OF DAMAGE ALLOWED AT ANY TYPICAL CROSS-SECTION, REF CRJ-700 SRM. REMOVED AND INSTALLED NEW RT FLOOR SEAT TRACK RAIL AT APPROX FS 349-FS 485, REF CRJ-700 AMM.

Part: SEAT TRACK — CORRODED (BS 573-669) · airframe 37,418 hrs · 27,504 cycles

RT SIDE SEAT TRACK RAIL AT APPROX FS 573-FS 669.40 HAS CORROSION. C-CHECK RO 9/27/2020. REMOVED CORROSION DAMAGE ON RT SEAT TRACK RAIL AT APPROX FS 573-FS 669.40, REF CRJ-700 SRM. SEE CONTINUATION CARD FOR DETAILS.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 37,418 hrs · 27,504 cycles

LT FLOOR SEAT TRACK RAIL AT APPROX FS 485-FS 581 HAS CORROSION. C-CHECK RO 9/27/2020. REMOVED AND REPLACED LT FLOOR TRACK RAIL AT APPROX FS 485-581, REF CRJ700 AMM.

Part: DIAPHRAGM — CRACKED (BS 909) · airframe 37,418 hrs · 27,504 cycles

FS 909.00 STRG 24LH DIAPHRAGM CRACKED BOTTOM CORNER, MARKED. C-CHECK RO 9/27/2020. REPAIRED CRACK AT FS 909.00 STRG 24LH, DIAPHRAGM BOTTOM CORNER BY COMPLYING WITH REO. SEE CONTINUATION CARD FOR DETAILS.

Part: STRAP — CORRODED (EMERGENCY EXIT) · airframe 37,418 hrs · 27,504 cycles

LT EMER EXIT SURROUND, LOWER INNER STRAP HAS CORROSION. C-CHECK RO 9/27/2020. REPAIRED CORROSION ON LT EMERGENCY EXIT SURROUND LOWER INNER STRAP, IAW CRJ 700 SRM. BLEND OUT WAS WITHIN LIMITS. SEE CONTINUATION CARD FOR DETAILS.

Part: SEAT TRACK — CORRODED (BS 379-485) · airframe 37,418 hrs · 27,504 cycles

RT SIDE SEAT TRACK RAIL AT APPROX FS 379-FS 485 HAS CORROSION. C-CHECK RO 9/27/2020. REMOVED & REPLACED WITH NEW RT SEAT TRACK RAIL AT APPROX FS 379.00-FS 485.00, REF CRJ700 AMM. SEE CONTINUATION CARD FOR DETAILS.

Part: DOOR SILL — CORRODED (CARGO DOORWAY) · airframe 37,418 hrs · 27,504 cycles

CARGO DOOR SURROUND STRUCTURE SILL CORRODED MULTIPLE AREAS, AS MARKED. C-CHECK RO 9/27/2020. EVALUATED CARGO DOOR SILL OUT OF LIMITS. REMOVED AND REPLACED CARGO DOOR LOWER SILL, REF CRJ700 SRM AND DWG. NO LEAKS NOTED. COMPLIED WITH TASK CARD.

Part: DOOR FRAME — CRACKED (BS 1047) · airframe 37,418 hrs · 27,504 cycles

CARGO DOOR SURROUND STRUCTURE FS 1047 BETWEEN STGRS 12L/13L, DOOR FRAME STRUCTURE BRACKET HAS SUSPECTED CRACK, AS MARKED. C-CHECK RO 9/27/2020. REMOVED AND INSTALLED NEW BRACKET, GUSSET, AND INTERCOSTAL, REF CRJ700 SRM, AND DWG. NO LEAKS NOTED. COMPLIED WITH TASK CARD.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 37,418 hrs · 27,504 cycles

RT FLOOR SEAT TRACK RAIL AT APPROX FS 485-FS 581 HAS CORROSION. C-CHECK RO 9/27/2020. REMOVED CORROSION ON RT FLOOR SEAT TRACK RAIL AT APPROX FS 485-FS 581, REF CRJ-700 SRM. MEASURED AND EVALUATED SEAT TRACK, FOUND TO BE OUT OF LIMITS AND HAS MORE THAN ONE TYPE OF DAMAGE ALLOWED AT ANY TYPICAL CROSS-SECTION, REF CRJ-700 SRM. REMOVED AND INSTALLED NEW RT FLOOR SEAT TRACK RAIL AT APPROX FS 485-FS 581, REF CRJ-700 AMM.

Part: SEAT TRACK — CORRODED (BS 581-683) · airframe 37,418 hrs · 27,504 cycles

RT FLOOR SEAT TRACK RAIL AT APPROX FS 581-FS 683 HAS CORROSION. C-CHECK RO 9/27/2020. REMOVED AND REPLACED FLOOR TRACK AT APPROX FS 581-683 ON THE RT SIDE, REF CRJ700 AMM.

Part: SEAT TRACK — CORRODED (BS 784-855) · airframe 37,418 hrs · 27,504 cycles

LT SIDE SEAT TRACK MOUNTING CHANNEL AT APPROX FS 784-FS 855 HAS CORROSION. C-CHECK RO 9/27/2020. REMOVED & REPLACED WITH NEW LT SIDE SEAT TRACK MOUNTING CHANNEL AT APPROX FS 784-FS 855, REF CRJ 700 SRM. SEE CONTINUATION CARD FOR DETAILS.

Part: SEAT TRACK — CORRODED (BS 485-573) · airframe 37,418 hrs · 27,504 cycles

RT SIDE SEAT TRACK RAIL AT APPROX FS 485-FS 573 HAS CORROSION. C-CHECK RO 9/27/2020. REPLACED WITH NEW RT SIDE SEAT RAIL TRACK AT APPROXIMATELY FS 485.00-FS 573.00, REF CRJ700 AMM.

Part: SEAT TRACK — CORRODED (BS 581-683) · airframe 37,418 hrs · 27,504 cycles

LT FLOOR SEAT TRACK RAIL AT APPROX FS 581-FS 683 HAS CORROSION. C-CHECK RO 9/27/2020. REMOVED AND REPLACED LT FLOOR SEAT TRACK AT APPROX FS 581-FS 683, REF CRJ-700 SRM.

Part: SEAT TRACK — CORRODED (BS 784-855) · airframe 37,418 hrs · 27,504 cycles

LT SIDE SEAT TRACK RAIL AT APPROX FS 784-FS 855 HAS GOUGES AND CORROSION. C-CHECK RO 9/27/2020. REMOVED & REPLACED SEAT TRACK A NEW LT SIDE SEAT TRACK RAIL APPROX AT FS 784.00-FS 855.00, REF CRJ 700 SRM. SEE CONTINUATION CARD FOR DETAILS.

Part: SEAT TRACK — CORRODED (BS 747-763) · airframe 37,418 hrs · 27,504 cycles

LT SIDE SEAT TRACK MOUNTING CHANNEL AT APPROX FS 741-FS 763 HAS CORROSION. C-CHECK RO 9/27/2020. CORROSION REMOVED FROM LT SIDE SEAT TRACK MOUNT CHANNEL FS 741-FS 763, REF CRJ SRM. SEE CONTINUATION CARD FOR WORK COMPLETED.

Part: RETAINER — CRACKED (RT TRU DOOR) · airframe 37,418 hrs · 27,504 cycles

RT TRU AFT LATCH RETAINER IS POSSIBLY CRACKED, FLAGGED. C-CHECK RO 9/27/2020. REMOVED AND REPLACED WITH NEW RT TRU DOOR LAND, REF CRJ-700 SRM 51-42-06-001-001-A01 AND MHIRJ REO COMPLIED WITH.

Part: HINGE FITTING — DAMAGED (RT AILERON) · airframe 37,418 hrs · 27,504 cycles

RT AILERON CENTER HINGE FITTING INBOARD LUG HAS SMALL NICK ON THE LOWER SURFACE. C-CHECK RO 9/27/2020. REPAIRED NICK DAMGE TO RT AILERON, CENTER HINGE FITTING, INBOARD LUG, REF CRJ-700 SRM AND REO. SEE CONTINUATION FOR DETAILS.

Part: ROLL PIN — MIGRATED (PAX DOOR HINGE) · airframe 37,418 hrs · 27,504 cycles

ROLL-PIN IN PAX DOOR HINGE HAS MIGRATED AND GOUGED THE LAST (AFT) LUG LAND ON THE PAX DOOR HINGE FUSELAGE SIDE. C-CHECK RO 9/27/2020. PAX DOOR HINGE FUSELAGE SIDE FOUND TO BE OUT OF LIMITS. ALL LUGS INNER HOLES ARE OVER SIZES TOOL NR TUC8495, IAW BOMBARDIER REO.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 37,418 hrs · 27,504 cycles

LT V/STAB TO FUSELAGE ATTACHMENT DRAG ANGLE FWD POSSIBLE CRACK, MARKED. C-CHECK RO 9/27/2020. PERFORMED NDT INSP OF LT V/STAB TO FUSELAGE ATTACHMENT FWD DRAG ANGLE. FOUND AFT DRAG ANGLE CRACKED, REF CRJ-700 NDT. PERFORMED REO REPAIR TO V/STAB TO FUSELAGE ATTACHMENT FWD AND AFT DRAG ANGLES. COMPLIED WITH SKYWEST TASK CARD. SEE CONTINUATION CARD FOR DETAILS.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 37,418 hrs · 27,504 cycles

LT V/STAB TO FUSELAGE ATTACHMENT DRAG ANGLE AFT POSSIBLE CRACK, MARKED. C-CHECK RO 9/27/2020. PERFORMED NDT INSP OF LT V/STAB TO FUSELAGE ATTACHMENT AFT DRAG ANGLE. FOUND AFT DRAG ANGLE CRACKED, REF CRJ-700 NDT. PERFORMED REO REPAIR TO V/STAB TO FUSELAGE ATTACHMENT FWD AND AFT DRAG ANGLES. COMPLIED WITH SKYWEST TASK CARD. SEE CONTINUATION CARD FOR DETAILS.

Part: SKIN — GOUGED (AFT CARGO DOOR) · airframe 37,418 hrs · 27,504 cycles

AFT CARGO DOOR ENTRANCE EXTERIOR SKIN GOUGED FWD LOWER CORNER, MARKED. C-CHECK RO 9/27/2020. PERFORMED GOUGE REPAIR ON AFT CARGO DOOR CUT OUT SKIN FWD LOWER CORNER BY COMPLYING WITH REO DISPOSITION STEPS 1-4. SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH TASK CARD.

Part: SKIN — CHAFED (BS 977) · airframe 37,418 hrs · 27,504 cycles

CHAFE IN EXTERNAL FUSELAGE SKIN AFT OF CIRCUMFERENTIAL JOINT AT FS 977 AND STGR 27. C-CHECK RO 9/27/2020. BLENDED OUT CHAFE, FOUND TO BE IN LIMITS. RESTORED FINISH, IAW MHIRJ REO AND CRJ700 SRM.

Part: SKIN — GOUGED (AFT CARGO DOOR) · airframe 37,418 hrs · 27,504 cycles

AFT CARGO DOOR ENTRANCE EXTERIOR SKIN GOUGED AFT LOWER CORNER, MARKED. C-CHECK RO 9/27/2020. PERFORMED GOUGE REPAIR ON AFT CARGO DOOR CUT OUT SKIN AFT LOWER CORNER BY COMPLYING WITH REO. DISPOSITION STEPS 1-4. SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH TASK CARD.

Part: SKIN — CHAFED (BS 977) · airframe 37,418 hrs · 27,504 cycles

CHAFE IN EXTERNAL FUSELAGE SKIN FWD OF CIRCUMFERENTIAL JOINT AT FS 977 AND STGR 27. C-CHECK RO 9/27/2020. BLENDED OUT CHAFE, FOUND TO BE OUT OF LIMITS, REQUESTED ENGINEERING. COMPLIED WITH MHIRJ REO. RESTORED FINISH IAW CRJ700 SRM. ALL STEPS OF THE REO COMPLIED WITH.

Part: SKIN — DAMAGED (LT WING LE) · airframe 37,418 hrs · 27,504 cycles

SKIN BEHIND LEFT WING LEADING EDGE PANEL 522HZ HAS ELONGATED HOLE. C-CHECK RO 9/27/2020. EVALUATED AND FOUND DAMAGE ONLY ON SUPPORT ANGLE OF PANEL 522HZ. ANGLE FOUND TO BE OUT OF LIMITS, REF CRJ-700 SRM. REMOVED AND INSTALLED NEW 522HZ SUPPORT ANGLE, REF DWG CRJ-700 SRM. COMPLIED WITH TASK CARD. SEE CONTINUATION CARD FOR DETAILS.

Part: FLOOR PANEL — CRACKED (COCKPIT) · airframe 37,418 hrs · 27,504 cycles

COCKPIT PANEL 222EZ IS CRACKED. C-CHECK RO 9/27/2020. REPAIRED PANEL 222EZ USING FG-778138-504 PO T47401 AND 828-3223 RESIN, PER C&D ZODIAC CMM. COMPLIED WITH TASK CARD.

Part: LINER — DAMAGED (CARGO DOOR) · airframe 37,418 hrs · 27,504 cycles

CARGO LINER 281KLW HAS WORN/DAMAGED COMPOSITE. C-CHECK RO 9/27/2020. REPAIRED PANEL 281KLW USING FG-778138-504 PO T47401 AND 828-3223 RESIN, PER ZODIAC AEROSPACE CMM. COMPLIED WITH TASK CARD.

Part: SKIN — CHAFED (NR 1 SLAT TE) · airframe 37,418 hrs · 27,504 cycles

RT SLAT NR 1 INNER SKIN UPPER TRAILING EDGE CHAFED IN SEVERAL AREAS, MARKED. C-CHECK RO 9/27/2020. REPAIRED CHAFE DAMAGE AT RT SLAT NR 1 INNER SKIN UPPER TRAILING EDGE, REF REO. SEE CONTINUATION CARD FOR WORK DETAILS.

Part: SKIN — CHAFED (NR 2 SLAT TE) · airframe 37,418 hrs · 27,504 cycles

RT SLAT NR 2 INNER SKIN UPPER TRAILING EDGE CHAFED IN SEVERAL AREAS, MARKED. C-CHECK RO 9/27/2020. REPAIRED CHAFE DAMAGE AT RT SLAT NR 2 INNER SKIN UPPER TRAILING EDGE, REF REO. SEE CONTINUATION CARD FOR WORK DETAILS.

Part: PANEL — DAMAGED (AFT CARGO) · airframe 37,418 hrs · 27,504 cycles

AFT CARGO AFT RT CORNER VERTICLE GILLINER PANEL W/DECOM PANEL, SHOWS EVIDENCE OF PHYSICAL DAMAGE SEVERAL AREAS, AS MARKED. C-CHECK RO 9/27/2020. REPAIRED AFT CARGO RT CORNER VERTICLE GILLINER AREAS, AS MARKED. APPLIED GLASS CLOTH REPAIR RESIN RESTORED FINISH. COMPLIED SKY WEST, PER CRJ 700 SRM.

Part: SKIN — CHAFED (LT AILERON LE) · airframe 37,418 hrs · 27,504 cycles

LT AILERON UPPER LEADING EDGE CHAFED IN SEVERAL AREAS, MARKED. C-CHECK RO 9/27/2020. ORIGINAL MATERIAL THICKNESS OF LT AILERON UPPER LEADING EDGE PANEL IS 0.090? AND 0.055? CHEM MILLED POCKET, REF CRJ700 SRM. TOTAL MATERIAL REMOVED IS 0.032? MEASURED USING TOTAL MATERIAL REMAINING IS 0.058?, OUT OF LIMITS IN REF REO. DAMAGE EXCEEDS 0.027? MAX DEPTH. INSTALLED NEW LT AILERON UPPER LEADING EDGE SKIN PN CC670-13052-1, REF BOMBARDIER DWG CRJ700 SRM. SEE CONTINUATION CARD FOR WORKED PERFORMED. COMPLIED WITH SKYWEST TASK CARD.

Part: SKIN — NICKED (FUSELAGE) · airframe 37,418 hrs · 27,504 cycles

PANEL 521AT NICKED ON OUTER SKIN, MARKED. C-CHECK RO 9/27/2020. BLENDED OUT NICK ON OUTER SKIN OF PANEL 521AT, WITHIN ALLOWABLE LIMITS. ORIGINAL .090, REMAINING .083" WITH .007" MATERIAL LOSS, REF CRJ-700 SRM AND RESTORED FINISH REF CRJ-700 SRM. SEE CONTINUATION FOR DETAILS.

Part: SKIN — ERODED (NR 3 SLAT LE) · airframe 37,418 hrs · 27,504 cycles

LT SLAT NR 3 LEADING EDGE HAS EROSION THE ENTIRE LENGTH. C-CHECK RO 9/27/2020. REMOVED EROSION DAMAGE FROM LT SLAT NR 3 LEADING EDGE, REF MHIRJ REO. SEE CONTINUATION FOR WORK DETAILS.

Part: SKIN — CHAFED (NR 3 SLAT TE) · airframe 37,418 hrs · 27,504 cycles

RT SLAT NR 3 INNER SKIN UPPER TRAILING EDGE CHAFED IN SEVERAL AREAS, MARKED. C-CHECK RO 9/27/2020. REMOVED CHAFING IN SEVERAL AREAS ON RT SLAT NR 3 INNER SKIN UPPER TRAILING EDGE, REF CRJ700 SRM. COMPLIED WITH ALL STEPS OF MHIRJ REO.

Part: SKIN — CHAFED (GALLEY DOOR) · airframe 37,418 hrs · 27,504 cycles

GALLEY SERVICE DOOR INTERIOR FWD SKIN IS CHAFED, FLAGGED. C-CHECK RO 9/27/2020. REMOVED CHAFE AREA ON SERVICE DOOR INTERIOR SKIN, REF CRJ700 SRM. FOUND TO BE WITHIN LIMITS, REF CRJ700 SRM. SEE CONTINUATION CARD FOR DETAILS.

Part: SKIN — CHAFED (NR 2 SLAT TE) · airframe 37,418 hrs · 27,504 cycles

LT SLAT NR 2 INNER SKIN UPPER TRAILING EDGE CHAFFED IN SEVERAL AREAS, MARKED. C-CHECK RO 9/27/2020. REWORKED CHAFE DAMAGE TO LT SLAT NR 2 TRAILING EDGE, PER REO.

Part: INTERCOSTAL — DENTED (PAX DOOR) · 24,673 cycles

PASSENGER DOOR INTERCOSTAL DD7 (P/N 601R318826-1) TOP FLANGE DENTED. (C-CHECK) RO: 12/06/2018 REMOVED AND REPLACED PASSENGER DOOR INTERCOSTAL DD7 IAW SRM. PRESSURIZED THE AIRCRAFT IAW AMM AND CHECKED FOR LEAKS IN THE REPAIR AREA. NO LEAKS NOTED.

Part: SKIN — DENTED (RT NR 2 SLAT) · 24,673 cycles

RH#2 SLAT HAS DENT AT WS178.00 - WS295.00. (C-CHECK) RO: 12/06/2018 DRESSED DENT IAW REO. OPS TEST GOOD AT THIS TIME.

Part: SKIN — DENTED (NR 1 SLAT) · 24,673 cycles

RH #1 SLAT DENT AT WS48.95 - WS178.00. (C-CHECK) RO: 12/06/2018 DRESSED DENT IN R/H #1 SLAT AT SS110.00 BACK TO ORIGINAL CONTOUR IAW REO. ALL CHECKS GOOD.

Part: SKIN — DENTED (BS 409-421) · 24,673 cycles

DENT ON RHS OF FUSELAGE AT FS409 TO FS421. (C-CHECK) RO: 12/06/2018 COMPLIED WITH REPAIR TO THE DENT ON R/H FUSELAGE FS 409 TO FS 421 IAW SRM ALL STEPS. PRESSURIZED THE AIRCRAFT IAW AMM AND CHECKED FOR LEAKS AT THE REPAIR AREA. NO LEAKS NOTED.

Part: SPIGOT — CRACKED (LT ENGINE PANEL) · 24,673 cycles

LH ENGINE PANEL 433AL HAS CRACKED SPIGOT. (C-CHECK) RO: 12/06/2018 REMOVED AND REPLACED SPIGOT P/N CN624-2067-205 ON TO PANEL 433AL IAW SRM.

Part: PANEL — CHAFED (LT ENGINE) · 24,673 cycles

LH ENGINE PANEL 433AL HAS CHAFING ON THE TOPHAT. (C-CHECK) RO: 12/06/2018 REMOVED AND REPLACED P/N CN624-2025-201 IAW SRM.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 32,844 hrs · 23,745 cycles

DURING MX INSPECTION, THE GALLEY LOWER AFT EMERGENCY LIGHT WAS FOUND TO HAVE ONE BULB INOPERATIVE. MX REMOVED AND REPLACED THE BULB AND OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,844 hrs · 23,745 cycles

DURING MX INSPECTION, THE CEILING ROW 10 EXIT LIGHT WAS FOUND INOPERATIVE. MX REMOVED AND REPLACED THE BULB AND OPS CHECKED GOOD. THE AC WAS APPROVED FOR RETURN TO SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,844 hrs · 23,745 cycles

DURING MX INSPECTION, THE LEFT, FWD OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MX REMOVED AND REPLACED THE BULB AND OPS CHECKED GOOD. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DRAG ANGLE — DAMAGED (PAX DOOR) · airframe 31,196 hrs · 22,519 cycles

COMPLY WITH GREO 670-52-11-072, REPAIR TYPE II. UPON REMOVAL OF AFT DRAG ANGLE, MAINTENANCE DISCOVERED SEVERAL OVER-SIZED HOLES. REPAIRED DRAG ANGLE AND PAX DOOR INNER SKIN PER REO 670-52-11-955 AND EC/TC REO 670-52-11-955. THIS IS A MAJOR REPAIR.

Part: SKIN PANEL — CRACKED (FUSELAGE) · airframe 31,196 hrs · 22,519 cycles

FUSELAGE SKIN CRACKED AT AFT LATCH FOR TRU DOOR 211 AL. REMOVED AND REPLACED LT SKIN PANEL AT TRU DOOR / HYDRAULIC BAY IAW EC/TC REO 670-53-11-1289 DATED 2017-06-05.

Part: FRAME — CORRODED (FUSELAGE) · airframe 31,196 hrs · 22,519 cycles

FS319 FRAME HAS CORROSION STR 26L - 26R. EVALUATED AND FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 53-21-06-101-002-A01. REPAIRED FRAME FS319 STR26L-26R IAW EC/TC REO 670-53-21-799 02 REV A AND REO 670-53-21-799 02.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 31,196 hrs · 22,519 cycles

FS280 BUTTSTRAP HAS CORROSION STR 27 - 23R. REMOVED CORROSION DAMAGE ON FS280 BUTT STRAP BTW STR 27 - 23R. COMPLIED WITH ECTC EA 32-2017-117 AND EA 32-2017-117. ALL DEFECTS CORRECTED.

Part: BRACKET — CORRODED (CARGO BAY) · airframe 31,196 hrs · 22,519 cycles

AFT CARGO DOOR NETTING FLOOR ANCHOR BRACKETS ARE CORRODED. REMOVED 3 EACH AFT CARGO DOOR NETTING FLOOR ANCHOR BRACKETS IAW SRM 51-42-06-001-001 A01& 51-42-21-001-001 A01. COMPLIED WITH EC/TC EO 700-53-00-00013 BY COMPLYING WITH THE FOLLOWING: FABRICATED PLATE ASSEMBLY P/N MM670-35329-009 IAW DRAWING MM670-35329. HEAT TREATED PART FOR EO 700-53-00-00013 IAW AMS 2770 REV N & AMS 2658 REV C. INSTALLED 2 OF 3 AFT CARGO DOOR NETTING FLOOR ANCHOR BRACKETS IAW SRM 51-42-06-001-001 A01 & 51-42-21-001-001 A01.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 31,197 hrs · 22,519 cycles

FS 280 FLOORBEAM CORRODED ON FWD SIDE. REMOVED AND REPLACED THE LT SIDE FLOORBEAM IAW SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, AND 51-42-22-001-001-A01.

Part: FLOOR SUPPORT — CORRODED (BS 280-319) · airframe 31,196 hrs · 22,519 cycles

RIGHT FLOOR SUPPORT CORRODED AT BS 280 - 319. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-06-001-001-A01, 51-42-20-001-001-A01, AND EC/TC SNIEO SH670-32170 S27.

Part: SKIN — DENTED (BS 202.75) · airframe 31,196 hrs · 22,519 cycles

SKIN AT BS 202.75, RBL 16 DENTED. REPAIRED IAW EA 20-2017-089 AND EC/TC EA 20-2017-089.

Part: ANGLE — CORRODED (BS 280) · airframe 31,196 hrs · 22,519 cycles

BS 280 FLOORBEAM ANGLE IS CORRODED. REMOVED AND REPLACED THE FLOORBEAM ANGLE IAW SRM 51-40-11-001-001-A01, SRM 51-42-00-001-001-A01, AND 51-42-21-001-001-A01.

Part: STRIKER — CORRODED (BS 319) · airframe 31,196 hrs · 22,519 cycles

GALLEY SERVICE DOOR LOWER SEAL STRIKER HAS CORROSION AT BS 319. REMOVED AND REPLACED GALLEY SERVICE DOOR SEAL STRIKER IAW SRM 51-42-06-001-001A01, AND DRAWING SH67031950.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 31,196 hrs · 22,519 cycles

BS 280 FLOORBEAM ANGLE IS CORRODED. REMOVED AND REPLACED THE FLOORBEAM ANGLE IAW SRM 51-40-11-001-001-A01, SRM 51-42-00-001-001-A01, AND 51-42-21-001-001-A01.

Part: ANGLE — CRACKED (BS 280) · airframe 31,196 hrs · 22,519 cycles

BS 280 WEB ANGLE CRACKED AT LBL 26. REMOVED AND REPLACED THE WEB ANGLE IAW SRM 51-42-06-001-001-A01, AND 51-40-11-001-001-A01.

Part: ANGLE — CORRODED (BS 280) · airframe 31,197 hrs · 22,519 cycles

FS 280 COCKPIT DOOR POST CORRODED AT LOWER CORNER. REMOVED AND REPLACED THE ANGLE IAW EA 32-2017-129 AND EC/TC EA 32-2017-129. T MAJOR REPAIR.

Part: BUTTSTRAP — CORRODED (BS 280) · airframe 31,197 hrs · 22,519 cycles

BS 280 BUTTSTRAP CORRODED AT STRINGERS 26L - 24R. REPAIRED IAW EA 32-2017-132, AND EC/TC EA 32-2017-132.

Part: POST — CORRODED (BS 280) · airframe 31,197 hrs · 22,519 cycles

LEFT BS 280 COCKPIT DOOR POST CORRODED AT LOWER CORNER. REMOVED & REPLACED CORRODED POST IAW EA 32-2017-128, & EC/TC EA 32-2017-128. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,196 hrs · 22,519 cycles

RT FLOOR SEAT TRACK CORRODED AT FS 349-485 RBL 9. REMOVED, FABBED NEW SECTION, INSTALLED PER EC/TC REO 670-53-00-343.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,196 hrs · 22,519 cycles

SEAT TRACK CORRODED AT FS 1047 RBL 9. REMOVED, FABBED NEW SECTION, INSTALLED PER EC/TC REO 670-53-00-343.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,196 hrs · 22,519 cycles

RT FLOOR SEAT TRACK CORRODED AT FS 677-830 RBL 9. REMOVED, FABBED NEW SECTION, INSTALLED PER EC/TC REO 670-53-00-343.

Part: PANEL — GOUGED (RT WING) · airframe 31,196 hrs · 22,519 cycles

PANEL 684 EB HAS CHAFE DAMAGE. REMOVED PANEL. ORDERED AND FABBED NEW PANEL PER SRM 51-40-11-001-001-A01.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 31,196 hrs · 22,519 cycles

INTERCOSTAL 27R HAS CORROSION BETWEEN FS 349-FS 364. REMOVED CORRODED INTERCOSTAL, LOCATED AND DRILLED NEW INTERCOSTAL, INSTALLED AND FINISHED PER SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01, 51-42-06-001-001-A01.

Part: FRAME — CORRODED (FUSELAGE) · airframe 31,196 hrs · 22,519 cycles

FS 310 FRAME CORRODED BETWEEN STR 27-26R. REMOVED CORROSION AND DAMAGED RIVETS. INSTALLED SERVICEABLE RIVETS AND RESTORED FINISH PER ECTC REO 670-53-21-1308.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,196 hrs · 22,519 cycles

LT SIDE WALL SEAT RAIL BETWEEN FS 785.15 + 863.00 HAS CORROSION DAMAGE. REMOVED, FABBED NEW SECTION, INSTALLED PER EC/TC REO 670-53-00-343.

Part: FRAME — CORRODED (FUSELAGE) · airframe 31,196 hrs · 22,519 cycles

FS 333 FRAME CORRODED BETWEEN STR 26L-26R. REMOVED CORROSION AND DAMAGED RIVETS. INSTALLED SERVICEABLE RIVETS AND RESTORED FINISH PER ECTC REO 670-53-21-1308.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 31,196 hrs · 22,519 cycles

STRINGER 25R HAS CORROSION BETWEEN FS 280-FS 319. REMOVED CORRODED INTERCOSTAL, LOCATED AND DRILLED NEW INTECOSTAL, INSTALLED AND FINISHED PER SRM 51-42-06-001-001-A01.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 31,196 hrs · 22,519 cycles

FLOOR SUPPORT ANGLE CORRODED FS 280. REMOVED AND INSTALLED A NEW SUPPORT ANGLE PER SRM 51-42-06-001-001-A01, 51-46-11-001-001-A01, 51-42-13-001-001-A01 AND DRAWING CC670-34010 REV J.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 31,196 hrs · 22,519 cycles

STRINGER 26R HAS CORROSION BETWEEN FS 280- FS 310. REMOVED STRINGER, RECEIVED AND LOCATED HOLES IN NEW STRINGER AND INSTALLED PER SRM 51-42-06-001-001-A01.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 31,196 hrs · 22,519 cycles

STRINGER 27L SPLICE HAS CORROSION BETWEEN FS 333-FS 349. REMOVED CORRODED INTERCOSTAL, LOCATED AND DRILLED NEW INTERCOSTAL, INSTALLED AND FINISHED PER SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01, 51-42-06-001-001-A01.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 31,196 hrs · 22,519 cycles

STRINGER 26L SPLICE HAS CORROSION BETWEEN FS 333-FS 349. REMOVED CORRODED INTERCOSTAL, LOCATED AND DRILLED NEW INTERCOSTAL, INSTALLED AND FINISHED PER SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01, 51-42-06-001-001-A01.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 31,196 hrs · 22,519 cycles

STRINGER 26R SPLICE HAS CORROSION BETWEEN FS 333-FS 349. REMOVED CORRODED INTERCOSTAL, LOCATED AND DRILLED NEW INTECOSTAL, INSTALLED AND FINISHED PER SRM 51-42-06-001-001-A01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,196 hrs · 22,519 cycles

LT SIDE WALL SEAT RAIL BETWEEN FS 708.00 + 761.85 HAS CORROSION DAMAGE. REMOVED CORRODED SEAT RAIL, FABBED NEW SEAT RAIL AND INSTALLED PER ECTC REO 670-53-343 AND 53-00-49-000/400-801-A17.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 31,196 hrs · 22,519 cycles

STRINGER 26L HAS CORROSION BETWEEN FS 295 - FS 310. REMOVED STRINGER, RECEIVED AND LOCATED HOLES IN NEW STRINGER AND INSTALLED PER SRM 51-42-06-001-001-A01.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 31,196 hrs · 22,519 cycles

INTERCOSTAL 26L CORRODED BETWEEN FS 349-FS 364. REMOVED CORRODED INTERCOSTAL, LOCATED AND DRILLED NEW INTERCOSTAL, INSTALLED AND FINISHED PER SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01, 51-42-06-001-001-A01.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 31,196 hrs · 22,519 cycles

STRINGER 26R SPLICE HAS CORROSION BETWEEN FS 333-FS 349. REMOVED CORRODED INTERCOSTAL, LOCATED AND DRILLED NEW INTECOSTAL, INSTALLED AND FINISHED PER SRM 51-42-06-001-001-A01.

Part: FRAME — CORRODED (FUSELAGE) · airframe 31,196 hrs · 22,519 cycles

FS 295 FRAME CORRODED BETWEEN STR 26L-25R. REMOVED CORROSION AND DAMAGED RIVETS. INSTALLED SERVICEABLE RIVETS AND RESTORED FINISH PER ECTC REO 670-53-21-1308.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,196 hrs · 22,519 cycles

RT SIDE WALL SEAT RAIL BETWEEN FS 677.00-724.08 HAS CORROSION DAMAGE. REMOVED CORRODED SEAT RAIL, FABBED NEW SEAT RAIL AND INSTALLED PER ECTC REO 670-53-343 AND 53-00-49-000/400-801-A17.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 31,196 hrs · 22,519 cycles

TCAS DOUBLER CORRODED BETWEEN FS 295- FS 310. REMOVED STRINGER, RECEIVED AND LOCATED HOLES IN NEW STRINGER AND INSTALLED PER SRM 51-42-06-001-001-A01.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 31,196 hrs · 22,519 cycles

STRINGER 25L HAS CORROSION BETWEEN FS 310- FS 319. REMOVED STRINGER, RECEIVED AND LOCATED HOLES IN NEW STRINGER AND INSTALLED PER SRM 51-42-06-001-001-A01.

Part: TAB — DAMAGED (HORIZ STAB) · airframe 30,796 hrs · 22,228 cycles

BOTH ANTI-ROTATION TABS OF THE HORIZONTAL STAB DAMAGED. REFER TO EC/TC 670BA-55-012 01 REV E AND SB 670BA-55-012 REV F PROCEDURE E, ITEMS A THRU M FOR ALL WORK ACCOMPLISHED.

Part: BULB — BURNED OUT (EMERENCY LIGHT) · airframe 29,900 hrs · 21,556 cycles

OVERHEAD EMERGENCY LIGHT INOPERATIVE AT ROW 9. REMOVED AND REPLACED THE BULB, OPS CHECKED GOOD IAW MM 33-51-09.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 27,167 hrs · 19,344 cycles

GALLEY AFT LOWER EMERGENCY LIGHT HAVE 2 LIGHT BULBS BURNED. R & R GALLEY AFT LOWER EMERGENCY LIGHT LIGHT BULBS IAW AMM 33-51-05. OPS CHECK GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 27,167 hrs · 19,344 cycles

CEILING EMERGENCY LIGHT BULB BURNED BY ROW 16. R & R CEILING EMERGENCY LIGHT BULB BY ROW 16 IAW AMM 33-51-09. OPS CHECK GOOD.

Part: POWER SUPPLY — DISCHARGED (EMERGENCY LIGHTS) · airframe 26,967 hrs · 19,180 cycles

FIRST FLIGHT OF DAY, EMERGENCY LIGHTS WOULD NOT ILLUMINATE. FOUND F/A EMERGENCY LIGHT GUARDED SWITCH IN ON POSITION. RECONFIGURED SWITCH TO NORMAL, CHARGED EMERGENCY LIGHT POWER SUPPLY IAW SDS 33-50-00, DISCREPANCY NO LONGER EXISTS, IAW MCC, NO FURTHER ACTION IS REQUIRED .

Part: SUPPORT — CORRODED (PAX DOOR) · airframe 25,531 hrs · 18,069 cycles

AIRSTAIR DOOR HAS CORROSION AT LOWER FWD STEP SUPPORT STRUCTURE. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. REMOVED CORROSION FROM LOWER FWD STEP SUPPORT STRUCTURE IAW SRM 51-21-06-001-001-A01.

Part: ANGLE — CORRODED (BS 939) · airframe 25,531 hrs · 18,069 cycles

ANGLE ON BS 939, BL 0, AFT WING TO FUSELAGE SUPPORT STRUCTURE IS CORRODED OUT OF LIMITS, UNDERLYING SUPPORT IS ALSO CORRODED. THIS REPAIR IS CLASSIFIED AS A MAJOR MINOR REPAIR IAW SOP 5702. REMOVED CORRODED ANGLE IA SRM 51-42-06-001-001-A01. REPLACED ANGLE REF SRM 51-40-11-001-001-A01 & SRM 51-42-06-001-001-A01. REMOVED CORROSION FOR UNDERLYING STRUCTIVE IAW SRM 51-21-06-001-001-A01. RESTORED FINISH REF: 51-25-01-001-001-A01 & 51-21-16-001-001-A01 SRM.

Part: ANGLE — CORRODED · airframe 25,531 hrs · 18,069 cycles

MOUNTING ANGLE HAS CORROSION AT SERVICE DOOR. CORROSION IS OUT OF LIMITS IAW SRM 53-21-23-101-002-A01. REMOVED DAMAGED ANGLE IAW SRM 51-42-06-001-001-A01. INSTALLED A NEW ANGLE IAW SRM 51-42-06-001-001 AND DWG SH670-31950. MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (BS 320) · airframe 25,524 hrs · 18,063 cycles

FLOOR SUPPORT HAS CORROSION AT BS 320 AT RBL 45. REMOVED THE SERVICE DOOR LOWER SILL ANGLE, REFERRED TO AS UPPER SUPPORT ANGLE IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. DRILLED AND INSTALLED FLOOR SILL UPPER SUPPORT KOT MOUNTING ANGLE IAW SRM 51-42-06-001-001-A01. INSTALLED LIGHTNING DIVERTER PANEL BRACKETS ON NEW LOWER SILL ANGLE IAW SRM 51-42-00-001-001 AND DWG SH690-32120.

Part: FLOOR SUPPORT — CORRODED (BS 310) · airframe 25,531 hrs · 18,069 cycles

FLOOR SUPPORT HAS CORROISON AT FWD END OF ASD, NEAR BS 310. INSTALLED NEW FLOOR SUPPORT IAW DWG SH670-31810 AND SRM 51-42-06-001-001-A01. MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (BS 333) · airframe 25,524 hrs · 18,063 cycles

FLOOR SUPPORT HAS CORROSION AT LBL 9 AT BS 333. R & R PACKER IAW DWG SH670-32120 AND SRM 51-42-06-001-001. MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (BS 319) · airframe 25,524 hrs · 18,063 cycles

FLOOR SUPPORT HAS CORROSION AT RBL 45 AT BS 319. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. COMPLIED WITH REO 670-53-21-1125. FABRICATED ANGLES FOR REPAIR IAW SRM 51-24-21-001-001-A01 FROM 70750-0.063" & REO 670-53-21-1125.

Part: STRUCTURE — CORRODED (BS 333) · airframe 25,524 hrs · 18,063 cycles

CORROSION ON PACKER ON FLOOR SUPPORT AT FS 333 AT LBL9. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. REMOVED PACKER CORROSION IAW SRM 51-21-06-001-001-A01 MATERIAL REMOVED EXCEED LIMITS. INSTALLED NEW PACKER ON FLOOR SUPPORT AT FS 333 ON IAW SRM 51-42-06-001-001, AND DWG SH670-32120.

Part: DOOR SILL — CORRODED (BS 310-349) · airframe 25,531 hrs · 18,069 cycles

PAX DOOR SILL HAS CORROSION SEVERAL PLACES AT BS 310-349. INSTALLED NEW DOOR SILL IAW DWG SH670-31810 AND SRM 51-42-06-001-001-A01. MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (BS 333) · airframe 25,531 hrs · 18,069 cycles

FLOOR SUPPORT HAS CORROSION BS 333 RBL 9. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01, SRM. REPAIRED IAW REO 670-53-21-1123. MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (BS 349) · airframe 25,531 hrs · 18,069 cycles

FLOOR SUPPORT HAS CORROSION AT FS 349, LBL5. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. REPAIRED IAW REO 670-53-21-1126.

Part: ANGLE — CORRODED · airframe 25,531 hrs · 18,069 cycles

TWO LOWER SILL ANGLES HAVE CORROSION AFT SERVICE DOOR. R & R THE ANGLES IAW SRM 51-42-06-001-001-A01.

Part: HINGE — DETERIORATED (MLG DOOR) · airframe 25,524 hrs · 18,063 cycles

AFT MLG DOOR HINGE FWD HOLE IS OVERSIZED OVER SB 670BA-57-020 LIMITS. REMOVED AFT LANDING GEAR DOOR HINGE AND FASTENERS IAW SRM 51-42-21-001-001-A01. COMPLIED WITH REO 670-57-21-734 P-1. DRILLED BRUSH CAD, AND RESTORED FINISH TO NEW SERVICEABLE FITTING, IAW SRM 51-40-11-001-001, 51-21-11-001-001, 51-25-06-001-001, AND REO 670-57-21-734. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 813-985) · airframe 25,515 hrs · 18,058 cycles

LEFT SEAT TRACK BS 813 - 985 CORRODED IN SEVERAL AREAS ALONG THE LENGTH OF THE TRACK. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 (A03), AMM 53-00-49-400-801 (A03).

Part: SEAT TRACK — CORRODED (BS 693-813) · airframe 25,515 hrs · 18,058 cycles

LEFT SEAT TRACK BS 693 - 813 CORRODED ALONG THE LENGTH THE TRACK. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-00-49-000-801(A03) AND AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 813-985) · airframe 25,515 hrs · 18,058 cycles

RIGHT SEAT TRACK BS 813 - 985 CORRODED IN SEVERAL AREAS ALONG THE LENGTH OF THE TRACK. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801(A03), AMM 53-00-49-400-801-A03, AND REO 670-53-00-343.

Part: SEAT TRACK — CORRODED (BS 693-813) · airframe 25,515 hrs · 18,058 cycles

RIGHT SEAT TRACK BS 693 - 813 CORRODED IN SEVERAL AREAS ALONG THE LENGTH OF THE TRACK. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 (A03), EC/TC 670-53-00-343 BP570692, AND AMM 53-00-46-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 675-712) · airframe 25,492 hrs · 18,041 cycles

SEAT TRACK BS 675 - 712 CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-49-101-001-A01. R & R SEAT TRACK IAW AMM TASKS 53-00-49-000-801, 53-00-49-400-801, AND REO 670-53-00-343.

Part: SEAT TRACK — CORRODED (BS 379-485) · airframe 25,515 hrs · 18,058 cycles

LEFT SEAT TRACK BS 379 - 485 CORRODED AND SCRATCHED ALONG THE LENGTH OF THE TRACK. R & R THE SEAT TRACK IAW AMM 53-00-49-000 AND AMM 53-00-49-400-801. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 860-969) · airframe 25,513 hrs · 18,057 cycles

SEAT TRACK BS 860 - 969 CORRODED & SCRATCHED ALONG THE LENGTH OF THE TRACK. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 AND AMM 53-00-49-400-801. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 785-860) · airframe 25,513 hrs · 18,057 cycles

SEAT TRACK BS 785-860 CORRODED ALONG THE LENGTH OF THE TRACK. R & R THE SEAT TRACK IAW AMM TASK 53-00-49-000-801, & REO 670-53-00-343, REV F. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 349-485) · airframe 25,515 hrs · 18,058 cycles

RIGHT SEAT TRACK BS 349 - 485 CORRODED AND SCRATCHED ALONG THE LENGTH OF THE TRACK. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-900-801, REO 670-53-00-343, REV F, AND AMM 53-00-49-400-801. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 712-761) · airframe 25,513 hrs · 18,057 cycles

SEAT TRACK BS 712 - 761 CORRODED & SCRATCHED ALONG THE LENGTH OF THE TRACK. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 AND AMM 53-00-49-400-801. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 681-677) · airframe 25,515 hrs · 18,058 cycles

RIGHT SEAT TRACK FROM BS 581 - 677 CORRODED AND SCRATCHEED ALONG THE LENGTH OF THE TRACK. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801, SRM 53-31-49-101-001-A01, AND AMM TASK 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 860-969) · airframe 25,513 hrs · 18,057 cycles

SEAT TRACK BS 860 - 969 CORRODED & SCRATCHED ALONG THE LENGTH OF THE TRACK. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801, AND AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 712-761) · airframe 25,513 hrs · 18,057 cycles

SEAT TRACK BS 712 - 761 CORRODED ALONG THE LENGTH OF THE TRACK. R & R SEAT TRACK IAW AMM 53-00-49-000 AND 400-801-A03.

Part: SEAT TRACK — CORRODED (BS 581-677) · airframe 25,515 hrs · 18,058 cycles

LEFT SEAT TRACK BS 581 - 677 CORRODED AND SCRATCHED ALONG THE LENGTH OF THE TRACK. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 53-00-49-000-801-A03, AND SRM 51-45-00-001-001-A01. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 570-675) · airframe 25,513 hrs · 18,057 cycles

SEAT TRACK BS 570 - 675 CORRODED & SCRATCHED ALONG THE LENGTH OF THE TRACK. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 AND AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 485-570) · airframe 25,515 hrs · 18,058 cycles

RIGHT SEAT TRACK BS 485 - 570 CORRODED ALONE THE LENGTH OF THE TRACK. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801, AND AMM 53-00-49-400-801. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 785-860) · airframe 25,513 hrs · 18,057 cycles

SEAT TRACK BS 785 - 860 CORRODED & SCRATCHED ALONG THE LENGTH OF THE TRACK. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801, AMM 53-00-49-40-801, AND EC/TC REO 670-53-00-343.

Part: SEAT TRACK — CORRODED (BS 485-570) · airframe 25,515 hrs · 18,058 cycles

LEFT SEAT TRACK BS 485 - 570 IS CORRODED AND SCRATCHED ALONG THE LENGTH OF THE TRACK. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801, AND AMM 53-00-49-400-801. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 517-581) · airframe 25,515 hrs · 18,058 cycles

LEFT SEAT TRACK BS 517-581 CORRODED AND SCRATCHED ALONG THE LENGTH OF THE TRACK. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801, REO 670-53-00-343, GREO 670-53-00-343 REV F, AND AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 379-485) · airframe 25,515 hrs · 18,058 cycles

RIGHT SEAT TRACK BS 379 - 485 CORRODED AND SCRATCHED ALONG THE ENTIRE LENGTH. THIS REPAIR IS CLASSIFIED AS A REMOVED AND REPLACED THE SEAT TRACK IAW AMM TASK 53-00-49-000-801, REO 670-53-00-343, GREO 670-53-00-343, REV F, AND AMM TASK 53-00-49-400-801. MAJOR REPAIR.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 25,515 hrs · 18,058 cycles

DURING INSTALLATION OF THE BS 280 FLOORBEAM, FOUND A CRACKED ANGLE AT RBL38.50. REMOVED THE DAMAGED ANGLE IAW SRM 51-42-06-001-001-A01. INSTALLED SERVICEABLE ANGLE FABRICATED IAW SNIEO CC670-34010, EXCEPT WHERE ALTERNATE FASTENERS WERE SPECIFIED BY SB 670BA-53-041, REV D AND GREO 670-53-11-594. RECEIVED EO SNEIEO CC670-3410-S04 AMD COMPLIED WITH STEPS 1-3 AS NEEDED.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 25,515 hrs · 18,058 cycles

RIGHT SEAT TRACK BS 485 - 581 CORRODED ALONG THE LENGTH OF THE TRACK. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801, REO 670-53-00-343, REV F, AND AMM 53-00-49-400-801. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 570-675) · airframe 25,513 hrs · 18,057 cycles

SEAT TRACK BS 570 - 675 CORRODED & SCRATCHED ALONG THE LENGTH OF THE TRACK. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-49-101-001-A01, FIG 53-31-49-991-804. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 A03 AND AMM TASK 53-00-49-400-801.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 25,513 hrs · 18,057 cycles

DURING ACCOMPLISHEMENT OF SB FOUND RT BULKHEAD LOWER WEB BS 280 CORRODED. BLENDED CORROSION DAMAGE IAW SRM 51-21-06-001-001-A01 DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-11-10-201-003-A01. COMPLIED WITH REO 670-53-11-594. LOCATED & DRILLED UP HOLES IN STRAP & WEB IAW REO 670-53-11-594. MAJOR REPAIR.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 25,513 hrs · 18,057 cycles

DURING ACCOMPLISHMENT OF SB FOUND LT BULKHEAD LOWER WEB BS 280 CORRODED. BLENDED CORROSION DAMAGE IAW SRM 51-21-06-001-001-A01. FOUND DAMAGE TO BE OUT OF LIMITS IAW SRM 53-11-10-201-003-A01. R & R BULKHEAD WEB IAW REO 670-53-11-594. LOCATED & DRILLED UP HOLES WEB IAW REO 670-53-11-594. MAJOR REPAIR.

Part: HINGE — GOUGED (PAX DOOR) · airframe 25,513 hrs · 18,057 cycles

PAX DOOR HINGE HAS TWO LUGS GOUGED NR 14 AND NR 23 COUNTING FWD TO AFT. REPAIRED IAW REO 670-52-11-511. MAJOR REPAIR.

Part: LIGHT — DETERIORATED (CABIN) · airframe 25,515 hrs · 18,058 cycles

EMERGENCY LIGHT WORN & FADED. R & R THE EMERGENCY LIGHT IAW AMM 33-51-01-000-801, 33-51-01-400-801, AND AMM 33-51-01, REV A.

Part: SKIN — DAMAGED (BS 1031-1070) · airframe 25,531 hrs · 18,069 cycles

FOUR BURNED FASTENERS ON STRINGER 24L BETWEEN FS 1031 AND 1070.70. REMOVED 4 EA BLIND FASTENERS IAW SRM 51-42-10-001-001-A01 AND 53-00-00-201-003-A01, STEP 3.C 1, A. EVALUATED 4EA FASTNER HOLES FOR PERMANENT REPAIR DISPOSITION. REMOVED SEALANT FROM 4EA FASTENERS HOLES IAW AMM 51-23-00-100-801 AND FOUND NO DAMAGE TO COUNTERSINK OR SHAFT OF 4 EA INSTALLED 4EA FASTENERS IAW SRM 53-00-00-201-003-A01, REPAIR TYPE III 51-42-06-001-001-A01, 51-23-00-001-001-A0, STEP F.

Part: SKIN — DENTED (BS 409-421) · airframe 25,531 hrs · 18,069 cycles

DENT RT FUSELAGE BETWEEN FS 409 AND FS 421 BETWEEN STR 16R AND 17R. COMPLIED WITH EC/TC EA 32-2014-060 PERMANENT REPAIR. EVALUATED DAMAGE AND SUBMITTED TO STS ENGINEERING FOR PERMANENT REPAIR. COMPLIED WITH STS EA 32-2014-060. RECEIVED AND COMPLIED WITH ECTC EA 32-2014-060.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 24,632 hrs · 17,409 cycles

NR 5 LT AFT, EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMPS IAW AMM 33-51-15, OPS CHECKED GOOD.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 24,417 hrs · 17,257 cycles

EMERGENCY EXIT SIGN BY FWD ENTRY DOOR. R & R EMERGENCY EXIT SIGN COVER/LENS BY FWD ENTRY DOOR IAW AMM 33-51-05, NEF CLEARED.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 22,701 hrs · 16,012 cycles

PAX DOOR DRAG ANGLE, AFT SIDE, CRACKED, MARKED. REPAIRED IAW 601R-31772-5.

Part: DOOR — OUT OF ADJUST (SERVICE) · airframe 21,814 hrs · 15,397 cycles

CATERING REPORTS THAT SERVICE DOOR IS DIFFICULT TO OPEN & CLOSE. ADJUSTED SERVICE DOOR. LINAGE IAW AMM 52-41-00. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: DOOR — LACK OF LUBE · airframe 21,814 hrs · 15,397 cycles

SERVICE DOOR IS VERY DIFFICULT TO OPEN FROM THE OUTSIDE. LUBRICATED DOOR IAW AMM TASK 12-20-52-640-801-A01. OPS CHECKED GOOD, NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: CONTROL PANEL — UNSERVICEABLE (TRIM SYS) · airframe 21,576 hrs · 15,231 cycles

AILERON AND RUDDER TRIM UNCOMMANDED DEFLECTIONS. EMERGENCY DECLARED, ACFT RETURNED TO DEPARTURE. R & R AILERON/RUDDER TRIM CONTROL PANEL IAW 700 27-12-10. PERFORMED OPS TEST OF AILERON/RUDDER TRIM IAW AMM 27-11-00-710-802 AND 27-22-00-710-801. NO FAULTS FOUND AT THIS TIME.

Part: FLAP SYSTEM — FAILED · airframe 21,228 hrs · 14,962 cycles

FLAPS FAIL & SLATS FAIL. RAN QRH AND FAULTS CLEARED. EMERGENCY DECLARED. SYSTEM RESET IAW MCC, NO FURTHER ACTION REQUIRED.

Part: SILL — CORRODED (AFT CARGO DOOR) · airframe 20,539 hrs · 14,461 cycles

AFT CARGO DOOR SILL CORRODED. REPAIRED IAW SRM 51-42-06-001-001-A01.

Part: STRINGER — CORRODED (BS 333-349) · airframe 20,539 hrs · 14,461 cycles

AVIONICS COMPARTMENT, STRINGER 26R IS CORRODED BETWEEN BS 333-349. REMOVED AND REPLACED STRINGER IAW SRM 51-42-06-001-001-A01.

Part: STRINGER — CORRODED (BS 319-333) · airframe 20,533 hrs · 14,453 cycles

STRINGER 26R IS CORRODED BETWEEN FS 319 - 333. APPLIED FINISH COAT TO ALL BARE FASTENERS SRM 5142-06-001-001-A01.

Part: FLOOR PANEL — CRACKED (E/E BAY) · airframe 20,533 hrs · 14,453 cycles

RIGHT ELECTRICAL BAY FLOOR AT FS 193 IS CRACKED. REPAIRED IAW REO 670-53-11-509.

Part: FLOOR SUPPORT — CORRODED (BS 1015-1031) · airframe 20,533 hrs · 14,453 cycles

AFT CARGO RT FLOOR SUPPORT IS CORRODED BETWEEN FS 1015 - 1031. REMOVED CORROSION DAMAGE IAW SRM DAMAGE IAW SRM 51-21-06-001-001-A01 AND FOUND AREA TO OUT OF LIMITS IAW SRM 51-61-43-101-001-A01. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW MAC NDT INSPECTION PROCEDURE UT-3. MIN MATERIAL REMAINING IS .0259", ORIGINAL IS .063", MATERIAL REMOVED IS .004". REPAIRED IAW REO 670-53-61-875.

Part: FLOOR SUPPORT — CORRODED (BS 1015) · airframe 20,533 hrs · 14,453 cycles

AFT CARGO RT FLOOR SUPPORT IS CORRODED JUST FORWARD OF FS 1015. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01 AND FOUND AREA TO OUT OF LIMITS. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW MAC NDT INSPECTION UT-3. MIN MATERIAL REMAINING IS .062", ORIGINAL IS .063" MATERIAL REMOVED IS .001". REPAIRED IAW REO 670-53-61-875.

Part: FLOOR SUPPORT — CORRODED (BS 1031-1051) · airframe 20,533 hrs · 14,453 cycles

AFT CARGO RT FLOOR SUPPORT IS CORRODED BETWEEN FS 1031 - 1051. REMOVED CORROSION DAMAGE IAW SRM 51-21-06-001-001-A01 AND FOUND TO BE OUT OF LIMITS IAW SRM 51-61-43-101-001-A01. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW MAC NDT INSPECTION PROCEDURE UT-3, MIN MATERIAL REMAINING IS .049", ORIGINAL IS .063" MATERIAL REMOVED IS .014" REPAIRED IAW REO 670-53-61-875.

Part: SILL — CORRODED · airframe 20,533 hrs · 14,453 cycles

PAX DOOR SILL IS CORRODED ON FORWARD SIDE. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-21-23-101-001-A01. REMOVED SILL IAW SRM 51-42-06-001-001-A01. INSTALLED NEW DOOR SILL IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 20,533 hrs · 14,453 cycles

FLOOR SUPPORT AT PAX DOOR IS CORRODED. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-21-23-101-001-A01. REMOVED FLOOR SUPPORTAW SRM 51-41-02-001-001-A01. INSTALLED NEW ANGLE IAW SRM 51-41-02-001-001-A01.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 20,533 hrs · 14,453 cycles

FLIGHT COMPARTMENT FLOORBEAM ANGLE AT FS 280 IS CORRODED AROUND NUTPLATES. REMOVED CORROSION, OUT OF ALLOWABLE LIMITS IAW SRM 51-21-06-001-001-A01, & 53-00-00-101-001-A01. REMOVED CORRODED ANGLE, LOCATED, DRILLED AND INSTALLED NEW ANGLE IAW SRM 51-40-06-001-00-1-A01, SRM 51-40-11-001-001-A01, SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 20,533 hrs · 14,453 cycles

REMOVED AND REPLACED FOUR CORRODED ANGLES FROM UPPER ASD JUST BELOW HINGE IAW SRM 51-42-06-001-001-A01. REPAIR CLASSIFIED AS A MINOR.

Part: SUPPORT — CORRODED (BS 265-280) · airframe 20,539 hrs · 14,461 cycles

FWD JACKING POINT SUPPORT IS CORRODED BETWEEN FS 265-280 AND S26L-26R. FOUND FWD JACKING POINT SUPPORTS OUT OF LIMITS, REPLACED LT & RT SUPPORTS IAW SRM 51-42-06-001-001 & 51-42-21-001-001.

Part: FLOOR SUPPORT — CORRODED (BS 280) · airframe 20,533 hrs · 14,453 cycles

FLOOR SUPPORT AT FS 280.00 IS CORRODED. PERFORMED CUT-OUT IAW REO 670-53-21-139 STEP 1 & 2. COMPLIED WITH STEP 3 OF REO 670-53-139 IAW NDTM PART 1, 51-20-006, NO INDICATIONS NOTED. INSTALLED REPAIR IAW WITH REO 670-53-21-139.

Part: FLOOR PANEL — CRACKED (E/E BAY) · airframe 20,533 hrs · 14,453 cycles

LEFT ELECTRICAL BAY FLOOR AT FS 193 IS CRACKED. COMPLY WITH ECTC REO 670-53-11-509. COMPLIED WITH ECTC REO 670-53-11-509 AND REO 670-53-11-509, REV.

Part: FLOOR PANEL — CRACKED (E/E BAY) · airframe 20,533 hrs · 14,453 cycles

RIGHT ELECTRICAL BAY FLOOR AT FS 193 IS CRACKED. CUT OUT CRACK IAW REO 670-53-11-509. COMPLIED WITH STEP 11 OF EC/TC REO 670-53-11-509 IAW NDTM PART 1, 51-20-006. NO CRACK INDICATIONS NOTED. FABRICATED AND INSTALLED DOUBLER IAW REO 670-53-11-509.

Part: STRINGER — CORRODED (BS 319-333 S26R) · airframe 20,533 hrs · 14,453 cycles

STRINGER 26R IS CORRODED BETWEEN FS 319 - 333. REMOVED CORROSION IAW SM 51-21-06-001-001-0-A01, OUT OF LIMITS IAW SRM 53-21-03-101-02-A01. REMOVED STRINGER IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. DRILLED EXISTING HOLES IN NEW STRINGER IAW SRM 51-40-11-001-001-A01. LOCATED HOLES IN NEW STRINGER SPLICE IAW SRM 51-40-11-001-001-A01 AND INSTALLED NEW STRINGER & NEW SPLICE IAW SRM 51-42-06-001-001-A01.

Part: STRINGER — CORRODED (BS 319-33) · airframe 20,533 hrs · 14,453 cycles

STRINGER 25 RIGHT IS CORRODED BETWEEN FS 319-333. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW MAC NDT INSPECTION PROCEDURE UT-3. MIN MATERIAL REMAINING IS .042", ORIGINAL IS .063:, MATERIAL REMOVED IS .021". REPAIRED IAW REO 670-53-21-865.

Part: STRINGER — CORRODED (BS 333-349) · airframe 20,539 hrs · 14,461 cycles

AVIONICS COMPARTMENT, STRINGER 26R IS CORRODED BETWEEN FS 333-349. REMOVED CORROSION IAW SRM 51-21-06-001-001-0-A01, OUT OF LIMITS IAW SRM 53-21-03-101-02-A01. REMOVED STRINGER IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01. INSTALLED NEW STRINGER & SPLICE IAW SRM 51-42-06-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 708-701.85) · airframe 20,533 hrs · 14,453 cycles

LEFT SIDE SEAT TRACK AT FS 708 TO 701.85 CORRODED. REMOVED CORROSION AND FOUND TO BE OVER ALLOWABLE LIMITS IAW SRM 53-14-49-101-001-A01. R & R SEAT TRACK AT FS 708-761.85 IAW AMM TASKS 53-00-49-000-801 (CONFIG A03) & 53-00-49-400-801 (CONFIG A03).

Part: CAP — CORRODED (DOOR) · airframe 20,533 hrs · 14,453 cycles

CAP ON HINGE SIDE OF ASD CORRODED. REMOVED ASD HINGE CORNER CAPS IAW SRM 51-42-06-001-001-A01. INSTALLED NEW FWD & AFT HINGE CORNER CAPS IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01.

Part: STRINGER — CORRODED (BS 319-333 S25L) · airframe 20,533 hrs · 14,453 cycles

STRINGER 25L IS CORRODED BETWEEN FS 319.00-333.00. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW MAC NDT PROCEDURES UT-3, MIN MATERIAL REMAINING IS .038", ORIGINAL IS .063:, MATERIAL REMOVED IS .025". REPAIRED IAW REO 670-53-21-865.

Part: STRINGER — CORRODED (BS 319-333) · airframe 20,533 hrs · 14,453 cycles

STRINGER 26L IS CORRODED BETWEEN FS 319.00-333. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW MAC NDT INSPECTION PROCEDURES UT-3, MIN MATERIAL REMAINING IS .052", ORIGINAL IS .063:, MATERIAL REMOVED IS .011". REPAIRED IAW REO 670-53-21-865.

Part: DOOR — UNSECURE (EMERGENCY EXIT) · airframe 17,779 hrs · 12,518 cycles

RT EMERGENCY EXIT CAUTION LIGHT COMES ON INTERMITTENTLY. RESECURED RT OVERWING EMERGENCY DOOR IAW AMM 52-21-00. RESECURED RT OVERWING EMERGENCY DOOR IAW AMM 52-21-00.

Part: LIGHT — TORN (CABIN) · airframe 17,628 hrs · 12,407 cycles

EMERGENCY FLOOR STRIP AT RT EXIT ROW IS TORN UP. R & R EMERGENCY FLOOR PATH STRIP WITH RED ARROWS AT THE RT EMERGENCY ROW IAW AMM 33-51-01.

Part: BATTERY — WEAK (MEGAPHONE) · airframe 16,622 hrs · 11,695 cycles

MEGAPHONE WEAK. R & R BATTERY IAW AMM 25-90-01.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 16,566 hrs · 11,652 cycles

PAX DOOR AFT DRAG ANGLE IS CRACKED AT POWER ASSIST PULLEY BRACKET. COMPLIED WITH EC/TC REO 670-52-11-072 PER REO 670-52-11-072 REV C AND REO 670-52-11-533.

Part: SEAT TRACK — CORRODED (BS 581-677) · airframe 16,566 hrs · 11,652 cycles

RT FLOOR SEAT TRACK HAS CORROSION FROM FS 581.0 TO FS 677.0. REMOVED AND REPLACED FLOOR SEAT TRACK IAW SRM 51-41-02 AND 51-40-06.

Part: SEAT TRACK — CORRODED (BS 377) · airframe 16,566 hrs · 11,652 cycles

LEFT SEAT TRACK HAS CORROSION AT FS 677. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-41-02 AND 51-40-06 AND AMM 33-00-49.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 16,566 hrs · 11,652 cycles

RT NR 5 SIDE SEAT TRACK CORRODED. REMOVED SEAT TRACK & INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-00-49.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 16,566 hrs · 11,652 cycles

FROM LEFT TO RIGHT AT FS 280 FOUND HEAVY CORROSION ON TOP OF BEAM. REMOVED AND REPLACED BEAM AT FS 280 IAW SRM`S 51-40-06, 51-41-02, 51-42-06, 51-42-15, 51-42-28, 51-42-02, 51-40-11, 51-23-00, 51-21-11, & 51-21-16.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 16,566 hrs · 11,652 cycles

LEFT NR 5 SEAT TRACK IS CORRODED. REMOVED SEAT TRACK IAW AMM 53-00-49 & INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-00-49.

Part: BEAM — CORRODED (FUSELAGE) · airframe 16,566 hrs · 11,652 cycles

ON BOTTOM OF FS 280 BEAM, BOTH LEFT AND RIGHT OF DRIP DRAINS HAVE CORROSION AROUND DRAINS. (17550 P.75) R & R 280 BEAM IAW BA. REO 670-53-11-026 REV B.

Part: FASTENER — CORRODED (FUSELAGE) · airframe 16,566 hrs · 11,652 cycles

6 BLIND FASTENERS CORRODED ON LEFT AND RIGHT DRIP TRAYS AT DRAIN AREA (17550 P.75) RESOLVED ON W/O: 178779 TASKCARD: N/R-00149, S\N 144 51939-1000-0022. REMOVED AND REPLACED 6 BLIND FASTENERS ON LT AND RT DRIP TRAYS REF AAR W/C 51939-1000-0020 FOR DETAILS INSTALLATION.

Part: PLACARD — DAMAGED (CABIN) · airframe 16,566 hrs · 11,652 cycles

CREW ESCAPE HATCH EXTER PLACARDS (OPEN, CLOSED, EMER EXIT, AND ARROW) REQUIRE REPLACEMENT. APPLIED "EMERGENCY EXIT HANDLE INSTRUCTIONS" SILKSCREEN PRINT IAW AMM 20-60-11-000-801 ALSO RE-APPLIED "ARROW" FOR OPEN TO CLOSE".

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 16,467 hrs · 11,582 cycles

FLOOR LEVEL EMERGENCY FLOODLIGHT AFT OF SERVICE DOOR INOP. RELAMPED FLOOR LEVEL EMERGENCY FLOODLIGHT AFT OF SERVICE DOOR IAW AMM 33-51-11. RELAMPED FLOOR LEVEL EMERGENCY FLOODLIGHT AFT OF SERCICE DOOR IAW AMM 33-51-11. (CLOSED)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 15,818 hrs · 11,079 cycles

LEFT EXTERIOR FUSELAGE AFT EMERGENCY LIGHT INOP. RELAMPED BY REMOVED LENS COVER BY REMOVING 4 SCREWS RELAMPED BY PUSHING & TURNING OLD LAMP, INSERTED NEW LAMP PUSHED & TURNED TO LOCK INPLACE REINSTALLED LENS COVER & SCREWS IAW SOP806 PERFORMED OPS TEST OF EXTERIOR EMERG LIGHTS IAW AMM 33-51-15-710-801 OPS TEST GOOD SL7318 6/29/10.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 15,495 hrs · 10,838 cycles

MAIN CABIN EMERGENCY EXIT LIGHT HAS 2EA LAMPS BURNED OUT, LT ESCAPE HATCH LOWER LIGHT. REPLACED 2EA BURNED OUT LAMPS AT ESCAPE HATCH LT LOWER EMERGENCY LIGHT. OPS CHECK GOOD IAW AMM 33-51-05.

Part: SEAT TRACK — CORRODED (BS 430-549) · airframe 15,474 hrs · 10,822 cycles

MAIN CABIN RT INBD SEAT TRACK HAS SPOTS OF CORROSION FROM STA 430 TO 549 AS MARKED. R & R RT INBD CABIN SEAT TRACK FROM STA 485 TO 581 IAW MM 53-00-49.

Part: SEAT TRACK — CORRODED (BS 349) · airframe 15,474 hrs · 10,822 cycles

MAIN CABIN RT IB SEAT TRACK HAS CORR. R & R CABIN RT INBD SEAT TRACK FROM STA 349 TO 485 IAW MM 53-00-49.

Part: LIGHT — DAMAGED (CABIN) · airframe 14,821 hrs · 10,340 cycles

ABOUT 18 INCHES OF FLOOR EMERGENCY LIGHTING STRIP IS DAMAGED NEAR GALLEY CARTS. REMOVED & REPLACED EMERGENCY LIGHTING STRIP IN FRONT OF GALLEY CARTS IAW AMM 33-51-01.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 14,494 hrs · 10,085 cycles

EMERGENCY EXIT ROWS SMALL "EXIT" SIGNS HAVE MULTIPLE LIGHTS OUT.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 13,268 hrs · 9,161 cycles

IN THE ARM POSITION, THE EMERGENCY LIGHTS WOULD CONTINUOUSLY FLASH ON AND TURN OFF DURING FLIGHT. FLT 5188 DEL 134 MINS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,879 hrs · 8,842 cycles

RIGHT SIDE FUSELAGE AFT EMERGENCY LIGHT INOP.

Part: STRUCTURE — CORRODED (ASD) · airframe 11,575 hrs · 7,830 cycles

BOTTOM ASD STEP CORRODED WHERE BOTTOM FOLDING STEP ATTACHES.

Part: SUPPORT — CRACKED (LT MLG WW) · airframe 11,575 hrs · 7,830 cycles

LT WHEEL WELL FWD OUTBOARD BIN ATTACH SUPPORT IS CRACKED.

Part: INTERCOSTAL — CRACKED (ASD) · airframe 11,575 hrs · 7,830 cycles

INTERCOSTAL CRACKED INSIDE ASD AFT ACCESS PANEL 832BR. REMOVED AND REPLACED INTERCOSTAL IN ACCESS PANEL 832BR IAW CRJ 700 SRM 51-42-06 AND 51-42-21. SUPPLEMENTAL-SDR CLOSED 11/17/2008.

Part: FRAME — CORRODED (BS 280) · airframe 11,575 hrs · 7,830 cycles

CORROSION ON 280 FRAME AT RBL 9. CORROSION OUT OF LIMITS. REMOVED AND REPLACED FRAME.

Part: WEB — CORRODED (FUSELAGE) · airframe 11,575 hrs · 7,830 cycles

CORROSION ON RT 280 WEB. REMOVED AND REPLACED RT 280 WEB PER CRJ 700 SRM 51-42-06 AND 51-42-13. REMOVED AND REPLACED 4 EA ATTACH ANGLES CUT RT 280 WEB. CC670-34117-5 WAS PRE-FAB REMAINING ATTACH ANGLES IAW CRJ 700 SRM DWG CC670-34-100 AND 51-24-16. COMPLIED WITH FP 1 OF FABBED PARTS IAW NDTM 51-20-08. FABRICATED RT SPLICE PLATE (P/N CC670-34251-2 ) IAW CRJ 700 SRM 51-24-16 AND 700 SRM 53-11-10. INSTALLING RT WEB AND ATTACH ANGLES PER CRJ 700 SRM 51-42-06 AND 51-42-13. SUPPLEMENTAL-SDR CLOSED 11/17/2008.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 11,575 hrs · 7,830 cycles

CORROSION ON FWD FLOOR SUPPORT AT STA 280. CORROSION ON FWD FLOOR SUPPORT AT STA 280 IS OUT OF LIMITS. REMOVED CORRODED SUPPORT, LOCATED DRILL AND INSTALLED NEW SUPPORT PER CRJ 700 SRM 51-40-00, 51-42-06 AND 51-44-00. SUPPLEMENTAL-SDR CLOSED 11/17/2008.

Part: WEB — CORRODED (FUSELAGE) · airframe 11,575 hrs · 7,830 cycles

CORROSION ON LT 280 WEB. REMOVED AND REPLACED LT 280 WEB PER CRJ 700 SRM 51-42-06 AND 51-42-13. FINISHED REMOVING REMAINING FASTENERS AND UNINSTALLED LT WEB AND WEB STRAP AT FS 280 IAW CRJ 700 SRM 51-42-06 AND 51-52-21. FABRICATED NEW LT SPLICE PLATE (P/N CC670-34251-1) IAW CRJ 700 SRM 51-24-16 AND 700 SRM 53-11-10. INSTALLED LT WEB AND ATTACH ANGLES PER CRJ 700 SRM 51-42-06 + 51-42-13. SUPPLEMENTAL-SDR CLOSED 11/17/2008.

Part: FRAME — CORRODED (BS 280) · airframe 11,575 hrs · 7,830 cycles

CORROSION ON 280 FRAME AT LBL 9. REMOVED AND REPLACED FRAME. REMOVED MINOR CORROSION ON FRAME. BEGAN REMOVAL OF 280 BEAM LT PER SB670BA-53-026.

Part: STEP — CRACKED (PAX DOOR) · airframe 9,426 hrs · 6,338 cycles

PAX DOOR LOWER STEP CRACKED.

Part: STEP — BROKEN (PAX DOOR) · airframe 9,426 hrs · 6,338 cycles

PAX DOOR LOWER STEP BROKEN.

Part: SIGN — MISSING (CABIN) · airframe 9,404 hrs · 6,322 cycles

EXIT SIGN MISSING AFT OF SVC DOOR. FLT 4425 DEL 42 MINS.

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT) · airframe 8,960 hrs · 6,000 cycles

BOTH OVERWING EMERGENCY EXIT SIDEWALL LIGHT INOP. CABIN INTERIOR LIGHTS.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 8,370 hrs · 5,596 cycles

RIGHT 2ND FROM AFT EXTERNAL EMERGENCY LIGHT INOP.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 8,213 hrs · 5,489 cycles

F/A FWD FLASHLIGHT INOP.

Part: ENGINE — VIBRATION (LEFT) · airframe 7,785 hrs · 5,199 cycles

DIVERTED TO PVD. INFLIGHT LT ENGINE N1 VIB READS 2.0. FOLLOWED QRH FOR SINGLE ENGINE OPERATION. LT ENGINE N1 VIB REMAIN IN AMBER UNTIL ENGINE SHUTDOWN. EMERGENCY DECLARED. EN ROUTE TO ATL A/C DIVERTED TO PVD DUE TO MTC. RELATED TO DEFECT 360406-3, 360407-1, 2, 3 AND 360408-1. FLT 4140 DEL 110 MINS.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 7,610 hrs · 5,079 cycles

PAX DOOR OUTER HANDLE CRACKED. [SUP 05-24-07] REMOVED CRACKED OUTER PAX DOOR HANDLE, IAW CRJ 700 AMM 52-11-03. REMOVED SERVICEABLE PAX DOOR HANDLE FLAP, P/N 601R317045-1 FROM UNSERVICEABLE OUTER PAX DOOR HANDLE, IAW CRJ 700 SRM 51-42-06. OKAY TO INSTALL HANDLE. INSTALLED SERVICEABLE PAX DOOR HANDLE, P/N 601R31763-1, IAW CRJ 700 AMM 52-11-03. PAX DOOR HANDLE FLAP REQUIRES HINGE REPLACEMENT FOR INSTALLATION. LOCATED AND COUNTERSUNK HOLES ON PAX DOOR HANDLE FLAP HINGE, P/N 601R317046-3, IAW CRJ SRM 51-40-11. INSTALLED FLAP WITH SERVICEABLE SPRING, P/N 601R317044-3, IAW CRJ SRM 51-42-06. REQUIRES OPS CHECK. OPS CHECK GOOD, IAW CRJ AMM 52-11-03.

Part: PLACARD — TORN (PAX DOOR) · airframe 7,610 hrs · 5,079 cycles

PAX DOOR -TO OPEN- PLACARD TORN. [SUP 05-22-07] REMOVED AND REPLACED WITH NEW SERVICEABLE ONE PN S7247-1 IAW CRJ 700 AMM 11-30-02 AJONES 1017 5-14-07.

Part: PLACARD — TORN (PAX DOOR) · airframe 7,610 hrs · 5,079 cycles

PAX DOOR EXIT PLACARD TORN. [SUP 05-17-07] REMOVED AND REPLACED PAX DOOR "EXIT" PLACARD WITH NEW SERVICEABLE ONE IAW CRJ AMM 11-30-02.

Part: WEB — CORRODED (BS 280) · airframe 7,610 hrs · 5,079 cycles

RIGHT LOWER FS 280 WEB HAS CORROSION. [SUP 05-22-07] RESOLVED ON W/O: 58937 TASKCARD: N/R-00073.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 7,610 hrs · 5,079 cycles

FS 280.00 FWD CENTER FLOOR SUPPORT ANGLE CORRODED. [SUP 05-25-07] REMOVED CENTER FLOOR SUPPORT ANGLE FROM FS 280. LOCATED SERVICEABLE FS 280. FWD CENTER FLOOR SUPPORT ANGLE PN CC670-33292-13S/ OK TO INSTALL SERVICEABLE ANGLE. INSTALLED SERVICEABLE FLOOR SUPPORT ANGLE IAW CRJ 700 SRM 51-42-06 AND CRJ SRM 51-42-21.

Part: WEB — CORRODED (BS 280) · airframe 7,610 hrs · 5,079 cycles

LEFT LOWER FS 280 WEB HAS CORROSION. [SUP 05-22-07] REMOVED FASTENERS ON LT FS 280 BULKHEAD SKIN LOWER TO FOM REMOVAL OF LT LOWER FS 280 WEB. REMOVED LT LOWER FS 280 WEB IAW REO 670-53-11-052. OK TO INSTALL LT WEB STARTED INSTALLING FASTENERS IN LT WEB. FINISHED INSTALLING FASTENERS IN LT WEB IAW BOMBARDIER REO 670-53-11-052. OK TO PRIME.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 7,610 hrs · 5,079 cycles

PAX DOOR AFT DRAG ANGLE CRACKED (MARKED). [SUP 05-17-07] CUTOUT DAMAGED SECTION OF PAX DOOR AFT DRAG ANGLE IAW REO 670-52-11-072. DC699 5-14-07.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 7,610 hrs · 5,079 cycles

FS 280 CROSSBEAM HAS CORROSION ON UPPER FLANGE. [SUP 05-24-07] REMOVED CROSSBEAM FROM FS 280. BEGAN LOCATING RT CROSSBEAM SPLICE PN CC670-34175-7 IAW REO670-53-11-047. LOCATED LT AND RT SECTION AND GABLE FLOORBEAM FS 280 PN CC670-34175-7, IAW BOMBARDIER REO 670-53-11-047. OK TO INSTALL LT SERVICEABLE FLOORBEAM SECTION. OK TO INSTALL RT SERVICEABLE FLOORBEAM SECTION. STARTED INSTALLING LT BS 280 CROSSBEAM IAW REO 670-53-11-047. INSTALLED ALL REQUIRED FASTENERS. LT & RT BS 280 CROSSBEAM SECTION IAW REO 670-53-11-047. OK TO PRIME, LOCATED AND DRILLED NUTPLATE HOLES FOR FLOORBOARDS IAW SRM 51-40-11. INSTALLED NUTPLATES NAS1870-3-3 PO 10001 IAW SRM 51-42-15.

Part: WARNING SYSTEM — ACTIVATED (NLG STEERING) · airframe 7,610 hrs · 5,079 cycles

STEER INOP CAUTION MSG DISPLAYED. C/W QRH. REPEAT WRITE UP. FLT 4737 CX. EMERGENCY DECLARED.

Part: WARNING SYSTEM — MALFUNCTIONED (NLG STEERING) · airframe 7,610 hrs · 5,079 cycles

NWS CAUTION AFTER TAKEOFF. RAN QRH TURNED OFF. RESET ON THE GROUND AND OPERATION NORMAL. EMERGENCY DECLARED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,392 hrs · 4,921 cycles

CABIN AFT MOST CEILING EMERGENCY LIGHT INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,392 hrs · 4,921 cycles

GALLEY AREA HAS SEVERAL INOP EMERGENCY BULBS.

Part: LIGHT — INOPERATIVE (CAPTAIN'S MAP) · airframe 7,335 hrs · 4,882 cycles

COCKPIT/FLIGHT DECK/FLIGHT COMPARTMENT AND INSTRUMENT LIGHTING SYSTEMS (EXCLUDING EFIS) - INDIVIDUAL LIGHTS, CAPT'S MAP LIGHT INOP. REMOVED AND REPLACED CAPT'S MAP LIGHT IAW AMM 33-10-01. OPS CHECK GOOD. REMOVED PLACARD.

Part: STEERING SYS — INOPERATIVE (NLG) · airframe 7,093 hrs · 4,741 cycles

FOUND NOSE WHEEL STEERING INOP MSG AFTER TAKEOFF, EMERGENCY DECLARED.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 7,051 hrs · 4,715 cycles

FWD FLIGHT ATTENDANT FLASHLIGHT INOP.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 6,980 hrs · 4,668 cycles

MSP--MEGAPHONE INOP. FLT 4215 CX.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 6,887 hrs · 4,596 cycles

FA MEGAPHONE INOP.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 6,758 hrs · 4,509 cycles

FOUND LOWER EMERGENCY EXIT SIGN AT SEAT 14CD HAS SEVERAL BULBS BURNED OUT.

Part: DOOR — UNKNOWN (SERVICE DOOR) · airframe 6,477 hrs · 4,334 cycles

FWD SERVICE DOOR DIFFICULT TO OPEN AND CLOSE.

Part: RUDDER — MALFUNCTIONED (TAIL) · airframe 5,636 hrs · 3,788 cycles

RUDDER WILL NOT CENTER AFTER FULL DEFLECTION RIGHT AND TAKES EXCESSIVE FORCE TO GET FULL DEFLECTION LEFT. AIR RETURN TO ATLANTA (EMERGENCY DECLARED).

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 5,090 hrs · 3,459 cycles

CAPT`S FLASHLIGHT INOP.

Part: LAMP — BURNED OUT (CABIN)

DURING A HANGAR INSPECTION, THE EMERGENCY CEILING LIGHT, SECOND FROM THE FRONT, WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY CEILING LIGHT, SECOND FROM THE FRONT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: FLASHLIGHT — DEFECTIVE (COCKPIT)

DURING A GROUND INSPECTION IN ATL, THE FIRST OFFICERS FLASHLIGHT ON/OFF SWITCH KEPT MOVING INTO THE ON POSITION. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS FLASHLIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

DURING A GROUND INSPECTION, THE 2 AFT EMERGENCY CEILING LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMPS IN THE 2 AFT EMERGENCY CEILING LIGHTS. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K)