N730EV

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 44,477 hrs · 32,530 cycles

ANTI ICE DUCT WARNING MESSAGE MOMENTARILY THEN ANTI ICE CAUTION ASSOCIATED WITH L/R WING A/I CCAUTION MESSAGES. PERFORMED EMER CHECKLIST AND ANTI ICE DUCT MESSAGES DISAPPEARED. (FLIGHT 4903 - FILED CLOSED)INTERROGATED MDC FOUND NO CURRENT FAULTS POSTED AT THIS TIME. PERFORMED BITE TEST OF AILC IN REF TO AMM 30-12-12, CHECKS GOOD AT THIS TIME. PERFORMED LEAK TEST OF WING ANTI-ICE DUCTS IN REF TO AMM 30-11-00, CHECKS GOOD AT THIS TIME. NO FURTHER DEFECTS NOTED, A/C OK FOR CONTINUED SERVICE.

Part: STOP FITTING — CRACKED (ZONE 800) · airframe 44,355 hrs · 32,431 cycles

UPON TROUBLESHOOTING HARD TO CLOSE PAX DOOR FOUND FORWARD STOP BRACKET CRACKED. (FILED CLOSED)REMOVED AND REPLACED PAX DOOR FORWARD STOP BRACKET WITH REFERENCE TO SRM 51-42-21. COMPLIED WITH TASK CARD 51-900-1002-SKY. COMPLETED M-337. REFERENCE CHILD CAMP FOR ADJUSTMENT / TEST.

Part: MOUNT — UNKNOWN · airframe 42,615 hrs · 31,065 cycles

COMPLY WITH SCHEDULED MAINTENANCE CODE: ENGINE FORWARD FITTING MOUNT, YOKE AND LINK - PART IS DUE SPECIAL DETAILED INSPECTION. REMOVE AND REPLACE WITH SERVICEABLE PART IAW AMM. SEND REMOVED PART TO VENDOR FOR INSPECTION (MRB 71-21-101, REF TASK CARD(S) 71-410-600, 71-410-601, 71-410-602, 71-420-600, 71-420-601, 71-420-602), PART NUMBER: BA670-37071-1 - LINK ASSY, W/BUSHINGS INST ENG, SERIAL NUMBER: N730EV-RH, POSITION: RIGHT (FILED CLOSED)REMOVED AND REPLACED ENGINE FORWARD FITTING MOUNT YOKE LINK ON RH ENGINE IN REFERENCE TO AMM 71-21-01

Part: SKIN — DENTED (ZONE 100) · airframe 42,422 hrs · 30,899 cycles

TRANSFER FROM EAML 1414568 : DENT ON LOWER L/H SIDE OF NOSE FUSELAGE BETWEEN FS210.92 AND FS220.00 AND STGR 23L AND STGR 24L, DENT IS 0.115 INCHES DEEP BY 1.50 INCHES WIDE AND 1.75 INCHES LONG. INSPECTED DENT FOUND TO BE OUT OF LIMITS PER SRM 53-11-01 AND 53-00-01 (FILED CLOSED) REPAIRED DENT ON LOWER L/H SIDE OF NOSE FUSELAGE BETWEEN FS210.92 AND FS220.00 AND STGR 23L AND STGR 24L, IN REF. TO REO 670-53-11-2008, REV.--, DATED 2024-09-03. COMPLETED TASK CARD 51-900-1002-SKY AND M-337.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 41,874 hrs · 30,472 cycles

WINDSHIELD CRACKED. (FLIGHT 4955 FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS.

Part: WINDSHIELD — CRACKED (COKCPIT) · airframe 41,874 hrs · 30,472 cycles

WINDSHIELD CRACKED. (FLIGHT 4955 FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 28207743 WITH THE FOLLOWING CORRECTIVE ACTION: "REMOVED AND REPLACED RH WINDSHIELD PER CRJ 700 AMM 56-11-01 AND COMPLIED WITH TASK CARD 56-220-1000-SKY. SEE ML 28207742 FOR OPERATIONAL TEST OF THE WINDSHIELD AND SIDE WINDOW HEAT. SEE CP 28211616 FOR LEAK CHECK OF RH WINDSHIELD"

Part: STRINGER — CORRODED (BS 863 S20R) · airframe 41,874 hrs · 30,472 cycles

WHILE APPLYING CIC, CORROSION WAS DISCOVERED ON STRINGER 20R AFT OF FS863.00 (C-CHECK RO 5/6/2024) CORROSION FOUND TO BE OUT OF LIMITS ON STGR 20R AT APPROX FS863 - FS879. PERFORMED SPLICE REPAIR REF REO 670-53-51-280 REV -- 2024-04-15, CRJ-700 SRM 51-42-06-001-001-A01, CRJ-700 SRM 51-41-02-001-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY. ALL CHECKS GOOD.PRESSURE LEAK CHECK GOOD

Part: ATTACH FITTING — CRACKED (RT SLAT TRACK) · airframe 41,874 hrs · 30,472 cycles

RH SLAT TRACK 1-3, TRACK CANNISTER ATTACH FITTING CRACKED INSIDE FUEL PANEL 651AB (MARKED) (C-CHECK RO 5/6/2024) COMPLIED WITH REO 670-57-42-577 REV-- DATED: 2016-12-02 AND REPAIRED RH SLAT TRACK 1-3 TRACK CANNISTER ATTACH FITTING. SEE CONTINUATION FOR DETAILS

Part: FRAME — CORRODED (BS 265 S27L) · airframe 41,874 hrs · 30,472 cycles

FRAME AT FS265 STGR27 HAS AREAS CORROSION (C-CHECK RO 5/6/2024) PERFORMED FRAME SPLICE REPAIR AT F.S 265 BETWEEN 26L TO 26R REF. REO 670-53-11-1937 REV. -- DATED 2024-04-29 ALL STEPS COMPLIED WITH.. COMPLIED WITH TAK CARD 51-900-1002-SKY. PRESSURE CHECKS GOOD.

Part: DIAPHRAGM — CORRODED (BS 581-597) · airframe 41,874 hrs · 30,472 cycles

BACKUP DIAPHRAGM HAS CORROSION ON UPPER FLANGE BENEATH NUTPLATE @ APPROX FS581.00 - FS597.00 BETWEEN STGR22L & STGR23L (C-CHECK RO 5/6/2024) REMOVED CORROSION ON BACKUP DIAPHRAGM ON UPPER FLANGE @ FS581.00 - FS597.00 BETWEEN STGR22L & STGR23L WITH NO NOTED MATERIAL LOSS PER CRJ700 SRM 51-21-06-001-001-A01. INSTALLED NEW BACKUP DIAPHRAGM P/N SH670-33084-1 @ FS581.00 - FS597.00 & STGR23L PER REO 670-53-31-867, REV --, 2024-04-16 AND CRJ700 SRMS 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 AND COMPLIED WITH TASK CARD 51-900-1002-SKY.PRESSURE LEAK CHECK GOOD

Part: PLATE — CORRODED (FWD CARGO) · airframe 41,874 hrs · 30,472 cycles

FWD CARGO HOLD DOWN PLATE AFT OF CARGO DOOR CORRODED AT FS 581 MARKED (C-CHECK RO 5/6/2024) REPLACED FWD CARGO HOLD DOWN PLATE (BRACKET ) WITH NEW PN SH670-33390-2 AT FS 581 BETWEEN STR 22L -23L REF CRJ 700 SRM 51-42-21-001-001-A01 AND DWG SH670-33600 REV AD.COMPLIED WITH 51-900-1002-SKY

Part: FRAME — CORRODED (BS 250 S26-27L) · airframe 41,874 hrs · 30,472 cycles

FRAME AT FS250 STGR27-26L HAS AREAS CORROSION (FWD AND AFT) MARKED (C-CHECK RO 5/6/2024) REPAIRED FRAME AT FS250, STGR 25L - 25R REF REO 670-53-11-1936 REV -- 2024-04-10. COMPLIED WITH TASK CARD 51-900-1002-SKY. ALL CHECKS GOOD

Part: DOOR SILL — CORRODED (SERVICE DOOR) · airframe 41,874 hrs · 30,472 cycles

SERVICE DOOR SILL HAS AREAS OF CORROSION (C-CHECK RO 5/6/2024) PERFORMED REPAIR OF SERVICE DOOR SILL BY COMPLYING WITH ALL STEPS OF REO 670-53-21-2380 REV -- DATED 2024-03-30. SEE CONTINUATION FOR WORK PERFORMED.COMPLIED WITH 51-900-1002-SKY

Part: STRIKER — DENTED (PAX DOOR) · airframe 41,874 hrs · 30,472 cycles

FWD LOWER PAX DOOR SEAL STRIKER ON FUSELAGE HAS A DENT. (C-CHECK RO 5/6/2024) COMPLIED WITH REO 670-53-22-001 REV -J DATED 2016-11-10 FOR REPAIR (TYPE 1) TO FWD LOWER PAX DOOR SEAL STRIKER. COMPLIED WITH ALL STEPS OF REO FOR REPAIR (TYPE 1). LEAK TEST GOOD WITH NO LEAKS NOTED. SEE CONTINUE CARD FOR WORK PERFORMED. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY AND MAJOR REPAIR FORM M-337.

Part: SKIN — CHAFED (LT AILERON) · airframe 41,874 hrs · 30,472 cycles

LH AILERON LOWER LEADING EDGE CHAFED (C-CHECK RO 5/6/2024) REMOVED AND REPLACED LH AILERON LOWER LEADING EDGE SKIN (PN CC670-13054-1) PER CRJ700 SRMS 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 AND COMPLIED WITH TASK CARD 51-900-1002-SKY.

Part: SKIN — CHAFED (BS 985 S26L&R) · airframe 41,874 hrs · 30,472 cycles

PREVIOUS REPAIR PLATE HAS CHAFING FS985.00 STGR26L - STGR26R. (MARKED) (C-CHECK RO 5/6/2024) REMOVED EXISTING REPAIR PER REO 670-53-00-290 REV -F DATE 2019/04/26 AND INSTALLED NEW REPAIR PER REO 670-53-00-290 REV -F DATE 2019/04/26 SOLUTION #1, PRESSURE LEAK CHECK GOOD,COMPLIED WITH 51-900-1002-SKY

Part: SKIN — CHAFED (RT AILERON) · airframe 41,874 hrs · 30,472 cycles

RH AILERON LOWER LEADING EDGE CHAFED. (C-CHECK RO 5/6/2024) INSTALLED NEW R/H AILERON SKIN LOWER OTBD LEADING EDGE PANEL P/N: CC670-13054-2 REF DRW CC670-13000 REV -D, CRJ 700 SRM 51-42-21-001-001-A01 AND CRJ 700 SRM 51-42-06-001-001-A01. AND INSTALLED NEW R/H AILERON SKIN LOWER INBD LEADING EDGE PANEL P/N: CC670-13053-2 REF DRW CC670-13000 REV -D, CRJ 700 SRM 51-42-21-001-001-A01 AND CRJ 700 SRM 51-42-06-001-001-A01. SEE CONTINUATION FOR WORK PERFORMED. COMPLIED WITH 57-900-1002-SKY.

Part: SKIN — CHAFED (LT NACELLE) · airframe 41,874 hrs · 30,472 cycles

LEFT ENGINE UPPER FAN COWL INNER SKIN IS CHAFED AT THE OUTBOARD SIDE. (C-CHECK RO 5/6/2024) REMOVED DAMAGED OUTBOARD GUSSET P/N CN622-0333-203 FROM L/H UPPER FAN COWL, REF. CRJ700 SRM 51-42-13-001-001-A01 AND INSTALLED NEW OUTBOARD GUSSET P/N CN622-0333-203 ON L/H UPPER FAN COWL, REF. CRJ700 SRM 51-42-13-001-001-A01 & FAN COWL DOOR ASSEMBLY UPPER L/H / LOWER R/H DWG. CN622-0101, REV. J. FUNCTIONAL TEST GOOD COMPLIED WITH SKYCARD 51-900-1002-SKY

Part: RETAINER — DENTED (AFT PAX DOOR) · airframe 41,874 hrs · 30,472 cycles

AFT UPPER PAX DOOR SEAL RETAINER ON FUSELAGE HAS A DENT (C-CHECK RO 5/6/2024) COMPLIED WITH REO 670-53-22-001 REV -J DATED 2016-11-10 REPAIR (TYPE 1) FOR AFT UPPER PAX DOOR SEAL STRIKER REPAIR. COMPLIED WITH ALL STEPS OF REO REPAIR (TYPE 1). LEAK TEST GOOD WITH NO LEAKS NOTED. SEE CONTINUE CARD FOR WORK PERFORMED.COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY AND MAJOR REPAIR FORM M-337.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 41,874 hrs · 30,472 cycles

PAX DOOR INTERCOSTAL DD6 FS338.00 - FS347.25 IS CORRODED (C-CHECK RO 5/6/2024) REMOVED AND DISCARDED EXISTING PAX DOOR INTERCOSTAL DD6 FS338.00 - FS347.25. RE F: CRJ-700 SRM 51-42-06-001-001-A01 AND INSTALLED NEW PAX DOOR INTERCOSTAL DD6 FS338.00 - FS347.25. REF: CRJ-700 SRM 51-42-06-001-001-A01 AND DRAWING 601R31702 REV N, COMLIED WITH 51-900-1002-SKY, PRESSURE LEAK GOOD

Part: INTERCOSTAL — CORRODED (BS 320-327) · airframe 41,874 hrs · 30,472 cycles

PAX DOOR INTERCOSTAL DD7 FS320.00 - FS327.763 IS CORRODED (C-CHECK RO 5/6/2024) REMOVED AND DISCARDED EXISTING PAX DOOR INTERCOSTAL DD7 FS320.00 - FS327.763. RE F: CRJ-700 SRM 51-42-06-001-001-A01 AND INSTALLED NEW PAX DOOR INTERCOSTAL DD7 FS320.00 - FS327.763. REF: CRJ-700 SRM 51-42-06-001-001-A01 AND DRAWING 601R31702 REV N, PRESURE LEAK GOOD , COMPLIED 51-900-1002-SKY

Part: INTERCOSTAL — CORRODED (BS 320-338) · airframe 41,874 hrs · 30,472 cycles

PAX DOOR INTERCOSTAL DD4 FS320.00 - FS338.00 IS CORRODED (C-CHECK RO 5/6/2024) REMOVED AND DISCARDED EXISTING PAX DOOR INTERCOSTAL DD4 FS320.00 - FS338.00. REF: CRJ-700 SRM 51-42-06-001-001-A01 AND CRJ-700 SRM 51-42-21-001-001-A01 AND INSTALLED NEW PAX DOOR INTERCOSTAL DD4 FS320.00 - FS338.00. REF: CRJ-700 SRM 51-42-06-001-001-A01, CRJ-700 SRM 51-42-21-001-001-A01, AND DRAWING 601R31702 REV N, COMPLIED WITH 51-900-1002-SKY,PRESSURE LEAK GOOD

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 41,874 hrs · 30,472 cycles

PAX DOOR INTERCOSTAL DD1A FS338.00 - FS347.25 IS CORRODED (C-CHECK RO 5/6/2024) REMOVED AND DISCARDED EXISTING PAX DOOR INTERCOSTAL DD1A FS338.00 - FS347.25. RE F: CRJ-700 SRM 51-42-06-001-001-A01 AND INSTALLED NEW PAX DOOR INTERCOSTAL DD1A FS338.00 - FS347.25. REF: CRJ-700 SRM 51-42-06-001-001-A01 AND DRAWING 601R31702 REV N,PRESSURE LEAK WAS GOOD, COMPLIED WITH 51-900-1002-SKY

Part: SKIN — CRACKED (THRUST REVERSER) · airframe 41,874 hrs · 30,472 cycles

L/H UPPER TRANSCOWL PERFORATED SKIN UNDER Z STIFFENER IS CRACKED (C-CHECK RO 5/6/2024) L/H ENGINE UPPER TRANSCOWL INNER SKIN HAS BEEN REPAIRED REF REO# 670-54-21-1626, REV --, DATED 3/29/24. SEE CONTINUATION SHEET FOR DETAILS. COMPLIED FULLY W/SKYCARD 51-900-1002-SKY.

Part: SKIN — CORRODED (PAX DOOR) · airframe 41,874 hrs · 30,472 cycles

PAX DOOR OUTER SKIN IS CORRODED BETWEEN TOP OF DOOR CENTER AND DD1 NEAR STANDOFF (C-CHECK RO 5/6/2024) REPAIRED PAX DOOR OUTER SKIN BETWEEN FS320.163 - FS338.963 AND UPPER DOOR BEAM - DOOR DATUM 1 PER REO 670-51-11-1378 REV -- DATED: 2024-03-25. COMPLIED WITH ALL STEPS OF REO. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY AND MAJOR REPAIR FORM M-337. LEAK CHECK GOOD WITH NO LEAKS NOTED.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 41,874 hrs · 30,472 cycles

CRACK FOUND AT LBL12 COCKPIT FLOOR BEAM FS280 (C-CHECK RO 5/6/2024) PERFORMED CENTER COCKPIT FLOOR BEAM AT BL12.00 TYPE 4 REPAIR IAW CRJ 700 SRM 53-11-43-201-003-A01, SEE CONTINUATION CARD FOR FURTHER DETAILS.COMPLIED WITH 51-900-1002-SKY

Part: FLOORBEAM — CRACKED (BS 280) · airframe 41,874 hrs · 30,472 cycles

CRACK FOUND AT RBL12 COCKPIT FLOOR BEAM FS280 (C-CHECK RO 5/6/2024) PERFORMED REPAIR TO THE RH CENTER COCKPIT FLOOR BEAM AT RBL12.00 REF CRJ-700 SRM 53-11-43-201-003-A01 TYPE IV. COMPLIED WITH TASK CARD 51-900-1002-SKY

Part: HINGE — CHAFED (PAX DOOR) · airframe 41,874 hrs · 30,472 cycles

PAX DOOR HINGE (DOOR SIDE) HAS CHAFE DAMAGE TO LUGS 1, 3, 5, 11, 16, 18, 19, 25, 26, AND 27 (C-CHECK RO 5/6/2024) BLENDED OUT CHAFFNG AND RESTORED FINISH TO REWORKED AREA ON PAX DOOR HINGE (DOOR SIDE) LUGS 1, 3, 5, 11, 16, 18, 19, 25, 26, AND 27.REF: CRJ-700 SRM 52-11-01-201-007-A01 TYPE I. NO WEIGHT CHANGE

Part: HINGE — GOUGED (PAX DOOR) · airframe 41,874 hrs · 30,472 cycles

FOUND GOUGE ON PAX DOOR HINGE (FUSELAGE SIDE) LAND #27 (C-CHECK RO 5/6/2024) REPLACED PAX. DOOR HINGE WITH A NEW ONE (FUSELAGE SIDE) . REF: CRJ-700 SRM 53-21-13-201-007-A01 REV 38 DATED JULY 25/2020 AND DWG SH670-31810 REV AE. LEAK CHECK GOOD WITH NO LEAKS NOTED. SEE CONTINUE CARD FOR WORK PERFORMED. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY AND MAJOR REPAIR FORM M-337.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 41,874 hrs · 30,472 cycles

PAX DOOR INTERCOSTAL DD1A FS323.00 - FS336.00 IS CORRODED (C-CHECK RO 5/6/2024) REMOVED AND DISCARDED EXISTING PAX DOOR INTERCOSTAL DD1A FS323.00 - FS336.00. REF: CRJ-700 SRM 51-42-06-001-001-A01 AND CRJ-700 SRM 51-42-21-001-001-A01 AND INSTALLED NEW PAX DOOR INTERCOSTAL DD1A FS323.00 - FS336.00. REF: CRJ-700 SRM 51-42-06-001-001-A01, CRJ-700 SRM 51-42-21-001-001-A01, AND DRAWING 601R31702 REV N, PRESSURE LEAK CHECK GOOD, COMPLIED WITH 51-900-1002-SKY

Part: SKIN — DAMAGED (LT WING TE FLAP) · airframe 41,874 hrs · 30,472 cycles

LEFT INBOARD FLAP LOWER SKIN HAS A CREASE FLS 41 AND 5.5 INCHES FROM THE TRAILING EDGE. (MARKED) (C-CHECK RO 5/6/2024) L/H I/B FLAP LOWER SKIN HAS BEEN REPAIRED REF CRJ SRM 57-52-01-201-002-A01, TYPE 4, PERMANENT NON FLUSH REPAIR.. COMPLIED FULLY W/SKYCARD 51-900-1002-SKY. SEE CONTINUATION SHEET FOR DETAILS.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 41,874 hrs · 30,472 cycles

R/H VERTICAL STAB TO FUSELAGE ATTACHMENT DRAG ANGLE AFT POSSIBLE CRACK. (MARKED) (C-CHECK RO 5/6/2024) COMPLIED WITH ALL STEPS OF REPAIR TO RH VERTICAL TO FUSELAGE AFT DRAG ANGLE AND INSTALLED ALL FABRICATED REPAIR PARTS -6 R/H AFT ANGLE DOUBLER AND -8 R/H AFT ANGLE FILLER USING 2024-T3 .090" ALCLAD SHEET, PO #T-62096, REF CRJ 700 SRM 55-31-00-201-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 41,874 hrs · 30,472 cycles

RIGHT INBOARD FLAP, FLAP VANE. LEADING EDGE AT FLS72 IS CHAFED. (MARKED) (C-CHECK RO 5/6/2024) REMOVED AND INSTALLED 1EA NEW R/H INBD FLAP VANE CAP AT FLS72 PER CRJ700SRM 51-42-13-001-001-A01 AND CRJ700SRM 51-23-00-001-001-A01 AND DWG CC670-14010 REV -F. SEE CONTINUATION FOR DETAILS.

Part: NONE — NONE · airframe 41,367 hrs · 30,030 cycles

DURING DECENT PASSING THROUGH 24000 L WSHLD HEAT CAUTION MESSAGE APPEARED. WHILE FOLLOWING QRH ARCING ON WINDSHIELD WAS NOTED. PASSING 20000 WINDSHIELD PLY SHATTERED. (FLIGHT #3027 FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 25727129 WITH THE FOLLOWING CORRECTIVE ACTION: "REMOVED AND REPLACED CAPT SIDE WINDSHIELD REF TO CRJ 700 AMM 56-11-01 ,"

Part: SELECTOR VALVE — INOPERATIVE (MLG) · airframe 37,389 hrs · 27,010 cycles

GEAR DISAGREE WARNING MESSAGE WHILE ON FINAL EXTENDING THE LANDING GEAR. ON 6 MILE FINAL MOVED THE LANDING GEAR LEVER TO DOWN AND THE GEAR DID NOT MOVE. COMPLIED WITH THE QRH FOR A GEAR DOWN DISAGREE. CYCLED THE GEAR SEVERAL TIMES ACCORDING TO THE QRH. COMPLETED THE QRH PROCEDURE WITH AN EMERGENCY EXTENSION OF THE LANDING GEAR. FLIGHT 3014. UPON TROUBLESHOOTING, IN REF TO AMM FIM, FOUND B1 CODE 005968 AND B1 007450, GEAR DISAGREE WARNING MESSAGE, JACKED PLANE AND SWUNG LG IN REF TO AMM, VERIFIED NO GEAR MOVEMENT WITH GEAR HANDLE SELECTED IN DOWN POSITION, FOUND MLG SELECTOR VALVE ASSEMBLY TO BE INOP, REMOVED AND REPLACED MLG SELECTOR VALVE ASSEMBLY IN REF TO AMM, SWUNG LG MULTIPLE TIMES AFTER REPLACEMENT, OPS CHECK GOOD AT THIS TIME

Part: ANGLE — CORRODED (PAX DOOR SILL) · airframe 36,311 hrs · 26,163 cycles

PAX DOOR LOWER SILL ANGLE MID CAP ANGLE HAD CORROSION. REMOVED AND REPLACED THE ANGLE IAW DWG.

Part: ANGLE — CORRODED (PAX DOOR SILL) · airframe 36,311 hrs · 26,163 cycles

PAX DOOR LOWER SILL ANGLE FWD CAP ANGLE HAD CORROSION. REMOVED AND REPLACED THE ANGLE IAW DWG SH670-31810, REV AE, AND SRM.

Part: INTERCOSTAL — CORRODED (BS 310-333) · airframe 36,311 hrs · 26,163 cycles

INTERCOSTAL, BS 310 TO 333, STRINGER 21L HAD CORROSION. BLENDED AND FOUND TO BE OUT OF LIMITS. REMOVED & INSTALLED A NEW INTERCOSTAL IAW DWG SH670-31810, REV Y, AND SRMS.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 36,311 hrs · 26,163 cycles

PAX DOOR FWD INTERCOSTAL WAS CORRODED. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM AND DWG.

Part: CLEAT — CORRODED (PAX DOOR) · airframe 36,311 hrs · 26,163 cycles

PAX DOOR CENTER INTERCOSTAL, FWD CLEAT HAD CORROSION. INSTALLED A NEW CLEAT IAW SRM.

Part: CLEAT — CORRODED (PAX DOOR) · airframe 36,311 hrs · 26,163 cycles

PAX DOOR AFT CLEAT ON INTERCOSTAL WAS CORRODED. REMOVED AND INSTALLED THE CLEAT ON INTERCOSTAL IAW SRM.

Part: CLEAT — CORRODED (PAX DOOR) · airframe 36,311 hrs · 26,163 cycles

PAX DOOR FWD INTERCOSTAL AFT CLEAT HAD CORROSION. INSTALLED A NEW CLEAT IAW SRM.

Part: CLEAT — CORRODED (PAX DOOR) · airframe 36,311 hrs · 26,163 cycles

PAX DOOR FWD INTERCOSTAL, FWD CLEAT HAD CORROSION. INSTALLED A NEW CLEAT IAW SRM.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 36,311 hrs · 26,163 cycles

PAX DOOR AFT INTERCOSTAL WAS CORROED. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM.

Part: FORMER — CORRODED (PAX DOOR) · airframe 36,311 hrs · 26,163 cycles

PAX DOOR FWD FORMER WAS CORRODED. INSTALLED A NEW FORMER IAW SRM.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 36,311 hrs · 26,163 cycles

PAX DOOR INTERCOSTAL WAS CORRODED. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM AND DWG.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 36,311 hrs · 26,163 cycles

PAX DOOR INTERCOSTAL WAS CORRODED. INSTALLED A NEW INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 36,311 hrs · 26,163 cycles

PAX DOOR INTERCOSTAL WAS CORRODED. INSTALLED A NEW INTERCOSTAL AND CLEATS IAW SRM.

Part: ANGLE — CORRODED (BS 761-785) · airframe 36,311 hrs · 26,163 cycles

RIGHT SILL ANGLE AT APPROX BS 761.85 TO 785.15 WAS CORRODED. REPAIRED THE ANGLE IAW REO. ALL STEPS OF REO COMPLIED WITH IN THIER ENTIRITY. LEAK CHECKED GOOD.

Part: ANGLE — CORRODED (BS 761-785) · airframe 36,311 hrs · 26,163 cycles

LEFT SILL ANGLE AT BS 761.85 TO 785.15 WAS CORRODED. COMPLIED WITH REO, BLENDED THE CORROSION.

Part: STRINGER — CORRODED (BS 333-364) · airframe 36,311 hrs · 26,163 cycles

MAIN AVIONICS BAY STRINGER 26L, BS 333 TO 364 HAD SEVERAL SPOTS OF CORROSION. REPAIRED THE SPOTS OF CORROSION IAW DWG SH670-31350, REV A, AND SRM. LEAK CHECKED GOOD.

Part: STRINGER — CORRODED (BS 280-333) · airframe 36,311 hrs · 26,163 cycles

MAIN AVIONICS BAY STRINGER 26L, BS 280 TO 333 HAD SEVERAL SPOTS OF CORROSION. REMOVED THE CORROSION IAW SRM, FOUND OUT OF LIMITS IAW SRM. REPLACED THE STRINGER IAW SRM & DWG SH670-31630, REV K.

Part: SEAT TRACK — CORRODED (BS 349-485) · airframe 36,311 hrs · 26,163 cycles

SEAT TRACK AT RBL 9, BS 349 - 485 HAD CORROSION. REPLACED THE SEAT TRACK IAW AMM.

Part: SEAT TRACK — CORRODED (BS 797-813) · airframe 36,311 hrs · 26,163 cycles

BS 797 TO 813 SIDE SEAT TRACK WAS CORRODED. REMOVED THE CORROSION IAW SRM. THE SEAT TRACK WAS WITHIN LIMITS IAW SRM.

Part: FRAME — CORRODED (BS 549) · airframe 36,311 hrs · 26,163 cycles

FRAME AT FS549.00 AT STGR 18LH HAS CORROSION. (C-CHECK) RO 12/24/2019 REPAIRED CORROSION ON FRAME FS549.00 AT STGR18LH, REF BOMBARDIER DWG. ALL STEPS OF REO COMPLIED WITH IN THEIR ENTIRITY. LEAK CHECK PERFORMED AND LEAK CHECK GOOD. SEE CONTINUATION CARD FOR FURTHER DETAILS.

Part: SEAT TRACK — CORRODED (BS 693-830) · airframe 36,311 hrs · 26,163 cycles

SEAT TRACK AT LBL9, BS 693 TO 830 CORRODED. REMOVED AND INSTALLED A NEW SEAT TRACK IAW AMM.

Part: INTERCOSTAL — CORRODED (BS 310) · airframe 36,311 hrs · 26,163 cycles

BS 310 BELOW FLOOR SUPPORT, STRINGER 20R INTERCOSTAL HAS CORROSION ON FWD PORTION. REMOVED AND REPLACED THE INTERCOSTAL IAW DWG SH670-31950, REV Y, AND SRM.

Part: ANGLE — CORRODED (BS 310-349) · airframe 36,311 hrs · 26,163 cycles

PAX DOOR LOWER FLOOR SILL ANGLE HAS CORROSION IN BETWEEN BS 310 TO 349.0 LT SIDE. REMOVED AND REPLACED THE LOWER SILL ANGLE IAW DWG AND SRM. ALL CHECKED GOOD.

Part: FRAME — CORRODED (BS 349) · airframe 36,311 hrs · 26,163 cycles

CORROSION FOUND ON THE BS 349 FRAME NEAR STRINGERS 26L AND 26R. REPAIRED THE FRAME IAW DWG. PERFORMED LEAK CHECK AND LEAK CHECK GOOD.

Part: SEAT TRACK — CORRODED (BS 736-953) · airframe 36,311 hrs · 26,163 cycles

LEFT SIDE FUSELAGE, SIDE SEAT TRACK HAD AREAS OF CORROSION FROM BS 736 - 953. REMOVED CORROSION FROM THE SEAT TRACK IAW SRM, FOUND TO BE WITHIN LIMITS IAW SRM,

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 36,311 hrs · 26,163 cycles

CORROSION FOUND ON INTERCOSTAL STRINGER 27L, BS 349 AND 364. REMOVED THE CORROSION IAW SRM, FOUND TO BE OUT OF LIMITS IAW SRM. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM, & DWG SH670-32050, REV. J.

Part: MOUNT — CORRODED (GALLEY) · airframe 36,311 hrs · 26,163 cycles

TWO GALLEY NR 2 FLOOR MOUNTS ATTACHED TO SEAT TRACK CORRODED. REPLACED THE FLOOR MOUNTS ON SEAT TRACK IAW SRM.

Part: STRINGER SPLICE — CORRODED (BS 333) · airframe 36,311 hrs · 26,163 cycles

STRINGER SPLICE 25R, BS 333 WAS CORRODED. REPAIRED THE STRINGER SPLICE IAW DWG SH670-32420, REV E, AND SRM. LEAK CHECK PERFORMED AND CHECKED GOOD.

Part: SEAT TRACK — CORRODED (BS 485-963) · airframe 36,311 hrs · 26,163 cycles

PASSENGER CABIN RT INBD FLOOR SEAT TRACK RBL 9 BS 485 TO 693 HAD AREAS OF CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM. THE SEAT TRACK WAS REPLACED.

Part: FRAME — CORRODED (BS 333) · airframe 36,311 hrs · 26,163 cycles

CORROSION ON FRAME BS 333 BETWEEN STRINGERS 26L AND 26R. REMOVED CORROSION IAW SRM, FOUND OUT OF LIMITS IAW SRM, REPLACED THE FRAME IAW SRM. LEAK CHECKED GOOD.

Part: SEAT TRACK — CORRODED (BS 485-693) · airframe 36,311 hrs · 26,163 cycles

PASSENGER CABIN LT INBD FLOOR SEAT TRACK AT LBL 9 APPROXIMATELY BS 485 TO 693 HAD AREAS OF CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-31-49-101-001-A01. THE SEAT TRACK WAS REPLACED.

Part: SUPPORT — CRACKED (WNG-BDY FAIRING) · airframe 36,311 hrs · 26,163 cycles

RIGHT FUSELAGE WING TO FUSELAGE AFT FAIRING SUPPORT AT BS 909, RBL 17.63 WAS CRACKED. COMPLIED WITH ALL THE STEPS OF REO STEPS 1 TO 13. INSTALLED ALL REPAIR PARTS AND WET INSTALLED ALL REPAIR FASTENERS ON RT FUSELAGE WING TO FUSELAGE AFT FAIRING SUPPORT.

Part: TEE FITTING — CORRODED (WNG-BDY FAIRING) · airframe 36,311 hrs · 26,163 cycles

UNDER FWD WING TO FUSELAGE FAIRING CENTER TEE HAS CORROSION AROUND (4) EA. FASTENER LOCATIONS PN SH670-39063-1 MACHINED ATTACHMENT. REMOVED OUT OF LIMITS TEE AND INSTALLED NEW UNDER FWD WING FUSELAGE FAIRING CENTER TEE IAW SRM.

Part: SUPPORT — CORRODED (WNG-BDY FAIRING) · airframe 36,311 hrs · 26,163 cycles

AFT FUSELAGE SUPPORT STRUCTURE FOR BODY FAIRINGS 195DL/196DR, SPLICE ANGLE CORRODED LOCATED AT BS 939. AFT FUSELAGE SUPPORT STRUCTURE FOR BODY FAIRINGS 195DL/196DR, SPLICE ANGLE REMOVED AND REPLACED WITH NEW ANGLE REF SRM.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 36,311 hrs · 26,163 cycles

VERTICAL STAB SUSPECT CRACK 2EA AT THE LH SIDE DRAG ANGLE AFT, JUST AFTER THE EXISTING REPAIR. PERFORMED A PERMANENT REPAIR ON THE LT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE IAW SRM.

Part: FRAME — CORRODED (BS 379) · airframe 34,279 hrs · 24,503 cycles

CORROSION FOUND ON FRAME AT FS379, STGR 21R. (C-CHECK) RO: 11/1/2018. REMOVED CORROSION FROM FRAME AT FS379, STGR 21R.

Part: STRINGER SPLICE — CORRODED (BS 333) · airframe 34,279 hrs · 24,503 cycles

STRINGER SPLICE FOUND CORRODED AT FS333. (C-CHECK) RO: 11/1/2018. REMOVED AND INSTALLED NEW SERVICEABLE STRINGER SPLICE AT FS333.00 REF SRM 51-42-06-001-001-A01.

Part: STRINGER — CORRODED (BS 349-364) · airframe 34,279 hrs · 24,503 cycles

STRINGER 21R FOUND CORRODED BETWEEN FS349 AND FS364. (C-CHECK) RO: 11/1/2018. REMOVED & INSTALLED NEW STRINGER SECTOR AT STGR 21R, FS 333 - FS 379 REF SRM 51-42-06-001-001-A01. ALL CHECKS GOOD.

Part: STRINGER — CORRODED (BS 333-364) · airframe 34,279 hrs · 24,503 cycles

CORROSION FOUND ON STR 26R, FS333 TO FS364. (C-CHECK) RO: 11/1/2018. REPLACED STRINGER AT STR26, FS333 - FS364 REF SRM 51-42-06-001-001-A01. LEAK CHECK GOOD.

Part: STRINGER SPLICE — CORRODED (BS 333) · airframe 34,279 hrs · 24,503 cycles

CORROSION FOUND ON STRINGER SPLICE AT FS333, STGR 26R. (C-CHECK) RO: 11/1/2018. REPLACED STRINGER SPLICE AT FS333, STGR 26R REF SRM 51-42-06-001-001-A01. LEAK CHECK GOOD.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 34,279 hrs · 24,503 cycles

CORROSION FOUND ON TCAS ANTENNA DOUBLER IN AVIONICS BAY. (C-CHECK) RO: 11/1/2018. REMOVED AND REPLACED TCAS ANTENNA DOUBLER REF SRM 51-42-06-001-001-A01. LEAK CHECK GOOD AND OPERATIONAL TEST GOOD.

Part: PANEL — CORRODED (ZONE 100) · airframe 34,279 hrs · 24,503 cycles

STRAP LOCATED ON PANEL 196DR IS CORRODED. (C-CHECK) RO: 11/1/2018. REPLACED STRAP ON PANEL 196DR REF SRM 51-42-13-001-001-A01. COMPLIED WITH 51-900-1002-SKY (CL600-2C10) STRUCTURAL MAJOR REPAIR (**RII**).

Part: PANEL — CORRODED · airframe 34,279 hrs · 24,503 cycles

FWD UNDERWING FAIRING PANEL 193AB HAS CORROSION. (C-CHECK) RO: 11/1/2018. REMOVED AND INSTALLED (2) NEW STRAPS REF SRM 51-42-06-001-001-A01.

Part: SKIN — GOUGED (BS 977) · airframe 34,279 hrs · 24,503 cycles

GOUGE LOCATED ON LOWER FUSELAGE AT APPROX FS977 AT STR 27. (C-CHECK) RO: 11/1/2018. REPAIRED GOUGE, COMPLIED WITH REO 670-53-00-290. LEAK CHECK GOOD.

Part: SKIN — DENTED (LT NACELLE) · airframe 34,279 hrs · 24,503 cycles

DENT FOUND ON LH ENGINE LOWER TRANSCOWL 8.750" FROM LEADING EDGE. (C-CHECK) RO: 11/1/2018. REPAIRED AREA REF REO 670-54-21-1308 REV A 2018-10-02. COMPLIED WITH 51-900-1002-SKY (CL600-2C10) STRUCTURAL MAJOR REPAIR (**RII**).

Part: SKIN — CHAFED (RT AILERON) · airframe 34,279 hrs · 24,503 cycles

RH AILERON LEADING EDGE CHAFED. (C-CHECK) RO: 11/1/2018. REMOVED AND REPLACED AILERON UPPER SKIN LEADING EDGE REF SRM 51-42-06-001-001-A01.

Part: SKIN — CORRODED (BS 280-295) · airframe 34,279 hrs · 24,503 cycles

FOUND CORROSION ON INTERNAL FUSELAGE SKIN BETWEEN FS280 AND FS295. (C-CHECK) RO: 11/1/2018. REPAIRED CORROSION ON INTERNAL FUSELAGE SKIN BETWEEN FS280 AND FS295.

Part: PANEL — CHAFED (RT AILERON) · airframe 34,279 hrs · 24,503 cycles

RIGHT AILERON PANEL 699CB HAS CHAFE DAMAGE. (C-CHECK) RO: 11/1/2018. REPAIRED RH AILERON PANEL 669CB. COMPLIED WITH REO 670-57-61-296.

Part: ENGINE — DAMAGED (LEFT) · airframe 34,279 hrs · 24,503 cycles

DAMAGE FOUND ON THE LH ENGINE THAT NEEDS TO BE REPAIRED. (C-CHECK) RO: 11/1/2018. DENT REPAIRED REF REO 670-54-21-1310. COMPLIED WITH 51-900-1002-SKY (CL600-2C10) STRUCTURAL MAJOR REPAIR (**RII**)

Part: SKIN — DAMAGED (BELLY) · airframe 34,279 hrs · 24,503 cycles

FOURTEEN SMALL AREAS OF DAMAGE ON THE AIRCRAFT BELLY AFT OF THE NLG DOOR. (C-CHECK) RO: 11/1/2018. REPAIRED MULTIPLE DENTS ON AIRCRAFT BELLY JUST AFT OF THE NLG DOOR REF REO 670-53-21-1570. LEAK CHECK GOOD NO DEFECT NOTED.

Part: FAN — FAILED (RECIRCULATION) · airframe 32,938 hrs · 23,436 cycles

THE CREW REPORTED AT FL320 STARTED TO SMELL ELECTRICAL BURNING ODOR. FLIGHT ATTENDANTS SMELLED FUMES NEAR 15 A&B. AIRCRAFT DIVERTED. MAINTENANCE INSPECTED AND FOUND RECIRCULATION FAN NR 1 TRIPPING THE CIRCUIT BREAKER. OPEN

Part: FLOOR SUPPORT — CORRODED (BS 1021-1037) · airframe 31,350 hrs · 22,238 cycles

DURING C-CHECK, THE FLOOR SUPPORT AT RBL 9, BETWEEN BS 1021 & 1037 WAS FOUND CORRODED BEYOND LIMITS. REPAIRED THE FLOOR IAW EO700-53-10-00047, REV 0, SRM 53-00-41-201-001-A01, AND REO 670-53-0-029, REV A.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 31,350 hrs · 22,238 cycles

FLOORBEAM AT LBL 9 BTW FS 977-1037 CORRODED BEYOND LIMITS. REPAIRED FLOORBEAM USING SPLICE REPAIR PER EO 700-53-10-00046 REV 0 DATED 2017-03-27, SRM 53-00-41-201-001-A01 AND REO 670-53-00-029 REV A DATED 8/31/2010.

Part: FLOOR SUPPORT — CORRODED (BS 977-1037) · airframe 31,350 hrs · 22,238 cycles

DURING C-CHECK, THE FLOOR SUPPORT AT LBL 9, BETWEEN BS 977 & 1037 WAS FOUND CORRODED BEYOND LIMITS. REPAIRED THE FLOOR SUPPORT IAW EO700-53-10-00046, REV 0, SRM 53-00-41-201-001-A01, AND REO 670-53-0-029, REV A.

Part: CIRCUIT BREAKER — TRIPPED (EMERGENCY LIGHTS) · airframe 30,573 hrs · 21,680 cycles

PILOT REPORTED THE EMERGENCY LIGHTS CAME ON UNCOMMANDED DURING FLIGHT. COCKPIT SWITCH IN ARM. CABIN SWITCH IN OFF. ALL ELECTRICAL POWER INDICATIONS NORMAL. FOUND EMERGENCY LIGHT CIRCUIT BREAKER TRIPPED. RESET THE CIRCUIT BREAKER AND OPERATIONAL CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 30,088 hrs · 21,316 cycles

12 CD LOWER EXIT SIGN HAS 1 LIGHT BULB BURNED OUT. R & R 12 CD LOWER EXIT SIGN LIGHT BULB IAW AMM 33-51-05. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,088 hrs · 21,316 cycles

ROW 17, CEILING EMERGENCY LIGHT BULB BURNED. R & R ROW 17 CEILING EMERGENCY LIGHT IAW AMM 33-51-07. OPS CHECKED GOOD.

Part: CONNECTOR — DAMAGED (BLEED WARNING) · airframe 30,054 hrs · 21,292 cycles

BLEED DUCT MASTER WARNING (LT COWL) DIVERTED. REMOVED AND REPLACED ELECTRICAL CONNECTORS MT142P2 AND MT141P2 IAW ESPM 20-26-07. PERFORMED FUTHER TROUBLESHOOTING IAW VCMM 36-10-00 AND FOUND NO OTHER FAULTS AT THIS TIME OK FOR SERVICE.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 28,962 hrs · 20,410 cycles

AISLE OVERHEAD EMERGENCY LIGHT INOPERATIVE AT ROW 9. REPLACED OVERHEAD EMERGENCY LIGHT ROW 9. R & R ISLE OVERHEAD EMERGENCY FLOOD LIGHT BULB IAW AMM 33-51-09. OPS CHECK GOOD.

Part: SMOKE DETECTOR — FALSE INDICATION (AFT LAVATORY) · airframe 28,734 hrs · 20,245 cycles

SMOKE AFT LAV CAME ON IN FLIGHT A MECHANIC ON BOARD RESET THE ALARM MSG WENT AWAY. SYSTEM RESET DISCREPENCY, NO LONGER EXIST IAW MCC, NO FUTHER ACTION REQUIRED.

Part: SEAT TRACK — CORRODED (BS 485-649) · airframe 28,709 hrs · 20,224 cycles

FLOOR SEAT RAIL HAS CORROSION FROM FS 649-FA 485, RBL 9. EVALUATED SEAT RAIL FS 349-485 RBL 9 FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. REMOVED SEAT RAIL AT FS 349-485, RBL9 IAW AMM 53-00-49-000-801, A03. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343 REV M AS WRITTEN. INSTALLED NEW SEAT RAIL AT FS 349-485, RBL 9 IAW AMM 53-00-49-400-801, CONFIG, A03.

Part: SEAT TRACK — CORRODED (BS 581-629) · airframe 28,709 hrs · 20,224 cycles

RT SIDE FLOOR SEAT TRACK IS CORRODED AT FS581 TO FS629. RT SIDE FLOOR SEAT TRACK AT FS 581- FS 629 FOUND TO BE OUT OF LIMITS IAW CREO 670-53-00-013. REMOVED RT SIDE FLOOR SEAT TRACK AT FS 581-629 IAW AMM 53-00-49-000-801, A03. FABRICATED NEW RT SIDE FLOOR SEAT TRACK AT FS 581-629 IAW REO 670-53-00-343. INSTALLED NEW FABRICATED RT SIDE FLOOR SEAT TRACK AT FS 581-629 IAW AMM 53-00-49-400-801 A03. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV M, AS WRITTEN.

Part: SEAT TRACK — CORRODED (BS 364-485) · airframe 28,709 hrs · 20,224 cycles

FLOOR SEAT RAIL CORRODED AROUND SCREW HOLES FS 364-FS 485, LBL 9. EVALUATED SEAT RAIL LBL9, FS 485- FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. REMOVED SEAT RAIL, LBL 9, FS 485 IAW AMM 53-00-49-000-801, A03. FABRICATED SEAT RAIL IAW REO 670-53-00-343, REV K. INSTALLED NEW SEAT RAIL AT FS 364-485, LBL 9 IAW AMM 53-00-49-400-801, CONFIG A03. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV M, AS WRITTEN.

Part: SEAT TRACK — CORRODED (BS 465) · airframe 28,709 hrs · 20,224 cycles

LT SIDE INBD FLOOR SEAT TRACK IS CORRODED AT FS465. LT SIDE FLOOR TRACK AT FS 485. FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. REMOVED LT SIDE IB FLOOR SEAT TRACK AT FS 485 IAW AMM 53-00-49-000-801, A03. FABRICATED NEW SEAT TRACK LT SIDE INBD FLOOR TRACK IAW REO 670-53-00-343. INSTALLED NEW FABRICATED LT SIDE INBD FLOOR SEAT TRACK AT FS 485 IAW AMM 53-00-49-400-801, A03. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV M, AS WRITTEN.

Part: SEAT TRACK — CORRODED (BS 708-761) · airframe 28,709 hrs · 20,224 cycles

SIDEWALL SEAT RAIL IS CORRODED AT FS 708.00-761.85 RT SIDE. CORROSION DAMAGE EXCEEDS ALLOWABLE LIMITS OF REO 670-53-00-013. R & R SEAT RAIL. COMPLIED WITH EC/TC REO 670-53-00-343, REV K AND GREO 670-53-00-343, REV M. REMOVED SEAT RAIL IAW AMM 53-00-49-000-801-A03. INSTALLED SIDE WALL SEAT RAIL AT FS708.00-761.85 IAW AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 785-813) · airframe 28,709 hrs · 20,224 cycles

SIDEWALL SEAT RAIL IS CORRODED AT FS 785.15 - 813 LT SIDE. COMPLIED WITH EC/TC REO 670-53-00-013 AND GREO 670-53-00-013, REV J.

Part: RETAINER — CHAFED (CARGO DOOR SEAL) · airframe 28,709 hrs · 20,224 cycles

SEAL RETAINER FWD AND AFT CORNER ON FWD CARGO DOOR. REPAIRED IAW REO 670-52-35-127 & ECTC REO 670-52-35-127 01. COMPLIED WITH ECTC REO 670-52-35-127 01 FOR THE PERMANENT REPAIR. RECEIVED EC/TC REO 670-52-35-127 01. REMOVED LOWER PLATE FORM FWD RT BAGGAGE DOOR TO FOM IAW 51-41-02-001-001 A01. INSTALLED LOWER PLATE FOR FWD BAGGAGE BAY DOOR IAW AMM 52-38-27-400-802 A01.

Part: SEAT TRACK — CORRODED (BS 677-708) · airframe 28,709 hrs · 20,224 cycles

SIDE WALL SEAT RAIL IS CORRODED AT FS 677 - 708 LT SIDE. CORROSION DAMAGE EXCEEDS ALLOWABLE LIMITS OF REO 670-53-00-013. REMOVED SIDE WALL SEAT RAIL AT 677.00-708.00 LT SIDE IAW AMM 53-00-49-000-801, A03. FABRICATED NEW SEAT RAIL AT FS 677.00-708 IAW REO 670-53-00-343 INSTALLED NEW FABRICATED SIDE SEAT RAIL WALL AT FS 677.00-708.00 LT SIDE IAW AMM 53-00-49-400-801-A03. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV M AS WRITTEN.

Part: FLOOR SUPPORT — CORRODED (BS 1000-1047) · airframe 28,709 hrs · 20,224 cycles

CARGO COMPARTMENT FLOOR SUPPORT CORRODED AT BS 1000-1047, LBL 27. CORROSION OUT OF LIMITS IAW SRM 53-61-43-101-001-A01. CUT OUT DAMAGED SECTION OF THE FLOOR SUPPORT IAW SRM 53-00-41-201-001-A01 & RIG 53-00-41-991-830. COMPIED WITH REPAIR IAW EC/TC EO 700-53-0288 & GREO 670-53-00-029, REV A.

Part: SEAT TRACK — CORRODED (BS 708-761) · airframe 28,709 hrs · 20,224 cycles

SIDE WALL SEAT RAIL IS CORRODED AT FS 708.00-761.85 LT SIDE. CORROSION EXCEEDS LIMITS ALLOWED BY REO 670-53-00-013, REMOVED AND REPLACED SEAT RAIL. REMOVED SIDE WALL SEAT RAIL AT FS708.00-761.85 LT SIDE IAW AMM 53-00-49-000-801-A03. FABRICATED NEW SEATRAIL SIDE WALL AT FS708.00-761.85 IAW REO 670-53-00-343. INSTALLED NEW FABRICATED SIDE SEAT RAIL, LT SIDE AT FS708.00-761-85 IAW AMM 53-00-49-400-801-A03. COMPLIED WITH ECTC REO 670-53-00-383 AND GREO 670-53-00-34, REV M AS WRITTEN.

Part: FLOORBEAM — CORRODED (BS 333) · airframe 28,709 hrs · 20,224 cycles

ANGLE CORRODED UNDER FLOORBEAM CAP AT FS 333.00, RBL 9. R & R THE FLOORBEAM ANGLE IAW SRM 51-42-06-001-001, A01 AND 51-25-01-001-001, A01.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 28,709 hrs · 20,224 cycles

ANGLE CORRODED UNDER FLOORBEAM CAP AT FS 349, RBL 9. R & R ANGLE UNDER FLOORBEAM CAP IAW SRM 51-42-06-001-001, A01 AND 51-25-01-001-001, A01.

Part: DOOR SILL — CORRODED (SERVICE DOORWAY) · airframe 28,709 hrs · 20,224 cycles

SERVICE DOOR SILL HAS SEVERAL AREAS OF CORROSION. ANGLE WAS FOUND TO BE OUT OF LIMITS. R & R LOWER MOUNTING ANGLE AND LOWER SILL ANGLE AT SERVICE DOOR SILL IAW SRM 51-42-06-001-001-A01, SRM 51-42-13-001-001-A01, SRM 51-42-21-001-001-A01, SRM 51-42-15-001-001-A01 AND DWG SH670-31950.

Part: FLOOR SUPPORT — CRACKED · airframe 28,709 hrs · 20,224 cycles

FLOOR SUPPORT CRACKED UNDER ADG HYD PUMP. COMPLIED WITH EC/TC REO 670-53-11-509 RT SIDE REPAIR TYPE 2 AND GREO 670-53-11-509, REV B DATED 01-28-2014.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 28,709 hrs · 20,224 cycles

FLOOR SUPPORT ANGLE AT FS 280.00 IS CORRODED. REMOVED THE AFT COCKPIT FLOOR SUPPORT ANGLE AT FS 280 IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. INSTALLED NEW, SERVICEABLE AFT FLOOR SUPPORT ANGLE AT FS 280 IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-21-16-001-001-A01, DWG CC670-34010, CC670-33052, CC670-51-620. LOCATED FASTENER HOLES IN NEW, SERIVCABLE ANGLE ASSY IAW SRM 51-40-11-001-001-A01 CROSSBEAM AND ANGLE IAW SRM 51-42-06-001-001-A01.

Part: INTERCOSTAL — CORRODED (BS 364) · airframe 28,709 hrs · 20,224 cycles

SEVERAL AREAS OF CORROSION FOUND ON INTERCOSTALS AT FS 364 JUST FORWARD OF AVIONICS DOORS CUTOUT. REMOVED CORROSION ON INTERCOSTAL 27R FOUND TO BE OUT OF LIMITS REF: SRM 51-21-06-001-001, A01 AND SRM 53-21-23-101-003, A01. R & R INTERCOSTAL AT STR 27R BETWEEN FS 349.00 & 364.00, REF: SRM 51-42-06-001-001 A01, 51-42-21-001-001, A01 DWG: SH670-32075 REV NC & SH670-32050, REV NC. REMOVED LIGHT SURFACE CORROSION ON INTERCOSTAL AT STR 26R & 26L AREAS FOUND TO BE WITHIN LIMITS RESTORED FINISH REF: SRM 51-21-06-001-001 A01, 51-25-06-001-001 A01, 51-25-11-001-001-A01, SRM 53-21-23-101-003-A01, 53-00-00-101-001-A01 NO MATERIAL LOSS.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 27,822 hrs · 19,506 cycles

CEILING EMERGENCY LIGHT INOPERATIVE BY ROW 14. REPLACED CEILING EMERGENCY LIGHT BULB IAW AMM 33-51-09. OPS CHECK GOOD.

Part: HANDLE — LACK OF LUBE (PAX DOOR) · airframe 26,249 hrs · 18,298 cycles

F/A REPORTS PAX DOOR VERY DIFFICULT TO OPEN AND CLOSE. CLEANED AND LUBED PAX DOOR HANDLE IAW AMM 52-11-00. OPS CHECK GOOD.

Part: RETAINER — DAMAGED (CARGO DOOR SEAL) · airframe 25,289 hrs · 17,557 cycles

FWD CARGO DOOR SEAL RETAINER DAMAGED AT FWD AND AFT CORNERS. COMPLIED WITH ECTC REO 670-52-35-127 01. CONSIDERED A MAJOR REPAIR IAW GMM 5-3.

Part: FLOOR SUPPORT — CORRODED (BS 285-589) · airframe 24,572 hrs · 17,030 cycles

CORROSION ON RT FLOOR SUPPORT AT BS 285-289. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. FOUND TO BE OUT LIMITS IAW SRM 53-00-00-101-001. REPAIRED FLOOR SUPPORT IAW SRM 53-21-43-201-002-A01. MAJOR REPAIR.

Part: WEB — CORRODED (BS 280) · airframe 24,572 hrs · 17,030 cycles

RT 280 WEB CORRODED. COMPLIED WITH REO 670-53-11-594. CROSSBEAM, LOWER RT WEB AND STRAP REQUIRES ASSY IAW GREO 670-53-11-594. INSTALLED STRAP TO RT LOWER WEB AND CROSSBEAM TO RT LOWER WEB IAW GREO 670-53-11-594. COMPLIED WITH ECTC REO 670-53-11-594-01. MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (COCKPIT) · airframe 24,572 hrs · 17,030 cycles

COCKPIT FLOOR SUPPORT CORRODED. R & R COCKPIT FLOOR SUPPORT IAW SB670-53-041.

Part: WEB — CORRODED (BS 280) · airframe 24,572 hrs · 17,030 cycles

LT 280 WEB CORRODED. COMPLIED WITH GREO 670-53-11-594. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED · airframe 24,572 hrs · 17,030 cycles

RT SIDE OF CABIN AFT AT THE LAV THE WALL SEAT TRACK IS CORRODED. R & R SEAT TRACK IAW AMM 53-00-49-000-801-A03 AND 53-00-49-400-801-A03.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 24,572 hrs · 17,030 cycles

RIGHT BS 280 FLOORBEAM CORRODED. R & R FLOORBEAM IAW SB670BA-53-041 AND SB670BA-53-041, PART A.

Part: SEAT TRACK — CORRODED · airframe 24,572 hrs · 17,030 cycles

LT SIDE SEAT TRACK JUST AFT OF EMERGENCY EXIT IS CORRODED. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801-A03. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801-A03.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 24,572 hrs · 17,030 cycles

LT BS 280 FLOORBEAM CORRODED. R & R FLOORBEAM IAW SB670BA-53-041 AND ECTC SB670BA-53-041, PART A.

Part: SEAT TRACK — CORRODED · airframe 24,572 hrs · 17,030 cycles

RT SIDE WALL SEAT TRACK JUST AFT OF THE EMERGENCY EXIT IS CORRODED. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801-A03. INSTALLED SEAT TRACK JUST AFT OF EMERGENCY EXIT IAW AMM 53-00-49-400-801-A03.

Part: SKIN — CHAFED (BS 977) · airframe 24,572 hrs · 17,030 cycles

AFT LOWER FUSELAGE SKIN AND RIVET CHAFED FWD OF REPAIR PATCH AT APPROXIMATELY FS 977. R & R CHAFED AREA WITH DOUBLERS IAW REO 670-53-61-1034 AND AUTHORIZED BY REO 670-53-61-1034.

Part: SKIN — CRACKED (FUSELAGE) · airframe 24,572 hrs · 17,030 cycles

RIGHT TRU DOOR AFT LATCH FRAME AFT UPPER CORNER HAS A CRACK. REMOVED LANDING AND DRILLED UP NEW LANDING IAW SRM 51-42-06-001-001-A01 & 51-40-11-001-001-A01. INSTALLED LANDING SHOOTING 70 EA RIVETS IAW SRM 51-42-06-001-001-A01 AND IAW SRM 51-42-13-001-001-A01 AND EO CC670-33-040.

Part: SIGN — DAMAGED (SERVICE DOOR) · airframe 24,500 hrs · 16,976 cycles

SERVICE DOOR INNER HANDLE SELF ILLUMINATED EXIT BETA SIGN UNREADABLE. R & R SERVICE DOOR INNER HANDLE SELF ILLUMINATED EXIT BETA SIGN IAW AMM 33-51-13.

Part: DOOR — FROZEN (MAIN PAX) · airframe 24,413 hrs · 16,912 cycles

PASSENGER DOOR WILL NOT OPEN. THAWED ICE FROM PASSEAGER DOOR, OPENS AND CLOSES NORMALLY IAW AMM 52-11-00, ACFT OK FOR SERVICE.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 23,907 hrs · 16,543 cycles

COVER MISSING FROM EMERGENCY LIGHT. REPLACED COVER IAW AMM 33-51-11. NO DEFECTS NOTED. ACFT OK FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 22,408 hrs · 15,493 cycles

EMERGENCY LIGHTS BATTERY DEAD. CHARGED EMERGENCY LIGHTS POWER SUPPLY WITH ACFT POWER. DISCREPANCY NO LONGER EXISTS IAW NO FURTHER ACTION IS REQUIRED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 20,407 hrs · 14,021 cycles

CABIN CEILING EMERGENCY LIGHT ROW 1 INOPERATIVE. RELAMPED CABIN CEILING EMERGENCY FLOOD LIGHT AT ROW 1. OPS CHECKED GOOD IAW AMM 33-51-00.

Part: SKIN — DENTED (VERTICAL STAB) · airframe 20,117 hrs · 13,820 cycles

DURING BIRD STRIKE INSPECTION, FOUND DENTS IN VERTICAL STAB L/E. REPAIRED IAW SRM 51-40-11-001-001

Part: SILL — CORRODED (BS 1000-1047) · airframe 20,117 hrs · 13,820 cycles

CORROSION FOUND ON AFT CARGO DOOR SILL, FS 1000.00 TO 1047.00 AT STRINGER 17.

Part: STRUCTURE — CORRODED (BS 265) · airframe 20,117 hrs · 13,820 cycles

FUSELAGE AT FS 265 BETWEEN STR 26 -27R IS CORRODED. REPAIRED IAW REO 670-53-11-688.

Part: ATTACH ANGLE — CORRODED (BS 349-364) · airframe 20,117 hrs · 13,820 cycles

AVIONICS COMPARTMENT FORWARD ATTACHMENT ANGLE BETWEEN FS 349 - 364 JUST LT OF S27R IS CORRODED. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR.

Part: SUPPORT ANGLE — CORRODED · airframe 20,117 hrs · 13,820 cycles

LT AND RT FORWARD JACKING FITTING SUPPORT ANGLES ARE CORRODED. REPAIRED IAW REO 670-53-11-689.

Part: ATTACH ANGLE — CORRODED (BS 349-364) · airframe 20,117 hrs · 13,820 cycles

AVIONICS COMPARTMENT FORWARD ATTACHMENT ANGLE BETWEEN FS 349 - 364 JUST RIGHT OF S27R IS CORRODED. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR.

Part: CROSSBEAM — CORRODED · airframe 20,117 hrs · 13,820 cycles

CROSSBEAM HAS CORROSION. REPAIRED IAW REO 670-53-11-047.

Part: SKIN — CORRODED (BS 310-395) · airframe 20,117 hrs · 13,820 cycles

CORROSION ON INNER AND OUTER FUSELAGE SKIN BETWEEN FS 310 -395 AND STR 25-26R. REPAIRE IAW REO 670-53-21-824, REV A.

Part: ATTACH ANGLE — CRACKED (VERTICAL STAB) · airframe 20,117 hrs · 13,820 cycles

VERTICAL STAB RT ATTACH ANGLE CRACKED AT AFT T/E AREA. REMOVED RT SIDE VERTICAL STAB AFT ATTACH ANGLE IAW SRM 51-42-13-001-001-A01, 51-42-21-001-001-A01, 51-42-22-001-001-A01. INSTALLED ANGLE IAW AMM 51-42-13-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 708-767) · airframe 20,117 hrs · 13,820 cycles

LEFT SEAT TRACK SEGMENT BETWEEN FS 767 AND 708 HAS ONE SPOT OF CORROSION. REMOVED SIDE SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 20,117 hrs · 13,820 cycles

RIGHT FLOOR SEAT TRACK SEGMENT BETWEEN FS485 AND 581 HAS ONE SPOT WITH MINOR CORROSION. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801/9A03. FOUND SEAT TRACK CORROSION IS OUT OF LIMITS IAW SRM 53-31-49-101-A01. INSTALLED TRACK IAW AMM 53-00-49-400-807-A03.

Part: SEAT TRACK — CORRODED (BS 785.15-863) · airframe 20,117 hrs · 13,820 cycles

LEFT SEAT TRACK SEGMENT BETWEEN FS 785.15 AND 863 HAS 2 SPOT OF CORROSION. REMOVED SIDE SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801-A03.

Part: SILL — CORRODED (BS 1000-1047) · airframe 20,117 hrs · 13,820 cycles

CORROSION FOUND ON AFT CARGO DOOR CUTOUT FLOOR SILL UNDER FLOOR PANEL 281JLF FS 1000.00 TO 1047.00 AT STRINGER 17. REMOVED CORROSION IAW SRM 51-21-06-001-001. FOUND TO BE OUT OF LIMITS 100 PERCENT MATERIAL LOSS FROM DEEP PITTING IAW SRM 53-00-00-101-001. REMOVED AFT CARGO DOOR SILL IAW SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-42-20-001-001-A01, 51-42-21-001-001-A01 AND INSTALLED NEW SERVICEABLE SILL IAW SRM 51-42-21-001-001-A01 51-42-06-001-001-A01,51-42-13-001-001-A01, MM 670-35085 DWG JH161727.

Part: SEAT TRACK — CORRODED (BS 379-485) · airframe 20,117 hrs · 13,820 cycles

SEAT TRACK BETWEEN FS 379-485 AT LBL 9.0 CORRODED. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801. COMPLIED WITH EC/TC REO 670-53-00-343 AND GENERIC REO 670-53-00-343 REV B.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 20,117 hrs · 13,820 cycles

RT 280 BULKHEAD IS CORRODED AT FLOOR SUPPORT INBD SIDE. REMOVE CORROSION FOR FURTHER EVALUATION IAW SRM 51-21-06-001-001. FOR REPAIR TO RT SIDE 200 BULKHEAD WEB.

Part: WEB — CORRODED (BS 280) · airframe 20,117 hrs · 13,820 cycles

RIGHT FS 280 WEB HAS CORROSION. REMOVE CORROSION IAW SRM 53-11-10-201-003 & 51-21-06-001-001. FOUND TO BE OUT OF LIMITS IAW 53-11-10-201-203. REMOVED WEB AND FABRICATED REPLACEMENT PARTS IAW REO 670-53-11-594, STEPS 1-4. NDT IAW REO 670-53-11-594 IAW NDTM PART 1, 51-20-006, NO INDICATIONS NOTED. INSTALLED NEW PART IAW REO 670-53-11-594.

Part: PANEL — DETERIORATED (CABIN) · airframe 20,117 hrs · 13,820 cycles

FWD CARGO WALL PANEL 151KLW HAS HOLE WORN THROUGH. LOCATED AND DRILLED NEW WALL PANEL 151KLW IAW SRM 51-41-02-001-001-A01. REPLACED WALL PANEL 151KLW WITH A SERVICEABLE PANEL.

Part: SEAT TRACK — CORRODED (BS 677-708) · airframe 20,117 hrs · 13,820 cycles

RIGHT SEAT TRACK SEGMENT BETWEEN FS 677 AND 708 HAS ONE SPOT OF CORROSION. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801-A03.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 20,117 hrs · 13,820 cycles

FS 280.00 CROSSBEAM HAS CORROSION. REMOVED CORRODED CROSSBEAM IAW REO 670-53-11-047. INSTALLED CROSSBEAM IAW REO 670-53-11-047.

Part: ATTACH ANGLE — CORRODED (BS 349-364) · airframe 20,117 hrs · 13,820 cycles

AVIONICS COMPARTMENT FORWARD ATTACHMENT ANGLE BETWEEN FS 349-364. JUST RIGHT OF STR 27 IS CORRODED. FOUND NO DAMAGE ALLOWED AT DAMAGED AREA REF SRM 53-21-23-101-003-A01. REMOVED ATTACH ANGLE IAW SRM 51-42-06-001-001. INSTALLED ATTACH ANGLE IAW SRM 51-42-06-001-001.

Part: FLOOR SUPPORT — CORRODED (BS 280) · airframe 20,117 hrs · 13,820 cycles

AVIONICS COMPARTMENT FLOOR SUPPORT ANGLE AT FS 280 IS CORRODED. FOUND DAMAGE TO BE OUT OF LIMITS IAW SRM 53-22-55-101-001-A01. REMOVED FLOOR SUPPORT ANGLE IAW SRM 51-42-06-001-001. INSTALLED FLOOR SUPPORT ANGLE IAW SRM 51-42-06-001-001, 51-42-10-001-001.

Part: SKIN — CORRODED (BS 295-310) · airframe 20,117 hrs · 13,820 cycles

CORROSION ON INNER AND OUTER FUSELAGE SKIN BETWEEN FS 295-310 AND STR 25-26R. BLENDED DAMAGE, FOUND OUT OF LIMITS REF SRM 51-26-00-001-001-A01 & SRM 51-21-06-001-001-A01. REPAIERED IAW REO 670-53-21-824.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 20,117 hrs · 13,820 cycles

AVIONICS COMPARTMENT FORWARD INTERCOSTAL FS 349-364 LEFT OF STR 27 IS CORRODED. FOUND NO DAMAGE ALLOWED AT DAMAGED AREA REF SRM 53-21-23-101-003-A01. REMOVED INTERCOSTAL IAW SRM 51-42-06-001-001. LOCATED AND DRILLED INTERCOSTAL IAW SRM 51-40-11-001-001, SERVICEABLE INTERCOSTAL. INSTALLED INTERCOSTAL IAW SRM 51-42-06-001-001.

Part: BULKHEAD — CORRODED (BS 280) · airframe 20,117 hrs · 13,820 cycles

LEFT BS 280 BULKHEAD IS CORRODED AT FLOOR SUPPORT INBD SIDE. REMOVED LIGHT CORROSION SRM 51-21-06-001-001-A01. RESTORED FINISH IAW SRM 51-21-06-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 677-830.4) · airframe 20,117 hrs · 13,820 cycles

RIGHT SEAT TRACK SEGMENT BETWEEN FS 677 AND 830.40 HAS 2 SPOTS WITH CORROSION. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801(A03). INSTALLED NEW FABRICATED SEAT TRACK SEGMENT IAW AMM 53-00-49-400-801-A03.

Part: ANGLE — CORRODED (SILL) · airframe 20,117 hrs · 13,820 cycles

PAX DOOR SILL UPPER ANGLE FOR FLOOR SUPPORT IS CORRODED AROUND SCREW. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 51-21-06-001-001-A01 AND 53-21-23-101-001-A01. REMOVED ANGLE IAW SRM 51-42-06-001-001-A01. INSTALLED ANGLE IAW SRM 51-41-02-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 830.4-869) · airframe 20,117 hrs · 13,820 cycles

LEFT SEAT TRACK SEGMENT BETWEEN FS 830.40 AND 869 HAS ONE SPOT WITH CORROSION. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801(A03). INSTALLED NEW FABRICATED SEAT TRACK SEGMENT IAW AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 785.15-863) · airframe 20,117 hrs · 13,820 cycles

RIGHT SEAT TRACK SEGMENT BETWEEN FS 785.15 AND 863 HAS 3 SPOT WITH CORROSION. REMOVED SIDE SEAT TRACK IAW AMM 53-00-49-00-801. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-A03.

Part: FRAME — CORRODED (BS 265) · airframe 20,117 hrs · 13,820 cycles

FUSELAGE FRAME AT FS 265 BETWEEN STR 26-27 R IS CORRODED. BLENDED CORROSION IAW SRM 51-42-06-001-001 & SRM 51-21-06-001-001. PERFORMED UT THICKNESS INSPECTION IAW MAC NDT PROCEDURES UT-3. MINIMUM MATERIAL REMAINING .049" ORIGINAL .050" MATERIAL REMOVED .001". REPAIRED IAW REO 670-53-11-688, STEP 1.

Part: SEAT TRACK — CORRODED (BS 581-677) · airframe 20,117 hrs · 13,820 cycles

LEFT SEAT TRACK SEGMENT BETWEEN FS 581 AND 677 HAS ONE SPOT WITH CORROSION. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED NEW FABRICATED SEAT TRACK SEGMENT IAW AMM 53-00-49-400-801-A03.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 20,117 hrs · 13,820 cycles

COCKPIT FLOORBEAM AT FS 280 CORRODED. R & R FWD COCKPIT FLOORBEAM IAW SRM 51-42-06-001-001-+A01 AND 51-42-21-001-001-A01. REPAIR CLASSIFIED AS MINOR.

Part: SEAT TRACK — CORRODED (BS 581-677) · airframe 20,117 hrs · 13,820 cycles

RIGHT FLOOR SEAT TRACK SEGMENT BETWEEN FS581 AND 677 HAS ONE SPOT WITH CORROSION. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801-A03.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 20,117 hrs · 13,820 cycles

LEFT AND RIGHT FORWARD JACKING SUPPORT ANGLES ARE CORRODED. BLEND SUPPORT ANGLES IAW SRM 51-42-06-001-001 & 51-21-06-001-001. PERFORMED UT THICKNESS OF BLEND AREAS IAW MAC NDT INSPECTION PROCEDURE UT-3. MINIMUM MATERIAL REMAINING LT .060", RT .061", ORIGINAL IS .063" MATERIAL REMOVED IS .003". REPAIRED IAW REO 670-53-11-689, STEP 1.

Part: ATTACH ANGLE — CORRODED (BS 349-364) · airframe 20,117 hrs · 13,820 cycles

AVIONICS COMPARTMENT FORWARD ATTACHMENT ANGLE BETWEEN FS 349-364 AT STR 26R IS CORRODED. REMOVED CORROSION, NO MATERIAL LOSS, FOUND TO BE WITHIN THE ALLOWABLE DAMAGE LINIT OF 10 PERCENT IAW SRM 51-21-06-001-001 AND 53-21-06-101-006.

Part: FITTING — CORRODED (BS 280) · airframe 20,117 hrs · 13,820 cycles

RT FITTING CORRODED AT FS 280 BETWEEN FLIGHT COMPARTMENT FLOOR SUPPORT AND RT BULKHEAD POST. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. RESTORED FINISH IAW SRM 51-21-06-001-001-A01.

Part: ATTACH ANGLE — CRACKED (VERTICAL STAB) · airframe 20,117 hrs · 13,820 cycles

VERTICAL STAB RT ATTACH ANGLE APPEARS CRACKED AT T/E AREA. REMOVE PAINT IAW SRM 51-25-01-001-001-A01. PERFORMED EDDY CURRENT INSPECTION IAW MAC NDT INSPECTION PROCEDURE ET-2, CONFIRMED CRACKED. REPAIRED IAW GREO 670-55-31-018 AND REO 670-53-31-018.

Part: SUPPORT ANGLE — CRACKED (PAX DOOR) · airframe 20,117 hrs · 13,820 cycles

PAX DOOR AFT ANGLE CHANNEL SUPPORT FOR STEPS SKIN CRACKED BY MOTOR PULLEY. REMOVED CRACKED ANGLE SECTION AND FABRICATED SERVICEABLE ANGLE SECTION IAW SRM 51-24-36-001-001-A01, 51-40-11-001-A01, 52-11-04-201-002-A01. INSTALLED ANGLE SECTION IAW SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-42-22-001-01-A01, 52-11-04-2014-002-A01. REPAIR CLASSIFIED AS MINOR.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 19,262 hrs · 13,220 cycles

RT OVER WING EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP IAW AMM 33-51-15. OPS CHECKED GOOD.

Part: PLACARD — DETERIORATED (CABIN) · airframe 17,737 hrs · 12,146 cycles

PAX DOOR EXIT PLACARD PEELING. R & R PAX DOOR EXIT PLACARD IAW AMM 20-60-04. R & R PAX DOOR EXIT PLACARD IAW AMM 20-60-04. OK FOR SERVICE.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 17,326 hrs · 11,868 cycles

IN CABIN REAR FACING EMERGENCY CALL LIGHT IS INOP. RELAMPED EMERGENCY CALL LIGHT CENTER CABIN. OPS CHECKED GOOD IAW MM 33-51-00.

Part: SMOKE DETECTOR — FALSE INDICATION (LAVATORY) · airframe 17,131 hrs · 11,734 cycles

MOMENTARY SMOKE AFT LAV WARNING. R & R AFT LAV SMOKE DETECTOR, OPS CK GOOD, REF AMM 26-16-01. (CLOSED)

Part: FAN — FAILED (GALLEY) · airframe 16,529 hrs · 11,338 cycles

STRONG SMOKE /FUME ODOR IN CABIN AND FLT DECK AFTER TAKEOFF. ACFT RETURNED TO DEPARTURE AFTER T/O. REPLACED GALLEY EXHAUST FAN B05 AND OPS CKD GOOD IAW AMM 21-23-93. (CLOSED)

Part: FLOORBEAM — CORRODED (BS 280) · airframe 15,186 hrs · 10,312 cycles

FWD FLOOR SUPPORT ANGLE OF FS 280 BEAM CORRODED. REMOVED FS 280 FWD SUPPORT ANGLE IAW SRM 51-42-21. INSTALLED FLOOR SUPPORT ANGLE PN CC670-33292-135 IAW SRM 51-42-06-001-001-A01 AND 51-42-20-001-001-A01.

Part: CROSSBEAM — CORRODED (BS 280) · airframe 15,186 hrs · 10,312 cycles

RT 280 CROSS BEAM REQUIRES REMOVAL FOUND CORRSION. REMOVED RT 280 CROSSBEAM IAW SRM 51-42-06 & 51-42-21 TASK 51-42-06-001-001-A01, 51-42-21 001-001-A01. INSTALLED RT 280 BEAM.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 15,186 hrs · 10,312 cycles

LT 280 CROSSBEAM REQUIRES REMOVAL FOUND CORROSION. REMOVED LT 280 CROSSBEAM IAW SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. PICKED UP FASTENERS HOLES IN NEW FS 280 LT CROSSBEAM FOR SOLID RIVETS AND LOCK FASTENERS IAW SRM 51-42-05-001-001-A01 & 51-42-06-001-001-A01. INSTALLED LT 280 BEAM. OK TO INSTALL. INSTALLED 280 BEAM IAW SRM 51-42-06-001-001-A01.

Part: WEB — CORRODED (FUSELAGE) · airframe 15,186 hrs · 10,312 cycles

ON INSP, FOUND LT 280 VERTICAL WEB TO BE CORRODED. (RESOLVED ON W/O: 145698 TASKCARD: N/R-00420 ) (JOB 7114125, OPERATION 32) REMOVED LT 280 LOWER WEB IAW REO 670-53-11-052 REPAIR NR 2 STEP 8. AK 161734 02/19/10 (LT) BENT UP NEW WEB FOR LT SIDE 280, NEW WEB BEND RADIUS REQUIRES NDT FOUND NOT TO BE REQUIRED IAW REO 670-53-11-052. AK 161734 02/20/10 (LT) ROUGH FORMED E/H 280 WEB, DRILLED ALL HOLES THROUGH AFT SIDE OF WEB AND DRILLED 1ST 2 I/B BAYS OF FWD SIDE OF WEB IAW REO 670-53-11-052 STEP 9. AK 161734 02/20/10 (LT 02/22/10). WEB REQUIRES FINAL TRIM AND THE COMPLETION OF BEING DRILLED UP ON FWD SIDE. FINISHED DRILLING LT WEB, FINAL TRIMED, DEBURRED, ALIODENE, PRIMED AND PAINTED IAW REO 670-53-11-052.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 15,186 hrs · 10,312 cycles

ON INSP, FOUND 280 BEAM TO BE CORRODED OUT OF LIMITS. EO 700-53-0061 ITEM 3 CUT OUT DAMAGED 280 LT AND RT BEAM SECTIONS. REMOVED FS 280 FLOORBEAM FASTENERS IAW SRM 51-42-06 AND 51-42-21 TO COMPLETELY REMOVE DAMAGED BEAM SECTIONS FOR REPLACEMENT. CUT FLOORBEAM AS SHOWN IN REO 670-53-11-047 PER NOTE 1. IAW NOTE 2 OF REO 670-53-11-047 AND EO 700-53-0061 ITEM 4, PERFORMED ET INSP OF CUT LINE ON FLOORBEAM IAW REO670-53-11-047 AND EO700-53-0061 IAW NDTM PART 1, 51-20-006. NO INDICATED NOTED AT THIS TIME. -2 & -3 FABRICATED DOUBLERS REQUIRED IAW NDTM PART 1, 51-20-006 OR PART 1,

Part: WEB — CORRODED (FUSELAGE) · airframe 15,186 hrs · 10,312 cycles

ON INSP FOUND RT 280 VERTICAL WEB TO BE CORRODED. (RESOLVED ON W/O: 145698 TASKCARD: N/R-00423 ) JOB 7114125, OPERATION 35 COMPLIED WITH EO 700-53-0062 REPAIR 2 WEB REPLACEMENT OF RT 280 LOWER WEB PN CC670-34170-2.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 15,186 hrs · 10,312 cycles

UPON INSP, FOUND CORROSION AT FWD END OF FLOOR SUPPORT BEAM LBL 9 AT 280 ATTACH BRACKET UNDER FLOOR BEAM CAP. REMOVED RIVETS TO SEPARATE CAP FROM FLOORBEAM AT FS 280, LBL 9 BLENDED CORROSSION REMOVED DAMAGE REF. 51-42-06-001-001-A01 & 51-21-06-001-001-A01 SUBMITTED DAMAGE TO MFG. RECEIVED REO 670-53-21-535 AND CORRESPONDING ASA EC/TC. TW 161752. REINSTALL RIVETS TO RE-ATTACHED CAP TO FLOORBEAM. COMPLIED WITH EC/TC REO 670-53-21-535 AND REINSTALLED RIVETS THRU UPPER CAP AND LONGITUDINAL FLOORBEAM AT LBL9, FS280 - 285.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,186 hrs · 10,312 cycles

MINOR SURFACE CORROSION ON RT SIDE SEAT RAIL BETWEEN 10CD AND 12CD. REMOVED MINOR SURFACE CORROSION ON RT SIDE SEAT RAIL BETWEEN 10CD AND 12CD IAW SRM 51-21-06-001-001-A01 AND TREATED AREA IAW SRM 51-21-11-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 477.4) · airframe 15,186 hrs · 10,312 cycles

LF FWD FLOOR SEAT TRACK AT SEAL 1B HAS SEVERE CORROSION AND MINOR SURFACE CORROSION FROM 1AB TO FS 477.40. REMOVED LEFT HAND FLOOR SEAT TRACK DUE TO BEING OUT OF LIMITS FOR SEVERE CORROSION PER SRM 53-21-49-101-001-A01. INSTALLED FWD MOST LEFT SEAT TRACK IAW AMM 53-00-49-400-801. PO 10141-0001.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,186 hrs · 10,312 cycles

MINOR SURFACE CORROSION ON RT FLOOR SEAT TRACK FROM 10CD TO 19CD. REMOVED RT SEAT RAIL AT FS 669.40 TO FS 855.40 AND FS 855.40 TO FS 977.00 WITCH COVERS FROM 10CD TO 19CD DUE TO BEING OUT OF LIMITS AFTER BLENDING ON CORROSION IAW SRM 53-51-49-101-001-A01. NEW SEAT RAILS FOR FS669.40 TO FS 977.00 ARE ON ORDER AND NEEDS TO BE INSTALLED. INSTALLED NEW SEAT TRACK ON RT SIDE OF FUSELAGE FROM FS 836.50 TO FS 977 IAW AMM 53-00-49-400-801 PO M321, M232. 3. SEAT RAILS FS 669.40 TO FS 836.50 RT FUSELAGE SIDE REQUIRES INSTALLATION. INSTALLED NEW SEAT TRACK RAILS ON RT SIDE AT FS 669.40 TO FS 836.50 IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,186 hrs · 10,312 cycles

MINOR SURFACE CORROSION ON LT SIDE SEAT RAIL BETWEEN SEATS 14AB TO 19AB. REMOVED MINOR SURFACE CORROSION ON LT SIDE SIDE WALL SEAT RAIL BETWEEN FS 785.15 THRU FS 985.00 IAW SRM 53-41-49-101-001-A01 AND 53-51-49-991-805 AND IS IDENIFIED AS REO 670-53-00-013- JOB COMPLETED.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 15,186 hrs · 10,312 cycles

RT FLOOR SEAT TRACK BADLY CORRODED FROM 2CD TO 10CD. CLEANED RT FLOOR SEAT TRACK FROM 2CD TO 10CD AT THE MOST SEVERELY ERRODED LOCATION IAW SRM 51-21-06-001-001-A01 AND FOUND DAMAGE TO BE BEYOND LIMITS IAW SRM53-31-49-101-001-A01. REMOVED RIGHT HAND SEAT RAILS WHICH COVERS FROM 2CD TO 10CD DUE TO BEING OUT OF LIMITS AFTER BEING BLENDED ON (CORROSION) PER SRM 53-21-49-101-001-A01 AND 53-31-49-101-001-A01. NEW SEAT RAILS. INSTALLED NEW SEAT TRACK RAILS IAW AMM 53-00-49-400-801. PO 10141-0001.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 15,186 hrs · 10,312 cycles

CORROSION ON LT SIDE SEAT RAIL AT 11AB. REMOVED MINOR CORROSION ON LEFT SIDE SEAT RAIL FROM 11AB TO 12AB AT 6EA LOCATIONS IAW SRM 51-21-06-001-001-A01 AND TREATED AREAS IAW SRM 51-21-11-001-001-A01. REMOVED .015 IN. MATERIAL AT 11AB LT TO CLEAN CORROSION AND PITTING. SEAT TRACK IS STILL WITHIN LIMITS IAW SRM 53-31-49-101-001-A01. IDENTIFIED BLENDED AREA WITH REO 670-53-00-013.

Part: PLACARD — ERODED (ESCAPE HATCH) · airframe 15,186 hrs · 10,312 cycles

CREW ESCAPE HATCH EXTERIOR PLACARDS FADED. INSTALLED SILKSCREENS S1859 AND S1875 IAW AMM TASK 20-60-11-400-801 (CONFIG A01) ON THE CREW ESCAPE HATCH. INSTALLED SILKSCREEN S1874 IAW AMM TASK 20-60-11-400-801. INSTALLED SILKSCREEN S1887 IAW AMM TASK 20-60-11-400-801. FADED PLACARDS WERE REMOVED PRIOR TO SILKSCREEN INSTALLATION IAW AMM TASK 20-60-11-000-801.

Part: LINK — CORRODED (EMERGENCY EXIT) · airframe 15,186 hrs · 10,312 cycles

RT OVERWING ESCAPE HATCH FAILED FUNCTION CHECK AT 89 LBS OF FORCE. FOUND LINK ROD BOLT CORREDED ON LATCH ASSY. REMOVED BOLT AND LINK ROD ASSY WITH SPRING IAW AMM 52-21-02-000-801. INSTALLED LINK ROD BOLT WITH SPRING LINK ROD ASSY PER AMM 52-21-02-400-801, ADJUSTED OVERWING FUNCTIONAL TEST OF OVERWING & EXIT PER AMM TASK 52-21-00-720-801 FUNCTIONAL CK GOOD.

Part: SIGN — DETERIORATED (CABIN) · airframe 15,160 hrs · 10,291 cycles

EXIT SIGN NEXT TO MAIN DOOR FADED UNABLE TO READ.

Part: PLACARD — WORN (CABIN) · airframe 15,160 hrs · 10,291 cycles

REINSTALLED PLACARD AMM 11-30-00 ACFT MX READY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,699 hrs · 9,176 cycles

RT GALLEY FLOOR LEVEL EMERGENCY FLOOD LENS COVER DAMAGED AND SEVERAL BULBS BURNED OUT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,762 hrs · 8,456 cycles

CEILING EMERGENCY LIGHT 4TH FROM FRONT INOP.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 11,380 hrs · 7,435 cycles

CAPTAIN EMERGENCY FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT IAW CRJ 700 AMM 25-61-00. (S)

Part: HANDLE — CRACKED (ASD) · airframe 10,748 hrs · 6,987 cycles

ASD OUTER HANDLE CRACKED.

Part: CASTING — CRACKED (E&E DOOR) · airframe 10,748 hrs · 6,987 cycles

AVIONICS DOOR HANDLE CASING CRACKED IN THE RADIUS AND CRACK CONFIRMED BY EDDY CURRENT.

Part: INTERCOSTAL — CRACKED (ASD) · airframe 10,748 hrs · 6,987 cycles

ASD INTERCOSTAL CRACKED BETWEEN ACCESS PANELS 832AR AND 832BR (MARKED).

Part: SKIN — CRACKED (DOOR) · airframe 10,748 hrs · 6,987 cycles

VDOOR INNER SKIN AT UPPER AFT CORNER (DOOR OPEN) CRACKED (MARKED) (RESOLVED ON W/O: 89292 TASKCARD: N/R-00122). JOB COMPLETE. 2 CUT OUT DAMAGED AREA. FABRICATED FILLER. FABRICATED DOUBLER DRILLED FILLER. SMOOTHED OUT ROUGH EDGES ON ASD INNER SKIN AT UPPER AFT CORNER PER REO 670-52-11-154. PERFORMED ET INSPECTION OF REWORKED AREA PER REO 670-52-11-154 IAW CRJ 700 NDTM 51-20-006. NO DEFECTS NOTED. PICKED UP EXISTING HOLES, LAYED OUT NEW HOLES AND ALODINED, AND PRIMED AND INSTALLED IAW REO 670-52-11-154. INSTALLED UPPER STIFFENER ON ASD DOOR IAW CRJ 700 SRM 51-42-06.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 10,398 hrs · 6,755 cycles

FLOOR EMERGENCY LIGHTING PHOTOLUMINESCENT STRIP MISSING IN FRONT OF GALLEY CARTS.

Part: WARNING LIGHT — ILLUMINATED (BRAKE OVERHEAT) · airframe 10,347 hrs · 6,719 cycles

BRAKE OVHT MSG EMERGENCY IN FLIGHT AT FL 340 C/W QRH ALL INDICATIONS NORMAL. REOCCURRED APPROX 15 MINS LATER AGAIN FOLLOWED QRH ALL IND RET TO NORMAL BUT LEFT GEAR DOWN AND RET TO ATL. AIRCRAFT RETURNED BACK TO ATL AFTER T/O, EMERGENCY DECLARED.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 8,747 hrs · 5,646 cycles

FWD F/A FLASHLIGHT INOP.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 8,690 hrs · 5,606 cycles

MEGAPHONE INOP.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 8,305 hrs · 5,342 cycles

CAPTAIN`S FLASHLIGHT INOP.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 7,289 hrs · 4,675 cycles

FOUND RT SIDE I/B ( FLOOR) SEAT TRACK FWD END CORRODED.

Part: SEAT TRACK — CORRODED (B S 400-700) · airframe 7,284 hrs · 4,670 cycles

LIGHT SURFACE CORROSION DETECTED THROUGHOUT LEFT FLOOR SEAT RAIL BETWEEN FS 400 TO FS 700.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 7,284 hrs · 4,670 cycles

LITE SURFACE CORROSION DETECTED THROUGHOUT RIGHT SIDE WALL SEAT RAIL BETWEEN FS 400 TO FS 953. REMOVED LITE SURFACE CORROSION ON RT SIDE WALL SEAT RAIL FROM FS 752.50 TO FS 953.00 IAW CRJ 700 SRM 51-21-49. SUPPLEMENTAL - SDR.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 7,284 hrs · 4,670 cycles

PAX DOOR AFT DRAG ANGLE CRACKED AT AFT MOTOR PULLEY BRACKET. REPAIRED IAW ALL SRMS.

Part: SEAT TRACK — CORRODED (BS 400-953) · airframe 7,284 hrs · 4,670 cycles

LIGHT SURFACE CORROSION DETECTED THROUGHOUT LEFT SIDE WALL SEAT RAIL BETWEEN FS 400 TO FS 953. REMOVED SURFACE CORROSION AND TREATED AS REQUIRED IAW CRJ 700 SRM 53-31-49 AT FS 400 THRU FS 953 SM17032 JOB COMPLETE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 7,284 hrs · 4,670 cycles

LITE SURFACE CORROSION DETECTED THROUGHOUT RIGHT FLOOR SEAT RAIL BETWEEN FS 400 TO FS 700.

Part: RIB — CRACKED (RT WING) · airframe 7,283 hrs · 4,669 cycles

RIGHT WING TRAILING EDGE SUPPORT RIB CRACKED AT WS 216. REPAIRED IAW SRM.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 7,283 hrs · 4,669 cycles

LEFT BS 280 BULKHEAD AFT WEB CORRODED. REMOVED AND REPLACED LT 280 WEB SPLICE IAW REO 670-53-11-052.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 7,284 hrs · 4,670 cycles

RIGHT STA 280 AFT BULKHEAD AFT WEB CORRODED.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 7,283 hrs · 4,669 cycles

STA 280 CROSSBEAM CORRODED BETWEEN RBL 9 AND LBL 9. COMPLIED WITH EC/TC EO700-53-0054 01 AND EO700-53-0061.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 7,283 hrs · 4,669 cycles

RT STA 280 AFT BULKHEAD AFT WEB CORRODED.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 7,283 hrs · 4,669 cycles

POSSIBLE CRACK AT LEFT VERTICAL STAB TO FUSELAGE ATTACH ANGLE AFT END (MARKED). PERFORMED ET INSPECTION OF LT ATTACH ANGLE IAW CRJ 700 NDT MANUAL PART 1, CHAPTER 51-20-006. ANGLE IS CRACKED IN RADIUS. CUT OUT DAMAGED AREA PER REO 670-55-31-015. ALL WORK DONE IAW REO 670-55-31-016 DK 7022603 1-9-7

Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,134 hrs · 4,581 cycles

LEFT FUSELAGE AFT EMERGENCY LIGHT INOP.

Part: ODOR — DETECTED (CABIN) · airframe 5,984 hrs · 3,848 cycles

ABOUT 10 AFTER TAKE OFF FROM MEN F/A NOTICED A BURNING ODOR, CAPT DID NOT. THEN CAPT NOTICED IT. THE ODOR THEN WENT AWAY, THEN CAME BACK STRONGER THAN BEFORE. CREW DONNED THE SMOKE MASKS. FTL DIV. F/A REPORTED BURNING SMELL CAME AND WENT SEVERAL TIMES AND WAS STILL PRESENT ON DECENT. CAPT REPORTS IT DID NOT SMELL LIKE PACK / BLEED ODOR. APU BLEED WAS NOT SELECTED ON. SMELL WAS FAINT DURING TAXI IN. (AN EMERGENCY WAS DECLARED, DIVERTED TO TUL)

Part: WARNING LIGHT — ILLUMINATED (MLG) · airframe 5,574 hrs · 3,591 cycles

AFTER TAKEOFF WHEN SELECTING GEAR UP ALL 3 GEAR REMAINED EXTENDED AND "GEAR DISAGREE" MSG ILLUMINATED. FOLLOWED QRH PROCEEDURES" GEAR UP DISAGREE" GEAR DISAGREE MSG DISAPPEARED. A/C RETURNED TO ATL AFTER T/O, AN EMERGENCY WAS DECLARED.

Part: STEP — BROKEN (PAX DOOR)

DURING A HANGAR INSPECTION IN MCN, THE PASSENGER DOOR BOTTOM STEP WAS FOUND TO BE BROKEN AT THE ATTACH LINK. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STEP — CRACKED (PAX DOOR)

DURING A C-CHECK IN MCN, THE BOTTOM STEP ON PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE BOTTOM STEP ON THE PASSENGER DOOR. (M)

Part: WIRE HARNESS — INOPERATIVE (LT MLG PROX SENS)

DURING DESCENT, AT APPROX 18,000 FT, THE CREW RECEIVED A BRAKE OVERHEAT WARNING MESSAGE ON EICAS WITH THE LT OB BRAKE INDICATOR GOING TO TWENTY AND FLUCTUATED ERRATICALLY. AFTER COMPLYING WITH THE QRH, ALL INDICATIONS RETURNED TO NORMAL. UPON LOWERING THE GEAR FOR FINAL APPROACH, THE OVERHEAT MESSAGE ACTIVATED AGAIN WITH THE LT OB MAIN BRAKE INDICATOR SHOWING RED AND AL OTHER SHOWING GREEN AND THE TEMP INDICATOR SHOWING ONE. EMERGENCY VEHICLES WERE REQUESTED AS PRECAUTION. AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE LT OB PROXIMITY SENSOR HARNESS ASSEMBLY. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: WARNING LIGHT — FALSE INDICATION (BRAKE OVERHEAT)

DURING DESCENT FROM SLC-SAT, AT APPROXIMATELY 18,000 FEET THE CREW RECEIVED A BRAKE OVERHEAT WARNING MESSAGE ON EICAS WITH THE LEFT OUTBOARD BRAKE INDICATOR GOING TO TWENTY AND FLUCTUATED ERRATICALLY. AFTER COMPLYING WITH THE QRH ALL INDICATIONS RETURNED TO NORMAL. UPON LOWERING THE GEAR FOR FINAL APPROACH, THE OVERHEAT MESSAGE ACTIVATED AGAIN WITH LEFT OUTBOARD MAIN BRAKE INDICATOR SHOWING RED AND ALL OTHERS SHOWING GREEN AND THE TEMP INDICATOR SHOWING ONE. EMERGENCY VEHICLES WERE REQUESTED AS A PRECAUTION. THE AIRCRAFT LANDED SAFELY IN SAT. MAINTENANCE DEFERRED THE EICAS BRAKE TEMP MONITORING INDICATION UNDER MEL NR 32-46-01, CAT B EXPIRING 7/13/2005. AIRCRAFT OK FOR SERVICE. (M)