N710EV

Part: NONE — DAMAGED · airframe 37,821 hrs · 27,092 cycles

PASSENGER DOOR F.S. 310, BETWEEN STRINGER 17 LH AND STRINGER 18LH, REQUIRE FURTHER EVALUATION DUE TO DAMAGE. (C-CHECK RO 3/10/2022) REPAIRED DAMAGED PAX DOOR CUT OUT ON FUSELAGE FWD,LWR CORNER AT FS310 FROM STGR 17L TO STGR18L PER REO 670-53-21-2206 REV -- DATED: 2021-12-30. PLEASE REFER TO CONTINUATION CARD FOR DISPOSITION AND CORRECTIVE ACTION.

Part: NONE — CORRODED · airframe 37,821 hrs · 27,092 cycles

DURING INSPECTION WAS FOUND CORROSION ON STRINGER 20L AT FS. 310.00 TO FS. 349.00 REQUIRES CLEANING AND EVALUATION. (C-CHECK RO 3/10/2022) REMOVED CORRODED STRINGER STGR20L FROM FUSELAGE STATION FS310-FS349 / INSTALLED WITH NEWSTRINGER STGR20L PER CRJ700 TASK SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01 PER APPLICABLE STEPS. / PLEASE REFER TO CONTINUATION CARD FOR DISPOSITION AND CORRECTIVE ACTION.NO DISCREPANCIES OR DEFECTS NOTED. / NOTE: PLEASE REFERENCE CAMP# 23937600 CONTINUATION CARD ITEM 11 FOR PRESSURIZATION CHECK. NO FURTHER ACTION REQUIRED AT THIS TIME

Part: EXTENSION — CORRODED · airframe 37,821 hrs · 27,092 cycles

FS 863 TO FS 954, LBL 9 FLOOR BEAM UNDER SEAT TRACK SEVERAL SPOTS OF CORROSION. (C-CHECK RO 3/10/2022) REMOVED CORRODED FLOOR BEAM SUPPORT AND REPLACED WITH NEW FLOOR BEAM SUPPORT, FILLERS AND CLIPS AT LBL9 FROM FS863 TO FS954 PER TASK CARD 51-900-1002-SKY AND CRJ 700 SRM 53-00-41-201-001-A01 / PLEASE REFER TO CONTINUATION CARD FOR DISPOSITION AND CORRECTIVE ACTION. NO FURTHER ACTION REQUIRED AT THIS TIME.

Part: FRAME — CORRODED · airframe 37,821 hrs · 27,092 cycles

DURING INSPECTION WAS FOUND CORROSION ON FRAME LOCATION FS 319.00 BETWEEN STGR 21L TO STGR 18L NEED TOBE EVALUATED. (C-CHECK RO 3/10/2022) REMOVED AND REPLACED CORRODED FRAME SECTION AT FS319 FROM SGTR18L TO SGTR20L PER TASK CARD 51-900-1002 SKY AND CRJ700 SRM 51-42-06-001-001-A01. PLEASE REFER TO CONTINUATION CARD FOR DISPOSITION AND CORRECTIVE ACTION. / NOTE. PLEASE REFERENCE CAMP# 23937600 CONTINUATION CARD ITEM 8 FOR PRESSURIZATION CHECK. NO FURTHER ACTION REQUIERE AT THIS TIME.

Part: NONE — CORRODED · airframe 37,821 hrs · 27,092 cycles

CORROSION ON STRINGER STRG20R BETWEEN FUSELAGE FS879 THRU FS893 (C-CHECK RO 3/10/2022) REMOVED CORRODED STGR20R FROM FS879-FS893 AND REPLACED WITH NEW STGR SECTION PER NHIRJ REO 670-53-51-241 REV. -- DATED:2021-12-27. PLEASE REFER TO CONTINUATION CARD FOR DISPOSITTION AND DETAILS OF CORRECTIVE ACTION. NO FURTHER ACTION ACTION REQUIRED AT THIS TIME.

Part: NONE — CORRODED · airframe 37,821 hrs · 27,092 cycles

INTERCOSTAL AT STRG20R FROM FS310 TO FS319, UNDER SERVICE DOOR, CORRODED AND OUT OF LIMITS, REF CAMP #23764037. REQUIRES TO BE REPLACED. (C-CHECK RO 3/10/2022) REMOVED CORRODED INTERCOSTAL AT STGR20R FROM FS310-FS319 AND REPLACED WITH NEW INTERCOSTAL PER CRJ700 SRM 51-40-11-001-001-A01, CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-25-06-001-001-01,& CRJ700 SRM 51-25-16-001-001-A01. NO FURTHER ACTION REQUIRED AT THIS TIME.

Part: NONE — CORRODED · airframe 37,821 hrs · 27,092 cycles

INTERCOSTAL ON STRG20R FROM FS319 TO FS349, UNDER SERVICE DOOR, CORRODED. FOUND OUT OF LIMITS ON CAMP#23764037, REQUIRES TO BE REPLACED. (C-CHECK RO 3/10/2022) REMOVED AND REPLACED CORRODED INTERCOSTAL ON STGR 20R AT FS 319.00 TO FS 349.00. REF. CRJ700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01. REFER TO CONTINUATION CARD FOR REPAIR DISPOSITION AND CORRECTIVE ACTIONS. NO FURTHER ACTION REQUIRED AT THIS TIME.

Part: NONE — CHAFED · airframe 37,821 hrs · 27,092 cycles

FS 975 - FS 981, STR 27 EXT SKIN DOUBLER CHAFED/GOUGED BY WING TO BODY FAIRINGS 196DL/DR SPLICE STIFFENER. (C-CHECK RO 3/10/2022) REMOVED GOUGED DOUBLER AND TOP DOUBLER AND REPLACED WITH NEW DOUBLER AND TOP DOUBLER PER TASK CARD 51-900-1002-SKY AND REO 670-53-00-677 REV-- DATED: 2021-12-09. AND REO 670-53-00-277 REV- DATED 2010-09-23 / PLEASE REFER TO CONTINUATION CARD FOR DISPOSITION AND CORRECTIVE ACTION. / NOTE; REFER TO CAMP# 23937050 STEP 8 FOR PRESSURIZATION CHECK. NO FURTHER ACTION REQUIRED AT THIS TIME.

Part: NONE — CORRODED · airframe 37,821 hrs · 27,092 cycles

CORROSION FOUND ON STRINGER STR19 BETWEEN FS333 AND FS349 UNDER SERVICE DOOR. (C-CHECK RO 3/10/2022) REMOVED AND REPLACED SGTR19R FROM FS333-FS349 PER CRJ700 SRM 51-42-06--01-001-A01. PLEASE REFER TO CONTINUATION CARD FOR DISPOSITION AND CORRECTIVE ACTION. NO FURTHER ACTION REQUIRED AT THIS TIME.

Part: NONE — CORRODED · airframe 37,821 hrs · 27,092 cycles

CORROSION AT FS310 TO FS349 & L/H STRINGER 21LH (C-CHECK RO 3/10/2022) REMOVED AND REPLACED CORRODED BACK UP SILL AT FS 310.00 TO FS 349.00 STGR 21L WITH NEW BACK UP SILL. REF. CRJ700 SRM 51-40-11-001-001-A01, SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, 51-25-06-001-001-A01AND SRM 51-25-16-001-001-A01. REFERENCE CONTINUATION CARD FOR REPAIR DISPOSITION AND CORRCTIVE ACTIONS. NO FURTHER ACTION REQUIRED AT THIS TIME.

Part: NONE — CRACKED · airframe 37,821 hrs · 27,092 cycles

ABOVE FLOOR FS333.00 FRAME CRACKED BEBOW STGR 1RH (C-CHECK RO 3/10/2022) REMOVED AND REPLACED CRACKED FRAME AT FS333 FROM STGR0 TO STGR9R WITH NEW FRAME SECTION PER CRJ700 SRM 51-42-06-001-001-A01. PLEASE REFER TO CONTINUATION CARD FOR DISPOSITION AND DETAILS OF CORRECTIVE ACTIONS. NO FURTHER ACTION REQUIRED AT THIS TIME.

Part: NUT — DENTED · airframe 37,821 hrs · 27,092 cycles

L/H SIDE FUSELAGE FS533, BETWEEN STR16L & 17L DENT; MEASURE AT 7"X 4" ; .012" IN DEPTH; NO ALLOWABLE DAMAGE IN AREA. (C-CHECK RO 3/10/2022) PERFORMED REPAIR ON DENTED SKIN AT FS535, SGTR16L TO SGTR18L PER REO 670-53-31-761 REV. -- DATED: 2021-12-28. PLEASE REFER TO CONTINUATION CARD FOR DISPOSITION AND CORRECTIVE ACTION. NO FURTHER ACTION REQUIRED AT THIS TIME.

Part: NONE — DENTED · airframe 37,821 hrs · 27,092 cycles

L/H SIDE FUSELAGE FS453, BETWEEN STR14L & 15L DENT; MEASURE AT 3"X 4" .010" DEPTH; NO ALLOWABLE DAMAGE IN AREA. (C-CHECK RO 3/10/2022) PERFORMED REPAIR ON FRAME AT FS453 BETWEEN STGR14L & 15L PER MHIRJ REO 670-53-21-2198 REV. -- DATED: 2021-12-21 AND REO 670-51-00-085 REV. -A DATE: 2017-08-23. REFER TO CONTINUATION CARD (2) FOR DISPOSITION AND CORRECTIVE ACTION. NO FURTHER ACTION REQUIRED AT THIS TIME.

Part: NONE — CRACKED · airframe 37,821 hrs · 27,092 cycles

FORWARD FUSELAGE LEFT WINDSHIELD SUPPORT POST BETWEEN PILOT'S SIDE WINDSLIELD AND FORWARD WINDSHIELD IS CRACKED. (C-CHECK RO 3/10/2022) REMOVED CRACKED PILOT SIDE WINDOW SUPPORT POST AND REPLACED WITH NEW SUPPORT POST. REF. CRJ700 SRM 53-11-35, 51-40-11 AND 51-42-21. REFERENCE CONTINUATION CARD FOR REPAIR DISPOSITION AND CORRECTIVE ACTIONS.

Part: NONE — CORRODED · airframe 37,821 hrs · 27,092 cycles

FS549 AND STGR18L FRAME CORROSION /BARE METAL (C-CHECK RO 3/10/2022) REMOVED CORRODED FRAME SECTOR AT FS549 FROM STGR9L TO STGR18L AND REPLACED WITH NEW FRAME SECTOR PER TASK CARD 51-900-1002-SKY, CRJ700 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01. / PLEASE REFER TO CONTINUATION CARD FOR DISPOSITION AND DETAILS OF CORRECTIVE ACTION. / NOTE: PLEASE REFERENCE CAMP# 23937600 CONTINUATION CARD ITEM 8 FOR PRESSURIZATION CHECK.NO FURTHER ACTION REQUIRED AT THIS TIME.

Part: NONE — CORRODED · airframe 37,821 hrs · 27,092 cycles

FS565 AND STGR18L FRAME CORROSION /BARE METAL (C-CHECK RO 3/10/2022) REMOVED AND REPLACED CORRODED FRAME AT FS565, STGR18L TO STGR8L REF CRJ700 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01. PLEASE REFER TO CONTINUATION CARD FOR DISPOSITION AND CORRECTIVE ACTION. NO FURTHER ACTION REQUIRED AT THIS TIME.

Part: NONE — WORN · airframe 37,821 hrs · 27,092 cycles

RIGHT HAND SLAT NO.# 3 AT SLAT SATATION SS337.66 INBOARD CONNER RUBBING ON TOP OF THE WING LEADING EDGED AREA (C-CHECK RO 3/10/2022) PERFORMED REPAIR TO RIGHT HAND #3 SLAT AT SS337.66 INBOARD CORNER PER TASK CARD 51-900-1002- SKY AND MHIRJ REO 670-57-41-481 REV. -- DATED:2021-12-24. PLEASE REFER TO CONTINUATION CARD FOR DISPOSITION AND DETAILS OF CORRECTIVE ACTIONS. NO FURTHER ACTION REQUIRED AT HIS TIME.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 37,728 hrs · 26,706 cycles

DAMAGED FOUND AT STR 7L BETWEED FS 1144-1162. BLENDED DAMAGE TO STR 7L BETWEEN FS 1144-1162. PERFORMED NDI NO DEFECTS FOUND. INSTALLED REPAIR AND RETURNED TO ORIGINAL FINISH IAW STS EA 32-2018-162.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 37,728 hrs · 26,706 cycles

FOUND DAMAGE AT STR 7R BETWEEN FS 1144-1162. BLENDED DAMAGE TO 7R FS 1144-1162. PERFORMED NDI NO DEFECTS FOUND. INSTALLED REPAIR AND RESTORED TO ORIGINL FINISH IAW REO 670-53-61-292.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 37,728 hrs · 26,706 cycles

TYS-DAMAGED FOUND AT STRINGER 6L, BETWEEN FR 1144.00 AND FR 1162. MAINTENANCE BLENDED THE DAMAGED TO STR 6L AT STA 1144.00 TO 1162.00. PERFORMED A NDT INSPECTION AND NO DEFECTS FOUND. INSTALLED THE REPAIR, RETURNED TO ORIGINAL FINISH IAW STS EA 32-2018-161.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 36,095 hrs · 25,738 cycles

DURING MX INSPECTION, THE EMERGENCY CEILING LIGHT AT ROW 9 WAS FOUND INOPERATIVE. MX CRIMPED NEW PINS IN THE CONNECTOR. OPS CHECKED GOOD.

Part: STRAP — DAMAGED (LT WING) · airframe 35,873 hrs · 25,569 cycles

REF: CO# EJA150D JOB# EJA050D OP# 49: STRAP LANDING FIXED LEADING EDGE PN CC670-12106-3 REQUIRES FABRICATION DUE TO PART AVAILABILITY.C/A: FABRICATED STRAP LANDING FIXED LEADING EDGE PN CC670-12106-3 IAW BOMBARDIER SNIEO CC670-12106-S01 AND COMPLIED WITH EXPRESS JET EC/TC CC670-12106-S01..

Part: RIB — DAMAGED (LT WING) · airframe 35,873 hrs · 25,569 cycles

REF: CO# EJA150D JOB# EJA050D OP# 14: LEFT WING STATION 15.5 RIB IS DAMAGED. C/A: REMOVED AND REPLACED LEFT WING STATION 15.5 RIB IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-13-001-001-A01, AND 51-42-06-001-001-A01.

Part: STRAP — DAMAGED (LT WING) · airframe 35,873 hrs · 25,569 cycles

REF: CO# EJA150D JOB# EJA050D OP# 51: STRAP LANDING FIXED LEADING EDGE PN CC670-12107-3 REQUIRES FABRICATION DUE TO PART AVAILABILITY.C/A: FABRICATED STRAP LANDING FIXED LEADING EDGE PN CC670-12107-3 IAW BOMBARDIER SNIEO CC670-12107-S01 AND COMPLIED WITH EXPRESS JET EC/TC CC670-12107-S01..

Part: SMOKE DETECTOR — FAILED (CARGO BAY) · airframe 34,352 hrs · 24,424 cycles

FIRE SYS FAULT STATUS MSG. REMOVED AND REPLACED FWD CARGO SMOKE DET 2 (A227 ) IAW AMM 26-17-01, IPC REF 26-17-01 ITEM 5, OPS CHECK GOOD DEFER CLEARED, PLACARD REMOVED.

Part: FLOOR SUPPORT — CORRODED (BS 547) · corrosion level 2 · airframe 33,962 hrs · 24,135 cycles

LEFT FLOOR SUPPORT CORRODED AT BS 547. REPAIRED IAW EC/TC REO 970-53-00-390. AIRCRAFT APPROVED FOR RETURN TO SERVICE.

Part: DOUBLER — CORRODED (BS 295-310) · corrosion level 2 · airframe 33,962 hrs · 24,135 cycles

TCAS ANTENNA DOUBLER CORRODED AT STRINGER 27L BETWEEN BS 295-310. REMOVED AND REPLACED DOUBLER IAW SRM 51-40-001-001-A01 AND 51-42-06-001-001-A01. AIRCRAFT APPROVED FOR RETURN TO SERVICE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,962 hrs · 24,135 cycles

RT SEAT RAIL CORRODED FS 677-708. REMOVED RAIL. C/W EC/TC REO 670-53-00-343. INSTALLED NEW RAIL. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (BS 351) · corrosion level 2 · airframe 33,962 hrs · 24,135 cycles

RIGHT FLOOR SUPPORT CORRODED BS 351 RBL 45. REPAIRED IAW EC/TC REO 670-53-00-390. AIRCRAFT APPROVED FOR RETURN TO SERVICE.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 33,962 hrs · 24,135 cycles

RIGHT INBD FLAP DENTED. REPAIRED IAW SRM 57-52-01-201-001-A01 REPAIR IV. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 33,962 hrs · 24,135 cycles

NUT PLATE CHANNEL CORRODED BETWEEN 193AB AND 194AB. COMPLIED WITH EC/TC EA 32-2016-202 AND EA 32-2016-202. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: ANGLE — CORRODED (BS 280 FLOORBEAM) · corrosion level 2 · airframe 33,962 hrs · 24,135 cycles

AVIONICS BAY FLOORBEAM ANGLE ON AFT SIDE OF BS 280 IS CORRODED. REMOVED AND REPLACED THE ANGLE IAW SRM 51-42-06-001-001-A01 AND DRAWING CC670-34010. AIRCRAFT APPROVED FOR RETURN TO SERVICE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,962 hrs · 24,135 cycles

LT SEAT RAIL CORRODED FS 677-708. REMOVED RAIL AND C/W EC/TC REO 670-53-00-343. INSTALLED NEW RAIL. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 33,962 hrs · 24,135 cycles

AFT CARGO FLOOR SILL CORRODED. REMOVED AND REPLACED AFT CARGO FLOOR SILL PER SRM 700 51-42-06-001-001, 51-42-13-001-001. P/N MM670-35655-003 DRAWING MM670-35655. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CORRODED (BS 333) · corrosion level 2 · airframe 33,962 hrs · 24,135 cycles

FRAME CORRODED AT BS 333 STRINGER 26-27R. REPAIRED THE FRAME IAW EC/TC 25-2016-247. AIRCRAFT APPROVED FOR RETURN TO SERVICE.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 33,962 hrs · 24,135 cycles

RT FLOOR SILL CORRODED FS 1000-1080. C/W EC/TC REO 970-53-00-390 AND REO 670 53-00-390. A/C APPROVED FOR RETURN TO SERVICE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,962 hrs · 24,135 cycles

LT SEAT RAIL CORRODED FS 785-863. REMOVED RAIL. C/W EC/TC REO 670-53-00-343. INSTALLED NEW RAIL. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,962 hrs · 24,135 cycles

FLOORBEAM CORRODED FS 1000-1031. COMPLIED WITH EC/TC 700-53-0356 AND REO 670-53-029.

Part: DOOR FRAME — CORRODED (BS 280) · corrosion level 2 · airframe 33,962 hrs · 24,135 cycles

LEFT FLIGHT DECK DOOR POST CORRODED AT BOTTOM, BS 280 LBL 9. REPAIRED IAW EC/TC EA 25-2016-248. AIRCRAFT APPROVED FOR RETURN TO SERVICE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,962 hrs · 24,135 cycles

LT SEAT RAIL CORRODED FS 708-761. REMOVED RAIL. COMPLIED WITH EC/TC REO 670-53-00-343. INSTALLED NEW RAIL. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,962 hrs · 24,135 cycles

RT SEAT RAIL CORRODED FS 785-863. REMOVED RAIL. COMPLIED WITH EC/TC REO 670-53-00-343. INSTALLED NEW RAIL. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (BS 280) · corrosion level 2 · airframe 33,962 hrs · 24,135 cycles

BUTTSTRAP CORRODED FS 280 BETWEEN STRINGERS 26-27L. REPAIRED THE BUTTSTRAP IAW EA 12-2016-146 AND EC/TC EA 12-2016-146. AIRCRAFT APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,962 hrs · 24,135 cycles

FLOORBEAM CORRODED FS 797-813. COMPLIED WITH EC/TC REO 670-53-41-289 AND REO 670-53-41-289. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,962 hrs · 24,135 cycles

RT SEAT RAIL CORRODED FS 581-677. REMOVED RAIL. C/W EC/TC REO 670-53-343. INSTALLED NEW RAIL. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: HEAT SHIELD — DAMAGED (RIGHT) · airframe 33,962 hrs · 24,135 cycles

HOLE WORN THROUGH RT ENGINE LOWER CORE COWL INNER HEAT SHIELD. REPAIRED HOLE TO LOWER CORE COWL IAW REO 670-54-23-959 AND ECTC REO 670-54-23-959. AIRCRAFT APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (BS 549-638) · corrosion level 2 · airframe 33,962 hrs · 24,135 cycles

LBL 9 FLOOR SUPPORT CORRODED AT BS 549 - 638. REPAIRED IAW EC/TC EO 700-53-0358 AND EO 700-53-0359. AIRCRAFT APPROVED FOR RETURN TO SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,859 hrs · 24,046 cycles

DURING MX INSPECTION, THE NR 1 EMERGENCY FLOOD LIGHT WOULD NOT ILLUMINATE. THE BATTERY CHARGER WAS REMOVED AND REPLACED AND OPS CHECKED GOOD. RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (AFT CARGO) · corrosion level 3 · airframe 33,834 hrs · 24,025 cycles

DURING C CHECK INSPECTION, AFT CARGO FLOOR SUPPORT HAS CORROSION. R & R THE FLOOR SUPPORT IAW SRM 51-42-06-001-001-A01. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CHANNEL — CORRODED (BS 677-830) · corrosion level 2 · airframe 33,834 hrs · 24,025 cycles

DURING C CHECK INSPECTION, ENTIRE LENGTH OF NUT PLATE CHANNEL FRAME FOR FAIRINGS 193AB AND 194AB HAS CORROSION. MX COMPLIED WITH EA 32-2016-202. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (BS 549-638) · corrosion level 2 · airframe 33,834 hrs · 24,025 cycles

DURING C CHECK INSPECTION, FLOOR SUPPORT CAP BS 549 - 638 LBL 9 CORRODED. COMPLIED WITH EC/TC EO 700-53-0358& EO 700-53-0359. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOUBLER — CORRODED (BS 295-310) · corrosion level 3 · airframe 33,834 hrs · 24,025 cycles

DURING C CHECK INSPECTION, ANTENNA DOUBLER HAS CORROSION AT STRINGER 27 BETWEEN BS 295 - 310. R & R THE TCAS DOUBLER IAW SRM 51-40-001-001-A01. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 33,834 hrs · 24,025 cycles

DURING C CHECK, FOUND THE SEAT TRACK CORRODED LBL 9 BS 581 - 693. REPAIRED IAW EC/TC REO 670-53-00-343 REV K & 670-53-00-343 REV M.

Part: SEAT TRACK — CORRODED (BS 481-485) · airframe 33,834 hrs · 24,025 cycles

SEAT TRACK CORRODED. COMPLIED WITH ECTC REO 670-53-00-343 REV K AND REO 670-53-00-343 REV M.

Part: SEAT TRACK — CORRODED (BS 677-830) · airframe 33,834 hrs · 24,025 cycles

DURING C CHECK, FOUND SEAT TRACK BS 677 - 830 RBL 9 CORRODED. REPAIRED IAW EC/TC REO 670-53-00-343.

Part: STRIKER — CORRODED (SERVICE DOOR) · airframe 33,834 hrs · 24,025 cycles

DURING C CHECK, FOUND SERVICE DOOR SILL CORRODED. R & R THE DOOR SILL IAW SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01, 51-42-21-001-001-A01, & DWG SH670-31412.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 33,834 hrs · 242,025 cycles

DURING C CHECK, FOUND THE SEAT TRACK CORRODED LBL 9 BS 485 - 581. REPAIRED IAW EC/TC REO 670-53-00-343 REV K. & REO 670-53-00-343 REV M.

Part: SEAT TRACK — CORRODED (BS 581-693) · airframe 33,834 hrs · 24,025 cycles

SEAT TRACK HAS CORROSION. COMPLIED WITH ECTC REO 670-53-00-343 REV K AND REO 670-53-00-343 REV M.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 33,834 hrs · 24,025 cycles

SEAT TRACK HAS CORROSION. COMPLIED WITH ECTC REO 670-53-00-343 REV K AND REO 670-53-00-343 REV M.

Part: SEAT TRACK — CORRODED (BS 677-830) · airframe 33,834 hrs · 24,025 cycles

DURING C CHECK, FOUND THE SEAT TRACK CORRODED LBL 9 BS 677 - 830. REPAIRED IAW EC/TC REO 670-53-00-343 REV K & 670-53-00-343 REV M.

Part: SEAT TRACK — CORRODED (BS 349-477) · airframe 33,834 hrs · 24,025 cycles

SEAT TRACK CORRODED. COMPLIED WITH ECTC REO 670-53-00-343 REV K AND REO 670-53-00-343 REV M.

Part: SEAT TRACK — CORRODED (BS 349-477) · airframe 33,834 hrs · 24,025 cycles

DURING C CHECK, FOUND THE SEAT TRACK CORRODED RBL 9 BS 349-477. REPAIRED IAW EC/TC REO 670-53-00-343 REV K & 670-53-00-343 REV M.

Part: SEAT TRACK — CORRODED (BS 581-693) · airframe 33,834 hrs · 24,025 cycles

DURING C CHECK, FOUND SEAT TRACK CORRODED LBL 9 BS 581 - 693. REPAIRED IAW EC/TC REO 670-53-00-343 REV K & 670-53-00-343 REV M.

Part: SEAT TRACK — CORRODED (BS 581-693) · airframe 33,834 hrs · 24,025 cycles

DURING C CHECK, FOUND SEAT TRACK RBL 9 BS 581 - 693 CORRODED. REPAIRED IAW EC/TC REO 670-53-00-343.

Part: FRAME — CORRODED (BS 349) · airframe 33,834 hrs · 24,025 cycles

DURING C CHECK, FOUND AFT SIDE OF FRAME BS 349 CORRODED BETWEEN STRINGERS 26 & 27R. REPAIRED IAW EC/TC EA45-2016-136.

Part: DOOR SILL — CORRODED (SERVICE DOOR) · airframe 33,834 hrs · 24,025 cycles

SERVICE DOOR SILL IS CORRODED. REMOVED AND REPLACE THE DOOR SILL IAW SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01, 51-42-21-001-001-A01 AND DRAWING SH670-31412-1.

Part: FLOOR SUPPORT — CORRODED (BS 677-830) · airframe 33,834 hrs · 24,025 cycles

DURING C CHECK, FOUND FLOOR SUPPORT AT BS 677 - 830 RBL 9 CORRODED. REPAIRED IAW EC/TC REO 670-53-41-292.

Part: FLOOR SUPPORT — CORRODED (BS 581-589) · airframe 33,834 hrs · 24,025 cycles

DURING C CHECK, FOUND FLOOR SUPPORT BS 581 - 589, RBL 9 CORRODED. REPAIRED IAW EC/TC REO 670-53-31-382.

Part: FLOOR SUPPORT — CORRODED (BS 469-549) · airframe 33,834 hrs · 24,025 cycles

DURING C CHECK, FOUND FLOOR SUPPORT BS 469 - 549 RBL 9 CORRODED. REPAIRED IAW EC/TC REO 670-53-31-382.

Part: FLOOR SUPPORT — CORRODED (BS 1031-1047) · airframe 33,834 hrs · 24,025 cycles

DURING C CHECK FOUND FLOOR SUPPORT BS 1031-1047 RBL 9 CORRODED. REPAIRED IAW EC/TC REO 670-53-61-1269.

Part: INTERCOSTAL — CORRODED (BS 364) · airframe 33,834 hrs · 24,025 cycles

DURING C CHECK, FOUND CORROSION ON LT INTERCOSTAL AT STR 27 & BS 364. R & R THE INTERCOSTAL IAW SRM 51-40-11-001-001-A01 & DRAWING SH670-32075.

Part: BRACKET — CORRODED (ZONE 100) · airframe 33,834 hrs · 24,025 cycles

MAC - DURING C CHECK FOUND PAX DOOR SUPPORT WHEEL PULLEY BRACKET CRACKED. MTC R & R BRACKET IAW SRM 51-42-06-001-001-A01 AND DRAWING CC670-38625.

Part: FLOOR SUPPORT — CORRODED (BS 1000-1031) · corrosion level 2 · airframe 33,834 hrs · 24,025 cycles

DURING C CHECK INSPECTION, THE FLOOR SUPPORT AT BS 1000 - 1031 LBL 27 IS CORRODED. REPAIRED IAW EC/TC EO 700-53-0356 AND REO 670-53-00-029. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (BS 797-813) · corrosion level 2 · airframe 33,834 hrs · 24,025 cycles

MCN DURING C CHECK INSPECTION, FLOOR SUPPORT BS 797 - 813, LBL 9 CORRODED. COMPLIED WITH EC/TC REO 670-53-41-289. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CORRODED (BS 333) · corrosion level 3 · airframe 33,834 hrs · 24,025 cycles

DURING C CHECK INSPECTION, FRAME AT BS 333 IS CORRODED. REMOVED AND REPLACED THE FRAME IAW EA 25-2016-247E. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (BS 280) · airframe 33,834 hrs · 24,025 cycles

DURING C CHECK INSPECTION, BS 280 BUTT-STRAP IS CORRODED BETWEEN STRINGERS 26 AND 27L. REMOVED AND REPLACED THE BUTT STRAP IAW EA 12-2016-146 AND EC/TC 12-2016-146. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SEAT TRACK — CORRODED (BS 785-863) · airframe 33,834 hrs · 24,025 cycles

DURING C CHECK INSPECTION, THE RT SEAT TRACK FS 785 - 863 HAS CORROSION. REMOVED THE SEAT TRACK AND COMPLIED WITH EC/TC REO 670-53-00-343 AND INSTALLED A NEW TRACK. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ANGLE — CORRODED (BS 280) · airframe 33,834 hrs · 24,025 cycles

DURING C CHECK INSPECTION, THE AVIONICS BAY FLOOR PANEL 141ALF SUPPORT ANGLE ON AFT SIDE OF BS 280 FRAME WAS CORRODED. MX REMOVED ANGLE AND INSTALLED NEW ANGLE IAW SRM 51-42-06-001-001-A01 AND DWG CC670-34010. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (BS 1000-1080) · airframe 33,834 hrs · 24,025 cycles

DURING C CHECK INSPECTION, THE RT FLOOR SUPPORT BS 1000-1080 HAS CORROSION. MX REMOVED AND REPLACED THE FLOOR SUPPORT. COMPLIED WITH EC/TC REO 670-53-00-390. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: POST — CORRODED (FLIGHT DECK) · airframe 33,834 hrs · 24,025 cycles

DURING C CHECK INSPECTION, THE LT FLIGHT DECK DOOR POST CORRODED AT BOTTOM. MX COMPLIED WITH EC/TC EA 25-2016-248. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (BS 351) · airframe 33,834 hrs · 24,025 cycles

DURING C CHECK INSPECTION, THE RT FLOOR SUPPORT HAS CORROSION. MX REMOVED THE FLOOR SUPPORT AND COMPLIED WITH EC/TC REO 670-53-00-390 AND REO 670-53-00-390 AND INSTALLED NEW. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (BS 547) · airframe 33,834 hrs · 24,025 cycles

DURING C CHECK INSPECTION, THE LT FLOOR SUPPORT HAS CORROSION. MX REMOVED AND REPLACED THE FLOOR SUPPORT. COMPLIED WITH EC/TC REO 670-53-00-390. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 33,834 hrs · 24,025 cycles

MCN DURING C CHECK INSPECTION, THE RT INBD FLAP IS DENTED. REPAIRED IAW SRM 57-52-01-201-001-A01 REPAIR IV.THIS IS A MAJOR REPAIR. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (BS 1031) · airframe 33,834 hrs · 24,025 cycles

DURING C CHECK, FOUND THE FLOORBEAM CORRODED BS 1031 LBL 9. REPAIRED IAW EO 700-53-0357.

Part: SEAT TRACK — CORRODED (BS 677-708) · airframe 33,834 hrs · 24,025 cycles

MCN DURING C CHECK INSPECTION, THE RT SEAT TRACK BS 677 - 708 FOUND CORRODED. MX REMOVED AND REPLACED THE SEAT TRACK IAW EC/TC REO 670-53-00-343. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SEAT TRACK — CORRODED (BS 677-708) · airframe 33,834 hrs · 24,025 cycles

THE LT SIDE SEAT TRACK BS 677 - 708 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW EC/TC REO 670-53-00-343. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SEAT TRACK — CORRODED (BS 581-677) · airframe 33,834 hrs · 24,025 cycles

DURING C CHECK INSPECTION, THE RT SEAT TRACK BS 581 - 677 CORRODED. MX REMOVED THE SEAT TRACK IAW EC/TC REO 670-53-00-343. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CHAFED (RT WING LE) · airframe 33,834 hrs · 24,025 cycles

RIGHT WING L/E PANEL 632AR HAS A DEEP CHAFE ON UPPER SIDE. REPAIRED THE PANEL IAW EA 20-2016-290 AND ECTC REO EA 20-2016-290.

Part: SEAT TRACK — CORRODED (BS 785-863) · airframe 33,834 hrs · 24,025 cycles

DURING C CHECK INSPECTION, THE LT SEAT TRACK BS 785 - 863 CORRODED. MX REMOVED AND REPLACED THE SEAT TRACK IAW EC/TC REO 670-53-00-343 AND. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SEAT TRACK — CORRODED (BS 708-761) · airframe 33,834 hrs · 24,025 cycles

DURING C CHECK INSPECTION, THE LT SEAT TRACK BS 708 - 761 CORRODED. MX REMOVED AND REPLACED THE SEAT TRACK IAW EC/TC REO 670-53-00-343 AND. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: HEAT SHIELD — CHAFED (RT NACELLE) · airframe 33,834 hrs · 24,025 cycles

THE RIGHT ENGINE LOWER CORE COWL INNER HEAT SHIELD WAS FOUND WITH A HOLE WORN THROUGH. MX COMPLIED WITH REPAIR OF FWD COWL IAW REO 670-54-23-959 AND ECTC REO670-54-23-959. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CORRODED (BS 364) · airframe 33,834 hrs · 24,025 cycles

DURING C CHECK FOUND THE FRAME CORRODED BS 364 BETWEEN STRINGER 26R. REPAIRED IAW EC/TC REO 670-53-21-687 & GREO 670-53-21-687.

Part: PIN — LACK OF LUBE (PAX DOOR) · airframe 30,354 hrs · 21,206 cycles

PAX DOOR DIFFICULT TO OPEN. CLEANED AND LUBED PAX DOOR LOCKING PINS IAW AMM 12-20-52. OPS CHECK GOOD, NO FURTHER DEFECT NOTED.

Part: FITTING — GOUGED (RT WING) · airframe 29,629 hrs · 20,651 cycles

RT REAR SPAR LINK REAR TOP FITTING GOUGED. REMOVED UT THICKNESS FROM THE FWD OF THE AFT LUG ON THE UPPER FUSELAGE FRAME, RT SIDE, FS797 TO A DIMENSION OF 1.6"L X .6" W IAW SRM 51-12-00-001-001-A01. ROTO-PEENED REWORKED AREA IAW SRM 51-24-11-001-001-A01. RESTORED FINISH IN REWORKED AREA IAW SRM 51-25-00-001-001-A01.

Part: ATTACH BRACKET — CRACKED · airframe 29,629 hrs · 20,651 cycles

AFTER REMOVAL OF STRINGER 7R, BS 1144-1162, FOUND ATTACHED BRACKET CRACKED. R & R BRACKET IAW SRM 51-42-06-001-001-A01.

Part: INTERCOSTAL — CHAFED (BS 1144-1162) · airframe 29,607 hrs · 20,635 cycles

CHAFE DAMAGE ON STRINGER 9R INTERCOSTAL BETWEEN BS 1144 - 1162. REPAIRED IAW REO 670-53-61-292 REV C, 2014-06-04. MAJOR REPAIR.

Part: FLOORBEAM — CRACKED (COCKPIT) · airframe 29,608 hrs · 20,636 cycles

RIGHT COCKPIT FLOORBEAM IS CRACKED AND FOUND WITHIN .600 AREA IAW SB 670 BA-53-041. COMPLIED WITH REO 670-53-11-977, REV A. MAJOR REPAIR.

Part: FLOORBEAM — CRACKED (COCKPIT) · airframe 29,608 hrs · 20,636 cycles

LEFT COCKPIT FLOORBEAM IS CRACKED AND FOUND WITHIN .600 AREA IAW SB670BA-53-041. COMPLIED WITH REO 670-53-11-977, REV A. MAJOR REPAIR.

Part: ANGLE — CRACKED (BS 280) · airframe 29,607 hrs · 20,635 cycles

ANGLE AT BS 280 IS CRACKED. REMOVED AND REPLACED THE ANGLE IAW SRM 51-40-11-001-001-A01 AND SRM 51-12-13-001-001-A01.

Part: SUPPORT ANGLE — CRACKED (BS 280 BULKHEAD) · airframe 29,608 hrs · 20,636 cycles

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

Part: ANGLE — CORRODED (PAX DOOR) · airframe 29,607 hrs · 20,635 cycles

PAX DOOR LOWER MID CAP ANGLE IS CORRODED AT INBD AND OTBD SIDE. REMOVED AND REPLACED THE CAP ANGLE IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.

Part: SUPPORT ANGLE — CRACKED (BS 280 BULKHEAD) · airframe 29,607 hrs · 20,635 cycles

BULKHEAD SUPPORT ANGLE CRACKED AT LBL 26, BS 280. REMOVED AND REPLACED THE BULKHEAD SUPPORT ANGLE IAW SRM 51-42-06-001-001-A01, AND SRM 51-42-06-001-001-A01. MAJOR REPAIR.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 29,608 hrs · 20,636 cycles

LT COCKPIT FLOORBEAM ANGLE CRACKED AT BS 280. REMOVED LT COCKPIT FLOOR SUPPORT ANGLE IAW SRM 51-42-06-001-001-A01. INSTALLED LT COCKPIT FLOOR SUPPORT ANGLE. COMPLIED WITH REO 670-53-11-977. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702.

Part: ANGLE — CRACKED (BS 280 FLOORBEAM) · airframe 29,608 hrs · 20,636 cycles

RT COCKPIT FLOOR SUPPORT ANGLE CRACKED AT BS 280. REMOVED RT COCKPIT FLOOR SUPPORT ANGLE IAW SRM 51-42-06-001-001-A01. INSTALLED RT COCKPIT FLOOR SUPPORT ANGLE. COMPLIED WITH REO 670-53-11-977. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 29,608 hrs · 20,636 cycles

PAX DOOR ACCESS HOLE 832BR INTERCOSTAL CRACKED. REMOVED PAX DOOR INTERCOSTAL IAW SRM 51-42-06-001-001-A01. LOCATED AND DRILLED FASTENERS HOLES IN NEW INTERCOSTAL IAW SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01. RECEIVED AND COMPLIED EO 25-2014-298 10/06/14 WITH SEC I 1-2 OF 25-2012-298. INSTALLED INTERCOSTAL IAW SRM 51-42-13-001-001-A01.

Part: DOUBLER — CHAFED (BS 977) · airframe 29,629 hrs · 20,651 cycles

REPAIR AT BS 977 STRINGER 27 IS CHAFED. REMOVED AND REPLACED THE REPAIR DOUBLER IAW SRM 51-42-20-001-001-A01 AND REO 670-53-00-922, REV-10-03-14.

Part: DRAG ANGLE — CORRODED (PAX DOOR) · airframe 29,608 hrs · 20,636 cycles

CRACK ON PAX DOOR AFT DRAG ANGLE. REMOVED PAX DOOR AFT DRAG ANGLE IAW SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01. LOCATED DRILLED AND INSTALLED NEW DRAG ANGLE IAW SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01. MAJOR REPAIR.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 29,607 hrs · 20,635 cycles

PAX DOOR UPPER MID CAP ANGLE IS CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00-101-001. REMOVED AND REPLACED THE CAP ANGLE IAW SRM 51-42-06-001-001-A01, 51-41-02-001-001-A01, AND 51-40-11-001-001-A01.

Part: CHANNEL — CORRODED (BS 280) · airframe 29,608 hrs · 20,636 cycles

J CHANNEL AT BS 280 CORRODED. J CHANNEL REPLACED IAW SB 670BA-53-041.

Part: STRINGER — CRACKED (BS 280) · airframe 29,608 hrs · 20,636 cycles

STRINGER 3L HAS A CRACK AFT OF FS 280, BULKHEAD. COMPLIED EC/TC SB670BA-53-040 01, REV A. COMPLIED WITH REO 670-53-21-493, REV C.

Part: FRAME — CORRODED (BS 319) · airframe 29,607 hrs · 20,635 cycles

BS 319.7 AT STRINGER 27 IS CORRODED IN AVIONICS BAY. BLENDED CORROSION IAW SRM 51-21-06-001-001-A01. MAJOR REPAIR.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 29,607 hrs · 20,635 cycles

PAX DOOR UPPER AFT CAP ANGLE IS CORRODED. REMOVED AND REPLACED THE CAP ANGLE IAW SRM 51-42-06-001-001-A01, SRM 51-40-11-001-001-A01.

Part: STRUCTURE — CHAFED (PAX DOOR) · airframe 29,629 hrs · 20,651 cycles

PAX DOOR FWD OUTER CORNER CHAFED. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. BLENDED CHAFED AREA, FWD OUTER CORNER, OF PAX DOOR IAW SRM 52-11-01-101-001-A01 AND 52-00-01-101-001-A01 AND ASA 51-12-00, REV A.

Part: HOUSING — GOUGED (CARGO DOOR) · airframe 29,629 hrs · 20,651 cycles

AFT CARGO DOOR HANDLE HOUSING GOUGED FROM HANDLE ALIGNMENT PIN, UPPER CORNER. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. RECEIVED AND COMPLIED WITH ECTC REO 670-52-31-031, REV OF NOV 07. BLENDED DAMAGE ON AFT CARGO DOOR HANDLE HOUSING IAW REO 670-52-31-031.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 29,608 hrs · 20,636 cycles

FS 280, LT BULKHEAD WEB IS CORRODED. DAMAGE EXCEEDS ALLOWABLE LIMITS IAW SRM 53-00-00-101-001-A01. REPAIRED IAW REO 670-53-11-594-01. RECEIVED AND COMPLIED WITH EC/TC REO 670-53-11-594 AND GREO 670-53-11-594 REV. MAJOR REPAIR.

Part: FRAME — CORRODED (BS 595) · airframe 29,608 hrs · 20,636 cycles

BS 595 FRAME IS CORRODED AT STRINGER 27 IN AVIONICS BAY. REMOVED CORROSION FROM FRAME IAW SRM 51-21-06-001-001-A01.

Part: DOOR SILL — CORRODED (BS 649) · airframe 29,608 hrs · 20,636 cycles

RBL 36 AT FS 649.0 AT SERVICE DOOR IS CORRODED ON DOOR SILL THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. DAMAGE IS FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-390. BLENDED CORROSION IAW SRM 51-21-06-001-001-A01.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 29,608 hrs · 20,636 cycles

RT FS 280 BULKHEAD WEB IS CORRODED. DAMAGE EXCEEDS ALLOWABLE LIMITS IAW SRM 53-00-00-101-001-A01 REPAIR IAW REO 670-53-11-594-01. RECEIVED AND COMPLIED WITH EC/TC REO 670-53-11-594 01 AND GREO 670-53-11-594, REV-. MAJOR REPAIR.

Part: FITTING — CRACKED (DOOR HAND RAIL) · airframe 29,629 hrs · 20,651 cycles

PAX DOOR FWD HAND RAIL STOP FITTING CHAFED AND GROMMET HOLE CRACKED. REMOVE CRACKED STOP FITTING IAW SRM 51-42-21-001-001-A01. LOCATED FASTENER HOLES IN NEW FITTING AND DRILLED TO SIDE IAW SRM 51-42-01-001-001. INSTALLED NEW FITTING IAW SRM 51-42-06-001-001.

Part: FRAME — CORRODED (BS 310) · airframe 29,607 hrs · 20,635 cycles

BS 310 AT STRINGER 27 IS CORRODED IN AVIONICS BAY. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 29,607 hrs · 20,635 cycles

BS 280 FLOORBEAM IS CORRODED. REPLACED ON S/B 670BA-53-041.

Part: FRAME — CORRODED (BS 333) · airframe 29,607 hrs · 20,635 cycles

BS 333 AT STRINGER 27 IS FWD AVIONICS BAY IS CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. MAJOR REPAIR.

Part: RUB STRIP — DEBONDED (LT AILERON) · airframe 29,607 hrs · 20,635 cycles

LEFT AILERON TEFLON STRIP IS DISBONDED ON OTBD END. REPAIRED IAW REO 670-57-61-006-01, REV E.

Part: DOOR FRAME — CORRODED (E/E BAY) · airframe 29,608 hrs · 20,636 cycles

MAIN AVIONICS BAY DOOR CUT OUT FWD SIDE HAS CORROSION BETWEEN STR 25R AND STR 25L WHERE THE DOOR SEAL CONTACTS THE FUSELAGE. REMOVED CORROSION AT FWD SIDE AVIONICS DOOR CUTOUT IAW SRM 51-21-06-001-001-A01.

Part: PANEL — CRACKED (PAX DOOR) · airframe 29,629 hrs · 20,651 cycles

PAX DOOR AFT SIDE PANEL AT TOP STEP AND MID STEP CORNERS CRACKED. REMOVED AFT SIDE PANEL FROM PAX DOOR IAW SRM 51-42-06-001-001-A01. INSTALLED AFT SIDE PANEL TO PAX DOOR IAW SRM 51-42-06-001-001-A01.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 29,585 hrs · 20,619 cycles

INNER PAX DOOR HANDLE CRACKED IN 3 PLACES ON SHAFT FITTING. R & R PAX DOOR INNER PULL HANDLE WITH NEW IAW AMM 52-11-02. MAJOR REPAIR IAW GMM 5-3.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 29,280 hrs · 20,377 cycles

F/A REPORTS AFT FLASHLIGHT DOES NOT WORK. R & R AFT FLASHLIGHT IAW GMM-3-8.

Part: RETAINER — DAMAGED (CARGO DOOR SEAL) · airframe 28,931 hrs · 20,111 cycles

FWD CARGO DOOR LOWER SEAL RETAINER DAMAGE. COMPLIED WITH EC/TC, REO 670-52-35-127-01, PERMANENT REPAIR. THIS IS CONSIDERED A MAJOR REPAIR IAW GMM 5-3.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 28,931 hrs · 20,111 cycles

MEGAPHONE INOPERATIVE. R & R MEGAPHONE IAW AMM 25-61-14, REF IPC 25-61-14, FIG 1, ITEM 5.

Part: PANEL — CRACKED (PAX DOOR) · airframe 27,621 hrs · 19,198 cycles

PAX DOOR FWD SIDE PANEL CRACKED AT THE TOP STEP. REPAIRED IAW REO 670R-52-11-705, REV B. MAJOR REPAIR IAW GMM 5-3.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 27,402 hrs · 19,035 cycles

AFT INTERIOR CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP IAW AMM 33-51-09, OPS CHECKED GOOD.

Part: SILL — CORRODED (CARGO DOORWAY) · airframe 24,821 hrs · 17,198 cycles

AFT CARGO DOOR SILL CORRODED. REPAIRED IAW REO 670-53-61-901.

Part: STRINGER — CORRODED (BS 319.7-349) · airframe 24,826 hrs · 17,204 cycles

STRINGER 18L HAS SEVERAL SMALL AREAS OF LIGHT CORROSION BETWEEN FS 319.7 AND 349. FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 53-21-23-101-002-A01, REMOVED CORROSION IAW SRM 51-21-06-001-001-A01 IAW SRM 53-21-23-000-A11.

Part: SILL — CORRODED (FUSELAGE) · airframe 24,821 hrs · 17,198 cycles

SERVICE DOOR LOWER SILL ANGLE IS CORRODED FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 53-21-23-101-002-A01 DAMAGE IS MORE THAN 10 PERCENT THICKNESS OF MATERIAL. REMOVED SERVICE DOOR LOWER SILL IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. INSTALLED ANGLE, ALL WORK DONE IAW SRM 51-42-06-001-001-A01.

Part: ANGLE — CORRODED (BS 280) · airframe 24,821 hrs · 17,198 cycles

SUPPORT ANGLE RBL 11, WC 71.10 AT FS 280 CORRODED. REMOVED SUPPORT ANGLE AT RBL 11 IAW SRM 51-42006-001-001-A01. INSTALLED SUPPORT ANGLE IAW SRM 51-42-13-001-001.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 24,821 hrs · 17,198 cycles

FWD BS 280 FLOORBEAM CORRODED. REMOVED FLOORBEAM AND ANGLE IAW SRM 51-42-06-001-001. LOCATED AND DRILLED NEW FLOORBEAM ANGLE IAW SRM 51-40-11-001-001. INSTALLED FWD FLOORBEAM ANGLE IAW SRM 51-42-06-001-001.

Part: FLOOR SUPPORT — CORRODED (BS 580) · airframe 24,821 hrs · 17,198 cycles

FLOOR SUPPORT LBL 11, WC 71.10 AT FS 580 CORRODED. REMOVED FLOOR SUPPORT AT LBL11 IAW SRM 51-42-06-001-001-A01. INSTALLED NEW FLOOR SUPPORT AT LBL 11, FS 280 IAW SRM 51-42-13-001-001.

Part: SILL — CORRODED · airframe 24,821 hrs · 17,198 cycles

LOWER SILL ANGLES ARE CORRODED. FOUND CORROSION ON SILL ANGLES TO BE OUT OF LIMITS IAW SRM 53-21-23-101-002-A01. REMOVED LOWER SILL ANGLES IAW SRM 51-42-06-001-001-A01. INSTALLED ANGLES IAW 51-42-06-001-001-A01 SRM.

Part: ANGLE — CORRODED (DOOR HINGE) · airframe 24,821 hrs · 17,198 cycles

FOUR ASD HINGE SIDE L ANGLES ARE CORRODED. REMOVED FOUR ASD HINGE L ANGLES IAW SRM 51-42-06-001-001-A01. INSTALLED HINGE L ANGLES IAW SRM 51-42-06-001-001-A01.

Part: FRAME — CORRODED (BS 319 S26-27L) · airframe 24,826 hrs · 17,204 cycles

FOUND SIGNS OF CORROSION ON FWD FACE OF FRAME BS 319 BETWEEN STR 26-27L. REMOVED CORROSION IAW SRM 51-21-06-001-001 A01. FOUND BLEND AREA TO BE OUT OF LIMITS AT 12 PERCENT OF MATERIAL THICKNESS IAW SRM 53-21-06-101-002-A01. REO 670-53-21-887 --

Part: DOOR FRAME — CRACKED (BS 327.76) · airframe 24,826 hrs · 17,204 cycles

PAX DOOR FRAME FS 327.76 CRACKED, FOUND DURING CMS REMOVAL. REMOVED DOOR FRAME IAW SRM 51-42-06-001-001-A01/51-42-21-001-001-A01. INSTALLED DOOR FRAME IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01.

Part: FLOOR SUPPORT — CORRODED (BS 280-319.7) · airframe 24,821 hrs · 17,198 cycles

RT FLOOR SUPPORT FS 280.00 TO 319.70 IS CORRODED IN SERVERAL AREAS. INSTALLED REPAIR DOUBLER IAW SRM 51-42-06-001-001, 51-42- 13-001-001.

Part: DOUBLER — CORRODED (TCAS ANTENNA) · airframe 24,821 hrs · 17,198 cycles

TCAS ANTENNA INTERNAL DOUBLER CORRODED AT CONNECTOR FS 303.00, STGR27. FOUND TCAS ANT DOUBLER EXFOLIATED. REMOVED CORRODED TCAS ANTENNA DOUBLER, LOCATED, DRILLED AND INSTALLED NEW SERVICABLE TCAS ANTENNA INTERNAL DOUBLER IAW SRM 51-42-06-001-001-A01. FOUND CORROSION ON STR 27 EXFOLIATED AND BEYOND ALLOWABLE LIMITS. RECEIVED, LOCATED, DRILLED AND INSTALLED NEW SERVICABLE STR 27 AT FS 295-280 IAW SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 736.05) · airframe 24,821 hrs · 17,198 cycles

SEAT TRACK HAS CORROSION FS 736.05 RT SIDE. FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 53-41-49-101-001-A01. REMOVED AND INSTALLED SIDE SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 785.15-797) · airframe 24,821 hrs · 17,198 cycles

SEAT TRACK HAS CORROSION BETWEEN FS 785.15 & 797.00 LT SIDE. DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-41-49-101-001-A01. R & R UNSERVICABLE SEAT TRACK IAW SRM 51-41-02-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 421) · airframe 24,821 hrs · 17,198 cycles

SEAT TRACK AT RBL 9, STA 421 CORRODED. FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 53-21-49-101-001-A01 AND REO 670-53-00-013, REV F. REMOVED AND INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SILL — CORRODED (SERVICE DOOR) · airframe 24,821 hrs · 17,198 cycles

SERVICE DOOR SILL CORRODED. EVALUATED SERVICE DOOR SILL AND FOUND DAMAGE TO BE OUT OF LIMITS IAW SRM 53-21-23-101-002-A01. REMOVED SERVICE DOOR SILL ANGLE, MOUNTING ANGLE IAW SRM 51-42-06-001-001-A01. INSTALLED NEW ANGLE ALL WORK DONE IAW SRM 51-42-06-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 785.15) · airframe 24,821 hrs · 17,198 cycles

SIDE SEAT TRACK HAS CORROSION AT FS 785.15, RT SIDE. FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 53-41-49-101-001-A01 AND REO 670-53-00-013, REV F. REMOVED AND INSTALLED SEAT TRACK IAW AMM 53-0-49-400-801. (CONFIG) A03.

Part: CROSSBEAM — CORRODED (BS 280) · airframe 24,821 hrs · 17,198 cycles

BS 280 CROSSBEAM CORRODED AT COCKPIT ENTRANCE. BS 280 CROSSBEAM EXFOLIATED AT CORRODED AREA BEAM FOUND TO BE OUT OF LIMITS IAW SRM 53-11-41-201-002-A01. COMPLIED WITH ECTC REO 670-53-11-047 AND REO 670-53-11-047, REV E.

Part: SEAT TRACK — CORRODED (BS 421) · airframe 24,821 hrs · 17,198 cycles

SEAT TRACK AT LBL 9, BS 421 CORRODED. EVALUATED DAMAGE AND FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 53-21-49-101-001-A01 AND REO 670-53-00-13, REF F. R & R NEW SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SILL — CORRODED (CARGO DOORWAY) · airframe 24,821 hrs · 17,198 cycles

AFT CARGO DOOR SILL CORRODED. REMOVED CORROSION IAW SRM 51-21-06-01-001-A01. COMPLIED WITH REO 670-53-61-901.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 24,713 hrs · 17,119 cycles

FWD WINDSCREEN EMERGENCY FLOOR FLOOD LIGHT INOPERATIVE. RELAMPED EMERGENCY LIGHT. OPS CHECKED GOOD IAW AMM 33-51-00.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 24,614 hrs · 17,043 cycles

F/A EMERGENCY LIGHT SWITCH FOUND IN OP POSITION, EMGERGENCY BATTERY DISCHARGED. RESET AND PERFORMED OPS CHECK OF EMERGENCY LIGHTS IAW FIM 33-51-00. NO FURTHER DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,219 hrs · 14,656 cycles

EMERGENCY LIGHTS WILL NOT TEST-F/A REPORTS THAT THE SWITCH WAS FOUND IN THE ON POSITION. COMPLIED WITH OPS CHECK OF THE EMERGENCY LIGHTS IAW AMM 33-51-00. OPS CHECKED GOOD IAW AMM. OK FOR SERVICE.

Part: LIGHT — BROKEN (CABIN) · airframe 21,025 hrs · 14,530 cycles

LOWER EMERGENCY EXIT LIGHT ASSY BROKEN ON FWD WARDROBE AT ENTRY WAY. REMOVED AND REPLACED FWD GALLEY LWR EMERGENCY LIGHT ASSY IAW AMM 33-51-11. OPS CHECKED GOOD.

Part: HEATER — FIRE (COCKPIT) · airframe 20,922 hrs · 14,464 cycles

CAPT'S WINDSHIELD WITH WINDSHEILD HEAT ON , WINDSHIELD HEATING ELEMENT AT TOP EDGE CAUGHT FIRE. TURNED OFF WINDSHIELD HEAT. FIRE EXTINGISHED. WINDSHIELD THEN CRACKED. NO SMOKE IN COCKPIT OR CABIN. EVENT HAPPENED ON GROUND. R & R CAPTS WINDSHIELD IAW AMM 56-11-01. OPS AND LEAK CHECKED GOOD.

Part: FLOOR SUPPORT — CORRODED (BS 469-597) · airframe 19,988 hrs · 13,816 cycles

CORROSION ON FLOORBEAM AT RBL 9.0 BETWEEN FS 469 - 597 MULTIPLE LOCATIONS COMING FROM UNDER FLOOR TRACK. FABRICATED ALL REPAIR PARTS AND FITTED BEAM AT RBL9 IAW REO 670-53-000-029 STEP 1-10. COMPLIED WITH STEP 3 OF REO 670-53-00-029 PERFORMED EDDY CURRENT INSP IAW NDTM 51-20-006-250-A01 ON FLOORBEAM FS 485.00 TO 581 AT RBL 9 CUT LINES AND FABRICATED PARTS. NO INDICATIONS NOTED. COMPLY WITH STEP 4 OF REO 670-53-029. COMPLIED WITH STEP 4, PAINTED CUT LINES & PARTS, ALL REPAIR PARTS DRILLED TO MATCH ACFT IAW REO 670-53-00-029. JOB 7104121 OP 268 OF REO 670-53-00-278. INSTALLED NEW FLOOR SUPPORT AT RBL 9 FS 469-597 IAW REO 670-53-00-029 STEPS 11-12. INSTALLED NUTPLATES AT FLOOR PANEL AND SEAT TRACK LOCATIONS IAW SRM 51-45-00-001-A01. TOP COAT IAW SRM 51-25-01.

Part: FLOORBEAM — CORRODED (BS 570) · airframe 19,988 hrs · 13,816 cycles

CORROSION OF FLOORBEAMS AFT OF SPLICE AT FS 570 LBL9 - RBL9, REPAIRED IAW REO 670-53-21-591.

Part: SEAT TRACK — CORRODED (BS 374) · airframe 19,988 hrs · 13,816 cycles

SEAT TRACK AT LBL9 FS 374, FOUND TO BE CORROSION DAMAGED BEYOND LIMITS IAW AMM 53-21-49-TR-0015, PAGE 5, NOTE 8. SEAT TRACK NEEDS TO BE REPLACED. INSTALLED NEW SEAT AT LBL9 FWD TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 374) · airframe 19,988 hrs · 13,816 cycles

SEAT TRACK AY RBL9 FWD NEEDS TO BE REMOVED TO FOM OF REPAIR OF FLOORBEAM. REMOVED PASSENGER SEAT TRACK AT RBL 9 FWD TRACK AT 374FS IAW AMM 53-00-49-800-801. INSPECTED SEAT TRACK AT RBL 9 FWD FS 374, FOUND TO BE DAMAGED BEYOND LIMITS IAW AMM 53-21-49-TR 53-0015, PAGE 5, NOTE 9. SEAT TRACK CORRODED. SEAT TRACK NEEDS TO BE REPLACED. INSTALLED NEW SEAT TRACK AT RBL9 FWD TRACK IAW AMM 53-00-49-400-801. (CLOSED)

Part: FLOOR SUPPORT — CORRODED (BS 469-597) · airframe 19,988 hrs · 13,816 cycles

CORROSION ON FLOOR SUPPORT AT LBL 9 BETWEEN FS 469-597 MULTIPLE LOCATION COMING FROM UNDER SEAT TRACK. CUT LINE ON NEW PARTS REQUIRE NDT IAW REO 670-53-00-029. PERFORMED EDDY CURENT INSP OF CUT LINES ON NEW PARTS IAW REO 670-53-00-029 IAW NDTM PART 1, NO INDICATIONS NOTED. PRIMED & PAINTED CUT LINES & FABRICATED PARTS IAW REO 670-53-00-0029 FABRICATED CLEATS IAW REO 670-53-00-278, INSTALLED LBL 9 FLOOR SUPPORT 485-565 IAW REO 670-53-00-29 FIG 13 PRIMED AND PAINTED IAW SRM 51-21-16. 4 EA NUTPLATES, INSTALLED 4 EA NUTPLATES AT AFT END OF SUPPORT FS 565 IAW SRM 51-45-00-001-001-A01.

Part: PANEL — CHAFED (WING) · airframe 20,346 hrs · 14,053 cycles

PANEL 622CB CHAFED ON L/E (MARKED) RESOLVED ON W/O: 173017 TASKCARD: N/R-00312. BLENDED OUT CHAFING ON L/E PANEL 622CB ALL WORK DONE IAW CRJ700 SRM 57-12-00-001-001-A01. BLENDED AREA REQUIRE NDT. RECEIVED NEW PANEL, LOCATED HOLES AND TRIMMED IAW CRJ700 SRM 51-40-11-001-001-A01, 51-34-36-001-001-A01. NEW PANEL AWAITING ADR FOR PILOT HOLES, LOCATED HOLES NEED TO BE COUNTERSUNK. COUNTERSUNK SCREW HOLES IAW CRJ700 SRM 51-40-11-001-001-A01, INSTALLED DOUBLE FLUSH RIVET IN DOUBLE DRILLED HOLE IAW REO 670-57-41-196 AND CRJ700 SRM 51-42-06-001-001-A01, REFINISHED PANEL IAW CRJ700 SRM 51-25-01-001-001-A01. REFER M212 PANEL 622CB PG 61 FOR INSTALLATION. AWAITING EC/TC. CR 161779 10/02/10 (LH 10/06/10) RECEIVED EC/TC REO 670-57-41-196 REV RW 161752 10/06/10 (LH 10/06/10) ASA RII BD 5500008 161723 10/06/10 .

Part: FLOOR SUPPORT — CORRODED (BS 752-797) · airframe 19,988 hrs · 13,816 cycles

LT FLOOR TRACK LBL 9.0 CORRODED AT APPROX FS 752-797, MULTIPLE LOCATIONS. REMOVED FLOOR SEAT TRACK IAW AMM 53-00-49-000-801. LOCATED HOLES IN NEW FLOOR SEAT TRACK IAW SRM 51-40-11-001-001-A01. STEPPED HOLES UP TO NOMINAL AND COUNTERSUNK AS REQUIRED IAW SRM 51-40-11-001-001-A01. INSTALLED LT FLOOR SEAT TRACK AT FS 752-797, IAW AMM 53-00-49-400-801-A03.

Part: FLOOR SUPPORT — CORRODED (BS 469-597) · airframe 19,988 hrs · 13,816 cycles

RT FLOOR TRACK AT RBL 9.0 CORRODED BETWEEN FS 469 - 597 MULTIPLE LOCATIONS. REMOVED SEAT RAIL RBL9 FROM FS 485- FS 581 IAW AMM 53-00-49-000-801. INSTALLED NEW SEAT TRACK AT RBL9 469-597 IAW AMM 53-00-49-400-801.

Part: FLOOR SUPPORT — CORRODED (BS 597-661) · airframe 19,988 hrs · 13,816 cycles

LEFT FLOOR TRACK CORRODED AT LBL 9.0 BETWEEN FS 597 - FS 661.0 MULTIPLE LOCATIONS. REMOVED FLOOR TRACK IAW AMM 53-00-49-000-801. STOPPED HOLES TO FOR SCREWS, COUNTERSUNK ALL HOLES IAW SRM 51-40-11-001-001-A01. INSTALLED NEW FLOOR SEAT TRACK AT LBL9.0 597-661 IAW AMM 53-00-49-400-801.

Part: FLOOR SUPPORT — CORRODED (BS 752-797) · airframe 19,988 hrs · 13,816 cycles

RT FLOOR TRACK AT RBL 9.0 CORRODED BETWEEN FS 752-797. REMOVED CORROSION FROM SEAT RAIL RBL9 BETWEEN FS 752- FS 797 IAW SRM 51-21-06. BLENDED AREA NEEDS MEASURED TREATED. PERFORMED DIMENSIONS LIMIT CHECK OF BLENDED AREAS OF RT FLOOR SEAT TRACK BETWEEN FS752-FS797 FOUND MAXIMUM MATERIAL REMOVED TO BE .015IN, WITHIN LIMITS IAW 53-41-49-101-001-A01 ALSO PERFORMED ALKALINE TREATMENT IAW SRM 51-21-16-CODE.

Part: FLOOR SUPPORT — CORRODED (BS 469-597) · airframe 19,988 hrs · 13,816 cycles

LT FLOOR TRACK AT LBL 9.0 CORRODED BETWEEN FS 469 - 597 MULTIPLE LOCATIONS. BLENDED CORROSION ON FLOOR TRACK AT LBL9.0 BETWEEN FS 469-FS 597 FOUND TO BE OUT OF LIMITS IAW SRM 53-31-49-101-A01. REMOVED FLOOR TRACK AT LBL9 BETWEEN FS 469-597 IAW AMM 53-00-49-000-801 (CONFIG-A03) INSTALLED NEW FLOOR SEAT TRACK AT LBL9 469-597 IAW AMM53-00-49-400-801.

Part: FLOORBEAM — CORRODED (BS 469-597) · airframe 19,988 hrs · 13,816 cycles

CORROSION ON FLOORBEAM AT RBL 9.0 BETWEEN FS 469.00 FS 597 MULTIPLE LOCATIONS COMING FROM UNDER FLOOR TRACK. BLENDED CORROSION AND REMOVED 2 NUTPLATES IAW SRM 51-21-06-001-001-A01. AND 51-42-10-001-001-A01. PERFORMED UT THICKNESS INSP OF BLEND AREAS ON FLOORBEAM IAW MAC NDT INSP PROCEDURE UT-3. PERFORMED STEP 1 AND 2 OF REO 670-53-21-591.

Part: FLOORBEAM — CORRODED (BS 469-597) · airframe 19,988 hrs · 13,816 cycles

CORROSION ON FLOORBEAM AT LBL 9.0 BETWEEN FS 469.00 - FS 597 MULTIPLE LOCATION COMING FROM UNDER SEAT TRACK. REMOVED SEAT RAILS IAW AMM 53-00-49-000-801. CORROSION REMOVED FROM TOP OF FLOORBEAM IN 3 LOCATIONS BETWEEN FS 469 & FS 661.00 LBL9 IAW SRM 51-21-06-001-001-A01, PERFORMED UT THICKNESS INSP OF BLEND AREA IN FLOORBEAMS IAW MAC NDT INSP PROCEDURES UT.3 MINIMUM CATERIAL REMAINING IS AS FOLLOWS; LOCATION JUST ADT OF FS 469.00 IS .017", LOCATION NR3 AT FS581.00 IS 063." IN REF TO STEP 2 ABOVE SUBMIT FINDING TO THD. REMOVED DAMAGED BEAM SECTION AT LBL9 FS 485-565 PREPARED NEW BEAM ASSY AND FABRICATED ALL PARTS IAW REO 670-53-00-029.

Part: FLOOR SUPPORT — CORRODED (BS 629-661) · airframe 19,988 hrs · 13,816 cycles

RT FLOOR TRACK AT RBL 9.0 CORRODED BETWEEN FS 629 - FS 661.0. REMOVED CORROSION FROM SEAT RAIL RBL9 BETWEEN FS 629 + FS 661 IAW SRM 51-21-06-001-001 AFTER CORROSION REMOVAL SEAT RAIL IS WITHIN ALLOWABLE LIMITS IAW SRM 53-31-49-101-001 TREATED BARE METAL IAW SRM 51-21-11. PERFORMED LPI, TYPE 1, METHOD C ON BLEND AREAS OF SEAT TRACK AT RBL9.00 BETWEEN FS 629 AND FS 661 IAW MAC NDT INSP PROCEDURE PT-1. NO INDICATIONS NOTED AT THIS TIME.

Part: DOOR — OUT OF ADJUST (EMERGENCY EXIT) · airframe 19,988 hrs · 13,816 cycles

LT OVERWING EMERGENCY EXIT DOOR HARD TO OPEN. ADJUSTED BOTH SHOOT BOLTS ON LT OVERWING EMERGENCY EXIT DOOR. OPS CHECK GOOD IAW AMM TASK 52-21-00-820-801.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 19,275 hrs · 13,278 cycles

MAIN CABIN INTERIOR AISLE EXIT SIGN AND EXIT LIGHTS INOP AT OVERWING EMERGENCY EXITS. REPLACED FUSE AT PL124 BATTERY PACK NR2 OPS CHECK GOOD IAW MM 33-51-17.

Part: ANGLE — CORRODED (THRESHOLD) · airframe 19,275 hrs · 13,278 cycles

MAIN PASSENGER CABIN L1 DOOR THRESHOLD ANGLE HAS CORROSION. REMOVED AND INSTALLED THRESHOLD, INSTALLED NUTPLATES AND NUTPLATE CLIPS ON NEW ANGLE IAW SRM 51-24-06,53-00-00,51-40-11 AND 51-40-02 TOOL DI-114450 DUE DATE 3JAN11.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 19,251 hrs · 13,261 cycles

MAIN CABIN EXIT IDENTIFIER AT LT OVERWING EMERGENCY DOOR HAS 2EA BULBS INOP. REMOVED AND REPLACED 2 EA BULBS AT MAIN PAX CABIN EXIT INTERFACE AT LH OVERWING EMERGENCY DOOR EXIT OPS CHECK GOOD IAW AMM 33-51-05.

Part: LENS — CRACKED (EMERGENCY LIGHTS) · airframe 19,251 hrs · 13,261 cycles

MAIN CABIN EXIT IDENTIFIER AT PP1 DOOR HAS CRACKED LENS. REMOVED AND REPLACED MAIN CABIN EXIT INTERFACE LENS AT PP1 DOOR IAW AMM 33-51-05.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 19,251 hrs · 13,261 cycles

MAIN CABIN SIDEWALL LIGHT AT LT OVERWING EXIT INOP. REMOVED AND REPLACED BULB AT MAIN PAX CABIN LT EMERGENCY LIGHT OPS CHECK GOOD IAW MM 33-21-07.

Part: SEAT TRACK — CORRODED (BS 349-549) · airframe 19,251 hrs · 13,261 cycles

MAIN PASSENGER CABIN LT I/B SEAT TRACK AT STA 379 TO 549 HAS CORRSION. REMOVED SEAT TRACK FROM CABIN LT IB IAW SRM 51-41-02. INSTALLED SEAT TRACK.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 19,251 hrs · 13,261 cycles

MAIN CABIN EXIT IDENTIFIER AT RT OVERWING EMERGENCY DOOR HAS 1 EA BULBS INOP. REMOVED AND REPLACED BULB AT MAIN PAX CABIN EXIT INTERFACE AT RT OVERWING EMERGENCY DOOR OPS CHECK GOOD IAW AMM 33-51-05.

Part: SEAT TRACK — CORRODED (BS 349-549) · airframe 19,251 hrs · 13,261 cycles

MAIN PASSENGER CABIN RT I/B SEAT TRACK AT STA 349 TO 549 HAS CORRODED. REMOVED CORRSION FROM RT IB SEAT TRACK. MAX REMOVED .035 FOUND OUT OF LIMITS PER SRM 53-21-43. REMOVED AND INSTALLED NEW SEAT TRACK ASSY AS PER AMM 53-21-49.

Part: UPLOCK SENSOR — OUT OF ADJUST (MLG) · airframe 19,187 hrs · 13,216 cycles

GEAR UP DISAGREE ASSOCIATED WITH LOUD NOISE IN NLG AREA. NLG RED (DISAGREED). RESET GEAR HANDLE DOWN, NOSE GEAR LOCKED DOWN AT 160KIAS, VERY LOUD VIBRATION NOISE COMING FROM EXTENDED NOSEGEAR [ACFT RETURNED TO BTR AFTER T/O - EMERGENCY DECLARED] INSPECTED AND FOUND NLG UPLOCK PROX SENSOR OUT OF RANGE. ADJUSTED NLG UPLOCK PROX SENSOR IAW AMM 32-61-05. PREFORMED OPS TEST OF THE MLG EXTENSION/ RETRACTION SYSTEM IAW AMM TEMP. REVISION 32-30-00. OPS TEST GOOD.

Part: PLACARD — MISSING (PAX DOOR) · airframe 17,900 hrs · 12,248 cycles

EXIT PLACARD ON ENTRANCE DOOR MISSING.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,366 hrs · 11,825 cycles

AFT GALLEY EMERGENCY LIGHT HAS SEVERAL INOP BULBS.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 17,366 hrs · 11,825 cycles

LEFT PACK FAULT STATUS MSG.

Part: TIRE — WORN (MLG) · airframe 16,569 hrs · 11,207 cycles

RT INBD AND OTBD MLG WHEEL AND TIRE ASSY WORN TO LIMITS. EMERGENCY DECLARED AND EMERGENCY VEHICLES REQUESTED TO BE ON STANDBY AS A PRECAUTION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,351 hrs · 10,299 cycles

RT FWD EMERGENCY LIGHT INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,351 hrs · 10,299 cycles

LT AFT EMERGENCY LIGHT INOP.

Part: TORQUE TUBE — CORRODED (TE FLAP) · airframe 15,156 hrs · 10,163 cycles

LT WING O/B FLAP I/B TORQUE TUBE CORRODED.

Part: SEAT TRACK — CORRODED (FUSELAGE)

RT FLOOR SEAT RAIL FROM FS 581.00 TO FS 683.00 CORRODED REMOVED AND REPLACED FLOOR SEAT RAIL FROM FS581 - FS 683 IAW MM 53-00-49. (K)

Part: PIN — CORRODED (MLG TRUNNION) · airframe 15,156 hrs · 10,163 cycles

CORROSION AT LT MLG FWD TRUNNION PIN.

Part: PIN — CORRODED (MLG TRUNNION) · airframe 15,156 hrs · 10,163 cycles

CORROSION AT RT MLG FWD TRUNNION PIN.

Part: PIN — CORRODED (LT MLG TRUNNION) · airframe 15,156 hrs · 10,163 cycles

CORROSION AT LT MLG FWD TRUNNION PIN.

Part: PIN — CORRODED (MLG TRUNNION) · airframe 15,156 hrs · 10,163 cycles

CORROSION AT LT MLG AFT TRUNNION PIN.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 15,156 hrs · 10,163 cycles

R/H FS 280 FLOOR SUPPORT BEAM CORRODED.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 15,156 hrs · 10,163 cycles

L/H 280 FLOOR SUPPORT BEAM CORRODED.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 15,156 hrs · 10,163 cycles

FWD FLOOR SUPPORT ANGLE AT FS 280 CORRODED.

Part: WEB — CORRODED (BS 280) · airframe 15,156 hrs · 10,163 cycles

BS 280 WEB CORRODED.

Part: FLOOR SUPPORT — CORRODED (BS 310-349) · airframe 15,156 hrs · 10,163 cycles

MINOR CORROSION ON FLOOR SUPPORT RAIL INBD OF ASD @ FS 310-349.

Part: WEB — CORRODED (BS 280) · airframe 15,156 hrs · 10,163 cycles

R/H 280 WEB CORRODED.

Part: SILL — CORRODED (BS 280) · airframe 15,156 hrs · 10,163 cycles

FLOOR SILL STRUCTURE AT FS 280, RBL 45 CORRODED.

Part: STEP — CRACKED

LOWER STEP CRACKED FWD SIDE. (K)

Part: STEP — CRACKED (ASD) · airframe 15,156 hrs · 10,163 cycles

ASD UPPER STEP LOWER HALF FWD SIDE CRACKED (DOOR OPEN).

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,966 hrs · 10,014 cycles

BOTH AFTMOST CEILING EMERGENCY LIGHTS INOP. RESOLVED ON W/O 98211 TASKCARD N/R 00006. RELAMPED BOTH AFT MOST CABIN CEILING EMERGENCY LIGHTS. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,665 hrs · 9,113 cycles

EMERGENCY FLOOD LIGHT CEILING ROW 8 INOP, CABIN EMERGENCY LIGHTS, CEILING LEVEL FLOODLIGHTS.

Part: STEP — CRACKED (PAX DOOR) · airframe 13,295 hrs · 8,869 cycles

PAX DOOR BOTTOM STEP IS CRACKED ON FWD SIDE.

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 12,939 hrs · 8,619 cycles

RIGHT SIDE EXTERNAL OVERWING AFT EMERGENCY EXIT LIGHT IS INOP.

Part: WARNING SYSTEM — ACTIVATED (BLEED AIR SYS) · airframe 11,526 hrs · 7,674 cycles

RIGHT BLEED DUCT WARNING. A/C RETURNED TO ATL AFTER T/O. RELATED TO DEFECT 306811-2. EMERGENCY DECLARED. FLT 4331, 4899 CX.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 11,305 hrs · 7,527 cycles

CAPTAIN`S FLASHLIGHT INOP.

Part: CARGO TRACK — CRACKED (FUSELAGE) · airframe 11,229 hrs · 7,476 cycles

AFT CARGO BAY FWD TRACK SUPPORT ANGLE MIDDLE CHANNEL CRACKED (MARKED). [SUP 05-02-07] REPAIRED IAW ALL SRM`S.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 11,229 hrs · 7,476 cycles

PAX DOOR OUTER HANDLE CRACKED. REMOVED PAX DOOR LATCH MECHANISM TO FOM. REMOVED PAX DOOR OUTER HANDLE JB422. INSTALLED SERVICEABLE FLAP HANDLE ONTO SERVICEABLE HANDLE MECHANISM PN 601R31763-1 IAW CRJ SRM 51-42-04. OK TO PRIME & PAINT PAX DOOR OUTER HANDLE. PAINTED AND PRIMED PAX DOOR OUTER HANDLE IAW CRJ 700 SRM 51-25-01 INSTALLED OUTER HANDLE IAW CRJ 700 AMM 52-11-02. REQUIRES OPS CK. PERFORMED OPS & LEAK CHECK OF PAX DOOR IAW CRJ MM 52-11-02. NO DEFECTS NOTED.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 11,229 hrs · 7,476 cycles

RIGHT LOWER FS BULKHEAD WEB HAS CORROSION. REPLACED WEB.

Part: WEB — CORRODED (BS 280) · airframe 11,229 hrs · 7,476 cycles

LEFT LOWER FS 280 WEB HAS CORROSION. REMOVED LEFT 280 WEB SPLICE DOUBLER. REMOVED LEFT 280 LOWER CORRODED WEB IAW CRJ 700, 51-42-06. RE-INSTALLED SPLICE WET WITH SOLID FASTENERS; BOTTOM 2EA ROWS TO LOWER LEFT 280 WEB IAW CRJ SRM 51-42-02. STARTED INSTALLATION OF FASTENERS IN LEFT 280 WEB AND SPLICE DOUBLER IAW REO 670-53-11-052. COMPLETED INSTALLATION OF LEFT FS 280.00 LOWER WEB FASTENERS IAW BOMBARDIER REO 670-53-11-052. FILLET SEALED REPAIR AREA IAW CRJ 700 SRM 51-23-00. TOPCOATED REPAIR AREA IAW CRJ 700 SRM 51-25-16. SUPPLEMENTAL - SDR CLOSED 03/15/07.

Part: CROSSBEAM — CORRODED (BS 280) · airframe 11,229 hrs · 7,476 cycles

LEFT FS 280 CROSSBEAM HAS CORROSION ON UPPER FLANGE. REMOVED LEFT 280.00 CROSSBEAM IAW 700/900 SERIES SRM 51-42-06, 51-42-13, 51-42-21. LOCATED HOLES ON SERVICEABLE CROSSBEAM P/N CC670-34175-7, IAW CRJ 700 SRM 51-40-11. INSTALLED LEFT 280.00 CROSSBEAM SECTION, SOLID FASTENERS, AND HI-LITES AND CHERRY FASTENERS AS REQUIRED IAW CRJ 200 SRM 51-42-06, 51-42-13, AND 51-42-21. RE-INSTALLATION OF LBL 20.00 AND LBL 37.00 INTERCOSTALS. O/B UPPER FLANGE FASTENERS REQUIRE INSTALLATION FOR COMPLETION OF REPAIR. INSTALLED REMAINING FASTENERS AS REQUIRED IAW CRJ 700 SRM 51-42-06. TOPCOATED REPAIR AREA IAW CRJ 700 SRM 51-25-16. APPLIED DINITROL AV8 TO REPAIR AREA IAW CRJ 700 SRM 51-21-11. LOCATED FASTENER HOLES FOR F

Part: FLOOR SUPPORT — CORRODED (BS 280) · airframe 11,229 hrs · 7,476 cycles

FS 280 FWD CENTER FLOOR SUPPORT ANGLE CORRORED. REPAIRED IAW ALL SRM`S.

Part: CROSSBEAM — CORRODED (BS 280) · airframe 11,229 hrs · 7,476 cycles

RIGHT FS 280 CROSSBEAM HAS CORROSION ON UPPER FLANGE. [SUP 05-02-07] REMOVED RT 280.00 CROSSBEAM IAW CRJ 700/900 SERIES SRM 51-42-06. 51-42-13, 51-42-21. LOCATED ALL HOLES IN NEW SERVICEABLE R CROSSBEAM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,144 hrs · 7,408 cycles

NUMEROUS LIGHTS ARE BURNED OUT ON BOTH THE LT AND RT LOWER OVERWING EMERGENCY EXIT SIGNS.

Part: DOOR — MALFUNCTIONED (PAX DOOR) · airframe 11,123 hrs · 7,391 cycles

ENTRANCE DOOR WILL NOT CLOSE.

Part: ENGINE — VIBRATION (NR 2) · airframe 9,904 hrs · 6,619 cycles

NR 2 ENGINE N1 VIBE AT 1.6-1.7 DURING CLIMB. 1.8 AT TOC. REDUCED POWER N1 VIB REDUCED TO 1.6. MDC SHOWED 2.3 FOR 42.5 SECONDS AFTER ON GROUND. ENROUTE, A/C DIVERTED DUE TO MTC (EMERGENCY DECLARED).

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 9,599 hrs · 6,434 cycles

F/A'S FLASHLIGHT IS INOP

Part: LIGHT — INOPERATIVE (CABIN) · airframe 8,818 hrs · 5,919 cycles

CABIN CEILING, EMERGENCY LIGHT AT SEAT 17 INOP

Part: STEP — CRACKED (FUSELAGE)

DURING A HANGAR INSPECTION, THE PASSENGER DOOR BOTTOM STEP WAS FOUND TO BE CRACKED AT THE ATTACHMENT POINT. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: WIRE HARNESS — DISCONNECTED (EMERGENCY LIGHT)

DURING A HANGAR INSPECTION IN MCN, THE EMERGENCY EXIT LIGHT, ON THE FORWARD LEFT WINDSCREEN, WAS FOUND TO BE INOPERATIVE. MAINTENANCE RECONNECTED THE EMERGENCY EXIT LIGHT HARNESS ASSEMBLY. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: SIGN — DAMAGED (EMERGENCY EXIT)

DURING A GROUND INSPECTION, THE EMERGENCY EXIT SIGN ON THE PASSENGER DOOR WAS FOUND DAMAGED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT SIGN ON THE PASSENGER DOOR. AIRCRAFT OK FOR SERVICE. (K)