N709EV

Part: NONE — MALFUNCTIONED · airframe 38,206 hrs · 27,599 cycles

GEAR DISAGREE WARNING MESSAGE UPON GEAR RETRACTION AFTER TAKEOFF. RAN QRH. WARNING MESSAGE WENT AWAY, BUT THE MOTOR CONTINUED TO RUN FOR THE DURATION OF THE FLIGHT. ALL THREE GEAR INDICATED DOWN AND LOCKED. (FLIGHT 3251 FILED CLOSED) T/S GEAR DISAGREE WARNING MESSAGE TO NLG WOW CENTERED PROX SENSER PX37 SENSOR TARGET MISSING. INSTALLED A NEW PX37 SENSOR TARGET IN REF. TO AMM 32-61-05. PERFORMED AIRCRAFT JACKING FROM THE NOSE POINT IN REF. TO AMM 07-13-01. PERFORMED OPERATIONAL TEST OF THE LANDING GEAR PSS IN REF. TO AMM 32-61-00. PERFORMED OPERATIONAL TEST OF THE LANDING GEAR EXTENSION SYSTEM IN REF. TO AMM 32-34-00. OPS CHECKS GOOD AT THIS TIME. NO OTHER DEFECTS NOTED AT THIS TIME. A/C OK FOR SERVICE.

Part: NONE — DENTED · airframe 37,676 hrs · 27,178 cycles

RH OUTBOARD FLAP VANE LEADING EDGE HAS TWO DENTS AT WING STATION 185.10 (C-CHECK RO 10/9/2021) REPAIRED THE RIGHT HAND OUTBOARD VANE LEADING EDGE AT WING STATION WS185.10 IN ACCORDANCE WITH REPAIR ENGINEERING ORDER (REO) 670-57-53-001 REV A DATED:2012-12-06. NO DEFECTS NOTED.

Part: NONE — CRACKED · airframe 37,676 hrs · 27,178 cycles

FIRST OFFICER WINDSHIELD CONTAINS MINOR CRACKS IN THE (STRUCTURAL) GLASS PLIES ALL AROUND EDGES. (C-CHECK RO 10/9/2021) REMOVED OF THE FIRST OFFICER WINDSHIELD PER AMM TASK 56-11-01-000-801 (CONFIG A01) / REMOVAL OF THE WINDSHIELD SIDE STRAP AMM TASK 56-10-05-000-801 (CONFIG A01) / INSTALLED A NEW FIRST OFFICER WINDSHIELD PER CRJ 700 AMM 56-11-01-400-801 (CONFIG A01). / RE-INSTALLED THE WINDSHIELD SIDE STRAP PER CRJ 700 AMM 56-10-05-400-801 (CONFIG A01 / NO DISCREPANCIES NOTED. / PLEASE REFERENCE CAMP 23165335 FORTHE PRESSURIZATION LEAK CHECK.

Part: NONE — DENTED · airframe 37,676 hrs · 27,178 cycles

DENT ON FUSELAGE SKIN AT LEFT HAND FS517, STR16 (C-CHECK RO 10/9/2021) PERFORMED REPAIR ON LEFT HAND FUSELAGE SKIN AT FS517, STR16L IAW MHIRJ REO 670-53-31-689. IAW CRJ700 NDTM 51-20-006, CRJ700 SRM 51-24-36,51-24-16,51-21-16,51-23-00,51-40-11,51-42-21. SEE CAMP# 23165335 FOR PRESSURIZATION CHECK. ANALYSIS TO DETERMINE ADDITIONAL REQUIREMENTS WILL BE COMPLETED WITHIN 12 MONTHS OF THE ISSUE DATE OF THIS REPAIR. 2021-08-12 / STS-6796 090921

Part: NONE — DAMAGED · airframe 37,676 hrs · 27,178 cycles

FUSELAGE EXTERNAL SKIN, FS 501, BETWEEN STR 20R & STR21R COUNTERSINK UNEVEN, RIVET HEAD NOT FLUSH WITH SURFACE AFT OF HOLE. (C-CHECK RO 10/9/2021) REPAIR OF FASTENER HOLE ON EXTERNAL FUSELAGE SKIN AT FS 501.00 BETWEEN STGR 20R AND STGR 21R PER STRUCTURAL MAJOR REPAIR (**RII**) PER CARD 51-900-1002-SKY MTCM REV: REV DATE: 06 OCT 20 IN ACCORDANCE WITH MHIRJ REO 670-53-31-697 REV-- / DATED 2021-09-06. PLEASE REFERENCE CONTINUATION CARD FOR REPAIR DISPOSITION AND CORRECTIVE ACTION DETALIS. NO DISCRAPENCIES NOTE.

Part: NONE — CORRODED · airframe 37,676 hrs · 27,178 cycles

INTERCOSTAL AT STR20R, BETWEEN FS300-FS310 UNDER SERVICE DOOR CORRODED. (C-CHECK RO 10/9/2021) REMOVED CORRODED INTERCOSTAL AT STGR 20R FS 300.00 TO FS 310.00 AND REPLACED WITH NEW INTERCOSTAL IAW CRJ700 SRM 53-21-23, 51-24-21, 51-24-06, 51-40-11, 51-25-06, 51-25-21 AND 51-42-06.

Part: NONE — CORRODED · airframe 37,676 hrs · 27,178 cycles

SEAT TRACK FS. 581.00 TO FS. 685.00 AT RBL 9.00 FOUND PITTING CORROSION AT MULTIPLE LOCATIONS. (C-CHECK RO 10/9/2021) REMOVED CORROSION AND EVALUATED SEAT TRACK AT RBL9.00 FROM FS581.00 TO FS 685.00 IAW CRJ700 SRM 51-21-06 FOUND TO BE OUT OF LIMITS. REMOVED MORE THAN 0.035" FROM ECTION "U" IAW CRJ700 SRM 53-31-49. REMOVED, RECIEVED NEW SEAT TRACK PN: 20276 7075T6511 LOT# R00022115-001, LOCATED, DRILLED, DEBURRED IAW CRJ700 SRM 51-40-11 AND 51-24-36. TREATED AND INSTALLED NEW SEAT TRACK IAW CRJ 700 SRM 51-21-11 AND 51-41-02. / TOOL; STS-5292 CAL DUE DAE; 29 MR 22

Part: NONE — CORRODED · airframe 37,676 hrs · 27,178 cycles

SEAT TRACK AT FS. 364.00 TO FS 485.00 AT LBL 27.00 FOUND PITTING CORROSION AT MULTIPLE LOCATIONS (C-CHECK RO 10/9/2021) REMOVED CORROSION ON SEAT TRACK AT FS. 364.00 TO FS 485.00 AT LBL 27.00, MATERIAL REMOVED IS GREATER THAN 0.035" EXCEEDING ALLOWABLE LIMITS AS PER CRJ700 SRM 53-21-49. REMOVED AND REPLACED SEAT TRACK PN:20276 7075T6511 LOT# R00022115-001 AT FS. 364.00 TO FS 485.00 AT LBL 27.00, IAW REO 670-53-00-589 REV -A DATE:2020-07-14 NO FURTHER DAMAGE NOTED. / DEPTH GAGE: STS-0283 DUE: 11MAR22

Part: NONE — CORRODED · airframe 37,676 hrs · 27,178 cycles

SEAT TRACK FS. 376.00 TO FS. 485.00 AT LBL 9 FOUND PITTING CORROSION AT MULTIPLE LOCATIONS. (C-CHECK RO 10/9/2021) REMOVED DAMAGED SEAT TRACK AT FS 376.00 TO FS 485.00 LBL 9.00 IAW CRJ700 AMM 53-00-49. INSTALLED NEW SEAT TRACK P/N 202767075T6511 LOT# R00022115-001 IAW REO 670-53-00-589 REV-A 2020-07-14 AND CRJ700 AMM 53-00-49.

Part: NONE — CORRODED · airframe 37,676 hrs · 27,178 cycles

FLOOR SUPPORT FS. 525.00 TO FS. 575.00, RBL 9.00 HAS CORROSION ON UPPER SECTION (C-CHECK RO 10/9/2021) REMOVED AND REPLACED CORRODED FLOOR SUPPORT FROM FS 525 TO FS575, RBL 9.00 IAW CRJ700 SRM 53-00-41. NO FURTHER ACTION REQUIRED.

Part: NONE — CORRODED · airframe 37,676 hrs · 27,178 cycles

SEAT TRACK FS. 1005.00 TO 1041.00 AT LBL 9 FOUND PITTING CORROSION AT MULTIPLE LOCATIONS. (C-CHECK RO 10/9/2021) REMOVED DAMAGED SEAT TRACK AT FS 1005.00 TO FS 1041.00 LBL 9.00 IAW CRJ700 AMM 53-00-49. INSTALLED NEW SEAT TRACK P/N 20276 7075T6511 LOT# R0022115-001 IAW REO 670-53-00-589 REV. -A DATE 2020-07-14 AND CRJ700 AMM 53-00-49.--------

Part: NONE — CORRODED · airframe 37,676 hrs · 27,178 cycles

SIDEWALL SEAT TRACK, LH SIDE FS. 853.00 TO 960.00 FOUND PITTING CORROSION AT MULTIPLE LOCATIONS. (C-CHECK RO 10/9/2021) REMOVED AND REPLACED SIDE WALL SEAT TRACK L/H SIDE FS 853.00 TO 960.00 IAW CRJ 700 SRM 51-41-02. AND AMM 53-00-49.

Part: NONE — CORRODED · airframe 37,676 hrs · 27,178 cycles

SEAT TRACK FS. 978.00 TO FS. 1005.00 FOUND PITTING CORROSION AT MULTIPLE LOCATIONS. (C-CHECK RO 10/9/2021) SEAT TRACK DAMAGE AT FS. 978.00 TO FS. 1005.00 RBL27 FOUND TO BE OUT OF LIMIT AS PER CRJ700 SRM 53-51-49. REMOVED AND OBTAINED NEW SEAT TRACK, LOCATED, DRILL, DEBURRED AND INSTALLED NEW SEAT TRACK IAW CRJ700 SRM 51-40-11, 51-41-02

Part: NONE — CORRODED · airframe 37,676 hrs · 27,178 cycles

SIDEWALL SEAT TRACK, RH SIDE FS. 853.00 TO FS. 960.00 FOUND PITTING CORROSION AT MULTIPLE LOCATIONS (C-CHECK RO 10/9/2021) REMOVED AND REPLACED DAMAGED R/H SIDEWALL SEAT TRACK FROM FS853 TO FS960 IAW CRJ700 SRM 53-51-49, 51-41-02, 51-24-36, 51-40-11 AND 51-21-11. NO FURTHER ACTION REQUIRED AT THIS TIME.

Part: NONE — CORRODED · airframe 37,676 hrs · 27,178 cycles

SEAT TRACK FS. 684.00 TO FS.724.00 AT RBL 9.00 FOUND PITTING CORROSION (C-CHECK RO 10/9/2021) REMOVED AND REPLACED DAMAGED SEGMENT OF RBL 9.00 SEAT TRACK FROM FS684 TO FS724 IAW MHIRJ REO 670-53-00-589. NO FURTHER ACTION REQUIRED AT THIS TIME.

Part: NONE — CORRODED · airframe 37,676 hrs · 27,178 cycles

SEAT TRACK FS. 581.00 TO FS. 684.00 AT LBL 9.00 FOUND PITTING CORROSION AND NICKS AT MULTIPLE LOCATIONS. (C-CHECK RO 10/9/2021) REMOVED DAMAGED SEAT TRACK AT FS 581.00 TO FS 684.00 LBL 9.00 IAW CRJ700 AMM 53-00-49. INSTALLED NEW SEAT TRACK P/N 202767075T6511 LOT# R00022115-001 AT FS 581.00 TO FS 684.00 LBL 9.00 IAW REO 670-53-00-589 REV-A 2020-07-14 AND CRJ700 AMM 53-00-49.

Part: NONE — CORRODED · airframe 37,676 hrs · 27,178 cycles

SILL/INTERCOSTAL AT STR21L BETWEEN FS310 AND FS333, SHOWS EVIDENCE OF CORROSION. (C-CHECK RO 10/9/2021) REMOVED AND REPLACED CABIN SILL/INTERCOSTAL AT STR 21L BETWEEN F.S. 310 AND F.S. 333 IAW CRJ 700 AMM 51-42-06 AND SRM 51-42-21

Part: NONE — CORRODED · airframe 37,676 hrs · 27,178 cycles

FS280 SKIN JOINT SPLICE CORRODED BETWEEN STR 20R & 22R. (C-CHECK RO 10/9/2021) COMPLIED WITH MHIRJ REPAIR ENGINEERING ORDER#670-53-21-2092 FASTENERS REMOVED 3 AREAS BLENDED AT FS280.00 SKIN JOINT SPLICE BETWEEN STR20R AND STR22R ALL FASTENERS REINSTALLED. SEE CAMP # 23165335 FOR PRESSURAZATION CHECK.SEE ATTACHED DOCUMENTS AND M-337 FOR DETAILS. ANALYSIS REQUIREMENTS WILL BE COMPLETED WITHIN 12 MONTHS OF REO ISSUE DATE.

Part: NONE — CORRODED · airframe 37,676 hrs · 27,178 cycles

FS310.00 THRU FS333.00 RIGT SIE FUSELAGE STGR20R CORRODED UNERFLOOR BELOW SREVICE DOOR. (C-CHECK RO 10/9/2021) AFTER FURTHER INVESTIGATION STR20R STRINGER NOT CORRODED, CORROSION IS ON INTERCOSTAL ON STR20R FROM FS310-333. REMOVED AND REPLACED CORRODED INTERCOSTAL/SILL AT STR20R FROM FS310-333 IAW CRJ700 SRM 51-42-06 AND BOMBARDIER DWG SH670-32004. NO FURTHER ACTION REQUIRED AT THIS TIME. SEE CP 22931418 AND CP 22931429 FOR ALL GND TERMINAL INSTALLATIONS.

Part: NONE — DENTED · airframe 37,676 hrs · 27,178 cycles

DENT LOWER OUTER BOTTOM REAR FUSELAGE SKIN RBL 8, F.S. 1053 (C-CHECK RO 10/9/2021) REPAIRED DENT OF LOWER OUTER FUSELAGE SKIN AT RIGHT BUTT LINE 8 AT FUSELAGE STATION 1035. PER MHIRJ REO 670-53-61-1923 REV. -- DATED: 18 AUG 2021. ANALYSIS TO BE COMPLETED WITH IN 12 MONTHS OF THE ISSUE DATE OF THIS REPAIR.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,928 hrs · 24,339 cycles

FOUND RT FS 235.00 UPPER FRAME SECTOR TO BE VISUALLY CRACKED. REMOVED AND REPLACED RT FS 235.00 FRAME SECTOR IAW SRM 51-40-11-001-001-A01, 51-42-21-001-001-A01 AND 51-42-06-001-001-A01.

Part: STIFFENER — CRACKED (BS 202 BULKHEAD) · airframe 33,928 hrs · 24,339 cycles

DURING A C CHECK, FOUND THE BS 202.75 FWD SIDE OF BULKHEAD LBL 30 STIFFENER HAS AN INDICATION OF .15" LONG CRACK IN THE UPPER EDGE OF FLANGE. REPAIRED IAW SRM 53-11-10-201-005-A01.

Part: STIFFENER — CRACKED (BS 202 BULKHEAD) · airframe 33,928 hrs · 24,339 cycles

DURING A C CHECK, FOUND THE BS 202.75 FWD SIDE OF BULKHEAD RBL 30 STIFFENER HAS AN INDICATION OF .15 INCH LONG CRACK IN THE UPPER EDGE OF FLANGE. REPAIRED IAW SRM 53-11-10-201-005-A01.

Part: BEAM — CRACKED (BS 821) · airframe 33,495 hrs · 24,011 cycles

RIGHT APRON STRUCTURE, MACHINED BEAM BS 821.31 IS CRACKED. COMPLIED WITH EA 32-2016-237 AND EC/TC EA 32-2016-237.

Part: BEAM — CRACKED (BS 821) · airframe 33,495 hrs · 24,011 cycles

LEFT APRON STRUCTURE MACHINED BEAM BS 821.31 IS CRACKED. COMPLIED WITH STS EA 32-2016-240 AND EC/TC EA 32-2016-240.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 33,495 hrs · 24,011 cycles

DURING C CHECK, FOUND KICK PLATE ANGLE AT PAX DOOR SURROUND CORRODED. R & R PAX DOOR KICK PLATE ANGLE IAW SRM 53-21-23-101-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01, AMM 52-70-04-400-802-A01, & 52-70-04-820-802-A02.

Part: SEAT TRACK — CORRODED (BS 985-1015) · airframe 33,495 hrs · 24,011 cycles

DURING C CHECK, FOUND THE SEAT TRACK CORRODED AT RBL 9 BS 985 & 1015. R & R THE SEAT TRACK IAW AMM 53-00-49-400-802-A02

Part: FITTING — CORRODED (PAX DOOR) · airframe 33,495 hrs · 24,011 cycles

DURING C CHECK FOUND PAX DOOR HANDRAIL CUPS CORRODED. R & R PAX DOOR HINGE CUPS IAW SRM 51-42-15-001-001-A01, 51-42-06-001-001-A01, & 51-42-15-001-001-A01.

Part: FLOOR SUPPORT — CRACKED (ZONE 100) · airframe 33,495 hrs · 24,011 cycles

DURING C CHECK, FOUND TRU FLOOR SUPPORT CRACKED AT AFT LATCH ON LEFT SIDE. R & R THE FLOOR SUPPORT IAW SRM 51-42-06-001-001, 51-42-13-001-001, & EC/TC SNIEO CC670-33040 S05.

Part: SEAT TRACK — CORRODED (BS 995-1015) · airframe 33,495 hrs · 24,011 cycles

DURING C CHECK, FOUND SEAT TRACK CORRODED AT LBL 9 BETWEEN BS 995-1015. R & R THE SEAT TRACK IAW AMM 53-00-49-000-802-A02, & 53-00-49-400-802-A02.

Part: SEAT TRACK — CORRODED (BS 565-677) · airframe 33,495 hrs · 24,011 cycles

DURING C CHECK, FOUND THE LEFT SEAT TRACK AT BS 565-677 CORRODED. FABRICATED A NEW SEAT TRACK IAW EC/TC REO 670-53-00-343. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000/400-801-A03.

Part: SEAT TRACK — CORRODED (BS 581-677) · airframe 33,495 hrs · 24,011 cycles

DURING C CHECK, FOUND THE SEAT TRACK AT BS 581-677 LBL 9 CORRODED. FABRICATED A NEW SEAT TRACK IAW EC/TC REO 670-53-00-343. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000/400-801-A03.

Part: SEAT TRACK — CORRODED (BS 677-830) · airframe 33,495 hrs · 24,011 cycles

DURING C CHECK, FOUND THE SEAT TRACK AT RBL9 BETWEEN BS 677-830 CORRODED. REMOVED AND REPACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03 AND COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343 REV M.

Part: SEAT TRACK — CORRODED (BS 379-485) · airframe 33,495 hrs · 24,011 cycles

DURING C CHECK, FOUND SEAT TRACJ AT BS 379-485 CORRODED. FABRICATED A NEW SEAT TRACK IAW EC/TC REO 670-53-00-343. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000/400-801-A03.

Part: SEAT TRACK — CORRODED (BS 677-708) · airframe 33,495 hrs · 24,011 cycles

DURING C CHECK, FOUND THE SEAT TRACK AT BS 677-708 CORRODED. FABRICATED A NEW SEAT TRACK IAW EC/TC REO 670-53-00-343. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000/400-801-A03.

Part: SEAT TRACK — CORRODED (BS 847-977) · airframe 33,495 hrs · 24,011 cycles

DURING C CHECK, FOUND SEAT TRACK CORRODED AT RBL 9 BETWEEN BS 847-977. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03 AND COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343 REV M.

Part: SEAT TRACK — CORRODED (BS 379-485) · airframe 33,495 hrs · 24,011 cycles

RIGHT SEAT TRACK BS 379-485 CORRODED. FABRICATED A NEW SEAT TRACK IAW EC/TC REO 670-53-00-343. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000/400-801-A03.

Part: SEAT TRACK — CORRODED (BS 485-565) · airframe 33,495 hrs · 24,011 cycles

DURING C CHECK, FOUND THE RIGHT SEAT TRACK AT BS 485-565 CORRODED. FABRICATED A NEW SEAT TRACK IAW EC/TC REO 670-53-00-343. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000/400/801/A03.

Part: SEAT TRACK — CORRODED (BS 785-863) · airframe 33,495 hrs · 24,011 cycles

DURING C CHECK, FOUND THE RIGHT SIDE SEAT TRACJ AT BS 785-863 CORRODED. FABRICATED A NEW SEAT TRACK IAW EC/TC REO 670-53-00-343. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000/400-801-A03.

Part: SEAT TRACK — CORRODED (BS 485-565) · airframe 33,495 hrs · 24,011 cycles

DURING C CHECK, FOUND THE SEAT TRACK AT BS 485-565 CORRODED. FABRICATED A NEW SEAT TRACK IAW EC/TC REO 670-53-00-343. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000/400-801-A03.

Part: SEAT TRACK — CORRODED (BS 893-977) · airframe 33,495 hrs · 24,011 cycles

DURING C CHECK, FOUND SEAT TRACK CORRODED AT LBL 9 BETWEEN BS 893 - 977. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-801-A03 AND COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343 REV M.

Part: SEAT TRACK — CORRODED (BS 469-581) · airframe 33,495 hrs · 24,011 cycles

DURING C CHECK, FOUND THE SEAT TRACK AT BS 469-581, LBL 9 CORRODED. FABRICATED A NEW SEAT TRACK IAW EC/TC REO 670-53-00-343. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000/400-801-A03.

Part: SEAT TRACK — CORRODED (BS 349-469) · airframe 33,495 hrs · 24,011 cycles

DURING C CHECK, FOUND THE SEAT TRACK AT BS 349-469 RBL 9 CORRODED. FABRICATED A NEW SEAT TRACK IAW EC/TC REO 670-53-00-343. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000/400-801-A03.

Part: FLOOR SUPPORT — CORRODED (BS 280-319) · airframe 33,495 hrs · 24,011 cycles

DURING C CHECK FOUND RT FLOOR SUPPORT CORRODED FROM BS 280-319. R & R THE FLOOR SUPPORT IAW SRM 51-40-11-001-001-A01 AND 51-42 13-001-001-A01.

Part: FLOOR SUPPORT — CORRODED (BS 1015-1070) · airframe 33,495 hrs · 24,011 cycles

RBL 9 FLOOR SUPPORT CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT FROM BS 1015 - 1070 IAW REO 670-53-0369, EC/TC EO700-53-0369 AND EC/TC REO 670-53-61-1287.

Part: FLOOR SUPPORT — CORRODED (BS 349) · airframe 33,495 hrs · 24,011 cycles

DURING C CHECK, FOUND FLOOR SUPPORT AT BS 349 RBL9 CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-21-06-001-001-A01, 51-42-06-002-002-A01, AND 51-40-11-001-001-A01

Part: FLOOR SUPPORT — CORRODED (BS 1015-1070) · airframe 33,495 hrs · 24,011 cycles

LBL 9 FLOOR SUPPORT CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT FROM BS 1015 - 1070 IAW REO 670-53-61-1288, EC/TC EO700-53-0360 AND EC/TC REO 670-53-61-1288.

Part: SKIN — CHAFED (BS 969-985) · airframe 33,495 hrs · 24,011 cycles

SKIN CHAFED BY FAIRING AT BS 969 - 985. COMPLIED WITH REO 670-53-00-476 AND EC/TC REO 670-53-00-476.

Part: SIGN — BROKEN (CABIN) · airframe 32,794 hrs · 23,449 cycles

EMERGENCY EXIT SIGN HOUSING ABOVE SERVICE DOOR IS BROKEN, HANGING LOOSE. R & R EMERGENCY EXIT SIGN HOUSING ABOVE SERVICE DOOR IAW AMM 33-51-05. OPS CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 32,250 hrs · 22,998 cycles

EMERGENCY LIGHTS NOT WORKING, CHARGED AND PERFORMED OPS CHECK OF EMERGENCY LIGHTS IAW AMM 33-51-00. NO FURTHER DEFECT.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 31,160 hrs · 22,148 cycles

CAPTAIN'S SIDE FLASHLIGHT IS NOT WORKING. R & R THE FLASHLIGHT BATTERIES IAW GMM. OPS CHECKED GOOD.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 30,214 hrs · 21,349 cycles

ON SERVICE DOOR, 6 IN GLOWSTRIP MISSING. R & R SERVICE DOOR AFT GLOWSTRIP IAW AMM 20-60-04.

Part: BATTERY — INOPERATIVE (MEGAPHONE) · airframe 29,892 hrs · 21,107 cycles

MEGAPHONE INOPERATIVE. R & R MEGAPHONE BATTERIES IAW 25-61-14, OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 29,586 hrs · 20,890 cycles

EMERGENCY LIGHTS INOPERATIVE. CHARGED BATTERYS WITH SWITCH IN ARM POSTION. EMERGENCY LIGHTS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 28,996 hrs · 20,459 cycles

F/A REPORTS FORWARD FLASHLIGHT IS INOPERATIVE. REPLACED FLASHLIGHT IAW AMM 25-61-00. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 28,958 hrs · 20,430 cycles

FOUND AFT EMERGENCY LIGHTS INOPERATIVE. R & R NR 4 EMERGENCY POWER PACK & OPS CHECK GOOD IAW AMM 33-51-17, NO FURTHER FAULTS IPC 33-51-17, ITEM 6.

Part: CONNECTOR — DAMAGED (FIRE LOOP) · airframe 28,941 hrs · 20,415 cycles

FIRE SYSTEM FAULT STATUS MESSAGE MDC REPORTS LT ENGINE FIRE LOOP B OPEN. FOUND PUSHED BACK CONTACT ON CONNECTOR J551 PIN EE R & R CONTACT IAW ESPM 20-16-43, FIRE SYS FAULT IS GONE, COMPLIED WITH OPS TEST OF THE FIRE EXINGUISHER SYSTEM IAW AMM 21-10-00-710-801(A01) OPS TEST GOOD. PERMANENTLY INSTALLED CONNECTOR J551 IAW SB670BA-71-012 REV A OF THE CRJ700. IAW SB 670BA-71-012.

Part: TAB — DETERIORATED (HORIZONTAL STAB) · airframe 28,941 hrs · 20,415 cycles

TAB DETERIORATED. REPAIRED HORIZONTAL STABILIZER PIVOT FITTING ANTI-ROTATION TABS. REPAIRED IAW SB 670BA-55-012.

Part: FRAME — CORRODED (BS 311) · airframe 28,941 hrs · 20,415 cycles

CORROSION ON INTERIOR SIDE OF DOOR FRAME BS 311.75, 15 INCHES BELOW LOWER TENSION TIE BAR FWD FITTING TO 13 INCHES ABOVE LOWER TENSION TIE BAR FWD FITTING. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. BLENDED AREAS ARE OUT OF LIMITS IAW SRM 52-00-01-001-001-A01. REPAIRED IAW EA 24-2014-572. MAJOR REPAIR.

Part: STRINGER — CORRODED (BS 280) · airframe 28,941 hrs · 20,415 cycles

STRINGER 27 CORRODED AT BS 280. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-03-101-002-A01. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-20-001-001-A01 AND 51-42-06-001-001-A01. MAJOR REPAIR.

Part: SKIN — CORRODED (PAX DOOR) · airframe 28,934 hrs · 20,411 cycles

ASD DOOR INNER SKIN IS CORRODED OUT OF LIMITS IAW SRM 52-00-001-101-001-A01. REMOVED AND REPLACED IAW REO 670-52-11-793, REV.

Part: SKIN — DAMAGED (RT WING) · airframe 28,934 hrs · 20,411 cycles

RT WING LOWER SKIN INCOMING HOLE DIAMETER 0.398" AND 0.402" DO NOT AGREE WITH HOLE DIAMETER REQUIREMENT OF 0.3910"-0.3940" IAW SB670BA-53-020. COMPLIED WITH REO 670-57-21-742 REV P2 DATED SEP 29,2014.

Part: SKIN — CRACKED (RT WING) · airframe 28,934 hrs · 20,411 cycles

ONE CRACK INDICATION IN RT WING LOWER SKIN. REPAIRED IAW IAW REO 670-57-21-742, REV P1, P2, P3, P4, P5, P6, P7 AND P8.

Part: SKIN — CRACKED (RT WING) · airframe 28,934 hrs · 20,411 cycles

FOUND A CRACK INDICATION IN RT WING LOWER SKIN. REPAIRED IAW REO 670-57-21-742, REV P1, P2, P3, P4, P5, P6, P7.

Part: ANGLE — CORRODED (PAX DOORWAY) · airframe 28,933 hrs · 20,410 cycles

AFTER REMOVAL OF PAX DOOR SILL ANGLE, TOP ANGLE FOUND LOWER CAP ANGLE TO BE CORRODED ALONG THE NUTPLATE HOLES AND NUTPLATES. CORROSION ON PAX DOOR LWR SILL ANGLE FOUND TO BE OUT OF LIMITS IAW SRM 53-21-23-101-001-A01, REMOVE LOWER SILL ANGLE. REMOVED 2EA DOOR HINGES AND LWR SILL ANGLE AT PAX DOOR IAW SRM 51-42-20-001-001-A01 AND 51-42-00-001-001-A01. LOCATED & DRILLED NEW LWR SILL ANGLE IAW SRM 51-40-11-001-001-A01. REINSTALLED 2 EA DOOR HINGES FITTINGS IAW SRM 51-42-21-001-00-A01 AND DWG SH670-31810. INSTALLED NEW LWR SILL ANGLE AT PAX DOOR THRESHOLD IAW SRM 51-42-06-001-001-A01.

Part: ANGLE — CRACKED (DOOR LEVER) · airframe 28,933 hrs · 20,410 cycles

CRACK ON INNER ANGLE OF ATTACHMENT STRUCTURE FOR INNER DOOR LEVER. REMOVED AND REPLACED THE ANGLE, IAW PJ162163, SRM 51-42-06-001-001-A01, AND SRM 51-40-11-001-001-A01.

Part: PLATE — CRACKED (CARGO DOOR) · airframe 28,933 hrs · 20,410 cycles

FWD CARGO BAY DOOR LOWER PLATE IS CRACKED. REMOVED LOWER PLATE IAW AMM 52-35-07-000-802-A01. FITTED AND DRILLED NEW LOWER PLATE IAW DRN LE670-39647, SRM 51-40-11-001-001-A01. INSTALLED SERVICEABLE LOWER PLATE IAW AMM TASK 52-35-04-410-802.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 28,933 hrs · 20,410 cycles

FLOORBEAM ANGLE CRACKED BS 280 LBL 26. R & R CRACKED ANGLE IAW SRM 51-42-06-001-001-A01 AND DWG CC670-34117. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 28,933 hrs · 20,410 cycles

CORROSION ON FLOORBEAM AT BS 280, LBL 35. BLENDED DAMAGE AREA AND FOUND TO BE IN LIMITS IAW SRM 51-21-06-001-001.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 28,933 hrs · 20,410 cycles

BS 280 FLOORBEAM LT SIDE CORRODED. REMOVED CORRODED FLOORBEAM AND REPLACED IAW SB670BA-53-041.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 28,933 hrs · 20,410 cycles

FLOOR SUPPORT CORRODED. REMOVED AND REPLACED THE CORRODED ANGLE IAW SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01 AND 51-42-21-001-001-A01.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 28,933 hrs · 20,410 cycles

BS 280 FLOORBEAM RT SIDE CORRODED. REMOVED CORRODED FLOORBEAM AND REPLACED IAW SB670BA-53-041.

Part: ATTACH ANGLE — CRACKED (LT MLG WW) · airframe 28,933 hrs · 20,410 cycles

PANEL 194AB, ATTACH ANGLE CRACKED LT MLG W/W. REMOVED ANGLE FROM ACFT AND FABRICATED NEW ANGLE IAW EA 32-2014-120, SECTION 1. COMPLIED WITH EA 32-2014-120, REV P1.

Part: COVER — DAMAGED (POWER CABLE) · airframe 28,933 hrs · 20,410 cycles

APU STARTER POWER CABLES ABRADABLE SHEATH TORN. WRAPPED APU POWER CABLES WITH ELECTRICAL INSULATING TAPE IAW GREO 670-24-22-001, REV A. COMPLIED WITH GREO REO 670-24-22-001, REV A DATED 11-25-2010. REPAIRED APU POWER OUTPUT CABLE IAW REO 670-24-22-001, REV A COMPLIED ECTC REO 670-24-22-001. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 28,933 hrs · 20,410 cycles

COCKPIT FLOORBOARD 221ALF AFT FLOORBEAM ANGLE AT BS 280 CORRODED. REMOVED CORRODED ANGLE AND REPLACED IAW SB 670BA-53-041.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 28,933 hrs · 20,410 cycles

LEFT BS 280, LOWER WEB IS CORRODED. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. BLENDED CORROSION DAMAGE IAW SRM 51-21-06-001-001-A01. REPAIRED IAW REO 670-53-11-594, DATED APR. 27, 2011.

Part: SKIN SPLICE — CORRODED (BS 280) · airframe 28,933 hrs · 20,410 cycles

CIRCUMFERENTIAL SPLICE JOINT AT FS 280 INNER SKIN CORRODED BETWEEN STR 24LT-24RT. REMOVED CORROSION AT FS 280 BETWEEN STR 27-26R AND BETWEEN STR 25R-24R IAW SRM 51-21-06-001-001-A01. REMOVED CORROSION FROM FS 280, ST 26L-25L AND STR 26R-25R IAW SRM 51-21-06-001-001-A01. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702.

Part: DOOR FRAME — CORRODED (E/E BAY) · airframe 28,933 hrs · 20,410 cycles

AVIONICS BAY DOOR CUT-OUT, ENTIRE CUTOUT, CORRODED. BLENDED CORROSION ALONG THE FWD EDGE OF THE AVIONICS BAY DOOR CUT OUT IN REF TO SRM 51-21-06-001-001-A01, CORROSION IN A NON DAMAGEABLE AREA. THIS REPAIR IS CLASSIFIED AS MAJOR REPAIR IAW SOP 5702. COMPLIED WITH ECTC REO 670-53-21-242 AND REO 670-53-21-242, REV B DATED 07-29-2014.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 28,933 hrs · 20,410 cycles

RIGHT BS 280 LOWER WEB IS CORRODED. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. BLENDED CORROSION DAMAGE IAW SRM 51-21-06-001-001-A01. REPAIRED BLENDED AREA AT RT 280, LOWER WEB IAW SRM 53-11-10-201-003-A01, PARA 3.B (1)-3.C.

Part: DOUBLER — GOUGED (BS 977) · airframe 28,933 hrs · 20,410 cycles

REPAIR DOUBLER GOUGED AT BS 977. REPAIRD IAW REO 670-53-00-421 REV-A MAJOR REPAIR.

Part: FRAME — CORRODED (BS 319) · airframe 28,933 hrs · 20,410 cycles

FRAME 319.70 CORRODED FWD SIDE BETWEEN STR 26RT-26LT. BLENDED OUT CORROSION ON FRAME ATTACH FLANGE AND IN RADIUS IAW SRM 51-21-06-001-001-A01 FRAME OUT OF LIMITS IAW SRM 53-21-06-101-002-A01. BLENDED CORROSION ON FRAME 319.70 BETWEEN STR 27 AND 26L IAW SRM 51-21-06-001-001-A01 OUT OF LIMITS IAW SRM 51-21-06-101-002-A01. REMOVED REMAINDER OF CORROSION FROM FWD SIDE OF FRAME 319.70 BETWEEN STR 26R-26L IAW SRM 51-21-06-001-001-A01.

Part: FRAME — CORRODED (BS 333) · airframe 28,933 hrs · 20,410 cycles

FRAME BS 333 CORRODED AFT SIDE AT STR 27. REMOVED CORROSION FROM FRAME 333 AT AFT SIDE OF FRAME ON STR 27 LOCATION IAW SRM 51-21-06-001-001-A01.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 28,933 hrs · 20,410 cycles

INTERCOSTAL CORRODED AT S27R, BETWEEN BS 349 & 364. REMOVED CORROSION IAW 51-21-06-001-001-A01.

Part: VENT — GOUGED (PAX DOOR) · airframe 28,912 hrs · 20,393 cycles

ASD VENT FLAP GOUGED. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. BLENDED GOUGED AREA OF ASD VENT FLAP IAW SRM 51-12-00-001-001-A01, TEMP REV 51-12-00-001-001-A01, TEMP REV 51-005D. REPAIR OF THE DAMAGE ON THE PRESSURE VENT ON PAX DOOOR IS COMPLETED IAW 670-52-11-238 AND MEETS WITH ALL ITS REQUIREMENTS. COMPLIED WITH GREO 670-52-11-238.

Part: FITTING — CRACKED (PAX DOOR) · airframe 28,912 hrs · 20,393 cycles

REINFORCEMENT FITTING ON ASD FS 338.963 HAS CRACK ON REINFORCEMENT FITTING INSIDE PANEL 832AR. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. REMOVED CRACKED PULL IN CAM DOUBLER, PN 601R31-8094-2 IAW SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. REMOVED AFT ASD PULL IN LEVER, BEARING HOUSING AND TQ TUBE FOR ACCESS IAW CRJ700 AMM 52-11-02-000-806, CONFIG A01 & SRM 51-42-21-001-001-A01. INSTALLED TQ TUBE, BEARING HOUSING AND PULL IN LEVER ON AFT SIDE OF ASD IAW AMM 52-11-02-400-806 AND SRM 51-42-21-001-001-A01. INSTALLED PULL IN CAM DOUBLER AFT SIDE OF ASD IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.

Part: FRAME — GOUGED (LT NACELLE) · airframe 28,912 hrs · 20,393 cycles

LEFT AFT CORE COWL MID FRAME GOUGED. REMOVED DAMAGE IAW SRM 54-13-00-101-001-A01. FROM AFDL 520336, Z MID JOINT OUT OF LIMITS DUE TO BLEND AREA WITHIN 2D OF FASTENER NEEDS TO BE SUBMITTED FOR REPAIR. RECEIVED AND COMPLIED WITH STS EA 32-2014-102, SECTION I- PERMANENT REPAIR. RECEIVED ECTC EA 32-2014-102, REV 1R AND ACCOMPLISHED ALL STEPS.

Part: DOOR SILL — CORRODED (PAX DOOR) · airframe 28,933 hrs · 20,410 cycles

DURING AVDEC INSPECTION, FOUND CORROSION AT PAX DOOR AT BS 315, LBL 35 ON SILL STRUCTURE. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-42-06-001-001-A01, 51-41-02-001-001-A01 AND DWG SH670-31810.

Part: DOOR SILL — CORRODED (BS 340) · airframe 28,933 hrs · 20,410 cycles

DURING AVDEC INSPECTION, FOUND CORROSION AT PAX DOOR AT BS 340 LBL 35.SILL STRUCTURE REMOVED AND REPLACED IAW SRM 51-42-06-001-001-A01, 51-41-02-001-001-A01, AND DWG SH670-31810.

Part: HOUSING — GOUGED (CARGO DOOR HANDL) · airframe 28,933 hrs · 20,410 cycles

AFT CARGO DOOR HANDLE HOUSING GOUGED. REMOVED HANDLE IAW AMM 52-31-03-000-801 A01, DRILLED NEW SERVICEABLE HANDLE ASSY AND INSTALLED IAW SRM 52-31-03-400-801 A01 AND SRM 51-42-21-001-001-A01. MAJOR REPAIR .

Part: PANEL — CRACKED (PAX DOOR) · airframe 28,912 hrs · 20,393 cycles

ASD UPPER MID STEP AFT SIDE PANEL CRACKED. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. REMOVED AFT SIDE PANEL, PN 601R-31707-7 IAW SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01. NEW SIDE WALL PANEL TO BE INSTALLED.

Part: DOOR SILL — CORRODED (BS 349) · airframe 28,933 hrs · 20,410 cycles

DURING AVDEC INSPECTION, FOUND CORROSION AT PAX DOOR AT BS 349, LBL 35 SILL STRUCTURE. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-42-06-001-001-A01, 51-41-02-001-001-A01, AND DWG SH670-31810.

Part: PANEL — CRACKED (PAX DOOR) · airframe 28,912 hrs · 20,393 cycles

ASD BOTTOM STEP FWD SIDE PANEL CRACKED. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. FWD SIDE PANEL, PN 601R317071-8, REMOVED IAW SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01. REMOVED SUPPORT STRUCTURE FROM SIDE PANEL SKIN IAW SRM 51-42-06-001-001-A01. INSTALLED SUPPORT STRUCTURES ON NEW SIDE PANEL, PN 601R317071-8 IAW SRM 51-42-06-001-001-A01 & DWG 601317071, REV E. INSTALLED FWD SIDE PANEL ON PAX DOOR IAW SRM 51-42-06-001-001-A01, DWG 601R31772 & DWG 601R317071.

Part: FLOOR PANEL — CRACKED (BS 193) · airframe 28,905 hrs · 20,389 cycles

FORWARD EQUIPMENT COMPARTMENT FLOOR CRACKED AT SIDE FS 193. REPAIRED IAW ECTC REO 670-53-11-509, REV A, REV. MAJOR REPAIR.

Part: FLOOR PANEL — CRACKED (E/E BAY) · airframe 28,905 hrs · 20,389 cycles

FORWARD EQUIPMENT COMPARTMENT FLOOR CRACKED LT SIDE, FS 193.00. REPAIRED IAW REO 670-53-11-509, REV B. MAJOR REPAIR.

Part: SKIN — DAMAGED (RT NACELLE) · airframe 28,905 hrs · 20,389 cycles

RT ENGINE CORE COWL HAS CHAFE DAMAGE DUE TO CONTACT WITH GREEN HARNESS. REPAIRED IAW REO 670-54-23-959. MAJOR REPAIR.

Part: LIGHT — DAMAGED (CABIN) · airframe 28,905 hrs · 20,389 cycles

EMERGENCY LIGHT BROKEN AND DEBONDED. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-51-01-000-801-A03 AND AMM 33-51-01-400-801-A03.

Part: SKIN — DENTED (LT NACELLE) · airframe 28,920 hrs · 20,402 cycles

LEFT ENGINE LOWER FWD COWL DOOR DENTED. REPAIRED IAW EA 32-2014-098, REV 1R.

Part: ATTACH ANGLE — CRACKED · airframe 28,920 hrs · 20,402 cycles

VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE CRACKED LT SIDE AT APPROX STR DATUM 55.62 PERCENT. FOUND TO BE OUT OF LIMITS IAW SRM 55-00-00-101-001. INSTALLED NEW SERVICEABLE ATTACH ANGLE IAW DWG JBA 670-23103, & SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01.

Part: SKIN — DENTED (NR 1 SLAT) · airframe 28,920 hrs · 20,402 cycles

DENT ON LEFT NR 1 SLAT SS 135.75. FOUND TO BE OUT OF LIMITS IAW SRM 57-42-01-101-001-A01. REPAIRED IAW EA 25-2014-275 ITEM 3 COMPLIED WITH ITEM 4 .

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 28,920 hrs · 20,402 cycles

VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE CRACKED RT SIDE AT APPROX STG DATUM 55.62 PERCENT. EVALUATED DAMAGES TO BE OUT OF LIMITS IAW SRM 55-00-00-101-001. SUMITTED TO ENGINEERING FOR PERMANENT REPAIR DISPOSITION. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. RECEIVED RESPONCE FROM THD REF: ADR JLFB-14-26550542, CAR 83335, PART HAS TO BE REPLACED. REMOVED DAMAGED RT DRAG ANGLE AT STR DATYUM 55.62 PERCENT IN REF TO SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. LOCATED HOLES COMMON TO FUSELAGE FOUND PREDRILLED PILOT HOLES ON DRAG ANGLE 73EA MISMATCHED FROM HOLES ON VERTICAL SKIN REF SRM 51-40-11-001-001-A01 AND DWG BA670-23-103.

Part: ANGLE — CHAFED (BS 1144) · airframe 28,774 hrs · 20,284 cycles

FOUND CHAFING DAMAGE AT FS 1144.00 STR 9R CAUSED BY WATER SENSE LINE BONDING CLAMP. RECEIVED AND COMPLIED DISPOSITION REO 670-53-61-1084. THIS IS CLASSIFIED AS A MAJOR REPAIR, ALL STEPS ARE CONSIDERED RII. CUT AWAY DAMAGE AT FRAME 1144 BETWEEN STR8R AND STR9R REF REO 670-53-61-1084. FABRICATED, -1 REPAIR ANGLE IAW FLAG, NOTE 11 FROM EXTRUSION, PN-S1710-2 BATCH 1854589, TRIMMED TO FIT SURRONDING STRUCTURE. PICKED UP EXISTING AND ADDED FASTENER HOLES, ALL WORK ACCOMPLISHED IAW REO 670-53-61-1084 FAY SEALED AND WET INSTALLED ALL FASTENERS, AND APPLIED SURFACE FINISH. ALL WORK ACCOMPLISHED IAW REO 601R-53-61-1084, CREATED M-318 IAW SOP 5702.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 28,774 hrs · 20,284 cycles

F/A FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT BATTERIES AND OPS CHECKED IAW AMM 25-61-00.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 28,555 hrs · 20,111 cycles

MEGAPHONE DOESN'T WORK. R & R MEGAPHONE IAW AMM 25-61-14 5. OPS CHECKED GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 28,498 hrs · 20,068 cycles

SIDE WALL LIGHT AT RT EMERGENCY EXIT IS OUT. R & R SIDE WALL LIGHT LAMP AT RT EMERGENCY EXIT IAW 33-21-07.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 28,471 hrs · 20,049 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 7 INOPERATIVE. REPLACED THE LAMP AT ROW 7 EMERGENCY LIGHT IAW AMM 33-51-09. OPS TESTED GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 27,329 hrs · 19,233 cycles

INTERIOR CEILING EMERGENCY LIGHT AT 7 ABCD IS OUT. REPLACED LAMPS AND OPS CHECKED GOOD IAW AMM 33-51-00.

Part: FLOOR PANEL — DAMAGED · airframe 26,452 hrs · 18,590 cycles

DURING INSPECTION OF PRESSURE FLOOR PANEL AWL7 53-41-117. FOUND EXISTING DAMAGE AND BLEND OUT AROUND HYD UNION NR 3 ON LT SIDE UPPER SURFACE BETWEEN LBL 9.00 AND LBL 18.00 AND BETWEEN FS 693.00 AND 847.00. REPAIRED IAW REO 670-53-41-186. THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 26,400 hrs · 18,546 cycles

ON ARRIVAL TO THE ACFT WITH GROUND POWER DISCONNECTED, FOUND EMERGENCY LIGHTS SWITCH IN ARMED POSITION, EMERGENCY LIGHTS INOP. CHARGED EMERGENCY LIGHTS, OPS TEST GOOD IAW AMM 33-51-00. AC OK FOR SERVICE.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 26,252 hrs · 18,436 cycles

EMERGENCY LIGHT LENS ENTRY DOOR CRACKED. REPLACED EMERGENCY LIGHT LENS IAW AMM 33-51-15. ACFT OK FOR SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (LAV SMOKE DETECT) · airframe 24,723 hrs · 17,349 cycles

AFT LAVATORY SMOKE WARNING ON APROACH, WARNING EXTINGUISHED AFTER APROX 4 MINUTES. INSPECTED AFT LAVATORY, NO SMOKE FOUND, TESTED LAVATORY SMOKE DETECTOR, OPS CHECKED GOOD IAW AMM 26-16-00. ACFT OK FOR SERVICE.

Part: DOUBLER — CRACKED (BS 280) · airframe 24,509 hrs · 17,179 cycles

DURING REPLACEMENT OF FS 280 TRANSVERSE BEAM, FOUND BOTH LT & RT UPPER ANGLE DOUBLERS TO BE CRACKED APPROX 1 INCH LONG. LOCATED & DRILLED FASTENER HOLES FOR SERVICEBLE ANGLE DOUBLERS IAW SRM 51-40-11-001-001-A01. INSTALLED IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01 AND SRM 51-42-22-001-001-A01.

Part: CHANNEL — CORRODED · airframe 24,526 hrs · 17,189 cycles

FOUND LT LOWER FLIGHT DECK ENTERANCE JAMB AT LBL 9 CORRODED. FOUND CORROSION OUT OF LIMITS. COMPLIED WITH REO 670-53-11-745 IAW NDTM PT01, 51-20-006-250-A01 AND IAW NDTM PT01, 51-20-008-230-A01. FOUND TO BE SATISFACTORY.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 24,509 hrs · 17,179 cycles

PAX DOOR FWD CORNER CORRODED BEYOND LIMITS. REMOVED DAMAGED FWD CORNER IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. INSTALLED PAX DOOR FWD CORNER IAW SRM 51-42-21-001-001-A01 & SRM 51-42-06-001-001-A01.

Part: CHANNEL — CORRODED (BS 280) · airframe 24,509 hrs · 17,179 cycles

FS 280 FWD "J" CHANNEL IS CORRODED BEYOND REPAIR. CORROSION GOES ALL THE WAY THROUGH THE PART. REMOVED CHANNEL IAW SRM 51-42-06-001-001-A01 & SRM 51-42-21-001-001-A01. LOCATED & DRILLED NEW CHANNEL IAW SRM TASK 51-40-00-001-001-A01. INSTALLED CHANNEL IAW SRM 51-42-21-001-001-A01 AND SRM 51-42-06-001-001-A01.

Part: FLOOR SUPPORT — CORRODED (BS 280-319) · airframe 24,526 hrs · 17,189 cycles

RT FLOOR SUPPORT CORRODED FROM FS 280 - 319. REMOVED RT FLOOR SUPPORT FROM FS 280 TO 319 IAW SRM 51-42-06 & 51-42-21. LOCATED, DRILLED & INSTALLED NEW FLOOR SUPPORT IAW SRM 51-40-11-001-001-A01, SRM 51-42-06-001-001-A01 & SRM 51-42-13-001-001.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 24,524 hrs · 17,188 cycles

SERVICE DOOR LOWER SILL AND ANGLE HAVE SEVERAL AREAS OF CORROSION. REMOVED SERVICE DOOR LOWER SILL AND ANGLE IAW SRM 51-42-06-001-001-A01. LOCATED, DRILLED AND SUBASSEMBLED THE NEW SILL ANGLE TO THE NEW UPPER ANGLE IAW THE SRM 51-40-11-001-001, 51-42-06-001-001. INSTALLED NEW SERVICEABLE SERVICE DOOR SILL ANGLE IAW SRM TASK 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.

Part: FINGER DOUBLER — CORRODED (BS 295-310) · airframe 24,509 hrs · 17,179 cycles

RT FLOOR SILL FINGER DOUBLER FROM FS 295 TO FS 310 IS CORRODED. LOCATED AND INSTALLED NEW FINGER DOUBLER ON NEW RT FLOOR SILL IAW SRM 51-42-06-001-001-A01.

Part: SILL — CORRODED · airframe 24,509 hrs · 17,179 cycles

PAX DOOR SILL ANGLE HAS CORROSION AROUND FASTENER HOLES. REMOVED CORRODED PAX DOOR SILL ANGLE. LOCATED DRILLED NEW PARTS IAW SRM 51-40-11-001-001-A01, INSTALLED NEW PARTS IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-45-00-001-001-A01.

Part: CROSSBEAM — CORRODED (BS 280) · airframe 24,526 hrs · 17,189 cycles

FS 280.00 CROSSBEAM CORRODED IN NUMEROUS AREAS. REMOVED CROSSBEAM IAW SRM 51-42-06-001-001-A01 & SRM 51-42-21-001-001-A01 & SRM 51-42-10-001-001-A01.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 24,473 hrs · 17,153 cycles

EMERGENCY LIGHT OVER GALLEY SERVICE DOOR INOPERATIVE. FOUND CONNECTOR AT GALLEY SERVICE LIGHT HAD PUSHED OUT. ATTACHED AND FUNCTION TESTED IAW AMM 33-50-00. NO FURTHER DEFECT NOTED.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 23,732 hrs · 16,582 cycles

F/A REPORTS PHOTOLUMINESCENT STRIPS MISSING IN FRONT OF FIRST CLASS CLOSET. INSTALLED LT AND RT PHOTOLUMINESCENT STRIPS IN FRONT OF FIRST CLASS CLOSET IAW AMM 33-51-01.

Part: BATTERY — WEAK (FLASHLIGHT) · airframe 20,193 hrs · 14,085 cycles

FWD F/A FLASHLIGHT WEAK & INTERMITTENT. R & R FWD F/A FLASHLIGHT BATTERIES, REF AMM 25-60-00.

Part: BATTERY — WEAK (FLASHLIGHT) · airframe 20,193 hrs · 14,085 cycles

AFT F/A FLASHLIGHT WEAK & INTERMITTENT. R & R AFT F/A FLASHLIGHT BATTERIES REF AMM 25-60-00.

Part: BATTERY — WEAK (FLASHLIGHT) · airframe 20,193 hrs · 14,085 cycles

CAPT FLASHLIGHT WEAK & INTERMITTENT. R & R CAPT FLASHLIGHT BATTERIES REF AMM 25-60-00. (CLOSED)

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 19,934 hrs · 13,902 cycles

CROSSBEAM FOUND TO BE CORRODED AT RT AND LT SIDE PANEL NUTPLATE LOCATIONS. INSTALLED 5 EA RIVETS CROSSBEAM IAW SRM 51-42-06-001-001-A01. RESTORED A023 FINISH IAW SRM 51-21-16-001-001-A01. APPLIED CIC AT REPAIRED AREA IAW SRM 51-21-11-001-001-A01.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 19,934 hrs · 13,902 cycles

BOTH EMERGENCY EXIT LIGHT LENS COVERS CRACKED ON WARDROBE AT ASD ENTRANCE. ( OPEN )

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 19,934 hrs · 13,902 cycles

EMERGENCY EXIT LIGHT COVER CRACKED AT SERVICE DOOR (GALLEY ACCESS PANEL). (OPEN)

Part: ANGLE — CORRODED (FUSELAGE) · airframe 19,934 hrs · 13,902 cycles

SERVICE DOOR LOWER SILL ANGLE IS CORRODED OUT OF LIMITS. (OPEN)

Part: SEAT TRACK — CORRODED (CABIN) · airframe 19,934 hrs · 13,902 cycles

SIDE WALL SEAT TRACK HAS CORROSION JUST FWD OF RT EMERGENCY EXIT. REMOVED SEAT TRACK IAW AMM 53-00-000-801. INSTALLED SIDE WALL SEAT TRACK IAW AMM 53-00-49-400-801.

Part: FLOOR SUPPORT — CORRODED (BS 319-333) · airframe 19,934 hrs · 13,902 cycles

BETWEEN FS 319.00 AND FS 333.00, RBL 36.00 FLOOR SUPPORT HAS CORROSION. (OPEN)

Part: FLOOR SUPPORT — CORRODED (BS 349-364) · airframe 19,934 hrs · 13,902 cycles

BETWEEN FS 349.00 AND FS 364.00 AT RBL 36.0, FLOOR SUPPORT SILL PLATE HAS CORROSION. (OPEN)

Part: BULKHEAD — CORRODED (BS 280) · airframe 19,934 hrs · 13,902 cycles

FS 280.00 BULKHEAD LT AFT SIDE AT WL73.50 JUST ABOVE FLOOR SUPPORT STRUCTURE BETWEEN LBL9.00 AND LBL18.00 HAS CORROSION.

Part: SILL — CORRODED (BS 280-319) · airframe 19,934 hrs · 13,902 cycles

BETWEEN FS 280.00 AND FS 319.70 AT RBL 36.00 FLOOR SUPPORT SILL PLATE HAS CORROSION. (OPEN)

Part: SHIM — CORRODED (BS 333 FLOORBEAM) · airframe 19,934 hrs · 13,902 cycles

FS 333.00, RBL 9.00, FLOORBEAM SHIM INBD AND OTBD ATTACH POINTS CORRODED. (OPEN)

Part: FLOORBEAM — CORRODED (BS 349) · airframe 19,934 hrs · 13,902 cycles

FS 349.00 BETWEEN RBL 9.00 AND RBL 18.00 FLOORBEAM HAS 1EA BROKEN AND CORRODED SCREW. R & R NUTPLATE AND SCREW IAW SRM CH 51-42-15-001-001. (CLOSED)

Part: FLOOR SUPPORT — CORRODED (BS 698-830.4) · airframe 19,934 hrs · 13,902 cycles

FLOOR SUPPORT CAP CORRODED UNDER SEAT TRACK FROM FS 698 TO FS 830.4. BLENDED CORROSION IAW SRM 51-12-00-001-001-A01. NO DAMAGE ALLOWED ON FLOOR SUPPORT CAP IAW SRM 51-41-00-001-001-A01.

Part: STRINGER SPLICE — CORRODED (BS 333 S25R) · airframe 19,934 hrs · 13,902 cycles

REMOVED STRINGER SPLICE 25R AT FS 333 IAW SRM 51-42-06-001-001-A01. SPLICE WAS REMOVED AND FOUND TO BE CORRODED A SPLICE ORDERED AND RECEIVED. LOCATED AND DRILLED EXISTING HOLES IN NEW STRINGER SPLICE. INSTALLED NEW STRINGE SPLICE WET IAW SRM 51-42-06-001-001-A01 & 51-42-20-001-001-A01 & 51-23-00-001-001-A01.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 19,934 hrs · 13,902 cycles

LIGHT CORROSION ON THE FLOOR SUPPORT CHANNEL WHICH IS MOUNTED TO FS 280 FRAME BETWEEN STGR 26L AND 26R. R & R FLOORBOARD SUPPORT ANGLE AT FS280 BETWEEN STGR 26L AND 26RT PN CC670-34-256-3 IAW SRM 53-11-10-991-803 AND 51-42-06-001-001-A01 AND REAPPLIED A023 FINISH AND CIC IAW SRM 51-25-00-001-001 AND 51-21-16-001-001. (CLOSED)

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 19,934 hrs · 13,902 cycles

RT FUSELAGE AFT EMERGENCY LIGHT LENS IS CRACKED. INSTALLED NEW LENS IAW AMM 33-51-15-400-801.

Part: CROSSBEAM — CORRODED (BS 280) · airframe 19,934 hrs · 13,902 cycles

BS 280 CROSSBEAM FOUND TO BE CORRODED AT RT AND LT SIDE FLOOR PANEL NUTPLATE LOCATIONS. FOUND DAMAGED AREA TO BE OUT OF LIMITS IAW SRM. REMOVED CROSSBEAM IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-42-13-001-001-A01. INSTALLED NEW CROSSBEAM IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-42-13-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 379-485) · airframe 19,934 hrs · 13,902 cycles

SEAT TRACK 9L AT FS 379 TO FS 485 HAS CORROSION ON SIDE OF TRACK AND IS UNSERVICEABLE. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 19,934 hrs · 13,902 cycles

LT FUSELAGE AFT EMERGENCY LIGHT LENS IS CRACKED. R & R EMERGENCY LIGHT LENS IAW AMM 20-21-00-910-801.

Part: SEAT TRACK — CORRODED (BS 83.4-644) · airframe 19,934 hrs · 13,902 cycles

SEAT TRACK 9 R AT FS 677 TO 83.40 IS CORRODED. REMOVED UNSERVICEABLE SEAT TRACK & INSTALLED IAW AMM 53-00-49-400-801.

Part: FLOORBEAM — CORRODED (BS 479) · airframe 19,934 hrs · 13,902 cycles

CORROSION ON TOP OF FLOORBEAM 9L AROUND SEAT TRACK AND FLOOR PANEL NUTPLATE HOLES AT FS 479. BLENDED CORRODED AREA. COMPLIED WITH NDT STEP 2 OF REO 670-53-31-177, NO INDICATIONS NOTED. COMPLIED WITH STEPS 3-5 OF REO 670-53-31-177.

Part: FLOOR SUPPORT — CORRODED (BS 686-698) · airframe 19,934 hrs · 13,902 cycles

FLOORBEAM CAP CORRODED UNDER SEAT TRACK FROM APPROX FS 686 TO FS 698. REPAIRED IAW REO 670-53-41-109.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 19,934 hrs · 13,902 cycles

SEAT TRACK 9R AT FS 485 TO FS 581 CORRODED AND UNSERVICEABLE. REMOVED SEAT TRACK IAW SRM 51-47-02-001-0001-A01. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 581-677) · airframe 19,934 hrs · 13,902 cycles

SEAT TRACK 9R AT FS 581 TO FS 677 HAS MINOR SURFACE CORROSION. REMOVED SEAT TRACK AT 9R, FS 581 TO FS 697 IAW SRM51-41-02-001-001-A01. INSTALLED NEW SEAT TRACK. FABRICATED NEW SEAT TRACK USING SEAT TRACK EXTRUSTION PN N126-2075 6, TRIMED BACK UPPER FLANGE ON END IAW ORIGINAL LOCATED MOUNTED HOLES USING SEAT TRACK DRILL BUSHING. REAMED HOLES TO .1935 DIAMETER AND COUNTER SUNK HOLES FOR 100 DEGREES TENISON HEAD SCREW. INSTALL NEW SEAT TRACK PJ80054 10/12/10 (KF). OK TO INSTALL SEAT TRACK (SH670-3342-3) INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801-A01. (CLOSED)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 19,533 hrs · 13,580 cycles

LT AFT EXT EMERGENCY LIGHT INOP. RELAMPED LT AFT EXT EMERGENCY LIGHT IAW AMM 33-51-15, OPS CHECK GOOD. (CLOSED)

Part: SEAT TRACK — CORRODED (BS 364-549) · airframe 19,004 hrs · 13,183 cycles

MAIN PASSENGER CABIN RT FLOOR SEAT TRACK STA 364 TO 549 HAS CORROSION. SEAT TRACK FOUND TO BE OUT OF LIMITS REMOVED SEAT TRACK RT STA 364 TO STA 485 RCVD NEW RT SEAT TRACK PN SHO670-32159-1, PO 30340005 AND INSTALLED RT SEAT TRACK IAW SRM 51-41-02. BLENDED RT SEAT TRACK FROM STA 485 TO STA 549, REMOVED .004 AT STA 485 REMOVED .010 AT STA 501, REMOVED .007 AT STA 517 AND REMOVED .005 AT STA 533 MAXIMUM BLEND IS .035 WITHIN LIMITS IAW SRM 53-21-49-991-804.

Part: UNKNOWN — MALFUNCTIONED (NLG) · airframe 17,880 hrs · 12,332 cycles

ON NOSE WHEEL TOUCH DOWN ACFT PULLED LT AND EXITED RUNWAY. (EMERGENCY DECLARED)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,649 hrs · 11,360 cycles

RT FLOOR EMERGENCY LIGHTS AT SERVICE BAY DOOR HAS 2 INOP BULBS

Part: STEP — CRACKED (ASD) · airframe 16,525 hrs · 11,259 cycles

ASD BOTTOM STEP CRACKED.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 14,942 hrs · 10,055 cycles

CORROSION ON SEVERAL LOCATIONS OF THE BELLY SKIN DOUBLER JUST AFT OF FS 280 BETWEEN STR 25L AND 25R.

Part: FRAME — CORRODED (FUSELAGE) · airframe 14,942 hrs · 10,055 cycles

CORROSION AT AFT SIDE OF FS 295 FRAME BETWEEN STR 26L AND 26R. 9/13/2008 SUP- RESOLVED ON W/O 99022 TASKCARD NR 00165. WORK COMPLETED IAW: REMOVED (6) RIVETS FROM FS 295 BETWEEN STR 26L AND 26R TO GAIN ACCESS TO THE CORROSION. REMOVED .003" OF CORROSION FROM THE FS295 WITHIN LIMITS IAW CRJ700 SRM 53-21-06. REINSTALLED RIVETS AND ALODINE, PRIME, PAINTED FS 295 FRAME IAW CRJ 700 SRM 51-42-06. REINSTALLED RIVETS AND ALODINE, PRIME, PAINTED FS 295 FRAME IAW CRJ 700 SRM 51-42-06. DK 7022603 JOB COMPLETE 9/15/2008. (K)

Part: FRAME — CORRODED (FUSELAGE) · airframe 14,942 hrs · 10,055 cycles

CORROSION AT FWD SIDE OF FS 319 FRAME BETWEEN STR 26 AND 27L. 9/15/2008 SUP - W/O 99022 TASKCARD N/R 00164) WORK COMPLETED IAW REMOVED 5 RIVETS FROM THE 319 TO GAIN ACCESS TO THE CORROSION. REMOVED .004 OF CORROSION FROM THE FS 319 WITHIN LIMITS IAW CRJ 700 SRM 53-21-06. REINSTALLED RIVETS AND ALODINE, PRIME, PAINTED FS 319 FRAME IAW CRJ 700 SRM 51-42-06. DK 7022603 JOB COMPLETE. (K)

Part: WEB — CORRODED (FUSELAGE) · airframe 14,942 hrs · 10,055 cycles

LT 280 WEB CORRODED.

Part: BEAM — CORRODED (FUSELAGE) · airframe 14,942 hrs · 10,055 cycles

LT SIDE OF 280 BEAM CORRODED

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 14,942 hrs · 10,055 cycles

LT AFT V/STAB TO FUSELAGE DRAG ANGLE CRACKED AT 67.5% REAR SPAR DATUM.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 14,942 hrs · 10,055 cycles

RT AFT V/STAB TO FUSELAGE DRAG ANGLE CRACKED AT 67.5% REAR SPAR DATUM.

Part: WEB — CORRODED (FUSELAGE) · airframe 14,942 hrs · 10,055 cycles

RT 280 WEB CORRODED.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 14,942 hrs · 10,055 cycles

FWD ANGLE OF 280 BEAM (COCKPIT FLOOR LAND) BADLY CORRODED. SUP - REMOVED FWD ANGLE OF THE 280 BEAM ( COCKPIT LAND) IAW CRJ 700 SRM 51-42-06. CB 7015474 DRILLED NEW FWD ANGLE TO NEW FS 280 BEAM IAW CRJ 700 SRM 51-42-06 AND 51-42-13. (K)

Part: BEAM — CORRODED (FUSELAGE) · airframe 14,942 hrs · 10,055 cycles

RT SIDE OF 280 BEAM CORRODED.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 14,942 hrs · 10,055 cycles

CRACKED DRAG ANGLE RT LOWER VERT STAB. MARKED.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB)

CRACKED DRAG ANGLE RT LOWER VERT STAB (MARKED). PERFORMED EDDY CURRENT INSPECTION OF RT V/ STAB TO FUSELAGE DRAG ANGLE IAW CRJ 700 NDTM 51-20-006. DRAG ANGLE IS VERIFIED CRACKED AND END OF CRACK IS MARKED 9/4/08 VTJ7010159. GUT AWAY DAMAGED AREA OF RT DRAG ANGLE IAW RFO 670-55-31-018. (K)

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 14,942 hrs · 10,055 cycles

CRACKED DRAG ANGLE LT LOWER VERT STAB. MARKED.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB)

CRACKED DRAG ANGLE LEFT LOWER VERT STAB (MARKED). PERFORMED EDDY CURRENT INSPECTION OF LEFT V/STAB TO FUSELAGE DRAG ANGLE IAW CRJ 700 NDTM 51-20-006. DRAG ANGLE IS VERIFIED CRACKED AND END OF CRACK IS MARKED. PERFORMED CUTOUT OF DAMAGED AREA LOCATED OF LT LOWER VERTICAL STAR AND REMOVED BURS AND SHARP EDGES IAW RFO 670-55-31-018. (K)

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 14,521 hrs · 9,756 cycles

REFER TO AFDL 380596 NR 1 CABIN EMERGENCY SIGN INOP. REMOVED AND REPLACED NR 1 EMERGENCY LIGHT BATTERY CHARGER ASSY AS PER AMM 33-51-17, OPS CHECK AS PER AMM 33-51-17. (B)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 14,521 hrs · 9,756 cycles

CABIN EXIT SIGN INOP. FLT 4756 DEL 12 MINS NC FLT 4374 CX. REMOVED AND REPLACED NR 1 AND 2 BATTERIES FOR EMERGENCY LIGHT ASSY AS PER AMM 33-51-17. OPS CHECK AS PER AMM 33-51-17. (B)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,308 hrs · 8,917 cycles

LEFT AND RIGHT O/W EMERGENCY EXITS, LOWER LIGHTS HAVE SEVERAL BULBS INOP.

Part: STEP — BROKEN (STAIRS) · airframe 12,358 hrs · 8,255 cycles

BOTTOM CABIN STEP BROKEN. FLT 4476 DEL 92 MINS.

Part: WARNING SYSTEM — ACTIVATED (BLEED AIR SYS) · airframe 12,055 hrs · 8,021 cycles

L BLEED LEAK WARNING MSG ILLUMINATED ON CLIMBOUT AFTER DEPARTURE FROM ATL. COMPLIED WITH QRH. RETURNED TO ATL UNPRESSURIZED. A/C RETURNED TO ATL AFTER T/O. EMERGENCY DECLARED.

Part: COVER — MISSING (CABIN) · airframe 11,909 hrs · 7,915 cycles

SERVICE DOOR EMERGENCY EXIT SIGN COVER MISSING.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,286 hrs · 7,488 cycles

AFT MOST CEILING EMERGENCY LIGHT INOP.

Part: BATTERY PACK — DEFECTIVE (CABIN) · airframe 11,026 hrs · 7,311 cycles

NR 1 EMERGENCY BATTERY PACK WILL NOT KEEP A CHARGE.

Part: HOUSING — CRACKED (E&E DOOR) · airframe 11,026 hrs · 7,311 cycles

AVIONIC DOOR OUTER HANDLE HOUSING CRACKED AROUND BOSS. REMOVED AND REPLACED AVIONICS DOOR HANDLE PER CRJ700 SRM 51-42-06 AND SRM 51-21-16. PRESSURIZATION LK CK GOOD IAW CRJ 700 MM 21-30

Part: HANDLE — CRACKED (AIR STAIR DOOR) · airframe 11,026 hrs · 7,311 cycles

ASD EXTERNAL HANDLE CRACKED.

Part: LIGHT — LOOSE (GALLEY) · airframe 10,299 hrs · 6,858 cycles

FOUND EMERGENCY LIGHT STRIP IN GALLEY LOOSE.

Part: LAMP — BURNED OUT (CABIN)

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

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

DURING A GROUND INSPECTION IN SLC, THE RIGHT AFT EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT AFT EXTERIOR EMERGENCY LIGHT ASSEMBLY LAMP. OPERATIONAL CHECKS TOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

DURING A GROUND INSPECTION IN SLC, THE EMERGENCY EXIT LIGHT, AT THE RIGHT SIDE EMERGENCY EXIT DOOR, WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT SIDE EMERGENCY EXIT DOOR LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STEP — CRACKED (PAX DOOR)

DURING A C-CHECK IN MCN, THE PASSENGER DOOR TOP STEP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR TOP STEP AND THE STEP TO FUSELAGE HINGE (P/N CC670-31981-3). (M)

Part: ATTACH ANGLE — CORRODED (FUSELAGE)

DURING A C-CHECK IN MCN, THE FLOORBOARD ATTACH ANGLE AT, THE PASSENGER DOOR ENTRANCE, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOORBOARD ATTACH ANGLE, AT THE PASSENGER DOOR ENTRANCE. (M)

Part: SEAT TRACK — CORRODED (BS 379-969)

DURING A C-CHECK IN MCN, THE FLOOR SEAT TRACKS, AT LBL 9 AND RBL 9, FS 379 TO FS 969, WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE WILL REMOVE AND REPLACE THE FLOOR SEAT TRACKS, FROM FS 379 TO FS 969, LBL 9 AND RBL 9. (M)

Part: SEAT TRACK — CORRODED (BS 379-969)

DURING A C-CHECK IN MCN, THE LEFT AND RIGHT SIDEWALL SEAT TRACKS, AT FS 379 TO FS 969, WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE WILL REPAIR THE LEFT AND RIGHT SEAT TRACKS, AT FS 379 TO FS 969, IAW BOMBARDIER

Part: FLOORBEAM — CORRODED (BS 280)

DURING A C-CHECK, THE FORWARD FS 280 FLOOR ANGLE WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE WILL REMOVE AND REPLACE THE FORWARD FS 280 FLOOR ANGLE. (K)

Part: HANDLE — CORRODED (ESCAPE HATCH)

DURING A C-CHECK, THE CREW ESCAPE HATCH OUTER HANDLE WAS FOUND TO BE CORRODED ON THE INSIDE. THIS MRR WILL REMAIN OPEN, PENDING MAINTENANCE DETERMINATION OF APPROPRIATE CORRECTIVE ACTION. (K) MAINTENANCE REMOVED AND REPLACED THE CREW ESCAPE HATCH OUTER HANDLE IAW CRJ 700 AMM 52-22-02. OPS CHECKS GOOD. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DURING A C-CHECK, THE EMERGENCY FLOODLIGHT, NEAR ROW 17, WAS FOUND TO BE INOPERATIVE. MAINT WILL REMOVE AND REPLACE THE LAMP IN THE EMERGENCY FLOODLIGHT ASSY, NEAR ROW 17. (K)

Part: LIGHT — MALFUNCTIONED (CABIN)

DURING A GROUND INSPECTION IN SLC, THE EMERGENCY LIGHTS WOULD NOT TEST. MAINTENANCE CYCLED CIRCUIT BREAKERS. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING HANGAR MAINTENANCE, THE FS 280 FLOORBEAM WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED THE FS 280 FLOORBEAM IAW EO. (K)

Part: BULKHEAD — CORRODED (FUSELAGE)

DURING HANGER MAINTENANCE, THE LT AND RT FS 280 LOWER WEB AT THE BULKHEAD WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED THE LT AND RT FS 280 LOWER WEB AT THE BULKHEAD IAW EO. (K)

Part: PANEL — CRACKED (FUSELAGE)

DURING HANGAR MAINTENANCE, THE RT LUNCH BOX UPPER PANEL ASSY AT THE HYDRAULIC CASE DRAIN LOCATION WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RT LUNCH BOX UPPER PANEL ASSY AT THE HYDRAULIC CASE DRAIN LOCATION IAW. (K)

Part: LIGHT — INOPERATIVE (CABIN)

FLT 4818 - DURING A GROUND INSPECTION IN SLC, THE EMERGENCY CEILING FLOODLIGHTS AT ROWS 10/17 WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMPS IN THE EMERGENCY CEILING FLOOD LIGHT AT ROWS 10 AND 17. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: FAN — BURNED OUT (GALLEY)

DURING A GROUND INSPECTION IN ATL, THE FLIGHT ATTENDANT NOTICED AN ODOR FROM THE AIR CONDITIONING SYSTEM. IT PERSISTED DURING THE FLIGHT FROM ATL-IAH CAUSING EYE IRRITATIONS AND DIFFICULTY BREATHING FOR THE FLIGHT ATTENDANT AND PASSENGERS. THE AIRCRAFT LANDED SAFELY IN IAH. MAINTENANCE REMOVED AND REPLACED THE LAVATORY/GALLEY EXHAUST FAN, BOTH RECIRCULATION FAN FILTERS AND CLEANED THE LAVATORY DRAIN TUBE. NO FURTHER SMELLS WERE NOTICED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: SKIN — CRACKED (WING)

DURING HANGER MAINTENANCE, THE SKIN UNDER THE RT IB MULTIFUNCTIONAL SPOILER AT THE IB BRACKET WAS FOUND CRACKED. MAINT IS TO PERFORM A DETAILED VISUAL INSP FOR PROGRESSION OF THE CRACK AT EVERY SUBSEQUENT SERVICE CHECK, UP TO A MAX OF 100 FLIGHT HRS IAW REO 670-57-73-008, AT WHICH TIME THE PERMANENT REPAIR IS TO BE PERFORMED.

Part: BRACKET — CRACKED (FUSELAGE)

DURING A HANGAR CHECK IN BTR, THE BLEED AIR DUCT SUPPORT BRACKET ON THE LEFT SIDE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE BLEED AIR DUCT SUPPORT BRACKET ON THE LEFT SIDE IAW ASA EO 700-36-0003A. (M)

Part: SWITCH — INOPERATIVE (COCKPIT)

DUIRNG CRUISE, LEVELING AT 37,000 FT THE CREW RECEIVED STABILIZER, MACH AND PITCH TRIM MESSAGES. UNABLE TO GET STABILIZER CHANNELS ONE OR TWO TO RE-ENGAGE. QRH PROCEDURES WERE COMPLIED WITH AND AN EMERGENCY WAS DECLARED AS A PRECAUTION. THE AIRCRAFT LANDED SAFELY IN DFW. MAINTENANCE REMOVED AND REPLACED THE STABILIZER TRIM ENGAGE SWITCH. OPERAITONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)