N368CA

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 46,442 hrs · 36,337 cycles

RH OVERWING EMER LT OUT RELAMPED RH OVERWING EMER LT IAW CRJ 700 AMM 33-51-15, OPS TEST GOOD, P/N OFF/ON: 8GH002473-88

Part: WEB — CORRODED (ZONE 200) · airframe 45,928 hrs · 35,810 cycles

CORROSION ON LH LOWER WEB AT BULKHEAD FS280.00 LBL12 ABOVE FLOOR WAS FOUND CORROSION ON LH LOWER WEB, AT BULKHEAD FS280.00 LBL12 ABOVE FLOOR WAS FOUND OUT OF LIMITS PER CRJ700 SRM 53-00-01-101-001-A01, WAS FABRICATED PER CRJ700 SRM 53-11-10-201-004-A01 AND WAS REPLACED PER CRJ-700 SRM 51-42-10-001-001-A01,

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 45,928 hrs · 35,810 cycles

INITIAL INSPECTION: CORROSION ON FLOOR SILL BTW FS280.00 AND 319.70 AT CABIN FLOOR STRUCTURE. FLOOR SILL BTW FS280.00 AND 319.70 WAS EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-00-45-201-001-A01 AND WAS REPLACED PER EA CRJ753-17650 REV A AND CRJ700S SRM 51-42-06-001-001-A01

Part: WEB — CORRODED (ZONE 200) · airframe 45,928 hrs · 35,810 cycles

CORROSION ON RH LOWER WEB AT BULKHEAD FS280.00 LBL12 ABOVE FLOOR WAS FOUND CORROSION ON RH LOWER WEB, AT BULKHEAD FS280.00 LBL12 ABOVE FLOOR WAS FOUND OUT OF LIMITS PER CRJ700 SRM 53-11-10-201-003-A01, WAS FABRICATED PER CRJ700 SRM 53-11-10-201-004-A01 AND WAS REPLACED PER CRJ-700 SRM 51-42-10-001-001-A01,

Part: STRINGER — CORRODED (ZONE 100) · airframe 45,928 hrs · 35,810 cycles

AFTER FRAME REMOVAL: CORROSION ON STGR23R AT FS379.00 WAS FOUND. DUE TO EXCESSIVE DAMAGE ON STGR 23RH AT FS379 WAS REPAIRED PER CRJ700 SRM 53-00-03-201-001-A01

Part: SKIN — CHAFED (ZONE 100) · airframe 45,928 hrs · 35,810 cycles

IN REF TO: DURING INSPECTION OF THE TASK CARD 700-53-900-303 IT WAS DETECTED WEAR ON EXTERNAL LOWER FUSELAGE SKIN BTW FS 977.00 TO 985.00 AND STGR 26L-26R. WEAR ON EXTERNAL LOWER FUSELAGE SKIN BTW FS 977.00 TO 985.00 AND STGR 26L-26R WAS REPAIRED PER EA CRJ753-11451 REV. IR

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 45,928 hrs · 35,810 cycles

CORROSION ON CROSSBEAM AT FS280.00 BTW LBL45.00/RBL45.00 AT CABIN FLOOR STRUCTURE. CORROSION ON CROSSBEAM AT FS280.00 WAS EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-00-01-101-001-A01 AND WAS REPLACED PER CRJ700 SRM 51-42-06-001-001-A01; SRM 51-42-21-001-001-A01 AND SRM 51-42-10-001-001-A01

Part: BRACKET — CRACKED (BS 1088) · airframe 41,033 hrs · 31,064 cycles

PANEL 443BT SECOND MOUNTING TAB FROM AFT IS BROKEN NEEDS REPAIR. - REMOVED & REPLACED SECOND MOUNTING TAB ON PANEL 443BT IAW CRJ 700 SRM 51-42-06-001-001(A01) WVAC EMP #56399

Part: SKIN — CHAFED (BS 985 S27L) · airframe 41,033 hrs · 31,064 cycles

FUSELAGE LOWER SKIN AND RIVETS CHAFFED AT APPROXIMATELY FS985.00 STGR 27. - REPAIRED DAMAGE IAW ENDEAVOR EA CRJ753-11451 REV IR, DATED 4/21/2021

Part: ANGLE — CORRODED (BS 280 CROSSBEAM) · airframe 41,033 hrs · 31,064 cycles

L/H FS 280 BULKHEAD CROSSBEAM IS CORRODED. - REMOVED AND REPLACED R/H CROSSBEAM, UPPER DOUBLE ANGLE AND LOWER DOUBLER ANGLE IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-22-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01 AND 53-11-41-201-003-A01.

Part: TEE FITTING — CORRODED (BS 280) · airframe 41,033 hrs · 31,064 cycles

R/H FS 280 BULKHEAD CROSSBEAM IS CORRODED. - REMOVED AND REPLACED R/H CROSSBEAM, UPPER DOUBLE ANGLE, LOWER DOUBLER ANGLE, TEE FITTING AT RBL 9 AND J-ANGLE IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-20-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01 AND 53-11-41-201-003-A01.

Part: FRAME — GOUGED (BS 144 S10R) · airframe 41,033 hrs · 31,064 cycles

AFT EQUIPMENT BAY RH SIDE FRAME AT FS 1144.00 GOUGED BELOW STGR 10R. - REPAIRED FRAME IAW ENDEAVOR EA CRJ753-11441 REV IR, DATED 5/6/2021.

Part: CROSSBEAM — CORRODED (BS 280) · airframe 41,033 hrs · 31,064 cycles

L/H FS 280 BULKHEAD CROSSBEAM IS CORRODED. - REMOVED & REPLACED LH 280 CROSSBEAM IAW CRJ 700 AMM 53-11-41-201-003-A01.

Part: CROSSBEAM — CORRODED (BS 280) · airframe 41,033 hrs · 31,064 cycles

L/H FS 280 BULKHEAD CROSSBEAM IS CORRODED. - REMOVED & REPLACED LH 280 CROSSBEAM IAW CRJ 700 AMM 53-11-41-201-003-A01. WVAC EMP #6027

Part: ANGLE — CORRODED (BS 280 CROSSBEAM) · airframe 41,033 hrs · 31,064 cycles

R/H FS 280 BULKHEAD CROSSBEAM IS CORRODED. - REMOVED AND REPLACED R/H CROSSBEAM, UPPER DOUBLE ANGLE, LOWER DOUBLER ANGLE, TEE FITTING AT RBL 9 AND J-ANGLE IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-20-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01 AND 53-11-41-201-003-A01.

Part: ANGLE — CORRODED (BS 280 CROSSBEAM) · airframe 41,033 hrs · 31,064 cycles

R/H FS 280 BULKHEAD CROSSBEAM IS CORRODED. - REMOVED AND REPLACED R/H CROSSBEAM, UPPER DOUBLE ANGLE, LOWER DOUBLER ANGLE, TEE FITTING AT RBL 9 AND J-ANGLE IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-20-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01 AND 53-11-41-201-003-A01.

Part: CROSSBEAM — CORRODED (BS 280 BULKHEAD) · airframe 41,033 hrs · 31,064 cycles

R/H FS 280 BULKHEAD CROSSBEAM IS CORRODED. - LOCATED,DRILLED AND INSTALLED NEW SERVICEABLE FS 280 CROSSBEAM P/N CC670-34175-7 PER CRJ 700 SRM 53-11-41-201-003-A01. WVAC EMP #7322

Part: CROSSBEAM — CORRODED (BS 280 BULKHEAD) · airframe 41,033 hrs · 31,064 cycles

R/H FS 280 BULKHEAD CROSSBEAM IS CORRODED. - REMOVED AND REPLACED R/H CROSSBEAM, UPPER DOUBLE ANGLE, LOWER DOUBLER ANGLE, TEE FITTING AT RBL 9 AND J-ANGLE IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-20-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01 AND 53-11-41-201-003-A01.

Part: ANGLE — CORRODED (BS 310-349 S17L) · airframe 41,033 hrs · 31,064 cycles

PAX DOOR MID CAP ANGLE CORRODED AT STGR 17L BETWEEN FS310.00 & FS 349.00. - REMOVED & REPLACED MID CAP ANGLE, I.A.W. CRJ 700 SRM 51-41-02-001-001-A01, 51-42-06-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 752) · airframe 41,033 hrs · 31,064 cycles

L/H SIDE SEAT TRACK AT STR L15 AT FS 752.00 SEAT TRACK U CHANNEL IS CORRODED. - REMOVED AND REPLACED U CHANNEL IAW CRJ 700 AMM 53-00-49-400-801-A17. WVAC EMP STAMP #711 MTC

Part: BRACKET — CORRODED (HYD LINE) · airframe 41,033 hrs · 31,064 cycles

R/H MLG WHEEL WELL FWD BULKHEAD HYDRAULIC BRACKET CORRODED. - REPLACED BRACKET IAW CRJ 700 SRM 51-40-11-001-001-A01. WVAC EMP STAMP #711 MTC

Part: SEAT TRACK — CORRODED (BS 752 LBL 15) · airframe 41,033 hrs · 31,064 cycles

L/H SIDE SEAT TRACK AT STR L15 AT FS 752.00 IS CORRODED AROUND FASTENER HOLES - RECEIVED, LOCATED AND INSTALLED REPLACEMENT SEAT TRACK PN SH670-37509-1 IAW CRJ 700 AMM 53-00-49-400-801-A17. WVAC EMP STAMP #789 MTC

Part: ANGLE — CORRODED (BS 310-349 S17L) · airframe 41,033 hrs · 31,064 cycles

PAX DOOR KICKPLATE ANGLE CORRODED AT STRGR 17L BETWEEN FS310.00 AND FS 349.00 - LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE PAX DOOR KICKPLATE ANGLE P/N SH670-31875-7S IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. WVAC EMP #574786

Part: SEAT TRACK — CORRODED (BS 693-761) · airframe 41,033 hrs · 31,064 cycles

RH CABIN SIDE SEAT RAIL AT STR R15 FS 785.00 TO FS 847.0 SEAT TRACK U CHANNEL CORRODED. - REMOVED & REPLACED U-CHANNEL IAW CRJ 700 SRM 51-41-02-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 797-813) · airframe 41,033 hrs · 31,064 cycles

L/H SIDE SEAT TRACK AT FS 797.00 TO FS 813.00 STR L15 IS CORRODED. - SEAT TRACK WAS REMOVED AND REPLACED AS REQ IAW CRJ 700 AMM 53-00-49-400-801-A03. WVAC EMP #161529

Part: SEAT TRACK — CORRODED (BS 755-847 S15R) · airframe 41,033 hrs · 31,064 cycles

RH CABIN SIDE SEAT TRACK AT STR R15 FS 785.00 TO FS 847.00 IS CORRODED - REMOVED & REPLACED SEAT TRACK AT STR R15 FS713.00 TO FS763.00 IAW CRJ 700 AMM 53-00-49-000/400-801-A03. WVAC EMP STAMP #774 MTC

Part: ATTACH ANGLE — CORRODED (BS 280) · airframe 41,033 hrs · 31,064 cycles

RH ELECTRICAL CONNECTOR PLATE ATTACHMENT ANGLE HAS NUMEROUS OVERSIZED HOLES & CORROSION AND REQUIRES REPLACEMENT. P/N: CC670-51876-3. LOCATED @ FS 280 CROSSBEAM - LOCATED, DRILLED, INSTALLED AND TOPCOATED SERVICEABLE RH ATTACH ANGLE IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-25-16-001-001-A01. WVAC EMP #89523

Part: SEAT TRACK — CORRODED (BS 693-761 S15R) · airframe 41,033 hrs · 31,064 cycles

R/H CABIN SIDE SEAT TRACK STR R15 AT FS 693.00 TO FS 761.55 U CHANNEL IS CORRODED LOWER EDGE. - FABRICATED R/H U CHANNEL IAW ENDEAVOR EA CRJ 753-11486 REV IR DATED 04/18/21 AND INSTALLED FABRICATED CHANNEL IAW CRJ 700 AMM 53-00-49-400-801-A03. WVAC EMP STAMP #774 MTC

Part: STIFFENER — CRACKED (BS 260) · airframe 41,033 hrs · 31,064 cycles

UPON REMOVAL OF FS260 WEBS (R/H & L/H) FOUND 5 VERTICAL STIFFENER ANGLES TO BE CRACKED OR HAVE DAMAGED HOLES (4 ON L/H AND 1 ON R/H SIDE.) - REMOVED,LOCATED AND DRILLED ALSO INSTALLED 5EA NEW SERVICEABLE STIFFENERS AT L/H 280 WEB 4EA AND 1EA AT RH 280 WEB, P/N CC670-34117-4 CC670-34106-3, CC670-34151-5 AND CC670-34152-1 IAW CRJ 700 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND 51-40-11-001-001-A01. WVAC EMP #88277

Part: SEAT TRACK — CORRODED (BS 485 RBL 9) · airframe 41,033 hrs · 31,064 cycles

FLOOR SEAT TRACK AT RBL 9 BEGINNING AT APPROXIMATELY FS 485.00 CORRODED IN SEVERAL LOCATIONS. - RECEIVED, FABRICATED, LOCATED AND DRILLED REPLACEMENT MATL FOR SEAT TRACK BEGINNING RBL 9 FS 485 IAW CRJ 700 SRM 53-00-49-201-002-A01. INSTALLED IAW CRJ 700 AM 53-00-49-400-801-A17. WVAC EMP STAMP #774 MTC

Part: BRACKET — CORRODED (BS 533 S22-23L) · airframe 41,033 hrs · 31,064 cycles

FWD CARGO TIE DOWN RING SUPPORT BRACKET CORRODED AT FS533.00 , STRGR 22L TO 23L - REMOVED AND REPLACED CARGO NET TIE DOWN SUPPORT BRACKET IAW CRJ 700 SRM 51-42-21-001-001-A01 AND 51-40-11-001-001-A01

Part: SEAT TRACK — CORRODED (BS 354 LBL27) · airframe 41,033 hrs · 31,064 cycles

FLOOR SEAT TRACK AT LBL27 BEGINNING AT APPROX. FS 354.00 CORRODED IN SEVERAL LOCATIONS. - FABRICATED AND REPLACED SEAT TRACK IAW SRM 51-40-11-001-001-A01 AND AMM 53-00-49-400-801-A17. WVAC EMP #6027

Part: SEAT TRACK — CORRODED (BS 847 LBL 9) · airframe 41,033 hrs · 31,064 cycles

SEAT TRACK SEGMENT AT LBL 9 IS CORRODED B/W FS 847 TO FS 977. - REMOVED AND REPLACED DISCREPANT SEAT TRACK B/W FS 847-TO FS 977 @ LBL9 IAW CRJ 700 AMM 53-00-49-400-801-A17 INSTALLED USING WVACT1996. WVAC EMP STAMP #774 MTC

Part: SEAT TRACK — CORRODED (BS 847-977 RBL9) · airframe 41,033 hrs · 31,064 cycles

SEAT TRACK SEGMENT IS CORRODED BETWEEN FS 847 TO FS 977 AT RBL 9. - REMOVED AND REPLACED DISCREPANT SEAT TRACK IAW CRJ 700 AMM 53-00-49-400-801-A17 INSTALLED USING WVACT1996. WVAC EMP STAMP #774 MTC

Part: SEAT TRACK — CORRODED (BS 581) · airframe 41,033 hrs · 31,064 cycles

FLOOR SEAT TRACK AT LBL 9 BEGINNING AT APPROXIMATELY FS 581.00 CORRODED IN SEVERAL LOCATIONS. - RECEIVED, FABRICATED, LOCATED AND DRILLED REPLACEMENT SEAT TRACK BEGINNING AT LBL 9 FS 581 IAW CRJ 700 SRM 53-00-49-201-002-A01. THEN INSTALLED IAW CRJ 700 AM 53-00-49-400-801-A17.

Part: ESCAPE HATCH — NO TEST (COCKPIT) · airframe 41,033 hrs · 31,064 cycles

CREW ESCAPE HATCH FAILED FUNCTIONAL TEST OUTER HANDLE DOES NOT EJECT FROM HANDLE RECESS EVEN AFTER SOAKING IN KROIL FOR HOURS. - REMOVED & REPLACED HANDLE ASSY IAW CRJ 700 SRM 51-42-06-001-001-A01. OP CK'S GOOD. WVAC EMP STAMP #774 MTC

Part: INTERCOSTAL — CORRODED (BS 394-409 S26R) · airframe 41,033 hrs · 31,064 cycles

INTERCOSTAL AT FS 394.00 - 409.00 AND STR 27-26R HAS CORROSION. - INTERCOSTAL @ FS 394.00-409.00 & STGR 27-26R WERE REPAIRED IAW ENDEAVOR AIR EA CRJ753-11514 REV IR DATED 4-28-2021 & CRJ 753-11513 REV IR DATED 4/16/21. WVAC EMP #161529

Part: SEAT TRACK — CORRODED (BS 349 RBL 9) · airframe 41,033 hrs · 31,064 cycles

FLOOR SEAT TRACK AT RBL9 BEGINNING AT APPROX. FS 349.00 CORRODED IN SEVERAL LOCATIONS. - REMOVED AND REPLACED DISCREPANT SEAT TRACK IAW CRJ 700 AMM 53-00-49-400-801-A17 INSTALLED USING WVACT1996. WVAC EMP STAMP #774 MTC

Part: INTERCOSTAL — CORRODED (BS 310-333 S21L) · airframe 41,033 hrs · 31,064 cycles

INTERCOSTAL AT STRG 21L HAS MULITPLE SPOTS OF CORROSION FROM FS 310.0 TO FS 349.00. - UPON FURTHER INVESTIGATION FOUND NO CORROSION ON INTERCOSTAL BETWEEN 310+333 REMOVED & REPLACED INTERCOSTAL BETWEEN FS 349+333 WITH SERVICEABLE IAW CRJ 700 SRM 51-42-11-001-001-A01 AND 51-42-06-001-001-A01. WVAC EMP STAMP #774 MTC

Part: STRINGER — CORRODED (BS 280-310) · airframe 41,033 hrs · 31,064 cycles

STGR 19R HAS AREAS OF CORROSION FROM F.S. 280.00 TO F.S. 310.00. - REPLACED STRINGER IAW CRJ 700 SRM.

Part: FRAME — CORRODED (BS 863 S26L-R) · airframe 41,033 hrs · 31,064 cycles

FRAME SECTOR AT FS 863 IS CORRODED ON FWD AND AFT SIDE BETWEEN STRG 26R - 26L. - REPAIRED FRAME SECTOR IAW ENDEAVOR AIR EA CRJ753-11438 IR DATED 4/29/2021.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 41,033 hrs · 31,064 cycles

L/H FS 280 BULKHEAD WEB IS CORRODED. - L/H FS 280 BULKHEAD WEB WAS REPAIRED IAW CRJ 700 SRM 53-11-10-201-004-A01. WVAC EMP #161529

Part: FILLER — CORRODED (BS 295 CROSSBEAM) · airframe 41,033 hrs · 31,064 cycles

FS 295 CROSSBEAM FILLER AT LBL 9 IS CORRODED. - REMOVED & REPLACED FILLER FOR CROSSBEAM AT FS295 LBL9 IAW SRM 51-42-06-001-001-A01. WVAC EMP #6027

Part: BRACKET — CORRODED (ELEC CONNECTOR) · airframe 41,033 hrs · 31,064 cycles

L/H WHEEL WELL AT FWD BULKHEAD ELECTRICAL CONNECTION BRACKET IS CORRODED. - REMOVED AND REPLACED BRACKET IAW CRJ 700 SRM 51-41-02-001-001-A01, 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01 AND AMM 20-22-00-910-801-A01. WVAC EMP STAMP #711 MTC

Part: BRACKET — CORRODED (BULKHEAD) · airframe 41,033 hrs · 31,064 cycles

L/H WHEEL WELL AT FWD BULKHEAD HYDRAULIC CONNECTION BRACKET IS CORRODED. - REMOVED L/H FWD BULKHEAD HYD CONNECTION BRACKET REMOVED CORROSION FOUND IN ALLOWABLE LIMITS TREATED AND INSTALL SAME SERVICEABLE BRACKET IAW CRJ 700 SRM 51-40-11-001-001-A01. LEAK CK GOOD. WVAC EMP STAMP #789 MTC

Part: LIGHT — OUT OF POSITION (CABIN) · airframe 39,532 hrs · 29,651 cycles

EME. EXIT LIGHT NEAR L/H EME. EXIT DOOR IS OUT OF PLACE. RESECURED EXIT LIGHT IAW CRJ 700 AMM 35-51-05 PERFORM OPS CHECK IAW CRJ 700 AMM 33-50-00

Part: BRACKET — CORRODED (PAX DOOR) · airframe 37,148 hrs · 27,419 cycles

PASSENGER DOOR BRACKET HAS SIGNS OF CORROSION. CORRECTIVE ACTION: REMOVED AND REPLACED BRACKET (P/N:601R318084-1) IAW CRJ700 SRM 51-42-06.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 37,148 hrs · 27,419 cycles

PASSENGER DOOR ANGLE HAS SIGNS OF CORROSION. CORRECTIVE ACTION: REMOVED AND REPLACED ANGLE (P/N:601R317726-3) IAW CRJ700 SRM 51-42-06.

Part: STIFFENER — CRACKED (PAX DOOR) · airframe 37,148 hrs · 27,419 cycles

PASSENGER DOOR TOP PANEL STIFFENER CRACKED. CORRECTIVE ACTION: REMOVED AND REPLACED STIFFENER (P/N:601R317725-1) IAW CRJ700 SRM 51-42-06 AND 51-42-13.

Part: PULLEY BRACKET — BENT (PAX DOOR) · airframe 37,148 hrs · 27,419 cycles

PASSENGER DOOR PULLEY BRACKET BENT. CORRECTIVE ACTION: REMOVED AND REPLACED PULLEY BRACKET (P/N:601R317186-1) IAW CRJ700 SRM 51-42-06.

Part: BRACKET — CORRODED (PAX DOOR) · airframe 37,148 hrs · 27,419 cycles

PASSENGER DOOR BRACKET HAS SIGNS OF CORROSION. CORRECTIVE ACTION: REMOVED AND REPLACED BRACKET (P/N:601R38921-9) IAW CRJ700 SRM 51-42-06.

Part: PANEL — CORRODED (PAX DOOR) · airframe 37,148 hrs · 27,419 cycles

PASSENGER DOOR FWD SIDE PANEL HAS SIGNS OF CORROSION. CORRECTIVE ACTION: REMOVED AND REPLACED PASSENGER DOOR SIDE PANEL (P/N: 601R317071-12) IAW CRJ700 SRM51-42-06 AND 51-42-13.

Part: BRACKET — CORRODED (PAX DOOR) · airframe 37,148 hrs · 27,419 cycles

PASSENGER DOOR BRACKET ASSY HAS SIGNS OF CORROSION. CORRECTIVE ACTION: REMOVED AND REPLACED BRACKET ASSY (P/N: 601R38721-13) IAW CRJ700 SRM 51-42-06

Part: FORMER — CORRODED (BS 311.75) · airframe 37,148 hrs · 27,419 cycles

PASSENGER FWD FORMER HAS SIGNS OF CORROSION. CORRECTIVE ACTION: REMOVED AND REPLACED FWD FORMER (P/N: 601R318031-5S) IAW CRJ700 SRM 51-42-06.

Part: SUPPORT — CRACKED (PAX DOOR GATE) · airframe 37,148 hrs · 27,419 cycles

PASSENGER DOOR VENT FLAP AFT HINGE SUPPORT ASSY. CRACKED. CORRECTIVE ACTION: REMOVED AND REPLACED VENT FLAP HINGE SUPPORT ASSY. (P/N 601R31813-9) IAW CRJ 700 SRM 51-42-13.

Part: STIFFENER — CRACKED (PAX DOOR) · airframe 37,148 hrs · 27,419 cycles

PASSENGER DOOR STIFFENER ON PASSENGER DOOR FWD SIDE PANEL CRACKED. CORRECTIVE ACTION: REMOVED AND REPLACED STIFFENER (P/N:601R317725-1) IAW CRJ700 SRM 51-42-06.

Part: BEAM — CRACKED (PAX DOOR) · airframe 37,148 hrs · 27,419 cycles

PASSENGER DOOR AFT GAS SPRING BEAM CRACKED. CORRECTIVE ACTION: REMOVED AND REPLACED AFT GAS SPRING BEAM (PN:601R318011-1) IAW CRJ 700 SRM 51-42-06 AND 51-40-11.

Part: BEAM — CRACKED (PAX DOOR) · airframe 37,148 hrs · 27,419 cycles

PASSENGER DOOR GAS SPRING BEAM IS CRACKED. REMOVED AND REPLACED PAX DOOR GAS SPRING BEAM(PN:601R318011-10 IAW SRM 51-42-06.

Part: WEB — CRACKED (PAX DOOR) · airframe 37,148 hrs · 27,419 cycles

PASSENGER DOOR AFT STAIR WEB IS CRACKED. REPAIRED AFT STAIR WEB BY CUTTING OUT DAMAGE, FABRICATING AND INSTALLING REPAIR PARTS IAW REO 670-52-11-104 REV H DATED 2019-08-14, ZONE 6 REPAIR.

Part: DOUBLER — CRACKED (PAX DOOR) · airframe 37,148 hrs · 27,419 cycles

PASSENGER DOOR FWD AND AFT CAM DOUBLERS ARE CRACKED. REMOVED AND REPLACED FWD AND AFT CAM DOUBLERS(PN: 601R318074-1 AMD -2) IAW SRM 51-42-06 AND 51-42-21.

Part: UNKNOWN — UNKNOWN (PAX DOOR) · airframe 37,271 hrs · 27,535 cycles

FA REPORTED THE MAIN PAX DOOR WAS NOT ALIGNED AND RATTLES UNTIL 6K FEET. PERFORMED AN OPS CHECK OF THE PAX DOOR IAW AMM 52-11-00. NO FURHTER DISCREPANCY FOUND AT THIS TIME.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 37,148 hrs · 27,419 cycles

RT FLOOR SILL AT FS 280.0-FS 319.0 HAS SIGNS OFF CORROSION. CUT DAMAGED AREA AND FABRICATED AND INSTALLED REPAIRED PARTS IAW REO 670-53-00-390 DATED 22 JAN 2014 AND REO 670-53-21-1545 DATED 2018-07-23 AND IAW AMM 20-70-00 AND NDTM PART 1 51-20-006.

Part: CLEAT — CRACKED (FUSELAGE) · airframe 37,148 hrs · 27,419 cycles

CLEAT AT FLOORBEAM AT FRAME STATION 333.0 LT SIDE FOUND CRACKED. REMOVED, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 51-24-16, 51-40-11, 51-25-06, 51-21-11, 51-25-21 AND 51-42-13.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 37,148 hrs · 27,419 cycles

LT 280.00 BEAM HAS SIGNS OF CORROSION AND RT 28 BEAM CRACKED. REMOVED AND REPLACE 280 CROSSBEAM IAW SRM 53-11-41, 51-42-21, 51-42-06, 51-42-13, 51-40-11, 53-21-03, 51-21-11, 51-25-16, 51-41-02, AMM 20-70-00 AND NDTM 51-20-006-250.

Part: FRAME — CORRODED (FUSELAGE) · airframe 37,148 hrs · 27,419 cycles

FRAME STATION 349.0 REQUIRE SPLICE REPAIR. CUT OUT DAMAGED AREA FABRICATED AND INSTALLED REPAIRED PARTS IAW REO 670-53-21-1541 REV-- 2018-07-23 AND SRM 51-25-16.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 37,148 hrs · 27,419 cycles

LT AND RT FRAME STATION BULKHEAD LOWER AFT WEBS HAVE SIGNS OF CORROSION. CUT OUT DAMAGED AREA FABRICATED AND INSTALLED REPAIR PARTS IAW REO 670-53-11-594 REV- DATED 2011/04/27, SRM 51-25-06, 51-42-06, 51-21-11, 51-25-16, 51-26-01 AND AMM 20-70-00, 51-21-01.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 37,148 hrs · 27,419 cycles

STRINGER 25R HAS SIGNS OF CORROSION BETWEEN FS 319.00 AND FS 349 ON STRINGER AND STRINGER SPLICE. REMOVED AND REPLACED STRINGER 25R IAW SRM 51-40-11, 51-42-21, 51-42-06 AND 51-25-16.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,148 hrs · 27,419 cycles

FRAME 333 AT STR 1 IS CRACKED. REMOVED AND REPLACED FRAME 333(SH670-32056-5) AT STR 1 IAW SRM 51-42-06, 51-40-11, 51-25-16, AND 51-21-11.

Part: STRIKER — CORRODED (FUSELAGE) · airframe 37,148 hrs · 27,419 cycles

GALLEY/SERVICE DOOR LOWER SEAL STRIKER IS CORRODED. REMOVED AND REPLACED GALLEY/SERVICE DOOR LOWER SEAL STRIKER(PN:SH670-31412-951-3) IAW SRM 51-42-026, 51-42-21, AND 51-41-00.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 37,148 hrs · 27,419 cycles

LT SILL BETWEEN FS 310.00 AND 349.00 AT STR 21L IS CORRODED. REMOVED AND REPLACED LT SILL(PN: SH670-31822-1)BETWEEN FS 310.00 AND 349.00 AT STR 21L IAW SRM 51-25-16, 20-70-00, 51-21-11, 51-42-21, 51-42-06, 51-440-11, 20-23-00, AND 20-23-01.

Part: BRACKET — CRACKED (PAX DOOR) · airframe 37,148 hrs · 27,419 cycles

PASSENGER DOOR SUPPORT WHEEL PULLY BRACKET BROKEN. REMOVED AND REPLACED PAX DOOR SUPPORT WHEEL PULLEY BRACKET(PN:601R317186-1) IAW SRM 51-42-09, 51-40-11.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 35,917 hrs · 26,318 cycles

LEFT EMERGENCY EXIT LIGHT INOPERATIVE. ONE BULB INOPERATIVE.

Part: HANDLE — BROKEN (SERVICE DOOR) · airframe 35,727 hrs · 26,136 cycles

SERVICE DOOR PLASTIC GREY HANDLE BROKEN.

Part: AXLE — CORRODED (RT MLG) · airframe 34,708 hrs · 25,226 cycles

RIGHT MLG PISTON AXLE ROOT RADIUS IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED THE RT MLG PISTON ASSY IAW AMM 32-11-09

Part: AXLE — CORRODED (RT MLG STRUT) · airframe 34,708 hrs · 25,226 cycles

RIGHT MLG AXLE ROOT RADIUS IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED THE RT MLG PISTON ASSEMBLY IAW AMM 32-11-09.

Part: LIGHT — INOPERATIVE (ROW 4) · airframe 34,282 hrs · 24,878 cycles

EMERGENCY LIGHT IN CEILING ABOVE ROW 4 BURNED OUT.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 33,341 hrs · 24,147 cycles

LEFT EMERGENCY EXIT SIGN BULB INOPERATIVE.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 32,830 hrs · 23,780 cycles

WHILE PERFORMING SB 670BA-53-036, CORROSION WAS FOUND ON THE FS 693.0 BULKHEAD CAP ANGLE AT BL 0.00.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 32,830 hrs · 23,780 cycles

FS 202.75 BULKHEAD LBL 30, STIFFENER IS CRACKED AT TOP APPROXIMATELY 0.25" LONG. REPAIRED IAW SRM 53-11-10-2001-005-A01.

Part: FRAME — CORRODED (FUSELAGE) · airframe 32,719 hrs · 23,691 cycles

FRAME 295.00, BETWEEN STRINGER 25L & 25R IS CORRODED. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS & INSTALLED SERVICEABLE FRAME, PN SH670-31353-1, IAW REO 670-53-21-799 DATED 30 JAN 2012. NDT PERFORMED CRS W2XR853X, PO 134129 & WO A16-1076.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 32,719 hrs · 23,691 cycles

RIGHT FLOOR SILL AT FS 280.00 IS CORRODED. R & R RT FLOOR SILL AT FS 280.00 IAW SRM 51-42-06, 51-42-13, 51-40-11, 51-32-06, 51-25-06, 51-25-16, 51-21-11, AMM 20-70-00, 51-21-01 & DWG SH670-33336.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 32,719 hrs · 23,691 cycles

RIGHT VERTICAL FWD & AFT DRAG ANGLES ARE CRACKED. CUT & REMOVED CRACKED SECTIONS OF ANGLES. FABRICATED ANGLES, FILLERS & INSTALLED IAW REO 670-55-31-085 DATED 5 MAY 16 & 670-55-31-085 REV A DATED 09 MAY 2016.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 32,719 hrs · 23,691 cycles

LEFT VERTICAL TO FUSELAGE FWD DRAG ANGLE IS CRACKED. CUT & REMOVED CRACKED SECTION OF DRAG ANGLE. FABRICATED ANGLE, FILLER & INSTALLED IAW REO 670-55-31-085 REV A DATED 09 MAY 2016.

Part: SKIN — DAMAGED (PAX DOOR) · airframe 32,719 hrs · 23,691 cycles

PASSENGER DOOR EXTERNAL AFT STAIRCASE PULLEY ATTACH BRACKET HAS JO BOLT PULLED THROUGH SKIN. CUT & REMOVED DAMAGE. FABRICATED FILLER, REPAIR ANGLE & SHIM, INSTALLED WITH PULLEY IAW REO 670-52-11-882 DATED 09 MAY 2016. AVMAX WO 80399 & WC 8062.

Part: LOOP — OUT OF POSITION (BLEED AIR SYS) · airframe 32,719 hrs · 23,699 cycles

BLEED DUCT WARNING MSG IN FLIGHT. RE-ROUTED P139 & P140 LOOPS IAW AMM 36-21-01, RAN BOTH ENGS IAW AMM 71-00-00, FOUND NO LEAKS & NO FAULTS MSGS OCCURRED.

Part: SENSING ELEMENT — OUT OF POSITION (BLEED AIR SYS) · airframe 32,705 hrs · 23,683 cycles

LEFT BLEED DUCT WARNING MSG. REPOSITIONED ELEMENT MT226 & HAD CREW PERFORM GND RUN, FOUND NO BLEED LEAKS OR FURTHER MSGS FIM 36-21-01.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,352 hrs · 23,422 cycles

LAST EMERGENCY CEILING FLOODLIGHT INOPERATIVE SEAT 18B.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,352 hrs · 23,422 cycles

LAST EMER CEILING FLOODLIGHT INOPERATIVE SEAT 18B. DEFERRED CEILING FLOODLIGHT IAW MEL 33-51-01B CAT C.

Part: HOOK AND LOOP — UNSECURE (EMERGENCY EXIT) · airframe 32,090 hrs · 23,213 cycles

RIGHT SIDE EMER EXIT DOOR HANDLE COVER DOES NOT STAY SECURE. SECURED VELCRO TO RT SIDE EMER EXIT DOOR HANDLE COVER IAW AMM 51-22-01.

Part: COVER — OUT OF POSITION (EMERGENCY EXIT) · airframe 31,737 hrs · 22,947 cycles

RIGHT EMER EXIT DOOR HANDLE COVER NOT STOWED. SECURED OVERWING EMER EXIT HANDLE COVER IAW AMM 51-22-61.

Part: LIGHT — UNSECURE (CABIN) · airframe 31,558 hrs · 22,814 cycles

CEILING FLOOD LIGHT AT SEAT 6D INOPERATIVE. SECURED CEILING EMER LIGHT BULB AT SEAT 6D IAW AMM 33-51-02. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: COVER — UNSECURE (EMERGENCY EXIT) · airframe 31,537 hrs · 22,798 cycles

RIGHT SIDE EMER EXIT COVER FELL OFF. SECURED RT SIDE EMER COVER IAW AMM 51-22-61.

Part: DOOR SEAL — DIRTY (PAX DOOR) · airframe 30,947 hrs · 22,328 cycles

WHISTLE SOUND COMING FROM PAX DOOR. CLEANED & LUBED PAX DOOR SEAL AS REQUIRED. PERFORMED A PRESSURIZATION CHECK IAW AMM 21-50-00. OPERATIONS CHECKED GOOD.

Part: COVER — UNSECURE (EMERGENCY EXIT) · airframe 30,822 hrs · 22,229 cycles

RIGHT WING EMERGENCY EXIT HANDLE COVER NOT STAYING STOWED. SECURED THE RT OVERWING EMERGENCY DOOR HANDLE COVER IAW AMM 51-22-61.

Part: MOTOR — INOPERATIVE (PAX DOOR) · airframe 30,817 hrs · 22,225 cycles

PASSENGER DOOR MOTOR ASSIST INOPERATIVE. DEFERRED PAX DOOR ASSIST MOTOR IAW MEL 52-11-01A CAT C.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 3,066,603 hrs · 22,103 cycles

RUDDER LIMITER CAUTION MSG IN FLIGHT. SWAPPED NR ONE & NR TWO SSCU'S. PERFORMED SPOST IAW AMM 27-61-05. CLEANED CONNECTORS TO RUDDER TRAVEL LIMITER ACTUATOR & INSPECTED COMPONENTS IAW AMM 27- 25-03. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: DEAD BOLT — INOPERATIVE (COCKPIT DOOR) · airframe 30,435 hrs · 21,925 cycles

COCKPIT DOOR DEADBOLT IS INOPERATIVE. SECURED COCKPIT DOOR DEADBOLT ASSEMBLY IAW CMM 25-17-03.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,368 hrs · 21,879 cycles

EMERGENCY FLOODLIGHT ON CEILING AT ROW 15 INOPERATIVE. DEFERRED FLOODLIGHT AT ROW 15 IAW MEL 33-51-01B CAT C.

Part: CABLE — FRAYED (PAX DOOR) · airframe 30,324 hrs · 21,846 cycles

PASSENGER DOOR ASSIST MOTOR CABLE FRAYED. DEACTIVATED & DEFERRED PAX DOOR ASSIST MOTOR CABLE IAW MEL 52-11-01A CAT A.

Part: SEALANT — MISSING (EMERGENCY EXIT) · airframe 29,997 hrs · 21,578 cycles

LEFT EMER DOOR MISSING SEALANT AROUND WINDOW. APPLIED SEALANT, VERIFIED CURED ON LT EMER DOOR WINDOW IAW AMM 51-23-00.

Part: HINGE — DIRTY (PAX DOOR) · airframe 29,982 hrs · 21,565 cycles

POPPING NOISE HEARD COMING FROM PAX DOOR ASSIST MOTOR WHEN CLOSING. PERFORMED INSPECTION, FOUND DEBRIS IN HINGE. REMOVED IAW AMM 52-11-00. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,953 hrs · 21,543 cycles

6 EMER LIGHTS INOPERATIVE. PERFORMED OPERATIONS CHECK OF EMER LIGHT SYS IAW AMM 33-51-00. OPERATIONS CHECKED GOOD.

Part: BRAKE SYS — CONTAMINATED (MLG) · airframe 29,806 hrs · 21,438 cycles

UNABLE TO MAINTAIN DIRECTIONAL CONTROL ON TAKEOFF. REJECTED TAKEOFF. NOTICED STICKY BRAKE DURING TROUBLESHOOTING. BLED BRAKE SYS IAW AMM 32-43-00. OPERATIONS CHECKED ON ALL BRAKES GOOD.

Part: UNKNOWN — MALFUNCTIONED (CABIN) · airframe 29,794 hrs · 21,429 cycles

EMERGENCY LIGHTS CAME ON IN FLIGHT. PERFORMED OPERATIONS CHECK ON EMER LIGHTS ON GND IAW AMM 33-51-00. ALL OPERATIONS CHECKS OK. COULD NOT DUPLICATE PROBLEM.

Part: DOOR SEAL — DIRTY (PAX DOOR) · airframe 29,713 hrs · 21,375 cycles

MAIN PAX DOOR SQUEAL. INSPECTED & CLEANED MAIN PAX DOOR SEAL IAW AMM 52-11-00.

Part: DOOR SEAL — DIRTY (PAX DOOR) · airframe 29,702 hrs · 21,367 cycles

MAIN PAX DOOR SQUEAL. REMOVED DEBRIS FROM PAX DOOR SEAL IAW AMM 52-11-00.

Part: PSEU — MALFUNCTIONED (WARNING SYS) · airframe 29,029 hrs · 20,828 cycles

ALL CABIN DOORS INDICATE OPEN. POWERED DOWN ACFT, RE-RACKED PSEU, RE-ENERGIZED ACFT POWER, MSG CLEARED IAW AMM 32-61-00. OPERATIONS CHECKED NORMAL.

Part: UNKNOWN — MALFUNCTIONED (PAX DOOR) · airframe 28,937 hrs · 20,760 cycles

PAX DOOR SLAMS DOWN ON OPENING. INSPECTED DOOR & FOUND NO DAMAGE IAW 52-11-00. DEFERRED PAX DOOR ON DMI 33913184.

Part: CABLE — BROKEN (PAX DOOR) · airframe 28,964 hrs · 20,758 cycles

PAX DOOR ASSIST CABLE BROKEN. R & R PAX DOOR POWER ASSIST CABLE IAW 52-11-08. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: DOOR SEAL — DIRTY (PAX DOOR) · airframe 28,745 hrs · 20,595 cycles

PASSENGER DOOR SQUEALS IN FLIGHT. CLEANED PAX DOOR SEAL OF DEBRIS IAW AMM 12-21-00. PRESSURIZED ACFT IAW AMM 21-31-00. OPERATIONS CHECKED GOOD AT THIS TIME. NO NOISE OF DEFECTS NOTED. ACFT OK FOR SERVICE.

Part: FRAME — CORRODED (FUSELAGE) · airframe 28,741 hrs · 20,593 cycles

FRAME AT FS 364.00 IN FWD AVIONICS BAY HAS SIGNS OF CORROSION ON FWD FACE. REPAIRED FRAME BY CUTTING & REMOVING DAMAGED SECTION OF FRAME FROM STRINGER 24L TO 24R. CUT & DRILLED NEW FRAME SECTION PN SH670-32090-9. FABRICATED REPAIR PARTS & ASSEMBLED ALL PARTS IAW REO 670-53-21-687, DATED 3 AUG 2012.

Part: SKIN — CORRODED (FUSELAGE) · airframe 28,741 hrs · 20,593 cycles

FUSELAGE SKIN UNDER T CAS ANTENNA HAS CORROSION. REMOVED CORROSION WITH MATERIAL LOSS OF.005 FOUND TO BE WITHIN LIMITS IAW REO 670-53-21-1107 DATED 20 JUNE 2014, NDT PERFORMED.

Part: LATCH — LOOSE (SERVICE DOOR) · airframe 28,741 hrs · 20,593 cycles

SERVICE DOOR LATCH LOOSE. R & R LOOSE FASTENERS ON SERVICE DOOR LATCH IAW WITH SRM 51-42-10.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 28,741 hrs · 20,539 cycles

FORWARD AVIONICS DOOR SURROUND TWO CTR INTERCOSTAL AT STATION 364.00 ARE CORRODED. R & R TWO CTR INTERCOSTAL AT STATION 364.00 PN SW670-32075-3 & SW670-32075-4 IAW SRM 51-42-06, 51-42-21, 51-21-16 & AMM 52-70-08.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 28,741 hrs · 20,593 cycles

SIDE SEAT RAILS FS 708.00 TO 736.05 & FS 736.05 TO 761.85 SHOW SIGNS OF CORROSION. BLENDED CORROSION ON SIDE SEAT RAILS 708.00- 736.05 & 736.05- 761.85 FOUND TO BE OUT OF LIMITS IAW REO670-53-00-13 REV H 04 JUNE 2014. REPLACED WITH SERVICEABLE SIDE SEAT RAILS PN SH670-36-255-3 & SH670-37509-1 IAW AMM 53-00-49. ADDITIONAL PN FOR BELOW SH670-37509-1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 28,741 hrs · 20,593 cycles

LEFT SIDE SEAT RAIL FROM FS 708 TO 736.05 HAS CORROSION. BLENDED OUT CORROSION WITH .020 MATERIAL LOSS & FOUND TO BE WITHIN LIMITS IAW REO 670-53-00-013 REV H DATED 4 JUN 2014.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 28,741 hrs · 20,593 cycles

LINTEL STRINGER 03L IS CRACKED AT FS 280. REPAIRED STRINGER WITH LINTEL REPAIR KIT PN 670BA53040K1A IAW REO 670-53-21-493 REV C DATED 8 DEC 2011 & SB 670BA53-040 REV C DATED 20 SEP 2012.

Part: FRAME — CORRODED (FUSELAGE) · airframe 28,741 hrs · 20,593 cycles

FORWARD AVIONICS COMPARTMENT FRAME AT FS 319 IS CORRODED FROM STRINGER 26L TO 26R. EVALUATED CORROSION & FOUND TO BE OUT OF LIMIT. CUT & REMOVED CORRODED SECTION. CUT & INSTALLED NEW FRAME SECTOR PN 670-31355-1 & INSTALLED WITH NEW ANGLES PN S1710-4 & S6144-13. FABRICATED STRINGER CLEATS & SPLICE PARTS IAW REO 670-53-21-799, DATED 30 JAN 2012. REPAIR ACCOMPLISHED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 28,741 hrs · 20,593 cycles

LEFT SIDE SEAT RAIL AT FS 797 HAS SIGNS OF CORROSION. EVALUATED SEAT RAIL & FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013 REV H DATED 4 JUN 2014. R & R SEAT RAIL IAW AMM 53-00-49.

Part: LATCH — DIRTY (ESCAPE HATCH) · airframe 28,741 hrs · 20,593 cycles

CREW ESCAPE HATCH OUTER LATCH WON’T OPEN FROM OUTSIDE. CREW ESCAPE HATCH OUTER LATCH REMOVED & CLEANED IAW 51-26-00. REINSTALLED IAW AMM 52-22-02. OPERATIONS CHECKED GOOD.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 28,741 hrs · 20,593 cycles

FS 280 FLOOR CROSSBEAM IS CORRODED ON LT & RT SIDES. R & R ENTIRE CROSSBEAM WITH NEW ANGLES BA670-30069-7, BA670-30069-8, BA670-30069-9 & BA670-30069-11 IAW SRM 53-42-06. FABRICATED SHIMS IAW DWG BA670-30070 & INSTALLED IAW SRM 51-42-21.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 28,741 hrs · 20,593 cycles

T CAS CHANNEL CORRODED. R & R T CAS CHANNEL IAW SRM 51-42-06.

Part: ANGLE — CORRODED (SERVICE DOOR) · airframe 28,741 hrs · 20,593 cycles

SERVICE DOOR KICK ANGLE CORRODED. R & R SERVICE DOOR KICK ANGLE IAW SRM 51-42-06, 51-42-21 & 51-25-16.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 28,741 hrs · 20,593 cycles

GALLEY SERVICE DOOR FLOOR PROTECTOR L ANGLES, THREE FWD, SHOW SIGNS OF CORROSION. EVALUATED CORROSION, CLEANED THREE L ANGLES FOUND TWO NOT CORRODED & ONE CORRODED. R & R ONE CORRODED GALLEY SERVICE DOOR FLOOR PROTECTOR L ANGLE IAW SRM 51-42-06.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 28,741 hrs · 20,593 cycles

FS 280.00 CRAWLWAY ANGLE CORRODED. R & R ANGLE AT FS 280.00 IAW SRM 51-42-21 & 51-42-06.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 28,741 hrs · 20,593 cycles

PASSENGER DOOR KICK ANGLE SHOWS SIGNS OF CORROSION. R & R PAX DOOR KICK ANGLE IAW AMM 52-70-04, SRM51-41-02, 51-42-06, 51-42-21, 51-40-11 & 51-25-16.

Part: SERVICE DOOR — CORRODED (CABIN) · airframe 28,741 hrs · 20,593 cycles

GALLEY SERVICE DOOR LOWER CTR HAS SIGNS OF CORROSION. EVALUATED CORROSION, BLENDED AREA WITH .0003 MATERIAL LOSS. WITHIN LIMITS IAW SRM 51-42-01.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 28,741 hrs · 20,593 cycles

RIGHT SILL CORRODED AT FS 280 CROSSBEAM. R & R RT SILL AT FS 280 - 349 IAW SRM 51-42-06.

Part: STEP — CRACKED (PAX DOOR) · airframe 28,741 hrs · 20,593 cycles

PASSENGER DOOR BOTTOM MOVEABLE STEP DISBONDED & CRACKED. R & R BOTTOM STEP & TREAD IAW AMM 52-11-04. PANEL INSTALLED PN 601R31670-13, SN 72521. TREAD INSTALLED PN 601R40508-35.

Part: BUMPER — LOOSE (SERVICE DOOR) · airframe 28,741 hrs · 20,593 cycles

GALLEY SERVICE DOOR HINGE BUMPER IS LOOSE & DISPLACED. R & R BUMPER IAW AMM 20-21-00.

Part: DOOR SEAL — TORN (EMERGENCY EXIT) · airframe 28,741 hrs · 20,593 cycles

LEFT OVERWING EMER EXIT DOOR PRESS SEAL HAS FOUR TEARS ON AFT LOWER SIDE. R & R SEAL IAW AMM 52-21-07.

Part: DOOR SEAL — TORN (EMERGENCY EXIT) · airframe 28,741 hrs · 20,593 cycles

RIGHT OVERWING EMER EXIT DOOR PRESS SEAL HAS TEAR AT BOTTOM FWD CORNER. R & R SEAL IAW AMM 52-21-07.

Part: DOOR SEAL — DAMAGED (PAX DOOR) · airframe 28,741 hrs · 20,593 cycles

PASSENGER DOOR SEAL DAMAGED. R & R SEAL IAW AMM 52-11-07.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 28,741 hrs · 20,593 cycles

AFT FUSELAGE FAIRING, INTERNAL SUPPORT WEB STRUCTURE SPLICE AT BL0, FS 939 IS CORRODED. R & R WITH NEW ANGLE IAW SRM 51-42-06.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 28,741 hrs · 20,593 cycles

AT FRAME STATION 280 BEAM FLOOR SUPPORT CTR CORRODED. RECEIVED SERVICEABLE 280 BEAM FLOOR SUPPORT CTR TO BE INSTALLED IAW SRM 51-42-06. WORK ORDER 80234 WORK CARD 1063 REPLACEMENT OF 280 BEAM.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 28,741 hrs · 20,593 cycles

PASSENGER DOOR AFT DRAG ANGLE CRACKED. REPAIRED PAX DOOR DRAG ANGLE BY CUTTING AWAY DAMAGED SECTION & INSERTING NEW SECTION & SPLICES IAW REO 670-52-11-072 REV E DATED 26 OCT 2009.

Part: FRAME — CORRODED (FUSELAGE) · airframe 28,741 hrs · 20,593 cycles

FORWARD AVIONICS COMPARTMENT FRAME 333 FROM STRINGER 26L TO 26R IS CORRODED. REMOVED CORROSION WITH .001 MATERIAL LOSS. WITHIN LIMIT IAW SRM 53-21-06.

Part: FRAME — CORRODED (FUSELAGE) · airframe 28,741 hrs · 20,593 cycles

FORWARD AVIONICS COMPARTMENT FRAME 310 FROM 26L TO 26R IS CORRODED. REMOVED CORROSION WITH .003 MATERIAL LOSS. WITHIN LIMIT IAW SRM 53-21-06.

Part: FRAME — CORRODED (FUSELAGE) · airframe 28,741 hrs · 20,593 cycles

FORWARD AVIONICS COMPARTMENT FRAME 295 FROM 26L TO 26R IS CORRODED. REMOVED CORROSION WITH .002 MATERIAL LOSS. WITHIN LIMIT IAW SRM 53-21-06.

Part: STOP FITTING — OUT OF ADJUST (PAX DOOR) · airframe 28,741 hrs · 20,593 cycles

PASSENGER DOOR WARNING MSG. INSPECTED & FOUND OUTER HANDLE ON MAIN PAX DOOR OUT OF ADJUSTMENT. ADJUSTED HANDLE STOP IAW AMM 52-11-02 & PERFORMED OPERATIONS CHECK IAW AMM 52-00-00, OPERATIONS CHECKED GOOD, NO MSG NOTED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 28,734 hrs · 20,587 cycles

PASSENGER DOOR OUTER HANDLE CAUTION MSG. OPERATIONS CHECKED PAX DOOR & PROX SENSORS IAW AMM 52-11-00, OPERATIONS CHECKED GOOD AT THIS TIME.

Part: HANDLE — LOOSE (PAX DOOR) · airframe 28,734 hrs · 20,587 cycles

PASSENGER DOOR HANDLE LOOSE. R & R PAX DOOR HANDLE IAW AMM 52-11-02, PERFORMED OPERATIONS CHECK OF DOOR HANDLE, NO DEFECTS NOTED AT THIS TIME.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,393 hrs · 20,295 cycles

3RD CEILING EMERGENCY FLOODLIGHT INOPERATIVE. RELAMPED CEILING EMERGENCY FLOODLIGHT IAW AMM 33-51-07, OPERATIONS CHECKED GOOD.

Part: PROXIMITY SENSOR — FAILED (PAX DOOR) · airframe 28,297 hrs · 20,214 cycles

MULTIPLE PAX DOOR HANDLE CAUTION MESSAGES IN FLIGHT. R & R PAX DOOR HANDLE PROXIMITY SENSOR PX 107, SYS OPERATIONS CHECKED GOOD IAW AM 52-70-04.

Part: PROXIMITY SENSOR — DIRTY (PAX DOOR) · airframe 28,282 hrs · 20,204 cycles

PAX DOOR OUTER HANDLE CAUTION MSG. CLEANED PROX SENSOR PX 107, PERFORMED DOOR OPERATIONS CHECK IAW CRJ700 AMM 52-11-00. OPERATIONS CHECKED GOOD, OK FOR SERVICE.

Part: INDICATION SYS — MALFUNCTIONED (PAX DOOR) · airframe 28,250 hrs · 20,176 cycles

PASSENGER DOOR OUT CAUTION MSG. DEFERRED PAX DOOR INDICATING SYS IAW MEL 52-70-01 CAT A.

Part: CABLE — BROKEN (CABIN DOOR) · airframe 28,120 hrs · 20,073 cycles

MAIN CABIN DOOR SUPPORT WHEEL CABLE BROKEN. R & R MAIN CABLE DOOR SUPPORT WHEEL IAW CRJ700 AMM 52-11-13, OPERATIONS CHECK IAW CRJ700 AMM 52-11-00, OPERATIONS CHECKED GOOD AT THIS TIME.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,053 hrs · 20,024 cycles

EMERGENCY CEILING LIGHT AT ROW 15 INOPERATIVE. R & R OVERHEAD EMERGENCY FLOOD LIGHT BULB IAW AMM 33-51-09. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: LIGHT — LOOSE (CABIN) · airframe 27,242 hrs · 19,396 cycles

LEFT EMERGENCY LIGHT PEELING UP AT ROW 12. SECURED EMERGENCY LIGHT IAW AMM 33-51-00.

Part: ROD END — DAMAGED (PAX DOOR) · airframe 26,876 hrs · 19,112 cycles

PAX DOOR FWD HAND RAIL ROD END DAMAGED. R & R DOOR ROD END IAW AMM 52-11-05.

Part: ROD END — DAMAGED (HAND RAIL) · airframe 26,876 hrs · 19,112 cycles

PAX DOOR FWD HAND RAIL ROD END DAMAGED. R & R PAX DOOR FWD ROD END IAW AMM 52-11-05.

Part: FAIRING — MISSING (PAX DOOR HINGE) · airframe 26,798 hrs · 19,054 cycles

PAX DOOR AFT HINGE FAIRING MISSING.

Part: WARNING MESSAGE — ILLUMINATED (BLEED SYS) · airframe 26,493 hrs · 18,828 cycles

LEFT BLEED CAUTION MESSAGE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 2,545,704 hrs · 18,045 cycles

ROW 15 CEILING LEVEL EMERGENCY LIGHT INOPERATIVE. R & R LIGHT BULB.

Part: HANDLE — UNSECURE (CARGO DOOR) · airframe 24,959 hrs · 17,683 cycles

AFT CARGO DOOR CAUTION MSG DURING CLIMB OUT, AFT CARGO DOOR MSG SHORTLY AFTER PROX 2 FAULT STATUS MESSAGE. PROPERLY STOWED AFT CARGO HANDLE AND PERFORMED OP'S CHECK IAW AMM 52-70-02, OP'S CHECK GOOD AT THIS TIME.

Part: WARNING LIGHT — FALSE ACTIVATION (CARGO DOOR) · airframe 24,959 hrs · 17,683 cycles

AFT CARGO DOOR CAUTION MESSAGE WITH PROXIMITY SYS FAULT 2 STATUS MSG IN FLIGHT. VERIFIED AFT CARGO DOOR IS CLOSED AND LATCHED. APPLIED SPEED TAPE TO EXTERIOR OF ACFT HANDLE. ACFT SAFE FOR ONE TIME FLIGHT.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 24,606 hrs · 17,425 cycles

RT FORWARD EMERGENCY LIGHT FACING AFT IS LOOSE. INSTALLED RT FWD EMERGENCY LIGHT LENS IAW AMM 33-51-15.

Part: SWITCH — FAILED (PAX DOOR) · airframe 24,442 hrs · 17,302 cycles

PASSENGER DOOR WARNING MESSAGE WHILE PARKED ON TARMAC. R & R PAX DOOR SWITCH PX 101. OP'S CHECKED GOOD IAW AMM 52-70-04.

Part: SENSOR — DIRTY (PAX DOOR) · airframe 24,442 hrs · 17,302 cycles

PASSENGER DOOR WARNING MESSAGE, PERFORMED GVI OF PX101 SENSOR, WIRING AND CONNECTORS. CLEANED SENSOR AND PERFORMED OPS CHECK OF PASSENGER DOOR IAW AMM 52-70-00, OPS CHECKED GOOD AT THIS TIME.

Part: LENS — DELAMINATED (EMERGENCY LIGHT) · airframe 24,434 hrs · 17,296 cycles

EXTERIOR EMERGENCY LIGHT LENS AFT OF MAIN PASSENGER DOOR DELAMINATING. R & R LENS IAW AMM 33-51-15.

Part: LENS — DELAMINATED (EMERGENCY LIGHTS) · airframe 24,434 hrs · 17,296 cycles

EXTERIOR EMERGENCY LIGHT LENS AFT OF MAIN PASSENGER DOOR DELAMINATING, R & R LENS IAW AMM 33-51-15.

Part: ANGLE — DAMAGED (ZONE 200) · airframe 23,852 hrs · 16,871 cycles

PASSENGER DOOR MID CAP DAMAGED BEYOND SERVICEABLE LIMITS. R & R PASSENGER DOOR KICK ANGLE MID CAP, IAW SRM 51-41-02, 51-42-06. 51-40-11.

Part: SILL — CORRODED (ZONE 100) · airframe 23,852 hrs · 16,871 cycles

FS 280, SILL CORRODED BEYOND SERVICEABLE LIMITS. R & R SILL AND INSTALLED IAW SRM 51-40-11, 51-42-13, 51-42-06.

Part: BULKHEAD WEB — CORRODED (ZONE 100) · airframe 23,852 hrs · 16,871 cycles

FS 280 LT BULKHEAD WEB CORRODED BEYOUND SERVICEABLE LIMITS. R & R FS 280 LT BULHEAD WEB LAW SRM 51-42-06, 51-42-13, 51-42-21, 51-23-00, REO670-53-11-052.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 23,852 hrs · 16,871 cycles

PASSENGER DOOR LOWER THRESHOLD KICK ANGLE CORRODED BEYOND SERVICEABLE LIMITS. REMOVED AND CLEANED CORROSION FROM KICK ANGLE,.004" MATERIAL REMOVED, PART WITHIN LIMITS, TREATED, PRIMED,AND PAINTED WITH TOPCOAT LAW SRM 53-21-23, 51-21-06,51-25-06, 51-25-16, 51-42-06, AMM 51-21-01, 51-23-00. (REF W/O 80069, W/C 1070)

Part: ANGLE — DAMAGED (ZONE 200) · airframe 23,852 hrs · 16,871 cycles

PASSENGER DOOR END CAPS DAMAGED BEYOND SERVICEABLE LIMITS. R & R PASSENGER DOOR KICK ANGLE END CAP, LAW SRM 53-21-23, 51-42-06.

Part: ANGLE — DAMAGED (ZONE 200) · airframe 23,852 hrs · 16,871 cycles

PASSENGER DOOR FORWARD CAP DAMAGED BEYOND SERVICEABLE LIMITS. R & R PASSENGER DOOR KICK ANGLE FORWARD CAP, LAW SRM 53-21-23, 51-42-06. 51-40-11, AMM 51-21-01-380-801.

Part: ANGLE — CORRODED (ZONE 100) · airframe 23,852 hrs · 16,871 cycles

FS 260 TO 280, LT RECEPTICLE ANGLE CORRODED BEYOND SERVICEABLE LIMITS. REMOVED AND CLEANED CORROSION, TREATED AND INSTALLED PROTECTIVE FINISH IAW SRM 51-21-11, 51-25-06.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 23,852 hrs · 16,871 cycles

FS 280 FLOORBEAM CORRODED BEYOND SERVICEABLE LIMITS. R & R FS 280 FLOORBEAM, LAW REO 670-53-11-0047 & REO 670-53-11-046 AND SRM 51-42-20, 51-42-06.

Part: FLOOR SUPPORT — CRACKED (ZONE 100) · airframe 23,852 hrs · 16,871 cycles

FLOOR SUPPORT ANGLE AT BS 310 TO 333, FOUND CRACKED. FABRICATED AND INSTALLED REPLACEMENT FLOOR SUPPORT IAW SRM 51-25-06 AND DG SH670-33332.

Part: ANGLE — DEFORMED (ZONE 200) · airframe 23,852 hrs · 16,871 cycles

PASSENGER DOOR KICK ANGLE CLOSING PLATE DAMAGED BEYOND SERVICEABLE LIMITS (DEFORMED/DENTED). R & R PASSENGER DOOR KICK ANGLE CLOSING PLATE IAW SRM 53-21-23, 51-42-06, 51-42-21, 51-40-11 AND AMM 51-21-01-380-801.

Part: CABLE GUIDE — UNSAFETIED (ZONE 800) · airframe 23,852 hrs · 16,871 cycles

PASSENGER DOOR SUPPORT WHEEL BRACKET PULLEY CABLE GUIDES NOT SAFETIED. SAFETIED PASSENGER DOOR SUPPORT WHEEL BRACKET PULLEY CABLE GUIDES IAW AMM 52-11-13-400-802.

Part: FLEX LINE — BROKEN (OXYGEN SYSTEM) · airframe 22,308 hrs · 15,846 cycles

O2 BOTTLE PRESSURE FLEX LINE TO O2 BOTTLE BROKE. (SERVICE) REPLACED O2 BOTTLE AND O2 BOTTLE PRESSURE FLEX LINE. P/N ON 38035-04 / P/N ON 806371-120 S/N OFF ALT281-14090.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,608 hrs · 15,372 cycles

THE 2ND FROM AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4771) RELAMPED EMERGENCY LIGHT.

Part: WIRE — DISCONNECTED (CABIN) · airframe 20,166 hrs · 14,431 cycles

RIGHT GALLEY EMERGENCY LIGHT INOPERATIVE. (FLT 4781) RECONNECTED WIRES AT RIGHT GALLEY EMERGENCY LIGHT.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 19,454 hrs · 13,951 cycles

FLOOR STRUCTURE AT FS 580, RBL 9.0 CORRODED. (C CHECK) REPAIRED PER SRM.

Part: STRUCTURE — CORRODED (PAX DOOR) · airframe 19,454 hrs · 13,951 cycles

PAX DOOR LOWER AFT CORNER (HINGE END) CORRODED. (C-CHECK) REMOVED AND REPLACED PAX DOOR LOWER AFT CORNER PER SRM.

Part: CHANNEL — CORRODED (PAX DOOR) · airframe 19,454 hrs · 13,951 cycles

PAX DOOR LOWER CHANNEL HAS CORROSION ON INSIDE UNDER DRAIN RAMP. (C-CHECK) REMOVED AND REPLACED CHANNEL PER SRM.

Part: SKIN — CORRODED (PAX DOOR) · airframe 19,454 hrs · 13,951 cycles

PAX DOOR INNER SKIN REQUIRES REPLACEMENT DUE TO CORROSION. (C-CHECK) REMOVED AND REPLACED PAX DOOR INNER SKIN PER SRM.

Part: BEAM — CORRODED (FUSELAGE) · airframe 19,739 hrs · 14,153 cycles

FS 280 BEAM CORRODED ON BOTH SIDES. (C-CHECK) REPLACED PER SRM.

Part: SKIN — CORRODED (PAX DOOR) · airframe 19,739 hrs · 14,153 cycles

PAX DOOR INNER SKIN REQUIRES REPLACEMENT DUE TO SEVERE CORROSION DAMAGE AT ACCESS PANEL CUTOUTS. (C-CHECK) REPAIRED PER SRM.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 19,739 hrs · 14,153 cycles

PAX DOOR INTERCOSTAL CRACKED AT STA 344 STR 16. (C-CHECK) REPAIRED PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,907 hrs · 12,824 cycles

NR 5 EMERGENCY EXIT LIGHT INOP. (FLT 4591)RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,668 hrs · 12,649 cycles

SECOND FROM AFT OVERHEAD EMERGENCY LIGHT INOP. (FLT 4739) RELAMPED EMERGENCY LIGHT.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 16,780 hrs · 12,009 cycles

FLT 4870 - EMERGENCY LIGHT AFT OF SERVICE DOOR INOP. RELAMPED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 16,454 hrs · 11,773 cycles

FLT 4437 - RIGHT EMERGENCY EXIT SIGN HAS ONE OF THREE BULBS OUT. RELAMPED.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 15,554 hrs · 11,105 cycles

FLT 4399 - TWO EMERGENCY LIGHTS AND EXIT LIGHT IN AFT CABIN INOP. REPLACED BATTERY PACK.

Part: OXYGEN MASK — UNWANTED DEPLOY (LAVATORY) · airframe 14,810 hrs · 10,601 cycles

THE O2 MASK DEPLOYED IN FORWARD LAV. FLIGHT 3800. RESTOWED O2 MASK PER MM 35-20-00.

Part: IGNITION LEAD — ARCED (RT ENGINE) · airframe 14,783 hrs · 10,581 cycles

RIGHT ENGINE IGNITION B-IGNITOR AND LEAD SHOW SIGNS OF ARCING. REPLACED THE IGNITION B IGNITOR AND LEAD IAW 74-20-03. OPS CHECK GOOD.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 15,376 hrs · 10,985 cycles

C-CHECK, FS 280 CROSSBEAM CRACKED. REPLACED PER SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,376 hrs · 10,985 cycles

C-CHECK, RIGHT SIDE FORWARD SEAT TRACK RAIL CORRODED, REPLACED.

Part: BOLT — CORRODED (LT MLG) · airframe 15,376 hrs · 10,985 cycles

C-CHECK, LEFT AND RIGHT MAIN LANDING GEAR OUTBOARD PINTLE PIN SLEEVE BOLTS CORRODED, REPLACED.

Part: WEB — CRACKED (PAX DOOR) · airframe 15,376 hrs · 10,985 cycles

C-CHECK, PASSENGER DOOR FORWARD WEB CRACKED AT ZONE 2. REPAIRED PER REO.

Part: WEB — CRACKED (PAX DOOR) · airframe 15,376 hrs · 10,985 cycles

C-CHECK, PASSENGER DOOR AFT WEB CRACKED AT ZONE 2 AND 3. REPAIRED PER REO.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 15,376 hrs · 10,985 cycles

C-CHECK, FS 280 COCKPIT FLOOR SUPPORT ANGLE CRACKED. REPLACED PER SRM.

Part: SENSOR — DAMAGED (LT AOA) · airframe 13,692 hrs · 9,813 cycles

FLT 4029 - DURING TAKEOFF, RECEIVED A STALL WARNING MESSAGE ALONG WITH AN AURAL WARNING. REPLACED LEFT AOA VANE ASSEMBLY IAW MM 27-35-05. OPS CHECK GOOD, PN C1625AA, SN OFF 532.

Part: BUSHING — CORRODED (ENGINE MOUNT) · airframe 12,741 hrs · 9,201 cycles

RIGHT ENGINE FORWARD MOUNT LINK BUSHING IS CORODED. INSTALLED NEW LINK WITH NEW BUSHING IAW MM 71-00-00.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 12,525 hrs · 9,066 cycles

CRACK IN PAX DOOR AFT DRAG ANGLE. REPAIRED CRACK IN PAX DOOR AFT DRAG ANGLE IAW REO 670-52-11-0054.

Part: OXYGEN MASK — UNWANTED DEPLOY (LAVATORY) · airframe 11,571 hrs · 8,496 cycles

THE O2 MASKS IN FORWARD LAV DEPLOYED IN FLIGHT. RESTOWED LAV O2 MASKS.

Part: CROSSBEAM — CRACKED (FS 280) · airframe 11,048 hrs · 8,166 cycles

FLOOR SUPPORT CROSSBEAM IS CRACKED. REPAIRED CROSSBEAM I/A/W REO 670-53-11-047.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 10,329 hrs · 7,686 cycles

FLIGHT 4998 - CAPTAIN'S WINDSHIELD SHATTERED DURING CRUISE. SPARKS NOTED ON LEFT CORNER PRIOR TO SHATTERING. DECLARED EMERGENCY AND DIVERTED TO LGA. LANDED WITHOUT INCIDENT. REPLACED CAPTAIN'S WINDSHIELD.

Part: BLEED VALVE — FAULTED (RT ENGINE) · airframe 10,130 hrs · 7,547 cycles

FLIGHT 5456 - RIGHT ENGINE BLEED CAUTION MESSAGE DURING CLIMB, FLIGHT RETURNED TO THE FIELD. CHECKED FAULT LOG IN MDC CURRENT AND HISTORY NO FAULTS OR MESSAGES PRESENT. PERFORMED OPS CHECK OF BLEED SYSTEM, ALL CHECKS GOOD.

Part: SMOKE DETECTOR — FAULTY (AFT LAVATORY) · airframe 9,554 hrs · 7,194 cycles

FLIGHT 5410 - DURING CLIMBOUT OF COS RECEIVED AN AFT LAVATORY SMOKE WARNING MESSAGE, FLIGHT RETURNED TO THE FIELD. REPLACED THE AFT LAVATORY SMOKE DETECTOR.

Part: BATTERY — FAULTY (EMERGENCY LIGHT) · airframe 8,762 hrs · 6,683 cycles

FLIGHT 5379 - DURING TEST OF THE EMERGENCY LIGHTING, SYSTEM ONLY ILLUMINATED MOMENTARILY THEN EXTINGUISHED. REPLACED THE AFT CABIN CEILING EMERGENCY BATTERY PACK.

Part: BATTERY — FAULTY (EMERGENCY LIGHT) · airframe 8,762 hrs · 6,683 cycles

FLIGHT 5379 - DURING TEST OF THE EMERGENCY LIGHTING, SYSTEM ONLY ILLUMINATED MOMENTARILY THEN EXTINGUISHED. REPLACED THE CENTER CABIN CEILING EMERGENCY BATTERY PACK.

Part: BATTERY — FAULTY (EMERGENCY LIGHT) · airframe 8,762 hrs · 6,683 cycles

FLIGHT 5379 - DURING TEST OF THE EMERGENCY LIGHTING, SYSTEM ONLY ILLUMINATED MOMENTARILY THEN EXTINGUISHED. REPLACED THE FORWARD CABIN CEILING EMERGENCY BATTERY PACK.

Part: BATTERY — FAULTY (EMERGENCY LIGHT) · airframe 8,762 hrs · 6,683 cycles

FLIGHT 5379 - DURING TEST OF THE EMERGENCY LIGHTING, SYSTEM ONLY ILLUMINATED MOMENTARILY THEN EXTINGUISHED. REPLACED THE EMERGENCY BATTERY PACK IN THE AVIONICS BAY.

Part: CONTROL UNIT — FAULTY (AVIONICS BAY) · airframe 8,285 hrs · 6,384 cycles

FLIGHT 4985 - AFTER TAKEOFF FROM ORD WITH A/P ENGAGED, RECEIVED A STAB CHANNEL 2 WARNING. REPLACED THE NR 2 SSCU.

Part: SKIN — CORRODED (BS 364-394) · airframe 7,849 hrs · 6,066 cycles

SEVERAL MINOR NICKS AROUND THE CIRCUMFERENCE OF AVIONICS BAY DOOR CUTOUT. REPAIRED AVIONICS BAY DOOR CUTOUT IAW BRAS EO 601R-53-7495.

Part: SKIN — CORRODED (BS 364-394) · airframe 7,849 hrs · 6,066 cycles

CORROSION FWD EDGE OF AVIONICS BAY DOOR CUTOUT. REMOVED CORROSION IAW BRAS EO 601R-53-7495.

Part: WARNING LIGHT — ILLUMINATED (SPOILERS) · airframe 7,383 hrs · 5,704 cycles

FLIGHT 5289 - SPOILERS CAUTION MESSAGE. LEFT GROUND LIFT DUMP INOPERABLE. RESET SYSTEM NO DEFECTS NOTED.

Part: FRAME — CORRODED (FUSELAGE) · airframe 6,764 hrs · 5,217 cycles

FS 280 - FUSELAGE TRANSVERE BEAM IS CORRODED BEYOND LIMITS. PERFORMED A MAJOR REPAIR TO FS 280 TRANSVERSE BEAM BY REMOVING CORRODED BEAM AND INSTALLING NEW BEAM P/N CC670-34175-71AW CRJ 700 SRM 51-42-06-001-001-A01 AND INSTALLING REPAIR DOUBLERS P/NS 670-53-11-047-2 AND 670-53-11-047-3 AND INSTALLED RADIUS PLATE PN 670-53-11-047-4 IAW BOMBARDFIER REO 670-53-11-047 REV A.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 6,764 hrs · 5,217 cycles

FS 280 LEFT AND RIGHT LOWER BULKHEAD WEBS (FLOOR LEVEL) ARE CORRODED BEYOND LIMITS. PERFORMED A MAJOR REPAIR TO FS 280 LOWER BULKHEAD WEBS BY REMOVING AND REPLACING CORRODED WEBS IAW CRJ 700 SRM 51-42-06-001-001-A01 P/NS 670-53-11-052-1 AND 670-53-11-052-2.

Part: TORQUE TUBE — CORRODED (NLG) · airframe 6,764 hrs · 5,217 cycles

NLG TORQUE TUBE AND OUTER CYCLINDER ARE CORRODED. PERFORMED A MAJOR REPAIR TO NLG BY REMOVING AND REPLACING THE TORQUE TUBE P/N 52105-1 IAW CRJ 700 AMM 32-21-22-400-801-A02 AND REMOVING CORROSION ON OUTER CYLINDER IAW GOODRICH SCR DAO NR 94-0-01 AND BOMBARDIER REO 670-32-21-053. REFERENCE BOMBARDIER SB 670BA-32-013 REV B AND GOODRICH 52000-32-16 DATED MAY 20/04.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILERS) · airframe 6,520 hrs · 5,031 cycles

FLIGHT 5866 SPOILERON AND FLIGHT SPOILER CAUTION. RESET THE SSCU AND SYSTEM OPERATION NORMAL. COULD NOT DUPLICATE.

Part: WARNING LIGHT — ILLUMINATED (E/E BAY DOOR) · airframe 6,451 hrs · 4,970 cycles

FLIGHT 5286 DURING TAKEOFF RECEIVED AN AVIONICS BAY DOOR CAUTION MESSAGE, ABORTED TAKEOFF AND RETURNED TO THE GATE. DEFERRED DOOR INDICTION PER MEL.

Part: WARNING SYSTEM — ACTIVATED (E/E BAY DOOR) · airframe 6,179 hrs · 4,752 cycles

FLIGHT 5511 AVIONICS DOOR WARNING DURING T/O. DEFERRED MAINT ON DOOR WARNING PER MEL.

Part: BLADE — DIRTY (COMPRESSOR FAN) · airframe 5,462 hrs · 4,197 cycles

FLIGHT 4997 - N1 VIBE, BECAME UNCONTROLLABLE. REPLACED THE ENGINE FAN BLADES.

Part: WARNING LIGHT — ILLUMINATED (THRUST REVERSER) · airframe 4,038 hrs · 3,094 cycles

FLIGHT 5249 RT THRUST REVERSER UNSAFE CAUTION DURING T/O. DEFERRED MAINT ON T/R PER MEL.

Part: CONTROL UNIT — MALFUNCTIONED (AVIONICS) · airframe 3,251 hrs · 2,483 cycles

FLIGHT 5660 FORWARD AND AFT LAV SMOKE WARNING. REPLACED THE FIDEY CONTROL UNIT.

Part: PANEL — MALFUNCTIONED (RUDDER TRIM) · airframe 2,650 hrs · 2,025 cycles

DURING TAKE OFF RUDDER TRIM MOVED 1 UNIT LT. REPLACED THE RUDDER TRIM SWITCH PANEL.

Part: DAMPER — MALFUNCTIONED (AUTOPILOT SYS) · airframe 2,374 hrs · 1,815 cycles

FLIGHT 5666 DURING TAKEOFF ROLL RECEIVED A YAW DAMPER NR 2 MESSAGE. REJECTED TAKEOFF AND AIRCRAFT RETURNED TO THE GATE. CYCLED POWER TO THE LEFT AND RIGHT AUTOMATIC FLIGHT CONTROL SYSTEM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 2,349 hrs · 1,804 cycles

FS 1098.20 BULKHEAD WEB BETWEEN STRINGERS 8L AND 9L IS CRACKED. REPAIRED BY REMOVING DAMAGE AND INSTALLING A BATHTUB FITTING IAW BOMBARDIER, INC REO 670-53-61-034 REV B.

Part: RELAY — MALFUNCTIONED (THRUST REVERSER) · airframe 1,233 hrs · 941 cycles

FLIGHT 5743 LEFT THRUST REVERSER UNSAFE MESSAGE DURING FLIGHT. REPLACED RELAYS K27 AND K29.

Part: WARNING LIGHT — ACTIVATED (THRUST REVERSER) · airframe 1,230 hrs · 938 cycles

FLIGHT 5877 LEFT THRUST REVERSER UNSAFE MESSAGE DURING TAKE-OFF, ABORTED AND RETURNED TO THE GATE. DEFERRED LEFT THRUST REVERSER PER MEL.

Part: COMPUTER — MALFUNCTIONED (AVIONICS) · airframe 182 hrs · 140 cycles

FLIGHT 5899 FLAPS FAIL CAUTION MESSAGE.REPLACED THE SFECU