N376CA

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 45,522 hrs · 36,230 cycles

RIGHT REAR EMERGENCY LIGHT INOPERATIVE. R & R RT REAR EMERGENCY LIGHT BULB IAW AMM 33-51-15.

Part: BUSHING — LOOSE (ZONE 500 AILERON) · airframe 44,460 hrs · 35,084 cycles

"DURING INSTALLATION NEW BUHINGS LH AILERON, OVERSIZE ON LUG ""L1,L2,L5,L6"" WAS DETECTED OVERSIZE BUSHINGS OF LUG L1,L2,L5 & L6 WERE FABRICATED AND INSTALLED PER REO 670-57-61-107 REV-B "

Part: FRAME — CRACKED (ZONE 200) · airframe 44,460 hrs · 35,084 cycles

CRACK AT FRAME FS 319.00 BTW STGR 1RH TO STGR 2RH AT CABIN PAX. FRAME FS 319.00 BTW STGR 1RH TO STGR 2RH AT CABIN PAX WAS REPAIRED PER EA CRJ753-18820 REV IR

Part: HINGE — CORRODED (ZONE 100) · airframe 44,460 hrs · 35,084 cycles

CORROSION AND DEEP NICKS IN FWD AND AFT HINGE FITTING LOCATED NEAR TO STRG 25L AND BETWEEN FS533.00/FS581.00 IN FORWARD BAGGAGE BAY DOOR CUTOUT FWD AND AFT HINGE FITTING LOCATED NEAR TO STRG 25L AND BETWEEN FS533.00/FS581.00 IN FORWARD BAGGAGE BAY DOOR CUTOUT WERE REPLACED PER CRJ700 SRM 51-41-02-001-001-A01

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 44,460 hrs · 35,084 cycles

CORROSION IN ANGLE LOCATED IN CROSS BEAM UNDER FLOOR LEVEL IN FS349.00 AND RBL 30.0 AT FLOOR STRUCTURE PASSENGER CABIN DUE TO EXCESSIVE DAMAGE IN ANGLE LOCATED IN CROSS BEAM UNDER FLOOR LEVEL IN FS349.00 AND RBL 30.0 AT FLOOR STRUCTURE PASSENGER CABIN WAS FABIRCATED AND REPLACED PER CRJ700 SRM 51-10-06-001-001-A01, SRM 51-42-06-001-001-A01 AND EA CRJ752-18956 REV A

Part: DRAG ANGLE — CRACKED (ZONE 300) · airframe 44,460 hrs · 35,084 cycles

AFTER NDT EVALUATION (CRACK NOT VISIBLE), CRACK AT FWD DRAG ANGLE, VERTICAL STABILIZER RH SIDE. FWD DRAG ANGLE AT VERTICAL STABILIZER RH SIDE WAS REPAIRED PER CRJ700 SRM 55-31-00-201-001-A01

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 44,460 hrs · 35,084 cycles

CORROSION IN SEAT TRACK LOCATED AT LBL 27.0 AND BETWEEN FS394.00/FS409.00 IN FLOOR STRUCTURE FWD PASSENGER CABIN DUE TO EXCESIVE CORROSION AT SEAT TRACK LOCATED AT LBL 27.0 AND BETWEEN FS394.00/FS409.00 IN FLOOR STRUCTURE FWD PASSENGER CABIN WAS REPLACED PER CRJ-700 SRM 53-21-49-101-001-A01, CRJ-700 AMM 53-00-49-000-801 (CONFIG A03) AND AMM 53-00-49-400-801 (CONFIG A17)

Part: STRIKER — WORN (ZONE 100) · airframe 44,460 hrs · 35,084 cycles

"INITIAL INSPECTION: WEAR IN MID FWD AND MID AFT SEAL STRIKER IN FWD BAGGAGE BAY DOOR CUTOUT LOCATED IN FS533.00 AND FS581.00 MID FWD AND MID AFT SEAL STRIKER OF FWD BAGGAGE BAY DOOR CUTOUT LOCATED IN FS533.00 AND FS581.00 WERE REPLACED PER CRJ700 SRM 51-42-06-001-001-A01 AND SRM 51-41-02-001-001-A01 / "

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 44,460 hrs · 35,084 cycles

CORROSION ON FLOOR PANEL SUPPORT ANGLE BTW LBL 11 TO RBL11 AT CROSSBEAM FS280. FLOOR PANEL SUPPORT ANGLE BTW LBL 11 TO RBL11 AT CROSSBEAM FS280 WAS REPLACED PER CRJ 700 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01

Part: DRAG ANGLE — CRACKED (ZONE 300) · airframe 44,460 hrs · 35,084 cycles

IN REFERENCE TO CARD 700-53-900-310: CRACK ON AFT DRAG ANGLE AT VERTICAL STABILIZER RH SIDE. AFT DRAN ANGLE AT VERTICAL STABILIZER RH SIDE WAS REPAIRED PER CRJ-700 SRM 55-31-00-201-001-A01

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 44,460 hrs · 35,084 cycles

CRACK ON CROSSBEAM FS280.00 BTW RBL13.00/RBL15.00 AT CABIN FLOOR STRUCTURE. CROSSBEAM FS280.00 BTW RBL13.00/RBL15.00 AT CABIN FLOOR STRUCTURE WAS REPLACED PER REO 670-53-11-579REV-B

Part: LAMP — INOPERATIVE (UNKNOWN) · airframe 41,954 hrs · 32,654 cycles

3 EMERGENCY LIGHT BULBS INOP IN GALLEY. RE-LAMPED EMERGENCY LIGHT P/N: 6100928 IAW CRJ 700 AMM 33-51-05. OPS C HECK GOOD.

Part: LAMP — INOPERATIVE · airframe 41,566 hrs · 32,296 cycles

FOUND SERVICE DOOR EMERGENCY LIGHT INOP DURING LINE CHECK. REMOVED AND REPLACED SERVICE DOOR EMERGENCY LIGHT BULB IAW CRJ-700 AMM 33-50-01. PERFORMED OPS CHECK OF PAX DOOR EMERGENCY LIGHT. OPS CHECK GOOD. P/N ON/OFF: 8GA411060-06

Part: FITTING — CORRODED · airframe 39,669 hrs · 30,604 cycles

UPON REMOVAL OF RH OUTBOARD SIDE STAY BUSHING, FOUND CORROSION ON SIDE STAY FITTING UNDER BUSHING HAT OUTBOARD SIDE. REPLACED RH SIDESTAY FITTING OUTBOARD BUSHING IAW REO 670-57-11-183 REV-- WVAC EMP STAMP # 750 MTC

Part: HANDLE — CRACKED · airframe 39,669 hrs · 30,604 cycles

PAX DOOR INNER HANDLE IS CRACKED. P/N 000-31887-15. REMOVED AND REPLACED PAX DOOR INNER HANDLE IAW CRJ700 SRM 51-40-11-001-001-A01 AND 51-43-00-001-001-A01. INSTALLED IAW CRJ 700 AMM 52-11-02-400-809-A01. OPS CHECK GOOD. WVAC EMP STAMP # 776 MTC

Part: SKIN — CORRODED · airframe 39,669 hrs · 30,604 cycles

PAX DOOR SKIN IS CORRODED IN SEVERAL PLACES. "AFTER FURTHER CLEANING AND INSPECTION FOUND SKIN TO BE BEYOND REPAIR. REFERENCE CORRECTIVE ACTION #1 FOR REPLACEMENT OF PAX DOOR SKIN. WVAC EMP STAMP # 794 MTC."

Part: ANGLE — BENT · airframe 39,669 hrs · 30,604 cycles

ATTACHMENT ANGLE UNDER PNL 692BB IS BENT. MARKED WITH TAPE. REMOVED, FABRICATED AND REPLACED ANGLE IAW CRJ 700 SRM

Part: YOKE — CHAFED · airframe 39,669 hrs · 30,604 cycles

R/H ENGINE FWD MOUNT YOKE CHAFFED ON TOP SIDE - COMPLIED WITH STEP M SECTION 7.1 OF GREO 670-71-21-057 REV---DATED 2013-09-13. WVAC EMP STAMP # 794 MTC

Part: RETAINER — DAMAGED · airframe 39,669 hrs · 30,604 cycles

LOWER SEAL RETAINER BESIDE HINGE IS DAMAGED BEYOND SERVICEABLE LIMITS, P/N:601R318722-1. REMOVED & REPLACED PAX DOOR LOWER SEAL RETAINER P/N 601R318722-1 IAW CRJ 700 SRM 51-40-11-001-001-A01 & 51-42-06-001-001-A01 REV 38 7-25-20. WVAC EMP # 56392

Part: WEB — CRACKED · airframe 39,669 hrs · 30,604 cycles

PAX DOOR AFT WEB HAS CORROSION IS CRACKED AND REQUIRES REPLACEMENT PN:601R317071-7. FIT, DRILLED & INSTALLED NEW AFT WEB P/N 601R317071-11.

Part: BRACKET — CORRODED · airframe 39,669 hrs · 30,604 cycles

ITEM #76 & #77 BRACKET P/N:601R31902-347 & TARGET P/N:601R31902-349 HAS CORROSION & IS DAMAGED BEYOND SERVICEABLE LIMITS & REQUIRE REPLACEMENT. REMOVED & REPLACED BRACKET 601R31902-347 & TARGET IAW CRJ 700 SRM 51-40-11-001-001-A01, INSTALLED BRACKET & TARGET IAW CRJ 700 SRM 51-42-06-001-001-A01 TARGET P/N 601R31902-349. REV 38 07/25/20 WVAC EMP # 56392

Part: ANGLE — DAMAGED · airframe 39,669 hrs · 30,604 cycles

ANGLE SUPPORT FOR LIGHTNING DIVERTER FLOOR PANEL LOCATED BTW FS 333 TO FS 349 RH SIDE IS DAMAGED. REMOVED AND INSTALLED SERVICEABLE SUPPORT ANGLE IAW CRJ 700 SRM 51-42-06/13-001-001-A01. LOCATED AND DRILLED SERVICEABLE ANGLE IAW CRJ 700 SRM 51-40-11-001-001-A01.

Part: ANGLE — DAMAGED · airframe 39,669 hrs · 30,604 cycles

ANGLE SUPPORT FOR LIGHTNING DIVERTER FLOOR PANEL LOCATED BTW FS 310 TO FS 333 RH SIDE IS DAMAGED. REMOVED AND INSTALLED SERVICEABLE ANGLE IAW CRJ 700 SRM 51-42-06/13-001-001-A01. LOCATED AND DRILLED SERVICEABLE ANGLE IAW CRJ 700 SRM 51-40-11-001-001-A01.

Part: PLATE — GOUGED · airframe 39,669 hrs · 30,604 cycles

RH FWD FUSE PITOT STATIC PROBE CUTOUT HAS GOUGES, FWD OF FS 220, BETWEEN STR 14R/15R. REMOVED AND REPLACED RH PITOT STATIC PROBE MOUNTING PLATE IAW CRJ 700 SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-21-001-001-A51-42-21-001-001-A01.

Part: FORMER — CORRODED · airframe 39,669 hrs · 30,604 cycles

AFT FORMER HAS CORROSION & REQUIRES REPLACEMENT P/N: 601R318034-3. REMOVED FORMER ANGLE AND AFT UPPER, MID, AND LOWER SEAL RETAINER REMOVED AND REPLACED AFT FORMER IAW CRJ 700 SRM 51-40-11-001-001-A01. REINSTALLED AFT UPPER, MID, AND LOWER SEAL RETAINER IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01.

Part: STRINGER — CORRODED · airframe 39,669 hrs · 30,604 cycles

STRINGER 19R BETWEEN FS 364 TO FS 394 IS CORRODED. REMOVED AND REPLACED STR 19R BETWEEN FS 364 AND FS 394 IAW CRJ700 SRM'S 51-42-06-001-001-A01, 51-40-11-001-001-A01 AND 51-42-21-001-001-A01 WVAC EMP STAMP # 776 MTC

Part: ANGLE — CORRODED · airframe 39,669 hrs · 30,604 cycles

GALLEY SERVICE DOOR LOWER SEAL STRIKER CORRODED AROUND FASTENER HOLES. REMOVED AND REPLACED SERVICE DOOR LOWER SEAL STIKER IAW ENDEAVOR EA CRJ 753-11940 AND CRJ 700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.

Part: ANGLE — CORRODED · airframe 39,669 hrs · 30,604 cycles

ANGLE AND CLIPS QTY 2 LOCATED ON OUTER HANDLE ASSY IS CORRODED AND REQUIRES REPLACEMENT, P/N:ANGLE 601R317052 P/N:CLIP 601R318058 QTY:2. REMOVED & REPLACED ANGLE & QTY 2 CLIPS ON OUTER HANDLE ASSY P/N ANGLE-1, CLIPS 601R318058-1 IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01 REV 38 7-25-20

Part: INTERCOSTAL — CORRODED · airframe 39,669 hrs · 30,604 cycles

FOUND INTERCOSTAL DD5 P/N: 601R318075-3 WITH ELONGATED HOLES & CORROSION WITH A CORRODED CLEAT P/N: 600-31902-269 REMOVED & REPLACED INTERCOSTAL DD5 P/N: 601R318075-3 & CLEAT PN 600-31902-269 IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01 REV 38 07/25/20 WVAC EMP STAMP #769 MTC

Part: FORMER — CORRODED · airframe 39,669 hrs · 30,604 cycles

PAX DOOR FORMER AT FS 329.41 AND BETWEEN DD5 AND DD6 CORRODED. LOCATED & DRILLED NEW FORMER P/N 601R318078-3 IAW CRJ 700 SRM 51-40-11-001-001-A01. INSTALLED NEW FORMER IAW SRJ 700 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 REV 38 7/25/20. WVAC EMP STAMP #769 MTC

Part: INTERCOSTAL — CORRODED · airframe 39,669 hrs · 30,604 cycles

SRM REF 52-11-06 ITEM # 46 ON INTERCOSTAL 601R3109-317 3RD & 4TH FROM HINGE ON THE AFT SIDE HAS CORROSION & REQUIRES REPLACEMENT QTY 2 P/N 601R318084-2. REMOVED & REPLACED BRACKET ON INTERCOSTAL 3RD & 4TH FROM HINGE ON AFT SIDE P/N 601R318084-2 IAW CRJ 700 51-40-11-001-001-A01, 51-42-06-001-001-A01 REV. 38 7-25-20. WVAC EMP STAMP # 769 MTC.

Part: FRAME — CORRODED · airframe 39,669 hrs · 30,604 cycles

PAX DOOR FRAME AT FS 327.763 IS CORRODED. LOCATED AND DRILLED FRAME AT FS 327.763 IAW CRJ 700 SRM 51-40-11-001-001-A01. INSTALLED NEW FRAME P/N 601R318062-3 IAW 51-42-06-001-001-A01, 51-42-21-001-001-A01 REV 38 7-25-20. WVAC EMP STAMP # 769 MTC

Part: WEB — CORRODED · airframe 39,669 hrs · 30,604 cycles

REMOVED AND REPLACED SERVICE DOOR LOWER SEAL STIKER IAW ENDEAVOR EA CRJ 753-11940 AND CRJ 700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.

Part: INTERCOSTAL — CORRODED · airframe 39,669 hrs · 30,604 cycles

SRM REF 52-11-06 ITEM #73 PAGE 17 P/N:601R31902-317 INTERCOSTAL 3RD AND 4TH FROM HINGE ON THE AFT SIDE, HAVE CORROSION AND REQUIRE REPLACEMENT. REMOVED & REPLACED INTERCOSTAL 3RD & 4TH FROM HINGE ON AFT SIDE P/N 601R31902-317 IAW CRJ 700 SRM 51-42-06-001-001-A01 REV 38 7-25-20 WVAC EMP STAMP # 769 MTC.

Part: LUG — CHAFED · airframe 39,669 hrs · 30,604 cycles

PASSENGER DOOR HINGE, DOOR SIDE LUGS #1, 18, 20, 22, 23, 26 AND 27 FROM FRONT ARE CHAFED. REMOVED AND REPLACED PAX DOOR HINGE DOOR SIDE PN 601R318073-5 IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01 REV 38 7-25-20.

Part: INTERCOSTAL — CORRODED · airframe 39,669 hrs · 30,604 cycles

PAX DOOR DD6 INTERCOSTAL CORRODED. REPLACED PAX DOOR INTERCOSTAL DD6 AND CLEAT PN 600-31902-269 IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01.

Part: STRIKER — CORRODED · airframe 39,669 hrs · 30,604 cycles

GALLEY SERVICE DOOR LOWER SEAL STRIKER CORRODED AROUND FASTENER HOLES. REMOVED AND REPLACED SERVICE DOOR LOWER SEAL STIKER IAW ENDEAVOR EA CRJ 753-11940 AND CRJ 700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.

Part: INTERCOSTAL — CORRODED · airframe 39,669 hrs · 30,604 cycles

PAX DOOR INTERCOSTAL DD3 P/N 601R3180541 FWD SIDE FOURTH FROM UPPER END IS CORRODED. LOCATED AND DRILLED INTERCOSTAL DD3 PN 601R318054-1 IAW CRJ 700 SRM 51-40-11-001-001-A01. INSTALLED INTERCOSTAL IAW CRJ 700 SRM 51-42-06-001-001-A01 REV 38 7-25-20. WVAC EMP STAMP # 769 MTC.

Part: INTERCOSTAL — CORRODED · airframe 39,669 hrs · 30,604 cycles

PAX DOOR INTERCOSTAL DD7A P/N 601R318083-1 MID 1ST FROM LOWER END IS CORRODED. REPLACED PAX DOOR INTERCOSTAL DD7 AND CLIP PN 601R-38058-1 IAW 700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01. WVAC EMP # 56392.

Part: FORMER — CORRODED · airframe 39,669 hrs · 30,604 cycles

PAX DOOR FWD FORMER CORRODED IN MULTIPLE LOCATIONS. PAX DOOR FWD FORMER IAW CRJ 700 SRM 51-40-11-001-001-A01, -42-06-001-001-A01, 51-42-21-001-001-A01. REMOVED AND REINSTALLED REINSTALLED FWD FORMER ANGLE IAW CRJ 700 SRM 51-42-06-001-01-A01 AND 51-42-21-001-001-A01. WVAC EMP STAMP # 794 MTC.

Part: FRAME — CORRODED · airframe 39,669 hrs · 30,604 cycles

PAX DOOR FRAME AT FS 327.763 IS CORRODED. LOCATED AND DRILLED FRAME AT FS 327.763 IAW CRJ 700 SRM 51-40-11-001-001-A01. INSTALLED NEW FRAME P/N 601R318062-3 IAW 51-42-06-001-001-A01, 51-42-21-001-001-A01 REV 38 7-25-20. WVAC EMP STAMP # 769 MTC.

Part: INTERCOSTAL — CORRODED · airframe 39,669 hrs · 30,604 cycles

INTERCOSTAL DD3 P/N: 601R318056-1 IS CORRODED AND REQ REPLACEMENT. REF ITEM #32 IN CRJ 700 SRM 52-11-06. REMOVED & REPLACED INTERCOSTAL DD3 P/N 601R318056-1 IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01 REV 38 7-25-20 WVAC EMP STAMP # 769 MTC.

Part: STRINGER — CORRODED · airframe 39,669 hrs · 30,604 cycles

STRINGER 19R FROM FS 280 TO FS 319.70 IS CORRODED. REMOVED AND REPLACED STR 19R FROM FS 280-FS 319.70 IAW CRJ 700 SRM'S 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-21-06-001-001-A01 AND ENDEAVOR EA #CRJ753-12019.

Part: STRINGER — CORRODED · airframe 39,669 hrs · 30,604 cycles

STRINGER 22L FROM FS. 333 TO FS. 349 HAS CORROSION AT RIVET HOLES. REPAIRED STRINGER 22L FS 333 - 353 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 53-00-03-201-001-A01. WVAC EMP # 56392

Part: INTERCOSTAL — CORRODED · airframe 39,669 hrs · 30,604 cycles

INTERCOSTALS AT STGR 21L FROM FS 310 TO FS 349 ARE CORRODED. REMOVED AND REPLACED INTERCOSTAL AT STR 21L FROM FS 310 - FS 333 AND REPAIRED INTERCOSTAL AT STR 21L FROM FS 333-349 IAW CRJ 700 SRM 51-21-06-001-001-A01, 51-42-06-001-001-A01 AND 51-40-11-001-001-A01.APPLIED PAINT AND CIC AT RIVETS AT INTERCOSTAL AT 21L FROM FS 310 TO FS 344 IAW CRJ 700 SRM 51-25-16-001-001-A01 AND 51-21-00-001-001-A01. REMOVED FOD. CORRECTIVE ACTION STEP 1 RF SHOULD READ CRJ 700 ESPM 20-26-31 AND 20-21-000-910-801-A01. WVAC EMP STAMP # 776 MTC

Part: STRINGER — CORRODED · airframe 39,669 hrs · 30,604 cycles

CORROSION ON STRINGER 23L BETWEEN FS 501-485. REPAIRED CORRODED AREA OF STR 23L BETWEEN FS 501-FS 485 IAW ENDEAVOR EA CRJ 753-12024. WVAC EMP STAMP # 776 MTC

Part: ANGLE — CORRODED · airframe 39,669 hrs · 30,604 cycles

PASSENGER DOOR MID CAP ANGLE AT STGR 18 CORRODED AROUND FASTENER HOLES. REMOVED AND REPLACED CAP ANGLE IAW CRJ 700 AMM 20-21-00-910-801-A01 AND 51-40-11-001-001-A01.

Part: HINGE — CHAFED · airframe 39,669 hrs · 30,604 cycles

PAX DOOR HINGE FUSELAGE SIDE, SEVERAL LUGS CHAFED ON OUTER AND INNER SURFACE OF LUGS. REMOVED AND REPLACED PAX DOOR HINGE IAW CRJ 700 SRM 53-21-23-2001-007-A01. WVAC EMP STAMP #769 MTC

Part: STRINGER — CORRODED · airframe 39,669 hrs · 30,604 cycles

TWO STRINGERS CORRODED 23L AND 24L BETWEEN FS 501 & 517 REMOVED AND REPLACED STRINGERS IAW CRJ 700 SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01, 51-21-06-001-001-A01

Part: FRAME — CORRODED · airframe 39,669 hrs · 30,604 cycles

FRAME 379 CORRODED AT STR 23R. REMOVED AND REPLACED FS 379.00 FRAME

Part: SKIN — DAMAGED · airframe 39,669 hrs · 30,604 cycles

FWD CARGO COMPARTMENT DOOR THRESHOLD SKIN PANEL HAS A DRILL START HOLE BETWEEN F.S. 533.00 AND F.S. 549.00 REPAIRED FWD CARGO DOOR THRESHOLD SKIN PANEL IAW ENDEAVOR EA CRJ 753-11898 REV B DATED 8/10/2021 WVAC EMP # 56392

Part: INTERCOSTAL — CORRODED · airframe 39,669 hrs · 30,604 cycles

INTERCOSTAL AT STRINGER 20R BETWEEN FS. 333 TO FS. 349 IS CORRODED ON BOTTOM EDGE. INSTALLED NEW SERVICEABLE INTERCOSTAL AT STR 20R FS 333-349 IAW CRJ700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01. WVAC EMP # 56392

Part: TIE CLIP — CORRODED · airframe 39,669 hrs · 30,604 cycles

COCKPIT FLOOR BOARD 221 ALF RH SUPPORT ANGLE CORRODED IN 2 LOCATIONS JUST FWD OF F.S. 280.00. INSTALLED (2) CLIPS AND (2) GUSSETS AT FS 280 BULKHEAD IAW CJR 700 SRM 51-42-10-001-001-A01 AND 51-42-06-001-001-A01. WVAC EMP # 56392

Part: GUSSET — CORRODED · airframe 39,669 hrs · 30,604 cycles

COCKPIT FLOOR BOARD 221 ALF RH SUPPORT ANGLE CORRODED IN 2 LOCATIONS JUST FWD OF F.S. 280.00. INSTALLED (2) CLIPS AND (2) GUSSETS AT FS 280 BULKHEAD IAW CJR 700 SRM 51-42-10-001-001-A01 AND 51-42-06-001-001-A01. WVAC EMP # 56392

Part: CLEAT — CORRODED · airframe 39,669 hrs · 30,604 cycles

AFT BAG COMPARTMENT FRAME/STRINGER CLEAT AT F.S. 985.00, STR 20L IS CORRODED. REMOVED CORRODED CLEAT FROM F.S.985, STGR 20L AND INSTALLED NEW FABRICATED CLEAT IAW CRJ 700 SRM 51-42-21-001-001-A01, 51-24-36-001-001-A01, 51-42-06-001-001-A01 AND 51-40-11-001-001-A01.

Part: SEAT TRACK — CORRODED · airframe 39,669 hrs · 30,604 cycles

SEAT TRACK AT RBL 9 BEGINNING AT APPROX F.S. 985 CORRODED IN SEVERAL AREAS. REMOVED AND REPLACED SEAT TRACK AT RBL 9 FROM FS 977 TO FS 1005 IAW CRJ 700 SRM 53-00-49-201-002-A01 BOMBARDIER REO 670-53-00-07H REV B AND AMM 53-20-49-000/400-801-A01. WVAC EMP STAMP # 776 MTC

Part: ANGLE — CRACKED · airframe 39,669 hrs · 30,604 cycles

COCKPIT FLOOR SUPPORT ANGLE L/H CRACKED, FWD OF F/S 280. REMOVED AND REPLACED COCKPIT FLOOR SUPPORT ANGLE IAW CRJ 700 SRM'S 51-42-06-001-001-A01 AND 51-40-11-001-001-A01. WVAC EMP STAMP # 776 MTC."

Part: PLATE — CORRODED · airframe 39,669 hrs · 30,604 cycles

AFT CARGO DOOR NET TIE DOWNS ARE CORRODED 3EA (STRUCTURE). REMOVED AND REPLACED 3 EA AFT CARGO DOOR NET TIE DOWN PLATES IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01.

Part: SEAT TRACK — CORRODED · airframe 39,669 hrs · 30,604 cycles

RH SIDE SEAT RAIL FS 379.00 TO FS 485.00 HAS CORROSION IN SEVERAL LOCATIONS. "REMOVED AND REPLACED RH SIDE SEAT RAIL FROM FS 379.00 TO FS 485 AND REPLACED BROKEN RIVNUTS IAW CRJ 700 AMM 53-00-49-000/400-801-A03 AND SRM 51-42-36-001-001-A01.

Part: ANGLE — CRACKED · airframe 39,669 hrs · 30,604 cycles

COCKPIT FLOOR SUPPORT ANGLE R/H CRACKED, FWD OF FS 280. "REMOVED AND REPLACED COCKPIT FLOOR SUPPORT ANGLE IAW CRJ 700 SRM'S 51-42-06-001-001-A01, 51-40-11-001-001-A01. WVAC EMP STAMP # 776 MTC."

Part: PANEL — CHAFED · airframe 39,669 hrs · 30,604 cycles

FLAP LEADING EDGE PANEL 584EB IS CHAFED. - REMOVED & REPLACED #584EB IAW CRJ 700 SRM 51-40-11-001-001-A01 WVAC EMP # 603145 REFERENCE MASTER PANEL BOOK, PG 94 FOR INSTALLATION OF PNL 584EB. WVAC EMP STAMP # 776 MTC

Part: PLATE — CHAFED · airframe 39,669 hrs · 30,604 cycles

LOW PRESSURE AIR CONNECTION STRUCTURE HAS CHAFE DAMAGE A 4 LOCATIONS AROUND ADAPTER PLATE MOUNT AREA. REPAIRED LOW PRESSURE AIR CONNECTION STRUCTURE CHAFED AREAS IAW BOMBARDIER GREO 670-53-61-1385 REV-A, DATED 2017-10-19 AND ENDEAVOR EA# CRJ753-12018. WVAC EMP STAMP # 776 MTC

Part: ANGLE — CORRODED · airframe 39,669 hrs · 30,604 cycles

PAX DOOR KICKPLATE ANGLE HAS CORROSION AROUND NUTPLATES. REMOVED AND REPLACED PAX DOOR KICK PLATE ANGLE IAW CRJ 700 SRM'S 51-21-06-001-001-A01, 51-40-11-001-001-A01 AND 51-42-06-001-001-A01. WVAC EMP STAMP # 776 MTC.

Part: SEAT TRACK — CORRODED · airframe 39,669 hrs · 30,604 cycles

RH FLOOR SEAT RAILS AT RBL 9.00 CORRODED AND CHAFED BETWEEN FS 349 AND FS 469. REMOVED AND REPLACED RH SEAT RAIL IAW CRJ 700 AMM 53-00-49-000-801-A03 AND CRJ 700 AMM 53-00-49-400-801-A03. WVAC EMP STAMP #776 MTC

Part: ANGLE — CORRODED · airframe 39,669 hrs · 30,604 cycles

AVIONICS FLOORBOARD SUPPORT ANGLE AT F.S. 280 IS CORRODED. BLENDED CORROSION IAW CRJ 700 SRM 53-00-00-101-001-A01 OUT OF LIMITS CRJ 700 SRM 51-21-06-001-001-A01. REMOVED, LOCATED, DRILLED AND IN-STALLED SERVICEABLE SUPPORT ANGLE IAW CRJ 700 SRM 51-42-06-001-001-(A01), 51-42-21-001-001-A01 & 51-40-11-001-001-A01 WVAC EMP # 603145

Part: ANGLE — CRACKED · airframe 39,669 hrs · 30,604 cycles

L/H VERT. STAB TO FUSELAGE DRAG ANGLE (AFT ANGLE) APPEARS TO BE CRACKED ON L/E IN RADIUS. - PERFORMED EDDY CURRENT FOR SUSPECTED CRACK IAW CRJ 700 NDTM PART 1, 51-20-006-250-A01 FAILED NDT. REMOVED AND LOCATED, DRILL AND INSTALLED SERVICEABLE DRAG ANGLE IAW CRJ 700 SRM 51-42-21-001-001-A01, 51-42-22-001-001-A01, 51-42-13-001-001-A01, AND 51-40-11-001-001-A01. WVAC EMP # 603145

Part: SEAT TRACK — CORRODED · airframe 39,669 hrs · 30,604 cycles

SEAT TRACK @ LBL 27 BEGINNING AT APPROX FS 985.00 CORRODED IN SEVERAL AREAS. INSTALLED NEW SEAT TRACK LBL 27 FS 985 IAW CRJ 700 AMM 53-00-49-00-49-00-802-A06, CRJ 700 AMM 53-00-49-400-802-A06 AND CRJ 700 SRM 53-00-49-201-002-A01. WVAC EMP #603145

Part: SEAT TRACK — CORRODED · airframe 39,669 hrs · 30,604 cycles

SEAT TRACK SEGMENTS AT RBL 27 BEGINNING AT APPROX FS 985.00 CORRODED IN SEVERAL LOCATIONS. REMOVED AND REPLACED SEAT TRACK SEGMENT, RBL 27 FS 977 THRU FS 1005 IAW CRJ 700 SRM 53-00-49-201-002-A01, CRJ 700 AMM 53-00-49-00-812-A06, 53-00-49-400-802-A06. WVAC EMP #603145

Part: SEAT TRACK — CORRODED · airframe 39,669 hrs · 30,604 cycles

SEAT TRACK AT F.S. 923 TO F.S. 985, LBL 27 IS CORRODED REMOVED AND REPLACED SEAT TRACK AT LBL27 FROM FS 923-985 IAW CRJ700 SRM 53-00-49-201-002-A01 AND AMM'S 53-00-49-000/400-801-A03.

Part: WEB — CORRODED · airframe 39,669 hrs · 30,604 cycles

R/H F.S. 280 WEB IS CORRODED IN SEVERAL AREAS. REMOVED, LOCATED, DRILLED AND INSTALLED SERVICEABLE WEB IAW CRJ 700 SRM 53-11-10-201-004-A01 PERFORMED EDDY CURRENT IAW CRJ 700 SRM 53-11-10-201-004-A01. WVAC EMP # 603145

Part: SEAT TRACK — CORRODED · airframe 39,669 hrs · 30,604 cycles

LH FLOOR SEAT RAIL AT LBL 9 CORRODED BETWEEN FS 485 TO FS 677. REMOVED & REPLACED LH FLOOR SEAT RAILS @ LBL 9 FS 485-677 IAW CRJ 700 SRM 53-00-49-201-007-A01 CRJ 700 AMM 53-00-49-00-801-A03 AND CRJ 700 AMM 53-00-49-400-801-A03. WVAC EMP STAMP #781 MTC. SH670-33426-1, SH670-33425-3

Part: SEAT TRACK — CORRODED · airframe 39,669 hrs · 30,604 cycles

SEAT TRACK AT FS 863 TO FS 977, RBL 9 IS CORRODED. REMOVED CORRODED SEAT TRACK FROM F.S.863 TO F.S.977 AT RBL 9 AND INSTALLED NEW SERVICABLE SEAT TRACK IAW CRJ 700 AMM 53-00-49-400-801-A03.

Part: FLOORBEAM — CORRODED · airframe 39,669 hrs · 30,604 cycles

FS 280 R/H CROSS BEAM IS CORRODED ON TOP SURFACE. BLENDED CORROSION IAW CRJ700 SRM 51-21-06-001-001-A01. FOUND OUT OF LIMITS IAW CRJ700 53-00-00-101-001-A01. REMOVED & LOCATED DRILLED AND INSTALLED SERVICEABLE CROSS BEAM IAW CRJ 700 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-42-22-001-001-A01, 51-42-13-001-001-A01, 51-40-11-001-001-A01. WVAC EMP # 603145

Part: CROSSBEAM — CORRODED · airframe 39,669 hrs · 30,604 cycles

F.S. 280, L/H CROSSBEAM HAS CORROSION AT FASTENER HOLE. REPLACED LH FS 280 CROSSBEAM IAW BOMBARDIER REO 670-53-11-047 REV F 2013-03-14. REMOVED AND REINSTALLED LBL9 AND LBL27 INTERCOSTALS IAW CRJ 700 SRM 51-42-21-001-001-A01 AND 51-42-22-001-001-A01. REMOVED AND REINSTALLED VENT BRACKET IAW CRJ 700 SRM 51-42-13-001-001-A01. WVAC EMP # 56392.

Part: STRINGER — CORRODED · airframe 39,669 hrs · 30,604 cycles

STRINGER 20R CORRODED NEAR FS 319.70. REMOVED AND REPLACED STR 20R SEGMENT FROM FS280-FS 319.

Part: SEAT TRACK — CORRODED · airframe 39,669 hrs · 30,604 cycles

SEAT TRACK AT F.S. 677 TO F.S. 863, LBL 9 IS CORRODED. REMOVED AND REPLACED SEAT TRACK AT FS 677 TO FS 863 AT LBL 9 IAW CRJ 700 SRM'S 53-00-49-201-002-A01 AND 51-40-11-001-001-A01 AND AMM 53-00-49-000/400-801-A03.

Part: PLATE — CORRODED · airframe 39,669 hrs · 30,604 cycles

FLOOR SUPPORT PLATE AT FS 533.00 STGR 27 IS CORRODED. REMOVED AND REPLACED FLOOR SUPPORT PLATE AT FS 533.00 STR 27 IAW CRJ 700 SRM 51-42-06-001-001-A01, 51-42-15-001-001-A01, AND 51-40-11-001-001-A01.

Part: SEAT TRACK — CORRODED · airframe 39,669 hrs · 30,604 cycles

SEAT TRACK AT F.S. 677 TO F.S. 863, RBL 9 IS CORRODED. REMOVED AND INSTALLED NEW SEAT RAIL FROM FS 677.00 TO FS 830.00 RBL9.0 WL 85.25 IAW A/C CRJ700 AMM 53-00-49-400-801 CONFIG A03 WVAC EMP STAMP # 776 MTC

Part: SEAT TRACK — CORRODED · airframe 39,669 hrs · 30,604 cycles

RH SIDE SEAT RAIL FS 677.00 TO FS 761.00 HAS CORROSION IN SEVERAL LOCATIONS. "REMOVED PN:SH670-37504-1 IAW CRJ 700 AMM 53-00-49-000-801-A03, AND REPLACED WITH NEW PART# SH670-36255-3 AND SH670-37509-1 IAW CRJ 700 53-00-49-400-8-01-A03."

Part: FLOORBEAM — CORRODED · airframe 39,669 hrs · 30,604 cycles

AFT CARGO FLOOR BEAM @ LBL 27 IS CORRODED FROM APPROX F.S. 1015.00 TO 1031.00 REMOVED AND REPLACED SECTION OF AFT CARGO FLOOR BEAM AT LBL 27 BETWEEN FS 1015-1031 IAW CRJ 700 SRM 53-00-41-201-001-A01, 51-42-21-001-001-A01 AND 51-42-06-001-001-A01. WVAC EMP STAMP # 776 MTC

Part: DOOR SILL — CORRODED · airframe 39,669 hrs · 30,604 cycles

AFT CARGO DOOR CUT-OUT FLOOR SILL IS CORRODED. REMOVED AND REPLACED AFT CARGO CUT-OUT FLOOR SILL IAW CRJ 700 SRM'S 51-42-06-001-001-A01, 51-42-21-001-001-A01, 53-61-23-201-001-A01, 51-40-11-001-001-A01 AND 51-42-02-001-001-A01.

Part: SEAT TRACK — CORRODED · airframe 39,669 hrs · 30,604 cycles

RH SIDE SEAT RAIL FS 677.00 TO FS 761.00 HAS CORROSION IN SEVERAL LOCATIONS. "REMOVED PN:SH670-37504-1 IAW CRJ 700 AMM 53-00-49-000-801-A03, AND REPLACED WITH NEW PART# SH670-36255-3 AND SH670-37509-1 IAW CRJ 700 53-00-49-400-8-01-A03."

Part: INTERCOSTAL — CORRODED · airframe 39,669 hrs · 30,604 cycles

INTERCOSTAL AT STRINGER 20R BETWEEN FS. 333 TO FS. 349 IS CORRODED ON BOTTOM EDGE. INSTALLED NEW SERVICEABLE INTERCOSTAL AT STR 20R FS 333-349 IAW CRJ700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01. WVAC EMP # 56392

Part: ANGLE — CRACKED · airframe 39,669 hrs · 30,604 cycles

LH VERT. STAB TO FUSELAGE DRAG ANGLE (FWD ANGLE) APPEARS TO BE CRACKED ON T/E IN RADIUS. - REPAIRED L/H FWD DRAG ANGLE IAW CRJ 700 SRM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,996 hrs · 29,971 cycles

CEILING EMERGENCY LIGHT FOUND INOP. REMOVED AND REPLACED CEILING EMERGENCY LIGHT BULB IAW CRJ 700 AMM 33-51-09. OPS CHECK GOOD.

Part: SEAT TRACK — CORRODED (BS 784-861) · airframe 37,732 hrs · 28,793 cycles

RH SIDE SEAT TRACK AFT OF EMERGENCY EXIT HATCH FROM FFS 784.00 TO FS 861.00 CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED RH SIDE SEAT TRACK IAW CRJ 700 SRM 51-41-02 AND BOMBARDIER REO 670-53-00-343 REV N 2019-07-16.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 37,732 hrs · 28,793 cycles

LH FS280.00 FLOOR BEAM WEB SIGNS OF CORROSION. CORRECTIVE ACTION: REPAIRED LH FS 280.00 FLOOR BEAM WEB IAW GOJET EO C700/900-53MR-010 REV "O" DATED 02/26/2019. AND BOMBARDIER REO 670-53-11-594 REV "A" DATED 2015/06/26.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 37,732 hrs · 28,793 cycles

L/H AND R/H 280 BEAM WEBS HAVE SIGNS OF CORROSION AND MISSING RIVET HEADS. CORRECTIVE ACTION: REPAIRED 280 BEAM IAW BOMBARDIER REO 60-53-11-594 REV-A DATED 2018-06-26, GOJET EO C700/900-53MR-010 REV O, DATED 02-26-2019, CRJ700 SRM 51-42-06, 51-26-00, 53-11-41, 53-11-10.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 37,732 hrs · 28,793 cycles

L/H F.S. 280.00 FLOOR BEAM HAS SIGNS OF CORROSION. CORRECTIVE ACTION: REPAIRED L/H F.S. 280.00 FLOOR BEAM IAW GOJET EO C700-53MR-011-O, CRJ700 SRM 53-11-41, 51-42-06, 51-24-36, 51-42-21, 51-26-00, 51-42-13, 51-21-11, 51-25-06, 51-42-11, 53-11-41, 51-25-16, 51-40-06, 51-40-11, 51-21-00, 51-41-02, CRJ 700 AMM 20-70-00, BOMBARDIER ADR# RROY-1932422046.

Part: FLOOR SUPPORT — CORRODED (BS 280-329) · airframe 37,732 hrs · 28,793 cycles

RH FLOOR SILL AT FS 280.00 TO FS 329.00 HAS SIGNS OF CORROSION,CORRECTIVE ACTION: REMOVED RH FLOOR SILL AT FS 280.00 TO 319.00 IAW CRJ700 SRM 51-42-06, 51-21-06, AND 51-42-00.

Part: STRINGER SPLICE — CORRODED (BS 333) · airframe 37,732 hrs · 28,793 cycles

STRINEGR 25R STRINGER SPLICE AT FA 333.00 CORRODED. CORRECTIVE ATCION: REPLACED STINGER SPLICE ON STRINGER 25R AT FS 333.00 IAW CRJ 700 51-21-11, 51-25-16, 51-40-11, 51-42-06, 51-42-21, 53-21-03.

Part: STRINGER — CORRODED (BS 333-349) · airframe 37,732 hrs · 28,793 cycles

STRINGER 26R BETWEEN FS 333.00 AND 349.00 CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED STRINGER 26R BETWEEN FS 333.00 AND 349.00 IAW CRJ 700 AMM 53-21-03, 51-21-11, 51-42-21, 51-42-06, 51-40-11, 51-25-16.

Part: STRINGER SPLICE — CORRODED (BS 333) · airframe 37,732 hrs · 28,793 cycles

STRINGER 25R STRINGER SPLICE AT FS 333.00 CORRODED. CORRECTIVE ACTION: REPLACED STRINGER SPLICE ON STRINGER 25R AT FS 333.00 IAW CRJ 700 SRM 51-21-11, 51-25-16, 51-40-11, 51-42-16, 51-42-21, 53-21-03.

Part: STRINGER SPLICE — CORRODED (BS 333) · airframe 37,732 hrs · 28,793 cycles

STRINGER 26R SPLICE AT FS 333.00 CORRODED, CORRECTIVE ACTION: REPLACED STRINGER SPLICE ON STINGER 26R AT FS 333.00 IAW CRJ 700 SRM 51-21-03, 51-42-06, 51-40-11, 51-25-16, 51-21-11,

Part: WARNING LIGHT — FALSE ACTIVATION (LT ENGINE FIRE) · airframe 37,530 hrs · 28,597 cycles

L ENG FIRE SWITCH LIGHT ILLUMINATED ON CLIMB OUT NO OTHER ASSOCIATED WARNINGS ENGINE ROLLED BACK.INSPECTED LH ENG FIRE LOOPS IAW CRJ700 AMM 26-11-00. NO DEFECTS NOTED. INSPECTED LH AND RH ENG FIRE BOTTLE SQUIBS IAW CRJ700 AMM 26-21-13 NO DEFECTS NOTED. REMOVED AND REPLACED FIDEX CONTROL UNIT IAW CRJ700 AMM26-10-01 OPS CHECK GOOD. REMOVED, CLEANED AND INSPECTED LH BOTTLE DISCHARGE PUSHBUTTON IAW CRJ700 AMM 26-21-01. PERFORMED OPS TEST OF FIRE DETECTION SYSTEM IAW CRJ700 AMM 26-10-00 NO DEFECTS NOTED. PERFORMED LH ENGINE OPERATIONAL TEST IAW CRJ 700 AMM 71-00-00 NO DEFECTS NOTED

Part: SEAL — DIRTY (EMERGENCY EXIT) · airframe 39,747 hrs · 29,467 cycles

PASSENGER IN SEAT 12A COMPLAINS ABOUT NOISE COMING FROM EMERGENCY EXIT DOOR. CLEANED AND LUBED SEAL ON LH OVERWING EMER EXIT DOOR IAW CRJ 700AMM 52-21-00 OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,020 hrs · 27,172 cycles

CEILING LEVEL EMERGENCY FLOODLIGHT INOP. AS PER TELECOM WITH MX CONTROL DEFERRED CEILING LEVEL EMERGENCY FLOOD LIGHT ON DMI OCN 70049927 PER MEL 33-51-01B-2A CAT C.

Part: BRACKET — BROKEN (ZONE 400) · airframe 36,004 hrs · 27,160 cycles

RT LOWER ENGINE COWL BRACKET BROKEN(P/N:CN624-0104-001 S/N: SB/0207). CORRECTIVE ACTION: REMOVED AND REPLACED RT LOWER THRUST REVERSER ASSY (P/N:CN624-0104-003 S/N: SB0681) IAW AMM 78-33-01, 71-11-01, 78-30-00, 78-34-01, AND 78-30-00.

Part: LIGHT — DETACHED (CABIN) · airframe 34,748 hrs · 25,966 cycles

LEFT EMERGENCY EXIT LIGHT ON THE GALLEY PARTITION IS DETACHED. SECURED THE EMERGENCY EXIT LIGHT IAW AMM 33-51-05. OPS CHECKED GOOD.

Part: LIGHT — DETACHED (ROWS 1 & 2) · airframe 34,327 hrs · 25,596 cycles

EMERGENCY LIGHT AT RT ROWS 1 AND 2 UNATTACHED. SECURED THE EMERGENCY LIGHT STRIP IAW SRM 51-22-00. OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,234 hrs · 24,605 cycles

EMERGENCY EXIT LIGHTS OUT AT MID CABIN OVERHEAD, FRONT BULKHEAD, AND MAIN CABIN DOOR FLOOR LEVEL FLOOD LIGHT. R & R EMERGENCY BATTERY, OPS CHECKED GOOD IAW AMM 33-51-017,

Part: STRINGER — CORRODED (BS 250-265) · airframe 33,142 hrs · 24,525 cycles

STRINGER 26R IS CORRODED BETWEEN BS 250 AND 265. REMOVED THE DAMAGED SECTION OF THE STRINGER IAW SRM 53-00-03.

Part: PANEL — CRACKED (PAX DOOR) · airframe 33,142 hrs · 24,525 cycles

PASSENGER DOOR FWD STAIR PANEL HAS A CRACK AT THE MIDSTEP. REPAIRED FWD STAIR PANEL IAW REO 670-52-11-104, REV H, SRM 51-41-00, 51-42-06, 51-25-06, AND NDT MANUAL PART 1 51-20-006.

Part: SKIN — CRACKED (PAX DOOR) · airframe 331,419 hrs · 24,525 cycles

PASSENGER DOOR SKIN IS CRACKED. CUT OUT DAMAGE, FABRICATED AND INSTALLED A REPAIR IAW REO 670-52-11-291, REV A, AND REO 670-52-11-965.

Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 33,142 hrs · 24,525 cycles

INTERCOSTAL AT STR 9L BETWEEN FS 1144.0 AND FS 1162.0 DAMAGED OUT OF LIMITS. REPAIRED INTERCOSTAL AT STR 9L BETWEEN FS 1144.0 AND FS 1162.0 IAW REO760-53-61-1394 REV-- DATED 2017-07-17. NDT PERFORMED, NO DEFECTS NOTED DATED 18 JULY 2017, IAW NDTM PART 1 51-20-006.

Part: SKIN — DENTED (BS 549-565) · airframe 33,142 hrs · 24,525 cycles

THREE SCRATCHES AND A DENT BETWEEN BS 549 - 565, STRINGERS 16 - 17L. CUT AWAY DAMAGED AREA, FABRICATED AND INSTALLED A REPAIR IAW REO 670-53-31-415, REV B.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 33,142 hrs · 24,525 cycles

LONGERON AT STGR 25R FS 349 IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED LONGERON AT STGR 25R AT FS 349 IAW SRM 51-42-06, 51-42-21, 51-40-11, 51-21-11, 51-25-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,142 hrs · 24,525 cycles

RT FLOOR SEAT RAIL FROM FS 350 TO 485 CORRODED. REPLACED RT SEAT RAIL FROM FS 350 TO 485 IAW AMM 53-00-49.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 33,142 hrs · 24,525 cycles

STR 25R IN FWD AVIONICS BAY CORRODED OUT OF LIMITS. REMOVED AND REPLACED STR 25R FROM FS 280-FS 333 IAW SRM 51-42-06, 51-42-21, 51-40-11, 51-24-36, 51-25-06, 53-21-08.

Part: FRAME — CORRODED (FUSELAGE) · airframe 33,142 hrs · 24,525 cycles

FRAME 295 BETWEEN 26R AND 24R IS OUT OF LIMITS. CUT AND REMOVED DAMAGED FRAME, FABRICATED FRAME, SPLICE ANGLES, AND CLEATS, INSTALLED PARTS IAW REO 670-53-21-1438 P1 DATED 2017-07-17, REO 670-53-21-1438 R2 DATED 2017-07-20, AND REO 670-53-21-1438 REV-- DATED 2017-07-25.

Part: ANGLE — CRACKED (PAX DOOR) · airframe 33,142 hrs · 24,525 cycles

PASSENGER DOOR VENT FLAP SUPPORT ANGLE IS CRACKED. REMOVED AND REPLACED PASSENGER DOOR VEN FLAP SUPPORT ANGLE IAW SRM 51-42-06, 51-25-06, 51-40-11, AND 51-25-16.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 33,142 hrs · 24,525 cycles

FS 280 CROSSBEAM RT SIDE IS CORRODED. REMOVED AND REPLACED FS 280 CROSSBEAM RT SIDE IAW SRM 53-11-41, 51-42-13, 51-42-21, 51-40-11, 51-42-06, 51-21-11, 51-25-16, AMM 20-70-00, AND NDTM 51-20-006-250.

Part: BRACKET — CRACKED (PAX DOOR) · airframe 33,142 hrs · 24,525 cycles

PASSENGER DOOR INTERNAL AFT UPPER SIDE (BY LOWER PULLEY) INTERNAL BRACKET IS CRACKED, AND FWD SIDE SAME BRACKET IS CRACKED. REMOVED AND REPLACED PASSENGER DOOR INTERNAL AFT AND FWD UPPER BRACKETS IAW SRM 51-46-06, 51-42-21, 51-25-16, 51-25-06, AND 51-40-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,142 hrs · 24,525 cycles

RT FLOOR SEAT RAIL FROM FS 677 TO 863 IS CORRODED. REPLACED RT SEAT RAIL FROM FS 677 TO 863 IAW AMM 53-00-49.

Part: SEAL — DETACHED (EMERGENCY EXIT) · airframe 33,072 hrs · 24,464 cycles

LEFT OVERWING EMERGENCY EXIT SQUEALS DURING FLIGHT. FOUND SIDEWALL FILLET SEAL PROTRUDING TO EXTERIOR OF ACFT. REMOVED AND REINSTALLED THE LT OVERWING EMERGENCY EXIT DOOR IAW AMM 52-21-07. NO DEFECTS NOTED AT THIS TIME.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,849 hrs · 24,282 cycles

SECOND LAST EMERGENCY LIGHT CEILING INOPERATIVE. REPLACED THE LAMPS IAW AMM 20-41-00, NO FURTHER DEFECTS NOTED.

Part: SEAL — NOT SEATED (PAX DOOR) · airframe 32,385 hrs · 23,881 cycles

LOUD WHISTLING NOISE FROM PAX DOOR DURING CRUISE. PERFORMED INSPECTION OF MAIN DOOR SEAL AND RESEATED SEAL IAW AMM 52-11-07. PERFORMED LEAK TEST IAW AMM 52-00-00, LEAK CHECKED GOOD.

Part: DOOR — LEAKING (MAIN PAX) · airframe 32,168 hrs · 23,701 cycles

PAX DOOR SQUEAL. PERFORMED GENERAL VISUAL INSPECTION OF AIRCRAFT AND FOUND TO BE SAFE FOR A ONE TIME FERRY FLIGHT.

Part: SMOKE DETECTOR — FALSE ACTIVATION (AFT LAVATORY) · airframe 31,780 hrs · 23,388 cycles

SMOKE AFT LAVATORY MASTER WARNING. INSPECTED AND FOUND NO SIGNS OF SMOKE.

Part: SMOKE DETECTOR — FALSE ACTIVATION (AFT LAVATORY) · airframe 31,780 hrs · 23,388 cycles

SMOKE AFT LAV MASTER WARNING .INSPECTED AND FOUND NO SIGNS OF SMOKE.

Part: CONNECTOR — LOOSE (SMOKE DETECTOR) · airframe 31,778 hrs · 23,385 cycles

SMOKE AFT LAV MASTER WARNING MESSAGE, EMERGENCY DECLARED. OPS CHECKED AFT SMOKE DETECTOR IN LAV OPS CHECKED GOOD IAW AMM 26-16-00. FOUND THE AFT LAV SMOKE DETECTOR CONNECTOR LOOSE. TIGHTEN CONNECTOR IAW AMM 26-16-01 STEP A (5) PULLED TOILET SHROUD NO DEFECTS NOTED SYS OPS CHECK GOOD IAW 26-16-00

Part: SEAL — MISSING (PBE) · airframe 31,512 hrs · 23,189 cycles

HUMIDITY SEAL ON FWD PBE IS MISSING. RESEATED FWD PBE IAW AMM 35-31-06, NO DEFECTS NOTED

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,358 hrs · 23,072 cycles

1 OVERHEAD EMERGENCY LIGHT IN CABIN IS INOPERATIVE. PLACED 2ND TO LAST OVERHEAD EMERGENCY CEILING FLOODLIGHT ON MEL 33-51-01B-2A, CAT-C CORRECT PRIOR TO 9-22-16, OCN 70008257.

Part: FRAME — CRACKED (BS 333) · airframe 31,342 hrs · 23,058 cycles

BS 333 FRAME IS CRACKED. CUT AND REMOVED CRACKED SECTION OF FRAME FROM STRINGER 1 - 2R. FABRICATED AN ANGLE, FILLER, AND STRAP. INSTALLED REPAIR WITH TWO NEW ANGLES IAW REO 670-53-21-1327, REV. A.

Part: FITTING — CORRODED (ZONE 100) · airframe 31,342 hrs · 23,058 cycles

INTERNAL FORWARD JACK FITTING, LT AND RT INTERCOSTALS ARE CORRODED OUT OF LIMITS. REMOVED AND REPLACED INTERNAL FORWARD JACK FITTING, LT AND RT INTERCOSTALS IAW AMM 21-23-79 AND SRM 51-42-21, 51-42-06, 51-40-11, 51-42-13, 51-25-16, 51-21-11, AND 51-45-00

Part: STIFFENER — CRACKED (BS 202 BULKHEAD) · airframe 31,320 hrs · 23,042 cycles

BS 202.75 FWD SIDE OF BULKHEAD LBL 30 STIFFENER HAS A CRACK INDICATION .15 LONG AT THE UPPER EDGE OF FLANGE. FAILED NDT

Part: FRAME — CRACKED (BS 202 BULKHEAD) · airframe 31,320 hrs · 23,042 cycles

AFT SIDE OF BULKHEAD LEFT CAP ANGLE HAS TWO CRACK INDICATIONS IN THE RADIUS, ONE IS .4 LONG JUST BELOW STRINGER 13A AND THE OTHER IS .35 LONG ONE INCH BELOW STRINGER 13A. FAILED NDT INSPECTION. VISUALLY FOUND GOUGE NEAR INSPECTION AREA NEXT TO THE RADIUS ON HORIZONTAL FLANGE .030 DEEP APPROXIMATELY 6 INCHES BELOW STRINGER 12L, .2 LONG BY .1 WIDE

Part: DOOR — OUT OF ADJUST (SERVICE) · airframe 31,270 hrs · 23,009 cycles

SERVICE DOOR WILL NOT OPEN. ADJUSTED DOOR IAW AMM 52-49-01. OPS CHECKED GOOD.

Part: WARNING MESSAGE — ILLUMINATED (PAX DOOR) · airframe 31,113 hrs · 22,898 cycles

PASSENGER DOOR OUTER HANDLE CAUTION MESSAGE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,067 hrs · 22,115 cycles

LOWER FLOOR LEVEL EXIT LIGHT 1 BULB NOT WORKING. DEFERRED LOWER FLOOR LEVEL EXIT LIGHT IAW MEL 33-51-01F CAT C.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,630 hrs · 21,788 cycles

EMERGENCY LIGHT OVER ROW 15 BURNT OUT. DEFERRED EMER LIGHT OVER ROW 15 IAW MEL 33-51-01B.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 28,997 hrs · 21,299 cycles

PROX SYS FAULT 1 STATUS MSG. TROUBLE SHOT & FOUND HANDLE NOT FAULT OPENED POSITION. PERFORMED DOOR WARNING SYS & DOOR OPERATIONS CHECK, NORMAL OPERATION, MSG EXTINGUISHED IAW AMM 52-70-00.

Part: WARNING FLAG — FALSE ACTIVATION (FLT DIRECTOR) · airframe 28,925 hrs · 21,250 cycles

LOW SPEED, ABORTED TAKEOFF DUE TO FLIGHT DIRECTOR FLAG. FLIGHT DIRECTOR FAULT PREVIOUSLY DEFERRED IAW MEL 22-10-01, 22-10-02B & 22-11-03. ABORTED TAKEOFF INSPECTION IAW AMM 05-51-27. FOUND NOT REQUIRED.

Part: HANDLE — BROKEN (SERVICE DOOR) · airframe 28,813 hrs · 21,159 cycles

SERVICE DOOR SUPPORT HANDLE IS BROKEN. R & R SERVICE DOOR ASSIST HANDLE IAW AMM 25-26-07.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,751 hrs · 21,111 cycles

IN CEILING EMER LIGHT AT ROW 15 NOT WORKING. R & R EMER LIGHT BULB IAW AMM 33-51-01.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,487 hrs · 20,908 cycles

CEILING LEVEL EMER LIGHT INOPERATIVE. R & R CEILING EMER LIGHT AT ROW 15.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 28,083 hrs · 20,603 cycles

PASSENGER DOOR SILL CORRODED. R & R PAX DOOR SILL IAW SRM 51-42-21, 51-42-06, 51-40-11 & 51-25-21.

Part: ATTACH FITTING — CRACKED (ZONE 200) · airframe 28,083 hrs · 20,603 cycles

ENGINE START GND AIR SUPPLY ADAPTOR PULLED THROUGH ITS ATTACHMENT BOX HOUSING. R & R CONNECTOR BOX IAW AMM 36-17-03 & SRM 51-42-06.

Part: TUBE — DAMAGED (PAX DOOR) · airframe 28,083 hrs · 20,603 cycles

PASSENGER DOOR HARNESS CONVOLUX TUBING DAMAGED. REPAIRED HARNESS IAW AMM 52-11-00 & REO 670-52-70-006 REV A DATED 06 NOV 2014. WO 80260 & WC 8075.

Part: PROXIMITY SWITCH — GROUNDED (PAX DOOR) · airframe 28,083 hrs · 20,603 cycles

PASSENGER DOOR PX 101 & PX 107 SENSORS READ TO GND AT ALL TIMES AT PSEU DISCRETE INPUTS D116 & D117. REPLACED BOTH SENSORS IAW AMM 52-70-04. WO 80260 & WC 8075.

Part: PANEL — BUCKLED (PAX DOOR) · airframe 28,083 hrs · 20,603 cycles

PASSENGER DOOR FWD & AFT SIDE PANEL BUCKLED. PERFORMED REPAIR IAW REO 670-52-11-803 REV A DATED 2014-12-06.

Part: MOUNT BRACKET — CORRODED (FUSELAGE) · airframe 28,083 hrs · 20,603 cycles

NUMBER 1 GALLEY HAS THREE CORRODED MOUNTING BRACKETS. R & R THREE BRACKETS IAW C & D CMM 25-33-42. WO 80260 & WC 2144. ADDITIONAL PN CDSP2019-7C-760.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 28,083 hrs · 20,603 cycles

RIGHT SILL FROM STATION 280 - 310 HAS CORROSION. R & R RT SILL FROM STATION 280 - 310 IAW SRM 51-42-06 & 51-42-13.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 28,083 hrs · 20,603 cycles

PASSENGER DOOR AFT DRAG ANGLE CRACKED. REPAIRED DRAG ANGLE IAW SRM 51-42-06, 51-40-11, 51-42-13 & 51-42-15. NDT PERFORMED, CRS K9QR554B ON 4 DEC 2014. WO 80260, WC 8066.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 28,083 hrs · 20,603 cycles

T CAS CHANNEL CORRODED. R & R T CAS ANTENNA CHANNEL IAW SRM 51-42-06, 51-40-11, 51-42-21 & AMM 34-43-07.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 28,083 hrs · 20,603 cycles

GALLEY SERVICE DOOR ENTRY FLOOR KICK ANGLE SUPPORT CORRODED. R & R FLOOR MOUNTING ANGLE IAW SRM 51-42-06, 51-41-02, 51-40-11 & 51-42-21.

Part: FRAME — CORRODED (FUSELAGE) · airframe 28,083 hrs · 20,603 cycles

FRAME AT FS 310 CORRODED BETWEEN STRINGER 26L & 26R. REPAIRED FRAME BY CUTTING & REMOVING FRAME SECTION FROM 26L & 26R. INSTALLED NEW FRAME SECTION WITH FABRICATED SPLICE, CLEATS & TAPERED SHIM IAW REO 670-53-21-799, DATED 30 JAN 2012. WO 80260 & WC 1072.

Part: MOUNT BRACKET — CRACKED (SERVICE DOOR) · airframe 28,083 hrs · 20,603 cycles

GALLEY SERVICE DOOR PROX SWITCH P36 MOUNT BRACKET CRACKED. R & R BRACKET IAW AMM 52-70-06. WO 80260 & WC 2141.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 28,083 hrs · 20,603 cycles

COCKPIT FLOORBEAM ANGLE ON BS 280 CORRODED. R & R THE FLOORBEAM ANGLE IAW SRM 51-42-06.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 28,083 hrs · 20,603 cycles

AFT CARGO COMPARTMENT FLOORBEAM AT FS 1031 & LBL 27 IS CORRODED. CUT & REMOVED APPROX 24 IN OF BEAM. CUT & INSTALLED NEW FLOORBEAM FROM PN CC670-34175-7S. FABRICATED ANGLES, SHIMS & SPLICES, ASSEMBLED IAW REO 670-53-00-029 REV A DATED 31 AUG 2010. WO 80260 & WC 1065.

Part: RETAINER SEAL — DAMAGED (PAX DOOR) · airframe 28,083 hrs · 20,603 cycles

FORWARD PAX DOOR SEAL RETAINER GOUGED & BENT UNDER PAX DOOR BONDING WIRE ADJACENT TO DOOR HINGE. R & R FWD PAX DOOR SEAL RETAINER IAW SRM 51-42-13.

Part: CROSSBEAM — CRACKED (FUSELAGE) · airframe 28,083 hrs · 20,603 cycles

FS 280 CROSSBEAM CRACKED ON LT & RT SIDES. R & R CROSSBEAM IAW SRM 53-11-41, 51-21-11, 51-25-16, 51-25-06, 51-42-06, 51-42-21 & 51-42-13. WO 80260 & WC 2094.

Part: SUPPORT BRACKET — LOOSE (SERVICE DOOR) · airframe 28,083 hrs · 20,603 cycles

GALLEY SERVICE DOOR LATCH SUPPORT BRACKET LOOSE. REMOVED RIVETS & INSTALLED LOCK FASTENERS IAW SRM 51-42-21. WO 80260 & WC 2113.

Part: DIAPHRAGM — CRACKED (FUSELAGE) · airframe 28,083 hrs · 20,603 cycles

LEFT DIAPHRAGM, WEB, UNDER AFT WING TO BODY FAIRING CRACKED AT FS 909. REPAIRED WEB IAW REO 670-53-82-478 REV A DATED 11 DEC 2014. WO 80260 & WC 1064.

Part: LINER — UNSECURE (EMERGENCY EXIT) · airframe 27,281 hrs · 19,953 cycles

EMERGENCY EXIT LINER BROKE OFF. SECURED EMER EXIT LINER IAW AMM 52-21-02.

Part: BEARING — DEFECTIVE (SERVICE DOOR) · airframe 27,268 hrs · 19,942 cycles

SERVICE DOOR HARD TO OPEN. R & R SERVICE DOOR LOWER TORQUE TUBE BEARING IAW AMM 52-41-02. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: HINGE — UNKNOWN (CABIN DOOR) · airframe 27,255 hrs · 19,932 cycles

STOW PANEL HINGE ON MAIN DOOR. R & R HINGE & REPLACED UPPER DOOR STEP IAW AMM 52-11-4.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,003 hrs · 19,736 cycles

FLOOR LEVEL EMERGENCY FLOOD LIGHT IN THE GALLEY HAS INOPERATIVE BULBS. DEFERRED FLOOR LEVEL EMERGENCY LIGHT BULBS IAW MEL 33-51-01C.

Part: BATTERY — DISCHARGED (CABIN) · airframe 27,003 hrs · 19,736 cycles

EMERGENCY LIGHTS INOPERATIVE, DEAD BATTERY. RECHARGED BATTERY & PERFORMED OPERATIONS CHECK OF EMERGENCY LIGHTS IAW AMM 33-51=15. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,999 hrs · 19,734 cycles

SERVICE DOOR EMERGENCY LIGHT HAS INOPERATIVE BULBS. DEFERRED SERVICE DOOR EMERGENCY LIGHT BULBS IAW MEL 33-51-01E.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,999 hrs · 19,734 cycles

EXIT ROW EMERGENCY LIGHT HAS BULBS INOPERATIVE. R & R EMERGENCY LIGHT BULBS ON RT SIDE IAW AMM 33-51-05, OPERATIONS CHECKED GOOD AT THIS TIME.

Part: PIN — UNSECURE (PAX DOOR) · airframe 26,999 hrs · 19,734 cycles

PASSENGER DOOR TOP STEP HAS FWD & AFT HINGE PIN STICKING OUT. SECURED PINS IAW AMM 52-11-04.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,984 hrs · 19,722 cycles

EMERGENCY CEILING FLOOD LIGHT INOPERATIVE. DEFERRED EMERGENCY CEILING FLOOD LIGHT IAW MEL 33-51-01B CAT C.

Part: OVERHEAT SENSOR — OUT OF POSITION (RT MLG) · airframe 26,929 hrs · 19,677 cycles

MAIN LANDING GEAR BAY OVERHEAT WARNING ON TAKEOFF, ABORTED TAKEOFF. REPOSITIONED RT MLG OVERHEAT SENSOR TC10 IAW AMM 26-14-04. OPERATIONS CHECKED GOOD IAW 26-14-00, NO DEFECTS AT THIS TIME.

Part: COVER — LOOSE (EMERGENCY EXIT) · airframe 26,909 hrs · 19,118 cycles

BOTH EMER EXIT HANDLE COVERS ARE LOOSE. SECURED LT & RT EMER EXIT HANDLE COVERS IAW AMM 51-22-61.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,822 hrs · 19,597 cycles

EMERGENCY FLOOD LIGHT OVER ROW 8 & 9 INOPERATIVE. DEFERRED CEILING LEVEL EMERGENCY FLOOD LIGHT IAW MEL 33-51-01B.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 28,689 hrs · 20,304 cycles

CIRCUMFERENTIAL SPLICE AT FS 280.00 CORRODED. CLEANED AREA FOUND LIGHT CORROSION. REMOVED LIGHT CORROSION IAW WITH SRM 51-21-06.

Part: SEAL — DEBONDED (OVERWING EXIT) · airframe 28,689 hrs · 20,304 cycles

RIGHT OVERWING EXIT PRESS SEAL DISBONDED. SEALED DISBONDED SEAL ON RT OVERWING EXIT DOOR IAW AMM 25-21-07.

Part: WHEEL — ABNORMAL (PAX DOOR) · airframe 26,571 hrs · 19,409 cycles

PASSENGER DOOR SUPPORT WHEEL COLLAPSED. LUBED MAIN CABIN DOOR SUPPORT WHEEL, PERFORMED OPERATIONS CHECK IAW CRJ700 AMM 52-11-13, OPERATIONS CHECKED GOOD.

Part: ESCAPE HATCH — LEAKING · airframe 26,431 hrs · 19,309 cycles

EMERGENCY HATCH LEAKING AROUND SEAL. RESEALED EMERGENCY HATCH IAW CRJ700 AMM 52-22-00, NO LEAK NOTED AT THIS TIME, ACFT OK FOR SERVICE.

Part: SENSOR — SHORTED (PAX DOOR) · airframe 26,366 hrs · 19,256 cycles

PASSENGER DOOR PROX SYS 1, UP LOCK SENSOR PX 23 SHORTED. SECURED WIRING HARNESS, PERFORMED VISUAL INSPECTION OF HARNESS & DOOR. OPERATIONAL CHECK OF DOOR, VERIFIED PAX DOOR SECURED WITH GREEN LOCK INDICATORS. ACFT APPROVED FOR ONE TIME FERRY LIGHT FROM ROC TO LGA.

Part: WHEEL — CRACKED (PAX DOOR) · airframe 26,243 hrs · 19,163 cycles

PASSENGER DOOR WHEEL ASSEMBLY BENT & CRACKED. REMOVED SUPPORT WHEEL, INSTALLED DOOR CABLE KIT & INSURED PAX DOOR OPENS & CLOSES WITHOUT INTERFERENCE. ACFT SAFE FOR ONE TIME FERRY FLIGHT FROM LGA TO STL.

Part: WHEEL — LACK OF LUBE (PAX DOOR) · airframe 26,154 hrs · 19,098 cycles

PASSENGER DOOR SUPPORT WHEEL DID NOT DEPLOY. FOUND DOOR WHEEL NOT TO BE LUBRICATED, LUBED DOOR WHEEL AS REQUIRED. PERFORMED OPERATIONS CHECK OF MAIN DOOR IAW CRJ700 AMM 52-11-00, OPERATIONS CHECKED GOOD AT THIS TIME.

Part: SENSOR — FAULTY (LT WING) · airframe 26,149 hrs · 19,094 cycles

LEFT & RT ANTI-ICE CAUTION MESSAGES. R & R LT OTBD WING ANTI-ICE TEMP SENSOR IAW CRJ700 AMM 30-12-08. OPERATIONS CHECKED GOOD, NO DEFECTS NOTED AT THIS TIME.

Part: LOOP — UNSECURE (LT WING) · airframe 26,056 hrs · 19,020 cycles

ANTI-ICE DUCT WARNING & CAUTION MESSAGE IN FLIGHT. APPLIED DC4 TO LT WING LOOP A MT 167, 164, 171 & 173 IAW CRJ700 SL 36-016. PERFORMED OPERATIONS CHECK IAW CRJ700 AMM 36-21-00, NO DEFECTS NOTED AT THIS TIME.

Part: SEAL — LACK OF LUBE (EMERGENCY EXIT) · airframe 25,609 hrs · 18,670 cycles

LEFT OVERWING EMERGENCY EXIT MAKING AIR NOISE WHILE FLYING. INSPECTED DOOR SEAL IAW AMM 52-21-06, LUBRICATED LT OVERWING EMERGENCY EXIT DOOR SEAL IAW AMM 52-21-00, OP'S CHECK GOOD AT THIS TIME.

Part: WARNING MESSAGE — FALSE ACTIVATION (FLT DIRECTOR) · airframe 25,244 hrs · 18,385 cycles

FLIGHT DIRECTOR INOPERATIVE, WARNING MESSAGE PFD. PERFORMED OP'S CHECK OF AHRS IAW AMM 34-21-00. OP'S CHECKED GOOD AT THIS TIME.

Part: HOOK AND LOOP — DAMAGED (EMERGENCY EXIT) · airframe 25,089 hrs · 18,264 cycles

RT OVERWING EMERGENCY EXIT HANDLE COVER WILL NOT STAY CLOSED. RESECURED HOOK AND LOOP TAPE ON RT EMERGENCY EXIT COVER HANDLE IAW AMM 51-22-61. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,899 hrs · 18,122 cycles

EMERGENCY LIGHTS INOPERATIVE. OP'S CHECKED EMERGENCY LIGHTS IAW AMM 33-51-00.

Part: SEAL — LOOSE (EMERGENCY EXIT) · airframe 24,889 hrs · 18,114 cycles

LEFT EMERGENCY EXIT DOOR SQUEALING IN FLIGHT. FOUND SEAL AROUND VENT FLAP LOOSE, RESECURED SEAL IAW AMM 52-21-03, LEAK CHECK C/W NO DEFECTS NOTED IAW AMM 52-00-00.

Part: DOOR — UNSECURE (LT OVERWING) · airframe 24,882 hrs · 18,108 cycles

LEFT OVERWING EXIT SQUEALING IN FLIGHT. RESECURED LT OVERWING EXIT DOOR IAW AMM 52-21-00, OPS CHECK AND LEAK CHECKED GOOD IAW AMM 52-00-00.

Part: SWIVEL FITTING — DAMAGED (PAX DOOR) · airframe 24,859 hrs · 18,091 cycles

PAX DOOR FWD SWIVEL ASSY DAMAGED. R & R PAX DOOR FWD SWIVEL LEVER ASSY IAW AMM 52-11-17, OP'S CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 24,409 hrs · 17,751 cycles

OVERHEAD EMERGENCY FLOODLIGHT AT ROW 17 INOPERATIVE. R & R BULB IAW AMM 33-51-09. OP'S CHECKED GOOD.

Part: SEAL — LEAKING (ESCAPE HATCH) · airframe 24,108 hrs · 17,527 cycles

WATER LEAKING FROM COCKPIT ESCAPE HATCH. REMOVED ESCAPE HATCH, CLEANED HATCH AND SEAL AS REQUIRED, INSTALLED ESCAPE HATCH IAW AMM 52-22-00. OP'S CHECK GOOD AT THIS TIME.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,906 hrs · 18,189 cycles

CABIN CEILING EMERGENCY FLOOD LIGHT AT ROW 9 INOPERATIVE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,938 hrs · 17,402 cycles

SECOND TO LAST EMERGENCY FLOOD LIGHT IN CEILING IS INOPERATIVE. R & R EMERGENCY LIGHT IAW AMM 33-51-09. OPS CHECK TESTED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,809 hrs · 17,306 cycles

ROW 17 EMERGENCY CEILING LIGHT INOPERATIVE. REMOVED AND REPLACED BULB IN EMERGENCY CEILING LIGHT ROW 17,OP'S CHECKED GOOD IAW AMM 33-51-09.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 223,792 hrs · 17,294 cycles

EMERGENCY CEILING LIGHT AT ROW 17 INOPERATIVE.

Part: WARNING LIGHT — FALSE ACTIVATION (PAX DOOR) · airframe 23,109 hrs · 16,782 cycles

PAX DOOR MASTER WARNING IN FLIGHT. INSPECTED ACFT FOR A 1 TIME FERRY FLIGHT, VERIFIED DOOR INDICATOR ALIGNED WITH DOOR CLOSED. ACFT SAFE FOR FERRY FLIGHT.

Part: PROXIMITY SENSOR — FAILED (PAX DOOR) · airframe 23,098 hrs · 16,774 cycles

PASSENGER DOOR MASTER CAUTION WARNING, PROXIMITY SYS FAULT 1. R & R PASSENGER DOOR PX 101, PROXIMITY SENSOR IAW AMM 52-70-04, SYS OP'S CHECK GOOD AT THIS TIME.

Part: ROLLER — LOOSE (PAX DOOR HANDLE) · airframe 23,098 hrs · 16,774 cycles

PAX DOOR MASTER WARNING. FOUND INNER HANDLE DENT ROLLER ASSY LOOSE. SECURED ROLLER, PAX DOOR OP'S CHECK GOD AT THIS TIME, IAW AMM 52-11-02 & 52-11-00.

Part: CHANNEL — CORRODED (PAX DOOR) · airframe 23,095 hrs · 16,772 cycles

PASSENGER DOOR CORRODED BEYOND SERVICEABLE LIMITS FROM FS 311.75 TO FS 347.25, END CAPS. R & R LOWER SECTION, FORWARD BOTTOM CORNER IAW SRM 51-42-06, 51-42-13, 51-21-11, 51-21-06.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,025 hrs · 16,720 cycles

CEILING LEVEL FLOOD LIGHT OUT AT ROW 15-16.

Part: PLACARD — PEELING (CAIBN) · airframe 22,906 hrs · 16,629 cycles

EXIT PLACARD PEELING OFF OF MAIN CABIN DOOR STAIR. PLACED ON NEF 25-500-1, CAT 5.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 22,729 hrs · 16,492 cycles

SMOKE ON FLIGHT DECK AND CABIN DURING FINAL APPROACH. INSPECTED ACFT FOR EVIDENCE OF SOURCE OF SMOKE AND FOUND CEILING LIGHTS AT ROWS 1 ANS 2 LT TO SHOW SIGNS OF OVERHEATING . BOTH AIR CONDITIONING PACKS WERE RUN ISOLATED AND TOGETHER ON EA ENGINE BLEED SOURCE AND NO EVIDENCE OF SMOKE WAS FOUND.

Part: MOTOR — FAULTY (PAX DOOR) · airframe 22,341 hrs · 16,199 cycles

PAX DOOR DOES NOT FALL COMPLETLY TO THE GROUND. R & R PAX DOOR MOTOR IAW AMM 52-11-08.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 21,970 hrs · 15,922 cycles

NR 3 CABIN CEILING EMERGENCY LIGHT INOP. RELAMPED NR 3 CABIN CEILING EMERGENCY LIGHT. OPS CHECKED GOOD IAW AMM 33-51-00.

Part: RELAY — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 21,566 hrs · 15,636 cycles

AFTER THE ACFT WAS POWERED UP FOR AWHILE, EMERGENCY LIGHTS CAME ON WHILE MASTER WAS IN THE ARM POSITION. R & R A/C POWER SENSE RELAY K135 IAW AMM 24-06-11 AND OPS CHECKED IAW AMM 33-51-00, ALL CHECKED GOOD.

Part: MANIFOLD — LEAKING (HYD SYSTEM) · airframe 21,523 hrs · 15,606 cycles

APPROX 15 MINS AFTER TAKEOFF RECEIVED HYD 3 LOW PRESSURE CAUTION MESSAGE. SYS 3 DID REFLECT 0 FLUID. APPLIED QRIT PROCEDURES, RETURNED TO DEPARTURE. EMERGENCY DECLARED. R & R HYD SYS NR 3 FILTER PRESSURE MANIFOLD IAW AMM 29-12-09 OPS AND LEAK CHECKED GOOD. NO FURTHER SEFECTS NOTED AT THIS TIME.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 21,174 hrs · 15,365 cycles

FUSELAGE RT AFT MOST EXTERNAL EMERGENCY LIGHT INOPERATIVE. RELAMPED RT FUSELAGE AFT EMERGENCY LIGHT IAW AMM 33-51-21. RELAMPED RT FUSELAGE AFT EMERGENCY LIGHT IAW AMM 33-51-21. (CLOSED)

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 19,915 hrs · 14,464 cycles

F/A FLASHLIGHT INOP. REPLACED FLASHLIGHT BATTERIES IAW AMM 25-60-00. (CLOSED)

Part: SEAT TRACK — CORRODED (BS 565-693) · airframe 19,418 hrs · 14,136 cycles

LT SIDE WALL SEAT TRACK AT FS 565.00 TO FS 693.00 HAS AREAS OF CORROSION (MARKED) AND WORN LUG. AWAITING EC/TC, SL 7318 01/10/11. RECEIVED EC/TC REO 670-53-00-294, COMPLIED WITH ALL STEPS OF REO 670-53-00-294, REV A FOR LT SIDEWALL SEAT TRACK FS565.00 TO FS669.00 DOCUMENTED ON THIS NONROUTINE, COMPLIED WITH EC/TC, REO 670-53-00-294.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 19,417 hrs · 14,134 cycles

WHILE PERORMING OPS TEST FOR THE EMERGENCY LIGHT, FOUND RT EXIT FLOOR SIGN WAS DIM. R & R THE EMERGENCY FLOOR FLOOD LIGHT BULB IAW AMM CH 20-19-00. OPS CK GOOD.

Part: CROSSBEAM — CORRODED (BS 280) · airframe 19,417 hrs · 14,134 cycles

F/S 280 CROSSBEAM HAS CORROSION. R & R SEAT TRACK RT SIDE FS 485.00 TO FS 549.00 IAW AMM 53-00-49-000-801 AND 53-00-49-400-800-801.

Part: WEB — CORRODED (BS 280) · airframe 19,417 hrs · 14,134 cycles

FS 280 RT WEB HAS CORROSION.

Part: LIGHT — UNSERVICEABLE (CABIN) · airframe 19,417 hrs · 14,134 cycles

CANNED EMERGENCY DOOR HANDLE BETA LIGHT FOR ACFT FROM LT DOOR. INSTALLED BETA LIGHT ON EMERGENCY EXIT DOOR HANDLE LT SIDE AND PERFORMED FUNCTIONAL TEST IAW AMM 33-51-13-400-801. OPS CHECK GOOD AT THIS TIME.

Part: SEAT TRACK — GOUGED (BS 364-469) · airframe 19,417 hrs · 14,134 cycles

RT OTBD AISLE FLOOR SEAT TRACK AT FS 364.00 TO FS 469.00 HAS GOUGE AND HAS AREAS OF CORROSION. BLENDED CORROSION AREAS & FOUND TO BE OUT OF SERVICABLE LIMITS IAW SRM 53-21-49-101-001-A01. COMPLIED WITH REO 670-53-00-249 AND INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 19,417 hrs · 14,134 cycles

RT SIDE WALL SEAT TRACK AT FS 485.00 TO FS 581.00 HAS AREAS OF CORROSION. FABRICATED NEW SEAT TRACK IAW REO 670-53-00-294. INSTALLED IAW AMM 53-00-49-400-801-A03 AND REO 670-53-00-294.

Part: SEAT TRACK — CORRODED (BS 469-597) · airframe 19,417 hrs · 14,134 cycles

LT INBD FLOOR SEAT TRACK AT FS 469.00 TO FS 597.00 HAS AREAS OF CORROSION (MARKED) 1ST CLASS TRACK. REMOVED CORROSION ON SEAT TRACK IAW SRM 53-21-49-101-001-A01, FOUND TO BE OUT OF LIMITS, NEED TO REPLACE SEAT TRACK. R & R SEAT TRACK IAW AMM 53-00-49-000-801. (CLOSED)

Part: SEAT TRACK — CORRODED (BS 565-693) · airframe 19,417 hrs · 14,134 cycles

LT SIDE WALL SEAT TRACK AT FS 565.00 TO FS 693.00 HAS AREAS OF CORROSION. BLENDED 6 AREAS AND REMOVED CORROSION FROM LT SIDE SEAT RAIL AT FS 565-669 IAW SRM 51-12-00-001-001. FOUND TO BE OUT OF LIMITS AT FS 565-669 IAW SRM 53-31-49-101-001-0-A01. R & R SEAT TRACK IAW AMM 53-00-49-000-801.

Part: SEAT TRACK — CORRODED (BS 469-597) · airframe 19,417 hrs · 14,134 cycles

RT OTBD AISLE FLOOR SEAT TRACK AT FS 469.00 TO FS 597.00 HAS AREAS OF CORROSION. BLENDED CORROSION AREA AS MARKED IAW SRM 53-21-49-101-001-001-A01. COMPLIED WITH REO 670-53-00-249 AND INSTALLED SERVICEABLE SEAT TRACK AT FS469-597 IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 879-969) · airframe 19,417 hrs · 14,134 cycles

RT SIDE WALL SEAT TRACK AT FS 879.00 TO FS 969.00 HAS AREAS OF CORROSION. REMOVED, FABRICATED, AND INSTALLED SEAT TRACK IAW AMM 53-00-49-000-801.

Part: SEAT TRACK — CORRODED (BS 708-969) · airframe 19,417 hrs · 14,134 cycles

LT FLOOR SEAT TRACK (AISLE) AT FS 708.00 TO FS 969.00 HAS SCRAPE AND AREAS OF CORROSION. R & R SEAT TRACK FROM STA 836-969 IAW AMM 53-00-49-000-801.

Part: SEAT TRACK — CORRODED (BS 379-485) · airframe 19,417 hrs · 14,134 cycles

RT SIDE WALL SEAT TRACK AT FS 379.00 TO FS 485.00 HAS AREAS OF CORROSION. BLENDED SEAT TRACK AND REMOVED DAMAGE IN SEVERAL AREAS IAW SRM 53-21-49-101-001-A01. COMPLIED WITH RO 670-53-00-294 AND INSTALLED SERVICEABLE SEAT TRACK AT FS 379-485 IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 677-708) · airframe 19,417 hrs · 14,134 cycles

LT FLOOR SEAT TRACK (AISLE) FROM FS 677.00 TO FS 708.00 HAS AREAS OF CORROSION. R & R FLOOR SEAT TRACK (AISLE) FROM FS 677.00 TO FS 708.00 IAW AMM 53-00-49-000-801-A03 AND 53-00-49-400-801-A03 AND REO 670-53-00-294.

Part: SEAT TRACK — CORRODED (BS 708-752) · airframe 19,417 hrs · 14,134 cycles

RT SIDE WALL SEAT TRACK AT FS 708.00 TO FS 752.00 HAS AREAS OF CORROSION. REMOVED, FABRICATED, AND INSTALLED IAW AMM 53-00-49-000-801.

Part: SEAT TRACK — CORRODED (BS 597-677) · airframe 19,417 hrs · 14,134 cycles

LT INBD FLOOR SEAT TRACK AT FS 597.00 TO FS 677.00 HAS AREAS OF CORROSION. 1ST CLASS TRACK.

Part: SEAT TRACK — CORRODED (BS 469-565) · airframe 19,417 hrs · 14,134 cycles

LT SIDE WALL SEAT TRACK AT FS 469.00 TO FS 565.00 HAS AREAS OF CORROSION AND SEVERAL NICKS. BLENDED AREAS OF CORROSION IAW SRM 51-12-00-001-001. FOUND SEAT TRACK TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-31-51-101-001-A01. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLLED NEW SEAT RAIL AT FS469.00 TO 565.00 LT SIDE WALL IAW IAW AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 597-677) · airframe 19,417 hrs · 14,134 cycles

LT INBD FLOOR SEAT TRACK AT FS 597.00 TO FS 677.00 HAS AREAS OF CORROSION (MARKED) 1ST CLASS TRACK. R & R SEAT TRACK AT FS 597.00 TO 677.00 LT INBD SIDE IAW AMM 53-00-49-000/(400)-801.

Part: SEAT TRACK — CORRODED (BS 752-893) · airframe 19,417 hrs · 14,134 cycles

LT SIDE WALL SEAT TRACK HAS AREAS OF CORROSION AT FS 752.00 TO FS 893.00. REMOVED OLD SEAT TRACK, CLEANED AREA, INSTALLED NEW IAW AMM 53-00-49-400-801-A03 AND 53-00-49-000-801-A03.

Part: SEAT TRACK — CORRODED (BS 893-969) · airframe 19,417 hrs · 14,134 cycles

LT SIDE WALL SEAT TRACK AT FS 893.00 TO FS 969.00 HAS AREAS OF CORROSION. REMOVED CORRODED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALL NEW TRACK. INSTALLED NEW SEAT TRACK IAW AMM 53-00-43-400-801.

Part: SEAT TRACK — CORRODED (BS 597-677) · airframe 19,417 hrs · 14,134 cycles

RT OTBD AISLE FLOOR SEAT TRACK AT FS 597.00 TO FS 677.00 HAS AREAS OF CORROSION. R & R RT OTBD FLOOR SEAT TRACK AT FS 597.00 TO FS 677.00 IAW AMM 53-00-49-000-801 AND 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 469-597) · airframe 19,417 hrs · 14,134 cycles

LT OTBD (AISLE) FLOOR SEAT TRACK AT FS469.00 TO FS597.00 HAS NICK AND AREAS OF CORROSION. REMOVED DAMAGE IAW SRM 51-12-00-001-001. FABRICATED NEW SEAT TRACK IAW REO 670-53-00-294. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801-A03 AND REO 670-53-00-294.

Part: SEAT TRACK — CORRODED (BS 379-469) · airframe 19,417 hrs · 14,134 cycles

LT SIDE WALL SEAT TRACK AT FS 379.00 TO FS 469.00 HAS AREAS OF CORROSION. R & R SEAT TRACK FROM FS 836-708 IAW AMM 53-00-49-000-801.

Part: SEAT TRACK — CORRODED (BS 785-879) · airframe 19,417 hrs · 14,134 cycles

RT SIDE WALL SEAT TRACK AT FS 785.00 TO FS 879.00 HAS AREAS OF CORROSION. REMOVED CORRODED SEAT TRACK AND FABRICATED NEW IAW AMM 53-00-49-00-801 AND REO 670-53-00, FI4, REV A. INSTALLED NEW SEAT TASK IAW AMM 53-00-49-400 AND REO 670-53-00-294, REV A.

Part: SEAT TRACK — CORRODED (BS 693-752) · airframe 19,417 hrs · 14,134 cycles

LT SIDE WALL SEAT TRACK AT FS 693.00 TO FS 752.00 HAS AREAS OF CORROSION. R & R WALL SEAT TRACK AT FS 693.00 TO FS 752.00 LT SIDE IAW AMM 53-00-49-00/(400)-801.

Part: SEAT TRACK — CORRODED (BS 708-969) · airframe 19,417 hrs · 14,134 cycles

RT OTBD AISLE FLOOR SEAT TRACK AT FS 708.00 TO FS 969.00 HAS AREAS OF CORROSION. BLENDED AREAS IS CRACK FREE, MAX DEPTH OF .035" WAS NOT EXCEEDED. PERFORMED UT THICKNESS MEASUREMENT OF BLEND AREAS IAW MAC NDT INSP PROCEDURE UT-3. MINIMUM MATERIAL REMAINING FWD OF FS 977 IS .091".

Part: SEAT TRACK — CORRODED (BS 677-847) · airframe 19,417 hrs · 14,134 cycles

RT OTBD AISLE FLOOR SEAT TRACK AT FS 677.00 TO FS 847 00 HAS AREAS OF CORROSION. R & R SEAT TRACK AT FS 683.50-836.50 IAW AMM 53-00-49-000-801.

Part: SEAT TRACK — CORRODED (BS 364-469) · airframe 19,417 hrs · 14,134 cycles

LT INBD FLOOR SEAT TRACK AT FS 364.00 TO FS 469.00 HAS AREAS OF CORROSION 1ST CLASS TRACK. REMOVED UNSERVICABLE SEAT TRACK AND INSTALLED SERVICABLE SEAT TRACK ALL WORK DONE IAW AMM 53-00-44-000-801 (CONFIG, A03) AND AMM 53-00-49-400-801 (CONGIG A03).

Part: CROSSBEAM — CORRODED (BS 280) · airframe 19,417 hrs · 14,134 cycles

FS 280, CROSSBEAM HAS CORROSION. REMOVED FS280 CROSSBEAM FOR CORROSION IAW SRM 51-42-06-001-001-A01. INSTALLED CROSSBEAM.

Part: WEB — CORRODED (BS 280) · airframe 19,417 hrs · 14,134 cycles

FS 280 RT WEB HAS CORROSION. BLENDED CORROSION AND CHECKED WITH DEPTH GAUGE .014" DEEP = BEYOND LIMITS IAW SRM 53-11-10-991-804. REMOVED OLD WEB PILOT DRILLED NEW WEB FROM OLD WEB IAW CRJ 700 51-40-11-001-001-A01. INSTALLED WEB.

Part: UNKNOWN — CORRODED (LT WING) · airframe 19,417 hrs · 14,134 cycles

LEFT WING HAS CORROSION. BLENDED CORROSION AND CHECKED WITH DEPTH GAUGE IS.010" DEEP AND UNDER THE HEAD OF THE FASTENERS IS BEYOND LIMITS IAW SRM 53-11-10-991-804. REMOVED LT WEB GOT NEW WEB, INSTALLED LT WEB IAW SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01.

Part: ANGLE — CORRODED (THRESHOLD) · airframe 19,417 hrs · 14,134 cycles

PASSENGER DOOR THRESHOLD TOP ANGLE CORRODED. REMOVED .025" DEPTH X 1" LENGTH X 1" WIDTH FROM PASSENGER DOOR LOWER MID CAP ANGLE AT FS 325, OUT OF LIMITS IAW SRM 53-21-23-101. R & R ANGLE. DRILLED NEW ANGLE TO FIT ACFT IAW SRM 51-40-11-001-001-A01 INSTALLED NUT PLATES ON ANGLE ASSY IAW SRM 51-42-06-001-001-A01. INSTALLED FASTENERS IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. INSTALLED PAX DOOR PROX SWITCH IAW AMM 52-70-04-400-802. MINOR REPAIR.

Part: PLACARD — FADED (COCKPIT) · airframe 19,417 hrs · 14,134 cycles

PLACARDS FADDED ON EXTERIOR OF CREW ESCAPE HATCH. REMOVED FADED SILKSCREEN PRINT FROM CREW ESCAPE HATCH IAW AMM 20-60-11-000-801. INSTALLED NEW SERVICEABLE SILKSCREEN PRINT TO CREW ESCAPE HATCH IAW MM 20-60-11-400-801.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 19,417 hrs · 14,134 cycles

RT AFT MOST FUSELAGE EMERGENCY LIGHT LENS IS CRACKED. REMOVED CRACKED EMERGENCY LIGHT LENS IAW CMM 33-52-07, REV 1 AND REPLACED WITH NEW LENS IAW CMM 33-52-07, REV 1.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 18,975 hrs · 13,843 cycles

NR 4 CABIN CEILING EMERGENCY FLOOD LIGHT INOP. RELAMPED NR 4 CABIN CEILING EMERGENCY FLOOD LIGHT IAW AMM 33-51-09, OPS CHECK GOOD. RELAMPED NR4 CABIN CEILING EMERGENCY FLOOD LIGHT IAW AMM 33-51-09, OPS CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 17,992 hrs · 13,118 cycles

MAIN CABIN INTERIOR, LT OVERWING EMERGENCY EXIT, LOWER INDENTIFIER SIGN HAS 3 EA BULBS INOP. R & R 3 EA BULBS AT LT OVERWING EMERGENCY EXIT ROW LOWER ID SIGN OPS CHECK GOOD IAW AMM 33-51-05. ACC BY 5600128, P238, INSP BY Q968,RII BY 7025460. (CLOSED)

Part: SEAT TRACK — CORRODED (BS 485-549) · airframe 17,992 hrs · 13,118 cycles

RT FLOOR INBD SEAT TRACK HAS CORROSION. REMOVED CORROSION ON RT INBD SEAT TRACK STA 485-549 IAW SRM 51-20-06 MAX MAT .035 REMOVED .040 FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49. REMOVED 3 EA TRACK RT INBD STA 485-549 IAW SRM 51-41-02. NEW SEAT TRACK POSH670-RPA0042 IAW IPC 53-00-49 INSTALLED NEW RT INBD SEAT TRACK STA 485-549 IAW SRM 50-40-11.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 17,487 hrs · 12,747 cycles

GALLEY EMERGENCY LIGHTS AFT OF THE SERVICE DOOR NEAR THE FLOOR ARE INOP EXCEPT FOR ONE BULB. RELAMPED GALLEY EMERGENCY LIGHTS AFT OF THE SERVICE DOOR NEAR THE FLOOR AS REQUIRED.

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 17,019 hrs · 12,406 cycles

INSTALLED EXIT LIGHT COVER. REF; AMM 33-50-00. (CLOSED)

Part: SIGN — MISSING (SERVICE DOOR) · airframe 17,020 hrs · 12,406 cycles

ILLUMINATED EXIT SIGN BY SERVICE DOOR IS MISSING.

Part: LIGHT — INOPERATIVE (EXTERNAL) · airframe 16,247 hrs · 11,808 cycles

RT AFTMOST EXTERNAL EMERGENCY LIGHT INOP.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 15,550 hrs · 11,290 cycles

ANGLE CRACKED AT RBL 26.00 FS 280.00 (14211/PG 100). REMOVED UNSERVICEABLE ANGLE AT RBL 26.00 FS 280.00 & REPLACED WITH FABRICATED SERVICEABLE ANGLE IAW CRJ 700 SRM 53-11-00 & 51-24-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,550 hrs · 11,290 cycles

SEQ 169 \ 2000-0060 CORROSION ON RT FWD SEAT RAIL JUST AFT OF FWD LAV AREA. REMOVED CRACKED "CLEAT" P/N CC670-33528-1 AND DUPLICATED USING 2024 T3 BY .050 ALUMINUM. INSTALLED NEW SERVICEABLE CLEAT WITH LOCK FASTENERS. ALL WORK DONE IAW SRM REFERENCE AAR FORM 412 FOR DETAILS OF WORK PERFORMED.

Part: ATTACH BRACKET — CRACKED (FUSELAGE) · airframe 15,550 hrs · 11,290 cycles

FLIGHT COMPARTMENT FLOORBEAM, CROSSBEAM ATTACH BRACKETS AT FS 232.00, RBL 9, IS CRACKED. REMOVED UNSERVICEABLE SEAT RAIL JUST AFT OF FWD LAV IAW SRM 53-00-49. SOLVENT CLEANED AREA WHERE SEAT RAIL IS TO BE INSTALLED IAW AMM 51-26-00. INSTALLED SERVICEABLE SEAT RAIL IAW AMM 53-00-49.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 15,550 hrs · 11,290 cycles

SEQ 37 \ 2000-0016 LT LOWER FS280 BULKHEAD WEB HAS AREA OF SURFACE CORROSION AT LBL15 ON EXISTING REPAIR INSERT. BLENDED CORROSION .003 INCH MATERIAL REMOVED OVER A SURFACE AREA OF APPROX 1 SQUARE INCH, .005 INCH MAX BLEND DEPTH ALLOWED. OK TO APPLY FINISH CODE (16064), APPLIED ALODINE AND PRIMER TO TREATED AREA. ALL WORK DONE IAW CRJ 700 SRM 53-11-10-201-003-A01 REPAIR A. WEB IS SERVICEABLE AND OK FOR CONTINUED SERVICE.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 15,550 hrs · 11,290 cycles

FS 280 FLOORBEAM T-BRACKETS CRACKED AT LBL 9 AND RBL 9. REMOVED FLOORBEAM T-BRACKETS IAW SRM 51-42-06 & SRM 51-42-21. LOCATED, DRILLED AND PREPPED BRACKETS IAW SRM 51-40-11. INSTALLED BRACKETS IAW SRM 51-42-21. APPLIED PRIMER & TOPCOAT IAW SRM 51-25-06 & 51-25-16.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 15,550 hrs · 11,290 cycles

FLOOR SUPPORT CORRODED AT MULTIPLE LOCATIONS BETWEEN LBL 37 AND RBL 37. REMOVED AND REPLACED FLOOR SUPPORT IAW REO NR 670-53-11-047 REV D.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 15,550 hrs · 11,290 cycles

FLIGHT DECK FLOOR SUPPORT ANGLE AT FS 280 CORRODED. REMOVED FLIGHT DECK FLOOR SUPPORT ANGLE IAW ARM 51-42-06 & SRM 51-42-21. FABRICATED NEW SERVICEABLE FLT DECK FLOOR SUPPORT ANGLE USING SAMPLE PART IAW SRM 5124-21 & SRM 51-42-06. INSTALLATION OF NEW SERVICEABLE FLOOR SUPPORT ANGLE COMPLETE. APPLIED PRIMER AND TOPCOAT TO FASTENERS IAW SRM 51-25-06 & SRM 51-25-16.

Part: DOOR — STIFF (PAX) · airframe 14,832 hrs · 10,712 cycles

STATION REPORTS PAX DOOR DIFFICULT TO CLOSE.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 11,709 hrs · 8,530 cycles

LOWER COAMING AFT CARGO DOOR SURROUND FRAME IS GOUGED BEYOND LIMITS. REPAIRED IAW EA 70-5361-01934.

Part: SEAL — DAMAGED (PAX DOOR) · airframe 11,709 hrs · 8,530 cycles

PAX DOOR SEAL NIB PREVIOUS REPAIR APPEARED DAMAGED BY SHOOT BOLT. REMOVED PREVIOUS REPAIR, STRIPPED PAINT, LPI INSPECTED REPAIR PART AND FOUND NO DAMAGE. REINSTALLED REPAIR PART AND RE-PAINTED IAW REO 670-53-22-001.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 11,709 hrs · 8,530 cycles

THE 280 BULKHEAD AND CROSSBEAM ARE CORRODED. REPAIRED DAMAGE IAW REO 670-53-11-047 AND SRM 51-40-11.

Part: COWL DOOR — DAMAGED (RT ENGINE) · airframe 11,709 hrs · 8,530 cycles

RIGHT ENGINE LOWER FAN COWL DOOR I/B AFT CORNER IS DAMAGED. FABRICATED AND INSTALLED DOUBLER REPAIR IAW SRM 54-14-00 AND 51-14-00.

Part: SPOILER — DAMAGED (WING) · airframe 11,709 hrs · 8,530 cycles

MULTI FUNCTION SPOILER SURROUND STRUCTURE HAS WORKING RIVETS. REMOVED RIVETS AND PERFORMED HOT BOND REPAIR TO DAMAGED AREA IAW EA 70-5751-01925.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 7,719 hrs · 5,884 cycles

FLIGHT 5294 - FOUND EMERGENCY LIGHTS WILL NOT ILLUMINATE. REPLACED BATTERY PACK.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 7,719 hrs · 5,884 cycles

FLIGHT 5294 - FOUND EMERGENCY LIGHTS WILL NOT ILLUMINATE. REPLACED BATTERY PACK.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 7,719 hrs · 5,884 cycles

FLIGHT 5294 - FOUND EMERGENCY LIGHTS WILL NOT ILLUMINATE. REPLACED BATTERY PACK.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 7,719 hrs · 5,884 cycles

FLIGHT 5294 - FOUND EMERGENCY LIGHTS WILL NOT ILLUMINATE. REPLACED BATTERY PACK.

Part: SKIN — CRACKED (PAX DOOR) · airframe 7,717 hrs · 5,881 cycles

FOUND PASSENGER DOOR AFT SIDE PANEL CRACKED. REPAIRED IAW BOMBARDIER REO 670-52-11-104.

Part: SKIN PANEL — DENTED (BS 1031-1051) · airframe 7,717 hrs · 5,881 cycles

FOUND SKIN DAMAGE BETWEEN FS 1031.00 AND FS 1051.30, STGR 13R AND STGR 14R. DAMAGE IS 1.5LX1.5WX.025D. PERFORMED PERMANENT NON-FLUSH SKIN REPAIR IAW CRJ700 SRM 53-00-01-201-001-AO1.

Part: WARNING LIGHT — ILLUMINATED (SPOILERS) · airframe 7,436 hrs · 5,716 cycles

FLIGHT 5383 - DURING MSP APPROACH RECEIVED AN OUTBOARD SPOILERON AND OUTBOARD FLIGHT SPOILER CAUTION MESSAGE, CREW DECLARED AN EMERGENCY, ABORTED APPROACH THEN LANDED WITHOUT INCIDENT ON SECOND ATTEMPT. PERFORMED RESET OF THE SPOILER SYSTEM.

Part: ENGINE — OVERHEATED (RIGHT) · airframe 7,002 hrs · 5,429 cycles

FLIGHT 5281- RT MOTOR OVERTEMP DURING T/O, ITT 960 C. INSPECTED ENGINE AND FOUND NO DEFECTS. OPERATIONAL CHECKS WERE NORMAL.

Part: WINDOW — FAILED (COCKPIT) · airframe 6,298 hrs · 4,893 cycles

FLT 5841 - COPILOT'S SIDE WINDOW SHATTERED. REPLACED WINDOW.

Part: WARNING LIGHT — ILLUMINATED (THRUST REVERSER) · airframe 5,569 hrs · 4,342 cycles

FLIGHT 5173 - RIGHT THRUST REVERSER UNSAFE WARNING DURING AKEOFF.DEFERRED MAINTENANCE ON THRUST REVERSER PER MEL.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 5,331 hrs · 4,160 cycles

FS 280 LT BULKHEAD LOWER WEB IS CORRODED IN VARIOUS PLACES ALONG THE BOTTOM EDGE FROM LBL36 TO LBL9. REPLACED THE FS 280 LT BULKHEAD LOWER WEB IAW BOMBARDIER INC REO 670-53-11-052, REV A REPAIR NR 2 AND CRJ 700 SRM 51-42-13-001-001-A01 AND CRJ 700 SRM 51-42-06-001-001-A01.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 5,331 hrs · 4,160 cycles

TRANSVERSE BEAM AT FS 280 FROM LBL36 TO RBL 36 IS CORRODED ALONG THE UPPER AN LOWER EDGES. REPLACED THE TRANSVERSE BEAM AT FS 280 IAW BOMBARDIER AEROSPACE REO 670-53-11-047, REV A., CRJ 700 SRM 51-25-16-001-001-A01, CRJ 700 SRM 51-40-11-001-001-A01 AND CRJ 700 SRM 51-42-06-001-001-A01.

Part: BULKHEAD — CORRODED (FS280) · airframe 5,330 hrs · 4,160 cycles

LOWER WEB AT LT FS 280 (BACK OF PILOTS CB BULKHEAD) IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED THE LOWER LT WEB P/N 670-53-11-052-1 IAW CRJ 700 SRM 51-42-06-001-A01.

Part: ENGINE — VIBRATION (RIGHT) · airframe 1,476 hrs · 1,159 cycles

FLIGHT 5874 RIGHT ENGINE VIBRATION CAUTION MESSAGE. COULD NOT DUPLICATE. RUN CHECKS WERE NORMAL.

Part: CONNECTOR — DIRTY (BRAKE TEMP) · airframe 537 hrs · 440 cycles

FLIGHT OVERHEAT WARNING. COULD NOT DUPLICATE, CLEANED BRAKE TEMPERATURE MONITORING SYSTEM WIRING CONNECTOR.

Part: THERMOCOUPLE — CONTAMINATED (BRAKE OVERHEAT) · airframe 218 hrs · 194 cycles

BRAKE OVERHEAT WARNING, LEFT INBOARD BRAKE INDICATED 20. CLEANED CONTAMINATION FROM BTMS WIRING CONNECTOR.