N695CA

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 38,746 hrs · 27,759 cycles

AFT 2 EMERGENCY CEILING LIGHTS INOP REMOVED AND REPLACED BULBS IAW CRJ 900 AMM 33-51-09. OPS CHECK GOOD.

Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 38,433 hrs · 27,500 cycles

WHEN TROUBLESHOOTING ISOLATION VALVE FOUND INTERCOSTAL AT STR 22L BETWEEN FRAME STATIONS 295 TO 333 CORRODED AND GROUND STUDS NOT ATTACHED DUE TO CORROSION. SHEET METAL EVALUATION REQUIRED. UPON FURTHER INVESTIGATION FOUND CORRODED INTERCOSTAL TO BE AT STRINGER 21L REPLACED STGR 21L INTERCOSTAL P/N:SH670-31822-1 BETWEEN FS295 AND FS333 IAW CRJ900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.

Part: SKIN — CHAFED (ZONE 100) · airframe 38,433 hrs · 27,500 cycles

FOUND CHAFE ON BELLY OF AIRCRAFT AT FS 913 LBL 27. COMPLIED WITH BOMBARDIER GREO 670-53-00-290 REV F DATED 2019/04/26 SOLUTION 2. THIS REPAIR HAS SDIR/ REINSPECT REQUIREMENTS.

Part: DRAG ANGLE — CRACKED (ZONE 300) · airframe 38,433 hrs · 27,500 cycles

LH VERTICAL STAB FWD DRAG ANGLE IS CRACKED. REPAIRED LH VERTICAL STAB FWD DRAG ANGLE IAW CRJ-900 SRM 55-31-00-201-A01

Part: DOOR — CRACKED (ZONE 800) · airframe 38,433 hrs · 27,500 cycles

L/H AFT EMERGENCY EXIT DOOR ON TOP BETWEEN PROX SENSOR STRIKER APPEARS TO BE CRACKED REMOVED LH AFT EMERGENCY EXIT DOOR LINER TO FACILITATE SHEETMETAL REPAIR IAW CRJ900 AMM 25-26-09-000-801 (CONFIG A02). COMPLIED WITH MHIRJ REO# 670-52-21-103 REV -- DATED 2024-11-06. INSTALLED LH AFT EMERGENCY EXIT DOOR LINER IAW CRJ900 AMM 25-26-09-400-801/A02.

Part: DOOR — CRACKED (ZONE 800) · airframe 38,433 hrs · 27,500 cycles

R/H FORWARD EMERGENCY EXIT DOOR ON TOP BETWEEN PROX SENSOR STRIKER APPEARS TO BE CRACKED REMOVED RH FWD EMERGENCY EXIT DOOR LINER TO FACILITATE SHEETMETAL REPAIR IAW CRJ900 AMM 25-26-09-000-801 (CONFIG A02). COMPLIED WITH MHIRJ REO# 670-52-21-103, REV --, DATED 2024-11-06. INSTALLED RH FWD EMERGENCY EXIT DOOR LINER REPAIR IAW CRJ900 AMM 25-26-09-400-801/A02

Part: DOOR — CRACKED (ZONE 800) · airframe 38,433 hrs · 27,500 cycles

L/H FORWARD EMERGENCY EXIT DOOR ON TOP BETWEEN PROX SENSOR STRIKER APPEARS TO BE CRACKED REMOVED LH FWD EMERGENCY EXIT DOOR LINER TO FACILITATE SHEETMETAL REPAIR IAW CRJ900 AMM 25-26-09-000-801 (CONFIG A02). COMPLIED WITH MHIRJ REO# 670-52-21-103 REV -- DATE 2024-11-06. INSTALLED LH FWD EMERGENCY EXIT DOOR LINER REPAIR IAW CRJ900 AMM 25-26-09-400-801/A02

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,016 hrs · 26,298 cycles

PASSENGER DOOR EXTERIOR EMERGENCY LIGHT OUT. RELAMPED PASSENGER DOOR EXTERIOR EMER LIGHT, OPS TEST GOOD PER AMM 33-51-15.

Part: DOUBLER — CORRODED (BS 300 S27) · airframe 31,515 hrs · 21,731 cycles

LOWER TCAS ANTENNA INTERNAL DOUBLER CORRODED AT FS 300 STR 27. - REMOVED & REINSTALLED TCAS ANTENNA IAW CRJ 900 AMM 34-43-01-001-400-801-A03, REMOVED AND REPLACED ANTENNA DOUBLER IAW SRM 51-42-06-001-A01, 51-40-11-001-001-A01, OPS CHECK IAW AMM 34-43-00-710-801-A01, RESTORED SURFACE IAW SRM 51-25-01-001-001-A01, NO FAULTS NOTED.

Part: FRAME — CORRODED (BS 969 S25-26R) · airframe 31,515 hrs · 21,731 cycles

FRAME AT FS 969.00 CORRODED BETWEEN STGR 26R AND 25R. - COMPLIED WITH REMAINING STEPS OF SRM CRJ 900 53-00-06-201-001-A03.

Part: INTERCOSTAL — CORRODED (BS 865-881 S24R) · airframe 31,515 hrs · 21,731 cycles

INTERCOSTAL @ STRINGER 24R IS CORRODED BETWEEN FS865-FS881. - REMOVED & REPLACED INTERCOSTAL AT STR 24R FS 865 - 881 IAW REO 690-53-51-298.

Part: INTERCOSTAL — CORRODED (BS 881-897 S24R) · airframe 31,515 hrs · 21,731 cycles

INTERCOSTAL @ 24R IS CORRODED BETWEEN FS881-FS897 - REMOVED AND REPLACED INTERCOSTAL @ 24R FS 881-FS 897 IAW REO 690-53-51-299.

Part: FRAME — CORRODED (BS 942 S25-26R) · airframe 31,515 hrs · 21,731 cycles

FRAME AT FS 942.00 CORRODED BETWEEN STGR 26R AND 25R. - PERFORMED LEAK CHECK IAW CRJ 900 AMM 21-23-00-790-801(A01) LEAK CHECK GOOD AT THIS TIME.

Part: INTERCOSTAL — CORRODED (BS 897-913 S24R) · airframe 31,515 hrs · 21,731 cycles

INTERCOSTAL @ 24R IS CORRODED BETWEEN FS913 & FS897 - REMOVED AND REPLACED INTERCOSTAL @ STR 24R FS 913-FS 897 IAW REO 690-53-51-300.

Part: INTERCOSTAL — CORRODED (BS 913-927 S24R) · airframe 31,515 hrs · 21,731 cycles

INTERCOSTAL & CLEAT ARE CORRODED @ 24R BTW FS 927-913. - REMOVED & REPLACED INTERCOSTAL & CLEAT AT STR 24R FS913-927 IAW CRJ900 SRM 53-42-06-001-001-A01 & REO 690-53-51-301 SRM 51-42-06-001-001-A01.

Part: STRINGER — CORRODED (BS 927-977 S23R) · airframe 31,515 hrs · 21,731 cycles

STRINGER 23R IS CORRODED BETWEEN FS 927 - FS 977. - REPAIRED STRINGER 23R IAW EA #CRJ 953-11858 DATE 08-11-21 REV IR. INSTALLED SPLICE IAW CRJ 900 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01 AND INSTALLED 3 CLEATS COMMON TO STRINGER 23 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-010-A01.

Part: INTERCOSTAL — CORRODED (E/E BAY DOOR FRM) · airframe 31,515 hrs · 21,731 cycles

AVIONICS BAY DOOR SURROUND STRUCTURE, INTERCOSTAL CORRODED AT STGR 27L AND BETWEEN FS349 AND FS364 - "REMOVED & REPLACED AVI BAY DOOR SURROUND INTERCOSTAL AT STR 27 BETWEEN FS 349-364 IAW CRJ900 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. RESTORED FINISH IAW SRM 51-21-11-001-001-A01. REMOVED & REINSTALLED PROXIMITY SENSOR PX41 IAW CRJ900 AMM 52-70-08-000/400-801-A01. PERFORMED OPS CHECK IAW AMM 52-42-00-710-801(A01) OPS CHECK GOOD. WVAC EMP # 56399"

Part: INTERCOSTAL — CORRODED (BS 913-927 S23R) · airframe 31,515 hrs · 21,731 cycles

INTERCOSTAL @ 23R IS CORRODED BETWEEN FS913 TO FS927. - REMOVED AND REPLACED FABRICATED INTERCOSTAL OF STR 23R FS 913 TO FS 927 IAW REO 690-53-51-217 WVAC EMP STAMP #750 MTC

Part: CLEAT — DAMAGED (BS 310 S21R) · airframe 31,515 hrs · 21,731 cycles

CLEAT ON STRINGER 21R @ FS 310 REQUIRES REPLACEMENT PN#SH670-32605-2. @ FS 310 REQUIRES REPLACEMENT PN#SH670-32605-2. - REMOVED CLEAT IAW CRJ 900 SRM 51-42-06-001-001-A01. FABRICATED NEW SERVICEABLE CLEAT PER SAMPLE ON STRINGER 21R @ FS 310 OUT OF S6144-13 MATERIAL IAW CRJ 900 SRM 51-24-16-001-001-A01. LOCATED, DRILLED AND INSTALLED CLEAT ON STG 21R @ FS 310 IAW CRJ 900 51-40-11-001-001-A01, 51-42-06-001-001-A01.

Part: ANGLE — CORRODED (BS 310-349) · airframe 31,515 hrs · 21,731 cycles

PAX DOOR SILL ANGLE CORRODED AT FASTENER HOLES. - "REMOVED UNSERVICEABLE PAX DOOR SILL ANGLE AND INSTALLED SERVICEABLE SILL ANGLE IAW CRJ 900 SRM'S 51-41-02-001-001-A01, 57-42-06-001-001-A01REMOVED AND INSTALLED GROUND STUD AND PAX DOOR SILL ANGLE IAW CRJ 900 AMM AND SRM 51-41-02-001-001-A01 51-80-00-910-804-A01, 51-80-00-140-801-A01, 52-70-04-000-805-A02 AND 52-70-04-400-802-A02. WVAC EMP STAMP #792 MTC"

Part: FITTING — GOUGED (RT MLG) · airframe 31,515 hrs · 21,731 cycles

R/H MLG SIDE STAY FITTING HAS A GOUGE ON THE UPPER O/B SIDE (MARKED WITH ORANGE TAPE). - REPAIRED R/H MLG SIDE STAY FITTING ON THE UPPER O/B SIDE IAW BOMBARDIER REO 670-57-11-043. REV A WVAC EMP #7358

Part: FRAME — CORRODED (BS 954 S25-26R) · airframe 31,515 hrs · 21,731 cycles

FRAME AT FS 954.00 CORRODED BETWEEN STGR 25R AND 26R. - PERFORMED CUT OUT OF FRAME AT STGR 27 AND REMOVED FRAME SECTION FROM STGR 20 TO 27 @ 954 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 AND 53-00-06-201-001-A03. PERFORMED EDDY CURRENT OF FRAME @ FS 954 CUTLINE IAW CRJ 900 SRM 53-00-06-101-001-A03

Part: FLOOR SUPPORT — CORRODED (BS 1000-1098) · airframe 31,515 hrs · 21,731 cycles

FLOOR BEAM AT LBL27 HAS MULTIPLE SPOTS OF CORROSION FROM FS 1000.00 TO FS 1098.00. - REMOVED AND REPLACED FLOORBEAM AT LBL 27 FS 1000-1098 IAW CRJ 900 SRM 53-00-41-201-001-A03. RESTORED FINISH IAW SRM 51-25-00-001-001-A01.

Part: HANDLE — GOUGED (GALLEY DOOR)

GALLEY SERVICE DOOR OUTER HANDLE HOUSING IS GOUGED AROUND THE FWD EDGE - REMOVED GALLEY SERVICE DOOR & INSTALLED GALLEY SERVICE DOOR & REMOVE & REPLACE GALLEY SERVICE DOOR OUTER HANDLE HOUSING BY REMOVING & REINSTALLING GALLEY SERVICE DOOR HANDLE & PEELING BACK & REINSTALLING THE INNER SKIN IAW CRJ 900 AMM'S & SRM'S 52-41-00-000/400-801, 52-41-03-000/400/801-A01, SRM 51-42-06-001-001-A01 & 51-42-13-001-001-A01, 51-42-06-001-001-A01, 51-42-73-001-001-A01.

Part: STRINGER — CORRODED (BS 954-977 S21R) · airframe 31,515 hrs · 21,731 cycles

STRINGER 21R IS CORRODED BETWEEN FS 977-FS 954 IS CORRODED. - REMOVED AND INSTALLED SPLICE AT STR 21R IAW SRM 51-42-11-001-001-A01 AND REPAIRED STR 21R FS 977-954 IAW EA CRJ953-11815. WVAC STAMP #750 MTC

Part: STRINGER — CORRODED (BS 942-977 S22R) · airframe 31,515 hrs · 21,731 cycles

STRINGER 22R IS CORRODED BETWEEN FS 942 - FS 977 - REPAIRED STR 22R FS 942-977 IAW EA CRJ 953-11908. REMOVED AND REINSTALLED STRINGER SPLICE ON STR 22R IAW CRJ900 SRM 51-42-01-001-001-A01 REPAIRED STR 22R IAW EA CRJ953-11816. COMPLIED WITH WORK REPAIR OF STR 22R IAW EA CRJ 953-11816.ALL STEPS COMPLETED.

Part: STRINGER — CORRODED (BS 927-977 S24R) · airframe 31,515 hrs · 21,731 cycles

STRINGER 24R IS CORRODED BETWEEN FS 927 - FS 977. - REPAIRED STRINGER IAW ENDEAVOR AIR EA CRJ953-11862.

Part: STRINGER — CORRODED (BS 942-977 S25R) · airframe 31,515 hrs · 21,731 cycles

STRINGER 25R IS CORRODED BETWEEN FS 977 TO 942. - REPAIRED STRINGER 25R BETWEEN FS 977 TO 942 IAW EA CRJ 953-11864.

Part: BRACKET — CRACKED (FAIRING) · airframe 31,515 hrs · 21,731 cycles

INBOARD AFT UPPER HINGE LINE FAIRING HAS A BROKEN TAB BEHIND IT, ATTACHES TO PANEL 433BT. - REMOVED AND REPLACED IB AFT HINGE LINE FAIRING BRACKETS L/S PYLON IAW CRJ 900 SRM 51-42-06-001-001-A01, INSTALLED NUTPLATE ON SAME BRACKET IAW SRM 51-42-10-001-001-A01. WVAC EMP # 56399

Part: INTERCOSTAL — CORRODED (BS 985-1000) · airframe 31,515 hrs · 21,731 cycles

LH FLOOR SILL HAS MULTIPLE SPOTS OF CORROSION FROM FS 985.00 TO FS 1000.00 - REMOVED CORROSION ON FWD CARGO BAY SURROUND STRUCTURE IAW CRJ900 SRM 51-21-06-001-001-A01. FOUND TO BE WITHIN LIMITS. REFINISHED BLENDED AREA IAW CRJ00 SRM 51-26-16-001-001-A01.

Part: FRAME — CORRODED (BS 1088 S24L-R) · airframe 31,515 hrs · 21,731 cycles

FRAME AT FS1088.00 HAS MULTIPLE SPOTS OF CORROSION FROM STGR 24L TO 24R. - REPAIRED FRAME SECTOR FROM F.S.1088, 25L-25R IAW CRJ 900 SRM 53-00-06-201-001-A03. WVAC EMP STAMP # 750 MTC

Part: STRINGER — CORRODED (BS 333-379 S21R) · airframe 31,515 hrs · 21,731 cycles

STRINGER 21R CORRODED BTW F.S. 333- F.S. 379 - REMOVED AND REPLACED STR 21R. AT F.S. 333.00 TO F.S. 379.00 P/N SH670-31383-15 IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01. FINISHED SURFACE IAW CRJ 900 SRM 51-25-01-001-001-A01 & 51-21-11-001-001-A01.

Part: INTERCOSTAL — CORRODED (BS 333-349 S20R) · airframe 31,515 hrs · 21,731 cycles

INTERCOSTAL AT STR R20 IS CORRODED FROM FS 333 TO 349. - REMOVED CORRODED INTERCOSTAL, LOCATED, DRILLED & INSTALLED 1 EA NEW INTERCOSTAL P/N: SH670-320-004-1 ON STG R 20R BTW FS 319- FS 349 IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, & 51-42-21-001-001-A01 & RESTORED SURFACE FINISH IAW CRJ 900 SRM'S 51-25-01-001-001-A01 & 51-21-11-001-001-A01. WVAC STAMP #722TC

Part: STRINGER — CORRODED (BS 319-333 S21R) · airframe 31,515 hrs · 21,731 cycles

STRINGER R21 CORRODED BETWEEN FS 319 - FS 333. - REMOVED & INSTALLED DCU2 FOR ACCESS IAW CRJ 900 AMM 31-41-04/05-000/400-801-A01. OP TEST PERFORMED NO FUALTS NOTED. REMOVED & REPLACED 1 NEW SPLICE P/N SH670-31197-12 STR R21 PN SH670-31 IAW CRJ SRM 51-40-11-001-001-A01, 51-42-06-001-001-A02 & 51-42-21-001-001-A01. RESTORED FINISH IAW SRM 51-25-01-001-001-A01 & 51-21-11-001-001-A01.

Part: STRINGER — CORRODED (BS 364-379 S23R) · airframe 31,515 hrs · 21,731 cycles

STRINGER 23R CORRODED BTW F.S. 364- F.S 379. - REMOVED & REPLACED STGR 23R FROM FS 364.00 - FS 379 PN SH670-31380-15 IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01. RESTORED FINISH IAW CRJ 900 SRM 51-2-01-001-001-A01 AND 51-21-11-001-001-A01.

Part: DIAPHRAGM — CORRODED (SERVICE DOOR) · airframe 31,515 hrs · 21,731 cycles

FORWARD WATER WASTE DRAIN SERVICE DOOR INNER STRUCTURE IS CORRODED. - REMOVED AND REINSTALLED 1 EA NEW IMPACT ANGLE AND NEW DIAPHRAGM AND ORIGINAL ANGLE IAW CRJ 900 SRM 51-42-06-001-001-A01 REMOVED AND REINSTALLED SERVICABLE DOOR IAW SRM 51-42-06-001-001-A01. LOCATED AND DRILLED PARTS IAW CRJ 900 SRM 51-40-11-001-001-A01 AND APPLIED CIC IAW CRJ 900 SRM 51-21-11-001-001-A01. WVAC EMP #7358

Part: STRINGER — CORRODED (BS 280-333 S23R) · airframe 31,515 hrs · 21,731 cycles

STRINGER 23RH FROM FS 280.00 TO FS 333.00 REQUIRES REMOVAL FOR CORROSION. - REMOVED AND REPLACED CORRODED STR 23R AND STRINGER SPLICE STR 23R 280-333 IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.

Part: STRINGER — CORRODED (BS 333-349 S22R) · airframe 31,515 hrs · 21,731 cycles

STR 22R CORRODED FROM FS 333- FS 349. - LOCATED, DRILLED & INSTALLED 1 EA NEW STGR 22R PN: SH670-31379-1 IAW CRJ900 SRM 51-40-11-001-001-A01 & 51-42-06-001-001-A01. RESTORED SURFACE FINISH IAW CRJ900 SRM 51-25-01-001-001-A01 & 51-21-11-001-001-A01.

Part: STRINGER SPLICE — CORRODED (BS 280-333 S23R) · airframe 31,515 hrs · 21,731 cycles

STRINGER 23RH FROM FS 280.00 TO FS 333.00 REQUIRES REMOVAL FOR CORROSION. - REMOVED AND REPLACED CORRODED STR 23R AND STRINGER SPLICE STR 23R 280-333 IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.

Part: ANGLE — CORRODED (BS 310-319 S20R) · airframe 31,515 hrs · 21,731 cycles

INTERCOSTAL AT STR R20 IS CORRODED AT FS 310.00 & FS 319.00. - REMOVED & REPLACED ANGLE AT STR R20 AT F.S. 310-319 IAW CRJ900 SRM 51-40-11-001-001-A01/51-42-06-001-001-A01/51-42-21-001-001-A01, CIC IAW 51-21-11-001-001-A01. P/N SH670-32046-3, SH670-32047-1. WVAC EMP # 56399

Part: STRINGER — CORRODED (BS 285-310 S20R) · airframe 31,515 hrs · 21,731 cycles

STRINGER R20 CORRODED AT FS 285 TO FS 310.00. - REMOVED AND REPLACED STR 20R FS 285-310 IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. WVAC EMP STAMP #750 MTC

Part: LONGERON — CORRODED (BS 333) · airframe 31,515 hrs · 21,731 cycles

LONGERON @ FS 333.00 CORRODED. - COMPLIED WITH LONGERON REPLACEMENT @ FS 333.00 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 AND ALSO IAW MHIRJ REO# 690-53-21-1407 REV -- DATED 2021-08-02

Part: STRINGER — CORRODED (BS 285-310 S19R) · airframe 31,515 hrs · 21,731 cycles

STRINGER R19 IS CORRODED FS 285.00 TO FS 310.00. - REMOVED & REPLACED STR R19 AT FS 285.00 TO FS 310.00 IAW EA CRJ 953-11798. WVAC EMP #56399

Part: SEAT TRACK — CORRODED (BS 988-1015 LBL9) · airframe 31,515 hrs · 21,731 cycles

SEAT TRACK AT LBL9 CORRODED FROM FS 985.00 TO FS 1015.00. - R/R UNSERVICEABLE SEAT TRACK @ LBL 9.0 FROM FS 988-1015 IAW CRJ 900 AMM 53-00-49-000/400-802(A02) AND SRM 53-00-48-201-002-A01 AND 51-40-11-001-001-A01.

Part: INTERCOSTAL — CORRODED (BS 310-319 S20R) · airframe 31,515 hrs · 21,731 cycles

INTERCOSTAL AT STR R20 IS CORRODED AT FS 310.00 & FS 319.00. - REMOVED & REPLACED INTERCOSTAL AT STR R20 AT F.S. 310-319 IAW CRJ900 SRM 51-40-11-001-001-A01/51-42-06-001-001-A01/51-42-21-001-001-A01, CIC IAW 51-21-11-001-001-A01. P/N SH670-32046-3, SH670-32047-1. WVAC EMP # 56399

Part: FRAME — CORRODED (BS 379 S20-23R) · airframe 31,515 hrs · 21,731 cycles

FRAME SEGMENT @ F.S. 379 IS CORRODED BTW STGR R20-R23 - REMOVED & REPLACED FRAME SEGMENT AT FS 379 BETWEEN STR R20-R23 P/N SH670-32118-3A, REMOVED & INSTALLED STR 22R BTW FS 264-379 & 1 POST IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 & 51-40-11-001-001-A01. RESTORED FINISH IAW SRM 51-25-01-001-001-A01 & 51-21-11-001-001-A01.

Part: STRINGER SPLICE — CORRODED (BS 333 S22R) · airframe 31,515 hrs · 21,731 cycles

STG 22 CORRODED FROM FS 319-333 AND STG 22 SPLICE @ FS 333 CORRODED. - REMOVED AND REPLACED STR SPLICE OF STR 22 FS 333 IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01 REF 81509751 OP:565 FOR STRINGER REPLACEMENT.

Part: STRINGER — CORRODED (BS 280-333 S24R) · airframe 31,515 hrs · 21,731 cycles

STRINGER 24 RH FROM FS 280.00 TO FS 333.00 CORRODED, REQUIRES REMOVAL. - REMOVED & REPLACED STGR 24R FROM FS 280 TO FS 333 IAW CRJ 900 SRM 51-42-00-001-001-A01, 51-42-20-001-001-A01, 51-40-11-001-001-A01 INSTALLED CLEATS FOR STGR 24R (ORIGINAL CLEATS) BTW FS 280-333 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND RESTORED FINISH SURFACE IAW CRJ 900 SRM 51-25-01-001-001-A01 & 51-21-11-001-001-A01.

Part: CLEAT — CORRODED (BS 333-379) · airframe 31,515 hrs · 21,731 cycles

STRINGER 21R & CLEAT CORRODED BETWEEN FS 333 - FS 379. - REMOVED & REPLACED STRINGER & CLEAT IAW CRJ 900 SRM 51-40-11-001-001-A01 & 51-42-06-001-001-A01.

Part: STRINGER — CORRODED (BS 319-333 S22R) · airframe 31,515 hrs · 21,731 cycles

STG 22 CORRODED FROM FS 319-333 AND STG 22 SPLICE @ FS 333 CORRODED. - REMOVED AND REPLACED STR SPLICE OF STR 22 FS 333 IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01 REF 81509751 OP:565 FOR STRINGER REPLACEMENT.

Part: STRINGER — CORRODED (BS 319-333 S21R) · airframe 31,515 hrs · 21,731 cycles

STRINGER 21R & JOINT PIECE CORRODED BETWEEN FS 319 - FS 333. - REMOVED & REPLACED STRINGER & JOINT PIECE IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-21-001-001-A01 & 51-42-06-001-001-A01.

Part: ANGLE — CORRODED (SERVICE DOOR) · airframe 31,515 hrs · 21,731 cycles

FORWARD WATER WASTE DRAIN SERVICE DOOR INNER STRUCTURE IS CORRODED. - REMOVED AND REINSTALLED 1 EA NEW IMPACT ANGLE AND NEW DIAPHRAGM AND ORIGINAL ANGLE IAW CRJ 900 SRM 51-42-06-001-001-A01 REMOVED AND REINSTALLED SERVICABLE DOOR IAW SRM 51-42-06-001-001-A01. LOCATED AND DRILLED PARTS IAW CRJ 900 SRM 51-40-11-001-001-A01 AND APPLIED CIC IAW CRJ 900 SRM 51-21-11-001-001-A01.

Part: FLOOR SUPPORT — CORRODED (BS 661) · airframe 31,515 hrs · 21,731 cycles

FLOOR BEAM CAP CORRODED AT RBL9 BETWEEN FS661+16 AND FS661+90. - REPAIRED FLOORBEAM @ RBL 9.0 BETWEEN FS 661+16 TO 661+90 IAW CRJ-900 SRM 53-00-41-201-001 (A03).

Part: INTERCOSTAL — CORRODED (BS 349-364 S20R) · airframe 31,515 hrs · 21,731 cycles

INTERCOSTAL AT STR R20 AT FS 349.00 TO FS 364.00 CORRODED. - REMOVED AND REPLACED INTERCOSTAL AT STR 20R FROM FS 349-364 IAW CRJ900 SRM 51-42-21-001-001-A01. WVAC EMP # 56399

Part: FLOOR SUPPORT — CORRODED (BS 708-720) · airframe 31,515 hrs · 21,731 cycles

FLOOR BEAM AT LBL 9 HAS CORROSION BETWEEN FS 708.00 AND FS 720.00 - REPAIRED FLOORBEAM @ LBL 9.0 BETWEEN FS 708-720 IAW CRJ900 SRM 53-00-41-201-001-A03. WVAC EMP STAMP # 722 MTC

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 31,515 hrs · 21,731 cycles

PAX DOOR AFT DRAG ANGLE IS CRACKED ABOVE PULLY MOUNT BRACKET IN PREVIOUS REPAIR. - REPAIRED PAX DOOR AFT DRAG ANGLE IAW CRJ900 SRM 51-42-22-001-001-A01 AND AFT WEB (PAX DOOR) 3RD STIFFENER IAW EA CRJ952-11857, REV.IR DATE 7/8/21. WVAC EMP # 56399

Part: FLOORBEAM — CORRODED (BS 280) · airframe 31,515 hrs · 21,731 cycles

MULTIPLE SPOTS OF CORROSON ON THE LH FLOORBEAM AT FS 280 BETWEEN BL 0 AND LBL 36. - REMOVED & REPLACED LH FLOORBEAM AT FS 280 BETWEEN BL 0 AND LBL 36 IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 AND 57-40-11-001-001(A01). WVAC EMP STAMP #722 MTC

Part: BRACKET — CORRODED (CARGO DOOR) · airframe 31,515 hrs · 21,731 cycles

CENTER BAGGAGE BAY DOOR MACHINED BRACKET CORRODED AT LB 24 AND APPROX FS 631.34. - R/R UNSERVICEABLE BRACKET WITH A SERVICEABLE BRACKET ON CBBD IAW CRJ900 SRM 51-42-22-001-001-A01 & 51-42-23-001-001-A01.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 31,515 hrs · 21,731 cycles

MULTIPLE SPOTS OF CORROSION ON THE RH FLOORBEAM AT FS 280 BETWEEN BL 0 - RBL 36. - R/R 280 CROSSBEAM AND REMOVED CORROSION FROM RH 280 FLOORBEAM IAW CRJ 900 SRM 51-42-06-001-001(A01), 51-42-21-001-001, 51-42-13-001-001-(A01) AND 51-21-06-001-001(A01). WVAC EMP STAMP #722 MTC

Part: BRACKET — BROKEN (RT NACELLE) · airframe 31,515 hrs · 21,731 cycles

R/H ENGINE UPPER HINGE LINE FAIRING AFT MOUNT BRACKET BROKEN. - REMOVED AND REPLACED DAMAGED HINGE LINE FAIRING SUPPORT BRACKET IAW CRJ900 SRM 51-42-06-001-001-A01 AND CRJ900 SRM 51-45-00-001-001-A01 ON L/H PYLON. WVAC EMP # 7358

Part: FLOORBEAM — CORRODED (BS 280) · airframe 31,515 hrs · 21,731 cycles

FLOORBOARD ATTACH ANGLE AT FS 280 IN AVIONICS BAY CORRODED. - LOCATED, DRILLED AND INSTALLED 1 EA NEW FLOORBOAD ATTACH ANGLE AT FS 280 BETWEEN STGR 26L-26R IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 PN CC670-34256-3. WVAC EMP STAMP # 769 MTC

Part: FRAME — CORRODED (BS 661 S26L-R) · airframe 31,515 hrs · 21,731 cycles

FRAME CORRODED AT FS 661+90 BETWEEN STGR 26R AND STGR 26L - REMOVED LIGHT SURFACE CORROSION IAW CRJ900 SRM 51-21-06-001-001-A01. PAINTED FASTENER HEADS IAW CRJ900 SRM 51-21-16-001-001-A01. WVAC EMP STAMP # 775 MTC

Part: PLATE — CORRODED (BS 631 S25L-26R) · airframe 31,515 hrs · 21,731 cycles

FWD BAGGAGE BAY DOOR JOINT PLATE CORRODED AT FS 631.34 AND BETWEEN STGR 25L AND STGR 26L. - REMOVED 0.005 OF SURFACE CORROSION FROM JOINT PLATE IAW CRJ900 SRM 53-21-23-101-001-A02. FOUND TO BE OUT OF LIMITS. REPAIRED JOINT PLATE IAW EA CRJ 953-11810. RESTORED TO FINISH IAW CRJ900 SRM 51-21-16-001-001-A01.

Part: DOOR SILL — CORRODED (BS 349-364 RBL2) · airframe 31,515 hrs · 21,731 cycles

RH FLOOR SILL HAS MULTIPLE SPOTS OF CORROSION FROM FS 954.00 TO FS 969.00. - REMOVED CORROSION ON R/H FLOOR SILL FS 954-969 IAW CRJ 900 SRM 51-12-00-001-001(A01). REMOVED 0.003", REMAINING THICKNESS 0.060" , ORIGINAL 0.063". WITHIN LIMITS. WVAC EMP STAMP #722 MTC

Part: FLOOR SUPPORT — CORRODED (BS 280-310) · airframe 31,515 hrs · 21,731 cycles

RH FLOOR SILL HAS MULTIPLE SPOTS OF CORROSION FROM FS280.00 TO FS310.00. - BLENDED AND PAINTED CORROSION IAW CRJ900 SRM 5-12-00-001-001-A01, 53-00-45-201-001-A01. WVAC EMP STAMP # 775 MTC

Part: BULKHEAD WEB — CORRODED (BS 280 RBL 36) · airframe 31,515 hrs · 21,731 cycles

F.S. 280.00 UPPER WEB IS CORRODED AT RBL 36. - REMOVED AND INSTALLED FASTENERS IAW CRJ 900 SRM 51-42-13-001-001-A01 AND 51-42-14-001-001-A01. REMOVED CORROSION IAW CRJ 900 SRM 53-11-10-201-003-A01 AND 51-12-00-001-001-A01.

Part: FRAME — CORRODED (BS 310 S26L-R) · airframe 31,515 hrs · 21,731 cycles

FRAME AT FS 310.00 CORRODED AT STR L26 TO STR R26. - REMOVED AND REPLACED FRAME SEGMENT AT FS 310 BETWEEN STGR L23-R25 IAW CRJ 900 SRM 51-42-21-001-001-A01. WVAC EMP STAMP # 722 MTC. FRAME WAS NOT REPLACED, IT WAS REPAIRED PER SRM 51-112-21-001-001-A01. WVAC EMP # 7195

Part: FRAME — CORRODED (BS 333 S26L-R) · airframe 31,515 hrs · 21,731 cycles

FRAME AT FS 333.00 CORRODED AT STR L26 TO STR R26 - REMOVED & REPLACED FRAME SECTION AT FS 333.00 STR L26 TO R26 IAW CRJ 900 SRM 53-21-06-001-006-A02 WVAC EMP # 56399

Part: FRAME — CORRODED (BS 319 S26L-R) · airframe 31,515 hrs · 21,731 cycles

FRAME AT FS 319.00 CORRODED AT STR L26 TO STR R26. - REMOVED AND REPLACED FRAME SEGMENT @ FS 319 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 53-00-06-201-006-A01. WVAC STAMP #722 MTC

Part: INTERCOSTAL — CORRODED (BS 661) · airframe 31,515 hrs · 21,731 cycles

STRINGER CLEAT AT STGR 19R CORRODED BETWEEN FS661+90 AND FS677 - DRILLED LOCATED AND INSTALLED NEW SERVICEABLE CLEAT IAW CRJ 900 SRM 51-42-21-001-001-A01 REMOVED AND REINSTALLED DIAPHRAGM IAW CRJ 900 SRM 51-42-21-001-001-A01 AND REPAIRED CORROSION IAW CRJ 900 SRM 53-00-00-101-001-A01.

Part: FLOOR SUPPORT — CORRODED (BS 280-310) · airframe 31,515 hrs · 21,731 cycles

LH FLOOR SILL HAS MULTIPLE SPOTS OF CORROSION FROM FS280.00 TO FS310.00. - REMOVED CORROSION ON L/H FLOOR SILL 280 TO 310 IAW CRJ 900 SRM 51-12-00-001-001-A01 AND 53-00-5-201-001(A01). WITHIN ALLOWABLE LIMITS.

Part: SEAT TRACK — CORRODED (BS 744-762) · airframe 31,515 hrs · 21,731 cycles

LH SIDE SEAT TRACK RAIL MOUNT IS CORRODED BETWEEN FS 744.15 TO FS 762.85. - REMOVED LH SEAT TRACK RAIL AND HAT CHANNEL IAW CRJ900 AMM 53-00-49-000-801 FOUND SEAT RAIL TO BE OUT OF LIMITS IAW CRJ900 SRM 51-21-06 001-001-A01 AND 53-41-49-001-001-A02. INSTALLED SERVICEABLE SEAT RAIL AND REINSTALLED SEAT RAIL MOUNT IAW CRJ900 AMM 53-00-49-400-801-A07. WVAC EMP # 7195

Part: DOOR SILL — CORRODED (BS1000-1047 S17L) · airframe 31,515 hrs · 21,731 cycles

AFT CARGO DOOR CUTOUT SEAL PLATE IS CORRODED ALONG 2B RADIUS ON TOP & IB FACE IN SEVERAL LOCATIONS. - REMOVED FASTENERS, BLENDED CORROSION AND INSTALLED FASTENERS IAW CRJ 900 SRM'S 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01,AND 53-61-23-201-001-A01.

Part: ATTACH PLATE — CORRODED (BS 629 BL 0) · airframe 31,515 hrs · 21,731 cycles

ATTACH PLATE AT BLO AND FS 629 IS CORRODED. - REMOVED AND REPLACED PLATE IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-15-001-001-A01.

Part: BRACKET — CORRODED (BS 319 S19L) · airframe 31,515 hrs · 21,731 cycles

PAX DOOR ELECTRICAL CONNECTOR AT STR L19 FS 319 ANGLE BRACKET CORRODED - MICROMETER WVACT 1446 CAL DUE 30JUNE2022. REMOVED LIGHT CORROSION IAW CRJ 900 SRM 51-21-06-001-001-A01, STEP 5.A.1-B.1-5. NO PITTING NOTED. ORG NOMINAL THICKNESS .040". REMOVED LESS LESS THAN .001" MATERIAL, REMAINING THICKNESS APPROX .040".

Part: FLOOR SUPPORT — CORRODED (BS 565-661) · airframe 31,515 hrs · 21,731 cycles

LH FLOOR SILL CORRODED AROUND FASTENERS AT FS565, FS629, AND FS661+16 (MARKED WITH TAPE). - REMOVED AND INSALL 2 RIVETS IAW CRJ900 SRM 51-42-00-001-001-A01 REMOVED CORROSION ON L/H FLOOR SILL AT FS 565,629 & 661+16 IAW SRM 51-12-00-001-001-A01 AND L/W LPI IAW SRM 51-00-45-001-001-A01. WVAC EMP # 7358

Part: FRAME — CORRODED (BS 581 S26L-R) · airframe 31,515 hrs · 21,731 cycles

FRAME CORRODED AT FS 581 BETWEEN STGR 26R AND STGR 26L. - REMOVED & INSTALLED RIVETS, BLENDED AND APPLIED PAINT & PRIMER IAW CRJ900 SRM'S 51-42-06-001-001-A01, 51-42-06-001-001-A01, 51-25-06/16-001-001-A01, 51-21-11-001-001-A01.

Part: RIVET — CORRODED (BS 631) · airframe 31,515 hrs · 21,731 cycles

BAGGAGE CENTER BAY DOOR SURROUND STRUCTURE CORRODED AT FS 631.34 BETWEEN STGR 25L AND STGR 24L. - CHEMICALLY REMOVED PAINT TO FOM IAW CRJ 900 SRM 51-26-01-001-001-A01, AFTER FURTHER INVESTIGATION FOUND ONLY 4 EACH CORRODED BLIND RIVETS, REMOVED AND REPLACED 4EA BLIND RIVETS IAW CRJ 900 51-42-13-001-001-A01. RESTORED FINISH IAW CRJ 900 SRM 51-25-06-001-001-A01, SRM 51-25-16-001-001-A01, AND SRM 51-21-11-001-001-A01.

Part: LINE — SHORT (LT OVERWING) · airframe 31,515 hrs · 21,731 cycles

LH OVERWING EMER EXIT SAFETY LINE WILL NOT REACH THE WING FITTING - REMOVED/REPLACED L/H EMER EXIT SAFETY LINE P/N:BA690-40604-1 IAW CRJ 900 AMM 25-63-04-000-801-A01, 25-63-04-400-801-A01.

Part: LINE — SHORT (RT OVERWING) · airframe 31,515 hrs · 21,731 cycles

RH OVERWING EMER EXIT SAFETY LINE WILL NOT REACH THE WING FITTING. - INSTALLED NEW SERVICEABLE RH OVERWING EMER EXIT SAFETY LINE IAW CRJ 900 AMM 25-63-04-400-801-A02.

Part: FLOOR SUPPORT — CORRODED (BS 1000-1098) · airframe 31,515 hrs · 21,731 cycles

FLOOR BEAM AT RBL 9 HAS MULTIPLE SPOTS OF CORROSION FROM F.S. 1000.00 TO F.S. 1098.00 - REMOVED & REPLACED FLOORBEAM LBL9 AT FS 1000.00-1095.00 IAW EA CRJ953-11818. RESTORED SURFACE IAW CRJ900 SRM 51-25-00-001-001-A01.

Part: FLOOR SUPPORT — CORRODED (BS 1000-1098) · airframe 31,515 hrs · 21,731 cycles

FLOOR BEAM AT LBL9 HAS MULTIPLE SPOTS OF CORROSION FROM F.S. 1000.00 TO F.S. 1098.00. - REMOVED VAPOR BARRIER ATTACHED TO FLOOR BEAM AT LBL9 FROM FS 1000 TO FS 1098 FOR ACCESS TO CORROSION. INSTALLED 12EA NEW NUTPLATES IAW CRJ 900 SRM 51-42-15-001-001-A01. PERFORMED UT THICKNESS MEASUREMENTS OF REWORKED AREAS IAW CRJ 900 NDTM PART 1, 51-20-004-270-A01. FOUND LOWEST REMAINING THICKNESS TO BE .041 OR GREATER. ENGINEERING NOT REQ. REPAIRED IAW CRJ900 SRM 53-00-41-201-001-A03. REMOVED CORROSION AT LBL 9 FROM FS 1000.00 TO FS 1098.00 IAW CRJ 900 SRM 51-21-06-001-001-A01. FABRICATED, LOCATED AND DRILLED FLOOR BEAM SECTION FROM FS 1005.5-1064 IAW BOMBARDIER REO 670-53-00-029, REV.A 8/31/10, FIG. 13. PERFORMED EDDY CURRENT INSPECTION OF CUTLINE EDGES IAW BOMBARDIER REO 670-53-00-020, REV.A DATED 8/31/10, STEP 3. NO INDICATIONS NOTED AT THIS TIME. LOCATED SPLICES AND COUNTERSUNK NUTPLATE RIVET HOLES IAW CRJ 900 SRM 53-00-41-201-001-A03 AND REO 670-53-00-029. PAINTED FLOOR BEAM LBL 9 SECTOR IAW CRJ 900 SRM 51-25-00-001-001-A01. INSTALLED FLOOR BEAM, SPLICES AND REPAIR PARTS IAW CRJ 900 SRM 53-60-41-201-001-A03.

Part: STRINGER — CORRODED (BS 927-969 S26R) · airframe 31,515 hrs · 21,731 cycles

STGR 26R CORRODED FROM FS 927.00 TO FS 969.00. - REPAIRED STGR 26R FROM FS 927.00 TO FS 969.00 IAW EA# CRJ 953-11865. WVAC EMP STAMP #766 MTC

Part: ANGLE — CORRODED (BS 280) · airframe 31,515 hrs · 21,731 cycles

F.S. 280.00 FWD "J" ANGLE IS CORRODED - REMOVED AND REPLACED FS 280.00 FWD J ANGLE IAW CRJ900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-42-13-001-001-A01. WVAC EMP# 579269

Part: LIGHT — FAILED (F/A CALL LIGHT) · airframe 30,216 hrs · 20,539 cycles

F/A CALL INDICATOR LIGHT INOPERABLE OVER CENTER ISLE. REMOVED AND REPLACED LIGHT ASSEMBLY, EMERGENCY SIGN ABOVE ROW 12 & 13 AISLE. ALL CHECKS GOOD. WORK DONE IAW CRJ 900 AMM 33-51-07.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 29,954 hrs · 20,285 cycles

LEFT AFT OVERWING EXTERIOR EMERGENCY LIGHT LENS CRACKED. REPLACED LENS, REFERED TO AMM 33-51-15.

Part: LIFE VEST — MISSING (SEAT 9B) · airframe 25,224 hrs · 16,665 cycles

SEAT 9B MISSING THE LIFE VEST. INSTALLED THE SEAT 9B LIFE VEST IAW AMM 25-61-03. OK FOR SERVICE.

Part: LIFE VEST — MISSING (SEAT 14A) · airframe 25,183 hrs · 16,637 cycles

SEAT 14A LIFE VEST WAS MISSING. REPLACED THE LIFE VEST IAW AMM 25-61-03.

Part: LIFE VEST — MISSING (CABIN) · airframe 24,638 hrs · 16,004 cycles

SEAT 8A LIFE VEST MISSING. INSTALLED LIFE VEST AT SEAT 8A IAW JOBCARD EE-900. NO DEFECTS NOTED AT THIS TIME. A/C OK FOR SERVICE.

Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 24,846 hrs · 16,393 cycles

FIRST OFFICER`S OXYGEN MASK HOSE HAS A LEAK. REMOVED AND REPLACED THE OXYGEN MASK IAW AMM 35-11-12.

Part: SEAT TRACK — CORRODED (BS 661-693) · airframe 24,703 hrs · 16,295 cycles

LEFT SIDEWALL SEAT TRACK, BS 661 TO 693 ARE CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-400-801-A07.

Part: SEAT TRACK — CORRODED (BS 669.4-977) · airframe 24,703 hrs · 16,295 cycles

LEFT SEAT TRACK, BS 669.4 - 977 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW 53-00-49-400-801-A07.

Part: STOWAGE BOX — INOPERATIVE (OXYGEN SYSTEM) · airframe 24,703 hrs · 16,295 cycles

CO-PILOT'S OXYGEN BOX INDICATOR WILL NOT CLOSE. REMOVED AND REPLACED THE CO-PILOT'S OXYGEN BOX, OPS AND LEAK CHECKED GOOD IAW AMM 35-11-15-400-801-A01.

Part: BATTERY PACK — WEAK (FLASHLIGHTS) · airframe 24,703 hrs · 16,295 cycles

ALL EMERGENCY FLASHLIGHTS BATTERIES ARE WEAK.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 24,216 hrs · 15,931 cycles

DURING OPS TEST OF THE EMERGENCY POWER SUPPLY UNIT. FOUND THE EPSU FAILED THE OPS CHECK.

Part: FRAME — CORRODED (FUSELAGE) · airframe 23,116 hrs · 15,109 cycles

FS 310.00 FRAME, STR 26L-25R, FWD & AFT SIDES CORRODED. REPAIRED FRAME STA 310 IAW REO 670-53-21-799& ECTC REO 670-53-21-799 REV A.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 23,116 hrs · 15,108 cycles

STRINGER 26R FS 295-349 CORRODED. REMOVED AND REPLACED STRINGER AT FS 295-349 26R. PER SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. P/N-SH670-31634-2. DRAWING SH670-31634.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 23,116 hrs · 15,108 cycles

STRINGER SPLICE FS 333 CORRODED, STR 26R. REMOVED AND REPLACED STRINGER SPLICE AT FS 333 26R. PER SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. P/N-SH670-32429-4. DRAWING SH670-32429.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 23,116 hrs · 15,108 cycles

STRINGER 26L,FS 319.70- FS 333.00 CORRODED. REMOVED AND REPLACED STRINGER AT FS 319.70-333.00 26L PER SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. P/N-SH670-31654-1. DRAWING SH670-343651.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 23,116 hrs · 15,108 cycles

INTERCOSTAL, FS349-364, STR 27R CORRODED. REMOVED AND INSTALLED NEW INTERCOSTAL, FS349-364, STR 27R IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-42-20-001-001-A01, 51-40-11-001-001-A01, 51-23-00-001-001-A01, 51-25-16-001-001-A01, 51-21-11-001-001-A01.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 23,116 hrs · 15,108 cycles

TCAS ANTENNA INTERNAL DOUBLER BETWEEN FS 295.00 AND 310.00, NEAR STRINGER 27 IS CORRODED. REMOVED AND REPLACED TCAS ANTENNA INTERNAL DOUBLER BETWEEN FS 295.00 AND 310.00 NEAR STRINGER 27 IAW SRM 51-42-06-001-001 A01.

Part: FRAME — CORRODED (FUSELAGE) · airframe 23,116 hrs · 15,108 cycles

FS 333.00 FRAME BETWEEN STRINGERS 25L AND 26R, AFT SIDE IS CORRODED. REMOVED CORROSION ON FS 333.00 IAW SRM 51-21-06-001-001 A01 AND 6 RIVETS IAW SRM 51-42-06-001-001-A01. PERFORMED UT THICKNESS INSPECTION OF FRAME IAW NDTM PT 1 51-20-004-270 A01. MINIMUM THICKNESS IS .047". ORIGINAL IS .050". REMOVED IS .003". PERFORMED EDDY CURRENT INSPECTION IAW NDTM PT 1 51-20-006-250 A01. NO INDICATIONS NOTED AT THIS TIME. PER REO 670-53-21-1308: BLENDED OUT CORROSION IN FRAME WEBS & FRAME ATTACHED FLANGES. PERFORMED LPI/EDDY CURRENT INSPECTION ON BLENDED AREAS PER NDTM 51-20-008/006 TO ENSURE AREAS ARE CRACK FREE. FINISHED AREAS A023 PER SRM 51-21-16; AND APPLIED CORROSION-INHIBITING COMPOUND OVER ALL REWORKED AREAS PER SRM 51-21-11.

Part: FRAME — CORRODED (FUSELAGE) · airframe 23,116 hrs · 15,108 cycles

FS 319.70 BETWEEN STRINGER 25L AND 25R, FWD AND AFT SIDES CORRODED. REMOVED CORROSION AND 5 RIVETS IAW SRM 51-21-06-001-001 A01 AND 51-42-06-001-001 A01. PERFORMED UT THICKNESS INSPECTION OF FRAME IAW NDTM PT 1 51-20-004-270 A01. MINIMUM THICKNESS IS .047", ORIGINAL IS .050", REMAINING IS .003". PERFORMED EDDY CURRENT INSPECTION IAW NDTM PT 1 51-20-006-250 A01. NO INDICATIONS NOTED AT THIS TIME. FRAME 319.70 FOUND TO BE OUT OF LIMITS. PER REO 670-53-21-1308: BLENDED OUT CORROSION IN FRAME WEBS & FRAME ATTACHED FLANGES. LPI/EDDY CURRENT INSPECT BLENDED AREAS PER NDTM 51-20-008/ -006 TO ENSURE AREAS ARE CRACK FREE. FINISHED AREAS A023 PER SRM 51-21-16; AND APPLIED CORROSION-INHIBITING COMPOUND OVER ALL REWORKED AREAS PER SRM 51-21-11.

Part: DOOR — OUT OF ADJUST (MAIN PAX) · airframe 21,214 hrs · 13,729 cycles

UNABLE TO OPEN FWD PAX DOOR FROM INSIDE OR FROM OUTSIDE GRD CREW. FOUND THE PAX DOOR LATCH SPRINOTS OUT OF ADJUSTMENT CAUSING THE LATCH OCMS TO BIND WICH COUSED THE SECONDARY LOCK MECHONISM TO BIND AND NOT UNLOCK. ADJUSTED THE PAX DOOR LATCH SPGOTS IAW AMM 53-21-23 C/W FUNCTIONAL TERT OF PAX DOOR IAW AMM 52-91-00 OPS CHECKED GOOD.

Part: LEVER — UNKNOWN (PAX DOOR) · airframe 21,165 hrs · 13,689 cycles

MAIN CABIN DOOR LEVER DIFFICULT TO RAISE AND LOWER. PERFORMED OPS TEST OF THE PASSENGER DOOR IAW AMM 52-11-00. OPS CHECKED GOOD. NO DEFECTS NOTED AT THIS TIME.

Part: DOOR — BINDING (MAIN PAX) · airframe 21,111 hrs · 13,652 cycles

MAIN PASSSENGER DOOR STICKS WHEN OPENING FROM INSIDE. COMPLIED WITH OPERATIONAL TEST OF PASSENGER DOOR PER AMM 52-11-00 WITH NO FAULTS FOUND.

Part: DOOR — JAMMED (CABIN) · airframe 21,066 hrs · 13,621 cycles

MAIN PASSENGER DOOR WOULD NOT OPEN, TOOK SEVERAL ATTEMPTS TO OPEN BEFORE DOOR WOULD OPEN. COMPLIED WITH INSPECTION OF PASSENGER DOOR AND DOOR FRAME NO DEFECTS NOTED. COMPLIED WITH FUNCTIONAL TEST OF PASSENGER DOOR, OPS CHECK GOOD. NO DEFECTS NOTED OK IAW AMM 52-11-00.

Part: SHAFT — LACK OF LUBE (PAX DOOR) · airframe 21,079 hrs · 13,631 cycles

F/A REPORTS PASSENGER DOOR VERY DIFFICULT TO OPEN. CYCLED PASSENGER DOOR SEVERAL TIMES, OPS TEST GOOD IAW AMM 52-11-00. APPLY LUBE TO PASSENGER DOOR INNER HANDLE SHAFT ASSY IAW AMM 12-20-52. ACFT OK FOR SERVICE.

Part: DOOR — STUCK (MAIN PAX) · airframe 21,015 hrs · 13,584 cycles

PASSENGER DOOR WILL NOT OPEN. PERFORMED OPS CHECK IAW AMM 52-11-00, NO DEFECTS NOTED. ACFT OK FOR SERVICE.

Part: DOOR — UNKNOWN · airframe 20,939 hrs · 13,527 cycles

CABIN DOOR VERY DIFFICULT TO OPEN AFTER FLIGHT. OPS CHECK OF THE CABIN DOOR CHECK GOOD AFTER SEVERAL CYCLES. NO FURTHER DEFECT NOTED AT THIS TIME. REF AMM 52-11-00.

Part: ICE BREAKER — BROKEN (PAX DOOR) · airframe 20,909 hrs · 13,515 cycles

MAIN PAX DOOR T-HANDLE OUTSIDE DIFFICULT TO OPEN EVERY NOW AND THEN. FOUND ICE BREAK BROKEN ON THE T-HANDLE. R & R ICE BREAKER. OPS CHECK TEST GOOD. REF AMM 52-11-15.

Part: MEGAPHONE — UNSERVICEABLE (CABIN) · airframe 20,895 hrs · 13,506 cycles

DMEGA PHONE INOPERATIVE. R & R MEGAPHONE IAW AMM 25-61-14, IPC 25-61-14, ITEM 5. ACFT OK FOR SERVICE.

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 20,758 hrs · 13,400 cycles

PAX DOOR DIFFICULT TO LATCH CLOSED AND EVEN MORE DIFFICULT TO UNLATCH OPEN. INSPECTED PAX DOOR; NO DEFECTS NOTED. LUBED ROLLERS AND OPS CHECKED DOOR IAW AMM 52-11-00.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 20,687 hrs · 13,350 cycles

F/A COULD NOT OPEN DOOR UPON PARKING, RAMPER COULD NOT OPEN FROM OUTSIDE, THE F/O FINALLY GOT IT WITH A LOT OF SHOULDER. F/A SAYS IT IS NOT FUNCTIONING PROPERLY. SPRAY LUBED AND OPS CHECKED IAW AMM 52-11-00. OPS CHECKED GOOD.

Part: LOCK — MALFUNCTIONED (PAX DOOR) · airframe 20,256 hrs · 13,041 cycles

F/A REPORTS DIFFICULTY OPERATING MAIN PAX DOOR. COMPLIED WITH INSP OF PAX DOOR LOCKING MECHANISM NO DEFECTS NOTED, C/W OPS CHECK OF PASSENGER DOOR CHECK GOOD, NO DEFECTS NOTED, OK IAW AMM 52-11-00.

Part: MEGAPHONE — UNKNOWN (CABIN) · airframe 19,802 hrs · 12,722 cycles

MEGAPHONE TO BE REPLACED TO C/W TC EO 700-25-0166. R & R MEGAPHONE IAW AMM 25-61-14.

Part: WEB — CORRODED (FUSELAGE) · airframe 27,541 hrs · 20,203 cycles

LEFT & RIGHT WEBS AT FS 280.00 CORRODED. R & R WEBS AT FS 280.00 WITH FABRICATED WEBS IAW REO 670-53-11-594 DATED 27 APRIL 2015.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 18,968 hrs · 12,130 cycles

F/A UNABLE TO OPEN PASSENGER DOOR F/O WAS ABLE TO ASSIST BY PUSHING ON TOP LATCH TO RELEASE. LUBRICATED PASSENGER DOOR IAW AMM 12-20-52. OPS CHECK GOOD. AIRCRAFT READY FOR SERVICE.

Part: LATCH — DIRTY (PAX DOOR) · airframe 18,564 hrs · 11,818 cycles

CABIN DOOR LATCH IS STICKING INTERMITTENTLY, F/A WAS UNABLE TO OPEN DOOR ON ARRIVAL. CLEANED LATCH AND LUBRICATED AND OPS CHECKED IAW AMM 52-11-00. OPS CHECKED GOOD.

Part: SMOKE DETECTOR — FALSE INDICATION (AFT LAVATORY) · airframe 18,111 hrs · 11,516 cycles

AFT LAV SMOKE WARNING MESSAGE IN FLT. COMPLIED WITH QRH, BREAKERS PULLED, FALSE FIRE WARNING DURING FLIGHT. PERFORMED OPS TEST OF THE AFT LAVATORY SMOKE DETECTOR IAW AMM 26-16-00. OPS CHECK GOOD, ACFT OK FOR SERVICE.

Part: FLOOR SUPPORT — CORRODED (BS 280-319) · airframe 17,173 hrs · 10,921 cycles

RIGHT CABIN FLOOR SUPPORT BETWEEN BS 280 & 319.70 WAS FOUND CORRODED AND NEW PART WAS MIS-DRILLED. RECEIVED REO678-53-21-684. COMPLIED WITH REO 690-53-21-684. RECEIVED & COMPLIED WITH EC/TC REO 690-53-21-684.

Part: STIFFENER — CRACKED (BS 280 BULKHEAD) · airframe 17,163 hrs · 10,912 cycles

BS 280 LOWER BULKHEAD WEB STIFFENER IS CRACKED AT LBL 38.50. R & R CRACKED STIFFNER WITH NEW STIFFNER IAW SRM 51-42-06-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 785) · airframe 17,167 hrs · 10,916 cycles

RT SIDE SEAT TRACK HAS CORROSION, FS 785.15. DAMAGED IS BEYOND ALLOWABLE LIMITS IAW SRM 53-41-49-101-001-A01. REMOVED THE SEAT TRACK IAW AMM 53-00-49-0000-801, CONFIG A07. FABRICATED NEW SEAT TRACK IAW SRM 51-40-11-001-001-A01 & REO 670-53-00-343. INSTALLED NEW SERVICEABLE SEAT TRACK IAW AMM 53-00-49-400-801-A07.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 17,173 hrs · 10,921 cycles

PASSENGER DOOR AFT DRAG ANGLE CRACKED. REPAIRED AFT DRAG ANGLE ON PAX DOOR IAW SRM 52-11-04-201-002-A01.

Part: SEAT TRACK — CORRODED (BS 661-692) · airframe 17,163 hrs · 10,912 cycles

LBL 9 SEAT TRACK SEGMENT BS 661+32-692.97 CORRODED SEVERAL AREAS. CORROSION IS BEYOND ALLOWABLE DAMAGE LIMITS IAW SRM 53-41-49-101-001-A01. REMOVED SEAT RAIL AT LBL 9 IAW AMM 53-00-49-000-801-A07. FABRICATED NEW SEAT TRACK IAW REO670-53-00-343, REV G 9/25/14. INSTALLED SERVICABLE SEAT TRACK IAW AMM 53-00-49-400-801, CONFIG A07.

Part: FRAME — CORRODED (BS 295) · airframe 17,173 hrs · 10,921 cycles

FRAME BS 295 CORRODED FWD & AFT SIDES BETWEEN STR'S 26LT-25RT. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. REPAIRED FRAME SECTION IAW REO 670-53-21-799 & 670-53-21-687.

Part: FLOOR SUPPORT — CORRODED (BS 280-319) · airframe 17,167 hrs · 10,916 cycles

RT CABIN FLOOR SUPPORT CORRODED BETWEEN BS 280 & 319.7. FOUND TO BE OUT OF LIMITS. R & R THE FLOOR SUPPORT IAW SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 661-692) · airframe 17,163 hrs · 10,912 cycles

RBL 9 SEAT TRACK SEGMENT BS 661+32-692.97 CORRODED SEVERAL AREAS. CORROSION IS BEYOND ALLOWABLE DAMAGE LIMITS IAW SRM 53-41-49-001-A01. REMOVED SEAT TRACK AT RBL 9 IAW AMM 53-00-49-000-801-A07. FABRICATED SEAT TRACK IAW REO670-53-00-343, REV G 9/25/14. INSTALLED SERVICABLE SEAT TRACK IAW AMM 53-00-49-400-801, CONFIG A07.

Part: SEAT TRACK — CORRODED (BS 374) · airframe 17,167 hrs · 10,916 cycles

LBL 9 SEAT TRACK SEGMENT CORRODED AT BS 374. REMOVED THE SEAT TRACK IAW AMM 53-00-49-000-801. FABRICATED A NEW SEAT TRACK IAW REO 670-53-00-343. INSTALLED THE SEAT TRACK IAW AMM 53-00-49-400-801-A07.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 17,167 hrs · 10,916 cycles

PAX DOOR UPPER CAP ANGLE CORRODED. R & R THE CAP ANGLE IAW SRM 51-40-11-001-001-A01, SRM 51-41-02-001-001-A01 & SRM 51-45-00-001-001-A01.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 17,167 hrs · 10,916 cycles

INTERCOSTAL CORRODED BETWEEN BS 349 & 364, STR 27RT. R & R INTERCOSTAL IAW SRM 51-42-06-001-001-A01.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 17,163 hrs · 10,912 cycles

COCKPIT FLOORBEAM CORRODED AT BS 280.00. FLOORBEAM ANGLE R & R IAW SB 670BA-53-041.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 17,163 hrs · 10,912 cycles

LEFT BS 280 FLOORBEAM CORRODED. FLOORBEAM R & R.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 17,167 hrs · 10,916 cycles

BULKHEAD WEB AT BS 280 IS CORRODED. REPAIRED IAW REO 670-53-11-594 AND GREO 670-53-11-594 REV. MAJOR REPAIR.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 17,167 hrs · 10,916 cycles

INTERCOSTAL CORRODED BETWEEN BS 349 & 364 AT STR 27L. R & R INTERCOSTAL IAW SRM 900 51-42-06-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 349-485) · airframe 17,163 hrs · 10,912 cycles

RBL9, SEAT TRACK SEQMENT 349.50-485.00 CORRODED SEVERAL AREAS. DAMAGE BEYOND ALLOWABLE LIMITS IAW SRM 53-21-49-101-001-A01. REMOVED SEAT TRACK RBL 9 IAW AMM 53-00-49-000-801-A07. FABRICATED NEW SEAT TRACK IAW GREO670-53-00-343, REV G 9/25/14. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801 A07.

Part: SEAT TRACK — CORRODED (BS 581-661) · airframe 17,163 hrs · 10,912 cycles

RBL 9 SEAT TRACK SEGMENT BS 581-661+32 CORRODED SEVERAL AREAS. BEYOND ALLOWABLE DAMAGE LIMITS IAW GREO670-53-00-013. REMOVED THE SEAT TRACK IAW AMM 53-00-49-000-801-A07. FABRICATED NEW SEAT TRACK IAW GREO670-53-00-343, REV G 9/25/14. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801 A07.

Part: RETAINER — DENTED (CARGO DOOR SEAL) · airframe 17,173 hrs · 10,921 cycles

CENTER BAGGAGE BAY DOOR LOWER SEAL RETAINER DENTED AT LOWER FWD CORNER. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. RECEIVED AND COMPLIED WITH EC/TC REO 690-52-35-013 FOR THE PERMENENT REPAIR IAW REO 690-52-35-013, REV A.

Part: STRINGER — CORRODED (BS 336) · airframe 17,173 hrs · 10,921 cycles

STRINGER 25R CORRODED AT BS 336. REMOVED AND INSTALLED NEW JOINT SPLICE IAW SRM 51-42-06-001-001-A01.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 17,163 hrs · 10,912 cycles

RIGHT BS 280 FLOORBEAM CORRODED. FLOORBEAM R & R .

Part: ANGLE — CORRODED (DOOR SILL) · airframe 17,167 hrs · 10,916 cycles

GALLEY SERVICE DOOR LOWER SILL ANGLE IS CORRODED. REMOVED THE DOOR SILL ANGLE IAW SRM 51-42-06-001-001-A01AND INSTALLED IAW SRM 51-42-06-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 681-661) · airframe 17,163 hrs · 10,912 cycles

LBL 9 SEAT TRACK SEGMENT 581-661+32 CORRODED SEVERAL AREAS. FOUND BEYOND ALLOWABLE DAMAGE LIMITS IAW GREO670-53-00-013. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801-A07. FABRICATED NEW SEAT TRACK IAW GREO670-53-00-343, REV G 9/25/14. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801 A07.

Part: SKIN — CORRODED (BS 280) · airframe 17,167 hrs · 10,916 cycles

CIRCUMFERENTIAL JOINT AT FS 280.00 INTERNAL SKIN CORRODED FROM STR 24LT-25RT. REMOVED CORROSION AT FS 280.00 BETWEEN STR 24LT AND 24RT IAW SRM 51-22-06-001-001-A01. RECEIVED AND COMPLIED WITH STS EA 32-2014-171. RECEIVED AND COMPLIED WITH ECTC EA 32-2014-161. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. INSTALLED FS 295 STRINGER CLEAT AT STRINGER 27 IAW REO 670-53-21-799 & 690-53-21-687. MAJOR REPAIR.

Part: DOUBLER — CORRODED (BS 295-310) · airframe 17,167 hrs · 10,916 cycles

TCAS DOUBLER INTERNAL SKIN CORRODED AT STR27 BETWEEN FRAMES 295-310. NO DAMAGE ALLOWED IAW SRM 53-21-01-101-02-A02. RECEVIED SERIVCEABLE TCAS DOUBLER FROM STORES. REMOVED UNSERVICABLE TCAS ANTENNA DOUBLER REF TO SRM 51-42-06-001-001-A01 AND 5-42-21-001-001-A01. R & R DOUBLER IAW SRM 900 51-42-06-001-001-A01.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 17,167 hrs · 10,916 cycles

BULKHEAD WEB AT BS 280 IS CORRODED. REPAIRED IAW REO 670-53-11-594 AND GREO 670-53-11-594 REV. MAJOR REPAIR.

Part: RETAINER — GOUGED (CARGO DOOR SEAL) · airframe 17,173 hrs · 10,921 cycles

CENTER BAGGAGE BAY DOOR LOWER SEAL RETAINER IS GOUGED AT LOWER AFT CORNER. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. RECEIVED AND COMPLIED WITH EC/TC REO 690-52-35-013 FOR THE PERMANENT REPAIR IAW REO 690-52-35-013, REV A.

Part: PANEL — DAMAGED (PAX DOOR) · airframe 16,409 hrs · 10,406 cycles

PAX DOOR AFT SIDE PANEL DAMAGED. CUT OUT DAMAGED AREA IAW EA 05-2014-002. INSTALLED REPAIR IAW EA 05-2014-002 REV F. MAJOR REPAIR IAW GMM 5-3.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 16,339 hrs · 10,351 cycles

EMERGENCY EXIT SIGN AFT 1ST CLASS WILL NOT ILLUMINATE. R & R 1 BATTERY PACK IN FWD AVIONIC BAY IAW AMM 33-51-17, IAPC 33-51-17, FIG 1, ITEM 8. OPS CHECK GOOD.

Part: DOOR — BINDING (MAIN PAX) · airframe 15,037 hrs · 9,496 cycles

AIR STAIR WOULD NOT OPEN, HAD TO FORCE THE DOOR DOWN.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 14,859 hrs · 9,383 cycles

NR 1 EMERGENCY FLOOD LIGHT, INOPERATIVE. REPLACED LAMP IAW AMM 33-51-09. OPS CHECKED GOOD.

Part: BATTERY PACK — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 12,092 hrs · 7,677 cycles

EMERGENCY LIGHTS POWER SUPPLY NR 4 WILL NOT HOLD A CHARGE. R & R EMERGENCY LIGHT POWER SUPPLY UNIT NR 4 IAW AMM 33-51-17.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 11,950 hrs · 7,577 cycles

AFT F/A FLASHLIGHT IS INOPERATIVE. INSTALLED NEW FLASHLIGHT TO AFT F/A STATION IAW AMM 25-61-01. OK FOR SERVICE.

Part: ECU — MALFUNCTIONED (TE FLAP) · airframe 9,982 hrs · 6,227 cycles

ON APPROACH INTO HOU RECEIVED FLAPS FAIL CAUTION MSG. EMERGENCY DECLARED, A/C LANDED SAFELY. RESET SFECU, OPS CHECK GOOD.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 3 · airframe 9,706 hrs · 6,046 cycles

FLOOR SILL FWD OF SERVICE DOOR CORRODED. REMOVED AND REPLACED RT SIDE SILL IAW CRJ SRM 51-42-00.

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 3 · airframe 9,706 hrs · 6,046 cycles

FS 280 CROSSBEAM CORRODED ALONG TOP SURFACE OF UPPER ANGLE. REMOVED AND REPLACED FS 280 FLOORBEAM IAW REO 690-53-11-092 AND SRM 51-42-00.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 9,706 hrs · 6,046 cycles

FUSELAGE LOWER SKIN SCRAPED 18" FORWARD OF AFT DRAIN MAST. CUT OUT DAMAGED SKIN AND INSTALLED A DOUBLER IAW BOMBARDIER REO 690-53-61-133.

Part: SPLICE — SHORTED (BLEED AIR SYS) · airframe 9,332 hrs · 5,791 cycles

EN ROUTE FROM MEM TO BWI RECEIVED ANTI-ICE DUCT MSG. MSG REMAINED ON FOR 45 MIN. EMERGENCY DECLARED, A/C DIVERTED TO CVG LANDED SAFELY. INSPECTED A/C FOUND LEFT WING CONNECTOR MT171P1 TO HAVE HIGHT RESISTANCE, CLEANED CONNECTOR. ALSO FOUND RIGHT WING SPLICE SP724 SHORTED. REMOVED AND REPLACED SPLICE SP724. OPS CHECK GOOD.

Part: DOOR — MALFUNCTIONED (EMERGENCY EXIT) · airframe 2,534 hrs · 1,632 cycles

LEFT FWD OVERWING EMERGENCY EXIT DOOR WILL NOT CLOSE. RESTOWED AND SECURED LEFT FWD OVERWING EMERGENCY EXIT DOOR. NO FURTHER DEFECTS NOTED, OPS CHECK GOOD.