N929XJ

Part: LATCH — INOPERATIVE (PSU) · airframe 35,014 hrs · 24,589 cycles

PAX O2 DEPLOYMENT SYSTEM FAILS OPS CHECK. THE MASKS AT THE FOLLOWING SEAT LOCATIONS FAILED TO DROP: 10DC, 14DC, 17BA, AND 20BA. TROUBLESHOT AND FOUND LATCHES TO BE BAD. REMOVED AND REPLACED PAX O2 MASK BOX LATCHES FOR SEATS 10DC, 14DC, 17BA, AND 20BA IAW CRJ-900 AMM 35-21-05-000/400-801-A01. PN OFF/ON- CDSP4633-5 PERFORMED OPS CHECK OF PAX O2 MANUAL DEPLOYMENT SYSTEM IAW CRJ-900 AMM TASK 35-20-00-710-803-A01. OPS CKS GOOD AT THIS TIME.

Part: DOOR FRAME — CRACKED (RT AFT EMER EXIT) · airframe 35,014 hrs · 24,589 cycles

RH AFT EMERGENCY EXIT FWD LUG IS CRACKED. REPAIRED IAW ENDEAVOR EA CRJ952-16335 REV IR DATED 4-9-2024.

Part: DOOR FRAME — CRACKED (RT FWD EMER EXIT) · airframe 35,014 hrs · 24,589 cycles

RH FWD EMERGENCY EXIT AFT LUG IS CRACKED. REPAIRED IAW ENDEAVOR EA CRJ952-16334 REV IR DATED 4-9-2024.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 27,535 hrs · 18,175 cycles

ON WAKE UP FOUND MASTER BATTERY SWITCH ON. EMER. LIGHTS WERE NOT COMING ON DUE TO LOW BATTERY CHARGE R/R MAIN BATTERY IAW CRJ900 JC 24-210-901. OPS TEST GOOD AT THIS TIME

Part: HINGE — DAMAGED (ACCESS DOOR) · airframe 27,300 hrs · 17,973 cycles

INITIAL INSPECTION: SPRING DAMAGED AT GROUND POWER ACCESS DOOR(122DR). (SM)(FUS). SUMMARY: HINGE AT GROUND POWER ACCESS DOOR WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01.

Part: INTERCOSTAL — CORRODED (BS 349-364) · corrosion level 2 · airframe 27,300 hrs · 17,973 cycles

INITIAL INSPECTION: CORROSION ON INTERCOSTAL 27(RH SIDE) AND 26R BTW. FS349 AND FS364 (FWD TO E/E DOOR) [IN REFERENCE TASK 900-53-140-300 APPENDIX A].(E/E)(TCI 100-09) SUMMARY:INTERCOSTAL 27RH AND 26RH BTW. FS349 AND FS364, WERE REPLACED PER CRJ900 SRM 51-42-21-001-001-A01 AND 51-42-06-001-001-A01. LEVEL CORROSION II. ADDITIONAL PART NUMBER INSTALLED SH670-32077-4

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 27,300 hrs · 17,973 cycles

INITIAL INSPECTION: CORROSION ON [INTERCOSTAL] 26L AND 27(LH SIDE) BTW. FS349 AND FS364 (FWD TO E/E DOOR) AT MAIN AVIONICS COMPARTMENT [IN REFERENCE TASK 900-53-140-300 APPENDIX A]. (E/E)(TCI 100-09) SUMMARY: CORROSION LEVEL 2.INTERCOSTAL 27(LH SIDE) AND 26LH BTW. FS349 AND FS364, WERE REPLACED PER CRJ900 SRM 51-42-21-001-001-A01 AND 51-42-06-001-001-A01.

Part: COAMING — CRACKED (RT NACELLE) · airframe 27,300 hrs · 17,973 cycles

INITIAL INSPECTION : CRACKED COAMING LATCH DOOR AND AFT CHANNEL ON LOWER HALF TRANSCOWL RH ENGINE ( MOT 2 ). SUMMARY: ON NRC. 00041, COAMING LATCH DOOR AND AFT CHANNEL ON LOWER HALF TRANSCOWL RH ENGINE WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-13-001-001-A01. ADDITIONAL PART NUMBER REPLACED: CN624-2048-201

Part: FRAME — CORRODED (BS 265) · airframe 27,300 hrs · 17,973 cycles

INITIAL INSPECTION: CORROSION ON FRAME FS=265 BTW STGR 26R / 26L AT INTERNAL STRUCTURE OF FWD FUSELAGE (SM) (TCI 100-06) SUMMARY: CORROSION ON FRAME FS=265 BTW STGR 26R / 26L AT INTERNAL STRUCTURE OF FWD FUSELAGE WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 AND WAS FOUND WITHIN LIMITS PER CRJ900 SRM 53-00-00-101-001-A01.

Part: HINGE FITTING — CORRODED (NLG DOOR) · airframe 27,300 hrs · 17,973 cycles

AWR HIDDEN DISCREPANCY: AFTER BUSHINGS REMOVAL CORROSION WAS FOUND ON LH/RH HINGE FITTING IN REF JC 900-32-710-902 STEP 5. (FYT) SUMMARY: ON NRC 00369 LH/RH FITTINGS OF NLG AFT DOOR WERE REPLACED FOR NEW ONES PER CRJ-900 SRM 51-42-21-001-001 A01.

Part: STRINGER — CORRODED (BS 280-333) · airframe 27,300 hrs · 17,973 cycles

INITIAL INSPECTION: CORROSION ON STRINGER 25R BTW. FS280 AND FS333 ALSO HYDRAULIC LINES STANDOFF (2E/A) AT MAIN AVIONICS COMPARTMENT [IN REFERENCE TASK 900-53-140-300 APPENDIX A] SUMMARY: ON NRC. 00167 CORROSION LEVEL 2, STRINGER 25R BTW. FS280 AND FS333 AND STANDOFF (2E/A) AT MAIN AVIONICS COMPARTMENT WERE REPLACED PER CEJ-900 SRM 51-42-06-001-001-A01.

Part: STRINGER — CORRODED (BS 319-349) · corrosion level 2 · airframe 27,300 hrs · 17,973 cycles

INITIAL INSPECTION: CORROSION ON STRINGER 25R BTW. FS319.70 AND FS349 AT MAIN AVIONICS COMPARTMENT [IN REFERENCE TASK 900-53-140-300 APPENDIX A].(E/E)(TCI 100-09). SUMMARY OF NRC; 00170: CORROSION LEVEL #2 ON STRINGER 25R BTW. FS319.70 AND FS349 AT MAIN AVIONICS COMPARTMENT, STRINGER 25R BTW. FS319.70 AND FS349 WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01.

Part: SUPPORT — CORRODED (BS 265-280) · airframe 27,300 hrs · 17,973 cycles

INITIAL INSPECTION: CORROSION ON JACK FITTING SUPPORT (2EAS) BTW FS=280 / FS=265 AND STGR 26R / 26L AT INTERNAL STRUCTURE OF FWD FUSELAGE (SM) (TCI 53-10-305). SUMMARY OF NRC: 00267 CORROSION ON JACK FITTING SUPPORT (2EAS) BTW FS=280 / FS=265 AND STGR 26R / 26L AT INTERNAL STRUCTURE OF FWD FUSELAGE. SUPPORT BTW FS. 280/FS. 265 AND STGR 26LH WAS CLEANED PER CRJ 900 SRM 51-26-00-001-001-A01 AND DAMAGE AS NOT FOUND. CORROSION LEVEL # 2 ON SUPPORT BTW FS=280 / FS=265 AND STGR 26 RH WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.

Part: STRINGER — CORRODED (BS 280-364) · airframe 27,300 hrs · 17,973 cycles

INITIAL INSPECTION: CORROSION ON STRINGER 26R BTW FS280 AND FS364 AT MAIN AVIONICS COMPARTMENT [IN REFERENCE TASK 900-53-140-300 APPENDIX A].(E/E)(TCI 100-09). SUMMARY: STRINGER 26R BTW FS280 AND FS364 AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.

Part: STRINGER — CORRODED (BS 333-349) · airframe 27,300 hrs · 17,973 cycles

INITIAL INSPECTION: CORROSION ON STRINGER 26L BTW FS333 AND FS349 AT MAIN AVIONICS COMPARTMENT [ IN REFERENCE TASK 900-53-140-300 APPENDIX A].(E/E)(TCI). SUMMARY: STRINGER 26LH FROM FS 333-364 AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01.

Part: FLOOR SUPPORT — CORRODED (BS 1000-1047) · corrosion level 2 · airframe 27,300 hrs · 17,973 cycles

INITIAL INSPECTION: CORROSION ON FLOOR BEAM 27LBL FROM FS1000 TO FS1047 AT AFT BAGGAGE BAY. (CCT) (TCI: 53-30-306). SUMMARY : DUE CORROSION LEVEL 2 ON FLOOR BEAM LBL27 STA FS 1000 TO FS 1047 AT AFT CARGO COMPARTMENT WAS REPAIRED PER CRJ/900 SRM 53-00-41-201-001-A03 PAR. 5.B. FIG.53-00-41-995-829.

Part: STRINGER — CORRODED (BS 280-310) · corrosion level 2 · airframe 27,300 hrs · 17,973 cycles

INITIAL INSPECTION: CORROSION ON STRINGER 27 BTW.FS280 AND FS310 AT MAIN AVIONICS COMPARTMENT [IN REFERENCE TASK 900-53-140-300 APPENDIX A].(E/E) (TCI 100-09). SUMMARY: ON NRC. 00160 CORROSION LEVEL 2, STRINGER 27 BTW.FS280 AND FS310 AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.

Part: STRIKER — WORN (CARGO DOOR) · airframe 27,300 hrs · 17,973 cycles

INITIAL INSPECTION: WEAR FWD STRIKER SEAL AT CENTER BAGGAGE BAY DOOR SURROUND STRUCTURE (C1) (SM). SUMMARY: FWD STRIKER SEAL AT CENTER BAGGAGE BAY DOOR SURROUND STRUCTURE NO DAMAGE ALLOWED PER CRJ-900 SRM 53-31-23-101-001-A02. DAMAGED FWD STRIKER SEAL AT CENTER BAGAGGE BAY DOOR SURROUND STRUCTURE (C1) WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-41-02-001-001-A01

Part: DOUBLER — CORRODED (ANTENNA) · airframe 27,300 hrs · 17,973 cycles

HIDDEN DAMAGE IN REF. JOBCARD 900-34-900-702. CORROSION ON DOUBLE IN SETTLEMENT AREA OF TRANSMIT ANTENNA 2 E19. (SM) (FUS). SUMMARY: DOUBLES (SPACER) WAS FABRICATED PER E/A CRJ 953-09832 REV IR. AND WAS INSTALLED PER CRJ 900 SRM 51-42-06-001-001-A01.

Part: FRAME — CORRODED (BS 295) · airframe 27,300 hrs · 17,973 cycles

INITIAL INSPECTION: CORROSION ON FRAME FS295 BTW. STGR.26L AND 26R AT MAIN AVIONICS COMPARTMENT [IN REFERENCE TASK 900-53-140-300 APPENDIX A].(E/E)(TCI 100-09). SUMMARY:ON NRC. 00163 CORROSION LEVEL 1 ON FRAME FS295 BTW. STGR.26L AND 26R AT MAIN AVIONICS COMPARTMENT WAS REMOVED PER CRJ-900 SRM 51-21- 06-001-001-A01 AND FOUND WITHIN LIMITS PER CRJ-900 SRM 53-00-06-201-005-A01.

Part: FLOOR SUPPORT — CORRODED (BS 310-349) · airframe 27,300 hrs · 17,973 cycles

AWR: CORROSION ON FLOOR SUPPORTS BTW FS310 TO FS349 AT PAX CABIN FLOOR STRUCTURE, PASSENGER DOOR LOWER SILL. (CPAX). SUMMARY OF NRC 00233: FLOOR SUPPORTS BTW FS310 TO FS349 AT PAX CABIN FLOOR STRUCTURE, PASSENGER DOOR LOWER SILL WERE REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01. AND SRM 51-41-02-001-001-A01. ADDITIONAL PART INSTALLED: SH670-31825-9

Part: STRINGER SPLICE — CORRODED (BS 333) · airframe 27,300 hrs · 17,973 cycles

INITIAL INSPECTION: CORROSION ON SPLICE STA FS333 OF STRINGERS (3 E/A) STGR. 26L, 26R, AND 25R AT MAIN AVIONICS COMPARTMENT[IN REFERENCE TASK 900-53-140-300 APPENDIX A].(E/E)(TCI 100-09). SUMMARY: SPLICE STA FS333 OF STRINGERS (3 E/A) STGR. 26L, 26R, AND 25R AT MAIN AVIONICS COMPARTMENT WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.

Part: FRAME — CORRODED (BS 319) · airframe 27,300 hrs · 17,973 cycles

INITIAL INSPECTION: CORROSION ON FRAME FS319.70 BTW STGR 26L AND 26R AT MAIN AVIONICS COMPARTMENT [IN REFERENCE TASK 900-53-140-300 APPENDIX A].(E/E)(TCI 100-09). SUMMARY OF NRC 00172: CORROSION LEVEL-1 ON FRAME FS319.70 BTW STGR 26L AND 26R AT MAIN AVIONICS COMPARTMENT WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 AND BLENDED AREAS WERE MEASURED AND DIMENSIONS AS FOLLOW: ORIGINAL THICKNESS IS 0.050'', MAXIMUM REMOVED MATERIAL IS ON FRAME WEB INNER SURFACE IS 0.003'' OF DEPTH (0.047'' MIN. REMAINING THICKNESS) AND MAXIMUM REMOVED MATERIAL IS ON LOWER FLANGE IS 0.004'' OF DEPTH (0.046'' MIN. REMAINING THICKNESS) THEREFORE FRAME IS WITHIN LIMITS PER CRJ900 SRM 53-00-06-201-005-A01.

Part: FRAME — CORRODED (BS 310) · airframe 27,300 hrs · 17,973 cycles

INITIAL INSPECTION: CORROSION ON FRAME FS310 BTW. STGR.26L AND 25R AT MAIN AVIONICS COMPARTMENT [IN REFERENCE TASK 900-53-140-300 APPENDIXA].(E/E)(TCI 100-09). CORROSION LEVEL 1 ON FRAME FS310 BTW. STGR.26L AND 25R AT MAIN AVIONICS COMPARTMENT WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01, THEREFORE IT IS WITHIN LIMITS PER CRJ-900 SRM 53-00-06-201-005-A01

Part: FRAME — CORRODED (BS 333) · airframe 27,300 hrs · 17,973 cycles

INITIAL INSPECTION: CORROSION ON FRAME FS333 BTW. STGR 26L AND 25R AT MAIN AVIONICS COMPARTMENT [IN REFERENCE TASK 900-53-140-300 APPENDIXA]. (E/E)(TCI 100-09). SUMMARY: CORROSION LEVEL 1 ON FRAME FS333 BTW. STGR 26L AND 25R AT MAIN AVIONICS COMPARTMENT WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01, THEREFORE IT IS WITHIN LIMITS PER CRJ-900 SRM 53-00-06-201-005-A01.

Part: SUPPORT ANGLE — CORRODED (BS 280) · airframe 27,300 hrs · 17,973 cycles

INITIAL INSPECTION: CORROSION ON FLOOR SETTLEMENT (141ALF) AT MAIN AVIONICS COMPARTMENT FS280 BTW. STGR 25L AND 25R.(E/E)(100-09). SUMMARY: DAMAGED ANGLE SUPPORT, CRAWLWAY FLOOR ON FS=280.00 BTW STGR 25L AND 25R AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 PAR. 6C AND SRM 51-42-20-001-001-A01. PAR 6A

Part: FRAME — CORRODED (BS 349) · airframe 27,300 hrs · 17,973 cycles

INITIAL INSPECTION: CORROSION ON FRAME FS349 BTW. STGR. 26L AND 25R AT MAIN AVIONICS COMPARTMENT [IN REFERENCE TASK 900-53-140-300 APPENDIX A].(E/E)(TCI 100-09). SUMMARY: ON NRC. 00175, CORROSION LEVEL 1, FRAME FS349 BTW. STGR. 26L AND 25R AT MAIN AVIONICS COMPARTMENT WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 AND FOUND WITHIN LIMITS PER CRJ-900 SRM 53-21-06-101-006-A02

Part: DOOR FRAME — CORRODED (SERVICE DOORWAY) · corrosion level 2 · airframe 27,300 hrs · 17,973 cycles

INITIAL INSPECTION: CORROSION ON MOUNTING ANGLE OF SERVICE DOOR SURROUND STRUCTURE LOWER SILL.(PTAS)(TCI 53-20-219). SUMMARY: ON NRC: 00218 CORROSION LEVEL 2, MOUNTING ANGLE OF SERVICE DOOR SURROUND STRUCTURE LOWER SILL WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01

Part: SCUFF PLATE — CORRODED (SERVICE DOOR) · corrosion level 2 · airframe 27,300 hrs · 17,973 cycles

INITIAL INSPECTION: CORROSION ON SCUFF PLATE SUPPORTS AND ANGLES AT GALLEY SERVICE DOOR LOWER SURROUND STRUCTURE. (PTAS)(TCI:53-20-219). SUMMARY: ON NRC. 00215 CORROSION LEVEL 2 SCUFF PLATE SUPPORTS AND ANGLES AT GALLEY SERVICE DOOR LOWER SURROUND STRUCTURE WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. ADDITIONAL PART INSTALLED: SH670-32040-1

Part: FLOOR SUPPORT — CORRODED (BS 565-581) · corrosion level 2 · airframe 27,300 hrs · 17,973 cycles

INITIAL INSPECTION: CORROSION ON FLOOR SUPPORT AT FUSELAGE STRUCTURE BTW FS 565 / FS 581 AND STGR 22L/23L (C1). SUMMARY OF NRC 00257 CORROSION LEVEL 2: FLOOR SUPPORT AT FUSELAGE STRUCTURE BTW FS 565 / FS 581 AND STGR 22L/23L WAS REPLACED PER CRJ 900 SRM 51-42-06-001-001-A01 PAR.6A AND 51-42-02-001-001-A01.

Part: FLOORBEAM — CORRODED (BS 280) · corrosion level 2 · airframe 27,300 hrs · 17,973 cycles

AWR HIDDEN DISCREPANCY: AFTER FLOOR PANEL SUPPORT ANGLE REMOVAL CORROSION WAS FOUND ON FLOOR BEAM STA 280 BTW BL0.00 AND RBL 11 AT PAX CABIN (W1) IN REF NRC S/N 00159. SUMMARY: ON NRC. 00263, CORROSION LEVEL 2, CROSSBEAM AT FS 280.00 BTW BL 0 TO RBL 42 WAS REPLACED PER CRJ/900 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01 AND 51-42-20-001-001-A01

Part: FLOORBEAM — CORRODED (BS 280) · corrosion level 2 · airframe 27,300 hrs · 17,973 cycles

AWR HIDDEN DISCREPANCY: AFTER FLOOR PANEL SUPPORT ANGLE REMOVAL CORROSION WAS FOUND ON FLOOR BEAM STA 280 BTW BL0.00 AND LBL 11 AT PAX CABIN (W1) IN REF NRC S/N 00159. SUMMARY: ON NRC. 00264 CORROSION LEVEL 2, CROSSBEAM AT FS 280.00 BTW BL 0 TO LBL 42 WAS REPLACED PER CRJ/900 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01 AND 51-42-20-001-001-A01

Part: INTERCOSTAL — CORRODED (BS 327-338) · airframe 27,300 hrs · 17,973 cycles

INITIAL INSPECTION: CORROSION ON INTERCOSTAL DD6 BTW FORMER FS 338.9 AND FRAME FS 327.7 INSIDE STRUCTURE AT PASSENGER DOOR. (PTAS)(TSI: 52-10-301). SUMMARY: INTERCOSTAL DD6 WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 PAR. 6. (C) AND SRM 51-42-21-001-001-A01 PAR. 6 (C).

Part: FLOORBEAM — CRACKED (BS 280) · airframe 27,300 hrs · 17,973 cycles

AWR HIDDEN DAMAGE: DURING REMOVAL FLOOR BEAM FS=280, ANGLE WAS FOUND CRACKED AT STA FS280 LBL26 PAX CABIN (CPAX) (IN REF. NRC 00264) SUMMARY: ON NRC. 00393, ANGLE AT STA FS280 LBL26 PAX CABIN WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-13-001-001-A01

Part: FLOORBEAM — CRACKED (BS 280) · airframe 27,300 hrs · 17,973 cycles

AWR HIDDEN DAMAGE: DURING REMOVAL FLOOR BEAM 280, ANGLE WAS FOUND CRACKED AT STA FS280 RBL26 PAX CABIN (CPAX) (IN REF. NRC 00263) SUMMARY: ON NRC. 00392, ANGLE AT STA FS280 RBL26 PAX CABIN WAS REPLACED PER CRJ-900 SRM 51-42-06-001 AND SRM 51-42-13-001-001-A01

Part: STRAP — CORRODED (ACCESS PANEL) · airframe 27,300 hrs · 17,973 cycles

INITIAL INSPECTION: CORROSION ON SETTLEMENT AREA AT PANEL ACCESS 193AB AND 195AB (SM). SUMMARY: ON NRC. 00110, ON SETTLEMENT AREA AT PANEL ACCESS 193AB AND 195AB, STRAPS WERE REPLACED PER CRJ-900 SRM 51-42-10-001-001-A01 PAR. 8

Part: STRUCTURE — DENTED (PAX DOOR) · airframe 27,300 hrs · 17,973 cycles

INITIAL INSPECTION: DENT ON FWD/AFT UPPER CORNER AT PASSENGER DOOR. (PTAS). SUMMARY OF NRC 00132: FWD/AFT UPPER CORNER AT PASSENGER DOOR WERE REPLACED PER CRJ-900 S.R.M. 51-42-13-001-001-A01. ADDITIONAL PART REPLACED 600-31902-287.

Part: CANISTER — CRACKED (LT FUEL TANK) · airframe 27,300 hrs · 17,973 cycles

INITIAL INSPECTION: CRACK IN CANISTER, WELDED NO.3 IN STA. WS148 AT LH MAIN FUEL TANK. (AI) SUMMARY: ON NRC. 00303 CANISTER, WELDED NO.3 IN STA. WS148 AT LH MAIN FUEL TANK WAS REPAIRED PER CRJ-900 REO 670-57-42-577 REV.

Part: STRINGER SPLICE — CORRODED (BS 333) · corrosion level 2 · airframe 27,300 hrs · 17,973 cycles

INITIAL INSPECTION: CORROSION ON STGR SPLICE 22 RH AND FS=333 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT (SM) (TCI 53-20-319). SUMMARY: ON NRC. 00289 CORROSION LEVEL 2, STGR SPLICE 22 RH AND FS=333 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-20-001-001-A01

Part: FASTENER — CORRODED (BS 669-677) · airframe 27,300 hrs · 17,973 cycles

INITIAL INSPECTION: CORROSION ON FASTENERS (2E/A) BTW FS669.40 AND FS677 STGR.25R AT FUSELAGE SKIN.(FUS) SUMMARY: ON NRC. 00119 FASTENERS (2E/A) BTW FS669.40 AND FS677 STGR. 25R AT FUSELAGE SKIN WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01

Part: FLOORBEAM — CORRODED (BS 280) · corrosion level 2 · airframe 27,300 hrs · 17,973 cycles

INITIAL INSPECTION: CORROSION ON FLOOR PANEL SUPPORT ANGLE OF ACCESS PANEL 221ALF IN STA. FS= 280 BETWEEN 11 LBL/RBL AT COCKPIT. (CPIL) TCI 53-10-219. SUMMARY: ON NRC. 00159 CORROSION LEVEL 2, FLOOR PANEL SUPPORT ANGLE OF ACCESS PANEL 221ALF IN STA. FS= 280 WAS REPLACE PER CRJ-900 SRM 51-42-06-001-001-A01

Part: STRINGER — CORRODED (BS 280-349) · airframe 27,300 hrs · 17,973 cycles

INITIAL INSPECTION: CORROSION ON STGR 22 RH BTW FS=280 / FS=349 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT (SM) (TCI 53-20-319). SUMMARY: ON NRC. 00288, CORROSION LEVEL 2, STGR 22 RH BTW FS=280 / FS=349 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND 51-42-20-001-001-A01.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 27,300 hrs · 17,973 cycles

AWR: CORROSION ON RH FLOOR SILL BTW FS349 TO FS379 AT PAX CABIN FLOOR STRUCTURE. (CPAX). SUMMARY: RH FLOOR SILL BTW FS349 TO FS379 AT PAX CABIN FLOOR STRUCTURE WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-10-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 744-977) · corrosion level 2 · airframe 27,300 hrs · 17,973 cycles

INITIAL INSPECTION: CORROSION ON SIDE SEAT RAILS IN SECTIONS [FS744.15 TO FS761.85,STGR 15LH] [FS785.15 TO FS847+16 STGR 15LH ] [ FS847+16 TO FS904, STGR 15LH] [FS904 TO FS977, STGR 15LH ] [FS744.15 TO FS761.85, STGR 15RH] [FS785.15 TO FS847+16 STGR 15RH] [FS847+16 TO FS865, STGR 15RH] [FS865 TO FS977, STGR 15RH] AT PAX CABIN. (CPAX) (TCI: 53-20-233). SUMMARY OF NRC:00149 CORROSION LEVEL # 2 ON SIDE SEAT RAILS IN SECTIONS [FS744.15 TO FS761.85,STGR 15LH] [FS785.15 TO FS847+16 STGR 15LH ] [FS847+16 TO FS904, STGR 15LH] [FS904 TO FS977, STGR 15LH ] [FS744.15 TO FS761.85, STGR 15RH] [FS785.15 TO FS847+16 STGR 15RH] [FS847+16 TO FS865, STGR 15RH] [FS865 TO FS977, STGR 15RH] WERE REPLACED PER CRJ-900 AMM 53-00-49-400-801 (CONFIG.7) AND SRM 51-41-02-001-001-A01.

Part: FRAME — CORRODED (BS 501) · airframe 27,300 hrs · 17,973 cycles

INITIAL INSPECTION: CORROSION ON FRAME FS= 501.00 BTW STGR 27/24LH AT INTERNAL STRUCTURE OF FWD CARGO COMPARTMENT (C1) (SM) (TCI 53-20-333). SUMMARY:CORROSION ON FRAME FS= 501.00 BTW STGR 27/24LH AT INTERNAL STUCTURE OF FWD CARGO COMPARTMENT (C1) WAS REMOVED PER CRJ-900 SRM 51-2 -06-001-001-A01 AND AREA WAS MEASURED WITH THE FOLLOWING PARAMETERS: ORIGINAL THICKNESS 1) 0.050"",REMAINING THICKNESS 0.045"",DEPTH 0.005"" AD ORIGINAL THICKNESS 2)0.071"",REMAINING THICKNESS 0.064"",DEPTH 0.007"", THEREFORE IT´S WITHIN LIMITS PER CRJ-900 SRM 53-31-06-101-003-A04.

Part: SEAT TRACK — CORRODED (BS 581-693) · corrosion level 2 · airframe 27,300 hrs · 17,973 cycles

INITIAL INSPECTION: CORROSION ON FLOOR SEAT RAIL FROM [FS581 TO FS661+32] [FS661+32 TO FS693.00] , LBL 9 AND RBL 9 AT PAX CABIN. (CPAX).( TCI 53-20-245 ). SUMMARY OF NRC:00155 CORROSION LEVEL # 2 ON SEAT RAILS IN SECTIONS [FS581 TO FS661+32] [FS661+32 TO FS693.00] , LBL 9 AND RBL 9 WERE REPLACED PER CRJ-900 AMM 53-00-49-400-801 (CONFIG.A07) AND SRM 51-41-02-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 581-669) · corrosion level 2 · airframe 27,300 hrs · 17,973 cycles

INITIAL INSPECTION: CORROSION ON SIDE SEAT RAIL FROM [FS581 TO FS661+16] [FS661+16 TO FS669.40] , AT STGR 15L AND STGR 15R AT PAX CABIN. (CPAX).( TCI 53-20-217) SUMMARY OF NRC:00156 CORROSION LEVEL # 2 ON SIDE SEAT RAILS ON SECTIONS [FS581 TO FS661+16] [FS661+16 TO FS669.40] , AT STGR 15LH AND STGR 15RH WERE REPLACED PER CRJ-900 AMM 53-00-49-400-801 (CONFIG.A07) AND SR M 51-41-02-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 693-977) · corrosion level 2 · airframe 27,300 hrs · 17,973 cycles

INITIAL INSPECTION: CORROSION ON FLOOR SEAT RAIL FROM [FS693 TO FS838] [FS838 TO FS847+62][FS847+62 TO FS977], LBL 9 AND RBL 9 AT PAX CABIN. (CPAX). SUMMARY OF NRC 00150, CORROSION LEVEL-2: FLOOR SEAT RAIL FROM [FS693 TO FS838] [FS838 TO FS847+62][FS847+62 TO FS977], LBL 9 AND RBL 9 AT PAX CABIN WERE REPLACED PER CRJ-900 AMM 53-00-49-400-801 (CONFIG.7) PAR. 4B AND SRM 51-41-02-001-001-A01.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 24,860 hrs · 16,167 cycles

FWD FA FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED THE FLASHLIGHT IAW AMM 25-61-02.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 24,502 hrs · 15,898 cycles

EMERGENCY EXIT SIGN FLOOR LEVEL HAS MORE THAN 50% OF LIGHTS INOP NEEDS TO BE RELAMPED. RELAMPED EMERGENCY EXIT SIGN LIGHT BULBS IAW AMM 33-51-11. OPS CHECK GOOD.

Part: PBE — FAILED (MAIN CABIN) · airframe 24,338 hrs · 15,769 cycles

AFT CABIN PBE LOST FIRMNESS. REMOVED AND REPLACED THE PBE IAW EE-900.

Part: MEGAPHONE — INOPERATIVE (MAIN CABIN) · airframe 24,338 hrs · 15,769 cycles

VOLUME CONTROL DOES NOT WORK ON THE MEGAPHONE. REMOVED AND REPLACED THE MEGAPHONE IAW JC EE-900. OPS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 24,224 hrs · 15,682 cycles

FWD FA GALLEY FLASHLIGHT INOP . REMOVED AND REPLACED GALLEY FLASH LIGHT IAW AMM 25-61-05, OPS CHECK GOOD. TIFIED.

Part: EXTINGUISHER — LOW PRESSURE (COCKPIT) · airframe 22,838 hrs · 14,730 cycles

COCKPIT FIRE EXTINGUISHER LOW. INSTALLED A NEW FIRE EXTINGUISHER IN THE COCKPIT IAW AMM 26-23-01. ACFT OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (FWD FLASHLIGHT) · airframe 22,702 hrs · 14,637 cycles

FWD FA FLASHLIGHT NOT BLINKING. REMOVED AND REPLACED THE FLASHLIGHT BATTERY IAW CMM 25-60-02, OPS CHECKED GOOD.

Part: SEAL — BROKEN (PBE) · airframe 22,702 hrs · 14,637 cycles

AFT PBE SEAL BROKEN. INSTALLED A NEW SEAL IAW AMM 20-00-00. CHECKED GOOD.

Part: SEAL — BROKEN (FLASHLIGHT) · airframe 22,577 hrs · 14,554 cycles

FORWARD FA FLASHLIGHT SEAL BROKEN. REMOVED AND REPLACED FWD FA FLASHLIGHT SEAL IAW AMM 25-60-02.

Part: ACM — MALFUNCTIONED (AC BAY) · airframe 22,577 hrs · 14,554 cycles

LEFT PACK INOP. DEFERRED LEFT PACK IAW MEL 21-51-16. R&R LT AIR CYCLE MACHINE IAW AMM 21-51-08. OPS CHECK GOOD AT THIS TIME MM02 UPDATED. PLACARD REMOVED.

Part: OXYGEN BOTTLE — EMPTY (CABIN) · airframe 22,360 hrs · 14,390 cycles

FA REPORTED FWD CABIN PORTABLE O2 BOTTLE AT 0. REPLACED FWD CABIN O2 BOTTLE IAW MM 35-31-01-400-801-A05. ALSO REF TS000755-2013. VERIFIED PRESS FULL.

Part: SEAT TRACK — CORRODED (BS 881-977) · airframe 22,196 hrs · 14,264 cycles

RIGHT AISLE SEAT TRACK HAS CORROSION BETWEEN BS 881 & 977, IN THE PAX CABIN. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49.

Part: SEAT TRACK — CORRODED (BS 847-881) · airframe 22,196 hrs · 14,264 cycles

RIGHT AISLE SEAT TRACK HAS CORRODED AND IS GOUGED BETWEEN BS 847 & 881, IN THE PAX CABIN. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49.

Part: SEAT TRACK — CORRODED (BS 881-977) · airframe 22,196 hrs · 14,264 cycles

LEFT AISLE SEAT TRACK HAS CORROSION BETWEEN BS 881 - 977, IN CABIN. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49, AND REO 670-53-00-343.

Part: SEAT TRACK — CORRODED (BS 847-881) · airframe 22,196 hrs · 14,264 cycles

LEFT AISLE SEAT TRACK HAS CORROSION BETWEEN BS 847 - 881, IN THE PAX CABIN. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49, AND REO 670-53-00-343.

Part: PANEL — CHAFED (LT WING) · airframe 22,196 hrs · 14,264 cycles

PANEL 584EB HAS AREA OF CHAFING. LOCATED AND DRILLED A NEW PANEL IAW SRM 51-40-11. INSTALLATION THE NEW PANEL.

Part: PANEL — CORRODED (RT WING) · airframe 22,196 hrs · 14,264 cycles

PANEL 622DB CHAFED ON LEADING EDGE. LOCATED AND DRILLED A NEW PANEL IAW SRM 51-40-11. INSTALLED THE NEW PANEL.

Part: ANGLE — CORRODED (BS 280 FLOORBEAM) · airframe 22,196 hrs · 14,264 cycles

BS 280 FLOORBEAM ANGLE BETWEEN LBL 9 AND RBL 9 HAS CORROSION. REMOVED AND REPLACED THE FLOORBEAM ANGLE IAW SRM 51-40-11, 51-21-11, 51-25-16, 51-42-21, AND 51-42-06.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 21,803 hrs · 13,992 cycles

AFT EMERGENCY LIGHTS INOPERATIVE. R & R AFT EMERGENCY BATTERY PACK IAW AMM 33-51-17. OPS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 21,795 hrs · 13,986 cycles

CAPTAIN`S FLASHLIGHT IS INOPERATIVE. R & R THE FLASHLIGHT & HOLDER ASSY IAW AMM 25-61-02.

Part: OXYGEN MASK — NO TEST (COCKPIT) · airframe 21,068 hrs · 13,476 cycles

OBSERVER OXYGEN MASK FAILED FFOD TEST, TEST & RESET VALVE REMAINS OPEN. REPLACED THE OXYGEN MASK IAW AMM 35-11-12. OPS AND LEAK CHECKED PASSED.

Part: PRINTER — OVERHEATED (COCKPIT) · airframe 20,180 hrs · 12,859 cycles

NOTICED A BURNING ODOR IN THE COCKPIT. AFTER INVESTIGATION FOUND ACARS PRINTER VERY HOT TO TOUCH. OPENED PRINTER AND FOUND SMOKE COMING OUT. FOUND PRINTER PAPER WITH HOLES BURNED THROUGH AND APPEARED CLOSE TO CATCHING FIRE CB PN CBP2-A13 OPENED TO REMOVE POWER TO PRINTER. REMOVED AND REPLACED ACARS PRINTER IAW AMM 23-22-05. OPS CHECKED GOOD.

Part: LIGHT — MISSING (CABIN) · airframe 19,946 hrs · 12,692 cycles

ROW 13C EMERGENCY LIGHT STRIP MISSING. REPLACED THE EMERGENCY LIGHT STRIP IAW AMM 33-51-01

Part: STOWAGE BOX — LOOSE (COCKPIT) · airframe 19,659 hrs · 12,482 cycles

FIRST OFFICERS LIFE VEST METAL BOX HAS COME LOOSE & ROTATED 90 DEGREES, MAKING IT IMPOSSIBLE TO RETRIEVE LIFE VEST. SECURED METAL BOX IAW AMM 25-11-01. OK FOR SERVICE.

Part: ATTACH ANGLE — CORRODED (BS 319) · airframe 19,608 hrs · 12,449 cycles

ANGLE IS CORRODED ATTACHING TO FRAME BS 319 & STRINGER 21R. R & R FRAME ATTACH ANGLE IAW SRM 51-40-11-001-001-A01 & 51-42-06-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 813) · airframe 19,608 hrs · 12,449 cycles

LEFT SIDE SEAT TRACK BS 813.7 IS CORRODED. R & R LT SIDE SEAT TRACK IAW AMM 53-00-49-000 400-801-A07.

Part: DOOR SILL — CORRODED (BS 1000-1047) · airframe 19,608 hrs · 12,449 cycles

AFT CARGO DOOR SILL IS CORRODED AROUND FASTENER HOLES, BETWEEN BS 1000 - 1047 & IS CHAFED FROM STEP PLATE. R & R CARGO DOOR SILL IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 & 51-42-13-001-001-A01.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 19,608 hrs · 12,449 cycles

SERVICE DOOR SILL IS CORRODED AT MULTIPLE LOCATIONS ON LOWER ANGLE & PROTECTOR PLATE BRACKET. CONTINUATION CARD 81519111 OP 16 REMOVED 2 FITTINGS & REINSTALLED IAW SRM 51-42-02-001-001-A01. REMOVED FOUR WEB FLOOR PROTECTORS & REINSTALLED IAW SRM 51-42-21-001-001-A01. R & R LOWER SILL ANGLE IAW SRM 51-42-06-001-001-A01.

Part: PANEL — CRACKED (ZONE 400) · airframe 19,608 hrs · 12,449 cycles

PANEL 433BT HAS SEVERAL CRACKS RADIATING FROM MID-MOUNTING HOLE. REPAIRED PANEL 433BT IAW EA CRJ954-04390.

Part: STRINGER — CORRODED (BS 1051-1088) · airframe 19,608 hrs · 12,449 cycles

STRINGER 26L, BETWEEN FS 1051 & 1088 HAS CORROSION AROUND RIVETS. REPAIRED THE STRINGER IAW EA CRJ953-04410.

Part: DOUBLER — CORRODED (BS 349) · airframe 19,608 hrs · 12,449 cycles

FRAME DOUBLER ARE CORRODED AT BS 349, WL 72.5. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01 & 53-21-23-101-001-A02.

Part: FLOOR SUPPORT — CORRODED (BS 280-319) · airframe 19,608 hrs · 12,449 cycles

RIGHT FLOOR SILL IS CORRODED FROM FS 280 - 319. CONTINUATION CARD 81519111 OP 100. R & R FLOOR SILL IAW SRM 51-42-06-001-001-A01 & SRM 51-42-13-001-001-A01.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 19,608 hrs · 12,449 cycles

RIGHT FLOOR SILL FS 349 - 364 IS CORRODED. REPAIRED RT FLOOR SILL FS 349 - 364 IAW EA CRJ953-04405.

Part: SEAT TRACK — CORRODED (BS 572-661) · airframe 19,608 hrs · 12,449 cycles

RIGHT SIDE SEAT TRACK BETWEEN BS 572 - 661+16, IS CORRODED AT MULTIPLE LOCATIONS. SEAT TRACK FABRICATED IAW GREO 670-53-00-343 & AMM 53-00-49-000 400-801-107.

Part: ANGLE — CORRODED (BS 280) · airframe 19,608 hrs · 12,449 cycles

FS 280 FLIGHT DECK ENTRANCE WAY, LOWER ANGLES ARE CORRODED. REPLACED ANGLES IAW SRM 51-42-13-001-001-A01. REPAIRED CORROSION ON RT WEB IAW EA CRJ953-044416. PN CC670-34191-1/-2 & CC670-34142-1.

Part: STRUCTURE — CRACKED (POWER RECEPTICAL) · airframe 19,608 hrs · 12,449 cycles

AC POWER RECEPTACLE STRUCTURE CRACKED. CONTINUATION CARD 81519115 OP 142. REMOVED CRACKED BRACKET & INSTALLED NEW PN CC670-33401-3 IAW SRM 51-42-06-001-001-A01. "

Part: FLOORBEAM — CORRODED (BS 280) · airframe 19,608 hrs · 12,449 cycles

BS 280 FLOORBEAM IS CORRODED AROUND FLOORBOARD SCREW HOLE. THE FLOORBEAM WAS R & R IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-13-001-001-A01 & 51-42-22-001-001-A01.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 19,608 hrs · 12,449 cycles

LEFT FS 280 WEB CORRODED AT FLIGHT DECK ENTRANCE. REPAIRED LT FS 280 WEB IAW REO 670-53-11-594 REV A DATED 6 26 15.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 19,608 hrs · 12,449 cycles

RIGHT FS 280 LOWER WEB IS CORRODED. REPAIRED RT FS 280 WEB IAW REO 670-53-11-594 REV A DATED 6 26 15.

Part: ANGLE — CORRODED (BS 280) · airframe 19,608 hrs · 12,449 cycles

BS 280 FWD J ANGLE IS CORRODED. REMOVED & REINSTALLED LT & RT CORNER BRACES IAW SRM 51-42-21-001-001-A01. R & R FWD J ANGLE IAW SRM 51-42-06-001-001-A01.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 19,608 hrs · 12,449 cycles

LEFT FS 280 CROSSBEAM IS CORRODED AT LBL 9 & AROUND CORROSION CUP FASTENER. LT FS 280.00 CROSSBEAM, PN CC670-34094-1 WAS R & R IAW SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01 & 51-42-22-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 661-693) · airframe 19,608 hrs · 12,449 cycles

SEAT TRACK BS 661 - 693 ON LBL 9 IS CORRODED. INSTALLED A NEW SEAT TRACK IAW AMM 53-00-49-400-801-A07.

Part: SEAT TRACK — CORRODED (BS 847-865) · airframe 19,608 hrs · 12,449 cycles

RIGHT SIDE SEAT TRACK BETWEEN BS 847+16 - 865, HAS LIGHT CORROSION AT SEVERAL LOCATIONS. THE TRACK WAS REPLACED IAW REO 670-53-00-343 REV M & AMM 53-00-49-400-801-A07.

Part: SEAT TRACK — CORRODED (BS 744-761) · airframe 19,608 hrs · 12,449 cycles

RIGHT SIDE SEAT TRACK BETWEEN BS 744.15 - 761.85 HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-80 1-A07, 53-00-49-400-801-A07, SRM 51-40-11-001-001-A01 & REO 670-53-00-343 REV M.

Part: SEAT TRACK — CORRODED (BS 661-693) · airframe 19,608 hrs · 12,449 cycles

SEAT TRACK RBL 9, BS 661 - 693 IS CORRODED. REPAIRED IAW AMM 53 -00-49-400-801-A07, SRM 51-40-11-001-001-A01 & REO 670-53-00-343 REV M.

Part: SEAT TRACK — CORRODED (BS 661-669) · airframe 19,608 hrs · 12,449 cycles

LEFT SIDE SEAT TRACK BETWEEN BS 661+16 - 669.9, IS CORRODED. THE SEAT TRACK WAS REPLACED WITH NEW SEGMENT. FABRICATED & INSTALLED IAW GREO 670-53-00-343 & AMM 53-00-49-000-400-801-A07.

Part: SEAT TRACK — CORRODED (BS 669-720) · airframe 19,608 hrs · 12,449 cycles

LEFT SIDE SEAT TRACK BETWEEN BS 669.4 - 720.85 HAS AREAS OF CORROSION. THE SEAT TRACK WAS REPAIRED IAW REO 670-53-00-343 & AMM 53-00-49-400-801-A07.

Part: SEAT TRACK — CORRODED (BS 581-661) · airframe 19,608 hrs · 12,449 cycles

SEAT TRACK ON LBL 9 IS CORRODED, FS 581 - 661. LOCATED, DRILLED & INSTALLED NEW SEAT TRACK, IAW REO 670-53-00-343 & AMM 53-00-49-400-801 A07.

Part: SEAT TRACK — CORRODED (BS 477-597) · airframe 19,608 hrs · 12,449 cycles

SEAL TRACK LBL 27, BS 477 - 597 IS CORRODED. THE SEAT TRACK WAS REPLACED IAW AMM 53-00-49- 400-801-A07 & REO 670-53-00-343.

Part: SEAT TRACK — CORRODED (BS 669-720) · airframe 19,608 hrs · 12,449 cycles

RIGHT SIDE SEAT TRACK BETWEEN FS 669.4 - 720.85, HAS MULTIPLE AREAS OF CORROSION. SEAT TRACK WAS REPLACED IAW REO 670-53-00-343 REV M & AMM 53-00-49-400-801-A07.

Part: SEAT TRACK — CORRODED (BS 581-661) · airframe 19,608 hrs · 12,449 cycles

SEAT TRACK ON RBL 9, FS 581 - 661 IS CORRODED. LOCATED, DRILLED & INSTALLED NEW SEAT TRACK, PN N126-2075 IAW REO 670-53-00-343 & AMM 53-00-49-400-801 A07.

Part: DOOR SILL — CORRODED · airframe 19,608 hrs · 12,449 cycles

PASSENGER DOOR LOWER SILL IS CORRODED. REPLACED ANGLE IAW SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01 & 51-42-21-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 744-761) · airframe 19,608 hrs · 12,449 cycles

LEFT SIDE SEAT TRACK BETWEEN BS 744.15 - 761.85 IS CORRODED. REMOVED AND REPLACED THE SEAT TRACK, IAW AMM 53-00-49-000-801-A07, 53-00-49-400-801-A07, SRM 51-40-11-001-001-A01 & REO 670-53-00-343 REV M.

Part: SEAT TRACK — CORRODED (BS 349-501) · airframe 19,608 hrs · 12,449 cycles

SEAT TRACK RBL 9, BS 349 - 501 IS CORRODED. R & R SEAT TRACK, IAW AMM 53-00-49-000-801 & 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 661-669) · airframe 19,608 hrs · 12,449 cycles

RIGHT SIDE SEAT TRACK BETWEEN FS 661+16 - 669.4, CORRODED. REMOVED CORROSION IAW REO 670-53-00-013.

Part: SEAT TRACK — CORRODED (BS 501-581) · airframe 19,608 hrs · 12,449 cycles

SEAT TRACK ON RBL 9, FS 501 - 581 IS CORRODED. REMOVED SEAT TRACK ON RBL 9, FS 501 - 581 & REPLACED IT WITH NEW SERVICEABLE SEAT TRACK IAW AMM 53-00-49-000-801 & 53-00-49-400-801.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 19,608 hrs · 12,449 cycles

CORROSION FOUND ON STRINGER 27 RT INTERCOSTAL, JUST FWD OF FS 364.00. R & R INTERCOSTAL FROM FS 349 - 364, RT OF STRINGER 27 IAW SRM 51-42-06-001-001-A01 & SRM 51-42-21-001-001-A01. LOCATED & DRILLED NEW PART IAW SRM 51-40-11-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 485-572) · airframe 19,608 hrs · 12,449 cycles

LEFT SIDE SEAT TRACK BETWEEN BS 485 - 572, HAS CORROSION AT MULTIPLE LOCATIONS. R & R THE SEAT TRACK IAW AMM 53-00-49-000-801 CONFIG A07 & 53-00-49-400-801 CONFIG A07.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 19,608 hrs · 12,449 cycles

CORROSION FOUND ON STRINGER 26R INTERCOSTAL, JUST FWD OF FS 364.00. REMOVED INTERCOSTAL AT STRINGER 26R, BETWEEN FS 349 - 364 & REPLACED IAW SRM 51-42-21-001-001-A01.

Part: SKIN — DAMAGED (LT WING AILERON) · airframe 19,608 hrs · 12,449 cycles

LT WING, INBD LE AILERON PANEL HAS CHAFE DAMAGE, APPROX 1"" X 3"" & 0.015"" DEEP. ADJACENT TO FASTENER HOLE. DRILLED & LOCATED HOLES FOR NEW PANEL 599AB IAW SRM 51-40-11-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 572-661) · airframe 19,608 hrs · 12,449 cycles

LEFT SIDE SEAT TRACK BETWEEN FS 572 - 661+16 IS CORRODED AT MULTIPLE LOCATIONS. R & R THE SEAT TRACK IAW AMM 53-00-49-000-801 CONFIG A07 & 53-00-49-400-801CONFIG A07.

Part: SEAT TRACK — CORRODED (BS 785-847) · airframe 19,608 hrs · 12,449 cycles

RIGHT SIDE SEAT TRACK BETWEEN BS 785 - 847+16 IS CORRODED AT MULTIPLE LOCATIONS. INSTALLED A NEW SEAT TRAC IAW AMM 53-00-49-400-801-A07.

Part: LIGHT — OUT OF POSITION (CABIN) · airframe 19,153 hrs · 12,170 cycles

FLOOR TRACK LIGHTING AT SEAT 18 - 20 ON RT SIDE NOT PROPERLY INSTALLED. REPOSITIONED EMER TRACK FLOOR MOUNTED LIGHT NORMAL POSITION & CHECKED GOOD IAW AMM 33-51-01.

Part: OVEN — DEFECTIVE (GALLEY) · airframe 18,875 hrs · 11,996 cycles

SMOKE FWD LAVATORY WENT OFF AT FL 370. SUSPECT FROM OVEN. NO SIGN OF SMOKE. REMOVED ALL OLD PAPER & DEBRIS FROM BEHIND THE OVEN. DUPLICATED FAULT WITH OVEN IN HIGH & WARMED UP, OPENED DOOR & RECEIVED MSG. REPLACED THE OVEN ASSEMBLY & ALL THE COOKING SHELVES IAW AMM 25-32-01. ALL CHECKED NORMAL, DURING OVEN OPERATION RECEIVED NO CAUTIONS FOR SMOKE.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 18,591 hrs · 11,827 cycles

GLOW STRIP MISSING IN EXIT ROW 12B. REPLACED MISSING STRIP IAW AMM 33-51-01. OK FOR SERVICE.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 17,532 hrs · 11,100 cycles

DURING DETAILED LIGHTNING STRIKE FOUND MELTED SPOT ON TE OF RT ELEVATOR. PERFORMED NON-FLUSH REPAIR OF RT ELEVATOR TE BETWEEN RIBS 8 & 9 UPPER & LOWER SKIN IAW SRM REPAIR 55-21-01-201-001-A01. ELEVATOR PN AV670-24100-036 & SN GH280. SEE CONTINUATION CARD FOR DETAILS 093819,093820.

Part: SEAL — MISSING (PBE) · airframe 17,419 hrs · 11,021 cycles

FLIGHT DECK PBE 1 SEAL MISSING, TAMPER SEAL. INSPECTED PBE, NOTED STILL SERVICEABLE. INSTALLED TAMPER SEAL AS REQUIRED. ACFT OK FOR CONTINUED SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 16,888 hrs · 10,659 cycles

FOUND BOTH GALLEY & AFT FLIGHT ATTENDANT STATION EMER FLASHLIGHTS INOPERATIVE. R & R ALL 3 EMER FLASHLIGHTS IAW AMM 25-61-02. PART NR ON & OFF P2-07-0001-214.

Part: LIGHT — MISSING (CABIN) · airframe 16,703 hrs · 10,547 cycles

GALLEY FLOOR PANEL LIGHTING MISSING. INSTALLED EMERGENCY FLOOR TRACK LIGHT STRIP IAW AMM 33-51-00.OK FOR SERVICE.

Part: PBE — UNSERVICEABLE (CABIN) · airframe 16,591 hrs · 10,475 cycles

AFT PBE LOOKS INFLATED BUT ALL SEALS LOOK NORMAL & THE INDICATION IS BLUE. R & R AFT FLIGHT ATTENDANT POSITION PBE, PN MR-10047N. INSTALLED NEW PBE SECURITY SEALS PN 1001-GREEN AS REQUIRED.

Part: LIGHT — BROKEN (CABIN) · airframe 16,491 hrs · 10,416 cycles

EMERGENCY LIGHT FLOOR STRIP IS BROKEN. R & R EMER LIGHT COVER & FILM IAW AMM 33-51-01.

Part: GROUND WIRE — OUT OF POSITION (EMERGENCY LIGHTS) · airframe 15,105 hrs · 9,475 cycles

RIGHT WING FWD OVERWING EMERGERNY EXIT LIGHT IS INOPERATIVE. REPOSITIONED GROUNDING WIRE GS846, 6 VOLTS TO LIGHT. OPS CHECKED GOOD IAW AMM 33-51-00.

Part: LIGHT — MISSING (CABIN) · airframe 14,926 hrs · 9,348 cycles

TASK CARD CR LT & RT FWD FLOOR PATH EMER ILLUMINESCENT STRIPS NOT INST. LT & RT FWD FLOOR PATH EMER ILLUMINESCENT STRIPS IAW AMM 33-51-01-400-801-A21.

Part: PIN — NOT SEATED (CONNECTOR) · airframe 14,926 hrs · 9,348 cycles

TASK CARD 900-25-900-910 CEILING EMER LIGHT AT ROW 13 ABCD IS INOPERATIVE. RESEATED CONNECTOR PINS PROVIDING GNDS TO DS 192P1 2 IAW ESPM 20-16-00. PERFORMED OPERATIONAL TEST IAW AMM 33-51-00-710-802-A16. ALL EMER LIGHTS CHECKED GOOD WITH EXTERNAL ELEC POWER.

Part: LIGHT — BROKEN (CABIN) · airframe 14,926 hrs · 9,348 cycles

TASK CARD 192 ON PANEL 171CL LT AFT EMER EXIT LIGHT HAS CONNECTOR PIN BROKEN IN LIGHT ASSEMBLY SOCKET. LIGHT ASSEMBLY REPLACED ON NR 32296.

Part: HEAT SHIELD — DAMAGED (LT NACELLE) · airframe 14,926 hrs · 9,348 cycles

TASK CARD 900-54-430-301 LT ENG LOWER CORE HEAT SHIELD CORNER PULLING UP ITEM 40 IPC 54-23-01. REPAIRED LT ENG LOWER CORE HEAT SHIELD CORNER IAW EA CRJ954-02663.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 14,926 hrs · 9,348 cycles

TASK CARD CR LT SIDE WALL SEAT TRACK HAS CORROSION DAMAGE AT FS 710 & FS 696. REMOVED OLD SEAT TRACK IAW AMM 53-00-49-000-801-A07. FABRICATED NEW TRACK IAW REQ 670-53-00-343 & DWG PL SH 690-36284. INSTALLED NEW TRACK IAW AMM 53-00-49-400-801-A07.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 14,926 hrs · 9,348 cycles

TASK CARD CR RT SIDE WALL SEAT TRACK HAS CORROSION DAMAGE AT FS 710 & FS 696. REMOVED OLD SEAT TRACK IAW AMM 53-00-49-000-801-107. FABRICATED NEW TRACK IAW REQ 670-53-00-343 & DWG PL SH690-36284. INSTALLED NEW TRACK IAW AMM 53-00-49-400-801-A07.

Part: LIGHT — BROKEN (CABIN) · airframe 14,926 hrs · 9,348 cycles

TASK CARD 900-53-900-106 PNL 172CR EMER LIGHT PINS BROKEN OFF IN LIGHT. R & R LIGHT ASSEMBLY IAW AMM 33-51-15-00-801-A08 & 33-51-15-400-801-A08 BONDING METER TC01B03-01. CRIMPED NEW CONTACTS ON THE WIRES IAW ESPM 20-1600 PG 8 - 10.

Part: LENS — DEFECTIVE (OVERWING EXIT) · airframe 14,926 hrs · 9,348 cycles

TASK CARD 900-52-830-306 LT CTR OVERWING EMER EXIT LIGHT LENS CLOUDY. REMOVED LT FUSELAGE OVERWING EMER LIGHT ASSEMBLY IAW CMM 33-51-02 & INSTALLED NEW SERVICEABLE LIGHT ASSEMBLY IAW CMM 33-51-02.

Part: LENS — CRACKED (CABIN) · airframe 14,926 hrs · 9,348 cycles

TASK CARD 900-52-830-306 LT FWD OVERWING EMER EXIT LIGHT LENS CRACKED. R & R LIGHT ASSEMBLY ON PNL 171CL IAW CMM 33-51-02.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 14,301 hrs · 8,931 cycles

ANTI-ICE DUCT WARNING, THEN ANTI-ICE DUCT CAUTION IN ICING CONDITIONS. RAN NON-NORMAL CHECKLIST. FLIGHT ATTENDANT REPORTED LIGHT ICE FORMING ON FRONT OF WING. WE INCREASED SPEED TO DISPERSE ICE. WHEN DISPERSAL WAS NOT SUCCESSFUL TURNED ANTI-ICE WING SWITCH BACK ON, MESSAGE DID NOT RETURN. AS NOTED ON WINDSHIELD WIPERS. INSPECTED & OPERATIONS CHECKED LT WING ANTI-ICE DUCTING IAW FIM 36-19-01. OPERATIONS CHECKED GOOD, ACFT OK FOR SERVICE.

Part: A/C PACK — OVERTEMP (LEFT) · airframe 13,880 hrs · 8,666 cycles

NOTICED ODOR AND SMOKE IN THE COCKPIT COMING FROM THE F/O'S SIDE PANEL AREA. SMOKE DISPERSED AND RETURNED TO THE GATE. SMOKE IN THE COCKPIT WAS VERY LIGHT BUT CLEARLY NOTICEABLE. (AMBER) "LT PACK AUTO FAIL" ILLUMINATED AFTER SMOKE HAD ALREADY CLEARED. PERFORMED OPS TEST OF LT PACK IAW AMM 21-51-00. FOUND LT PACK OVERTEMP DURING OPS CHECK. OPEN

Part: LIFE VEST — ABNORMAL (CABIN) · airframe 13,697 hrs · 8,552 cycles

THREE INFANT LIFE PRESERVERS MISSING. INSTALLED THREE INFANT LIFE PRESERVERS.

Part: LIGHT — MISSING (GALLEY) · airframe 13,251 hrs · 8,274 cycles

EMERGENCY LIGHT MISSING. REPLACED EMERGENCY LIGHT IN FWD GALLEY AREA.

Part: LIGHT — UNSECURE (CABIN) · airframe 12,994 hrs · 8,111 cycles

EMERGENCY LIGHT UNSECURE. SECURED EMERGENCY LIGHT IAW AMM 33-56-00. OPS CHECKED NORMAL, OK FOR SERVICE.

Part: BEAM — CRACKED (FUSELAGE) · airframe 11,757 hrs · 7,359 cycles

LBL 12 IN THE VERY FWD E & E BAY, IS CRACKED. PERFORMED REPAIR ON LBL 12 BEAM IAW REO 690-53-11-46R.

Part: FRAME — CORRODED (FUSELAGE) · airframe 11,757 hrs · 7,359 cycles

900-53-140-300, FRAME 310 HAS CORROSION BETWEEN STGR 26L AND 26R, IN THE FWD E & E BAY. REMOVED CORROSION FRAME 310 STGR 26L & 26R. FOUND TO BE WITHIN LIMITS IAW CRJ 900 SRM 51-21-06 AND EO R53277.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 11,757 hrs · 7,359 cycles

900-53-140-300, STGR 26L HAS CORROSION BETWEEN FRAMES 349 AND 333, IN THE FWD E & E BAY. REMOVED & REPLACED STRINGER 26L FRAMES 349 & 333. IAW CRJ 900 SRM 51-42-06 AND EO R53277. P/N SH670-31372-3.

Part: FRAME — CORRODED (FUSELAGE) · airframe 11,757 hrs · 7,359 cycles

900-53-140-300, FRAME 295 HAS CORROSION BETWEEN STGR 26L AND 26R, IN THE FWD E & E BAY. REMOVED CORROSION FRAME 295 BETWEEN STGR 26L & 26R. FOUND WITHIN LIMITS IAW CRJ 900 SRM 51-21-06. EO R53277.

Part: FRAME — CORRODED (FUSELAGE) · airframe 11,757 hrs · 7,359 cycles

900-53-140-300, FRAME 349 HAS CORROSION BETWEEN STGR 25L AND 25R, IN THE FWD E & E BAY. REMOVED CORROSION FRAME 349 STGR 25 L & 25R. FOUND WITHIN LIMITS IAW CRJ 900 SRM 51-21-06 AND EO R53277.

Part: FRAME — CORRODED (FUSELAGE) · airframe 11,757 hrs · 7,359 cycles

900-53-140-300, FRAME 319.70 HAS CORROSION BETWEEN STGR 25L AND 26R, IN THE FWD E & E BAY. REMOVED CORROSION FRAME 319.70 BETWEEN STGR 25L & 26R. FOUND WITHIN LIMITS IAW CRJ 900 SRM 51-21-06. EO R53277.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 11,757 hrs · 7,359 cycles

900-53-140-300, ANTENNA DOUBLER AT A/C BELLY HAS CORROSION, BETWEEN FRAMES 310 AND 295, IN THE FWD E & E BAY. REMOVED & REPLACED ANTENNA PBLR BETWEEN FS 295 & FS 310 ON E&E BAY IAW CRJ 900 SRM 51-42-06 & 51-42-21. AAR SM-31.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 11,757 hrs · 7,359 cycles

900-53-140-300, SPLICE ON STGR 25R HAS CORROSION AT FRAME 333, IN THE FWD E & E BAY. REMOVED AND REPLACED STGR 25R SPLICE IAW CRJ 900 SRM 51-42-06 EO R53277. P/N SH670-32429-3.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 11,757 hrs · 7,359 cycles

900-53-140-300, STGR 26R HAS CORROSION BETWEEN FRAMES 349 AND 333, IN THE FWD E & E BAY. REMOVED AND REPLACED STGR FRAMES 349 & 333. IAW CRJ 900 SRM 51-42-06. P/N SH670-31372-4.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 11,757 hrs · 7,359 cycles

900-53-900-300, RBL 12 IN THE VERY FWD E & E BAY, IS CRACKED. REMOVED AND REPLACED RBL 12 IAW EO R53294. P/N 670-53-11-755-2B.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 11,757 hrs · 7,359 cycles

900-53-900-126, SEAT TRACK IS CORRODED RBL 12 AT FS 349. REMOVED AND REPLACED RIGHT NR 1 FLOOR SEAT TRACK AT RBL 12 AND FS 349.00 IAW CRJ 900 AMM 53-00-49. P/N SH670-32159-1.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 11,757 hrs · 7,359 cycles

900-53-140-509, COCKPIT FLOOR PANEL LANDING AT FS 280 IS CORRODED. REMOVED AND REPLACED COCKPIT FLOOR PANEL LANDING IAW CRJ 900 SRM 51-42-06.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 11,757 hrs · 7,359 cycles

900-53-900-126, SEAT TRACK IS CORRODED LBL 12 AT APPROX FS 373. REMOVED AND REPLACED CORRODED SEAT TRACK AT LBL 9 FS 374-FS 485 IAW CRJ 900 AMM 53-00-49 P/N SH670-32249-3 AAR SM-31.

Part: BEAM — CORRODED (FUSELAGE) · airframe 11,757 hrs · 7,359 cycles

900-53-140-509, 280 BEAM IS CORRODED BETWEEN ANGLE AND BEAM AT APPROX RBL 12. REMOVED & REPLACED RIGHT 280 BEAM IAW EO R53293. P/N CC670-34094-2S AAR SM-10.

Part: BEAM — CRACKED (FUSELAGE) · airframe 11,757 hrs · 7,359 cycles

900-53-140-509, 280 BEAM IS CORRODED BELOW 280 WALL ANGLE AND BEAM AT APPROX LBL 12. REMOVED & REPLACED C 280 BEAM IAW EO R53293. P/N CC670-34094-1S AAR SM-10.

Part: PBE — UNSERVICEABLE (CABIN) · airframe 11,510 hrs · 7,198 cycles

PBE BEHIND SEAT 29B IS SOFT - SEAL IS VIOLATED. REMOVED & REPLACED PBE SMOKE HOOD IAW AMM 25-60-00. P/N ON/OFF MR-10042N S/N OFF E0801355 S/N ON EO406832. OK FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 9,566 hrs · 6,001 cycles

FWD MIDDLE CABIN EMERGENCY CURVE EXIT SIGN DS191 INOP. REMOVED AND REPLACED EPSU BATTERY PACK AT PS37 PER AMM 33-51-17 P/N ON/OFF 2013-1A S/N OFF 97713 SN/ ON 101256. OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 9,566 hrs · 6,001 cycles

RIGHT FWD OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EPSU BATT PACK AT PS37 PER AMM 33-51-17 P/N 2013-1A S/N OFF 97713 S/N ON 101256. OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 9,566 hrs · 6,001 cycles

LEFT AFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EPSU BATT PACK AT PS37 PER AMM 33-51-17 P/N 2013-1A S/N OFF 97713 S/N ON 101256. OPS CHECK GOOD.

Part: STRUT — FAILED (RT MLG) · airframe 8,819 hrs · 5,557 cycles

RIGHT MAIN STRUT HAS STRUCTURAL DAMAGE THAT OCCURRED DURING TOUCHDOWN AFTER NOSEWHEEL CAME DOWN. ONLY COCKPIT INDICATION WAS A MASTER CAUTION FOR WOW INPUT AND A PROX SYS FAULT 1 STATUS MESSAGE. THERE WAS FLUID POOLING AROUND RT MAIN STRUT AND PERSONNEL REPORTED A SMALL AMOUNT OF SMOKE FORM RT MAIN STRUT AREA. R & R RT MLG ASSY, RT MLG SIDE STAY IAW JOB CARD 900-32-740-702, RT IB/RT OB BRAKES PER JOB CARD 900-32-730-901, AND RT IB/RT OB MAIN TIRE & WHEEL IAW JOB CARD 900-32-730-708, NO DEFECTS NOTED AT THIS TIME.

Part: LIGHT — MISSING (CABIN) · airframe 8,391 hrs · 5,291 cycles

F/A NOTICED DURING PREFLIGHT, ROW 12AB FLOOR PATH LIGHTING STRIP (EMERGENCY EXIT ROW) IS MISSING. INSTALLED NEW EMERGENCY EXIT AISLE LIGHTS P/N PL88-900LH00 P/N PL88-910LH00, P/N PL88-930LH05 IAW AMM 33-51-01. SECURITY CHECK GOOD.

Part: LIGHT — DAMAGED (CABIN) · airframe 7,137 hrs · 4,504 cycles

LT EMERGENCY FLOOR PATH LIGHTING AT GALLEY CARTS DAMAGED. REPLACED EMERGENCY LIGHTING STRIP.

Part: LIGHT — MISSING (CABIN) · airframe 6,549 hrs · 4,180 cycles

F/A REPORTS EMERGENCY FLOOR REFLECTIVE STRIP IN GALLEY AREA IS MISSING. R & R FLOOR TRACK LIGHTING STRIP PN PL88-900LH00 IAW AMM 33-51-01.

Part: PIN — NOT SEATED (CONNECTOR) · airframe 5,956 hrs · 3,853 cycles

ROUTINE CHECK, RT WING EXIT LIGHTS ARE INOP PS94 AND DS101 NO VOLTAGE AT THE LAMP ASSY. FOUND PUSH PIN AT CONNECTOR P396 SEATED PIN INTO CONNECTOR AND RECONNECTED CONNECTOR OPS CHECK GOOD IAW CRJ AMM 33-51-15-710-801.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 5,956 hrs · 3,853 cycles

ROUTINE CHECK, EMERGENCY LIGHTS FOR LT FWD WARDROBE DO NOT WORK. REMOVED AND REPLACED THE BATTERY PACK S/N OFF 73409 S/N ON 100673 IAW CHAPTER 33-51-14 OF THE AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 5,956 hrs · 3,853 cycles

THE NR 4 EMERGENCY BATTERY PACK IS DISCHARGED BATTERY PACK NEEDS REPLACEMENT. REPLACED BATTERY PACK S/N 101353 INSTALLED BATTERY PACK S/N 101411 IAW CHAPTER 33-51-17 OF AMM.

Part: LIGHT — MISSING (CABIN) · airframe 4,456 hrs · 2,983 cycles

EMERGENCY FLOOR TRACK LIGHTING MISSING AT FWD GALLEY LT SIDE. INSTALLED NEW FLOOR TRACK LIGHTING.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 3,969 hrs · 2,702 cycles

EMERGENCY FLOOR PATH LIGHTING DAMAGED ON RT SIDE OF GALLEY. R & R EMERGENCY FLOOR PATH LIGHTING ON RT SIDE OF GALLEY, PN ON/OFF PL88-900LH00, PL88-930LH05 IAW AMM CH 33-51-00 (CONFIG A210 LIGHTING CHECKS GOOD).