N916FJ

Part: NONE — NONE · airframe 40,635 hrs · 32,625 cycles

LH PCK TEMP CTN IN FLIGHT. AIRCRAFT STILL OUT OF SERVICE.

Part: NONE — NONE · airframe 40,635 hrs · 32,625 cycles

RH PACK TEMP CAUTION IN FLT - EMER DECLARED. AIRCRAFT CURRENTLY OOS.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,605 hrs · 31,871 cycles

14F FLOOR LEVEL EMER SIGN 1 BULB INOP. RELAMPED

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 39,049 hrs · 31,458 cycles

ROW 14F LWR EMER EXIT LIGHT INOP- RELAMPED

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,048 hrs · 31,457 cycles

EXIT LIGHT 1 BULB INOP ROW 14F. RELAMPED

Part: SMOKE WARNING — FALSE ACTIVATION (LAVATORY) · airframe 38,868 hrs · 31,339 cycles

SMOKE AFT LAV WARNING IN FLIGHT, FALSE INDICATION. RESET SYSTEM, OPERATIONS CHECK GOOD.

Part: SMOKE WARNING — FALSE ACTIVATION (AFT LAVATORY) · airframe 38,825 hrs · 31,315 cycles

SMOKE AFT LAV WARNING IN FLT FALSE INDICATION. CREW VERIFED NO ACTUAL SMOKE. SYSTEM WAS RESET AND OPERATIONS CHECKED GOOD.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 38,824 hrs · 31,314 cycles

CRACKED STRINGER NR 3 (LINTEL AREA) IN STA FS 280 AT CIRCUMFERENTIAL SKIN JOINT. CRACKED STRINGER NR 3 (LINTEL AREA) IN STA FS 280 AT CIRCUMFERENTIAL SKIN JOINT WAS REPAIRED, PER REO 670-53-21-493 REV-D.

Part: STRINGER — CORRODED (E/E BAY) · airframe 38,824 hrs · 31,314 cycles

CORROSION ON STRINGER 21R FROM FS 280 TO 333 AT MAIN AVIONICS COMPARTMENT. CORRECTIVE ACTION: STRINGER 21R FROM FS 280 TO 333 WAS REPLACED, PER CRJ900 SRM 51-42-06-001-001-A01 PAR 6C AND SRM 51-42-20-001-001-A01 PAR 6 C.

Part: INTERCOSTAL — CORRODED (E/E BAY) · airframe 38,824 hrs · 31,314 cycles

CORROSION ON INTERCOSTALS (2 EA) IN STA FS 349 TO FS 364 NEAR STGR 27 AT MAIN AVIONICS COMPARTMENT. CORRECTIVE ACTION: INSTERCOSTALS (2 EA) WAS REPLACED, PER CRJ900 SRM 51-41-06-001-001A01 PAR 6 A AND SRM 51-42-20-001-A01 PAR 6A.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 38,824 hrs · 31,314 cycles

CORROSION ON STRINGER 24RT FROM FS 333 TO 364 AT MAIN AVIONICS COMPARTMENT. STRINGER 24RT FROM FS 333 TO 370 WAS REPLACED, PER CRJ900-SRM-51-42-06-001-001-A01.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 38,824 hrs · 31,314 cycles

CORROSION ON SIDE SEAT RAILS IN SECTION FS 847 +16-FS 897 +70 STGR 15LT AND FS 677 TO FS 720 +85 STGR 15RT AT PAX CABIN. NEW SIDE SEAT RAILS IN SECTION FS 847 +16-FS 897 +70 STGR 15LT AND FS 677 TO FS 720 +85 STGR 15RT WERE REPLACED, PER CRJ900 AMM 53-00-49-400-801 CONF A04.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 38,824 hrs · 31,314 cycles

CORROSION ON SIDE SEAT RAILS IN SECTION FS 847 +16 TO FS 8971 +70 STGR 15LT AND FS 677 TO FS 720 +85 STGR 15RT AT PAX CABIN. NEW SIDE SEAT RAILS IN SECTION FS 847 +16 TO FS 8971 +70 STGR 15LT AND FS 677 TO FS 720 +85 STGR 15RT WERE REPLACED, PER CRJ900 AMM 53-00-49-400-801 CONF A04.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 38,824 hrs · 31,314 cycles

CORROSION ON SIDE SEAT RAILS IN SECTION FS 847 +16-FS 897 +70 STGR 15LT AND FS 677 TO FS 720+85 STGR 15RT AT PAX CABIN. NEW SIDE SIDE SEAT RAILS IN SECTION FS 847 +16-FS 897 +70 STGR 15LT AND FS 677 TO FS 720+85 STGR 15RT WERE REPLACED, PER CRJ900 AMM 53-00-49-400-801 CONF A04.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 38,824 hrs · 31,314 cycles

CORROSION ON STRINGER 21RT IN STA FS 865 TO FS 881 AT AFT GALLEY SERVICE DOOR SURROUND STRUCTURE. CORRECTIVE ACTION: STRINGER 21 RT WAS REPAIRED PER EA: 79-2020-067 REV: P2.

Part: STRINGER — CORRODED (CABIN) · airframe 38,824 hrs · 31,314 cycles

CORROSION ON INTERCOSTAL ATTACHED TO STRINGER 20RT IN STA FS 310 TO FS 319 AT MAIN AVIONICS COMPARTMENT (E/E) W1. INTERCOSTAL ATTACHED TO STRINGER 20RT IN STA FS 310 TO FS 319 AT MAIN AVIONICS COMPARTMENT WAS INSTALLED, PER CRJ900 SRM 51-42-21-001-001-A01 PAR 6C.

Part: STRINGER SPLICE — CORRODED (CABIN) · airframe 38,824 hrs · 31,314 cycles

AFTER REMOTION INTERCOSTAL CORROSION ON STRINGER SPLICE 21RT FS 333 AT E/E. NEW SPLICE 21RT ON STA. 333 WAS REPLACED, PER CRJ900 SRM 51-42-06-001-A01 AND 51-42-21-001-001-A01.

Part: DOUBLER — CORRODED (FUSELAGE AFT) · airframe 38,824 hrs · 31,314 cycles

AWR HIDDEN DAMAGE IN REF NRC S/N 00252, AFTER INTERNAL PRODUCTION DOUBLER REMOVAL, CORROSION ON INTERNAL FUSELAGE SKIN WAS FOUND ON DOUBLER SETTLEMENT AREA. CORRECTIVE ACTION: AFTER INTERNAL PRODUCTION DOUBLER REMOVAL, ON INTERNAL FUSELAGE SKIN WAS FOUND ON DOUBLER SETTLEMENT AREA WAS REPAIRED. PERFORMED PER CRJ900 AND EA 79-2020-069 REV P2.

Part: SKIN — CORRODED (E/E BAY) · airframe 38,824 hrs · 31,314 cycles

HIDDEN DISCREPANCY IN REF NRC S/N 00733 DURING LOWER TCAS ANTENNA REMOVAL CORROSION ON EXTERNAL FUSELAGE SKIN WAS FOUND (SETTLEMENT ON ANTENNA AREA). CORRECTIVE ACTION: CORROSION ON EXTERNAL FUSELAGE SKIN (SETTLEMENT ON ANTENNA AREA) WAS REPAIRED PER REO 670-53-21-1250 REV B.

Part: STRINGER — CORRODED (E/E BAY) · airframe 38,824 hrs · 31,314 cycles

COROSSION ON STRINGER 21RT BETWEEN FS 349-FS 364 AT E/E. CORRECTIVE ACTION: STRINGER 21 WAS REPLACED, PER CRJ900 SRM 51-42-06-001-A01 PAR 6 AND SRM 51-42-20-001-001-A01 PAR 6.

Part: STRINGER — CORRODED (PAX CABIN) · airframe 38,824 hrs · 31,314 cycles

CORROSION ON STRINGER 22RT IN STA FS 280 TO FS 333 AT MAIN AVIONICS COMPARTMENT (E/E) (W1) TCI:53-20-304. STRINGER 22RT, OF STA 295, 310, 319 AND 333 WAS REPLACED, PER CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.

Part: CANISTER — CRACKED (LT WING) · airframe 38,824 hrs · 31,314 cycles

CRACK ON CANISTER NR 3 THROUGHOUT ACCESS PANEL 5551AB LT WING. REPAIRED PER RE0 670-57-42-577 REV.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 38,824 hrs · 31,314 cycles

CORROSION FLOOR SUPPORT ON FUSELAGE FLOOR STRUCTURE FS 310-FS 333. CORRECTIVE ACTION: NEW SUPPORT ON FUSELAGE FLOOR STRUCTURE FS 310-FS 333 AND RBL 6 WAS REPLACED, PER CRJ900 SRM 51-42-20-001-A01 PAR 6C.

Part: ANGLE — CRACKED (ZONE 200) · airframe 38,824 hrs · 31,314 cycles

CRACK ON ANGLE OF LBL 9 STA 280 AT PAX CABIN FWD WET AREA (W1) (CPAX) CRACK ON ANGLE OF LBL 9 STA 280 AT PAX CABIN FWD WET AREA WAS REPLACED, PER CRJ900-SRM 51-42-21-001-001-A01 PAR G C.

Part: CANISTER — CRACKED (RT WING) · airframe 38,824 hrs · 31,314 cycles

CRACK ON CANISTER NR 3 THROUGHOUT ACCESS PANEL 5551AB RT WING. REPAIRED PER RE0 670-57-42-577 REV.

Part: FLOOR SUPPORT — CORRODED (PAX CABIN) · airframe 38,824 hrs · 31,314 cycles

CORROSION FLOOR SUPPORT ON FUSELAGE FLOOR STRUCTURE BETWEEN FS 364-FS 394 AND LBL 30. CORRECTIVE ACTION: FLOOR SUPPORT ON FUSELAGE FLOOR STRUCTURE BETWEEN FS 364-FS 394 AND LBL 30 WAS REPLACED, PER CRJ900 SRM 51-42-20-001-A01 PAR 6C.

Part: FLOOR SUPPORT — CORRODED (PAX CABIN) · airframe 38,824 hrs · 31,314 cycles

CORROSION FLOOR SUPPORT ON FUSELAGE FLOOR STRUCTURE BETWEEN FS 364-FS 394 AND LBL 15. CORRECTIVE ACTION: NEW FLOOR SUPPORT ON FUSELAGE FLOOR STRUCTURE BETWEEN FS 364-FS 394 AND LBL 15 WAS REPLACED, PER CRJ900 SRM 51-42-20-001-A01 PAR 6C.

Part: ANGLE — CORRODED (PAX CABIN) · airframe 38,824 hrs · 31,314 cycles

CRACK ON ANGLE IN STA FS 280 AND 26 RBL AT PAX CABIN FWD WET AREA ANGLE WAS REPLACED, PER CRJ900 SRM 51-42-06-001-001-A01.

Part: ANGLE — CRACKED (PAX CABIN) · airframe 38,824 hrs · 31,314 cycles

CRACK ON ANGLE OF RBL 9 STA 280 AT PAX CABIN FWD WET AREA. CORRECTIVE ACTION: ANGLE OF RBL 9 STA 280 WAS REPLACED, PER EA 74-2020-106 REV IR.

Part: FLOOR SUPPORT — CORRODED (AFT CARGO) · airframe 38,824 hrs · 31,314 cycles

CORROSION ON FLOOR BEAM LBL 9 BETWEEN FS 1015 TO FS 1031 AT AFT CARGO COMPARTMENT AT FLOOR BEAM LBL 9 BETWEEN FS 1015 TO FS 1031 AT AFT CARGO COMPARTMENT WAS REPAIRED, PER CRJ900 SRM 53-00-41-201-001-A03 FIG 53-00-41-4995-829 REP 001-A03.

Part: INTERCOSTAL — CORRODED (ZONE 200) · airframe 38,824 hrs · 31,314 cycles

CORROSION ON INTERCOSTAL IN STA FS 865 TO FS 881 ON STGR 21 AT AFT GALLEY SERVICE DOOR SURROUND STRUCTURE. CORRECTIVE ACTION: INTERCOSTAL IN STA FS 865 TO FS 881 ON STGR 21 WAS REPLACED, PER EA 20-2020-194 REV IR.

Part: DOUBLER — CORRODED (AFT CARGO) · airframe 38,824 hrs · 31,314 cycles

CORROSION ON DOUBLER BETWEEN FS 1031 TO FS 1047 STGR 26RT AND 27, AFT CARGO COMPARTMENT. CORRECTIVE ACTION: DOUBLER BETWEEN FS 1031 TO FS 1047 STGR 26RT AND 27 WAS REPLACED, PER CRJ900 SRM 51-42-06-001-001-A01.

Part: FLOORBEAM — CORRODED (AFT CARGO) · airframe 38,824 hrs · 31,314 cycles

CORROSION ON FLOOR BEAM RBL 9 BETWEEN FS 105 AT AFT CARGO COMPARTMENT BEAM FLOOR WAS REPAIRED, PER CRJ900 SRM 53-00-41-201-001-A03 AND 53-00-41-995-829 REPAIRED 001-A03.

Part: STRINGER — CORRODED (AFT CARGO BAY) · airframe 38,824 hrs · 31,314 cycles

CORROSION ON STGR 26RT BETWEEN FS 1031 TO FS 1047 AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: STGR 26RT BETWEEN FS 1031 TO FS 1047 WAS REPAIRED, PER EA 20-2020-198 REV P1.

Part: WEB — CORRODED (CABIN) · airframe 38,824 hrs · 31,314 cycles

DURING REMOTION OF CROSSBEAM FS 280.00 RELATED WITH NRC 00277, CORROSION ON BULKHEAD WEB LBL 12 AT PAX CABIN FWD WET AREA (W1) (CPAX). REPAIRED BULKHEAD WEB LBL 12 AT PAX CABIN FWD WET AREA, PER CRJ900 SRM 53-11-10-201-004-A01.

Part: FLOOR SUPPORT — CORRODED (AFT CARGO) · airframe 38,824 hrs · 31,314 cycles

CORROSION ON FLOOR BEAM LBL 27 BETWEEN FS 1015 TO FS 1031 AT AFT CARGO COMPARTMENT (C2). FLOOR BEAM LBL 27 BETWEEN FS 1015 TO FS 1031 AT AFT CARGO COMPARTMENT WAS REPLACED, PER CRJ900 SRM 51-42-06-001-001-A01, 51-42-21-001-A01 AND 53-00-41-995-829.

Part: FRAME — CRACKED (ZONE 200) · airframe 38,824 hrs · 31,314 cycles

CRACK ON FUSELAGE FRAME FS 333 BETWEEN STGR 1RT AND 2RT AT APSSENGER CABIN. CORRECTIVE ACTION: FRAME WAS REPAIRED, PER CRJ900 EA 20-2020-167 REV IR.

Part: RIB — CRACKED (RT WING) · airframe 38,824 hrs · 31,314 cycles

CRACK ON RIB LEADING EDGE SS58.41 AT RIGHT WING (AD) (SM). CORRECTIVE ACTION: RIB WAS REPAIR PER EA 80-2020-057 REV IR.

Part: WEB — CORRODED (CABIN) · airframe 38,824 hrs · 31,314 cycles

DURING REMOTION OF CROSSBEAM FS 280.00 RELATED WITH NRC 00278, CORROSION ON BULKHEAD WEB RBL 12 AT PAX CABIN FWD WET AREA (W1) (CPAX). REPAIRED BULKHEAD WEB RBL 12 AT PAX CABIN FWD WET AREA, PER CRJ900 SRM 53-11-10-201-004-A01.

Part: SEAT TRACK — CORRODED (PAX CABIN) · airframe 38,824 hrs · 31,314 cycles

CORROSION ON FLOOR SEAT RAIL IN SECTIONS FS 661 +16 TO FS 693 27 LBL; FS 661 +16 TO FS 677 9 LBL 9 RBL AT CABIN PAX. SECTION OF SEAT RAILS FS 661 +16 TO FS 693 27 LBL; FS 661 +16 TO FS 677 9 LBL 9 RBL WERE REPLACED, PER CRJ900 AMM 53-00-49-400-801 CONF A04.

Part: SEAT TRACK — CORRODED (CABIN PAX) · airframe 38,824 hrs · 31,314 cycles

CORROSION ON FLOOR SEAT RAILS IN SECTION FS 485 TO FS 565; FS 581 TO FS 661 +16 27 LBL; FS 485 TO FS 565 9 LBL 9 RBL; FS 581 TO FA 661+16, 9 LBL 9 RBL AT PAX CABIN. NEW SECTIONS OF SEAT RAILS FS 485 TO 565 27 LBL; FS 485 TO FS 565 9 LBL 9 RBL; FS 581 TO 661 9 LBL 9 RBL WERE REPLACED, PER CRJ-900 AMM 53-00-49-400-801-A04.

Part: SEAT TRACK — CORRODED (PAX CABIN) · airframe 38,824 hrs · 31,314 cycles

NEW SECTIONS OF SEAT RAILS FS 485 TO 565 27 LBL, FS 845 TO FS 565 9 LBL 9 RBL, FS 581 TO 661 + 16 9 LBL 9 RBL WERE REPLACED, PER CRJ-900 AMM 53-00-49-400-801-A04.

Part: SEAT TRACK — CORRODED (PAX CABIN) · airframe 38,824 hrs · 31,314 cycles

CORROSION ON FLOOR SEAT RAIL IN SECTION FS 693 TO FS 830 +40 9 LBL 9 RBL; FS 847 TO 48 TO 847 9 LBL 9 RBL; FS 847+48 TO 969 9 LBL AT CABIN PAX. FLOOR SEAT RAIL IN SECTION FS 693 TO FS 830 +40 9 LBL 9 RBL; FS 847 TO 48 TO 847 9 LBL 9 RBL; FS 847+48 TO 969 9 LBL REPLACED, PER CRJ900 AMM53-00-49-400-801 CONT A04.

Part: ANGLE — CORRODED (CABIN) · airframe 38,824 hrs · 31,314 cycles

CORROSION ON MID CAP ANGLE IN STA FS 310 TO FS 349 AND 41 LBL AT MAIN ENTRANCE DOOR LOWER SILL, FWD WET AREA. NEW MID CAP ANGLE WAS REPLACED, PER CRJ900 SRM-51-41-02-001-A01.

Part: ANGLE — CORRODED (CABIN) · airframe 38,824 hrs · 31,314 cycles

ANGLE KICKPLATE CORRODED AND REPLACED, PER CRJ-900-SRM 51-42-06-001-001-A01.

Part: ANGLE — CORRODED (E/E BAY) · airframe 38,824 hrs · 31,314 cycles

CORORSION ON ANGLE ATTACHED TO STRINGER 26LT/26RT IN STA F2-349 TO FS 364 AT MAIN AVIONICS COMPARTMENT (E/E). CORRECTIVE ACTION: ANGLE ATTACHED TO STRINGER 26LT/26RT IN STA F2-349 TO FS 364 AT MAIN AVIONICS COMPARTMENT WAS REPLACED, PER CRJ900 SRM-51-42-20-001-001-A01. ANGLE ATTACHED TO STRINGER 26LT WAS CLEANED, PER CRJ900 SRM-51-26-00-001-001-A01.

Part: STRINGER SPLICE — CORRODED (E/E BAY) · airframe 38,824 hrs · 31,314 cycles

CORROSION ON STRINGER SPLICE 25RT IN STA FS 327 TO FS 337. CORRECTIVE ACTION: CORROSION ON STRINGER SPLICE 25RT IN STA FS 327 TO FS 337 AT MAIN AVIONICS COMPARTMENT WAS REPLACED, PER CRJ-900-SRM 51-42-20-001-001 A01 PAR 6A AND SRM 51-42-06-001-A01 PAR 6A.

Part: SEAT TRACK — CORRODED (PAX CABIN) · airframe 38,824 hrs · 31,314 cycles

CORROSION ON SIDE SEAT RAILS IN SECTIONS FS 379 TO FS 485, STGR 15 LT/RT, FS 485 TO FS 565, STGR 15 LT/RT, FS 581 TO FA 661 + 16 STGR 15 LT/RT, FS 661 +16 TO FS 661+90 STGR 15 LT/RT AT PAX CABIN. NEW SIDE SEAT RAILS IN SECTIONS FS 379 TO FS 485, STGR 15 LT/RT, FS 485 TO FS 565, STGR 15 LT/RT, FS 581 TO FA 661 + 16 STGR 15 LT/RT, FS-661 +16 TO FS 661+90 STGR 15 LT/RT WERE REPLACED, PER CRJ900 AMM 53-00-49-400-801 CONF A04.

Part: FITTING — DAMAGED (CABIN) · airframe 38,824 hrs · 31,314 cycles

ELONGATED HOLES ON FWD CLOSING FITTING IN STA FS 314 AND BETWEEN 37 LBL TO 41 LBL AT MAIN ENTRANCE DOOR LOWER SILL, FWD WET AREA (W1) (CPAX). FITTING WAS REPLACED IN STA FS 314 AND BETWEEN 37 LBL TO 41 LBL AT MAIN ENTRANCE DOOR LOWER SILL, FWD WET AREA, PER CRJ900 SRM 51-42-06-001-A01.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 38,824 hrs · 31,314 cycles

CORROSION ON FLOOR SEAT RAIL IN SECTIONS FS 364-FS 485 27LBL, FS 379-485 9 LBL AND FS 485 9 RBL AT PAX CABIN FWD WET AREA (W1). NEW SEAT RAILS IN SECTION FS 364 TO FS 485 27 LBL FS 379-485 9 LBL AND FS 485 9 RBL WERE REPLACED, PER CRJ900 AMM 53-00-49-400-801 CONF A0H.

Part: FRAME — CORRODED (E/E BAY) · airframe 38,824 hrs · 31,314 cycles

CORROSION ON FRAME FS 349 BETWEEN STGR 25LT TO 25RT AT E/E. CORRECTIVE ACTION: FRAME FS 349 WAS REPLACED, PER CRJ900 SRM 51-42-06-001-001-A01 PAR 6 AND SRM 51-42-20-001-001-A01 PAR 6.

Part: STRINGER — CORRODED (E/E BAY) · airframe 38,824 hrs · 31,314 cycles

CORROSION ON STRINGER 26RT IN STA FS 280 TO FS 327 AT MAIN AVIONICS COMPARTMENT (E/E). STRINGER WAS REPLACED FOR A NEW ONE.

Part: SUPPORT — CORRODED (E/E BAY) · airframe 38,824 hrs · 31,314 cycles

CORROSION ON LIGHT CLIP SUPPORT ASSEMBLY IN STA FS 897 BETWEEN STGR 23RT TO 24RT AT RT AFT LAVATORY SERVICE PANELS. CORRECTIVE ACTION: GHT CLIP SUPPORT ASSEMBLY IN STA FS 897 BETWEEN STGR 23RT TO 24RT AT RT AFT LAVATORY SERVICE PANELS WAS REPLACED, PER CRJ900 SRM-51-41-02-001-001-A01.

Part: STRINGER — CORRODED (E/E BAY) · airframe 38,824 hrs · 31,314 cycles

CORROSION ON STRINGER 26RT IN STA FS 337 TO FS 364. CORRECTIVE ACTION: STRINGER 26RT IN STA FS 337 TO FS 364 WAS REPLACED, PER CRJ900-SRM-51-42-20-001-001-A01 PAR 6A AND SRM 51-42-06-001-001-A01 PAR 6A.

Part: HINGE FITTING — CORRODED (LT AILERON) · airframe 38,824 hrs · 31,314 cycles

INBOARD/OUTBOARD PCU'S BUSHINGS HINGE FITTINGS NR 2 STA, WS 319 AT LT AILERON WERE REPAIRED, PER REO 670-57-61-107 REV B, REO 690-57-61-196 REV A.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 38,824 hrs · 31,314 cycles

CORROSION ON FLOOR BEAM (UPPER/AFT FLANGE) IN STA FS 280 AND 11 RBL AT PAX CABIN FWD WET AREA. (W1) (CPAX) FLOOR BEAM FS 280.00 RT WAS REPLACED, PER CRJ900 SRM 51-42-06-001-AO1 PAR 6 AND SRM 51-42-001-001-A01 PAR 8.

Part: FLOORBEAM — CORRODED (COCKPIT) · airframe 38,824 hrs · 31,314 cycles

CORROSION ON FLOOR PANEL SUPPORT ANGLE OF ACCESS PANEL 221ALF IN STA FS 280 BETWEEN 11 LBL/RBL AT COCKPIT. SUPPORT ANGLE OF ACCESS PANEL 221ALF IN STA FS 280 BETWEEN 11 LBL/RBL AT COCKPIT WAS REPLACED, PER CRJ900 SRM 51-42-06-001-001-A01.

Part: STRINGER — CORRODED (E/E BAY) · airframe 38,824 hrs · 31,314 cycles

CORROSION ON STRINGER 25RT IN STA FS 337 TO FS 364. CORRECTIVE ACTION: STRINGER 25RT IN STA FS 337 TO FS 364 AT MAIN AVIONICS.

Part: STRINGER — CORRODED (E.E BAY) · airframe 38,824 hrs · 31,314 cycles

CORROSION ON STRINGER 24RT IN STA FS 280 TO FS 327 AT MAIN AVIONICS COMPARTMENT. CORRECTIVE ACTION: STRINGER 24RT IN STA FS 280 TO FS 327 WAS REPLACED, PER CRJ900-SRM-51-42-20-001-A01 PAR 6A AND SRM 51-42-06-001-A01 PAR 6A.

Part: STRINGER — CORRODED (E/E BAY) · airframe 38,824 hrs · 31,314 cycles

CORROSION ON STRINGER 26RT IN STA FS 280 TO FS 327 AT MAIN AVIONICS COMPARTMENT (E/E). STRINGER WAS REPLACED FOR A NEW ONE.

Part: HINGE FITTING — CORRODED (RT AILERON) · airframe 38,824 hrs · 31,314 cycles

INBOARD/OUTBOARD PCU'S BUSHINGS HINGE FITTING NR 3 STA WS 323 AT RT AILERON WERE REPAIRED, PER REO 670-57-61-107 REV B, REO 690-57-61-196REV A AND 690-57-61-195 REV A.

Part: STRINGER — CORRODED (E/E BAY) · airframe 38,824 hrs · 31,314 cycles

CORROSION ON STRINGER 18RT FROM FS 280 TO 310 AT MAIN AVIONICS COMPARTMENT. CORRECTIVE ACTION: STRINGER 18RT FROM FS 280 TO 310 WAS REPLACED, PER CRJ900 SRM-51-42-06-001-001-A01.

Part: HINGE FITTING — CORRODED (RT AILERON) · airframe 38,824 hrs · 31,314 cycles

INBOARD/OUTBOARD PCU'S BUSHINGS HINGE FITTINGS NR 2 STA, WS 319 AT RT AILERON WERE REPAIRED, PER REO 670-57-61-107 REV B, REO 690-57-61-196 REV A AND 690-57-61-195 REV A.

Part: FLOORBEAM — CORRODED (E/E BAY) · airframe 38,824 hrs · 31,314 cycles

CORROSION ON FLOOR SUPPORT IN STA FS 260 BETWEEN STRG 26LT TO 26RT. CORRECTIVE ACTION: FLOOR SUPPORT IN STA FS 260 BETWEEN STRG 26LT TO 26RT WAS REPLACED, PER CRJ-900-SRM 51-42-20-001-001 AO1 PAR 6A.

Part: SKIN SPLICE — CORRODED (ZONE 100) · airframe 38,824 hrs · 31,314 cycles

CORROSION ON SKIN SPLICE IN STA FS 281 BETWEEN STRG 20LT TO 20RT WAS REPAIRED, PER EA 79-2020-075 REV IR.

Part: STRINGER SPLICE — CORRODED (CABIN) · airframe 38,824 hrs · 31,314 cycles

CORROSION ON STINGER SPLICE 24RT IN STA FS 327 TO FS 337 AT MAIN AVIONICS COMPARTMENT. NEW SPLICE ON STRG 24RT IN STA FS 333 WAS REPLACED, PER CRJ-900 SRM 51-42-20-001-001-A01 PAR 6A AND SRM 51-42--06-001-001-A01 PAR 6A.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 38,824 hrs · 31,314 cycles

CORROSION ON FLOOR BEAM, UPPER/AFT FLANGE IN STA F2-280 AND LBL AT PAX CABIN FWD WET AREA. (W1) (CPAX) FLOOR BEAM UPPER/AFT FLANGE IN STA F2-280 AND LBL AT PAX CABIN FWD WET AREA WAS REPLACED, PER CRJ900 SRM-51-42-06-001-001-A01 AND SRM 51-42-10-001-001-A01 PAR 8.

Part: FRAME — CORRODED (E/E BAY) · airframe 38,824 hrs · 31,314 cycles

CORROSION ON FRAME FS 364 BETWEEN STGR 25LT TO 25RT AT E/E. CORRECTIVE ACTION: FRAME SECTION 364 WAS REPLACED, PER CRJ900 SRM-51-42-06-001-A01 PAR 6 AND SRM 51-42-20-001-001-A01 PAR 6.

Part: STRINGER — CORRODED (E/E BAY) · airframe 38,824 hrs · 31,314 cycles

CORROSION ON STRINGER 25RT IN STA FS 280 TO FS 327. CORRECTIVE ACTION: STRINGER 25RT IN STA FS 280 TO FS 327 AT MAIN AVIONICS COMPARTMENT WAS REPLACED, PER CRJ-900 SRM 41-42-20-01-001-A01 PAR 6A AND SRM 51-42-06-001-A01 PAR 6A.

Part: SKIN — CORRODED (FUSELAGE) · airframe 38,824 hrs · 31,314 cycles

CORROSION ON SKIN IN STA FS 881 TO FS 913 BETWEEN STGR 22RT TO 24RT AT FUSELAGE SKIN. CORRECTIVE ACTION: CORROSION WAS REMOVED, PER CRJ900-SRM 51-21-06-001-001-A01.

Part: INTERCOSTAL — CORRODED (PASSENGER DOOR) · airframe 38,824 hrs · 31,314 cycles

CORROSION ON INTERCOASTAL DD6 OF PASSENGER DOOR STRUCTURE BETWEEN FRAME FS 320-FS 338. INTERCOASTAL DD6 OF PASSENGER DOOR STRUCTURE BETWEEN FRAME FS 320-FS 338 WAS REPLACED, PER CRJ900 SRM 51-42-21-001-001-A01 AND SRM 51-42-06-001-001-A01.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 38,824 hrs · 31,314 cycles

CORROSION ON INTERCOSTAL DD5 OF PASSENGER DOOR STRUCTURE BETWEEN FORMER 311.75 FRAME 320 WAS REPAIRED, PER EA 79-2020-064 REV IR SECTION 1, PERMANENT REPAIR.

Part: INTERCOSTAL — CORRODED (PASSENGER DOOR) · airframe 38,824 hrs · 31,314 cycles

CORROSION ON INTERCOSTAL DD3 OF PASSENGER DOOR STRUCTURE BETWEEN FWD FORMER FS 311 FRAME FS 320 WAS REPAIRED, PER EA 48-2020-197 REV "IR" SECTION 1, PERMANENT REPAIR.

Part: SKIN — GOUGED (FUSELAGE) · airframe 38,824 hrs · 31,314 cycles

SEVERAL GOUGES IN STA FS 1010 TO FS 1045 BETWEEN STGR 22RT TO 27 AT FUSELAGE SKIN. CORRECTIVE ACTION: GOUGES IN STA FS 1010 TO FS 1045 BETWEEN STGR 22RT TO 27RT WERE REPAIRED, PER EA 48-2020-215 REV IR.

Part: DOUBLER — CORRODED (E/E BAY) · airframe 38,824 hrs · 31,314 cycles

CORROSION ON INTERNAL PRODUCTION DOUBLER IN STA FS 295 TO FS 310 BETWEEN STGR 26LT TO 26RT. CORRECTIVE ACTION: INTERNAL PRODUCTION DOUBLER IN STA FS 295 TO 310 BETWEEN STGR 26LT TO 26RT WAS REPLACED, PER CRJ900 SRM 51-42-06-001-001-A01 PAR 6C.

Part: UNKNOWN — MALFUNCTIONED (RT ENGINE) · airframe 38,537 hrs · 31,119 cycles

RT ENG OIL TEMP HI IN CRUISE AT 250- EMERG DECLARED

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,423 hrs · 31,043 cycles

FIRST CLASS CEILING EMER FLOOD LT INOP. RELAMPED

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,071 hrs · 30,797 cycles

RT FWD/AFT & LT FWD EMR EXT LIGHTS INOP 1 EA.

Part: BATTERY — INOPERATIVE (C/P FLASHLIGHT) · airframe 37,938 hrs · 30,700 cycles

FO FLASHLIGHT INOP. REPLACED BATTERY

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,409 hrs · 29,494 cycles

14F LWR EMER EXIT SIGN BULB INOP. PLACED ON MEL

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,077 hrs · 29,243 cycles

EMER LIGHTS INOP AT SERVICE DOOR. PLACED ON MEL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,555 hrs · 28,842 cycles

CEILING EMER FLOOD LIGHTS INOP. PLACED ON MEL.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 34,678 hrs · 28,145 cycles

FWD FA FLASHLIGHT NOT BLINKING. PLACED ON MEL.

Part: LIGHT — INOPERATIVE (ROW 19) · airframe 34,547 hrs · 28,042 cycles

CEILING OVERHEAD EMERGENCY FLOOD LIGHT AT ROW 19 WAS INOPERATIVE.

Part: LIGHT — INOPERATIVE (AFT) · airframe 34,506 hrs · 28,012 cycles

AFT CEILING EMERGENCY FLOOD LIGHT INOPERATIVE.

Part: HINGE — CHAFED (PAX DOOR) · airframe 33,997 hrs · 27,607 cycles

PAX DOOR HINGE, FUSELAGE SIDE, AFT 16 HINGE LUGS LANDS CHAFED AND LUG HINGE PIN HOLES OBLONG, ALL HINGE PINS HOLES WERE WORN.

Part: HINGE — GOUGED (PAX DOOR) · airframe 33,997 hrs · 27,607 cycles

PASSENGER DOOR HINGE, DOOR SIDE, NR 3 AND 15 LUGS GOUGED, AFT 6 LUGS HAVE SIGNS OF CHAFING.

Part: STRUCTURE — DAMAGED (PAX DOOR) · airframe 33,997 hrs · 27,607 cycles

PASSENGER DOOR DAMAGED AT MULTIPLE AREAS.

Part: DOOR — BINDING (MAIN PAX) · airframe 33,956 hrs · 27,574 cycles

PAX DOOR HARD TO OPEN AND CLOSE.

Part: DOOR — BINDING (MAIN PAX) · airframe 33,951 hrs · 27,570 cycles

PAX DOOR DIFFICULT TO OPEN AND CLOSE.

Part: SMOKE DETECTOR — ACTIVATED (AFT GALLEY) · airframe 33,267 hrs · 27,065 cycles

AFT LAVATORY SMOKE WARNING, HOT ODOR IN CABIN.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 32,637 hrs · 26,540 cycles

FWD FA FLASHLIGHT INOP. PLACED ON MEL.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 32,537 hrs · 26,457 cycles

FWD F/A FLASHLIGHT WOULD NOT CHARGE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 32,514 hrs · 26,436 cycles

FWD FA FLASHLIGHT LED NOT BLINKING. PLACED ON MEL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,436 hrs · 26,372 cycles

ROW 21 EMERGENCY CEILING LIGHT INOP. PLACED ON MEL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,248 hrs · 26,220 cycles

ROW 11 CEILING EMERG FLOOD LIGHT INOP. PLACED ON MEL.

Part: UNKNOWN — MALFUNCTIONED (TE FLAP) · airframe 31,493 hrs · 25,620 cycles

FLAP FAIL CAUTION IN FLIGHT- DIVERT DUE TO RUNWAY LENGTH. CLEARED INHIBITS AND OPS CHECKED FLAPS.

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 30,927 hrs · 25,183 cycles

PAX DOOR, SILL ANGLE CORRODED AROUND NUT PLATES.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,927 hrs · 25,183 cycles

DURING HEAVY CHECK INSPECTION , FOUND THE RT FLOOR SILL, FS280.00 - FS319.70 CORRODED BEYOND REPAIRABLE LIMITS. REMOVED AND REPLACED RT FLOOR SILL IAW EO SH690-32170

Part: FASTENER — LOOSE (LT PYLON) · airframe 30,927 hrs · 25,183 cycles

WHILE PERFORMING AD 2016-11-02 FOUND LT PYLON LWR, TO HAVE 8 LOOSE FASTENERS. RT PYLON, LWR TO HAVE 5 LOOSE FASTENERS, REPAIRS WERE ACCOMPLISHED IAW REO 670-54-51-034.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 30,534 hrs · 24,888 cycles

CAPTAIN FLASHLIGHT INOPERATIVE.

Part: GARLOCK SEAL — DAMAGED (LT ENGINE) · airframe 30,214 hrs · 24,637 cycles

LEFT ENGINE OIL PRESSURE WARNING IN FLT. R & R NR 1 EDP AND GARLOCK SEAL.

Part: STIFFENER — CRACKED (BS 202) · airframe 30,044 hrs · 24,514 cycles

BS 202.75 FORWARD SIDE OF BULKHEAD RBL 30 STIFFENER HAS AN INDICATION .250 INCH LONG IN THE UPPER EDGE OF THE FLANGE . FAILED NDT INSPECTION.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 29,246 hrs · 23,907 cycles

FORWARD F/A FLASHLIGHT INOPERATIVE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,928 hrs · 23,650 cycles

CABIN SIDEWALL EMERGENCY EXIT LIGHT AT ROW 14A HAD ONE BULB INOPERATIVE. REPLACED THE BULB IAW AMM 35-51-11; OPS CHECKED GOOD IAW AMM 35-51-00.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,915 hrs · 23,636 cycles

14A EMERGENCY EXIT SIGN HAD ONE BULB INOPERATIVE.

Part: STRUCTURE — DAMAGED (BS 202) · airframe 28,877 hrs · 23,607 cycles

INSPECTION FOUND DAMAGE TO FUSELAGE STRUCTURE AT BS 202.75 DUE TO BIRD STRIKE

Part: LIGHT — INOPERATIVE (ROW 18) · airframe 28,802 hrs · 23,550 cycles

ROW 18 CEILING EMERGENCY FLOOD LIGHT INOPERATIVE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,700 hrs · 23,466 cycles

FWD CABIN BULKHEAD EXIT SIGN INOPERATIVE. REPLACED BATTERY AND LIGHT ASSY.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 28,675 hrs · 23,445 cycles

LIGHTED EXIT SIGN IN FIRST CLASS INOPERATIVE.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 28,462 hrs · 23,274 cycles

FORWARD F/A FLASHLIGHT INOPERATIVE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 28,934 hrs · 23,225 cycles

FWD EMERGENCY LIGHTS INOPERATIVE. CHARGED BATTERY.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,389 hrs · 23,219 cycles

ROW 14, EMERGENCY LIGHT HAS ONE BULB INOPERATIVE. REPLACED THE BULB IAW AMM 33-51-05. OPS CHECKED GOOD IAW AMM 33-51-00.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 28,382 hrs · 23,211 cycles

ONE BULB, ROW 14 A/C, MID LEVEL EMERGENCY EXIT OUT.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 23,100 hrs · 370,190 cycles

AFT CABIN EMERGENCY FLASHLIGHT LED NOT BLINKING.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,226 hrs · 23,187 cycles

EMERGENCY EXIT LIGHT FLOOR LEVEL, ROW L14 1 BULB OUT. REPLACED THE LAMP, OPS CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 27,946 hrs · 22,872 cycles

ALL CABIN EMERGENCY EXIT LIGHTS INOPERATIVE. CHARGED BATTERIES.

Part: HOOK AND LOOP — MISSING (DOOR HANDLE) · airframe 27,707 hrs · 22,665 cycles

LT EMERGENCY DOOR HANDLE COVER MISSING HOOK AND LOOP. REPLACED HOOK AND LOOP.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,681 hrs · 22,659 cycles

ONE LAMP INOPERATIVE, ROW 14F EXIT SIGN.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,681 hrs · 22,659 cycles

ONE LAMP INOPERATIVE, ROW 13A EXIT SIGN.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 4,750 hrs · 3,628 cycles

F/A FLASHLIGHT INOPERATIVE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,262 hrs · 22,345 cycles

EMERGENCY EXIT SIGN AT 3DF INOPERATIVE. REPLACED LIGHT BULBS.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,238 hrs · 22,329 cycles

LT OVERWING EXIT SIGN LIGHT INOPERATIVE. MAINTENANCE IS TROUBLESHOOTING.

Part: FLASHLIGHT — INOPERATIVE · airframe 27,060 hrs · 22,199 cycles

FLASHLIGHT INOPERATIVE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,958 hrs · 22,118 cycles

EMERGENCY LIGHT 13A FLOOR LEVEL, HAS ONE BULB OUT.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,942 hrs · 22,105 cycles

EMERGENCY LIGHT OUT ROW 15. MAINTENANCE REPLACED THE LAMPS.

Part: LAMP — INOPERATIVE (FLASHLIGHT) · airframe 27,065 hrs · 22,366 cycles

FWD F/A FLASHLIGHT INOPERATIVE. REPLACED THE LAMP.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 26,885 hrs · 22,055 cycles

CAPTAIN`S FLASHLIGHT INOPERATIVE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 26,788 hrs · 21,974 cycles

CAPTAIN`S FLASHLIGHT INOPERATIVE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 26,475 hrs · 21,710 cycles

ALL EMERGENGY LIGHTS INOPERATIVE. CHARGED BATTERIES,

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 26,325 hrs · 21,594 cycles

14DF EXIT SIGN HAS BURNED OUT BULB. REPLACED BULB.

Part: TAB — CHAFED (HORIZONTAL STAB) · airframe 26,176 hrs · 21,455 cycles

LEFT AND RT HORIZONTAL STABILIZER PIN ANTI-ROTATION TABS HAVE CHAFE DAMAGE.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 26,176 hrs · 21,455 cycles

FS 280 FLOORBEAM IS CRACKED ON AFT SIDE JUST OTBD OF LBL 9 .750 INCH LONG AND JUST OTBD OF RBL 9 .250 INCH LONG.

Part: BULKHEAD WEB — CORRODED (BS 280) · corrosion level 2 · airframe 26,176 hrs · 21,455 cycles

RIGHT SIDE LOWER FS 280 BULKHEAD WEB IS CORRODED.

Part: BULKHEAD WEB — CORRODED (BS 280) · corrosion level 2 · airframe 26,176 hrs · 21,455 cycles

LEFT SIDE LOWER FS 280 BULKHEAD WEB IS CORRODED.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 26,176 hrs · 21,455 cycles

VERTICAL STABILIZER RT LOWER FWD DRAG ANGLE IS CRACKED APPROXIMATELY 1" AT AFT SIDE OF ANGLE.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 26,176 hrs · 21,455 cycles

VERTICAL STABILIZER RT LOWER AFT DRAG ANGLE IS CRACKED APPROXIMATELY 1" AT FWD SIDE OF ANGLE.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 261,076 hrs · 21,455 cycles

BS 280 FLOORBEAM FOUND CRACKED.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 26,176 hrs · 21,455 cycles

VERTICAL STAB LT FORWARD AND AFT DRAG ANGLES CRACKED, APPROXIMATELY ONE INCH LONG.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,105 hrs · 21,396 cycles

LOWER EXIT SIGN AT RT EXIT ROW, HAS ONE BULB OUT.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,625 hrs · 20,966 cycles

14A FLOOR EXIT SIGN HAS ONE BULB INOPERATIVE.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 25,243 hrs · 20,627 cycles

FWD F/A FLASHLIGHT INOPERATIVE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 25,219 hrs · 20,605 cycles

ALL EMERGENCY LIGHTS AT FWD GALLEY INOPERATIVE. MAINTENANCE REPLACED NR 1 BATTERY.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 24,899 hrs · 20,318 cycles

AFT CEILING EMERGENCY FLOOD LIGHT INOPERATIVE. REPLACED LAMP.

Part: WARNING LIGHT — FALSE ACTIVATION (FWD CARGO DOOR) · airframe 24,842 hrs · 20,280 cycles

FWD CARGO DOOR OPENED IN FLIGHT. MAINTENANCE INSPECTED & FOUND NO DEFECTS IAW AMM 52-35-00-710-801.

Part: PLACARD — WORN (CABIN) · airframe 24,621 hrs · 20,080 cycles

PLACARD WORN. REPLACED PLACARD.

Part: PLACARD — WORN (CABIN) · airframe 24,621 hrs · 20,080 cycles

PLACARD WORN. REMOVED AND REPLACED PLACARD.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 24,594 hrs · 20,051 cycles

AFT F/A FLASHLIGHT INOPERATIVE.

Part: LIGHT — INOPERATIVE (ROW 6) · airframe 24,488 hrs · 19,957 cycles

ROW 6 EMERGENCY CEILING FLOOD LIGHT INOPERATIVE.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 24,473 hrs · 19,944 cycles

AFT F/A FLASHLIGHT INOPERATIVE. R & R BATTERIES.

Part: WIRE HARNESS — FAILED (ZONE 100) · airframe 24,453 hrs · 19,927 cycles

ADG WIRES, SILVER PLATING CORROSION PROTECTION BREAKS DOWN IN AREAS OF TIGHT RADIUS AND PLATING MAY CRACK AS A RESULT OF MECHANICAL STRESS, LEADING TO THE POSSIBLE ONSET OF CORROSION ON ALL OR A MAJORITY OF THE WIRE STRANDS.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 24,218 hrs · 19,710 cycles

PAX DOOR EMERGENCY LIGHTS INOPERATIVE, CHARGED BATTERIES,

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 23,957 hrs · 19,460 cycles

BOTH COCKPIT FLASHLIGHTS INOPERATIVE. MX REPLACED BATTERY PACKS.

Part: CONTROL UNIT — FAULTED (ANTI-SKID SYS) · airframe 23,842 hrs · 19,353 cycles

OTBD GROUND SPOILER FAULT STATUS MESSAGE. MX REPLACED ANTI-SKID CONTROL UNIT.

Part: TRANSDUCER — INOPERATIVE (WHEEL SPEED) · airframe 23,842 hrs · 19,353 cycles

ANTI SKID OTBD CAUTION MESSAGE. MX REPLACED WHEEL SPEED TRANSDUCER.

Part: TIRE — DEFLATED (MLG) · airframe 23,842 hrs · 19,353 cycles

NR 4 MLG TIRE FLAT. MX REPLACED NR 3 & NR 4 MAIN TIRES.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 23,825 hrs · 19,337 cycles

FWD F/A FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,757 hrs · 19,279 cycles

CEILING EMERGENCY LIGHT, ROW 3 INOPERATIVE. REPLACED BULB.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 23,165 hrs · 18,743 cycles

ALL EMERGENCY EXIT LIGHTS INOPERATIVE UPON PRE FLIGHT INSPECTION. THE CREW CHARGED THE EMERGENCY EXIT LIGHT BATTERY PACKS WITH AIRCRAFT POWER AND NO FURTHER ACTION WAS REQUIRED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,819 hrs · 18,419 cycles

LEFT ROW 13 EXIT SIGN BULBS INOPERATIVE UPON PRE FLIGHT INSPECTION. R2 LAMPS

Part: BATTERY — DISCHARGED (CABIN) · airframe 22,704 hrs · 18,310 cycles

NUMEROUS CABIN EMERGENCY EXIT LIGHTS INOP. MX CHARGED SYSTEM, OPS CHECK GOOD.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 22,704 hrs · 18,310 cycles

AFT F/A FLASHLIGHT NOT CHARGING. REMOVED AND REPLACED FLASHLIGHT.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 22,683 hrs · 18,286 cycles

FWD F/A'S FLASHLIGHT DEAD. REMOVED AND REPLACED FWD F/A'S FLASHLIGHT.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 22,428 hrs · 18,032 cycles

4 ENTRY EMER EXIT SIGNS INOP. REMOVED AND REPLACED 2 EPSU BATTERY CHARGER AMM 33-51-17.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,270 hrs · 17,900 cycles

LEFT AFT WING EMERGENCY LIGHT INOP. RELAMPED EMERGENCY LIGHT.

Part: BATTERY — DISCHARGED (CABIN) · airframe 21,786 hrs · 17,439 cycles

CABIN FLASH LT MAIN CABIN DOOR LT NO FLASH. REMOVED AND REPLACED BATTERY.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 21,314 hrs · 16,995 cycles

CAPTAIN'S FLASHLIGHT DISCOVERED INOPERATIVE UPON PRE-FLIGHT INSPECTION. REMOVED AND REPLACED BATTERIES.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,018 hrs · 16,727 cycles

EMERGENCY CEILING LT AT FWD LAV INOP. REPLACED LIGHT BULB.

Part: BATTERY — UNKNOWN (MEGAPHONE) · airframe 20,909 hrs · 16,617 cycles

MEGAPHONE BATTERY NEEDS REPLACEMENT. R & R MEGAPHONE BATTERY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,427 hrs · 16,162 cycles

CEILING LEVEL FLOOD LIGHT INOP AT SEAT 9F. RELAMPED AND OPS GOOD.

Part: A/C PACK — ODOR (ZONE 100) · airframe 20,310 hrs · 16,042 cycles

MOMENTARY BURNING SMELL IN THE COCKPIT AND CABIN. MX TROUBLESHOT TO NR 2 A/C PACK. REMOVED AND REPLACE NR 2 A/C PACK

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 20,240 hrs · 15,974 cycles

F/O FLASHLIGHT LED NOT FLASHING. REPLACED FLASHLIGHT.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 20,226 hrs · 15,962 cycles

F/O FLASHLIGHT LED NOT FLASHING. REMOVED AND REPLACED FLASHLIGHT

Part: SEAL — DIRTY (PAX DOOR) · airframe 20,226 hrs · 15,962 cycles

PAX DOOR SQUEALS IN FLT. CLEANED & LUBED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 20,203 hrs · 15,946 cycles

CEILNG EMERGENCY FLOOD LIGHT ROW 17 INOPERATIVE. RELAMPED EMERGENCY LIGHT.

Part: FITTING — CORRODED (FUSELAGE) · airframe 20,182 hrs · 15,928 cycles

FWD JACKING FITTING LT SUPPORT STRUCTURE AT FS 278.00 CORRODED. REMOVED AND REPLACED FWD JACKING FITTING LT SUPPORT STRUCTURE AT FS 278.00 IAW SRM 51-42-06 AND 51-42-21 AS ON WO 1007647-1300-0017 AND WO 711014360.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 20,184 hrs · 15,929 cycles

LT FLOOR SEAT TRACK NR 7 STICK CORRODED. REPLACED SEAT TRACK IAW AMM 53-00-49. NEW TRACK AFT END REPAIRED IAW RO CRJ9-53-0910.

Part: STRUCTURE — CORRODED (BS 278) · corrosion level 2 · airframe 20,184 hrs · 15,929 cycles

FWD JACK FITTING RT SUPPORT STRUCTURE CORRODED AT FS 278. REPLACED SUPPORT STRUCTURE IAW SRM 51-42-06 AND 51-42-21.

Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 20,184 hrs · 15,929 cycles

FWD SERVICE DOOR FLOOR FITTING AT FS 319 CORRODED. REPLACED FLOOR FITTING IAW SRM 51-42-21.

Part: DRAG ANGLE — CORRODED (PAX DOOR) · corrosion level 2 · airframe 20,184 hrs · 15,929 cycles

PAX DOOR NEAR DOOR MOTOR PULL HAS CRACKED DRAG ANGLE. REPAIRED DRAG ANGLE IAW SRM 52-11-04.

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 20,184 hrs · 15,929 cycles

FLOOR SILL AT FWD CORNER OF GALLEY SERVICE DOOR CORRODED. REPLACED FLOOR SILL IAW SRM 51-42-06 AND 51-42-21.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 20,182 hrs · 15,928 cycles

WHILE WORKING PAX DOOR THRESHOLD FLOOR LANDING ANGLE REPAIR FOUND SUPPORT ANGLE CORRODED. REPAIRED PAX DOOR THRESHOLD FLOOR LANDING ANGLE IAW CRJ900 SRM 51-42-06 AS ON AAR WO 1007647-2700-0212 AND WO 711014360.

Part: LUG — DAMAGED (RT AILERON) · airframe 20,182 hrs · 15,928 cycles

RT AILERON NR 2, 3, 4 PCU LUGS DAMAGED. REPAIRED RT AILERON NR 2, 3, 4 PCU LUGS IAW RO CRJ9-57-0349 AS ON WO 1007647-6700-0038 AND WO 711015947.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 20,182 hrs · 15,928 cycles

FLOOR LANDING AT PAX DOOR CORRODED. REMOVED AND REPLACED FLOOR LANDING AT PAX DOOR IAW CRJ 900 SRM 51-42-06 AS ON WO 1007647-2700-0148 AND WO 711014360.

Part: BULKHEAD WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 20,184 hrs · 15,929 cycles

LT LOWER 280 BULKHEAD WEB CORRODED, REPLACED BULHEAD IAW SRM 51-42-06.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 20,182 hrs · 15,928 cycles

INTERCOSTAL AND ATTACHING CLIP CORRODED FROM FS 310.00 TO 319.70 AT STGR 20R. REMOVED AND REPLACED INTERCOSTAL AND ATTACHING CLIP FROM FS 310 TO 319 AT STGR 20R IAW CRJ 900 SRM 51-42-21 AS ON AAR WO 1007647-1300-0026 AND WO 711014360.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 20,184 hrs · 15,929 cycles

RT FLOOR SEAT TRACK NR 7 STICK CORRODED. REPLACED SEAT TRACK IAW AMM 53-00-49.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 20,182 hrs · 15,928 cycles

INTERCOSTAL FROM FS 319.00 TO FS 333.00 CORRODED. REMOVED AND REPLACED INTERCOSTAL FROM FS 319 TO 349 IAW CRJ 900 SRM 51-42-21 AS ON AAR WO 1007647-1300-0033 AND WO 711014360.

Part: BULKHEAD WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 20,184 hrs · 15,929 cycles

RT LOWER 280 BULKHEAD WEB CORRODED, REPLACED BULHEAD IAW SRM 51-42-06.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 20,182 hrs · 15,928 cycles

STGR 24R CORRODED AT FS 306.00. REMOVED AND REPLACED STRINGER IAW CRJ 900 SRM 51-42-06 AND 51-42-21. AS ON WO 1007647-1300-0023 AND WO 711014360.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 20,182 hrs · 15,928 cycles

STGR 25R SPLICE CORRODED AT FS 337.00. REMOVED AND REPLACED SPLICE IAW CRJ 900 SRM 51-42-06 AND 51-42-21. AS ON AAR WO 1007647-1300-0010 AND WO 711014360.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 20,184 hrs · 15,929 cycles

FRAME AT FS 319.70 CORRODED FROM STR 26L TO 26R - REPAIRED FRAME IAW RO CRJ9-53-0875.

Part: FLOOR PANEL — CORRODED (COCKPIT) · airframe 20,182 hrs · 15,928 cycles

FLIGHT DECK FLOOR PANEL LANDING AT FS 280 CORRODED. REMOVED AND REPLACED FLIGHT DECK FLOOR PANEL LANDING IAW CRJ 900 SRM 51-42-21. AS ON AAR WO 1007647-1000-0129 AND WO 711014360.

Part: BUSHING — DAMAGED (ELEVATOR) · airframe 20,182 hrs · 15,928 cycles

LT ELEVATOR INBOARD PCU ATTACH POINT INBOARD LUG BUSHING IS DAMAGED. REMOVED AND REPLACED LT ELEVATOR INBD PCU ATTACH POINT INBD LUG BUSHING IAW CRJ 900 AMM 20-31-00 AND RO CRJ9-55-0148.AS ON AAR WO 1007647-3000-0013 AND WO 711015947.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 20,182 hrs · 15,928 cycles

LONGERON AT STGR 25R CORRODED FS 333 TO FS 364. REMOVED AND REPLACED LONGERON IAW CRJ 900 SRM 51-42-06 AND 51-42-21 AS ON AAR WO 1007647-1300-0039 AND WO 711014360.

Part: STRAP — CORRODED (ZONE 100) · corrosion level 2 · airframe 20,184 hrs · 15,929 cycles

FS 333 CIRCUMFERENTIAL JOINT STRAP CORRODED BETWEEN STR 26L AND 27 - REPAIRED JOINT IAW RO CRJ9-53-0886.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 20,184 hrs · 15,929 cycles

LT SIDE OF 280 FLOORBEAM CORRODED AND CRACKED. REPLACED LT SIDE OF 280 FLOORBEAM IAW RO CRJ9-53-0888.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 20,182 hrs · 15,928 cycles

STGR 24R CORRODED BETWEEN FS 333 TO FS 349. REPAIRED STGR 24R IAW RO CRJ9-53-0884. AS ON AAR WO 1007647-1300-0041 AND WO 711015947.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 20,184 hrs · 15,929 cycles

RT SIDE OF 280 FLOORBEAM CORRODED AND CRACKED. REPLACED RT SIDE OF 280 FLOORBEAM IAW RO CRJ9-53-0887.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 20,184 hrs · 15,929 cycles

FRAME AT FS 364 CORRODED AT STR 27 - REPAIRED FRAME IAW RO CRJ9-53-0883.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 20,182 hrs · 15,928 cycles

STGR 24R SPLICE AT FS 333 CORRODED. REMOVED AND REPLACED SPLICE IAW CRJ 900 SRM 51-42-06 AND 51-42-21. AS ON AAR WO 1007647-1300-0040 AND WO 711014360.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,182 hrs · 15,928 cycles

LT FLOOR SEAT TRACK STICK 5 REQUIRES REPLACEMENT DUE TO CORROSION OUT OF LIMITS. REMOVED AND REPLACED LT NR 5 FLOOR SEAT TRACK IAW CRJ 900 AMM 53-00-49. AS ON WO 1007647-2000-0197 AND WO 711014360.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 20,182 hrs · 15,928 cycles

STGR 25R CORRODED FROM FS 297.00 TO FS 327.00. REMOVED AND REPLACED STRINGER IAW CRJ 900 SRM 51-42-06 AND 51-42-21 AS ON AAR WO 1007647-1300-0022 AND WO 711014360.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 20,184 hrs · 15,929 cycles

FRAME AT FS 333 CORRODED AT STR 27 - REPAIRED FRAME IAW RO CRJ9-53-0885.

Part: BUSHING — DAMAGED (ELEVATOR) · airframe 20,182 hrs · 15,928 cycles

RT ELEVATOR NR 1 HINGE O/B LUG BUSHING PITTED. REMOVED AND REPLACED RT ELEVATOR NR 1 HINGE O/B LUG BUSHING IAW CRJ 900 AMM 20-31-00 AND RO CRJ9-55-0147. AS ON WO 1007647-3000-0022 AND WO 711015947.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 20,184 hrs · 15,929 cycles

STRINGER 23R CORRODED AT FS 333-280. REPLACED STRINGER IAW SRM 51-42-06 & 51-42-23.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 20,184 hrs · 15,929 cycles

STRINGER 26R CORRODED AT FS 333-349. REPLACED STRINGER IAW SRM 51-42-06 & 51-42-21.

Part: SKIN — CHAFED (ZONE 100) · airframe 20,184 hrs · 15,929 cycles

SKIN DAMAGED ABOVE AFT CARGO DOOR FS 985-1000 STRINGERS 13-16L. REPAIRED SKIN IAW RO CRJ9-53-0882.

Part: SKIN — CHAFED (ZONE 100) · airframe 20,184 hrs · 15,929 cycles

SKIN DAMAGED AFT CARGO DOOR SURROUND ABOVE PROTECTOR PLATE FS 1045-1047 STRINGER 16L - REPAIRED SKIN IAW RO CRJ9-53-0881.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 20,184 hrs · 15,929 cycles

STRINGER 27, CORRODED AT FS 314-325. REPLACED STRINGER IAW SRM 51-42-06 & 51-42-22.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 20,184 hrs · 15,929 cycles

STRINGER 22R CORRODED AT FS 280-295. REPLACED STRINGER IAW SRM 51-42-06 & 51-42-23.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 20,184 hrs · 15,929 cycles

MAIN AVIONICS DOOR SURROUND INTERCOSTAL RT OF STRINGER 27 CORRODED. REPLACED INTERCOSTAL IAW SRM 51-42-06 & 51-42-23.

Part: STRINGER — CORRODED (BS 333-349) · corrosion level 2 · airframe 20,184 hrs · 15,929 cycles

STRINGER 26R CORRODED AT FS 333-349 - REPLACED STRINGER IAW SRM 51-42-06 & 51-42-22.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 20,184 hrs · 15,929 cycles

MAIN AVIONICS DOOR SURROUND INTERCOSTAL LT OF STRINGER 27 CORRODED. REPLACED INTERCOSTAL IAW SRM 51-42-06 & 51-42-24.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 20,184 hrs · 15,929 cycles

STRINGER 27 CORRODED AT FS 333-349. REPLACED STRINGER IAW SRM 51-42-06 & 51-42-23.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 20,184 hrs · 15,929 cycles

STRINGER 26L CORRODED AT FS 333-349. REPLACED STRINGER IAW SRM 51-42-06 & 51-42-21.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 20,184 hrs · 15,929 cycles

STRINGER 22R CORRODED AT FS 333-349. REPLACED STRINGER IAW SRM 51-42-06 & 51-42-23.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 20,184 hrs · 15,929 cycles

STRINGER 21R SPLICE CORRODED AT FS 477 - REPLACED STRINGER IAW SRM 51-42-06 & 51-42-21.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 20,184 hrs · 15,929 cycles

FRAME AT FS310 CORRODED BETWEEN STR 26L AND 25R. REPAIRED IAW RO CRJ9-53-0880.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 20,184 hrs · 15,929 cycles

RT FLOOR SEAT TRACK STICK 3 HAS CORROSION. REPLACED SEAT TRACK IAW AMM 53-00-49.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 20,184 hrs · 15,929 cycles

RT FLOOR SEAT TRACK STICK 2 HAS CORROSION. REPLACED SEAT TRACK IAW AMM 53-00-49.

Part: STAND OFF — CORRODED (TRANS COWL) · airframe 20,182 hrs · 15,928 cycles

RT LOWER TRANS COWL INBD STAND OFF IS CRACKED. REMOVED AND REPLACED RT LOWER TRANS COWL INBD STAND OFF IAW CRJ700 SRM 51-42-14 AND 51-42-21 AS ON AAR WO 1007647-4000-0003 AND MESA WO 711014360.

Part: STAND OFF — CORRODED (TRANS COWL) · airframe 20,182 hrs · 15,928 cycles

RT LOWER TRANS COWL OUTBD STAND OFF IS CRACKED. REMOVED AND REPLACED RT LOWER TRANS COWL OUTBD STAND OFF IAW CRJ700 SRM 51-42-14 AND 51-42-21 AS ON AAR WO 1007647-4000-0004 AND MESA WO 711014360.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 20,150 hrs · 15,903 cycles

INBOARD FLIGHT SPOILER SPOILERON CAUTION. RESET.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,936 hrs · 15,712 cycles

CEILING EMERGENCY LIGHT ROW 20 INOP. RELAMPED EMERGENCY LIGHT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 19,812 hrs · 15,602 cycles

ALL EMERGENCY LIGHTS GO OUT DURING TEST. RE-CHARGE EMER BATT PACKS WITH ACFT POWER, TEST GOOD.

Part: ENGINE — VIBRATION (NR 1) · airframe 19,696 hrs · 15,492 cycles

NR 1 ENG N1 VIB REACHED 1.8 IN FLT. SHOOK BLADES AND COMPLIED WITH THE RO CRJ9-72-0111.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,489 hrs · 15,311 cycles

CEILING EMERGENCY FLOOD LIGHT ROW 4 INOP. RELAMPED EMERGENCY LIGHT.

Part: OXYGEN MASK — DEPLOYED (CABIN) · airframe 19,467 hrs · 15,291 cycles

RTG - ALL PAX O2 MASKS DEPLOYED. INSPECT AND REPACK ALL MASKS.

Part: PROXIMITY SENSOR — OUT OF ADJUST (LANDING GEAR) · airframe 19,027 hrs · 14,879 cycles

INTERMITTENT PROX SYSTEM 1 FAULT. ADJSTED NR 1 WOW PX 02 NEAR.

Part: PROXIMITY SENSOR — OUT OF ADJUST (LT MLG) · airframe 19,019 hrs · 14,873 cycles

PROX SYS FAULT 1 INTERMIT ON TAXI. ADJUSTED LT GEAR WOW (PX102) SENSOR.

Part: PUMP — INTERMITTENT (FUEL SYSTEM) · airframe 18,964 hrs · 14,829 cycles

CROSSFLOW PUMP CAUTION AFTER LAND. RESET PUMP.

Part: SERVICE DOOR — NOT CLOSED (CABIN) · airframe 18,833 hrs · 14,715 cycles

PROX SYSTEM 2 FAULT. CLOSED SERVICE DOOR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,826 hrs · 14,709 cycles

ROW 17 OVERHEAD EMER FLOOD INOP. RELAMPED EMERGENCY LIGHT.

Part: ENGINE — VIBRATION (RIGHT) · airframe 18,791 hrs · 14,677 cycles

RT ENG N1 VIBE 1.2 DURING CLIMB. SHOOK BLADES RAN ENGINE VIBE WENT TO 0.4.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,760 hrs · 14,649 cycles

ROW 2 OVERHEAD EMERGENCY LIGHT INOP. R2 OVERHEAD LIGHT BULB.

Part: SENSOR — OUT OF ADJUST (EMERGENCY EXIT) · airframe 18,680 hrs · 14,591 cycles

FWD LT EMERGENCY DOOR CAUTION ON GROUND. MX ADJUSTED PX 43 SENSOR AND CLEANED TARGET.

Part: SENSOR — DIRTY (EMERGENCY EXIT) · airframe 18,386 hrs · 14,326 cycles

RT FWD EMERGENCY DOOR CAUTION MSG. MX CLEANED SENSOR.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 18,201 hrs · 14,169 cycles

FWD F/A LED FLASHLIGHT INOP. MX R2 FLASHLIGHT.

Part: SENSOR — DIRTY (EMERGENCY EXIT) · airframe 18,162 hrs · 14,133 cycles

LT FWD EMERGENCY DOOR CTN INTERMITTENT. MX CLEANED SENSOR PX43.

Part: DOOR — UNSECURE (LEFT) · airframe 18,110 hrs · 14,075 cycles

LT AFT EMERGENCY LIGHT CAUTION MESSAGE AFTER LANDING. MX RE-SEATED DOOR.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 18,096 hrs · 14,065 cycles

F/O FLASHLIGHT INOP. MX REPLACED THE BATTERY.

Part: SENSOR — OUT OF RIG (NLG) · airframe 18,039 hrs · 14,016 cycles

NLG DOOR OPEN WARNING, STAGE OF FLIGHT NOT REPORTED, POSSIBLY DURING CLIMB. AIRCRAFT RTF. MX RIGGED NOSE GEAR DOOR SENSOR PX31, OPS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,989 hrs · 13,974 cycles

OVERHEAD EMERGENCY CEILING LIGHT OUT. MX RELAMPED EMERGENCY FLOOD LIGHT OPS GOOD.

Part: SPRING — WORN (CABIN DOOR) · airframe 17,948 hrs · 13,938 cycles

MAIN ENTRY DOOR FREE FALLS TOO FAST. MX REPLACED AFT GAS SPRING.

Part: SEAL — LEAKING (NR 2 ENGINE) · airframe 17,870 hrs · 13,872 cycles

FUEL LEAK FROM DRAIN MAST. MX R2 NR 2 ENG FUEL FEED LINE SEAL.

Part: SEAL — LEAKING (NR 2 ENGINE) · airframe 17,869 hrs · 13,871 cycles

AFT FUEL DRAIN MAST DISCHARGING FUEL. MX R2 NR 2 ENG FUEL FEED LINE SEAL. SAME CORRECTIVE ACTION AS MASA2010120801412. REPAIR COMPLETED ON 12/8/10.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,734 hrs · 13,745 cycles

ROW 20 EMERGENCY FLOOD LIGHT INOP. MX RELAMPED.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 17,726 hrs · 13,739 cycles

FWD F/A EMERGENCY FLASHLIGHT INOP. MX REPLACED FLASHLIGHT.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 17,726 hrs · 13,739 cycles

CAPT EMERGENCY FLASHLIGHT INOP. MX REMOVED AND REPLACED CAPT EMERGENCY FLASHLIGHT BATTERY, OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,626 hrs · 13,645 cycles

ONE CEILING FLOOD LT INOP. MX RELAMPED.

Part: FADEC — FAULTY (RT ENGINE) · airframe 17,586 hrs · 13,615 cycles

UNCOMMANDED RT ENG S/D AFTER LANDING. MX REPLACED THE RIGHT FADEC.

Part: SENSOR — DIRTY (RT ENGINE) · airframe 17,586 hrs · 13,615 cycles

RIGHT ENGINE ABORT CTN / AUTO S/D. MX CLEANED THE N2 SENSOR, FADEC, & THROTTLE QUADRANT CONNECTORS.

Part: PLACARD — DAMAGED (STAIRS) · airframe 17,389 hrs · 13,449 cycles

STAIRS OPEN PLACARD DAMAGED. MX REMOVED AND REPLACED ASD OPEN PLACARD, NO OTHER DEFECTS NOTED.

Part: QUICK DISCONNECT — UNSECURE (BRAKE SYSTEM) · airframe 17,303 hrs · 13,371 cycles

AFTER LANDING CREW NOTED NR 1 BRAKE TEMP AT 3 & NR 2 AT 7. MX SECURED QD AND BLED HYD SYSTEM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,019 hrs · 13,131 cycles

CEILING EMERGENCY FLOOD LIGHT INOP. MX RELAMPED EMERGENCY LIGHT.

Part: GLAND NUT — CORRODED (MLG) · airframe 16,448 hrs · 12,678 cycles

CORROSION FOUND IN MLG OUTER CYL GLAND NUT THREADS AND IN CHROME OF STRUT ASSY IN EXCESS OF LIMITS PER BOMBARDIER REO 670-32-11-221-REV A, AND GOODYEAR SCR 0003-07 REV NC. MX REPLACED OUTER CYLINDER ASSEMBLY.

Part: TRANSDUCER — MALFUNCTIONED (NR 3) · airframe 16,459 hrs · 12,687 cycles

THE CREW ABORTED TAKEOFF DUE TO A SENSATION OF BRAKES GRABBING FOLLOWED BY A "R ANTI-SKID INBD" CAUTION MESSAGE. THE CREW DECELERATED ENOUGH TO EXIT THE RUNWAY. WHILE ON THE TAXIWAY HEADED BACK TO THE GATE THE NR 3 & 4 MLG TIRES BLEW. MX REMOVED AND REPLACED THE LOWER PISTON, NR 3 AND NR 4 TIRES AND BRAKES, AND THE NR 3 WHEEL SPEED TRANSDUCER. PARTS INVOLVED: TIRE P/N 90001200-1 S/N MAR04-0184, TIRE P/N 90001200-1 S/NAPR05-0380, PISTON AXLE ASSY P/N 49203-5 S/N SPP530034, WHEEL SPEED TRANSDUCER P/N 6007047 S/N SEP03-1152, BRAKE P/N 90001201 S/N APR03-0064, BRAKE P/N 90001201 S/N S-FEB06-0017.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 16,387 hrs · 12,628 cycles

EMERGENCY LIGHTS STAY ON IN ARM POSITION. RE-RACKED JB11.

Part: TRANSDUCER — FAULTY (ANTI-SKID SYS) · airframe 16,305 hrs · 12,567 cycles

ANTI SKID OUTBOARD CAUT AND NR 4 MAIN TIRE BLEW ON TAXI CHECK. R2 NR 4 WHEEL SPEED TRANSDUCER AND R2 TIRES NR 3 AND NR 4. COMPLIED WITH TAXI.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,577 hrs · 11,948 cycles

ROW 7 EMERGENCY FLOODLIGHT OUT. REPLACED ROW 7 EMERGENCY FLOODLIGHT BULB.

Part: SENSOR — DIRTY (EMERGENCY EXIT) · airframe 14,091 hrs · 10,707 cycles

ASH FLT 2884 PHX. CREW RETURNED TO THE GATE DUE TO LEFT FWD EMERGENCY DOOR CAUTION MESSAGE. MX CLEANED DOOR SENSOR AND SILL AND OPS CHECKED GOOD.

Part: SMOKE DETECTOR — ACTIVATED (AFT LAVATORY) · airframe 13,447 hrs · 10,153 cycles

ASH 2774 PHX. CREW RETURNED TO THE FIELD DUE TO AFT LAV SMOKE WARNING. MX INSPECTED SMOKE DETECTOR, OPS NORMAL.

Part: SMOKE WARNING — ACTIVATED (COCKPIT) · airframe 13,394 hrs · 10,099 cycles

ACFT RETURNED TO GATE DUE TO FWD LAV SMOKE WARNING. MX RAN ENGINES AND NO SMOKE OR WARNINGS NOTED. MX SERVICED APU OIL TO PROPER LEVEL AND CLEARED OUT DRAIN LINES.

Part: SMOKE WARNING — ACTIVATED (COCKPIT) · airframe 13,380 hrs · 10,090 cycles

CREW ABORTED TAKEOFF DUE TO FWD LAV SMOKE WARNING ON TAKEOFF ROLL. MX SERVICED APU OIL PROPER LEVEL AND CLEARED OUT DRAIN LINES.

Part: FAN — MALFUNCTIONED (FWD LAVATORY) · airframe 13,363 hrs · 10,077 cycles

ASH FLT 2964 PHX-MZT. SMOKE FWD LAV WARNING - SMOKE FORWARD GALLEY. MX R&R GALLEY EXHAUST FAN.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,171 hrs · 8,900 cycles

ASH 2812 PHX-OKC - PILOT REPORTED THAT THE EMERGENCY CEILING LEVEL FLOOD LIGHT 3RD FROM FRONT IS INOP. MX RELAMPED AND OPS CHECKED GOOD.

Part: ELT — UNKNOWN · airframe 11,611 hrs · 8,786 cycles

ASH FLT 2681 CLT-ATL - ELT ON CAUTION MESSAGE. MX REPLACED THE ELT, OPS CHECK GOOD.

Part: DOOR — OUT OF ADJUST (EMERGENCY EXIT) · airframe 11,491 hrs · 8,685 cycles

ASH FLT 2934 PHX-MEM. LEFT FWD EMERGENCY DOOR CAUTION TRANSIENT MESSAGE DURING LANDING. MX CLEANED AND ADJUSTED DOOR. OPS GOOD.

Part: BRACKET — BROKEN (OXYGEN BOTTLE) · airframe 11,193 hrs · 8,449 cycles

ASH FLT 2632 CLT-ORF - FWD POB HOLD DOWN CLIP BROKEN. MX CHANGED HOLD DOWN CLIP.

Part: GLOWSTRIP — INOPERATIVE (CABIN) · airframe 10,786 hrs · 8,121 cycles

ASH FLT 2834 (INBOUND) TUS - EXIT PATH STRIP PHOTO ILLUM IN EXIT ROW INOP. REMOVED AND REPLACED LIGHT STRIP.

Part: LATCH — STIFF (PAX DOOR) · airframe 10,565 hrs · 7,922 cycles

ASH 2824 PHX-TUS - PAX DOOR DIFFICULT TO UNLATCH. MX CYCLED DOOR AND DOOR LATCH SEVERAL TIMES. FOUND NO DEFECTS IN THE PROCESS.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILERS) · airframe 8,003 hrs · 5,829 cycles

ASH 2716 PHX - AIRCRAFT HAD A FLIGHT SPOILERS FAULT STATUS MESSAGE. MX RESET THE SSCU.

Part: STALL WARNING — CONTAMINATED · airframe 7,477 hrs · 5,443 cycles

ASH 2959 AUS. STALL SYSTEM FAILED. MX FERRIED TO PHX, PURGED THE WATER.

Part: RELAY — FAILED (THRUST REVERSER) · airframe 7,444 hrs · 5,419 cycles

ASH 2730 DSM. LEFT T/R UNSAFE MESSAGE ON TAKEOFF ROLL. MX REPLACED K29 RELAY.

Part: PCU — MALFUNCTIONED · airframe 7,284 hrs · 5,294 cycles

ASH 2783 IAH. OUTBOARD SPOILERS AND SPOILERONS CAUTION MESSAGE. MX REMOVED AND REPLACED RIGHT OUTBOARD PCU.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 7,232 hrs · 5,249 cycles

ASH 2686 MCI. RTL STATUS MESSAGE. MX PERFORMED SPOST 1/2. NO FURTHER DEFECTS NOTED.

Part: CONTROL UNIT — MALFUNCTIONED (STABILIZER SYS) · airframe 7,168 hrs · 5,185 cycles

ASH 2617 CLT. PITCH FEEL FAULT. MX REMOVED AND REPLACED SSCU.

Part: WARNING MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 7,165 hrs · 5,184 cycles

ASH 2617 EWR. PITCH FEEL FAULT STATUS MESSAGE. MX RESET THE SYSTEM AND FAULT CLEARED.

Part: WARNING SYSTEM — MALFUNCTIONED (RUDDER) · airframe 7,109 hrs · 5,140 cycles

ASH 2779 PHX - RUDDER LIMIT FAULT. MX PERFORMED SPOST. NO FURTHER DEFECTS NOTED.

Part: ODOR — DETECTED (CABIN) · airframe 7,180 hrs · 5,139 cycles

ASH 2908 TUS - ABORTED TAKEOFF AND RTG DUE TO LAVE SMOKE CAUTION/SMELL OF SMOKE IN CABIN. COMP WASH RESIDUE CAUSING THE SMELL AND SMOKE. MX PERFORMED ENGINE RUNS AND CLEARED DISCREPANCIES WITH NO FURTHER ISSUES NOTED.

Part: PROXIMITY SWITCH — OUT OF ADJUST (PAX DOOR) · airframe 6,656 hrs · 4,767 cycles

ASH 6434 TUS - PAX DOOR OUTER HANDLE CAUTION MESSAGE. PLACED ON MEL. MX R2 OUTER HANDLE PROX SENSOR SWITCH PX107.

Part: CAUTION MESSAGE — ILLUMINATED (SPOILIERS) · airframe 6,182 hrs · 4,414 cycles

ASH 6263 PHX. SPOILERONS ROLL CTN MSG. MX RESET SPOILER ROLL DISCONNECT SYSTEM. OP'S CHECK GOOD.

Part: WARNING MESSAGE — ILLUMINATED (SPOILERS) · airframe 5,918 hrs · 4,208 cycles

ASH 5010 DFW - SPOILER STAB FAULT. PERFORMED SPOST 1 W/FLIGHT CREW. NO FURTHER DEFECTS NOTED.

Part: WARNING MESSAGE — ILLUMINATED (SPOILERS) · airframe 5,897 hrs · 4,188 cycles

ASH 5094 STL - SPOILER STAB FAULT STATUS MESSAGE. MAINTENANCE RESET.

Part: WARNING MESSAGE — ILLUMINATED (SPOILERS) · airframe 5,890 hrs · 4,182 cycles

ASH 5094 STL - SPOILER/STAB FAULT STATUS MESSAGE. MAINTENANCE RAN SPOST. OP'S CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILERS) · airframe 5,861 hrs · 4,152 cycles

ASH 5012 ATL - SPOILER STAB FAULT STATUS MESSAGE. RESET SSCU WITH CREW. OP'S CHECK GOOD.

Part: SEAT — LACK OF LUBE (FA JUMPSEAT) · airframe 5,799 hrs · 4,094 cycles

ASH 5011 CLT - FWD FA JUMPSEAT WAS STUCK IN THE DEPLOYED POSITION BLOCKING THE FLIGHT DECK DOOR. MX LUBED THE SEAT TRACKS. OP'S CHECK AND STOWED GOOD.

Part: WARNING MESSAGE — ILLUMINATED (SPOILER) · airframe 5,790 hrs · 4,082 cycles

ASH 5088 CLT - SPOILER STAB FAULT STATUS MESSAGE. MOC RESET THE SYSTEM WITH CREW.

Part: SPOILER SYS — FAULTED · airframe 5,745 hrs · 4,041 cycles

ASH 6611 SEA - SPOILER/STAB FAULT ON INITIAL POWER UP. PERFORMED SPOST 1 W/FLIGHT CREW. NO FURTHER DEFECTS NOTED.

Part: UNKNOWN — UNKNOWN · airframe 5,769 hrs · 4,065 cycles

ASH 6611 SEA - SPOILER STAB FAULT STATUS MESSAGE. PERFORMED SPOST TEST WITH CREW. OP'S CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 4,678 hrs · 3,246 cycles

ASH 6104 PHX - RT AFT EXTERIOR EMERGENCY EXIT LIGHT INOP. MX RELAMPED.

Part: LENS — MISSING (EMGCY EXIT SIGN) · airframe 3,832 hrs · 2,684 cycles

RED LIGHT LENS COVER ON EMERGENCY EXIT SIGN IS MISSING. MX REPLACED THE LENS COVER.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 1,412 hrs · 990 cycles

REJECTED TAKEOFF FOR A F/O WINDSHIELD SHATTERED ON TAKEOFF ROLL. AIRCRAFT WAS FERRIED TO PHX FOR REPAIR. 9/4/04 MAINTENANCE REPLACED THE RT CO-PILOT WINDSHIELD.