N654BR

Part: PSEU — MALFUNCTIONED (MLG) · airframe 15,124 hrs · 17,139 cycles

ASH FLT 1028 HNL - GEAR DISAGREE WITH NOSE DOOR OPEN WARNING MESSAGE. REPLACED PSEU AND RIGGED UPLOCK SENSOR.

Part: LIFE VEST — TORN · airframe 14,887 hrs · 16,611 cycles

ASH FLT 1023 HNL-KOA - 2 INFANT LIFE VEST WERE TORN. MX REPLACED THE LIFE VESTS.

Part: LIFE VEST — MISSING (CABIN) · airframe 14,485 hrs · 15,721 cycles

ASH 1020 HNL-LIH. SEAT 11A LIFE VEST WAS MISSING. MX INSTALLED A NEW LIFE VEST.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 14,471 hrs · 15,688 cycles

ASH 1019 HNL-OGG - PILOT REPORTED THE FLOOR LEVEL EMERGENCY LIGHT STRIP AT ROW 6 WAS OUT. MX, RELAMPED.

Part: LIFE VEST — MISSING (CABIN) · airframe 14,458 hrs · 15,659 cycles

ASH RON HNL. THREE ADULT LIFE VEST AND 1 INFANT LIFE VEST WERE MISSING. MX INSTALLED NEW LIFE VESTS.

Part: SECU — MALFUNCTIONED (SPOILER SYS) · airframe 12,674 hrs · 11,646 cycles

ASH 1027 HNL - INBD GND SPOILER STATUS MESSAGE. MX RESET THE SECU UNITS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,560 hrs · 11,411 cycles

ASH 1026 HNL. LEFT HAND EMERGENCY EXIT LIGHT INOP. MX RELAMPED THE LIGHT.

Part: PROXIMITY SWITCH — DIRTY (NLG) · airframe 12,328 hrs · 10,876 cycles

ASH 1007 HNL - NLG STAYED YELLOW ON GEAR EXTENSION ON FIRST TRY. MX CLEANED PROX SWITCH AND PERFORMED GEAR SWINGS. OP'S CHECK GOOD.

Part: STRIP — CRACKED (CABIN) · airframe 12,443 hrs · 10,678 cycles

ASH HNL. EMERGENCY FLOOR LIGHT STRIP CRACKED. MX REPLACED THE LIGHT STRIP.

Part: FRAME — CRACKED (FUSELAGE) · airframe 11,303 hrs · 9,754 cycles

RT FS 640 FRAME DOUBLER CRACKED IN RADIUS AT 3.0 IN LENGTH.

Part: SUPPORT BEAM — CRACKED (RT ENGINE) · airframe 11,303 hrs · 9,754 cycles

RT ENGINE SUPPORT BEAM CRACKED IN LOWER WEB AT 0.75 IN.

Part: RIB — CRACKED (RT WING) · airframe 11,303 hrs · 9,754 cycles

RT BATTERY RIB CRACKED 0.75 IN BETWEEN ATTACHING FASTENERS.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 11,303 hrs · 9,754 cycles

PAX DOOR FRAME TOP RADIUS CRACKED AT 1.0 IN LENGTH FORWARD OF DATUM 1 AT FS 338.90.

Part: RIB — CRACKED (LT WING) · airframe 11,303 hrs · 9,754 cycles

LT BATTERY RIB CRACKED 1.5 IN.

Part: SUPPORT BEAM — CRACKED (LT ENGINE) · airframe 11,303 hrs · 9,754 cycles

LT ENGINE SUPPORT BEAM CRACKED IN LOWER WEB AT 0.75 IN.

Part: STALL WARNING — ACTIVATED (COCKPIT)

STALL FAIL MESSAGE ON TAKEOFF. FOUND AOA VANE DISAGREE CODE.

Part: PISTON — NOT SEATED (NLG STRUT)

EVENT SUMMARY NOSE GEAR DOOR DISAGREE. FOUND NLG STRUT PISTON TO NOT BE FULLY SEATED. SEATED PISTON & SERVICED NLG. PERFORMED GEAR SWINGS WITH NO DEFECTS NOTED.

Part: POWER SUPPLY — DISCHARGED (EMERGENCY LIGHT)

DURING INSPECTION THE FORWARD EXTERNAL EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB AND BATTERY WERE REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT)

DURING INSPECTION THE LEFT AND RIGHT HAND EMERGENCY LIGHTS WERE FOUND INOPERATIVE. THE BATTERY CHARGER WAS FOUND INOPERATIVE AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL UNIT — FAULTY (TE FLAPS) · airframe 7,878 hrs · 6,570 cycles

DURING OPERATION OF AIRCRAFT THE CREW REPORTED A FLAP CONTROL SYSTEM FAILURE AT ZERO DEGREES. FLIGHT LANDED UNEVENTFULLY AND PASSENGERS DEPLANED NORMALLY. THE LEFT BRAKE PRESSURE SENSING UNIT AND THE FLAP ELECTRONIC CONTROL UNIT WERE REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE.

Part: ACTUATOR — FAILED (T/E FLAP)

DURING APPROACH TO YYZ ON FLT 7218 CREW REPORTED FLAP FAIL WHEN SELECTING FLAPS 8 DEGREES. CREW DECLARED AN EMERGENCY AND PERFORMED A ZERO FLAP LANDING. FLIGHT LANDED WITHOUT INCIDENT AND PASSENGERS DEPLANED NORMALLY AT GATE. THE BPSU AND FLAP ACTUATOR WERE FOUND TO BE THE CAUSE OF THE FLAP FAIL AND WERE REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE.

Part: SKIN — OUT OF LIMITS (FUSELAGE) · airframe 7,382 hrs · 6,166 cycles

DURING HEAVY INSPECTION A REPAIR TO THE FUSELAGE SKIN WAS MADE AT FS 625-640 AND STRINGER 20-21 ON THE LEFT HAND SIDE. REPAIRED WITH DOUBLER, HI LITE, AND COLLAR.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 7,382 hrs · 6,166 cycles

DURING HEAVY INSPECTION THE FLOOR SUPPORT ANGLE AT FS 621 BL 41 WAS FOUND CRACKED.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 7,382 hrs · 6,166 cycles

DURING INSPECTION THE LT HAND FLOOR SUPPORT ANGLE AT FS 621 BL 41 WAS FOUND CRACKED.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 7,219 hrs · 6,031 cycles

DURING INSPECTION THE EMERGENCY LIGHT 2ND FROM REAR WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

DURING MAINTENANCE INSPECTION, THE NR 3 RT EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LAMP

During preflight inspection, the crew reported that the r/h fwd exterior emergency exit light was inoperative. Maintenance personnel removed and replaced the lamp in the emergency exit light. An operational check was satisfactory and the aircraft was returned to service.

Part: BATTERY — FAILED (CABIN)

PASSENGER DOOR EMERGENCY LIGHTS FAILED. REMOVED AND REPLACED NR 1 BATTERY POWER SUPPLY. MAINTENANCE PERSONNEL PERFORMED OPERATIONAL CHECK OF EMERGENCY LIGHTING SYSTEM AND RELEASED AIRCRAFT FOR CONTINUED SERVICE.