N347AG

Part: LATCH — DIRTY (CABIN DOOR) · airframe 37,138 hrs · 41,429 cycles

FLIGHT 0142 FPO/FLL. MAIN CABIN DOOR INSIDE RELEASE LATCH NOT RELEASING PROPERLY. CLEANED & LUBE CABIN DOOR RELEASED LATCH IAW AMM 52-10-00. CABIN DOOR RELEASE LATCH OPS CHECKED NORMAL.

Part: SPRING — LACK OF LUBE (LATCH) · airframe 36,862 hrs · 41,134 cycles

MAIN CABIN DOOR MUST BE FORCED TO LATCH OPEN. CLEANED AND LUBRICATED THE LATCH SPRING. OPS CHECKED GOOD IAW AMM 52-10-00-05.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 35,606 hrs · 39,828 cycles

FLIGHT 0073, CABIN EMERGENCY LIGHT STAY ON HALF OF THE CABIN WITH EMERGENCY LIGHT SWITCH OFF POSITION. R&R EMERGENCY LIGHT POWER SUPPLY IAW AMM 33-50-10-04-1, OPS CHECK GOOD IAW AMM 33-50-00.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 35,123 hrs · 39,317 cycles

EMERGENCY LIGHTS IN CABIN INOPERATIVE FROM EXIT ROW AFT. R & R THE BATTERY PACK ON 24LN IAW AMM 33-50-10-04-01. OPS CHECKED GOOD, NO DEFECTS NOTED. PERFORMED OPS TEST IAW AMM 33-50-00, OPS TESTED GOOD.

Part: SPRING — DEFECTIVE (AIRSTAIRS) · airframe 34,449 hrs · 38,592 cycles

PNS-MCO REPORT, ENTRANCE STAIRS NOT EXTENDING. R&R AIRSTAIR GAS SPRING IAW AMM 20-10-00. OPS CHECK GOOD.

Part: BULB — BURNED OUT (CONTROL PANEL) · airframe 33,893 hrs · 37,893 cycles

FLIGHT 0094, FLIGHT ATTENDANT REPORTED THAT ON EMERGENCY PANEL, THE EMERGENCY LIGHT IS NOT TURNING ON. R & R BULB ON THE EMERGENCY LIGHT PUSH BUTTON IAW AMM 33-50-00. OPS CHECKED NORMAL.

Part: TIRE — MISSING (NLG) · airframe 33,893 hrs · 37,986 cycles

FLIGHT 94, DURING POST FLIGHT INSPECTION, FOUND RIGHT NOSE WHEEL TIRE MISSING. R & R NLG SHOCK STRUT, OPS AND LEAK CHECK GOOD.

Part: RAIL — DIRTY (PAX DOOR) · airframe 33,496 hrs · 37,549 cycles

MCD HAS DIFFICULTY SLIDING CHECK FOR OPERATION. CLEANED INSIDE OF RAIL AND SLIDING UNIT IAW 52-60-05-02 D1.

Part: LIGHT — UNKNOWN (COCKPIT) · airframe 33,413 hrs · 37,450 cycles

EMERGENCY LIGHT ARMED LIGHT ON F/A PANEL FLICKERED WHEN EMERGENCY LIGHTS WERE ARMED. PERFORMED OPS CHECK NO DEFECT NOTED IAW 33-50-60.

Part: DOOR — STUCK (LT MLG) · airframe 33,173 hrs · 37,063 cycles

LEFT SIDE INBD MLG DOOR WAS FOUND TO BE OPEN DURING FLIGHT. ONCE ON THE GROUND CREW NOTICED A CHUNK OF ICE WAS KEEPING THE DOOR FROM CLOSING. REMOVED ICE FROM L/E OF LT INBD LANDING GEAR DOOR. CHECKED IAW AMM 32-12-10-02. DOOR IS CLOSED AS REQUIRED. NO DEFECTS NOTED.

Part: SWITCH — UNKNOWN (LT WOW) · airframe 33,070 hrs · 36,894 cycles

GEAR HANDLE WOULD NOT COME UP FOR ABOUT 15 MINS IN FLIGHT AND THE FLIGHT IDLE STOP REMAINED OPEN AS WELL. POSSIBLE WOW SWITCH MALFUNCTION. R & R LT INBD WOW SWITCH IAW AMM REF 32-31-10, OPS CHECK GOOD.

Part: PDU — FAILED (LEFT GENERATOR) · airframe 33,031 hrs · 36,825 cycles

LT GENERATOR FAILED INFLIGHT. R & R LT PDU IAW AMM 24-31-20.

Part: DOOR — MISSING (NR 2 NACELLE) · airframe 32,608 hrs · 36,232 cycles

AT ROTATION, F/A NOTIFIED CREW OF NR 2 ENGINE MISSING INSIDE COVER. EMERGENCY DECLARED. AIR RETURN WAS NORMAL. POST INSPECTION SHOWS COWL MISSING ON NR 2 ENGINE. R & R FWD COWLINGS AND FRAMES IAW AMM 71-10-05-04.

Part: OVERHEAT SENSOR — FAILED (RT BLEED SYS) · airframe 32,525 hrs · 36,147 cycles

RT BLEED AIR LEAK ILLUMINATED. RAN THE QRH, THE LIGHT WENT OUT THEN CAME BACK ON. WE RAN THE QRH AGAIN AND SHUT THE NR 2 ENGINE DOWN. HEAVY SOOT DEPOSITS IN DUCT AREA. LOOP INSULATOR GROMMETS ON AFT ELEMENT DRY-ROTTED. R & R RT NACELLE DUCT ASSY ELEMENT SENSOR, PN: 51533-378. R & R RT NACELLE ENGINE AFT BLEED DUCT. OPS CHECKED GOOD. R & R LOOP INSULATOR GROMMETS.

Part: OVERHEAT SENSOR — BENT (RT BLEED SYS) · airframe 32,523 hrs · 36,144 cycles

RT BLEED AIR LEAK ILLUMINATED. IT EXTINGUISHED AND RE-ILLUMINATED. WE RAN QRH WITH 2 RESET ATTEMPTS, THEN SHUTDOWN THE NR 2 ENGINE. ALL PARAMETERS OTHER. R & R ELEMENT SENSING OVER HEAT TUBE IAW AMM 36-23-10-02. OPS CHECK GOOD ON GROUND.

Part: OVERHEAT SENSOR — BENT (RT BLEED SYS) · airframe 32,523 hrs · 36,144 cycles

RIGHT BLEED AIR LEAK ILLUMINATED. IT EXTINGUISHED AND RE-ILLUMINATED. WE RAN QRH WITH 2 RESET ATTEMPTS, THEN SHUTDOWN THE NR 2 ENGINE. ALL PARAMETERS OTHER. R & R ELEMENT SENSING OVER HEAT TUBE IAW AMM 36-23-10-02. OPS CHECK GOOD ON GROUND.

Part: HANDLE — OBSTRUCTED (PAX DOOR) · airframe 31,932 hrs · 35,543 cycles

MAIN CABIN DOOR WOULD NOT CLOSE. RESET AIRSTAIR DOOR HANDLE, OPS CHECK NORMAL.

Part: INDICATOR — MALFUNCTIONED (LT AIRSPEED) · airframe 30,971 hrs · 34,475 cycles

DURING FLIGHT AT FL 190 LT AIRSPEED INDICATOR WENT OVER 250 KNOTS AND RUDDER LIMIT INDICATOR ON, OAT -10 DEGREES RT AIRSPEED INDICATOR WAS READING 140 AND STBY 160, THEN THE LT AIRSPEED WENT 0 BELOW 8,000 FT ALL INDICATOR WERE READING NORMAL. INSPECTED LT STBY, RIGHT PITOT TUBES AND WATER TRAPS. DRAIN WATER FROM TRAPS ALL CHECKED GOOD, ALSO CHECKED ADC PITOT/STATIC CONNECTION ALL CHECKS GOOD.

Part: INDICATOR — INOPERATIVE (AIR SPEED) · airframe 30,578 hrs · 34,031 cycles

DISCREPANCY EXIST BETWEEN AIRSPEED 80 KNOTS IN FLIGHT AND LOST LT AIRSPEED INDICATION, DECLARED AN EMERGENCY LANDED WITHOUT INCIDENT. REPLACED LT AIRSPEED INDICATOR OPS TEST OK.

Part: SENSOR — MALFUNCTIONED (PROPELLER SPEED) · airframe 30,572 hrs · 34,025 cycles

DURING CRUISE, LEFT PROPELLER DROPPED FROM 1230-1100 RPM, FOLLOWED BY A DROP FROM 1230-800 RPM TWICE WAS NOT AN INDICATION EVENT, RETURNED TO DEPARTURE, LANDED WITHOUT INCIDENT. REPLACED PROPELLER SPEED INDICATOR AND SPEED SENSOR.

Part: RELAY — INTERMITTENT (EADI) · airframe 29,426 hrs · 32,712 cycles

CAPTAIN AND F/O PRIMARY AVIONICS EADI EHSI FAILURE. PULLED AND RESET DPU1 AND DPU2 CIRCUIT BREAKERS ALL SCREENS CAME BACK UP AND OPS CHECKED GOOD. REPLACED NR 1 DPU AND 69PC TO 70PC RELAYS, OPS CHECKED GOOD.

Part: TIRE — MISSING (NR 2) · airframe 28,821 hrs · 32,012 cycles

FLIGHT 4012. ON LANDING, TOWER INFORMED CREW OF MISSING NR 2 TIRE. INSTALLED NR 2 TIRE.

Part: ROLLER — STICKING (CABIN DOOR) · airframe 28,706 hrs · 31,834 cycles

FLIGHT:3607 ATL/MEI MAIN CABIN DOOR WILL NOT CLOSE. FOUND ROLLER STICKING. RESET DOOR ROLLER, OPERATIONAL CHECK GOOD.