N416QS

Part: DOOR SEAL — TORN (ZONE 200) · airframe 7,084 hrs · 5,484 cycles

DOOR SEAL SQUEAL DURING CLIMB OUT BETWEEN 14,000 AND 20,000 AND DESCENT 8,500 AND 6,000 DELTA P 3.3PSI. SMALL DAMAGE TO SEAL ON FUSELAGE FRAME TOP LEFT CORNER. CORRECTIVE ACTION: REPLACED MED SEAL WORK PERFORMED IAW EMBRAER PHENOM 300 AMM CH. 52-10-20. PERFORMED PRESSURIZATION OF AIRCRAFT IAW EMBRAER PHENOM 300 AMM CH. 21-31-00. OPS CHECK GOOD. NO LEAKS NOTED.

Part: POWER SUPPLY — DEFECTIVE (ZONE 200)

AFTER ENGINE START AND WITH EMERGENCY LIGHT SWITCH IN ARM SOME OF THE CABIN EMERGENCY LIGHTS ILLUMINATED. MOVING SWITCH TO OFF DID NOT EXTINGUISH THE LIGHTS. A COUPLE CEILING LIGHTS WERE ILLUMINATED AND DOOR STEP LIGHTS. EXIT SIGNS WERE NOT ILLUMINATED. CORRECTIVE ACTION: REPLACED EMERGENCY BATTERIES IAW EMB-505S AMM 33-52-1 OPS CHECK GOOD

Part: INTERFACE UNIT — DEFECTIVE · airframe 6,314 hrs · 4,898 cycles

GEA 2 FAIL WHITE CAS: DURING CRUISE FLIGHT AT FL410 WE RECEIVED A WHITE GEA 2 FAIL CAS. THIS WAS ACCOMPANIED BY YELLOW E2 FUEL IMP BYPASS, YELLOW A-I E1 FAIL, WHITE FUEL2 FEED FAULT, AND WHITE ENG NO DISPATCH. ALL SYNOPTIC SCREENS SHOWED MULTIPLE FAILED EQUIPMENT WITH YELLOW X INDICATION. RIGHT MAIN GEAR SHOWED RED BOX TRANSITION INDICATION. TRIM INDICATIONS WERE FAILED, AS WELL AS E2 OIL AND FUEL FLOW INDICATIONS. CORRECTIVE ACTION: REPLACED GEA #2 IAW EMB-505 AMM 31-41-03. OPS CHECK GOOD. NO DEFECTS NOTED.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 5,959 hrs · 4,624 cycles

CABIN EMERG LIGHT: AFTER TURNING OFF EMER LIGHT SWITCH IN COCKPIT, AND TURNING THE BATTERIES OFF, THE CABIN EMER LIGHTS CONTINUED TO STAY ON. PERFORMED ,LIGHT CHECK OF THE EMERGENCY OPERATIONAL LIGHTS IAW AMM CHAPTER 33-52-00. NO FAULT DISCREPANCIES NOTED

Part: CONTROL UNIT — FAULTED (BRAKE SYS) · airframe 5,909 hrs · 4,588 cycles

BRK FAIL YELLOW CAS: ON TAXI, YELLOW BRAKE FAIL MESSAGE ILLUMINATED. NEITHER PILOTS BRAKES WERE OPERATIONAL WITH THE CAS ILLUMINATED. HAD TO USE EMERGENCY BRAKE TO STOP AIRCRAFT FROM TAXIING. REMOVED "FAULTY" BRAKE CONTROL MODULE DAP00101-02 SN 019RK AND INSTALLED A "REPAIRED" UNIT PN: DAP00101-02. SN 75LP. BLED SYSTEM AND PERFORMED FUNCTIONAL CHECK. AS A PERCAUTION, PERFORMED TAXI CHECK WITH NO FAULTS OR DEFECTS NOTED. ALL WORK ACCOMPLISHED IN REFERENCE TO EMB AMM 32-41-07. LEAK CHECK AND OPS CHECK FOUND TO BE SATISFACTORY AT THIS TIME.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 5,393 hrs · 4,215 cycles

UPPER RIGHT DOOR PIN GREEN FLAG FOR THE CLOSED AND LOCKED INDICATION IS NOT VISIBLE THROUGH THE VIEW WINDOW. VERIFIED DISCREPANCY. GREEN FLAG ON UPPER RIGHT PIN HAS WORN OFF. REMOVED AIRSTAIRS IAW EMB-505 MM, 52-14-00. NOTIFIED NETJETS. GREEN PAINT IS ON ORDER. NO TRACKING AS OF 1800H 10/08. EPZ NOTED GREASE COVERING GREEN FLAG FOR CLOSED AND LOCK ON UPPER RIGHT DOOR PIN. CLANEO GREASE FROM ALL LOCK PINS ANO REASSEMBLED DOOR. OPS AND VISUAL CHECKS GOOD. REF AMM 52-10·22.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 4,788 hrs · 3,729 cycles

MAIN DOOR HANDLE: DOOR WILL NOT CLOSE FROM EITHER INSIDE OR OUTSIDE DOOR IS STUCK IN THE OPENING POSITION. //SIGNOFF// PERFORMED DVI OF DOOR MECHANISM, HANDLE, LOCKING MECHANISM AND SEAL IAW EMBRAER OUTSIDE DOOR IS STUCK IN TL IE OPENING POSITON. PHENOM 300 AMM SOS 52-10-00/1 , 52- 11 -23-720-801 -A/500. FOUND EXCESS RTV SILICONE AROUND AND ON SEAL AREA. REMOVED EXCESS RTV (SILICONE) AROUND THE SEAL AREA AND PERFORMED OPERATIONAL CHECK IAW EMBRAER PHENOM 300 AMM SDS 505 52-10-00/1, AMM SDS- 52-10-00/12 NO DEFECTS NOTED

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 4,594 hrs · 3,578 cycles

EXCESSIVE FORCE REQUIRED ON BOTH INTERIOR AND EXTERIOR HANDLES TO LOCK MAIN CABIN DOOR. DOOR SEAL RECENTLY REPLACED AND STIFF SO YOU HAVE TO PULL DOOR IN AND LATCH ON BOTH SIDES .. LUBRICATED ENGAGEMENT PINS, DOOR MECHANISM WORKS WITH NO DEFECTS NOTED AT THIS TIME. IAW EMBRAER PHENOM 300 AMM 52-11-21, 52-11-23

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 4,542 hrs · 3,540 cycles

EMERGENCY LIGHTS REMAIN ILLUMINATED WITH SWITCH IN ARM POSITION. REMOVED & REPLACED THE FWD NR 1 BATTERY PACK IAW AMM 33-52-00. OPS CHECKED GOOD. NO DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 3,908 hrs · 3,054 cycles

EMERG EXIT SIGN/LIGHT: ENTRY DOOR LOWER SIDEWALL EMERGENCY EXIT LIGHT IS INOP. REMOVED LOWER EMERGENCY EXIT SIGN LIGHT AND INSTALLED CUSTOMER SUPPLIED "NEW" EXIT IDENTIFIER, OPS CHECK GOOD. ALL WORK DONE IAW AMM 33-52-13.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 3,003 hrs · 2,361 cycles

FORWARD EMERGENCY LIGHT BATTERY FAILED THE FUNCTIONAL TEST IN ACCORDANCE WITH PHENOM 300 AMM 33-52-01, BATTERY FAILED AT 15:35 SECONDS AT 20VDC. PASSING TIME IS 22 MIN AT 20VDC. PERFORMED REPLACEMENT #1 FORWARD EMERGENCY LIGHT BATTERY WITH A NEW BATTERY IN ACCORDANCE WITH PHENOM 300 AMM CHAPTER 33-52-01. PERFORMED OPERATIONAL TEST OF EMERGENCY LIGHTS BATTERY IN ACCORDANCE WITH PHENOM 300 AMM CHAPTER 33-52-00. NO DEFECTS NOTED.

Part: ROD — BINDING (MAIN DOOR) · airframe 2,370 hrs · 1,885 cycles

MAIN DOOR MAKES A LOUD "SNUBBING" SOUND UPON OPENING AND CLOSING. STOPS MOVEMENT IN 2 POSITIONS (SEE PHOTOS). CAN BE FORCED OPEN/CLOSED IF YOU MOVE IT HARD ENOUGH AND START THE MOTION OUT FAST, BUT DEFINITELY STRONGER THAN NORMAL FORCES ARE NEEDED AND FROM THE INSIDE AND YOU NEED TO FORCE IT DOWN WITH YOUR FEET IF YOU DO IT AT NORMAL SPEED. THE FORCES AND SPEED REQUIRED TO OPEN/CLOSE THE DOOR MAY CAUSE FURTHER DAMAGE AT THE BOTTOM WHEN OPENING AS IT HAS TO BE SLAMMED DOWN. CORRECTIVE ACTION: INSPECTED DOOR INTERNAL MECHANISMS AND FOUND NO DEFECTS. COMPLETED CHECK OF MAIN ENTRY DOOR OPENING SPEED, IAW EMBRAER PHENOM 300 AMM TASK 25-10-00-820-804-A. DOOR SPEED WAS FOUND TO BE ACCEPTABLE IN OPENING AND CLOSING. VERIFIED LENGTH OF THE HOISTING ROD TO BE, IAW EMBRAER PHONOM 300 AMM TASK 52-10-00-820-801-A. VISUAL INSPECTION OF ASSIST REEL SHOWS NO OBVIOUS DAMAGE OR EXCESSIVE WEAR. FOUND FWD AND AFT TELESCOPING RODS BINDING ON EXTEND AND RETRACT. REPLACED BOTH FWD AND AFT TELESCOPING RODS WITH NEW CONDITION PARTS, IAW EMBRAER PHENOM 300 AMM 52-12- TASK 52-12-25-400-801-A. DOOR OPERATIONS CHECKS GOOD AT THIS TIME.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 1,834 hrs · 1,461 cycles

FLAP FAIL YELLOW CAS ILLUMINATED - WHILE DESCENDING THROUGH FL270 CAS CAUTION ILLUMINATED YELLOW "SWPS FAULT","FLAP FAIL","PTRIM BKP FAIL" AND A WHITE "SPOILER FAULT". THE AUTO PILOT WAS UNAVAILABLE AS WAS EXPECTED. PRIMARY TRIM WAS WORKING, WITH NO TRIM INDICATION THOUGH. RAN ALL ASSOCIATED CHECKLISTS. ALL REMAINED ILLUMINATED THROUGH LANDING AND TAXI TO SHUTDOWN. DID A ZERO FLAP LANDED. // SIGNOFF // COULD NOT DUPLICATE DISCREPANCY. PERFORMED CMC DOWNLOAD AND SENT DOWNLOADS TO COMMAND CENTER FOR REVIEW. EMBRAER COMMAND CENTER SUGGESTED TO PERFORM FIM-4885- 27-36-00-810-816-A, ALL CHECKS SATISFACTORY. PERFORMED DETAILED VISUAL INSPECTION OF IASP NO.1, NO DEFECTS NOTED AT THIS TIME. PER CONTACT CENTER RECOMMENDATIONS PERFORMED SATISFACTORY OPERATIONAL CHECK OF THE IASP HEATING SYSTEM IAW EMB 505 AMM TASK 30-30-00-710-801-A/500 AND OPERATIONAL TEST OF THE ADS IAW EMB505 AMM TASK 34-1~00-710-801-A/500.NO FURTHER MAINTENANCE REQUIRED AT THIS TIME.

Part: FLAP TRACK — CORRODED (ZONE 600) · corrosion level 2 · airframe 12,433 hrs · 6,092 cycles

FLAP TRACK CORRODED, ULTRA SONIC NDT INSPECTION COMPLIED WITH. AFTER ENGINEERING EVALUATION, REMAINING THICKNESS WAS UNACCEPTABLE. REF B/P SE05811901, REV D. REF CMP GIV MESSAGE 3575111 FOR INSPECTION.

Part: PAN — MISINSTALLED (OVEN)

CABIN SMOKE DUE TO DRIP PAN IN OVEN BEING IMPROPERLY INSTALLED CAUSING DRIPPINGS FROM FOOD TO CONTACT OVEN LOWER BURNER ELEMENTS. (K)

Part: STEERING SYS — FAILED (NLG) · airframe 9,438 hrs · 4,551 cycles

AFTER LANDING AIRCRAFT, STEERING MADE AN UNCOMMANDED TURN TO THE RIGHT.

Part: FITTING — CORRODED (LT MLG) · airframe 8,061 hrs · 3,884 cycles

LEFT MAIN LANDING GEAR UNIVERAL FITTING CORRODED.

Part: TIE BOLT — CORRODED (LT MLG) · airframe 8,061 hrs · 3,884 cycles

LEFT MAIN LANDING GEAR ACTUATOR TIE ROD AND PIN CORRODED.

Part: STRUCTURE — CORRODED (ELEVATOR) · airframe 8,061 hrs · 3,884 cycles

LEFT AND RIGHT ELEVATOR ATTACH HARDWARE CORRODED AND PITTED.

Part: PIN — CORRODED (LT MLG) · airframe 8,061 hrs · 3,884 cycles

LEFT MAIN LANDING GEAR SPINDLE PIN CORRODED.

Part: TORQUE TUBE — CORRODED (RUDDER) · airframe 8,061 hrs · 3,884 cycles

RUDDER TORQUE TUBE HAS CORROSION AND PITTING.

Part: FITTING — CORRODED (RT MLG) · airframe 8,061 hrs · 3,884 cycles

RIGHT MAIN LANDING GEAR UNIVERAL FITTING CORRODED.

Part: CABIN PRESSURE — MALFUNCTIONED · airframe 8,010 hrs · 3,855 cycles

AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF. NO FAULTS FOUND AFTER TEST WERE PERFORMED. A/C WAS FLOWN WITH NO FURTHER FAULTS DETECTED.

Part: O-RING — LEAKING (HYD SYSTEM) · airframe 7,662 hrs · 3,670 cycles

LOSS OF HYDRAULIC FLUID ON THE FLIGHT SIDE HYDRAULIC SYSTEM. FOUND PRESSURE TRANSMITTER O-RING AT FAULT.

Part: SOLENOID VALVE — FAILED (NLG STEERING) · airframe 6,882 hrs · 3,334 cycles

ON TOUCHDOWN CREW RECEIVED NOSE WHEEL STEERING FAILURE MESSAGE WITH NO NOSE WHEEL STEERING.