N429QS

ATA 3416

Part: ALTIMETER — OUT OF TOLERANCE (ZONE 200) · airframe 6,488 hrs · 4,977 cycles

AT FL180 STANDBY ALTIMETER READS 90 FEET ABOVE TOLERANCE CORRECTIVE ACTION: PERFORMED A GVI OF STANDBY PITOT TUBE, NO DAMAGE OR OBSTRUCTIONS NOTED, PER TASK 34-11-02-210-801A. PERFORMED TASK 34-11-02-100-801A PITOT-STATIC PROBE -DRAIN HOLE CLEANING. GAINED ACCESS AND BLEW NITROGEN THRU PITOT AND STATIC LINES BACK TO PROBE, NO DEBRIS COLLECTED. PERFORMED IESI FUNCTIONAL CHECK IN REF TO TASK 34-11-00-720-801A ALL ALTITUDES WITHIN TOLERANCE LEVELS OF TABLE 501.

ATA 3350

Part: SIGN — INOPERATIVE (ZONE 200) · airframe 5,975 hrs · 4,571 cycles

EMERG EXIT SIGN/LIGHT: THE EMERGENCY EXIT SIGN LIGHT ABOVE MAIN CABIN DOOR IS INOP. RE-SECURED CONNECTOR FOR THE EMERGENCY EXIT SIGN ABOVE MAIN CABIN DOOR. EMERGENCY EXIT SIGNS OPS CHECKS GOOD AT THIS TIME, REF, EMB-505 AMM 33-50-00.

ATA 3240

Part: TRANSDUCER — FAILED (BRAKES) · airframe 3,813 hrs · 4,967 cycles

BRK FAIL CAS MESSAGE AND BRAKE FAILURE ON TAXI. HAD TO USE EMERGENCY BRAKE TO STOP THE AIRCRAFT. BRK FAIL YELLOW CAS: BRK FAIL CAS MESSAGE AND BRAKE FAILURE ON TAXI. HAD TO USE EMERGENCY BRAKE TO STOP THE AIRCRAFT. BRAKE FALL CAS MESSAGE. REMOVED AND REPLACED UH WHEEL SPEED TRANSDUCER WITH AN INSPECTED UNIT IAW MM 32-41-06. OPS, LEAK CHECK GOOD BRAKE FALL CAS MESSAGE. R & R BRAKE CONTROL UNIT WITH A MODIFIED UNIT IAW MM 32-41-001 OPS CHECK GOOD. BRAKE FAIL CAS MESSAGE. R & R RT BRAKE ASSY WITH AN OVERHAULED UNIT IAW MM 32-41-001 OPS, LEAK CHECK GOOD. BRAKE FAIL CAS MESSAGE. R & R BRAKE CONTROL MODULE WITH A REPAIRED UNIT IAW MM 32-41-001 OPS, LEAK CHECK GOOD.

ATA 3010

Part: WARNING LIGHT — FALSE ACTIVATION (ANTI ICE) · airframe 4,913 hrs · 3,767 cycles

DURING CLIMB THROUGH FL180 WITH THE WINGSTAB SWITCH IN OFF POSSITION, WE RECIEVED A A-I WINGSTAB LEAK. CREW COMPLEATED THE A-I WINGSTAB QRH. A-I WINGSTAB CAS REMAINED ON FOR THE REMAINDER OF THE FLIGHT. NOTE THAT ALL SWITCHES ARE LEFT IN THE EMERGENCY CONDITION. IAW INSTRUCTIONS FROM CONTACT CENTER, COMPLETED THE FIM TASK 36-21-00-810-808-A - LEAKAGE IN THE RH ANTI-ICING OF THE CENTRAL FUSELAGE .. ALL CHECKED OUT NORMALLY WHEN GOING THROUGH THE OPERATIONAL CHECK OF THE WING/HORIZONTAL ICE PROTECTION SYSTEM. ALL CAS MESSAGES NORMAL. NO A-I WINGSTB LEAK CAS MESSAGE APPEARED. THE FIM SHOWS THAT AS A TRANSITORY CONDITION OF THE ENGINE PNEUMATIC INDICATING SYSTEM.

ATA 3240

Part: CONTROL UNIT — DEFECTIVE (BRAKE SYS) · airframe 4,237 hrs · 3,247 cycles

RIGHT MLG BRAKE: AFTER LANDING IT BECAME VERY DIFFICULT TO MAKE RIGHT TURN ON THE TAXIWAY AND TO MAINTAIN CENTERLINE. THE RIGHT BRAKE APPEAR TO GRAB EXCESSIVELY. ENTIRE AIRFRAME SHUDDERS WHEN APPLYING RIGHT BRAKE DURING LOW SPEED TAXI. //SIGNOFF// REMOVED AND INSTALLED A MODIFIED BRAKE CONTROL UNIT. OPS CHECK GOOD IAW EMBRAER PHENOM 300 MM 32-41-01

ATA 3350

Part: BATTERY — DEFECTIVE (ZONE 100) · airframe 4,227 hrs · 3,235 cycles

EMERG EXIT SIGN/LIGHT STARTED FLICKERING IN CRUISE ONE HR INTO THE FLIGHT. DURING THE CHARGE PART OF TASK CARD TC·E50·33-1001 THE EMER LIGHTS WOULD NOT EXTINGUISH LN ARM. GAINED ACCESS TO BOTH #LAND #L BATTERIES AND TROUBELSHOT TO THE #L BATTERY. REMOVED ANO REPLACED THE #L BATTERY ALL OPS CHECKS SATISFACTORY. CLOSED ALL ACCESS. REF EMBSOS AMM 33·52·01 AND EMBSOS FIM 33-50-00

ATA 3240

Part: BRAKE ASSY — DEFECTIVE (ZONE 700) · airframe 2,799 hrs · 2,121 cycles

RIGHT MLG BRAKE: ON TAXI OUT NOTICED ENTIRE AIRCRAFT SHUDDERS WHEN BRAKES WERE APPLIED. ON TAXI IN TRIED JUST LEFT BRAKE AND APPEARED TO BE SMOOTH. APPLIED JUST RIGHT BRAKE AND SHUDDER WAS EVIDENT. // SIGNOFF// REMOVED AND INSTALLED "OVERHAULED" RH BRAKE ASSEMBLY. IAW PHENOM 300 AMM 32-41·00, 32-45-01, 32-45-21

ATA 5210

Part: INDICATOR — CONTAMINATED (MAIN ENRTY DOOR) · airframe 1,694 hrs · 1,282 cycles

MAIN DOOR: LOWER RIGHT GREEN FLAG IS NOT VISIBLE IN THE WINDOW. SIGN OFF REMOVED MAIN ENTRY DOOR AIR STAIRS AND CLEANED DEBRIS FROM GREEN INDICATOR PAINT ON PINS AS REQUIRED REINSTALLED MAIN ENTRY DOOR AIR STAIRS IAW EMB PHENOM 300 AMM 52-14-00-400-80 1-A.