N316QS
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| NETJETS AVIATION, INC. (DXTA) | Certificate holder | — | Matched by certificate designator |
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
TAXIING FOR TAKEOFF, ALL EMERGENCY LIGHTS STARTED FLICKERING. WHEN EMERGENCY SWITCH IN THE OFF POSITION, EMERGENCY LIGHTS SOMETIMES ON & SOMETIMES OFF. REMOVED NR 1 EMERGENCY BATTERY DUE TO LIGHTS FLICKER AND INSTALLED A REPAIRED ASSY IAW AMM 33-52-01. ALL CHECKS GOOD. REMOVED NR 2 EMERGENCY BATTERY DUE TO LIGHT FLICKER AND INSTALLED REPAIRED ASSY IAW AMM 33-52-01. ALL OPS CHECKED GOOD.
CABIN EMERG LIGHT: DURING POST-FLIGHT, THE OVERHEAD EMERGENCY LIGHT LOCATED BETWEEN SEAT 3 AND SEAT 4 IS INOPERATIVE. CORRECTIVE ACTION: FOUND THE CONNECTOR TO BE LOOSE ON EMER/COURTESY LIGHT. RECONNECTED CONNECTOR AS REQUIRED. PERFORMED OPS CHECK. OPS CHECK GOOD. NO FAULTS NOTED. IN REF ENB-505 AMM 33-52-00 & 33-26-00
MAIN ENTRY DOOR NEEDS TO BE EVALUATED; DOOR TENDS TO DROP/SLAM WITHOUT GUIDANCE. REMOVED FOD. OPS CHECK GOOD. IAW EMB-505 AMM CH 52-14-00.
LG LEVER DISAG RED CAS: REPEAT WRITE UP. ON TAKEOFF, RECIEVED RED "LG LEVER DISAG" CAS WHEN LG LEVER SELECTED UP. CYCLED LG PER QRH AND CONDITION RETURNED. RECIEVED 3-GREEN INDICATION WHEN LG LEVER SELECTED DOWN. LANDED UNEVENTFULLY. CORRECTIVE ACTION: REPLACED NLG SHOCK STRUT. OPS CHECK GOOD. IAW EMBRAER PHENOM 300 AMM CH, 32-21-01. OSD: 1/21/2025
AC GENERATION AND CONTROL: AFTER TAKEOFF, WE GOT CAS EMER LIGHT NOT ARMED AND THE EMER LIGHTS WERE PHYSICALLY ON (THIS SEEMED TO SUPPORT WHAT WE LATER DISCOVERED, AS THEY WERE RESPONDING TO THE ELECTRICAL PROBLEM) WE THEN NOTICED BOTH MAIN BATTERIES WERE NOT BEING CHARGED. BOTH GENS WERE OPERATING NORMALLY AND POWERING ONLY THE DC BUS 1 & 2. THE BATTERIES WERE POWERING THE EMER & HOT BUSSES. BOTH BATTERIES WERE AT 25.5V AND CONTINUED TO DECREASE TO 24.3 AT LANDING. UPON SHUTTING DOWN 1 ENGINE, THE AIRPLANE WENT INTO WHAT SEEMED LIKE AN ELECTRICAL EMERGENCY AND HALF OF THE COCKPIT DEPOWERED. AT NO TIME WERE SWITCHES OUT OF PLACE OR IMPROPERLY ILLUMINATED. C/W EMERGENCY BATTERY OPERATIONAL TEST IAW AMM 33-52-01-710-801-A NO DEFECTS NOTED OPS TEST GOOD
CABIN PRESSURIZATION CONTROL: DURING CLIMB OUT ~12000-14000' WE HAD AN ECS VALVE 2 FAILURE - PULLED UP THE ECS PAGE AND CONFIRMED IT. APPROXIMATELY 17000' IT CLEARED AND THE CABIN PRESSURE BEGAN TO READJUST (DECREASING). AT APPROXIMATELY 22000-23000' WE RECEIVED THE ECS VALVE 2 FAILURE AGAIN, THIS TIME IT DIDNT EXTINGUISH AMD THE CABIN CONTINUED TO CLIMB TO 10800'. WE STOPPED THE CLIMB AT FL240, TOLD ATC - DONNED THE MASKS, AND BEGAN AN EMEGENCY DESCENT BACK TOWARDS 10000'. WE WERE ENROUTE TO KILM, AND KGSP WAS OFF THE LEFT WINGTIP - WE ADVISED ATC THATS WHERE WE WANTED TO GO - WE VERIFIED GOOD WEATHER, ACCEPTABLE RUNWAY LENGTH AND APPROPRIATE CFR/ GROUND SUPPORT. WITHIN 5 MINUTES OF DECLARING THE EMERGENCY, WE WERE ON FINAL FOR AN "UNEVENTFUL" LANDING ON RWY 4. PICTURES INCLUDED REMOVED FAILED RH FCSOV PN 1300250-11 SN 1663 AND INSTALLED REPAIRED FCSOV PN 1300250-11 SN 1855 WITH NEW ORINGS PN FF200 2-222 IAW PHENOM 300 AMM 21-21-01.
WITH THE CABIN DOOR, OPEN, TOP RIGHT BOLT CAME OUT. WASHER FELL INTO THE DOOR COWLING. THIS HAPPENED DURING PASSENGER BOARDING. GAINED ACCESS TO MED INTERIOR AND RETRIEVED THE WASHER AND THE SCREW REINSTALLED THE PREVIOUSLY GAINED ACCESS INSTALLED THE HARDWARE AS REQUIRED. ALL WORK DONE IAW 52-14-00.
MAIN ENTRANCE DOOR HANDLE BROKE OFF AT THE BASE WHILE A HUB SERVICE TECH WAS CLOSING THE DOOR. PERFORMED AN OPS CHECK AND TROUBLESHOOTING PLUS VISUAL INSPECTION OF INNER DOOR OPEN AND LOCKING MECHANISM AND LATCH PINS. NO OBVIOUS DEFECTS NOTED AT THIS . COULD NOT GET THE HANDLE TO JAMM. REMOVED AND REPLACED M.E.D DOOR HANDLE IAW PHENOM 300 AMM CHAPTER 52-11-24, OPS CHECK GOOD. MIXED AND APPLIED SEALANT TO DOOR LOCK HOUSING. REF STEP. RE-INSTALLED DOOR STEPS AND LIGHT CONNECTORS. LUBED DOOR AND DOOR LOCK PERFORMED DOOR LOCKING AND OPENING. OPS CHECK GOOD.
CABIN EMERG LIGHT: EMERGENCY LIGHTS FLICKERING ON/OFF IN FLIGHT.
CABIN EMERGENCY LIGHTS FLASHING IN ARM POSITION. // SIGNOFF// GAINED ACCESS TO FWD EMERGENCY BATTERY BY REMOVING FLOOR PANEL 223CLF. REMOVED INOP EMERGENCY BATTERY P/N 6450LS-00 S/N 001876 AND INSTALLED NEW CUSTOMER SUPPLIED EMERGENCY BATTERY P/N 7450LS-00 S/N 006285. FUNCTIONAL CHECK IS GOOD WITH NO DEFECT NOTED. DONE AT KPBI. WORK DONE PER PHENOM 300 AMM 33-52-00-710-801.
DURING ACCOMPLISHMENT OF EMBRAER SERVICE BULLETIN 505-55-0004 REV 01 (DATED 06/24/2020) WE NOTED THE FOLLOWING MASS BALANCE WEIGHTS BELOW TOLERANCE AT LEFT ELEVATOR: ADJUSTABLE WEIGHTS PART NUMBER PE915109-L33 (11 EACH BELOW MINIMUM OF 84G); HORN MASS WEIGHT PART NUMBER PE915109-L42 (1 EACH BELOW MINIMUM OF 1095G); MASS WEIGHT INBOARD PART NUMBER PE915109-L40 (1 EACH BELOW MINIMUM OF 2809G) ALL WEIGHTS HAS BEEN REPLACED WITH A NEW MASS WEIGHTS AND THE ELEVATOR BALANCING WAS PERFORMED WITH NO FURTHER DEFECTS NOTED. THE ELEVATOR WAS RE-IDENTIFIED TO PART NUMBER 505-11094-615, AS PER SERVICE BULLETIN INSTRUCTIONS. WE ALSO NOTED THE FOLLOWING RIGHT ELEVATOR MASS BALANCE WEIGHTS BELOW TOLERANCE: ADJUSTABLE WEIGHTS PART NUMBER PE915109-L33 (11 EACH BELOW MINIMUM OF 84G); HORN MASS WEIGHT PART NUMBER PE915109-L42 (1 EACH BELOW MINIMUM OF 1095G) ALL WEIGHTS HAS BEEN REPLACED WITH A NEW MASS WEIGHTS AND THE ELEVATOR BALANCING WAS PERFORMED WITH NO FURTHER DEFECTS NOTED.THE ELEVATOR WAS RE-IDENTIFIED TO PART NUMBER 505-11094-616, AS PER SERVICE BULLETIN INSTRUCTIONS. THIS REPORT COMPLIES WITH FAA 14 CFR PART 135 OPERATORâS GMM REQUIREMENTS.
WHEEL BRAKES PULSE & GRAB UNEVENLY DURING LANDING ROLLOUT, CAUSING SIGNIFICANT DIRECTIONAL CONTROL DIFFICULTY DURING BRAKING. THEREAFTER THE BRAKES PULSE DURING TAXI-IN. IT FEELS LIKE THE RT BRAKE IS GRABBING MORE THAN THE LT. PERFORMED MAIN BRAKE SYS INSPECTION CHECK IAW AMM CH 32-41-00. PERFORMED WHEEL, TIRES & BRAKES INSPECTION CHECK IAW AMM CH 32-45-00. FOUND BOTH TIRES MAINS TO BE UNDER SERVICED BY 10 PSI. SERVICED BOTH MAIN TIRES IAW AMM CH 12-14-00. PERFORMED CVDR DOWNLOAD FEF SEQ 1913 IAW CCCN E-EJ-00152324 RECOMMENDED TO SWAP WSTS. REQUESTED THAT WE CHANGE THE RT WIST. R & R WITH NEW THE RT WST IAW AMM CH 32-41-06.
WHEN THE GEAR IS SELECTED TO THE DOWN POSITION THE NOSE GEAR REMAINS IN THE UP & LOCKED POSITION UNTIL THE MAIN GEAR IS DOWN & LOCKED THEN THE NOSE GEAR EXTENDS. R & R NLG DOWN LOCK RELEASE ACTUATOR. OPERATIONS CHECKED IAW 300 MM 32-21-03. R & R NLG UP LOCK BOX, OPERATIONS CHECKED GOOD IAW 300 MM 32-31-05. SYSTEM OPERATIONS CHECKED GOOD. PARTS ACTUATOR ON 2117-2000-401, SN ON 00065. ACTUATOR OFF 2117-2000-401, SN OFF 00174. UP LOCK BOX ON 2617-1000-401, SN ON 00016. UP LOCK BOX OFF 2617-1000-401, SN OFF 00324.
NORMAL BRAKE FAILED ON LANDING ROLL. ON SHORT FINAL (100 FT AGL) "POWER BRAKE LOW PRESS" AND "ANTI SKID INOP" ANNUNCIATORS ILLUMINATED, ON LANDING NORMAL BRAKES SLOWED THE AIRCRAFT TO A WALKING SPEED, THEN FAILED COMPLETELY. THE EMERGENCY BRAKE HANDLE WAS USED TO BRING AIRCRAFT TO A STOP. ANTI SKID WAS IN THE ON POSITION THE ENTIRE TIME. R & R HIGH PRESSURE SWITCH. BLED BRAKES AND PERFORMED ANTISKID FUNCTIONAL TEST WITH NO DEFECTS NOTED. IAW MM 32-42-05 AND 32-42-00.
OUT OF 4000 FT THE LT ENG FIRE LIGHT CAME ON, PULLED POWER TO IDLE AND LIGHT WENT OUT. LANDED WITH NO OTHER LIGHTS. REMOVED COWLING AND INSPECTED ENGINE FOR HOT STAB. NO DAMAGE NOTED RAN ENG AND FOUND INBD BLEED AIR LINE LEAKING. INSTALLED NEW LINE ASSY IAW MM CH 36-12-01, PERFORMED HIGH POWER LEAK CHECKS. LEAK CHECKED GOOD, INSTALLED COWLING.
SMOKE SEEN COMING FROM HELLHOLE, AC NOW INOP, NO SIGN OF CHARRING OR ANY OTHER SIGN OF DAMAGE. ODOR COMING FROM INSIDE MOTOR. REMOVED FREON FROM SYS. REMOVED ACFT PALLET FROM TAIL OF ACFT, WORK COMPLETED IAW MM 21-52-00. REMOVED FAILED FUSE LIMITER. INSTALLED NEW FUSE LIMITER. REMOVED ACFT MOTOR REC. DRYER/ BINDING SWITCH, BOLT & PULLEY. INSTALLED O/H MOTOR, NEW REC DRYER/BINAY SWITCH, BOLT & PULLEY IAW ENGINE SYS R134A MM PG 20 THRU 31. CHARGED SYS WITH FREON, OPS CHECKED GOOD. WORK COMPLETED IAW MM 12-19-02. SYS PRESSURES CHECK GOOD TEMPERATURE TEMP CHECKED GOOD. SYS IS COLD NO FURTHER ACTION REQUIRED.
CO-PILOT'S BRAKE PEDALS SEEM TO BE SOFTER THAN NORMAL, ADDITIONALLY THE RT BRAKE PEDAL GOES FARTHER DOWN THAN THE LT WHEN PRESSURE IS APPLIED. COMPLIED WITH BLEEDING OF ANTI-SKID BRAKING SYS. OPS CHECK, BRAKES GOOD AT THIS TIME IAW MM 32-40-00.
WITH PITCH TRIM INDICATOR IN T/O POSITION, UPON ROTATION, ACFT OVER ROTATED AND IT TOOK BOTH HANDS TO CONTROL. NORMAL FLIGHT CONTROL FORCES WITH TRIM INDICATOR AT FULL NOSE DOWN. FOUND TRIM INDICATOR SHOWING INCORRECT T/O POSITION. REMOVED ELEV TRIM TAB CONTROL WHEEL AND CORRECTED TRIM TAB INDICATOR POS. INSTALLED ELEV TRIM TAB CONTROL WHEEL IAW MM 27-31-08. ELEVATOR AND ELEV TRIM TAB TRAVEL/DEFLECTION CHECKS GOOD IAW MM 27-31-00-221.
PILOTS RT BRAKE PEDAL GOES SOFT AFTER 15-20 SEC OF INITIAL BRAKE APPLICATION. (LOSSED APPX 2-3 INCHES OF PEDAL TRAVEL). INSTALLED 1EA NEW PILOTS RH BRAKE MASTER CYLINDER AND BLED SYSTEM. OPERATED ENGINES AND TAXI CHECKED NORM, WORK DONE IAW C560 M/M 32-42-02, 32-42-00 AND P.O.H.
PILOTS RT BRAKE PEDAL GOES SOFT AFTER INITIAL APPLICATION. THE RT PEDAL TRAVELS SIGNIFICANTLY FURTHER THAN THE LT BRAKE PEDAL. BLED LT AND RT BRAKES IAW MM 32-42-00.
RT BRAKE ON CAPTAIN'S SIDE DEPRESSES FURTHER THAN LT SIDE AND IS SOFT. CO-PILOTS SIDE HAS SIMILAR PROBLEM. REMOVED AND REPLACED RT MAIN BRAKE IAW CE-560 MAINTENANCE MANUAL 32-42-01.
WHEN TAXIING AND MAINTAINING LIGHT BRAKE PRESSURE ON BOTH BRAKE PEDALS, RT PEDAL PRESSURE DROPS AND PEDAL DEPRESSES ALL THE WAY TO STOP. BLED BOTH LT AND RT BRAKES IAW CE-560 MM, CHAPTER 32-42-00. OPERATIONAL CHECKS GOOD. FOR DETAILS OF WORK ACCOMPLISHED, SEE EJM HPN WO 8216.
LT BRAKE PEDAL PRESSURE ON F/O SIDE IS LOW. NEEDS TO BE PUMPED UP MANUALLY. PREFORMED BRAKE BLEEDING PROCEDURE IAW CESSNA 560 MM 32-42-00. OPS AND LEAK CHECK GOOD AT THIS TIME.
POWER BRAKE LOW PRESS AND ANTI-SKID INOP LIGHTS FAILED TO EXTINGUISH WHEN GEAR WERE EXTENDED. POST FLIGHT REVEALS NO FLUID SEEN THROUGH SITE GAUGES. FOUND LT BRAKE FLEX LINE LEAKING. REMOVED LT BRAKE HYDRUALIC FLEXLINE. INSTALLED A NEW FLEXLINE. PERFORMED BLEEDING PROCEDURE. SERVICED BRAKE RESERVOIR, LEAK CHECK AND OPS CHECK GOOD. WORK PERFORMED IAW CE560 MM CHAP 32-42-01.
RIGHT PILOT'S BRAKE PEDAL SOFT. REMOVED AND REPLACED CO-PILOT'S LT & RT BRAKE MASTER CYLINDERS AND BLED BRAKE SYSTEM IAW 560 ULTRA MM 32-42, OPS CHECK GOOD.
DURING CLIMB BETWEEN FL180-FL190, NOTICED A STRONG FUEL SMELL IN THE COCKPIT AND AT THE REFRESHMENT CENTER, DURING DECENT AND LANDING THE SMELL FADED AWAY. ITEM IS UNDER INVESTIGATION.
A STRONG FUEL SMELL WAS NOTED IN THE CABIN WHILE AT CRUISE. FOUND PRE-CHECK VALVE LEAKING, INSTALLED NEW VALVE WITH NEW PACKINGS IAW MM CHAPTER 28-22-00. OPS CHECKS AND LEAK CHECKS GOOD.
DURING ROUTINE INSP LOCKED INTO NACA DORSAL SCOOP AND FOUND THE LOWER AIR VANE PN 6512072-12 CRACKED 1.50 INCH IN A CIRCLE PATTERN AND READY TO BREAK OFF. FOUND SEVERAL OTHER AIRCRAFT OF THIS SAME MODEL WHERE THE PART HAS BROKEN OFF AND BEEN FOUND DOWN STREAM (2 EA PIECES IN DUCT WORK AND 1 EA WEDGED IN FRESH AIR CHECK VALVE, 1 EA MADE IT PAST FRESH AIR CHECK VALVE AND OVERHEAD BLOWER FAN IN CABIN WEDGED INTO AFT BULKHEAD VERTICAL DUCT WORK). REMOVED VANE AND ALSO NOTICED THE LACK OF EA 9309 SECURING INTO PLACE AND THAT V NOTCH WAS CUT WITH HAND SNIPS WITH NO RELIEF HOLE AT INTERSECTION. INSTALLED NEW PART IAW MFG SP. SENT TO MFG FOR EVALUATION. (SCR 91292)