N352QS
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
AIRCRAFT HAS A MUSTY ODOR WHILE THE VCS OPERATES. ARRIVED TO ACFT AND RAN VCS SYSTEM. MUSTY ODOR COMING OUT OF COCKPIT VENTS. GAINED ACCESS AS NECESSARY TO COCKPIT EVAP AND FOUND EVAP TO BE LEAKING WATER FROM PLASTIC SHROUD DUE TO SEPARATION AND THE FACE OF EVAP TO CAKED IN DUST. FOUND CARPET NEXT TO RETURN VENT TO BE DAMP AND HAVE A MUSTY ODOR. CLEANED EVAP FACE AND RE-SEALED SEPERATION IN PLASTIC SHROUD ON EVAP. NO MUSTY ODOR AT THIS TIME.
DURING EXTERIOR PREFLIGHT LIGHT CHECK PUT THE EMERGENCY LIGHTS IN THE ON POSITION AND OBSERVED THE EMERGENCY LIGHTS FLASHING. SHUT POWER OFF TO AIRCRAFT AND TURNED EVERYTHING BACK ON AND OBSERVED THE EMERGENCY LIGHTS ON WITH THE SWITCH IN THE ARM POSITION. PERFORMED FIM 33-50-00-810-802-A, FOUND NR 2 EMERGENCY BATTERY FAILED TO CHARGE. REMOVED AND REPLACED NR 2 EMERGENCY BATTERIES IAW AMM 33-52-01, OPS CHECK GOOD IAW AMM 33-52-00. REMOVED NR 2 BATTERY REPAIRED BATTERY INSP.
CABIN EMERG LIGHT: EMERGENCY LIGHTS STAY ON IN THE ARM POSITION AFTER BOTH ENGINES ARE RUNNING. RESOLUTION: REMOVED EMERGENCY BATTERY I PN 7450LS-00 SN 006361 AND LNSTALLED "NEW" EMERGENCY BATTERY PN 7450LS-00 SN 007616 ALSO REMOVED EMERGENCY BATTERY 2 PN 7450LS-00 SN 005246 AND INSTALLED "NEW" EMERGENCY BATTE1Y PN 7450LS-00 SN 007319 IA W PENOM 300 AMM 33-52-0 I OPS CHECK GOOD.
EMERG LIGHTS CAME ON DURING FLIGHT IN THE ARM POSITION. LIGHTS STARTED FLICKERING UPON DESCENDING (ABOUT 15 MIN LATER). POWERED UP AIRCRAFT AND DUPLICATED SQUAWK. FOUND LIGHTS FLASHING IN THE ARMED MODE. COMPLIED WITH THE RECHARGING OF THE EMERGENCY BATTERIES IAW AMM 24~41-00. OPS CHECK SATISFACTORY WITH NO DEFECTS NOTED. COMPLIED WITH NJATASK CARO FORM TC-505-33-200403 DATED 04/23 12020
EMERGENCY LIGHTS ARE ACTIVATED CONTINUOUSLY WHEN SWITCH IS IN THE ARMED POSITION. STARTED TO FLICKER AS WELL. REMOVED BATTERY NR 1 AND INSTALLED TESTED BATTERY IN THE 1 POSITION AND REMOVED BATTERY NR 2 AND INSTALLED TESTED BATTERY INTO NUMBER 2 POSTION PREFORMED OPS TEST AND BONDING CHECK OPS CHECK GOOD NO DEFECTS NOTED AT THIS TIME IAW AMM 25-27-05,06-46-00,06-48-00,20-13-21,33-52-00,32-52-01.
NR 2 GENERATOR FAILED IN FLIGHT CAUSING NR 2 ENGINE TO VIBRATE AND MAKE NOISE, PER THE CHECKLIST WE SHUTDOWN NR 2 ENGINE IN FLIGHT. REMOVED AND INSTALLED OVERHAULED STARTER/GENERATOR. PERFORMED ENGINE RUN CHECKS IAW EMM 71-00-00 WITH NO LEAKS OR DISCREPANCIES NOTED. PERFORMED THE RT ENGINE STARTER/GENERATOR OPERATIONAL CHECK IAW MM 24-31-00 WITH NO DISCREPANCIES NOTED. PERFORMED UNSCHEDULED WINDMILLING INSPECTION IAW EMM 05-50-00-210-809 PART B WITH NO DISCREPANCIES NOTED. ORIG SUBMISSION DATE: 1/3/2023
MAIN DOOR: MAIN CABIN DOOR WILL NOT OPEN. WE CAN ROTATE RED HANDLE OUTSIDE WHICH FEELS NORMAL AND PRESSURE RELIEF FLAP OPENS. THE DOOR WILL THEN ONLY MOVE OUT ABOUT ONE INCH AT TOP AND THEN BINDS. IT FEELS LIKE A SOLID STOP...SOMETHING IS NOT CLEARING PAST SOMETHING ELSE BUT HITTING IT. // SIGNOFF// FOUND AFT DOOR SHROUD TO BE INTERFERING WITH AFT MED DOOR FRAME NEAR LOWER STEP. INSTALLED CUSTOMER SUPPLIED NEW SHROUD AFT PAX DOOR ASSEMBLY P/N 506-45261-4001, S/N DH00027354 AND ACCQMPLISHED SATIFACTORY OPERATIONAL CHECKS. REF EMB SOS AMM 25·23-05. UNIT REMOVED P/N 506-45261-4001, S N 17736159 001
CABIN EMERG LIGHT: EMERGENCY LIGHTS ON CABIN ARE ALL ONE WHEN THE SWITCH IS IN THE ARMED POSITION. EMERGENCY BATTERIES ARE MOST LIKELY LOW. /// CORRECTIVE ACTION /// REMOVED AFT EMERGENCY BATTERY P/N 6450LS-00 S/N 001398 AND INSTALLED NEW EMERGENCY BATTERY P/N 7450LS-00 S/N 006172 REF. EMBRAER PHENOM 300 AMM 33-52-01. OPS CHECKS GOOD.
AFT LIGHT ON THE MAIN DOOR AIRSTAIRS FAILED TO OPERATE DURING THE EMERGENCY LIGHTS OPERATIONAL TEST PER PHENOM 300 AMM 33-52-00. TROUBLESHOT TO OPEN FUSE F0047. FUSE WAS REPLACED WITH NEW AND SUBSEQUENT OPERATIONAL TEST WAS SATISFACTORY.
RUDDER AND AILERON WEIGHTS FOUND SURFACE CORROSION AND DETERIORATION OF MASS BALANCE WEIGHTS. COMPLIED WITH EMBRAER SB505-55-0004 REV 01. ACCOMPLISHED PART II AND III. AILERON AND RUDDER MASS BALANCE AND ATTACHMENT PARTS REPLACEMENT.
AFTER LANDING THE BRAKES WERE VERY INEFFECTIVE INITIALLY FROM COPILOT SIDE. THE BRAKES THEN GRABBED VERY AGGRESSIVELY AND THE AIRCRAFT PULLED HARD TO THE LEFT. NO CAS MESSAGES ILLUMINATED. REMOVED AND REPLACED THE RT MAIN GEAR BRAKE ASSY. PERFORMED BRAKE SYSTEM BLEED. FUNCTIONAL CHECK OF BRAKE SYSTEM AND BLEED MAIN HYDRAULIC SYSTEM IAW MM 32-45-21, 32-40-00, 32-41-00, AND 29-10-00. TAXI AND LEAK CHECKED GOOD.
MLG UNSAFE LIGHT AFTER RETRACTION, DUE TO ICE AND SLUSH ON TAXI OUT, LT MLG EXTENDED TO 400 FT AGL. UPON SELECTING GEAR UP ACFT YAWED GENTLY TO THE LEFT, RED GEAR UNSAFE LIGHT REMAINED ILLUMINATED & HYD SYS REMAINED ENERGIZED. ATTEMPTED TO RECYCLE GEAR, SAME RESULTS. AFTER GEAR EXTENDED NORMALLY SEVERAL TIMES HYD PRESSURE LIGHT INTERMITTENT ON APPROACH. LANDED NORMALLY, POST FLIGHT REVEALED ICE, SLUSH & SAND IN VICINITY OF LT MLG AND WHEEL WELL. MOVED ACFT INTO HEATED HANGAR AND REMOVED ICE AND SLUSH. PERFORMED 12 GEAR SWINGS WITH ALL NORMALL INDICATIONS. INSPECTED GEAR WALLS, NO DEFECTS NOTED. ALL DONE IAW MM. OPS CHECKED GOOD.
ABOVE 40 KTS, LT AIRSPEED FAILED WITH RED X ACCOMPANIED BY GPWS WINDSHEAR FAIL ANNUNCIATOR. INSPECTED GPWS SYSTEM PERFORMED GPWS SELF TEST NO FAULTS FOUND CHECKE IAC FAULTS NONE FOUND PERFORMED OPS CHECK OPS CK GOOD IAW MM 34-41-04.
ABOVE 40 KTS LT AIRSPEED FAILED WITH RED X ACCOMPANIED BY GPWS WINDSHEAR FAIL ANNUNCIATOR.
COPILOTS SIDE BRAKES REQUIRE MORE THAN NORMAL PRESSURE TO GET ANY BRAKING. RAN AC WITH ANTI-SKID ON AND OFF CONDUCTING HIGH SPEED STOPS AND MANY MANUVERING TURNS WITH NO DISCREPANCIES NOTED FROM EITHER PILOT OR COPILOT SIDE. ANTI-SKID BIT INDICATORS WERE CHECKED BEFORE AND AFTER RUN WITH NONE TRIPPED EITHER TIME. FORCE REQUIRED TO ACTUATE BRAKING IS EQUAL BETWEEN LT AND RT, BRAKE AND EQUAL BETWEEN PILOT AND COPILOT SIDE.
NO GREEN LIGHT ON LT MAIN GEAR DURING GEAR EXTENTION, RAN THE EMERGENCY EXTENTION CHECKLIST. BLOWED GEAR DOWN FOR POSITIVE DOWN AND LOCKED. CREW VERIFIED GREEN VISUAL INDICATOR IS SHOWING ON THE MLG ACTUATOR. AT THIS TIME WITH ROTARY TEST, THE LT MAIN GEAR INDICATOR LIGHTS DO NOT LIGHT. RELAMPED INDICATOR, JACKED A/C. RESET EMERG. BLOWDOWN BOTTLE SYSTEM, SERVICED BOTTLE, CYCLED GEAR MULTIPLE TIMES, SERVICED RESERVOIR. ALL IAW REFS: 560 AMM 32-60-00, 12-13-01. LAMP SUPPLIED FROM N352QS FLYAWAY KIT. SYSTEM OPS CHECK GOOD.
THE BRAKES ON THE SIC SIDE OF THE AIRCRAFT MOMENTARILY FEEL INOP THEN AFTER SEVERAL MOMENTS AGGRESSIVELY GRAB WITH THE SAME AMOUNT OF PRESSURE. REMOVED FAULTY ANTI-SKID CONTROL BOX AND INSTALLED INSPECTED UNIT BY HYDRO-AIRE CRS#QD3R78SL. PERFORMED OPERATIONAL CHECK GOOD. IAW C560 M.M. 32-42-00.
THE BRAKES ON THE SIC SIDE OF THE AIRCRAFT MOMENTARILY FEEL INOP THEN AFTER SEVERAL MOMENTS AGGRESSIVELY GRAB WITH THE SAME AMOUNT OF PRESSURE. BLED LT AND RT BRAKES. FOUND EVIDENCE OF AIR IN RT BRAKES. BLED BOTH L/H AND R/H AN ADDITIONAL 4 TIMES TO MAKE SURE ALL THE AIR WAS OUT OF THE SYSTEM. OPS CHECKED GOOD. WORK DONE IAW CE-560 M/M 32-42-00. ALSO INSPECT ANTI-SKID CONTROL BOX AND FAULT DISPLAY UNIT FOR ANY LOOSE CONNECTIONS OR TRIPPED INDICATORS. OPS CHECKED GOOD IAW CE-560 M/M 32-42-08 .
BRAKES NOT WORKING WELL AT SPEEDS ABOVE 5 KNOTS. WITH ANTI SKID OFF BRAKES WORK FINE. [SUP 05-16-07] INSPECTED ANTI SKID WIRING FOUND BAD GROUND FROM P1007 LT WHEEL TRANSNDUCER. CLEANED CORROSION FROM PLUG PL008. PERFORMED ANTISKID SYSTEM OPS CHECK OPS CHECKS GOOD ALL WORK DONE IAW CE-560 M.M. 32-42-00-710.
DURING TAXI OUT OF GSO, CO PILOT SIDE BRAKES BECAME INOP AT APPROX 15 KNOTS FOR ABOUT 5 SECONDS. BRAKES RESPONDED NORMAL AFTER INITIAL LOSS. CHECKED ANTI-SKID BITE INDICATOR, NO BITES FLAGGED, C/W NETJETS 560 ANTI-SKID WIRING CHECKLIST. FOUND RT TRANSDUCER CONNECTOR (STEP 4) SHIELD TERMINAL LUG BROKEN. REPLACED TERMINAL. FOUND LEFT CONNECTOR (STEP 5) BACKSHELL TO GROUND WAS OPEN. REPAIRED GROUND. FOUND WHEEL WELL CONNECTOR ANTI-SKID WIRING NOT PROPERLY GROUNDED. REPAIRED GROUND, C/W LEAK AND OPS CHECK OF ENTIRE SYSTEM. OPS AND LEAK CHECKS GOOD. BLED BRAKES AND SERVICED IAW CE560 M/M CH 32-42-00/32-40-01/12-12-02/12-13-00.
ON TAXI OUT OF RAMP. CO-PILOT SIDE BRAKES FAILED. REPEAT WRITE UP. BOTH PEDALS WERE FULLY DEPRESSED TO THE FLOOR WITH NO BRAKING ACTION. INSPECTED ALL MASTER CYLINDERS. NO LEAKS. C/W BRAKE FUNCTIONAL CHECK WITH POWER ON. PILOT AND CO-PILOT BRAKES HAVE GOOD ACTUATION. ALL PEDALS FEEL THE SAME C/W SATISFACTORY TAXI CHECK. BOTH BRAKE ASSEMBLIES CHECK GOOD. NO LEAKS. WEAR PINS ARE NOT FLUSHED. C/W SATISFACTORY ANTI-SKID FUNCTIONAL CHECK. C/W BRAKE BLEED. C/W SATISFACTORY TAXI CHECK OF BRAKE SYSTEM WITH ANTI-SKID ON AND OFF. ALL WORK IAW CE 560 MM 32-40.
DURING LANDING (SPEED ,40 KTS) RT BRAKE STOPPED FUNCTIONING. WHEN PUMPED, STARTED FUNCTIONING AGAIN. PROCESS CONFIRMED BY USING BRAKES PEDALS ON RT SIDE. BRAKES ACTED NORMAL AT SLOW SPEEDS (ESTIMATED 15KTS) PERFORMED A VISUAL INSPECTION OF THE RT BRAKE. NO PHYSICAL DEFECTS NOTED ON THE BRAKE CALIPER OR ASSOCIATED COMPONENTS. PERFORMED A VISUAL CHECK OF HYDRAULIC FLUID RESERVOIR AND FOUND FLUID TO BE AND SERVICEABLE LEVEL. PERFORMED A BRAKE BLEED ON RT BRAKE AND NOTED AIR IN SYSTEM. BLED BRAKES UNTIL NO AIR WAS IN SYSTEM. PERFORMED AN OPS CK OF RT GOOD. IAW MM 32-00-00.
ON LANDING THE POWER LEVERS WERE BROUGHT TO IDLE AND LEFT ENGINE FAILED (AT IDLE). ADJUSTED FLOW DIVIDER TO FUEL CONTROL INTERCONNECT ROD FOR PROPER IDLE DETENT. RIGGED AFT POWER CONTROL CABLE TO PROVIDE SLIP FIT OF ROD END AT BOLT. GROUND RAN AND NUMEROUS RAPID POWER LEVER REDUCTIONS TO IDLE DID NOT CAUSE ENGINE TO SHUT DOWN, ALL WORK PERFORMED IN ACCORDANCE WITH CESSNA 560 MAINTENANCE MANUAL CHAPTER 76-11-00.
APPARENT PARTIAL THRUST REVERSER DEPLOYMENT AT CRUISE FLIGHT 30,000 FT. RIGHT UNLOCK LIGHT WAS ON, DEPLOY LIGHT DID NOT LIGHT. RUMBLING AND DECELERATION WAS FELT. METAL TAB ON OUTBOARD SIDE OF RIGHT THRUST REVERSER IS BENT UPWARD APPROXIMATELY .5 INCH. ITEM IS UNDER INVESTIGATION.
LEFT ENGINE FLAMED OUT AFTER DOING PREFLIGHT WING SPOILER CHECK. INSPECTED LEFT ENGINE CONTROLS AT FUEL CONTROL UNIT AND ACCOMPLISHED ENGINE POWER CONTROLS CHECK. PERFORMED ADJUSTMENT AND RIGGING CHECK IAW CESSNA 560 MM CHAPTER 76-11-00 PG. 501 NO DISCREPANCIES NOTED.
DURING ROUTINE MAINT, A FUEL LEAK WAS BEING WORKED IN RT WING AREA FORWARD OF MLG. DURING INSTALLATION OF PLUMBING WHICH WAS REMOVED FOR ACCESS A LINE WAS DAMAGED. PART WAS ORDERED AND RECEIVED BEFORE INSTALLATION LINES WERE COMPARED THE CORRECT PART NR WAS ON LINE ASSY, BUT THE LINE HAD THE CONNECTIONS SWAPPED (FLARED B-NUT AND WIGGINS CLAMP FITTING), MFG PULLED BUILD UP PRINT AND AGREED THAT THE LINE WAS BUILT INCORRECT.
DID NOT GET 3 GREEN LIGHTS UPON GEAR EXTENSION. RAN CHECKLIST AND CONFIRMED DOWN AND LOCKED. BLEW EMERGENCY BOTTLE TO COMPLETE CHECKLIST. RT MAIN GEAR DID NOT ILLUMINATE. RELAMPED LANDING GEAR INDICATOR MODULE WITH 4 NEW LAMPS IAW M.M. 33-1-01.