N101QS
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
AFTER TAKEOFF, CARGO DOOR EICAS ILLIMINATED WITH THE CARGO DOOR SHOWING OPEN. ON LANDING, VISUALLY INSPECTED DOOR, IT WAS LOCKED & SECURE. POWERED ON & VERIFIED CARGO DOOR AMBER CAS MESSAGE PRESENT, WHILE BAGGAGE DOOR IS CLOSED & LOCKED. CYCLED THE DOOR MULTIPLE TIMES & THE CASS WOULD NOT DEACTIVATE. INTERROGATED OMS & FOUND BOTH CARGO DOOR SENSORS STATUS GOOD, BUT THE CARGO DOOR LOCKED PROXIMITY SENSOR SHOWED HANDLE NOT STOWED WHETHER IT WAS STOWED OR NOT. PROXIMITY SENSOR MT46 CONNECTION AT SPLICE SP702 GOOD. WHEN VERIFYING MT46 SENSOR CLEARANCE, THE CRANK ASSY WITH THE SENSOR TARGET WAS ABLE TO MOVE ALONG THE MOUNTING BOLT MOVING IN & OUT OF TOLERANCE. REMOVED THE VENT PUSHROD, COTTER PINS, & WASHERS FROM THE CRANK ASSY IAW AMM 52-31-01-000-801. INSTALLED THE PUSHROD, NEW WASHERS, & NEW COTTER PINS IAW AMM 52-31-01-400-801. VERIFIED CORRECT CLEARANCE TO THE TARGET IAW AMM 52-70-05-710-801. OPS TESTED IAW AMM 52-70-05-710-801 AND AMM 52-70-03-710-801. NO CARGO DOOR AMBER CAS MESSAGE. SYSTEM CHECKED GOOD AT THIS TIME.
WHILE IN FLIGHT COULD NOT OPEN LAV DOOR DOOR KNOB WILL TURN BUT DOES NOT MOVE LATCH INSIDE IF THE JAM MADE SEVERAL ATTEMPTS TO OPEN COULD NOT CORRECTIVE ACTION: COMPLETED FULL ADJUSTMENT OF THE AFT LAVATORY DOOR AS REQUIRED FOR PROPER DOOR OPERATION. WORK DONE IN REF TO GL5500 SMM # 25-24-62
AFTER LOWERING THE LANDING GEAR WE RECIEVED AN AUTOBRAKE FAIL CAS AND A BRAKE 50%DEGRADED CAS MESSAGE. POWERED UP AIRCRAFT & PERFORMED FAULT MESSAGES NVM & BCU DOWNLOADS. SET TO MCC/BOMBARDIER FOR EVALUATION. MANUFACTURER ADVISED SUSPECT & BAD LT BRAKE SOV. ACCESSES SYSTEM PARAMETERS & OBSERVED BRAKE PSI RISE & DROP FOR ANY DISCREPACIES. NOTED LT & RT OB BRAKES NOT REACHING FULL 3000 PSI. INSPECTED BRAKES & NOTED HYD FLUID LEAK AT RT IB BRAKE FUSE. GAINED ACCESS TO RT IB BRAKE HYD FUSE. REMOVED FUSE. FOUND O-RINGS AT UNION DETEREORATED. REMOVED & REPLACED WITH NEW O-RINGS. INSTALLED HUD FUSE. LEAK CHECKED GOOD. BLED BRAKES. OPS CHECKED GOOD & NO DEFECTS NOTED. WORK PERFORMED IAW AMM 32-43-33.
- PROBLEM DESCRIPTION: DURING OIL SERVICE TECH FOUND THE #2 ENGINE HYD PRESSURE LINE HAS LOOSE JAM NUT AND THREADS ARE MISSING FROM NUT AND LINE. LOOSE HARDWARE ON #2 ENGINE HYD PX LINE ALLOWED THE TROUGH-FITTING TO WEAR THE SUPPORT BRACKET THIN AND EXPAND THE HOLE IN THE BRACKET ASSEMBLY. - RESOLUTION: REMOVED & REPLACED HYDRAULIC PRESSURE LINE P/N GD478-1201-5 IAW GLOBAL 5000 M/M 29-12-09. RE-INSTALLED #2 HYDRAULIC SHUT OFF VALVE AND HYDRAULIC LINES ASSOCIATED WITH BRACKET P/N GD477-1703-9 IAW GLOBAL 5000 M/M 29-12-33. REMOVED & REPLACED #2 ENGINE HYD LINE SUPPORT BRACKET IAW GLOBAL 5000 SRM 51-42-08. P/N OFF GD477-1703-7 S/N UNK P/N ON GD477-1703-9 S/N PLF3344112. BLEED, LEAK, & OPS CHK GOOD OF #2 HYDRAULIC SYSTEM.
LEFT ENG LOWER AFT ENG MOUNT RETAINING BOLT IS BROKE & MOUNT PIN IS BACKING OUT OF ENG SN 22081. REPLACED FWD ENG MOUNT LINKS & RETAINING HARDWARE WITH NEW & REPLACED AFT UPPER ENG MOUNT LINK & RETAINING HARDWARE WITH NEW, SERVICED LT ENG RENTAL ENG WITH 9 QUARTS TURBO OIL 2380, REPLACED AFT LOWER MOUNT LINK & HARDWARE WITH NEW REMOVED LT ENG & INSTALLED LOWER REPAIRED ENG. REPLACED TRUNNION PIN & RETAINING HARDWARE WITH NEW. ALL WORK DONE IAW MM CH 71-00 REV 47. ENG INSTALLED IS A REPAIRED RENTAL UNIT. OK TO INSTALL OK TO CLOSE OPERATIONAL TEST, FUNCTIONAL TEST, LEAK TEST VERIFIED ALL MOUNTING HARDWARE FOR LT ENG SN 12145.
LT THRUST LEVER BINDING; UNABLE TO MOVE. WORKED NORMALLY ON TAXI OUT, TAKEOFF, AND CLIMBOUT. ONCE LEVELED OUT AT ALTITUDE IT WAS EXTREMELY DIFFICULT TO REDUCE POWER. WERE ABLE TO MOVE LEVER TO CUTOFF ONCE PARKED. FOUND MOISTURE INGRESSION PRESENT IN LT AFT ENGINE CONTROL CABLE. R & R CABLE & RIGGED. IN ADDITION, FOUND FWD LT ENGINE CONTROL CABLE JOINT BENT. R & R JOINT IAW MM 76-10-00.
NR 1 ENGINE THROTTLE LEVER STUCK AT CRUISE POWER SETTING. ALTITUDE FL360/-49DEG C SAT. DESCENDED AND REGAINED FULL CONTROL AT FL260/ -27DEG C SAT. REMOVED LT ENG LWR COWLINGS. VERIFIED AFT CABLE ROUTING, NO DEFECTS NOTED. LUBERCIATED AFT CONTROL CABLE WITH KRYTOX 240AB. RAN ENG FOR OPS CHECK, NO DEFECTS NOTED. ALL WORK DONE IAW MM, CHAP 12-20-00 AND 21-10-00. INSTALLED LT LWR ENG COWLING.
ON LANDING APPROACH, DID NOT GET A LT GEAR SAFE INDICATION. EXECUTED A GO-AROUND AND COMPLIED WITH THE CHECKLIST. LANDED UNEVENTFULLY. REMOVED PANELS IN LT WHEEL WELL AND ACCESSED CONNECTOR P-271. OHMED OUT GEAR SWITCHES AND FOUND THE GEAR DOWN LOCK SWITCH S017 WITH 42 OHMS ACROSS CLOSED CONTACTS, LIGHTLY TAPPED SWITCH HOUSING AND READINGS DROPPED TO .08 OHMS. JACKED ACFT AND INSTALLED HYDR MULE. REMOVED DEFECTIVE SWITCH P/N MS24331-1, AND INSTALLED NEW CUSTOMER SUPPLIED SWITCH P/N MS24331-1, IAW MM 32-00-00 NO DEFECTS WERE NOTED. REMOVED HYDR MULE AND REMOVED ACFT FROM JACKS.
ON LANDING APPROACH, WE DID NOT GET A LT GEAR SAFE INDICATION. (K)
DURING TAXI OUT, CREW PERFORMED TR CHECK. LT THRUST REVERSER DEPLOYED NORMALLY WITH APPROPRIATE ANNUNCIATOR LIGHT SEQUENCE. RT THRUST REVERSER COULD NOT BE VERIFIED TO DEPLOY AND ASSOCIATED LIGHTS ON RT PANEL DID NOT ILLUMINATE. RT THRUST REVERSER PIGGYBACK LEVER CLOSED AND RT ENGINE SPOOLED DOWN. RT ENGINE BOOST PUMP TURNED ON, AS WELL AS ALL THE ASSOCIATED ANNUNCIATOR LIGHTS FOR A RT ENGINE FAILURE. BLUE COLORED SMOKE WAS SEEN EMITTING FROM RT ENGINE BY GROUND CREW. INVESTIGATED AND FOUND THRUST REVERSER THROTTLE CONTROL LEVER HITTING THROTTLE LEVER BRACKET REPOSITION BRACKET. OPS CHECK SEVERAL TIME DURING TAXI OPS CHECKED GOOD WORK DONE IAW AMM 76-10-00.
AFTER TAKEOFF PITCHTRIM FAILED AT 2000 FT AGL, PITCH TRIM WOULD NOT LEAVE GREEN ARC. FOUND PILOTS PITCH TRIM SWITCH INOP. REMOVED PILOTS YOKE ASSY. PN 128284060-13 SN 0039 AND INSTALLED NEW PILOTS YOKE ASSY. PN 128384060-13, SN 0076. IAW CMM 27-10-15 OPERATIONAL CHECKS OF SWITCHES ON YOKE SATISFACTORY.
AIRCRAFT ROLLS LT AND RT 2 TO 3 DEGREES OF BANK EACH WAY WITH THE AUTOPILOT ENGAGED (WHEN AUTOPILOT IS DISCONNECTED THE AIRCRAFT HAS RT ROLL TRIM AND DOES EACH TIME. SPOILER BRIDLE CABLE TENSION TO WITHIN LIMITS. OPS CHECK GOOD ON GROUND, IAW MM 27-60-00.
CO-PILOTS RT BRAKE PEDAL WENT ALL THE WAY TO THE FLOOR. PRESSURE CAME BACK AFTER SEVERAL PUMPS, NOTICED DURING TAXI. T/S: REMOVED AND REPLACED COPILOTS RT BRAKE MASTER CYLINDER, BLEED AND SERVICED. OPS CHECKS GOOD REF H400 XP MM 32-40-00.
DURING INSPECTION, LEFT ENGINE OUTBOARD IGNITER WOULD NOT OPS CHECK. FOUND IGNITION CABLE DEFECTIVE DUE TO AN INTERNAL FAULT. COULD NOT DETERMINE CAUSE AS EXTERNAL INSPECTION OF IGNITION CABLE APPEARED SERVICEABLE.