N596QS
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
P/S COLD L AMBER CAS: L ON TAKE OFF WE PRESSED THE L/R AS PRESCIBED IN PROCEDURE. THE P/S COLD MESSAGE REMAINED. WE ABORTED THE TAKE OFF, THE SWITCH LIGHT IS NOT ILLUMINATING. CORRECTIVE ACTION: PERFORMED THE AIR DATA ANTI-ICING SYSTEM ADJUSTMENT/TEST. OPS CHECK GOOD. IAW CE 680A MM 30-30-00
WHEN BATTERES ARE SWITCHED OFF, AND THE EMER LIGHTS ARE IN ON POSITION, THE EMER LIGHTS DONT ILLUMINATE, BUT DO ILLUMINATE IF IN ARM POSITION. CORRECTIVE ACTION: REPLACED EMERGENCY BATTERY POWER SUPPLY. OPS CHECK GOOD. IAW AMM 33-50-06
A/I STAB COLD R AMBER MASSAGE WOULD NOT EXTINGUISH WHEN SYSTEM TURNED ON. CREW ATTEMPTED SEVERAL TIME TO CYCLE SYSTEM AND NO CHANGE. CORRECTIVE ACTION: REPLACED PRESSURE REGULATOR S/O VALVE. OPS CHECK GOOD. IAW CE680A MM 30-15-05.
EMERGENCY LIGHTING: DURING POST FLIGHT INSPECTION, WE DISCOVERED THAT THE #3 AND #7 SEAT OVERHEAD AND FLOOR LEVEL EMERGENCY LIGHTS WERE INOPERATIVE IN BOTH THE EMER LIGHT ARM, AND ON SWITCH POSITIONS. WE BELEIVE THESE LIGHTS ARE ASSOCIATED WITH EMERGENCY BATTERY PACKS #2 AND #3 NOT CHARGING PROPERLY. LIGHTS FUNCTION PROPERLY WHEN MAIN SHIP BATTERIES ARE TURNED ON. COMPLIED WITH TASK TC-FLT-33-1001 AND FOUND EMERGENCY BATTERIES #2 & #3 REQUIRE REPLACEMENT. STANDING BY FOR PARTS. (JH,HM - 11/18/24) COMPLIED WITH TASK TC-FLT-33-1001 AND FOUND EMERGENCY BATTERIES #2 & #3 REQUIRE REPLACEMENT. STANDING BY FOR PARTS. (JH,HM - 11/18/24) REMOVED AND REPLACED #2 AND #3 EMERGENCY BATTERIES WITH "REPAIRED" JAW CE-680A MM 33-50-00.
EMERGENCY LIGHTING: WHEN DOING THE POWER ON CHECKLIST, EMER LIGHTS REMAIN ON WITH BATTERY POWER AND APU POWER IN THE ARM POSITION. COMPLIED WITH EMERGENCY LIGHTING OPERATIONAL CHECK IAW CE-680A AMM 33-50-00. NO DEFECTS NOTED. COULD NOT DUPLICATE.
FLAPS FAIL AMBER CAS: FLAPS FAIL CAS MESSAGE ILLUMINATED WHEN SELECTING FLAPS FULL. FLAP INDICATOR ON MFD WAS YELLOW INDICATING FULL. COMPLETED EMERGENCY CHECKLIST AND FLAPS RESET TO WHITE INDICATING FULL. CLEANED UP AIRPLANE TO FLAPS 0. ATTEMPTED ANOTHER APPROACH WITH THE SAME FLAPS FAIL CAS MESSAGE APPEARED WHEN SELECTED FULL FLAPS. COMPLETED THE EMERGNECY CHECKLIST. RESET THE FLAPS WITH A WHITE FULL INDICATION ON THE MFD. WE DECIDED TO LEAVE THE AIRCRAFTED FULLY CONFIGURED AND LANDED WITHOUT INCIDENCE. 2). OVERSPEED: DURING A MISSED APPROACH WITH A FLAP FAIL CAS MESSAGE WE EXCEEDED THE FLAPS FULL SPEED LIMIT OF 175KTS. WE EXCELERATED TO 189KTS DURING THE GO AROUND AND REDUCED THE SPEED ONCE RECOGNIZED. THE GEAR WAS DOWN THE ENTIRE TIME HOWEVER WE DIDN'T EXCEED THE 210KT LIMIT. GAINED ACCESS TO AIRCRAFT, CLEARED FAULT MEMORY WITH FLAP RESET SWITCH AND CYCLED THE FLAPS SEVERAL TIMES WITH NO FAULTS. INSPECTED FLAP TRACKS WITH NO DEFECTS. STARTED TASK 27-50-00 (FLAP SYSTEM MECHANICAL TROUBLESHOOTING) AND COMPLETED THE CLEARANCE BETWEEN AFT ROLLER AND END OF TRACK WORKSHEET 1 WITH ALL MEASUREMENTS WELL WITHIN SPECIFICATION. OPERATED FLAPS AGAIN WITH NO FAULTS. WE ARE AT STEP C (PDU CLUTCH TROUBLESHOOTING) AND NEED THE PDU CLUTCH CHECK TOOL P/N CJMDX27-014 TO COMPLETE THE INSPECTION OF THE PDU'S. ORDERED TOOL WITH MCC, NO UPDATE ON SHIPPING. OREDERED INCLINOMETERS FROM VELOCITY MX FOR TRAVEL CHECKS. CN/EM 1/23/24. RECEIVED TOOLING. PERFORMED FLAP BINDING T/S WITH NO DEFECTS NOTED. PERFORMED PDU CLUTCH T/S WITH CURRENT LESS THAN 220AMPS. PER TROUBLESHOOTING GUIDE IT IS REQUIRED TO REPLACE PDU. REMOVED PDU AND INSTALLED AN OVERHAULED PDU. PERFORMED FLAP MOVEMENT CHECK WITH TIMES/FLAP ANGLES IN TOLERANCE. CYCLED FLAPS WITH NO DEFECTS NOTED. FLAP SYSTEM OPS CHECK GOOD AT THIS TIME. PERFORMED IAW CE680A MM CH 27-50-00/27-50-20. ORIGINAL SUBMISSION DATE: 1/23/2024
CABIN EMERG LIGHT: EMER LIGHT AT POSITIONS SEAT THREE OVERHEAD INOP. EMER LIGHT AT SEAT THREE FLOOR INOP. EMER LIGHT OVERHEAD LAV INOP. PERFORMED INERTIA SWITCH ADJUSTMENT ON ALL EMERGENCY LIGHT BATTERY PACKS, AND LEFT AIRCRAFT POWER ON FOR 2 HOURS TO LET PACKS FULLY CHARGE IAW CESSNA 680A MM 33-50-00 BATTERY PACKS EMER LIGHT AT POSITIONS SEAT THREE OVERHEAD, EMER LIGHT AT SEAT THREE FLOOR, AND EMER LIGHT OVERHEAD LAV, AND ALL EMERGENCY LIGHTS ON AIRCRAFT ALL OPS CHECK GOOD AT KMIV IAW CESSNA 680A MM 33-SO·OO WITH NO DEFECTS NOTED
MULTIPLE AERAS OF CORROSION ON RH AND LH UPPER WING SKINS. SUBJECT: MULTIPLE AERAS OF CORROSION ON RH AND LH UPPER WING SKINS AIRCRAFT: 680A-0153 | N596QS. TT: 4007.5 TL: 2650. REF: DQ36499M1. DATED: SEPTEMBER 28,2022.
CORROSION FOUND, LH HORIZONTAL LOWER SKIN AT THE I/B FWD EDGE OF THE WEDGE PANEL. TEXTRON AVIATION ENGINEERING REPAIR LETTER DQ36489, DATED: SEPTEMBER 25,2022. SUBJECT: 680A-0153, N596QS, REPAIR RECOMMENDATION.
CORROSION FOUND, RH HORIZONTAL STABILIZER AT AFT INBOARD EDGE OF THE UPPER SKIN. TEXTRON AVIATION ENGINEERING REPAIR LETTER DQ36490, DATED: SEPTEMBER 25,2022. SUBJECT: 680A-0153, N596QS, REPAIR RECOMMENDATION.
MULTIPLE AERAS OF CORROSION ON RH AND LH UPPER WING SKINS. SUBJECT: MULTIPLE AERAS OF CORROSION ON RH AND LH UPPER WING SKINS AIRCRAFT: 680A-0153 | N596QS. TT: 4007.5 TL: 2650. REF: DQ36499M1. DATED: SEPTEMBER 28,2022.
UPON LH MLG OLEO INSTALLATION, FOUND LH MLG TRAILING LINK/AXLE ASSY. P/N: 7441030-3, S/N: 27693055 LOCATED AT L/H MLG OLEO ATTACH FITTING PITTED AND CORRODED AROUND OUTBOARD SIDES OF LUGS. TEXTRON AVIATION STRUCTURES ENGINEERING ORDER: DQ34849M1 DATE:5/19/2022. ENGINEERING EVALUATION DEEMED DAMAGE "MINOR" IN SCOPE AND CAN BE ADDRESSED WITH THE FOLLOWING: APPLY CORROSION RESISTANT PRIMER TO OLEO ATTACH LUG BORES ON LH MLG TRAILING LINK/AXLE ASSY. P/N: 7441030-3, S/N: 27693055. REINSTALL OLEO IAW CE680A M/M 32-10-10.
RIGHT MAIN LANDING GEAR SIDE BRACE ACTUATOR (INBOARD FITTING) CHAFE DAMAGE. ACCOMPLISHED TEXTRON AVIATION ENGINEERING REPAIR LETTER DQ34793M1 REV A DATED MAY 17, 2022; 680A-0153 (N596QS) RIGHT MAIN LANDING GEAR SIDE BRACE ACTUATOR (INBOARD FITTING) CHAFE DAMAGE.
RIGHT MAIN LANDING GEAR AXLE PLATING DAMAGE (CHIPPED). ACCOMPLISHED TEXTRON AVIATION ENGINEERING REPAIR LETTER DQ34811M1 DATED MAY 17, 2022; 680A-0153 (N596QS) RIGHT MAIN LANDING GEAR AXLE PLATING DAMAGE (CHIPPED).
CHAFE DAMAGE ON THE LEFT MLG SIDE-BRACE FITTING. ACCOMPLISHED TEXTRON AVIATION ENGINEERING REPAIR LETTER DQ34792 DATED MAY 16, 2022; 680A-0153, N596QS REPAIR RECOMMENDATION.
GSD FAIL 2 AMBER CAS: GSD FAIL 2 AMBER CAS MESSAGE ILLUMINATED IN FLIGHT DURING CRUISE AND REMAINED ON FOR DURATION OF FLIGHT. // SIGNOFF// REMOVED AND REPLACED THE GSD41 P/N 011-01457-01 S/N 2JH006728 WITH SAME P/N, S/N 2JH007258, OPS CHECK GOOD REF THE CE680A MM 31-40-10.
FUSELAGE SKIN GOUGE MARKS. FUSELAGE LOWER SKIN HAS TWO SMALL GOUGE MARKS FROM PREVIOUS CROSSFLOW VALVE ORIENTATION. ACCOMPLISHED TEXTRON AVIATION STANDARD REPAIR SR-680A-ATA53-22175 DATED 07/19/2019, STANDARD REPAIR - 680A ALL S/N LWR SKIN CHAFE FROM ANTI-ICE CROSS-FLOW VALVE. WITH FAA FORM 8100-9 SUBMITTAL LETTER NO. 19-1711 DATED 07/19/2019.
IN CRUISE, WHEN ENG ANTI ICE SELECTED, A BURNING ODOR AT FL370, NOT STRONG. ON GROUND, STRONG ODOR WITH APU BLEED ON, HOT AIR OUT OF DUCTS. LOUD SQUEAL FROM ACM AREA. PERFORMED APU BLEED AIR TEST IAW AMM 21-10-00. APPLIED BLEED AIR, BURNING ODOR PRESENT. USED MAX COOL SWITCH. BLEED AIR RAN FOR A FEW SECONDS & AN ACM OVER TEMP CAS. SYS CLOSED APU BLEED AIR VALVE. CHECKED CMC. FOUND NR 3 ACM OVER TEMP FAULTS RELATE TO ACM. MANUFACTURER STATED A BAD ACM & OPS CHECK APU BLEED AIR & WATER SEP FOR MOISTURE & IF IT`S COOL TO TOUCH. WATER SEP HOT & NO MOISTURE. STATED THE TURBINE WAS SEIZIED. REMOVED ACM COOLING TURBINE, INSTALLED CUSTOMER SUPPLIED UNIT IAW AMM 21-50-67. OPS CHECKED GOOD. AMM 21-50-00.
AT FLIGHT ALTITUDE, "NOSE DOOR OPEN L" AMBER LIGHT ILLUMINATED. LIGHT EXTINGUISHED UPON LANDING AT DIVERSION AIRPORT. SIGN OFF. ARRIVED AT THE AIRCRAFT WITH THE MESSAGE NOT PRESENT. CHECKED RECENT FAULT MESSAGES AND FOUND CODE 1420 "NOSE DOOR OPEN L" WHICH POINTS TO THE FRONT LOWER PROXIMITY SWITCH. PERFORMED VISUAL INSPECTION OF SENSOR WIRING AND INTEGRITY OF LATCH ASSEMBLY, NO DEFECTS NOTED. CLEANED FRONT LOWER PROXIMITY SWITCH AND LATCH. PERFORMED 10 OPERATIONAL CHECKS OF THE DOOR AND LATCH ASSEMBLY WHILE VERIFYING SENSOR POSITIONING ON THE WIRE DIAGRAM PAGE OF THE CDMS. COULD NOT DUPLICATE FAULT. OPERATIONS CHECK GOOD AT THIS TIME. WORK PERFORMED IAW CE-680A AMM 52-70-00.