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N707QS

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2019 Bombardier BD-100-1A10 · Honeywell AS907-2-1A

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© OpenStreetMap
Registered owner
Netjets Sales Inc
Location
Oklahoma City, OK
Owner type
Corporation
Serial number
20818
Year built
2019
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
September 30, 2019
Certificate issued
December 27, 2024
Expires
December 31, 2031
Mode S code
A96FFE
Bombardier BD-100-1A10Airframe model · 8 seats · 2 engines · 874 registeredTCDS T00005NYAirframe · Bombardier BD-100-1A10TCDS E00010LAEngine · Honeywell AS907-2-1A

From the FAA registry file of October 24, 2026.

On this page

Airworthiness directives that may apply · 55

Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.

2006In forceSuperseded2026
See all 61 ADs

Information bulletins that may apply · 2

Advisory, not mandatory.

Historical bulletins · 2
SAIB AIR-22-02Pitot/Static Anti-Ice SystemIssued Feb 25, 2022SAIB NM-18-32Electrical Power - Direct Current Power CenterIssued Dec 3, 2018

NTSB investigations

No NTSB investigations matched to N707QSMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Bombardier BD-100-1A10 aircraft

FAA incident reports

No FAA accident or incident reports matched to N707QSMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Bombardier BD-100-1A10 aircraft

Service difficulty reports

No reports matched to N707QSGeneral aviation reporting is voluntary. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Reports on Bombardier BD-100-1A10 aircraft
Reports on N707QS not matched to an aircraft · 16

They name N707QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

SDR DXTA2014042505742Control Column · chafedLEFT PILOT CONTROL COLUMN HAS CHAFING MARKS FROM THE AILERON CABLE INSIDE COLUMN. REMOVED PILOT'S CONTROL COLUMN. MACHINED AND BLENDED DAMAGED AREA. ALODINED AND PRIMED AS REQUIRED. RE-INSTALLED PILOT'S CONTROL COLUMN. PERFORMED ALL FLIGHT CONTROL TRAVEL TApr 24, 2014 · N707QS · Gulstm 200 · Control Column SectionSDR DXTA2014040705720Brake Sys · weakDURING LANDING, THE BRAKES WERE SPONGY WITH THE PEDALS TO THE FLOOR. PERFORMED BLEEDING OF THE BRAKE SYSTEM IAW MM 32-40-20. BRAKE SYSTEM OPS & LEAK CHECKED GOOD.Mar 29, 2014 · N707QS · Gulstm 200 · Landing Gear Brake SystemSDR DXTA2014040405715Unknown · vibrationVIBRATION BEGINS AT FL260 AT 290KTS, INCREASED INTENSITY TO 350KTS. FELT IN CONTROL COLUMN & NOT IN RUDDER PEDALS. VIBRATION FELT IN COCKPIT SEATS & IN CABIN SEATS. CHECKED ALL ELEVATOR BELLCRANKS, PUSHRODS, CONTROL COLUMS AND HINGE POINTS FOR CONDITION ANDMar 29, 2014 · N707QS · Gulstm 200 · Flight Control System
See all 16 unmatched reports

STCs that may be installed · 141

Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.

See all 141 STCs