TTSN: 6,861 hours
TLSN: 2,645 landings
Time/Landings as of 25 January 2018
Type: Honeywell TFE731‐60‐1C
Plan: Honeywell Maintenance Service Plan (MSP) Gold
#1 (Left) #2 (Center) #3 (Right)
Serial Number: P112165 P112169 P112174
TTSN: 6,799 hours 6,713 hours 6,587 hours
TCSN: 2,627 cycles 2,586 cycles 2,549 cycles
Times/Cycles as of 25 January 2018
Type: Honeywell GTCP36‐150[F]
Serial Number: P‐302
TTSN: 2,911 hours
HSI Due: 4,500 hours
Time as of 25 January 2018
Max Ramp: 49,200 lbs.
Max Takeoff: 49,000 lbs.
Max Landing: 44,500 lbs.
Empty Weight: 25,604 lbs.
Usable Fuel: 20,944 lbs.
Computer Maintenance Tracking Program: CAMP
Inspection Program: 14 CFR 135.411(a)(2)
A/A+, 2A/2A+, and 4A+ Inspections due May 31, 2018
3A and Z Inspections due September 30, 2019
1B Inspection due @ 7,498.5 hours
2C Inspection due September 30, 2021
Landing Gear Overhaul due September 30, 2021
Honeywell Primus® 2000 ‐– Enrolled on Honeywell Avionics Protection Plan (HAPP)
AFCS: Honeywell Primus® 2000 Automatic Flight Control System with Autothrottles
EFIS: Five (5) Honeywell DU‐870 Display Units
FMS: Triple Honeywell FMZ‐2000 with Software NZ5.2.A w/TOLD (SB F900EX‐211)*
FMC: Triple Honeywell IC‐800 Integrated Avionics Computers with DL‐950 Data Loader
CDU: Triple Honeywell CD‐810 Control Display Units
ADS: Dual Honeywell AZ‐840 Air Data Computers
VHF COM: Triple Collins VHF‐422C Transceivers with 8.33 kHz Spacing (SB F900EX‐053R1)
HF COM: Dual Collins KHF‐950 HF COM System with SELCAL
AUDIO: Triple Audio Control Panels
RTU: Dual Collins RTU‐4220 Radio Tuning Units
SATCOM: Cobham SB‐400 Inmarsat Satellite Telecommunications System*
PHONE: Cockpit ICG Corded Handset and Cabin Cordless Handset*
DATA: Cobham SB‐400 SwiftBroadband Internet with Wi‐Fi*
DATALINK: Honeywell SAT AFIS® via TrueNorth Data Link Unit (Iridium Data Only)*
GPS: Dual Honeywell GNSSU’s
LRNAV: Triple Honeywell LASEREF III™ Inertial Reference System
NAV: Dual Collins VIR‐432 Navigation Receivers with FM Immunity (MOD M2288)
DME: Dual Collins DME‐442 Receivers
ADF: Dual Collins ADF‐462 Receivers
RADAR: Honeywell Primus® 880 Weather Radar System with 2nd Control
RADALT: Honeywell RT‐300 Radio Altimeter Transceiver
TAWS: Honeywell MARK V EGPWS™ (SB F900EX‐140R1 & SB F900EX‐226)
ACAS: Collins TTR‐921 TCAS II with Change 7.1 (STC ST00881WI‐D)
XPNDR: Dual Collins TDR‐94D Mode S Enhanced Transponders (SB F900EX‐239)
FDR: AlliedSignal (Honeywell) Solid‐State Flight Data Recorder
CVR: AlliedSignal (Honeywell) Solid‐State Cockpit Voice Recorder
ELT: Socata ELT97A2560000000 406 MHz Transmitter (SB F900EX‐090)
*Certain Installed Applications/Equipment Require Optional Subscriptions
Passenger Seating: Twelve (12) Approved for Taxi, Takeoff & Landing
Jump Seat: Yes – Crew Members Only
Configuration, Storage & Miscellaneous:
This 900EX includes twelve (12) passenger seats, a forward right‐hand galley and left‐hand
auxiliary galley, and forward and aft lavatories. The cockpit features a privacy curtain, there is a
main entrance door acoustical curtain, mid‐cabin bulkheads with curtains, and a hinged door
separating the aft lavatory from the cabin and baggage compartment.
The cabin seating consists of a forward four‐place club seating group, followed by two forwardfacing
single seats, all with executive foldout tables, and dual three‐place divans with berthing
capability in the aft of the cabin. A cockpit jump seat is installed for crew use only.
The cabin lighting was upgraded to an EMTEQ LED lighting system, including the entryway, cabin
and lavatories, as well as the cabin reading and table lights. Various storage compartments and
cabinets are located throughout the interior, including a crew closet, a mid‐cabin right‐hand
settee with built‐in storage, a mid‐cabin left‐hand work cabinet with an all‐in‐one Wi‐Fi printer,
and aft cabin wardrobe and entertainment/storage cabinets. The interior features a 115 VAC
electrical system with multiple outlets.
The cabin entertainment system consists of a forward left‐hand bulkhead LCD monitor, mid‐cabin
left‐hand bulkhead forward‐facing and aft‐facing LCD monitors, a DVD player, a cabin speaker
system, and Airshow® 4000. The cabin’s right‐hand forward‐facing VIP seat has enhanced
controls. This aircraft also features a Cobham SB‐400 Inmarsat satellite telecommunications
system with an ICG cabin cordless handset and an ICG cockpit corded handset, and
SwiftBroadband internet is available via onboard Wi‐Fi.
The interior features “Redwood Burl” gloss cabinetry veneer, “Polished Nickel” cabin hardware
plating, and off‐white Corian® galley and lavatory countertops. Scott Group “Tan Trac Tuft” wool
carpet is located throughout the cabin and lavatory, and “Sonic Gray” vinyl flooring is installed in
the galley. The cabin headliner, PSU panels, and aft lavatory closeout are covered in “Almond”
Ultraleather®, the window panels are finished in “Sand” Ultraleather®, and the lower sidewalls are
covered in “Antelope” fabric. The cabin seats, jump seat and lavatory seat are finished in “Oak”
leather, and the divans are covered in “Bijou” Chenille and “Wheat Geneve” fabrics.
The forward right‐hand galley provides for generous storage and functionality. Equipment
includes a TIA coffee maker, dual TIA ovens, a hot cup, dual stainless ice drawers, a trash
compartment, a countertop with pop‐out work surface, and multiple dedicated storage
compartments and drawers. The left‐hand galley annex features a gasper‐cooled catering storage
compartment, a pop‐out work surface, and multiple storage drawers.
Lavatories: Forward & Aft
The forward lavatory includes an electric‐flushing toilet with fold‐down sink and faucet, and the
aft lavatory contains a right‐hand electric‐flushing toilet opposite a lighted vanity with mirror and
multiple storage drawers and compartments.
An in‐flight accessible baggage compartment features fold‐down shelves and a coat rod.
The exterior was painted in November, 2011 by StandardAero – Springfield, IL in overall
Matterhorn White with Medium Silver & Squadron Blue stripes.
Remote Cabin Temperature Indicating System
ERDA Jump Seat with 3rd Crew Oxygen System
Main Entry Door Removable Forward Handrail
Pylon Baggage Light & Tow Bar Installation
Cockpit Dual Air Lite® LED Rechargeable Flashlights
Rear Service Compartment Ladder Installation (M2199)
DeVore Upper & Lower Tail Floodlights (STC SA3862SW)
Major SBs, STCs, and Modifications Incorporated:
SB F900EX‐001B – Extended CG & Increased Weight Limits
SB F900EX‐002 Rev. 1 – Installation of a Brake Heating System
SB F900EX‐178 – Lateral Engine Air Intakes ‐ Deflectors Added at the Air Discharge Louvers
SB F900EX‐193 – High Altitude Landing and Take‐off Capability
SB F900EX‐235 – New DEEC P/N 2118882‐2009 (Honeywell SB TFE731‐76‐5121)
SB F900EX‐259 Rev. 1 – Installation of an Automatic Bleed Override Controller
SB F900EX‐329 Rev. 3 – Wing Tank Modification
SB F900EX‐333 – Extension of “A” and “B” Inspection Intervals
SB F900EX‐459 – Passenger Door Electrical Lifting System Installation
SB 20 Rev. 1 – LED Nose Taxi Lamp Installation
STC ST02188SE – Aviation Partners Inc. Blended Winglets