1986 CESSNA CITATION SII
Cessna Citation SII · Systems Description
Overview
This document provides a detailed overview of the specifications and features of the 1986 Cessna Citation SII, a business jet known for its performance and comfort. It includes information on airframe specifications, engine details, avionics, and interior configurations. The document is intended for potential buyers and aviation enthusiasts looking to understand the capabilities and features of this aircraft model. Key performance metrics such as maximum takeoff weight, fuel capacity, and range are highlighted, along with descriptions of the aircraft's interior and additional equipment.
- Total Time: 5,411.9 hours
- Max Takeoff Weight: 15,100 lbs
- Range: 1,990 nautical miles
- Cabin Length: 15 ft 9 in
- Fuel Burn per Hour: 175 gallons per hour
Document
Source
Originally published by avskyjets.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Systems Description
- Year
- 1986
- Pages
- 5
- File size
- 1.1 MB
- Publisher
- avskyjets.com
Common. Rarer than 24% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the Cessna Citation SII.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
Free — save the S550 Citation SII to your watchlist and track it in one place.
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In this document
Specifications
The specifications section outlines the airframe and engine details of the 1986 Cessna Citation SII. The aircraft has a total time of 5,411.9 hours and has completed 5,213 landings. The engines are Pratt & Whitney JT15D-4B turbofans, with a total time since new (TTSN) of 5,411.9 hours. The aircraft is equipped with various avionics systems, including dual Collins VHF COMMS and a Garmin MX20 MFD.
Physical & Performance Specs
This section details the physical dimensions and performance capabilities of the Citation SII. The external length is 47 ft 2 in, width is 52 ft 2 in, and height is 15 ft. The cabin dimensions are 15 ft 9 in in length, 4 ft 10 in in width, and 4 ft 8 in in height. The maximum takeoff weight is 15,100 lbs, with a balanced field length of 3,240 ft and a landing distance of 3,437 ft. The aircraft has a maximum range of 1,990 nautical miles and a service ceiling of 43,000 ft.
Interior Features
The interior of the Citation SII is configured for eight passengers in a center four-place club arrangement, with additional seating options. The cabin features caramel leather seating, African Mahogany cabinetry, and a fully equipped aft lavatory. The interior was refurbished in November 2010, enhancing its comfort and aesthetics.
Avionics
The avionics suite of the Citation SII includes advanced systems such as Collins 2 Tube EFIS, dual Collins VHF COMMS, and a Global GNS-XLS FMS with GPS. Additional equipment includes a Garmin GPS 500, Sperry SPZ-500 autopilot, and a Stormscope for weather monitoring.
Full document text
AVSKY CORPORATION 1-941-882-5391 | sales@avskyjets.com | 1460 S. McCall Rd. Bldg-A, Unit 3G, Englewood, FL Asking Price: $995,000 Only 5,411.9 Total Hours Garmin MX20 MFD Thrust Reversers Freon Air 1986 CESSNA CITATION SII Serial Number: S550-0094 Registration: N19ZA Specifications Airframe Year Model: 1986 Total Time: 5,411.9 Total Landing: 5,213 MX Tracking Upon Request Engines TTSN: 5,411.9 / 5,411.9 TSOH: 0 / 1,819 SHOT: 0/1,819 Avionics Collins 2 Tube EFIS Dual Collins VHF COMMS Dual Collins VIR NAV Collins ADF-60A Dual Collins DME-42 Dual Collins RMI-30 Dual Collins TDR-90 Collins HF-220 HFC Sperry AA-300 ALT GDL 69 Sirius XM Weather Stormscope Global GNS-XLS FMS w/ GPS Garmin GPS 500 Garmin MX20 MFD BF Goodrich SKY-497 TAS Socata ELT Sperry SPZ-500 AP Sperry Primus 800 Radar Exterior Exterior Paint Overall Matterhorn White with Baby Blue and Black Decal Stripping. Interior Eight-passenger interior configured in a center four-place club arrangement, two forward facing seats located aft, and an aft facing seat located forward opposite the entry door. All passenger seating is completed in Caramel leather and complemented with a Camel carpet. Cabinetry is African Mahogany and includes a left-hand forward refreshment center with heated Mapco. Center club seating includes dual executive tables. Aft lavatory includes a hardwood door and a belted flushing toilet seat. Interior refurbished in November 2010. General S550-0094; N19ZA; This Low Time Citation SII is ready for its next owner. It is well equipped with Freon Air, Thrust Reversers and much more. Please contact us today for more information. FLIE PHOTOS DEPICTED HEREIN. AIRCRAFT SUBJECT TO PURCHASERS SOLE VERIFICATION, PRIOR SALE OR REMOVAL FROM THE MARKET Additional Equipment Freon Air Iridium Satcom Fairchild GA100 CVR Thrust Reversers Improved TKS System Aft Baggage Mod Cleveland Wheels and Brakes Recognition Lights 64 Cu. Ft. Oxygen System Davtron Digital Clock Additional Photographs Additional Photographs Physical & Performance Specs Engine Type: P&W JT15D-4B External Length: 47 ft 2 in External Width: 52 ft 2 in External Height: 15 ft Cabin Length: 15 ft 9 in Cabin Width: 4 ft 10 in Cabin Height: 4 ft 8 in Crew + Passengers: 2+11 Max Takeoff : 15,100 lbs Balanced Field Length: 3,240 ft Landing Distance: 3,437 ft Max Payload: 839 lbs Max / LRC Speed: 386kts/348kts Fuel Burn per Hour: 175 gph Useable Fuel: 869 gal Service Ceiling: 43,000 ft Range: 1,990 nm Information provided by Conklin & de Decker assumes certain flight profile characteristics Characteristics INFORMIATON HEREIN IS PROVIDED BY SOURCES BELIEVED TO BE ACCURATE BUT AVSKY PROVIDES NO WARRANTY. ALL INFROMAITON IS SUBJECT TO PURCHASERS VERIFICATION The improved Citation S/II (Model S550) was announced in October 1983 and first flew on February 14, 1984, before certification in July. It gained a supercritical airfoil developed for the Citation III and JT15D4B turbofans. It replaced the II from 1984, but the II resumed production from late 1985, and both were built until the Bravo introduction. Deliveries of the S/II amount to 160. The improved 2,500 lbf (11 kN) JT15D-4B has higher temperatures components, allowing more thrust at higher altitudes. It could seat 11 people and fuel capacity was increased to 5820 lbs. TKS fluid de-icing was used on airfoils leading edges in addition to bleed air for the engines. Courtesy: Wikipedia More About the Cessna Citation II