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1982 Cessna II (550)

CESSNA 550 Citation II · Systems Description

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Overview

This document provides a detailed overview of the 1982 Cessna II (550) aircraft, including specifications, engine details, avionics, and interior and exterior ratings. It serves as a reference for potential buyers and aviation enthusiasts interested in the performance and features of this light business jet. Key information includes engine specifications, performance metrics, and cabin configurations, highlighting the aircraft's capabilities and modifications. The document emphasizes the aircraft's history, operational costs, and maintenance status, making it a comprehensive resource for understanding the Cessna 550 Citation II.

  • Total airframe time: 8,983.7 hours
  • Maximum certified ceiling: 43,000 feet
  • Fuel consumption: 193 gallons per hour
  • High-speed cruise: 376 knots
  • Typical seating: 6 passengers, maximum seating: 11 passengers

Document

Source

Originally published by flightsolution.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

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Document details

Type
Systems Description
Year
1982
Pages
2
File size
3.9 MB
Publisher
flightsolution.com
How rare is it?
4CESSNA 550 Citation II registered worldwide · 0 active

Common. Rarer than 12% of the aircraft models we track.

Documentation completeness
6/7

Most owners only have the POH. Here's the essential set for the CESSNA 550 Citation II.

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In this document

Aircraft Overview

The Cessna II (550) is a light business jet manufactured in 1982, with a total airframe time of 8,983.7 hours and 7,965 landings. It is available for sale or trade, with specific details on the aircraft's registration and serial number.

Engine Details

The aircraft is powered by two Pratt and Whitney JT15D-4 engines. Engine #1 has a total time since new (TTSN) of 1,983 hours and 1,787 cycles, while Engine #2 has a TTSN of 5,137 hours and 4,630 cycles, with a time since major overhaul (SMOH) of 1,550 hours.

Performance Specifications

The Cessna II has a maximum takeoff weight at sea level of 3,450 feet and at 5,000 feet and 25°C, it is 6,870 feet. The landing distance is 2,078 feet, and it has a certified ceiling of 43,000 feet. The aircraft consumes 193 gallons of fuel per hour and has a high-speed cruise of 376 knots.

Cabin and Baggage Capacity

The cabin can typically seat 6 passengers, with a maximum configuration of 11. The total cabin volume is 263 cubic feet, and the baggage capacity includes 36 cubic feet internally and 41 cubic feet externally.

Avionics and Equipment

The aircraft is equipped with a Sperry SPZ-500 avionics package, dual Collins communication radios, and a Honeywell CAS-67A TCAS-II system. It also features a Universal UNS-1K FMS with GPS, and a Fairchild F800 flight data recorder.

Full document text

Flight Solutions® 1982 Cessna II (550) 1521 Airport Blvd., Sumner County Regional Airport (M33), Gallatin, TN USA 37066 • Phone: (615) 452-5001 Fax: (615) 451-2371 • Email: info@flightsolution.com f l i g h t s o l u t i o n . c o m Aircraft Overview Price: Make Offer! Sale Type: For Sale, Trade, Year:1982 Manufacturer: Cessna Model: II (550) S/N: 550-0441 Registration: N476RS TTAF: 8983.7 Total Landings: 7965 Engine #1 Details Type: Pratt and Whitney JT15D-4 S/N: PCE-71203 Cycles SNEW: 1787 TTSN: 1983.0 SMOH: since NEW SHSI: “183” Engine #2 Details Type: Pratt and Whitney JT15D-4 S/N: PCE-71278 Cycles SNEW: 4630 TTSN: 5137.0 SMOH: 1,550.0 SHSI: due in 200 hours Avionics • EASA Equipped! • Avionics Package: Sperry SPZ-500 5-inch IFCS / Collins Pro Line II • FMS: Universal UNS-1K w/GPS • TCAS: Honeywell CAS-67A TCAS-II • FDR: Fairchild F800 • Communication Radios: Dual Collins VHF-22C w/8.33 spacing • Navigation Radios: Dual Collins VIR-30A w/FM immunity • Transponder: Dual Honeywell MST-67A enhanced Mode S • Weather Radar: Primus 300SL color • Autopilot: Sperry SPZ-500 IFCS • ADF’s: Dual Collins ADF-60 • Compass: Dual Sperry C-14D • CVR: Fairchild A100A • DME’s: Dual Collins DME-40 • Flight Director: Sperry SPZ-500 5-inch IFCS • Radar Altimeter: Sperry AA-300 • RMI: Dual Collins 332C-10 / Sandel ST-3400 • Stormscope: BF Goodrich WX-11J • TAWS: Sandel ST3400 • Artex C406 Three Frequency ELT Equipment • Sierra Radome • Hi Gross Weight • Aft Baggage Mod • 76 Cu Ft Oxygen System • RVSM • Freon Air Conditioning Interior Rating: 8 New complete custom interior in 2012 with Beige Leather seats, dark quilted custom inserts, Mid-Cabin Club arrangement, Ultra suede Headliner, aft belted private lav, Refreshment Center, LH & RH Executive Slim line Tables. It is beautiful. Exterior Rating: 7 New paint in 2012 in Sand Horn base with Copper and Gold Trim in a custom elegant scheme. Inspection Details Type: Phase 1-5B Date: 15 August 2019 Recent 91.411 & 91.413 & RVSM Cert. (April 2016) New Pilots Windscreen & Co-Pilots side window (April 2016) ** Please request a CESCOM 10/20 status for a complete maintenance summary ** General Characteristics • Takeoff at Sea Level, feet 3,450 • Takeoff at 5000’ 25°C 6,870 • Landing Distance, feet 2,078 • Certified Ceilings, feet 43,000 • Fuel Consumption, gallons per hour 193 • Total Variable Cost $1,447 • High Speed Cruise, knots 376 • Ranges, Four Pax, Nautical Miles (NM) • 1,355 • 600 NM Mission, Fight Time 1+45 • 1000 NM Mission, Flight Time 2+55 • Passenger Seating Configuration • Typical Seating 6 • Max Seating Configuration 11 • Cabin Volume (Cubic Feet) • Total Volume 263 • Cabin Dimensions • Length 16 • Height 4.8 • Width: Max/Flr 4.9/3.2 • Baggage Capacity (Cubic Feet) • Internal 36 • External 41 • Total Volume 77 Description: When the Citation II debuted in the light business jet market, it was one-of-a-kind. It sold 1,000 jets in its first four years on the market and was manufactured for sixteen years, making its Cessna’s best-selling private jet to date. The Citation II can carry eight passengers up to 1400 nm at a max cruise speed of 374 knots. Its two Pratt & Whitney JT15D-4 engines provide 2,500 pounds of thrust apiece on takeoff. It climbs quickly at a little more than 3,000 feet per minute and has a maximum service ceiling of 43,000 feet. The cockpit boasts 340 degrees visibility and simple controls for vital systems like fuel and de-icing. The Citation II can be configured to be flown by a single pilot, reducing travel/operating costs and allowing for more flexibility in flight planning. The Citation II has very good handling characteristics, due largely to its engineers’ decision to use the straight wing design. Not only does this make the jet less susceptible to Dutch rolls caused by strong gusts, but it also increases the ratio of lift per increment of angle-of-attack, which makes for effortless takeoffs and landings. Just because the Citation II’s systems are simple does not mean that they are not safe. The Citation II is certified under FAR part 25 airworthiness standards – these standards are mandatory for big airliners like the Boeing 747. Damage History No known damage history. Disclaimer The offer for sale of this aircraft is subject to contract and the aircraft may at any time be withdrawn from the market without prior notice. Specification is subject to verification by the purchaser and is not guaranteed for accuracy and Buyer should rely on their inspection as all aircraft are sold “as is, where is”. Delivered with fresh Phase 1-5B and ADS B compliance currently in progress now! This corporate owned and operated Citation II (550) has excellent history and care. Fully EASA equipped for European theater operations. Universal UNS 1K with GPS, TCAS II traffic advisory, Fairchild Flight Data Recorder (FDR) and much more. High Gross Weight modification allowing for greater payloads with aft baggage modification for greater volume. This is a great opportunity to own one of the most popular light jets ever produced and historically low pricing. Call today to learn more and reserve this aircraft in your name! Flight Solutions® 1982 Cessna II (550) 1521 Airport Blvd., Sumner County Regional Airport (M33), Gallatin, TN USA 37066 • Phone: (615) 452-5001 Fax: (615) 451-2371 • Email: info@flightsolution.com f l i g h t s o l u t i o n . c o m