Airplane Flight Manual
CESSNA 550 Citation II · Flight Manual
Overview
This document is the Airplane Flight Manual (AFM) for the Cessna 550 Citation II. It serves as a comprehensive guide for pilots operating this aircraft, detailing essential information regarding performance, limitations, and operational procedures. The manual is designed to ensure safe and efficient flight operations, providing critical data such as weight and balance, fuel requirements, and emergency procedures. It is intended for use by pilots and aviation personnel to enhance their understanding of the aircraft's capabilities and operational guidelines.
- Maximum takeoff weight: 14,000 lbs (6,350 kg)
- Maximum cruise speed: 400 knots
- Service ceiling: 45,000 feet
- Takeoff distance at sea level: approximately 3,500 feet
- Emergency procedures must be reviewed before flight.
Document
Source
Originally published by skybrary.aero. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Flight Manual
- Pages
- 58
- File size
- 5.1 MB
- Publisher
- skybrary.aero
Specifications & performance
Extracted from this document.
V-speeds
- VREF
- 110
Common. Rarer than 12% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the CESSNA 550 Citation II.
Free — save the CESSNA 550 Citation Ii to your watchlist and track it in one place.
More CESSNA 550 Citation IImanuals & documents
See all 35 →- Installation Instructions for Citation Sunbeam LED Wing Landing/Taxi/Recognition LightsWiring Diagram
- APPENDIX 1 to AMC for CAR-66 AIRCRAFT TYPE RATINGS FOR CAR-66 AIRCRAFT MAINTENANCE ENGINEER’S LICENCESupplemental Type Certificate
- Master Minimum Equipment List (MMEL)Checklist
- Maintenance Service Plan – Business AviationService Bulletins
- SAFO 18015Airworthiness Directives
- INSTALLATION MANUAL FUEL/AIR DATA COMPUTERPerformance Data
- Type Acceptance Report TAR 10/21B/23 – Cessna 501-551Other Documents
- Cessna Citation CE-550 JT-15 Note Taking GuideChecklist
- Type Acceptance Report TAR 10/21B/12 – Cessna 500/550/560Other Documents
- PARTS LIST 199-164 CONVERSION KITParts Catalog
- AAIB Bulletin: 1/2010 G-JBIZ EW/C2008/03/02Other Documents
- Airworthiness Directives for CESSNA 550 Citation IIAirworthiness Directives
If you fly the CESSNA 550 Citation II, you may also be researching these.
In this document
Aircraft Specifications
The Cessna 550 Citation II features a maximum takeoff weight of 14,000 lbs (6,350 kg) and a maximum landing weight of 13,000 lbs (5,897 kg). The aircraft is powered by two Pratt & Whitney Canada JT15D-1A turbofan engines, each producing 3,500 lbs of thrust.
Performance Data
The Citation II has a maximum cruise speed of 400 knots and a service ceiling of 45,000 feet. The takeoff distance at sea level is approximately 3,500 feet under standard conditions.
Weight and Balance
The document provides detailed charts for calculating weight and balance, emphasizing the importance of adhering to the maximum weight limits to ensure safe flight operations.
Emergency Procedures
Emergency procedures are outlined for various scenarios, including engine failure, cabin depressurization, and electrical failures. Pilots are advised to familiarize themselves with these procedures to ensure preparedness.
Operating Limitations
The manual specifies operating limitations, including maximum airspeed, altitude, and load factors. Pilots must adhere to these limitations to maintain safety and compliance.
Safety notes
- Always adhere to the specified weight and balance limits.
- Review emergency procedures prior to each flight.
Full document text
AIRCRAFT ACCIDENT REPORT 5/94 Air Accidents Investigation Branch Department of Transport Report on the accident to Cessna 550 Citation II, G-JETB at Southampton (Eastleigh) Airport on 26 May 1993 This investigation was carried out in accordance with The Civil Aviation (Investigation of Air Accidents) Regulations 1989 London: HMSO © Crown copyright 1994 Applications for reproduction should be made to HMSO First published 1994 ISBN 0 11 551298 5 October 1992 5/92 6/92 LIST OF RECENT AIRCRAFT ACCIDENT REPORTS ISSUED BY AIR ACCIDENTS INVESTIGATION BRANCH British Aerospace ATP, G-LOGA, at Edinburgh Airport, Scotland, on 5 February 1992 British Aerospace ATP, G-BTPE, December 1992 at Sumburgh Airport, Shetland Islands, on 23 December 1991 Piper PA-28-161 Cadet, G-BPJT, April 1993 1/93 2/93 at Oxford Airport, Kidlington, on 12 July 1992 AS 332L Super Puma, G-TIGH, near the Cormorant 'A' platform, East Shetland Basin, on 14 March 1992 May 1993 3/93 4/93 5/93 1/94 2/94 Lockheed 1011 Tristar, 9Y-TGJ, near 'KIRN' VOR, Germany, on 9 March 1992 British Aerospace 146-300, G-UKHP, at Aberdeen Airport, Dyce, Scotland, on 31 March 1992 British Aircraft Corporation/SNIAS Concorde 102, G-BOAB, over the North Atlantic, on 21 March 1992 Aerospatiale AS355F1 Twin Squirrel, G-OHMS, Near Llanbedr Airfield, Gwynedd, on 8 December 1992 June 1993 August 1993 November 1993 January 1994 RAF Tornado GR1, ZG754 June 1994 and Bell JetRanger III, G-BHYW, at Farleton Knott near Kendal, Cumbria, on 23 June 1993 3/94 Boeing 737-2Y5A, 9H-ABA, June 1994 at London Gatwick Airport, on 20 October 1993 These Reports are available from HMSO Bookshops and Accredited Agents (iii) Department of Transport Air Accidents Investigation Branch Defence Research Agency Farnborough Hampshire GU14 6TD 9 June 1994 The Right Honourable John MacGregor Secretary of State for Transport Sir, I have the honour to submit the report by Mr M M Charles, an Inspector of Air Accidents, on the circumstances of the accident to Cessna 550 Citation II, G-JETB at Southampton (Eastleigh) Airport on 26 May 1993. I have the honour to be Sir Your obedient servant KPR Smart Chief Inspector of Air Accidents (v) Contents Glossary of Abbreviations Synopsis 1 Factual Information Page (ix) 1 2 1.1 History of the flight 2 1.2 Injuries to persons 4 1.3 Damage to aircraft 4 1.4 Other damage 4 1.5 Personnel information 5 1.5.1 Commander 5 1.5.2 First Officer 5 1.6 Aircraft information 5 1.6.1 Leading particulars 5 1.6.2 Aircraft weight and centre of gravity 6 1.6.3 Limiting wind conditions 6 1.6.4 Description of braking system 7 1.6.5 Scheduled landing performance 7 1.7 1.6.6 Distance required to go-around Meteorological information 8 8 1.7.1 Synoptic situation 8 1.7.2 Actual observation 9 1.7.3 Aftercast 9 1.7.4 Anemometry 9 1.8 Aids to navigation 9 1.9 Communications 10 1.10 Aerodrome and approved facilities. 10 1.10.1 Runway physical characteristics 10 1.10.2 Runway lighting 10 1.10.3 Runway slope 10 1.10.4 Runway friction measurements 10 1.11 Flight recorders 12 (vi) 1.12 Contents (continued) Wreckage and impact information 1.12.1 Accident site examination 1.12.2 1.12.3 Examination of the aircraft Subsequent detailed examination of the aircraft 1.13 Medical and pathological information 1.14 Fire 1.14.1 General 1.14.2 Fire service response 1.14.3 Fire damage to aircraft 1.14.4 Fire damage to the car 1.15 Survival aspects 1.15.1 Aircraft 1.15.2 Vehicles Page 13 13 14 15 20 20 20 20 21 22 22 22 1.17 1.16 Tests and research 1.16.1 Testing of the anti-skid components Additional information 1.17.1 Aerocharter (Midlands) Ltd company manuals 23 1.17.2 Tyre wear limitations 25 1.17.3 Factors affecting hydroplaning 25 1.17.4 Estimated braking performance 26 1.17.5 UK standards for measuring and reporting wheel braking action 23 23 23 222222222 27 on wet runways 1.17.6 Airport information 28 1.17.7 Arresting systems 29 1.18 New investigation techniques 30 2 Analysis 31 2.1 General 31 2.2 The runway surface 31 2.3 Aircraft braking performance assessment. 31 2.4 Crew performance 33 2.4.1 General 33 (vii) 2.4.2 Contents (continued) Crew working relationship Page 33 2.4.3 Flight preparation 34 2.4.4 Flight profile 34 2.4.5 Visual approach and landing 35 2.4.6 After landing 36 2.4.7 Evacuation 37 2.4.8 Summary 38 2.5 Airport Safety Aspects 38 2.6 Reaction of the Fire Services 39 2.7 The flight crew 27 2.8 3 Approach monitoring aid Conclusions 28 41 41 41 42 3(a) Findings 3(b) Causes 4 Safety Recommendations 5 Appendices Appendix A Photograph of accident site Appendix B Mu-meter Test Results Appendix C Figure C-1 Figure C-2 Comparison of Theoretical and Measured Runway Friction Ground Distance Required to Stop Appendix D Photographs of left and right tyres Appendix E Plan of Southampton (Eastleigh) Airport (viii) GLOSSARY OF ABBREVIATIONS USED IN THIS REPORT AAIB AIP amsl APS ATC BCARS °C, M, T CAP DME DFO ESDU FDR g hrs IAS ILS JARS km kt lb LDA mb mm mu NDB Air Accidents Investigation Branch Aeronautical Information Publication above mean sea level Aircraft Prepared for Service Air Traffic Control British Civil Airworthiness Requirements °celsius, true, magnetic Civil Aviation Publication distance measuring equipment Duty Fire Officer Engineering Science Data Unit Flight Data Recorder normal acceleration hours indicated airspeed Instrument landing system Joint Airworthiness Requirements kilometre(s) knot(s) pound(s) Landing Distance Available millibar(s) millimetre(s) coefficient of sliding friction non-directional beacon nautical mile(s) Precision Approach Path Indicators Public Safety Zone Public Transport pressure setting to indicate height above aerodrome pressure setting to indicate elevation above mean sea level Runway End Safety Area nm ОАТ PAPIS outside air temperature PSZ PT QFE QNH RESA RFFS RPM UK UTC VMC VOR Rescue and Fire Fighting Service revolutions per minute United Kingdom Co-ordinated Universal Time Visual Meteorological Conditions VHF omni range
Show full textShow less
(ix) Air Accidents Investigation Branch Aircraft Accident Report No: 5/94 Registered Owner: European Jet Ltd Operator: Aerocharter (Midlands) Ltd (EW/C93/5/1) Aircraft Type: Nationality: Registration: Place of Accident: Date and Time: Cessna 550 Citation II British G-JETB Southampton (Eastleigh) Airport Latitude: Longitude: 50° 56.98' N 001° 21.32' W 26 May 1993 at 0534 hrs All times in this report are UTC Synopsis The accident was notified to the Air Accidents Investigation Branch (AAIB) at 0550 hrs on 26 May 1993 and an investigation began the same day. The investigation was conducted by Mr M M Charles (Investigator in Charge), Mr R W Shimmons (Operations), Mr A H Robinson (Engineering) and Ms A Evans (Flight Recorders). The accident occurred when the aircraft, with two crew members aboard, was on a positioning flight from Oxford to Southampton and overran Runway 20 after landing with a tailwind on a wet runway. After leaving the runway, the aircraft came to rest on the nearby motorway, collided with two cars, and caught fire. The two flight crew sustained minor whiplash injuries, and the three car occupants also sustained minor injuries. The aircraft was destroyed. The investigation identified the following causal factors: (i) (ii) (iii) The commander landed with a reported tailwind of 15 knots (kt) which was outside the aircraft maximum tailwind limit of 10 kt specified in the Cessna 550 Flight Manual. The co-pilot did not warn the commander that he was landing with a reported tailwind component which was outside the aircraft limit. With a tailwind component of 10 kt, the landing distance available was less than the landing distance required. Three safety recommendations were made during the course of the investigation. 1 1 Factual Information 1.1 History of Flight The crew of G-JETB reported for duty at Oxford between 0430 and 0505 hrs on 26 May 1993. Their roster for the day was to position the aircraft to Southampton, pick up eight passengers and fly them to Eindhoven, take split-duty rest, fly eight passengers to Southampton and finally fly G-JETB to Biggin Hill for some engineering maintenance. G-JETB had arrived at Oxford the previous evening and had then been refuelled to full tanks. The charter movement between Southampton and Eindhoven was a regular occurrence each Wednesday; the normal arrangement had been for the aircraft and crew to position at Southampton the previous evening but, over the last few weeks the practice was for the operating crew to position the aircraft early on the Wednesday morning. The co-pilot had agreed with the airport authorities at both Oxford and Southampton that the aircraft would operate outside normal hours on the understanding that no fire cover would be provided. On the evening of 25 May 1993 he had telephoned Southampton operations to submit a flight plan for the flight to Eindhoven and also to confirm the early arrival at Southampton the next morning. Throughout the flight from Oxford to Southampton, the commander handled the aircraft from the left seat and the co-pilot operated the radio. Following the takeoff from Oxford at 0519 hrs the crew contacted Brize Norton ATC and agreed a Flight Information Service. They maintained VMC for the transit at 2,400 feet QNH and called Southampton ATC on their alternate radio at 0525 hrs when they were approximately 30 nautical miles (nm) from Southampton. The Southampton controller was surprised at their initial call and advised them that the airport did not open until 0600 hrs. The crew informed him that arrangements had been made for an early arrival and the controller asked them to standby while he checked this agreement. At 0527 hrs he called G-JETB, informed the crew that they could land before the normal opening hours and asked them to confirm that no fire cover was required. The crew confirmed this and were then told that Runway 02 was in use with a wind of 020°/14 kt and that there was a thunderstorm right over the airport. The crew then advised Brize Norton radar that they were going to Southampton ATC and left the Brize Norton frequency. Following a further check with Southampton they were given the 0520 hrs weather observation: "SURFACE WIND 040°/12 KT, THUNDERSTORMS, 2 OKTAS OF STRATUS AT 800 FEET, 3 OKTAS OF CUMULONIMBUS AT 1,800 FEET, TEMPERATURE 12°C, QNH 1007 MB, QFE 1006 MB, THE RUNWAY IS VERY WET." At 0530 hrs the controller asked the crew for the aircraft type and, after being told that it was a Citation II, told the crew that the visibility was deteriorating ("NOW 2,000 METRES IN HEAVY THUNDERSTORMS") and cleared them to the 2 Southampton VOR at 3,000 feet QNH. After checking that they were now IFR the controller confirmed the clearance, and the QNH of 1007 mb, and informed the crew that there was no controlled airspace and that he had no radar available to assist them. Shortly afterwards the controller advised the crew that: "ENTIRELY AT YOUR DISCRETION YOU MAY ESTABLISH ON THE ILS LOCALISER FOR RUNWAY 20 FOR VISUAL BREAK-OFF TO LAND ON RUNWAY 02." The commander accepted this offer and, within the cockpit, asked the co-pilot for the surface wind. He was informed that it was 040° but that earlier they had been given 020°/14 kt. At 0532 hrs the commander had positioned on the ILS for Runway 20 and began his descent; the co-pilot advised Southampton that they were established. The controller acknowledged this and again passed the QNH. Shortly afterwards he asked the crew to report at the outer marker and this message was acknowledged. At 0533 hrs the crew called that they were visual with the runway and the controller cleared them for a visual approach, left or right at their convenience, for Runway 02. As this transmission was taking place, the commander informed his co-pilot that they would land on Runway 20. The commander decided this because he could see that the weather at the other end of the runway appeared very black and he had mentally computed the tailwind component to be about 10 kt. After a confirmation request from the co-pilot to the commander, the co-pilot informed the Southampton controller that they would land on Runway 20. The controller then advised them that: "YOU'LL BE LANDING WITH A FIFTEEN KNOT, ONE FIVE KNOT, TAILWIND COMPONENT ON A VERY WET RUNWAY"; this was immediately acknowledged by the co-pilot with: "ROGER, COPIED THANK YOU". The crew continued with their approach, initially at 15 kt above their computed threshold speed (VREF) of 110 kt and then at a constant VREF+10 kt. Within the cockpit the commander briefed the co-pilot that if they were too fast the co-pilot was to select flap to the take-off position and they would go-around; they also discussed the use of the speedbrake and the commander stated that he would call for it when he wanted it. The speed at touchdown was within 5 kt of the target threshold speed and touchdown was in the vicinity of the Precision Approach Path Indicators (PAPIs), according to witnesses in the Control Tower and on the airport; the commander was certain that he had made a touchdown within the first 300 feet of the runway. The PAPIs are located 267 metres along the runway. Speedbrake was selected as the aircraft touched down and, although the commander applied and maintained heavy foot pressure on the brakes, no retardation was apparent; external observers reported heavy spray from around the aircraft. At some stage down the runway the commander stated that the brakes were not stopping them and the co-pilot called for a go-around; the commander replied: "NO WE CAN'T" as he considered that a go-around at that stage would be more dangerous. He maintained brake pressure and, in an attempt to increase distance, steered the aircraft to the right edge of the runway before 3 trying to steer back left. Initially the aircraft nose turned to the left and the aircraft slid diagonally off the right side of the runway on to the grass. It continued across the grass for a distance of approximately 233 metres while at the same time yawing to the left. However, 90 metres beyond the end of the runway there is an embankment which forms the side of the M27 motorway and G-JETB slid down this embankment on to the motorway. The aircraft continued to rotate as it descended and came to rest, having turned through approximately 150°, with its tail on the central barrier (see Appendix A). During these final manoeuvres the aircraft collided with two cars travelling on the eastbound carriageway; the aircraft and one of the cars caught fire. During the approach of the aircraft, the airport Rescue and Fire Fighting Service (RFFS) duty officer had discussed with the duty ATC controller the imminent arrival of G-JETB. Although not all checks had been complete, the fire officer offered his two fire vehicles as a weather standby; he did not declare his section operational but agreed with ATC that they would position themselves to the west of the runway. When the aircraft was 1/2 to 2/3 down the runway, the ATC controller considered that the aircraft would not stop in the runway available and activated the crash alarm. The fire section obtained clearance to enter the runway after G-JETB had passed their position and followed the aircraft. Assessing the situation on the move, the fire officer ordered the FIRE 2 vehicle to disperse through the crash gate to the motorway, and took his own vehicle (FIRE 1) to the edge of the embankment. On arrival, the fire section contained the fires. The occupants of the aircraft and cars escaped with minor injuries. 1.2 Injuries to persons Injuries Crew Passengers Others Fatal Serious Minor / None 2 3 1.3 Damage to aircraft Aircraft destroyed. 1.4 Other damage A Ford Sierra and a Renault 18 GTS, travelling eastbound on the M27 motorway, were struck by the aircraft. The Ford came to rest on its roof and the Renault engine compartment caught fire. Additionally, both vehicles had sustained heavy impacts. 4 1.5 1.5.1 1.5.2 1.6 1.6.1 Personnel information Commander: Licence: Instrument rating: Base check: Line check: Medical: Flying experience: Male, aged 63 years Airline Transport Pilot's Licence Renewed on 1 May 1992 6 March 1993 10 March 1993 Class 1 valid until 1 December 1993 Total all types Total on type Duty time: First officer: Licence: Instrument Rating: Base check: Line check: Medical: Flying experience: Last 90 days Last 28 days 16,700 hours 850 hours 71 hours 44 hours 32 hours rest prior to commencing duty at 0500 hrs on 26 May 1993. Male, aged 43 years Commercial Pilot's Licence Renewed 21 December 1992 21 December 1992 21 December 1992 Class 1 valid until 30 June 1993 Total all types 1,322 hours Total on type 109 hours Last 90 days 77 hours 33 hours Duty time: Aircraft information Leading particulars Type: Constructor's number: Year of manufacture: Certificate of Registration: Last 28 days 12 hours rest prior to commencing duty at 0430 hrs on 26 May 1993. Cessna 550 Citation II 550-0288 1981 Registered to European Jet Ltd 5



