CITATION CJ4 - Africair, Inc.

SPECIFICATION AND DESCRIPTIONCITATION CJ4October 2015Revision HUnits 525C-0200 to TBD

CITATION CJ4SPECIFICATIONAND DESCRIPTIONUNITS 525C-0200 TO TBDOCTOBER 2015REVISION HC e ssna A irc raft C ompanyP.O. B ox 7 7 06W ic hita, Kansas 6 7 27 7 -7 7 06

CITATION CJ4INTRODUCTIONCombining the latest technology sensors and displays in anintegrated package that is both smaller and lighter than traditional avionics, the Collins Pro Line 21 suite for the CJ4 isa true breakthrough in flight deck efficiency and pilot workload reduction. It integrates pilot information into intuitive,easy to interpret new formats with safety enhancing reversion capability.At the heart of all the advancements found in the Pro Line 21system are the Pro Line 21 radios and the Collins File Server Unit (FSU). The FSU serves as a portal for software anddatabase uploads, allowing new capabilities to be addedas airspace requirements and technology evolve. The netresult is a flexible, cost-effective, reusable architecture withinherent growth capability and true software mobility. Maximizing the system’s high-performance, partitioned processing capabilities, Ethernet interfaces and active matrix liquidcrystal display (AMLCD) flight displays, the FSU integrateswith this new technology to provide enhancements such asIntegrated Flight Information System (IFIS) with functionalities including electronic charting, graphical weather andenhanced mapping for the flight deck.All primary flight, navigation, engine and sensor data isgraphically presented on the system’s four large liquid crystal displays for easy scanning and integration. Standardpilot and copilot primary flight displays (PFDs) are teamedwith two enhanced multi-function displays (MFDs) featuring a flexibly displayed Engine Indicating and Crew AlertingSystem (EICAS) for maximum awareness of both the internalhealth of the aircraft and the external situation. Additionally,a Collins FMS-3000 Flight Management System and dualControl Display Units (CDUs) streamline and automate navigation and communication input functions. This helps to ensure more eyes-up time at the controls, giving pilots a betteroverall view of their real-time flight situation.There’s never been a system this capable in this category ofaircraft. But then, offering exceptional value is what Cessnaand the Citation CJ4 are all about.This Specification and Description is published for the purpose of providing general information for the evaluation ofthe design, performance, and equipment of the Cessna Citation CJ4, Units 525C-0200 to TBD. This document supersedes all previous Specification and Description documentsand describes only the Cessna Citation CJ4 Model 525C, itspowerplants and equipment.Due to the time span between the date of this Specificationand Description and the scheduled delivery date of the Aircraft, Cessna reserves the right to revise the Specificationwhenever occasioned by product improvements, government regulations or other good cause as long as such revisions do not result in a material reduction in performance.In the event of any conflict or discrepancy between thisdocument and the terms and conditions of the purchaseagreement to which it is incorporated, the terms and conditions of the purchase agreement govern.For additional information contact:Cessna Aircraft CompanyP.O. Box 7706Wichita, Kansas 67277-7706Telephone: 316-517-6449Telefax: 316-517-6640WARNING: This product contains Halon 1211, Halon 1301, and also R-134A. Furthermore, the product was manufacturedwith CFC-12 and 1-1-1 Trichloroethane, substances which harm public health and environment by destroying ozone in theupper atmosphere.Oc tober 2015, Revision H1

CITATION CJ4TABLE OF CONTENTSCESSNA CITATION CJ4 SPECIFICATION AND DESCRIPTIONSECTION PAGE1.General Description .1.1Certification .1.2Approximate Dimensions .1.3Design Weights and Capacities .2.Performance .3.Structural Design Criteria .4.Fuselage .5.Wing .6.Empennage .7.Landing Gear .8.Powerplants .9.Systems.9.1Flight Controls .9.2Fuel System .9.3Hydraulic System .9.4Electrical System .9.5Pressurization and Environmental System .9.6Oxygen System .9.7Ice and Rain Protection .10.Avionics .10.1General .10.2Instrument and Control Panels .10.3Avionics .10.4Miscellaneous Cockpit Equipment .11.Interior .11.1General .11.2Standard Interior Configuration .11.3Baggage .12.Exterior .13.Additional Equipment .14.Emergency Equipment .15.Documentation and Technical Publications .16.Computerized Maintenance Record Service .17.Limited Warranties .17.1Cessna Citation CJ4 Limited Warranty .11.2Williams FJ44-4A Limited Engine Warranty .18.Citation CJ4 Crew Training Agreement .FIGURE I — CITATION CJ4 EXTERIOR DIMENSIONS .FIGURE II — CITATION CJ4 INTERIOR DIMENSIONS .FIGURE III — CITATION CJ4 INSTRUMENT PANEL AND PEDESTAL LAYOUT .FIGURE IV — CITATION CJ4 STANDARD FLOORPLAN 323232424242528451320Oc tober 2015, Revision H

CITATION CJ41. GENERAL DESCRIPTION1. GENERAL DESCRIPTIONThe Cessna Citation CJ4 is a low-wing aircraft with retractable tricycle landing gear and a “T” tail. A pressurized cabin accommodates a crew of two and up to ninepassengers (eight is standard). Two Williams InternationalCo., LLC (Williams) FJ44-4A Full Authority Digital EngineControl (FADEC) controlled turbofan engines are pylonmounted on the rear fuselage. Fuel stored in the wingsoffers generous range for missions typical of this class aircraft. Space for baggage is provided in the nose and tailcone with additional storage space available in the cabin.Multiple structural load paths and system redundancieshave been built into the aluminum airframe. Metal bonding techniques have been used in many areas for addedstrength and reduced weight. Certain parts with non-critical loads such as the nose radome and fairings are madeof composite materials to save weight. The airframe design incorporates anti-corrosion applications and lightning protection.thorized service facilities provides a complete source forall servicing needs.1.1 CERTIFICATIONThe Model 525C is certified to the requirements of U.S.14 CFR Part 23, Commuter Category, including day, night,VFR, IFR, and flight into known icing conditions. It will alsobe certified for single pilot operations for U.S. registeredaircraft and for steep approach operations. The CitationCJ4 is compliant with all RVSM certification requirements.(Note: specific approval is required for operation withinRVSM airspace; Cessna offers a no charge service to assist with this process.)The Purchaser is responsible for obtaining aircraft operating approval from the relevant civil aviation authority.International certification requirements may include modifications and/or additional equipment; such costs are theresponsibility of the Purchaser.Cessna offers a third-party training package for pilots andmechanics, and various manufacturers’ warranties as described in this book. Cessna’s worldwide network of au-Oc tober 2015, Revision H3

CITATION CJ41. GENERAL DESCRIPTION(CONTINUED)50 ft 10in (15.49 m)22 ft 1 in (6.73 m)12 ft 4 in(3.76 m)15 ft 5 in(4.69 m)21 ft 2 in (6.45 m)53 ft 4 in (16.26 m)FIGURE I — CITATION CJ4 EX TERIOR DIMENSIONS4Oc tober 2015, Revision H

CITATION CJ41. GENERAL DESCRIPTION(CONTINUED)27 in(.69 m)181 in(4.60 m)60 in(1.52 m)58 in(1.47 m)24 in(.61 m)48 in(1.22 m)19 in(.48 m)15 in(.38 m)11 in(.28 m)29 in(.74 m)57 in(1.45 m)58 in(1.47 m)FIGURE II — CITATION CJ4 INTERIOR DIMENSIONSOc tober 2015, Revision H5

CITATION CJ41. GENERAL DESCRIPTION(CONTINUED)1.2 APPROXIMATE DIMENSIONSOverall Height . 15 ft 5 in (4.69 m)Overall Length . 53 ft 4 in (16.26 m)Overall Width . 50 ft 10 in (15.49 m)WINGSpan (does not include tip lights) . 50 ft 5in (15.37 m)Area . 330.0 ft2 (30.66 m2)Sweepback (at 25% chord) . 12.5 degreesHORIZONTAL TAILSpan (overall) . 22 ft 1 in (6.73 m)Area . 79.6 ft2 (7.40 m2)Sweepback (at 25% chord) . 20 degreesVERTICAL TAILHeight . 7 ft 5 in (2.26 m)Area . 59.3 ft2 (5.51 m2)Sweepback (at 25% chord) . 49 degreesCABIN INTERIORHeight (maximum over aisle) . 57 in (1.45 m)Width (trim to trim) . 58 in (1.47 m)Length (forward pressure bulkhead to aft pressure bulkhead) . 22 ft 4 in (6.81 m)LANDING GEARTread (main to main) . 12 ft 4 in (3.76 m)Wheelbase (nose to main) . 21 ft 2 in (6.45 m)1.3 DESIGN WEIGHTS AND CAPACITIESMaximum Ramp Weight . 17,230 lb (7,815 kg)Maximum Takeoff Weight . 17,110 lb (7,761 kg)Maximum Landing Weight . 15,660 lb (7,103 kg)Maximum Zero Fuel Weight . 12,500 lb (5,670 kg)Standard Empty Weight* . 9,920 lb (4,500 kg)Full Fuel Payload . 1,000 lb (454 kg)Maximum Payload . 2,180 lb (989 kg)Fuel Capacity (useable) at 6.70 lb/gal . 5,828 lb. (2,644 kg)* Standard empty weight includes unusable fuel, full oil, standard interior, and standard avionics.6Oc tober 2015, Revision H

CITATION CJ42. PERFORMANCEAll performance data is based on a standard aircraft configuration, operating in International Standard Atmosphere (ISA) conditions with zero wind. Takeoff and landing field lengths are based on a level, hard surface, dry runway. Actual performancewill vary with individual airplanes and other factors such as environmental conditions, aircraft configuration, and operational/ATC procedures.Takeoff Runway Length . 3,410 ft (1,039 m)(Maximum Takeoff Weight, Sea Level, 15 Flaps)Climb Performance . . . . 29 min to 45,000 ft (13,716 m)(Maximum Takeoff Weight, from Sea Level)Maximum Altitude . 45,000 ft (13,716 m)Maximum Cruise Speed ( 3%). 451 KTAS (836 km/hr or 519 mph)(14,000 lb, 31,000 ft (9,449 m))NBAA IFR Range (100 nm alternate) ( 4%) . 1,920 nm (3,556 km or 2,209 mi)(Maximum Takeoff

CITATION CJ4 1. GENERAL DESCRIPTION The Cessna Citation CJ4 is a low-wing aircraft with re-tractable tricycle landing gear and a “T” tail. A pressur-ized cabin accommodates a crew of two and up to nine passengers (eight is standard). Two Williams International Co., LLC (Williams) FJ44-4A Full Authority Digital Engine