Beechjet 400A / Hawker 400XP (Model 400A) FAA Approved Airplane Flight Manual – PDF

Description

Beechjet 400A / Hawker 400XP (Model 400A) FAA Approved Airplane Flight Manual – PDF

The Beechjet 400A / Hawker 400XP (Model 400A) FAA Approved Airplane Flight Manual is the complete pilot-side operational manual for the Hawker Beechcraft 400A series, issued as P/N 128-590001-167B with a reissue date of June 23, 2011. This PDF combines the current AFM text with its Log of Temporary Changes, Log of Revisions, Log of Supplements, and the manufacturer-approved supplement pack into a single reference package covering the Beechjet 400A and Hawker 400XP by serial number.

File Details

• Manual Type: FAA Approved Airplane Flight Manual (AFM) with supplements
• Brand / Publisher: Hawker Beechcraft Corporation
• Models Covered: Beechjet 400A, Hawker 400XP (Model 400A)
• Engines Covered: Pratt & Whitney Canada JT15D-5, JT15D-5R
• Document Number: P/N 128-590001-167B
• Reissue Date: June 23, 2011
• Language: English
• Page Count: 1002 pages
• File Format: PDF

Chapters Covered

• Introduction, Certification Basis, Notations, Use of the Flight Manual, Revising the Flight Manual, Kit List
• Section 1 – General
• Section 2 – Operating Limitations (Airspeed Limitations, Instrument Markings for RK-1 thru RK-97 and RK-98 and After, Power Plant, Engine Limits, Thrust Reverser Limits, Starter/Generator, External Power Assisted Start, Battery Start, Generator Assisted Start, In-Flight Operation, Oil Specification, Weight Limits, Structural Limitations, Take-off Weight, Landing Weight, Fuel System, Approved Engine Fuels & Additives, Fuel Temperature Limitations, Fuel Management, Hydraulic System, Cabin Pressurization, Maneuvering Load Factors, Occupancy Limits, Avionic System, Autopilot, EFIS, TCAS, Flight Management System, Kinds of Operations, All Operations, Take-off and Landing Operations, En Route Operations)
• Section 3 – Emergency Procedures (Engine Failure During Takeoff Below/Above V1, Engine Fire, Engine Fire Detector Failure, Engine Shutdown or Failure In Flight, Dual Engine Flameout, Engine Failure In Landing Configuration, Engine Failure Autopilot Coupled, Low Oil Pressure, Low Fuel Pressure, Inadvertent Thrust Reverser Deployment On Takeoff and In Flight, Main Landing Gear Ground Safety Switch Failure, Inadvertent Overspeed, Emergency Landing, Loss of Airspeed Indication, Ditching Procedures, Fire and Smoke Protection, Electrical Fire or Smoke, Environmental System Smoke or Odor, Smoke Removal, Cabin Decompression, Oxygen Duration, Emergency Descent, Overpressurization, Windshield Overheat, Wing Anti-Ice Overheat, Horizontal Stab Ice Protection Failure, Loss of Both Generators, Battery Overheat, Trim Systems Malfunctions, Pitch/Roll/Rudder Trim Runaway, Power Brake Failure, Autopilot Disengagement, Autopilot Trim Fail, Autopilot Overspeed Recovery, Flight Director Malfunctions, Maximum Altitude Losses, Air Data Computer Failure, Electronic Flight Display Messages, PFD/MFD/ND/CDU Messages, Master Annunciator Panels)
• Section 3A – Abnormal Procedures (False Engine Start, Air Start Envelope 1 and 2, Pre-Start Check, Starter Assisted Start, Windmilling Start, Post-Start Check, Thrust Reverser Arm and Unlock Annunciators, High Oil Temperatures, Oil Filter Bypass, Engine Anti-Ice System Inoperative, EFC Failure, One Engine Inoperative Approach and Landing, Single Engine Reversing, One Engine Inoperative with a Reverser Deployed, Approach Climb, No-Flap Approach and Landing, Flaps 10° Approach and Landing, Landing with Ice Accumulation, Side Window Landing, Inadvertent Icing Encounter, Ice Detector Fail, Turbulent Air Penetration, Stall Warning Failure, Wing Tank Overpressure, Jet Pump Failure, Low Fuel Transfer Pressure, Low Fuel Quantity, Low Engine Fuel Feed Tank Quantity, Fuel Filter Bypass, Air Conditioning Overpressure/Overtemperature, Refrigeration Air Conditioning Malfunction, Bleed Air Duct Failure, Cabin Air Temperature, Defog Overtemperature, Vacuum Source Failure, Cabin or Aft Fuselage Door Unlocked, Windshield Cracked, Battery Feeder Failure, Emergency Bus Feeder Failure, Bus Feeder Failure, Battery Cutoff, Single Generator Failure, Inverter Failure, Pitot Heat Failure, Rudder Boost Failure, Take-Off Mistrim, Main/Aft Flap Asymmetry, Elevator/Rudder Control Binding, Jammed Stabilizer/Elevator/Spoiler/Rudder, Low Hydraulic Fluid Quantity, Low/High Hydraulic Pressure, Landing Gear Handle Lock, Landing Gear Not Down and Locked, Alternate Gear Extension, Anti-Skid Failure, Yaw Damp Failure, Single/Dual RTU Failure, Radio Remote Tuning Disabled, Electronic Flight Display Messages)
• Section 4 – Normal Procedures (Preflight Inspection, Cockpit/Cabin Inspection, Exterior Inspection, Cabin Door, Left/Right Nose, Right/Left Wing, Right/Left Nacelle, Empennage, Aft Baggage Compartment, Before Starting Engines, Starting Engines, Before Taxi, Taxi, Anti/Deice System Preflight Check, Engine and Wing Anti-Ice Checks, Horizontal Stabilizer Deice System Check, Before Takeoff, Takeoff, After Takeoff, Anti/Deice Systems In-Flight Operation, Climb FL180, Cruise, Fuel Management Procedures, Descent, Approach, Before Landing, Landing, Balked Landing, After Landing, Shutdown, Turnaround, Autopilot and Flight Director Preflight Checks and In-Flight Operation, Vertical Synchronization, Pitch/Turn Knob, Turbulence Mode, Autopilot Transfer, Yaw Damp Operation, Automatic Trim Operation, Mode Selection, Go-Around, Heading, Navigation, Approach, Half Bank, Vertical Speed, Level Change, Speed Hold, VNAV, Altitude Hold, FD Off, Flight Management System Programming, In-Flight Operation, TCAS Preflight Checks, Ground Operation, In-Flight Operation)
• Section 5 – Performance (Performance Limitations, Acoustic Levels, Supplemental Acoustic Levels, Operational Factors, Flight Test Performance Conditions, Definitions, General Information on Using Graphs, Pressure Altitude, Procedures for Use of Take-off Performance Charts, Take-off Weight Analysis, Take-off Flap Setting Selection, ECS OFF Takeoff, Icing-Conditions Takeoff, Take-off Flight Path Profile, Obstacle Clearance Analysis, Example Close-In and Distant Obstacle Clearance, Take-off Speeds, Approach and Landing Performance, Landing Weight Analysis, ECS OFF Approach/Landing, Icing-Conditions Approach/Landing, Unfactored and Factored Landing Distance, Take-off Speeds and Field Length Tables and Correction Graphs for Flaps 0°, 10° and 20°, Net Take-off Flight Path Segments, Enroute Net Climb Gradient, Maximum Landing Weight Charts, Landing Brake Energy, Accelerate-Stop Brake Energy, Turnaround Time)
• Section 6 – Weight & Balance / Equipment List (Basic Empty Weight and Balance, Sample Loading, Weight and Balance Terminology, Basic Empty Weight and Balance Form, Empty Weight and Balance Record, Dimensional Data, Airplane Loading Form Instructions, Weight and Balance Loading Form, Loading Envelope Table and Graph, Zero Fuel Weight Table, Usable Fuel Moment Table, Payload Data for RK-1 thru RK-97 / RK-98, RK-110 thru RK-379 / RK-380 and After, Cabin Arrangement Diagrams, Unusable Fuel, Engine Oil, Personnel Movement, Weighing Instructions)
• Section 7 – Supplements (Log of Supplements, HF-9000, Category II Operation, German Registered Airplanes, FDR, Mod Drawing 004359, AMS-5000 with and without FMS-97, WG ICE TEMP LO Annunciator, Austrian Registered Airplanes, Increased Gross Take-Off Weight to 16,300 Pounds, Optional Galley Configurations, JAR-OPS 1 Wet/Contaminated Runway Operation, Mode S Enhanced Surveillance, Honeywell AFIS, EGPWS with RAAS, Collins GPS-4000S, CDL, TDR-94D ADS-B Out)
• Manufacturer Approved Supplements (Deicing/Anti-Icing Fluids Type I, II, III, IV; Wet or Contaminated Runways; Metric Conversion Factors; Standard Instrument Departure Charts)

Across its seven AFM sections and full supplement pack, this Beechjet 400A / Hawker 400XP manual gives the flight crew a complete operational reference. Limitations, emergency and abnormal procedures, normal checklists, performance charts, and weight & balance data are all written directly for the Model 400A airframe and its JT15D engines, matching the serial-number effectivity used by Beechjet 400A and Hawker 400XP operators.

What This Manual Enables

• Operating the Beechjet 400A and Hawker 400XP within approved airspeed, weight, altitude, fuel, and system limitations
• Managing every emergency and abnormal checklist the FAA has approved for the 400A
• Computing take-off and landing performance, obstacle clearance, brake energy, and climb gradients
• Completing accurate weight and balance loading with the current loading envelope
• Reviewing anti/deice, fuel, hydraulic, electrical, and avionics system operation
• Applying the correct temporary changes and supplements that affect limitations, procedures, or performance

Because the Model 400A is certified under 14 CFR Part 25 and Part 36, the exact limitations and procedures in this AFM are what make a flight legal and safe. Crews who rely on second-hand notes or outdated revisions risk operating outside approved envelopes, misreading a fuel or weight limit, or following a procedure that no longer matches the installed configuration. Keeping the correct AFM on board is required – and keeping the correct revision level is just as important.

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This Beechjet 400A / Hawker 400XP (Model 400A) FAA Approved Airplane Flight Manual PDF is delivered instantly after payment. There is no shipping, no waiting, and no physical book to keep current by hand. Open the file on a laptop, tablet, or phone, print only the pages you need for a given flight, or load it on a shop computer for reference. The complete 1002-page Beechjet 400A / Hawker 400XP FAA Approved Airplane Flight Manual is ready to use the moment your download completes.