Eurofighter EF2000 Two Seater Series Flight Manual 2002 – Twin Seat PDF

Description

Eurofighter EF2000 Two Seater Series Flight Manual 2002 – Twin Seat PDF

This is the EF2000 Two Seater Series Flight Manual issued under document reference AER(EP).1F-EF2000(T)-1 and dated 01 December 2002. Running to 749 pages, it is the complete flight manual for the twin-seat Eurofighter EF2000, covering every phase of operating the aircraft from cockpit familiarisation and pre-flight checks through to landing, emergency handling and adverse weather operation. The manual is aligned to the EJ200 MK 101 engine fit and to software configuration PSC 1.1 (APSP1 avionics, FPSP1a flight control, UPSP1b utilities control).

File Details

• Manual type: Flight Manual (aircrew operating manual)
• Aircraft: Eurofighter EF2000 Two Seater Series (Twin Seat)
• Document number: AER(EP).1F-EF2000(T)-1
• Edition: Original, Issue 0 (with change symbol convention described)
• Date of issue: 01 December 2002
• Engine fit: Two Eurojet EJ200 MK 101 two-spool turbofans with reheat
• Software configuration: PSC 1.1 / APSP1 / FPSP1a / UPSP1b
• Language: English
• Total pages: 749 (737 NATO RESTRICTED, 12 NATO UNCLASSIFIED, 1 blank)
• File format: PDF

Chapters Covered

The Eurofighter EF2000 Two Seater Series Flight Manual is organised into six independent sections plus a separate performance data volume (AER(EP).1F-EF2000(T)-1-1). The structure below reflects the manual’s own table of contents.

• Section 1 – Description: The Aircraft, Aircraft Dimensions, Cockpit Displays and Controls, Head Up Display, Multifunction Head Down Display, Manual Data Entry, HOTAS, Utilities Control System, Engines and Engine Systems, Secondary Power System and APU, Engine/APU Fire Protection, Fuel Supply and Transfer, Fuel Pressurisation and Venting, Air-to-Air Refuelling, Electrical Power Supply, Hydraulic Power Supply, Landing Gear System, Arrester Hook and Brake Chute, Flight Control System (Twin Seat), Autopilot and Autothrottle, Air Data System, Canopy and Windscreen, Escape System and Ejection Seat, Environmental Control System, Oxygen System, Lighting System, Avionic System Integration, Navigation System (LINS, GPS, Radar Altimeter, TACAN), Communication System, Warning Equipment, Recorders, Surveillance/Attack and Identification Subsystem, Defensive Aids Subsystem, Weapon System (gun, AMRAAM, SRAAM), Cockpit Access Ladder and Servicing Diagram.
• Section 2 – Normal Procedures: Alert Mode/Scramble and Cocking, Pre-Flight Checks (Safe for Parking, Initial, External, Ejection Seat), Strapping In and Unstrapping, Internal Checks Front/Rear Cockpit, Rear Cockpit Safety Checks (Solo Flight), Starting Engines, Crossbleed Engine Start, Start Failures, Dry Crank, Pre-Taxi and Before Take-Off Checks, Taxiing, Line Up, Takeoff, Normal and Minimum Time Climb, Cruise, In-Flight Refuelling, Holding, Descent and Recovery, TACAN, Radar/GCA and Circling Approaches, Go Around, Normal and Crosswind Landing, Touch and Go, Braking Technique, After Landing and Engine Shut Down, plus full Recovery Data tables.
• Section 3 – Emergency Procedures: Ground Emergencies and Ladder Not Locked, Abandoning and Emergency Ground Egress, Ejection, Abort and Tire Failure During Take-Off, Engine and Reheat Failure During Take-Off, APU, Engine and In-Flight Fires, Double and Single Engine Flame-out, Windmill and Assisted Relight, Engine Vibration, Oil Pressure and Oil Overtemperature, Engine Surge, DECU and Engine Control System Failures, SPS Computer, SPS Air Leak, Fuel Supply, Transfer, Over Temperature and Fuselage Leak, In-Flight Refuelling Probe Failure, Double and Single AC Generator Failure, Essential DC and Electrical Level 1/2 Failures, Battery and Generator Over Temperature, Gearbox Failure and Overtemperature, PTO Shaft Failure, SPS Overpressure, ATS/M Failure, Double and Single Hydraulic Failure, Double and Single Utility Failure, Hydraulic Over Temperature, Air in Hydraulics, FCS/Airdata Failures (Slats, Air Intake Cowl, Probe Heater, Airbrake, Baro Set, Datum Adjust/Trim, Low Speed Recovery, Autothrottle), Avionic Failures (Radar, LINS, Radar Altimeter, Nav Computer, TACAN, Attack Computer, CIU, CSG, GPS, Monitor Trip, IFF, GPWS, DASS, Flare and Chaff Dispensers), ECS Failures and Smoke/Fumes, Oxygen Failures, UCS Front Computer, Windscreen Heater, Canopy Not Locked, Single Engine Operations, Approach and Landing Emergencies, Landing Gear Failures and Armament System Failures.
• Section 4 – Adverse Weather: Turbulence and Thunderstorms, Snow, Ice, Rain and Slush, Effects of Ice and Snow during Takeoff, and Operation in Extreme Conditions.
• Section 5 – Operating Limitations: References the applicable Airworthiness Flight Limitation document.
• Section 6 – Flight Characteristics: Flight with Asymmetrical Stores, Flights with Autopilot/Autothrottle, Flights under Subsonic Conditions, Flights under Transonic and Supersonic Conditions and Single Engine handling.

As a whole, this EF2000 twin-seat flight manual gives an aircrew member or maintenance engineer a complete, integrated picture of how the aircraft is meant to be operated. The Description section alone covers every major aircraft system – engine, fuel, electrical, hydraulic, flight control, environment, escape and the whole avionic and weapon chain – while the Normal Procedures section lays out the exact switch selections, speeds and sequence for every routine phase. Emergency Procedures then provide the boldface actions and subsequent drills behind each DWP caption, and the Flight Characteristics section explains how the airframe actually behaves at low speed, in the transonic region and on a single engine. Technical values throughout are printed in the manual’s own units – bar for hydraulic pressures, knots KDAS for speeds, kilograms for mass and fuel – so the numbers a reader sees are the numbers used on the flight line.

What This Flight Manual Lets You Do

Owning the Eurofighter EF2000 Two Seater Series Flight Manual means you can follow the same operating logic the crew uses: preparing the aircraft on the ground, running the correct pre-taxi and pre-takeoff checks, and understanding what every warning caption on the Dedicated Warning Panel is actually telling you. The emergency section is written as a sequence – indications, boldface action, then the follow-up drill – so a reader can see exactly what would be done for a double hydraulic failure, an engine fire in flight, a fuel transfer fault, a DECU failure or an in-flight refuelling probe that will not lock.

It also serves as a systems reference. Instead of a block diagram alone, you get the full fuel transfer sequence with its stage order and low-flow mode, the hydraulic system’s utility isolation logic, the FCS control law behaviour in reversionary mode, the ejection seat sequence and minimum ejection heights, the ECS airflow paths during normal, alert and RAM AIR operation, and the full weapon chain from stores configuration monitoring through to AMRAAM and SRAAM launch sequencing.

IMAGES PREVIEW

For anyone training on, supporting or studying the twin-seat Eurofighter, this manual is the reference that ties the systems chapters, the procedures and the limitations together in one place. It is delivered as an instant PDF download – no shipping, no waiting – and can be read on a laptop, tablet or phone, or printed page by page for bench or cockpit-side use.