McDonnell-Douglas T-45 Goshawk PDF eBook + Aircraft Flight Manuals

Price: $29.95

  • 1 magazine, 14 manuals, & photos
  • PDF contains 4,236 pages
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  • International orders welcome!
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July 1989

  • A-10 Close Support
  • Dyna-Soar – Also Ran in the Race for Space
  • Navy Wings of Gold

Manuals & Photos

  • T-45A NATOPS Flight Manual
  • T-45A NATOPS Flight Manual Changes
  • T-45AC Performance Charts
  • T-45AC Pocket Checklist Changes
  • T-45C Advanced NFO Strike Procedures
  • T-45C NATOPS Flight Manual 2000
  • T-45C NATOPS Flight Manual 2007
  • T-45C Pilots Pocket Checklist Changes
  • T-45 Weapons Strike
  • T-45 Aerodynamics Workbook
  • T-45 Carrier Qualification Flight Procedures
  • T-45 Familiarization
  • T-45 Out of Control Flight
  • McDonnell-Douglas T-45 TS Brochure
  • Over 90 T-45 Goshawk photos

McDonnell-Douglas T-45 Goshawk

  • T-45A Specifications
  • Variants
  • Cutaway
  • Videos

General Characteristics

  • Crew: 2
  • Length: 39 ft 4 in (11.99 m)
  • Wingspan: 30 ft 9.75 in (9.3917 m)
  • Height: 13 ft 6 in (4.11 m)
  • Wing area: 190.1 sq ft (17.66 m2)
  • Airfoil: root: Hawker 10.9%; tip: Hawker 9%
  • Empty weight: 9,394 lb (4,261 kg)
  • Gross weight: 12,750 lb (5,783 kg)
  • Max takeoff weight: 13,500 lb (6,123 kg)
  • Fuel capacity: 432 US gal (360 imp gal; 1,640 l) / 3,159 lb (1,433 kg) internal fuel (2,893 lb (1,312 kg) – early production aircraft), with provision for 2x 156 US gal (130 imp gal; 590 l) drop tanks underwing
  • Powerplant: 1 × Rolls-Royce Turbomeca F405-RR-401 turbofan engine, 5,527 lbf (24.59 kN) thrust de-rated (nominal thrust 5,845 lbf (25,999.86 N))

Performance

  • Maximum speed: 543 kn (625 mph, 1,006 km/h) at 8,000 ft (2,438 m), M0.84 at 30,000 ft (9,144 m)
  • Carrier launch speed: 121 kn (139 mph; 224 km/h)
  • Approach speed: 125 kn (144 mph; 232 km/h)
  • Never exceed speed: 575 kn (662 mph, 1,065 km/h) / M1.04 design dive limit at 3,281 m (10,764 ft)
  • Range: 700 nmi (810 mi, 1,300 km)
  • Ferry range: 700 nmi (810 mi, 1,300 km)
  • Service ceiling: 42,500 ft (13,000 m)
  • g limits: +7.33 3
  • Rate of climb: 8,000 ft/min (41 m/s) at sea level
  • Time to altitude: 30,000 ft (9,144 m) in 7 minutes 40 seconds
  • Wing loading: 346.7 lb/sq ft (1,693 kg/m2)
  • Thrust/weight: 0.41
  • Take-off distance to 50 ft (15 m): 3,610 ft (1,100 m)
  • Landing distance from 50 ft (15 m): 3,310 ft (1,009 m)

Armament

  • Usually none: One hardpoint under each wing can be used to carry practice bomb racks (can carry up to 12 Mk-76 practice bombs), rocket pods, or fuel tanks. A centerline hardpoint can carry a cargo pod for crew baggage.

Avionics

  • Smiths Industries, Ltd. AN/USN-2(V) Standard Attitude Heading and Reference System, later replaced by the BAE/Marconi AN/ASN-180 Navigation Guidance System
  • Rockwell Collins AN/ARN-144 VHF Omnidirectional Radio Range / Instrument Landing System
  • Honeywell AN/APN-194 Radar altimeter
  • Northrop Grumman AN/ASN-166 Inertial Guidance Set [1] Incorporates a Northrop Grumman (formerly Litton) LN-100G ring laser gyroscope, a Rockwell Collins Global Positioning System, and a Kalman filter

Communications Suite

  • Rockwell Collins AN/ARC-182 UHF/VHF radio
  • Honeywell AN/APX-100 identification friend or foe system
T-45A
Two-seat basic and advanced jet trainer for the US Navy and US Marine Corps
T-45B
Proposed land-based version which would have been basically a conventional Hawk furnished with a US Navy-spec cockpit and no carrier capability. The US Navy had wanted to procure the T-45B so that trainee pilots could benefit from an earlier training capability, but abandoned the idea during 1984 in favor of less-costly updates to the TA-4J and T-2C.
T-45C
Improved T-45A, outfitted with a glass cockpit, inertial navigation, and other improvements. All existing T-45As have been upgraded to the T-45C standard.
T-45D
Tentative designation for an envisioned upgrade of the T-45, potentially incorporating various manufacturing improvements and additional equipment, such as helmet-mounted displays.