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Boeing 80A-1

January 5, 2009 by R.Vogelaar · Leave a Comment 

 

Boeing 80A-1 NC224M United Air Lines

Boeing 80A-1 NC224M United Air Lines

The Boeing 80 was designed in response to increased demand on Boeing Air Transport’s San Francisco-Chicago route. The Model 80 carried passengers in a spacious cabin appointed with leather upholstery, reading lamps, forced-air ventilation, and hot and cold running water. The first version carried 12 people.

  • Model 80 – original production version with Pratt & Whitney Wasp engines (4 built)
  • Model 80A – improved aerodynamics and Pratt & Whitney Hornet engines (10 built)
    • Model 80A-1 – version with revised empennage; all 10 Model 80As converted to this standard
  • Model 80B-1 – single Model 80A built with open flight deck. Later modified to Model 80A-1 standard
  • Model 226 – one-off Model 80A converted to executive transport for Standard Oil. Modified tail surfaces later adopted on all Model 80As (see Model 80A-1)

The Boeing 80A introduced aviation’s first female flight attendants.

NC224M is the only surviving example of the Boeing Model 80 series.

NC224M is the only surviving example of the Boeing Model 80 series.

Developing nation:

 United States of America

Manufacturer/designer: 

 Boeing Aircraft Company

Type aircraft:

 Transporter

First flight:

- 1929 September 12

 

 Boeing 80A-1

Cockpit crew:

2 pilots.

Passengers:

- 18  

Wing span:

24.38 m.

Wing area:

113.34 m².

Fuselage length:

17.22 m.

Height:

4.65 m.

Engines:

- 3  Pratt & Whitney 525-horsepower “Hornet”.

Weight:

- empty: 4800 Kg.

Max. take off weight:

7.983 Kg.

Cruise speed:

201 km/h.

Max. speed:

224 km/h.

Max. ceiling:

4.267 m.

Range:

740 km.

Lockheed Martin / Boeing F-22 Raptor

January 3, 2009 by Marcel van Leeuwen · 1 Comment 

f-22-lockheed-martin-boeing2

The Lockheed Martin/Boeing F-22 Raptor is an air dominance fighter due to replace the F-15C Eagle’s of the United States Air Force. 

In October 1986 the USAF launched the Advanced Tactical Fighter program and invited Lockheed and Northrop to build two prototypes each, by specification of the USAF, to be evaluated and tested.

For the engines General Electric (YF120) and Pratt & Whitney (YF119) were the choice of the USAF to build test models for the new ATF. 

Lockheed got together with General Dynamics and Boeing and their YF-22 flew for the first time on September 29th 1990. Northrop/McDonnell Douglas’s YF-23 made it’s first flight on August 27th that same year. 

The USAF selected Pratt &Whitney to develop their YF119 in April 1991 

The first F-22A (first of eleven) development aircraft took off on September 7th 1997, and the second on June 28th 1998. The first production Raptor will be delivered to the USAF around early 2003, after that the first operational unit will be active in 2005. A production of 295 Raptors has been authorized so far.


 

Developing Nation: United States
Task: Strike Fighter
First Flight: September 29th 1990
Crew: 1
Wing Span: 13,56 m
Wing Area: 78,04 m²
Length: 18,90 m
Height: 5,08 m
Engine (s): Class Pratt & Whitney F119-PW-100 afterburning turbofans with 156+ kN thrust
Thrust to Weight 1.08 (1.26 with 50% fuel)
Radar: RWR (Radar warning receiver) 463 km or more.Radar: 200-240 km against 1 m² targets (estimated)
Weight: 19700 kg
Max.Take off weight: 38000 kg
Wing load: 322 kg/m²
Max. Speed: - At altitude: 2410 Km/h (Mach 2.25)- Supercruise: 1963 km/h (Mach 1.82)
Max. Range: 2960 km with 2 external fuel tanks
Combat radius: 759 km
Ferry range: 3219 km
Service ceiling: 19812 m
Weapons: - Long barrel GE M61A2 Vulcan 20 mm cannon (internal)Air to Air:

- 6x AIM-120 AMRAAM and

- 2x AIM-9 Sidewinder and one of the following:

- 2x 450 kg JDAM or

- 2x Wind Corrected Munitions Despensers (WCMDs) or

- 8x 110 kg GBU-39 Small Diameter Bombs.

Hardpoints:

- 4x under-wing pylon stations can be fitted to carry 600 US gallon Sargent Fletcher drop tanks or weapons, each with a capacity of about 2268 kg.

   

The Raptor is only in service with the US air force, 122 are in service (July 2008)

Mc Donnel Douglas F/A-18 Hornet

January 2, 2009 by Marcel van Leeuwen · Leave a Comment 

F/A 18C Swiss air force

F/A 18C Swiss air force

The McDonnell Douglas F/A-18A/C is a single seat shipboard and shore-based multi-role fighter and attack aircraft. The F/A-18B/D is a two seat operational trainer. The F/A-18 fills a variety of roles: air superiority, fighter escort, suppression of enemy air defenses, reconnaissance, forward air control, close and deep air support, and day and night strike missions.

The Boeing F/A-18E/F Super Hornets are a third bigger than the F-18A/B/C and D Hornet with half as much parts. 

In the early 1970’s the US Navy would procure a version of the USAF’s winning light weight fighter contender as a low-cost supplement to the F-14 and as an A-7 replacement. The US Navy however was implacably hostile to the winning single-engine YF-16, and decided to adopt an aircraft developed from the losing Northrop YF-17 Cobra. McDonnell Douglas was brought in as prime contractor and the F/A-18 was born. 

The first flight of the Northrop YF-17A Cobra (72-1569) was on June 9th 1974, first flight of the YF-18A Hornet came on November 18th 1978 (160775) with McDonnell Douglas test pilot Jack Krings. The maiden flight of the F/A-18C (163427) took place on September 3rd 1986. First flight of the F/A-18E Super Hornet (165164) was November 29th 1995, the two seats F/A-18F followed on April 1st 1996. 

The F/A-18 has a digital control-by-wire flight control system which provides excellent handling qualities, and allows pilots to learn to fly the airplane with relative ease. At the same time, this system provides exceptional maneuverability and allows the pilot to concentrate on operating the weapons system. The F/A-18C/D Hornets carry the Advanced Medium Range Air-to-Air Missile (AMRAAM) and the infrared imaging Maverick air-to-ground missile. Two years later, the C/D models came with improved night attack capabilities. The new components included a navigation forward looking infrared (NAVFLIR) pod, a raster head-up display, night vision goggles, special cockpit lighting compatible with the night vision devices, a digital color moving map and an independent multipurpose color display. Although the F/A-18C/D’s future growth is now limited, it will also continue to fill a critical role in the U.S. Navy’s carrier battle group for many years to come and will be an excellent complement to the larger, longer range, more capable F/A-18E/F Super Hornet. 

A total of 1.670 F/A-18A/B/C/ and D Hornets have been delivered since 1978. 

F/A-18F Super Hornet US Navy

F/A-18F Super Hornet US Navy

The multi-mission F/A-18E/F “Super Hornet” strike fighter is an upgrade of the combat-proven night strike F/A-18C/D. The Super Hornet will provide the battle group commander with a platform that has range, endurance, and ordnance carriage capabilities comparable to the A-6 which have been retired. F/A-18E/F’s avionics and software have a 90 percent commonality with current F/A-18C/Ds. However, the F/A-18E/F cockpit features a touch-sensitive, upfront control display; a larger, liquid crystal multipurpose color display; and a new engine fuel display. The Boeing F/A-18E/F Super Hornets are a third bigger, with half as much parts. Increased engine power comes from the F414-GE-400, an advanced derivative of the Hornet’s current F404 engine family. The F414 produces 35 percent more thrust and improves overall mission performance. Enlarged air inlets provide increased airflow to the engines. This gives for aircraft carrier operations, about three times more payload can be brought back to the ship.

The US Navy is planning to procure a minimum of 432 Super Hornets.

The EA-18G will retain everything in it that the F/A-18F Super Hornet has today with two exceptions. The wing tip stations will have receiving antennas. The gun will be replaced with avionics boxes containing the LR-700 receiver and satellite communications, which interface with the ALQ-99 Tactical Jamming System pods. In November 15th 2001 Boeing successfully completed an initial flight demonstration of its EA-18G Airborne Electronic Attack (AEA) concept aircraft. The test used an F/A-18F Super Hornet to carry three ALQ-99 jamming pods and two fuel tanks while measuring noise and vibration data and assessing aircraft flying qualities.

The 5-year SDD (system design and development) program for the EA-18G runs from FY04 until early FY09 and encompasses all laboratory, ground test, and flight tests from component level testing through full-up EA-18G weapons system performance flight-testing. The EA-18G is 99 percent common with the F/A-18F Super Hornet.


 

Developing Nation: United States of America.
Manufacturer/Designer:  McDonnell Douglas.                    Major sub-contractor Northrop.
Task: Shipboard and shore-based multi-role fighter and attack aircraft.
First Flight: - YF/A-18A November 18th 1978 (160775).                          – F/A-18C September 3rd 1986 (163427).                                   – F/A-18E November 29th 1995 (165164).                                   – F/A-18F April 1st 1996 (165166).-EA-18G November 15th 2001 (165166).
First Delivery: F/A-18A May 1980.
First Operational: - F/A-18A/B October 1983.        – F/A-18C/D September 1987.   – F/A-18E/F September 2001.
Crew: - F/A-18A/C/E 1                       – F/A-18B/D/F 2                        – EA-18G 2
Ejection Seat: - Martin Baker MK.14 NACES (New USN ACES).
  Specifications: F/A-18C Hornet
Wing Span: 11,43 m and with tip-mounted AAM’s 12,31 m.
Wing Area: 37,16 m².
Length: 17,07 m.
Height: 4,66 m.
Engine (s): - Two General Electric F404-GE-400 turbofans with 71,2 kN.- Two General Electric F404-GE-402 EPE turbofans (since 1992) with 78,7 kN.
Weight: - Empty: 10.445 Kg.- Internal fuel: 4.926 Kg.

- External fuel: 3.053 Kg.

- Max. payload: 7.031 Kg.

Max. Take off weight: Max. take off: 25.401 Kg.
Max. Speed: 1.915 km/h at high altitude.
Operating altitude: 15.240 m.
Max. Range: - >3.336 km Ferry range.- 1.065 km Attack mission combat radius.

- 740 km Air to Air mission.

Performance: - CAP endurance from carrier 1 hour 45 min.
g limits: -3 to +9
Radar: - Hughes AN/APG-65 multi mode digital fire control unit. -  Hughes AN/APG-73 multi mode digital fire control unit (since 1994)
Centerline hardpoints): 3.
Underwing hardpoints: 6.
Wingtip hardpoints 2.
Weapons: - 20 mm M61A1 Vulcan six barrel rotary cannon with 578 rounds of ammunition.- AIM-7F/M Sparrow.

- AIM-9L/M Sidewinder.

- AIM-120 AMRAAM.

- AGM-62 Walleye.

- AGM-65 Maverick.

- AGM-84 Harpoon.

- AGM-84K Stand-off Land Attack Missile-Expanded Response.

- AGM-88A HARM.

- CBU-52 bombs.

- CBU-58 bombs.

- CBU-59 cluster bombs.

- CBU-71 bombs.

- CBU-87 cluster bombs.

- CBU-89 bombs.

- CBU-90 bombs.

- CBU-92 bombs.

- CBU-93 bombs.

- GBU-10 Paveway II.

- GBU-12 Paveway II.

- GBU-15 guided weapons.

- B57 nuclear bombs.

- B61 nuclear bombs.

- GP Bombs.

- Joint Direct Attack Munitions.

- Paveway bombs.

- 5-in Zuni unguided rockets.

Extra: FLIR Sensor on the starboard intake is an infra-red sensor pod.

 

  Specifications: Boeing F/A-18E Super Hornet
Manufacturer:  Boeing.
Ejection Seat: Martin Baker MK. US-10S (SJU5/6).
Wing Span: - 13,62 m with missiles.                 – 9,32 m with folded outer wings.
Wing Area: 46,45 m².
Length: 18,31 m.
Height: 4,88 m.
Engine (s): Two General Electric F414-GE-400
Weight: - Empty: 13.864 Kg.- Internal fuel: 6.171 Kg.

- External fuel: 7.439 Kg.

- Max. payload: 8.050 Kg.

Max. Take off weight: Max. take off: 29.937 Kg.
Max. Landing weight: Max. landing: 19.460 Kg.
Max. Speed: 1.950 km/h at high altitude.
Operating altitude: 15.240 m.
Max. Range: 3.054 km.
Performance: Combat radius:
- 720 km hi-lo-lo-hi attack profile with two 480 gallon tanks and four 1000 lbs bombs plus two Sidewinders for self-defense.
- 855 km on interdiction mission with three 480 gal tanks.
- 1230 km hi-hi-hi profile with two AIM-9, four Mk.83 bombs, three tanks, two sensor pods.
- 800 km for fighter escort with two Sidewinders and two AMRAAM’s, internal fuel only    Max. endurance from carrier 2 hours 15 minutes.
g limits: + 7,5.
   
Radar: Raytheon APG-79 Active Electronically Scanned Array.
   
Centerline hardpoints): 3.
Underwing hardpoints: 6.
Wingtip hardpoints 2.
Weapons: - M61A1 20mm cannon with 400 rounds.- AIM-7 Sparrow.

- AIM-9 Sidewinder.

- AIM-120 AMRAAM.

- AGM-45 Shrike.

- AGM-62 Walleye ER/DL.

- AGM-65E Maverick.

- AGM-84 Harpoon.

- AGM-84H SLAM-ER land attack missiles.

- AGM-88 HARM anti-radiation missiles.

- AGM-114 Hellfire.

- AGM-130.

- AGM-154 JSOW.

- CBU-52 bombs.

- CBU-59 bombs.

- CBU-72 bombs.

- CBU-87 cluster bombs.

- CBU-89 bombs.

- CBU-90 bombs.

- CBU-92 bombs.

- CBU-93 bombs.

- Mk 20 Rockeye bombs.

- GBU-10 Paveway II.

- GBU-12 Paveway II.

- GBU-15 guided weapons.

- GBU-24 laser-guided bombs.

- GBU-31 JDAM.

- GBU-32 JDAM

- B57 nuclear bombs.

- B61 nuclear bombs.

- Mk.84, Mk.82LD, Mk.82HD, Mk.63, Mk.62, Mk.65, Mk.20 and Mk.83 GP Bombs.

- LAU 58 rocket launcher.

- Mk.20 Rockeye bombs

- Paveway bombs.

- 5-in Zuni unguided rockets.

- MATRA Mistral.

- TALD (air-launched decoy).

Extra: Fast Tactical Imagery (FTI-II), a photo reconnaissance intelligence strike module.

Weapons for the F/A-18E Super Hornet:

f-18-weapons 

F/A-18 Hornet operators:
Australia. - 57 F/A 18A
  - 18 F/A-18B
Canada. - 98 F/A-18A (CF-188)
  - 40 F/A 18B (CF-188B)
Finland.  - 57 F/A-18C
  - 7 F/A-18D
Kuwait. - 32 F/A-18C
  - 8 F/A-18D
Malaysia. - 8 F/A-18D
Spain. - 60 EF-18A+
  - 12 EF-18B+
  - 24 F/A-18A (ex US Navy)
Switzerland. - 26 F/A-18C
  - 8 F/A-18D
United States. - 523 F/A-18A
  - 90 F/A-18B
  - 466 F/A-18C
  - 160 F/A-18D
  - 432 F/A-18E/F (on-order)

F/A-18 in combat: 

United States:

In operation Prairie Fire March 15th-24th 1984, the Hornet went into action for the first time, flying several ship to shore air strikes against Libyan shore installations that were harassing the US fleet. All Hornets returned to the carriers without any mishap’s.

Desert Storm January 17- February 28 1991:

During the Gulf War (Iraq), 190 navy and US Marines Hornets were used in action, 106 from aircraft carriers and 84 from land based US Marine units. One Hornet was lost in combat, and two in non-combat accidents. Two F/A-18C’s scored air-to- air kills with the AIM-9 sidewinder (two Iraqi Chinese built MiG-21 F-7A’s)

Canada was the second nation with the Hornet in Desert Storm, they had the nickname “Desert Cats”

Southern Watch: March 1 1991- May 1 2003:

Most of the US Marine and US Navy F/A-18 Hornet squadrons were in Operation Southern Watch (non-flying zone southern Iraq) land-based (Saudi Arabia) of from aircraft-carriers (Gulf). 

In July 2002, the VFA-115 “Eagles” embarked on the first ever Super Hornet combat deployment.  Their performance was nearly flawless, flying 214 combat missions in support of “Operation Enduring Freedom” and “Operation Southern Watch” with a 100% combat sortie completion rate.  The Eagles dropped 22 JDAM on 14 targets in OSW with total success.

Deliberate Force: Aug.- Sept. 1994:

During the war in Yugoslavia F/A-18’s of the following countries were in action: 

United States:    

- US Navy

- US Marines Corps

Canada:

Nickname “Balkan Rats”

Spain:

Allied Force: March 24 – June 10 1999:

From Aviano AB, Italy, Canadian and Spanish Hornets flew combat-missions in Kosovo and former Yugoslavia.

Enduring Freedom October 7 2001 – :

Most of the US Marine and US Navy F/A-18 Hornet squadrons were in Operation Enduring Freedom, land-based (Manas, Kyrgyzstan) or from aircraft-carriers (Northern Indian Ocean). They flew combat-air-patrol and air-to-ground missions against the Taliban regime and Al-Qaeda in Afghanistan.

Iraqi Freedom March 20 2003 – April 9 2003:

These from land-based and aircraft-carriers operating Hornets squadrons were in the Area of Operations:

VMFA-115 US Marines and VFA-201 US Navy with F/A-18A(+)

VMFA(AW)-121, VMFA(AW)-225, VMFA-323, VMFA-314, US Marines and VFA-27, VFA-192, VFA-195, VFA-151, VFA-137, VFA-113, VFA-25, VFA-37, VFA-105, VFA-15, VFA-87, VFA-94, VFA-146, VFA-22 and VFA-147 US Navy with F/A-18C/D.

VFA-14, VFA-41 and VFA-115 US Navy with F/A-18E/F Super Hornet.

On April 2nd 2003 a F/A-18C of VFA-195 from USS Kitty-Hawk (CV-63) was shot-down by friendly-fire (Patriot missile) in central Iraq, pilot killed. 

Before hostilities ceased and victory declared on April 9, 2003, the VFA-115 “Eagles” with F/A-18E/F dropped 380,000 pounds of ordinance and passed three and a half million pounds of fuel in the tanker support role. 

The first operational flight of the Fast Tactical Imagery (FTI-II), a photo reconnaissance intelligence strike module, takes place aboard an F/A-18F from USS Abraham Lincoln (CVN-72), flying over Iraq during Operation Iraqi Freedom.

Boeing 787

December 26, 2008 by Marcel van Leeuwen · 2 Comments 

b787-roll-out

Unparalleled Performance

The 787-8 Dreamliner will carry 210 – 250 passengers on routes of 7,650 to 8,200 nautical miles (14,200 to 15,200 kilometers), while the 787-9 Dreamliner will carry 250 – 290 passengers on routes of 8,000 to 8,500 nautical miles (14,800 to 15,750 kilometers). A third 787 family member, the 787-3 Dreamliner, will accommodate 290 – 330 passengers and be optimized for routes of 2,500 to 3,050 nautical miles (4,600 to 5,650 kilometers).

In addition to bringing big-jet ranges to mid-size airplanes, the 787 will provide airlines with unmatched fuel efficiency, resulting in exceptional environmental performance. The airplane will use 20 percent less fuel for comparable missions than today’s similarly sized airplane. It will also travel at speeds similar to today’s fastest wide bodies, Mach 0.85. Airlines will enjoy more cargo revenue capacity.

Passengers will also see improvements with the new airplane, from an interior environment with higher humidity to increased comfort and convenience.

boeing-787-roll-out

Advanced Technology

The key to this exceptional performance is a suite of new technologies being developed by Boeing and its international technology development team.

Boeing has announced that as much as 50 percent of the primary structure — including the fuselage and wing — on the 787 will be made of composite materials.

An open architecture will be at the heart of the 787’s systems, which will be more simplified than today’s airplanes and offer increased functionality. For example, the team is looking at incorporating health-monitoring systems that will allow the airplane to self-monitor and report maintenance requirements to ground-based computer systems.

Boeing has selected General Electric and Rolls-Royce to develop engines for the new airplane. It is expected that advances in engine technology will contribute as much as 8 percent of the increased efficiency of the new airplane, representing a nearly two-generation jump in technology for the middle of the market.

Another improvement in efficiency will come in the way the airplane is designed and built. New technologies and processes are in development to help Boeing and its supplier partners achieve unprecedented levels of performance at every phase of the program. For example, by manufacturing a one-piece fuselage section, we are eliminating 1,500 aluminum sheets and 40,000 – 50,000 fasteners.

Continuing Progress

The Boeing board of directors granted authority to offer the airplane for sale in late 2003. Program launch occurred in April 2004 with a record order from All-Nippon Airways. Since that time, 45 customers have placed orders for 584 airplanes from six continents of the world, making this the most successful launch of a new commercial airplane in Boeing’s history.

The program has signed on 43 of the world’s most capable top-tier supplier partners and together finalized the airplane’s configuration in September 2005. These partners have started detailed design and, with Boeing, are connected virtually at 135 sites around the world to work toward major assembly in 2006. Eleven partners from around the world started facility construction for a total of 3 million additional square feet to create their major structures and bring the next new airplane to market.

The 787 program opened its final assembly plant in Everett in 2007. First flight  December 15, 2009 with certification, delivery and entry into service occurring in December 2010.

Developing Nation: United States of America.
Manufacturer/Designer: Boeing Company.
First Flight: December 15, 2009
First Delivery: Fourth quarter of 2010
Boeing 787-3 Dreamliner:
Brief Description:
The Boeing 787-3 Dreamliner is a super-efficient airplane with new passenger-pleasing features. It features a wing and structure optimized for shorter-range flights. It will bring the economics of large jet transports to the middle of the market, using 20 percent less fuel than any other airplane of its size.
Cockpit crew 2
Seating 290 – 330 passengers
Range 4650 – 5660 Km.
Configuration Twin aisle
Cross section 5.74 M.
Wing span 52 M.
Length 57 M.
Height 17 M.
Engine (s) - Two General Electric GENX (GE Next Generation).- Two Rolls Royce’s Trent 1000.
Cruise speed 902 Kph. (Mach 0.85)
Max. takeoff weight 165100 Kg.
Total cargo volume 124,6 M³
Program milestones - Authority to offer Late 2003- Certification/Entry into service 2010
  Boeing 787-800 Dreamliner.
Boeing 787-8 Dreamliner:
Brief Description:
The Boeing 787-8 Dreamliner is a super-efficient airplane with new passenger-pleasing features. It will bring the economics of large jet transports to the middle of the market, using 20 percent less fuel than any other airplane of its size.
Cockpit crew 2 (Similar flight deck of a 777)
Seating 210 -250 passengers
Range 14200 – 15200 Km.
Configuration Twin aisle
Cross section 5.74 M.
Wing span 60 M.
Length 57 M.
Height 17 M.
Engine (s) - Two General Electric GENX (GE Next Generation).- Two Rolls Royce’s Trent 1000.
Cruise speed 902 Kph. (Mach 0.85)
Max. takeoff weight 219540 Kg.
Total cargo volume 124,6 M³
Program milestones - Authority to offer late 2003- Assembly start 2006
Boeing 787-9 Dreamliner:
Brief Description:
The Boeing 787-9 Dreamliner is a slightly bigger version of the 787-8. Both are super-efficient airplanes with new passenger-pleasing features. It will bring the economics of large jet transports to the middle of the market, using 20 percent less fuel than any other airplane of its size.
Cockpit crew 2 (Similar flight deck of a 777)
Seating 250 – 290 passengers
Range 14800 – 15750 Km.
Configuration Twin aisle
Cross section 5.74 M.
Wing span 62 M.
Length 63 M.
Height 17 M.
Engine (s) - Two General Electric GENX (GE Next Generation).- Two Rolls Royce’s Trent 1000.
Cruise speed 902 Kph. (Mach 0.85)
Max. takeoff weight 244940 Kg.
Total cargo volume 152.9 M³
Program milestones -Entry into service in late 2011

Here’s a look at the primary testing being done on each airplane in the 787 flight test fleet. Additional tests will be conducted on all airplanes.

Airplane Tests
ZA001
Rolls-Royce
Flutter
  Systems – Landing Gear/Brakes/Hydraulics
FF 15-12-2009 Aero – Low Speed Performance
  Stability and Control
  Flight Controls
ZA002
Rolls-Royce
Stability and Control
  Systems – Electrics
FF 22-12-2009 Autopilot
  Avionics – miscellaneous
  Propulsion
ZA003
Rolls-Royce
Systems
  Noise
  Flight Deck
  Avionics
  Electromagnetic Effects (EME)/High Intensity Radio Frequency (HIRF)
  Cabin – interior
  Extended Twinjet Operations (ETOPS)
ZA004
Rolls-Royce
Aero – High-Speed Performance
  Propulsion – Performance
FF 24-02-2010 Flight Loads Survey
  Community Noise
  ETOPS
ZA005
GE
Flutter
  Aerodynamic Performance
  Propulsion
  Systems
  Stability and Control
  Flight Controls
  Avionics
  Community Noise
  ETOPS
ZA006
GE
EME
  HIRF
  ETOPS
CustomerName Country Region Model Engine Order Date Total
Aeroflot RUSSIA Europe 787-8   05-Sep-2007 22
Aeromexico MEXICO Central America and Mexico 787-8 GE 15-Aug-2006 2
Air Berlin GERMANY Europe 787-8   07-Jul-2007 25
Air Canada CANADA North America 787-8 GE 10-Nov-2005 14
Air Canada CANADA North America 787-8 GE 23-Apr-2007 23
Air China CHINA East Asia 787-8 RR 22-Aug-2005 15
Air Europa SPAIN Europe 787-8 RR 30-Mar-2007 8
Air India INDIA South Asia 787-8 GE 30-Dec-2005 27
Air New Zealand NEW ZEALAND Oceania 787-9 RR 25-Aug-2004 2
Air New Zealand NEW ZEALAND Oceania 787-9 RR 26-Oct-2005 2
Air New Zealand NEW ZEALAND Oceania 787-9 RR 14-Feb-2007 4
Air Pacific FIJI Oceania 787-9 GE 19-Apr-2006 5
Air Pacific FIJI Oceania 787-9 GE 14-Dec-2007 3
ALAFCO KUWAIT Middle East 787-8 GE 26-Sep-2006 6
ALAFCO KUWAIT Middle East 787-8 GE 14-Mar-2007 6
ALAFCO KUWAIT Middle East 787-8 GE 06-Jul-2007 10
All Nippon Airways JAPAN East Asia 787-3 RR 26-Jul-2004 30
All Nippon Airways JAPAN East Asia 787-8 RR 26-Jul-2004 20
Arik Air NIGERIA Africa 787-9   30-Mar-2007 3
Arik Air NIGERIA Africa 787-9   11-Sep-2007 4
Avianca COLOMBIA South America 787-8 RR 04-Oct-2006 10
Aviation Capital Group U.S.A. North America 787-8   30-Mar-2007 5
AWAS IRELAND Europe 787-8 RR 29-Dec-2004 4
AWAS IRELAND Europe 787-8 RR 17-Jul-2006 2
Azerbaijan Airlines AZERBAIJAN Central Asia 787-8 GE 22-Feb-2007 3
Biman Bangladesh Airlines BANGLADESH South Asia 787-8   22-Apr-2008 4
Boeing Business Jet U.S.A. North America 787-8   15-Aug-2006 1
Boeing Business Jet U.S.A. North America 787-8 GE 27-Jun-2007 1
Boeing Business Jet U.S.A. North America 787-8   31-Jul-2007 1
Boeing Business Jet U.S.A. North America 787-8   30-Nov-2007 1
Boeing Business Jet U.S.A. North America 787-8   20-Dec-2007 1
Boeing Business Jet U.S.A. North America 787-9   28-Jul-2006 2
Boeing Business Jet U.S.A. North America 787-9 GE 29-Sep-2006 1
Boeing Business Jet U.S.A. North America 787-9 GE 11-May-2007 1
British Airways UNITED KINGDOM Europe 787-8 RR 24-Dec-2007 8
British Airways UNITED KINGDOM Europe 787-9 RR 24-Dec-2007 16
C.I.T. Leasing Corporation U.S.A. North America 787-8 GE 19-Sep-2006 2
C.I.T. Leasing Corporation U.S.A. North America 787-8   19-Sep-2006 3
C.I.T. Leasing Corporation U.S.A. North America 787-8   03-Jul-2007 5
China Eastern Airlines CHINA East Asia 787-8 GE 14-Nov-2005 15
China Southern Airlines CHINA East Asia 787-8 GE 16-Dec-2005 10
Continental Airlines U.S.A. North America 787-8 GE 30-Jun-2005 5
Continental Airlines U.S.A. North America 787-8 GE 31-Dec-2005 2
Continental Airlines U.S.A. North America 787-8 GE 06-Jun-2006 1
Continental Airlines U.S.A. North America 787-9 GE 06-Jun-2006 12
Continental Airlines U.S.A. North America 787-9 GE 12-Mar-2007 5
Dubai Aerospace Enterprise UNITED ARAB EMIRATES Middle East 787-8   31-Dec-2007 15
Ethiopian Airlines ETHIOPIA Africa 787-8 GE 30-Jun-2005 8
Ethiopian Airlines ETHIOPIA Africa 787-9 GE 30-Jun-2005 2
Etihad Airways UNITED ARAB EMIRATES Middle East 787-9   10-Mar-2008 35
First Choice Airways – See cod UNITED KINGDOM Europe 787-8 GE 17-Feb-2005 6
First Choice Airways – See cod UNITED KINGDOM Europe 787-8 GE 25-Sep-2006 2
First Choice Airways – See cod UNITED KINGDOM Europe 787-8 GE 27-Feb-2007 4
Gulf Air BAHRAIN Middle East 787-8   18-Jan-2008 16
Hainan Airlines CHINA East Asia 787-8 GE 28-Nov-2005 8
Icelandair ICELAND Europe 787-8 RR 28-Feb-2005 2
Icelandair ICELAND Europe 787-8 RR 31-Mar-2006 2
ILFC U.S.A. North America 787-8 GE 07-Oct-2005 8
ILFC U.S.A. North America 787-8 RR 07-Oct-2005 2
ILFC U.S.A. North America 787-8   07-Oct-2005 6
ILFC U.S.A. North America 787-8   19-Jul-2006 2
ILFC U.S.A. North America 787-8   24-Jan-2007 1
ILFC U.S.A. North America 787-8   18-Jun-2007 48
ILFC U.S.A. North America 787-9 RR 07-Oct-2005 4
ILFC U.S.A. North America 787-9 RR 24-Jan-2007 1
ILFC U.S.A. North America 787-9 RR 18-Jun-2007 1
ILFC U.S.A. North America 787-9   18-Jun-2007 1
JAL International JAPAN East Asia 787-3 GE 10-May-2005 13
JAL International JAPAN East Asia 787-8 GE 10-May-2005 17
JAL International JAPAN East Asia 787-8 GE 30-Mar-2007 5
Jet Airways INDIA South Asia 787-8   29-Dec-2006 10
Kenya Airways KENYA Africa 787-8   06-Mar-2006 6
Kenya Airways KENYA Africa 787-8   15-Dec-2006 3
Korean Air SOUTH KOREA East Asia 787-8 GE 31-May-2005 10
LAN Airlines CHILE South America 787-8 RR 31-Oct-2007 18
LAN Airlines CHILE South America 787-9 RR 31-Oct-2007 8
LCAL CHINA East Asia 787-8   16-May-2005 1
LCAL CHINA East Asia 787-8 RR 16-May-2005 5
LCAL CHINA East Asia 787-8   13-Jul-2007 5
LCAL CHINA East Asia 787-8 RR 13-Jul-2007 1
LCAL CHINA East Asia 787-9   31-Dec-2005 8
LCAL CHINA East Asia 787-9   03-Mar-2006 1
LOT Polish Airlines POLAND Europe 787-8 RR 08-Sep-2005 7
LOT Polish Airlines POLAND Europe 787-8 RR 13-Feb-2007 1
Monarch Airlines UNITED KINGDOM Europe 787-8 RR 16-Aug-2006 6
Nakash U.S.A. North America 787-9 RR 01-Dec-2006 2
Northwest Airlines U.S.A. North America 787-8 RR 06-May-2005 18
PrivatAir SWITZERLAND Europe 787-8   14-Nov-2006 1
PrivatAir SWITZERLAND Europe 787-8   15-Jan-2008 1
Qantas AUSTRALIA Oceania 787-8 GE 30-Mar-2006 15
Qantas AUSTRALIA Oceania 787-9 GE 30-Mar-2006 30
Qantas AUSTRALIA Oceania 787-9 GE 30-Nov-2007 20
Qatar Airways QATAR Middle East 787-8 GE 05-Apr-2007 30
Royal Air Maroc MOROCCO Africa 787-8 GE 29-Nov-2005 4
Royal Jordanian JORDAN Middle East 787-8 GE 30-Mar-2007 2
Royal Jordanian JORDAN Middle East 787-8 GE 11-Nov-2007 2
S7 Group RUSSIA Europe 787-8   29-May-2007 15
Shanghai Airlines CHINA East Asia 787-8 GE 22-Aug-2005 9
Singapore Airlines SINGAPORE Southeast Asia 787-9   10-Oct-2006 20
Sky Peace Limited CHINA East Asia 787-8   21-May-2007 1
Travel Service CZECH REPUBLIC Europe 787-8   27-Mar-2007 1
TUI GERMANY Europe 787-8   15-Sep-2006 11
Unidentified Customer Unidentified Unidentified 787-8   28-Jul-2006 2
Unidentified Customer Unidentified Unidentified 787-8 GE 18-Jan-2007 2
Unidentified Customer Unidentified Unidentified 787-8 RR 23-Nov-2007 2
Unidentified Customer Unidentified Unidentified 787-8   04-Dec-2007 1
Unidentified Customer Unidentified Unidentified 787-8   14-Jan-2008 23
Uzbekistan Airways UZBEKISTAN Central Asia 787-8 GE 29-Jun-2007 2
VALC VIETNAM Southeast Asia 787-8   20-Dec-2007 8
Vietnam Airlines VIETNAM Southeast Asia 787-8   16-Nov-2005 4
Vietnam Airlines VIETNAM Southeast Asia 787-8   21-Dec-2007 4
Virgin Atlantic Airways UNITED KINGDOM Europe 787-9 RR 09-Mar-2007 15
Total 896
Customer Name Country Region Model Engine Order Date Total

(Boeing.com)

Boeing F-15 ‘Eagle’

December 21, 2008 by Marcel van Leeuwen · Leave a Comment 

f-15e-97-218-ln-usaf

McDonnell Douglas F-15A/C Eagle is a single-seat air superiority fighter.

The F-15E Strike Eagle is an all-weather two-seat dual role aircraft for strike / interdiction.

The F-15 was ordered “off the drawing board”, and there was to be no prototype as such and no competitive fly off against other manufacturer’s aircraft. One of the more unusual aspects of the Eagle development program was the use of large 3/8-scale glider models of the F-15 which were dropped from an NASA-operated NB-52B (52-0008) at the NASA Dryden Flight Research Center. The models were made of aluminum, wood, and fiberglass. During the drops, the models were under radio control from the ground, and were directed through high angle of attack, stalling, and spinning maneuvers. At the end of the flights, the models deployed a parachute and were recovered in midair by a helicopter.

The first flight of the F-15A (71-0280) was on 27 July 1972, first flight of the F-15B (71-290) took place on 7 July 1973. The operational career of the Eagle began with the first delivery of an F-15A (74-0083) to TAC’s 1st TFW at Langley AFB, Virginia. From June 1979 A and B models were succeeded in production by the F-15C (78-0468) and the two-seat trainer F-15D (78-0561).

The Multi-Stage Improvement Program (MSIP) MSIP II is that portion of the program which handles the F-15C/D. The major part of MSIP II is to fit the APG-70 radar and the AIM-120 AMRAAM. The first MSIP II aircraft was F-15C 84-001, first flown on 20 June 1985.


The F-15E Strike Eagle has been a kind of second generation F-15, after test flying with the second two-seater (71-0291), the first production F-15E (86-0183) flew on 11 December 1986. Although it possesses air to air combat capability the F-15E Strike Eagle specializes in the air to ground task and can carry a load of 11.113 kg, witch includes conventional and tactical nuclear weapons. Another key of the F-15’s weapons delivery system is the LANTIRN (Low Altitude Navigation and Targeting Infra-Red for Night) pods, they make the job of fighter-pilots much easier.

Developing Nation: United States.
Manufacturer/Designer: McDonnell Douglas from 1997 Boeing
Task: Air Defense/Ground Attack.
First Flight: - F-15A  71-0280 July 27th 1972.- F-15B 71-0290 July 7th 1973.- F-15C 78-0468 February 26th 1979.- F-15D  78-0561 July 12th 1979.

- F-15J  79-0280/02-8801 JASDF June 4th 1980.

- F-15E  86-0183 December 11th 1986.

- F-15S  93-0852/ 5505 RSAAF June 19th 1995.

- F-15I  94-0286/201 IDF September 12th 1997.

- F-15K  2005 ?

First Delivery: January 9th 1976 1st TFW at Langley AFB, VA. USA
First Operational:
Crew: F-15A/C/J single seat. F-15B/D/DJ/E/S/I/K dual seats
F-15A  specification:
Ejection Seat: McDonnell Escapac IC-7
Wing Span: 13,05 m.
Wing Area: 56,48 m².
Length: 19,43 m.
Height: 5,63 m.
Engine (s): - Pratt & Whitney F100-PW-100 turbofans each rated at 65.26 kN dry and 106.0 kN with afterburn. (2x)
Weight: - Empty: 12.973 Kg.- Empty F-15B: 13.337 Kg.- Internal fuel: 5.260 Kg.- External fuel: 5.395 Kg.

- Max. payload: 7.257 Kg.

Max. Take off weight: Max. take off: 25.401 Kg.
Cruise Speed: 917 km/h.
Max. Speed: 2.655 km/h at 10.975 m.
Max. Range: 4.631 km.
Performance: Max. endurance hours.
g limits: -3 to +9
Radar: - Hughes APG-63 coherent pulse-Doppler radar.- F-15A/B MSIP Raytheon APG-70 look-down/shoot-down radar.
Centre line hard point(’s): - 4 for AIM-7M and 1 for drop-tanks.
Underwing hard points: -2 (each pylon takes 2 AIM-9M and 1 drop-tank).
Weapons: - One M61A1 Vulcan 20-mm cannon with 940 rounds.- AIM-7M Sparrow.- AIM-9M Sidewinder.- AIM-120 AMRAAM only for F-15A/B MSIP.
F-15C specification:*
Ejection Seat: McDonnell Douglas ACES II zero-zero.
Engine (s): - Pratt & Whitney F100-PW-220 turbofans each rated  at  65.26 kN dry and 106.0 kN with afterburn. (2x)
Weight: - Empty: 12.973 Kg.- Empty F-15D: 13.337 Kg.- Internal fuel: 6.103 Kg.- External fuel: 4.423 Kg.

- Max. payload: 10.705 Kg.

Max. Take off weight: Max. take off: 30.844 Kg.
Operating altitude: 18.290 m, absolute ceiling 30.480 m.
Max. Range: 5.745 Km.
Performance: Max. endurance 5:15 hours and 15 hours with flight refueling.
Radar: - Hughes APG-63 X-band pulse-Doppler and- F-15C/D MSIP   Raytheon APG-70 look-down / shoot-down radar.
Extra: - Conformal fuel tanks (CFT) on the sides of the intakes.

* Generally similar to the F-15A except in the following particulars

F-15E specification:*
Task: Air-to-ground strike.
Crew: 2
Ejection Seat: McDonnell Douglas ACES II zero-zero.
Engine (s): - Two Pratt & Whitney F100-PW-229 each rated at 75,62 kN dry and 129,0 kN with afterburn. (2x)
Weight: - Empty: 14.379 Kg.- Internal fuel: 5.952 Kg.- External fuel: 9.818 Kg.- Max. payload: 11.113 Kg.
Max. Take off weight: -Max. take off: 36.741 Kg.
Cruise Speed: 917 km/h.
Max. Speed: 2.655 km/h at high altitude.
Operating altitude: 18.290 m.
Max. Range: 4.445 Km.
g limits: + 9
Radar: - Raytheon APG-70 look-down / shoot-down radar.
Centre line hard point(’s): 13.
Underwing hard points: 2.
Weapons: - Vulcan M61A1 cannon with 512 rounds.- AIM-7M Sparrow.- AIM-9M Sidewinder.- AIM-120 AMRAAM.

- AGM-45 Shrike.

- AGM-65 Maverick.

- AGM-88 HARM.

- AGM-130.

- CBU-52 bombs.

- CBU-58 bombs.

- CBU-71 bombs.

- CBU-87 cluster bombs.

- CBU-89 bombs.

- CBU-90 bombs.

- CBU-92 bombs.

- CBU-93 bombs.

- Mk 20 Rockeye bombs.

- GBU-10 Paveway II.

- GBU-12 Paveway II.

- GBU-15 guided weapons.

- B57 nuclear bombs.

- B61 nuclear bombs.

Extra: Martin-Marietta LANTIRN navigation (AN/AAQ-13) and targeting (AN/AAQ-14) pods.

* Generally similar to the F-15A except in the following particulars

F-15 operators:

Israel. 49 F-15A
10 F-15B
18 F-15C
15 F-15D
25 F-15I *
Japan. 165 F-15J
48 F-15DJ
Saudi Arabia. 86 F-15C
26 F-15D
72 F-15S *
South-Korea. 40 F-15K *
USAF. 355 F-15A
57 F-15B
420 F-15C
61 F-15D
236 F-15E

* F-15E variants .

F-15 in combat:

Israel :

The first IDF/AF action with Eagles took place on 27 June 1979, since that day the F-15’s of the Israeli Air Force scored 17 air to air victories.

Saudi Arabia:

On 5 June 1984, Eagles of No 6 Squadron were involved in an air battle with Iranian piloted F-4 Phantoms witch were threatening Saudi oil fields. Two of the intruders were shot down by AIM-7 Sparrows. This was the first time (and the only) that McDonnell Douglas fighters fought each other. One RSAF F-15 shot down a pair of Iraqi Dassault Mirage F-1’s during Desert Storm.

Desert Storm 17 January – 28 February 1991:

The USAF had five F-15C and two F-15E squadrons when the (air) war against Iraq began. Although the F-15E was still not fully combat-ready, 48 F-15Es flew in the Gulf War. F-15Es joined other Coalition aircraft in searching for and attacking Iraqi “Scud” missile launchers. These Scud hunt missions were largely unsuccessful, but the F-15Es attacked many other Iraqi targets of opportunity. The F-15C’s scored 32 aerial kills, of a total of 41 victories. Twenty-four of these kills were achieved with the Sparrow missile, eight by AIM-9 sidewinders. One F-15E scored an aerial kill by dropping a laser-guided bomb on an airborne Iraqi helicopter. No F-15C/D Eagle fighters were lost during Desert Shield / Storm, two F-15E Strike Eagles were lost in action.

Provide Comfort 1 March 1991 – 1 January 1997

Northern/Southern watch: 1 January 1997 – 1 May 2003:

F-15C’s of the USAF shot down three Iraqi Su-22’s with the AIM-9 and one Pilatus PC-9 trainer.

On 14 April 1994 there was a tragic ‘Friendly Fire’ incident over Northern Iraq, when a pair of F-15C’s shot down two UH-60 Black hawks, killing 26 American and United Nations personnel.

Deliberate Force: Aug.- Sept. 1994:

F-15C were in combat air patrols, and never shot down a Serbian aircraft (all F-16 kills) The F-15E was in air to ground actions.

Allied Force: 24 March – 10 June 1999:

On the first day of Allied Force 24 March 1999, F-15C’s killed four Serbian MiG-29’s with AIM-120 AMRAAM’s. One pilot Major J.Kwhang from the 493rd FS shot-down two aircraft.

Enduring Freedom 7 October 2001 – :

F-15E 89-0487 shot-down a Mi-24 Hind helicopter in Afghanistan.

Iraqi Freedom 20 March 2003 – April 2003:

USAF F-15C/D’s from Al Jaber AB, Kuwait and F-15C/D from Prince Sultan AB, Saudi Arabia flew together with F-15E Strike Eagles combat-missions in Iraq. One F-15E (88-1694/SJ) of 333rd FS, 4th FW from Seymour Johnson AFB, NC was shot-down near Tikrit in Iraq on 6 April 2003, the pilots were Killed in Action.

Boeing 757-200

December 10, 2008 by R.Vogelaar · Leave a Comment 

Boeing 757-236 OY-GRL Greenlandair

Boeing 757-236 OY-GRL Greenlandair

Known for its fuel efficiency and clean and quiet operation, the 757-200 entered production in 1981. Boeing delivered the first to launch customer Eastern Airlines on December 22, 1982.

Three principal models were eventually produced – the 757-200, 757-300, and the 757-200 freighter. In addition, Boeing produced one 757-200 Combi. October 28, 2004 was the 1.050th and final 757 a Shanghai Airlines 757-200, was the centerpiece of a ceremony at the company’s Renton, Washington factory. The final 757 will be the 1.049th delivered to an airline or military operator . Boeing uses the first 757 as a test bed. 

  • * 757-200: Standard version.
  • *
  • * 757-200PF Package Freighter: Developed for United Parcel Service. Large freight door forward, single crew door and no windows; up to 15 standard 2.24 × 3.18 m cargo pallets on main deck.
  • *
  • * 757-200M Combi: Boeing’s mixed cargo/passenger configuration with windows; upward-opening cargo door to port (forward) 3.40 × 2.18 m; carries up to three 2.24 × 2.74 m cargo containers and 150 passengers; one delivered to Royal Nepal Airlines.
  • *
  • * 757-200SF Special Freighter: Boeing Airplane Services will purchase 757-200s from British Airways and other operators and modify them to 757SF Special Freighter configuration for lease to DHL Worldwide Express. The modification, which is also available to other customers, provides 226.5 m3 of cargo space with payload of 27,215 kg and range of over 3.704 km.
  • *
  • * 757-200 `Catfish’: Boeing’s own 757-200 prototype (N757A) fitted with radar nose in Lockheed Martin F-22A profile and representative F-22A swept wing section above flight deck containing conformal radar antennas for advanced radar trials; first flight in this configuration March 11, 1999.
  • *
  • * VC-32A: Boeing 757-2G4. Four, with PW2040 engines, ordered August 8, 1996 as replacements for VC-137s of USAF’s 89th Airlift Wing at Andrews AFB, Maryland. First aircraft (98-0001) flew February 11, 1998 and was delivered to 89th AW on June 19, 1998. Further three followed on June 23, November 20 and November 25, 1998. Post-production modifications, performed at Boeing’s Wichita facility and completed on first aircraft on April 2, 1999, include installation of auxiliary fuel tanks, capacity 6.984 liters in forward and aft cargo holds, increasing range to 9,260 km; self-deploying forward airstairs; crew ladder; SATCOM upgrade; and 378 liter potable water tank.
  • *
  • * 757-300: Stretched version. Described separately.

 

Boeing 757-236 G-BIKB British Airways

Boeing 757-236 G-BIKB British Airways

Boeing 757-23A N510FP Hispania

Boeing 757-23A N510FP Hispania

 

Developing nation: United States of America.
Manufacturer/designer:  Boeing Commercial Airplane Company.
Production line: closed October 28, 2004.
Type aircraft: medium range narrow body airliner.
First flight: - 757-200 February 19, 1982, N757A.- 757-200F August 13, 1987, N401UP.- 757-300 August 2, 1998, N757X.
First delivery: - 757-200 December 22, 1982 to  Eastern Airlines.- 757-200F September 17, 1987 to UPS.- 757-300 March 10, 1999 to Condor
  Boeing 757-200
Cockpit crew: two pilots.
Passengers single class: 228.
Passengers two class: -   12 first class.- 188 economy class.
Cabin length: 36,09 m.
Cabin diameter: 3,54 m.
Cabin height: 2,13 m.
Cargo volume: - under floor 51 m³.
Wing span: 38,05 m.
Wing area: 185,24 m².
Wing sweep: 25 degrees.
Fuselage length: 47,32 m.
Fuselage diameter: 3,76 m.
Height: 13,56 m.
Horizontal tail unit: 15,24 m.
Wheelbase: 18,29 m.
Track: 7,32 m.
Engines: - two Pratt & Whitney  PW2037 each rated 162.8 kN.- two Pratt & Whitney  PW2040 each rated 178.4 kN.- two Rolls Royce RB211-535E4 each rated 179 kN.

- two Rolls Royce  RB211-535E4B each rated 193.5 kN.

Weight: - empty: 62.100 Kg.- max. zero-fuel weight: 85.300 Kg.- fuel: 43.490 liters.

- max. payload: 26.700 Kg.

Max. take off weight: 115.680 Kg.
Max. landing weight: 95.250 Kg.
Cruise speed: 852 km/h.
Max. speed: 935 km/h.
Max. ceiling: 11.887 m.
Range: - max. range 7.222 km.
Performance: - take-off run 1.646 m at max. take-off weight.- landing run 1.402 m at max. landing weight.

                                                

 

  Boeing 757-200PF*
Cargo volume: - main deck 187 m³.- under floor 51 m³.- total load 238 m³.
Standard 2.23m x 3.17m pallets: - main cargo deck of freighter 15.
Weight: - empty: 51.700 Kg.- max. zero-fuel weight: 90.700 Kg.- fuel: 42.680 liters.

- max. payload: 39.000 Kg.

Max. take off weight: 116.650 Kg.
Max. landing weight: 92.250 Kg.
Cruise speed: 852 km/h.
Max. speed: 935 km/h.
Max. ceiling: 11.887 m.
Range: - max. range 6.852 km.

* Generally similar to the Boeing 757-200 except in the following particulars. 

Boeing 757-200 production: 

Built 995, active 956, stored 29, scrapped 1 and written-off 8 at March 2005.

 

Boeing 757 of each type:
- 877 Boeing 757-200
-   78 Boeing 757-200PF.
-   35 Boeing 757-200SF.
-     4 Boeing VC-32A.
-     1 Boeing 757-200C.
-   55 Boeing 757-300

 

 

8 Boeing 757-200 written-off by accidents: 

  • * 02oct1990 B-2812 Boeing 757-21B China Southern Airlines While waiting for take-off clearance from Guangzhou-Baiyun Airport, China to Shanghai the aircraft was hit by a crashing Xiamen Airlines Boeing 737 (B-2510). The 737 struck the right wing and cut through the center fuselage. The 757 caught fire. 46 fatalities / 122 on board.
  • *
  • * 20dec1995 N651AA Boeing 757-223 American Airlines during approach of Cali-Alfonso B. Aragon Airport, Colombia, crashed into a mountain near Buga, Colombia 160 fatalities / 164 on board.
  • *
  • * 06feb1996 TC-GEN Boeing 757-225 Alas Nacionales Crashed 26 km NE off Puerto Plata, Dominican Republic in the Atlantic Ocean. 189 fatalities / 189 on board.
  • *
  • * 02oct1996 N52AW Boeing 757-23A AeroPeru Crashed 73 km NW off Lima, Peru in the Pacific Ocean. 70 fatalities / 70 on board.
  • *
  • * 14sep1999 G-BYAG Boeing 757-204 Britannia Airways During landing at Gerona-Costa Brava Airport, Spain, the captain lost his visual reference with the runway because all runway lights had suddenly failed, because of thunderstorm. The 757 runs at grassland beside the runway and both main landing gears collapsed. 0 fatalities / 245 on board.
  • *
  • * 11sep2001 N591UA Boeing 757-222 United Airlines The aircraft was hijacked by four terrorists. The hijackers took over control, reportedly switched off the transponder and changed course to, probably, Washington. The aircraft probably crashed near Somerset, PA following passengers attempt to take down the hijackers. 44 fatalities / 44 on board.
  • *
  • * 11sep2001 N644AA Boeing 757-223 American Airlines The 757 was hijacked by five terrorists. The hijackers took over control, reportedly switched off the transponder and changed course to Washington. The 757 crashed in the Pentagon. 44 fatalities / 44 on board / 125 fatalities on the ground.
  • *
  • * 01jul2002 A9C-DHL Boeing 757-23APF DHL Aviation Collided in the air with a Tupolev 154 of Bashkirian Airlines above Überlingen, Germany. 2 fatalities / 2 on board / 69 fatalities from Tupolev 154.
  • *

 

Boeing 757-200 airline operators:
American Airlines. - 124 757-223-     9 757-2Q8-     9 757-231
United Airlines. - 97 757-222
Delta Air Lines. - 80 757-232-   4 757-212-   1 757-26D
United Parcel Service – UPS. - 72 757-24APF
Northwest Airlines. - 51 757-251
Continental Air Lines. - 41 757-224
Song. - 36 757-232
US Airways. - 20 757-2B7- 11 757-225
China Southern Airlines. - 16 757-21B-   3 757-236-   1 757-2Z0

-   1 757-28S

DHL. - 21 757-236SF
Britannia Airways. - 16 757-204-   2 757-236-   2 757-28A
ATA Airlines. - 14 757-23N
European Air Transport. - 12 757-236SF-   1 757-236-   1 757-23PF
America West Airlines. - 6 757-2S7- 4 757-225- 3 757-2G7
British Airways. - 13 757-236
First Choice Airways. - 6 757-28A- 2 757-236- 2 757-2B7

- 2 757-2Y0

- 1 757-23A

Iberia. - 13 757-256
Shanghai Airlines. - 12 757-26D-   1 757-231
Thomas Cook Airlines. - 4 757-28A- 4 757-2Q8- 2 757-28A

- 2 757-25F

- 1 757-204

- 1 757-2G5

Icelandair. - 6 757-208- 3 757-256- 1 757-27B

- 1 757-28A

- 1 757-23APF

VIM Airlines. - 11 757-230
Air China. - 8 757-2Z0 - 1 757-2Y0 
Mexicana. - 8 757-2Q8- 1 757-230
Xiamen Airlines. - 9 757-25C
China Xinjiang Airlines. - 5 757-28S- 2 757-2Y0- 1 757-2Q8
Far Eastern Transport. - 5 757-27A- 1 757-2Q8- 1 757-29J

- 1 757-23APF

Skyservice Airlines. - 5 757-236- 2 757-28A- 1 757-21K
Monarch Airlines. - 7 757-2T7
Aeromexico. - 3 757-28A- 2 757-2Q8- 1 757-29J
Avianca. - 2 757-28A- 2 757-2Y0- 1 757-208

- 1 757-236

Transmeridian Airlines. - 3 757-231- 3 757-236
Uzbekistan Airways. - 3 757-231- 3 757-23P
Ethiopian Airlines. - 4 757-260- 1 757-260PF
Finnair. - 5 757-2Q8
North American Airlines. - 5 757-28A
Atlasjet. - 2 757-225- 2 757-2G5 
China Southwest Airlines. - 4 757-2Z0
El Al Israeli Airlines. - 4 757-258
My Travel. - 4 757-225
Ryan International Airlines. - 1 757-236- 1 757-23A- 1 757-25F

- 1 757-2G5

Varig. - 4 757-256
Air Astana. - 3 757-2G5 
Air Finland. - 2 757-28A- 1 757-2K2
Azerbaijan Airlines. - 2 757-22L- 1 757-256
CEBU Pacific Air. - 3 757-236
Harmony Airways. - 2 757-258- 1 757-28A
Pace Airlines. - 1 757-236- 1 757-256- 1 757-2T7 
Star Air. - 3 757-24APF
Turkmenistan Airlines. - 3 757-22K
Air Atlanta Icelandic.  - 2 757-225
Air Scandic. - 2 757-2Q8
Astraeus. - 1 757-23A- 1 757-28A
Belair. - 2 757-2G5
Flyjet. - 2 757-23A
Israir Airlines. - 2 757-258
L-3 Capital LLC. - 1 757-22L- 1 757-23A
Omni Air International. - 2 757-2Q8
Orient Thai Airlines. - 1 757-236- 1 757-2G5
Phuket Airlines. - 1 757-256- 1 757-2Q8
Royal Air Maroc. - 2 757-2B6
Royal Brunei Airlines. - 2 757-2M6
Royal Nepal Airlines. - 1 757-2F8- 1 757-2F8C
Sun d’Or International Airlines. - 1 757-236- 1 757-27B
TACV - 2 757-2Q8
Vulcan Aircraft Inc. - 1 757-23A- 1 757-2J4
Air Greenland. - 1 757-236
Air Scotland. - 1 757-236
Air Slovakia. - 1 757-236
American Trans Air. - 1 757-28A
Arkia Israeli Airlines. - 1 757-236
Berkut Air. - 1 757-2M6
Boeing. - 1 757-200
Condor. - 1 757-230
Excel Airways. - 1 757-225
Hola Airways - 1 757-256
Hooters Air. - 1 757-2G5
Mid East Jet. - 1 757-26D
One-Two-Go. - 1 757-28A
PLUNA. - 1 757-23A
Primaris Airlines. - 1 757-2G5
Privatair. - 1 757-23A
The Yucaipa Companies. - 1 757-2J4
Titan Airways. - 1 757-2Y0
TravelSpan. - 1 757-236
WFBN Wells Fargo Bank Northwest. - 1 757-236

 

 

Boeing 757-200 military operators:
United States Air Force. - 4  757-2G4(VC-32A)- 2  757-23A
New Zealand Air Defence Force. - 2 757-2K2 
Argentine Government. - 1 757-23A
Mexican Air Force. - 1 757-225
NASA. - 1 757-225
Saudi Arabian Government.  - 1 757-23A
Turkmenistan Government. - 1 757-23A

Boeing 777-300

December 10, 2008 by R.Vogelaar · 2 Comments 

Boeing 777-300ER N520TV Boeing Commercial Airplane Company

Boeing 777-300ER N520TV Boeing Commercial Airplane Company

Compared with the baseline Boeing 777-200 the 777-300 features a 10,13 m stretch, comprising plugs fore and aft of the wings. The longer fuselage allows seating for up to 550 passengers in a single class high density configuration. Boeing publicly announced it was developing the 777-300 at the Paris Airshow in mid June 1995. The 777-300 rolled out on September 8 1997, followed by first flight on October 16 that year.

The 777-300ER is the first of two new Longer-Range 777 models. The 777-300ER and the 777-200LR (Longer Range) were launched in February 2000 at the request of airline customers seeking airplanes with additional flexibility to serve the non-stop routes that passengers demand.

The twin-engine 777-300ER carries 365 passengers up to 14.270 kilometers, and is capable of serving such routes as Paris-Los Angeles and Paris-Tokyo.

During the 777-300ER’s 1,500-hour flight test program, the airplane exceeded its original design performance targets. As a result, the new jetliner provides increased payload and range capability over those promised to customers at the time of the airplane sale.

The 777-300ER has updated avionic, electrical, flight and environmental control systems. The airplane’s raked wingtips offer fuel efficiency improvements and its semi-levered landing gear permits takeoffs on shorter runways.

The 777-300ER also features the award-winning Boeing Signature Interior, known for its ambient lighting and easily accessible drop-down luggage bins.

General Electric Aircraft Engines manufactures the engines for both Longer-Range 777 models. The GE90-115B turbofan is the world’s largest and most powerful commercial jet engine, producing 115,000 pounds of thrust, currently a Guinness World Record.

On Friday, December 3, 2004 was the rollout of the 500th Boeing 777 commercial airplane. The Boeing 777 the fastest-selling twin-aisle airplane ever, will reach 500 airplanes delivered faster than any other twin-aisle airplane in commercial history. The 500th 777 is scheduled for delivery to International Lease Finance Corp. and operator Air France later this month. Thirty-eight customers have ordered 647 Boeing 777.

 

Developing nation:

United States of America

Manufacturer/designer: 

Boeing Commercial Airplane Company.

Production line:

Everett, WA.

Type aircraft:

long and ultra long range widebody airliner.

First flight:

- 777-300 October 16, 1997, N5014K.

- 777-300ER February 24, 2003, N5017V.

First delivery:

- 777-300 May 22, 1998 to Cathay Pacific Airways.

- 777-300ER April 29, 2004 to Air France.

 

Boeing 777-300

Cockpit crew:

Two pilots.

Passengers single class:

up to 550.

Passengers two class:

- 58 business class.

- 284 economy class.

Passengers three class:

- 30 first class.

- 84 business class.

- 254 economy class.

Cabin length:

59,24 m.

Cabin diameter:

5,86 m.

Baggage compartment:

17 m³.

Cargo volume:

213,9 m³.

LD3 Containers in belly:

20.

Standard 2.24m x 3.17m pallets:

8.

Wing span:

60,93 m.

Wing area:

427,8 m².

Wing sweep:

31,64 degrees.

Fuselage length:

73,86 m.

Fuselage diameter:

6,19 m.

Height:

18,51 m.

Horizontal tail unit:

21,53 m.

Wheelbase:

31,22 m.

Track:

10,97 m.

Engines:

- two Pratt & Whitney 4098 rated  424.1 kN.

- two Rolls Royce Trent 892 rated  411.48 kN.

- two General Electric GE90-94B rated 432.8 kN.

Weight:

- empty: 139.025 Kg.

- max. zero-fuel weight: 224.528 Kg.

- fuel: 171.160 liter.

- max. payload: 66.770 Kg.

Max. take off weight:

297.560 Kg.

Max. landing weight:

237.682 Kg.

Cruise speed:

895 km/h.

Max. speed:

941 km/h.

Take-off speed:

270 – 345 km/h.

Landing speed:

245 - 285 km/h.

Service ceiling:

13.135 m.

Range:

11.029 km.

Performance:

- take-off run 3.231 m at max. take-off weight.

- landing run 1.829 m at max. landing weight.

 

Boeing 777-300ER*

Passengers two class:

- 56 business class.

- 283 economy class.

Passengers three class:

- 12 first class.

- 42 business class.

- 316 economy class.

Wing span:

64,80 m.

Height:

18,85 m.

Cargo volume:

213,9 m³.

Engines:

- two General Electric GE90-115B rated 512 kN.

Weight:

- empty: 167.829 Kg.

- max. zero-fuel weight: 237.682 Kg.

- fuel: 181.280 liter.

- max. payload: 69.853 Kg.

Max. take off weight:

344.550 Kg.

Max. landing weight:

251.290 Kg.

Range:

14.270 km.

Performance:

- take-off run 3.353 m at max. take-off weight.

- landing run 1.585 m at max. landing weight.

* Generally similar to the Boeing 777-300 except in the following particulars.

Boeing 767-300

December 9, 2008 by R.Vogelaar · Leave a Comment 

Boeing 767-31AER PH-MCV Arke Fly

 

Boeing 767-31AER PH-MCV Arke Fly

The Boeing 767-300 is the stretched version of the 767-200, it features a 6,42 m stretch consisting of fuselage plugs forward (3,07 m) and behind (3,35 m) the wing center section. The flightdeck and systems were carried directly over from the 767-200.

Boeing 767-300F changes include strengthened undercarriage and wing structure, a cargo handling system, no cabin windows and a main deck freight door.

  • Boeing 767-300: standard stretched version of the 767-200.
  • Boeing 767-300ER: Extended-Range version, features higher weights and an additional wing center section fuel tank.
  • Boeing 767-300F: Freighter include strengthened undercarriage and wing structure, a cargo handling system, no cabin windows and a main deck freight door.

Developing nation:

United States of America

Manufacturer/designer:

Boeing Commercial Airplane Company.

Production line:

Everett, WA.

Type aircraft:

Medium to long range widebody airliner.

First flight:

- 767-300 January 30, 1986 N767S.

- 767-300ER December 9, 1986.

- 767-300F June 20, 1995..

First delivery:

- 767-300 September 25, 1986 to Japan Air Lines.

- 767-300ER February 19, 1988 to American Airlines.

- 767-300F October 12, 1995 to United Parcel Service..

 

Boeing 767-300

Cockpit crew:

two pilots.

Passengers single class:

290.

Passengers two class:

- 18 first class.

- 198 economy class.

Passengers three class:

- 15 first class.

- 40 business class.

- 119 economy class.

Cabin length:

40,36 m.

Cabin diameter:

4,72 m.

Cabin height:

2,87 m.

Cabin volume:

483,9 m³.

Baggage compartment:

12,2 m³.

Cargo volume:

147 m³.

LD2 Containers in belly:

30.

Standard 2.24m x 3.17m pallets:

- in belly 4 with 14 LD2 Containers.

Wing span:

47,57 m.

Wing area:

283,35 m².

Wing sweep:

31.5 degrees.

Fuselage length:

54,94 m.

Fuselage diameter:

5,03 m.

Height:

15,85 m.

Horizontal tail unit:

18,62 m.

Wheelbase:

22,76 m.

Track:

9,30 m.

Engines:

- two General Electric CF6-80A2 each rated 216.5 kN.

- two Pratt & Whitney JT9D-7R4D each rated 213.5 kN.

- two Rolls Royce RB211-524H each rated 264.4 kN.

Weight:

- empty: 85.637 Kg.

- max. zero-fuel weight: 112.099 Kg.

- fuel: 63.216 liter.

- max. payload: 44.497 Kg.

Max. take off weight:

159.755 Kg.

Max. landing weight:

136.078 Kg.

Cruise speed:

852 km/h.

Max. speed:

898 km/h.

Service ceiling:

11.887 m.

Range:

9.667 km.

Performance:

- take-off run 2.408 m at max. take-off weight.

 

Boeing 767-300ER*  

Engines:

- two General Electric CF6-80C2 each rated 231.3 kN.

- two General Electric CF6-80C2B4 each rated 254.34 kN.

- two General Electric CF6-80C2B6F each rated 267.03 kN.

- two Pratt & Whitney PW4056 each rated 252.4 kN.

- two Pratt & Whitney PW4060 each rated 266,9 kN.

- two Rolls Royce RB211-524H each rated 264.4 kN.

Weight:

- empty: 90.582 Kg.

- fuel: 94.625 liter.

- max. payload: 44.500 Kg.

Max. take off weight:

186.880 Kg.

Max. landing weight:

145.149 Kg.

Max. speed:

954 km/h.

Take-off speed:

206 – 330 km/h.

Landing speed:

215 – 300 km/h.

Service ceiling:

13.137 m.

Max. range:

11.482 km.

Performance:

- take-off run 2.408 m at max. take-off weight.

*Generally similar to the Boeing 767-300 except in the following particulars.

 
 
 
 
 

 

 
 
 
 

 

 

Boeing 767-300F*  

Cargo volume:

- Maine deck 339,5 m³.

- Under floor 114,1 m³.

- Total load 453,6 m³.

LD2 Containers in belly:

30.

LD3 Containers in belly:

15.

Standard 2.24m x 2.74m pallets:

- main cargo deck of freighter 24 and two special contoured pallets.

Standard 2.24m x 3.17m pallets:

- in belly 4 with 14 LD2 Containers.

- main cargo deck of freighter 14 and two special contoured pallets.

Engines:

- two General Electric CF6-80C2F each rated 257,6 kN.

- two Pratt & Whitney PW4084 each rated 369.6 kN.

- two Rolls Royce RB211-524G each rated 253 kN.

Weight:

- empty: 86.183 Kg.

- max. zero-fuel weight: 140.160 Kg.

- fuel: 91.380 liter.

- max. payload: 54.885 Kg.

Max. take off weight:

186.880 Kg.

Max. landing weight:

147.871 Kg.

Max. range:

5.926 km with max. payload: 54.885 Kg.

Performance:

- take-off run 2.408 m at max. take-off weight.

*Generally similar to the Boeing 767-300 except in the following particulars.

 
 
 
 

2 Boeing 767-300 written-off by accidents:

· 26may91 OE-LAV Boeing 767-3Z9ER Lauda Air Phu Khao Kao Chan, Thailand 223 fatalities / 223 on board.

· 31oct99 SU-GAP Boeing 767-366ER Egypt Air 100 km South off Nantucket Island, MA, USA in Atlantic Ocean 217 fatalities / 217 on board.

 

Boeing 767-400

December 7, 2008 by R.Vogelaar · Leave a Comment 

Boeing 767-424ER N76055 Continental Airlines

Boeing 767-424ER N76055 Continental Airlines

Boeing’s 767-400ER is a stretched development of the popular 767-300ER. The most significant change with the 767-300 is the 6,4 m fuselage stretch. Because of the increased fuselage length the -400 features all new, 46 cm taller landing gear to restore rotation angles for acceptable takeoff and landing speeds and distances which would otherwise have been adversely affected by the fuselage stretch. The wheels, tires and brakes are common with the Boeing 777. Compared to the 767-300, the 767-400ER’s wing features 2,34 m long raked wingtips which improve aerodynamic efficiency.

Developing nation:

United States of America

Manufacturer/designer: 

Boeing Commercial Airplane Company.

Production line:

Everett, WA.

Type aircraft:

Long range widebody airliner.

First flight:

- 767-400ER October 9, 1999 N76700.

First delivery:

- 767-400ER August 29, 2000 to Continental Airlines.

 

Boeing 767-400ER

Cockpit crew:

Two pilots.

Passengers single class:

409.

Passengers two class:

-  24 first class.

- 272 economy class.

Passengers three class:

- 20 first class.

- 50 business class.

- 175 economy class.

Cabin diameter:

4,72 m.

Cabin height:

2,87 m.

Baggage compartment:

12,2 m³.

Cargo volume:

129,6 m³.

LD2 containers in belly:

38.

Wing span:

51,99 m.

Wing area:

290,7 m².

Wing sweep:

31.5 degrees.

Fuselage length:

61,37 m.

Fuselage diameter:

5,03 m.

Height:

16,87 m.

Horizontal tail unit:

18,62 m.

Wheelbase:

26,16 m.

Track:

9,30 m.

Engines:

- two Pratt & Whitney PW4062 each rated 281.6 kN.

- two General Electric CF6-80C2B8F each rated 282.5 kN.

Weight:

- empty: 103.150 Kg.

- max. zero-fuel weight:149.730 Kg.

- fuel: 91.380 liter.

- max. payload: 46.540 Kg.

Max. take off weight:

204.170 Kg.

Max. landing weight:

158.800 Kg.

Cruise speed:

851 km/h.

Max. speed:

898 km/h.

Service ceiling:

11.550 m.

Max. ceiling:

13.198 m.

Range:

10.454 km.

Performance:

- take-off run 2.896 m at max. take-off weight.

- landing run 1.768 m at max. landing weight.

Boeing 757-300

December 6, 2008 by R.Vogelaar · Leave a Comment 

Boeing 757-330 D-ABOF Transavia

Boeing 757-330 D-ABOF Transavia

The 757-300, which is 7.1 meters longer than a 757-200, carries 20 percent more passengers and was launched in September, 1996, by German charter airline Condor Flugdienst.

Three principal models were eventually produced – the 757-200, 757-300, and the 757-200 freighter. In addition, Boeing produced one 757-200 combi. October 28, 2004 was the 1.050th and final 757 a Shanghai Airlines 757-200, was the centerpiece of a ceremony at the company’s Renton, Washington factory. The final 757 will be the 1.049th delivered to an airline or military operator . Boeing uses the first 757 as a test bed.

Developing nation:

United States of America

Manufacturer/designer: 

Boeing Commercial Airplane Company.

Production line:

closed October 28, 2004.

Type aircraft:

Medium range narrowbody airliner.

First flight:

- 757-300 August 2, 1998, N757X.

First delivery:

- 757-300 March 10, 1999 to Condor

 

Boeing 757-300

Cockpit crew:

two pilots.

Passengers single class:

279.

Passengers two class:

- 12 first class.

- 231 economy class.

Cabin length:

43,21 m.

Cabin diameter:

3,54 m.

Cabin height:

2,13 m.

Cargo volume:

- under floor 67,5 m³.

Wing span:

38,05 m.

Wing area:

185,24 m².

Wing sweep:

25 degrees.

Fuselage length:

54,43 m.

Fuselage diameter:

3,76 m.

Height:

13,60 m.

Horizontal tail unit:

15,24 m.

Wheelbase:

22,35 m.

Track:

7,32 m.

Engines:

- two Pratt & Whitney  PW2040 each rated 178.4 kN.

- two Pratt & Whitney  PW2043 each rated 189.4 kN.

- two Rolls Royce RB211-535E4 each rated 179 kN.

- two Rolls Royce  RB211-535E4B each rated 193.5 kN.

Weight:

- empty: 64.580 Kg.

- max. zero-fuel weight: 95.260 Kg.

- fuel: 43.495 liters.

- max. payload: 30.940 Kg.

Max. take off weight:

122.470 Kg.

Max. landing weight:

101.610 Kg.

Cruise speed:

852 km/h.

Max. speed:

9,35 km/h.

Max. ceiling:

11.887 m.

Range:

- max. range 6.287 km.

Performance:

- take-off run 2.743 m at max. take-off weight.

 

Boeing 757 of each type:

- 877 Boeing 757-200

-   78 Boeing 757-200PF.

-   35 Boeing 757-200SF.

-     4 Boeing VC-32A.

-     1 Boeing 757-200C.

-   55 Boeing 757-300

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