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BOEING 737-200

From SKYbrary Wiki
Name 737-200
Manufacturer BOEING
Body Narrow
Wing Fixed Wing
Position Low wing
Tail Regular tail, mid set
WTC Medium
Type code L2J
RFF Category 6
Engine Jet
Engine count Multi
Position Underwing mounted
Landing gear Tricycle retractable
Mass group 4

Manufacturered as:

BOEING Surveiller
BOEING 737-200
BOEING 737-200 Surveiller

BOEING 737-200

BOEING 737-200 BOEING 737-200 3D


Short range airliner. In service since 1969. The most used member of first generation of B737 family. Stretched version of the orginal 737-100. Production ceased in 1988. 1144 aircraft of 737-200 were built, approx. 900 remain in service in 1999. Mil. type: CT-43 and VC96.

For more information, see Boeing's B737 family specifications.

Technical Data

Wing span 28.35 m93.012 ft
Length 30.53 m100.164 ft
Height 11.23 m36.844 ft
Powerplant 2 x P&W JT8D-9A (64.5 kN) or

2 x P&W JT8D-15A (68.9 kN) or
2 x P&W JT8D-17 (71.2 kN) or
2 x P&W JT8D-17R (77.4 kN) turbofans.
Optional with Hush-Kits for noise reduction.

Engine model Pratt & Whitney JT8D

Performance Data

Take-Off Initial Climb
(to 5000 ft)
Initial Climb
(to FL150)
Initial Climb
(to FL240)
MACH Climb Cruise Initial Descent
(to FL240)
(to FL100)
Descent (FL100
& below)
V2 (IAS) 145 kts IAS 175 kts IAS 250 kts IAS 250 kts MACH 0.68 TAS 400 kts MACH 0.70 IAS 250 kts IAS 210 kts Vapp (IAS) 150 kts
Distance 1830 m ROC 1500 ft/min ROC 1200 ft/min ROC 1000 ft/min ROC 500 ft/min MACH 0.73 ROD 800 ft/min ROD 3500 ft/min MCS 210 kts Distance 1400 m
MTOW 5239052,390 kg
52.39 tonnes
Ceiling FL370 ROD 1500 ft/min APC C
WTC M Range 12001,200 nm
2,222,400 m
2,222.4 km
7,291,338.588 ft

Accidents & Serious Incidents involving B732

  • AT72 / B732, vicinity Queenstown New Zealand, 1999 (On 26 July 1999, an ATR 72-200 being operated by Mount Cook Airlines on a scheduled passenger flight from Christchurch to Queenstown entered the destination CTR without the required ATC clearance after earlier cancelling IFR and in marginal day VMC due to snow showers, separation was then lost against a Boeing 737-200 being operated IFR by Air New Zealand on a scheduled passenger flight from Auckland to Queenstown which was manoeuvring visually (circling) after making an offset VOR/DME approach in accordance with a valid ATC clearance.)
  • B732 / A321, Manchester UK, 2004 (On 29 February 2004, a Boeing 737-200 crossed an active runway in normal daylight visibility ahead of a departing Airbus A321, the crew of which made a high speed rejected take off upon sighting the other aircraft after hearing its crossing clearance being confirmed. Both aircraft were found to have been operating in accordance with their acknowledged ATC clearances issued by the same controller. An alert was generated by the TWR conflict detection system but it was only visually annunciated and had not been noticed. Related ATC procedures were subsequently reviewed and improved.)
  • B732, London Gatwick UK, 1993 (On 20 October 1993, a Boeing 737-200 being operated by Air Malta on a scheduled passenger flight from Malta to London Gatwick landed at destination on the taxiway parallel to the runway for which landing clearance had been given in good visibility at night after a Surveillance Radar Approach (SRA) terminating at 2 miles from touchdown had been conducted in VMC. There was no damage to the aircraft or injury to the occupants and the aircraft taxied to the allocated gate after the landing.)
  • B732, Manchester UK, 1985 (On 22nd August 1985, a B737-200 being operated by British Airtours, a wholly-owned subsidiary of British Airways, suffered an uncontained engine failure, with consequent damage from ejected debris enabling the initiation of a fuel-fed fire which spread to the fuselage during the rejected take off and continued to be fuel-fed after the aircraft stopped, leading to rapid destruction of the aircraft before many of the occupants had evacuated.)
  • B732, Medan Indonesia, 2005 (On 5 September 2005, a Boeing 737-200 being operated by Mandala Airlines on a scheduled domestic passenger flight from Medan, Indonesia to Jakarta failed to become properly airborne during the attempted take off from from runway 23 in day VMC and, after failing to remain airborne, overran the end of the runway at speed finally coming to a stop outside the airport perimeter. The aircraft was destroyed by impact forces and a subsequent fire and 100 of the 117 occupants were killed and 15 seriously injured. The aircraft collided with residential property, vehicles and various other obstructions and as a result a further 49 people on the ground were killed and a further 26 seriously injured.)
  • B732, Pekanbaru Indonesia, 2002 (On 14 January 2002, a Boeing 737-200, operated by Lion Air, attempted to complete a daylight take off from Pekanbaru, Indonesia without flaps set after a failure to complete the before take off checks. The rejected take off was not initiated promptly and the aircraft overran the runway. The take off configuration warning failed to sound because the associated circuit breaker was so worn that it had previously auto-tripped and this had not been noticed.)
  • B732, Seattle WA USA, 2006 (On 30 October 2006, at Seattle-Tacoma International Airport, Seattle, Washington a Boeing 737-200 operated by Alaska Airlines, took off in daylight from a runway parallel to that which had been cleared with no actual adverse consequences.)
  • B732, en-route, Maui Hawaii, 1988 (On 28 April 1988, a Boeing 737-200, operated by Aloha Airlines experienced an explosive depressurisation and structural failure at FL 240. Approximately 5.5 metres (or 18 feet) of cabin covering and structure was detached from the aircraft during flight. As result of the depressurisation, a member of the cabin crew was fatally injured. The flight crew performed an emergency descent, landing at Kahului Airport on the Island of Maui, Hawaii.)
  • B732, vicinity Abuja Nigeria, 2006 (On 29 October 2006, an ADC Airlines’ Boeing 737-200 encountered wind shear almost immediately taking off from Abuja into adverse weather associated with a very rapidly developing convective storm. Unseen from the apron or ATC TWR it stalled, crashed and burned after just over one minute airborne killing 96 of the 105 occupants. The Investigation concluded that loss of control during the wind shear encounter was not inevitable but was a consequence of inappropriate crew response. Concerns about the quality of crew training and competency validation were also raised.)
  • B732, vicinity Islamabad Pakistan, 2012 (On 20 April 2012, the crew of a Boeing 737-200 encountered negative wind shear during an ILS final approach at night in lMC and failed to respond with the appropriate recovery actions. The aircraft impacted the ground approximately 4 nm from the threshold of the intended landing runway. The Investigation attributed the accident to the decision to continue to destination in the presence of adverse convective weather and generally ineffective flight deck management and noted that neither pilot had received training specific to the semi-automated variant of the 200 series 737 being flown and had no comparable prior experience.)
  • B732, vicinity Resolute Bay Canada, 2011 (On 20 August 2011, a First Air Boeing 737-200 making an ILS approach to Resolute Bay struck a hill east of the designated landing runway in IMC and was destroyed. An off-track approach was attributed to the aircraft commander’s failure to recognise the effects of his inadvertent interference with the AP ILS capture mode and the subsequent loss of shared situational awareness on the flight deck. The approach was also continued when unstabilised and the Investigation concluded that the poor CRM and SOP compliance demonstrated on the accident flight were representative of a wider problem at the operator.)
  • B732, vicinity Tamanrassat Algeria, 2003 (On 6 March 2003, a Boeing 737-200 being operated by Air Algerie had just become airborne during a daylight departure when the left hand engine suddenly failed just after the PF had called for “gear up”. Shortly afterwards, the aircraft commander, who had been PNF for the departure, took control but the normal pitch attitude was not reduced to ensure that a minimum airspeed of V2 was maintained and landing gear was not retracted. The aircraft lost airspeed, stalled and impacted the ground approximately 1nm from the point at which it had become airborne. A severe post crash fire occurred and the aircraft was destroyed and all on board except one passenger, were killed.)
  • B732, vicinity Washington National DC USA, 1982 (On 13 January 1982, an Air Florida Boeing 737-200 took off in daylight from runway 36 at Washington National in moderate snow but then stalled before hitting a bridge and vehicles and continuing into the river below after just one minute of flight killing most of the occupants and some people on the ground. The accident was attributed entirely to a combination of the actions and inactions of the crew in relation to the prevailing adverse weather conditions and, crucially, to the failure to select engine anti ice on which led to over reading of actual engine thrust.)