Plane Manual For Pa28 161
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PA 28-161 Warrior II of at The Piper PA-28 Cherokee is a family of built by and designed for flight training, air taxi and personal use. The PA-28 family of aircraft comprises all-metal, unpressurized, single-engined, airplanes with low-mounted wings and. They have a single door on the copilot side, which is entered by stepping on the wing.
The first PA-28 received its type certificate from the in 1960 and the series remains in production to this day. Current models are the Warrior, Arrow and the Archer TX and LX. The Archer was discontinued in 2009, but with investment from new company ownership, the model was put back into production in 2010. The PA-28 series competes with the high-winged and the similarly low-winged and designs. Piper has created variations within the Cherokee family by installing engines ranging from 140 to 300 hp (105–220 kW), offering, retractable landing gear, and stretching the fuselage to accommodate six people.
The (initially known as 'Cherokee Six') is a larger, six-seat variant of the PA-28. The variant was in production until 2009. PA-28-151, built in 1976 At the time of the Cherokee's introduction, Piper's primary single-engined, all-metal aircraft was the, a larger, faster aircraft with retractable landing gear and a constant-speed propeller. Karl Bergey, and designed the Cherokee as a less expensive alternative to the Comanche, with lower manufacturing and parts costs to compete with the Cessna 172, although some later Cherokees also featured retractable gear and constant-speed propellers. The Cherokee and Comanche lines continued in parallel production, serving different market segments for over a decade, until Comanche production was ended in 1972, to be replaced by the family. The original design.
A record-breaking UK pilot, in her PA-28-236 Dakota: The aircraft was built in 1994. The original Cherokees were the Cherokee 150 and Cherokee 160 (PA-28-150 and PA-28-160), which started production in 1961 (unless otherwise mentioned, the model number always refers to horsepower). In 1962, Piper added the Cherokee 180 (PA-28-180) powered by a 180-horsepower (134-kW) engine. The extra power made it practical to fly with all four seats filled (depending on passenger weight and fuel loading) and the model remains popular on the used-airplane market. In 1968, the cockpit was modified to replace the 'push-pull'-style engine throttle controls with quadrant levers. In addition, a third window was added to each side, giving the fuselage the more modern look seen in current production. Piper continued to expand the line rapidly.
In 1963, the company introduced the even more powerful Cherokee 235 (PA-28-235), which competed favorably with the for load-carrying capability. The Cherokee 235 featured a Lycoming O-540 engine derated to 235 horsepower (175 kW) and a longer wing which would eventually be used for the Cherokee Six.
It included tip tanks of 17-gallon capacity each, bringing the total fuel capacity of the Cherokee 235 to 84 gallons. The aircraft had its fuselage stretched in 1973, giving much more leg room in the rear. The stabilator area was increased, as well. In 1973, the marketing name was changed from '235' to 'Charger'.
In 1974, it was changed again to 'Pathfinder'. Production of the Pathfinder continued until 1977. No 1978 models were built. In 1979, the aircraft was given the Piper tapered wing and the name was changed again, this time to Dakota. In 1964, the company filled in the bottom end of the line with the Cherokee 140 (PA-28-140), which was designed for training and initially shipped with only two seats. The PA-28-140 engine was slightly modified shortly after its introduction to produce 150 horsepower (112 kW), but kept the -140 name. In 1967, Piper introduced the PA-28R-180 Cherokee Arrow.
This aircraft featured a constant-speed propeller and retractable landing gear and was powered by a 180-horsepower (134-kW) Lycoming IO-360-B1E engine. A 200-hp (149-kW) version powered by a Lycoming IO-360-C1C was offered as an option beginning in 1969 and designated the PA-28R-200; the 180-hp model was dropped after 1971. At the time the Arrow was introduced, Piper removed the Cherokee 150 and Cherokee 160 from production. The Arrow II came out in 1972, featuring a five-inch fuselage stretch to increase legroom for the rear-seat passengers.
In 1977, Piper introduced the Arrow III (PA-28R-201), which featured a semitapered wing and longer stabilator, a design feature that had previously been introduced successfully on the PA-28-181 and provided better low-speed handling. It also featured larger fuel tanks, increasing capacity from 50 to 77 gallons. The first turbocharged model, the PA-28R-201T, was also offered in 1977, powered by a six-cylinder engine equipped with a Rajay turbocharger. A three-bladed propeller was optional.
In 1979, the Arrow was restyled again as the PA-28RT-201 Arrow IV, featuring a 'T' tail that resembled the other aircraft in the Piper line at the time. In 1971, Piper released a Cherokee 140 variant called the Cherokee Cruiser 2+2. Although the plane kept the 140 designation, it was, in fact, a 150-hp plane and was shipped mainly as a four-seat version. In 1973, the Cherokee 180 was named the Cherokee Challenger and had its fuselage lengthened slightly and its wings widened and the Cherokee 235 was named the Charger with similar airframe modifications.
In 1974, Piper changed the marketing names of some of the Cherokee models again, renaming the Cruiser 2+2 (140) simply the Cruiser, the Challenger to the Archer (model PA-28-181) and the Charger (235) to Pathfinder. Piper reintroduced the Cherokee 150 in 1974, renaming it the Cherokee Warrior (PA-28-151) and giving it the Archer's stretched body and a new, semitapered wing. In 1977, Piper stopped producing the Cruiser (140) and Pathfinder (235), but introduced a new 235-hp (175-kW) plane, the Dakota (PA-28-236), based on the Cherokee 235, Charger and Pathfinder models, but with the new semitapered wing. The PA-28-201T Turbo Dakota followed the introduction of the PA-28-236 Dakota in 1979. The airframe was essentially the same as a fixed-gear Arrow III and was powered by a turbocharged Continental TSIO-360-FB engine producing 200 hp (149 kW). The aircraft did not sell well and production ended in 1980.
In 1978, Piper upgraded the Warrior to 160 hp (119 kW) PA-28-161, changing its name to Cherokee Warrior II. This aircraft had slightly improved aerodynamic wheel fairings.
Later models of the Warrior II, manufactured after July 1982, incorporated a gross weight increase to 2,440 pounds, giving a useful load over 900 pounds. This same aircraft, now available with a, was available as the Warrior III and was marketed as a training aircraft. Main article: In 1965, Piper developed the Piper Cherokee Six, designated the PA-32, by stretching the PA-28 design. It featured a lengthened fuselage and seating for one pilot and five passengers.
Brazilian, Argentinian and Chilean production PA-28s were built under license in Brazil as the EMB-711A and EMB-711C Corisco (PA-28R-200), EMB-711B (PA-28R-201), EMB-711T (PA-28RT-201) and EMB-711ST Corisco Turbo (PA-28RT-201T) and the EMB-712 Tupi (PA-28-181). Argentinian production was carried out by of. Built 960 airplanes between 1972 and 1995, including the Cherokee Archer, Dakota, Arrow and Turbo Arrow. The PA-28-236 Dakota was also assembled under license by the Maintenance Wing of the (which later became known as ). By September 1982, 20 Dakotas had been assembled in Chile. New Piper Aircraft. Piper Archer DX The original company declared bankruptcy in 1991.
In 1995, the New Piper Aircraft company was created. It was renamed Piper Aircraft once again in 2006. The company originally produced one variant, the 180-horsepower (134 kW) Archer LX (PA-28-181), and began testing two versions, with 135 and 155 hp. The cockpit of a Piper PA-28-151 Cherokee Warrior (2016) Older Cherokees use an overhead crank for stabilator trim (correctly called an antiservo tab), while later ones use a trim wheel on the floor between the front seats, immediately behind the flap bar. All Cherokees have a brake lever under the pilot side of the instrument panel. Differential toe brakes on the rudder pedals were an optional add-on for earlier Cherokees and became standard with later models. Some earlier Cherokees used control knobs for the throttle, mixture, and propeller advance (where applicable), while later Cherokees use a collection of two or three control levers in a throttle quadrant.
Cherokees normally include a rudder trim knob, which actually controls a set of springs acting on the rudder pedals rather than an external trim tab on the rudder—in other words, the surface is trimmed by control tension rather than aerodynamically. Piper PA-28-140 Cherokee Cruiser of the lands at, England (2016). Variants PA-28-140 Cherokee Cruiser Two-place, fixed landing gear landplane, or O-320-E3D engine of 150 hp (112 kW), gross weight 1,950 lb (885 kg). First certified on 14 February 1964. Approved as a 2,150 lb (975 kg) gross weight four place aircraft on 17 June 1965. PA-28-150 Cherokee Four-place, fixed landing gear landplane, or O-320-E2A engine of 150 hp (112 kW), gross weight 2,150 lb (975 kg).
First certified on 2 June 1961. PA-28-151 Cherokee Warrior Four-place, fixed landing gear landplane, engine of 150 hp (112 kW), gross weight 2,325 lb (1,055 kg).
First certified on 9 August 1973. Changes from the PA-28-150 include a tapered wing.
PA-28-160 Cherokee Four-place, fixed landing gear landplane, or O-320-D2A engine of 160 hp (119 kW), gross weight 2,200 lb (998 kg). First certified on 31 October 1960. PA-28-161 Warrior II Four-place, fixed landing gear landplane, or O-320-D2A engine of 160 hp (119 kW), gross weight 2,325 lb (1,055 kg). First certified on 2 November 1976. Changes from the PA-28-160 include a tapered wing. Certified on 1 July 1982 for gross weight of 2,440 lb (1,107 kg).
Plane Manual For Pa 28 161 Poh Pdf
PA-28-161 Warrior III Four-place, fixed landing gear landplane, engine of 160 hp (119 kW), gross weight 2,440 lb (1,107 kg). First certified on 1 July 1994. PA-28-180 Cherokee Four-place, fixed landing gear landplane, or O-360-A4A engine of 180 hp (134 kW), gross weight 2,400 lb (1,089 kg).
First certified on 3 August 1962. PA-28-180 Archer Four-place, fixed landing gear landplane, or O-360-A4M engine of 180 hp (134 kW), gross weight 2,450 lb (1,111 kg).
First certified on 22 May 1972. Changes from the PA-28-180 Cherokee include a five inch fuselage extension, wing span increase, larger horizontal tail, gross weight increase and other minor changes.
PA-28-181 Archer II Four-place, fixed landing gear landplane, or O-360-A4A engine of 180 hp (134 kW), gross weight 2,550 lb (1,157 kg). First certified on 8 July 1975. Changes from the PA-28-180 include a tapered wing. PA-28-181 Archer III Four-place, fixed landing gear landplane, engine of 180 hp (134 kW), gross weight 2,550 lb (1,157 kg).
First certified on 30 August 1994. PA-28-201T Turbo Dakota Four-place, fixed landing gear landplane, turbocharged, engine of 200 hp (149 kW), gross weight 2,900 lb (1,315 kg). First certified on 14 December 1978. PA-28-235 Cherokee Pathfinder Four-place, fixed landing gear landplane, O-540-B1B5, or O-540-B4B5 engine of 235 hp (175 kW), gross weight 2,900 lb (1,315 kg). First certified on 15 July 1963.
PA-28-235 Cherokee Pathfinder Four-place, fixed landing gear landplane, engine of 235 hp (175 kW), gross weight 3,000 lb (1,361 kg). First certified on 9 June 1972. Changes from the 1963 certified PA-28-235 Cherokee Pathfinder include a five inch fuselage extension, wing span increase, larger horizontal tail, gross weight increase and other minor changes.
PA-28-236 Dakota Four-place, fixed landing gear landplane, engine of 235 hp (175 kW), gross weight 3,000 lb (1,361 kg). First certified on 1 June 1978. Changes from the 1972 certified PA-28-235 Cherokee Pathfinder include tapered wing.
PA-28S-160 Cherokee Four-place, fixed landing gear seaplane, engine of 160 hp (119 kW), gross weight 2,140 lb (971 kg). First certified on 25 February 1963.
Plane Manual For Pa28-161 Weight And Balance
PA-28S-180 Cherokee Four-place, fixed landing gear seaplane, or O-360-A4A engine of 180 hp (134 kW), gross weight 2,222 lb (1,008 kg). First certified on 10 May 1963. PA-28R-180 Arrow Four-place, retractable landing gear landplane, engine of 180 hp (134 kW), gross weight 2,500 lb (1,134 kg). First certified on 8 June 1967. PA-28R-200 Arrow Four-place, retractable landing gear landplane, engine of 200 hp (149 kW), gross weight 2,600 lb (1,179 kg).
First certified on 16 January 1969. PA-28R-200 Arrow II Four-place, retractable landing gear landplane, or C1C6 engine of 200 hp (149 kW), gross weight 2,650 lb (1,202 kg). First certified on 2 December 1971. Changes from the 1969 certified PA-28R-200 Arrow include a five inch fuselage extension, wing span increase, larger horizontal tail, gross weight increase and other minor changes. PA-28R-201 Arrow III Four-place, retractable landing gear landplane, engine of 200 hp (149 kW), gross weight 2,750 lb (1,247 kg). First certified on 2 November 1976. PA-28R-201T Turbo Arrow III Four-place, retractable landing gear landplane, turbocharged or TSIO-360-FB engine of 200 hp (149 kW), gross weight 2,900 lb (1,315 kg).
First certified on 2 November 1976. PA-28RT-201 Arrow IV Four-place, retractable landing gear landplane, engine of 200 hp (149 kW), gross weight 2,750 lb (1,247 kg). First certified on 13 November 1978.
PA-28RT-201T Turbo Arrow IV Four-place, retractable landing gear landplane, turbocharged engine of 200 hp (149 kW), gross weight 2,900 lb (1,315 kg). First certified on 13 November 1978.
Features a T tail. PA-28-161 Cadet Two-place, fixed landing gear landplane, engine of 160 hp (119 kW), gross weight 2,325 lb (1,055 kg). Replaced the trainer in the late 1980s. Features the older Cherokee '2 side window' fuselage with the later tapered wing. Archer DX Four-place, fix landing gear landplane, turbocharged diesel engine of 155 hp (116 kW).
Introduced at in April 2014. Operators The Cherokee series has been popular with private owners and flying clubs, with over 32,000 delivered. Military operators. – Retired.
– 14 x Cherokee Arrow 200 Retired 2005. Notable accidents and incidents. September 9, 1969, a Douglas DC-9-31, collided with a Piper PA-28-181 Archer over, killing all aboard both planes. August 28, 1972, was killed along with the copilot of his Piper Cherokee Arrow after crashing shortly after takeoff from in, England, in an air race. August 31, 1986, a Douglas DC-9-32, collided with a Piper PA-28-181 Archer, owned by William Kramer, over, killing all 67 people aboard both planes and 15 people on the ground. It was the worst air disaster in the history of Los Angeles, and resulted in regulatory changes requiring all airliners to be equipped with a (TCAS) and all light aircraft operating in to be equipped with a.
February 18, 2010, Andrew Joseph Stack III into Building 1 of the Echelon office complex in, in an apparent revenge attack on the office located there. November 17, 2011, a four miles south of, claimed the life of head women's basketball coach and assistant coach Miranda Serna, along with the pilot and another passenger.
Specifications (1964 model PA-28-140 Cherokee 140).