Specifications for the Piper PA-23 Apache
Piper PA-23 Apache · Specifications
Overview
This document provides detailed specifications for the Piper PA-23 Apache, a light twin aircraft introduced over 30 years ago. The Apache is noted for its rugged design and spacious cabin, making it an economical choice for pilots. The document outlines various modifications available for the Apache, including engine upgrades and structural enhancements, which have been popular among owners. It also discusses the performance characteristics of the aircraft, including takeoff distances, climb rates, and cruise speeds, making it a valuable resource for pilots and aviation enthusiasts interested in the Apache's capabilities and modifications.
- Maximum level speed: 174 knots
- Takeoff distance over 50-ft obstacle: 675 feet
- Single-engine service ceiling: 12,000 feet
- Climb rate: 2,000 feet per minute
- Recommended TBO for engines: 2,000 hours
Document
Source
Originally published by www.advancedaviation.com.au. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Specifications
- Year
- 1985
- Pages
- 7
- File size
- 5.3 MB
- Publisher
- www.advancedaviation.com.au
Specifications & performance
Extracted from this document.
Specifications
- Range (nm)
- 907
- Engine (hp)
- 180
- Height (ft)
- 9
- Length (ft)
- 35
- Propeller
- Hartzell two-blade
- Wingspan (ft)
- 29
- Engine model
- Lycoming 0-360-AID
- Max speed (kt)
- 174
- Cruise speed (kt)
- 168
- Empty weight (lb)
- 852
- Fuel capacity (gal)
- 108
- Rate of climb (fpm)
- 2,000
- Service ceiling (ft)
- 23,000
- Max takeoff weight (lb)
- 4,000
Performance
- Fuel burn (gph)
- 20
- Landing over 50ft
- 675
- Takeoff over 50ft
- 650
- Landing distance (ft)
- 400
- Takeoff distance (ft)
- 400
- Stall speed clean (kt)
- 52
- Stall speed landing (kt)
- 47
V-speeds
- VX
- 76
- VY
- 91
- VFE
- 87
- VNE
- 197
- VNO
- 156
- VS1
- 52
- VSO
- 47
Weight & balance
- Useful load (lb)
- 1,488
- Baggage allowance (lb)
- 250
- Basic empty weight (lb)
- 852
- Max takeoff weight (lb)
- 4,000
Common. Rarer than 8% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the Piper PA-23 Apache.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
Free — save the PA-23 Apache 150 to your watchlist and track it in one place.
More Piper PA-23 Apachemanuals & documents
- SERVICE BULLETIN NO. 1299Service Bulletins
- INSTALLATION INSTRUCTIONS FOR HEATER KIT #1 P/N CD11005K1Weight And Balance
- SERVICE LETTER NO. 1141Maintenance Manual
- PIPER PA-23-150/160 ApacheSystems Description
- AAIB Bulletin: 1/2007 G-MOLY EW/G2006/07/24Other Documents
- Piper Parts CatalogChecklist
- Piper PA-23 Apache Supplemental Type CertificateSupplemental Type Certificate
- FOR TRAINING PURPOSES ONLY!Pilot's Operating Handbook
- Airplane Flight ManualFlight Manual
- Piper Apache 235 SpecsChecklist
If you fly the Piper PA-23 Apache, you may also be researching these.
In this document
General Overview
The Piper PA-23 Apache was introduced as general aviation's first light twin aircraft. Built from 1954 to 1961, approximately 2,100 units were produced. The Apache is recognized for its rugged tubular structure and roomy cabin, although it has faced criticism for its aesthetics and performance, particularly with one engine inoperative.
Modifications and Upgrades
Various modifications have been made to the Apache over the years, including engine upgrades from 150-hp and 160-hp Lycoming O-320 engines to 180-hp O-360 engines. Companies like Seguin Aviation offer comprehensive conversion packages that enhance performance and appearance, including new fiberglass nacelles and extended nose sections.
Performance Specifications
The document details the performance specifications of the Apache, including a maximum level speed of 174 knots and a climb rate of 2,000 feet per minute at sea level. The aircraft requires 400 feet for takeoff and 675 feet for landing over a 50-foot obstacle. The single-engine service ceiling is noted at 12,000 feet.
Limiting and Recommended Airspeeds
Key airspeeds for the Apache include Vmc at 63 knots, Vy at 91 knots, and stall speeds of 52 knots clean and 47 knots in landing configuration. These figures are critical for pilots to understand the aircraft's handling characteristics.
Specifications Summary
The Apache is powered by Lycoming O-360-AID engines, producing 180 hp at 2,700 rpm, with a recommended time between overhauls of 2,000 hours. The aircraft has a wingspan of 35 feet 3.6 inches and a maximum gross weight of 4,000 pounds.
Safety notes
- Ensure compliance with all airworthiness directives and service bulletins on the model.
- Inspect fuel bladders for deterioration; about half may require replacement.
Full document text
contillued Piper Aircraft introduced general - aviation's first light twin, the Apache, more than 30 years ago. The airplane had a lot to offer, with its rugged tubular structure and roomy cabin. Best of all, it was a twin that could be acquired and oper- ated inexpensively. But every design is a product of compromises, and the Apache certainly was no exception. It suffered from aesthetic shortcomings and vapid performance, especially with one engine inoperative. The tweakers have had a field day with the Apache. The airplane was not in production long before various powerplant conversions and structural and cosmetic modifications became available from such companies as Doyne, Miller, Nyack and Vecto. The most common field-dressing was re- placement of the 150-hp and 160-hp Lycoming 0-320 engines with 180-hp 0-360s. Other popular modifications included longer nose sections, dorsal fins, squared-off vertical stabilizers and Hoerner-type wing tips. Piper built about 2,100 Apaches from 1954 through 1961. (The number does not include some 100 Apache 235s, basically small-engine Aztecs, produced thereafter.) About 1,500 of the light twins are still around, and it is a fair assumption that decades of wear and tear have taken their toll on the majority of these airplanes. (See "The Original Light Twin," November 1981 Pilot, p. 80.) Today, only one company continues to offer a series of modifications for the Apache. That company is Seguin Avia- tion, a fixed-base operator in Seguin, Texas. The company's roots are in Vecto, which was established in San Antonio in the early 1960s by three partners: Fred Burger, Ed Ondrej and L. B. Pete. Vecto began its aftermarket work on the Apache with a 16-inch nose extension and eventually ex- panded to offer comprehensive conver- sion packages for the airplane. Vecto was renamed when it was relocated to Seguin, 25 miles east of San Antonio. Following the deaths of his partners, L. B. Pete ran the company until 1983, when he sold it to Bryant Ingram, pres- ident of Ingram Manufacturing, located in San Antonio. General manager of Seguin Aviation is Paul Holman, who joined the com- 68· JANUARY 1985 I GERONIMO Aerodynamic tweaks and extra cubes turn a homely straggler into a good-looking screamer.;. ;;}::IJ~ ~t pany as a mechanic in 1977 after retir- ing from the Air Force as an instructor and command pilot. According to Holman, Vecto/Seguin has converted more than 100 Apaches into Geroni- mos. The name, that of the legendary chief of the Chiracahua Apache Indi- ans, is reserved for airplanes that un- dergo the full conversion treatment at Seguin Aviation. The treatment begins with a major airframe inspection and overhaul. The airplane is stripped, and all compo- nents are refurbished to factory speci- fications and tolerances. Through ex- perience, Seguin's mechanics know where to look for trouble. They ensure compliance with all airworthiness directives and service bulletins on the model. The control surfaces are opened up for inspection and reinforced during reassembly. The neoprene and nylon fuel bladders are checked carefully for deterioration (about half require re- placement, according to Holman). The tubular framework is filled with linseed oil and checked for leaks. All Apaches were zinc-chromated during assembly, and Seguin has found serious corrosion in very few airplanes. (There were two bad cases: one resulting from a broken relief tube; the other airplane had been ditched in water.) The overhaul includes new electrical wiring and dynafocal engine mounts. Typically, the inspection and overhaul cost about $18,000, including labor, parts, sheet metal repair and overhaul of the hydraulic power pack. The work is warrantied for six months. Next, the airplane is equipped with factory-new, 180-hp Lycoming 0-360- AID engines and lightweight, two- blade Hartzell propellers. Recom- mended time between major overhaul of the engines is 2,000 hours. The modification, which includes most en- gine accessories, costs $33,250. For $286 more, a customer can get two- blade Q-tip Hartzell propellers, which are two inches shorter (72 versus 74 inches). According to Seguin, the Q- tips are quieter and slightly improve climb performance. The engines are enclosed in fiberglass nacelles, which cost $5,575. The natelles provide im- proved engine cooling, reduce drag and are much easier to remove and re- install (about four minutes each, com- pared with 40 minutes for removing AOPA PILOT • 69 cOl/ti/lued and reinstalling the Apache cowling). A 31-inch extended nose section im- proves the airplane's appearance, as well as its loading flexibility and cabin ventilation. The fiberglass section ($3,250) includes a compartment that can hold up to 50 pounds of baggage. Another 150 pounds of baggage can be placed in a 33- by 36-inch compart- ment behind the rear seat. This modifi- cation costs $998. The Apache's round wing tips are re- placed with Hoerner-type, sculpted fi- berglass tips ($1,180), which reduce wing span by 22 inches. This modifica- tion, as well as a dorsal fin ($535) and a square vertical stabilizer ($845), im- prove the airplane's single-engine con- trol characteristics, according to Seguin. New tires are installed, and the wheels, which protrude from their wells when retracted, are enclosed in fiberglass doors ($3,250). Two extra brake pads are installed on both main wheels ($1,417). Other modifications include: a tail cone, $355; flap gap seals, $343, and nacelle and wing root fairings, $765; a one-piece windshield, $828; a third passenger window, $1,198, and inner panes for all cabin windows, $670; split nose cowls, $880;
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soundproofing, $632 ($882 for "super soundproofing"); and dual ram's-horn control wheels, $695. The Geronimo is finished with a cus- tom interior ($3,550, including a new headliner, seat upholstery, side panels and carpet), panel refabrication and re- arrangement, $4,100. New paint costs an additional $3,675. The previously mentioned prices are for modifications performed by Seguin Aviation. Except for the engines, props and nacelles, the modifications are available in kit form at lower cost. Many of the modifications also are ap- proved for the Piper Aztec. Several options are available for the Geronimo, including wing tip tanks, which hold 24 gallons of fuel each, $3,250; a sixth passenger seat and kick- out window, $1,205; a rear cargo door, $4,400; and an inflatable door seal, $478. None of the options for the Ge- ronimo are available as kits. While about half of Seguin's custom- ers have opted for full Geronimo con- versions (or have purchased Geroni- mos outright), others have chosen partial conversions. The most popular COllti/lued 70· JANUARY 1985 GERONIMO Two-piece, fiberglass nacelles improve cooling and reduce drag. They can be removed in a jiffy. AOPA PILOT • 71 cont;'lUfd GERONIMO N314KB IIll'allS March /4, Kathryll alld Bill: thl' hists' Wl'ddillg allllivl'rsary. A lIickllall/l' providl'd by his studl'lIts has bl'colI/l' a traditioll for Ed CraIlI'. Cause for Conversion modifications among the latter group are the extended nose section and the gear doors. For $6,500, these modifica- tions, alone, substantially improve the Apache's appearance and performance. The changes in appearance and per- formance that evolve from the full con- version, however, are startling. The Geronimo looks more like a trim Twin Comanche or a big Wing Derringer than an Apache, and its performance is superior to most modern light twins. According to Seguin Aviation's data, collected during flight tests at 3,800 pounds (200 pounds shy of gross weight), the airplane requires only 400 feet for takeoff or landing, and climbs at 2,000 fpm. It cruises at about 168 knots, burning 20 gallons of fuel per hour, at 75-percent power: At 65-per- cent power, it cruises at 162 knots burning about ] 8 gph. The Geronimo stalls at 52 knots, clean, and 47 knots in landing configuration. Single-engine performance is the Geronimo's forte. Vmc, the minimum airspeed at which the airplane can be controlled with its critical engine inop- erative, is 63 knots. Single-engine rate of climb, according to Seguin Aviation, is 750 fpm, and single-engine service ceiling is ] 2,000 feet. During a flight in N6918, a Geron- imo used by the company for flight in- struction and demonstration, Paul Holman shut down the right (critical) engine and feathered the propeller at about 5,000 feet. The temperature at that altitude was 95 degrees. At blue line (Vyse, best single-engine rate of climb speed: 83 knots), the airplane climbed at 100 fpm. Seguin Aviation not only modifies Apaches but sells completely converted aircraft, as well. The price for a fin- ished Geronimo is approximately $97,500. Avionics equipment is extra, and the company offers a good selec- tion, including installation of weather radar systems. Several new modifica- tions are in the works, including an electrothermal propeller 'deice system, air conditioning and a new windshield design. More information is available from Seguin Aviation, 2075 Highway 46, Seguin, Texas 78]55. Telephone: 5 ]2/379-3278. The Geronimo is worthy of consider- ation by anyone in the market for a light twin. One flight will convince to shut down his aircraft's right engine on two consecutive takeoffs because of water in the fuel that had gone undetected dur- ing preflight. Both times, Crane was able to bring "Bad Molly Trolley II" (a nick- name provided by his students) safely around for a single-engine landing. Frist, AOI'A 442660, is the owner of N314KB, the Geronimo that appe.us in the photographs accompanying these arti- cles. He bought an Apache about three years ago, intending to have the airplane modified. Initially, he considered having the work done by local mechanics but, af- ter visiting Seguin Aviation, decided to have the work done there. He is pleased with the decision. During the first annual inspection of his Geronimo, a broken en- gine mount had to be replaced; although the airplane's warranty had expired, Se- guin picked up the tab. "They sell a high- quality, first-class airplane," Frist notes, "and they stand behind their product 100 percent." -MML One of the most important considerations in purchasing a Seguin Geronimo conver- sion (or, for that matter, any other major airframe/engine conversion package) is resale value. The investment for the con- version is :iubstanti,ll and, generally, can- not be recouped on resale. The purchaser must decide that he is going to have to keep the airplane for awhile in order to realize a return on the investment. Geronimo owners Edward W. Crane and Dr. William H. Frist do plan to keep their airplanes for awhile. Neither Crane, a schoolteacher during the day and oper- ator of a thriving gymnastics and ski in- struction business in his spare time, nor Frist, a surgical resident, fly their Geroni- mos very often or have the time for fre- quent recurrent training. Their airplanes provide just what these general aviation pilots need: exceptional single-engine per- formance. The performance came in handy a few years ago for Crane, AOI'A 6955%, who had 72 • JANUARY 1985 even the most jaded skeptic that the airplane cannot be passed off as a $100,000 Apache. The Geronimo is an entirely different airplane. More than 20 years of refinement by Seguin Aviac tion have produced an attractive light twin that is easy to fly, economical to operate and capable of excellent perfor- mance when the chips are down. 0 168 kt/907 nm (120 pph/20 gph) 162 kt/972 nm (108 pph/18 gph) Service ceiling 23,000 ft Single-engine service ceiling 12,000 ft Landing distance over 50-ft obst 675 ft Landing distance, ground roll 400 ft Limiting and Recommended Airspeeds Vmc (Min control w / 63 KIAS critical engine inoperative) Vx (Best angle of climb) 76 KIAS Vy (Best rate of climb) 91 KIAS Vyse (Best single-engine rate of climb) 83 KIAS Vfe (Max flap extended) 87 or 109 KIAS Vie (Max gear extended) 109 or 130 KIAS Vno (Max structural cruising) 156 KIAS Vne (Never exceed) 197 KIAS Vs I (Stall, clean) 52 KIAS Vso (Stall in landing configuration) 47 KIAS All speeifieatiotls are based Otl matlufaeturer's ealeu/atiotls. 'Performatlee figures are based Otl aircraft gross weight of 3,800 poutlds. Seguin Geronimo Price $97,498 (fully converted aircraft) Specifications Lycoming 0-360-AID 180 hp @ 2,700 rpm Recommended TBO 2,000 hr Propellers Hartzell two-blade, constant- speed, full-feathering; 74 in dia. 29 ft 8.6 in 9 ft 6 in 35 ft 3.6 in 207.6 sq ft 19.3 Ib/sq ft 11.1 Ib/hp 5 8 ft 3.5 in 4 ft 4.3 in 3 ft II in 2,500 Ib 4,000 Ib 1,5001b 852 Ib 648 Ib (108 gal) 936 Ib (156 gal) 1,200 Ib (200 gal) 250lb Powerplants l.ength Height Wingspan Wing area Wing loading Power loading Seats Cabin length Cabin height Cabin width Empty weight Gross weight Useful load Payload w /full fuel Fuel capacity, std w /wing tip tanks w /nacelle tanks Baggage capacity Performance· Takeoff distance, ground roll Takeoff distance over 50-ft obst Rate of climb, sea level Single-engine ROC, sea level Max level speed, sea level Cruise speed/range, std fuel (total fuel consumption) @ 75% power @ 65% power 400 ft 650 ft 2,000 fpm 750 fpm 174 kt




