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Because of the raised zero-fuel weight and the raised maximum take-off weight, the Seneca III has the highest useful load of all the PA-34 variants. Some later models have electrically-actuated flaps. More than 930 Seneca IIIs were built; the last 37 Seneca IIIs built had a 28-volt electrical system rather than the 14-volt system of previous aircraft.
302:
192:
engines, a fixed nosewheel landing gear and a
Cherokee Six vertical tail. The second prototype flew on 30 August 1968, still with the 180 hp (134 kW) Lycomings but had retractable landing gear and a taller vertical tail. During development flying the wingspan was increased by two feet. The
321:
The Seneca V's gross weights remain the same as the Seneca III and IV at 4,750 lb (2,155 kg) for takeoff and 4,513 lb (2,047 kg) for landing, therefore, with all of the added features, the useful load is reduced by about 200 lb (91 kg). The standard useful load for the
279:
The horsepower increase, with the new engines limit of 2800 rpm (up from 2575 rpm), combined for much improved climb and cruise performance. The new aircraft also incorporated a one-piece windshield and a bare metal instrument panel instead of one covered with a removable plastic fascia.
292:
In 1994, the "New" Piper
Aircraft company introduced the Seneca IV, having achieved certification on 17 November 1993. This model was similar to the Seneca III offering minor improvements, such as a streamlined engine cowl for increased cruise performance. It continued to use the counter-rotating
309:
Certified on 11 December 1996, the Seneca V was put into production as a 1997 model year. Again the cowls were redesigned for increased performance, several cockpit switches were relocated from the panel to the headliner, and an improved engine variant, the
283:
The aircraft's gross weight was increased to 4,750 lb (2,155 kg) for takeoff and 4,513 lb (2,047 kg) for landing. A typical Seneca III with air conditioning and deicing equipment has a useful load of 1,377 lb (625 kg).
249:
The Seneca II also introduced optional "club seating" whereby the two center-row seats face rearwards and the two back seats face forward allowing more legroom in the passenger cabin. A total of 2,588 Seneca IIs were built.
915:
172:. The prototype was a Cherokee Six that had wing-mounted engines installed, retaining its nose engine. The prototype was flown as a tri-motor aircraft in the initial stages of the test-flying program.
217:
limitations of other light twins and make the aircraft more controllable in the event of a shut down or failure of either engine. A total of 934 Seneca models were built, including one prototype.
213:
engine variant, the "L" in its designation indicating that the crankshaft turns in the opposite direction, giving the Seneca counter-rotating engines. The counter-rotating engines eliminate the
253:
Gross weights are 4,570 lb (2,070 kg) for takeoff and 4,342 lb (1,969 kg) for landing, with all weight in excess of 4,000 lb (1,800 kg) required to be fuel.
322:
2014 model is 1,331 lb (604 kg) but typically is 1,134 lb (514 kg) when the aircraft is equipped with air conditioning, deicing equipment and co-pilot instruments.
236:
Responding to complaints about the aircraft's handling qualities, Piper introduced the PA-34-200T Seneca II. The aircraft was certified on 18 July 1974 and introduced as a 1975 model.
239:
The new model incorporated changes in the aircraft's control surfaces, including enlarged and balanced ailerons, the addition of a rudder anti-servo tab, and a stabilator bobweight.
355:
The aircraft is popular with air charter companies and small feeder airlines, and is operated by private individuals and companies. One notable civil operator is the Costa Rican
1143:
2905:
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220:
The early Seneca models have a maximum gross weight of 4,000 lb (1,810 kg), while later serial numbers allowed a takeoff weight of 4,200 lb (1,910 kg).
180:
With the decision to abandon the three-engined design tested on the PA-32-3M, the PA-34 was developed as a twin-engined aircraft. The prototype PA-34-180 Twin Six,
246:
or EB engines for improved performance, particularly at higher altitudes. The Seneca II retained the counter-rotating engine arrangement of the earlier Seneca I.
2920:
922:
1200:
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engines were used which produced 220 horsepower (165 kW), although only rated as such for five minutes and then dropping to 200 hp (149 kW).
1178:
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153:. It has been in non-continuous production since 1971. The Seneca is primarily used for personal and business flying as well as multi-engine
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third prototype was closer to the production standard and flew on 20 October 1969; it was fitted with 200 hp (149 kW)
911:
334:
as the EMB-810. The PA-34-200T was produced as the EMB-810C Seneca (452 built) and the PA-34-220T as the EMB-810D (228 built).
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Certified on 7 May 1971 and introduced in late 1971 as a 1972 model, the PA-34-200 Seneca is powered by a pair of
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870 nmi (1,000 mi, 1,611 km) max fuel, econ cruise at 18,000 ft (5,500 m), no reserves
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in a snowstorm. The pilot was trying to divert to KHTS due to a fuel emergency; all six aboard were killed.
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Continental TSIO-360-KB engines and gross weights remained unchanged. A total of 71 Seneca IVs were built.
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975:
Piper
Aircraft Seneca III Pilot Operating Handbook serial number 3448049, Section 6, Weight and Balance
269:
In 1981, the PA-34-220T Seneca III was introduced, having completed certification on 17 December 1980.
1201:"Small plane with DILG Secretary Jesse Robredo crashes off Masbate | News | GMA News Online"
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Piper
Aircraft Seneca V Pilot Operating Handbook serial number 3449270, Section 6, Weight and Balance
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Official website, Servicio de
Vigilancia AĂ©rea del Ministerio de Seguridad PĂşblica Costa Rica.
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home from an election campaign event crashed while attempting a night-time landing at the
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188 kn (216 mph, 348 km/h) econ cruise at 25,000 ft (7,600 m)
242:
The "T" in the new model designation reflected a change to turbocharged, six-cylinder
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English, Adrian J. "Air Power
Analysis:Central America and the Caribbean:Panama".
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188:, first flew on 25 April 1967. The prototype had two 180 hp (134 kW)
17:
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204 kn (235 mph, 378 km/h) at 23,000 ft (7,000 m)
2498:
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1227:, Volume 32 Spring 1998. London:Aerospace Publishing. pp. 142–157.
956:
573:
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841:, pages 106-107. Werner & Werner Corp, Santa Monica CA, 1977.
341:
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61 kn (70 mph, 113 km/h) wheels and flaps down
506:, killing Philippine Interior and Local Government Secretary
272:
The change in model designation reflected an engine upgrade.
495:
On 30 Janurary 2009 a Piper PA-34-200T Seneca crashed near
330:
From 1975 the Seneca was built under licence in Brazil by
168:
The Seneca was developed as a twin-engined version of the
1054:
1052:
1050:
1025:
1023:
2883:
are not included unless the designations were modified.
1329:
The Piper PA-34 Seneca V - Aircraft images and seat map
492:), killing Obenshain and the other two people on board.
2118:
1280:; Manual Part Number 753-817, dated October 30, 2003.
945:
The New Piper
Aircraft, Inc., 2003, Introduction, p.2
2114:
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Aircraft of comparable role, configuration, and era
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916:"Type Certificate Data Sheet No. A7SO Revision 17"
1144:"Pilot of Obenshain Plane Called 'Very Cautious'"
833:
831:
829:
827:
265:Piper Seneca III showing the one piece windshield
1283:Westerhuis, Rogier. "Fuerza AĂ©rea Ecuatoriana".
2122:
1289:, May 2000, Vol. 58, No. 5. pp. 277–281.
1278:Piper PA-34-200 Seneca Airplane Service Manual
795:Piper Aircraft – Freedom of Flight, Supplement
346:A Piper Seneca II with the engine cowl removed
2254:
1349:
612:6-cylinder, air-cooled, horizontally-opposed
504:crashed off the coast of Masbate, Philippines
8:
1103:Serbian air force receives multirole Seneca
777:, page 96. Houghton Mifflin Company, 1992.
2906:1960s United States civil utility aircraft
2261:
2247:
2239:
2190:
2110:
1387:
1380:
1356:
1342:
1334:
1239:Peperell, Roger W; Smith, Colin M (1987).
817:
815:
813:
811:
775:A Field Guide to Airplanes, Second Edition
29:
652:204 kn (235 mph, 378 km/h)
906:
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902:
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767:
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1263:Jane's All The World's Aircraft 1976-77
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676:21.2 lb/sq ft (104 kg/m)
557:38 ft 10.87 in (11.86 m)
610:Continental TSIO-360RB and LTSIO-360RB
1181:from the original on January 25, 2013
1171:"Crash victims possibly from Chicago"
551:28 ft 7.44 in (8.72 m)
502:On 18 August 2012 a PA-34-200 Seneca
7:
2921:Twin piston-engined tractor aircraft
1241:Piper Aircraft and their forerunners
1121:National Transportation Safety Board
773:Montgomery, MR & Gerald Foster:
569:208.7 sq ft (19.39 m)
563:9 ft 10.8 in (3.02 m)
515:Specifications (PA-34-220T Seneca V)
476:On 2 August 1978 a Seneca carrying
209:engines. The righthand engine is a
149:, produced in the United States by
1309:, 3 December 1988. pp. 22–87.
955:www.aerofiles.com (October 2008).
522:Piper Seneca V Information Manual
25:
1265:. London:Jane's Yearbooks, 1976,
1142:Harden, Blaine (August 4, 1978).
1116:"NTSB Identification: IAD78FA088"
670:1,550 ft/min (7.87 m/s)
1203:. Gmanetwork.com. 18 August 2012
696:
38:
2879:Designations carried over from
1062:. FlightGlobal. 4 December 2020
912:Federal Aviation Administration
797:, Air-Britain, Tonbridge 2020,
471:Notable accidents and incidents
58:Business and personal aircraft
1:
1276:The New Piper Aircraft, Inc.
664:25,000 ft (7,620 m)
602:4,750 lb (2,155 kg)
596:4,773 lb (2,165 kg)
590:3,212 lb (1,457 kg)
2916:Aircraft first flown in 1967
2881:American designation systems
1243:. Tonbridge, Kent, England:
1384:Single-engine prop aircraft
996:"Image of SVA Piper Seneca"
482:Chesterfield County Airport
2937:
821:Peperell 1987, pp. 227-232
27:Twin engine light aircraft
2877:
1301:"World's Air Forces 1988"
863:"Welcome to the Seneca V"
392:National Army of Colombia
387:Colombian Aerospace Force
37:
440:Panamanian Public Forces
357:Air Surveillance Service
305:Two examples of Seneca V
2682:Search & rescue (S)
1225:World Air Power Journal
1060:"World Air Forces 2021"
1032:"World Air Forces 2022"
839:1978 Aircraft Directory
616:, 220 hp (164 kW) each
530:General characteristics
312:Continental TSIO-360-RB
274:Continental TSIO-360-KB
44:Piper PA-34-220T Seneca
1017:3 December 1988, p.31.
746:List of civil aircraft
545:Five or six passengers
347:
326:Embraer EMB-810 Seneca
306:
266:
233:
2272:aircraft designations
1623:Multi-engine aircraft
1093:English 1998, p. 156.
957:"Piper aircraft page"
466:(PA-34-220T Seneca V)
345:
304:
264:
257:PA-34-220T Seneca III
244:Continental TSIO-360E
231:
211:Lycoming LIO-360-C1E6
1306:Flight International
1177:. February 1, 2009.
1035:. Flightglobal. 2022
1015:Flight International
685:0.1 hp/lb (164 W/kg)
478:Richard D. Obenshain
416:Ecuadorian Air Force
288:PA-34-220T Seneca IV
224:PA-34-200T Seneca II
207:Lycoming IO-360-C1E6
2270:Brazilian Air Force
1996:Post War Airplane 8
1991:Post War Airplane 6
1986:Post War Airplane 1
1791:Cherokee Pathfinder
1149:The Washington Post
928:on February 5, 2009
711:Related development
600:Max takeoff weight:
404:Dominican Air Force
374:Brazilian Air Force
297:PA-34-220T Seneca V
195:Lycoming IO-360-A1A
50:General information
2656:Reconnaissance (R)
1261:Taylor, John W.R.
914:(August 7, 2006).
648:Never exceed speed
524:(October 25, 2005)
490:Richmond, Virginia
452:Peruvian Air Force
428:Honduran Air Force
398:Dominican Republic
348:
307:
267:
234:
176:PA-34-180 Twin Six
170:Piper Cherokee Six
145:is a twin-engined
143:Piper PA-34 Seneca
124:Piper Cherokee Six
2911:Low-wing aircraft
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1286:Air International
1235:. ISSN 0959-7050.
1084:May 2000, p. 280.
1082:Air International
837:Plane and Pilot:
803:978-0-85130-524-0
464:Serbian Air Force
376:(EMB 810C Seneca)
314:, fitted with an
232:A Piper Seneca II
139:
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104:Introduction date
86:5037 (until 2019)
16:(Redirected from
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1801:Cherokee Warrior
1786:Cherokee Cruiser
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1322:Official website
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740:Related lists
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717:PZL M-20 Mewa
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134:PZL M-20 Mewa
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115:25 April 1967
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66:United States
65:
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2782:
2588:Maritime (M)
2107:designations
2066:Turbo Dakota
2051:Twin Stinson
2010:
1961:Pawnee Brave
1796:Cherokee Six
1654:
1377:designations
1304:
1284:
1277:
1262:
1240:
1224:
1218:Bibliography
1205:. Retrieved
1195:
1183:. Retrieved
1165:
1153:. Retrieved
1147:
1137:
1125:. Retrieved
1119:
1110:
1098:
1089:
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1076:
1064:. Retrieved
1037:. Retrieved
1014:
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999:. Retrieved
989:
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971:
960:. Retrieved
950:
941:
930:. Retrieved
923:the original
866:. Retrieved
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789:
774:
739:
738:
722:
721:
710:
709:
679:
673:
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641:Stall speed:
640:
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628:
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587:
579:laminar flow
572:
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318:, was used.
308:
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185:
179:
167:
155:class rating
142:
140:
112:First flight
99:1971–present
96:Manufactured
83:Number built
72:Manufacturer
33:PA-34 Seneca
2771:Utility (U)
2698:Trainer (T)
2535:Liaison (L)
2451:Fighter (F)
2091:Western Cub
2061:Turbo Arrow
1886:Grasshopper
1876:Flite Liner
1846:Cub Special
1841:Cub Cruiser
1245:Air-Britain
1080:Westerhuis
805:, p. 92–93.
622:Performance
606:Powerplant:
316:intercooler
164:Development
2895:Categories
2837:Glider (Z)
2625:Patrol (P)
2278:Attack (A)
1976:PiperSport
1951:Pathfinder
1771:Challenger
1207:2012-08-18
1001:2010-03-30
962:2010-03-30
932:2017-07-27
868:2017-07-27
752:References
734:Cessna 310
681:Power/mass
567:Wing area:
182:registered
2356:C-35 (II)
2309:Cargo (C)
2056:Tri-Pacer
2041:Super Cub
2031:Sky Sedan
2026:Sky Cycle
1851:Cub Cycle
1836:Cub Coupe
1811:Chieftain
1766:Caribbean
1391:High wing
1375:Numerical
1295:0306-5634
1066:5 January
555:Wingspan:
543:Capacity:
520:Data from
338:Operators
197:engines.
2351:C-35 (I)
2105:Military
2076:Vagabond
2046:Tomahawk
2021:Skycoupe
2006:Seminole
2001:Saratoga
1971:PiperJet
1921:Meridian
1881:Flitfire
1866:Enforcer
1826:Comanche
1806:Cheyenne
1781:Cherokee
1726:Aerostar
1603:Mid wing
1492:Low wing
1367:aircraft
1185:July 25,
1179:Archived
1127:July 27,
690:See also
422:Honduras
381:Colombia
363:Military
130:Variants
2096:Warrior
2016:Sequoya
1946:Papoose
1816:Clipper
1776:Charger
1741:Arapaho
1731:Altaire
1373:Company
1039:18 July
584:652-415
574:Airfoil
561:Height:
549:Length:
410:Ecuador
332:Embraer
91:History
2483:F-2000
2141:UC-83B
2136:UC-83A
2011:Seneca
1981:Pocono
1956:Pawnee
1936:Navajo
1931:Mojave
1926:Mirage
1916:Malibu
1861:Dakota
1746:Archer
1736:Apache
1650:PA-31T
1569:PA-32R
1293:
1269:
1251:
1231:
845:
801:
781:
656:Range:
458:Serbia
434:Panama
368:Brazil
186:N3401K
2514:VH-34
2478:F-103
2426:C-115
2421:C-105
2131:UC-83
2119:USAAF
2115:USAAC
1941:Pacer
1891:Lance
1761:Cadet
1756:Aztec
1751:Arrow
1719:Names
1706:PA-47
1690:PA-60
1685:PA-44
1680:PA-42
1675:PA-41
1670:PA-40
1665:PA-39
1660:PA-35
1655:PA-34
1645:PA-31
1640:PA-30
1635:PA-27
1630:PA-23
1610:PA-21
1594:PA-48
1589:PA-46
1584:PA-38
1579:PA-36
1574:PA-33
1564:PA-32
1559:PA-29
1554:PA-28
1549:PA-26
1544:PA-25
1539:PA-24
1534:PA-10
1514:PWA-8
1509:PWA-6
1504:PWA-1
1483:PA-22
1478:PA-20
1473:PA-19
1468:PA-18
1463:PA-17
1458:PA-16
1453:PA-15
1448:PA-14
1443:PA-12
1438:PA-11
1365:Piper
1155:8 May
926:(PDF)
919:(PDF)
757:Notes
537:Crew:
351:Civil
2869:Z-23
2864:Z-20
2859:Z-16
2854:Z-15
2849:Z-13
2828:U-93
2823:U-55
2818:U-45
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2673:R-99
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2647:P-99
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2595:M-16
2579:L-42
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2526:H-55
2521:H-50
2509:H-34
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2416:C-99
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2371:C-55
2366:C-42
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2341:C-26
2336:C-10
2300:A-29
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2290:A-10
2181:U-11
2171:TG-8
2166:O-59
2161:L-21
2156:L-18
2151:L-14
2123:USAF
1911:M700
1906:M600
1901:M500
1896:M350
1821:Colt
1699:Jets
1529:PA-8
1524:PA-7
1519:PA-6
1499:PT-1
1291:ISSN
1267:ISBN
1249:ISBN
1229:ISBN
1187:2024
1157:2016
1129:2017
1068:2021
1041:2022
843:ISBN
799:ISBN
779:ISBN
608:2 Ă—
582:NACA
497:KHTS
446:Peru
141:The
107:1971
55:Type
2844:Z-3
2793:U-9
2788:U-8
2783:U-7
2778:U-3
2710:T-8
2705:T-7
2616:O-6
2611:O-3
2567:A/E
2557:L-8
2552:L-7
2547:L-6
2542:L-3
2499:H-4
2463:F-8
2458:F-7
2331:C-9
2326:C-8
2321:C-2
2316:C-1
2285:A-1
2219:LBP
2214:LNP
2191:USN
2176:U-7
2146:L-4
1831:Cub
1433:P-4
1428:P-2
1423:P-1
1418:J-5
1413:J-4
1408:J-3
1403:J-2
1398:F-2
539:One
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