251:
29:
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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.
181:
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
310:
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
268:
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.
281:
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
298:
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
272:
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).
238:
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.
904:
161:. 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.
206:
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.
202:
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
242:
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.
311:
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.
225:
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.
228:
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.
344:
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
1132:
209:
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).
169:
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,
235:
or EB engines for improved performance, particularly at higher altitudes. The Seneca II retained the counter-rotating engine arrangement of the earlier Seneca I.
911:
1189:
265:
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).
2894:
2869:
2249:
1167:
2698:
1317:
2909:
142:. It has been in non-continuous production since 1971. The Seneca is primarily used for personal and business flying as well as multi-engine
1421:
1416:
1411:
1091:
1344:
2242:
182:
third prototype was closer to the production standard and flew on 20 October 1969; it was fitted with 200 hp (149 kW)
323:
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).
2904:
791:
1109:
982:
2235:
492:
1020:
2502:
2414:
1259:
1241:
1221:
835:
771:
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194:
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
900:
1104:
647:
870 nmi (1,000 mi, 1,611 km) max fuel, econ cruise at 18,000 ft (5,500 m), no reserves
2514:
2750:
2349:
2288:
1337:
488:
in a snowstorm. The pilot was trying to divert to KHTS due to a fuel emergency; all six aboard were killed.
282:
Continental TSIO-360-KB engines and gross weights remained unchanged. A total of 71 Seneca IVs were built.
2509:
2656:
2630:
2497:
2384:
470:
250:
2492:
2899:
1859:
1436:
964:
Piper
Aircraft Seneca III Pilot Operating Handbook serial number 3448049, Section 6, Weight and Balance
258:
In 1981, the PA-34-220T Seneca III was introduced, having completed certification on 17 December 1980.
1190:"Small plane with DILG Secretary Jesse Robredo crashes off Masbate | News | GMA News Online"
2324:
2278:
2059:
2024:
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1628:
1431:
973:
Piper
Aircraft Seneca V Pilot Operating Handbook serial number 3449270, Section 6, Weight and Balance
380:
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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
8:
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158:
112:
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188 kn (216 mph, 348 km/h) econ cruise at 25,000 ft (7,600 m)
231:
The "T" in the new model designation reflected a change to turbocharged, six-cylinder
2852:
2604:
2535:
2044:
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1929:
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485:
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2740:
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717:
474:
28:
1212:
English, Adrian J. "Air Power
Analysis:Central America and the Caribbean:Panama".
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2004:
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177:, first flew on 25 April 1967. The prototype had two 180 hp (134 kW)
139:
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65:
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204 kn (235 mph, 378 km/h) at 23,000 ft (7,000 m)
217:
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1216:, Volume 32 Spring 1998. London:Aerospace Publishing. pp. 142–157.
2811:
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2019:
2014:
2009:
1984:
1979:
1974:
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830:, pages 106-107. Werner & Werner Corp, Santa Monica CA, 1977.
1322:
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899:
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61 kn (70 mph, 113 km/h) wheels and flaps down
495:, killing Philippine Interior and Local Government Secretary
261:
The change in model designation reflected an engine upgrade.
484:
On 30 Janurary 2009 a Piper PA-34-200T Seneca crashed near
319:
From 1975 the Seneca was built under licence in Brazil by
290:
157:
The Seneca was developed as a twin-engined version of the
1043:
1041:
1039:
1014:
1012:
2872:
are not included unless the designations were modified.
1318:
The Piper PA-34 Seneca V - Aircraft images and seat map
503:
481:), killing Obenshain and the other two people on board.
1227:
2107:
1269:; Manual Part Number 753-817, dated October 30, 2003.
1036:
1009:
934:
The New Piper
Aircraft, Inc., 2003, Introduction, p.2
2103:
682:
712:
Aircraft of comparable role, configuration, and era
1019:
905:"Type Certificate Data Sheet No. A7SO Revision 17"
459:
1133:"Pilot of Obenshain Plane Called 'Very Cautious'"
997:
943:
822:
820:
818:
816:
254:Piper Seneca III showing the one piece windshield
2881:
1272:Westerhuis, Rogier. "Fuerza AĂ©rea Ecuatoriana".
2111:
1278:, May 2000, Vol. 58, No. 5. pp. 277–281.
1267:Piper PA-34-200 Seneca Airplane Service Manual
813:
784:Piper Aircraft – Freedom of Flight, Supplement
335:A Piper Seneca II with the engine cowl removed
2243:
1338:
958:
601:6-cylinder, air-cooled, horizontally-opposed
493:crashed off the coast of Masbate, Philippines
1092:Serbian air force receives multirole Seneca
766:, page 96. Houghton Mifflin Company, 1992.
2895:1960s United States civil utility aircraft
2250:
2236:
2179:
1345:
1331:
1228:Peperell, Roger W; Smith, Colin M (1987).
846:
806:
804:
802:
800:
764:A Field Guide to Airplanes, Second Edition
976:
641:204 kn (235 mph, 378 km/h)
314:
937:
895:
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1252:Jane's All The World's Aircraft 1976-77
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665:21.2 lb/sq ft (104 kg/m)
546:38 ft 10.87 in (11.86 m)
276:
212:
2882:
1130:
599:Continental TSIO-360RB and LTSIO-360RB
285:
2231:
1326:
1170:from the original on January 25, 2013
1160:"Crash victims possibly from Chicago"
751:
540:28 ft 7.44 in (8.72 m)
491:On 18 August 2012 a PA-34-200 Seneca
164:
2910:Twin piston-engined tractor aircraft
1230:Piper Aircraft and their forerunners
1110:National Transportation Safety Board
928:
864:
840:
762:Montgomery, MR & Gerald Foster:
558:208.7 sq ft (19.39 m)
552:9 ft 10.8 in (3.02 m)
504:Specifications (PA-34-220T Seneca V)
967:
465:On 2 August 1978 a Seneca carrying
198:engines. The righthand engine is a
189:
138:, produced in the United States by
13:
1352:
1298:, 3 December 1988. pp. 22–87.
944:www.aerofiles.com (October 2008).
511:Piper Seneca V Information Manual
14:
2921:
1302:
1254:. London:Jane's Yearbooks, 1976,
1131:Harden, Blaine (August 4, 1978).
1105:"NTSB Identification: IAD78FA088"
659:1,550 ft/min (7.87 m/s)
1192:. Gmanetwork.com. 18 August 2012
685:
27:
2868:Designations carried over from
1182:
1152:
1124:
1097:
1085:
1076:
1063:
1051:. FlightGlobal. 4 December 2020
901:Federal Aviation Administration
786:, Air-Britain, Tonbridge 2020,
460:Notable accidents and incidents
776:
152:
47:Business and personal aircraft
1:
1265:The New Piper Aircraft, Inc.
740:
653:25,000 ft (7,620 m)
591:4,750 lb (2,155 kg)
585:4,773 lb (2,165 kg)
579:3,212 lb (1,457 kg)
2905:Aircraft first flown in 1967
2870:American designation systems
1232:. Tonbridge, Kent, England:
326:
7:
1373:Single-engine prop aircraft
985:"Image of SVA Piper Seneca"
678:
471:Chesterfield County Airport
351:
10:
2926:
810:Peperell 1987, pp. 227-232
16:Twin engine light aircraft
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1290:"World's Air Forces 1988"
852:"Welcome to the Seneca V"
381:National Army of Colombia
376:Colombian Aerospace Force
118:
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79:
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51:
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38:
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429:Panamanian Public Forces
346:Air Surveillance Service
339:
294:Two examples of Seneca V
2671:Search & rescue (S)
1214:World Air Power Journal
1049:"World Air Forces 2021"
1021:"World Air Forces 2022"
828:1978 Aircraft Directory
605:, 220 hp (164 kW) each
519:General characteristics
301:Continental TSIO-360-RB
263:Continental TSIO-360-KB
33:Piper PA-34-220T Seneca
1006:3 December 1988, p.31.
735:List of civil aircraft
534:Five or six passengers
336:
315:Embraer EMB-810 Seneca
295:
255:
222:
2261:aircraft designations
1612:Multi-engine aircraft
1082:English 1998, p. 156.
946:"Piper aircraft page"
455:(PA-34-220T Seneca V)
334:
293:
253:
246:PA-34-220T Seneca III
233:Continental TSIO-360E
220:
200:Lycoming LIO-360-C1E6
1295:Flight International
1166:. February 1, 2009.
1024:. Flightglobal. 2022
1004:Flight International
674:0.1 hp/lb (164 W/kg)
467:Richard D. Obenshain
405:Ecuadorian Air Force
277:PA-34-220T Seneca IV
213:PA-34-200T Seneca II
196:Lycoming IO-360-C1E6
2259:Brazilian Air Force
1985:Post War Airplane 8
1980:Post War Airplane 6
1975:Post War Airplane 1
1780:Cherokee Pathfinder
1138:The Washington Post
917:on February 5, 2009
700:Related development
589:Max takeoff weight:
393:Dominican Air Force
363:Brazilian Air Force
286:PA-34-220T Seneca V
184:Lycoming IO-360-A1A
39:General information
2645:Reconnaissance (R)
1250:Taylor, John W.R.
903:(August 7, 2006).
637:Never exceed speed
513:(October 25, 2005)
479:Richmond, Virginia
441:Peruvian Air Force
417:Honduran Air Force
387:Dominican Republic
337:
296:
256:
223:
165:PA-34-180 Twin Six
159:Piper Cherokee Six
134:is a twin-engined
132:Piper PA-34 Seneca
113:Piper Cherokee Six
2900:Low-wing aircraft
2877:
2876:
2225:
2224:
2221:
2220:
1703:
1702:
1607:
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1275:Air International
1224:. ISSN 0959-7050.
1073:May 2000, p. 280.
1071:Air International
826:Plane and Pilot:
792:978-0-85130-524-0
453:Serbian Air Force
365:(EMB 810C Seneca)
303:, fitted with an
221:A Piper Seneca II
128:
127:
93:Introduction date
75:5037 (until 2019)
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1790:Cherokee Warrior
1775:Cherokee Cruiser
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910:. Archived from
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718:Beechcraft Baron
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651:Service ceiling:
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475:general aviation
190:PA-34-200 Seneca
31:
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729:Related lists
724:
721:
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706:PZL M-20 Mewa
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624:Cruise speed:
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497:Jesse Robredo
494:
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477:airport near
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123:PZL M-20 Mewa
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104:25 April 1967
103:
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55:United States
54:
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42:
37:
30:
25:
20:
2771:
2577:Maritime (M)
2096:designations
2055:Turbo Dakota
2040:Twin Stinson
1999:
1950:Pawnee Brave
1785:Cherokee Six
1643:
1366:designations
1293:
1273:
1266:
1251:
1229:
1213:
1207:Bibliography
1194:. Retrieved
1184:
1172:. Retrieved
1154:
1142:. Retrieved
1136:
1126:
1114:. Retrieved
1108:
1099:
1087:
1078:
1070:
1065:
1053:. Retrieved
1026:. Retrieved
1003:
999:
988:. Retrieved
978:
969:
960:
949:. Retrieved
939:
930:
919:. Retrieved
912:the original
855:. Retrieved
842:
827:
783:
778:
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711:
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630:Stall speed:
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568:laminar flow
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307:, was used.
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193:
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168:
156:
144:class rating
131:
129:
101:First flight
88:1971–present
85:Manufactured
72:Number built
61:Manufacturer
22:PA-34 Seneca
2760:Utility (U)
2687:Trainer (T)
2524:Liaison (L)
2440:Fighter (F)
2080:Western Cub
2050:Turbo Arrow
1875:Grasshopper
1865:Flite Liner
1835:Cub Special
1830:Cub Cruiser
1234:Air-Britain
1069:Westerhuis
794:, p. 92–93.
611:Performance
595:Powerplant:
305:intercooler
153:Development
2884:Categories
2826:Glider (Z)
2614:Patrol (P)
2267:Attack (A)
1965:PiperSport
1940:Pathfinder
1760:Challenger
1196:2012-08-18
990:2010-03-30
951:2010-03-30
921:2017-07-27
857:2017-07-27
741:References
723:Cessna 310
670:Power/mass
556:Wing area:
171:registered
2345:C-35 (II)
2298:Cargo (C)
2045:Tri-Pacer
2030:Super Cub
2020:Sky Sedan
2015:Sky Cycle
1840:Cub Cycle
1825:Cub Coupe
1800:Chieftain
1755:Caribbean
1380:High wing
1364:Numerical
1284:0306-5634
1055:5 January
544:Wingspan:
532:Capacity:
509:Data from
327:Operators
186:engines.
2340:C-35 (I)
2094:Military
2065:Vagabond
2035:Tomahawk
2010:Skycoupe
1995:Seminole
1990:Saratoga
1960:PiperJet
1910:Meridian
1870:Flitfire
1855:Enforcer
1815:Comanche
1795:Cheyenne
1770:Cherokee
1715:Aerostar
1592:Mid wing
1481:Low wing
1356:aircraft
1174:July 25,
1168:Archived
1116:July 27,
679:See also
411:Honduras
370:Colombia
352:Military
119:Variants
2085:Warrior
2005:Sequoya
1935:Papoose
1805:Clipper
1765:Charger
1730:Arapaho
1720:Altaire
1362:Company
1028:18 July
573:652-415
563:Airfoil
550:Height:
538:Length:
399:Ecuador
321:Embraer
80:History
2472:F-2000
2130:UC-83B
2125:UC-83A
2000:Seneca
1970:Pocono
1945:Pawnee
1925:Navajo
1920:Mojave
1915:Mirage
1905:Malibu
1850:Dakota
1735:Archer
1725:Apache
1639:PA-31T
1558:PA-32R
1282:
1258:
1240:
1220:
834:
790:
770:
645:Range:
447:Serbia
423:Panama
357:Brazil
175:N3401K
2503:VH-34
2467:F-103
2415:C-115
2410:C-105
2120:UC-83
2108:USAAF
2104:USAAC
1930:Pacer
1880:Lance
1750:Cadet
1745:Aztec
1740:Arrow
1708:Names
1695:PA-47
1679:PA-60
1674:PA-44
1669:PA-42
1664:PA-41
1659:PA-40
1654:PA-39
1649:PA-35
1644:PA-34
1634:PA-31
1629:PA-30
1624:PA-27
1619:PA-23
1599:PA-21
1583:PA-48
1578:PA-46
1573:PA-38
1568:PA-36
1563:PA-33
1553:PA-32
1548:PA-29
1543:PA-28
1538:PA-26
1533:PA-25
1528:PA-24
1523:PA-10
1503:PWA-8
1498:PWA-6
1493:PWA-1
1472:PA-22
1467:PA-20
1462:PA-19
1457:PA-18
1452:PA-17
1447:PA-16
1442:PA-15
1437:PA-14
1432:PA-12
1427:PA-11
1354:Piper
1144:8 May
915:(PDF)
908:(PDF)
746:Notes
526:Crew:
340:Civil
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