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Aircraft Performance Database

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Performance

TAKE-OFF CLIMB (to FL 150) CLIMB (to FL 240) MACH CLIMB CRUISE INITIAL DESCENT (to FL 240) DESCENT (to FL 100) APPROACH LANDING INITIAL CLIMB (to 5000 ft) CLIMB (to FL 240) CLIMB (to FL 150) DESCENT (to FL 100)

Select performance graph to see data.

TAKE-OFF MTOW: WTC: RECAT-EU: - Distance: V2 (IAS): - - INITIAL CLIMB (to 5000 ft) IAS: ROC: - - CLIMB (to FL 240) IAS: ROC: - - CLIMB (to FL 150) IAS: ROC: - - MACH CLIMB MACH: ROC: - - CRUISE MACH: Ceiling: - - TAS: - Range: - INITIAL DESCENT (to FL 240) MACH: - ROD: - DESCENT (to FL 100) IAS: - ROD: - APPROACH IAS: - MCS: - ROD: - LANDING Vat (IAS): - APC: - Distance: - - -

Take-off

V2 (IAS) 80 kts

Distance 300 m

WTC L

RECAT-EU Light

MTOW 2100 kg

Initial climb (to 5000ft)

IAS 110 kts

ROC 1300 ft/min

Climb (to FL 150)

IAS 140 kts

ROC 800 ft/min

Climb (to FL 240)

IAS 140 kts

ROC 100 ft/min

MACH climb

MACH no data

ROC no data ft/min

Cruise

TAS 160 kt

MACH no data

Ceiling FL 190

Range 980 NM

Initial Descent (to FL 240)

MACH no data

ROD no data ft/min

Descent (to FL 100)

IAS 160 kt

ROD 800 ft/min

Approach

IAS 140 kt

ROD 500 ft/min

MCS 90 kt

Landing

Vat (IAS) 80 kt

Distance 400 m

APC A

Type of Aircraft

Type

L2P

APC

A

WTC

L

RECAT-EU

Light

Technical

Wing Span

11.9 m

Length

8.7 m

Height

3 m

Power plant

2 x 200 HP Lycoming IO-360-A1A piston engines or 2 x 200 HP Continental TSIO-360-E turbocharged piston engines with 2 blade propellers. Seneca III & IV: 2 x 220 HP Continental TSIO-360-KB turbocharged piston engines with 3 blade propellers. Seneca V: 2x 220HP Continental TSIO-360-RB with 3 blade propellers

Performance Similarity

No data

Recognition

Wing position

Low wing

Engine position

(Front) Wing leading mounted

Tail configuration

Regular tail, mid set

Landing gear

Tricycle retractable

Recognition similarity

No data

Supplementary

IATA

no data

Accommodation

One pilot and 5 passengers.

Notes

Light twin aircraft. In service since 1971. Twin-engine development of PA-32R. First version PA-34-200 Seneca replaced by 200T Seneca II in 1974. Further development 210T Seneca III introduced in 1981, replaced by 220T Seneca IV in 1994. Licence production by CHINCUL, Argentinia, AICSA, Columbia, and by EMBRAER/NAIVA, Brazil, as EMB-810 Seneca. Seneca II built by PZL-MIELEC, Poland, as M-20 Mewa, Gemini. Latest model Seneca V (introduced in 1998) with Continental TSIO-360-RB engines and five seats.

Alternative names

  • PA-34 Seneca

  • PIPER PA-34 Seneca

  • Princess

  • PZL-MIELEC M-20 Mewa,Gemini

  • SEGUIN Princess

  • Seneca

  • TM-20 Flamingo 3

  • U-7 (PA-34)