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PIPER PA-44-180 Seminole Model Guide

PIPER PA-44-180 Seminole · Model Guide

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Overview

The PIPER PA-44-180 Seminole is a piston twin-engine airplane. The registry family (PA-44-180 and PA-44-180T) shows up to 4 passengers, up to 157 kt cruise, up to 830 nm range, up to 1700 kg MTOW and up to 17000 ft service ceiling. Those are family maximums, not figures for this variant. Take exact limits from the POH for your serial number.

  • Family data lists up to 4 passengers and up to 830 nm range. Use the POH for this exact airplane's limits.
  • Checklist single-engine speeds: Vmc 56 kt, Vyse 88 kt (blue line), Vxse 82 kt.
  • Losing one engine costs about 50% of power and roughly 80% of climb performance. The T-tail gives a lesser pitch-down.
  • Check the logs for ELT Service Bulletin 1020 and for the alternator replaced under Hartzell Service Letter 050.

Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.

Reference only, not for flight. Use the current approved manual for your aircraft. See terms, section 5.

Document

Source

Copy found at sprinkle.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

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Document details

Type
·
Model Guide
Year
·
2026
File size
·
49 KB
Copy found at
·
sprinkle.com

Specifications & performance

Extracted from this document.

Performance

Rotation speed (kt)
·
75
Cruise climb speed (kt)
·
105
Normal landing speed (kt)
·
80
Gear extended climb loss (fpm)
·
250
Short field landing speed (kt)
·
75
Short field rotation speed (kt)
·
70
Windmilling prop climb loss (fpm)
·
200

V-speeds

VFE_KTS
·
111
VLE_KTS
·
140
VMC_KTS
·
56
VNE_KTS
·
202
VS1_KTS
·
57
VSO_KTS
·
55
VXSE_KTS
·
82
VYSE_KTS
·
88
About this document
What are the key single-engine speeds?

For the PIPER PA-44-180 Seminole, the checklists give Vyse 88 kt (blue line), Vxse 82 kt and Vmc 56 kt (red line). The checklists tell you to hold blue line until on final in a single-engine landing.

What takeoff and climb speeds are listed?

The PIPER PA-44-180 Seminole checklists list rotation at 75 kt (70 kt short field) and climb at 88 kt. They list cruise climb at 105 kt, with 25 inches and 2500 RPM.

What are the landing gear speed limits?

The PIPER PA-44-180 Seminole checklists list maximum gear extension at 140 kt and retraction at 109 kt. Manual emergency gear extension is done below 100 KIAS.

What service documents apply to a used example?

For the PIPER PA-44-180 Seminole, review ELT Service Bulletin 1020 (ARTEX 110-4 battery pack) and Hartzell Service Letter 050, which approves an alternator replacement. Look for the logbook entry of compliance.

What is the PIPER PA-44-180 Seminole Model Guide?

The PIPER PA-44-180 Seminole Model Guide is a model guide for the PIPER PA-44-180 Seminole, dated 2026.

What year was the PIPER PA-44-180 Seminole Model Guide published?

The PIPER PA-44-180 Seminole Model Guide — the PIPER PA-44-180 Seminole model guide on file — is dated 2026.

How rare is it?
861PIPER PA-44-180 Seminole registered worldwide · 858 active

Common. More common than 95% of the aircraft models we track.

Documentation completeness
5/7

Most owners only have the POH. Here's the essential set for the PIPER PA-44-180 Seminole.

More PIPER PA-44-180 Seminolemanuals & documents

In this document

Handbook and applicability

The G1000 POH (Report VB-2636) covers serial numbers 4496395, 4496397 and up. It was issued November 3, 2016 and revised February 26, 2021. It is valid only for the airplane named on its title page and must be kept current. It does not cover non-Piper-approved STC installations, so inspect those separately.

Engine-out performance

The systems packet lists approximate single-engine climb penalties from the Seminole POH: flaps 25° -240 fpm, flaps 40° -275 fpm, windmilling prop -200 fpm, gear extended -250 fpm. Zero sideslip is a 2-3° bank into the operating engine with the ball half deflected. Ask any seller how the airplane flies on one engine.

Maintenance records to review

Service Bulletin 1020 (July 10, 1998) covers ARTEX 110-4 ELT battery packs that may vent acid. Compliance was due within 100 hours, with the ELT bracket checked for corrosion. Hartzell Service Letter 050 approves alternator ES-10024B-6 (24 volt, 100 amp) in place of Piper 651-756, for serial 4496331 and up.

Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.

Safety notes

  • After emergency landing gear extension, do not move any gear controls or reset circuit breakers until the airplane is on jacks.
  • One checklist says to feather and secure a failed engine below 2000 ft AGL and troubleshoot above it. Confirm against the POH.
  • The two checklists disagree on Vno (169 kt vs 129 kt), so confirm it in the POH.

Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.

Full document text

PIPER PA-44-180 Seminole Model Guide The PIPER PA-44-180 Seminole is a piston twin-engine airplane. The registry family (PA-44-180 and PA-44-180T) shows up to 4 passengers, up to 157 kt cruise, up to 830 nm range, up to 1700 kg MTOW and up to 17000 ft service ceiling. Those are family maximums, not figures for this variant. Take exact limits from the POH for your serial number. • Family data lists up to 4 passengers and up to 830 nm range. Use the POH for this exact airplane's limits. • Checklist single-engine speeds: Vmc 56 kt, Vyse 88 kt (blue line), Vxse 82 kt. • Losing one engine costs about 50% of power and roughly 80% of climb performance. The T-tail gives a lesser pitch-down. • Check the logs for ELT Service Bulletin 1020 and for the alternator replaced under Hartzell Service Letter 050. Handbook and applicability The G1000 POH (Report VB-2636) covers serial numbers 4496395, 4496397 and up. It was issued November 3, 2016 and revised February 26, 2021. It is valid only for the airplane named on its title page and must be kept current. It does not cover non-Piper-approved STC installations, so inspect those separately. Engine-out performance The systems packet lists approximate single-engine climb penalties from the Seminole POH: flaps 25° -240 fpm, flaps 40° -275 fpm, windmilling prop -200 fpm, gear extended -250 fpm. Zero sideslip is a 2-3° bank into the operating engine with the ball half deflected. Ask any seller how the airplane flies on one engine. Maintenance records to review Service Bulletin 1020 (July 10, 1998) covers ARTEX 110-4 ELT battery packs that may vent acid. Compliance was due within 100 hours, with the ELT bracket checked for corrosion. Hartzell Service Letter 050 approves alternator ES-10024B-6 (24 volt, 100 amp) in place of Piper 651-756, for serial 4496331 and up. Safety notes: • After emergency landing gear extension, do not move any gear controls or reset circuit breakers until the airplane is on jacks. • One checklist says to feather and secure a failed engine below 2000 ft AGL and troubleshoot above it. Confirm against the POH. • The two checklists disagree on Vno (169 kt vs 129 kt), so confirm it in the POH.