PIPER PA44 SEMINOLE VITAL SPEC. SHEET
Piper PA-44 Seminole · Specifications
Overview
This document is a vital specifications sheet for the Piper PA-44 Seminole, providing essential data for pilots and aviation enthusiasts. It includes critical weight limits, fuel capacities, operational speeds, oil specifications, and electrical system details. The information is crucial for safe operation and maintenance of the aircraft, ensuring that pilots are aware of the performance parameters and limitations of the Seminole. This reference is particularly useful for flight planning and pre-flight checks, as it consolidates important specifications into a single document.
- Max ramp weight: 3816 lbs
- Max takeoff weight: 3800 lbs
- Fuel capacity: 110 USG (usable: 108 USG)
- V A: 135 KIAS at 3800 lbs, 112 KIAS at 2700 lbs
- Max demonstrated cross-wind speed: 17 KIAS
- Oil capacity: 6 quarts (minimum: 2 quarts)
- Electrical system: 14 V, 60 Amps output per alternator
Document
Source
Originally published by www.sharperedgesolutions.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Specifications
- Pages
- 1
- File size
- 33 KB
- Publisher
- www.sharperedgesolutions.com
Most owners only have the POH. Here's the essential set for the Piper PA-44 Seminole.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
More Piper PA-44 Seminolemanuals & documents
See all 37 →- PILOT’S CHECKLISTPilot's Operating Handbook
- Multi-Engine Study GuideOther Documents
- Type Acceptance Report TAR 98/04 Rev 3Parts Catalog
- NSA Master Checklist Seminoles Fuel Injected Rev 12Checklist
- SERVICE BULLETIN NO. 1354Service Bulletins
- PA 44 Seminole Checklist (2126Y)Checklist
- Piper Seminole Normal ChecklistPilot's Operating Handbook
- Piper Seminole Training SupplementWeight And Balance
- Minimum Equipment List as a Mechanism of Motion in MIRCE MechanicsOther Documents
- PIPER PA-44 SEMINOLEChecklist
- TYPE-CERTIFICATE DATA SHEET No. EASA.IM.A.232 For Piper PA-44Pilot's Operating Handbook
- Garmin G1000 NXi Pilot’s Guide for the Piper PA-44-180 SeminoleV Speeds Reference
In this document
Weights
The document outlines the weight specifications for the Piper PA-44 Seminole, including a maximum ramp weight of 3816 lbs, a maximum takeoff weight of 3800 lbs, and a maximum landing weight (MLW) also at 3800 lbs.
Fuel Capacity
The fuel capacity for the Piper PA-44 Seminole is detailed as a total of 110 US gallons, with 108 US gallons being usable for flight operations.
Speeds for Safe Operation
Operational speeds are critical for safe flight. The document lists various speeds including V A (135 KIAS at 3800 lbs and 112 KIAS at 2700 lbs), V MCA (56 KIAS), V FE (111 KIAS), and V NO (169 KIAS), among others, providing a comprehensive overview of the aircraft's performance capabilities.
Oil Specifications
Oil capacity is specified as 6 quarts, with a minimum requirement of 2 quarts. The document also outlines the oil pressure range, indicating a green arc of 15 to 115 psi and a yellow arc for idle at 15 to 60 psi.
Electrical System
The electrical system of the Piper PA-44 Seminole operates at 14 volts, with each alternator providing an output of 60 amps.
Tire Pressures
Tire pressure specifications are provided, with the nose wheel requiring 50 psi and the main wheels needing 55 psi.
Safety notes
- Ensure oil pressure is within the green arc (15 to 115 psi) during operation.
- Monitor oil temperature to remain below 245 °F.
Full document text
PIPER PA44 SEMINOLE VITAL SPEC. SHEET Weights: Max ramp weight: 3816 lbs Max T/O weight: 3800 lbs MLW: 3800 lbs Fuel capacity: Total : 110 USG Useable : 108 USG Oil: Capacity : 6 Quarts Minimum : 2 Quarts Speeds for safe operation: V A : 135 KIAS at 3800 lbs 112 KIAS at 2700 lbs V MCA : 56 KIAS V FE : 111 KIAS V SSE : 82 KIAS V LE : 140 KIAS V so : 55 KIAS V LO : 140 KIAS extension V s1 : 57 KIAS 109 KIAS retraction V NO : 169 KIAS V XSE : 82 KIAS V NE : 202 KIAS V YSE : 88 KIAS Max demonstrated cross-wind speed – 17 KIAS Oil pressure range and limits: Yellow arc : Green arc : Red line : 15 to 60 psi (idle) 90 to 115 psi (Warm Up, Taxi and Take Off) 15 to 115 psi 15 psi (min) 115 psi (max) Oil temperature range and limits: Green arc : Red radial : 75 to 245 °F 245 °F Electrical system: 14 V, output per alternator: 60 Amps Tire pressures: Nose wheel : 50 psi Main wheels: 55 psi