Seminole Load Chart
PIPER PA-44-180 Seminole · Weight & Balance
Overview
This document provides the load chart for the Piper PA-44-180 Seminole, detailing weight limits and center of gravity specifications. It includes information on maximum takeoff weight, basic empty weight, and loading guidelines.
- Maximum Takeoff Weight (MTOW) is 1723 Kg.
- Basic Empty Weight (BEW) is 1161 Kg.
- Maximum ramp weight is 1730 Kg.
- Usable fuel capacity is 409 liters, equivalent to 294 Kg.
- The pilot must confirm loading results using the approved system from the Pilot's Operating Handbook.
- Center of Gravity (C of G) envelope specifications are provided.
- Maximum rear baggage weight is 91.0 Kg.
Document
Source
Originally published by com.au. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Weight & Balance
- File size ·
- 51 KB
- Publisher ·
- com.au
- Language ·
- en
Specifications & performance
Extracted from this document.
Specifications
- Bew kg ·
- 1161
- Mtow kg ·
- 1723
- Usable fuel l ·
- 409
- Max ramp weight kg ·
- 1730
- Rear baggage max kg ·
- 91.0
Weight & balance
- Rear seats weight kg ·
- 3000
- Front seats weight kg ·
- 2045
What is the Seminole Load Chart?
The Seminole Load Chart is a weight & balance for the PIPER PA-44-180 Seminole.
Where does the Seminole Load Chart come from?
This copy of the Seminole Load Chart was originally published by com.au and is hosted on Sprinkle as a free, searchable reference copy.
Most owners only have the POH. Here's the essential set for the PIPER PA-44-180 Seminole.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
More PIPER PA-44-180 Seminolemanuals & documents
- PA-44 2022Checklist
- Pilot’s Operating Handbook and FAA Approved Airplane Flight ManualPilot's Operating Handbook
- Service Letter No. 050Service Bulletins
- SERVICE BULLETIN NO. 1020Service Bulletins
- Seminole Systems PacketSystems Description
- Piper Seminole Normal ChecklistChecklist
- PIPER SEMINOLE PA44-180 CHECKLISTChecklist
Related documents
- Weight & Balance for the Piper PA-44 SeminolePiper PA-44 Seminole · Weight & Balance
- PIPER PA44 SEMINOLE VITAL SPEC. SHEETPiper PA-44 Seminole · Specifications
- SEMINOLE PA-44-180 INFORMATION MANUALPiper PA-44 Seminole · Pilot's Operating Handbook
- Weight & Balance for the Piper PA-44 SeminolePiper PA-44 Seminole · Weight & Balance
- PERFORMANCE PA-44-180, SEMINOLEPiper PA-44 Seminole · Performance Data
In this document
Weight Specifications
The document lists the Maximum Takeoff Weight (MTOW) as 1723 Kg and the Basic Empty Weight (BEW) as 1161 Kg.
Fuel Capacity
The usable fuel capacity is 409 liters, which weighs 294 Kg.
Loading Guidelines
The pilot must confirm loading results using the approved loading system from the Pilot's Operating Handbook.
Weight Limits
The maximum ramp weight is 1730 Kg.
Center of Gravity Envelope
The document provides specifications for the Center of Gravity (C of G) envelope.
Baggage Limitations
The maximum weight for rear baggage is 91.0 Kg.
Full document text
Seminole Load Chart Piper Model PA 44 - 180 Registration VH-WHV MTOW 1723 Kg BEW 1161 Kg Item Weight (Kg) Arm (mm) Basic Empty Weight 1161 2202 2556292 Front Seats 2045 Rear Seats 3000 3627 Zero Fuel Wt: Fuel Litres Kg 2413 Taxi & Run Up Fuel (-) 2413 Gross Wt: MTOW = 1723 Kg NOTE: Pilot must confirm result using approved loading system from Pilots Operating Handbook. mm Kg 2133.6 1000 2133.6 1270 2159 1542 2260.6 1723 2362.2 1723 2362.2 1000 Moment (mm.Kg) Rear Baggage (max 91.0Kg) Usable 409 lt 294 kg Ramp Weight. Max 1730 Kg CofG envelope specification 2100 2150 2200 2250 2300 2350 2400 1000 1100 1200 1300 1400 1500 1600 1700 Centre of Gravity Envelope C of G (mm AFT of Datum) Total Weight (Kg) C of G (mm AFT of Datum)