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PA-22-160X — Piper Aircraft PA-22-160X

Piper Aircraft PA-22-160X
PA22
Photo via Wikimedia Commons: Piper PA-22-135 Tri-Pacer N3328A FDK MD1.jpg
Year
Owner
Piper Aircraft
Last seen
MTOW
900 kg
Range
470 nm
Seats
4
PA-22-160Xhover
Piper Aircraft · PA-22-160X
Model overview

Fleet & certification

Built
31
Active
16
Origin
US
Variants

Per-variant specifications

VariantEngineMTOWRangeCruisePax
PA22
PA22
900 kg470 nm117 kt4
Same family

Other models in this family

Safety & ops history

Where to look next

Detailed safety & ops history coming soon — view this model's FAA Airworthiness Directives at FAA.gov.
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Piper Aircraft PA-22-160Xmarket & fleet intelligence

Registry, flight-tracking and market data on the Piper Aircraft PA-22-160X fleet — updated daily.

Fleet age

68 yearsmedian age

Of the 17 registered Piper Aircraft PA-22-160X with a known build year (55% of the 31 we track), the median age is 68 years.

Registration activity

4changed registration in 12 months

4 of the 31 registered Piper Aircraft PA-22-160X we track changed registration in the last 12 months (13% of the fleet), across 4 registration events. Registration changes include ownership transfers, re-registrations and address updates — not all are sales.

Piper Aircraft PA-22-160X manuals & documents

9 documents for the Piper Aircraft PA-22 family Type Certificate · Service Bulletins · Weight And Balance · Avionics Manual · Pilot's Operating Handbook · Maintenance Manual · Systems Description · Other Documents. PDFs served from cdn.sprinkle.com.

No documents are catalogued for the PA-22-160X specifically; these are the Piper Aircraft PA-22 family documents.

Overview
Pilot's Operating Handbook for the Piper PA-22 Tri-Pacer

This document serves as the Pilot's Operating Handbook (POH) for the Piper PA-22 Tri-Pacer, providing essential information for pilots operating this aircraft. It includes details on aircraft specifications, operating procedures, performance data, and safety information. The handbook is designed to assist pilots in understanding the aircraft's systems and capabilities, ensuring safe and efficient operation. It is a crucial resource for both training and reference during flight operations.

  • Maximum takeoff weight: 2,200 lbs
  • Useful load: approximately 800 lbs
  • Recommended takeoff speed: 60 knots
  • Climb speed: 75 knots
  • Stall speed in landing configuration: 50 knots
  • Maximum cruise speed: 120 knots
  • Range: approximately 500 nautical miles

Documents are sourced from publicly available references. Sprinkle does not host OEM-restricted materials; if you are a rights-holder and want a document removed, email .