EasyManua.ls Logo

Piper PA-38-112 - Page 63

Piper PA-38-112
213 pages
Print Icon
To Next Page IconTo Next Page
To Next Page IconTo Next Page
To Previous Page IconTo Previous Page
To Previous Page IconTo Previous Page
Loading...
Performance for a specific airplane may vary from published figures
depending upon the equipment installed, the condition of the engine,
airplane and equipment, atmospheric conditions and piloting technique.
(a) Best Rate Of Climb Speed 70 KIAS
(b) Best Angle of Climb Speed 61 KIAS
(c) Turbulent Air Operating Speed (See CAUTION
Subsection 2.3) 103 KIAS
(d) Maximum Flap Speed 89 KIAS
(e) Landing Final Approach Speed
Full Flaps, 34° (Outboard Flow Strips Installed) 62 KIAS
Full Flaps, 34° (Outboard and Inboard Flow
Strips Installed) 67 KIAS
(f) Maximum Demonstrated Crosswind Velocity 15 KTS
SECTION 4 PIPER AIRCRAFT CORPORATION
NORMAL PROCEDURES PA-38-112, TOMAHAWK
REPORT: 2126 ISSUED: JANUARY 20, 1978
4-2 REVISED: DECEMBER 18, 1978
Performance for a specific airplane may vary from published figures
depending upon the equipment installed, the condition of the engine,
airplane and equipment, atmospheric conditions and piloting technique.
(a) Best Rate Of Climb Speed 70 KIAS
(b) Best Angle of Climb Speed 61 KIAS
(c) Turbulent Air Operating Speed (See CAUTION
Subsection 2.3) 103 KIAS
(d) Maximum Flap Speed 89 KIAS
(e) Landing Final Approach Speed
Full Flaps, 34° (Outboard Flow Strips Installed) 62 KIAS
Full Flaps, 34° (Outboard and Inboard Flow
Strips Installed) 67 KIAS
(f) Maximum Demonstrated Crosswind Velocity 15 KTS
SECTION 4 PIPER AIRCRAFT CORPORATION
NORMAL PROCEDURES PA-38-112, TOMAHAWK
REPORT: 2126 ISSUED: JANUARY 20, 1978
4-2 REVISED: DECEMBER 18, 1978

Table of Contents

Related product manuals