Piper PA-38-112 User Manual

NOTES
Straight line variation between points given.
The datum used is 66.25 inches ahead of the
wing leading edge.
It is the responsibility of the airplane owner
and the pilot to insure that the airplane is
properly loaded. See Section 6 (Weight and
Balance) for proper loading instructions.
2.15 MANEUVER LIMITS
(a) Normal Category - All acrobatic maneuvers including spins
prohibited.
(b) Utility Category - Approved maneuvers for Utility Category Only.
MANEUVER ENTRY SPEED
Spins (flaps up) Stall
Steep Turns 100 KIAS
Lazy Eights 100 KIAS
Chandelles 100 KIAS
2.17 FLIGHT MANEUVERING LOAD FACTORS
Normal Utility
(a) Positive Load Factor (Maximum)
(1) Flaps Up 3.8 G 4.4 G
(2) Flaps Down 2.0 G 2.0 G
(b) Negative Load Factor (Maximum) No inverted maneuvers
approved.
PIPER AIRCRAFT CORPORATION SECTION 2
PA-38-112, TOMAHAWK LIMITATIONS
ISSUED: JANUARY 20, 1978 REPORT: 2126
REVISED: JANUARY 15, 1981 2-5
NOTES
Straight line variation between points given.
The datum used is 66.25 inches ahead of the
wing leading edge.
It is the responsibility of the airplane owner
and the pilot to insure that the airplane is
properly loaded. See Section 6 (Weight and
Balance) for proper loading instructions.
2.15 MANEUVER LIMITS
(a) Normal Category - All acrobatic maneuvers including spins
prohibited.
(b) Utility Category - Approved maneuvers for Utility Category Only.
MANEUVER ENTRY SPEED
Spins (flaps up) Stall
Steep Turns 100 KIAS
Lazy Eights 100 KIAS
Chandelles 100 KIAS
2.17 FLIGHT MANEUVERING LOAD FACTORS
Normal Utility
(a) Positive Load Factor (Maximum)
(1) Flaps Up 3.8 G 4.4 G
(2) Flaps Down 2.0 G 2.0 G
(b) Negative Load Factor (Maximum) No inverted maneuvers
approved.
PIPER AIRCRAFT CORPORATION SECTION 2
PA-38-112, TOMAHAWK LIMITATIONS
ISSUED: JANUARY 20, 1978 REPORT: 2126
REVISED: JANUARY 15, 1981 2-5

Piper PA-38-112 Specifications

General

Brand	Piper
Model	PA-38-112
Category	Aircrafts
Language	English