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Piper ARCHER III - Flight Load Factors; Fuel Limitations; Maneuver Limits; Types of Operations

Piper ARCHER III
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SECTION 2
LIMITATIONS PA-28-181, ARCHER III
SECTION 2
LIMITATIONS PA-28-181, ARCHER III
REPORT: VB-1611 ISSUED: JULY 12, 1995
2-6
REPORT: VB-1611 ISSUED: JULY 12, 1995
2-6
2.15 MANEUVER LIMITS
(a) Normal Category - All acrobatic maneuvers including spins
prohibited.
(b) Utility Category - Approved maneuvers for bank angles exceeding
60°.
Entry Speed
Steep Turns 113 KIAS
Lazy Eights 113 KIAS
Chandelles 113 KIAS
2.17 FLIGHT LOAD FACTORS
Normal Utility
(a) Positive Load Factor (Maximum) 3.8 G 4.4 G
(b) Negative Load Factor (Maximum) No inverted maneuvers
approved
2.19 TYPES OF OPERATION
The airplane is approved for the following operations when equipped in
accordance with FAR 91 or FAR 135.
(a) Day V.F.R.
(b) Night V.F.R.
(c) Day I.F.R.
(d) Night I.F.R.
(e) Non Icing
2.21 FUEL LIMITATIONS
(a) Total Capacity 50 U.S. GAL.
(b) Unusable Fuel 2 U.S. GAL.
The unusable fuel for this airplane has
been determined as 1.0 gallon in each
wing in critical flight attitudes.
(c) Usable Fuel 48 U.S. GAL.
The usable fuel in this airplane has been
determined as 24.0 gallons in each wing.
2.15 MANEUVER LIMITS
(a) Normal Category - All acrobatic maneuvers including spins
prohibited.
(b) Utility Category - Approved maneuvers for bank angles exceeding
60°.
Entry Speed
Steep Turns 113 KIAS
Lazy Eights 113 KIAS
Chandelles 113 KIAS
2.17 FLIGHT LOAD FACTORS
Normal Utility
(a) Positive Load Factor (Maximum) 3.8 G 4.4 G
(b) Negative Load Factor (Maximum) No inverted maneuvers
approved
2.19 TYPES OF OPERATION
The airplane is approved for the following operations when equipped in
accordance with FAR 91 or FAR 135.
(a) Day V.F.R.
(b) Night V.F.R.
(c) Day I.F.R.
(d) Night I.F.R.
(e) Non Icing
2.21 FUEL LIMITATIONS
(a) Total Capacity 50 U.S. GAL.
(b) Unusable Fuel 2 U.S. GAL.
The unusable fuel for this airplane has
been determined as 1.0 gallon in each
wing in critical flight attitudes.
(c) Usable Fuel 48 U.S. GAL.
The usable fuel in this airplane has been
determined as 24.0 gallons in each wing.

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