Our Piper PA28-180 Cherokee
G-AYAB
The Piper PA28 is a four seat light aircraft.
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ICAO Designator: P28A Built: 1970 (Part 21 / UK Certificate of Airworthiness)
Engine: Lycoming O-360-A4A (180 hp @ 2,700 rpm)
Max Take Off Weight: 2,400 lbs [1,089 kg]
Empty Weight: 1,470 lbs [667 kg] (weighing report 4 Nov 25)
Full Fuel (100LL): 50 USG [189 Ltrs] = 300 lbs [136 kg]
Oil Capacity (15W50): 8 US Qts [7.6 Ltrs] (normally between 5 & 6 US Qts)
“Tabs” Fuel: 36 USG [136 Ltrs] = 216 lbs [98 kg]
“Tabs” Fuel: 3½+ Hours Endurance (35 Ltrs / Hour for Planning Purposes)
Cruise Power: 2,300 rpm (100 kts IAS for Planning Purposes)
Fuel “At Tabs”: Allows 714 lbs [324 kg] available for Occupants/Baggage. (To keep within MTOW)
Full Fuel: Allows 630 lbs (286 kg) available for Occupants/Baggage. (To keep within MTOW)
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Take Off Run Required (TORR) - Flaps Two Stages 720 ft [220 m]
Take Off Distance Required to 50 ft (TODR) - Flaps Two Stages 1,625 ft [495 m]
Rotate (Normal Take Off) 50 - 60 mph [say 50 kts]
Best Angle of Climb (VX) - All Flap Settings 74 mph [say 65 kts]
Best Rate of Climb (VY) - All Flap Settings 85 mph [say 75 kts]
Landing Run Required (LRR) - Full Flap 600 ft [183 m]
Landing Distance Required from 50 ft (LDR) - Full Flap 1,150 ft [350 m]
Stall Speed - Flaps Up 67 mph [58 kts]
Stall Speed - Full Flap 57 mph [50 kts]
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MTOW, Sea Level, NIL Wind, Level/Paved Runway: TODR = 495 m
+20% Dry/Short Grass, +10% Uphill Slope, x 1.33 CAA Safety Factor = 870 m.
(Hot & High: +10% 1,000 ft Airport Elevation, +20% ISA + 20°C = 1,150m)
MTOW, Sea Level, NIL Wind, Level/Paved Runway: TORR = 220 m
+20% Dry/Short Grass, +10% Uphill Slope, x 1.33 CAA Safety Factor = 390 m.
(Hot & High: +10% 1,000ft Elevation, +20% ISA + 20°C = 515m)
Notes:
• “CAA Safety Factor” mitigates against POH figures being “over optimistic”.
• The POH provides no data for “Flaps Up” Take-Off.
• Full Weight and Balance calculations need to be considered.
Fuel “At Tabs”, plus 2 x 90 kg (2 x 200 lbs) Adults, No Baggage, equates to TOW 2,086 lbs
(945 kg) - circa 87% of MTOW = Possible Reduction of: TODR by 20% and LDR by 10%.
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