- Holder
- Phillips Aviation Company
- Revision
- 0
- Status
- Current
- Product
- Aircraft · Small Airplane
- Models
- 1
- Registered
- 2 aircraft
The release keeps the latest revision of each data sheet. Model names are as the data sheet lists them.
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Models · 1
| Model | Also known as | Note |
|---|---|---|
| CT-2 |
Airworthiness directives · 0
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STCs approved under this data sheet · 1
What the data sheet saysOCR
This is OCR from the scanned FAA data sheet. OCR can misread letters and numbers.
MODEIS: Phillips CT-2, 2 POLB
1.C. NUMBER: 731
Engine Phillips 333
Placard limits For all operations, 2100 rpm (120 hp)
Propeller Static rpm at maximum permissible throttle setting
- Not more than 1870
- Not less than 1870
Diameter
- Not more than 98 inches
- Not less than 81 inches
Placard speeds Level flight or climb - 125 mph True Ind.
Glide or dive - 154 mph True Ind.
Fuel capacity 20 gallons (2 tanks in upper wing) (-8.5)
oil capacity 2 gallons
No. passengers 1 (+7) or (+36.5) (See NOTE 2)
Eaggage
Standard weight
C.G. range (26.2 percent MAC) to (-0.5) (30.4 percent MAC)
MAC 44 in. L.E. MAC (-13.81)
Leveling means Raise tail until top longeron in rear cockpit is level
specification basis Type Certiricate No.
Serial numbers 101 and up eligible (See NOTE A)
EQUIPMENT: (Datum is lower wing leading edge)
Class I:
101- Propeller - wood (fixed pitch) with hub 25 lbs. (-83)
102. 6.00-6 wheels (Hayes 600M) with brakes
and 4-ply tires 28 1bs. (-20)
103- Steerable tail wheel and tire (Drawing
No. 5340) 5 lbs. (+163)
104. Oil cooler (Flexo Manufacturing Company
Drawing No. 537) 5 lbs. -41
105. Carburetor air heater (Drawing No. 5592) 1-71
106. Battery (Burgess Uniplex 6V)
(See NOTE 3) 15 Ibs. (-35)
Class II:
Miscellaneous items as listed under
this number in approved weight and
balance report.
Class III:
None
NOTE A. Prior to original certification, each aircraft must satisfactorily
pass:
(a) An inspection for workmanship, materials and conformity before any
covering, metal priming or final finish is applied. All woodwork
may be varnished.
A final inspection of the completed aircraft.
Check of flight characteristics.
NOTE 1. Eligible for export as follows, subject to inspection for equipment
specified in Chapter XII of Inspection Handbook:
Canada
- Landplane
- skiplane - not eligible.
(b) All other countries except Australia, Great Britain and New Zealand.
NOTE 2. Placard front cockpit, "Solo flying from rear seat only."
NOTE 3. Battery is required for balance only. It may be removed subject to
a check of C.G. range.
NOTE 4. Placard rear cockpit, "Fasten seat belt in empty seat before take-off."
NOTE 5. Aircraft Operation Record for Serial No. 101 must include the following placard: "Intentional Spinning Prohibited. '
NOTE 6. Eligible for certification with hatch enclosure as designation 2 PCLB
when revised tail surfaces and tail cone are installed in accordance with
manufacturer's drawing p-1000. Elevator tab area slso should be increased by 5 square inches.
Standard weight 1512 1bs.
C.G. range (-1.13) (28.8 percent MAC) to (+0.12) (31.7 percent MAC)