# TCDS TC 731: Phillips Aviation Company

- Type: Type certificate data sheet
- Status: Current
- Holder: Phillips Aviation Company
- Revision: 0
- Product: Aircraft, Small Airplane
- Registered aircraft: 2, by the registry models matched to it (OpenAirDocs)
- Data sheet PDF: https://openairdocs.org/files/sha256/4a/3b/4a3b6e0e5ed3e9a309ace291df254f5fba78253208c217990b77e7e36f6311ba
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/32ADB25E48970A828625717E00716F7A.0001
- Page: https://openairdocs.org/tcds/TC%20731

## Models (1)

As the data sheet lists them.

- CT-2

## What the data sheet says

This is OCR from the scanned FAA data sheet. OCR can misread letters and numbers.

```text
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)
```

## ADs

None name its models.

## Registered aircraft by registry model (OpenAirDocs)

- [Phillips CT-2](https://openairdocs.org/model/phillips-ct-2): 2 aircraft (registry code 6930102)

## STCs approved under this data sheet (1)

- [STC SA04652CH](https://openairdocs.org/stc/SA04652CH): To allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specification. Swift Fuels LLC

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.