# TCDS E-288: Fairchild Engine Division Fairchild Engine and Airplane Corp.

- Type: Type certificate data sheet
- Status: Current
- Holder: Fairchild Engine Division Fairchild Engine and Airplane Corp.
- Revision: 1
- Revised: May 1, 1956
- Product: Engine
- Data sheet PDF: https://openairdocs.org/files/sha256/e7/d9/e7d99a342cabe191eca44f19c690ca67ecac75e570081d154a1583f20635c9ad
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/A9F8937E10164A0D8525670C00525740.0001
- Page: https://openairdocs.org/tcds/E-288

## Models (1)

As the data sheet lists them.

- FT-101E

## What the data sheet says

From the PDF's text layer, line by line; tables lose their columns. The PDF is the record.

```text
Page No. 1 2
Rev. No. 1 1
DEPARTMENT OF COMMERCE
CIVIL AERONAUTICS ADMINISTRATION
E-288
Revision 1
FAIRCHILD
FT-101E
May 1, 1956
AIRCRAFT ENGINE SPECIFICATION
Engines of models described herein conforming with this specification and approved data on file with the Civil Aeronautics
Administration are rated as airworthy for use in certificated aircraft in accordance with pertinent aircraft specifications and the
manufacturer's installation, operation, repair and overhaul instructions.
Manufacturer Fairchild Engine Division
Fairchild Engine and Airplane Corporation
Deer Park, New York
Model FT-101E
Type  -  Turbojet Single-stage, mixed flow compressor
Single-stage, axial flow turbine
1 annular combustion chamber
Ratings
Maximum continuous static thrust, lbs., rpm, altitude 900-15,100-S.L.
Takeoff static thrust (5 minutes), lbs., rpm, altitude 1000-15,780-S.L.
Fuel control Woodward type 1374
Fuel (MIL-F-5572) Aviation Gasoline
Oil (MIL-L-7808A) Esso Turbo 15
Accessory housing oil capacity, pts. .75
Engine oil mist lubricator capacity, pts. .85
Principal Dimensions
Length overall, in. 90.4
Diameter, in. 24.3
Weight (dry), lbs. 380
Center of gravity, in. aft of trunnion 10.5
Ignition General Laboratories type 19800 with two igniters and a
dual ignition coil
Certification basis Type Certificate No. 288
Production basis Pending
NOTE 1. Maximum permissible temperatures are as follows:
Turbine outlet gas temperatures,
Takeoff, 1325°F
Maximum continuous, 1290°F
Transient, 1440°F for three seconds maximum.
Bearing temperatures (recommended limits)
Turbine bearing outer race, 300°F
Compressor bearing outer race, 150°F
NOTE 2. Fuel pump inlet pressure limits:
Minimum at pump inlet, 15 psia
Operating gage pressures, 14 to 50 psi
"psi"  = lbs./sq.in.
"psia"  =  lbs./sq.in. absolute.

E-288 2
NOTE 3. These ratings are based upon the following conditions:
Compressor inlet air, 59°F and 29.92 in.Hg. dry
Jet nozzle area, 118 sq.in.
Turbine outlet gas temperature, 1220°F
No turbine air bleed
NOTE 4. Oil supply level in both the accessory drive section and the oil mist lubricator must be checked frequently
when on the ground, to insure an adequate quantity since no provision is made for indicating oil pressure,
or temperature or quantity while in operation.
NOTE 5. The following accessory drive provisions are available:
Speed Ratio
to Torque (in.lb.) Overhang
Drive Rotation* Turbine Shaft Continuous Static (in.lb.)
Tachometer C .269 15 70 10.7
Fuel pump C .227 50 600 134.0
Starter CC .440 500 2200 187.0
  *C-Clockwise
**CC-Counter Clockwise
NOTE 6. The following accessories are provided with the engine at weight increase indicated:
Accessory Weight
Tachometer Generator   2 lbs.
*Starter (Jack & Heintz  - D62) 25 lbs.
*Starter (Jack & Heintz - D62-1) 22 lbs.
Power control actuator   2 lbs.
Accessory section fairing   5 lbs.
Electrical conduit   5 lbs.
*Optional
NOTE 7. This engine has no provision for anti-icing the inlet and has not been tested to determine the extent to
which flights in icing weather will adversely affect engine output.
.....END.....
```

## ADs

None name its models.

## Registered aircraft by registry model (OpenAirDocs)

- [Fairchild FT-101E](https://openairdocs.org/engine/fairchild-ft-101e): 0 aircraft (registry code 26010)

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