# TCDS ATC 384: Lockheed Aircraft Corporation

- Type: Type certificate data sheet
- Status: Current
- Holder: Lockheed Aircraft Corporation
- Revision: 0
- Product: Aircraft, Small Airplane
- Registered aircraft: 4, by the registry models matched to it (OpenAirDocs)
- Data sheet PDF: https://openairdocs.org/files/sha256/7a/22/7a228034b2202d9c2c375056711c0b1a98c99961492461e44339452e9a7a087d
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/17E864C8AB88970285256738006D4905.0001
- Page: https://openairdocs.org/tcds/ATC%20384

## Models (1)

As the data sheet lists them.

- Vega 5-C (Army UC-101)

## What the data sheet says

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

```text
MODEIS: Iockheed Vega 5-C (Army UC-101), 7 PCL-SM
I-C. NUMBER: ATC 384
Engine  P&W Wasp C1 402 hp, SC-1 450 hp or S3D1 450 hp
Fuel  96 gallons
cil  10 gallons
No. passengers
Baggage  Landplane 180 lts.
Seaplane  84 1bs.
Maximum weight  Landplane 4500 1bs. (See NOTE 1)
Seaplane 4880 1bs.
C.G. limits  22.2 in. and 36.5 in. aft of wing leading edge
at fuselage
Serial Nos.
Serials below 138 eligible upon
manufacturer's affidavit of conformity.
Class I equipment:
flectric starter; battery; heater; propeller - adj. metal; Fdo k floats
and auxiliary tail fin surface (Seaplane).
Class III equipment:
Engine ring cowl 50 1bs.; wheel streamlines 50 lbs.; landing lights 30 lbs.;
- in baggage compartment 45 lbs.; extra 48 gallon center
radiator 15 1rs.;
tires 25 1bs.; 15 gallon oil tank replacing 10  gallon tank, no change
weight; 300 lb. baggage compartment in center section substituted for center
controllable metal propeller (Hamilton Standard hub S84601,
Flades 6101A-12, low pitch setting  16 degrees) .
NOTE 1.  Landplane standard weight may ke increased to 4750 1bs.  provided the
following changes are made:  (These changes are also required on all
All plywood covering is removed from the top surface of the wings
between spars.
Additional stringers of same size as old stringers are installed
between the present stringers extending between the ribs and parallel
to the present stringers.  The total number of stringers between
each rib will be seven when completed.
The top surface is recovered using 1/8 inch plywood between the
spars and between the No. 10 ribs at
elsewhere should be the same thickness as the present installation.
```

## ADs (1, in force first)

- [AD 93-14-12](https://openairdocs.org/ad/93-14-12): Crewmember Protective Breathing Equipment Units · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 201 more. Effective Sep 2, 1993

## Registered aircraft by registry model (OpenAirDocs)

- [Lockheed VEGA 5C](https://openairdocs.org/model/lockheed-vega-5c): 4 aircraft (registry code 5261202)

## STCs approved under this data sheet (3)

- [STC SA04652CH](https://openairdocs.org/stc/SA04652CH): To allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specification. Swift Fuels LLC
- [STC SA6070NM](https://openairdocs.org/stc/SA6070NM): Installation of a 'quick-disconnect drain plug' on the engine rocker sump for the oil drain retrieval system after engine shutdown.. West Coast Air Creations
- [STC SA01282NY](https://openairdocs.org/stc/SA01282NY): Installation of Airwolf remote mounted engine oil filter kit AFC-K015 on aircraft powered by Pratt & Whitney radial reciprocating engine Series R-985, R-1340 and R-1830.. Airwolf Filter Corporation

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