# TCDS TC 2-546: Pasped Aircraft Corporation

- Type: Type certificate data sheet
- Status: Current
- Holder: Pasped Aircraft Corporation
- Revision: 0
- Product: Aircraft, Small Airplane
- Registered aircraft: 1, by the registry models matched to it (OpenAirDocs)
- Data sheet PDF: https://openairdocs.org/files/sha256/28/7b/287b5fcc5343d9b4fe738e9ab33ef7a9d1a5ee18f5463dd19d6a399890bfd0d7
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/6A4D8F8C55A083F28525673D00465713.0001
- Page: https://openairdocs.org/tcds/TC%202-546

## Models (1)

As the data sheet lists them.

- Skylark W-1

## What the data sheet says

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

```text
PASPED AIRCRAFT CORPORATION
MODELS: Pasped Skylark W-1, 2 PO-C-LM
I.C. NUMBER: 2-546
Engine  Warner Scarab Series 40
Placard limits  Maximum, except take-off
-- in. Ng., 2050 rpm (125 hp)
Take-off (one minute)
-- in.Hg...  2050 Ipm (125 hp)
Propeller  Maximum permissible diameter 9 feet
Placard speeds  Level flight or climb - 130 mph Indicated
Glide or dive - 160 mph Indicated
Flaps extended - 100 mph Ind.
Fuel capacity  31 gallons (1 tank aft firewall) (-1)
cil capacity  3-1/2 gallons  (-20)
No. passengers  1 (+34), pilot (+34)
Baggage  10 1bs.  (compartment aft of cockpit)  (*70)
weights  Empty - Use actual (approximately  1313  Ibs. (+21))
(with Class I items only)
Standard - 1900 1bs.
c.G. limits  (+17.9) and (+22.7)
Specification basis  Aeronautics Bulletin 7A, Section 3
Serial numbers  1 only eligible
EQUIPMENT:  (Datum is wing leading edge) (* Denotes net increase)
Class I:
101.  Propeller - wooden (includes hub)  30 1bs.  (-54)
102.  Engine ring cowl  6 lbs.  (-44)
103.  Exhaust manifold  6 lbs.  (-41)
104-  Standard instruments (airspeed,
altimeter, tachometer, electric fuel
oil temp., oil press  4-1/2 1bs. (+13)
105.  6.50-10 wheels  Autofan F-511) an‹
51 lbs.
106.  Shock struts (Pasped Drawing 16-2)  6 lbs.
107.  8 inch streamline tail wheel  and tire  4 Ibs.  (+213)
108.  Wheel streamlines  19-1/2 1bs. (+17)
109-  Aileron static balance weights and
arms at 4 1bs. each  8 1bs.  (+68)
110.  Elevator tab control unit  (rasped) ,
range up 6 degrees, down 23 degrees  1-1/2 1bs. (+193)
111. Sliding cockpit enclosure  10 1bs.  (+39)
112. Airplane rigging instructions
Class II:
200.  Miscellaneous items as noted in
approved weight and balance report.
Class III:
301.  Starter (Eclipse Y-150)  20 lbs.  (-34)
302.  Battery (6 volt) and box  22 1bs.  (-12)
303. Optional instruments (compass, rate of
climb, clock, turn and bank indicator,
head temperature indicator)  5 lts.  (+13)
304. Parachutes (2 at 20 1bs.)  40 lbs.  (+34)
Eligible for export as follows,  subject to inspection for equipment
specified in Chapter XII of Inspection Handbook (8/6/38):
Canada
- Landplane
- Skiplane - not eligible.
(b)  All other countries except Great Britain and Australia.
```

## ADs

None name its models.

## Registered aircraft by registry model (OpenAirDocs)

- [Pasped SKYLARK W1](https://openairdocs.org/model/pasped-skylark-w1): 1 aircraft (registry code 6790102)

## 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 SA4503NM](https://openairdocs.org/stc/SA4503NM): Remove original cloth covering and install Ceconite covering. Ceconite Division of Poly-Fiber Inc.
- [STC SA01734SE](https://openairdocs.org/stc/SA01734SE): Application of Stewart Systems synthetic fabric covering system to aircraft fuselage, wings, tail surfaces, control surfaces and related parts.. Andrew D. Humphrey

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