# TCDS ATC 680: Kaiser Fleetwings Inc.

- Type: Type certificate data sheet
- Status: Current
- Holder: Kaiser Fleetwings Inc.
- 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/af/d9/afd9ed28ead97ecee3e4eeb2dccab2e09eb48e5487960d6a1a7021a50e60d7b7
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/47A433E6DF177148852567380062AD5D.0001
- Page: https://openairdocs.org/tcds/ATC%20680

## Models (1)

As the data sheet lists them.

- F-5

## What the data sheet says

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

```text
KAISER FLEETWINGS& INC-
MODELS: Kaiser Fleetwings F-5, 4-5 PCAm
I.C. NUMBER: ATC 680
Engine  Jacobs L-5 (See Item 201)
Placard limits  Tavel fight at timo - 760 ph true tha.  except takeoff - in. Hg., 2000 rpm  (285 hp)
(See NOTE  3)  (285 hp)
Placard speeds
Glide or dive - 185 mph True Ind.
Flaps extended - 108 mph True Ind.
Fuel capacity  70 gallons (one 35 gallon tank in each wing) (+29)
oil capacity  5 gallons (*5)
No. passengers  3-4  (-7.5) and (+35) (See Item 305)
Baggage  Forward compartment  76 Ibs. (-64) (includes tools
and engine covers when carried)
Aft compartment 55 1bs.  (+65)  (may be increased to
150 1bs. when substantiated by weight and balance
report)
Standard weight  3800 1bs. (See NOTE 2)
C.G. limits
Spec.  basis  Approved Type Certificate No. 680
Serial Nos.  F-501 and up manufactured prior to 2/19/81 eligible.
Approval expired as of that date.
EQUIPMENT:
(Datum is wing leading edge) (* Means net increase)
Propeller - fixed metal  (-42)
7.50-10 wheels (Hayes 750A) with 6-ply
tires (Wheels must be placarded for
these tires.)  (+4)
10.5 in. streamline tail wheel with
(+126)
Battery (Reading ARL9)  (+11)
Generator and control box (Eclipse
(-8)
Engine driven hydraulic pump (Eclipse
Landing lights (Grimes GT-1000)
Starter (Eclipse  (-13)
Anchor and line  (-82)
(+33)
111. Cabin and carburetor heater
Class II:
200.  Miscellaneous items as noted in approved
weight and balance  report
201. Engine - Jacobs 1-51B with revised
engine mount  15 1bB.*
30 lbs.  (-38)
controllable metal propeller
(Hamilton Standard hub 2B30,
6109A) (low pitch setting 13
baggage must be
51 lbs.*  (-42)
Constant speed accessories for (a)  1bs.
Puncture proof tubes  16 1bs.
Battery (Reading R-40-1)  12 1bs.  (+11)
Auxiliary seat (required for 5-place
7. 1bs.  (+35)
306. Heater (including blower)  2 lbs.*
NOTE 1.  Eligible for export to all countries except Canada, australia anc
Great Britain (7/5/40).
NOTE 2. Eligible at 3850 1bs. standard weight when Item 302(a)  is installed.
Aircraft equipzed with e 9219,  serial Nos
1181, 1206,  and 1271 eligible with
the following placard limits:
except takeoff - in. Hg..
(one minute) - in. Hg., 2125 rpm
```

## ADs (1, in force first)

- [AD 49-32-01](https://openairdocs.org/ad/49-32-01): Engine Support Struts · Kaiser Fleetwings F-401 and F-5

## Registered aircraft by registry model (OpenAirDocs)

- [Kaiser F5](https://openairdocs.org/model/kaiser-f5): 1 aircraft (registry code 4762002)

## STCs approved under this data sheet (5)

- [STC SA04652CH](https://openairdocs.org/stc/SA04652CH): To allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specification. Swift Fuels LLC
- [STC SA01757WI](https://openairdocs.org/stc/SA01757WI): To allow the use of UL91 or UL94 (minimum) grade aviation fuel. Swift Fuels LLC
- [STC SA01831WI](https://openairdocs.org/stc/SA01831WI): To allow the use of UL91 (minimum) grade aviation fuel. Petersen Aviation Inc
- [STC SA00478CH](https://openairdocs.org/stc/SA00478CH): Installation of Cooper Superflite 102 Fabric.. Aviation Products Systems Inc.
- [STC SA3012SO](https://openairdocs.org/stc/SA3012SO): Installation of a Jacobs R-755 A-2 engine and a Hamilton Standard2B20-9-6135A propeller.. Edward Blake Oliver

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