- Holder
- Bellanca Aircraft Corporation
- Revision
- 0
- Status
- Current
- Product
- Aircraft · Small Airplane
- Models
- 1
- Registered
- 2 aircraft
The release keeps the latest revision of each data sheet. Model names are as the data sheet lists them.
On this page
Models · 1
| Model | Also known as | Note |
|---|---|---|
| CH-300 Pacemaker | Formerly Aeronca, American Champion |
Airworthiness directives · 3
ADs whose products are models on this data sheet, matched by model and maker.
Registered aircraft
Registry models that point at this data sheet, with their registered aircraft.
STCs approved under this data sheet · 7
STC SA04652CHTo allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specificationSTC SA4503NMRemove original cloth covering and install Ceconite coveringSTC SA02825NY PAGE 1Installation of Aerospace Logic Aircraft InstrumentsSTC SA4005NMPrecise Flight Inc. Pulselite Control SystemSTC SA01158WIInstallation of Aero Enhancements UV250-1 Supplemental Instrument Panel Lightning System.STC SA931NWInstallation of Hayes Industries tapered axles to accommodate Hayes 27 inch wheel assemblies (PN G31A), Hayes 11 x 2 brake assembly (PN H-12-19), Warner Aircraft brake master cylinders (PN 3150-5) and associated tires and plumbingSTC SA4-320Installation of Edo 6470 Floats
What the data sheet saysOCR
This is OCR from the scanned FAA data sheet. OCR can misread letters and numbers.
MODELS: Bellanca CH-300 Pacemaker, 6 PCI-SM
T.C. NUMBER: ATC 129
Engine Wright R-975 330 hp
Fuel 86 gallons
011 6 Or 7 gallons
No. passengers
Baggage
Standard weight Landplane 4075 1bs. (See NOTE 1)
4610 1bs. (See Class III equipment)
Spec. basis Approved Type Certificate
Serial Nos. Landplane - 119, 125, 128, 130 to 203 eligible
148 to 203 eligible
Approval for both expired 7/1/32.
Class I equipment:
(Seaplane) Edo K floats, anchor and rope, 25 1bs.
Class III equipment (* Means net increase):
108 gallon fuel capacity (2 additional tanks 11 gallons each, 14 1bs.*) -
maximum weight 4221 lbs. (land) and 4756 lbs. (sea); 112 gallons fuel
capacity (2 tanks: 1 in each wing at 56 gallons - right wing tank has
8 gallon auriliary compartment with separate filler cap) - maximum weight
4300 1bs. (land) and 4835 1bs. (sea); engine ring cowl 15 1bs.; wheel
Shoes absorbing taii Sheet With necessar! battery; flares; landing lights; change in bottom of rudder
clearance (serials 147, 149, 10ibs.*: skis; dammer 4500,*star Air
Xa-5400 floats with water rudders
Service 4500, McGee Sr. S.
NOTE 1. Landplane standard weight may be increased to 4300 1bs. provided
in empty weight is not due to concentrated loads capable of
altering flight characteristics.