- Holder
- Bellanca Aircraft Corporation
- Revision
- 0
- Status
- Current
- Product
- Aircraft · Small Airplane
- Models
- 1
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 |
|---|---|---|
| Pacemaker 31-42 | Formerly Aeronca, Inc., American Champion |
Airworthiness directives · 0
ADs whose products are models on this data sheet, matched by model and maker.
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STCs approved under this data sheet · 3
What the data sheet saysOCR
This is OCR from the scanned FAA data sheet. OCR can misread letters and numbers.
MODELS: Bellanca Pacemaker 31-42, 1 or 8 PCLM
I.C. NUMBER: 578
Engine Wright R975E-2 (See also Item 201)
placard limits except take-off -- in. Ho.. 2150 rpm
(one minute) -- in. Hg.. 2150 rpm (420 hp)
Placard speeds Level flight or climb - 160 mph True Ind.
Glide or dive - 198 mph True
Fuel 200 gallons (two tanks in wings at 100 gallons
each - right wing tank has built-in reserve tank
of 12 gallon capacity)
Oil 12-1/2 gallons
NO. passengers
Baggage Provision in fuselage bays 1, 2 and 3 (numbered
front to rear)
(a} Passenger type 1st bay 25 1hs.
(b) Cargo type Ist bay (1375 * 25) 1400 1bs.
Cargo type 2nd bay 400 1bs.
Cargo type 3rd bay 200 1bs.
Standard weight 5600 1bs.
C.G. limits (+11.8) and (+24.5)
Spec. basis Type Certificate No. 578 (Aero. Bulletin 7A
reguirements)
Serial Nos. 251 and p eligible per NOTE A.
(See also NOTES 2 and 3.)
EQUIPMENT: (Datum is wing leading care) (*Means net increase)
Class I:
101- Engine ring cowl 30 1bs.
102. Battery (under cabin floor) 40 1bs.
103. 20 1bs.
104. Generator 20 lbs.
105. Throw-over type control column
106- 31 in. streamline wheels
107. 5.00-4 tail wheel
108- Propeller - controllable metal
(Hamilton Standard 2D30 with blades
6101A-10)
Class II:
200- Miscellaneous items as noted in approved
weight and balance report
201. Wright R975E-3
Placard limits - Maximum, except take-
off 34-1/2 in. Hg.. Ipm (420 hp) :
Take-oft (one minute) 35 in. Hg., 2200
rpm (420 hp)
NOTE A. original certification vorkmanship. Each aircraft manufactured after July 18, 1941 must, prior to satisfactorily pass:
covering, metal priming or final finish is applied. An inspection for materials and conformity before any All woodwork
must be varnished.
A final inspection of the completed aircraft.
(c) A check of flight characteristics.
Eligible for export as follows subject to inspection for equipment
specified in Chapter XII of Inspection Handbook (12/12/41):
- Skiplane - not eligible. However, structure complies with Canadian
requirements for ski installation
(b) All other countries except Great Britain, Australia and New Zealand.
Serial No. 252 with Skyrocket F type ailerons, benches, replaced by
seats and fuselage same as Skyrocket 31-50 except engine mount is eligible
as 6 PCIM with the following:
No. passengers
150 1bs. (two compartments - 110 Ibs. forward in
cabin and 40 1bs. aft or rear seats)
Class I equipment: 106, 107, 109 PLUS:
16 1bs.; starter 32 1bs.; heater 20 lbs.; toilet
equipment 7 1hs.
Serial Nos. 253 is eligible as 6 PCIM with item 201 and the following:
6 (2 on rear seat in cabin; 3 on forward seats in
cabin one of which is folding type; 1 in pilot's
compartment)
(compartment in bottom in fuselage)
Class I equipment: Items 101 thru 107 PLUS: Propeller controllable
metal (Hamilton Standard hub 2D30-15 and blades
6101-12); landing lights 8 1bs.; heater; flares
15 1bs.; radio bonding and shielding 20 lbs.