- Holder
- Fairchild Industries Inc.
- Revision
- 0
- Status
- Current
- Product
- Aircraft · Small Airplane
- Models
- 3
- Registered
- 5 aircraft
The release keeps the latest revision of each data sheet. Model names are as the data sheet lists them.
On this page
Models · 3
| Model | Also known as | Note |
|---|---|---|
| 22 C7AS | ||
| 22 C7A | ||
| 22 C7AM |
Airworthiness directives · 1
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 · 4
STC SA04652CHTo allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specificationSTC SA01406NYInstallation of Airwolf remote mounted engine oil filter kit AFC-K017 on single and multi-engine fixed light aircraft and
rotary wingSTC SA01734SEApplication of Stewart Systems synthetic fabric covering system to aircraft fuselage, wings, tail surfaces, control surfaces and related parts.STC SA02033ATModification to install an air-oil separator to prevent oil from being aspirated from the engine breather line.
What the data sheet saysOCR
This is OCR from the scanned FAA data sheet. OCR can misread letters and numbers.
MODELS: Fairchild 22, C7A, C7AM, CIAS, 2 POL-SM
I.C. NUMBER: ATC 438
(For Model C7AM, See NOTE 4.)
I - Specifications Pertinent to All Models:
Engine American Cirrus Hi-Drive Mark III 95 hp
Fuel 3-1/2 gallons in fuselage)
Oil
No. passengers
Spec. basis Approved Type Certificate No. 438
Serial Nos. 5061igible. 511. 1001 and up manufactured prior to 7/1/35
Approval expired as of that date.
(See NOTE 4.)
Class I equipment:
Landplane
101. 6.50-10 wheels and brakes (Warner)
102. Tail skid
103. Propeller - wood
Seaplane
151. Edo I-1835 floats
152. Propeller - ajd. metal
153. Battery 10 1bs.
154. Starter (Eclipse hand inertia) › 1hs.
155. Position lights
*ass III equipment: (* Denotes net increase.) Landplane
Cast aluminum alloy rudder and brake
pedals
302. Fairchild shock absorber strut No. 3340
instead of Warner strut
303. 19x9-3 tires Net decrease 11 1bs.
304. Sport type landing gear with
(a) 6.50-10 tires 14 lbs.*
(b) 19x9-3 tires No change in weight
306- 305. 8x4 tail wheel Propeller - adj. metal (Goodyear) 13 1bs. *
307. Sparter (Inertia) ? ibs.
308. Battery (Hot shot) 10 1hs.
309. Starter and battery installation
(baggage to be reduced 30 Ibs.) 50 1bs.
Net decrease 13 1bs.
Aircraft with two piece wing or continuous spar type are eligible.
old type aileron hinges without ball bearings
also eligible with the hinges reamed out and 5/16 in. bolts installed
instead of 1/4 in. bolts.
NOTE 2. Stor should specifyear instal strut fairing and wheel streamlines.
Inspector should specify
NOTE 3.
rear stabilizer attachment fitting is revised to raise hinge
Distance from center line of longeron to center of hole in fitting is
1-7/16 inch.
(remodeled by Al Lary) is eligible as Model C7AM
POLM) with the following:
Placard limits laximum except takeoff - in. Hg., 2200 rpm (95 hp)
akeoff (one minute) - in. Hy. 2200 Ipm (95 hp)
Placard speeds Level flight or climb - 101 mph Ind.
Glide or dive - 125 mph Ind.
Propeller Maximum permissible diameter 98 in.
Fuel 21 gallons (in fuselage)
Oil 2-1/2 Jallons (-11.75)
No. passengers
Baggage (in fuselage) (+3.25)
Standard weight
C.G. Limits (*15.45) and (+22.45)
EQUIPMENT: (Datum is leading edge of wing)
101. 19x9-3 wheels.
Wing must be rigged so that wing leading edge is 5-3/4 in. forvard
of chassis arle. Pin (Pairchild Drawing No. 3690) and rudder (Fairchild
Draving No. 3668) must be installed.
II - Model C7A, Designation 2 POLM:
Baggage Porward compartment:
40 1bs. with 1503 lbs. standard weight
50 1bs. with 1550 1bs. standard weight
Pay load includes 2 parachutes 20 1bs. each and
tool roll 10 Ibs.
Standard weight 1503 1bs. (See NOTE 3)
III - Model C7AS, Designation 2 POSM:
Baggage 21 1bs.
Standard weight 1660 1bs.