- Holder
- The Waco Aircraft Company
- Revision
- 0
- Status
- Current
- Product
- Aircraft · Small Airplane
- Models
- 2
- 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 · 2
| Model | Also known as | Note |
|---|---|---|
| AGC-8 | ||
| ZGC-8 |
Airworthiness directives · 0
ADs whose products are models on this data sheet, matched by model and maker.
No ADs matched this data sheet’s models
Registered aircraft
Registry models that point at this data sheet, with their registered aircraft.
STCs approved under this data sheet · 9
STC SA04652CHTo allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specificationSTC SA01757WITo allow the use of UL91 or UL94 (minimum) grade aviation fuelSTC SA01831WITo allow the use of UL91 (minimum) grade aviation fuelSTC SA01406NYInstallation of Airwolf remote mounted engine oil filter kit AFC-K017 on single and multi-engine fixed light aircraft and
rotary wingSTC SA2693NMInstallation of Electronics International digital volt/amp gauges and accessories.STC SA02033ATModification to install an air-oil separator to prevent oil from being aspirated from the engine breather line.STC SA2350NM PAGE 2Installation of Electronics International Inc digital carburetor/outside air temperature gaugesSTC SA2190NM PAGE 2Installation of electronics International Digital Volt/Amp Gauges and Accessories.STC SA2350NMInstallation of Electronics International Inc digital carburetor/outside air temperature gauges listed on the attached continuation sheet and the associated accessories.
What the data sheet saysOCR
This is OCR from the scanned FAA data sheet. OCR can misread letters and numbers.
MODEIS: waco AGC-8 and ZGC-8
I.C. NUMEER: 664
I - SPECIFICATIONS PERTINENT TO ALL MODELS
Propeller Permissible diameter:
ximum 103 inches, minimum 99 inche‹
Placard speeds evel flight or climb - 158 mch True Ind.
Glide or dive - 213 mph True Ind.
Flaps extended - 100 mph True Ind.
Fuel capacity 70 gallons (2 tanks, one in each wing at 35 gallons)
(-14)
Cil capacity 5 gallons (-50)
No. passengers 4 (front -13, rear +22)
Paggage (Passenger type) 100 1bs. (+52)
(Cargo type) (See Item 211)
Standard weight 3800
C.G. limits (-19.2) and (-7.2)
Catum Lower wing leading edge
Leveling means Lower surface upper wing at strut point
Specification basis Type Certificate No. 664
EQUIPMENT:
(* Means net increase)
class I:
101. Engine ring cowl
(ZGC-8) 29 Its. (-77)
(AGC-8) 33 1bs. (-77)
102. Landing lights (Grimes retractable) 11 Its. (-23)
103- Starter (direct electric) 20 1bs. (-55)
104. Generator - 15 amp. 21 1bs. (-55)
105. Battery (Exide 6TS-13-1) 42 ibs. (-59)
106. Wheel cuffs 4 1bs.
107. 7.50-10 wheels (Hayes 750M hydraulic)
with 7.50-10 tubes and 8.50-10 tires)
(wheels must be placarded for these
108.
tire
(wheels must be placarded accordingly)
109. Throw-over type control column
110- Standard paint (gunmetal gray)
111. Oil cooler (Drawing 20965) 5 1bs. (-71)
112. Heater and ventilator (cabin)
113. Propeller - fixed metal
(Curtiss-Reed 55501) 55 lbs. (-92)
Class II:
200. Miscellaneous items as noted in
approved weight and balance report.
201. Additional 25 gallon fuel tank
installed under rear seat (including
gage and wobble pump) (Eligible as
4-place type only.) 23 1bs. (+9)
202. 7-1/2 gallon oil capacity (-50)
Leather upholstery 12 ibs. (0)
Air Corps type 25 1bs. (+72)
Precision (carried in baggage
25 lbs.
Parachute seats - rear 41 1bs.* (+27)
Extra door and wing walk 16 1bs.* (+19)
(-55)
Larger battery (Reading AR-9) 8 1bs-" (-59)
Larger starter (EClipse F-141) 10 1bs.* (-55)
And (nataLiation de between 1-22)
Cargo type with cargo compartment and
Large Daggage door (See NOTE 2)
212. Engines Use actual weight increase
(a) JacODS 1-5B Or 1-5ME
(b) Jacobs L-6B or L-6M
32 lbs. provided c.G. of instal-
lation is between (-28) and (+25)
Special paint Махітт 45 1bs• (-43) (*17)
Miscellaneous extra instruments 40 1bs.*
Pressure fire extinguisher
15 1bs. -53
(D) 19 Ibs. * 7
(Tank under rear seat)
305. Tail wheel lock Neglect weight increase
306- Flares (three 1-1/2 minute electric) 17 1bs. * (+78)
307. Parachute seats - front (Waco-Switlik) 30 1bs.* (-13)
308. "y" type control column 4 lbs.* (-33)
309- Cactus proof tubes 12 1bs. * (-27)
310. Shielding (Breeze) 11 1bs. (-68)
311. Vacuum pump 4 ibs. (-53)
312. 95 gallon fuel capacity (two tanks
at 47-1/2 gallons) 18 Its. * (-14)
313. 6 gallon oil tank No weight increase (-50)
314. Wheel pants 22 1bs. (-27)
315. Propeller - controllable metal
(Hamilton Standard hub 2B20, Llades
6109A or 6135A) 104 1bs. (-92)
NOTE 1. specified in Chapter Eligible for export as follows XII of Inspection Handbook: (5/31/41) subject to inspection for equipment
Canada
- Landplane
Skiplane - not eligible
(r) All other countries except New Zealand.
NOTE 2. Weight and balance report including list of equipment included in
certificated weight empty, and loading instructions when necessary, must
and each subsequent report covering changes in such equipment. be submitted for each cargo type aircraft with original inspector's report
II - MODEL AGC-8, DESIGNATION 5 PCLE
Engine
Placard limits Maximum, except take-off
-- in. Ng., 2000 rpm (295 hp)
-- in. Hg.. 2000 rpm (285 hp)
Serial numbers 5001 and up manufacturei prior to 2/28/41 eligible.
Approval expired as of that date.
III - MODEL AGC-8, DESIGNATION 5 PCIB
Engine
Placard limits Maximum, except take-oif
24.5 3.5 in:Hg., 2100 rpm (300 hp) 2100 pm (300 hp)
Take of tone in (one minute)
Serial numbers 26 in. Hg.. 2200 rpm (330 hp) up manufactured prior to 2/28/41 eligible.
Approval expired as of that date. (5001 to 5056
eligible when changed to conform.)