DEPARTMENT
OF COMMERCE
CIVIL AERONAUTICS ADMINISTRATION
A-766
Revision 15
Click above for .pdf file of latest revision via FAA website.
A-776
Revision 14
GLOBE
GC-1A
GC-1B
DECEMBER 4, 2003
AIRCRAFT SPECIFICATION NO. A-766
Holder of Type Certificate:
Swift Museum Foundation, Inc.
P.O. Box 644
Athens, Tennessee 74114 TYPE
CERTIFICATE DATE SHEET NO. A-766 Type
Certificate Holder:
Swift Museum Foundation, Inc.
P.O. Box 644
Athens, Tennessee 74114
I - Model GC-1A, 2 PCLM,
Approved May 7, 1946
Engine Continental, C-85-12
or C-85-12F
Fuel 73 min. octane aviation gasoline
Engine limits For all operations, 2575 rpm (85 hp)
Airspeed limits Level flight or climb 140 mph (122 knots)
True Ind.
Glide or dive 185 mph (161 knots) True Ind.
Flaps extended 90 mph ( 78 knots) True Ind.
C.G. Range (+31.4) to (+35.5) with L.G. extended.
Moment change due to retraction of gear +157 in. lbs.
Empty weight C.G. range (+29.3) to (+30.4)
If empty weight C.G. falls within pertinent range, it is unnecessary
to check critical forward and aft C.G. positions. Ranges are
not valid for non-standard arrangements.
Maximum weight 1570 lbs.
No. seats 2 (+42.5)\
Maximum baggage 50 lbs. (+60.5)
Fuel capacity 27.8 gals. (+47)
Oil capacity 4.5 qts. (-14.5)
Control
surface movements |
Flaps |
|
|
Down |
39°
or 30° |
|
Elevators
Up 22° |
Down
20° |
|
|
|
|
Elevator
trim tab |
Up |
23° |
Down |
17° |
|
Ailerons
Up 19.5° |
Down
15° |
|
|
|
|
Rudder
Right 24° |
Left
26° |
|
|
|
Serial Nos. eligible 2 to 1000,
inclusive (also eligible as GC-1B upon completion of conversion
according to TEMCO Customer Service Maintenance
Bulletin No. 27, dated June 18, 1948.)
Required equipment In addition to the pertinent required basic
equipment specified in CAR 4a, the following items of equipment
must be installed: Items 1, 101; 105 or 110 and111; 201, 202,
301, 302, and 303.Page No. 1 2 3 4 5 Rev. No. 14 11 11 14
13 A-766 Page 2 of 5
II - Model GC-1B, 2PCLM, approved September 20, 1946
Engine Continental C-125-1 or C-125-2
Fuel 80 min. octane aviation gasoline
Engine limits For all operations, 2550 rpm (125 hp)
Airspeed limits Level flight or climb 140 mph (122 knots)
True Ind.
Glide or dive 185 mph (161 knots) True Ind.
Flaps extended 90 mph ( 78 knots) True Ind.
C.G. Range (+29.6) to (+34.7) with L.G. extended.
(Moment change due to retraction of gear +157 in. lbs.)
Empty weight C.G. range None
Maximum weight 1710 lbs.
No. of seats 2 (+42.5)
Maximum baggage 100 lbs. (+60.5)
Fuel capacity 27.8 gals. (+47)
Oil capacity 2 gals. (-20.3)
Control
surface movements |
Flaps |
|
|
Down |
30° |
|
Elevators
Up 24° |
Down
18.5° |
|
|
|
|
Elevator
trim tab |
Up |
10° |
Down |
22° |
|
Ailerons
Up 19.5° |
Down
16° |
|
|
|
|
Rudder
Right 24° |
Left
26° |
|
|
|
Serial Nos. eligible 1001 and
up. (GC-1A, serial numbers 2 to 1000 inclusive are eligible
as GC-1B upon completion of conversion
according to TEMCO Customer Service Maintenance Bulletin
No. 27, dated June 18, 1948.)
Required equipment In addition to the pertinent required basic
equipment specified in CAR 4a, the followingitems of equipment
must be installed: Items 3, 107, 110, 111, 201, 202, 301,
302, and 303.
Specifications Pertinent to All Models
Datum Forward face of firewall at bottom
Leveling means Window sill between (+37) and (+62)
Certification basis Type Certificate No. 766 (CAR 4a)
Production basis None. Prior to original certification a CAA
agent must perform a detailed inspection for workmanship,
materials, and conformity with the approved technical data
and a check of the flight characteristics.
Export eligibility Eligible for export to all countries subject
to the provisions of MOP 2-4, except as follows:
Canada - Landplane - eligible.- Ski plane - not eligible.
Equipment: A plus (+) or minus (-) sign preceding the weight
of an optional item indicates the net weight change when that
item is installed.
Approval for the installation of all items of equipment listed
herein has been obtained by the aircraft
manufacturer except those items preceded by an asterisk (*).
The asterisk denotes that approval has
been obtained by someone other than the aircraft manufacturer.
An item marked with an asterisk may not have been manufactured
under a CAA monitored or approved quality control
system, and therefore attention should be paid to workmanship
and conformity with pertinent data called for in this specification.
Propellers and Propeller Accessories GC-1A
GC-1B
1 Propeller - Beech controllable,
R002 or R003 with R002-205-72, R003-230-72
or R003-235-72 blades. 30 lbs. (-35) - - - - - Dia.
72 in. Pitch at 26 in. sta.: Low 14°,
high 19°
2. Propeller - Koppers Aeromatic, F200 with 00-72C, 29 lbs.
(-34) - - - - -00-72D or 00-72F blades. Dia. 72 in.Pitch at
27 in. sta.: Low 11°,
high 23.5°
3. Propeller - Sensenich 73KR59, 73BR54 or any other - - -
- - 14 lbs. (-40) fixed pitch wood propeller
eligible for the engine speed and power
and which meets the following limits: Static
rpm at max. permissible throttle setting: Not
over 2250, not under 2000. No additional
tolerance permitted. Dia: Not over 73
in., not under 71.5 in.
4. Propeller - Koppers Aeromatic, F200 with 00-73D,
00-73E, or 00-73F blades with the following
limits:
(a) Model GC-1A 29 lbs. (-34) - - - - -Parts List Assembly
4305A. Low pitch setting 11°
at 24 in. sta. Static rpm at maximum
permissible throttle setting: Not over
2525, not under 2525. No additional
tolerance permitted. Dia: Not over 73
in., not under 71.5 in. Installation
and operation must be accomplished in accordance
with Koppers "Installation and Operation Procedure
No. 18C."
(b) Model GC-1B - - - - - 29 lbs. (-41) Item
108 required. Parts List assembly 4261
or 4277. Low pitch setting 13.6°
at 24 in. sta. Static rpm at maximum
permissible throttle setting: Not over
2500, not under 2500. No additional
tolerance permitted. Dia: Not under
73 in., not under 71.5 in. Installation and operation must
be accomplished in accordance with Koppers
"Installation and Procedure No.
9B."
5. Propeller - Beech controllable, R002 or R003 with 29
lbs. (-35) - - - - - R003-201-72T or
R003-231-72T blades. Dia. 72 in.
Pitch at 27 in. sta.: Low 14.5°,
high 19.5°
6. Propeller - Beech controllable R100-101 hub with - - -
- - +26 lbs. (-40) R100-217-73T blades.
Static rpm at maximum permissible throttle
setting: Not over 2275, not under 2175
No additional tolerance permitted. Pitch
at 3/4 radius: Low 15°,
high 23°.
Item 108 required with this item.
7. Hampton Spinner Model No. 1B, Dwg. No. 100 - - - - - 2
lbs. (-40) (Optional with Koppers Aeromatic
F-200 propeller)
8. Propeller - McCauley 1A170 (a) Model
1A170-DM7357 - - - - - 33 lbs. (-40) Static
rpm at maximum permissible throttle setting: Not
over 2050, not under 1950. No additional
tolerance permitted. Diameter: Not over
73 in., not under 71.5 in. Approved
on Continental C125-2 engine only GC-1A GC-1B
(b) Model 1A170-DM735 - - - - - - 33 lbs. (-40)
Static rpm at maximum permissible throttle
setting: Not over 2180, not under 2080.
No additional tolerance permitted. Diameter:
Not over 73 in., not under 71.5 in. Approved
on Continental C125-2 engine only
*9. Propeller - Sensenich M74DR-1, fixed pitch metal - - -
- - - 30 lbs. (-40) Static rpm at maximum
permissible throttle setting: Not over
2250, not under 2000. No additional
tolerance permitted. Diameter: Not over
73 in., not under 71.5 in. Approved
on Continental C125-2 engine only.
10. Propeller – Hartzell BHC-C2YF-1BF/7663DR, constant speed
- - - - - - 46 lbs. (-40) Pitch settings
at 41" station: low 12.8°
+ 0.2°
high 30.0°
+ 1.0°
Diameter: Not over 76", not under 72",
in one inch increments Spinners: Hartzell
82A229802, D-4798P Maintain propeller
in accordance with Hartzell Owners Manual #115N and Hartzell
Maintenance Manual #113B Approved on
Continental IO-360 series engine installed per STC SA53NW
only.
Engines and Engine Accessories - Fuel and Oil System
101. Carburetor air heater 2 lbs. (-15) - - - - -
102. Cabin air heater 2 lbs. (-11) - - - - -
103. Oil radiator 4 lbs. (-13) - - - - -
104. Starter - Delco-Remy 1109656 16 lbs. (- 8) - - - - -
105. Two engine-driven fuel pumps 4 lbs. (-26) - - - - -
(Upper AC10538-III or Continental 40585-III,
lower Continental 40452)
106. Carburetor air filter X X
107. Carburetor air heater - - - - - 1 lb. (-19)
108. Oil radiator (Harrison 3875) - - - - - 4 lbs. (-13)
Required when item 4 or 6 is installed.
109. Starter - Delco-Remy A-40098 - - - - - 15 lbs. (- 7)
110. Engine-drive fuel pump (AC1523066) 2 lbs. (-26) 2 lbs.
(-33)
111. (a) Wobble pump (Air Corps. Type D-2) 3 lbs. (+34) 3
lbs. (+34) (b) Wobble pump (Aero Supply
No. 54609) 1 lb. (+34) 1 lb. (+34)
112. 9-gallon auxiliary fuel tank installation GC-1B - - -
- - 14 lbs. (+61) eligible for this
installation in the baggage compartment
in accordance with Texas Engineering & Manufacturing
Company Drawing No. 11-420-5016, Rev A.
113. Fuel tank venting system (TEMCO Drawing No. 11-420-5060).
GC-1A (except serial nos. 2 thru 128) and
GC-1B below serial no. 3501 eligible for this item
in accordance with TEMCO Customer Service Maintenance
Bulletin No. 25 dated December 10, 1947.
GC-1A, Serial Nos. 2 through 128 eligible for this
item in accordance with TEMCO Customer Service Maintenance
Bulletin No. 25 Supplement No. 1 dated June 18, 1948.
114. Fram oil-filter (CAA Approved Fram Installation Sheet
No. 62604 and 62605) 5 lbs. (- 3) 5 lbs. (-
3)
115. "CODA" exhaust silencers - - - - - 3 lbs. (-22)
116. Davis Model W-125 exhaust silencer installed in accordance
- - - - - +8 lbs. (-18) with Davis Installation
Dwg. No. W-125-C and Davis Photograph
No. P-125-1 (with Item 401 only)
117. Hanlon-Wilson Model 193 muffler-heater exhaust system
- - - - - +6 lbs. (-25) per TEMCO Dwg. No. 11-440-5046 "C".
Landing Gear and Floats
201. 6.00-6 wheels and brakes (Goodyear L6H/MBL 31
lbs. (+24) 31 lbs. (+24) or LF6H/MDB)
with 6.00-6 tires` GC-1A GC-1B
202. Tail wheel assemblies
(a) Scott 6x2.00 4 lbs. (+179) 4 lbs. (+179)
(b) 6x2.00, steerable, installed in accordance with 4 lbs.
(+179) 4 lbs. (+179) Firestone Dwg.
DFA-277. (Item 203 required).
(c) 6x2.00, steerable, installed in accordance with 5 lbs.
(+179) 5 lbs. (+179) TEMCO Dwg. 11-350-5002.
(Item 203 required.)
(d) 6x2.00, steerable, TEMCO Assy. No. 11-350-5120. 5 lbs.
(+179) 5 lbs. (+179) (Item 203 required)
(e) Scott 3250, steerable, installed in accordance with 7
lbs. (+179) 7 lbs. (+179) TEMCO Dwg.
11-351-3630, C change. (Item 203 required)
203. Tail wheel steering mechanism 2 lbs. (+170) 2 lbs. (+170)
204. Copilot brake pedal installation. 5 lbs. (+9) 5 lbs.
(+9)
Electrical and Radio Equipment
301. (a) Reading R-24 battery and battery box - 26
lbs. (-4) 24 lbs. (-4) 12-volt, 23 amp.
hr., 5 hr. rate (b) Willard AW-12-25
manifold vent-battery 12-volt, 24 lbs. (-4) 24 lbs. (-4)
25 amp. hr., 5 hr. rate (c)
Concorde RG-35A battery12-volt, 29 amp. hr., 29.5 lbs. (-4)
29.5 lbs. (-4) 5 hr. rate
302. Engine-driven generator (Delco Remy 1101876) 10 lbs.
(-8) 10 lbs. (-7)
303. Hydraulic system energizer (Adel model N-15668) 6 lbs.
(-3) 6 lbs. (-3)
304. Two-way radio (General Electric AS-1B) 12 lbs. (+16)
12 lbs. (+16)
305. Deleted (equipment same as Item 302)
306. (a) Dual fixed landing lights per TEMCO Dwg. 5 lbs. (+21)
5 lbs. (+21) No. 11-552-R3718, change "B"
(b) "CODA" landing lights (Gordon
Beach Aircraft 2.5 lbs. (+35) 2.5 lbs. (+35) Service,
Installation Dwg. No. S-125-1102)
307. Safe flight stall warning indicator per TEMCO Dwg.
No. 11-600-5101, change "B". 1 lb.
(+19) 1 lb. (+19)
Interior Equipment
401. Draft seal bulkhead, TEMCO part 11-210-5014 No
wt. change No wt. change
Miscellaneous (not listed above)
601. (a) Cabin window installation TEMCO +4 lbs. (+73)
+4 lbs. (+73) Dwg. 11-213-5096, Assembly
Fuselage "New Look" Kit-without
turnover ring. (b) Cabin window and
turnover structure installation +7.5 lbs. (+68) +7.5 lbs.
(+68) TEMCO dwg. 11-213-5095 change
"A" fuselage window and Ring
Turnover Structure "New Look" kit.
*602. Hydraulic systems modified in accordance with Ruleto,
Use actual Ruleto Industries, Inc.,
4823 Rosecrans Avenue, weight change Hawthorne, CA, Drawing
Nos. R-1004, R-1005, R1006 and installation
instructions SHK-1.
NOTE 1. Weight and balance report including list of equipment
included in certificated weight empty, and loading instructions
when necessary, must be in each aircraft at the time of original
certification and at all times thereafter (except in the
case of air carrier operators having an approved
weight control system).
NOTE 2. Placard instrument panel:
(a) "INTENTIONAL SPINS PROHIBITED."
(b) "DO NOT LOWER LANDING GEAR ABOVE 100 MPH."
.....END....
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