Paint Codes, click here.
Please Note: Not all links are active at this time, this is a work in progress.
Thanks to Michael Gillespie for the following information.
"Grumman" Specifications
Updated: 99-05-21
| Manufacturer: |
American
Aviation
|
American
Aviation
|
Grumman
American
|
Gulfstream
American
|
Grumman
American
|
Gulfstream
American
|
Gulfstream
American
|
American
General
|
Gulfstream
American |
| Model: (Photo) |
AA-1
Yankee
|
AA-1A
Trainer
|

AA-1B
|
AA-1C
Lynx
|
AA-5
Traveler
|

AA-5A
|
AA-5B
Tiger
|
AG-5B
Tiger
|
GA-7
Cougar
|
| Years Built: |
1969-71
|
1971-72
|
1973-76
|
1977-78
|
1972-75
|
1976-79
|
1975-79
|
1990-93
|
1978-79
|
| Number Built: (S/N) |
459
|
470
|
551
|
211
|
834
|
900
|
1323
|
181
|
115
|
| Type: |
Single-eng
2-seats
Fixed Gear
|
Single-eng
2-seats
Fixed Gear
|
Single-eng
2-seats
Fixed Gear
|
Single-eng
2-seats
Fixed Gear
|
Single-eng
4-seats
Fixed Gear
|
Single-eng
4-seats
Fixed Gear
|
Single-eng
4-seats
Fixed Gear
|
Single-eng
4-seats
Fixed Gear
|
Twin-eng
4-seats
Retract Gear
|
| Wingspan: |
24'5"
|
24'5"
|
24'5"
|
24'5"
|
31'5"
|
31'5"
|
31'5"
|
31'5"
|
36'9"
|
| Length: |
19'3"
|
19'3"
|
19'2"
|
19'3"
|
22'
|
22'
|
22'
|
22'
|
29'7"
|
| Height: |
6'8"
|
6'8"
|
7'6"
|
7'7"
|
8'
|
8'
|
8'
|
7'8"'
|
10'4"
|
| Empty Weight: |
982 lbs
|
1,007 lbs
|
975 lbs
|
1,066 lbs
|
1,271 lbs
|
1,286 lbs
|
1,398 lbs
|
1,398 lbs
|
2,569 lbs
|
| Gross Weight: |
1,500 lbs
|
1,500 lbs
|
1,560 lbs
|
1,600 lbs
|
2,200 lbs
|
2.200 lbs
|
2,400 lbs
|
2,400 lbs
|
3,800 lbs
|
| Payload w/Std Fuel: |
386 lbs
|
361 lbs
|
453 lbs
|
402 lbs
|
707 lbs
|
692 lbs
|
780 lbs
|
780 lbs
|
846 lbs
|
| Engine(s): |
Lycoming
O235-C2C
108 hp
@2600 rpm
|
Lycoming
O235-C2C
108 hp
@2600 rpm
|
Lycoming
O235-C2C
108 hp
@2600 rpm
|
Lycoming
O235-L2C
115 hp
@2700 rpm
|
Lycoming
O320-E2G
150 hp
@2700 rpm
|
Lycoming
O320-E2G
150 hp
@2700 rpm
|
Lycoming
O360-A4K
180 hp
@2700 rpm
|
Lycoming
O360-A4K
180 hp
@2700 rpm
|
Lycoming
O320-D1D
160 hp
@2700 rpm
|
| TBO: |
2,400 hrs
|
2,400 hrs
|
2,400 hrs
|
2,400 hrs
|
2,000 hrs
|
2,000 hrs
|
2,000 hrs
|
2,000 hrs
|
2,000 hrs
|
| Useable Fuel (max): |
22 g
|
22 g
|
22 g
|
22 g
|
37 g
|
51 g
|
51 g
|
51 g
|
114 g
|
| Useable Fuel (std): |
22 g
|
22 g
|
22 g
|
22 g
|
37 g
|
37 g
|
37 g
|
37 g
|
80 g
|
| Takeoff Gnd Roll: |
900'
|
725'
|
810'
|
890'
|
880'
|
880'
|
865'
|
865'
|
1,000
|
| Takeoff over 50': |
1,615'
|
1,400'
|
1,550'
|
1,590'
|
1,600'
|
1,600'
|
1,550'
|
1,550'
|
1,850'
|
| Rate of Climb: |
710 fpm
|
765 fpm
|
660 fpm
|
700 fpm
|
660 fpm
|
660 fpm
|
850 fpm
|
915 fpm
|
1.160 fpm
|
| Landing over 50': |
1,240'
|
1,065'
|
1,100'
|
1,125'
|
1,100'
|
1,100'
|
1,120'
|
1,120'
|
1,330'
|
| Landing Gnd Roll: |
490'
|
395'
|
410'
|
425'
|
380'
|
380'
|
410'
|
410'
|
710'
|
| Stall Speed (VSo): |
60 kt
|
51 kt
|
52 kt
|
53 kt
|
50 kt
|
53 kt
|
53 kt
|
53 kt
|
63 kt
|
| Max Speed: |
125 kt
|
120 kt
|
120 kt
|
126 kt
|
130 kt
1975=136 kt
|
136 kt
|
148 kt
|
148 kt
|
168 kt
|
Cruise Speed:
(75% Power) |
117 kt
|
109 kt
|
108 kt
|
117 kt
|
122 kt
1975=128 kt
|
128 kt
|
139 kt
|
141 kt
|
160 kt
|
| Cruise Altitude: |
8,000'
|
3,000'
|
3,000'
|
8,500'
|
9,000'
|
8,500'
|
8,500'
|
8,500'
|
8,500'
|
Cruise Range:
(45-min Reserve) |
350 nm
|
350 nm
|
350 nm
|
300 nm
|
430 nm
|
657 nm
|
554 nm
|
530 nm
|
840 nm
|
| Service Ceiling: |
11,000'
|
13,750'
|
12,750'
|
11,500'
|
12,650'
|
12,650'
|
13,800'
|
13,800'
|
17,400'
|
| Wing Loading: |
15.3 lb/sqft
|
14.9 lb/sqft
|
15.5 lb/sqft
|
15.9 lb/sqft
|
15.7 lb/sqft
|
15.7 lb/sqft
|
17.1 lb/sqft
|
17.1 lb/sqft
|
20.65 lb/sqft
|
| Power Loading: |
13.9 lb/bhp
|
13.9 lb/bhp
|
14.4 lb/bhp
|
13.9 lb/bhp
|
14.7 lb/bhp
|
14.7 lb/bhp
|
13.3 lb/bhp
|
13.3 lb/bhp
|
11.88 lb/bhp
|
Propeller(s):
Diam/Pitch Type |
McCauley
71/53 Fix
|
McCauley
71/53 Fix
|
McCauley
71/53 Fix
|
McCauley
72/52 Fix
|
McCauley
73/59 Fix
|
McCauley
73/59 Fix
|
McCauley
75/63 Fix
|
Sensenich
76/61 Fix
|
Hartzell
73" CS
|
These data are correct to the best of my knowledge. Please send comments, corrections or missing data to Michael Gillespie.
C-GRCC Cheetah Page Grumman Gang Page
p=1?
|