USAF Designation
|
NAA Designation |
Number Built |
USAF Serial
No |
Construction
Number |
Remarks |
|
|
|
|
|
|
XP-86 |
NA-140 |
3 |
45-59597
to 59599 |
38424 to
38426 |
Prototype
for P-86A/F-86A model. J35 engine, later received J47 circa 1948. |
XP-86 photo: |
|
F-86A-1 |
NA-151 |
33 |
47-605 to
47-637 |
38432 to
38464 |
First production
aircraft, mainly for test use. Flush gun muzzle doors, two-piece
folding nose gear door, navigation lights repositioned from tail
fin to fin base. J47 GE-1 engine, Mk.18 gunsight. |
F-86A-1 photo: |
|
F-86A-5 |
NA-151 |
188 |
48-129 to
48-316 |
43498 to
43685 |
First aircraft
for operational use; vee-shaped windscreen and longer canopy plexiglass
portion. J47 GE-7 engine. |
48-fiscal year
F-86A-5 photo: |
|
F-86A-5 |
NA-161 |
333 |
49-1007 to
49-1339 |
161-1 to
161-333 |
J47 GE-13
engine, later retrofitted to earlier F-86As. |
49-fiscal year
F-86A-5 photo: |
|
F-86A-6 |
- |
- |
- |
- |
F-86A-5s
modified with A-1CM sight and AN/APG-5C radar . |
F-86A-7 |
- |
- |
- |
- |
F-86A-5s
modified with A-1CM sight and AN/APG-30 radar. |
F-86A-7 photo: |
|
F-86AO |
- |
- |
- |
- |
Unofficial
designation given to F-86A converted for Orenda engine - see also
F-86J, 49-1069. |
F-86AO (F-86J)
photo: |
|
DF-86A |
- |
- |
- |
- |
One Matador
missile control aircraft, 49-1144 |
EDF-86A |
- |
- |
- |
- |
Five pre-December
1955 'exempt' Matador missile control aircraft, 48-298, 48-299,
49-1075, 49-1144, 49-1247 |
EDF-86A photo: |
|
EF-86A |
- |
- |
- |
- |
25 pre-December
1955 'exempt' temporary test aircraft, 47-605, 47-606, 47-609,
47-611, 47-616, 47-619, 47-621, 47-622, 47-628, 47-629, 47-633,
47-637, 48-170, 48-209, 48-291, 48-295, 48-303, 49-1014, 49-1102,
49-1135, 49-1137, 49-1172, 49-1189, 49-1247, 49-1301 |
EF-86A photo: |
|
JDF-86A |
- |
- |
- |
- |
One post-December
1955 temporary test Matador missile control aircraft, 49-1247 |
JF-86A |
- |
- |
- |
- |
Seven post-December
1955 temporary test aircraft, 49-1014, 49-1067, 49-1102, 49-1135,
49-1137, 49-1172, 49-1189 |
RF-86A |
- |
- |
- |
- |
Seven aircraft
converted to reconnaissance configuration in Korea: forward oblique
24-inch K-11 camera and two 20-inch K-24 cameras mounted lengthways
with a mirror arrangement to provide vertical coverage, 48-183,
48-187, 48-195, 48-196, 48-217, 48-246, 48-257, |
RF-86A photo: |
|
F-86B |
NA-152 |
- |
- |
- |
190 aircraft
ordered on 20 December 1946 under Contract AC-16013. Aircraft
would have a slightly wider fuselage to accommodate larger main
undercarriage units; advances in wheel, tyre and brake technology
negated the need for a new design, order changed for 188 further
P-86As and two P-86C. |
F-86C |
NA-157 |
2 |
48-317 and
48-318 |
157-1 and
157-2 |
Two prototypes
for penetration fighter competition. J48 engine with reheat, NACA-style
side engine intakes. Later modified with conventional intakes. |
F-86C (YF-93A)
photo: |
|
YF-86D |
NA-164 |
2 |
50-577 to
50-578 |
164-1 and
164-2 |
Prototype
F-86 interceptor, radome nose, afterburning J47 GE-17, sliding
canopy with vee-screen. Hughes E-3 fire control system. |
YF-86D photo: |
|
F-86D-1 |
NA-165 |
37 |
50-455 to
50-491 |
165-1 to
165-37 |
First production
version; clamshell canopy, flat windshield, E-3 FCS, redesigned
rear fuselage. |
F-86D-1 photo: |
|
F-86D-5 |
NA-165 |
26 |
50-492 to
50-517 |
165-38 to
165-63 |
Introduced
Hughes E-4 fire control system (standard on all subsequent F-86Ds).
Additional oxygen cylinder for pilot, redesigned instrument panel,
engine-driven alternator for FCS, repositioned main electrical
battery from left hand nose area to lower rear fuselage. |
F-86D-5 photo: |
|
F-86D-10 |
NA-165 |
36 |
50-518 to
50-553 |
165-64 to
165-99 |
Power rudder
with no trim tab, engine featuring modified afterburner fuel pump,
gun camera introduced, installed in the left wing root. |
F-86D-10 photo: |
|
F-86D-11 |
- |
- |
- |
- |
F-86D-10
converted under Project Pull-Out; brought up to F-86D-45 standard
with brake parachute, etc. |
F-86D-15 |
NA-165 |
23 |
50-554 to
50-576 |
165-100 to
165-122 |
Single-point
pressure refuelling point introduced. |
F-86D-15 photo
(1st batch): |
|
F-86D-15 |
NA-165 |
31 |
50-704 to
50-734 |
165-123 to
165-153 |
As above. |
F-86D-15 photo
(2nd batch): |
|
F-86D-16 |
- |
- |
- |
- |
F-86D-15
converted under Project Pull-Out; brought up to F-86D-45 standard
with brake parachute, etc. |
F-86D-20 |
NA-177 |
188 |
51-2944 to
51-3131 |
177-1 to
177-188 |
External
power receptacles repositioned to position under the rear fuselage,
engine fuel filter de-icing system. |
F-86D-20 photo: |
|
F-86D-21 |
- |
- |
- |
- |
F-86D-20
converted under Project Pull-Out; brought up to F-86D-45 standard
with brake parachute, etc. |
F-86D-21 photo: |
|
F-86D-25 |
NA-173 |
88 |
51-5857 to
51-5944 |
173-1 to
173-88 |
Provision
for jettisonable drop tanks. |
F-86D-25 photo: |
|
F-86D-26 |
- |
- |
- |
- |
F-86D-25
converted under Project Pull-Out; brought up to F-86D-45 standard
with brake parachute, etc. |
F-86D-26 photo: |
|
F-86D-30 |
NA-173 |
200 |
51-5945 to
51-6144 |
173-89 to
173-288 |
Automatic
approach control system introduced. |
F-86D-30 photo: |
|
F-86D-31 |
- |
- |
- |
- |
F-86D-30
converted under Project Pull-Out; brought up to F-86D-45 standard
with brake parachute, etc. |
F-86D-31 photo: |
|
F-86D-35 |
NA-173 |
118 |
51-6145 to
51-6262 |
173-289 to
173-406 |
Introduced
AN/ARN-14 omni-directional range set (VOR), external receptacle
for inverter ground power in the right hand nose area. Rudder
trim tab system reintroduced. |
F-86D-35 (1st
batch) photo: |
|
F-86D-35 |
NA-173 |
232 |
51-8274 to
51-8505 |
173-407 to
173-638 |
As above. |
F-86D-35 (2nd
batch) photo: |
|
F-86D-36 |
- |
- |
- |
- |
F-86D-35
converted under Project Pull-Out; brought up to F-86D-45 standard
with brake parachute, etc. |
F-86D-36 photo: |
|
F-86D-40 |
NA-190 |
300 |
52-3598 to
52-3897 |
190-1 to
190-300 |
Fuel flow
meter replaced earlier engine fuel pressure gauge, further cockpit
refinements included the addition of electrical face mask defrost.
All D-40s except 52-3598 to -3847 deleted the wing-root gun camera,
the model introduced the AN/ARN-18 glide path receiver in place
of the earlier AN/ARN-5B item. |
F-86D-40 photo: |
|
F-86D-41 |
- |
- |
- |
- |
F-86D-40
converted under Project Pull-Out; brought up to F-86D-45 standard
with brake parachute, etc. |
F-86D-41 photo: |
|
F-86D-45 |
NA-190 |
300 |
52-3898 to
52-4197 |
190-301 to
190-600 |
First 238
D-45s introduced J47-GE-17B with 7,500-lb. thrust, remaining F-86D-45
and subsequent models equipped with J47-GE-33. First model to
feature braking parachute as standard. |
F-86D-45 photo: |
|
F-86D-50 |
NA-190 |
107 |
52-4198 to
52-4304 |
190-601 to
190-707 |
Modified
engine oil drains, brake chute (52-10026 and on) ceramic aspirator
liner (52-4198 to -10025). |
F-86D-50 (1st
batch) photo: |
|
F-86D-50 |
NA-190 |
194 |
52-9983 to
52-10176 |
190-708 to
190-901 |
As above. |
F-86D-50 (2nd
batch) photo: |
|
F-86D-55 |
NA-201 |
225 |
53-557 to
53-781 |
201-1 to
201-225 |
Alternate
Hydraulic System accumulator dump valve (53-707 and on), inverter
external power receptacle relocated to the right hand aft fuselage
area, AN/ARC-34 UHF command radio replaced AN/ARC-27, lap belts
opened automatically after ejection. |
F-86D-55 photo: |
|
F-86D-60 |
NA-201 |
290 |
53-782 to
53-1071 |
201-226 to
201-515 |
Modified
wing attachment fittings, provision for AN/APX-25 identification
radar (IFF) set. |
F-86D-60 (1st
batch) photo: |
|
F-86D-60 |
NA-201 |
36 |
53-3675 to
53-3710 |
201-516 to
201-551 |
As above. |
F-86D-60 (2nd
batch) photo: |
|
F-86D-60 |
NA-201 |
73 |
53-4018 to
53-4090 |
201-552 to
201-624 |
As above. |
F-86D-60 (3rd
batch) photo: |
|
EF-86D |
- |
- |
- |
- |
Nine pre-December
1955 temporary test aircraft, 50-458, 50-459, 50-464, 50-472,
50-477, 50-516, 51-6146, 51-6225, 51-8282. |
EF-86D photo: |
|
GF-86D |
- |
- |
- |
- |
One ground
instructional F-86D, 51-6211. |
GF-86D photo: |
|
GTF-86D |
- |
- |
- |
- |
Two ground
instructional TF-86D, 50-493, 50-501. |
JF-86D |
- |
- |
- |
- |
25 post-December
1955 temporary test aircraft, 50-456, 50-457, 50-462, 50-463,
50-464, 50-472, 50-474, 50-477, 50-494, 50-509, 51-2974, 51-3006,
51-5959, 51-5973, 51-6009, 51-6104, 51-6121, 51-6146, 51-6225,
52-4199, 53-557, 53-619, 53-637, 53-652, 53-1030. |
JF-86D photo: |
|
JDF-86D |
- |
- |
- |
- |
One temporary
test, post-December 1955 drone control aircraft used at Patrick
AFB for Navaho testing, 50-462. |
JDF-86D photo: |
|
NF-86D |
- |
- |
- |
- |
Engine test
aircraft bailed to General Electric and used at Edwards AFB, 50-480. |
NF-86D photo: |
|
TF-86D |
- |
- |
- |
- |
39 F-86D-1
and F-86D-5 aircraft converted to act as 'pacer' aircraft during
practice rocket firings at Yuma and Tyndall AFB, radome replaced
with metal version, rocket package and related hydraulic equipment
removed, Fire Control System, autopilot, engine-driven alternator,
glide path, localiser and marker beacon equipment removed. Ballast
installed to provide satisfactory centre of gravity, but these
aircraft were 750-lb lighter than standard; 50-458, 50-460, 50-461,
50-465, 50-467, 50-470, 50-473, 50-475, 50-478, 50-479, 50-481,
50-482, 50-483, 50-484, 50-485, 50-486, 50-487, 50-488, 50-489,
50-491, 50-492, 50-493, 50-495, 50-496, 50-497, 50-498, 50-499,
50-500, 50-501, 50-503, 50-504, 50-505, 50-506, 50-511, 50-512,
50-513, 50-514, 50-515, 50-517. |
UTF-86D |
- |
- |
- |
- |
Two ground
instructional TF-86D, 50-493, 50-501. |
F-86E-1 |
NA-170 |
60 |
50-579 to
50-638 |
170-1 to
170-60 |
Irreversible
hydraulically- powered all-flying tail. |
F-86E-1 photo: |
|
F-86E-5 |
NA-170 |
51 |
50-639 to
50-689 |
170-61 to
170-111. |
Minor cockpit
changes. |
F-86E-5 photo: |
|
F-86E-6 |
- |
- |
- |
- |
60 Canadian-built
Sabre 2s supplied for use in Korea, USAF s/n 52-2833 to 52-2892.
Also 60 surplus Canadair Sabre 4s delivered to RAF from June 1953
- USAF s/n 52-10177 to 52-10236. |
F-86E-6 photo: |
|
F-86E-10 |
NA-172 |
132 |
51-2718 to
51-2849 |
172-1 to
172-132 |
F-86F with
J47 GE-13 engine. |
F-86E-10 photo: |
|
F-86E-15 |
NA-172 |
93 |
51-12977
to 51-13069 |
172-268 to
172-360 |
F-86F with
J47 GE-13 engine. |
F-86E-15 photo: |
|
F-86E |
NA-178 |
184 |
- |
- |
Cancelled
order. |
F-86E(M) |
- |
- |
- |
- |
Name given
to Canadair Sabre 2 and 4 converted with '6-3' wing for overseas
service - Greece, Turkey, Italy and Yugoslavia. |
F-86E(M) photo: |
|
EF-86E |
- |
- |
- |
- |
11 pre-December
1955 temporary test aircraft, 50-588, 50-599, 50-605, 50-606,
50-639, 51-2720, 51-2725, 51-2726, 51-2750, 51-2848, 51-2849 |
EF-86E photo: |
|
JF-86E |
- |
- |
- |
- |
18 post-December
1955 temporary test aircraft, 50-579, 50-581, 50-582, 50-583,
50-588, 50-599, 50-605, 50-639, 51-2718, 51-2719, 51-2725, 51-2726,
51-2750, 51-2773, 51-2774, 51-2792, 51-2839, 51-2848 |
JF-86E photo: |
|
QF-86E |
- |
- |
- |
- |
Canadair
Sabre 5 and 6 converted for use by US Army as pilotless drones. |
QF-86E photo: |
|
F-86F-1 |
NA-172 |
51-2850 to
51-2927 |
. |
172-133 to
172-210 |
5,970-lb.thrust
J47-GE-27 engine. |
F-86F-1 photo: |
|
F-86F-2 |
- |
- |
- |
- |
Four F-86E-10
and six F-86F-1 modified to carry four T-160 20mm cannon, 51-2803,
51-2819, 51-2826, 51-2836, 51-2855, 51-2861, 51-2867, 51-2868,
51-2884, 51-2900. |
F-86F-2 photo: |
|
F-86F-3 |
- |
- |
- |
- |
Two F-86F-1
modified to carry four Oerlikon 206RK 20mm cannon, 51-2916, 51-2926. |
F-86F-3 photo: |
|
F-86F-5 |
NA-172 |
16 |
51-2928 to
51-2943 |
172-211 to
172-226 |
Capability
to carry 200-gallon drop tanks earlier 120-gallon tanks. |
F-86F-5 photo: |
|
F-86F-10 |
NA-172 |
34 |
51-12936
to 51-12969 |
172-227 to
172-260 |
A-4 gunsight
replaces earlier A-1CM sight. |
F-86F-10 photo: |
|
F-86F-15 |
NA-172 |
7 |
51-12970
to 51-12976 |
172-261 to
172-267 |
Repositioned
and redesigned control systems to improve battle damage tolerance. |
F-86F-15 photo: |
|
F-86F-20 |
NA-176 |
100 |
51-13070
to 51-13169 |
176-1 to
176-100 |
Columbus-built,
AN/ARC-33 VHF Command Radio in place of the earlier AN/ARC-3. |
F-86F-20 photo: |
|
F-86F-25 |
NA-176 |
341 |
51-13170
to 51-13510 |
176-101 to
176-441 |
Columbus-built
fighter- bomber, four-store wing, modified flight control system,
AN/ARC-27 VHF Command Radio installed. '6-3' wing from 171st aircraft
(51-13341) . |
F-86F-25 (1st
batch) photo: |
|
F-86F-25 |
NA-193 |
259 |
52-5272 to
52-5530 |
193-1 to
193-259 |
As above. |
F-86F-25 (2nd
batch) photo: |
|
F-86F-30 |
NA-191 |
859 |
52-4305 to
52-5163 |
191-1 to
191-859 |
Inglewood-built
fighter- bomber, as F-86F-25. '6-3' wing from 200th aircraft (52-4505). |
F-86F-30 photo: |
|
F-86F-35 |
NA-191 |
108 |
52-5164 to
52-5271 |
191-860 to
191-967 |
Nuclear-capable
fighter-bomber with capability to carry Mk.12 nuclear weapon under
inner left wing pylon. Low Altitude Bombing System (LABS) fitted,
M-1 LABS computer, redesigned instrument panel. |
F-86F-35 NA-191
photo: |
|
F-86F-35 |
NA-202 |
157 |
53-1072 to
53-1228 |
202-1 to
202-157 |
As above. |
F-86F-35 NA-202
photo: |
|
F-86F |
NA-206 |
240 |
- |
- |
Cancelled
order. |
F-86F-40 |
NA-227 |
215 |
55-3816 to
55-4030 |
227-1 to
227-215 |
Inglewood-built
export model with 12-inch wingtip extensions. To Japan, Tunisia,
Pakistan, Spain |
F-86F-40 NA-227
(1st batch) photo: |
|
F-86F-40 |
NA-227 |
65 |
55-4983 to
55-5047 |
227-216 to
227-280 |
As above,
to Pakistan, Taiwan, Korea. |
F-86F-40 NA-227
(2nd batch) photo: |
|
F-86F-40 |
NA-231 |
70 |
55-5048 to
55-5117 |
231-1 to
231-70 |
Mitsubishi-built
for Japanese Air Self Defense Force. |
F-86F-40 NA-231
photo: |
|
F-86F-40 |
NA-238 |
110 |
56-2773 to
56-2882 |
238-1 to |
Mitsubishi
built for Japanese Air Self Defense Force. |
F-86F-40 NA-238
photo: |
|
F-86F-40 |
NA-256 |
120 |
57-6338 to
57-6457 |
256-1 |
Mitsubishi
built for Japanese Air Self Defense Force. |
F-86F-40 NA-256
photo: |
|
EF-86F |
- |
- |
- |
- |
Eight pre-December
1955 temporary test aircraft, 51-13071, 51-13127, 51-13171, 51-13177,
52-4349, 52-4598, 52-5426, 53-1160. |
GF-86F |
- |
- |
- |
- |
Ground instructional
airframes, 51-13249, 52-5163. |
JF-86F |
- |
- |
- |
- |
36 post-December
1955 temporary test aircraft, 51-2916, 51-2926, 51-2928, 51-13127,
51-13171, 51-13173, 51-13179, 51-13188, 51-13258, 51-13290, 51-13299,
51-13300, 51-13311, 51-13313, 51-13314, 51-13321, 51-13323, 51-13331,
51-13461, 51-13506, 52-4347, 52-4349, 52-4598, 52-4608, 52-5143,
52-5158, 52-5162, 52-5163, 52-5412, 52-5426, 52-5485, 52-5489,
52-5521, 52-5527, 53-1080, 53-1160. |
JF-86F photo: |
|
QF-86F |
- |
- |
- |
- |
Remote-piloted
target drone for US Navy; converted from export F-86F-40s. |
QF-86F photo: |
|
RF-86F |
- |
- |
- |
- |
26 photo
reconnaissance aircraft for USAF, converted in-theatre for use
in Korea, 52-4330, 52-4354, 52-4357, 52-4377, 52-4379, 52-4418,
52-4435, 52-4451, 52-4459, 52-4492, 52-4514, 52-4518, 52-4522,
52-4529, 52-4543, 52-4572, 52-4587, 52-4763, 52-4767, 52-4800,
52-4808, 52-4858, 52-4859, 52-4863, 52-4864, 52-4874. |
RF-86F (USAF)
photo: |
|
RF-86F |
- |
- |
- |
- |
18 photo
reconnaissance aircraft converted for use by Japanese Air Self
Defense Force, 51-13368, 51-13385, 51-13390, 51-13494, 52-4679,
52-4684, 52-4693, 52-4699, 52-4708, 52-4742, 52-4745, 52-4758,
52-4836, 52-4844, 52-4905, 52-4913, 52-4939, 52-5439. |
RF-86F (JASDF)
photo: |
|
TF-86F |
NA-204 |
- |
- |
204-1 |
Two-seat
trainer prototype, 52-5016 |
TF-86F 1st
prototype photo: |
|
TF-86F |
NA-216 |
- |
- |
216-1 |
Two-seat
trainer, replacement for prototype, 53-1228 |
TF-86F No.2
aircraft photo: |
|
UF-86F |
- |
- |
- |
- |
Ground instructional
airframe, 52-5163 |
F-86F(R) |
- |
- |
- |
- |
Unofficial
designation associated with rocket-assisted test JF-86F 52-4608. |
'F-86F(R)'
photo: |
|
- |
NA-210 |
- |
- |
- |
Two F-86F-30
modified to incorporate internal rocket 2.5-inch rocket packs.
. |
F-86F NA-210
photo: |
|
F-86G |
- |
- |
- |
- |
Order re-named
F-86D-25. |
F-86H-1 |
NA-187 |
2 |
52-1975 and
52-1976 |
187-1 and
187-2 |
Inglewood-built
prototypes, sometimes called YF-86H. J73 GE-3 engine, clamshell
canopy, no armament. |
YF-86H photo: |
|
F-86H-1 |
NA-187 |
113 |
52-1977 to
52-2089 |
187-3 to
187-115 |
Columbus-built,
six, 0.50- inch calibre machine guns, J73 GE-3A engine from 61st
aircraft, '6-3' wing from 52-1991. |
F-86H-1 photo: |
|
F-86H-5 |
NA-187 |
45 |
52-2090 to
52-2124 |
187-116 to
187-150 |
Introduced
4xM39 20-mm cannon armament. |
F-86H-5 (1st
batch) photo: |
|
F-86H-5 |
NA-187 |
25 |
52-5729 to
52-5753 |
187-151 to
187-175 |
As above |
F-86H-5 (2nd
batch) photo: |
|
F-86H-10 |
NA-203 |
300 |
53-1229 to
53-1528 |
203-1 to
203-300 |
Empty weight
reduced by 187 lb, slatted wing on last ten aircraft. |
F-86H-10 photo: |
|
QF-86H |
- |
- |
- |
- |
F-86H aircraft
converted as pilotless drones for US Navy. |
QF-86H photo: |
|
F-86J |
NA-167 |
- |
- |
- |
F-86A 49-1069
converted for Orenda engine testing. |
F-86J photo: |
|
YF-86K |
NA-205 |
- |
- |
205-1 |
Prototype,
Inglewood-built, converted from F-86D-40 52-3630, MG-4 fire control
system, 8-inch fuselage extension, J47 GE-33 engine, no armament. |
YF-86K 1st
prototype photo: |
|
YF-86K |
NA-205 |
- |
- |
205-2 |
2nd prototype,
converted from F-86D-40 52-3804, as above but with 2xM39 20-mm
cannon. |
YF-86K 2nd
prototype photo: |
|
F-86K |
NA-207 |
50 |
53-8273 to
53-8322 |
207-1 to
207-50 |
FIAT-built
aircraft, production-standard with 4xM39 20-mm cannon for Italian
AF as MM6185 to MM6234. |
F-86K NA-207
photo: |
|
F-86K |
NA-213 |
120 |
54-1231 to
54-1350 |
213-1 to
213-120 |
Inglewood-built
for Norway and Holland. |
F-86K NA-213
photo: |
|
F-86K |
NA-221 |
70 |
55-4811 to
55-4880 |
221-1 to
221-70 |
FIAT-built
for Italian and French AF. |
F-86K NA-221
photo: |
|
F-86K |
NA-232 |
56 |
55-4881 to
55-4936 |
232-1 to
232-56 |
FIAT-built
for Lufwaffe, French and Dutch AF. |
F-86K NA-232
photo: |
|
F-86K |
NA-242 |
50 |
56-4116 to
56-4160 |
242-1 to
242-50 |
FIAT-built,
with 'F-40' wing, for Luftwaffe. |
F-86K NA-242
photo: |
|
F-86L-11 |
- |
- |
- |
- |
Two F-86D-11
aircraft converted to incorporate Semi-Automatic Ground Environment
(SAGE) equipment, 12-inch wingtip extension, increased chord wing. |
F-86L-11 photo: |
|
F-86L-16 |
- |
- |
- |
- |
24 F-86D-16
aircraft converted to incorporate Semi-Automatic Ground Environment
(SAGE) equipment, 12-inch wingtip extension, increased chord wing. |
F-86L-16 photo: |
|
F-86L-21 |
- |
- |
- |
- |
82 F-86D-21
aircraft converted to incorporate Semi-Automatic Ground Environment
(SAGE) equipment, 12-inch wingtip extension, increased chord wing. |
F-86L-21 photo: |
|
F-86L-26 |
- |
- |
- |
- |
19 F-86D-26
aircraft converted to incorporate Semi-Automatic Ground Environment
(SAGE) equipment, 12-inch wingtip extension, increased chord wing. |
F-86L-31 |
- |
- |
- |
- |
74 F-86D-31
aircraft converted to incorporate Semi-Automatic Ground Environment
(SAGE) equipment, 12-inch wingtip extension, increased chord wing. |
F-86L-31 photo: |
|
F-86L-36 |
- |
- |
- |
- |
One F-86D-36
aircraft converted to incorporate Semi-Automatic Ground Environment
(SAGE) equipment, 12-inch wingtip extension, increased chord wing. |
F-86L-36 photo: |
|
F-86L-41 |
- |
- |
- |
- |
13 F-86D-41
aircraft converted to incorporate Semi-Automatic Ground Environment
(SAGE) equipment, 12-inch wingtip extension, increased chord wing. |
F-86L-45 |
- |
- |
- |
- |
64 F-86D-45
aircraft converted to incorporate Semi-Automatic Ground Environment
(SAGE) equipment, 12-inch wingtip extension, increased chord wing. |
F-86L-45 photo: |
|
F-86L-50 |
- |
- |
- |
- |
121 F-86D-50
aircraft converted to incorporate Semi-Automatic Ground Environment
(SAGE) equipment, 12-inch wingtip extension, increased chord wing. |
F-86L-50 photo: |
|
F-86L-55 |
- |
- |
- |
- |
200 F-86D-55
aircraft converted to incorporate Semi-Automatic Ground Environment
(SAGE) equipment, 12-inch wingtip extension, increased chord wing. |
F-86L-55 photo: |
|
F-86L-60 |
- |
- |
- |
- |
F-86D-60
aircraft converted to incorporate Semi-Automatic Ground Environment
(SAGE) equipment, 12-inch wingtip extension, increased chord wing. |
F-86L-60 photo: |
|
JF-86L |
- |
- |
- |
- |
Temporary
test F-86L, 52-3680, 52-4234, 53-595, 53-689, 53-691, 53-932,
53- 1004, 53-1040, 53-1062, 53-1067. |
|
|
|
|
|
|