XTF30-P-1
8,250 lbf (36.70 kN) thrust.

YTF30-P-1
TF30-P-1
8,500 lbf (37.81 kN) thrust, 18,500 lbf (82.29 kN) with afterburner.

TF30-P-1A
Similar to -1 with a fuel filter-heater instead of a fuel filter, initially powered first two prototype F-111B.
TF30-P-2
10,200 lbf (45.37 kN) thrust, intended to power the F6D Missileer.

TF30-P-3
8,500 lbf (37.81 kN) thrust, 18,500 lbf (82.29 kN) with afterburner.

TF30-P-5
TF30-P-6
11,350 lbf (50.49 kN) thrust, powered the A-7A.
TF30-P-6A
TF30-P-6C
TF30-P-6E
TF30-P-7
12,350 lbf (54.94 kN) thrust, 20,350 lbf (90.52 kN) with afterburner.

TF30-P-8
12,200 lbf (54.27 kN) thrust, initially powered the A-7B/C.
TF30-P-9
12,000 lbf (53.38 kN) thrust, 19,600 lbf (87.19 kN) with afterburner.

TF30-P-12
10,750 lbf (47.82 kN) thrust, 20,250 lbf (90.08 kN) with afterburner, powered the two pre-production F-111B.
TF30-P-12A
Similar to -12 with a fuel filter instead of a fuel filter-heater and deactivated wave-off feature, powered early production FB-111A.
TF30-P-14
TF30-P-16
TF30-P-18
YTF30-P-100
TF30-P-100
Redesigned engine, 14,560 lbf (64.77 kN) thrust, 25,100 lbf (111.65 kN) with afterburner, powered the F-111F.
TF30-P-103
Redesignated -3 upgraded with -100 components under the Pacer 30 program, 9,800 lbf (43.59 kN) thrust, 18,500 lbf (82.29 kN) with afterburner.

TF30-P-107
Redesignated -7 upgraded with -100 components under the Pacer 30 program, 10,800 lbf (48.04 kN) thrust, 20,350 lbf (90.52 kN) with afterburner.

TF30-P-108
Hybrid of -107 aft section and -109 fore section.

TF30-P-108RA
Redesignated -108 when in RAAF service, powered the F-111G.
TF30-P-109
Redesignated -9 upgraded with -100 components under the Pacer 30 program, 20,840 lbf (92.70 kN) thrust with afterburner.

TF30-P-109RA
Redesignated -109 when in RAAF service, powered the F-111C.
TF30-P-408
Similar to -8, 13,390 lbf (59.56 kN) thrust, powered the A-7B/C.
TF30-P-412
Similar to -12
TF30-P-412A
Similar to -12A, 10,800 lbf (48.04 kN) thrust, 20,900 lbf (92.97 kN) with afterburner, powered early production F-14A.
TF30-P-414A
Similar to -412A, powered later production F-14A.
JTF10A
Company designation for the TF30 family of engines
JTF10A-1
(XTF30-P-1) Intended to power the Douglas Model 2067.

JTF10A-6
Intended to power the Douglas Model 2086.

JTF10A-7
(TF30-P-2)
JTF10A-8
(TF30-P-6)
JTF10A-9
(TF30-P-8)
JTF10A-10
JTF10A-15
(TF30-P-18)
JTF10A-16
(TF30-P-408)
JTF10A-20
(TF30-P-1)
JTF10A-21
(TF30-P-3)
JTF10A-27A
(TF30-P-12)
JTF10A-27B
(TF30-P-12A)
JTF10A-27D
(TF30-P-7)
JTF10A-27F
(TF30-P-412)
JTF10A-32C
(TF30-P-100)
JTF10A-36
(TF30-P-9)
Pratt & Whitney/SNECMA TF104
Subsonic TF30 derivative modified by SNECMA, installed in Mirage IIIT and Mirage IIIV-01.

Pratt & Whitney/SNECMA TF106
A derivative of the TF30 to power the Dassault Mirage IIIV VTOL fighter.

Pratt & Whitney/SNECMA TF306C
A derivative of the TF30 tested in the Dassault Mirage F2.

Pratt & Whitney/SNECMA TF306E
XTF30-P-1
8,250 lbf (36.70 kN) thrust.
YTF30-P-1
TF30-P-1
8,500 lbf (37.81 kN) thrust, 18,500 lbf (82.29 kN) with afterburner.
TF30-P-1A
Similar to -1 with a fuel filter-heater instead of a fuel filter, initially powered first two prototype F-111B.
TF30-P-2
10,200 lbf (45.37 kN) thrust, intended to power the F6D Missileer.
TF30-P-3
8,500 lbf (37.81 kN) thrust, 18,500 lbf (82.29 kN) with afterburner.
TF30-P-5
TF30-P-6
11,350 lbf (50.49 kN) thrust, powered the A-7A.
TF30-P-6A
TF30-P-6C
TF30-P-6E
TF30-P-7
12,350 lbf (54.94 kN) thrust, 20,350 lbf (90.52 kN) with afterburner.
TF30-P-8
12,200 lbf (54.27 kN) thrust, initially powered the A-7B/C.
TF30-P-9
12,000 lbf (53.38 kN) thrust, 19,600 lbf (87.19 kN) with afterburner.
TF30-P-12
10,750 lbf (47.82 kN) thrust, 20,250 lbf (90.08 kN) with afterburner, powered the two pre-production F-111B.
TF30-P-12A
Similar to -12 with a fuel filter instead of a fuel filter-heater and deactivated wave-off feature, powered early production FB-111A.
TF30-P-14
TF30-P-16
TF30-P-18
YTF30-P-100
TF30-P-100
Redesigned engine, 14,560 lbf (64.77 kN) thrust, 25,100 lbf (111.65 kN) with afterburner, powered the F-111F.
TF30-P-103
Redesignated -3 upgraded with -100 components under the Pacer 30 program, 9,800 lbf (43.59 kN) thrust, 18,500 lbf (82.29 kN) with afterburner.
TF30-P-107
Redesignated -7 upgraded with -100 components under the Pacer 30 program, 10,800 lbf (48.04 kN) thrust, 20,350 lbf (90.52 kN) with afterburner.
TF30-P-108
Hybrid of -107 aft section and -109 fore section.
TF30-P-108RA
Redesignated -108 when in RAAF service, powered the F-111G.
TF30-P-109
Redesignated -9 upgraded with -100 components under the Pacer 30 program, 20,840 lbf (92.70 kN) thrust with afterburner.
TF30-P-109RA
Redesignated -109 when in RAAF service, powered the F-111C.
TF30-P-408
Similar to -8, 13,390 lbf (59.56 kN) thrust, powered the A-7B/C.
TF30-P-412
Similar to -12
TF30-P-412A
Similar to -12A, 10,800 lbf (48.04 kN) thrust, 20,900 lbf (92.97 kN) with afterburner, powered early production F-14A.
TF30-P-414A
Similar to -412A, powered later production F-14A.
JTF10A
Company designation for the TF30 family of engines
JTF10A-1
(XTF30-P-1) Intended to power the Douglas Model 2067.
JTF10A-6
Intended to power the Douglas Model 2086.
JTF10A-7
(TF30-P-2)
JTF10A-8
(TF30-P-6)
JTF10A-9
(TF30-P-8)
JTF10A-10
JTF10A-15
(TF30-P-18)
JTF10A-16
(TF30-P-408)
JTF10A-20
(TF30-P-1)
JTF10A-21
(TF30-P-3)
JTF10A-27A
(TF30-P-12)
JTF10A-27B
(TF30-P-12A)
JTF10A-27D
(TF30-P-7)
JTF10A-27F
(TF30-P-412)
JTF10A-32C
(TF30-P-100)
JTF10A-36
(TF30-P-9)
Pratt & Whitney/SNECMA TF104
Subsonic TF30 derivative modified by SNECMA, installed in Mirage IIIT and Mirage IIIV-01.
Pratt & Whitney/SNECMA TF106
A derivative of the TF30 to power the Dassault Mirage IIIV VTOL fighter.
Pratt & Whitney/SNECMA TF306C
A derivative of the TF30 tested in the Dassault Mirage F2.
Pratt & Whitney/SNECMA TF306E
Pratt & Whitney TF30