. Selected Typical Aircraft Squadron Strengths

AFI 65-503 2 May 1996 Attachment 42

Table A42-1. Selected Typical Aircraft Squadron Strengths

				SQ		CREW			MAINTENANCE			SQUADRON			WEAPON SYSTEM			TOTAL PRIMARY			BASE
		CREW	CREW	SIZE	FHs/	PERSONNEL		MNX	PERSONNEL			STAFF			SECURITY			PROGRAM ELEMENT			OPERATING SUPPORT			GRAND TOTALS
MDS	CMD	RATIO	COMP	(PAA)	PAA	OFF	ENL	SPA	OFF	ENL	CIV	OFF	ENL	CIV	OFF	ENL	CIV	OFF	ENL	CIV	OFF	ENL	CIV	OFF	ENL	CIV
T001A	AETC	(note 2)	1	22	750	0	0		CLS *	CLS	CLS	25	8	1	0	0	0	25	8	1	0	3	1	25	11	2
(UPT)
T037B	AETC	(note 2)	1	39	553	0	0		CLS	CLS	CLS	29	10	2	0	0	0	29	10	2	0	3	1	29	13	3
(UPT/SUPT)
T038A	AETC	(note 2)	1	45	504	0	0		CLS	CLS	CLS	29	10	2	0	0	0	29	10	2	0	3	1	29	13	3
(UPT)
T038A	AETC	(note 2)	1	22	374	0	0		CLS	CLS	CLS	29	10	2	0	0	0	29	10	2	0	3	1	29	13	3
(SUPT)
T003	AETC	(note 2)	1	54	428	0	0		CLS	CLS	CLS	8	3	2	0	0	0	8	3	2	0	1	0	8	4	2
(FSP)
T043A	AETC	(note 2)	2.8	10	944	24	0	4.80	1	47	0	10	6	3	0	0	0	35	53	3	0	7	2	35	60	5
(UNT)
C005A/B	AMC	1.80	6.5	16	609	58	129	51.53	12	742	71	15	22	1	0	22	0	85	915	72	1	82	26	86	997	98
C009	AMC	2.00	3	11	610	44	22	21.50	7	229	0	2	5	2	0	0	0	53	256	2	0	24	8	53	280	10
C021A	AMC	1.13		4	669	10	0		CLS	CLS	CLS	2	5	1	0	0	0	12	5	1	0	1	0	12	6	1
C025	AMC	NA	NA	2		15	48		1	196	0	2	1	0	0	76	0	18	321	0	0	26	8	18	347	8
KC010	AMC	2.00	4.25	12	597	48	54	18.90	2	225	0	4	15	0	0	0	0	54	294	0	0	27	9	54	321	9
KC135R/T	AMC	1.27	4	12	256	46	15	17.16	2	204	0	3	18	0	0	0	0	51	237	0	0	22	7	51	259	7
C137	AMC	1.50	14.67	6	690	48	84	15.00	2	79	9	2	8	0	0	35	0	52	206	9	0	20	7	52	226	16
C141B	AMC	1.80	5.5	16	882	57	101	35.10	11	494	56	15	22	1	0	22	0	83	639	57	1	60	19	84	699	76
UH001N	AMC	1.00		17	394	34	17		3	129	0	1	3	0	0	0	0	38	149	0	0	14	5	38	163	5
AC130H	SOC	1.80	14	7	608	63	113	67.50	9	463	0	4	27	0	0	12	0	76	615	0	1	53	17	77	668	17
AC130U	SOC	1.80	13	10	608	90	144	62.00	12	608	0	4	27	0	0	12	0	106	791	0	1	69	22	107	860	22
HC130N	SOC	1.50	8	6	486	36	36	27.00	3	142	17	5	19	1	0	6	0	44	203	18	0	20	6	44	223	24
HC130P	SOC	1.50	8	6	486	36	36	27.00	3	142	17	5	19	1	0	6	0	44	203	18	0	20	6	44	223	24
MC130E	SOC	1.50	9	6	687	45	36	51.00	6	300	0	5	19	1	0	6	0	56	361	1	0	32	10	56	393	11
(CONUS)
MC130E	SOC	1.50	9	4	687	30	24	51.00	4	200	0	5	19	1	0	6	0	39	249	1	0	22	7	39	271	8
(O/S)
MC130H	SOC	1.50	7	9	376	54	41	47.00	8	415	0	5	19	1	0	12	0	67	487	1	1	42	14	68	529	15
MH053J	SOC	1.50	6	22	272	65	133	39.00	17	738	103	5	19	1	0	16	0	87	906	104	1	84	27	88	990	131
MH060G	SOC	1.50	4	8	456	24	24	18.50	3	136	9	5	19	1	0	6	0	32	185	10	0	17	6	32	202	16
A010	PAF	1.50	1	6	420	9	0	28.17	3	166	0	7	23	0	0	20	0	19	209	0	0	17	6	19	226	6
F015C/D	PAF	1.25	1	18	316	23	0	27.22	10	480	0	7	23	0	0	20	0	40	523	0	1	43	14	41	566	14
F015E	PAF	1.25	2	18	342	45	0	35.00	13	614	0	8	28	0	0	20	0	66	662	0	1	56	18	67	718	18
F016C/D	PAF	1.25	1	24	351	30	0	25.54	12	601	0	7	23	0	0	20	0	49	644	0	1	53	17	50	697	17
OA010	PAF	2.00	1	12	420	24	0	19.25	5	226	0		(Note 6)		0	0	0	29	226	0	0	20	6	29	246	6
A010	ACC	1.50	1	12	456	18	0	23.25	6	273	0	7	23	0	0	20	0	31	316	0	0	27	8	31	343	8
B001B	ACC	1.50	4	12	374	72	0	40.50	5	479	2	9	22	0	2	72	0	88	573	2	1	51	16	89	624	18
BO52H	ACC	1.40	5	12	368	84	0	46.42	6	549	3	9	22	2	2	117	0	101	688	5	1	61	19	102	749	24
EC130E	ACC	2.00	16	6	584	72	120	47.16	7	267	3	7	23	3	0	0	0	86	410	6	1	38	12	87	448	18
EC135C	ACC	1.78	10	7	1046	39	91	47.43	11	314	7	3	23	3	0	92	0	53	520	10	1	45	14	54	565	24
EC135K	ACC	2.00	18	2	600	24	48	27.00	1	53	0	7	8	0	0	0	0	32	109	0	0	11	3	32	120	3
C130E	ACC	2.00	5.5	16	0	96	80	26.52	8	416	0	7	34	1	0	20	0	111	550	1	1	51	16	112	601	17
C130H	ACC	2.00	5.5	12	0	72	60	26.52	6	312	0	7	34	1	0	20	0	85	426	1	1	39	13	86	465	14
E003	ACC	2.00	23	8	1027	128	240	65.55	10	508	6	9	23	2	0	(Note 5)	0	147	771	8	1	71	23	148	842	31
E004B	ACC	2.00	31	3	640	24	162	59.33	4	174	1	7	23	0	0	30	0	35	389	1	0	33	10	35	422	11
F015C/D	ACC	1.25	1	18	327	23	0	28.56	10	504	0	7	23	0	0	20	0	40	547	0	1	45	14	41	592	14
F015E	ACC	1.25	2	18	363	45	0	33.56	12	592	0	8	28	0	0	20	0	65	640	0	1	54	17	66	694	17
F016C/D	ACC	1.25	1	18	346	23	0	27.78	10	490	0	7	23	0	0	20	0	40	533	0	1	44	14	41	577	14
EF111A	ACC	1.25	2	24	360	60	0	31.90	15	750	0	11	26	0	0	20	0	86	796	0	1	67	22	87	863	22
F117A	ACC	1.25	1	18	306	23	0	27.44	10	484	0	9	40	0	0	20	0	42	544	0	1	45	14	43	589	14
OA010	ACC	2.00	1	12	492	24	0	20.58	5	242	0		(Note 6)		0	0	0	29	242	0	0	21	7	29	263	7
T038A	ACC	1.00	1	5	385	5	0		CLS	CLS	CLS	7	0	0	0	0	0	12	0	0	0	1	0	12	1	0
(ACE)
U002	ACC	2.50	3	7	540	53	0	49.30	2	343	0	7	5	0	0	0	0	62	348	0	0	31	10	62	379	10
A010	AFE	1.50	1	12	425	18	0	25.08	6	295	0	7	23	0	0	20	0	31	338	0	0	28	9	31	366	9
F015C/D	AFE	1.25	1	18	318	23	0	28.56	10	504	0	7	23	0	0	20	0	40	547	0	1	45	14	41	592	14
F015E	AFE	1.25	2	24	372	60	0	30.02	14	706	0	8	28	0	0	20	0	82	754	0	1	64	20	83	818	20
F016C/D	AFE	1.25	1	18	331	23	0	28.64	10	505	0	7	23	0	0	20	0	40	548	0	1	45	14	41	593	14
OA010	AFE	2.00	1	6	492	12	0	20.44	2	120	0		(Note 6)		0	0	0	14	120	0	0	10	3	14	130	3

* Contractor Logistics Support (i.e., maintenance performed by civilian contractors, vice in-house manpower.)

Notes:

1. Current as of March 1996, reflecting force structure decisions as of the FY97 President's Budget (PB). Figures may be superseded as further force structure decisions are made.

2. AETC crew ratios operate in a dynamic environment. Production quotas cause constant fluctions in crew ratios, unlike fixed PAA operational wings.

3. Crew ratio data provided by HQ USAF/XOOT.

4. WSS is a wing wide cost but has been divided by 3 to evenly distribute the cost per squadron.

5. WSS for AWACS is owned by AFMC

6. Squadron overhead in A-10/OA-10 squadrons provided in A-10 lines.

Data Source: HQ USAF/PEP, DSN 227-4781 or (703) 697-4781.