TB 1--1520--237--20--242
Nut, Plain Plate
3615185-1
1
.80
.80
5210-01-368-7405
Seal, Non-metallic Strip
3615692-1
1
.16
.16
NOTE
All parts above will not be required to be replaced on one end item. The first 4 parts are required
for the Hamilton Sunstrand APU and the remaining 3 are for the Honeywell APU.
Total Cost per Aircraft (Depends on type of APU installed) =
Hamilton Sunstrand APU - 11.76
Honeywell APU - 223.93
d. TB/MWOs to be applied prior to or concurrently with this inspection. N/A
e. Publications which require change as a result of this inspection. N/A.
13. References.
a. DA PAM 738-751, 15 March 1999.
b. TM 1-1500-328-23
c.
TM 1-1520-237-23-7
d. TM 1-1520-250-23-5.
e. TM 1-1520-250-23P-2
f.
TM 1-1520-237-23P-4
g. TM 55-2835-208-23
h. TM 55-2835-208-23P
i.
TM 55-2835-209-23
j.
TM 1-2835-209-23P
a.
Aircraft:
(1) TAMMS Reporting Compliance Suspense.
Upon entering requirements of this TB on DA Form 2408-13-1 for all affected aircraft, Commanders will for-
ward a priority message, datafax or email to Commander, AMCOM, ATTN: AMSAM-SF-A (SOF Compliance
Officer), Redstone Arsenal, AL 35898-5000, IAW AR 95-1, NLT date specified in paragraph 3. Datafax num-
ber is DSN 897-2111 or commercial (256) 313-2111. Email address is "safeadm@redstone.army.mil". The
report will cite this TB number , date of entry in DA Form 2408-13-1, the aircraft mission design series and
serial numbers of aircraft in numerical order.
(2) Task/Inspection Reporting Suspense.
Upon completion of inspection, Commanders will forward a priority message to the Logistical Point of Contact
listed in paragraph 16.b.. The report will cite this TB number, date of the inspection, aircraft serial number,
aircraft hours, and results of the inspection. Inspection and reports will be completed NLT date specified in
b. Wholesale Spare Parts/Assemblies. N/A.
c.
Retail Spare Parts/Assemblies. N/A.
d. The following forms are applicable and are to be completed in accordance with DA Pam 738-751,
15 Mar 99.
4
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