MAINTENANCE SERVICES ON SP2H AIRCRAFT; PROPOSAL FOR CORRECTION OF DISCREPANCIES

• Document Type: FOIA
• Collection: FOIA Collection
• Document Number (FOIA) /ESDN (CREST): 05751332
• Release Decision: RIPPUB
• Original Classification: U
• Document Page Count: 9
• Document Creation Date: March 9, 2023
• Document Release Date: February 10, 2021
• Case Number: F-2011-01575
• Publication Date: July 12, 1966

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GROUP
EXCLUDED M AUTOMATIC
NGEAEMG: AND
DECLASSIFICATION
SA-308h
Post Office Box 490
Greenville, Texas
12 July 1966
In Reply Refer To:
8435-60320C-05
REGISTERED
SUBJECT Maintenance Services on SP2H Aircraft;
Proposal for Correction of Discrepancies.
TO
ATTENTION Contracting Officer
REFERENCE
ENCLOSURE
(b)(3)
(a) Our Letter 8435-60320C-03 dated
1 July 1966.
(b) Contract File Ref. 1968.
(1) Itemized Discrepancy List and Price
Proposal.
This Contractor submits, as Enclosure (1) hereto, its formal cost-
plus-fixed-fee price proposal covering the correction of basic air-
frame discrepancies on SP2H Aircraft, S/N 135582. This proposal is
presented to supplement our Reference (a) submittal under Reference
(b) contract.
A detailed listing of discrepancies, proposed corrective action and
estimated labor cost, by line item, is set forth in Enclosure (1).
Material costs are shown as a separate item representing an estimate
of miscellaneous materials which are not normally available from
Navy Supply sources.
Other direct costs (premium pay) were developed on the basis of an
estimated 88 overtime manhours to be expended in accomplishing this
task. It is requested that the Task Order issued for this effort
include authorization for the expenditure of 88 overtime manhours.11
This Document contains Information affecting the onai Defense of he
United Stares within the meaning of the Espio a Laws, Title 13 LI.
Secficus and 794, its transmissi or the revelation of its contenta
In any manner to an ugauthorized can ta prchihited by law.
7
e4
g-/
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(z)
8435-60320C-05
Page 2
12 July 1966
Labor rates, overhead and general and administrative factors utilized
in developing cost and fee price are in accordance with the rates nego-
tiated for the basic maintenance program.
Your early approval of the effort defined herein and authorization to
proceed will be appreciated. Please direct any questions concerning
this proposal' to Mr. C. F. Wilson.
CFW:lw
end s.
cc: H. Chapman.
. K. Carr, Jr.
Controller
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ENCLOSURE (1)
ITEMIZED DISCREPANCY LIST AND PRICE PROPOSAL
Rejection
Number
Discrepancy Corrective Action
A229167 R/H Flap Bay. One stringer cracked Stop drill cracks; install -3
outboard of inboard flap track of repair.
outboard flap and one inboard of
same flap track.
A229168 R/H Flap Bay. Safety wire is bro- Remove old landing light; in-
ken on cannon plug for landing stall new one and run operation.
light. Also, light is not re-
tracted completely and loose.
A229169
A229170
A229171
A229172
R/H Flap. Lower nacelle fairing Drill out approximately six rivets;
on flap at trailing edge has two bump out cans; reinstall rivets.
cans in metal.
L/H Flap. Lower nacelle fairing Drill out approximately six rivets;
has two cans in metal at trailing bump out area; install rivets.
edge on flap.
R/H Flap Bay. Several rivets Remove loose rivets; install new
loose in trailing edge of bay ones.
skin. Rivet heads are worn in-
board flap area (15 rivets).
R/H Flap Bay. Seven rivets loose Remove loose rivets and install
in bottom bay skin next to fuse- new ones.
lage.
A229173 R/H Flap Bay. Five cable pulley
bearings are rusted and hard to
turn at both inboard flap tracks.
Remove old bearings; install new
ones; and install cable.
Manhours Labor Cost
9.6
$ 60.
2.4
15.
3.6
23.
3.6
23.
4.8
30.
2.4 15.
2.4 15.
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Enclosure
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Rejection
Number
(1)
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Discrepancy Corrective Action
A229174 R/H and L/H Flaps. Flap carriage Remove 12 bolts; install bondings.
to tracks; bondings are worn and
broken.
A229175 L/H Flap Bay. Two stringers Stop drill cracks; repair in ac-
cracked at inboard flap track of cordance with -3.
outboard flap.
A229176 L/H Flap Bay. At inboard flap
bay area next to trailing edge
about 15 rivets loose.
Remove loose rivets; install new
ones.
A229177 R/H and L/H Flap Carriage. 10 Remove old bearings; install new
each of the small bearings on ones.
leading edge and bottom are rough
and some will not turn.
A229178 R/H and L/H Flap Carriage. 10 Remove old bearings; install new
of the carriage track side ones.
bearings are rough and some
will not turn.
A229179 Engine Cowling R/H Air Scoop.
Two ribs inside of airscoop
has corrosion (top and bottom).
A229180 Engine Cowling R/H Air Scoop.
R/H side of scoop metal is bent
at hinge bracket.
Remove air scoop assembly from
cowling; open and resubmit.
Straighten and smooth up.
Manhours
Labor Cost
14.4
$ 90.
4.8
30.
4.8
30.
24.1
151.
12.0
75.
19.2
120.
2.4
15.
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Enclosure (1)
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Rejection
Number
A229181
A229182.
A229183
A229184
A229185
A229186
A229187
A229188
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Discrepancy
Engine Cowling Exhaust. R/H
Outboard center rub strip missing
and two small cracks at forward
brackets.
R/H Inboard R/H Engine Exhaust
Cowling. Three old welds cracked
and rub strip missing. Also,
several screw heads burned.
L/H Engine Exhaust Cowling. Rub
strip missing on two cowlings.
L/H Ergine Exhaust Cowling. In-
board bottom cowling cracked.
Close Out Panel, Aft of Engine.
Four rivets loose in center of
panel.
R/H Prop Cowling. (Three each).
Fastener head burred out; fastener
missing; two loose rivets and
three cracks.
Corrective Action
Install rub strips and rivets;
weld two cracks at brackets.
Weld cracks and smooth up;
install rub strip; replace
damaged screws.
Install rub strips on cowling.
Straighten cowling; trim off
damaged area and smooth up.
Remove loose rivets; install
new ones.
Remove loose rivets and damaged
fasteners; replace with new ones;
drill cracks and install -3
repair
L/H Engine Cowling. Several small Trim off damaged skin and smooth
-cracks along the-edge of cowling up.
and one large crack inside.
L/H Engine Cowling. Bonding-
broken and seals torn on cowl
flap.
Remove bondings and seals; in-
stall new ones.
Manhours
7.2
7.2
.8
3.6
1 .2
8.4
2.4
6.0
Labor Cost
$ 45.
45.
30.
23.
8.
53.
15.
38.
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Enclosure (1)
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Rejection
Number
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Discrepancy �Corrective Action
A229189 L/H Engine Cowling. Two rivets
loose in repair and small crack
at forward inside latch of cowling.
Remove old repair; stop drill
crack; install -3 repair.
Manhours
Labor Cost
9.6 $ 60.
A229190 R/H Engine Cowling. Rubber rub Remove torn strip; install new 4.8 30.
strip center inside cowling is strip and bumper washer.
torn and rubber bumper washer
missing.
A229191 R/H Engine Cowling. Repair Remove old repair; install -3 9.6 60.
loose at both latches, forward repair; stop drill cracks and
end and inside. Also, crack install -3 repair.
inside of latches.
A229192 R/H Engine Cowling. Two cowl
flap rubber seals are torn and
bonding broken.
A229193 R/H Engine Cowling. One edge
of cowling has small crack;
bent at trailing edge;center
skin is worn,
A229194 L/H Engine Cowling. Rubber
washer bumper missing and rubber
seal on cowl flap is torn and
worn.
Remove damaged seals and bonding;
install new seals and bonding.
Trim off damaged skin and smooth
up.
Remove washer and damaged seal;
install new washer and seal.
A229195 L/H Engine Cowling. Bondings Remove damaged bondings; re-
on cowl flap broken. place with new ones.
4.8 30.
1.2 8
6.0 38.
1.2 8
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Enclosure (1)
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Reject ion
Number
A229196
A229197
A229198
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Discrepancy Corrective Action
L/H Engine Cowling. Repair Angle Stop drill crack; install -3
is cracked aft end at latch. repair.
L/H Engine Cowling. Latch lever Oil latch mechanism and free up.
for lock pin is hard to turn.
L/H Engine Cowling. Several Remove loose rivets; install new
rivets loose throughout side skin ones.
at latches.
A229I99 L/H Engine Cowling. Skin cracked Stop drill cracks; repair in
and bent at both forward inside accordance with -3.
latches,
Manhours Labor Cost
9.6 $ 60.
1.2 8.
3.6 23.
19.2 120.
A229204 L/H Engine Cowling. Safety pin Install safety pin. 2.4 15.
is missing in hold open latch
rod.
A229205 R/H Engine Cowling. Pin is Install pin. 2.4 15.
missing in hold open cowling
rod.
A229206 R/H Engine Cowling for Oil Remove loose rivets; install 3.6 23. 410
Cooler. About six loose rivets new ones.
in cowling both sides at for-
ward end. (Outside skin).
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Enclosure (1)
Page 6
Rejection
Number Discrepancy Corrective Action Manhours Labor Cost
A229207
A229208
A229209
A229210
L/H Engine Cowling Air Intake. Remove air scoop assembly from 19.2 $ 120.
Corrosion under several fittings cowl; open and resubmit.
and under two webs inside air
intake.
L/H Engine Cowling Air Intake. Remove damaged seals; install
Rubber seal torn on both sides. new ones.
L/H Engine Cowling Oil Cooler. Remove loose rivets; install
Several loose rivets forward new ones.
end on both sides. (Outside).
L/H Engine Cowling Air Intake. Remove damaged hose; install
Rubber hose is damaged, aft new one.
end.
A229211 R/H Engine Cowling Oil Cooler. Remove raw stock from inside
Raw stock inside cowling. cowling.
A229212 L/H Engine Cowling Oil Cooler. Remove raw stock from inside
Raw stock inside cowling. cowling.
A229213 L/H Engine Cowling. Aft Stop drill crack; trim off
corner is cracked and bent, damaged area and smooth up.
A229214 L/H Engine Cowling. Safety Install safety pin.
pin is missing in hold open rod.
A229215 L/H Engine Cowling. Handle is Oil handle and lock pins and
hard to turn for lock pins. - free up.
Also, pins are rusted.
4.8
30.
3.6
23.
2.4
15.
1.2
8.
1.2
8.
2.4
15.
2.4
15.
2.4
15.
ilk
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-.Enclosure (1)
Page :7-
Rejection
Number
, A229216
A350861
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Discrepancy Corrective Action
L/H Engine Cowling. Skin is
cracked in several places and
torn at forward inside latch.
R/H Wheel Well. Shock mount
for air blower for AC generator
is damaged.
Stop Drill cracks; repair in
accordance with -3.
Manhours
9.6
Remove shock mounts; install 14.4
new ones and align unit.
Total Direct Labor Costs
Material (Estimated)
$200.
Material Burden
20.
G4-A on Materials
28.
Total Material
Labor Costs
$ 60.
90.
294.1 $1,846.
$ 21+8.
Other Direct Costs-Premium Pay 153.
Total Estim
r--,,
FixeA Fee t 8%
$2,247. ----
180. �111,
Total Estimated Cost and FO $22427.
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