MAINTENANCE SERVICES ON SP2H AIRCRAFT; PROPOSAL FOR CORRECTION OF DISCREPANCIES

• Document Type: FOIA
• Collection: FOIA Collection
• Document Number (FOIA) /ESDN (CREST): 05751377
• Release Decision: RIPPUB
• Original Classification: U
• Document Page Count: 11
• Document Creation Date: March 9, 2023
• Document Release Date: February 10, 2021
• Case Number: F-2011-01575
• Publication Date: July 1, 1966

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REGISTERED
SUBJECT
TO
OSA 6
Post Office Box 490
Greenville, Texas
1 July 1966
In Reply Refer To:
8435-60320C-03
Maintenance Services on SP2H Aircraft;
Proposal for Correction of Discrepancies.
ATTENTION Contracting Officer
REFERENCE
ENCLOSURE
(b)(3)
Telephone Conversation, 23 June 1966,
Contracting Officer/Wilson and Lane.
Your Message No. AD1C 2100
Itemized Discrepancy List and Price Proposal.
This Contractor submits, as Enclosure (1) hereto, its formal cost plus
fixed fee proposal for the correction of basic airframe discrepancies
on one each SP2H aircraft. This proposal is presented in response to
our Reference (a) discussion on this subject and your Reference (b)
authorization to proceed under Contract JG-1968.
Enclosure (1) contains a detailed listing of discrepancies, proposed
corrective actions and labor cost estimate by line item. Material costs
are shown as a separate item representing our best estimate of expendable
and/or stock materials which are not normally furnished from Navy Supply.
Major repair and/or replacement parts will be requisitioned through
established supply sources.
GROUP I
EXCLUDED FRO TOMATIC
DAV DING AND
CLASSIFICATIOO
This Document contains ini,ymiition at ng. the National Defense of thh
United States eth rrr oroun nr LAA,S,. Title 18 U,
Sactions 79:i; nod Y,. to �imii,n or the revelation of Its nantants
Ili 'Any manner to an u norized person In prohibited by law.
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8435-60320C-03
1 July 1966'
' Page 2
Other Direct Costs (Premium Pay) was developed on the basis of an esti-
mated 100 manhours to be expended on overtime in order to accomplish
this task within the schedule framework. It is, therefore, requested
that the Task Order issued for this effort include authorization for
the expenditure of 100 overtime manhours.
Labor rates, overhead and general and administrative factors utilized
in developing cost and fee price are in accordance with the rates
negotiated for the basic maintenance program.
We trust the above will be favorably received and a Task Order will be
received at an early date.
CFW:lw
encl.
cc: H. Chapman
K. arr, Jr.
ontroller
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ENCLOSURE (1)
ITEMIZED DISCREPANCY LIST AND PRICE PROPOSAL
Rejection
Number
A228573
A228575
A228576
A228577
Discrepancy
Hydraulic Hose. Change all hyd.
hose in accordance with 42E1-1-501;
engine, nose, wheel well and both
main wheel well areas.
R/H Main Wheel Well. Outboard
wheel well door has a crack,
forward end at bracket.
R/H Main Wheel Well. Inboard
door. Five blind NAS rivets
-ggramk
are lo i ose in repaired area of
door.
R/H Main Wheel Well. Outboard
door forward end and outside
skin. Four cracks.
A228578 R/H- Main Wheel Well. Cottes_KFv_
mi_ssina_on center bolt of inboard
.gear door.
A228579
A228580
R/H Main Wheel Well. Air duct
for AC generator clamp missing
below AC generator.
L/H Bomb Bay Door. Four rib
brackets cracked. Also rib
strap cracked in one place.
Corrective Action
Remove hyd. hose (16 each) in
referenced areas. Replace with
new hose. Pressure check
systems.
Stop drill crack; install doubler;
pick up existing rivets; add rivets
equally spaced as required.
Remove loose rivets and replace
with new blind. rivets.
Trim off damaged skin; smooth
up and prime.
Tighten bolt and align hole;
install cotter pin.
Install clamp and torque to
required limits.
Stop drill cracks; install angle
doublers nested inside ribs;
pick up existing rivets and add
required rivets.
Manhours
134.9
19.2
Labor Cost
$ 844.
120.
4.8 -)ed 30.
2.4
1.2
19.2
15.
8.
8.
120.
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Enclosure
Page 2
Rejection
Number
A228581
A228582
A228583
A228584
A228585
A228586
A228587
A228588
(1)
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Discrepancy
Outside skin forward of L/H bomb
bay door hinge; 24 loose rivets..
R/H Bomb Bay Door. Two rib
brackets cracked on door.
R/H Bomb Bay Door. Outside skin
of door and aft end of door has
two cracks.
Bulkhead, Aft end of Bomb Bay.
R/H side. Two MS bolts loose and
no nut on them. Aft of bomb bay
door hinge.
Forward End of Bomb Bay, R/H Side.
Two ground studs rusted and cor-
roded on heater system.
BonbBay Doors. Several spots
corrosion on doors.
Corrective Action
Remove loose rivets; install new
rivets.
Stop drill cracks; install angle
doublers nested inside ribs; pick
up existing rivet pattern and add
required rivets.
Stop drill cracks; trim off rough
skin; smooth up and prime.
Install nuts on two existing MS
bolts and tighten.
Remove two studs; clean and treat
contact surface; reinstall new
studs and functional test.
of Spot strip; paint in affected
areas; clean; treat and prime.
L/H Main Wheel Well. Angle
cracked on outbd. door, forward
end inside.
L/H Main Wheel Well. Rubber seal
is torn and parts of it missing
inside wheel well and on forward
bulkhead.
Stop drill crack; install S/M
doubler with AD-4 rivets equal
spaces one inch on center.
Remove damaged seal; reinstall
new seal.
Manhours
96.0
Labor Cost
$ 38.
601.
2.4
15.
1.2
8.
2.4
15.
14.4
90.
4.8
30.
2.4
15.
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Enclosure
Page 3
Rejection
Number
A228589
A228590
A228591
A228592
A228593
(i)
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Discrepancy Corrective Action
Oil Cooler Actuator. Door seal is Remove damaged seal; reinstall
torn and deteriorated, new seal.
L/H Main Wheel Well. Interphone Repair harness assemblies; re-
"J" box wires have been cut into, install and functional test.
just aft of "J" box.
L/H Main Wheel Well. Adell broken Remove bronken adel; reinstall 1.2
on hydraulic pressure line, forward new adel.
inboard side.
Nose Tunnel. Lord mount deteri-
orated and one rubber is torn at
autopilot fuse box.
Nose Tunnel. Several screws
missing on inboard side curtain
at top.
Remove damaged mounts; reinstall
new mounts.
Install metal screws in retaining
strip on curtain.
4.8 30.
2.4
15.
A228594 Nose Wheel Well. Landing light Protect wiring (Circo) and secure 2.4 15.
wires fouls mount bracket and by adel or string ties to clear.
they are worn.
A228595
A228596
A228597
Nose Wheel Well. Corrosion on
Stop strip; paint in corroded areas; 7.2 45,
forward bulkhead, clean; treat and prime.
Nose Wheel Well. Seal is broken
loose around wires going into
downlock microswitch.
Reseal wiring around microswitch.
1.2 8.
APS-20 Antenna Area. There is Remove brackets; clean and treat 4.8 30.
corrosion under four mount brackets. affected areas; reinstall brackets
and antenna.
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Enclosure
Page 4
Rejection
Number
A228598
A228599
A228600
A228601
A228602
A228603
A228604
( )
Discrepancy
Nose Wheel Well. Accumulator has
corrosion.
Radar Compartment. Accumulator
in top of compartment has cor-
rosion.
R/H Aileron. Trim tab bearings
and bolts rusted. Bonding strip
broken.
R/H Aileron. Aileron bearing
and bolts are rusted.
R/H Wing Bottom. Camera pod
receptacle is corroded at plug
mount.
R/H Wing Bottom. Six rivets
loose in flap bay skin outboard
of flap.
R/H Wing Bottom. Five fabric
patches are missing over re-
ceptacle aft of rocket pod.
Corrective Action
Remove accumulator; clean; treat
corrosion and reinstall.
Clean and treat top forward ac-
cumulator; remove forward lower
accumulator; clean; treat and
reinstall.
Remove tab from aileron; remove
old bearings, install new ones;
reinstall tab on aileron.
Remove aileron; remove old
bearings; install new ones.
Reinstall aileron rig con-
trols.
Remove receptacle; clean and
treat skin adjacent to unit;
install new receptacle and
functional test.
Remove loose rivets; install
new rivets.
Install five fabric patches over
receptacles on ppd.
Manhours
14.4
$ 90.
14.4
90.
9.6
60,
55.4
347.
9.6
60.
2.4
2.4
15.
15.
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Enclosure (1)
Page 5
Rejection
Number
A228605
A228606
A228607
A228608
A228609
A228610
A228611
A228612
A228613
Discrepancy
R/H Wing Bottom. Four rivets off
in leading edge of wing outboard
of rocket pods.
R/H Flap. Cherry rivet loose in
repair inboard end on top of out-
board flap.
R/H Wing Top. Two rivets loose at
each flap track on top.
R/H Inboard Flap. One rivet loose
in top skin of flap about center.
R/H Wing Top. Several rivets loose
in skin over inboard flap bay.
R/H Inboard Flap. Crack in bottom
skin and four rivets have worn
through skin next to trailing edge.
No. 2 Engine Cowling. Outboard
cable assembly is missing on
lower engine cowling.
Static Dischargers. Static dis-
chargers are too short and
materials around them are hard
and dete-riorated.
L/H Wing Top. Two rivets loose
at aileron flap track at trailing
edge.
�
Corrective Action
Remove leading edge and repair.
Remove old rivet; install new one.
Manhours
19.2
Labor Cost
$ 120.
15.
Remove loose rivets in four flap
tracks; install new ones.
6.0
38.
Remove old rivet; replace with new.
1.2
8.
Remove approximately 35 rivets and
19.2
120.
install new ones.
Open skin for access and repair.
Remove housing assembly (sleeve);
install cable assembly; reinstall
housing assembly.
Remove old static dischargers on
all surface controls; reinstall
new ones (16 each).
Remove old rivets; reinstall new
rivets.
7.2
19.2
9.6
2.4
45.
120.
60.
15.
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Enclosure (1)
Page 6
Rejection
Number
A228614
A228615
A228616
A228617
A228618
A228619
A228620
A228621
A228622
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Discrepancy
L/H Flaps. Several loose rivets
in both flaps, top and bottom.
L/H Wing Bottom. Six rivets loose
on outboard flap bay skin.
L/H Aileron. Aileron bearing and
bolt rusted.
L/H Aileron. Tab bearing and
bolts are rusted.
Aileron Tab. Both L/H and R/H
tab hinge cover deteriorated
and torn.
Crew Compartment. Handle is
missing top side of door that opens
into the crew compartment from
tunnel.
L/H Wing Bottom. At flap bay
several small cracks at rivets
forward edge of flap bay, in-
Corrective Action
Remove old rivets; reinstall
new rivets.
Remove old rivets; reinstall
new rivets.
Remove aileron; remove old bearings;
reinstall new or serviceable ones;
reinstall aileron; rig controls.
Remove tab from aileron; remove
old bearings; reinstall new ones;
reinstall tab on aileron.
Remove old tab covers; reinstall
new covers.
Remove pin and install new handle.
Stop drill cracks; install S/M
doubler and reinstall rivets.
Manhours
Labor Cost
6.0
$ 38.
3.6
23.
55.4
347.
9.6
60.
14.4
90.
1.2
8.
4.8
30.
board end.
L/H Flap Bay. Two loose rivets
at inboard end of bay.
Remov loose rivets; replace with
new blind rivets.
1.2
8
No. 1 Jet Cowling L/H. Several
cracks inside of jet cowling,
Remove cowling; stop drill cracks;
repair in accordance with AN-01-
84.0
526.
both sides.
75EEB-3, Sect. VI, Fig. 6-17E,
Page 198B-1 (13 each repairs).
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Enclosure (1)
Page 7
Rejection
Number
A228623
A228624
A229152
A229153
A229154
A229155
A229156
A229157
Discrepancy
No. 2 Jet Cowling RIP-I. Several
cracks inside of cowling, both
sides.
No. 1 Jet Pod L/H. Coating on
leading edge at bottom pealing
off.
Cockpit. Two fabric patches
are torn and deteriorated outside
between hatches.
Cockpit. At co-pilot's hatch
metal strip around hatch seal is
torn and bent.
Cockpit. Four rivets pulled
through metal strip on door in-
board of co-pilot's seat in floor.
L/H Wing. Several rivets have
worn through skin outboard of
No. 1 engine on leading edge.
No. I Engine. Two bad P.R.T.
No. 2 Engine. Two bad P.R.T.
Inboard top and bottom.
Corrective Action
Remove cowling; stop drill cracks;
repair in accordance with AN-01-
75EEB-3, Sect. VI, Fig. 6-17E,
Page 198B-1 (11 repairs)
Refinish pod in accordance with
BuWeps Report No. 10360.3.
Install new fabric patches.
Remove metal strip; straighten;
smooth up; cut away damage;
rein'stall and paint.
Remove metal strip; straighten;
smooth up; reinstall strip and
step up rivets one size in area
where hole enlarged.
Remove access cover and resubmit.
Remove old turbine; install
serviceable unit; check at engine
run up.
Remove old turbine; reinstall
serviceable unit..Note: to be
checked (operationally) during
engine run and flight test.
Manhours
72.0
19.2
2.4
7.2
4.8
2.4
14.4
Labor Cost
$ 451.
120.
15.
45.
30.
15.
90.
90.
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Enclosure (1)
Page 8
Rejectjpn
Number
A229158
A229159
A229160
A229161
A229162
A229163.
Discrepancy Corrective Action
R/H and L/H Varicam Bearing.
Bearings show to be frozen.
Bearings have worn bolt.
Remove varicam (two); remove
old-bearings; install new
bearings; reinstall units.
Varicam Assembly. Skin is bent Stop drill crack; smooth up area;
and cracked next to outboard hinge radius out damaged spot.
on top, L/H.
Varicam Assembly L/H. Two screws Remove damaged screws and install
loose in inspection door to elevator new screws.
hinges.
Manhours Labor Cost
67.4 $ 422.
2.4 15.
1.2 8.
Rudder. Bearing of rudder rusted. Remove rudder; remove old bearings; 55.4 347.
install new bearings; reinstall
rudder, rig controls.
R/H Horizontal Stabilizer. Fabric
drain hole patch missing bottom
side next to fuselage.
Rocket Pod Area. Under both
wings electrical receptacle (eight
each) broken aft of all rocket pod
in flap bay rocket igniters.
A229164 Oxygen Regulator Lights. Light
covers missing (six each lamp
assembly covers, P/N A-2362B).
Install fabric patch.
1.2 8.
Remove broken receptacle; install 14.4 90.
new units.
Install new light covers. (Six
each).
Total Direct Labor Costs
3.6 23.
1,003.3 $6,285.
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Enclosure (1)
Page 9
Total Direct Labor Costs
Material (Estimated) $300.
Material Burden and G&A 34.
Total Material Cost
Other Direct Costs - Premium Pay
Total Estimated Cost
Fixed Fee @ 8%
$ 6 , 285 .
334 .
17k.
$ 6,793.
543 .
Total Estimated Cost and Fee $ 7,336.
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