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VSP-68

September 10, 1986

A LEAR SIEGLER COMPANY

S/M

VENDOR SERVICE PUBLICATION

TO: All Affected Owners/Operators, Piper Distributors,

Factory Direct Dealers and Piper Field Service Facilities

SUBJECT:

Teledyne Continental Motors Service Bulletin M86-12

MODELS AFFECTED.:

PA-28-201T Turbo Dakota

PA-28R-201T Turbo Arrow III

PA-28RT-201T Turbo Arrow IV

PA-34-200T Seneca II

PA-34-220T Seneca III

PA-46-310P Malibu

SERIAL NUMBERSAFFECTED:

28-7921001 through 2807921091

28R-7703001 through 28R-7803372

28R-7931001 and up

34-7570001 through 34-8170092

34-8133001 and up

46-8408001 and up

PURPOSE:

To distribute Teledyne Continental Motors

Service Bulletin M86-12 to all affected Owners/Operators, Piper Distributors,

Factory Direct Dealers and Piper Field Service Facilities.

Detailed information is contained in the attached publication. Pay particular

attention to the note on Page 2, excluding X/C11 Aviation Oil from the

listing of approved oils.

NOTE: Ispropyl alcohol as a fuel additive is not approved by Piper Aircraft.

In the above listed aircraft, when an anti-icing additive is used, it

must conform to Mil-1-27686 and be properly blended in concentrations

not to exceed 0.15% by volume.

PIPER AIRCRAFT CORPORATION 2926 PIPER DRIVE. VERO BEACH, FL 32960 . (305) 567-4361

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TELEDYNE CONTINENTAL@ AIRCRAFT ENGINE

service bulletin

22 July 1986

SUBJECT: RECOMMENDED FUEL AND OIL GRADES

MODELS

AFFECTED: All

Minimum

Fuel

Grade

A Series 80

C Series

80

E Series 80

FSO-526A

100/100LL

R-670, W-670 80

O-200 & O-300 Series 80

GO-300 Series

80

IO-346 Series

100/100LL

IO-360 Series 100/100LL

TSIO-360 Series 100/100LL

LTSIO-360 Series

100/100LL

o-470-4, 11, 13, 13A, 15 80

0-470A,E,J,K,L,R,S 80

0-470B,G,H,M,N,P,

G-Cl ,U 100/100LL

IO-470J,K 80

IO-470 Series

(Except J & K)

100/100LL

TSIO-470 Series 100/100LL

GIO-470 Series

100/100LL

IO-520 Series

100/100LL

TSIO-520 Series

100/100LL

GTSIO-520 Series 100/100LL

IO-550 Series

100/100LL

6-285 Series 100/100LL

I

AMBIENT AIR TEMPERATURE TO

SELECT SINGLE VISCOSITY GRADE OIL

Recomd.

Below 40 F.

Above 40 F.

Minimum

Take-Off

Avia.

SAE

Avia. SAE

Oil Temp. Grade

Max.

Grade

Min.

75O F. 65 30 80 40

75OF. 65 30 80

40

75F. 65 30

100 50

75 F.

65 30

100 50

75F. 65 30 100 50

75O F.

65 30 80

40

75 F. 65 30 80

40

75 F.

65

30 100

50

75 F. 65 30 100

50

100 F.

65

30 100

50

lOOoF. 65 30 100

50

75 F.

65 30

100

50

75F. 65 30 100 50

75O F. 65 30 100 50

75 F. 65 30 100 50

75F. 65 30 100

50

lOOoF. 65 30

100

50

75O F.

65 30

100

50

75F. 65 30

100

50

lOOoF. 65 30

100

50

lOOoF. 65 30

100

50

75F. 65 30

100

50

100 F. 65 30 100 50

AMBIENT AIR TEMPERATURE TO

SELECT MULTI VISCOSITY GRADE OIL

Below 40 F.

Above 40 F.

SAE

SAE

10w-30

15w-50

15w-50

2OW-50

2OW-50

2OW-60

: .

When operating temperatures overlap indicated ranges, use the lighter grade of oil.

All Series Engine

@TELEDYNE INDUSTRIES. INC. 1986

TELEDYNE CONTINENTAL MOT

Aircraft Products Division

P. 0. Box 90 I MoblIe. Alabama 3

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22 July 1986

Page 2

* M86;1

When checking oil level remove dipstick and wipe with a lint free cloth. Replace dipstick insuring th

it is all the way in and locked. Remove dipstick and check oil level, fill to mark as indicated.

Use only lubricating oils conforming to TCM specification MHS-24C or D, lubricating oil, ashles

dispersant. The marketers of the aviation lubricating oils listed betow have sup,plied data to TC

indicating their products conform to all the requirements of TCM Specification MHS-24C or D

In listing the product names, TCM makes no claim of verification of marketers statementsor claim

Listing is made in the order in which the data was received by TCM and is provided only for t

convenience of the users.

NOTE . . . Since the airframe manufacturer furnishes certain parts which depend on engine oil f

lubrication, they may restrict the use of some lubricating oils.

Supplier

Brand

BP Oil Corporation

Castrol Limited (Australia)

Chevron U.S.A., Inc.

Continental Oil

Delta Petroleum Company

Exxon Company, U.S.A.

Gulf Oil Company

Mobil Oil Company

Mobil Oil Company

Pennzoil Company

Phillips Petroleum Company

Phillips Petroleum Company

Quaker State Oil 8 Refining Co.

Red Ram Limited (Canada)

Shell Canada Limited

Shell Oil Company

Sinclair Oil Company

Texaco, Inc.

Union Oil Company of California

BP Aero Oil

Castrolaero AD Oil

Chevron Aero Oil

Conco Aero S

Delta Avoil Oil

Exxon Aviation Oil EE

Gulfpride Aviation AD

Mobil Aero Oil

Mobil Aero Super Oil SAE 2OW-50

Pennzoil Aircraft Engine Oil

Phillips 66 Aviation Oil, Type A

l

X/C Aviation Multiviscosity Oil

SAE 2OW-50, SAE 2OW-60

Quaker State AD Aviation Engine Oil

Red Ram X/C Aviation Oil 2OW-050

Aeroshell Oil W, Aeroshell Oil W 15W-50

Aeroshell Oil W, Aeroshell Oil W 15W-50

Sinclair Avoil

Texaco Aircraft Engine Oil - Premium AD

Union Aircraft Engine Oil HD

*NOTE . . .

This does not include X/C II Aviation Oil.

NOTE . . .

The following procedures and schedules are recommended for engines which a

subjected to normal operation. If the aircraft is exposed to severe conditions, such as training

extreme weather, or infrequent operation, inspections should be more comprehensive and t

hourly intervals should be decreased.

To promote faster ring seating and oil control, a straight mineral oil conforming to MIL-L-608

should be used for the first 25 hours of operation of a new, rebuilt or overhauled engine. Following

this period we recommend changing to an ashless dispersant oil conforming to TCM Specification

MHS-24C or D. Since there is a possibility of widely dispersed metal flakes and lint showing up in t

first oil change, we recommend that the oil filter a lso be changed at this time.

WARNING

. . . Many new aircraft are delivered with a corrosion preventive oil conforming to MIL-C

6529 Type II which is a straight mineral oil with a corrosion preventive compound added. Since th

type oil can cause engine coking wlth extetded use, it should not be used after the first 25 hours

operation, or 6 months, whichever comes first.

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22

JuIy 1986

Page 3

The recommended oil change interval on engines without full flow oil filters is every 25 hours o

operation depending on dust, humidity and engine condition, or every six months, whichever comes

first. When using larger (approximately 5.80 high) full flow oil filters, the recommended number o

operating hours between oil changes and filters can be increased to 100 hours. However, on engines

equipped with smaller full flow filters (approximately 4.80 high) the filter should be changed each

50 hours.

The above recommendations apply to engines which incorporate the oil filters approved and

supplied by TCM.

With respect to Continental engine Model W670-23 after each 100 hours of operation, check the

battery ignition distributor drive adapter for oil supply. The adapter should carry 20 to 30CC

(approximately one fluid ounce) of Lubri-Plate No. 8 or SAE No. 600W oil. Inspect and fill through the

upper adapter plug.

On engines so equipped, the oil screen must be inspected and cleaned at each oil change. This fine

mesh screen filters out carbon and other particles from the lubricating system.

Full flow filters should be opened and inspected for contaminants at each filter change.

New engines frequently show widely dispersed metal flakes and lint on the first oil changes. This

should begin to progressively diminish and finally d isappear after a few oil changes. However, i

large amounts of metal are apparent on any oil change, it is an indication of possible malfunction and

should be investigated thoroughly.

There are many fuel and oil additives and/or concentrates on the market today which were

formulated primarily for automotive and industrial engine applications. From time to time, we

receive inquiries as to the use of these products in our aircraft engines. Most of these additives and

concentrates, while they may be highly beneficial to automotive and industrial operation, are not

compatible with air-cooled, light aircraft engines in their operating environments. With the

exception of the use of isopropyl alcohol and ethylene glycol monomethyl ether compound as

described in the following paragraph, we do not recommend the use of additives or concentrates in

any of our aircraft engines. In fact, the use of such can be cause for voiding the warranty. Use only

fuels and lubricants as recommended herein and in current engine operating manuals.

Under certain ambient conditions of temperature/humidity, water can be supported in the fuel in

sufficient quantities to create restrictive ice formation along various segments of fuel system. To

alleviate the possibility of this occurring, it is permissible to add Isopropyl Alcohol to the.fuel supply

in quantities not to exceed 3 percent of the total. Also, ethylene glycol monomethyl ether com-

pounds conforming to military specification MIL-I-27686E, if approved for use in the aircraft fuel

system by the aircraft manufacturer, may be added for this purpose. The ethylene glycol

monomethyl ether compound must be carefully mixed with the fuel in concentrations not to exceed

0.15 percent by volume.

WARNING

. . . Mixing of the EGME compound wlth the fuel Is extremely Important because concen-

tration In excess o f that recommended (0.15 percent volume maximum) can have a harmful effect on

engine components. Use only blending equipment that Is recommended by the manufacturer to

obtain proper proportioning.

All TCM aircraft engines are to be operated only on aviation grade fuel. If the specified fuel is not

available, the next higher grade fuel must be used. For further information with respectto useof low

lead grade 100 fuel in engines rated on grade 80, see TCM Service Bulletin M77-3.

I

WARNING . . ,

Automotive fuels are NOT TCM APPROVED for use In aircraft engines.

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VSP-69

September 12,

1986

S/M

VENDOR SERVICE PUBLICATION

TO: All Owners/Operators, Piper Distributors, Factory Direct

Dealers and Piper Field Service Facilities

SUBJECT:

Bendix Service Bulletin No. 629

MODELS AFFECTED: SERIAL NUMBERSAFFECTED:

PA-23-250 Aztec

PA-24-260 Comanche

PA-28-201T

Turbo Dakota

PA-28R-201T Turbo Arrow III

PA-28RT-201T Turbo Arrow

IV

27-01 through 27-8154030

24-3642 through 24-6000

28-7921001

through

28-7921091

28R-7703001 through 28R-7803372

28R-7931001

through 28R-8631001,

and 28R-8631005

31-05 through

31-8312019

31-5001 through 31-8452021

31P-03 through 31P-7730012

31-8253001 through 31-8553002

31-8414001

through 31-8414050

32-7887001 through 32-7987126

32-8024001 through 32-8424002

32-8029001

through 32-8629005

34-7570001 through

34-8170092

34-8133001 through 34-8633021

61-0001-004 through 61-0880-8162157

61P-0157-001 through 61P-0860-8163455

62P-0750-8165001 through 62P-0861-81650

through

62P-0932-8165055

and

60-8265001 through 60-8365021

60-8423001 through 60-8423025

PA-31-310/325 Navajo

PA-31-350 Navajo Chieftain

PA-31P Pressurized Navajo

PA-31-350 T-1020

PA-31P-350 Mojave

PA-32RT-300T Turbo Lance

II

PA-32-301T Turbo Saratoga

PA-32R-301T

Turbo Saratoga S.P.

PA-34-200T Se.neca

II

PA-34-220T Seneca III

I

PA-60-601 Aerostar 601

PA-60-601P Aerostar 601P

PA-60-602P Aerostar 602P

PA-60-700P Aerostar 700P

PURPOSE: To distribute Bendix Service Bulletin No. 629

to all Owners/Operators, Piper Distributors, Factory Direct Dealers and Piper

Field Service Facilities.

The attached Bendix Service Bulletin may affect Bendix equipment installed

in the above listed Piper Airplanes.

Refer to the attached publication for

specific information regarding compliance.

PIPER AIRCRAFT CORPORATION 2926 PIPER DRIVE. VERO BEACH. FL 32960

l

(305) 567-4361

5/21/2018 Vendor Service Publication Tcm

6/6

VSP-69

September 12, 1986

A LEAR SIEGLER

COMPANY

S/M

VENDOR

SERVICE PUBLICATION

TO: All Owners/Operators,

Piper Distributors, Factory Direct

Dealers and Piper Field Service Facilities

SUBJECT:

Bendix Service Bulletin No. 629

MODELS AFFECTED:

SERIAL NUMBERSAFFECTED:--

PA-23-250 Aztec

PA-24-260 Comanche

PA-28-201T Turbo Dakota

PA-28R-201T Turbo Arrow

III

PA-28RT-201T Turbo Arrow

IV

PA-31-310/325 Navajo

PA-31-350 Navajo Chieftain

PA-31P Pressurized Navajo

PA-31-350 T-1020

PA-31P-350 Mojave

PA-32RT-300T Turbo Lance

II

PA-32-301T Turbo Saratoga

PA-32R-301T Turbo Saratoga S.P.

PA-34-200T Seneca

II

PA-34-220T Seneca III

f

PA-60-601 Aerostar 601

PA-60-601P Aerostar 601P

PA-60-602P Aerostar 602P

PA-60-700P Aerostar 700P

27-01 through 27-8154030

24-3642 through 24-6000

28-7921001 through 28-7921091

28R-7703001 through 28R-7803372

28R-7931001

through 28R-8631001,

and 28R-8631005

31-05 through

31-8312019

31-5001

through 31-8452021

31P-03 through 31P-7730012

31-8253001 through 31-8553002

31-841400.1

through 31-8414050

32-7887001 through 32-7987126

32-8024001 through 32-8424002

32-8029001 through 32-8629005

34-7570001 through 34-8170092

34-8133001 through 34-8633021

61-0001-004 through 61-0880-8162157

61P-0157-001

through 61P-0860-8163455

62P-0750-8165001 through 62P-0861-81650

through

62P-0932-8165055

and

60-8265001 through 60-8365021

60-8423001 through 60-8423025

PURPOSE:

To distribute Bendix Service Bulletin No. 629

to all Owners/Operators, Piper Distributors,

Factory Direct Dealers and Piper

Field Service Facilities.

The attached Bendix Service Bulletin may affect Bendix equipment installed

in the above listed Piper Airplanes.

Refer to the attached publication for

specific information regarding compliance.

PIPER AIRCRAFT CORPORATION 2926 PIPER DRIVE. VERO BEACH. FL 32960 . (305) 5674361