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fiNQ A';;TFTFnSECURITY CLASSIFICATION OF THIS PAGE (Wg,.n Dots Itntereel

REPOR DOCMENTTIONPAGEREAD INSTRUCTIO14SREPOT DCUMNTATON AGEACCESIO NO BEFORe. COMPLETING FORMI.REPORT NUMSER 2. .3OVT ACESO O .RECIPIENT'S CATALOG NUMBER

76-9 ______________

%-5A la RteMauaFinal,/epo .ts C

'~ 58AFla Rae Mnua~ ~1 Jan 70-31 Dec 73,

-fPVVWMVV REPOR U ECR

I. NTRACT OR GRANT NUMSER(o)Harold W./Suphin /i AJl72Aj7(.C

9. PERFORMING ORGANIZATION NAME AND ADDRESS 10. PROGRAM ELEMENT. PROJECT. TAS.AREA & WORKC UNITNUERParks College of St. Louis University

Cahokia, IL 62206 5L FFC NýME bAND ADRESS :wMar DATE 4

S steins Performance Assessment Div (DRSAV-LS)ff'x 9MO. 6316614

14. MONITORING AGENCY NAME & AOORESS(if different from Cf.,iroilind Office) IS. SECURITY CLASS. (of this report)

7t 7S~fiUNCLASSIFIEDI~.OECLASI I CATION/ DOWN GRAOINCSCHEUL

Approved for. Public ReleaseDistributn Unlimited,

t&fract entered In iffork 20. It dlifferent from Revert)

If. SUJPPLEMENTARY N03TES

13. 99y WORDS (Coioeiau ant revaa aide if noeeeawa"g mid dmifify by 10 0weob nmr)

Flat Rate Data Tasks TimesMaintenance Man-hour Times TAMMS 2407 DataMan-hour Frequencies 014-58A Maintenance DataMan-hour Distributions

2 AtSuMAC? (Cesillwas towereef s ide if neses" aaa~d fdowgifp, ""a vea o)

The purpose of thi's Flat Rate Manual is to provide statistical man-hour* fparameters for the performance of tasks involved at the Organizational, 0ire(

and General maintenance' levels for the-Oh-58A aircraft. It is intendedi forevaluating and predicting maintenance requirements and/or comparing thePerformance of an activity against a recognized standard.

00 1 A 1473 to~l"O" OF itW so6s110304Lai UNCLASSIFIEDJ.'ilICURIIY CLA&UPICATION OF THIS PAG8t(019eneatoa8

*X ,

PREFACE

This publication is an updated version of the original

CH-58A (Aumi.st 1973) Flat Rate Manual. It is a result of

four years of data editing and validation procedures of

TAERS/TAI4W data through developmlent of ADP programs within

the RAI.IIT system. Manuals that have been published include

AH-lG (July 1973), CH-J47A (December 19Th) and TUH-,1H (July 1975).

- D.C.

NNO

777-=7

TABLE OF CONTENTS

Listing FigiurESection Page Nl_ bpl

T. Introduction1.1 Purpose 11.2 Scope and Limitations I1.3 ?!ethods 2

TI. Scheduled Maintenance Adtions Against End Item 7Aircraft (Daily and Periodic)

III. Functional Group 01 - Airframe System 9Covers and Loose Equipment 10Auxiliary Installations 1] 2Arm.ament Provisions Installations 17 3Fuselage Assembly 19 hCrew Door Installation 22Passenger Door Installation 25 6Fuselage Structure Assembly 28Fuselage Structure Assembly 30 8Nose' Installation 32 9Console Installation 34 IG,Crew Door Jettison Installation 36 |IConsole Cover and Bulkhead Installation Seat .8Fassenger Seat Panel Installation 4o I"Pylon Support Installation 4?!Bulkhead Installation 141 lAft Cabin Closure Installation 46 IfLower Cabin Shell Assembly 1,8Bulkhead Installation S0 UAft Fuselage Installation 52 1Aft Fuselage Installation 5.4. ""Tail Boom Installation 56 pStabilizer Installation * . 59Tail Boom Fin Installation ' - 61 2Engine Mount Installation . * 6h 2Cowl Installation 66 1Particle Separator and Fairing Assembly. 68 2Cowl Installation 71Passive Defense Installation .. ' . 76Soundproofing Installation ..... 78Crew Seating'and Restraint Installstioti 80Passenger's Seating and. Restraint Installation 814Nose and Tail Boom Ballast Instellation 87Cargo Platform 89Flyaway Items 91Miscellaneous Items 91

ii

,,_ _..,_

''F -~ #~i..27

ristinr giir(.Sect ion Page I h,,,

IV. Functional Group 02 - Landing Gear System 96Landing 'Gear Assembly 97 35

V. Finctional Group 01 - Power Plant System, 99Electrical System Assembly, Engine 100 36

Anti-Icing and Air Bleed System 102Fuel' System, Engine 0hPump Assembly, Fuel iO7 OTFlow Body Assembly and Related Parts 109 hoCompressor and Related Parts illCombustion System 113 1*.

Turbine Assembly, Gas (Power Turbine Rotor and Related 115Parts)

Gearbox, Cover, and Related Parts 117 hh.Gearbox Internal Oil System 119 ):,Engine Assembly 121 46Engine Assembly 123. 47Engine Anti-Icing Control Installation 129 48Freewheeling Assembly and Installation 131 49Bleed Air Installation 135 50Droop Compensator Cortrol Installation 137 51Gas Producer Control Installation 140 52Engine Oil System Installation 142 51Miscellaneous Items AB8

VI. Functional Group 04 - Transmissions, Drives and Rotors 150Pylon Installation 151 5)Rain Rotor Hub and Blade Installation 156 55Main Rotor Hlub Assembly 160 56Transmission Installation 165 57Transmission Assembly 168 58Transmission Assembly 170 59Transmission Oil Cooler Duct Installation 175 60Engine to Transmission Drive Shaft Assembly and

Installation - 17T 61Tail Rotor Drive Shaft Installation 180 62Tail Rotor Gearbox Assembly .189 63Tail Rotor Installation 1928 65

- Tail Rotor Hub and Blade Assembly .. . 65Miscellaneous Items 202

VII.. Functional Group 06 - Hydraulic System .205Flight Controls Hydraulic System Installation. 206 66Flight Controls Hydraulic System Installation 208 67Solenoid Valve 211. 68Hydraulic System Reservoir Assembly 213 69Miscellaneous Items 215

ii'

Listing Fimgir,'Sect ion Page Nin__ "

VIII. Fiunctional Group 08 - Instrument and Instrument Panels 21'7Pilot's Standby Compass Installation 218 70Instrument Piping Installation 220 71Instrument Panel Installation 222 7TEngine Gage Unit 230 7

IX. Functional Group 09 - Electrical System 233Electrical Installation 23),Electrical Installation 236Electrical Installation 20"Electrical Installation '"Overhead Console Installation 2IR'Miscellaneous Items 250

X. Functional Group 10 - Fuel System 253Fuel System Installation 254 79*Fuel System Installation P57 8(,

XI. Functicnal Group 1i - Flight Control System 259Collective Controls Installaticn 260 8'cy.elio Controls Installation 262Cyclic Controls Installation 264. 83Antitorque System Controls Install&tion 266 8),Antitorque System Controls Installation 268 85Cyclic and Collective Controls Installation 270 86Cylinder and Support Assembly 27? R7Miscel]aneous Items ?7 1

XII. Functional Group 12 - Utility System 276Ram Air and Defogging Ventilation System Insta]lation .277Bleed Air Heater Installation 279 A(IM.'ixing Valve Assembly 281 9()Mis.ellaneous Items 281.

XII7. Functional Group 19 - Avionic System 285Miscellaneous Items 286

"XIV. Appendix A -,Index of Reported Federal StockNumbers (FSN's) or Part Numbers (PN's) 299

4 ..

" ,. i , B •, ,I, -,,• •- . , .• - . , , , ,,* , "-,,' , .. ... , , ; ,

SECTION 1I NTRODUCT ION

N1I

.1 .Pu rmose

T1e purposee 'f this Fl'tit. Rate Manual is t', provid, :,;tatiit. i eal

:nauh,"param"eters for the pert'rrnatice of" tasks involved at. the Orr'ani-

zational, Pirect and General Support maintenance leveq4;. A total (;,unI-

:.:.ati,-c: ,f *r-ýanizational and Direct Support) maintenance manhour pa'rit-

meter is qlso <i-.ven.

T7his manual specifies a standard hour parameter set for each type

maintenance action reported at these levels. It should be understood

that these are actual times, and may Include some non-productive hours

caused by a nr.unber of problems which may arise during the perforr.ance of

.aintenance. -Also, since ideal conditions do not exist in maintenance,

the data presehted does not represent the most efficient time possible

to perf'!'rm the work ir. question. It is Intended that this inf'ormatl.on

will provide a basis for:

a. Evaluating and predicting maintenance requirements.

b. Coompari.n the performance of an activity against a recof~nized

standard.

1.2 S'ýope and Limitations

The data provided in this manual is for the OH-.59A fleet. The

inform'.ation includes data on the number of manhours required to perform

specific maintenance actions.

The data used in the statistical analysis portion of the manual was

extracted from DA Form 2407 and 2408-3. All data provided at the Sup-

port Lcvel was extracted from DA Form, 2407 and all data for the Orprani-

zational Level was from DA Form A108-3. The Total Levc. combines the

,. . , . . ,"

two, sources o'f reporting, to provide an overall 'vie-w or maintenance

actions.

This data is limited to the degree of accurate reporting., of manhour

times by field personnel. Also, as mentioned before, the data dries

include non-productive hours resulting from a number of factors.

1.3 Methods

Data from DA Forms 2407 and 240O8-3 were assigned anin~b digit Work

Unit Code (WTJC). The WIJC presents a system, subsystem, component and

part breakdown of' those items upon which a s pecific maintenance aetions

had been reported. Also provided was the noun nomenclature of t~he items,

and the manhour frequencies at the Organization and Support Levels; and

a total figure set of these frequencies.

Tthe WUC also provided Federal Stock Numbers (7311's) and Part Numbers

(PI's) of those items selected. The basis for selection was made on the

f~llowiaig criteria:

a. Sufficient data to establishi manhour parameters.

b. Valid FSX or PN &lou.ld accompany the-item for the purpose or~

identification. Exceptions were made in cases where an item c~ould easily

be, identified on the illustration without the use of PH or FSN.

After selecting those items to be-presented In the Flat Rate-Manual,

the next step was to set high and low -limits on the manhour- frequenc I es

at all. levels of maintenance.* The purpose of setting limits on the data

was to eliminate some of the more widely scattered, manhour frequency,

-2-

The majority of limitattons were made on the basis of an "engineerinr

decision." With this te-hni,-,ue, those samples which had an obviously

erroneous ma.nhour entry cr seemed abnormai in'comparison to the other.data

within the :a-ple were eliminated. An example of thi-; procedure is as

"follows:

Manhour Value Frequen-y

lower Limit -)1.0 3

1.5 i4

2.0 5

Upper limit - 3.0 2

1O.C 1

Note that the manhours show an approximately normal distribution up

to 3 manhours where it then Jiumps to 10. The data for this item would be

limited at the lover end by 1.0 and the upper endby 3.0. Since there -as

only one "hit" at the 10 manhour interval, a decision was made that this

entry was abnormally high for the maintenance action performed and should

not be included to determine statistical parameters.

For those items with large manhour frequencies that could not be

limited by the previous method, an alternate method of statistical com-

putation was available. In this method, the mean and standard deviation

of the sample is found. From these parameters, one can calculate manhour

limits by adding either tuo or three standard deviations to the mean,

derendin4g upon the distribution of the samples and natural breaki in

the sequence of values.

"3-|

1>nsidering only the data between the high and low limits, the fol-

lowing, statistical parameters were calcu•ated for each item seleeted

and its corresponding action codes for each level of maintenance (total,

crganizational, direct and general support);

a. 'Mean - Average manhours to perform the maintenanoe ,actions in

quest itr. This parameter is calculatei by the followinr! formula:

-=Ef__x(Mean) x

where;

-fx Sum.mtion of manhour f;equency products

N =' Number of observations

b. Median - The manhour value which divides the frequency distribu-

tion so that one-half of the items are equal to or greater than it. The

advanrage of this parameter over the mean is that the extreme larre or

small values do. not influence its value as much as they would the mean.

Example: Considering the following distribution:

1, 2, 5, 6, 8, 10, 20

the Median would be (6) since there is an equal number of items on both

sides.

c. Mode - Manhour value most frequently encountered for any parti-

cular maintenance action. Again, the extreme values of the distribution

would not effect this parameter.

*t -I.-

* . - ' P

Example: Given the following manhour frequency distribution:

Manhour Value Frequency

1.0 10

Mode 1.5 25

2.0 14

2.5 11

10.0 4&

The Mode would be 1.5 manhours since it is the value with the

largest number of encounters.

d. Standard Deviation - This parameter is the measitre of the spread

of the manhour distribution about the mean. A small standard deviation il

comparison to the mean indicates that the average manhour value does not

fluctuate greatly among the reported samples, and the mean value is a

relatively accurate representation of the time required to perform the

given t.bak.

If the standard deviation is large in comparison to the mean, it

indicates that the reported manhour values are widely dispersed, and the

mean value should be used conservatively when estimating manpower require.

ments. This latter condition will occur when the manhour distributions

are skewed to tht right or left of the mean.

* The standard deviation is calculated by the following formula:

e. Sample Size - Sample Size is zhe total number of maintenance

encounters in each level within the limits set for the item. Since the

limits for the Total, Organizational and Support levels do not necessarilý

, 4 I ., " -5"

coincide due to the scattered distribution of the manhour frequencies,

the sum of the Organizational and Support samples may not equal the sample

size of the Total. Though some samples are extremely, small, the

parameters are used with the intention that the manual will be updated

with more data.

Section II presents the data for scheduled maintenance actions

(daily and periodic inspections) against End Item Aircraft. Subsequent

sectli-nr are presented in functional group order. An illustration,

pointing out the items selected precedes its corresponding statistical

information. Those items which could not. be identified from the -34P

manual are shown on tables titled Miscellaneous at the end of each

functional group.

An index arranged in Federal Stock Number (FSN) or Part Number (PN)

sequence is provided in Appendix A for ease in locating'a particular item•

parameters.

-__ __'A6-

SECT ION I I

SCHEDULED MAINTENAM1CE ACTIONS AGAINST END-ITEM AIRCRAFT

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