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Power Plant Quality Assurance

Location:
Middleburg, FL, 32068
Posted:
November 12, 2010

Contact this candidate

Resume:

Markham (Birdie) L Cross

**** ********** *****

Middleburg, FL 32068

Contact Phone: 904-***-****

Work Phone: 904-***-**** ext.171

Email Address: abhxzk@r.postjobfree.com

EXPERIENCE

**/***4 to 10/2005; 40 hours per Week; Aircraft Engine

Examiner/Evaluator; WD-8602-06; last promoted 10/2004;

temporary employee; on temporary promotion; INDUSTRIAL

BUSINESS OPERATIONS DEPT, FRC/SE, JACKSONVILLE, FL 32212-

0016;

Walter Lastinger, 904-***-**** ; may contact supervisor.

Special assignment (MZ65886613000H), on temporary detail

to

J52 Build Standard Review (BSR) Core Team assisting J52

aerospace engineering, fleet support team (FST) for a

period

not to exceed one year starting on 10-17-2004 and ending

10-2005. Duties consisted of updating existing work

packages,

tables and figure schematics by analyzing the existing

maintenance processes, procedures, abstracting all

available

information from blue prints, general maintenance

manuals,

Fleet support team and Pratt Whitney engineering and

implementing these changes to schematics within figure

indexes

using Microsoft paint imaging to draw and insert blue

print

datum requirements. Updating inspection, repair work

scope

within work packages and tables adding cleaning, rework

support equipment as necessary. Other duties consisted of

deck

scrubs, updating all router work order work scopes to

include

all specific processes or procedures. This includes the

latest

cleaning process, numerous inspection, repair and rework

procedures such as precipitation and solution heat treat

requirements after weld repair in accordance to blue

print

specification, etc. Manual change request I performed

were

work packages 040, 041, 075, 076, 103 and 104 of NAVAIR

02B-10DAD-6-2V2/2V4 manuals.

Example of Build Standard Review Duties:

This is one example of detailed MCR(manual change

release)work

I performed FST engineering reviewed and released making

only

minimal changes:(NAVAIR 02B-10DAD-6-2V2,WP 040 00)

All support equipment for cleaning, etc. that previously

wasn't listed I added and also inserted the note to

reduce

blast media contaminates.

This was done prior the J52 oil contamination crisis era

and

helped considerably in reducing media entrapment suffered

during this period.

I revised the complete work package along with work

packages

041 00, 075 00, 076 00, 103 00 and 104 00 of NAVAIR

01B-10DAD-6-2V2 and 2V4 manuals.

DEPOT MAINTENANCE

REPAIR

CASE ASSEMBLY, FRONT COMPRESSOR

EFFECTIVITY: 2193699 (J52-408A/B) AND 2187971 (J52-

P408A/B)

EFFECTIVITY: ALL MODELS

This Work Package Supersedes WP 040 00 Dated Change 3 - 1

September 2001

Support Equipment Required

Type Design/

Part Number Nomenclature Figure No.

P-32145 Adapter V

PWA 9826 Gage 1c

PWA 9827 Master 1c

PWA 14266 Flaring tool 17

PWA 14412 Gage 1c

PWA 14414 Gage 1c

PWA 14416 Gage 1c

PWA 14418 Adapter 1c

PWA 14747 Pusher V

PWA 34348 Machining base V

PWA 34393 Machining fixture V

PWA 34558 Riveter V

E10-19042 Pusher, mount pin bushing

PWA 34990 Fixture, drill block

P V6381 VD Cover plate, Leak check equipment

P V6382 VD Cover plate, Leak check equipment

RBS V28 Relief valve, Leak check equipment

TM-02-64-01 Cover plate, Cleaning, Locally manufactured

TM-02-64-02 Cover plate, Cleaning, Locally manufactured

TM-02-64-03 Cover plate, Cleaning, Locally manufactured

TM-02-64-04 Adjustment Handle, Locally manufactured

TM-02-64-06 Cover plate, Cleaning, Locally manufactured

TM-02-64-09 Cover plate, Cleaning, Locally manufactured

TM-02-64-12 Cover plate, Cleaning, Locally manufactured

TM-02-64-13 Cover plate, Cleaning, Locally manufactured

Materials Required

Consumables

Specification/Identification Nomenclature

AMS 3410 Flux, brazing

AMS 4770 Metal, filler

AMS 5504 Metal (patch repair)

AMS 5613 Bar stock

AMS 5680 Metal, filler

AMS 5776 Metal, filler

METCO 450 V10 powder Plasma spray

Micro VSupreme (purple) Dye, layout

MIL VL V23699 Oil, engine

No. 40 Grit, steel

No. 80 or 90 Grit, aluminum oxide

No. 320 grit Cloth, abrasive, aluminum oxide

No. 320 grit Grit, aluminum oxide

Norton No. A601 VOBNA2

2 X 1/32 X 1/4 inch (or equivalent) Cutting wheel,

abrasive

Norton No. 441 Tape, masking, crepe paper backing

PS47 Acid, muriatic

PWA 1349 (METCO 601 powder) Plasma spray

Type 410 Rod, stainless steel

Expendables

Part Number Nomenclature Quantity

AN 125422 Rivet 45

Type 410 Pin stainless steel,

0.125 inch OD X 0.500 inch long 4 per mount pad

627867 Rivet 2

1. INTRODUCTION.

a. This work package (WP) contains instructions for

special

handling and repair of the front compressor case

assembly.

2. REPAIRS. Due to the brittle nature of case material

(AISI

410 Stainless Steel) handle case with extreme caution.

Rough

handling prior heat treat and improper heat treat

procedures

can reduce the impact properties of the material. Results

increase susceptibility to stress corrosion cracking and

can

reduce material hardness. To ensure quality measures are

satisfactory post weld and heat treat repairs, perform

Rockwell Hardness test near engine mount pads, gear box

mount

pads, PRBC mount pad, forward and rear flanges (Rockwell

Hardness C30 to C38), see paragraph 35A. Protective

coating,

Sermetel W paint, shall be applied to case assembly after

repairs are completed.

NOTE:

Prior to the usage of media blast materials throughout

the

repair procedures listed within this work package. Ensure

procedures outlined in paragraph (3), (Contamination

Entrapment Prevention and Removal) and applicable support

equipment is utilized to reduce blast media contaminates.

3. CONTAMINANT ENTRAPMENT V PREVENTION AND REMOVAL.

(Figure

1)

a. Contaminant prevention.

(1) Perform masking procedure prior to machining,

blasting,

blending, or any other process in which contaminants are

present and have a possibility of becoming entrapped

inside

the part.

(2) Mask, cap, or plug all openings to internal passages,

cavities, and tubes to prevent entrapment of contaminants

(Figure 1).

b. Contaminant removal.

(1) If contaminant introduction into internal passages,

cavities, or tubes is unavoidable or has been discovered,

comply with following cleaning procedure:

(a) Remove the No. 2 bearing rear heat shields.

(b) With masking removed, thoroughly flush all accessible

surfaces and cavities with kerosene.

(c) Suspend front compressor case horizontally. Using a

small

flexible tube (approximately 1/4 inch OD) attached to a

kerosene pressure washer, thoroughly flush front

compressor

case outer manifold by inserting the tube at each of the

oil

drain holes (located at the gearbox and PRBC mount pads)

and

flushing through the entire length of each section. Flush

each

section from both directions and rotate the front

compressor

case as necessary to position the hole, from which the

fluid

is draining, at the lowest point.

(d) Vapor degrease all accessible surfaces and cavities

(NAVAIR 02 V1 V517, SPOP 3).

(e) Allow compressor case to dry thoroughly.

(f) With the compressor case suspended horizontally and

the

outer manifold oil drain holes at the lowest position,

blow

compressed air through all vane cavities while vacuuming

outer

manifold.

(g) Remove vacuum and continue blowing compressed air

through

vane cavities and outer manifold until contaminants are

no

longer observed.

(h) Inspect front compressor case outer manifold for 360

degrees by inserting an appropriate bore scope through

the

outer manifold oil drain holes. If contaminants are still

present, re-flush as necessary, beginning at step (c).

10/2001 to 01/2002; 40 hours per Week; Planner and

Estimator,

Aircraft Engine; WD-8602-08; last promoted 10/2001;

temporary

employee; on temporary promotion; CODE 62642 / BLDG.797

Naval

Aviation Depot, FRC/SE NAS Jacksonville, FL. 32212-0016;

Mike

Montgomery, 904-***-**** X221 ; may not contact

supervisor.

Previous qualifications;

During the period between October 2001 and January 2002 I

was

promoted to the temporary position of aircraft engine

planner

(WD-8602-08). Duties while assigned to planning

department

included the coordination between planner and master

production scheduler to ensure TF34 Navy, Air Force

engines

and aeronautical materials are inducted in accordance

with

planned induction schedule. Attend TF34 engine production

meetings, conference calls, maintenance engineering

logistics

review seminar (MELR) reviewing repair, modifications,

rework,

production schedules, delivery dates with naval, air

force and

command representatives. Prepare comprehensive reports

such as

backlog and daily reports, to program analyst. Review and

complete assigned task in work flow manager through naval

air

technical data and engineering service command (NATEC).

Utilize Depot Maintenance System (DMS), Manufacturing

Resource

Planning II (MRPII), Workload Control Systems (WCS),

Naval

Industrial Material Management System (NIMMS). Automated

Data

Capturing System (ADCS). Depot Maintenance Interservice

Support Agreement (DMSIA), Comprehensive Engine

Management

System (CEMS), Ecomtrac all related technical

publications,

technical orders in applying analytical and evaluative

methods

to accomplish duties of the position. Prepared rough

order

magnitude (ROM) abstracting cost requirements of

component

materials estimated man-hour to perform disassembly and

assembly functions to complete requirement. Screen engine

and

equipment log books during induction phase to verify

incoming

configuration, previous incorporation of power plant

bulletins

and changes, local engineering specifications and

technical

orders. Verified tracking history of components and

accessories against incoming ecomtrack and comprehensive

engine management system records. Prepare engine repair

report

and technical directive installation record with incoming

configuration, reason for removal, job number, funding

line,

failure code, time since new, time since repair, last

repair

facility and automated engine management system report

(AEMS)

in accordance with Depot Processing Instruction. Create

production work orders to accomplish special repair

procedures

outlined under special funding lines, production orders

to

perform first article inspections and over and above

emergent

work orders. Analyze detail instructions, technical

manuals,

and local engineering specifications to establish work

breakdown structure requirements. Build routers utilizing

MRPII and in the past WCS, to clean, inspect, rework and

repair aeronautical equipment, assign operation lines to

responsible work centers, calculate estimated time

standards

to perform maintenance, assign compliance requirements to

work

center operation lines. Coordinate with Air Force

personnel on

delivery method and shipment of Air Force engine and

modules

ready for issue (RFI). Utilized resources obtained

through

close contact with budget analyst, program analyst,

master

program scheduler, program manager, shop supervisors,

shop hub

scheduler, production controller, quality assurance

specialist, engineering, industrial engineer

technician's,

aircraft engine examiner's, aircraft engine mechanic's

and

senior aircraft engine planner estimator's to perform

duties

at a fully successful level.

Other duties include loading earlier version (pen base)

now

automated data capturing system with the required J52

engine

data. This included how malfunction codes, processing

instruction reference material, power plant bulletins and

changes, local engineering instructions, local processing

specifications and inspection requirements.

11/1996 to Present ; 40 hours per Week; Aircraft Engine

Examiner; WD-8602-06; last promoted 11/1996; permanent

employee; not on a temporary promotion; Code 62642

BLDG.797

FRC/SE, NAS Jacksonville, FL. 32212-0016; Gary Dixon,

904-***-**** ext.221 ; may not contact supervisor.

Duties consist of examination and evaluation of aircraft

engines, accessories and components under minimal

processing

instructions. With the addition of computers to perform

maintenance I utilize DEP 103 requirements of

Manufacturing

Resource Planning II (MRP II) process guides and a wide

range

of technical data that includes maintenance manuals,

technical

orders, local engineering specifications, technical

engineering instructions, schematics, blueprints.

Functions

include XW01, XW02, and XW03 screens to perform work

order add

now, approval of charges and approval to release

documents.

Perform eng. bom 16 transactions to identify router

detail

characteristics in MTO function of MRP II. Delete, modify

work

order routers utilizing MTO XW10 functions as a tool.

Other

systems utilized include Depot Maintenance System,

Comprehensive Engine Management System. Ecomtrac and

Automated

Data Capturing System to process engines and components.

Attend engine production meetings, review Master Data

Records

with industrial engineering technicians, quality

assurance

specialist, engineers and shop artisans assigned to

engine and

components deck scrubs to update and correct deficiencies

on

work order documents. Submitted shop order changes to add

new

released technical requirements and to correct existing

discrepancies on Master Data Records, communicating with

industrial engineering technicians, subject matter

experts

such as shop artisans and shop supervisors directly

affected

by these changes. Analyzed operation description

functions,

occurrence factors, technical directive compliance fields

and

updated (MDR's) correcting any maintenance manual work

package

reference defects. Other corrections included proper

cleaning

procedures, Non destructive test requirements, stress

relieve,

shot peen, bake requirements prior to and post plating

procedures. Added any power plant changes or bulletins

along

with any local engineering specifications and local

processing

procedures related to components and parts screened

utilizing

analytical ability to abstract the full spectrum of

associated

processing requirements. This includes the conversion of

cleaning procedures to cleaning methods as LPS 260

replaced

LPS 341-167. Played a instrumental part in building the

structure of the J52 engine In MRP II data base working

close

with MRP II subject matter experts, equipment specialist

and

industrial engineering technicians creating engine

breakdown

structure (J52 Build of material), that all engines are

now to

be structured after. While assigned to the J52 engine

shop

during the competition contract I constructed emergent

work

documents to perform over and above processing. This

consisted

of creating a work order document assigning an exhibit

number

related to the engine serial number, job number and

sequence

number. Requirements in the construction of these type

documents as they where computer generated included

access to

enter the Unisys 1100 computer system. Work breakdown

structure (creating work order router), operation

description,

technical compliance field requirements and calculated

time

standards where analyzed in there construction under

Workload

Control System (WCS). Once this was accomplished a work

request number was assigned and submitted to the aviation

contract office for approval prior to processing. Duties

are

normally that of an over and above manager (GS-11),

however

these duties where assigned to aircraft engine examiners

during the period under competition contract. Once these

work

orders where completed, approved and WCS feedback updated

to

release the funding these documents could be printed and

attached to components for processing. Duties associated

with

TF-34 Stator Case Assemblies and Tf-34 Rotating

components

includes communicating with engineering, industrial

engineering technicians, quality assurance specialist,

shop

artisans and supervisors to improve routing procedures of

TF-34 rear Stator cases, ring and connector assemblies,

compressor and turbine assemblies. Team efforts where

conducted to improve process procedures to cut turn

around

time on rear stator case, by performing Z dimension and S

dimension run outs while cases where in the machine shop.

Prior processing had these cases visiting the machine

shop

twice conducting Z dimension run out inspection, and

returning

after cases where cleaned and florescent penetrate

inspections

where performed. Ring connector pinhole repair

corrections

where made to MDR's, adding three additional operation

lines

to work documents with distribution of the time standard

over

all four lines. Because as many as four pinholes could be

repaired engine examiners had the option to tailor work

documents according to number of repairs required.

Assisted

quality assurance specialist in the inspection phases and

processing on first article inspections, quality

deficiency

reports, quality deficiency notice and quality

investigations.

Attended material review boards evaluating material

condition

and disposition for repair or disposal with team member

from

engineering, quality assurance, and production shop and

production control.

Examine and evaluate various aircraft engine components,

accessories and engine parts through the use of precision

measuring instruments. Measure bearing housing bores,

coupling

journals, turbine seals, turbine disk snap diameters,

stator

case snap diameters, stator seal land dimensions, height

dimensions on bearing seats to case and housing flanges.

Tolerances held as close as .0002 in parts such as the

J52

front compressor drive turbine rotor shaft spacer.

Precision

measuring tools utilized to perform inspections include

the

following. Vanier calipers, depth micrometers, height

gauges,

dial indicators, intra-micrometers, GO and NO-GO gauges,

inside and outside micrometers, thickness gauges,

shadowgraph

machine, flow machine, 12-24 and 24-36 inch pie typesets.

Assist engineering and quality assurance in the

investigation

of engines returned under quality deficiency reports and

engineering investigation reports. Technical Data

Performed

above duties on the J52-P6, P8 and P408 series engines

and

components using the following guidelines.

A) Minimum processing procedures in accordance with Local

processing specification number 2403 revision D.

B) NAVAIR 02B-10DAC-6-3, NA 02B-10DAC-6-1, NA 02B-10DAC-6-

2

J52-P6 and P8 Intermediate and Depot maintenance manuals.

C) NAVAIR 02B-10DAD-6-3, NA 02B-10DAD-6-1, NA 02B-10DAD-6-

2

J52-408 Intermediate and Depot maintenance manuals.

D) Ecomtrac (Engine Component Tracking) on life limited

components. E) Local Engineering Specifications, Local

Engineering Instructions, Local Processing

Specifications,

Blueprints and Schematics.

1) TF34-100 and TF34-100A processing instructions listed

as

follows.

A) D.M.I.S.A. (Depot Maintenance Interservice Support

Agreement)

B) Technical Order 2J-TF34-116-1 through 2J-TF34-116-8

manuals.

C) CEMS (Comprehensive Engine Management System) used to

track

life limits of Air force components.

D) Local Engineering Specifications, Local Engineering

Instructions and Manual Change Request.

2) TF34-400, TF34-400A and TF34-400B Technical Data as

listed.

A) Processed per Opnavist 4790-2

B) Technical manual Navair 02B-105ALB-6-2-2

C) Local Engineering Specifications and Instructions

D) Periodic Maintenance Inspection Cards

E) Manual Change Request

11/1995 to 11/1996; 40 hours per Week; Aircraft Engine

Examiner/Evaluator; WD-8602-06; last promoted 11/1995;

temporary employee; on temporary promotion; Code

6.2.6.4.2

Bldg 797 FRC/SE, FRC/SE, JACKSONVILLE, FL 32212-0016;

Mike

Montgomery, 904-***-**** X221 ; may not contact

supervisor.

Presently assigned to original duties outlined in

position

description as detailed under (WD-8602-06), aircraft

engine

examiner. Previous detail assignments include temporary

Aircraft Engine Examiner Supervision not exceeding thirty

days. Functions included all required position

description

duties applicable and required to obtain fully successful

objectives within a specified time frame to achieve and

function individually. Duties entailed employee work

assignment, ensuring applicable required training, safety

goals are implemented and obtained to those individuals

assigned under my competency. Ensured work load was

distributed equally among assigned individuals within a

specific work area and overtime assignments where also

handled

accordingly. Utilized Lean Sigma and ISO 9000 concepts

during

oil contamination crisis the J52 engine program had

experienced. Assigned to black and green belt project

teams

utilizing value stream mapping techniques to identify and

resolve problem areas associated with media entrapment

during

this period. Ensured all employee regular pay hours,

annual

and sick leave hours and assigned overtime hours where

accurate as detailed on Bi-weekly shop dealers.

Correcting and

initialing errors to update dealer discrepancies. I

attend

production support meetings in support of engine

processing,

acting as a liaison to resolve issues affecting process

flow,

turn around time, quality, man hours, prioritized

components

and support to resolve bottleneck issues hampering the

processing functions of aeronautical equipment undergoing

repair though out the facility. Other supervisor duties

include Aircraft Engine Supervisor (WS-8602-10) for a

period

of 120 days while previously assigned in the J52 engine

branch. Performed all related duties applicable to this

position above satisfactory as specified within the

position

description.

Special assignment on temporary detail to J52 Build

Standard

Review (BSR) Core Team assisting J52 aerospace

engineering,

fleet support team (FST) for a period not to exceed one

year

starting on 10-17-2004 and ending 10-2005. Position

description during this one year detail was equivalent to

that

of engineering technician at the pay grade level of

(GS-0895-11). These duties consisted of updating existing

work

packages, tables and figure schematics by analyzing the

existing maintenance processes, procedures, abstracting

all

available information from blue prints, general

maintenance

manuals, Pratt and Whitney engineering instructions and

inserting these updates to schematics within figure

indexes

using Microsoft paint imaging to draw and insert blue

print

datum requirements. Updating inspection, repair work

scope

within work packages and tables adding cleaning, rework

support equipment as necessary. Other duties consisted of

deck

scrubs, updating all router work order work scopes to

include

all specific processes or procedures. This includes the

latest

cleaning process, numerous inspection, repair and rework

procedures such as precipitation and solution heat treat

requirements after weld repair in accordance to blue

print

specification, etc. Manual change request I performed

were

work packages 040, 041, 075, 076, 103 and 104 of NAVAIR

02B-10DAD-6-2V2/2V4 manuals. I was fortunate to be

selected

for the position based on the following grading factors

offered to all examiners within my competency.

J52 BSR Core Team Member - Technical (Preferred

Qualifications/Duties)

. Demonstrate a high level of familiarity within J52

engine

platform

o Technical Manuals/Publications

o Standard Practice Manuals

o Engineering Specifications

o SOW

o Military Standards

o Operational Procedures

o Maintenance Plans

. Demonstrate working knowledge of MRPII system as well

as

Microsoft Office Applications

. Able to interpret engineering drawings (BP) and

sketches

. Assist in documentation/review of work orders

. Demonstrate working knowledge of various duties

associated

with materials handling

. Identify and condition-classify materials and equipment

. Experience in routing and expediting movements of

parts,

supplies, and materials

. Experience in the following technical specializations:

Test

Cell operations and procedures (Sytronics, Process

Control

Computer Test Systems, Endevco Vibrations Analysis

System),

part examination, part disposition, and part handling

. Assist Engineering in design or modification of

equipment

and/or process improvement recommendations

. Assist in conducting various duties not limited to

examining, troubleshooting, and providing feedback on

technical matters

. Advise technicians on methodology for machine

operations

. Actively Participate in technical discussions

. Be able to assist with preparation of repair and

testing

procedures necessary for assigned projects

. Demonstrate the ability to monitor progress of assigned

projects, identify problems, and coordinate required

corrective action

. Act as liaison between shop floor artisan and FST

Engineering on technical issues

. Demonstrated knowledge and experience in J52 engine

assembly

and disassembly.

J52 BSR Core Team Member - Test Cell (Preferred

Qualifications/Duties)

. Demonstrate a high level of familiarity within J52

engine

platform

. Demonstrate a high level of familiarity with Test Cell

(IMA

and Depot)

. Experience in the following technical specializations:

Test

Cell operations and procedures (Sytronics, Process

Control

Computer Test Systems, Endevco Vibrations Analysis

System)

. Demonstrate working knowledge of Test Cell equipment,

instrumentation, and troubleshooting procedures

. Actively Participate in technical discussions related

to

Test Cell matters

. Experienced in planning and executing scheduled

maintenance

. Assist in conducting various duties not limited to

examining, troubleshooting, and providing feedback on

technical matters

Other duties include loading earlier version (pen base)

now

(ADCS), automated data capturing system with the required

J52

engine data. This included how malfunction codes,

processing

instruction reference material, power plant bulletins and

changes, local engineering instructions, local processing

specifications and inspection requirements.

11/1980 to 11/1995; 40 hours per Week; Aircraft Engine

Mechanic; WG-8602-10; last promoted 11/1988; permanent

employee; not on a temporary promotion; CODE 62622

BLDG.797

Naval Aviation Depot, FRC/SE NAS Jacksonville, FL. 32212-

0016;

Roy Luke, 904-***-**** ; may not contact supervisor.

Duties consisted of journeyman level maintenance on the

following aircraft engines, subassemblies, modules and

components. J52-P6, J52-P8, J52-P408 series aircraft

engines,

subassemblies and components. TF34-100, TF34-100A, TF34-

400,

TF34-400A, TF34-400B rotating components and F404-GE-400

engines and modules. This included the disassembly,

inspection

and assembly of listed equipment. Corrected test

functional

discrepancies on a variety of J52 engines rejected while

assigned to the J52 engine shop. Engines rejected from

test

cell with compressor stalls, high exhaust gas

temperature,

breather pressure defects, vibration defects, low oil

pressure

defects, spread check problems, speeder problems

associated

with P6 engines and other discrepancies. Performed first

article fit and function exams with quality assurance,

assisted engineering in disability, evaluation

characteristics

on engines undergoing investigation for mishaps due to

equipment and or component failure. Assisted Quality

assurance

specialist on engines returned due to discrepancies under

quality deficiency reports. All work performed in

compliance

with technical instructions and maintenance manuals

related to

equipment listed. Screened J52 engine log books and work

order

documents for compliance with Navair Note 4790. Certified

the

completeness of all disassembly, repair and assembly work

order documents. Ensured serviceability of all life

limited

components and low cycle fatigue components by screening

ecomtrac records. Screened all assembly record cards,

Schedule

Removal Cards and Equipment record cards for accuracy of

Time

Since New, Time Since Overhaul and Time Since Repair and

compliance of all power plant changes, bulletins and

local

engineering specification requirements. Reviewed

Technical

Directive Inventory Report for compliance with all

applicable

power plant changes and power plant bulletins. Completed

Engine Repair Report in accordance with Navair Note 4790.

All

maintenance performed under applicable engine processing

instructions as directed by NADEP Jacksonville

engineering

department (Fleet Support Team). Other duties included

the

following maintenance on all J52 P6,P8 and P408 series

engines, disassembly, inspection and assembly,

subassemblies,

J52 engine stack and final assembly, Main Gearbox

assemblies,

2&3 bearing housing, 4&5 scavenge pumps, front accessory

support assemblies and stud, helical repairs associated

with

aeronautical equipment while assigned to the J52 engine

shop.

Screened J52 engine log books and work order documents

for

compliance with Navair Note 4790. Certified the

completeness

of all disassembly, repair and assembly work order

documents.

Ensured serviceability of all life limited components and

low

cycle fatigue components by screening ecomtrac records.

Screened all assembly record cards, Schedule Removal

Cards and

Equipment record cards for accuracy of Time Since New,

Time

Since Overhaul and Time Since Repair and compliance of

all

power plant changes, bulletins and local engineering

specification requirements. Reviewed Technical Directive

Inventory Report for compliance with all applicable power

plant changes and power plant bulletins. Completed Engine

Repair Report in accordance with Navair Note 4790. Other

duties included disassembly, inspection and assembly of

all

subassemblies, engine stack and final assembly, Main

Gearbox

assemblies, 2&3 bearing housing, 4&5 scavenge pumps and

front

accessory support assemblies while assigned to the J52

engine

shop. Performed rework including stud replacement, heli-

coil

repairs utilizing applicable maintenance manuals such as

NAVAIR 02-1-517.

EDUCATION

Southeast Senior High, Whitsett, N.C.; 1973 GED

Florida Junior College Jacksonville, Jacksonville,

Florida;

No Degree in Certificate Applied Science, 1988; 3.0 out

of 4

Point GPA; 600 Other Hours

Florida Junior College at Jacksonville, Jacksonville,

Florida;

No Degree in Applied Science, 1988; 3.0 out of 4 Point

GPA;

600 Other Hours

Florida Junior College, Jacksonville, Florida; No Degree

in

Cert. Applied Science Industrial machine, 1988; 3.0 out

of 4

Point GPA; 600 Semester Hours

PROFESSIONAL TRAINING

LEVEL B - CODE OF CONDUCT VALIDATED 7/13/2009

DOD INFORMATION ASSURANCE AWARENESS VER. 7.0 VALIDATED

7/13/2009

DOD INFORMATION ASSURANCE AWARENESS DOD-IAA-V7.0

NTMPS/NKO

7/13/2009

PERSONALLY IDENTIFIABLE INFORMATION (PII) DOD-PII-V1

DCPDS-VALIDATED 7/13/2009

TRAFFICKING IN PERSONS BASIC AWARENESS TRAINING JKDDC-TIP-

1

DCPDS-VALIDATED 7/13/2009

NO FEAR ACT: NOTIFICATION AND FEDERAL EMPLOYEE ANTI-

DISCRIMI

DCPDS-VALIDATED 3/2/2009

DOD INFORMATION ASSURANCE AWARENESS DOD-IAA-V2.0

DCPDS-VALIDATED 3/2/2009

NO FEAR ACT: NOTIFICATION AND FEDERAL EMPLOYEE

ANTI-DISCRIMINATION AND RETALIATION ACT OF OCHR-NFA-1.0

NTMPS/NKO 3/2/2009

DOD INFORMATION ASSURANCE AWARENESS DOD-IAA-V7.0

NTMPS/NKO

1/28/2009

DOD INFORMATION ASSURANCE AWARENESS VER. 7.0 DCPDS-

VALIDATED

1/28/2009

DOD INFORMATION ASSURANCE AWARENESS DOD-IAA-V5.0

DCPDS-VALIDATED 3/4/2008

A) Word Level 1, 16 hours, 4-98

B) MRP2 training, 32 hours, 4-01

C) Pen Base Data, (ADCS) 8 hours, 1-01

D) Airframe and Power Plants Mechanic "General" 45 hours,

6-96

E) Bearing removal and installation, 3-00

F) Hazardous Materials and Waste Handling, 7-91

G) Blueprint Reading, 28 hours, 6-97

H) SH-3 Powerplant and Related Systems, 40 hours, 9-77

I) Corrosion Control, 8 hours, 1-77

PROFESSIONAL LICENSES/CERTIFICATES

Current qualifications Electronics Engineering

Technician,

GS-802-12 dated 8/31/2010. Copy of e-mail;

Congratulations!

Your resume has been forwarded for consideration for the

position of Electronics Engineering Technician, GS-802-

12, in

the Industrial Production Planning Division, 63100;

Announcement # SEO-GS0802-12-MZ737629-C-17.

Please let us know my COB 3 Sep 2010 if you are

interested in

being considered for this vacancy.

Thank you for your interest.

Ann Kelley

Industrial Production Planning Division

Code 63100

904-***-****

PROFESSIONAL RATINGS, AWARDS, AND RECOGNITIONS

Special Act or Service Award 5/10/2010 1324

Special Act or Service Award 2/15/2010 583

Special Act or Service Award 11/9/2009 537

Special Act or Service Award 8/12/2009 146

Special Act or Service Award 5/20/2009 758

Special Act or Service Award 2/10/2009 683

Special Act or Service Award 11/12/2008 762

Special Act or Service Award 8/7/2007 500

Suggestion Cash Award 9/12/2006 1200

Special Act or Service Award 6/23/2006 600

Special Act or Service Award 10/24/2005 1500

On the Spot Cash Award 7/1/2003 500

On the Spot Cash Award 6/10/2003 300

Performance Award 5/31/2002 375

Special Act or Service Award 2/25/2002 350

Special Act or Service Award 6/29/2001 325

Special Act or Service Award 6/15/2001 250

Suggestion Cash Award 5/12/2000 750

Special Act or Service Award 11/9/1999 100

Special Act or Service Award 9/29/1999 150

Notable Achievement Award 6/24/1998 150

Special Act or Service Award 12/5/1994 250

Productivity Gainsharing Award 9/30/1992 2090

Special Act or Service Award 7/30/1992 200

Performance Award 11/22/1991 201

Productivity Gainsharing Award 9/30/1989 240

Performance Award 9/24/1989 500

Performance Award 9/3/1987 250

Performance Awards, Outstanding, 1990-1997

Letter of Appreciation from Rear AdmiralD.B.McKinney,

0493

Network

Type Model Series Award for 12 consecutive months, Fiscal

Year

1981

Support of Oil Contamination Black Belt Project, Team

Assignment

OTHER INFORMATION

Typing 25 wpm

U.S. MILITARY SERVICE INFORMATION

Active Duty: 10/1974 to 07/1978 - U.S. Navy

Active Duty: 07/1978 to 06/1980 - U.S. Navy

Campaign badges and/or expeditionary medals received:

National

Defense Ribbon

Battle Efficiency Ribbon ( Operational Readiness

Evaluation )

Honorable Discharge

Percentage of service connected disability 50%

Date of last Veterans' Administration Letter: 10/31/2006

ADDITIONAL DATA SHEET

Markham (Birdie) L Cross

1. Appointment Eligibility:

Yes-Current Permanent Navy Civilian

Current Permanent Federal Civilian Employee

Interchange Agreement Eligible

Veterans Recruitment Appointment and/or 30% or More

Disabled Veteran

Veterans Employment Opportunity Act Eligible

Person with Disability

2. Citizenship: Yes

3. Appt Preference:

Temporary (positions lasting less than 1 year)

Term (positions lasting 1 year or more, but less

than 4

years)

4. Willing to Travel: 6 or More Days

5. Vet Preference: 10-Point 30% Compensable Preference

6. Low Salary Accept: $55,000

7. Qualified Typist: No

8. Birth Date: **None Specified

9. Geo Preference: FL, Cape Canaveral ; FL, Eglin Air

Force

Base ; FL, Fort Lauderdale ; FL, Jacksonville ; FL,

Orlando

; FL, Panama City ; FL, Tampa ; FL, West Palm Beach ;

NC,

Charlotte ; NC, Raleigh ; UNITED KINGDOM, London ;

SPAIN,

Madrid ; FL, St Augustine

RACE/ETHNIC STATUS: Ntv, Wht

SEX: Male

Deputy Assistant Secretary of the Navy (Civilian Human Resources)

This is an Official U.S. Navy Web Site



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