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
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
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
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
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
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