C-130/L382 Hercules Maintenance Planning Grant Little LM Aero / C-130 R&M Engineering

C-130/L382
Hercules Maintenance Planning
Grant Little
LM Aero / C-130 R&M Engineering
Maintenance Planning
[email protected]
770-494-8029
INFORMATION CONTAINED IN THIS BRIEFING IS FOR REFERENCE PURPOSES ONLY AND DOES NOT
NECESSARILY REFLECT THE LATEST AIRCRAFT MODEL(S) OR CONFIGURATION(S).
THIS PRESENTATION IS FOR INFORMATION ONLY. NO US GOVERNMENT COMMITMENT TO SELL, LOAN,
LEASE, CO DEVELOP OR CO-PRODUCE DEFENSE ARTICLES OR SERVICES IS IMPLIED OR INTENDED.
Copyright 2013, Lockheed Martin Corporation. All rights reserved.
Topics
• Organization
• Preventive Maintenance Program
• Continued Airworthiness
– FAA-Mandated Maintenance Plan Updates
• Service Center Programs
• Technical Inquiries
Copyright 2013, Lockheed Martin Corporation. All rights reserved.
Organization
Systems Integration
Director
Systems Engineering
Specialty Engineering
R & M Engineering
Diagnostic / Prognostic
Health Management
Configuration Management
Design & Analysis
Requirements Engineering
System Safety
Maintenance Planning
Data Management
Risk Management
Copyright 2013, Lockheed Martin Corporation. All rights reserved.
Preventive Maintenance
Program
• The maintenance engineering analysis is based
on Reliability-Centered Maintenance Analysis
(RCMA)
• The analysis process includes:
– Failure Mode Effects and Criticality Analysis
(FMECA)
• Failure for Maintenance Significant Items (MSIs)
• Damage for Structurally Significant Items (SSIs)
– LM Aero / Vendor / Historical data
Copyright 2013, Lockheed Martin Corporation. All rights reserved.
Preventive Maintenance
Program (Cont’d)
• Program was developed for 210/420 day
cycles with flight hour backstops
• On going analysis concluded that program can
be revised to fit 270/540 day cycles with the
same flight hour backstops
–
–
–
–
A Check 38 weeks
B Check 77 weeks (1.5 yrs) or 1200 F/Hs
C1 Check 156 weeks (3 yrs) or 2400 F/Hs
C2 Check 312 weeks (6 yrs) or 4800 F/Hs
Copyright 2013, Lockheed Martin Corporation. All rights reserved.
Continued Airworthiness
• Aging Aircraft Rule
– FAA-Mandated Updates Incorporated
• SFAR 88 (Fuel Tank Flammability) (2009)
• Damage Tolerance Analysis (DTA) (2010)
• Electrical Wiring Interconnection System
(EWIS) (2010)
Copyright 2013, Lockheed Martin Corporation. All rights reserved.
Continued Airworthiness
(Cont’d)
• Limit of Validity (LOV) 14 CFR Part 26,
Subpart C (Aging Aircraft Safety, Widespread
Fatigue Damage)
• 75,000 Flight Hours/58,000 Flight Cycles
– 5 WFD Maintenance Items Identified
• 3 New Service Bulletins
• 2 Updates to Existing Service Bulletins
• FAA to AD WFD Maintenance Actions
– Damage Tolerance Based Inspections in
SMP 515-C-SSID Added/Updated
Copyright 2013, Lockheed Martin Corporation. All rights reserved.
Service Center Programs
• LM Aero Certified Service Centers
– SMP 515-C-SC
• Complete aircraft and systems
• All configurations
• SMP 515-C-QEC
– QEC / Engine / Propeller
Both programs will deliver in October 2013
Copyright 2013, Lockheed Martin Corporation. All rights reserved.
Technical Inquires
• LM Technical Support Center
– [email protected]
– 770-494-9131
Copyright 2013, Lockheed Martin Corporation. All rights reserved.
Backup Information
Copyright 2013, Lockheed Martin Corporation. All rights reserved.
Continued Airworthiness
(Cont’d)
Electrical Wiring Interconnection System (EWIS)
• FAA AC 120-94, Aircraft Electrical Wiring
Interconnection Systems Training Program,
provides details of EWIS training that could be
adopted by air carriers and air operators.
Copyright 2013, Lockheed Martin Corporation. All rights reserved.
Continued Airworthiness
(Cont’d)
• Damage Tolerance Analysis (DTA) For
Operators of FAA N-registered Aircraft
– Title 14 of the Code of Federal Regulations (14
CFR) Part 26, Subpart E (Aging Airplane Safety—
Damage Tolerance Data for Repairs and
Alterations)
– FAA requires DAH (LM) to provide Damage
Tolerance Inspection (DTI) data for repairs and
alterations available to operators so they can
comply with the Aging Aircraft Rule
Copyright 2013, Lockheed Martin Corporation. All rights reserved.
Continued Airworthiness
(Cont’d)
Damage Tolerance Analysis (DTA)
• After December 20, 2010, 14 CFR Part
121.1109 and Part 129.109 require operators of
large transport category airplanes to
incorporate damage tolerance based
inspections which address the adverse effects
of repairs and alterations to fatigue critical
structure in their maintenance program
Copyright 2013, Lockheed Martin Corporation. All rights reserved.
Continued Airworthiness
(Cont’d)
• Notice of Proposed Ammendment-2011-17
"Volcanic Ash“
– EASA is updating the Operation and Inspection
requirements when exposed to volcanic ash
Copyright 2013, Lockheed Martin Corporation. All rights reserved.
LM Aero / C-130 R&M
Engineering
Maintenance Planning
Copyright 2013, Lockheed Martin Corporation. All rights reserved.