RECORRECTED_Aircraft_info_for_insurance_(2).docx

SOLICITATION AG-024B-S-15-0011 HC-130H MAINTENANCE SERVICES

Aircraft 1721

USCG SN 1721

USAF SN 87-0157

Lockheed Martin SN 5121 Model Version 382C-44C Current Model HC-130H Tanker Number 118

Transferred from Lockheed to the USCG 6/16/1988 TTAF as of 3/19/15 5194 Hours This aircraft will not have the center wing box replaced at this PDM due to low time.

Propeller, and Engine Times in Hours

Aircraft 1708

USCG SN 1708

USAF SN 83-0507

Lockheed Martin SN 5002 Model Version 382C-50E Current Model HC-130H Tanker Number 116

Transferred from Lockheed to the USCG 09/17/1984 TTAF as of 3/19/2015 22,807 Hours The center wing box times will be 0 when the aircraft is delivered to the USCG for bailment to the USFS.

Propeller, and Engine Times in Hours

* The propeller for the #3 position it not currently assigned, times TBD.

Certification Basis

The aircraft will be in Bail status from the USCG to the USFS for the duration of the IOC contracts or until the aircraft are delivered to Program Depot Maintenance (PDM) or delivered to the USAF for installation of the Retardant Delivery System (RDS).

The USFS will self-certify the aircraft as airworthy under the definition of 14 CFR 1 public use aircraft. The basis for self-certification of airworthiness will utilize the USCG PG-85-00-70A Aircraft Configuration Control Board Process Guide, Technical Airworthiness Assurance Certification Process to maintain configuration control and make airworthiness determinations that comply with governing documents and requirements. Final airworthiness authority and approval of the ACCB 2 Full Airworthiness Certification will be by the USFS and in accordance with FSM 5700 and FSH 5709.16.