1958 Lockheed C-130A “Hercules”

• 11,615 TTSN
• 2,324 Hrs. Since Lockheed Anti-Deterioration service check
• 751 Hrs. Since last “D” check
• 9,362 Landings since new

Engine #1:

• Allison T-56A-11
• 225 SOH
• 10 SHSI

Engine #2:

• Allison T-56A-11
• 775 SOH
• 10 SHSI

Engine #3:

• Allison T-56A-11
• 470 SOH
• 10 SHSI

Engine #4:

• Allison T-56A-11
• 1150 SOH
• 10 SHSI

Prop #1:

• Aero Products
• 1080 “s” time since spalling & NDI Insp.

Prop #2:

• Aero Products
• 1200 “s” time since spalling & NDI Insp.

Prop #3:

• Aero Products
• 1285 “s” time since spalling & NDI Insp.

Prop #4:

• Aero Products
• 875 “s” time since spalling & NDI Insp.

Propellers have been timed at half-life – approximately 1500 Hrs. remaining until the next inspection is due, as per FAA approved inspection program

• Ground Compressor Turbine (GCT)
• 170.0 Hrs. SMOH

• DUAL COLLINS 618‑S ‑ HRS*SCR 718 RANGE
• COLLINS VHF  10  –  VHF*AN/APN 22 LO RANGE RAD ALT
• AN/ARC  34  –  UHF*AN/APX   6 ‑ IFF
• AN/ARN 59  –  RADAR*MA 1  ‑  FLIGHT  DIRECTOR
• AN/ARN 14 VOR*AN/ARN 21 –  TACAN
• DUAL AN/ARN 6 ‑ ADFS*AN/ARN 32  –  MARKER BEACON
• AN/ARN  31 ‑ UHF/DF*KINGTRANSPONDER
• AN/ARN  31 – GS*ENCODER
• AN/APN  147 DOPPLER RADAR*KING VHF COM
• AN/ASN  35  DOPPLER COMPUTER
• TCAS: Honeywell TCAS 2 version 7
• GPS:  Becker Multi Function Display GPS worldwide
• COMMS:  dual SunAir HF’s with 8.33 spacing and the Navs have FM immunity
• RADAR:  APN-59

• 30,000 lbs.
• 41′ long floor (4 pallets)x 10′ W x 9′ H + 1 ramp regular pallet 88×108

• Complete LAPES roller system, the only one in the world in civilian hands

• Complete set of troop seats (96) including complete set of stanchions for litters

• All components for paratroop operations