Chart B (DER Powerplant)

• A1 – Airplane Turbine Engines – Installation (14 CFR: part 23, part 25)
• B1 – Airplane Piston Engines – Installation (14 CFR: part 23, part 25)
• C1 – Rotorcraft Turbine Engine – Installation (14 CFR: part 27, part 29)
• D1 – Rotorcraft Piston Engine – Installation (14 CFR: part 27)
• E1 – Auxiliary Power Unit (APU) – Installation (14 CFR: part 23, part 25, part 27, part 29)
• F1 – Major Repair / PMA Identicality Findings – Installation (14 CFR: part 23, part 25, part 27, part 29)

• A2 – Airplane Turbine Engines – Fuel & Oil (14 CFR: part 23, part 25)
• B2 – Airplane Piston Engines – Fuel & Oil (14 CFR: part 23, part 25)
• C2 – Rotorcraft Turbine Engine – Fuel & Oil (14 CFR: part 27, part 29)
• D2 – Rotorcraft Piston Engine – Fuel & Oil (14 CFR: part 27)
• E2 – Auxiliary Power Unit (APU) – Fuel & Oil (14 CFR: part 23, part 25, part 27, part 29)
• F2 – Major Repair / PMA Identicality Findings – Fuel & Oil (14 CFR: part 23, part 25, part 27, part 29)

• A4 – Airplane Turbine Engines – Thrust Reversers (14 CFR: part 23, part 25)
• F4 – Major Repair / PMA Identicality Findings – Thrust Reversers (14 CFR: part 23, part 25, part 27, part 29)

• A5 – Airplane Turbine Engines – Fire Protection (CFR: part 23, part 25)
• B5 – Airplane Piston Engines – Fire Protection (CFR: part 23, part 25)
• C5 – Rotorcraft Turbine Engine – Fire Protection (CFR: part 27, part 29)
• D5 – Rotorcraft Piston Engine – Fire Protection (CFR: part 27)
• E5 – Auxiliary Power Unit (APU) – Fire Protection (CFR: part 23, part 25, part 27, part 29)
• F5 – Major Repair / PMA Identicality Findings – Fire Protection (CFR: part 23, part 25, part 27, part 29)

• F9 – Major Repair / PMA Identicality Findings – Indicating Systems (CFR: part 23, part 25, part 27, part 29)

• F13 Major Repair / PMA Identicality Findings – Control System (Mechanical) (CFR: part 23, part 25, part 27, part 29)