Solo Flight and Aircraft Airworthiness

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Flashcards covering solo flight privileges, medical certificates, aeromedical factors, standard regulations, and DA40 technical specifications.

Last updated 5:10 AM on 7/8/26
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229 Terms

1
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Local Solo Flight Documents

Student Pilot Certificate, Government-issued Photo ID, and a valid FAA Medical Certificate (or BasicMed).

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FAR 61.3(a)(1)

Federal Aviation Regulation code governing the requirement for a student pilot certificate or pilot certificate for local solo flights.

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Emergency Deviation Authority

According to FAR 91.3, the PIC may deviate from instructor limitations only if necessary during an emergency requiring immediate action.

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Student Passenger Limitation

A student pilot may not carry passengers according to FAR 61.89(a)(1).

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Night Solo Requirement

Student pilots must complete required night training and receive a specific night solo endorsement per FAR 61.87(o).

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Cloud Layer Limitation

Student pilots may not operate above a cloud layer where visual reference to the surface is lost per FAR 61.89(a)(6).

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First-Class Medical Duration (Under 40)

6060 calendar months for student pilot privileges.

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First-Class Medical Duration (4040 or older)

2424 calendar months for student pilot privileges.

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Second-Class Medical Duration (Under 40)

6060 calendar months for student pilot privileges.

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Second-Class Medical Duration (4040 or older)

2424 calendar months for student pilot privileges.

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Third-Class Medical Duration (Under 40)

6060 calendar months for student pilot privileges.

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Third-Class Medical Duration (4040 or older)

2424 calendar months for student pilot privileges.

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FAR 61.53

Regulation stating a pilot may not act as PIC if they know of a medical condition that prevents safe operation, such as a broken leg.

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Hypoxia

A medical condition that can be caused or worsened by flying involving oxygen deficiency.

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Hyperventilation

A medical condition caused by abnormal breathing patterns during flight.

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Spatial Disorientation

An aeromedical factor where the pilot is unable to determine their body position or motion relative to the earth.

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Decompression Sickness

A medical condition resulting from rapid changes in pressure, often mentioned in PHAK Chapter 17.

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Dehydration

An aeromedical factor affecting fitness for flight by reducing judgement and reaction time.

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IMSAFE Checklist - I

Illness.

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IMSAFE Checklist - M

Medication.

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IMSAFE Checklist - S

Stress.

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IMSAFE Checklist - A

Alcohol.

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IMSAFE Checklist - F

Fatigue.

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IMSAFE Checklist - E

Emotion/Eating.

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Alcohol Bottle-to-Throttle Time

No flying within 88 hours of drinking alcohol.

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Legal BAC Limit

No flying with a blood alcohol concentration of 0.04%0.04\% or higher.

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FAR 91.17

The regulation specifically governing alcohol and drug limitations for pilots.

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Type Certificate Conformity

Requirement for an aircraft to be airworthy, meaning all required equipment is installed and no unapproved modifications exist.

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Safe Condition for Operation

The second essential component of airworthiness defined in FAR 91.7.

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Owner or Operator Responsibility

The party responsible for keeping an aircraft airworthy per FAR 91.403.

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Preflight Airworthiness Determination

The responsibility of the Pilot in Command (PIC) per FAR 91.7.

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ARROW - Airworthiness Certificate

Required document that never expires if the aircraft is registered and properly maintained.

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ARROW - Registration Certificate

Required document valid for seven years.

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ARROW - Radio Station License

Document only required for international flights.

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ARROW - Operating Limitations

Included in the AFM/POH, placards, and markings.

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ARROW - Weight & Balance

Information usually located within the AFM/POH.

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Airworthiness Certificate Location

Must be located in the cabin and visible.

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AAV1ATES - Annual Inspection

Required every 1212 calendar months.

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AAV1ATES - Airworthiness Directives (ADs)

Legally binding inspections or modifications required for safety.

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AAV1ATES - VOR Check

Required for IFR operations only, every 3030 days.

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AAV1ATES - 100-hour Inspection

Required if the aircraft is used for hire or flight instruction for hire.

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AAV1ATES - Altimeter Inspection

Required every 2424 calendar months for IFR.

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AAV1ATES - Transponder Inspection

Required every 2424 calendar months.

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AAV1ATES - ELT Inspection

Required every 1212 calendar months.

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AAV1ATES - Static System Inspection

Required every 2424 calendar months for IFR.

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UVU DA40 Inspection Program

A Progressive Inspection Program consisting of four phases.

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Progressive Inspection Phase Frequency

One phase is completed every 5050 flight hours.

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ELT Battery Replacement (Usage)

After 11 cumulative hour of use.

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ELT Battery Replacement (Life)

When 50%50\% of battery life has expired.

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ATOMATOFLAMES - A (Airspeed)

Airspeed Indicator required for VFR Day.

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ATOMATOFLAMES - T (Tachometer)

Tachometer required for VFR Day.

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ATOMATOFLAMES - O (Oil Pressure)

Oil Pressure Gauge required for VFR Day.

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ATOMATOFLAMES - M (Manifold)

Manifold Pressure Gauge required for constant-speed prop aircraft in VFR Day.

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ATOMATOFLAMES - A (Altimeter)

Altimeter required for VFR Day.

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ATOMATOFLAMES - T (Temperature)

Temperature Gauge required for liquid-cooled engines in VFR Day.

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ATOMATOFLAMES - O (Oil Temperature)

Oil Temperature Gauge required for VFR Day.

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ATOMATOFLAMES - F (Fuel)

Fuel Gauge required for VFR Day.

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ATOMATOFLAMES - L (Landing Gear)

Landing Gear Position Indicator for retractable gear aircraft in VFR Day.

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ATOMATOFLAMES - A (Anti-Collision)

Anti-Collision Lights required if certificated after 3/11/963/11/96.

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ATOMATOFLAMES - M (Magnetic)

Magnetic Compass required for VFR Day.

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ATOMATOFLAMES - E (ELT)

Emergency Locator Transmitter required for VFR Day.

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ATOMATOFLAMES - S (Safety Belts)

Safety Belts required for VFR Day.

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FLAPS - F

Fuses (or spare circuit breakers) required for VFR Night.

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FLAPS - L

Landing Light required for hire at night.

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FLAPS - A

Anti-Collision Lights required for VFR Night.

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FLAPS - P

Position Lights required for VFR Night.

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FLAPS - S

Source of Electrical Power (Alternator/Battery) required for VFR Night.

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FAR 91.103

Regulation requiring preflight action including weight/balance and environment data.

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NWKRAFT - N

Notams.

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NWKRAFT - W

Weather.

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NWKRAFT - K

Known ATC delays.

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NWKRAFT - R

Runway lengths.

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NWKRAFT - A

Alternatives.

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NWKRAFT - F

Fuel requirements.

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NWKRAFT - T

Takeoff and landing distance.

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MEL

Minimum Equipment List, checkable via the FAA to handle inoperative equipment.

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Inoperative Equipment Action

Deactivate or remove the equipment, then placard it as INOPERATIVE.

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Ferry Permit (Special Flight Permit)

Allows flight of a non-airworthy aircraft to maintenance, repair, storage, or alteration.

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DA40 GFRP

Glass fiber reinforced plastic, the primary material of the DA40 airframe.

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Ailerons

Primary flight controls for Roll.

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Elevator

Primary flight control for Pitch.

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Rudder

Primary flight control for Yaw.

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Elevator Trim

Secondary flight control used to remove control pressure for maintained airspeed.

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DA40 Main Gear

Composite spring main gear.

85
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DA40 Nosewheel Type

Free castering nosewheel.

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DA40 Braking

Hydraulic disc brakes with differential braking for steering.

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DA40 Engine Lycoming IO-360-M1A

Four-cylinder, horizontally opposed, air-cooled, fuel-injected engine producing 180HP180\,HP.

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Engine Displacement

361361 cubic inches.

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44 Handful - 4 Stroke

Intake, Compression, Power, Exhaust.

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44 Handful - Naturally Aspirated

An engine that relies on atmospheric pressure for air intake without a turbo or supercharger.

91
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Magneto Purpose

Generates electricity independently of the electrical system to fire spark plugs.

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Redundant Ignition

The DA40 utilizes two spark plugs per cylinder and two ignition systems for reliability.

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Alternate Air Purpose

Bypasses the normal air filter if the intake becomes blocked.

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Mixture Control Purpose

Adjusts the fuel-to-air ratio.

95
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Normal DA40 Cylinder Head Temperature

300300-400F-400^\circ F.

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Maximum DA40 Cylinder Head Temperature

475F475^\circ F.

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Normal Exhaust Gas Temperature (EGT)

13001300-1400F-1400^\circ F.

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Methods to Lower Engine Temps

Enrich mixture, increase airspeed, reduce climb angle, or reduce power.

99
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DA40 Max Oil Quantity

8quarts8\,quarts.

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DA40 Minimum Oil for Dispatch (UVU SOP)

6quarts6\,quarts.