Private Pilot EOC Stage-Check Oral – Comprehensive Bullet-Point Notes

References and Study Materials

  • 2024 FAR/AIM
  • Pilot’s Handbook of Aeronautical Knowledge (PHAK)
  • FAA-H-8083-25 (PHAK edition reference)
  • AC 00-45G Change 2 – Aviation Weather Services
  • AIM – Aviation Weather Information Manual
  • Cessna 152/172 POH (Information/Operating Manuals)
    • 152 POH Revision info
    • 172R & 172SP POH (Revision 5, 15 Jul 2004)

Stage-Check / Checkride – Required Items to Bring

  • Physical or online POH (aircraft specific)
  • Current FAR/AIM
  • Current sectional chart & Chart Supplement
  • Recent weather briefing printout/notes
  • Completed weight-&-balance + performance sheet
  • VFR nav-log (fully computed)
  • “Toy” aircraft or model (for teaching/explaining)
  • View-limiting device
  • Cash for examiner fee
  • Logbook tabbed & endorsements marked
  • Printed IACRA application with highlighted FTN
  • Required PIC docs: government ID, FAA medical, student cert.
  • Knowledge-exam report with ACS-coded missed questions

Certificates & Documents

  • Required on-person to act as PIC (61.3)
    • Pilot certificate
    • Medical certificate
    • Government photo ID
    • Student pilots additionally need logbook with endorsements
  • Student Pilot Limitations (61.89)
    1. No passengers
    2. No carriage of property for compensation/hire
    3. No flight in furtherance of a business
    4. Visibility ≥ 3sm3\,sm day / 5sm5\,sm night; must remain with surface reference
  • Private-Pilot Privileges & Limitations (61.113 / 91.146)
    • May act as PIC & carry passengers
    • May conduct SAR ops, charity/community flights, airplane sales demo (> 200200 hrs)
    • Must pay no less than pro-rata share; no hire/compensation
  • Certificate duration (61.19)
    • Student certs issued after 1 Apr 2016 – no expiration, superseded by higher rating
    • PPL, CPL, CFI, ATP, Ground Instructor – no expiration
  • Keeping Certificate Current (61.56/61.57)
    • Student = valid medical
    • PPL = Flight Review every 24 calendar months + valid medical
  • Passenger-Currency (61.57)
    33 TO&L within preceding 9090 days, same cat/class/type
    • At night: full-stop & between 11 hr after sunset ↔ 11 hr before sunrise
  • Medical validity (61.23)
    • <40 yr: 1st =12 mo (ATP), 2nd =12 mo (Commercial), 3rd =60 mo (PPL)
    • ≥40 yr: 1st =6 mo, 2nd =12 mo, 3rd =24 mo

Aircraft Documents – “ARROW” (91.9 / 91.203)

  • Airworthiness certificate (never expires if maintained)
  • Registration (expires every 3 yr; 7 yr on new issue post-2023)
  • Radio station license (only for international)
  • Operating limitations ( POH / placards )
  • Weight & Balance data list (updated equipment list in POH/AFM)

Certification Terminology (61.5 / 61.31)

  • Category – e.g. Airplane, Rotorcraft, Glider, LTA
  • Class – e.g. SEL, SES, MEL, MES
  • Type – specific model requiring type rating: >12,50012,500 lbs MTOW, turbojet, or FAA-designated
  • Address change: may fly 3030 days without notifying FAA (61.60)

Airworthiness & Required Inspections – “AVIATES”

  • Annual – 12 cal mo, IA/CRS (91.409)
  • VOR – 30 days (IFR only) (91.171)
  • 100-hr – if for hire; tach time (may overfly ≤1010 hrs en-route to inspection)
  • Altimeter/Static – 24 cal mo (IFR) (91.411)
  • Transponder – 24 cal mo (91.413)
  • ELT – 12 cal mo, or after 11 hr cumulative use, or ½ battery life (91.207)
  • Service bulletins & ADs – comply as required
  • Airworthiness Directives (PHAK 8-12)
    • Emergency (immediate) • One-time • Recurring
  • Annual may NOT be over-flown except by Special Flight Permit (FSDO)
  • ELT not required within 50nm50\,nm training radius

Required VFR Equipment

  • Day (91.205 b) – “ATOMATOFLAMES”
    • Altimeter | Tachometer | Oil-Temp | Manifold-Pressure (CS prop) | Airspeed | Temperature (liquid-cooled) | Oil-Pressure | Fuel-Quantity | Landing-gear position | Anti-collision lights (post-11 Mar 1996) | Magnetic compass | ELT | Seat-belts
  • Night (91.205 c) – “FLAPS”
    • Fuses (spares) | Landing light (for-hire) | Anti-collision lights | Position (nav) lights | Source of power
  • Inoperative equipment procedure (91.213 d)
    • If no MEL: check 91.205, ADs, Kind-of-Ops list (POH Eqpt List), Placard & deactivate
    • MEL: Cessna 152/172 do NOT have FAA-approved MEL; use regs.

Aerodynamics & Performance

  • Four forces: Lift | Weight | Thrust | Drag
  • Primary controls: Ailerons, Elevator/Stabilator, Rudder
  • Secondary: Flaps, Trim (servo tab)
  • Lift production
    • Newton 3rd Law (downwash) • Bernoulli (↑velocity ↓pressure)
  • Drag types
    • Parasite = form + skin-friction + interference (↑ with speed)
    • Induced = byproduct of lift, ↓ with speed; wingtip vortices, rear-tilted lift vector
    • L/D max = VGV_G (best glide)
  • Airfoil terms: camber (changeable via flaps); chord; angle of incidence (fixed); CG
  • CG shifts
    • Fwd: ↓cruise spd, ↑stall spd, ↑stability, easier recovery, long flare required
    • Aft: ↑cruise spd, ↓stall spd, ↓stability, poor stall/spin recovery
  • Stall cause: critical AoA exceeded
  • Density-altitude formulas
    PA=h<em>field+(29.92altimeter)×1000PA = h<em>{field} + (29.92 - altimeter) \times 1000DA=PA+120×(OATISA</em>temp)DA = PA + 120 \times (OAT - ISA</em>{temp})
  • Factors reducing air density: Heat ↑, Height ↑, Humidity ↑
  • C152 Weights (POH 1-5) – Ramp 16751675 lb | TO/Ldg 16701670 lb
  • C172R – Ramp 24572457 lb | TO/Ldg 24502450 lb; 172SP – Ramp 25582558 lb | TO/Ldg 25502550 lb
  • Fuel weight: 6lb/gal6\,lb/gal (100LL blue)
  • V-Speeds (example)
    V<em>SOV<em>{SO} (152) 35kt35\,kt | V</em>S1V</em>{S1} 40kt40\,kt
    V<em>XV<em>X best angle | V</em>YV</em>Y best rate
    V<em>AV<em>A varies with weight (heavier → higher) • V</em>FE,V<em>NO,V</em>NEV</em>FE, V<em>NO, V</em>NE per POH
  • VGV_G glide: 152 = 60kt60\,kt, 172R = 65kt65\,kt, 172S = 68kt68\,kt (slower at lower weight)
  • Use V<em>XV<em>X to clear obstacles; V</em>YV</em>Y for quickest climb to altitude
  • Left-Turning Tendencies “TGAS”
    1. Torque 2. Gyroscopic precession 3. Asymmetric (P-factor) 4. Spiraling slipstream – ↑ at high power, high AoA, low airspeed
  • Stability
    • Lateral: dihedral, fuel balance
    • Longitudinal: proper CG, tail-down force
    • Vertical: vertical stabilizer aft CG
    • Static vs Dynamic; Positive / Neutral / Negative

Instruments & Compass

  • Pitot-Static • ASI uses pitot + static; Altimeter static vs sealed 29.9229.92 wafer; VSI static vs delayed static (calibrated leak) • Blockages quick-ref:
    • Pitot & drain blocked → ASI acts as altimeter
    • Pitot blocked, drain open → ASI reads 0
    • Static blocked → ASI reverse-trend, Alt & VSI frozen
  • Gyros (vacuum except electric turn coordinator)
    • Principles: Rigidity in space; Precession (force felt 9090^{\circ} ahead)
    • Attitude Ind – pendulous vanes keep erect
    • Heading Ind – must align w/ mag compass every ≈15 min (precession drift)
    • Turn Coordinator – canted gyro shows rate-of-roll & rate-of-turn
  • Magnetic-Compass Errors “V.D.M.O.N.A.”
    • Variation, Deviation, Magnetic Dip (N/S turning; ANDS acceleration), Oscillation

Engines & Aircraft Systems

  • Engines
    • C152 – Lycoming O-235-L2C 110hp110\,hp
    • 172R – IO-360-L2A 160hp160\,hp | 172SP – 180hp180\,hp
    • Horiz-opposed, Air-cooled, Normally-aspirated, Direct-drive, 4-stroke
  • 4 strokes: Intake → Compression → Power (ignition) → Exhaust
  • Oil (C152 4-6 qt, 172 6-8 qt): lubricates, cools, seals, cleans
  • Propellers: fixed-pitch (152 67.5-69"; 172R 74-75"; 172S 75-76")
  • Mixture control: maintains optimal fuel/air as density ↓ with altitude (prevents fouling)
  • Fuel system (C152): two vented wing tanks 24.5gal24.5\,gal each, selector ON/OFF, engine-driven pump + gravity, fuel strainer, taped-primer lines
    • 100LL = blue; 100/130 = green; Jet-A = clear/straw; mixing grades → clear
  • Fuel-sumping: water (≈8lb/gal8\,lb/gal) sinks; check grade/contaminants
  • Brakes: single-disc hydraulics, toe-operated
  • Vacuum: engine pump, suction gauge 4.5-5.5" Hg; filters → gyros → relief → vent
  • Electrical: 28-V, 60-A alternator; 24-V battery; buses & circuit breakers; engine‐ignition via magnetos (independent)

Airspace Overview

  • Controlled vs uncontrolled (Class G only uncontrolled)
  • Class summary (enter, equip, Wx):
    • A = FL180FL180-FL600FL600 IFR only, Mode C, no Wx mins
    • B = up to 10,00010,000' MSL; ATC clearance, Mode C veil 30nm30\,nm; 3sm3\,sm & clear-of-clouds
    • C = 5/10 nm sectors SFC-4,0004,000' AGL; two-way comm, Mode C; 31523\,152 rule
    • D = ≈4 nm r, SFC-2,5002,500' AGL; two-way comm; 31523\,152
    • E = varied floors to but not incl FL180FL180 (and >FL600FL600); <10,00010,000' MSL 31523\,152; >10,00010,000' 51115\,111
    • G = SFC to E-floor or 14,50014,500'; Day <1,2001,200' AGL: 1sm1\,sm clr-cloud; Night 31523\,152
  • KCRQ: Class D surface → 2,8002,800' MSL; above is Class E to 18,00018,000'

Special Use & Other Airspace “TTMCPRAWNSS”

  • TFR, TRSA, MOA, CFA, Prohibited, Restricted, Alert, Warning, NSA, SFRA, SFR/TRSA specific
  • Other:
    • Military Training Routes (IR/VR), Parachute Jumps, Published VFR corridors
  • Mode C transponder required: Class A/B/C, inside 30nm30\,nm veil, above Class C upper ceilings, >10,00010,000' MSL

Weather Theory & Hazards

  • ISA: 15C15^{\circ}C, 29.92"Hg29.92"Hg (1013.2mb1013.2\,mb) at sea level
  • Isobars: close spacing ⇒ strong gradient ⇒ strong winds; surface winds cross isobars (friction); aloft ≈ parallel (Coriolis)
  • Stable vs Unstable air characteristics
  • Pressure systems: Low (cyclone CCW, rising) vs High (anticyclone CW, descending)
  • Ridge = elongated high; Trough = elongated low
  • Thunderstorm requirements: Moisture, Unstable lapse-rate, Lifting action
    • Stages: Cumulus (updraft) → Mature (precip, up & down) → Dissipating (downdrafts)
  • Wind shear: rapid wind velocity/direction change; hazardous on takeoff/landing
  • Fog types: Advection, Radiation, Upslope, Precip-induced
  • Icing
    • Structural: Rime, Clear, Mixed
    • Induction: carb ice, intake icing
    • Instrument: pitot/static blockage
    • Effect: ↑weight, ↓lift, ↑drag, ↓thrust → stalls possible

Weather Information & Briefings

  • FSS Briefings (AIM 7-1-4): Standard, Abbreviated, Outlook
  • METAR: routine or SPECI; issued hourly, valid point-obs ≤1 hr
  • TAF: issued 4×/day; valid 24-30 hr; 5sm5\,sm radius
    • Codes: FM (rapid ≤1 hr); BECMG (gradual within 2 hr window); TEMPO (≤1 hr in period); PROBXX
  • AIRMET (Sierra IFR/mt-obs, Tango turb/30kts, Zulu moderate icing) – valid 6 hr
  • SIGMET (severe turb/icing, dust, ash) – valid 4 hr
  • Convective SIGMET: severe T-storm, hail ≥3/4"3/4", winds ≥5050 kt; hourly +55, valid 2 hr.
  • Winds/Temps Aloft (FD): 2×/day; temps negative above 24,00024,000'; code example 710556710556 at 30,00030,000' → wind 210/105kt210^{\circ}/105kt, temp 56C-56^{\circ}C
    • No wind within 1,500' of station; no temp within 2,500'.
  • Charts
    • Surface Analysis (8×/day, valid 3 hr)
    • Weather Depiction (8×/day, valid 8 hr)
    • SIGWX Prog (4×/day, 12 & 24 hr forecasts)
    • Radar Summary (each hr+35, valid 1 hr)

Flight-Planning & Regulations

  • Pre-flight required info “NWKRAFT” (91.103)
    • NOTAMs, Weather, Known ATC delays, Runway lengths, Alternates, Fuel req., Takeoff/Landing data
  • Fuel minimums (91.151): Day → dest. + 3030 min; Night → dest. + 4545 min (at normal cruise)
  • Right-of-Way hierarchy “EBGAAR”
    • Emergency, Balloon, Glider, Refueling, Airship, Rotor/Fixed-wing
    • Same cat: Converging–yield to right; Head-on–both right; Overtake–pass right side
  • Max IAS <10,00010,000' MSL: 250kt250\,kt (91.117)
  • Minimum safe altitudes (91.119)
    • Congested: 10001000' above highest within 20002000' horizontal
    • Elsewhere: 500500' AGL; sparsely populated: 500500' from person/vessel/structure
  • Light-gun signals (steady green = cleared land / takeoff; flashing green = return for land; steady red = give way; flashing red = unsafe; etc.)
  • LAHSO, Wake turbulence spacing, Stall/Spin recovery (PARE)
  • Pilotage: visual landmarks; Dead-reckoning: time & heading computations
  • Magnetic variation: angle between true & magnetic north (“East is least, West is best”)
  • VOR limitations: line-of-sight; service volume 25-130 nm per class
  • Lost – “5 Cs”: Climb, Circle, Conserve, Communicate, Confess
  • Chart Supplement (A/FD): update 56-day; full airport info

Aeromedical Factors

  • Three orientation systems: Vestibular (inner ear), Somatosensory, Visual
  • Ear/sinus pressure – avoid flying ill; use Valsalva
  • Hypoxia types: Hypoxic, Hypemic, Histotoxic, Stagnant – symptoms: euphoria, cyanosis, headache, poor judgment
  • Hyperventilation – treat by controlled breathing, talking, paper-bag
  • Spatial illusions “ICEFLAGS” (Inversion, Coriolis, Elevator, False horizon, Leans, Autokinesis, Graveyard spiral, Somatogravic)
  • Runway illusions: narrow/runway-up-slope looks high → low approach; etc.

Aeronautical Decision Making & Risk Management

  • ADM = systemic risk-assessment & stress-management
  • Hazardous Attitudes “RAIIM” + antidotes
    • Resignation – “I can make a difference.”
    • Anti-authority – “Follow the rules.”
    • Impulsivity – “Think first.”
    • Invulnerability – “It could happen to me.”
    • Macho – “Taking risks is foolish.”
  • IMSAFE personal checklist; PAVE & 5-Ps (Pilot, Passengers, Plane, Programming/Plan) to evaluate risk
  • DECIDE model: Detect → Estimate → Choose → Identify → Do → Evaluate
  • Positive exchange of controls (3-way verbal) – “You have,” “I have,” “You have.”

Special Emphasis Quick-Refs

  • Stall/Spin Recovery “PARE”: Power idle, Ailerons neutral, Rudder opposite, Elevator forward
  • Wake turbulence: takeoff rotate prior to preceding rotation point; land past touchdown point; avoid below/behind heavy
  • LAHSO: must read back “will comply”; declining is pilot’s prerogative