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)
- No passengers
- No carriage of property for compensation/hire
- No flight in furtherance of a business
- Visibility ≥ 3sm day / 5sm 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 (> 200 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• Student certs issued after 1 Apr 2016 – no expiration, superseded by higher rating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)
• 3 TO&L within preceding 90 days, same cat/class/type
• At night: full-stop & between 1 hr after sunset ↔ 1 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: >12,500 lbs MTOW, turbojet, or FAA-designated
- Address change: may fly 30 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 ≤10 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 1 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 50nm 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.
- 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 = VG (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+(29.92−altimeter)×1000
• DA=PA+120×(OAT−ISA</em>temp) - Factors reducing air density: Heat ↑, Height ↑, Humidity ↑
- C152 Weights (POH 1-5) – Ramp 1675 lb | TO/Ldg 1670 lb
- C172R – Ramp 2457 lb | TO/Ldg 2450 lb; 172SP – Ramp 2558 lb | TO/Ldg 2550 lb
- Fuel weight: 6lb/gal (100LL blue)
- V-Speeds (example)
• V<em>SO (152) 35kt | V</em>S1 40kt
• V<em>X — best angle | V</em>Y best rate
• V<em>A varies with weight (heavier → higher)
• V</em>FE,V<em>NO,V</em>NE per POH - VG glide: 152 = 60kt, 172R = 65kt, 172S = 68kt (slower at lower weight)
- Use V<em>X to clear obstacles; V</em>Y for quickest climb to altitude
- Left-Turning Tendencies “TGAS”
- 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 29.92 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 90∘ 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 110hp
• 172R – IO-360-L2A 160hp | 172SP – 180hp
• 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 24.5gal 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/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 = FL180-FL600 IFR only, Mode C, no Wx mins
• B = up to 10,000′ MSL; ATC clearance, Mode C veil 30nm; 3sm & clear-of-clouds
• C = 5/10 nm sectors SFC-4,000′ AGL; two-way comm, Mode C; 3152 rule
• D = ≈4 nm r, SFC-2,500′ AGL; two-way comm; 3152
• E = varied floors to but not incl FL180 (and >FL600); <10,000′ MSL 3152; >10,000′ 5111
• G = SFC to E-floor or 14,500′; Day <1,200′ AGL: 1sm clr-cloud; Night 3152 - KCRQ: Class D surface → 2,800′ MSL; above is Class E to 18,000′
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 30nm veil, above Class C upper ceilings, >10,000′ MSL
Weather Theory & Hazards
- ISA: 15∘C, 29.92"Hg (1013.2mb) 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
- 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; 5sm 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", winds ≥50 kt; hourly +55, valid 2 hr.
- Winds/Temps Aloft (FD): 2×/day; temps negative above 24,000′; code example 710556 at 30,000′ → wind 210∘/105kt, temp −56∘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. + 30 min; Night → dest. + 45 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 <10,000′ MSL: 250kt (91.117)
- Minimum safe altitudes (91.119)
• Congested: 1000′ above highest within 2000′ horizontal
• Elsewhere: 500′ AGL; sparsely populated: 500′ 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)
Navigation & Lost Procedures
- 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