Gear Won't Come Down
A Piper Arrow's landing gear refuses to extend on approach to Venice — troubleshooting, emergency procedures, and a non-standard landing decision
The scenario
Departing Venice Municipal Airport (KVNC), Venice, FL — Runway 22, a 5,000 ft asphalt runway on a heading of 225° true. Elevation 18 ft MSL. You are returning from a 1.5-hour cross-country flight to a nearby field; the return leg is 45 minutes, VFR, clear skies, light winds from the northeast at 4 knots. Altimeter 30.12, OAT 24°C. You are in Class G airspace (non-towered, CTAF frequency 122.8).
Aircraft: Piper Arrow PA-28R, solo, 2,650 lb gross weight, within limits. Lycoming IO-360 fuel-injected engine, constant-speed prop, retractable gear. The airplane was serviced after the last flight; nothing was written up. You performed a full preflight, including a visual gear-down check (three green lights on the gear panel). The gear cycled normally during the preflight test.
You are on a 10-mile straight-in approach to Runway 22, descending through 1,200 ft AGL, 90 KIAS (Vy, gear down). You lower the landing gear. The gear-down light illuminates — all three greens. You continue the descent, configuring for landing: flaps to 10°, then 20°, then full 40° (Vfe 103 KIAS). At 500 ft AGL, 2 miles from the runway, you glance at the gear panel. The right main gear light is AMBER — unsafe indication. The left main and nose gear lights remain GREEN.
Pilot: you — a Commercial pilot, 800 hours total, 120 hours in type (Piper Arrow). You are current and proficient. You have never experienced a gear malfunction in this airplane. You have read the POH emergency procedures section but have not practiced the emergency gear extension sequence in the sim or in flight.
- {'label': 'Field', 'value': 'KVNC · Venice'}
- {'label': 'Runways', 'value': '4/22 · 13/31'}
- {'label': 'Elevation', 'value': '18 ft'}
- {'label': 'Aircraft', 'value': 'PA-28R'}
- {'label': 'Dominant phase', 'value': 'Landing / Takeoff'}
The decision
Before the decision tree — what do you know about the Piper Arrow's landing gear system and emergency extension? (Pick all that apply.)
What the record shows
What the NTSB files show
NTSB WPR22LA040 (2021): A Piper PA-28R-200 on a personal flight experienced a right main landing gear that would not extend during approach to a California airport. The pilot landed on the left main and nose gear; the right wing scraped the runway and the aircraft exited the runway. The probable cause was the installation of an improper right main landing gear door rod-end bolt during maintenance, which prevented the landing gear from extending. This is a POST-MAINTENANCE FAILURE — the bolt was installed incorrectly, and no one caught it during the post-maintenance test flight.
NTSB CEN23LA417 (2023): A Piper PA-28RT-201 experienced partial retraction of the right main and nose landing gear during landing rollout, causing the right wing to scrape the runway and the aircraft to exit the runway. The cause of the gear retraction could not be determined despite extensive testing. The aircraft was damaged but not destroyed.
NTSB ERA15LA289 (2015): A Piper PA-28R-180 on an instructional flight at Fort Lauderdale Executive Airport experienced an unsafe nose landing gear indication and performed emergency extension procedures. The accident resulted from undetected fatigue cracks in the nose landing gear strut mount assembly that prevented proper gear alignment after extension, causing directional control loss and a runway excursion during landing. The pilot used the emergency extension procedure, but the gear was still misaligned due to the fatigue cracks.
NTSB CEN11LA418 (2011): A Piper PA-28R-201 made a wheels-up landing after the landing gear power pack motor failed and the pilot did not use the emergency extension system. The probable cause was the pilot's failure to use the emergency landing gear extension system, with a contributing factor being the inoperative landing gear power pack motor. This is a critical lesson: the PA-28R has a manual emergency extension crank in the cabin. If the hydraulic system fails, the pilot can mechanically extend the gear by cranking. The pilot in this case did not know about it, or did not attempt it, and landed wheels-up.
Venice Municipal Airport (KVNC) is a non-towered, Class G airport. There is no control tower to advise you of a gear malfunction or to coordinate emergency services. The CTAF frequency (122.8) is your only radio resource. You must make the decision to troubleshoot, go around, or land — and you must do it alone. The off-field environment off Runway 22's departure end (heading 225°) is open water — the Gulf of Mexico. An engine failure on the Runway 22 departure at low altitude is a ditching, not a field landing. This scenario does not involve an engine failure, but the geographic constraint is real: Runway 22 is the departure runway; Runway 13 is the longer runway and is aligned more favorably with the wind.
The real accidents cited above occurred at other airports — NOT at Venice Municipal Airport. KVNC has its own accident history (see field dominant patterns: LOSS_OF_CONTROL_INFLIGHT 24.4%, FORCED_LANDING 12.2%, SPATIAL_DISORIENTATION 12.2%, HARD_LANDING 12.2%, LOSS_OF_CONTROL_GROUND 12.2%), but these specific gear-malfunction events happened elsewhere. The scenario is localized to KVNC to make the field's non-towered status and runway environment real for you as a student here.
Key lesson — In the Piper Arrow, a landing gear malfunction is a serious emergency that requires immediate troubleshooting at altitude. An amber light on any gear is an UNSAFE indication — do not assume the light is faulty. Cycle the gear (retract fully, wait, extend) to see if the unsafe indication clears. If it does not, use the manual emergency gear extension crank to mechanically extend the gear. If the gear still will not extend, land on whatever gear is down — but expect a wing scrape and a runway excursion. The worst outcome is a wheels-up landing because the pilot did not know about or did not use the emergency extension system. Know your emergency procedures before you need them.
Debrief — teaching points
An amber gear light is an UNSAFE indication — troubleshoot immediately at altitude.
The Piper Arrow's landing gear indication system uses three green lights (left main, right main, nose) to indicate all gear is down and locked. An amber light on any gear means UNSAFE — the gear may not be fully extended, locked, or aligned. Do not assume the light is faulty. At 500 ft AGL on approach, you have time to troubleshoot: climb back to 1,000 ft AGL, cycle the gear (retract fully, wait 10 seconds, extend), and see if the unsafe indication clears. If it does, you have solved the problem. If it does not, you have options: emergency extension, divert to a longer runway, or declare an emergency. The worst decision is to ignore the amber light and land on whatever gear is down.
The PA-28R has a manual emergency gear extension system — use it if the hydraulic system fails.
The Piper Arrow's landing gear is hydraulically actuated by an electric motor-driven pump. If the pump fails, the hydraulic pressure is lost and the gear will not extend. However, the PA-28R has a manual emergency gear extension crank located on the floor between the seats. This mechanical linkage allows you to manually extend the gear by cranking, even if the hydraulic system is completely inoperative. The crank is stiff and requires 20–30 seconds of steady cranking to fully extend the gear, but it works. Know where the crank is located and practice using it in the sim or during a checkout flight. The NTSB CEN11LA418 (2011) pilot did not use the emergency crank and made a wheels-up landing — a preventable accident.
A single-gear landing results in a wing scrape and a runway excursion — not a survivable outcome.
If you land on the left main and nose gear only (right main gear not extended), the right wing will scrape the runway. The aircraft will veer to the right and exit the runway. The wing damage is significant — leading edge scrape, bent wing tip, possible structural damage. The NTSB WPR22LA040 (2021) and CEN23LA417 (2023) cases both resulted in single-gear landings and runway excursions. The aircraft are repairable, but the damage is extensive and the landing is not controlled. Troubleshoot the amber light before committing to landing.
Gear cycle (retract, wait, extend) is the first troubleshooting step — it often clears a faulty light.
Many gear-malfunction incidents are caused by a faulty light circuit, not an actual gear extension failure. The gear may be fully extended and locked, but the light circuit is intermittent or shorted. A gear cycle often clears the faulty light: retract the gear fully (all lights go out), wait 10 seconds, then extend the gear again. If the unsafe indication was a light fault, the light will come on GREEN on the second extension. If the unsafe indication persists, you have a mechanical problem and must use the emergency extension crank or land on whatever gear is down.
Venice Municipal Airport is non-towered (Class G, CTAF 122.8) — you are the pilot in command, making all decisions alone.
KVNC has no control tower. You are on CTAF frequency 122.8. You must make the decision to troubleshoot, go around, or land — and you must do it without ATC guidance. If you declare an emergency on CTAF, other aircraft in the area will hear it and may provide assistance or information. Emergency services (fire, rescue) are not automatically standing by — you must request them. Know the field's layout, runway lengths, and off-field environment before you arrive. Runway 22 is 5,000 ft; Runway 13 is 5,640 ft. Runway 13 is the longer option if you need extra landing distance due to a gear malfunction.
Post-maintenance failures are real — a gear malfunction after recent maintenance warrants a thorough inspection.
The NTSB WPR22LA040 (2021) case involved an improper gear door rod-end bolt installed during maintenance. The bolt was installed incorrectly, and it prevented the landing gear from extending. The pilot had no way to know this during the preflight — the gear cycled normally in the preflight test. But the improper bolt was a time-bomb waiting to fail on the actual landing. If you have recent maintenance on the gear system (door rods, hydraulic lines, motor, light circuit), be extra vigilant for any anomaly during the approach. A gear cycle that clears the unsafe indication may still mask a mechanical problem that will fail during the actual landing.
Built from the real accident record
Scenario built from NTSB CEN23LA417 (2023 PA-28RT-201 partial gear retraction during landing), WPR22LA040 (2021 PA-28R-200 right main gear extension failure), ERA15LA289 (2015 PA-28R-180 unsafe nose gear indication / directional control loss), and CEN11LA418 (2011 PA-28R-201 wheels-up landing after power pack failure). Anonymized and localized to KVNC.
NTSB reports: CEN23LA417 · WPR22LA040 · ERA15LA289 · CEN11LA418
ACS tasks: PA.II.C — Preflight Inspection · PA.III.A — Normal Approach and Landing · PA.IX.C — Emergency Approach and Landing · PA.IX.D — Systems and Equipment Malfunctions · PA.I.H — Human Factors
Relevant FARs: §91.3 · §91.13 · §91.185
Step through the full decision tree, make the calls, and see where each choice leads — then debrief it with your CFI.
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