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ATL07LA004 · Piper PA-28R-180

7 Oct 2006 · Alabaster, AL, United States

Piper PA-28R-180 · Accident: main gear collapsed during landing

From Shelby County Airport (EET) to EET

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Event

NTSB case
ATL07LA004
Event typeAccident: someone killed or seriously injured, or the aircraft substantially damaged (NTSB definition). Incident: an occurrence that affected or could have affected safety, short of that. Glossary
Accident
InvestigationHow far the investigation had got when the record was published: preliminary, ongoing, final or completed. Unknown where the source does not say. Glossary
Completed
API-reported fatalities
0 · all aircraft and ground
Ground fatalities
Unknown
OperationWhat kind of flying it was, grouped by the rules it flew under: airline (US Part 121), air taxi and commuter (Part 135), general aviation (Part 91 and similar), military or government. Glossary
General aviation
WeatherVisual meteorological conditions (VMC): good enough to fly by looking outside. Instrument conditions (IMC): cloud or low visibility, flying by instruments. Glossary
Visual Meteorological Cond

Piper PA-28R-180

Aircraft type
Piper PA-28
Category
Airplane
RegistrationThe aircraft's tail number, such as N12345 or G-ABCD. Registrations are reissued, so the same one years apart can be a different aircraft. Glossary
N70SR
Onboard fatalities
Unknown
Route
From Shelby County Airport (EET), Alabaster, ALTo EET
Aircraft age
Not recorded
Flight rulesThe regulations the flight operated under: in the US, Part 91 (general aviation), Part 121 (airlines), Part 135 (air taxi and commuter) and others; for flights abroad, the NTSB's coarser commercial or non-commercial code. Glossary
Part 91: General Aviation
Phase of flightThe stage of the flight when things started to go wrong: standing, taxi, takeoff, initial climb, en route, maneuvering, approach or landing. Glossary
Landing · flare/touchdown
First occurrenceThe single coded event the NTSB judges best describes what happened (records from 2008 on). Older records name the first occurrence in the sequence instead. Glossary
Main gear collapsed
DamageDestroyed: beyond practical repair. Substantial: damage that affects the structure, performance or handling and normally needs major repair. Minor: less than that. Glossary
Substantial

Cause areas

  • Landing gear, normal retraction/extension assembly › Jammed

Approximate · Coordinates from the NTSB case API, which marks them as estimated or does not say; no uncertainty radius is established.

NTSB narrative

The pilot stated that he was practicing in preparation for his commercial pilot certificate. On the initial takeoff, after raising the gear, the pilot noticed the gear in-transit light remained on. The pilot pulled the landing gear pump circuit breaker. When he reset the breaker, he did not see a movement on the amp meter. He said this was an indication that the pump was not running. Although the in-transit light remained on, the pilot stated that the gear was up and locked. The pilot continued on to the practice area to do some air work, then he returned to the airport to do some touch-and-go landings. The pilot stated that on the first landing the gear went down normally and he had three green lights. On the takeoff he said the gear would not go up and lock. He cycled the gear handle several times. The pilot stated he had three green lights and the gear in-transit light was still on. The pilot stated the light was on for the entire flight. He said that he made a normal touchdown, and the right main gear collapsed veering the airplane to the right, off the runway. Examination of the airplane by an FAA Inspector found the nose and right main landing gear collapsed and structural damage to the wing ribs at the right main landing gear attach point. The airplane was placed in a hangar and jacked up for a retraction test. The gear handle was placed in the up position and the gear raised normally and the in-transit light was not on when the gear was up and locked. When the gear handle was placed in the down position the hydraulic pump operated but the gear did not extend. The landing gear remained up and locked. Striking the pump with a hammer freed the shuttle valve and the gear operated normally. According to the FAA Inspector the gear would not extend normally without striking the shuttle valve with a hammer.

Probable cause

The jammed landing gear hydraulic motor shuttle valve.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record ATL07LA004
Event ID
20061016X01523
Case number
ATL07LA004
Dataset
historical-pre2008
Source SHA-256
89e2df6d848e7ab3b42e7d7c7a03ff403303057a26ca04c95b3ea67201c3ce74
Source notes (4)
  • Unreviewed is an editorial label, not an investigation status. API-sourced is not report-checked or human-reviewed. Explicit event totals are used without summing aircraft injury tables; onboard allocation is withheld. Unknown values remain unknown. The operation category is mapped from the NTSB-reported FAR part and has not been reviewed.
  • Filled from the NTSB case API where the bulk record had no value: investigation status, coordinates. Values present in the bulk record are kept.
  • The date is the local date, which is the same as the UTC date the NTSB stores.
  • API snapshot SHA-256: 586f7260de2c247277372403bc92e2d9481bf9540e43da46a28721de14a94510; retrieved 2026-09-22T04:22:06.716Z.