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MIA99LA128 · Piper PA-44-180

14 Apr 1999 · Vero Beach, FL, United States

Piper PA-44-180 · Accident: airframe, component or system failure while maneuvering

From Vero Beach Regional Airport (VRB) to an unrecorded destination

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Event

NTSB case
MIA99LA128
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
0
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-44-180

Aircraft type
Piper PA-44
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
N30397
Operator
Unknown
Onboard fatalities
Unknown
Route
From Vero Beach Regional Airport (VRB)To not recorded
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
Maneuvering
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
Airframe, component or system failure
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

  • Other maintenance personnel › Maintenance, overhaul, improper
  • Other maintenance personnel › Procedures/directives, not followed

Approximate · Estimated position: the centre of Vero Beach, FL, the place the record names. Not the accident site.

NTSB narrative

While maneuvering the airplane at 4,000 feet above ground level, the flightcrew heard a loud noise from the left engine and saw that the left engine had dropped down about 45 degrees from the normal position. They returned to the departure airport for an emergency landing. When the landing gear was extended the left engine dropped down further. They were unable to maintain directional control due to the drag and made a forced landing in a wooded area. Post crash examination showed the left propeller hub had failed due to fatigue cracking causing a blade to separate. The remainder of the propeller separated when the propeller flange separated due to overstress and the engine dropped down when the engine mount separated due to overstress. The left propeller had sustained damage in a gear up landing 525 flight hours before the accident. The blades were bent beyond repairable limits and scrapped. The hub was inspected and returned to service with new blades. The manufacturer's procedures call for a hub to be retired if the blades receive damage beyond repairable limits and are scrapped.

Probable cause

The improper return to service of a propeller hub by a propeller overhaul company which according to manufacturer's procedures should have been retired due to damage to propeller blades from sudden stoppage. This resulted in undetected fatigue propagation through the hub and separation of a propeller blade in flight. This resulted in overstress separation of the propeller flange and the remainder of the propeller and overstress separation of the engine mount causing the engine to drop down making the aircraft uncontrollable.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record MIA99LA128
Event ID
20001205X00530
Case number
MIA99LA128
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. 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: 21d2b2c99f2319ca4442e57a67c8ea15ec86b329f098f85514bb9ae4a8f3d0a0; retrieved 2026-09-22T15:28:29.237Z.