N88AG - 1974 PIPER PA-34-200 - Complete Aircraft History & Registry Information

Quick Facts & Current Owner

Current Owner
RUIZ NAILE C
Location
DAVIE, Florida
Registration Status
Active until 02-29-2032
Serial Number
34-7450093
Last Seen on Market
Never Listed
Last Seen Airborne
No Recent Activity
Last FAA Action Date
February 2025
Owned Since
February 2025
Location of N88AG in DAVIE, Florida

About the PIPER PA-34-200

The Piper PA-34-200, commonly known as the Seneca I, is a well-regarded light twin-engine aircraft produced by Piper Aircraft. The PA-34 series was introduced to provide pilots and small-scale operators with a powerful and reliable multi-engine platform, ideal for both personal and business aviation needs. The Seneca I variant, which began production in 1971, laid the foundation for what would become one of Piper's mainstays in their twin-engine lineup.

The development of the PA-34-200 was motivated by Piper's desire to create a twin-engine aircraft that would bridge the gap between their highly popular single-engine models, such as the Piper Cherokee, and the more advanced twin-engine market. The Seneca I was specifically targeted at pilots seeking a twin-engine trainer as well as a dependable aircraft for personal and small business transportation.

Key Features and Capabilities

Production of the PA-34-200 lasted until 1975, during which time approximately 930 units were built. The aircraft's design featured two six-cylinder Lycoming O-360 engines, each producing 200 horsepower. This configuration provided the Seneca I with a healthy mix of performance, range, and reliability, making it attractive to flight schools and private owners alike. The Seneca I could carry up to six occupants, with comfortable seating arrangements and an impressive range of just over 700 nautical miles.

One of the unique aspects of the PA-34-200 was its counter-rotating propellers, which helped to reduce the aircraft's critical engine factor and improved overall handling, particularly in single-engine operations. This feature increased the safety margin for pilots and contributed to the aircraft’s reputation as a solid and dependable performer.

Market Position and Use Cases

The Piper Seneca series has evolved through several iterations beyond the initial PA-34-200 model, with each version bringing enhancements in avionics, performance, and comfort. However, the Seneca I remains noteworthy for establishing the series' legacy and proving Piper's ability to produce versatile and reliable twin-engine aircraft that continue to serve the general aviation community to this day.



Flight History and Activity for N88AG

No flight activity has been observed for this aircraft since 2022.

This could indicate the aircraft is in storage, undergoing maintenance, or operating in areas without flight tracking coverage.

Maintenance and Safety Records

Safety Record Summary

  • 4 accident/incident report(s) on file

Accident and Incident Reports

September 11, 2018 - OCHOPEE, Florida

Damage Level
Substantial
Description
PART 141 OPERATION, OPERATED BY AMERICAN FLIGHT TRAINING LLC AND OWNED BY MY WAY AVIATION LLC WESTON FLORIDA, PIPER PA-34-200, N88AG, AND SERIAL NUMBER: 34-7450093. AIRCRAFT WITH CFI AND PILOT ON BOARD PREFORMING SIMULATED ENGINE OUT SITUATION LOSING CONTROL OF AIRCRAFT LANDING HARD ON RUNWAY 9 AND RUNNING OFF THE EDGE OF RUNWAY COMING TO A STOP IN A RETENTION POND IN WATER, CFI AND PILOT ON BOARD UNINJURED.

September 21, 2019 - OPALOCKA, Florida

Damage Level
Minor
Description
A PART 141 FLIGHT OPERATED BY WAYMAN AVIATION (1WLS) LANDED AND THE NOSE GEAR COLLAPSED. AIRCRAFT ACCIDENT/INCIDENT PRELIMINARY NOTICE DESCRIPTION: N88AG WAS CLEARED TO LAND RY9L. ON TOUCHDOWN THE NOSE GEAR COLLAPSED. THE AIRCRAFT STAYED ON THE RUNWAY. THE FLIGHT WAS AN INSTRUCTIONAL FLIGHT WITH INSTRUCTOR AND STUDENT PREPARING FOR AMEL COMMERCIAL CHECK RIDE. AIRCRAFT WAS CLEARED FOR LANDING AND STUDENT COMPLETED PRE-LANDING CHECKLIST AND VERIFIED THREE LANDING GEAR GREEN LIGHTS. MADE A NORMAL FIRM LANDING AND THE NOSE GEAR COLLAPSED. BOTH PROPELLERS STOPPED DUE TO GROUND CONTACT AND AIRCRAFT CAME TO A STOP. EXAMINATION OF THE AIRCRAFT REVEALED LEFT AND RIGHT PROPELLER CURLED, NOSE CONE LOWER AREA SCARED, AND BOTH NOSE LANDING GEAR DOOR DAMAGE. INSPECTION OF THE NOSE GEAR REVEALED DOWN LOCK SPRING LINK (95829-00) ADJUSTMENT LOCK NUT WAS LOOSE AND CROSS PIN SLOT WAS ELONGATED. FURTHER EXAMINATION FOUND THE NUT (MS21042-3) AND WASHER (NAS1149C0363R) MISSING FROM NOSE GEAR DOOR LINK ASSEMBLY. MAINTENANCE RECORDS REVILED THE AIRCRAFT HAD PREVIOUSLY UNDERGONE THE REPLACEMENT OF THE NOSE LANDING GEAR FROM ANOTHER AIRCRAFT AT 6711.5 TOTAL TIME BY WAYMAN AVIATION LLC. FAA CRS# 4WVR269D UNDER WORK ORDER #000331 ON 08/29/2019. THE TOTAL TIME BETWEEN THE MAINTENANCE EVENT AND THE COLLAPSE WAS 34.1 HOURS. PRINCIPLE INSPECTORS (PI) NOTIFIED AND REGULATORY NON COMPLIANCE INITIATED BY PI FOR WAYMAN AVIATION LLC. FAA CRS# 4WVR269D.

May 24, 2014 - ST. PETERSBURG, Florida

Damage Level
Minor

September 11, 2018 - Miami, Florida

Damage Level
Substantial
Description
The flight instructor in the multiengine airplane reported that the pilot under instruction was conducting a simulated instrument approach in visual flight rules conditions. The instructor placed the left engine fuel selector in the "off" position to simulate an engine out, and the pilot under instruction initiated the left engine failure procedure by placing the engine and propeller levers in a simulated feathered zero-thrust configuration. The instructor became distracted by traffic and failed to place the left engine fuel selector back to the "on" position. With full flaps and the landing gear extended and while about 250 ft above ground level, the instructor terminated the simulated instrument approach and instructed the pilot to land visually; however, the airspeed decreased below safe limits, and he instructed the pilot to increase the airspeed. The pilot increased power on both engines; however, the left engine power did not increase, and the airplane rolled to the left about 45Β°. The instructor took the controls and applied right aileron and rudder, but the airplane settled down in a level attitude in a shallow lagoon on the left side of the runway. The airplane sustained substantial damage to the forward fuselage bulkheads. The instructor reported that there were no mechanical malfunctions or failures with the airplane that would have precluded normal operation.

Complete History Timeline

πŸ“‹

Feb 2025

Registration

Registered to RUIZ NAILE C in DAVIE, FL




πŸ“‹

Jan 2025

Registration

Registered to CSC DELAWARE TRUST CO TRUSTEE in WILMINGTON, DE




πŸ“‹

Sep 2023

Registration

Registered to DELAWARE TRUST CO TRUSTEE in WILMINGTON, DE




πŸ“‹

Apr 2022

Registration

Registered to DELAWARE TRUST CO TRUSTEE in WILMINGTON, DE




⚠️

Sep 2019

Accident/Incident

Accident with minor damage




πŸ“‹

Sep 2019

Registration

Registered to DELAWARE TRUST CO TRUSTEE in WILMINGTON, DE




⚠️

Sep 2018

Accident/Incident

Accident with substantial damage




⚠️

Sep 2018

Accident/Incident

Accident with substantial damage




πŸ“‹

May 2017

Registration

Registered to MY WAY AVIATION LLC in WESTON, FL




πŸ“‹

May 2015

Registration

Registered to DELAND AVIATION LLC in DELAND, FL




⚠️

May 2014

Accident/Incident

Accident with minor damage




πŸ“‹

Apr 2012

Registration

Registered to THORPE ARTHUR N in WASHINGTON, DC




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Frequently Asked Questions

Who owns N88AG?

N88AG is currently registered to RUIZ NAILE C in DAVIE, Florida.

What type of aircraft is N88AG?

N88AG is a 1974 PIPER PA-34-200 with serial number 34-7450093.

Has N88AG been in any accidents?

Yes, N88AG has 4 accident/incident report(s) on file with the FAA/NTSB.