Piper PA-28R-200 accident near Boscobel, Wisconsin, December 2, 2024
On December 2, 2024, a 1974 Piper PA-28R-200, registered N41997, was substantially damaged in an accident during enroute (cruise) near Boscobel, Wisconsin (Boscobel airport). It was an instructional flight under general aviation rules (Part 91). No one was hurt; 2 people were on board or involved. The weather was visual conditions (good weather).
The NTSB's probable cause their words, unchanged
The ice obstruction of the engine oil breather tube and alternate air outlet, which resulted in a failure of the crankcase oil seal and loss of engine oil. Contributing to the accident was the incorrect engine oil breather tube installed in the airplane by maintenance personnel.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- December 2, 2024
- Place
- Boscobel, Wisconsin · Boscobel · map
- Type
- Accident
- Injuries
- No one was hurt; 2 people were on board or involved.
- Weather
- visual conditions (good weather)
- Aircraft
- Piper PA-28R-200, built 1974 · all PA-28R-200s on the register
- Registration
- N41997 · registry record · serial 28R-7435235
- Damage
- Substantial damage
- Flight
- Instructional flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
During cruise on the return leg of a night cross-country instructional flight at 9,000 ft mean sea level (msl), the flight instructor and student pilot noticed an odor in the cockpit. The flight instructor then noticed an opaque windscreen and immediately thought they had encountered icing conditions. The flight instructor contacted air traffic control (ATC) and requested a lower altitude. Using a flashlight, the flight instructor illuminated the windscreen and noticed a “brown river” completely obscuring their forward visibility. The cockpit engine oil pressure gauge indicated little to no oil pressure. The flight instructor declared an emergency with ATC and assumed control of the airplane from the pilot receiving instruction. The flight instructor located the nearest airport to attempt a forced landing. However, due to restricted visibility due to the oil-covered windscreen, the airplane landed hard adjacent to the runway, bounced, and then came to rest upright on the ground. The airplane sustained substantial damage to the right horizontal stabilator, and the airframe contained engine oil on the top engine cowling, windscreen, and empennage. During recovery of the airplane, recovery personnel noted that ice obstructed the engine oil breather tube and the alternate air outlet. The obstructed breather tube created increased crankcase pressure and caused the extrusion of the solid-ring crankshaft oil seal from the crankcase and subsequent loss of engine oil. Airplane records showed that the oil engine breather tube was replaced about 18 years before the accident. The design, fabrication, and installation of the accident airplane’s oil breather tube did not comply with the airplane manufacturer’s original design criteria. Specifically, the oil breather tube protruded about 3” outside the engine cowling when it should only extend 0.5”. The additional length of oil breather tube outside of the engine cowling would be more susceptible to ice accretion during flight. Additionally, the replaced oil breather tube was not fabricated with alternate air outlets that were positioned within the engine compartment, which would have provided an unobstructed vent after the primary outlet became contaminated with ice during the flight.
The complete narrative as the NTSB published it. The NTSB's docket holds the report as a PDF and any photographs, statements and other documents from the investigation.
The factual record from the NTSB's investigation tables, in plain English
What happened, in order
- Powerplant sys/comp malf/fail during enroute (cruise)
- Collision with terrain or object (not controlled flight into terrain) during landing
- Structural icing during enroute (cruise) defining event
The NTSB's findings
- Environmental issues › Conditions/weather/phenomena › Temp/humidity/pressure › Conducive to structural icing › Effect on equipment
- Aircraft › Aircraft power plant › Eng oil sys (airframe furnish) › Pressure › Malfunction
- Personnel issues › Task performance › Maintenance › Installation › Maintenance personnel
Pilot
- Certificate: airline transport pilot, flight instructor, commercial pilot
- Ratings: multi-engine land; single-engine land; single-engine sea; instructor: airplane multi-engine; instructor: airplane single-engine; instructor: instrument airplane; instrument: airplane
- Flight time: 12,000 hours in all; 100 in this make and model; 200 in the last 90 days; 60 in the last 30 days; 4,300 as pilot in command; 2,200 on instruments
- Last flight review: June 29, 2024
- Medical certificate: Class 1 (with waivers/limitations)
- Seat: rgt
- Injury: no injuries
Dual student
- Certificate: private
- Ratings: single-engine land; instrument: airplane
- Last flight review: October 1, 2024
- Medical certificate: Unknown
- Seat: left
- Injury: no injuries
The aircraft
- Airframe total time: 4,972 hours
- Last inspection: annual inspection, August 26, 2024
- Maximum gross weight: 2,650 lb
- Seats: 4
- Landing gear: retractable
- Engine: Lycoming IO-360-C1C (piston); 3,000 hours total
The flight
- Departed from: FRM Fairmont MN at 11:05 pm
- Destination: 3CK Lake In The Hills IL
- Flight plan: IFR
- Runway 07/2, 5,000 ft by 75 ft
- A second pilot was aboard
Weather at the time
- Light: night, dark
- Wind: from 020° at 4 knots
- Visibility: 10 statute miles
- Sky: clear
- Temperature: 14°F (-10°C), dew point 7°F (-14°C)
- Altimeter: 30.34 inHg
- Observation at 6:53 pm from KOVS
Weather report (METAR): KOVS 020053Z AUTO 02004KT 10SM CLR M10/M14 A3034 RMK AO2 SLP292 T11001139 $
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 2 |
Photographs from the investigation 4 pictures from the NTSB's docket, as the NTSB released them
PG 2 Photograph 1 – Accident Airplane
PG 3 Photograph 2 – Ice obstructed engine oil breather tube and alternate air outlet
PG 4 Photograph 3 – Extruded crankshaft oil seal
PG 5 Photograph 4 – Engine oil breather tube with alternate air outlet and location of engine cowlingThe NTSB's photographs with the NTSB's captions, at screen size. Open a picture to see it full size or to report one that should not be shown.
Documents from the investigation the NTSB's docket: the evidence folder behind the report
7 documents, released by the NTSB on April 1, 2025. View them here, or download them; the NTSB redacts some personal details before release, and this site shows the NTSB's own titles rather than its file names.
| # | Document | What it is | |
|---|---|---|---|
| 1 | Pilot/operator Aircraft Accident Report, NTSB Form 6120.1 | PDF, 10 pages | View Download |
| 2 | Aircraft Examination Summary | PDF, 12 pages | View Download |
| 3 | Memorandum of Record - Recovery Company | PDF, 1 page | View Download |
| 4 | Maintenance Entry - Engine Oil Breather Tube Installation | PDF, 1 page | View Download |
| 5 | Investigation Photographs | PDF, 5 pages · our copy | View Download |
| 6 | Statement of Party Representatives to NTSB Investigation | PDF, 1 page | View Download |
| 7 | Release of Aircraft Wreckage, NTSB Form 6120.15 | PDF, 2 pages | View Download |
The same docket at the NTSB · documents without a copy here are fetched from the NTSB when you open them.
Everything on this page comes from the NTSB's public records. The narrative, probable cause and findings are the NTSB's own words; the coded tables behind the report are written out in plain English, with pilots' ages, home towns and medical details left out. The documents and photographs are the NTSB's docket, shown as the NTSB released them. This site's own text never names anyone involved. A preliminary report can change; the final report usually follows one to two years later, and the page is refreshed when it does.
