Schweizer 269C-1 accident near Allentown, Pennsylvania, June 17, 2014
On June 17, 2014 at about 4:05 pm local time, a 2002 Schweizer 269C-1 (helicopter), registered N152CC, was substantially damaged in an accident during standing (engine(s) operating) near Allentown, Pennsylvania (Lehigh Valley International airport). It was an instructional flight under general aviation rules (Part 91). 1 person had minor injuries. The weather was visual conditions (good weather).
The NTSB's probable cause their words, unchanged
Inadequate inspection and maintenance of the helicopter’s landing gear dampers, which resulted in ground resonance during helicopter shutdown.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- June 17, 2014 · about 4:05 pm local time
- Place
- Allentown, Pennsylvania · Lehigh Valley International · map
- Type
- Accident
- Injuries
- 1 person had minor injuries.
- Weather
- visual conditions (good weather)
- Aircraft
- Schweizer 269C-1, built 2002 · all 269C-1s on the register
- Registration
- N152CC · no longer on the register · serial 0144
- Damage
- Substantial damage
- Flight
- Instructional flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
The student pilot landed the helicopter after a 40-minute flight and started the engine shut down procedures. She stated that she applied the collective friction and started the timer, running the engine at 2,500 rpm for a cool-down period. She turned off the fuel boost pump and radios and referred to the checklist to ensure she had completed the proper items. She then engaged the collective friction and was tightening the cyclic friction at the cyclic base when the helicopter developed ground resonance. The student pilot could not get the helicopter airborne with the collective friction engaged, so she rolled the throttle to idle. The resonance continued to increase and, "in a matter of seconds, the helicopter shook itself apart." The helicopter had four poppet-type, nitrogen-charged hydraulic units (dampers) in the landing gear assembly to reduce landing shock and help prevent ground resonance. The four dampers were removed from the helicopter and pressure tested; all four failed to meet manufacturer's specifications. Without the airframe protection provided by the dampers, oscillations occurred that resulted in the helicopter rocking on its landing gear and the tailboom twisting toward the right side of the helicopter where it joined the main structure. Maintenance instructions noted that the landing gear dampers would experience a decrease in pressure with helicopter usage and required that they be extension-checked during each 100-hour inspection or every 6 months, whichever occurred first. The helicopter's most recent 100-hour inspection occurred about 2 months before the accident, and it had been operated 58 hours since the inspection. Review of maintenance records for the most recent 100-hour inspection and about 800 flight hours before the accident revealed no mention of any maintenance actions involving the dampers.
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
- Ground resonance during standing (engine(s) operating) defining event
- Aircraft structural failure during standing (engine(s) operating)
The NTSB's findings
- Aircraft › Aircraft systems › Landing gear system › Main gear strut/axle/truck › Damaged/degraded
- cause Aircraft › Aircraft systems › Landing gear system › Main gear strut/axle/truck › Not serviced/maintained
- cause Personnel issues › Task performance › Inspection › Scheduled/routine inspection › Maintenance personnel
Dual student
- Certificate: airline transport pilot, student
- Ratings: multi-engine land; single-engine land; instructor: airplane multi-engine; instructor: airplane single-engine; instrument: airplane
- Flight time: 5,500 hours in all; 38 in this make and model; 74 in the last 90 days; 14 in the last 30 days; 4,545 as pilot in command; 1,777 on instruments
- Last flight review: December 8, 2013
- Medical certificate: Class 1 (with waivers/limitations)
- Seat: rgt
- Injury: minor injuries
The aircraft
- Airframe total time: 3,345 hours
- Last inspection: 100-hour inspection, April 24, 2014; 58 hours since
- Maximum gross weight: 1,750 lb
- Seats: 2
- Landing gear: fixed
- Engine: Lycoming HIO-360-G1A (piston); 1,320 hours total
The flight
- Departed from: ABE Allentown PA
- Destination: ABE Allentown PA
- Flight plan: none
Weather at the time
- Light: daylight
- Wind: from 250° at 8 knots
- Visibility: 10 statute miles
- Sky: scat at 5,000 ft
- Temperature: 88°F (31°C), dew point 66°F (19°C)
- Altimeter: 30.04 inHg
- Observation at 3:51 pm from ABE
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 1 |
Documents from the investigation the NTSB's docket: the evidence folder behind the report
11 documents, released by the NTSB on March 2, 2017. 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, 9 pages | View Download |
| 2 | Memo of Record - Permission to Include Sikorsky Engineering Report in Docket | PDF, 1 page | View Download |
| 3 | Sikorsky Aircraft Engineering Examination Report | PDF, 9 pages | View Download |
| 4 | Sikorsky Alert Service Bulletin C1B-041 | PDF, 8 pages | View Download |
| 5 | Excerpt #1, Sikorsky Pilot Flight Manual as of 10-17-2014 | PDF, 9 pages | View Download |
| 6 | Excerpt #2, Sikorsky Pilot Flight Manual as of 10-17-2014 | PDF, 1 page | View Download |
| 7 | Excerpt, Basic Hmi, Section 12, Rev 2010 | PDF, 2 pages | View Download |
| 8 | Excerpt, Sikorsky Overhaul Manual as of 10-17-2014 | PDF, 3 pages | View Download |
| 9 | Memorandum for Record - Maintenance Summaries | PDF, 1 page | View Download |
| 10 | Statement of Party Representatives to NTSB Investigation | PDF, 1 page | View Download |
| 11 | Photo | PDF, 1 page | 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.
