Skip to main content

Interagency Aviation Lessons Learned 18-01 Aircraft Accident Success Story

· DOI Office of Aviation Services

Public domain · DOI Office of Aviation ServicesAviation Safety Documents

Overview

The Interagency Aviation Lessons Learned 18-01 Aircraft Accident Success Story () is a public-domain DOI Office of Aviation Services aviation safety document, republished here as a free chaptered HTML edition with a linked table of contents and the official PDF.

Publisher
DOI Office of Aviation Services
Document
Pages
2

Key points

  • On August 5, 2017, a P2V-5F aircraft experienced a significant control issue shortly after takeoff but was safely landed without injuries.
  • The incident was classified as an accident by the NTSB due to substantial damage caused by a missing drive coupling bolt in the aircraft's variable camber stabilizer.
  • Crew Resource Management (CRM) training played a crucial role in the successful handling of the emergency situation by the pilot and first officer.
  • The pilot and first officer had recently completed a CRM refresher course, which prepared them for managing the aircraft without trim or elevator control.
  • The absence of the drive coupling bolt compromised the torque capabilities of the drive shaft, affecting the aircraft's control surfaces.
Frequently asked questions
What was the cause of the aircraft accident?

The accident was caused by a missing drive coupling bolt in the variable camber stabilizer, which hindered the torque capabilities of the drive shaft.

How did the crew manage to land the aircraft safely?

The crew utilized their CRM training to coordinate adjustments using wing flaps and engine power to manage the aircraft's pitch during the landing.

What is Crew Resource Management (CRM)?

CRM is a set of training procedures designed to optimize the human/machine interface and interpersonal activities to minimize human error in aviation.

What was the role of the pilot in command (PIC) during the incident?

The PIC directed the first officer to make necessary adjustments and ultimately jettisoned the load of fire retardant to facilitate a safe landing.

What will be covered in the next Lessons Learned document?

The next document will address the circumstances surrounding the missing bolt that contributed to the aircraft's control issues.

Document

OAS 35A - (12/12)

I nteragency Aviation

Lessons Learned

No. IA LL 18 - 0 1 November 29 , 201 7 Page 1 of 2 Subje ct: Ai rcraft Accident Success Story Area of Focus : Crew Resource Management Distribution : All Aviation Operations Discussion: On August 5, 2017 , a P2V - 5F aircraft sustained substantial damage shortly after takeoff. The event was classified an accident by the NTSB . The events surrounding the aircrew ’ s successful return to the airfield is a Crew Resource Management (CRM) success story.

How could an accident be a success story you ask? The crew were able to land the aircraft safely without any injur ies or further damage to the aircraft despite the od ds against them . Here’s the rest of the story: T he flight departed on its third mission to disperse fire retardant over a nearby wildfire. During the climb, the P ilot - I n - C ommand (PIC) observed an uncommanded aft movement of the control yoke with a simu ltaneous increase in the airplane's pitch attitude. He instructed the F irst O fficer (FO) to retract the flaps while he re - trimmed the elevator, but was n ot able to regain pitch control . The FO attempted to adjust his trim wheel and then re - trim the airplan e using the emergency varicam, but the airplane continued to maintain a pitch up at titude. The PIC directed the FO to lower the flaps five degrees , which reduced the elevator backpressure.

The PIC subsequently jettisoned the load of fire retardant over vac ant farmland while the FO declare d an emergency with the tower . The PIC made a shallow turn to enter a left downwind for Runway 21 while maintaining a wide traffic pattern that allowed him to make adjustments due to the lack of pitch control .

During the f inal approach, the crew used a combination of wing flaps and engine power for pitch up adjustments, crew coordinated application of elevator for trimmed pitch, and turns to make pitch down adjustments. When the aircraft was approximately 500 feet above gro u nd level, the FO lower ed the remaining five degrees of flaps to increase the p itch attitude. With both pilots pulling back on the yoke to keep the nose up, the FO reduced power and the aircraft landed safely on the runway.

No. IA LL 18 - 01 November 29 , 2017 Page 2 of 2 The P2 V is equipped with a variable camber (varicam) horizontal stabilizer in place of an elevator trim tab.

When an adjustment is made in the cockpit, the varicam drive shaft rotates to move the varicam actuators and the secondary control surfaces down or up def lection. The varicam actuators are secured to the drive shaft through universal joints located at the outboard ends, comprised of two bolts that are threaded and safety wired to the drive stop and two bolts with castellated nuts and cotter pins to secure t he yoke to the drive coupling .

A post - acciden t examination of the varicam’s left h and outboard drive stop and yoke showed that one bolt had been secured to the drive coupli ng but not safety wired. A bolt hole was found on the opposing side of the drive coupling, but the bolt was missing . T he missing drive coupling bolt was found inside the varicam without any safety wire in t he bolt head . The remaining bolt and the bolt that came out should have been safety wi red to each other.

The absence of the drive coupling bolt hinders the torque capabilities of the drive shaft; thereby allowing one side of the varicam to move and the other side to remain stationary or turn incrementally.

Since the varicam is a secondary control surface that directly connects to the elevators and provides a primary structural load path for all elevator loads, the NTSB classified the damage as substantial (accident) .

Crew resource management or CRM optimizes the human/machine interface and accompanying interperso nal activities that include information transfer, problem solving, decision making, maintaining situation awareness, and dealing with automated systems. (CRM) is a set of training procedures for use in environments where human error can have devastating effects.

The PIC had previously demonstrated to the FO approaches to land without making any adjustments to power or pitch to simulate a varicam failure, so they were prepared for an approach without trim or elevator control.

As it turns out, both aircrew had recently completed a CRM refresher course prior to the beginning of the fire season. They were prepared . A re you?

So, what happened to the bolt ? Go od question. That will be the subject of another Lessons Learned in the near future . A s Paul Harvey would say: “ Stay tuned for the rest of the story . ” /s/ Keith C. Raley /s/ Kent Hamilton John Kent Hamilton Keith C. Raley Branch Chief, Aviation Safety Chief, Aviation Safety, Training , Program Evaluation, and Quality Management Management Systems DOI, Office of Aviation Services USDA , Forest Service

Source & rights

Source: doi.gov. Public-domain U.S. Government work (17 USC §105) — freely reproducible.

Permanent URL — we don’t break links.

Report a problem or request removal

Document details

Doc number
Publisher
DOI Office of Aviation Services
Pages
2
File size
452 KB