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Recorder reports
21Flight Data Recorder 10 - Specialist's Factual Report
about a half second later by right stick lateral and longitudinal
inputs. The dual stick inputs continued for about 8 seconds. During this time
COCKPIT VOICE RECORDER - SPECIALISTA��S FACTUAL REPORT
rattling were noted, while
the crew reacted verbally. The cavalry charge, dual input, and several
EICAS chimes were noted. The crew confirmed who had control ... entering into unusual
attitudes, and noted that the pilots “ended up dual inputting,” clarifying
that it was “instinct.”
1103:50.0
The recording ended.
Submitted
COCKPIT VOICE RECORDER
dual input [automated voice].
CAM
20:40:34.3 whoop.
HOT-?
20:40:35.7 [sound of noise].
CAM
DCA19LA134
Cockpit Voice Recorder Factual Report
Page ... took the, I tried and that's
when you heard the dual input-
20:43:10.2 naw I * thought
Cockpit Voice Recorder 12 - Specialist's Factual Report
touchdown
12:18:25 Sound of bang
12:18:29 Automated “dual input caution” callout
12:18:31 Sound of touchdown
12:24:02 Crew
NTSB Aircraft Accident Brief AAB-02/05 (final report, ntsb.gov)
engines. This model engine is a single-spool design consisting
of a dual centrifugal compressor, reverse-flow annular combustor, and a 3-stage axial flow ... dual engine failure was induced. However,
pilot workload increased considerably (the airplane was difficult to control and required constant
flight control and trim inputs) when
NTSB Aircraft Accident Report AAR-06/04 (final report, ntsb.gov)
system on the morning of the accident. The keystroke log reflected inputs for number of
passengers (eight), 300 pounds of cargo, and 14,600 pounds ... preference.
1.6.3 Longitudinal Flight Control System
The CL-600 is equipped with dual flight controls, such that the control wheels,
control columns, and rudder pedals
Aircraft Performance 13 - Study Addendum 1
both nonzero at a given time, both pilots are making control wheel inputs.
1 Report MDC 06K9011 defines Appendix A of report MDC 08K9005, “Boeing ... around modes, the 717 autopilot drives the rudder through the dual rudder servo. The
dual rudder servo is in parallel with the rudder pedals
NTSB Aircraft Accident Report AAR-10/02 (final report, ntsb.gov)
Main Landing Gear Tires
The airplane was equipped with dual wheel and tire assemblies at each MLG position.
Each MLG tire was a Goodyear Flight ... thrust levers, a mechanical linkage on each thrust lever rotates the input
shaft on a rotary variable differential transformer (RVDT) in the cockpit pedestal
NTSB Aircraft Accident Report AAR-07/02 (final report, ntsb.gov)
relative
airflow and transmits the sensed angle to the AOA system. Inputs from the AOA system
are transmitted to the stickshaker, which has an electric ... Citation V Operating Manual, the airplane
was equipped with an upgraded, dual-mode AOA computer, which incorporated normal
and ice modes. The ice mode
NTSB Aircraft Accident Report AAR-06/02 (final report, ntsb.gov)
pitch and roll
command cues in either a dual- or a single-cue format. With the dual-cue format, pitch
attitude is represented ... dual-cue format. With the SPZ-7000, both command cues appear simultaneously when
only one axis is engaged. However, with the SPZ-7600 dual
Aircraft Performance 13 - Group Chairman's Aircraft Performance Study
routed to the Heim Flight Recorder (FR). The Heim FR can
accept inputs from the TIS, multiple CDAU’s and individual ARINC 429 data sources ... that “the production ADS [Air Data System] will use two
Goodrich Aerospace dual-sensor Total Air Temperature (TAT) probes mounted below the cockpit
NTSB Aircraft Accident Report AAR-19/02 (final report, ntsb.gov)
flight management system, is an onboard computer system that integrates inputs from various
subsystems to aid the pilot in controlling the airplane’s lateral ... flight control inputs that could have eliminated the 9-kt margin. For
example, the left-wing-down aileron input required to make the turn
Aircraft Performance 13 - Factual Report of Group Chairman
airplane’s nose-up pitch response to progressively larger aft side
stick inputs made below 100 ft radio altitude.
The airplane touched down ... Airways Quick Reference Handbook (QRH) and the Airbus QRH ENG DUAL FAILURE procedures
both provided guidance that indicated flaps 3 (conf3) was to be used
NTSB Aircraft Accident Report AAR-03/01 (final report, ntsb.gov)
emergency.
The bus system includes four sub-buses that are dual-fed (that is, they receive
power from either generator’s main bus). All electrical ... four copilot-side instruments
would function because they would receive inputs from the pitot static or vacuum systems.
The airplane’s electrical system also includes
NTSB Aircraft Accident Report AAR-02/01 (final report, ntsb.gov)
trailing-edge-up direction from -0.4° to -7.0°,123 consistent with control inputs
being made to bring the nose up.
•
By 1609:42, the airplane ... These calculations provided an estimate of
control inputs for use in simulations when control inputs recorded on the FDR did not
produce the same response
NTSB Aircraft Accident Report AAR-20/01 (final report, ntsb.gov)
Avionics installed on the helicopter included a radio altimeter and a dual Garmin GTN 650
system.24 The Garmin GTN 650 system provided GPS navigational capabilities ... exhibited signatures consistent
with overload. Manual rotation of the main rotor transmission input flange resulted in a
corresponding rotation of the main rotor shaft
NTSB Aircraft Accident Report AAR-03/02 (final report, ntsb.gov)
pushrod attachment bolt from its crank fitting. With no
additional manual input, the right elevator control tab moved to a 29º TED deflection,
where ... further forward because of cable stretch; however, no
additional nose-down elevator input would result.
Figure 12 shows the control column position required
CVR SOUND SPECTRUM STUDY
audio
change. Channel 2 (red signal) was defined as an input of the 17 seconds post the audio
change. The level between the two signals ... exemplar GA
button activation (elevated sound energy at 5000 Hz). The dual clicking nature of the
exemplar recording was not detected in this region
COCKPIT VOICE RECORDER - SPECIALISTA��S FACTUAL REPORT
that records at minimum two hours
of digital audio from four input channels – one channel for each crew member (captain, first
officer, and observer ... flight. Further, it was determined that
the aircraft had a similar inflight dual generator failure the previous day, which was two flight
legs prior
AIRCRAFT PERFORMANCE 13-EXHIBIT 13A CRASH SITE FACTUAL REPORT AND ATTACHMENTS 1-10
FMGS) Set
a. For descent (approach), input data into FMS (FMGS) using Route
Guide and chart.
b. Input the alternate airport data in case ... Page
Input the route from the destination airport to the alternate airport.
When the active runway at the alternate airport is known, input
appropriate approach
AIRCRAFT PERFORMANCE STUDY
actual) landing distance required computed by the
PWB using the inputs provided by the flight crew prior to landing (131 kt. approach speed ... XMTR DUAL LOC-RE -6809/ -1.121 LCW-TAIL NRE-LON W118-20-59.86
ANT LON W118-22-20.91 EQUIP-TYPE MK20A
Cockpit voice
2DCA19LA1342019-04-11 · Airbus A321
19:40:08.6RDO-2left at kilo echo. 20:40:04.5 flex. CAM-1 20:40:05.0 flex set. CAM-2 20:40:13.4 eighty. HOT-2 20:40:14.8 check. HOT-1 20:40:29.7 V-1. HOT-2 20:40:31.4 rotate. HOT-2 20:40:32.2 @. HOT-1 20:40:33.6 w-. HOT-? 20:40:34.1 dual input [automated voice]. CAM 20:40:34.3 whoop. HOT-? 20:40:35.7 [sound of noise]. CAM DCA19LA134 Time and Intra-Aircraft Communication Time and Over-the-Air Communication Source Source 20:40:36.7 your airplane, your airplane, your airplane. HOT-2 20:40:39.2 I don't know what's goin' on. HOT-2 20:40:42.9 * *? HOT-2 20:40:44.7 what the # (happened) *? HOT-1 20:40:45.2 I don't know. ah the engines all go, good. HOT-2 20:40:50.7 positive rate, gear up. HOT-1 20:40:51.4 American three hundred Ranger transition and contact New
DCA19LA1342019-04-11 · Airbus A321
20:41:48.3HOT-2I looked and, that's when I took the, I tried and that's when you heard the dual input- 20:43:10.2 naw I * thought- HOT-1 20:43:11.5 you know I mean. HOT-2 20:43:13.6 It was, it was takin' a lot of left rudder. and then, you
Findings
1DCA21FA1742021-07-02 · BOEING 737-275C · RHOADES AVIATION INC
The flight crewmembers’ misidentification of the damaged engine (after leveling off the