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Recorder reports

21
DCA12CA0622012-04-15 · AIRBUS INDUSTRIE A319-132fdr
Flight 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
DCA23LA0962022-12-18 · AIRBUS A330-243cvr
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
DCA19LA1342019-04-11 · Airbus A321cvr
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
DCA09FA0472009-05-04 · AIRBUS A320cvr
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
DCA00MA0522000-05-21 · British Aerospace J-3101report
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
DCA05MA0312005-02-02 · Bombardier CL-600-1A11report
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
NYC05MA0832005-05-13 · BOEING 717-200performance
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
DCA08MA0982008-09-20 · Learjet LR60report
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
DCA05MA0372005-02-16 · Cessna 560report
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
DCA04MA0302004-03-23 · Sikorsky S76A++report
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
DCA11MA0762011-04-02 · GULFSTREAM GVIperformance
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
CEN17MA1832017-05-15 · LEARJET 35Areport
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
DCA09MA0262009-01-15 · AIRBUS A320performance
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
DCA01MA0172001-01-27 · Beech 200report
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
DCA00MA0232000-02-01 · Douglas MD-83report
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
CEN19FA0722019-01-29 · Bell 407report
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
DCA00MA0262000-02-17 · Douglas DC-8-71Freport
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
DCA19MA0862019-02-23 · Boeing 767cvr
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
ENG20LA0162020-02-15 · Airbus A319cvr
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
DCA13MA1202013-07-06 · BOEING 777-200ERperformance
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
DCA19IA0362018-12-06 · Boeing 737performance
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

2
DCA19LA1342019-04-11 · 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

1
DCA21FA1742021-07-02 · BOEING 737-275C · RHOADES AVIATION INC
The flight crewmembers’ misidentification of the damaged engine (after leveling off the