| Back to logs list
333926 2008 年 03 月 08 日 13:33 Reading (loading. ..) Comments (0) Category: Miscellaneous world Kan
China Southern Airlines plane crash black box recording
11 years after the return, over the last 12 minutes of recording audio content.
[00:00.00] China Southern Airlines, Shenzhen air crash black box the final 12 minutes of 5.8 audio: May 8, 1997,
[00:04.96] a company in Shenzhen China Southern Airlines CZ3456 (Chongqing to Shenzhen) Flight
[00:07.96] The Boeing 737 landed at the airport in Shenzhen Huangtian disintegration. The first aircraft grounded
[00:11.96] heard the captain shouted: ,],[
[00:16.96] aircraft circling in the air after landing the second time only to hear the co-pilot back shouted:
[00:18.46] ! down to 1500
[00:24.64] First Officer: I have reduced 1500
[00:30.88] nearly into the station: in front of a plane closer
[ ,],[
[00:42.26] First Officer: Yeah
[00:48.89] to lift the autopilot alarm
[00:53.94] First Officer: 308
[01:02.76] to contact Guangzhou 160.35
[01:08.29] First Officer: I ask the reduced height
[01:18.45] First Officer: It is now heading 135
[01:24.29] First Officer: I see on the runway in front of bad weather
[01:29.20] nearly into the station: you are immediately reduced to 900
[01:31.48] machine Length: 3456 to establish ILS
[01:33.97] co-pilot: 3456 Contact Tower, 6855 Goodbye
[01:36.71] Captain: Note height
[01 : 41.00] Captain: Note the rain large
[01:45.97] Tower: CZ3456
[01:49.30] Captain: Echo ~ ~ now established blind drop the
[01:54.59] First Officer: 330 degrees
[02:03.12] co-pilot: 3456 is now 6,000 feet altitude
[02:11.92] co-pilot: see the airport lights
[02:16.08] Captain: Wait a minute later put ah ~
[02:18.16] Length: throttle pre-bit
[02:25.55] machine Length: Note yaw
[02:36.50]] co-pilot: 3456 saw the introduction of light
[02:47.05] Length: decision height
[02: 49.49] the co-pilot: Note yaw ~ ~ ~ ~ good
[03:00.63] First Officer: glide path is too low
[03:04.61] engine room alarm (low glide path)
[03:06.35] First Officer: Note the speed
[03:06.75] Captain: Speed fine
[03:08.75] Length: bigger nothing
[03:12.54] First Officer: left point
[03:18.02] Length: with live points (stick )~~~~~ with live (the accelerator)
[03:20.97] The first touchdown
[03:22.28] engine room alarm (more than overload)
[03:23.62] First Officer: throttle! fuel door!
[03:25.26] The second touchdown
[03:27.90] First Officer: fuel door missed! fuel door missed!
[03:28.28 ] The third touchdown
[03:31.08] First Officer: fuel door missed! fuel door missed!
[03:33.25] cabin alarm (main warning - can no longer normal aircraft Flight - configuration destruction)
[03:40.69] Captain: Rod loss of weight of the
[03:45.84] Length: fuel door!
[03: 52.64] Captain: Check, right?
[04:34.68] Captain: Re perimeter
[04:49.34] engine room alarm (hydraulic system)
[04:56.08] Captain: Do not take too big!
[05:03.83] co-pilot: 3456 missed Rights
[05:05.96] Tower: see
[05:07.30] co-pilot: You sound great point
[05:14.78] You tell me course, I do not see you
[05:18.34] Captain: Now to die, too much rain
[05:21.03] Length: up 1200
[05:26.90] co-pilot: You look at my position, 3456
[05:45.05] co-pilot: the right, turn to your right
[05:49.02] Length: left the weather is not good
[05:57.74] First Officer: I now After a rendezvous point for left
[06:02.61] Tower: Please tell me the location of
[06:06.18] First Officer: I now turn left into the triangular pull ~ ~ ~ ~
[06:32.35] Tower: you are here?
[06:36.28] co-pilot: three edge
[06:40.39] another flight Aircraft: I can not avoid you, height 6000, from 14 km
[06:49.91] First Officer: I am now an emergency!!
[06:51.91] First Officer: I have an emergency situation, you ask them to give way to me!
[07:46.72] Tower: frequency 111.3
[08:11.94] Tower: CZ3456, you ask them to give way to me! I am now Emergency!!
[08:20.15] cabin alarm (landing gear)
[08:47.28] Tower: 3456 emergency evacuation after landing
[08:49.28] First Officer: I see, I have now informed the
[08:56.73] First Officer: I now sub-round
[09:04.34] Tower: What position are you now?
[09:10.46] First Officer: I now highly 1200
[09:16.76] co-pilot: I'm north of the airport, in the left
[09:21.78] Tower: I have to give way to all aircraft you
[09:38.64] Captain: Where is the runway, I have not found
[09:45.08] Here is a broken record
[10:09.54] engine room alarm (flaps)
[10:11.94] Captain: Do not drive this, not drive it!
[10:16.05] Tower: No other aircraft, and both sides of the runway clear
[10:25.82] co-pilot: The navigation station ah
[10:29.88] Captain: I saw the runway of the
[10:59.72] Tower: CZ3456, the ground ready to fire engines, ambulances
[11:03.59] Tower: You can use the 15 runway!
[11:08.11 ] Captain: I take back land
[11:08.45] Tower: Yes! floor in front of the unit reflects the good weather north of the south side of Five rain
[11:22.20] machine Length: Not a good situation Ah!
[11:50.49] Captain: Note height A
[12:06.01] First Officer: high altitude, right?
[12:08.88] co-pilot: the runway has to head out!
[12:15.72] cabin emergency alert (sink rate)
[12:18.25] cabin emergency alarm (pull up)
[12:23.99] First Officer: drop rate is too high
[12:26.66] First Officer: high rate of pull-down !!!!!!!!!!!!! !!!!!!!!!!!!!!!
[12:27.65] rattle ~~~~~~~~~~~~~~~~~~~~ plane crash)
Shenzhen,
lebron james shoes, Chongqing, 1997 crash MP3
China Southern Airlines 97, Shenzhen 5.8 air crash black box cockpit voice recorder (with a MP3 file downloads real + shock)
1997 年 5 8, a China Southern Airlines Shenzhen CZ3456 (Chongqing to Shenzhen) Boeing 737 flights in Shenzhen Huangtian airport landing disintegration. Grounded aircraft for the first time heard the captain shouted: Fuel door, go around! ......After the aircraft circled in the air, landing back the second time only to hear the co-pilot shouted:
hear the last words of the co-pilot ...
chilling ...
flight simulation, but I also frequently Hold Up ...
normal drop should be 400. . . 300. . . 200. . . 100. . . 50. . . 40,30,20,
nba basketball shoes,10. .
1.
the day after the situation, Unit 2925 19:45 from Chongqing Jiangbei Airport, is expected to arrive in Shenzhen Huangtian Airport at 21:30, 21:07 and Shenzhen Airport Approach Control to establish contacts the normal procedure to Runway 33 approach. 21:17 to establish contact with the control tower. Tower told the crew 21:18:07 Unit report Taiwan plane too close near the control tower saw the aircraft landing lights, but light rain is not clear, the ground radar display, aircraft flight path, down a high degree of normal. 21:19:33 southern end of the runway the aircraft for the first time grounding the aircraft after the jump triple jump, and then go around. Go around and turn left up to 1,200 meters, the tower opened to remind the crew answering machine, but has not been shown on the secondary radar. 21:23:57, the unit reported in the triangular position, requiring avoidance of other aircraft, 21:23:40, avoid other aircraft crew asked again, and reports on Tower has been told to avoid other aircraft. 21:24:58 requirements fall to the ground crew with the fire engines, ambulances, the tower told the crew have been prepared. Then they turn the plane around and landed south of the report prepared, agreed that the south tower floor, and told of Unit 2925, 21:28:30 landing, after landing the aircraft disintegrated on fire.
2. on-site inspection situation
(1) for the first time from south to north landing. Into the runway, the southern tip of 388.5 meters from the runway and found the first small piece of tire debris. 502 meters from the tip of the runway and found the first piece of metal debris. 561 meters from the tip of the runway, the runway centerline 25 meters left and found a 54 cm long, 28 cm wide, was torn like tire pieces. 570 meters from the tip of the runway centerline 20 meters left, that piece before the landing gear wheel revolvers, long 46 cm, width 21 cm. 580.5 m from the tip of the runway, near the center line, it was discovered the main round of the anti-magnetic hysteresis brake valve. The southern end of 801 meters from the runway centerline near the nose landing gear found in the inner left wheel hub (irregular broken edges). The above description, the plane landed front wheel first ground, the left front wheel burst, debris scattered on the runway.
from the tip of the runway from the 388-801 m range,
lebron james vii, road surface have more rivets (mostly cut marks), and a small amount of metal, hose, clips and other fallout. Above that, the first landing,
cheap lebron shoes, the aircraft was damaged.
(2) aircraft to go after the second landing from north to south. Into the runway, the runway from the north end of 427.2 meters, 4.5 meters at the center line on the right, there are clear signs of grazing the lower fuselage. This marks the right front, right side from the centerline of the fuselage scratches have the right engine at 4.8 m grazing traces. Traces in the body to the lower left front rub, scratch from the fuselage center line of 4.9 meters at the left side of the engine grazing have left traces. 441 meters from the runway at the northern end, near the center line pavement three distinct grooves rub, rub the deepest trough 2 cm and a maximum width of 12 cm. The investigation has revealed that three slots are rubbing the left landing gear wheel (left), towing lug and wheel steering actuator touchdown to draw the grooves.
wipe the aircraft, the drag of about 600 meters after sliding disintegration. Central and right-wing aircraft after severely damaged edge, where the northern end of the runway from 1,200 meters, or side of the runway centerline near 105.7 m before the landing gear, flaps film, slats debris, luggage rack, passenger seat, etc. fallout; body length of 12 meters in front,
nba shoes, local damage, but no burn marks are rolling, head north, local deformation of the cockpit, instrument panel and central console has a lot of mud, landing gear lever in neutral position, the nose lower depression, lower back bending weather radar antenna. The northern end of the runway from 1370 meters, 79.4 meters at the right side of the runway centerline, with a more complete aft fuselage. The left main landing gear and right engine left scattered on the runway, the left engine at the bottom of serious wear, the fan blade is broken off, part of the bend. Right main landing gear scattered on the runway on the right. Inside the right main landing gear tire burst, severe wear and tear the bottom of the right engine. At about 1230 m × 250 m within the wreckage and scattered material distribution center circle to the north of the runway pavement, and both sides of the grass.
3. the flight crew technical and physical condition
(1) technical conditions
Captain: Lin Yougui (left seat), male, born in July 1960, the weather criteria: 1 / 2. 12738:08 hours total flight time, including time of 9084:51 hours of radio operator, driver time to 3654:12 hours.
the fly model: TB-20 (120 小时), Y-7 (52:14 hours)
is Aircraft Type: Boeing 737-300 flight 3482:04 hours (22 hours solo flight)
1996 年 12 月 29 Japanese technical inspection and approval.
co-pilot: Comte new (right seat), male, born in April 1952, the weather criteria: 1 / 2. 15537:01 hours total flight time, including mechanics time 11203:25 hours, the driver time to 4334:36 hours.
the fly model: TB-20 (130 hours), Cheyenne (36 hours)
is Aircraft Type: Boeing 737-300 flight 4158:36 hours (88 hours solo flight)
1996 on December 25 qualifying technical inspection.
Observer: XIAO Rong, male, born in July 1948, the total flight time: 5179:53 hours, the Boeing 737-300 was 123:43 hours only on the simulator training. The last technical inspection time: April 18, 1997.
(2) permit conditions
Lin Yougui, driver's license is valid until November 1997, medical certificate valid until October 1997;
Comte new driver's license is valid until July 1997, physical examination certificate is valid until October 1997;
XIAO Rong, driver's license is valid until April 1998, medical certificate valid until September 1997;
(3) physical health of the crew
1997 Conclusions are flying pass annual physical examination. The pre-flight crew members according to the provisions of the attendance before the examination, 8 hours before the flight crew was not found drinking alcoholic beverages and medications. Cockpit Voice recording through the analysis and understanding of the crew with the crew, flight crew members in the body without exception, excluded unit air disability.
4. weather and communications, navigation equipment security situation
Shenzhen terminal weather forecast: at 17:00 on May 8 ~ 9 May 02:00,170 degree wind 7 m / s, visibility 6,000 meters, weak shower, the sky clouds 1,500 meters, sometimes 15 m / s wind, the wind variable, sometimes 1,500 meters visibility, strong thunderstorms, the cloud amount of 5 to 7 300 m, the amount of 3 to 4 cumulonimbus 900 meters, 1,200 meters cloud sky.
16:40 Dangerous weather thunderstorms occur, please note that the units. issued a revised forecast
16:50:
170 degree wind 7 m / s, gusts 15 m / sec, variable wind direction, visibility 1500 meters, has a strong thunderstorm, cloud amount of 1 240 m 2, 5 ~ 7 the amount of cloud 300 meters, 3 to 4 900 meters the amount of cumulonimbus, the sky clouds 1,200 meters.
18:00 Dangerous weather unit.
21:00 Weather Fact:
290 degree wind 7 m / sec, visibility 1,500 m, the direction of runway 33 runway visual range 1400 m, in the shower, the amount of 1 to 2 cumulonimbus 1,200 meters, 5 7 amount of cloud 1,200 m, temperature 23 ℃, dew point 23 ℃, market pressure 1010HPA. Selected
21:33 Weather:
240 degree wind 7 m / s, visibility 2000 m, in rain, low cloud amount of 1 to 2 210 meters, the amount of 3 to 4 cumulonimbus 1,200 meters, cloud amount of 5 to 7 1200 meters, temperature 22 ℃, dew point 22 ℃, market pressure 1010HPA.
call recording by listening to ground and air, watching the radar video, access to such information, confirmed at the time communications, navigation, radar and other security equipment work properly; weather, airport open standards compliance.
5. aircraft and engine condition
(1) Aircraft
Model: B737-300B
Manufacturer: Boeing
registration number: B-2925
factory number: 27288
Release Date: February 24, 1994, February 28, 1994 in Shenzhen, to May 7, 1997 flight 8457:53 hours.
Airworthiness 证号: AC0783
Nationality Registration No: NR0940
station license number: 95? 477
(2) Engine
Model: CFM-56-3CI
factory : CFMI company
number: 857794
from right to left 857 792 7 May 1997, left hair flying 8457:53 hours, the right hair flying 8457:53 hours.
3) documents,
zoom kobe v, data checking
AD: As of May 7, 1997 only, the completion of all airworthiness directives.
-time control control: all are in the period when the use of control
period, no super-life use cases.
keep the project: to May 8, 1997 plane crash before the project and to retain an unqualified failure.
Aircraft Maintenance Inspection in: from July 8, 1996 to April 29, 1997, has completed the review 2C 1, 1A-12A review of the 1, no major faults and major repairs.
(4) checks the wreckage of the fuselage
: In addition to the rear fuselage relatively intact (bottom friction marks), the other all the damage.
wings: the left wing tip was no serious damage than, the rest have all been burned, the right wing tip defect, before and after the edge are burned out.
Engines: Left Engine oil filter, oil filter clean and normal, most of the fan blades broken or bent. Loss of right engine fuel filters, oil filters clean and normal, most of the curved blade. Two engines scrapped.
landing: left landing gear: two main wheels in place, the wheel broken, the outer well.
the right landing gear: two main wheels in good condition, pillars of the outer cylinder compression damping in the end, and struck roots within the cylinder, there are traces of collision.
nose gear: retractable actuator rod off, wheel steering actuator rod broken, revolvers off, the right tire burst.
decoding by checking and flight data analysis, before the accident, aircraft, engines and systems in a state of airworthiness. Fuel, lubricating oil passing the tests.
6.
aircraft loading and center of gravity of this situation are set out the maximum amount of flights available to 14,248 kg. A total of 65 passengers (including 64 adults, baby 1), weight 4616 kg; loaded 58 bags, weighing 750 kg; loading cargo 29, weight 554 kg; loading message 13, 12 kg. Total load 5932 kg or more. Compared with the maximum available payload, load 8316 kg.
aircraft loaded in accordance with no oil center of gravity should be at 8.5%? 28%, the actual was 17%. Takeoff weight of 7.5% should be the focus? 28%, actual 17.2%, the center of gravity are in the best position to meet the requirements.
thus proved that there is no business of overloading the machine and load balance.
7. unlawful interference
(1) according to the scene, interviewed witnesses and found, before landing the aircraft found no fire or fire, you can rule out the possibility of fire after the landing.
(2) the flight of all passengers, baggage and cargo are required for a security check and found no prohibited items, exclude the possibility of inflammable and explosive dangerous goods installed.
(3) by extracting samples for testing and found no explosives on the wreckage residues, but also did not find traces of an explosive formed.
(4) by visiting some of the survivors of the crew members and passengers, to exclude acts of unlawful interference with aircraft flying there.
8. witnesses to reflect the situation
(1) At that time the aircraft on the tarmac crew then reflected, aircraft landing from south to north the rain very, very close. When the aircraft to go after landing from north to south, heavy rain, it was dark and visibility is poor, high altitude aircraft, speed, big, sinking fast.
(2) According to 3 minutes before the plane landed in Shenzhen Airlines Flight 822 captain reflected: Shilong radar point of view there is a flat state to the
According to the machine 5 minutes after the first ground floor of the Air 1305 flight crew reflected in terms of the airport from the south end of the radar thunderstorms, heavy rain cut into the encounter after the blind down, saw the runway 800 feet out of the cloud, rain is relatively large, As water on the runway, landing lighting is not good, can not see the ground, only to see the runway lights * close rate to control aircraft.
(3) 2925 crewman reflect: the first ground, sitting on the door of the three flight attendants after the seat was broken and the aircraft frame the central 17,18 ranked Lee raised arched, raised floor of the plane split, window deformation, part of the roof off, the cabin burning smell, instant power, cabin luggage rack some of the items after the drop.
Analysis
(1) 2925 Unit five-sided approach in the process, before the decision height, aircraft attitude, flight path, glide path to maintain all normal, but the speed is too large (142.5 nautical miles / when normal speed of 136 nautical miles / hours). Unit introduced the report to see light, then they reported seeing the runway. Decision height, because the aircraft was flying in heavy rain, the unit decided to
the night flying experience heavy rain, poor visibility, runway, water, lighting is not good, to see the ground is not clear. In this case, the unit did not go around to take decisive measures to break the rules, continue to approach descent, lost the initiative, delaying the timing, which is the main reason causing the abnormal landing, and the ultimate cause of the accident's cause.
(2) when the aircraft is too close to the station after the height of 170 feet, the cockpit of a that
height of 50 feet into the runway, due to Ground (stop Boeing 737 degree angle of -0.79 to -1, according to data record decoding data, grounded in the attitude of the aircraft between -1.4 to ten 1.7). 4 seconds before the aircraft ground decreased rate of 9? 3 feet / second, grounded vertical overload of 2.49G, and produce the first jump, the aircraft damaged.
aircraft grounded the first 2 to 3 seconds, cockpit voice recording has been called Too late to see the pavement, there is no ground to maintain the correct posture is a hard landing caused the aircraft the direct cause of jumping.
(3) aircraft, the first jump, the height of 5 feet, grounding vertical overload 1.9G, not determined to close the throttle unit. N1 RPM increases and decreases irregularly, the same time, putting action. The disposal of the error, resulting in continuous production of the aircraft and two jumps. The second jump 7 feet, grounding vertical overload 2.54G, the third jump 13 feet. Containing three successive jumps and more than cause serious damage to the aircraft structure.
(4) plane after the third jump as high altitude, coupled with the night rain, the unit has not identified the aircraft in case of damage to the program around.
the damage control system, complex flight, the aircraft to 183 sea miles / h speed, the small elevation of 2 degrees off the ground (the aircraft off the ground, the crew felt the stick is . Serious damage to the aircraft after the crew go around and give a second landing potential problems.
(5) missed, the cockpit a Aircraft damaged after two laps in the sky, the unit decided to close the reverse landing north to south. Due to heavy rain has not stopped, the aircraft control system failure (the change in the steering column and the elevator deflection angle obviously does not match the large bar, a small elevator in the yaw angle), although the crew pull the stick before landing in the end, but did not change the aircraft large angle is bent posture, the last aircraft is still under the 7.56 degree angle of depression, 227.5 sea miles / h speed, the decrease rate of 41 feet per second, with 3.2 degrees hit the ground after the disintegration of the left slope, fire.
accident concluded in the final approach the aircraft
encountered heavy rain, the unit not see the pavement in case of violation of the provisions of the blind down; the judge allowed a high degree, resulting in the ground plane did not maintain the correct posture, causing heavy landing jumps, combined with the captain disposal error is caused by the direct cause of major accidents. Missed, due to the aircraft has been seriously damaged, part of the control system failure, the unit can not control the landing attitude, so that the second aircraft landed, taken off the depression of the touch the ground at high speed, causing the disintegration of the aircraft crashed. This is a man-made causes of major accidents.
cursor pointer;
Hybrid Mode
