Accident | |
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Date | August 12, 1985 |
Summary | Crashed following in-flight structural failure |
Site | Mount Takamagahara, Ueno, Gunma Prefecture, Japan 36°0′5″N 138°41′38″E / 36.00139°N 138.69389°E / 36.00139; 138.69389 |
Aircraft | |
Aircraft type | Boeing 747SR-46 |
Operator | Japan Air Lines |
IATA flight No. | JL123 |
ICAO flight No. | JAL123 |
Call sign | JAPAN AIR 123 |
Registration | JA8119 |
Flight origin | Haneda Airport, Tokyo, Japan |
Destination | Itami Airport, Osaka, Japan |
Occupants | 524 |
Passengers | 509 |
Crew | 15 |
Fatalities | 520 |
Injuries | 4 |
Survivors | 4 |
Japan Air Lines Flight 123 (Japanese: 日航ジャンボ機墜落事故[1]) was a scheduled domestic passenger flight from Tokyo to Osaka, Japan. On August 12, 1985, the Boeing 747 operating the service suffered a severe structural failure and decompression 12 minutes into the flight. After flying under minimal control for a further 32 minutes, the 747 crashed in the area of Mount Takamagahara, 100 kilometres (62 mi; 54 nmi) from Tokyo.
The aircraft, featuring a high-density seating configuration, was carrying 524 people. All 15 crew members and 505 of the 509 passengers died in the accident. Some of the fatalities survived the initial impact but died of their injuries hours later while awaiting rescue. All four survivors were seriously injured. The crash of Flight 123 is the deadliest single-aircraft accident in aviation history.[2]
Japan's Aircraft Accident Investigation Commission (AAIC),[3]: 129 assisted by the U.S. National Transportation Safety Board,[4] concluded that the structural failure was caused by a faulty repair by Boeing technicians following a tailstrike incident seven years earlier. When the faulty repair eventually failed, it resulted in a rapid decompression that ripped off a large portion of the tail and caused the loss of all on-board hydraulic systems, disabling the aircraft's flight controls.
The accident aircraft, a Boeing 747SR-46, registration JA8119 (serial number 20783, line number 230), was built and delivered to Japan Air Lines in 1974. It had accumulated slightly more than 25,000 flight hours and 18,800 cycles at the time of the accident (one cycle consisting of takeoff, cabin pressurization, depressurization, and landing).[2]
On June 2, 1978, while operating Japan Air Lines Flight 115 along the same route, JA8119 bounced heavily on landing while carrying out an instrument approach to runway 32L at Itami Airport. The pilot then excessively flared the aircraft, causing a severe tail strike on the second touchdown. No fatalities occurred among the 394 people on board, but 25 people were injured, 23 minor and 2 serious. The tailstrike cracked open the aft pressure bulkhead. The damage was repaired by Boeing technicians, and the aircraft was returned to service.[5][3][6] The aircraft had flown for 8,830 hours at the time of the tailstrike incident.[5]: 4
At the time of the accident, the aircraft was on the fifth of its six planned flights of the day.[3] The flight had 15 crew members, including 3 cockpit crew and 12 cabin crew.
The cockpit crew consisted of:
The flight was around the Obon holiday period in Japan when many Japanese people make yearly trips to their hometowns or resorts.[10] Twenty-two non-Japanese were on board the flight.[11] By August 13, 1985, a spokesman for Japan Airlines stated that the list included four residents of Hong Kong, two each from Italy and the United States, and one each from West Germany and the United Kingdom.[12] Some foreigners had dual nationalities, and some of them were residents of Japan.[10]
The four survivors, all women, were seated on the left side and toward the middle of seat rows 54–60, in the rear of the aircraft.[3]: 22
Kyu Sakamoto, who was famous for singing "Ue o Muite Arukō", known in Anglophone countries under the title "Sukiyaki", was among those who perished in the crash.[13]
As the flight connected two of the largest cities of Japan, a number of other celebrities also initially booked this flight, but ultimately avoided the tragedy by either switching to another flight or opting to use the Tokaido Shinkansen instead. These include Sanma Akashiya, Masataka Itsumi and his family, Johnny Kitagawa, and the cast of Shōten at the time.[14][15][16] Members of the Shonentai were also scheduled to travel with Kitagawa, but ultimately stayed behind in Tokyo.[16]
Flight 123 audio transcript | |
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Flight 123 CVR and ATC transcript in English with map of flight on YouTube |
The aircraft landed at Haneda from Chitose Airport at 4:50 p.m. as JL514. After more than an hour on the ground, Flight 123 pushed back from gate 18 at 6:04 p.m.[3] and took off from Runway 15L[3] at Haneda Airport in Ōta, Tokyo, Japan, at 6:12 p.m., 12 minutes behind schedule.[17] At about 6:24 p.m. (or 12 minutes after takeoff), at near cruising altitude over Sagami Bay 3.5 miles (3.0 nmi; 5.6 km) east of Higashiizu, Shizuoka, the aircraft underwent rapid decompression,[3]: 83 bringing down the ceiling around the rear lavatories, damaging the unpressurised fuselage aft of the plane, unseating more than 60% of the vertical stabilizer, and severing all four hydraulic lines. A photograph taken from the ground confirmed that the vertical stabilizer was missing.[18]
The pilots set their transponder to broadcast a distress signal. Afterward, Captain Takahama contacted Tokyo Area Control Center to declare an emergency, and to request to return to Haneda Airport, descending and following emergency landing vectors to Oshima. Tokyo Control approved a right-hand turn to a heading of 090° east back towards Oshima, and the aircraft entered an initial right-hand bank of 40°, several degrees greater than observed previously. Captain Takahama ordered First Officer Sasaki to reduce the bank angle,[3]: 296 but when the aircraft did not respond to the control wheel being turned left, he expressed confusion. After this, the flight engineer reported that the hydraulic pressure was dropping. The captain repeated the order to reduce the bank angle, as the autopilot had disengaged. He then ordered the first officer to bank it back, then ordered him to pull up. All of these maneuvers produced no response. At this point, the pilots realised that the aircraft had become virtually uncontrollable, and Captain Takahama ordered the copilot to descend.[3]: 297
Heading over the Izu Peninsula at 6:26 p.m., the aircraft turned away from the Pacific Ocean, and back towards the shore.[3]: 150 Due to the apparent loss of control, the aircraft did not follow Tokyo Control's directions and only turned right far enough to fly a north-westerly course. Seeing that the aircraft was still flying west away from Haneda, Tokyo Control contacted the aircraft again. After confirming that the pilots were declaring an emergency, the controller asked the nature of the emergency. At this point, hypoxia appears to have begun setting in, as the pilots did not respond. Also, the captain and co-pilot asked the flight engineer repeatedly if hydraulic pressure had been lost, seemingly unable to comprehend it.[3]: 298 Tokyo Control then contacted the aircraft again and repeated the direction to descend and turn to a 90° heading to Oshima. Only then did the captain report that the aircraft had become uncontrollable. (Tokyo: "Japan Air 124 [sic] fly heading 090 radar vector to Oshima." JAL123: "But now uncontrol." Tokyo: "Uncontrol, roger understood.")[3]: 299
After traversing Suruga Bay and passing over Yaizu, Shizuoka,[3]: 7 at 6:31:02 p.m., Tokyo Control asked the crew if they could descend, and Captain Takahama replied that they were now descending, and stated that the aircraft's altitude was 24,000 feet (7,300 m) after Tokyo Control requested their altitude. Captain Takahama also declined Tokyo Control's suggestion to divert to Nagoya Airport 72 nautical miles (83 mi; 133 km) away, instead preferring to land at Haneda,[3]: 302 which had the facilities to handle the 747. The flight data recorder shows that the flight did not descend, but was instead rising and falling uncontrollably.[3]: 1–6 Hydraulic fluid completely drained away through the rupture. With the total loss of hydraulic control and non-functional control surfaces, the aircraft began up and down oscillations in phugoid cycles lasting about 90 seconds each, during which the aircraft's airspeed decreased as it climbed, then increased as it fell. The rise in airspeed increased the lift over the wings, which resulted in the aircraft climbing and slowing down, then descending and gaining speed again. The loss of the vertical stabiliser and the rudder removed the only means of damping yaw, and the aircraft lost virtually all meaningful yaw stability. Almost immediately after the separation of the stabiliser, the aircraft began to exhibit Dutch roll, simultaneously yawing right and banking left, before yawing back left and banking right. At some points during the flight, the banking motion became very profound, with banks in large arcs around 50° back and forth in cycles of 12 seconds.[19]
Despite the complete loss of control, the pilots continued to turn the control wheel, pull on the control column, and move the rudder pedals up until the moment of the crash.[3]: 7–12, 128 The pilots also began efforts to establish control using differential engine thrust,[3]: 19–24 as the aircraft slowly wandered back towards Haneda. Their efforts were of limited success. The unpressurised aircraft rose and fell in an altitude range of 20,000–25,000 feet (6,100–7,600 m) for 18 minutes, from the moment of decompression until around 6:40 p.m., with the pilots seemingly unable to figure out how to descend without flight controls.[3]: 1–6 This is possibly due to the effects of hypoxia at such altitudes, as the pilots seemed to have difficulty comprehending their situation as the aircraft pitched and rolled uncontrollably. The pilots possibly were focused, instead, on the cause of the explosion they had heard, and the subsequent difficulty in controlling the jet.[3]: 126, 137–38 The flight engineer did say they should put on their oxygen masks when word reached the cockpit that the rear-most passenger masks had stopped working. None of the pilots put on their oxygen masks, however, though the captain simply replied "yes" to both suggestions by the flight engineer to do so. The accident report indicates that the captain's disregard of the suggestion is one of several features "regarded as hypoxia-related in [the] CVR record[ing]."[3]: 97 Their voices can be heard relatively clearly on the cockpit area microphone for the entire duration, until the crash, indicating that they did not put on their oxygen masks at any point in the flight.[3]: 96, 126
At 6:35 p.m. the flight engineer responded to multiple (hitherto unanswered) calls from Japan Air Tokyo via the selective-calling system. Having just been informed about the inoperative oxygen masks, the flight engineer voiced the (erroneous) assumption that the R-5 door was broken and informed the company that they were making an emergency descent. Japan Air Tokyo asked if they intended to return to Haneda, to which the flight engineer responded that they were making an emergency descent, and to continue to monitor them.[3]: 306–07
Eventually, the pilots were able to regain limited control of the aircraft by adjusting engine thrust. In doing so, they were able to dampen the phugoid cycle and somewhat stabilise their altitude. However, given jet engines' inertia and the resulting response time (to changes in throttle), "[s]uppressing of Dutch roll mode by use of the differential thrust between the right and left engines is estimated practically impossible for a pilot."[3]: 89 Shortly after 6:40 p.m., the landing gear was lowered using an alternate gravitational system in an attempt to dampen the phugoid cycles and Dutch rolls further, and to attempt to decrease the aircraft's airspeed to descend. The system whis was somewhat successful, as the phugoid cycles were dampened almost completely, and the Dutch roll was damped significantly, but lowering the gear also decreased the directional control the pilots were getting by applying power to one side of the aircraft, and the aircrew's ability to control the aircraft deteriorated.[19]
Shortly after lowering the gear, the flight engineer asked if the speed brakes should be used, but the pilots did not acknowledge the request.[3]: 310 The aircraft then began a right-hand descending 420° turn from a heading of 040° at 6:40 p.m. to a heading of 100° at 6:45 p.m., flying in a loop over Otsuki, due to a thrust imbalance created from having the power setting on Engine 1 (the left-most engine) higher than the other three engines.[3]: 290 The aircraft also began descending from 22,400 feet (6,800 m) to 17,000 feet (5,200 m), as the pilots had reduced engine thrust to near idle from 6:43 to 6:48 p.m. Upon descending to 13,500 feet (4,100 m) at 6:45:46 p.m., the pilots again reported an uncontrollable aircraft.[3]: 324 At this time, the aircraft began to turn slowly to the left, while continuing to descend. The thicker air allowed the pilots more oxygen, and their hypoxia appeared to have subsided somewhat, as they were communicating more frequently.[3]: 97 The pilots also appeared to be understanding how grave their situation had become, with Captain Takahama exclaiming, "This may be hopeless" at 6:46:33 p.m.[3]: 317 At 6:47 p.m., the pilots recognised that they were beginning to turn towards the mountains. Despite efforts by the crew to get the aircraft to continue to turn right, it instead turned left, flying directly towards the mountainous terrain on a westerly heading.
Around 6:50 p.m., a photographer on the ground captured a photograph of the aircraft, which showed that the vertical stabiliser was missing. The image showed that around 55% of the tail was missing.[3]: 108
As the aircraft continued west, it descended below 7,000 feet (2,100 m) and was getting dangerously close to the mountains. Because of the thicker air at lower altitude, the cabin altitude alert momentarily turned off at this time, before resuming for the rest of the flight. The captain briefly ordered maximum engine power to attempt to get the aircraft to climb to avoid the mountains, and engine power was added abruptly at 6:48 p.m., before being reduced back to near idle, then at 6:49 p.m., it was ordered raised again.[3]: 319 This greatly excited the phugoid motion,[3]: 291 and the aircraft pitched up, before pitching back down after power was reduced. When power was added again, the aircraft rapidly pitched up to 40° and the airspeed dropped down to 108 knots (200 km/h; 124 mph) at 6:49:30 p.m.,[3]: 1–6 briefly stalling at 9,000 feet (2,700 m). The captain immediately ordered maximum power at 6:49:40 p.m. as the stick shaker sounded.[3]: 320 As the plane pitched downwards once again, the aircraft's airspeed increased bringing the plane into another unsteady climb. Possibly in order to prevent another stall, at 6:51 p.m., the captain lowered the flaps to 5 units[a] – due to the lack of hydraulics, using an alternate electrical system - in an additional attempt to exert control over the stricken jet. It took 3 minutes and 10 seconds for the trailing edge flaps to reach 5 units. The leading edge flaps except for the left and right outer groups were also extended and the extension was completed at 6:52:39 p.m.[3]: 291 [19] From 6:49:03 to 6:52:11 p.m., Japan Air Tokyo attempted to call the aircraft again via the selective-calling radio system. During the entire period, the SELCAL alarm continued to ring,[3]: 320–23 to which the pilots did not react.
The aircraft reached 13,000 feet (4,000 m) at 6:53 p.m., when the captain reported an uncontrollable aircraft for the third time. Shortly afterward, the controller asked the crew to switch the radio frequency to 119.7 for Tokyo Approach. Although the pilots did not acknowledge the request over the radio, they switched frequencies as instructed. Tokyo Approach then contacted the flight via the SELCAL system, briefly activating the corresponding alarm again until the flight engineer responded. At this point, the flight crew requested to be given their position, which, at 6:54 p.m., was reported to the flight as 45 nmi (83 km) northwest of Haneda, and 25 nmi (46 km) west of Kumagaya. At 6:55 p.m., the captain requested flap extension, and the co-pilot called out a flap extension to 10 units, but the flaps had already reached 15 units, and were continuing to extend even further.[3]: 291 Meanwhile, the aircraft had started banking towards the right, this may be most likely due to an imbalance in the lift generated by the left and right flaps. Power was increased at the same time. While the flaps continued to extend, a differential thrust setting caused engine power on the left side to be slightly higher than on the right side, adding to the roll to the right.[3]: 291–92
One minute later, the flaps reached about 25 units. Subsequently, the bank angle to exceed 60°, and the nose began to drop.[3]: 292 It is likely that the flaps were not evenly distributed, and instead operated asymmetrically, resulting in a lift imbalance between the left and right wing. Captain Takahama immediately ordered the flaps to be retracted.[3]: 326 The flaps slowly began to retract and power was added abruptly, but still with higher power settings on the left engines than on the right.[3]: 292 The asymmetric thrust settings continued to increase as the bank angle exceeded 80°, the captain was heard on the CVR desperately requesting for the flaps to be retracted and for more power to be applied in a last-ditch effort to raise the nose.[20][3]: 326–27 The aircraft continued an unrecoverable right-hand descent towards the mountains as the bank angle recovered to about 70° and the engines were pushed to full power and the bank angle had lessened somewhat, during which the ground proximity warning system sounded and the plane disappeared from radar at 6,800 feet (2,100 m).In the final moments, as the airspeed exceeded 340 knots (630 km/h; 390 mph), the pitch attitude leveled out and the aircraft ceased descending, with the aircraft and passengers/crew being subjected to 3 g of upward vertical acceleration.[3]: 292
The aircraft was still in a 40° right-hand bank when the right-most (#4) engine struck the trees on top of a ridge located 1.4 kilometres (0.87 mi) north-northwest of Mount Mikuni at an elevation of 1,530 metres (5,020 ft), which can be heard on the CVR recording. The backward shock of the impact, measuring 0.14 g, in addition to causing the loss of the thrust of the 4th engine, caused the aircraft to roll sharply to the right and the nose to drop again. The aircraft continued on this trajectory for 3 seconds until the right wing clipped another ridge containing a "U-shaped ditch" 520 metres (1,710 ft) west-northwest of the previous ridge at an elevation of 1,610 metres (5,280 ft). It is speculated that this impact separated the remainder of the weakened tail from the airframe, along with the outer third of the right wing, and the remaining three engines, which were "dispersed 500–700 metres (1,600–2,300 ft) ahead".[3]: 19, 91 After this impact, the CVR and FDR stopped recording at 6:56:28 p.m. and the aircraft flipped on its back, struck another ridge 570 metres (1,870 ft) northwest from the second ridge, near Mount Takamagahara, and exploded.
The impact registered on a seismometer located in the Shin-Etsu Earthquake Observatory at Tokyo University from 6:56:27 p.m. as a small shock, to 6:56:32 p.m. as a larger shock, believed to have been caused by the final crash. The shockwaves took an estimated 2.0–2.3 seconds to reach the seismometer, making the estimated time of the final crash 6:56:30 p.m.[3]: 108–09 Thus, 32 minutes had elapsed from the bulkhead failure to the crash.[3]: 123, 127 [21]
The aircraft crashed at an elevation of 1,565 metres (5,135 ft) in Sector 76, State Forest, 3577 Aza Hontani, Ouaza Narahara, Ueno Village, Tano District, Gunma Prefecture. The east-west ridge is about 2.5 kilometres (8,200 ft) north-northwest of Mount Mikuni.[3] Ed Magnuson of Time magazine said that the area where the aircraft crashed was referred to as the "Tibet" of Gunma Prefecture.[8]
18:24:35: Sound like "bang"
18:24:37: Cabin Altitude alert begins
18:24:39: (CAP) Something exploded?
18:24:42: (CAP) Squawk 77
18:24:43: (COP) Gear door (CAP) Check gear, gear.
18:24:47:(CAP) Engine?
18:24:48:(COP) Squawk 77
18:24:49:(F/E) All engine . . .
18:24:51:(COP) Look at this.
18:24:53:(F/E) Eh
18:24:55:(F/E) All engine…
18:24:57:(COP) Shall we check hydro pressure?
18:24:59:(CAP) Something exploded.
(CAP) Right turn
(CAP) Right turn
(COP) Pressure ? (F/E) Dropped.
(CAP) Ah, Tokyo, Japan Air 123 request from immediate e-- trouble request return back to Haneda descend and maintain 220 over.
(ACC) Roger, approved as you requested.
(CAP) Radar vector to OSHIMA, please.
(ACC) Roger, uh, you want right or left turn?
(CAP) Going to right turn, over.
(ACC) Alright, right heading 090, radar vector to Oshima.
(CAP) 090
(CAP) Don’t bank so much.
(COP) Yes.
(CAP) Don’t bank so much.
(COP) Yes.
(CAP) What’s is that?
(F/E) Hydraulic pressure has dropped, hydro.
(CAP) Don’t bank so much. It’s manual.
(COP) Yes.
(CAP) Turn it back.
(COP) It doesn’t go back.
(CAP) Pull up
(CAP) Hydro is all out?
(F/E) Yes.
(ACC) Ah, 123, negative, negative, negative, call you.
(ACC) Japan Air 123, confirm you are declaring an emergency, that's right?
(123) That's affirmative.
(ACC) 123, roger. And, uh, request your nature of emergency.
(CAP) Hydro?
(F/E) Yes.
(F/E) Hydro pressure all loss.
(COP) All loss?
(CAP) No, look.
(F/E) All loss.
(COP) All loss?
(F/E) Yes.
(ACC) Japan Air 124(sic), fly heading 090, radar vector to Oshima.
(123) But now uncontrol.
(ACC) Uncontrol, roger, understood.
(ACC) Japan Air 123, uh, can you descend?
(CAP) Ah, roger, now descending.
(ACC) Ok, say altitude now.
(123) 240.
(ACC) Alright, your position, 72 miles to Nagoya. Uh, can you land to Nagoya?
(123) Ah, negative, uh. Request back to Haneda.
(ACC) Alright, uh, (in Japanese from this point forward) You may speak in Japanese from now on.
(123) Yes, yes.
(F/E) Captain.
(CAP) Yes.
(F/E) The R5 masks have stopped, I think we'd better make an emergency descent.
(CAP) Yes.
(F/E) Shall we use our masks too?
(CAP) Yes. (COP) We'd better.
(F/E) If possible, I think it’d better to use oxygen masks.
(CAP) Yes
(F/E) Gear down, how about gear down?
(COP) Shall we gear down?
(CAP) Doesn't work. Gear won't go down.
(F/E) Shall I lower it slowly by alternate?
(CAP) Yes, wait a moment.
(F/E) I have lowered the gear.
(COP) Yes.
(ACC) Japan Air 123, Japan Air 123, can you switch to frequency 134.0?
Japan Air 123, Japan Air 123, Tokyo Control, if you read me ident, please.
(CAP) Lower the nose. Never mind that. You'll stall.
(COP) Yes.
(ACC) All station, all station, except Japan Air 123, contact Tokyo Control, contact Tokyo Control, 134.0, change frequency 134.0, and keep silent until further notice.
(CAP) Heavy. More, lower the nose a little more.
(COP) Yes.
(CAP) We're going down.
(CAP) Heavy.
(CAP) Is the wheel pushed all the way?
(COP) All the way, it's all the way.
(CAP) Ah, heavy.
(F/E) How about the flap? Shall we extend it?
(CAP) It's still too early.
(F/E) It's still to early?
(CAP) It's still too early.
(COP) Are the gears down?
(F/E) Gears are down.
(Yokota AFB) Japan Air One Twenty Three, Japan Air One Twenty Three, Yokota Approach on guard, if you hear me, attempt contact 129.4.
(123) Japan Air 123 uncontrollable
(ACC) Japan Air 123, go ahead.
(ACC) Japan Air 123 roger understood, understood, and uh.
(ACC) Japan Air 123, do you wish to contact Haneda?
(123) Stay with us please.
(ACC) Do you wish to contact?
(123) Stay with us please.
(ACC) Yes, understood, standby, please wait.
(CAP) This may be hopeless.
(CAP) Ah, request radar vector to Haneda ah Kisarazu1
. (ACC) Roger, understood. As the runway 22, keep heading 090.
(CAP) Roger.
(F/E) The hydraulic quantity is all lost.
(ACC) Can you control the aircraft now?
(123) It's uncontrollable.
(ACC) Roger.
Cabin Altitude alert stops
(CAP) Hey, mountain... Turn right. Mountain!
(COP) Yes.
(CAP) Take control, right! Right turn!
(COP) Right turn?
(CAP) We'll hit a mountain! (COP) Yes.
(CAP) Right turn.
Cabin Altitude alert begins again.
(CAP) Max power.
(COP) Max power.
Cabin Altitude alert stops.
(CAP) We'll go into the mountains. (COP) Yes.
(COP) Shall I increase power?
(CAP) Power, power.
Cabin Altitude alert begins again.
Selective calling system begins ringing, until 18:53:00.
18:49:35: Stick shaker begins vibrating
18:49:39: (CAP) Ah, not good.
Stall! Max power! Max power! Max power!
Stall. Altitude has dropped.
(COP) We're gaining speed, speed.
(CAP) Let's give it a try.
(CAP) Stick with it. (COP) Yes.
(CAP) Lower the nose. Stick with it, stick with it.)
(COP) Now, I've fully pushed the control.
(F/E) Max Power.
(COP) We're losing speed, speed.
(CAP) You'll have to control pitch with power.
(F/E) Power control is OK, let use power control, please.
(CAP) We're losing altitude. (COP) Yes.
(CAP) Raise, raise the nose.
(COP) Flap?
(F/E) Shall I lower it?
(CAP) It won't go down.
(F/E) Yes, eh, by alternate.
(COP) Alternate, as expected. (F/E) Yes, it is by alternate.
(F/E) Flap is now being extended by alternate. (CAP) Yes.
(CAP) Eh, uncontrol, Japan Air 123 uncontrol.
(ACC) 123, roger. Japan Air 123 Japan Air 123, switch frequency to 119.7, 119.7, please.
(F/E) Japan Air 123, eh, I've selected 119.7.
(CAP) Request position.
(F/E) Request position. Japan Air 123, request position.
(F/E) They say we're 25 miles west of Kumagaya.
(CAP) Can you extend flap?
(COP) Yes, flap 10.
(CAP) Raise the nose. Raise the nose. Raise the nose.
(CAP) Raise the nose.
(COP) I've been holding for a long time.
(COP) Power.
(CAP) Hey, halt the flap.
(?) Ah...
(CAP) Power! Don't extend the flaps so deeply!
(COP) Flap up, flap up, flap up, flap up.
(CAP) Flap up. (COP) Yes.
(CAP) Power. Power! Flap!
(F/E) It is up.
(CAP) It'll stall!
(CAP) Raise the nose. Raise the nose! Power!
(GPWS) Sink rate.
WHOOPWHOOP
PULL UP
WHOOPWHOOP
PULL UP
WHOOPWHOOP
PULL UP (CAP) It's the end!(?)
WHOOPWHOOP
PULL UP (Sound of Engine 4 impacting ridge)
WHOOPWHOOP
PULL UP
(Sound of right wing impacting ridge)
(Tape ends).
A United States Air Force navigator stationed at Yokota Air Base published an account in 1995 that stated that the U.S. military had monitored the distress calls and prepared a search-and-rescue operation that was aborted at the call of Japanese authorities. A U.S. Air Force C-130 crew was the first to spot the crash site 20 minutes after impact, while it was still daylight, and radioed the location to the Japanese and Yokota Air Base, where an Iroquois helicopter was dispatched.[22] An article in the Pacific Stars and Stripes from 1985 stated that personnel at Yokota were on standby to help with rescue operations, but were never called by the Japanese government.[23]
A JSDF helicopter later spotted the wreck after nightfall. Poor visibility and the difficult mountainous terrain prevented it from landing at the site. The pilot reported from the air no signs of survivors. Based on this report, JSDF personnel on the ground did not set out to the site on the night of the crash. Instead, they were dispatched to spend the night at a makeshift village erecting tents, constructing helicopter landing ramps, and engaging in other preparations, 63 kilometres (39 mi) from the crash site. Rescue teams set out for the site the following morning. Medical staff later found bodies with injuries suggesting that people had survived the crash only to die from shock, exposure overnight in the mountains, or injuries that, if tended to earlier, would not have been fatal.[19] One doctor said, "If the discovery had come 10 hours earlier, we could have found more survivors."[24]
One of the four survivors, off-duty Japan Air Lines flight purser Yumi Ochiai (落合 由美, Ochiai Yumi) recounted from her hospital bed that she recalled bright lights and the sound of helicopter rotors shortly after she awoke amid the wreckage, and while she could hear screaming and moaning from other survivors, these sounds gradually died away during the night.[19]
The official cause of the crash according to the report published by Japan's Aircraft Accident Investigation Commission is:
In an unrelated incident on 19 August 1982, while under the control of the first officer, JA8119 suffered a runway strike of the No. 4 engine on landing at Chitose Air Base in poor visibility. This was repaired successfully and the aircraft again returned to service. This incident did not contribute to the Flight 123 accident.[3]: 102
The Japanese public's confidence in Japan Air Lines took a dramatic downturn in the wake of the disaster, with passenger numbers on domestic routes dropping by one-third. Rumors persisted that Boeing had admitted fault to cover up shortcomings in the airline's inspection procedures, thereby protecting the reputation of a major customer.[19] In the months after the crash, domestic traffic decreased by as much as 25%. In 1986, for the first time in a decade, fewer passengers boarded JAL's overseas flights during the New Year period than the previous year. Some of them considered switching to All Nippon Airways, JAL's main competitor, as a safer alternative.[28]
JAL paid ¥780 million (US$7.6 million) to the victims' relatives in the form of "condolence money" without admitting liability. JAL president Yasumoto Takagi resigned.[19] In the aftermath of the incident, Hiroo Tominaga, a JAL maintenance manager, died from suicide intended to atone for the incident,[29] as did Susumu Tajima, an engineer who had inspected and cleared the aircraft as flightworthy, due to difficulties at work.[30]
In compliance with standard procedures, Japan Air Lines retired flight number 123 for their Haneda-Itami routes, changing it to Flight 121 and Flight 127 on September 1, 1985. While Boeing 747s were still used on the same route operating with the new flight numbers in the years following the crash, they were replaced by the Boeing 767 or Boeing 777 in the mid-1990s. Boeing 747-100SRs continued to serve JAL on domestic routes until their retirement in 2006, having been replaced by newer widebody aircraft such as the Boeing 747-400D and Boeing 777, introduced during the 1990s and early 2000s. Boeing 747 operations at JAL ended in 2011 when the last 747-400 was returned to the lessor as part of the airline's efforts to cut costs, with twin-engined widebodies such as the Boeing 777, Boeing 787 Dreamliner, and Airbus A350 utilised on the routes instead.[31]
In 2009, stairs with a handrail were installed to facilitate visitors' access to the crash site. Japan Land, Infrastructure, Transport, and Tourism Minister Seiji Maehara visited the site on August 12, 2010, to remember the victims.[32] Families of the victims, together with local volunteer groups, hold an annual memorial gathering every August 12 near the crash site in Gunma Prefecture.[33]
The crash led to the 2006 opening of the Safety Promotion Center,[34][35] which is located in the Daini Sogo Building on the grounds of Haneda Airport.[36] This center was created for training purposes to alert employees to the importance of airline safety and their responsibility to ensure safety. The center has displays regarding aviation safety, the history of the crash, and selected pieces of the aircraft and passenger effects (including handwritten farewell notes). It is open to the public by appointment made between one day and two months before the visit.[37]
The captain's daughter, Yoko Takahama, who was a high-school student at the time of the crash, went on to become a flight attendant for Japan Air Lines.[38]
Japanese banker Akihisa Yukawa had an undisclosed second family at the time he died in the crash. (His wife had earlier suffered severe brain injuries.) His girlfriend, Susanne Bayly, was pregnant with their second daughter at the time of the crash; she subsequently returned to London, where Yukawa and she had met, bringing with her their daughters. To avoid embarrassment to Yukawa's family, she accepted a settlement of £340,000, rather than claiming under the airline's compensation scheme. In 2002, the airline made a payment of an undisclosed amount to enable the daughters, Cassie and Diana, to complete their educations.[39]
On June 24, 2022, an oxygen mask belonging to Japan Air Lines Flight 123 was found near the crash site during road repair work. The discovery came nearly a year after engine parts were also found in the same area.[40]
Simulation of the final 32 minutes with the CVR on YouTube
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Category: Aviation accidents and incidents caused by loss of controlCategory: Airliner accidents and incidents caused by in-flight structural failureCategory: Airliner accidents and incidents involving in-flight depressurizationCategory: Airliner accidents and incidents caused by maintenance errorsCategory: Aviation accidents and incidents in JapanCategory: Aviation accidents and incidents in 1985Category:1985 in Japan123Category: Accidents and incidents involving the Boeing 747Category: August 1985 events in AsiaCategory: History of the Japan Air Self-Defense ForceCategory:Airliner accidents and incidents caused by tailstrikes