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Analysis of Radio Direction Finder Bearings in the Search for Amelia Earhart |
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| Introduction | |||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||
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| Computer Modeling | |||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||
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| Signal-to-Noise Ratio (SNR) Considerations | |||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||
| Reception probabilities were calculated from the signal statistics reported by ICEPAC. The value given in each case is the probability that the SNR would equal or exceed the required level.
International Telecommunications Union (ITU) Recommendation F.339-6 specifies the required SNR values for various signal types and grades of service. An amplitude-modulated double-sideband signal, such as emitted by the NR16020 transmitter, is classified by F.339-6 as an A3E emission. The lowest acceptable grade of service specified in F. 339-6 for an A3E emission is 90 percent understandability of sentences (“just usable”) for non-diversity6 reception in fading conditions. The F.339-6 required input SNR for this grade of service is 51 decibels (dB) in a 1 Hertz band, which yields a 6 dB audio output SNR in a receiver with a 6 kHz noise bandwidth. However, the F.339-6 results for analog systems are based on white Gaussian noise,7 and Spaulding8 has presented results showing that a given voice understandability can be achieved with a 6 dB smaller SNR in atmospheric noise, which is impulsive in nature. Applying this reduction would change the required SNR to 45 dB in a 1 Hertz band, for a 6 dB audio output SNR. This implies that a 39 dB input SNR would produce a 0 dB audio output SNR. This analysis assumes that the background noise at the DF sites was predominantly atmospheric, and that the 6-dB SNR reduction for voice signals applies, based on the following considerations:
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| Potential Signal Sources | |||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||
| Since Earhart was known to have transmitted only in voice (A3) mode, and all bearings obtained by the DF sites were at night on signals near 3105 kHz, the consideration of potential sources for those signals was constrained to ships, aircraft, and land stations capable of A3 transmission on frequencies near 3105 kHz, and to AM band broadcast stations operating on frequencies with harmonics near 3105 kHz.
Receiver selectivity, the ability to reject unwanted signals, must be considered when deciding whether signals can be heard on a frequency other than the one to which the receiver is tuned. The radio equipment at each mid-Pacific Pan Am DF site10 included an RCA type AR-60 state of the art superheterodyne communication receiver. It is assumed that the AR-60 was used to listen for Earhart signals. Although the AR-60 selectivity characteristics are not available, communication receivers of the day typically operated at a bandwidth of 6 kHz when listening for voice signals. This analysis assumes that the AR-60 selectivity was essentially the same as that of the Hammarlund SP-110 superheterodyne receiver,11 which was introduced in 1936 and is considered to be representative of the state of the art at the time. The SP-110 featured user-selectable bandwidth which, at 6 kHz, had a selectivity response that attenuated the output SNR of a signal on an unwanted frequency signal, relative to the SNR of a signal on the desired frequency, by 6 dB at a 3 kHz frequency difference, 23 dB at 5 kHz, 60 dB at 8 kHz, 90 dB at12 kHz, and 103 dB at 15 kHz. Accordingly, only signal source frequencies within 15 kHz of 3105, i.e., in the range 3090 kHz to 3120 kHz, were considered in this analysis. The characteristics of the receiving antennas at the DF sites are not known, so this analysis assumes isotropic antennas. Similarly, it is assumed that the transmitting antennas of the potential signal sources, under consideration were isotropic, with the exception of the dorsal antenna on NR16020, and the broadcast band vertical tower radiators. The broadcast band antenna gain characteristics are provided in the LFMF model. Aircraft 3105 kHz (A3) was an air-to-ground calling frequency for U.S. civilian aircraft.12 Ground stations responded on 278 kHz.13 Ships The ITU listed28 a total of 13 ships worldwide, 1 U.S. and 12 Soviet, capable of voice (A3) transmission on frequencies within 15 kHz of 3105 kHz. The U.S. ship and 11 of the Soviet ships operated on 3120 kHz. These ships were ruled out as possible DF signal sources, under the procedure described in Appendix A. The twelfth Soviet ship, the Magnitogorsk, had 3105 kHz among its assigned frequencies, but was ruled out as a possible DF signal source, under the procedure described in Appendix B. Coast Stations Coast stations provided two-way communications with ships at sea and also with ships on inland waterways. There were numerous coast stations,29 but few were capable of A3 transmission on frequencies within 15 kHz of 3105 kHz. Other Land Stations Aeronautical Service.There was an A3-capable aeronautical service station on 3088 kHz at Winslow, Arizona.Point-to-Point Communication.There was an A3-capable Soviet point-to-point communication station on 3090 kHz, at Voronej.AM Band Broadcast.There were two AM band broadcast stations operating on frequencies with harmonics near 3105 kHz. Station 3AR at Melbourne, Australia, operated on 620 kHz, at 4,500 watts. The fifth harmonic of 620 kHz is 3100 kHz. Station RW26, at Stalino, Soviet Union, operated on 776 kHz at 10,000 watts. The fourth harmonic of 776 kHz is 3104 kHz. | |||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||
| Compilation of Potential Signal Sources | |||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||
The potential signal sources are compiled in Table 1.
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| Functions: BC: Broadcast station; FA: Aeronautical support station; FC: Coast station, providing communication with ships at sea or on inland waterway system; FX: Fixed point -to-point communications. | |||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||
Each source in Table 1 was tested using the method described in Appendix A, to determine the feasibility of reception at each DF site under hypothetical ideal propagation conditions. This test provides a conservative basis for deciding whether the source can be ruled out as the potential origin of signals at a given DF site. If the source signal could not produce the required receiver input SNR under the ideal conditions of the test, then it could not do so under realistic propagation conditions. The test results are shown in Table 2.
The receiver selectivity attenuation corresponding to the source frequency is shown, together with the source distance from each DF site, and the free-space SNR resulting from the test. Recalling that the threshold input SNR, for detecting the presence of an A3 signal without distinguishing any words is 41 dB for this analysis, the results shown in Table 2 can be sorted into three categories. The SNR for signals from some sources robustly exceed the threshold at some or all DF sites; some marginally exceed or fall below the threshold; and some fall far below the threshold. Retaining the first two categories and deleting the third yields the following table of potential sources retained for further consideration in the analysis.
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| The Direction Finder Sites | |||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||
| The Pan American Airways (PAA) high frequency (HF) direction finder (DF) sites at Wake Island, Midway island, and Mokapu Point on Oahu, Hawaii, listened for post-loss radio signals and obtained bearings on a combined total of 6 signals on 3105 kHz on July 4 and July 5. Most of those bearings were approximate at best, due to weakness and short duration of signals. An additional bearing was taken by the Mokapu Point site on a signal believed to have originated from the Itasca, as part of an unsuccessful experiment to determine a corrective factor to be applied to post-loss signal bearings.
During the search the Itasca deployed an experimental high-frequency direction finder on Howland Island manned32 by Coast Guard Radioman Second Class Frank Cipriani. This equipment was used on July 5 to obtain an approximate bearing on a signal near 3105 kHz. The PAA DF System Sandretto’s description31 of the PAA Adcock DF system illustrates the importance of signal strength and duration. A signal bearing was indicated by an aural null. But instead of measuring the null bearing directly, the operator observed bearings on each side of the null where the signal level was high enough for accurate measurement, over a period of 2 to 3 minutes, and averaged those bearings to obtain the null bearing. The accuracy of the bearings on each side of a null, and thus the accuracy of the average bearing, would be adversely affected if a signal was weak or of short duration. Bearing Ambiguity The Adcock DF system produces a figure-eight antenna beam pattern, which is rotated via a goniometer to obtain a null, or signal minimum. The antenna pattern is symmetrical about the null axis, which allows bearing ambiguity because it is possible to get two null bearings 180 degrees apart. Adcock DF system designs of the 1930s usually incorporated a vertical sense antenna to eliminate bearing ambiguity. But some remarks in the PAA DF site logs indicate the possibility of bearing ambiguity, suggesting that PAA might have simplified their system design by omitting the sense antenna, since each DF site would know the general bearing of a Clipper flight. This is consistent with the recollection of Captain Almon A. Gray, USNR (ret), who was the Assistant Communications Superintendent for the PAA Pacific division during the Clipper era. Gray said32 of the PAA DF system:“The system was bi-directional hence one had to be ever mindful of the possibility of reciprocal bearings. That was not much of a problem however as one usually knew the general location of the aircraft”.This analysis assumes the PAA DF system was bi-directional and examines the possibility of a reciprocal bearing source in each case. Distances The distance from Wake Island to Midway Island is approximately 1,080 nautical miles (nmi), and the distance from Midway to Honolulu is approximately 1,150 nmi. Thus a flight on the route between Wake and Honolulu would never be more than about 600 nmi from the nearest DF site. In contrast, the distances from Gardner Island to Wake, Midway, and Honolulu are 1,825nmi, 1,990 nmi, and 1,850 nmi respectively. Signal Strength Considerations High frequency direction finding sites take bearings on skywaves, which travel long distances via refraction from the ionosphere. Short term variations in the ionosphere can cause signal strength fading, reducing the SNR and increasing the difficulty of getting an accurate bearing. If fading occurs on an already weak signal, the SNR can drop below the reception threshold, making it impossible to obtain a bearing. On the other hand, increasing atmospheric noise can cause the SNR of an already weak signal to drop below the threshold even without fading. The PAA DF system33 site locations, radio equipment, DF equipment, and operating procedures clearly were chosen to ensure accurate bearings would always be available for support of PAA flights . The 70-watt output power of transmitter34 on the Pan Am Clippers was roughly comparable to the 50-watt output of the transmitter on NR16020. However, as noted earlier, the distances from Gardner Island to the PAA DF sites were about 3 times the maximum distance from a Clipper to the nearest DF site on the route between Wake Island and Honolulu. Hence, the propagation loss for signals from Gardner Island was at least 10 times greater than for signals from a Clipper to the nearest DF site, making the SNR for any signals from Gardner Island correspondingly lower. And signals from the other potential sources, which were even further away, were likely to be much weaker than those expected from Clipper aircraft. The result, not surprisingly, was that bearings on potential post-loss signals were tenuous and approximate at best. That the DF site personnel were able to get any bearings at all in such conditions is a tribute to their skill and dedication. Each PAA DF site35 used two concentrically arranged sets of Adcock antennas, covering the frequency band 200 kHz to 6,000 kHz. Adcock antennas were used36 because, although they are electrically equivalent to loop antennas, they are immune to the effects of polarization shifts37 in radio waves refracted by the ionosphere. A downcoming skywave, will have both vertically and horizontally polarized components which fade38 independently of each other. The presence of a horizontally polarized component in a radio wave causesnight effect39 in a loop antenna by inducing voltages that do not cancel out when the plane of the loop is perpendicular to the bearing of the radio wave. This results in an inaccurate bearing, or an indistinct minimum, or both. The Adcock antenna, being insensitive to horizontally polarized waves, avoids this problem40 . Notwithstanding its ability to obtain usable skywave bearings, the performance of the Adcock antenna is limited41 by the fact that its ability to extract energy from a passing radio wave is the same as that of a loop antenna with a single turn of wire, and hence is quite small. Consequently, even with the Adcock antennas at the DF sites, it was difficult to obtain usable bearings on weak signals. Site Terrain EffectsTerrain interference of skywave signals at a DF site can reduce signal strength and cause bearingerrors. The elevation angle of arriving skywave signals is a key consideration in this regard . Thisangle depends on the height of the ionospheric reflection point and its distance from the receiving site,which in turn depend upon date, time, signal frequency, and conditions in the ionosphere. Wake Island , Midway Island, and Howland Island are essentially flat, so the DF sites there had no terrain interference. But the situation at the Mokapu Point DF site was quite different. Mokapu Point Terrain The Mokapu Point site was at approximately 21° 27' 21" North latitude, 157° 45' 44" West longitude, near the seaward edge of a large flat area in what later became the U.S. Marine Corps Air Station at Kaneohe Bay. The DF site coordinates were derived by correlating topographic map42 features with two photographs of the antenna array and associated buildings. One photo43 was taken from offshore looking westward toward the Koolau mountain range and shows the DF site near the shoreline at a height of about 40 feet above the beach. The other photo44 was taken from onshore looking north toward the sea. The crest of the Koolau range on the great circle bearing of Gardner Island (214 degrees) is 6.75 statute miles from the DF site coordinates. The mean orientation of the ridge line45 in that area is 340/160 degrees true, with some segments deviating from the mean by up to 50 degrees. The southwest slope46 of the Koolau range is a forested watershed with numerous ridges, valleys, and running streams. The terrain in this area, along the path of a signal arriving from Gardner Island, has a compound slope rising from sea level at Honolulu to about 1,800 feet over a distance of 6.3 miles at a vertical angle of approximately 3.1 degrees, and tilting downward to the right at a slope angle of approximately 10.8 degrees across the path to the DF. The terrain on the northeast slope of the range drops from the ridge line to near sea level in about one mile, and remains essentially flat from there to the DF site, and beyond to the sea. The elevation angle of the ridge line from the DF site coordinates, on the bearing of Gardner Island, is approximately 2.9 degrees, hence the DF site would be in the radio “shadow” of the Koolau range for skywave signals arriving with lesser elevation angles. But even signals with somewhat greater elevation angles could encounter terrain effects. The lower edge of the wavefront would contact the terrain on the southwest slope, potentially sustaining directional skewing. Moreover, diffractive scattering from the ragged ridge line could cause signals to arrive at the DF site from multiple directions, making it difficult to obtain a reliable signal bearing. The elevation angle at the DF site for signals on 3105 kHz arriving from Gardner Island and the Itasca ranged from 1.4 degrees to approximately 12 degrees at the times of the Mokapu bearings. Angles near the low end of this range were small enough to put the DF site in the radio shadow of the Koolau ridge. Angles near the middle of the range were small enough that, although the DF site was not in the radio shadow, there could have been significant terrain effects. Angles near the upper end of the range were large enough that terrain effects can be assumed to be minimal. The bearing of the Itasca from the Mokapu DF site varied between 225 and 232 degrees on July 3 through July 6. The height of the Koolau ridge in this sector varies between 2,600 feet and 2,800 feet, and the average terrain elevation angle from the DF site is approximately 4.8 degrees. This may have been a factor in the unsuccessful attempt to get a bearing on the Itasca on July 6, discussed later. The bearing of Midway from the Mokapu site coordinates is 295 degrees, and the Koolau ridge elevation angle on that bearing is 2 degrees. PAA flights on the Midway -Honolulu route operated only during daylight hours47 , and their signals arrived at the DF site with elevation angles of at least 30 degrees. Hence, terrain was not a significant factor in bearing accuracy for normal PAA operations. And the Mokapu site had an unobstructed “view” of the radio path of signals from PAA flights on the route to and from Alameda. Clearly, the Mokapu DF site was well-positioned for obtaining accurate bearings for its designed mission of supporting flights to and from Midway and Alameda, but was operating at a potential terrain disadvantage in the search for post-loss Earhart signals. ICEPAC does not take into account the terrain interference effects described above, so the SNR values given in this paper for low-angle signals from Gardner Island or the Itasca should be regarded as upper-bound values, i.e., the actual SNRs could have been less than the values computed by the model. The BearingsBearing reports and signal descriptions from source documents are presented and analyzed here, in chronological order. The analysis of each bearing includes a table showing, for each potential signal source, the times of sunrise and sunset, the bearing – and its reciprocal – of the source from the DF site, the mean SNR for a signal from the source, and the probability that the SNR would exceed the reception threshold. Most official messages and reports cited in this paper used Greenwich Civil Time (GCT), designated by the “Z” time zone and now known as Greenwich Mean Time (GMT), but some used Honolulu Standard Time (HST), which was 10.5 hours behind GCT. Both notations are retained in this paper, with each instance of HST time and date accompanied by the corresponding Z time and date to avoid confusion, since some events occurred on different HST and Z dates depending on the event time. For example, 4 PM (1600) HST on July 4 was 0230Z on July 5. Bearing 11512Z July 4 Mokapu Point Honolulu radio station KGMB (1320 kHz) made a series of broadcasts to Earhart, beginning at 2000 HST July 3 (0630Z July 4) and continuing at intervals of about 15 minutes for several hours48,requesting that she indicate her general location by sending a combination of dashes from a list of options provided in the broadcasts. At 1512Z July 4 (0442 HST July 4), Mokapu obtained a bearing of 175 degrees on a signal presumably on 3105 kHz. This signal is not mentioned in the Mokapu supervisor’s post-search report49 but was reported by the operator in charge at the Midway site50,who wrote:“At 1512 GCT, a very faint broad signal apparently a phone was heard here but again was far too weak to take a bearing. Wake reported unheard while Mokapu reported taking a bearing on it which might be 175 approximately.” Table 4 shows the source data for this signal. The “SSS” entries for sunset and sunrise at Billings signify that the site, being on the East Siberian Sea above the Arctic Circle, was continuously in daylight. Table 4 Signal Data for Bearing 1
Analysis
Bearing 2 1523Z to 1530Z July 4 Mokapu Point The Mokapu supervisor’s post-search report52 states“Carrier again heard on 3105 -rough bearing only possible due to weakness and swinging of signals. Get bearing from Mokapu of approximately 213 degrees. Advised Coast Guard.”Mr. G. W. Angus, the PAA Pacific Division Communication Superintendent, was at Midway when this bearing was taken, and later stated in his post-search report53 “On Sunday morning about 5:30 a.m., local time at Mokapu, Mr. Paulson stated he heard signals in the vicinity of 3105 KC, although the frequency could not be accurately determined and on which he obtained an approximate bearing of 210 degrees. The signals Mr. Paulson heard were, undoubtedly, carrier signals modulated with voice although he could not understand the voice part of it. Although it is true several of the domestic lines use frequencies close to 3105 KC, it is doubtful if these signals would have carried to Honolulu at this particular time of day, the time then being 8:00 a. m., Pacific Standard Time. Usually at this time, stations on the West Coast have changed to day frequencies. I believe the signals heard by Mr. Paulson were from the Itasca. This information was passed on to the Coast Guard at Honolulu for whatever it was worth and we continued to listen to the two frequencies used by the plane”. Table 5 Signal Data for Bearing 2
Analysis
6.Angus’ comment about signals from west coast aircraft --“ ...it is doubtful if these signals would have carried to Honolulu at this particular time of day, the time then being 8:00 a. m., Pacific Standard Time. Usually at this time, stations on the West Coast have changed to day frequencies.” - indicates that the DF system was bi-directional, hence the possibility of a reciprocal bearing must be considered. He was correct about commercial aircraft changing to day frequencies, but he failed to consider general aviation aircraft, for which 3105 was the designated calling frequency.
Bearing 3 0630Z July 5 Mokapu Point On the evening of Sunday, July 4, KGMB (1320 kHz) conducted its second night of broadcasts, beginning at 8 PM ( 2000) HST (0630Z July 5), with instructions56 for Earhart to turn on her transmitter for one minute for tuning purposes, then to send 4 long dashes, then wait for an acknowledgment by KGMB 15 minutes later. Mokapu obtained a bearing of approximately 215 degrees on a carrier signal at 3105 kHz immediately following the KGMB broadcast. The post-search report57 by K. C. Ambler, the Mokapu supervisor, described the signal as“close to 3105 but signals so weak that it was impossible to obtain even a fair check. Average seems to be around 215 degrees -very doubtful bearing”.He further stated that although the KGMB broadcast was repeated at half hour intervals during the evening, no further signals were heard that appeared to correlate with the broadcasts. But he did mention that at 1225Z the same day, Wake obtained an approximate bearing of 144 degrees, which seemed“to tie in fairly well with our two bearings of 213 and 215". The Wake bearing is discussed later in this paper. Mr. Angus, the Pacific Division Communication Superintendent, stated in his report58 “Arriving at Mokapu Sunday, I spent most of Sunday night at the radio station and we set up a watch on 3105 KC at the DF and the receiving station. At 7:30 p.m. local Honolulu time, the broadcast station KGMB arranged a special broadcast to the plane on their broadcast frequency, requesting the plane to transmit four long dashes on 3105 KC if they heard KGMB plane. broadcast. Immediately after the broadcast, Mr. Ambler and myself both distinctly heard four dashes on 3105 KC. We are certain of the frequency because the Coast Guard Cutter, Itasca, had previously set their transmitter on this frequency in an effort to contact the Shortly before, we had taken bearings on the Itasca on this frequency, obtaining an approximate bearing of 210 degrees. Upon hearing the four dashes mentioned above, we immediately called KGMB by phone and asked them to repeat the test. This was done and immediately after the second test, we again heard the same signals except at this time, only two dashes were received and the second dash trailed off to a weak signal as though the power supply on the transmitter had failed. Nothing was heard thereafter although a continuous watch was maintained on this frequency all night. During the time these dashes were heard, it was possible to obtain an approximate bearing of 213 degrees from Mokapu.” Table 6 Signal Data for Bearing 3
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