#spaceis
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deksus9.bsky.social
the reason so many billionaires want to go to spaceis because guillotines need gravity to function.
December 24, 2024 at 5:02 PM
cowboycat13.bsky.social
Feed Hungry Kids You Feckless Youknowwhats! 🤮🤮🤮🤮🤮 #Spaceis🐂💩
April 14, 2025 at 7:37 PM
kremacrypto.bsky.social
The great thing about prediction markets and we have several options like those on spaceis the massive upside potential.

You don't necessarily have to be right about the final outcome; if you see investors betting heavily on one extreme, entering early often pays off when the sentiment shifts.
April 7, 2026 at 12:53 PM
masterludwig9.bsky.social
Join the light 💡
#constitution #scarystories #stamendment #nonewnormal #cnnisfakenews #conspiracyfact #hardtruth #ndamendment #ufo #ronpaul #randpaul #msmlies #knowyourenemy #waronfreespeech #thethirdparty #psychologicaloperations #spittingfacts #msmpropaganda #klausschwab #creepypasta #spaceis
June 21, 2026 at 1:27 AM
stephscythes.bsky.social
⭐️ Very well said Mr. Shatner. ⭐️ #space #Earth #ClimateCrisis
William Shatner describes the profound grief he felt when he finally went to space for real (Upworthy)
Statistically speaking, the number of humans who have traveled into spaceis insignificant. But the experience of leaving our home planet and venturing into ...
l.smartnews.com
October 21, 2024 at 10:11 PM
masterludwig9.bsky.social
Join the light 💡
#constitution #scarystories #stamendment #nonewnormal #cnnisfakenews #conspiracyfact #hardtruth #ndamendment #ufo #ronpaul #randpaul #msmlies #knowyourenemy #waronfreespeech #thethirdparty #psychologicaloperations #spittingfacts #msmpropaganda #klausschwab #creepypasta #spaceis
June 21, 2026 at 1:23 AM
longtail-news.bsky.social
Feed: "Daniel Endicott"
By: 3dfle on Wednesday, May 21, 2025
misunderstanding
spaceis a placeto accellerate.Nothing personal.
3dfle.com
May 22, 2025 at 8:19 PM
epsteinweb.bsky.social
EFTA00278336.jpg
#epsteinweb #efta00278336
https://epsteinweb.org
Available in the iOS app store now!
https://apps.apple.com/us/app/epstein-web/id6758880661
EFTA00278135 | EFTA00278336 . NOTICE • Weight opdsbolance or operating, mitation changes shall be..entered in the appropriate aircraft record. An alteration must be compatible withall--previoas alterations to assure continued conformity with the applicable airworthiness requirements. DESCRIPTION OF WORK ACCOMPLISHED.(If more spaceis required, attach additional sheets. craft nationality and registration mark ancrdate work completed.) . . -. Identify with air• ACTL: 488 LANDINGS REF. GULFSTREAM AEROSPACE CORPORATION WORKORDER NO CO2-1517084-2924 INCORP. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT SERVICE CHANGE NO.299 "45,000 FOOT OPERATING ALTITUDE": SECTION . .•.,. NOTE:'-' 1 = REF.'41SC'299 "45,000 FOOT'ORERATIN6ALTITUDE - CERTIFICATION ..• 4k REVISE WEIGHT AND- BALANCE REPORT,AND AIRCRAFT EQUIPMENT LIST AS DUE 3.-'INCORP.'GULFSTREAM AEROSPACE CORPORATION AIRCRAFT SERVICE CHANGE NO.299 "45,000 FOOT OPERATING. ALTITUDE" AIRCRAFT FLIGHT MANUAL SUPPLEMENT NO. G-II-81 -02 (FAA APPROVED) PLACED IN OPERATOR AIRCRAFT FLIGHT MANUAL.. •,, PRE-REQUISITES INSTALLED: - 'NOTE: 1.- GULFSTREAM AEROSPACE CORPORATION A AIRCRAFT SERVICE CHANGE NO. 114-AIRCOND. AND STRUCTURE CABIN PRESSURIZATION 6000 FT. CABIN ALTITUDE AT 43,000 FEET,- REWORK OF: 2. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT SERVICE CHANGE NO. 122 "FUEL BOOST PUMP PROVISIONS FOR NEW=MODEL". 3' FUEL BOOST PUMP'P/N 1159SC011 INSTALLED. 4- ENGINE FUEL FLOW REGULATIONS (LEFT & RIGHT) PIN CASC174 OR LATER INSTALLED: 5. REF. GULFSTREAM AEROSPACE CORPORATION CUSTOMER BULLETIN NO. 302 "ENGINE ACCELERATION AND DECLERATION TIME TEST/ADJUSTMENT" - ENGINE ACCELERATIO, AND DECELERATION TIME CHECKS COMPLETED. 6 -PLACARD P/N 1159820283-11 INSTALLED. . . 7-- FOLLOWING -AIRCRAFT- RECORDS REVIEWED: ...iA -- B C (0 FAA FORM 337'S SUPPLEMENTAL TYPE CERTIFICATE ' CURRENT STATUS OF-ALTIMETER CERTIFICATION WEIGHT'AND BALANCE REPORT CURRENT STATUS' ... EFTA00278336 Epstein Web iOS app on the App Store.
April 26, 2026 at 2:16 AM
epsteinweb.bsky.social
Parts 1-2/2 — EFTA00278240.jpg
#epsteinweb #efta00278240
https://epsteinweb.org
Available in the iOS app store now!
https://apps.apple.com/us/app/epstein-web/id6758880661
EFTA00278135 | EFTA00278240 NOTICE Weight and balance or operating limitation changes shall be entered m the appropnate aircraft`record. An alteration must be compatibleWith all previous alterations to assure continued conformity with the applicable airworthiness requirements:8. Description of Work Accomplished • (Ifmore spaceis required, attach additional sheets. Identify with aircraft nationality and registration mark and date work complete d) Aircraft: Gulfstream, Type: G-1159, SIN 151, Date: 03119/98, W.O. 12307 Page 1 oft Removed the existing Universal Avionics model UNS-1A FMS systems and Canadian Marconi VLF/Omega sensor, and installed new Universal Avionics UNS-D FMS systems. The existing Universal Radio Ttining Unit, Database Transfer Unit and the Universal Loran C sensor were retained. This installation was accomplished using Jet Aviation drawings, FIVIS98001, FMS98002 and IPB98001, Rev. IR, dated 01/20/98 are substantiated by FAA Forms 8110-3, dated 03/11/98 submitted by FAA D.E.R. Mr. Norman J. Curran, FAA D.E.R. No. SO-780. The structural installation of 'the GPS antennas was accomplished using Jet Aviation Drawing HPA98001, Rev. A, dated 03/02/98 and is _structurally substantiated by FAA Form 8110-3, dated 03/12/98 submitted by Lauren Napier, D.E.R. No. SO-815. -The CDU's replaced the removed units at the same station using the existing DZUZ rails installed by the airframe manufacture. The Navigation Computer Units replaced the existing UNS-1A NCU's using the same mounting technique and hardware. The required annunciators were furnished and installed. The following annunciators were installed: MSG (message) annunciator, color amber WPT (wayoint) annuciator, color amber APPR (approach), color white SX (parallel track), color amber HDG (heading), color blue INTEG (integrity) color amber This system, the Universal Avionics UNS-1D FMS system has been previously installed and 'has obtained a STC approval in another type of aircraft, which qualifies this installation as a follow on installation per AC 20-130A and is qualified for FAA Form 337 Field Approval. • • ''sv- The existing No. 4 airdata computer was interfaced to provide the required airspeed input and barocorrected altitude. The existing Honeywell Laser-ref INS system was interfaced as a blended sensor as well as the existing Loran C sensor. The No. 1 compass system is interfaced to the No. 1 FMS and the No. 2 compass system is interfaced to the No. 2 FMS. c. The above annunciators were installed in each instrument panel for their associated system. The Static Loading of the installed equipment meets the requirements of AC 43.13-2A, Chapter 1, Paragraph 3 and was found to meet the requirements of Paragraph 2. Materials and practices comply with Paragraphs 4 through 12. The Electrical Load Analysis was performed in accordance with 43.13-1A, Chapter 11, Section 2, Paragraph 424 and was found to meet the requirements of paragraph 424, 426 and 428. Aircraft Metal Work involving metal repair or alteration complies with AC 43.13-1A, Chapter 2, Section 1 and 3, Chapter 6, Paragraphs 248 and 249. Hardware and materials used the installation conform to AC 43.13-1A, Chapter 5 and 7, Sections 1, 4 and 5 as applicable. Circuit Breakers, switches and connectors are of the type recommended by the aircraft manufacture or are MIL SPEC approved for aircraft use and meet the requirements of AC 43.13-1A, Chapter 11, Paragraphs 429 and 430. Electrical/electronic wiring was selected and installed lAW AC 43.13-1A, Chapter 11 and AC 43.13-2A Chapter 2, Paragraph 21, 22 & 27. Routing, lacing and tying complies with AC 43.13-1A, Chapter 11, Section 7. Wire marking complies with Section 4. Electronic equipment installation complies with yj Additional Sheets Are Attached U.S. GOVERNMENT PRINTING OFFICE: 1992-769-012160157 EFTA00278240
April 26, 2026 at 2:11 AM
epsteinweb.bsky.social
Parts 1-3/3 — EFTA01331177.jpg
#epsteinweb #efta01331177
https://epsteinweb.org
EFTA01331032 | EFTA01331177 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be avowable with allprevious alterations to assure continued conformity with the applicable airworthiness requirements. 8. Description of Work Accomplished (If more spaceIs required attach additional sheets, Identify with aircraft nationality andregistration mark and date work accompffshed) BOEING 727-31, S/N 20115. N9083E. W/O 16236. INSTALLED AN AIRCELL ATG.01 FLIGHT PHONE SYSTEM CONSISTING OF AN ANTENNA PIN CI-5O30, A TRANSCEIVER PIN 900002-2, and AN ANTENNA MATCHING UNIT P/N 83518, 4 EA HANDSETS P/N 440-10035-001 AND 4 EA HANDSET CRADLES P/N 400-10038-001. THESE MODIFICATIONS WERE COMPLETED USING THE FOLLOWING JET AVIATION DRAWINGS, WHICH ARE SUBSTANTIATED BY FAA 8110-3 FORMS RESPECTIVELY: WIRING DRAWING• • B727-13236-330, REV. 111, DATED 4/30/01, SHEETS I THRU 3. TITLED- AIRCELL ATO.01 AIR /GROUND TELEPHONE REFERENCE FAA FORM 8110.3 DATED 5/29/01, BY SYSTEMS & EQUIPMENT D.ER. NO. DERT-510087-NM. STRUCTURAL DRAWINGS AND REPORTS: • B727-16236-I330, REV. A, DATED 529/01, SHEETS 1 THRU 4, TITLED- AIRCELL ATG.01 AIR I GROUND TELEPHONE ANTENNA INSTALLATION REFERENCE FAA FORM 8110-3, DATED 6/18/01, BY STRUCTURAL D.E.R. NO. DERT-510024-CE. • B727-16236-1331, REV. IR, DATED 5/24/01, SHEETS 1THRU 6. -WILED -AIRCELL EQUIPMENT INSTALLATION REFERENCE FAA. FORM 8110-3, DATED 6/3/01, BY STRUCTURAL D.ER. NO. DERT-810028-NE. THE NEW EQUIPMENT AND ASSOCIATED SYSTEMS WERE FUNCTIONALLY TESTED PER AIRCELL ATG.01 FLIGHT PHONE SYSTEM INSTALLATION MANUAL REV IL DATED 611I/99 WITH NO DISCREPANCIES. AN EMI TEST, REPORT NO.: B727-16236-080 REV IR, SHEETS 5. DATED 06/19/01 WAS CONDUCTED AND THE INSTALLED EQUIPMENT DOES NOT INTERFERE WITH ANY OTHER INSTALLED EQUIPMENT. MAGNETIC DIRECTION INDICATORS WERE CHECKED FOR ACCURACY AND COMPENSATED AS NECESSARY PER AC 43.13-1B, CHAPTER 12, SECTION 3, PARAGRAPH 1237 AND AC 43.13.2A, CHAPTER 2 PARAGRAPH 23f. THE STATIC LOADING OF THE INSTALLED EQUIPMENT MEETS THE REQUIREMENTS OF AC 43.I3-2A, CHAPTER I, PARAGRAPH 3 AND WAS FOUND TO MEET THE REQUIREMENTS OF PARAGRAPH 2. MATERIALS AND PRACTICES COMPLY WITH PARAGRAPHS 4 THROUGH 12. THE ELECTRICAL LOAD ANALYSIS UPDATE REPORT NO. B727-16236-041, REV IR, SHEETS 1'MU 21, DATED 06/11/2001 WAS COMPLETED IN ACCORDANCE WITH AC43.13-18, CHAPTER II, SECTION 3. PARAGRAPH 11.37. . AIRCRAFT METAL WORK INVOLVING METAL REPAIR OR ALTERATION COMPLIES WITH AC43.13-1B, CHAPTER 4, SECTIONS 1, 2, 3 AND 4. CHAPTER 6, SECTIONS 3 AND 8. HARDWARE AND MATERIALS USED IN THE INSTALLATION CONFORM TO AC43.I3-1B, CHAPTER 7. SECTIONS I- 5 AS APPLICABLE. CIRCUIT BREAKERS, SWITCHES AND CONNECTORS ARE OF THE TYPE RECOMMENDED BY THE AIRCRAFT MANUFACTURER OR ARE MIL SPEC APPROVED FOR AIRCRAFT USE AND MEET THE REQUIREMENTS OF AC43.13-IB, CHAPTER 11, SECTION 4. ELECTRICAUELECTRONIC WIRING WAS SELECTED AND INSTALLED TAW AC43.13-1B, CHAPTER 11. SECTIONS 5-8, 13. 15. 17-19 AND AC43.13-2A CHAPTER 2, PARAGRAPHS 21.22 & 27. ROUTING, LACING AND TYING COMPLIES WITH AC43.13-1B, CHAPTER 11. SECTIONS 9-12. WIRE MARKING COMPLIES WITH AC43.13-1B SECTION 16. ELECTRONIC EQUIPMENT INSTALLATION COMPLIES WITH THE AIRCRAFT AND EQUIPMENT MANUFACTURERS INSTRUCTIONS AND AC43.13-2A, CHAPTER 2. PARAGRAPHS 21 THROUGH 26 AND CHAFFER 3, PARAGRAPH 44. A LOGBOOK ENTRY REFLECTING THIS INSTALLATION WAS COMPLETED PER F.A.R. 43.9 AND ENTERED INTO THE AIRCRAFT LOGBOOK. THE EQUIPMENT LIST WAS AMENDED AND THE NEW WEIGHT AND BALANCE WAS COMPUTED AND ENTERED IN THE AIRCRAFT RECORDS TAW AC43.13-1B, CHAPTER IQ SECTION 2 AND AC 43.13-2A, CHAPTER 1 PARAGRAPH 9. PER THE AIRCELL ATG.01 FLIGHT PHONE SYSTEM MANUAL ALL COMPONENTS ARE CONSIDERED LINE REPLACEABLE UNITS AND DO NOT AFFECT THE MANUFACTURERS INSTRUCTIONS FOR CONTINUING AIRWORTHINESS. STRUCTURAL CONTINUING AIRWORTHINESS INSPECTION REQUIREMENTS ARE CONTAINED IN A.T.E. INC. STRUCTURAL REPORT ATEAI 12001 DATED 6/12/01, SUBSTANTIATED BY F.A.A. FORM 8110-3 DATED 6/12/01 BY STRUCTURES DER NO. DERT-510333-CE THERE ARE NO FLIGHT MANUAL SUPPLEMENTS OR COCKPIT PROCEDURAL CHANGES REQUIRED FOR THIS INSTALLATION. END ❑ Addtional Sheets Are Attached * U.S. GPO 1990.761.753 SDNY_GM_02759792 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246714 EFTA01331177
February 18, 2026 at 12:39 AM
epsteinweb.bsky.social
Parts 1-2/2 — EFTA01327374.jpg
#epsteinweb #efta01327374
https://epsteinweb.org
EFTA01326943 | EFTA01327374 NOTICE Weight and balance or operagng limitation changes shalt be entered in the appropriate aircraft record. An alteration must be compatible with allprevious alterations to assure continued conformity with the applicable airworthiness requirements. S. Description of Work Accomplished Ofmere spaceis required, attach additional sheets identify with aircraft netionaRy endregistration mark and date stork completed.) MAKE: RAYTHEON 400A S/N- RK-244 REG. N428HR DATE- 12-T2-99 INSTALLED A SUNDSTRAND MK-VI GROUND PROXIMITY WARNING SYSTEM CONSISTING OF THE FOLLOWING EQUIPMENT: MOD/MFG MIC-VI ADC-500 DESCRIPTION GPWS COMPUTER CONVERTER BRACKET & PLATE WIRING & CONNECTOR P/N 965-0686-020 500-8020 WEIGHT AM 42 2.3 0.5 3.5 33.1 38.2 36.1 54.0 THE SUNDSTRAND MK-VI GPWS SYSTEM WAS INSTALLED IN ACCORDANCE WITH THE STC MSA3322SO ISSUED 09-18-92 AND REISSUED 10-04-95 AND THE HANGER ONE MASTER DRAWING LIST #11892-GPWS, REV. D DATED 03.22.93. THE ELECTRICAL WIRING WAS INSTALLED IN ACCORDANCE WITH THE RAYTHEON AIRCRAFT SERVICES DWG. #RAS-67-9917 REV. IR DATED 11-05-99, REFERENCE THE FORM 8110-3 DATED 11-23-99 APPROVED BY ROBERT M. HURLEY, DESIGNATED ENGINEERING REPRESENTATIVE #DERT-710I 37-SW, SYSTEMS AND EQUIPMENT. A FUNCTIONAL TEST OF THE EQUIPMENT HAS BEEN PERFORMED IN ACCORDANCE WITH FAR 25.1301, FAR 25.1309 AND CHECKED IN ACCORDANCE WITH FAR 25.1431 FOR OPERATING SATISFACTORILY AND DID NOT ADVERSELY AFFECT OTHER COMPONENTS INSTALLED IN THE AIRCRAFT. THE SUNDSTRAND MK-VI GPWS APPROVED FLIGHT MANUAL SUPPLEMENT, REV. B DATED 03-30-93 HAS BEEN INSERTED IN THE SUPPLEMENT SECTION OF THE AIRCRAFT FLIGHT MANUAL AND THE GPWS PILOTS GUIDE P/N 060-4087-000 REV. A DATED 10-96 HAS BEEN INSERTED IN THE AIRCRAFT AS PART OF THE AIRCRAFTS PERMANENT RECORDS. THE AIRCRAFT WEIGHT AND BALANCE FORM AND THE EQUIPMENT LIST WERE REVISED TO REFLECT THIS MODIFICATION AND BOTH FORMS WERE INSERTED IN THE AIRCRAFT FLIGHT MANUAL. Ern Q% Makin! Sheets Are Ma hod * US. GOVERNAGENT PRINTING OFFICE: 1992.769.012160157 SDNY_GM_02755334 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00242256 EFTA01327374
February 17, 2026 at 9:30 PM
epsteinweb.bsky.social
EFTA00012062.jpg
#epsteinweb #efta00012062
https://epsteinweb.org
EFTA00011669 | EFTA00012062 NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatiblewitlzall previous alterations to assure continued conformity with the applicable ainvorthiness requirements. 8 Description'9trork Accomplished (If more spaceis required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) INSTALLED ROCKWELL COLLINS, INC., SUPPLEMENTAL TYPE CERTIFICATE #ST00881WI-D, MODIFICATION OF COLLINS TCAS II SYSTEM INSTALLATION WITH COLLINS TTR-920 CHANGE 6.04a RECEIVER TRANSMITTER TO A COLLINS TCAS II SYSTEM INSTALLATION WITH COLLINS TTR-920 CHANGE 7 TCAS II RECEIVER TRANSMITTER IN ACCORDANCE WITH COLLINS INSTALLATION INSTRUCTIONS AS LISTED ON AML tt ST00881WI-D. AIRCRAFT FLIGHT MANUAL SUPPLEMENT INSERTED INTO AIRCRAFT FLIGHT MANUAL. NO CHANGE TO WEIGHT AND BALANCE. O Additional Sheets Are Attached *U.S.GPO:1994-568-012/CO019 EFTA00012062
February 12, 2026 at 8:36 AM
jimlo-hi.bsky.social
Read "Oncologists Are Begging People To Throw Out This Common Kitchen Item" on SmartNews: l.smartnews.com/p-7QBvF8hG/q...
Oncologists Are Begging People To Throw Out This Common Kitchen Item (Parade)
The wellness spaceis full of promises—"magic cures" and "one-stop shops" for preventing chronic illness. It would be great if any of those claims held up, es...
l.smartnews.com
June 3, 2026 at 11:34 PM
recon24.bsky.social
l.smartnews.com/p-iqrwN84/8d...
William Shatner describes the profound grief he felt when he finally went to space for real (Upworthy)
Statistically speaking, the number of humans who have traveled into spaceis insignificant. But the experience of leaving our home planet and venturing into ...
l.smartnews.com
January 27, 2025 at 3:08 AM
baaia.bsky.social
Loomer on konto alles ja vägagi ründas Elonit (teeb seda siiani). Samas üks isa sai bänni bsky.app/profile/baai... hunnik teisi kontosid ka kadunud, kes Twitter Spaceis "Adrianile" vastu vaidlesid

Siin pole vahet, kas keegi on ära teeninud või ei. Pigem kellest puudust tuntakse ja kellest ei
baaia.bsky.social Baaia @baaia.bsky.social · Dec 28
Ja noh, siis on ka see, kus ta eemaldab inimesi, kes toovad näite tema väitele, et USAs pole piisavalt häid ja motiveeritud insenere. See konto muidu vähemalt eile oli suspended
Screenshot of a tweets where elon says that the number of highly skilled and motivated people in the US ia too low. A father mentioned that his son graduated with honors in electrical and computer engineering, but can't find a job, not even an interview. Many of while males cannot also find it and work on jobs that don't require this education. The discussion around the tweets is about this person getting a lot more likes than Elon's tweet. Screenshot of the account being shown as suspended
December 28, 2024 at 6:46 PM