| LDR | 01248cam a2200313Ia 4500 | ||
| 001 | 011422768 | ||
| 003 | MiAaHDL | ||
| 005 | 20141013010000.0 | ||
| 006 | m d | ||
| 007 | cr bn ---auaua | ||
| 008 | 960911s1987 dcua b f000 0 eng d | ||
| 035 | ⊔ | ⊔ | ‡asdr-uiuc6342017 |
| 035 | ⊔ | ⊔ | ‡a(OCoLC)35519215 |
| 040 | ⊔ | ⊔ | ‡aABC ‡cABC |
| 049 | ⊔ | ⊔ | ‡aUIUU |
| 086 | 0 | ⊔ | ‡aNAS 1.60:2698 |
| 090 | ⊔ | ⊔ | ‡aTL521.3 ‡b.N18 no. 2698 |
| 100 | 1 | ⊔ | ‡aOswald, Fred B. |
| 245 | 1 | 0 | ‡aGear tooth stress measurements on the UH-60A helicopter transmission / ‡cFred B. Oswald. |
| 260 | ⊔ | ⊔ | ‡aWashington, D.C. : ‡bNational Aeronautics and Space Administration, Scientific and Technical Information Branch ; ‡aSpringfield, Va. : ‡bFor sale by the National Technical Information Service, ‡c1987. |
| 300 | ⊔ | ⊔ | ‡a13 p. : ‡bill. ; ‡c28 cm. |
| 490 | ⊔ | 0 | ‡aNASA technical paper ; ‡v2698 |
| 500 | ⊔ | ⊔ | ‡aPrepared at Lewis Research Center. |
| 500 | ⊔ | ⊔ | ‡a"March 1987"--Cover. |
| 504 | ⊔ | ⊔ | ‡aIncludes bibliographical references (p. 5). |
| 538 | ⊔ | ⊔ | ‡aMode of access: Internet. |
| 650 | ⊔ | 0 | ‡aBlack Hawk (Military transport helicopter) |
| 650 | ⊔ | 0 | ‡aHelicopters ‡xTransmission devices. |
| 650 | ⊔ | 0 | ‡aStrains and stresses ‡xMeasurement. |
| 650 | ⊔ | 0 | ‡aGearing, Planetary ‡xTesting. |
| 650 | ⊔ | 0 | ‡aGearing, Spiral ‡xTesting. |
| 710 | 2 | ⊔ | ‡aLewis Research Center. |
| CID | ⊔ | ⊔ | ‡a011422768 |
| DAT | 0 | ⊔ | ‡a20100927151808.0 ‡b20141013010000.0 |
| DAT | 1 | ⊔ | ‡a20141112173021.0 ‡b2023-03-14T18:19:21Z |
| CAT | ⊔ | ⊔ | ‡aSDR-UIUC ‡dUNKNOWN ‡lloader.pl-003-020 |
| FMT | ⊔ | ⊔ | ‡aBK |
| HOL | ⊔ | ⊔ | ‡0sdr-uiuc6342017 ‡auiug ‡bSDR ‡cUIUC ‡puiug.30112106605634 ‡sUIU ‡16342017 |
| 974 | ⊔ | ⊔ | ‡bUIU ‡cUIUC ‡d20230314 ‡sgoogle ‡uuiug.30112106605634 ‡y1987 ‡rpd ‡qbib ‡tUS fed doc--NTIS: pubdate < 2018 |