# N247US: Boeing 737-201, registration cancelled 2006-04-25 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: April 25, 2006 - Exported to: Lebanon - Status when cancelled: Valid registration - Airframe: [Boeing 737-201](https://openairdocs.org/model/boeing-737-201) (registry code 1384454) - Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (OpenAirDocs) - Serial number: 22754 - Type of aircraft: Fixed wing multi engine - Certificate issued: November 23, 2005 - Last registry action: April 19, 2006 - Mode S code: A24BD3 - Owner when cancelled: [Hamilton Aerospace Technologies Inc](https://openairdocs.org/faa-owner/HAMILTON%20AEROSPACE%20TECHNOLOGIES%20INC) - Location: [Tucson, AZ](https://openairdocs.org/faa-place/AZ/Tucson) - Owner type: Corporation - Owner's area on the map: 32.1478° N, 110.9354° W: Placed by OpenAirDocs at the center of ZIP code 85706, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N247US - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=247US - Page: https://openairdocs.org/deregistered/N247US-2006-04-25 From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Boeing 737-201: https://openairdocs.org/model/boeing-737-201.md ## Service difficulty reports (86, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR USAA010573](https://openairdocs.org/sdr/USAA010573), May 20, 2001: KEEL. CORRODED. CLT - FOUND KEEL CHORD OUTBOARD FLANGE WITH 3 INCH AREA OF CORROSION, BS 727A, RBL 7, BELLY AREA. REMOVED DAMAGE, INSTALLED SPLICE REPAIR PER TR 53-10-24, EA 69 - [SDR USAA010556](https://openairdocs.org/sdr/USAA010556), May 18, 2001: SHEAR TIE. CORRODED. CLT - FOUND FRAME SHEAR TIE CORRODED 5 INCHES BY 1 INCH, BS 986 STRINGER 24R/25R. FABRICATED AND REPLACED SHEAR TIE PER BAC DRAWING 65-46564, SRM 51-10-0 AND 51 - [SDR USAA010557](https://openairdocs.org/sdr/USAA010557), May 18, 2001: WEB. CRACKED. CLT - FOUND WEB CRACKED 1 INCH, BS 712, LBL 24. INSTALLED REPAIR DOUBLER, REPLACEMENT WEB AND 4 VERTICAL STIFFENERS PER EA 69504. (M) - [SDR USAA010558](https://openairdocs.org/sdr/USAA010558), May 18, 2001: FLOORBEAM. CRACKED. CLT - FOUND FLOORBEAM T-CAP CRACKED, BS 520, RBL 25, WL 208. INSTALLED DOUBLER AND PIVOT LINK ASSY PER SB 737-53-1120 AND EA 69537. (M) - [SDR USAA010559](https://openairdocs.org/sdr/USAA010559), May 18, 2001: FRAME. CRACKED. CLT - FOUND CHORD CRACKED 1 INCH, BS 663, LBL 24, WL 203. INSTALLED REPAIR CHORD PER EA 69538 AND SB 737-53-1184. (M) - [SDR USAA010560](https://openairdocs.org/sdr/USAA010560), May 18, 2001: WEB. CRACKED. CLT - FOUND PRESSURE BULKHEAD WEB WITH CRACKS .125 INCH TO 1 INCH, BS 178, LBL 12 TO RBL 17, WL 188 TO WL 214. DAMAGED REMOVED, INSTALLED REPAIR DOUBLER PER EO - [SDR USAA010561](https://openairdocs.org/sdr/USAA010561), May 18, 2001: FRAME. CRACKED. CLT - FOUND VERTICAL CHORD CRACKED 1.3 INCHES, BS 178, LBL 6, WL 198. INSTALLED REPAIR KIT PER EO 5300V155. (M) - [SDR USAA010562](https://openairdocs.org/sdr/USAA010562), May 18, 2001: ATTACH FITTING. CORRODED. CLT - FOUND FUSELAGE ATTACH LUGS CORRODED 3 SQUARE INCHES, VERT FIN, AFT OUTBOARD LEFT AND AFT OUTBOARD RIGHT ATTACH POINTS. CORROSION REMOVED AND LUGS REWORKED - [SDR USAA010563](https://openairdocs.org/sdr/USAA010563), May 18, 2001: BEAM. CRACKED. CLT - FOUND BEAM CRACKED 3 INCHES, BS 663, BL 0. INSTALLED REPAIR ANGLES PER EA 69611. (M) - [SDR USAA010564](https://openairdocs.org/sdr/USAA010564), May 18, 2001: SKIN. CRACKED. CLT - FOUND SKIN CRACKED .25 INCH, BS 345, AFT LOWER CORNER OF AIRSTAIR CUTOUT. REMOVED AND REPLACED REPAIR TRIPLER PER EA 69582. (M) - [SDR USAA010565](https://openairdocs.org/sdr/USAA010565), May 18, 2001: SKIN. CRACKED. CLT - FOUND FUSELAGE SKIN CRACKED .25 INCH AFT ENTRY DOOR, UPPER HINGE CUTOUT. INSTALLED DOUBLER PER SRM 543-30-3, FIG 21A. (M) - [SDR USAA010566](https://openairdocs.org/sdr/USAA010566), May 18, 2001: SKIN. CORRODED. CLT - FOUND FUSELAGE SKIN CORRODED, BS 468, BL 0. REMOVED DAMAGE, INSTALLED REPAIR DOUBLER PER SRM 51-20-4 AND 53-30-3. (M) - [SDR USAA010552](https://openairdocs.org/sdr/USAA010552), May 18, 2001: FRAME. CRACKED. CLT - FOUND FRAME CRACKED .25 INCH, BS 639, STRINGER 17R. INSTALLED REPAIR DOUBLER PER SRM 51-40-2, FIG 1. (M) - [SDR USAA010553](https://openairdocs.org/sdr/USAA010553), May 18, 2001: FRAME. CRACKED. CLT - FOUND FRAME CRACKED .375 INCH, LATERALLY THROUGH EDGE OF FRAME BS 440, LBL 21. INSTALLED FORMED FRAME REPAIR DOUBLER PER SRM 51-40-3, FIG 1. (M) - [SDR USAA010555](https://openairdocs.org/sdr/USAA010555), May 18, 2001: DOUBLER. CRACKED. CLT - FOUND DOUBLER CRACKED 2 INCHES, BS 676, BETWEEN LBL 24 AND RBL 24, WL 206. INSTALLED RE-INFORCEMENT CHANNELS PER EO 5791G632. (M) - [SDR USAA010525](https://openairdocs.org/sdr/USAA010525), May 10, 2001: SKIN. CRACKED. CLT - FOUND FUSELAGE SKIN WITH TWO CRACKS 1 INCH EACH, BS 727 PLUS 1 INCH AT STRINGER 17R AND BS 727A PLUS 6 INCHES AT STRINGER 19R. INSTALLED REPAIR DOUBLER. ( - [SDR USAA010524](https://openairdocs.org/sdr/USAA010524), May 10, 2001: FRAME. CRACKED. CLT - FOUND FRAME CRACKED 1.125 INCH, BS 277, STRINGER 16L. REMOVED DAMAGE, INSTALLED REPAIR FILLER AND DOUBLER PER SRM 51-40-2, FIG 1. (M) - [SDR USAA010523](https://openairdocs.org/sdr/USAA010523), May 10, 2001: FRAME. CRACKED. CLT - FOUND FRAME CRACKED .25 INCH, BS 480 STRINGER 21L. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 51-40-3, FIG 1. (M) - [SDR USAA010522](https://openairdocs.org/sdr/USAA010522), May 10, 2001: ANGLE. CRACKED. CLT - FOUND SUPPORT ANGLE CRACKED 1.5 INCH, BS 727, LBL 27, WHEEL WELL COMPRESSION CHORD. INSTALLED REPAIR STRAPS AND DOUBLER ANGLE PER BOEING DRAWING NR 691A00 - [SDR USAA010521](https://openairdocs.org/sdr/USAA010521), May 10, 2001: STRINGER. CRACKED. CLT - FOUND STRINGER CRACKED .070 INCH, BS 380, STRINGER 2L. REMOVED DAMAGE SECTION, SPLICED IN NEW STRINGER SECTION PER SRM 53-10-3. (M) - [SDR USAA010518](https://openairdocs.org/sdr/USAA010518), May 8, 2001: WEB. CRACKED. CLT - FOUND FLOOR STRUCTURE WEB CRACKED 1 INCH, BS 178, WL 207 AT LBL 24. REMOVED AND REPLACED WEB PER EO 5300V157. (M) - [SDR USAA010520](https://openairdocs.org/sdr/USAA010520), May 8, 2001: PRESSURE PANEL. DAMAGED. CLT - FOUND UNBEADED PRESSURE WEB APPROX 3 SQUARE FEET, BS 666 WL 55. REINFORCING ANGLES INSTALLED PER SB 737-57-1234 AND EA 69561. (M) - [SDR USAA010519](https://openairdocs.org/sdr/USAA010519), May 8, 2001: FRAME. CRACKED. CLT - FOUND SIDE CHORD CRACKED .25 INCH, BS 178, WL 195 LEFT SIDE CHORD. DAMAGE REMOVED, SPLICED IN NEW CHORD SECTION PER EO 5300V157. (M) - [SDR USAA010497](https://openairdocs.org/sdr/USAA010497), Apr 29, 2001: SKIN. CORRODED. CLT - FOUND FUSELAGE SKIN CORRODED 2 INCH BY 3 INCH AREA, BS 468 BL 0. DAMAGED AREA CUTOUT, REPAIR DOUBLER INSTALLED PER SRM 53-30-3. (M) - [SDR USAA010496](https://openairdocs.org/sdr/USAA010496), Apr 29, 2001: STRINGER. CORRODED. CLT - FOUND STRINGER CORRODED 1 INCH BY 10 INCH AREA, BS 1006 TO 1016, S24R. REMOVED DAMAGE, FABRICATED NEW SECTION AND INSTALLED PER SRM 53-10-2. (M) - [SDR USAA010493](https://openairdocs.org/sdr/USAA010493), Apr 29, 2001: FLOORBEAM. CORRODED. CLT - FOUND FLOORBEAM T-CAP CORRODED .125 INCH, BS 967, RBL 42. DAMAGE REMOVED, SPLICED IN T-CAP REPLACEMENT PER SRM 53-10-9. (M) - [SDR USAA010491](https://openairdocs.org/sdr/USAA010491), Apr 29, 2001: FLOORBEAM. CORRODED. CLT - FOUND FLOORBEAM T-CAP CORRODED APPROX 13 SQUARE INCHES, BS 986.5, LBL 45 TO RBL 45. REMOVED AND REPLACED T-CAP PER TYPICAL REPAIR 53-60-01 REV ''A''. (M) - [SDR USAA010475](https://openairdocs.org/sdr/USAA010475), Apr 29, 2001: ANGLE. CORRODED. CLT - FOUND AFT SERVICE DOOR Z-ANGLE CORRODED 40 INCHES BY .5 INCH, BS 947 TO 987, LBL 50. REMOVED AND REPLACED Z-ANGLE PER SRM 51-10-01. (M) - [SDR USAA010474](https://openairdocs.org/sdr/USAA010474), Apr 29, 2001: FLOORBEAM. CORRODED. CLT - FOUND FLOORBEAM T-CAP CORRODED 1 INCH BY .5 INCH AREA, BS 312, BL 0. DAMAGE REMOVED, SPLICED IN REPAIR ANGLES AND T-CAP SECTION PER TYPICAL REPAIR 53-10-1 - [SDR USAA010473](https://openairdocs.org/sdr/USAA010473), Apr 29, 2001: FLOORBEAM. CORRODED. CLT - FOUND FLOORBEAM CORRODED 2 INCHES BY 3 INCHES, BS 1006, LBL 10. DAMAGE REMOVED, INSTALLED FILLER AND REPAIR ANGLES PER SRM 53-10-9 FIG 2. (M) - [SDR USAA010503](https://openairdocs.org/sdr/USAA010503), Apr 29, 2001: TIE CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED .125 INCH, BS 597, STRINGER 4R. INSTALLED NEW TIE CLIP PER EO 5393G227. (M) - [SDR USAA010502](https://openairdocs.org/sdr/USAA010502), Apr 29, 2001: TIE CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED .125 INCH, BS 597, S5R. INSTALLED NEW TIE CLIP PER SRM 51-30-2. (M) - [SDR USAA010501](https://openairdocs.org/sdr/USAA010501), Apr 29, 2001: TIE CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED .5 INCH, BS 344 S11R. FABRICATED AND INSTALLED NEW TIE CLIP PER BOEING DRAWING NR 69-38939 AND SRM 51-30-2. (M) - [SDR USAA010500](https://openairdocs.org/sdr/USAA010500), Apr 29, 2001: TIE CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED .25 INCH, BS 706, S11R. FABRICATED NEW CLIP AND INSTALLED PER BLUEPRINT NR 69-45156 AND SRM 51-30-2. (M) - [SDR USAA010499](https://openairdocs.org/sdr/USAA010499), Apr 29, 2001: TIE CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED .125 INCH, BS 663, S10R. REMOVED AND REPLACED TIE CLIP PER EO 5393G227. (M) - [SDR USAA010498](https://openairdocs.org/sdr/USAA010498), Apr 29, 2001: BULKHEAD. CRACKED. CLT - FOUND BULKHEAD CRACKED 1 INCH, BS 178, WL 234, RBL 11. INSTALLED DOUBLER AND FILLER PER SRM 53-10-11 FIG 1. (M) - [SDR USAA010495](https://openairdocs.org/sdr/USAA010495), Apr 29, 2001: HINGE FITTING. CRACKED. CLT - FOUND HINGE CASTING CRACKED .5 INCH, RT AILERON, NR 2 HINGE SUPPORT CASTING, LOWER OUTBOARD PANEL. REMOVED AND REPLACED CASTING PER BOEING DRAWING NR 65-6 - [SDR USAA010494](https://openairdocs.org/sdr/USAA010494), Apr 29, 2001: ANGLE. CRACKED. CLT - FOUND VERTICAL TIE ANGLE CRACKED .75 INCH AND 1 INCH, BS 360, BETWEEN S14L AND S15L. REMOVED DAMAGED ANGLE, FABRICATED AND INSTALLED NEW ANGLE PER SRM 51- - [SDR USAA010492](https://openairdocs.org/sdr/USAA010492), Apr 29, 2001: TIE CLIP. CRACKED. CLT - FOUND TIE CLIP CRACKED .25 INCH, BS 360, S4L. REMOVED AND REPLACED STRINGER TIE CLIP PER SRM 51-30-2. (M) - [SDR USAA010490](https://openairdocs.org/sdr/USAA010490), Apr 29, 2001: STRINGER. CRACKED. CLT - FOUND STRINGER CRACKED 1 INCH, BS 787, S16R. INSTALLED STRINGER SPLICE REPAIR PER SRM 53-30-3, 53-10-2. (M) - [SDR USAA010489](https://openairdocs.org/sdr/USAA010489), Apr 29, 2001: INTERCOSTAL. CRACKED. CLT - FOUND INTERCOSTAL CRACKED 1 INCH, BS 178, WL 195, RBL 24. REMOVED AND REPLACED INTERCOSTAL PER EO 5300V155. (M) - [SDR USAA010488](https://openairdocs.org/sdr/USAA010488), Apr 29, 2001: STRINGER. CRACKED. CLT - FOUND STRINGER CRACKED .5 INCH, BS 360, S15L. REMOVED AND REPLACED STRINGER SECTION PER RM 51-10-1. (M) - [SDR USAA010487](https://openairdocs.org/sdr/USAA010487), Apr 29, 2001: SKIN. CRACKED. CLT - FOUND FUSELAGE SKIN CRACKED 1.7 INCH, RIGHT AFT GALLEY SERVICE DOOR CUTOUT, FORWARD LOW CORNER. DAMAGE CUTOUT, INSTALLED FILLER AND REPAIR DOUBLER, TEXAS - [SDR USAA010486](https://openairdocs.org/sdr/USAA010486), Apr 29, 2001: STRINGER. CRACKED. CLT - FOUND STRINGER CRACKED .5 INCH, BS 358, S7L. FABRICATED WEB CLIP, REPLACED STRINGER AND TIE CLIP PER SRM 51-10-1 AND 51-30-0. (M) - [SDR USAA010485](https://openairdocs.org/sdr/USAA010485), Apr 29, 2001: CREASE BEAM. CRACKED. CLT - FOUND CREASE BEAM WEB CRACKED .25 INCH, BS 637, RBL 70. REMOVED AND REPLACED WEB PER SRM 51-10-1. (M) - [SDR USAA010484](https://openairdocs.org/sdr/USAA010484), Apr 29, 2001: STRINGER. CRACKED. CLT - FOUND SHELF CRACKED .5 INCH, BS 727, S18A RIGHT, INBOARD FASTENER. REMOVED AND REPLACED SHELF PEER EA 69507 AND BAC DRAWING NR 65-46877-76. (M) - [SDR USAA010483](https://openairdocs.org/sdr/USAA010483), Apr 29, 2001: WEB. CRACKED. CLT - FOUND WEB CRACKED .5 INCH, BS 639, 2.75 INCH INBOARD OF S16L. REMOVED DAMAGED WEB SECTION, INSTALLED NEW WEB DOUBLER AND FILLER PER SRM 51-40-02, FIG 1. ( - [SDR USAA010482](https://openairdocs.org/sdr/USAA010482), Apr 29, 2001: FRAME. CRACKED. CLT - FOUND FRAME CHORD ANGLE .25 INCH, BS 639, 2.75 INCH INBOARD OF STRINGER 16L. REMOVED AND REPLACED INNER CHORD ANGLE PER SRM 51-10-1. (M) - [SDR USAA010481](https://openairdocs.org/sdr/USAA010481), Apr 29, 2001: FRAME. CRACKED. CLT - FOUND FRAME CRACKED .25 INCH, BS 639, S17R. INSTALLED REPAIR DOUBLER PER SRM 51-40-2 FIG 1 AND SRM 51-30-00. (M) - [SDR USAA010480](https://openairdocs.org/sdr/USAA010480), Apr 29, 2001: CREASE BEAM. CRACKED. CLT - FOUND CREASE BEAM WEB CRACKED .25 INCH, BS 616-639, S17R. REMOVED AND REPLACED WEB PER SRM 51-30-10. (M) All 86: https://openairdocs.org/deregistered/N247US-2006-04-25/reports.md ## FAA accident and incident reports (2) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 19910827041549I](https://openairdocs.org/incident/19910827041549I), Aug 27, 1991: Boeing 737201 (N247US), Indianapolis, IN. In flight engine shut down. Diverted to Indianapolis. NR2 compressor section had seized. - [Incident 19890112007069I](https://openairdocs.org/incident/19890112007069I), Jan 12, 1989: Boeing 737201 (N247US), Buffalo, NY, Minor damage. System a hydraulic quantity dropped on takeoff. Continued to Buffalo. Had a crushed hydraulic supply line. --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.