# N675UP: 1971 Boeing 747-123, registration cancelled 2010-07-19

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: July 19, 2010
- Status when cancelled: Valid registration (trainee)
- Airframe: [Boeing 747-123](https://openairdocs.org/model/boeing-747-123) (registry code 1384873)
- Data sheets: [TCDS A20WE](https://openairdocs.org/tcds/A20WE) (OpenAirDocs)
- Serial number: 20390
- Year built: 1971
- Type of aircraft: Fixed wing multi engine
- Airworthiness: Standard, transport
- Airworthiness date: January 7, 1977
- Last registry action: July 19, 2010
- Mode S code: A8F01B
- Owner when cancelled: [Stewart Industries International LLC](https://openairdocs.org/faa-owner/STEWART%20INDUSTRIES%20INTERNATIONAL%20LLC)
- Location: [Guthrie, OK](https://openairdocs.org/faa-place/OK/Guthrie)
- Owner type: Corporation
- Owner's area on the map: 35.8679° N, 97.4344° W: Placed by OpenAirDocs at the center of ZIP code 73044, within about 9 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N675UP
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=675UP
- Page: https://openairdocs.org/deregistered/N675UP-2010-07-19

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 747-123: https://openairdocs.org/model/boeing-747-123.md

## Service difficulty reports (387, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR UPS05445843](https://openairdocs.org/sdr/UPS05445843), Nov 27, 2005: BATTERY. DISCHARGED. EMERGENCY LIGHT OVER THE FLT DECK STAIRS INOP (LOW BATTERY). REMOVED AND REPLACED EMERGENCY LIGHT ASSY IAW MM 33-51-00, OPS NORMAL.
- [SDR UPS05444912](https://openairdocs.org/sdr/UPS05444912), Jul 17, 2005: INDICATION SYS. MALFUNCTIONED. NR 3 ENG N2 REACH 112 PERCENT DURING DEPARTURE. THRUST REVERSE LEVERS IDLE AND N2 WAS 10 PERCENT OR HIGHER THAN OTHER ENGS. NR 3 ENG SHUTDOWN AND RETURNED TO FI
- [SDR UPS05444888](https://openairdocs.org/sdr/UPS05444888), Jul 12, 2005: WEB. CRACKED. NLG RT SIDE WEB FOUND CRACKED AT STA 300 WL 150. CRACK LENGTH 0.25 IN. NLG W/W RHS SIDE WEB REPAIRED AT BS 300 WL 150 AREA AS PER SRM 53-10-04 FIG 116.
- [SDR UPS05444468](https://openairdocs.org/sdr/UPS05444468), May 15, 2005: FLOORBEAM. DAMAGED. FLOORBEAM AT STA 1800 HAS ELONGATED HOLES. A/C OOS AND WILL REQUIRE MX FERRY (9127) TO SAT. INSTALLED FREEZE PLUG AT STA 1800 LBL 99 IN FLOORBEAM IAW SA SK 675-
- [SDR UPS05444027](https://openairdocs.org/sdr/UPS05444027), Mar 4, 2005: CONTROL MODULE. INTERMITTENT. INSPECTION TYPE:N/A EMERGENCY LIGHT CONTROL SWITCH INTERMITTENT FOR EMERGENCY LIGHTS. REMOVED AND REPLACED EMERGENCY LIGHTS CONTROL MODULE AS PER MM 33-51-09, O
- [SDR UPS05443829](https://openairdocs.org/sdr/UPS05443829), Jan 13, 2005: STRINGER. CRACKED. BS 1560 - 1580 AFT RHS WINDOW FORGING REMOVED FOUND STRINGER CORROSION CRACKED. CORROSION BLEND OUT 0.040" BY 1" BY 5" EXCEED SRM LIMIT. NEW STRINGER SEGMENT AN
- [SDR UPS05443828](https://openairdocs.org/sdr/UPS05443828), Jan 13, 2005: STRINGER. CORRODED. BS 980 - 1000 AFTER LT WINDOW FORGING REMOVED FOUND STR CORROSION CRACKED. CORROSION BLEND OUT 0.060" BY 1" BY 3" EXCEED SRM LIMIT. NEW STRINGER SEGMENT AND SPL
- [SDR UPS05443827](https://openairdocs.org/sdr/UPS05443827), Jan 13, 2005: STRINGER. CORRODED. BS 1560 TO 1580 AFT LT WINDOW FORGING REMOVED FOUND STR CORROSION. CORROSION BLEND OUT 0.040 INCH BY 1" BY 5" EXCEED SRM LIMIT. NEW STRINGER SEGMENT AND SPLICE 
- [SDR UPS05443826](https://openairdocs.org/sdr/UPS05443826), Jan 13, 2005: STRINGER. CRACKED. BS 1438 TO 1460 AFT RT WINDOW FORGING REMOVED FOUND STR CORROSION CRACKED. CORROSION BLEND OUT 0.100" BY 1" BY 5" EXCEED SRM LIMIT. NEW STRINGER SEGMENT, REPAIR
- [SDR UPS05443825](https://openairdocs.org/sdr/UPS05443825), Jan 13, 2005: STRINGER. CRACKED. BS 1220 TO 1240 AFT RT WINDOW FORGING REMOVED FOUND STR CORROSION CRACKED. CORROSION BLEND OUT 0.080" BY 1" BY 5" EXCEED SRM LIMIT. NEW STRINGER SEGMENT, SPLICE
- [SDR UPS05443815](https://openairdocs.org/sdr/UPS05443815), Jan 13, 2005: STRINGER. CRACKED. BS 1020 TO 1040 AFT RT WINDOW FORGING REMOVED FOUND STR CORROSION CRACKED. CORROSION BLEND OUT 0.100 BY 1 BY 10 INCHES EXCEED SRM LIMIT. ALL REPAIR PARTS AND NE
- [SDR UPS05443814](https://openairdocs.org/sdr/UPS05443814), Jan 13, 2005: STRINGER. CORRODED. BS 1080 TO BS 1100 AFT RT WINDOW FORGING REMOVED FOUND STR CORROSION CRACKED. CORROSION BLEND OUT 0.100" BY 1" BY 5" EXCEED SRM LIMIT. ALL REPAIR PARTS AND NEW 
- [SDR UPS05443804](https://openairdocs.org/sdr/UPS05443804), Jan 13, 2005: STRINGER. CORRODED. INSPECTION TYPE:C M/D BS 1580 TO BS 1600 AFT RT WINDOW FORGING REMOVED FOUND STRINGER CORROSION CRACKED. CORROSION BLEND OUT 0.100 X 1 X 10 EXCEED SRM LIMIT. ST
- [SDR UPS05443803](https://openairdocs.org/sdr/UPS05443803), Jan 13, 2005: STRINGER. CORRODED. INSPECTION TYPE:C BS 1560 TO BS 1580 AFT RT WINDOW FORGING REMOVED FOUND STRINGER CORROSION CRACKED. CORROSION BLEND OUT 0.060 X 1 X 7 INCH, EXCEED SRM LIMIT. F
- [SDR UPS05443717](https://openairdocs.org/sdr/UPS05443717), Jan 12, 2005: SKIN. CORRODED. INSPECTION TYPE:C, CORROSION INDICATOR REVEALED ON FUSELAGE UPPER SKIN AT BS 1820 TO BS 1825 STR 46L. CORROSION BLEND OUT 0.035 X 2 X 2 INCHES EXCEED SRM LIMIT.
- [SDR UPS05443695](https://openairdocs.org/sdr/UPS05443695), Jan 11, 2005: FITTING. CRACKED. INSPECTION TYPE:C RT WING BS 1241 UPPER REAR SPAR SIDE-TO-BODY KICK FITTING AREA FOUND CRACK AT TERMINAL FITTING NR 2 HOLE. HOLE REPAIRED AS PER SB 747-57A2314.
- [SDR UPS05443819](https://openairdocs.org/sdr/UPS05443819), Jan 10, 2005: FRAME. CRACKED. BS 940, S25L FRAME I/B CHORD FOUND CRACK. M/D BS 940 FRAME AT S-25L, FRAME REPAIRED PER RS R-53-22-35244 AND EO B747-5310-21670-A.
- [SDR UPS05443833](https://openairdocs.org/sdr/UPS05443833), Jan 9, 2005: FLOOR PANEL. CORRODED. STA 1020 TO 1110, BTN L11" AND R11" FLR METAL PNL SKIN FOUND CORROSION. FLOOR PANEL REPAIRED AS PER RS R53-20-35251 AND EO B747-5320-21675-A AND THIS METAL PANE
- [SDR UPS05443832](https://openairdocs.org/sdr/UPS05443832), Jan 9, 2005: FLOOR PANEL. CORRODED. STA 1170 TO 1250, BTN L11 AND R11 FLR METAL PNL SKIN FOUND CORR. METAL FLOOR PANEL REPAIRED AS PER RS R53-20-35251 AND EO B747-5320- 21675-A AND THIS METAL PANE
- [SDR UPS05443802](https://openairdocs.org/sdr/UPS05443802), Jan 9, 2005: SEAT TRACK. CORRODED. INSPECTION TYPE:C M/D - BS 1180 RBL 97 I/B SEAT TRACK SUPPORT FOUND CORRODED. CORROSION BLEND OUT 0.050 X 1 X 1 INCH, EXCEED SRM LIMIT. SEAT TRACK REPAIR PARTS 
- [SDR UPS05443801](https://openairdocs.org/sdr/UPS05443801), Jan 9, 2005: SEAT TRACK. CORRODED. INSPECTION TYPE:C - BS 1160 - 1220 RBL 97 SEAT TRACK I/B FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.050 X 1 X 2 INCH. SEAT TRACK CUT OFF AT BS 1070 RBL 98 AS 
- [SDR UPS05443772](https://openairdocs.org/sdr/UPS05443772), Jan 9, 2005: WEB. CRACKED. INSPECTION TYPE:C - R3 DOOR LOWER WEB CRACKED AT LOWER GATE PUSH ROD CUTOUT. LOWER WEB REPAIRED AS PER SRM 51-40-02 FIG 1.
- [SDR UPS05443667](https://openairdocs.org/sdr/UPS05443667), Jan 9, 2005: SEAT TRACK. CORRODED. INSPECTION TYPE:C - BS 1000 LBL 33 O/B SEAT TRACK FLANGE CORRODED. M/D BS 990 - 1000 LBL 33 SEAT TRACK REPAIR PARTS FABRICATED AS PER SRM 53-10-05 FIG 1A. CORRO
- [SDR UPS05443659](https://openairdocs.org/sdr/UPS05443659), Jan 9, 2005: FLOORBEAM. CORRODED. INSPECTION TYPE:C - FLOORBEAM BS 340 LBL 11 - 39 UPPER CHORD CORRODED. REPAIR PARTS FABRICATED AS PER SRM 53-10-07 FIG 23. CORROSION BLEND OUT 0.050 X 2 X 2 INC
- [SDR UPS05443654](https://openairdocs.org/sdr/UPS05443654), Jan 9, 2005: SEAT TRACK. CORRODED. INSPECTION TYPE:C - BS 520 - 540 LBL 46 SEAT TRACK CORRODED AS MARKED. U/D BS 520 - 560 LBL 46 SEAT TRACK REPAIR PARTS FABRICATED AS PER SRM 53-10-05 FIG 6. COR
- [SDR UPS05443653](https://openairdocs.org/sdr/UPS05443653), Jan 9, 2005: SEAT TRACK. CORRODED. INSPECTION TYPE:C U/D - BS 480 LBL 46 SEAT TRACK CORRODED AS MARKED. U/D BS 480 - 500 LBL 46 SEAT TRACK REPAIR PARTS FABRICATED AS PER SRM 53-10-05 FIG 6. CORRO
- [SDR UPS05443650](https://openairdocs.org/sdr/UPS05443650), Jan 9, 2005: SEAT TRACK. CORRODED. BS 480 - 500 RBL 66 SEAT TRACK CORRODED AS MARKED. SEAT TRACK PART FABRICATED AS PER SRM 51-10-01 PG 9. CORROSION BLEND OUT 0.050 X 2 X 2 INCHES EXCEED SRM LIMI
- [SDR UPS05443812](https://openairdocs.org/sdr/UPS05443812), Jan 8, 2005: STRINGER. CRACKED. BS 1482 - 1485, STR 13R, STRINGER END FOUND CRACK. STRINGER REPAIRED PER RS 53-41-35250 AND ENGINEERING FILE NUMBER 747-53-20214.
- [SDR UPS05443808](https://openairdocs.org/sdr/UPS05443808), Jan 8, 2005: STRINGER. CRACKED. BS 1480 - 1485, S6L, STRINGER END FOUND CRACKED. STRINGER REPAIRED PER RS R53-41-35249 AND ENGINEERING FILE NUMBER 747-53-20215.
- [SDR UPS05443773](https://openairdocs.org/sdr/UPS05443773), Jan 8, 2005: STRINGER. CRACKED. INSPECTION TYPE:C - BS 736 - 738, S23R STRINGER END FOUND CRACK. M/D BS 736 TO BS 738 S-23R STRINGER END REPAIRED AS PER RS 53-61-35230 AND ENGINEERING FILE NUM
- [SDR UPS05443730](https://openairdocs.org/sdr/UPS05443730), Jan 8, 2005: STIFFENER. CRACKED. INSPECTION TYPE:C - BS 1080 RBL 99 BELOW FLOOR STIFFENER FOUND CRACKED. M/D BS 1080 RBL 99 BELOW FLOOR STIFFENER REPLACED IAW SRM 51-10-01 PAGE 9.
- [SDR UPS05443726](https://openairdocs.org/sdr/UPS05443726), Jan 8, 2005: INTERCOSTAL. CRACKED. INSPECTION TYPE:C M/D - BS 1220 RBL 118 BELOW FLOOR INTERCOSTAL WEB FOUND CRACKED. WEB REPAIR PER SRM 51-40-02 FIG 1.
- [SDR UPS05443720](https://openairdocs.org/sdr/UPS05443720), Jan 8, 2005: STRINGER. CRACKED. INSPECTION TYPE:C M/D - STR END BS 739 S-8L CRACKED. CRACKED STRINGER REPAIRED PER RS 53-21-35238 AND ENGINEERING FILE NUMBER 747-53-20206.
- [SDR UPS05443716](https://openairdocs.org/sdr/UPS05443716), Jan 8, 2005: FRAME. CRACKED. INSPECTION TYPE:C - BS 960, S8R, FRAME FOUND CRACK. FRAME REPAIRED PER SRM 53-10-04 FIG 54.
- [SDR UPS05443714](https://openairdocs.org/sdr/UPS05443714), Jan 8, 2005: FRAME. CRACKED. INSPECTION TYPE:C - FRAME BS 760 STR CUTOUT CRACKED AT S-6L AND S-7L. M/D BS 760 BETWEEN STR 6L AND STR 7L FRAME REPAIR CARRIED OUT IAW SRM 53-10-04 FIG 54.
- [SDR UPS05443712](https://openairdocs.org/sdr/UPS05443712), Jan 8, 2005: FRAME. CRACKED. INSPECTION TYPE:C - BS 740, BETWEEN S7 - 8R, FRAME FOUND CRACK. M/D BS 740 BETWEEN STR 7R AND STR 8R FRAME REPAIR CARRIED OUT IAW SRM 53-10-04 FIG 54.
- [SDR UPS05443711](https://openairdocs.org/sdr/UPS05443711), Jan 8, 2005: FRAME. CRACKED. INSPECTION TYPE:C - BS 760, BETWEEN STR 5 - 8R, FRAME FOUND CRACK. M/D BS 760 BETWEEN STR 5R AND STR 8R FRAME REPAIR CARRIED OUT IAW SRM 53-10-04 FIG 54.
- [SDR UPS05443678](https://openairdocs.org/sdr/UPS05443678), Jan 8, 2005: SPAR. CRACKED. INSPECTION TYPE:C, RIGHT WING UPPER REAR SPAR SIDE-OF-BODY SPLICE PLATE FITTING CRACK FOUND AT HOLE NR 5 RUNNING FWD APPROX 0.060 INCH AND AFT APPROX .125 INCH.
- [SDR UPS05443676](https://openairdocs.org/sdr/UPS05443676), Jan 8, 2005: SPLICE. CRACKED. INSPECTION TYPE: C, RIGHT WING STA 1241 UPPER REAR SPAR SIDE - OF - BODY SPLICE PLATE AREA FOUND HOLE NR 3 CRACKED AT WING UPPER SKIN AND INTERNAL SPLICE FITTIN
- [SDR UPS05443666](https://openairdocs.org/sdr/UPS05443666), Jan 8, 2005: STRINGER. CRACKED. INSPECTION TYPE:C - STRINGER END BS 990 S-7L CRACKED. STRINGER REPAIRED PER SRM 53-10-03 FIG 2.
- [SDR UPS05443665](https://openairdocs.org/sdr/UPS05443665), Jan 8, 2005: STRINGER. CRACKED. INSPECTION TYPE:C - STRINGER END BS 990 S-9L CRACKED. STRINGER REPAIRED PER SRM 53-10-03 FIG 2.
- [SDR UPS05443660](https://openairdocs.org/sdr/UPS05443660), Jan 8, 2005: STRINGER. CRACKED. INSPECTION TYPE:C U/D - BS 680, S9R, STRINGER END FOUND CRACK. STRINGER REPAIRED PER SRM 53-10-03 FIG 2.
- [SDR UPS05443658](https://openairdocs.org/sdr/UPS05443658), Jan 8, 2005: FRAME. CRACKED. INSPECTION TYPE:C, FWD CARGO COMPT - SUPPORT FRAME WEB SURFACE FOUND CRACKED AT STA 880 BETWEEN STRINGER 37L TO STRINGER 38L. SUPPORT FRAME REPAIRED PER SRM 53-
- [SDR UPS05443657](https://openairdocs.org/sdr/UPS05443657), Jan 8, 2005: STRINGER. CRACKED. INSPECTION TYPE:C U/D - BS 620, S9R, STRINGER END FOUND CRACK. STRINGER REPAIR PER SRM 53-10-03 FIG 2.
- [SDR UPS05443656](https://openairdocs.org/sdr/UPS05443656), Jan 8, 2005: STRINGER. CRACKED. INSPECTION TYPE:C U/D - BS 560, S9R, STRINGER END FOUND CRACK. STRINGER REPAIR PER SRM 53-10-03 FIG 2.
- [SDR UPS05443655](https://openairdocs.org/sdr/UPS05443655), Jan 8, 2005: STRINGER. CRACKED. INSPECTION TYPE:C - BS 640, S9R, STRINGER END FOUND CRACK. STRINGER REPAIR PER SRM 53-10-03 FIG 2.
- [SDR UPS05443652](https://openairdocs.org/sdr/UPS05443652), Jan 8, 2005: STRINGER. CRACKED. INSPECTION TYPE:C - BS 736 - 738, S8R, STRINGER END FOUND CRACK. STRINGER REPAIRED PER SRM 53-10-03 FIG 2.
- [SDR UPS05443824](https://openairdocs.org/sdr/UPS05443824), Jan 7, 2005: STRINGER. CRACKED. STR END BS 1476 S-6L CRACKED. CRACKED STRINGER REPAIRED PER RS R53-41-35242 AND ENGINEERING FILE NUMBER : 747-53-20217.
- [SDR UPS05443817](https://openairdocs.org/sdr/UPS05443817), Jan 7, 2005: STRINGER. CRACKED. STR END BS 1003 S-3L CRACKED. STRINGER REPAIRED PER RS R-53-41-35231 AND ENGINEERING FILE NUMBER 747-53-20216.
- [SDR UPS05443811](https://openairdocs.org/sdr/UPS05443811), Jan 7, 2005: STRINGER. CRACKED. STR END BS 1485 S-8L CRACKED. STRINGER REPAIRED PER RS 53-1-35249 AND ENGINEERING FILE NUMBER 747-53-20215.

All 387: https://openairdocs.org/deregistered/N675UP-2010-07-19/reports.md

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB CHI98IA164](https://openairdocs.org/ntsb/CHI98IA164), May 18, 1998: Boeing 747-123 (N675UP), Minneapolis, MN, incident, no damage. Probable cause: the open shielding on the #2 VHF transceiver coax connector which resulted in electromagnetic interference with the yaw damper system.

## FAA accident and incident reports (1)

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.

- [Accident 19980518020509A](https://openairdocs.org/incident/19980518020509A), May 18, 1998: Boeing 747123 (N675UP), Minneapolis, MN. Uncommanded rudder inputs, intermittant fire light. Warning cirucit replaced. Replaced VHF coaxial connector.

## Other aircraft with N675UP

- [Registered now](https://openairdocs.org/aircraft/N675UP): Raytheon 400A, S/N RK-363

---
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.