# N676UP: 1970 Boeing 747-123, registration cancelled 2011-05-24

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: May 24, 2011
- Status when cancelled: Valid registration
- Airframe: [Boeing 747-123](https://openairdocs.org/model/boeing-747-123) (registry code 1384873)
- Engine: [Pratt & Whitney JT9D-3A](https://openairdocs.org/engine/pratt-whitney-jt9d-3a) (registry code 52050)
- Data sheets: [TCDS A20WE](https://openairdocs.org/tcds/A20WE), [TCDS E20EA](https://openairdocs.org/tcds/E20EA) (OpenAirDocs)
- Serial number: 20101
- Year built: 1970
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 14, 1970
- Last registry action: May 24, 2011
- Mode S code: A8F3D2
- 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/N676UP
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=676UP
- Page: https://openairdocs.org/deregistered/N676UP-2011-05-24

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 (461, newest 50)

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

- [SDR UPS08451591](https://openairdocs.org/sdr/UPS08451591), Jan 30, 2008: SKIN. CRACKED. LT O/B AILERON UPPER SKIN HAS .5" BPT CRACK 4" FWD T/E, 11' IB OF OB END. APPLIED SPEED TAPE PER SRM 51-40-09 FIG 1 TABLE 1 AND TABLE II. REINSPECT EVERY "A" CH
- [SDR UPS07451115](https://openairdocs.org/sdr/UPS07451115), Nov 7, 2007: GENERATOR. INOPERATIVE. INSPECTION TYPE:N/A ATB FOR NR 3 BUSS TIE ON WITH FEEDER FAULT LT & CONST SPEED LIGHT. FIVE MIN LATER, CONST SPD LIGHT GEN 2 & GEN 4 W/LOSS OF BOOST PUMP IN TAN
- [SDR UPS07451107](https://openairdocs.org/sdr/UPS07451107), Nov 6, 2007: CSD. OVERHEATED. IFSD, NR 2 ENG CSD HAD HIGH OIL TEMP. FLIGHT CREW TRIED TO DISCONNECT BUT COULDN'T. FOLLOWED CHECK LIST AND SHUT DOWN ENGINE. MX INSPECTED NR 2 ENG CSD AND FOUN
- [SDR UPS07451082](https://openairdocs.org/sdr/UPS07451082), Oct 23, 2007: CONNECTOR. DAMAGED. EMERGENCY LIGHTS ABOVE R1 DOOR DO NOT WORK. FOUND TERMINAL END ON EXIT SIGN BROKEN. REPLACED PER BOEING SSWD 20-30-11. FUSE BLOWN ON POWER PACK MODULE. REPLACED
- [SDR UPS07450630](https://openairdocs.org/sdr/UPS07450630), Sep 10, 2007: ACCUMULATOR. LEAKING. INSPECTION TYPE:N/A PILOT REPORT - BRAKES SLOW TO RESPOND, FOUND BRAKE ACCUMULATOR LOW DURING ATTEMPTED SERVICE. FOUND LARGE AMOUNT OF HYD FLUID ON NITROGEN SID
- [SDR UPS07449812](https://openairdocs.org/sdr/UPS07449812), May 13, 2007: SPAR. BROKEN. INSPECTION TYPE:C RIGHT HORIZONTAL STABILIZER UPPER REAR SPAR AND SPLICE PLATE INSP BROKEN BOLTS INDICATION REVEALED ON BOLT 6 & 29. RIGHT HORIZONTAL STAB UPPER
- [SDR UPS07449139](https://openairdocs.org/sdr/UPS07449139), Feb 7, 2007: SWIVEL. LEAKING. INSPECTION TYPE:N/A COMPLETE LOSS OF HYD QTY IN FLIGHT, ON SYSTEM NR 4. NOTE: RESERVOIR NR 4 INDICATED 1 GALLON. FOUND RIGHT MAIN GEAR DOWNLOCK ACTUATOR FWD HOS
- [SDR UPS06448245](https://openairdocs.org/sdr/UPS06448245), Oct 15, 2006: TERMINAL. CORRODED. INSPECTION TYPE: N/A, SMOKE SMELLS, ABOUT 1:30 INTO FLIGHT. FOUND COPILOT WINDSCREEN CONNECTION AT LOWER RT SIDE SMOKING SECURED RT 1 OVERHEAD WINDOW HEAT, SMOK
- [SDR UPS06448035](https://openairdocs.org/sdr/UPS06448035), Sep 21, 2006: LIGHT. WEAK. INSPECTION TYPE: N/A EMERGENCY LIGHT ON CEILING ON MAIN DECK POS NR 1 IS VERY DIM. REMOVED AND REPLACED EMERGENCY CEILING LIGHT IAW MM 33-51-00. OPS CK GOOD. OK
- [SDR UPS06447998](https://openairdocs.org/sdr/UPS06447998), Sep 13, 2006: SKIN. PUNCTURED. RT OB FLAP LWR SKIN APPX 1 INCH PUNCTURE. REMOVED DAMAGED AREA OF SKIN AND CORE PER SRM 51-40-06. DAMAGE REMOVED OKAY TO INSTALL REPAIR. DRYED AREA-INSTALLED RE
- [SDR UPS06447934](https://openairdocs.org/sdr/UPS06447934), Sep 5, 2006: MODULE. INOPERATIVE. MAIN DECK EMERGENCY LIGHT IN CEILING AT STA 580R GOES OFF AFTER A FEW SECONDS OF TEST. REMOVED AND REPLACED CEILING LIGHT MODULE PER MM 33-51-07. OPS CHECK GOOD
- [SDR UPS06447932](https://openairdocs.org/sdr/UPS06447932), Sep 5, 2006: LIGHT. INOPERATIVE. MAIN DECK EMERGENCY LIGHT IN CEILING AT STA 340R DOES NOT COME ON DURING TEST. PERFORMED LIGHT TEST W/LIGHT CHECKING GOOD ON GROUND.
- [SDR UPS06447911](https://openairdocs.org/sdr/UPS06447911), Sep 4, 2006: LIGHT. INOPERATIVE. INSPECTION TYPE: N/A MAIN DECK EMERGENCY LIGHT IN CEILING AT STA 58DL AND ENTRY DOOR AFT EMERGENCY LIGHT GO OFF AFTER A FEW SECONDS OF TEST. THESE LIGHTS ARE TI
- [SDR UPS06447910](https://openairdocs.org/sdr/UPS06447910), Sep 4, 2006: LIGHT. INOPERATIVE. INSPECTION TYPE: N/A EMERGENCY LIGHT IN CEILING (FWD OF STAIRS) ON MAIN CARGO DECK INOPERATIVE. MAIN DECK UPPER DOOR FRAME FWD EMERGENCY LIGHT IS TIED TO THIS L
- [SDR UPS06447895](https://openairdocs.org/sdr/UPS06447895), Sep 4, 2006: POWER SUPPLY. INOPERATIVE. INSPECTION TYPE: ASE UPPER DECK DOOR FRAME EMEGENCY LIGHTS X 325 AND X 326 ARE INOP. REMOVED AND REPLACED UPPER DECK DOOR LIGHT POWER SUPPLY MODULE WITH REF TO 
- [SDR UPS06447541](https://openairdocs.org/sdr/UPS06447541), Jul 25, 2006: FLOORBEAM. CRACKED. INSPECTION TYPE:C U/D BS440 FLOORBEAM WEB FOUND CRACKED AFTER UPPER CHORD REMOVED JUST AT LBL 4, CRACK LENGTH 1". U/D BS440 BETWEEN LBL24 AND RBL16 FLOORBEAM WE
- [SDR UPS06447694](https://openairdocs.org/sdr/UPS06447694), Jul 21, 2006: SKIN. CRACKED. INSPECTION TYPE: C U/D FX SKIN AT BS 380 S6R REPAIR AREA FOUND 3 ADDITIONAL FASTENER HOLES CRACK AT OUTER SKIN. CRACK LENGTH 0.060" & 0.090" RESP. FX BS360-384 
- [SDR UPS06447676](https://openairdocs.org/sdr/UPS06447676), Jul 19, 2006: REVEAL. CRACKED. INSPECTION TYPE:C M/D BS 2231 FRAME INNER CHORD S25R-26R FOUND REVEAL CRACK AND PREVIOUSLY STOP DRILLED, CRACK LENGTH 1.5". REPAIR DOUBLER REINSTALLED AS PER RS
- [SDR UPS06447675](https://openairdocs.org/sdr/UPS06447675), Jul 19, 2006: REVEAL. CRACKED. INSPECTION TYPE:C M/D BS 2231 FRAME INNER CHORD S22L-S25L FOUND REVEAL CRACKED AT S22L AND S24L LOCATION AND PREVIOUSLY STOP DRILLED, CRACK LENGTH 1" AND 1.5". 
- [SDR UPS06447693](https://openairdocs.org/sdr/UPS06447693), Jul 14, 2006: SKIN. CRACKED. FX BS 340-380 S6R LAP SPLICE TOP ROW FASTENER HOLES FOUND CRACKS AT OUTER SKIN. FX BS340-360 S6R FASTENER REINSTALLED AS PER RS R53-15-35543 ITEM C. REFER NRC 7
- [SDR UPS06447681](https://openairdocs.org/sdr/UPS06447681), Jul 14, 2006: FRAME. CRACKED. INSPECTION TYPE:C FX BS340 FRAME FOUND 1 HOLE CRACK AT S6R LOCATION APPROX 0.030" LONG, CRACK LENGTH 0.030". FX BS 340 STR 6R AREA FRAME REPAIRED AS PER RS R53-
- [SDR UPS06447450](https://openairdocs.org/sdr/UPS06447450), Jul 14, 2006: STRINGER. CRACKED. INSPECTION TYPE:C FX BS 340-360 S6R FOUND FASTENER HOLES CRACK AT STRINGER (CRACK LENGTH 0.030 INCH). FX BS 340-375 STR 6R STRINGER REPAIRED AS PER SRM 53-10-03
- [SDR UPS06447692](https://openairdocs.org/sdr/UPS06447692), Jul 13, 2006: SKIN. CRACKED. FX BS 360-380 S6R LAP SPLICE 6EA TOP ROW FASTENER HOLE FOUND CRACKS AT OUTER SKIN, CRACK LENGTH 1/16 APPROX. FX BS 340 TO BS 360 STR 6R FASTENER REINSTALLED AS 
- [SDR UPS06447660](https://openairdocs.org/sdr/UPS06447660), Jul 13, 2006: FLOORBEAM. CORRODED. BS 520 FLOORBEAM UPPER CHORD FOUND CORRODED. CORROSION BLEND OUT 0.030" BY 2" BY 3" EXCEED SRM 53-10-01 FIG 1 LIMIT AND U/D BS 520 FLOORBEAM UPPER CHORD REPAIRE
- [SDR UPS06447659](https://openairdocs.org/sdr/UPS06447659), Jul 13, 2006: FLOORBEAM. MISDRILLED. BS 520 FLOORBEAM UPPER CHORD FOUND SHORT EDGE MARGIN AT LBL 76" TO LBL 78" APPROX. U/D BS 520 FLOORBEAM REPAIRED AS PER HX RS NR R53-25-35537 REFER NRC NR IB702
- [SDR UPS06447658](https://openairdocs.org/sdr/UPS06447658), Jul 13, 2006: FLOORBEAM. MISDRILLED. BS 520 FLOORBEAM UPPER CHORD FOUND SHORT EDGE MARGIN FROM RBL 48 TO RBL 82. BS 520 FLOORBEAM REPAIRED AS PER HX RS NR R53-25-35537 REFER NRC NR IB70247 FOR WORK
- [SDR UPS06447480](https://openairdocs.org/sdr/UPS06447480), Jul 13, 2006: FRAME. CRACKED. INSPECTION TYPE:C RT BLG W/W STA 1438 FRAME ATT HOLE FOUND CRACKED RBL 116 WL 156, CRACK LENGTH 3/8". RT BLG W/W BS 1438 RBL 116 WL 152 TO WL 165 FRAME REPAIRED
- [SDR UPS06447563](https://openairdocs.org/sdr/UPS06447563), Jul 12, 2006: VERTICAL BEAM. CRACKED. INSPECTION TYPE:C 1L MED FWD VERTICAL BEAM LOWER CORNER CRACK FOUND AS MARKED. CRACK LENGTH 1 INCH. 1L MED FWD VERTICAL BEAM LOWER CORNER REPAIRED AS PER SRM 52
- [SDR UPS06447562](https://openairdocs.org/sdr/UPS06447562), Jul 12, 2006: VERTICAL BEAM. CRACKED. INSPECTION TYPE:C 1R MED FWD VERTICAL BEAM LOWER CORNER FOUND CRACK. CRACK LENGTH 1 INCH. 1R MED FWD VERTICAL BEAM LOWER CORNER REPAIRED AS PER SRM 52-10-02 FIG
- [SDR UPS06447538](https://openairdocs.org/sdr/UPS06447538), Jul 12, 2006: ANGLE. CRACKED. INSPECTION TYPE:C RT SIDE BS2231 FRAME AT STR25 FOUND 2 HOLES CRACKED AT INTERCOSTAL TO FRAME WEB ATTACHED T-ANGLE AREA. CRACK LENGTH 1/8". RT SIDE BS 2231 FRAM
- [SDR UPS06447491](https://openairdocs.org/sdr/UPS06447491), Jul 12, 2006: SPLICE PLATE. CORRODED. INSPECTION TYPE:C FWD CARGO COMPT RT MAIN DECK FLOORBEAM LOWER CHORD SPLICE PLATE LOWER SURFACE FOUND SURFACE CORROSION AT STA 680 TO STA 700 RBL12. CORROSION B
- [SDR UPS06447662](https://openairdocs.org/sdr/UPS06447662), Jul 11, 2006: FLOORBEAM. DAMAGED. U/D RT BS 520 UPPER DECK FLOORBEAM FWD FLANGE 1 FASTENER HOLE FOUND OVAL AT RBL 70". U/D BS 520 FLOORBEAM REPAIRED AS PER HX RS NR R53-25-35537 REF NRC NR IB702
- [SDR UPS06447657](https://openairdocs.org/sdr/UPS06447657), Jul 11, 2006: FLOORBEAM. CORRODED. LT BS 520 UPPER DECK FLOORBEAM AFT FLANGE 5 FASTENER HOLES FOUND CRACK AND/OR CORROSION AT LBL 34, LBL 45, LBL 49, AND LBL 55" (CRACK LENGTH 0.060" , CORROSION 
- [SDR UPS06447635](https://openairdocs.org/sdr/UPS06447635), Jul 11, 2006: FLOORBEAM. DAMAGED. INSPECTION TYPE:C U/D RT BS 440 UPPER DECK FLOORBEAM FWD FLANGE 1 FASTENER HOLE FOUND OVAL AT RBL 48. U/DECK BS 440 LBL 68" TO RBL 68" FLOORBEAM UPPER CHORD REP
- [SDR UPS06447599](https://openairdocs.org/sdr/UPS06447599), Jul 11, 2006: FLOORBEAM. CRACKED. INSPECTION TYPE:C U/D LEFT BS 520 UPPER DECK FLOORBEAM FWD FLANGE 1EA FASTENER HOLE FOUND CRACK AT LBL 45. CRACK LENGTH 0.030 INCH. U/D BS 520 FLOORBEAM UPPER C
- [SDR UPS06447560](https://openairdocs.org/sdr/UPS06447560), Jul 11, 2006: FLOORBEAM. CORRODED. INSPECTION TYPE:C U/D RIGHT BS 520 UPPER DECK FLOORBEAM FWD FLANGE 2EA FASTENER HOLE FOUND CORROSION AT RBL 21 & RBL 25. FASTENER HOLE OVERSIZED TO 0.342" AT RB
- [SDR UPS06447559](https://openairdocs.org/sdr/UPS06447559), Jul 11, 2006: FLOORBEAM. CORRODED. INSPECTION TYPE:C U/D RIGHT BS 50 UPPER DECK FLOORBEAM AFT FLANGE 2EA FASTENER HOLE FOUND CORROSION AT RBL16 AND RBL 27. 0.310" & 0.326" OVERSIZED. FASTENER HOL
- [SDR UPS06447543](https://openairdocs.org/sdr/UPS06447543), Jul 11, 2006: FLOORBEAM. CORRODED. INSPECTION TYPE:C U/D RT BS 440 UPPER DECK FLOORBEAM AFT FLANGE 1 FASTENER HOLE FOUND CRACK AND CORROSION AT RBL7. CORROSION BLEND OUT 0.032" FASTENER HOLE OVER
- [SDR UPS06447542](https://openairdocs.org/sdr/UPS06447542), Jul 11, 2006: FLOORBEAM. CORRODED. INSPECTION TYPE:C U/D RT BS440 UPPER DECK FLOORBEAM FWD FLANGE 1 FASTENER HOLE FOUND CORROSION AT RBL24. CORROSION BLEND OUT 0.048". FASTENER HOLE OVERSIZED TO 
- [SDR UPS06447540](https://openairdocs.org/sdr/UPS06447540), Jul 11, 2006: FLOORBEAM. DAMAGED. INSPECTION TYPE:C U/D BS440 MOST OF FLOORBEAM FASTENER HOLE FOUND SHORT EDGE BELOW 0.44" AS MARKED AT BETWEEN LBL 44 TO LBL 53 AND RBL 44 TO RBL 53 AREA. U/D BS
- [SDR UPS06447539](https://openairdocs.org/sdr/UPS06447539), Jul 11, 2006: STRAP. CRACKED. INSPECTION TYPE:C U/D RT BS520 UPPER DECK FLOORBEAM FWD FLANGE AREA 1 FASTENER HOLE FOUND CRACK AT FLOOR CHORD STRAP AT RBL 35. CRACK LENGTH 0.030". STRAP REPLA
- [SDR UPS06447477](https://openairdocs.org/sdr/UPS06447477), Jul 11, 2006: SHEAR WEB. CRACKED. FOUND BS 820-840 STR -10L STRINGER ATT SHEAR WEB BOTH END FOUND CRACK (CRACK LENGTH 1"). SHEAR WEB REPLACED AS PER SRM 51-10-01 PG 9.
- [SDR UPS06447475](https://openairdocs.org/sdr/UPS06447475), Jul 11, 2006: GUSSET. CRACKED. RT BS 520 UPPER DECK FLOORBEAM FWD FLANGE AREA 2 FASTENER HOLES FOUND CRACK AT GUSSET AT RBL 35 AND RBL 39.5 (CRACK LENGTH 0.060"). U/DECK BS 820 RBL 31" TO RBL
- [SDR UPS06447413](https://openairdocs.org/sdr/UPS06447413), Jul 11, 2006: SHEAR WEB. CRACKED. BS 820-840 STR -10R STRINGER ATT SHEAR WEB FWD END FOUND CRACKED, CRACK LENGTH 1/2". SHEAR WEB REPAIRED AS PER SRM 51-40-03 FIG 3.
- [SDR UPS06447701](https://openairdocs.org/sdr/UPS06447701), Jul 10, 2006: FRAME. CRACKED. INSPECTION TYPE-C LT SIDE BS800 FRAME AT STR16 FOUND 1EA HOLE CRACKED AT FRAME STRAP APPROX .0625 INCH LONG RUNNING. CABIN LT SIDE BS800 FRAME ATTACH STRAP BETW
- [SDR UPS06447678](https://openairdocs.org/sdr/UPS06447678), Jul 10, 2006: REVEAL. CRACKED. INSPECTION TYPE:C M/D BS2231 BETWEEN S25L AND 26L REVEAL CRACK, CRACK LENGTH 0.8". M/D BS 2231 BETWEEN STR 25L-STR 26L REVEAL PANEL REPAIRED AS PER RS R53-62-35
- [SDR UPS06447661](https://openairdocs.org/sdr/UPS06447661), Jul 10, 2006: FLOORBEAM. CORRODED. BS 520 LBL 33-47 FLOORBEAM FOUND CORROSION AS MARKED. CORROSION BLEND OUT 0.051" BY 1.5" BY 2" EXCEED SRM 53-10-01 FIG 1 LIMITS, AND U/D BS 520 FLOORBEAM UPPER 
- [SDR UPS06447615](https://openairdocs.org/sdr/UPS06447615), Jul 10, 2006: FRAME. CRACKED. INSPECTION TYPE:C FWD CARGO COMPT - LT STA 980 STR39 FRAME FOUND CRACKED. CRACK LENGTH 1/2". FWD CARGO COMPT LT STA980 STR39 FRAME REPAIRED AS PER RS R53-10-355
- [SDR UPS06447609](https://openairdocs.org/sdr/UPS06447609), Jul 10, 2006: SKIN. CORRODED. RT BS 579 S44R LAP JOINT LOWEST FASTNENER HOLE FOUND CORROSION INDICATION AT OUTER SKIN AND INNER SKIN INTERFACE. CORROSION BLEND OUT AT INNER SKIN 0.009" BY 7/
- [SDR UPS06447473](https://openairdocs.org/sdr/UPS06447473), Jul 10, 2006: FLOORBEAM. CORRODED. BS 480 LBL 10- RBL 32 FLOORBEAM UPPER FACE FOUND CORRODED. CORROSION BLEND OUT 0.021" BY 1" BY 2" EXCEED SRM 53-10-01 FIG 1 LIMITS, U/D BS 480 LBL 10" - RBL 32"

All 461: https://openairdocs.org/deregistered/N676UP-2011-05-24/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.

- [Accident 20071221829409A](https://openairdocs.org/incident/20071221829409A), Dec 21, 2007: Boeing 747123 (N676UP), Philadelphia, PA, No damage. (-23) This event is classified as an accident due to the injuries sustained and the length of time of hospitalization by [privacy data omitted] an aircraft…
- [Incident 19881021057499I](https://openairdocs.org/incident/19881021057499I), Oct 21, 1988: Boeing 747123 (N676UP), Louisville, KY. Engine stalled after throttled back on descent. Unable to recover. Emergency landing. Cause undetermined.

## Other aircraft with N676UP

- [Registered now](https://openairdocs.org/aircraft/N676UP): Hawker Beechcraft 400A, S/N RK-570, built 2008

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