# N523UP: 1982 Boeing 747-283B, registration cancelled 2010-07-07

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: July 7, 2010
- Status when cancelled: Valid registration
- Airframe: [Boeing 747-283B](https://openairdocs.org/model/boeing-747-283b) (registry code 1384867)
- Engine: [Pratt & Whitney JT9D series](https://openairdocs.org/engine/pratt-whitney-jt9d-series) (registry code 52054)
- Data sheets: [TCDS A20WE](https://openairdocs.org/tcds/A20WE) (OpenAirDocs)
- Serial number: 22381
- Year built: 1982
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 1, 1997
- Last registry action: June 17, 2010
- Mode S code: A695E3
- 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/N523UP
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=523UP
- Page: https://openairdocs.org/deregistered/N523UP-2010-07-07

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 747-283B: https://openairdocs.org/model/boeing-747-283b.md

## Service difficulty reports (146, newest 50)

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

- [SDR UPS08451372](https://openairdocs.org/sdr/UPS08451372), Jan 3, 2008: CADC. MALFUNCTIONED. INSPECTION TYPE:N/A ATB - RVSM - CAPTAINS ALTIMETER 1500' OF ALTITUDE AT 330, WENT TO ALT STATIC SOURCE. AS PER MM 34-11-00 AND 34-12-01 INSP NR 1 CADC AND PITO
- [SDR UPS07450908](https://openairdocs.org/sdr/UPS07450908), Oct 10, 2007: STRINGER. DAMAGED. STR 45L DAMAGED. REMOVED STR 45L DAMAGE AS PER SRM 53-10-03. FABRICATED SPLICES FOR REPAIR AS PER SRM 53-10-03. INSTALLED NEW STRINGER AND SPLICES AS PER SRM 53
- [SDR UPS07450412](https://openairdocs.org/sdr/UPS07450412), Jul 27, 2007: FIRE LOOP. DAMAGED. INSPECTION TYPE:N/A ON CLIMBOUT THE FWD PANEL FIRE DETECTION LIGHT WAS FLICKERING; NR 4 ENGINE NACELLE TEMP IND -A- WAS FLICKERING FROM 0 TO 9 AT SAME TIME & RA
- [SDR UPS07450171](https://openairdocs.org/sdr/UPS07450171), Jul 15, 2007: FLOOR PANEL. CRACKED. 3.5 INCH CRACK IN BULK CARGO COMPARTMENT FLOOR BETWEEN OBI BOXES. REPAIRED IAW SRM 51-40-02 FIG 1.
- [SDR UPS07449325](https://openairdocs.org/sdr/UPS07449325), Mar 5, 2007: LIGHT. INOPERATIVE. INSPECTION TYPE:N/A EMERGENCY LIGHTS INOP AT ESCAPE SLIDE DOOR FRAME AND EXIT SIGN ABOVE SLIDE. REMOVED AND REPLACED POWER SUPPLY MODULE FOR EXIT SIGN PER MM 33
- [SDR UPS06448778](https://openairdocs.org/sdr/UPS06448778), Dec 17, 2006: LOCK. DAMAGED. ATB - NR 1 THRUST REVERSER UNLOCK LIGHT FLASHING DURING FLIGHT. NR 1 THRUST REVERSER DEFERRED AND LOCKED OUT M340031 ASSIGNED. NR 1 ENGINE SHUT DOWN AS A PRECAU
- [SDR UPS06448292](https://openairdocs.org/sdr/UPS06448292), Oct 20, 2006: A/C PACK. ODOR. INSPECTION TYPE:N/A NR 3 PACK OVERHEATS, ALSO BURNING SMELL. TRIPS RESET, TRIPPED AGAIN. NR 3 PACK AUTO FEATURE DEFERRED PER MEL 21-6-1, BYPASS VALVE GOES TO FU
- [SDR UPS06448249](https://openairdocs.org/sdr/UPS06448249), Oct 3, 2006: SKIN. CORRODED. INSPECTION TYPE: C FX BS 2180-2186 S46-47R EXISTING REPAIR REMOVE REQUIRE FOR CUTOUT EVALUATION. CORROSION BLEND OUT 0.048 INCH X 1INCH X .7500 INCH, FX BS 2180
- [SDR UPS06448211](https://openairdocs.org/sdr/UPS06448211), Sep 26, 2006: VERTICAL BEAM. CRACKED. INSPECTION TYPE-C NR 4L MED FWD LOWER CORNER VERTICAL BEAM FOUND CRACK APPROX 1 INCH LONG. NR 4L MED FWD LOWER CORNER VERTICAL BEAM REPAIRED IAW SRM 52-10-02 FI
- [SDR UPS06448207](https://openairdocs.org/sdr/UPS06448207), Sep 26, 2006: VERTICAL BEAM. CRACKED. INSPECTION TYPE-C NR 1R MED FWD LOWER CORNER VERTICAL BEAM FOUND CRACK APPROX 1.5 INCH LONG. NR 1R MED FWD LOWER CORNER VERTICAL BEAM REPAIRED IAW SRM 52-10-02 
- [SDR UPS06448206](https://openairdocs.org/sdr/UPS06448206), Sep 26, 2006: VERTICAL BEAM. CRACKED. INSPECTION TYPE-C NR 2L MED FWD LOWER CORNER VERTICAL BEAM FOUND CRACK APPROX .7500 INCH LONG. NR 2L MED FWD LOWER CORNER VERTICAL BEAM REPAIRED IAW SRM 52-10-0
- [SDR UPS06448212](https://openairdocs.org/sdr/UPS06448212), Sep 23, 2006: ATTACH FITTING. CORRODED. INSPECTION TYPE-C CORROSION FOUND AT 1 FASTENER HOLE AT FRAME WEB ATTACH FITTING LOCATED AT BS 979 S38L. FWD CARGO COMPT BS979 S38L FRAME ATTACHED FTG REPLACED 
- [SDR UPS06448208](https://openairdocs.org/sdr/UPS06448208), Sep 23, 2006: FITTING. CORRODED. INSPECTION TYPE-C FX LT BS 980 STR 38L UPPER AND LOWER DRAG SPLICE FITTINGS ATT BOLT HOLE AREA FOUND CORROSION. CORROSION BLEND OUT 0.092 INCH BY 1.5 INCH BY 3 
- [SDR UPS06448182](https://openairdocs.org/sdr/UPS06448182), Sep 23, 2006: STRINGER. CRACKED. CRACK FOUND AT 1 FASTENER HOLE LOCATED AT BS 983 STR 38L APPROX 1" LONG RUNNING FORWARD AS MARKED. FX BS 970 TO BS 990 STR 38L STRINGER REPAIRED AS PER SRM 53-1
- [SDR UPS06448209](https://openairdocs.org/sdr/UPS06448209), Sep 22, 2006: VERTICAL BEAM. CRACKED. INSPECTION TYPE-C M/D RT NR 5 DOOR INTERIOR FWD LWR CORNER VERTICAL BEAM FOUND CRACK, CRACK LENGTH 4.7500 INCH APPROX. M/D RT NR 5 DOOR INTERIOR FWD LOWER CORNE
- [SDR UPS06448231](https://openairdocs.org/sdr/UPS06448231), Sep 21, 2006: SKIN. CRACKED. INSPECTION TYPE:C AFT CARGO DOOR CUTOUT FWD UPPER CORNER HINGE FAIRING COVERED AREA FOUND 1 CRACK AT SKIN AT THE MOST AFT HOLE APPROX 0.040" (CRACK LENGTH 0.040
- [SDR UPS06448210](https://openairdocs.org/sdr/UPS06448210), Sep 21, 2006: DOOR FRAME. CRACKED. INSPECTION TYPE-C M/D RT DOOR FRAME INTERIOR FACE AFT LWR CORNER AREA FOUND CRACKED, CRACK LENGTH 2.5 INCH APPROX. M/D R4 DOOR FRAME AFT LOWER CORNER AREA REPAI
- [SDR UPS06448239](https://openairdocs.org/sdr/UPS06448239), Sep 20, 2006: FRAME. CRACKED. INSPECTION TYPE:C NR 3 PYLON REAR UPPER ENG MT BULKHEAD O/B FWD FRAME FOUND CRACK AT UPPER PORTION, CRACK LENGTH 1.5". NR 3 PYLON REAR BULKHEAD O/B FWD FRAME RE
- [SDR UPS06448233](https://openairdocs.org/sdr/UPS06448233), Sep 20, 2006: SKIN. CRACKED. INSPECTION TYPE:C FWD CARGO DOOR, DOOR EXTERNAL SKIN SURFACE FOUND DENT MARK AT STA 582, 6" TO LOWER EDGE, CRACK LENGTH 1/8". FWD CARGO DOOR EXTERNAL SKIN REPAI
- [SDR UPS06448181](https://openairdocs.org/sdr/UPS06448181), Sep 20, 2006: FRAME. CRACKED. APU COMPT BS 2675 LT WL325 FRAME FOUND CRACK AS MARKED, CRACK LENGTH .500 INCH. APU COMPT BS 2675 LT WL 325 FRAME REPAIRED AS PER SRM 51-40-03 FIG 1.
- [SDR UPS06448180](https://openairdocs.org/sdr/UPS06448180), Sep 20, 2006: FRAME. CRACKED. EMP APU COMPT LT BS 2701 WL 315 FRAME FOUND CRACK AS MARKED, CRACK LENGTH .7500. APU COMPT LT BS 2701 WL 315 FRAME REPAIRED AS PER SRM 51-40-03 FIG 1.
- [SDR UPS06448232](https://openairdocs.org/sdr/UPS06448232), Sep 19, 2006: SKIN. CRACKED. INSPECTION TYPE:C LT BS 980 STR 38L DRAG SLICE FTG AREA FOUND 1 FASTENER HOLE CRACKED AT FUSELAGE HOLE CRACKED AT FUSELAGE APPROX 1/8". FX BS 950 - BS 990 STR 3
- [SDR UPS06448226](https://openairdocs.org/sdr/UPS06448226), Sep 19, 2006: FLOORBEAM. CORRODED. INSPECTION TYPE:C, RT B/G W/W UPPER PRESSURE FLOOR PANEL ATTACH ANGLE SOME AREA FOUND CORROSION AS MARK AT STA 1403, RBL 34 TO RBL 104. CORROSION BLEND OUT 0.03
- [SDR UPS06448179](https://openairdocs.org/sdr/UPS06448179), Sep 19, 2006: INTERCOSTAL. CRACKED. N/G W/W TOP PANEL INTERNAL SIDE INTERCOSTAL AT BRAKE SNUBBER FOUND CRACK AS MARK AT STA 290 RBL 21, CRACK LENGTH 1/4". N/G W/W TOP PANEL INTERNAL SIDE INTERCOST
- [SDR UPS06447744](https://openairdocs.org/sdr/UPS06447744), Aug 22, 2006: CHIP DETECTOR. DAMAGED. ATB - OIL QTY ON NR 2 ENGINE DROPPED TO ZERO OIL PRESSURE DECREASING SHUT DOWN NR 2 ENGINE. LANDING WT 629.0. REPLACED NR 4 BEARING MAG PLUG PER MM 72-61-00.
- [SDR UPS06447496](https://openairdocs.org/sdr/UPS06447496), Jul 31, 2006: PUMP. LEAKING. NR 4 HYD SYS LOST ALL FLUID, SYS INOP. FOUND HYD LEAK FROM NR 4 EDP BODY. REPLACED NR 4 HYD PUMP PER MM 29-11-05 & REPLACED CASE DRAIN & PRESS FILTERS PER MM 29
- [SDR UPS06447304](https://openairdocs.org/sdr/UPS06447304), Jul 9, 2006: INDICATOR. ACTIVATED. PBE PRESS IND IS EXTENDED. INSTALLED NEW PBE.
- [SDR UPS05445857](https://openairdocs.org/sdr/UPS05445857), Dec 6, 2005: LINK. CRACKED. NR 4 ENGINE REAR MOUNT THRUST LINK FWD END LUG BORE LOWER AREA WITH CRACK INDICATION ( > 126 PERCENT FSH ) WHICH EXCEED LIMIT. NR 4 ENGINE REAR MOUNT THRUST LIN
- [SDR UPS05445856](https://openairdocs.org/sdr/UPS05445856), Dec 6, 2005: LINK. CRACKED. NR 3 ENGINE REAR MOUNT THRUST LINK FWD END LUG BORE UPPER AREA WITH CRACK INDICATION (90 PERCENT FSH ); AND AFT END LUG BORE UPPER AND LOWER AREA WITH CRACK IND
- [SDR UPS05445855](https://openairdocs.org/sdr/UPS05445855), Dec 6, 2005: LINK. CRACKED. NR 2 ENGINE REAR MOUNT THRUST LINK AFT END LUG BORE LOWER AREA WITH CRACK INDICATION 70 PERCEMT FSH WHICH EXCEED LIMIT. NR 2 ENGINE REAR MOUNT THRUST LINK REPLA
- [SDR UPS05445854](https://openairdocs.org/sdr/UPS05445854), Dec 6, 2005: LINK. CRACKED. NR 1 ENGINE REAR MOUNT THRUST LINK FWD END LUG BORE UPPER AND LOWER AREA WITH CRACK INDICATION 60 PERCENT FSH AND 80 PERCENT FSH RESPECTIVELY. WHICH EXCEED LIMI
- [SDR UPS05445406](https://openairdocs.org/sdr/UPS05445406), Sep 12, 2005: WINDSHIELD. DELAMINATED. INSPECTION TYPE:N/A F/O R1 WINDOW HAS CHIPPING AND CRACKING IN MAIN GLASS PLIES. COMPLETED R1 REMOVAL & INSTALLED NEW R1 REF TO MM 56-11-01 UP TO STEP 6.D. FIRS
- [SDR UPS05444404](https://openairdocs.org/sdr/UPS05444404), Apr 23, 2005: SKIN. CHAFED. EXTERIOR SKIN CHAFING MARK FOUND ABOVE STR 12L BS 2230. CHAFED AREA 0.016 INCH BY 3 INCH BY 1 INCH. SKIN REPAIRED AT BS 2220 TO BS 2240 BETWEEN S11L TO S12L ARE
- [SDR UPS05444426](https://openairdocs.org/sdr/UPS05444426), Apr 14, 2005: FRAME. CRACKED. NR 1 PYLON AFT BULKHEAD I/B FRAME ADJ TO UPPER SPAR FTG CRACKED APPROX .1875 RUNNING I/B AND O/B, CRACK LENGTH .1875. NR 1 PYLON AFT BULKHEAD I/B FRAME REPAIRED
- [SDR UPS05444422](https://openairdocs.org/sdr/UPS05444422), Apr 14, 2005: FRAME. CRACKED. NR 1 PYLON AFT BULKHEAD O/B FRAME ADJ TO UPPER SPAR FITTING FOUND CRACKED RUNNING I/B TO EDGE AND RUNNING O/B .9375 INCH LONG, (CRACK LENGTH .9375 ). NR 1 PYLON
- [SDR UPS05444353](https://openairdocs.org/sdr/UPS05444353), Apr 14, 2005: FITTING. CRACKED. INSPECTION TYPE:C RIGHT BS 1480 B/H NR 16 HOLE FOUND CRACK AT OUTER CHORD SPLICE FITTING RUNNING OUTBOARD APPROX 0.030 INCH LONG (CRACK LENGTH 0.030 INCH). RIGH
- [SDR UPS05444352](https://openairdocs.org/sdr/UPS05444352), Apr 14, 2005: FRAME. CRACKED. INSPECTION TYPE: C, RT BS 1480 BULKHEAD NR 11 HOLE FOUND CRACK AT BULKHEAD FRAME RUNNING AFT APPROX 0.040 INCH LONG (CRACK LENGTH .0625 INCH). RIGHT BS 1480 B/H
- [SDR UPS05444346](https://openairdocs.org/sdr/UPS05444346), Apr 14, 2005: SKIN. CRACKED. INSPECTION TYPE:C LT BS 1480 BHD NR 11 HOLE FOUND CRACK AT FUSELAGE SKIN THROUGH THICKNESS RUNNING FWD ( CRACK LENGTH 0.325 INCH ). BS 1480 LT STR 32 TO STR 34 
- [SDR UPS05444334](https://openairdocs.org/sdr/UPS05444334), Apr 14, 2005: SPLICE. CRACKED. INSPECTION TYPE:C RH BS 1480 B/H #18 HOLE FOUND CRACK AT WEB SPLICE PLATE RUNNING UP APPROX 0.080" LONG ( CRACK LENGTH 0.080" ) NR 18 BOLT HOLE OVERSIZED TO 0.5
- [SDR UPS05444333](https://openairdocs.org/sdr/UPS05444333), Apr 14, 2005: BULKHEAD. CRACKED. INSPECTION TYPE: C, RT BS 1480 B/H NR 7 HOLE FOUND CRACK AT FX, SKIN RUNNING AFT APPROX .0625 INCH LONG, CRACK LENGTH .0625. HOLE OVERSIZED TO 0.687" AS PER EO 
- [SDR UPS05444425](https://openairdocs.org/sdr/UPS05444425), Apr 13, 2005: FRAME. CRACKED. NR 2 PYLON AFT BULKHEAD I/B FRAME ADJACENT TO UPPER SPAR FITTING FOUND CRACKED, CRACK LENGTH .375 AND .250. NR 2 PYLON AFT BULKHEAD I/B FRAME REPAIRED AS PER HX
- [SDR UPS05444421](https://openairdocs.org/sdr/UPS05444421), Apr 13, 2005: FRAME. CRACKED. NR 2 PYLON AFT BULKHEAD O/B FRAME ADJACENT TO UPPER SPAR FITTING FOUND CRACKED, (CRACK LENGTH .25 INCH AND .9375 INCH ). NR 2 PYLON AFT BULKHEAD O/B FRAME REPAI
- [SDR UPS05444399](https://openairdocs.org/sdr/UPS05444399), Apr 12, 2005: SHEAR TIE. CRACKED. COCKPIT BS 360 STR 1R FRAME SHEAR TIE CRACKED, CRACK LENGTH 1/2 INCH. COCKPIT BS 360 FRAME WEB REPAIRED AT BTN STR 1R AND STR 2R AREA AS PER HX RS R53-12-35290 
- [SDR UPS05444398](https://openairdocs.org/sdr/UPS05444398), Apr 12, 2005: FRAME. CRACKED. COCKPIT BS 360 FRAME STR 2R WEB CRACKED, CRACK LENGTH 9/16". COCKPIT BS 360 FRAME WEB REPAIRED AT BETWEEN STR 1R AND 2R AREA AS PER HX RS R53-12-35290 AND UPS E
- [SDR UPS05444335](https://openairdocs.org/sdr/UPS05444335), Apr 12, 2005: STRINGER CLIP. CRACKED. INSPECTION TYPE:C COCKPIT - BS 360 S-8L FRAME/STR TIE CLIP CRACKED. ( CRACK LENGTH 0.5" ). COCKPIT BS 360 STR -8L TIE CLIP REPLACED AS PER SRM 51-10-01 P.9.
- [SDR UPS05444428](https://openairdocs.org/sdr/UPS05444428), Apr 11, 2005: FITTING. CORRODED. U/D - STA 496 RBL 70 TOILET TANK TIE DOWN FTG CORROSION FOUND. CORROSION BLEND OUT 0.020" BY 1" BY 1". TIE DOWN FTG REPLACED AS PER SRM 51-10-01 PG 9.
- [SDR UPS05444408](https://openairdocs.org/sdr/UPS05444408), Apr 11, 2005: FRAME. CRACKED. BS 480 FRAME S10AL STR CUTOUT CRACKED. CRACK LENGTH 3/4 INCH. BS 480 STR 10AL TO STR 12L FRAME REPAIRED AS PER SRM 53-10-04 FIG 22 REFER NRC 6374 FOR WORKING DE
- [SDR UPS05444407](https://openairdocs.org/sdr/UPS05444407), Apr 11, 2005: FRAME. CRACKED. U/DECK BS480 STR 12L STR CUTOUT CRACKED. CRACK LENGTH 3/4 INCH. U/DECK BS480 STR 10AL TO STR 12L FRAME REPAIRED AS PER SRM 53-10-04 FIG 22.
- [SDR UPS05444406](https://openairdocs.org/sdr/UPS05444406), Apr 11, 2005: FRAME. CRACKED. STA 440 STR 10R FRAME CRACKED. U/DECK BS440 STR 10R FRAME REPAIRED AS PER SRM 53-10-04 FIG 11.
- [SDR UPS05444405](https://openairdocs.org/sdr/UPS05444405), Apr 11, 2005: FRAME. CRACKED. BS440 LT FRAME, JUST BELOW U/D FLOORBEAM LWR CHORD, WEB CRACKED WL290, CRACK LENGTH 3/8 INCH. BS 440 LT FRAME WEB REPLACED BETWEEN STR 13L TO 16L AS PER SRM 51-

All 146: https://openairdocs.org/deregistered/N523UP-2010-07-07/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 20021015030929I](https://openairdocs.org/incident/20021015030929I), Oct 15, 2002: Boeing 747283B (N523UP), Ontario, CA, Minor damage. (-23) Aircraft landed short on runway 26L threshold and struck four runway threshold lights at ont. Aircraft taxied to gate without further incident. Aircraft…
- [Incident 20010718018579I](https://openairdocs.org/incident/20010718018579I), Jul 18, 2001: Boeing 747283B (N523UP), Anchorage, AK, Minor damage. (-23) Tail strike was a result of a possible flawed cockpit procedure in determining and setting approach and landing speeds. Second officer properly…

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