Boeing 747-123

Service difficulty reports · 2,292

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duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = '747123'
  ORDER BY difficulty_date DESC"

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SDR UPS04441925Strap · crackedINSPECTION TYPE:C BS 1241 RIGHT BULKHEAD SPLICE STRAP AFT HOLE CRACK FOUND RUNNING AFT APPROX .125 INCH. AFT BOLT HOLE REPAIRED AS PER RS R53-41-35107 BS 1241 RIGHT BULKHEAD SPLICE STRAP WILL BE REPLACED WITHIN 2 YEARS AFTER CRACK DISCOVERY AS PER EO B747-531Jan 29, 2004 · N672UP · Boeing 747123 · Fuselage Main, BulkheadSDR UPS04441906Skin · damagedINSPECTION TYPE: C, EO 747-5330-13494-H REPAIR ASSESSMENT PROGRAM DURING RAP INSPECTION, ITEM N672-46-24, BS 1840-1860 STR 42R AFT CARGO DOOR LWR EDGE REPAIR DOUBLER HAS LESS THAN 2 ROWS OF FASTENER BEYOND THE DAMAGE AREA. THIS REPAIR IS CLASSIFIED AS PER -DJan 28, 2004 · N672UP · Boeing 747123 · Cargo/Baggage DoorsSDR UPS04441870Stiffener · corrodedINSPECTION TYPE: C, AFT OF BULK CARGO COMPT- RT STA 2200 STR 44 FRAME AFT ATT STIFFENER FOUND CORROSION. AFT OF BULK CARGO COMPT RT STA 2200 STR 44 FRAME AFT ATT STIFFENER REPLACED AS PER SRM 51-10-01 PG 8. DUE TO CORROSION BLEND OUT DEPTH 0.020 , WIDTH 1 &Jan 28, 2004 · N672UP · Boeing 747123 · Fuselage Miscellaneous StructureSDR UPS04441922Doubler · damagedINSPECTION TYPE:C EO747-5330-13494-H REPAIR ASSESSMENT PROGRAM DURING MARK ACCOMPLISH, TAR 106855 REPAIR AGAIN AT BS 1905-1913 STR 42R AFT CARGO DOOR AFT EDGE AREA WHICH MAY INTERFERE WITH THE EXISTING REPAIR AT ITEM N672-46-26, BS 1915-1920 STR 41-42R. EXPENJan 27, 2004 · N672UP · Boeing 747123 · Cargo/Baggage DoorsSDR UPS04441912Shear Tie · crackedINSPECTION TYPE: C, AFT OF BULK CARGO COMPT- RT STA 2220 IN BETWEEN STR 40 AND STR 44 SHEAR TIE ATTACH ANGLE FOUND CORROSION CRACKED. CORROSION BLEND OUT 0.071 X 1 X 3 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT. ANGLE REPAIRED PER SRM 51-40-03 FIG 2. CIC APPLIEDJan 27, 2004 · N672UP · Boeing 747123 · Fuselage Main, StructureSDR UPS04441905Skin · damagedINSPECTION TYPE:C DURING REPAIR ASSESSMENT PROGRAM ACCOMPLISH, ITEM N672-41-08 AT BS 447-463 STR 42R-44R 2 LAYERS REPAIR DOUBLER FOUND SINCE THE OUTER DOUBLER IS ONLY 0.040 INCH THK WHICH WILL CREATE KNIFE-EDGE CONDITION, RE-DO THE REPAIR REQUIRE. EXISTING DOJan 27, 2004 · N672UP · Boeing 747123 · Fuselage Main, Plate/SkinSDR UPS04441897Stringer · crackedINSPECTION TYPE: C, AFT OF BULK CARGO COMPT- RT STA 2180 - 2200 STRINGER L51 FOUND CRACKED. DEFECTIVE AREA STRINGER REPAIRED AS PER SRM 53-10-03 FIG 14.Jan 27, 2004 · N672UP · Boeing 747123 · Fuselage Main, Longeron/StringerSDR UPS04441893Frame · crackedINSPECTION TYPE: C, SECTION 41, FS 250 BETWEEN STR 40L - 41L, FRAME WEB CRACKED BS 260 CANTED BULKHEAD WEB SEGMENT BETWEEN STR 38L AND STR 41L. REPLACED AS PER HX RS R-53-13-35101 AND UPS ENGINEERING FILE NUMBER 747-53-20167.Jan 27, 2004 · N672UP · Boeing 747123 · Fuselage Main, FrameSDR UPS04441871Stiffener · crackedINSPECTION TYPE: C, AFT OF BULK CARGO COMPT- LT STA 2160 STRINGER 40 STIFFENER ANGLE FOUND CRACKED. AFT OF BULK CARGO LT STA 2160 FRAME AT STRINGER 40 STIFFENER ANGLE REPLACED AS PER SRM 51-10-01 PG 8.Jan 27, 2004 · N672UP · Boeing 747123 · Fuselage Miscellaneous StructureSDR UPS04441863Floorbeam · corrodedINSPECTION TYPE:C M/D- RT STA 2240 FLOORBEAM LOWER SECTION FOUND CORRODED IN BETWEEN RBL 6 AND RBL 40. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.050 X 1 X 2 INCH EXCEED SRM 53-10-01 LIMITS. STA 2240 RBL 30 FLOORBEAM LOWER SECTION REPAIRED ASJan 27, 2004 · N672UP · Boeing 747123 · Fuselage Main, Floor BeamSDR UPS04441808Shear Tie · crackedINSPECTION TYPE: C, AFT CARGO COMPT - LT STA 1680 IN BETWEEN STR 45 AND STR 46 SHEAR TIE FOUND CRACKED. AFT CARGO COMPT BS 1680 BETWEEN STR 45L AND STR 46L SHEAR TIE REPAIR CARRIED OUT IAW SRM 53-10-04 FIG 3.Jan 27, 2004 · N672UP · Boeing 747123 · Fuselage Main, StructureSDR UPS04441900Strap · damagedINSPECTION TYPE: C, FX SKIN BUTT JOINT SPLICE STRAP OVAL HOLES FOUND AFTER REPAIR PATCH REMOVED AT FS 2180- 2181 ON BOTH SIDE OF STR 50R. FX SKIN BUTT JOINT SPLICE STRAP REPAIRED AT BS 2180-2181 ON BOTH SIDE OF STR 50R AREA AS PER RS R-53-61-35105 AND UPS ENJan 26, 2004 · N672UP · Boeing 747123 · Fuselage Main, Plate/SkinSDR UPS04441841Shear Tie · corrodedINSPECTION TYPE: C, AFT CARGO BILGE AREA - FX 1820, STR 44R - 46R SHEAR TIES CORRODED. BS 1820 TO 1820, STR R44-R46 CORROSION REMOVED IAW SRM 51-10-01, CORROSION BLEND OUT 0.040 INCH X 0.5 INCH X 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. FLANGE REPAIRED REFEJan 26, 2004 · N672UP · Boeing 747123 · Fuselage Main, StructureSDR UPS04441809Shear Tie · crackedINSPECTION TYPE:C AFT CARGO BILGE AREA - FS 1700, STR 49L - 50L SHEAR TIE CRACKED. AFT CARGO COMPT BS 1700 BETWEEN STR 49L AND STR 50L SHEAR TIE REPAIR CARRIED OUT IAW SRM 53-10-04 FIG 3.Jan 26, 2004 · N672UP · Boeing 747123 · Fuselage Main, StructureSDR UPS04441806Shear Tie · crackedINSPECTION TYPE: C, AFT CARGO BILGE AREA - FS 1680, STR S47L - 48L SHEAR TIE CRACKED. AFT CARGO COMPT BS 1680 BETWEEN STR 47L AND STR 48L SHEAR TIE REPAIR CARRIED OUT IAW SRM 53-10-04 FIG 3.Jan 26, 2004 · N672UP · Boeing 747123 · Fuselage Main, StructureSDR UPS04441802Shear Tie · crackedINSPECTION TYPE:C AFT CARGO BILGE AREA - FS 1720, STR 49R - 51R SHEAR TIES CRACKED. AFT CARGO COMPT BS 1720 STR 49R - STR 51R SHEAR TIE REPAIR CARRIED OUT IAW SRM 53-10-04 FIG 3.Jan 26, 2004 · N672UP · Boeing 747123 · Fuselage Main, StructureSDR UPS04441936Fitting · corrodedNR 4 PYLON DIAGONAL BRACE UNDERWING FITTING, HOLE NR 10 I/B ROW MOST AFT CORROSION FOUND ON BACKUP FITTING BORE AREA. DEFECTIVE AREA FASTENER HOLE CORROSION REPAIR CARRIED OUT AS PER HX RS R57-24-35102 AND EO B747-5740-19955-A. FINAL HOLE 0.562 INCH TO CLEANJan 25, 2004 · N672UP · Boeing 747123 · Nacelle/Pylon, Attach FittingsSDR UPS04441923Strap · crackedINSPECTION TYPE:C BS 1241 LEFT BULKHEAD SPLICE STRAP AFT HOLE FOUND CRACKS AT FWD AND AFT SIDE. BS 1241 LEFT BULKHEAD SPLICE STRAP WILL BE REPLACED WITHIN 2 YEARS AFTER CRACK DISCOVERY AS PER EO B747-5310-0323 PARA D (3).Jan 25, 2004 · N672UP · Boeing 747123 · Fuselage Main, BulkheadSDR UPS04441910Panel · crackedINSPECTION TYPE: C, M/D- BS 1238 - 1265 LBL 75.92 - 95.58 CLOSEOUT PANEL CRACKED. REPAIRED CLOSEOUT PANEL PER EO 747-5310-2758 APP-C. ALL RELATED STEPS RESTORED TO NORMAL CONFIGURATION.Jan 25, 2004 · N672UP · Boeing 747123 · Fuselage Main, Plate/SkinSDR UPS04441908Fitting · corrodedINSPECTION TYPE: C, NR 3 PYLON DIAGONAL BRACE FWD ATTACH FITTING BASE AREA PITTING CORROSION FOUND. NR 3 PYLON DIAGONAL BRACE ATTACH FITTING LOWER SURFACE CORROSION REPAIR CARRIED OUT AS PER HX RS R-54-54-35098. (FAA 8110-3 DATED FEB 5, 2004 & EO B747-5440-Jan 25, 2004 · N672UP · Boeing 747123 · Nacelle/Pylon, Attach FittingsSDR UPS04441902Reveal · crackedINSPECTION TYPE:C M/D- R4 DOOR CUTOUT FWD REVEAL CRACK, BETWEEN STRINGER 17 & 18 (BS 1662-1664, STR R17, R18). REPLACED DOOR CUTOUT FWD REVEAL PER SRM 51-10-01 PG 8. DOOR RIGGING & ADJUSTMENT DONE RESULT: SATISFACTORY PER MM 52-10-00.Jan 25, 2004 · N672UP · Boeing 747123 · Fuselage Miscellaneous StructureSDR UPS04441899Fitting · crackedINSPECTION TYPE:C BS 1241 RT CANTED PRESSURE DECK FITTING AFT HOLE FOUND CRACK APPROX 0.030 INCH RUNNING DOWN. BS 1241 RT CANTED P/D FITTING AFT BOLT HOLE REPAIRED PER RS R53-41-35107 & ENG'R FILE 747-53-20170, REPAIR IS CONSIDERED A TIME-LIMITED REPAIR 2 YEAJan 25, 2004 · N672UP · Boeing 747123 · Fuselage Main, Attach FittingsSDR UPS04441805Frame · crackedINSPECTION TYPE:C STA 1700 FRAME FOUND CRACK BETWEEN S-10 / S-11L. BS 1700 BETWEEN STR 10L AND STR 11L FRAME REPAIR CARRIED OUT IAW SRM 53-10-04 FIG 1.Jan 25, 2004 · N672UP · Boeing 747123 · Fuselage Main, FrameSDR UPS04441803Frame · crackedINSPECTION TYPE:C BS 1438 S-13 / S-14R FRAME CRACKED. BS 1438 BETWEEN S13R AND S14R FRAME REPAIR CARRIED OUT IAW SRM 53-10-04 FIG 1.Jan 25, 2004 · N672UP · Boeing 747123 · Fuselage Main, FrameSDR UPS04441800Shear Tie · crackedINSPECTION TYPE:C BS 960 LT BETWEEN STR 7L AND 6L SHEAR TIE FOUND CRACK. BS 960 LT FRAME BETWEEN S6L AND 7L SHEAR TIE REPAIR CARRIED OUT IAW SRM 53-10-04 FIG 4.Jan 25, 2004 · N672UP · Boeing 747123 · Fuselage Main, StructureSDR UPS04441799Stringer · crackedINSPECTION TYPE:C S-7L STRINGER FOUND CRACK AT STA 1349 STR 7L STRINGER REPAIR CARRIED OUT IAW SRM 53-10-03 FIG 5.Jan 25, 2004 · N672UP · Boeing 747123 · Fuselage Main, Longeron/StringerSDR UPS04441798Stringer · crackedINSPECTION TYPE:C M/D - BS 960 TO 980 LT STR 2AL STRINGER FOUND CRACK. BS 960 - BS 980 STR 2AL STRINGER REPAIR CARRIED OUT IAW SRM 53-10- 03 FIG 4.Jan 25, 2004 · N672UP · Boeing 747123 · Fuselage Main, Longeron/StringerSDR UPS04441935Floorbeam · corrodedINSPECTION TYPE: C, M/D - BS 2150 RBL 108 FLOOR SUPPORT FOUND CORRODED. FLOOR SUPPORT REPAIRED AS PER SRM 51-40-04 FIG 2. CORROSION BLEND OUT 0.030 X 1 X 2 INCH, EXCEED SRM LIMIT.Jan 24, 2004 · N672UP · Boeing 747123 · Fuselage Main, Floor BeamSDR UPS04441914Floor Support · corrodedINSPECTION TYPE:C M/D- BS 2240 TP 2270 LBL 80 FLOOR SUPPORT FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.030 X 1 X 1 EXCEED SRM 53-10-01 FIG 1 LIMITS. FLOOR SUPPORT REPLACED PER SRM 51-10-01 PG 8. CIC APPLIED IAW CPM53-10-17.Jan 24, 2004 · N672UP · Boeing 747123 · Fuselage Miscellaneous StructureSDR UPS04441807Attach Angle · crackedINSPECTION TYPE:C FWD CARGO COMPT - LT STA 900 IN BETWEEN STR 43 AND STR 44 SHEAR TIE ATTACH ANGLE FOUND CRACKED. FWD CARGO COMPT BS 900 BETWEEN STR 43L AND STR 44L SHEAR TIE REPAIR CARRIED OUT IAW SRM 53-10-04 FIG 3.Jan 24, 2004 · N672UP · Boeing 747123 · Fuselage Main, StructureSDR UPS04441793Frame · crackedINSPECTION TYPE: C, FWD CARGO COMPT - RT STA 980 IN BETWEEN STR 41 AND STR 42 FRAME FOUND CRACKED. FRAME REPAIRED AS PER SRM 53-10-04 FIG 52 AT FWD CARGO COMPT RT STA 980 BETWEEN STR 41 AND STR 42.Jan 24, 2004 · N672UP · Boeing 747123 · Fuselage Main, StructureSDR UPS04441862Channel · corrodedINSPECTION TYPE: C, M/D- BS 2315 LBL 11 TO LBL 38 HAT SECTION FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.030 X 1 X 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. HAT SECTION REPLACED AS PER SRM 51-10-01 PG 8. P/N: BAC1509-100312-70Jan 23, 2004 · N672UP · Boeing 747123 · Fuselage Miscellaneous StructureSDR UPS04441861Channel · corrodedINSPECTION TYPE: C, M/D- BS 2320 TO 2350 LBL 40 HAT SECTION FOUND CORROSION. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.040 X 1 X 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. HAT SECTION REPLACED PER SRM 51-10-01 PG 8 & P/N: BAC1509-100312-7075TJan 23, 2004 · N672UP · Boeing 747123 · Fuselage Miscellaneous StructureSDR UPS04441859Stringer · corrodedINSPECTION TYPE: C, FWD CARGO COMPT- LT STA 720 - STA 740 STRINGER 47 FOUND CORROSION. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.030 X 1 X 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1. CIC APPLIED IAWJan 23, 2004 · N672UP · Boeing 747123 · Fuselage Main, Longeron/StringerSDR UPS04441842Forging · corrodedINSPECTION TYPE:C M/D- BS 1560-1580 LT WINDOW FORGING AFT EDGE ATT SKIN FOUND CORROSION REVEALED. BS 1560-1580, STR L19-L22 CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.030 INCH X 1 INCH X 1 INCH EXCEED SRM 53-30-01 FIG 1 LIMIT. WINDOW FORGING Jan 23, 2004 · N672UP · Boeing 747123 · Fuselage Main, StructureSDR UPS04441804Frame · crackedINSPECTION TYPE:C NR 4 PYLON - LOWER CAVITY NEAR NAC STA 211 RT VERT SUPPORT RIB CRACKED. NR 4 PYLON - LOWER CAVITY NEAR NAC 221 RT VERTICAL SUPPORT FRAME REPLACED AS PER SRM 51-10-01 PAGE 8.Jan 23, 2004 · N672UP · Boeing 747123 · Nacelle/Pylon, Frame/Spar/RibSDR UPS04441924Strap · crackedINSPECTION TYPE:C RIGHT WLG W/W - BS 1241 SPLICE STRAP AFT HOLE CRACK. AFT BOLT HOLE REPAIRED AS PER RS R53-41-35107, RIGHT STA 1241 SPLICE STRAP WILL BE REPLACED WITHIN 2 YEARS AFTER CRACK DISCOVERY AS PER EO B747-5310-0323 PARA D (3).Jan 22, 2004 · N672UP · Boeing 747123 · Fuselage Miscellaneous StructureSDR UPS04441907Skin · chafedINSPECTION TYPE:C EMP- RT AFT FUSELAGE UPPER EXTERNAL SKIN SURFACE FOUND CHAFING MARK AT STA 2280 TO STA 2360 , STR 2R TO 3R VERTICAL STABILIZER SEAL INTERFACE AREA (AS MARK). BS 2280-2360 STR 2R-3R AREA SKIN SMOOTHED OUT & REPROTECTED AS PER SRM 51-10-01 & 5Jan 22, 2004 · N672UP · Boeing 747123 · Fuselage Main, Plate/SkinSDR UPS04441904Skin · chafedINSPECTION TYPE:C EMP- LT AFT FUSELAGE UPPER EXTERNAL SKIN SURFACE FOUND CHAFING MARK AT STA 2280 TO STA 2360 STR 2L TO STR 3L VERTICAL STABILIZER SEAL INTERFACE AREA (AS MARK). BS 2280-2360 STR 2L-4L AREA SKIN SMOOTHED OUT & REPROTECTED AS PER SRM 51-10-01 &Jan 22, 2004 · N672UP · Boeing 747123 · Fuselage Main, Plate/SkinSDR UPS04441913Stringer · crackedINSPECTION TYPE:C FWD CARGO COMPT- RT STA 790- STA 810 STRINGER 46 FOUND CORROSION CRACKED. CORROSION REMOVED IAW SRM 51-10-01, CORROSION BLEND OUT 0.050 X 1 X 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. STRINGER REPAIRED PER HX RS R53-21-35100 & UPS ENGINEERIJan 21, 2004 · N672UP · Boeing 747123 · Fuselage Main, Longeron/StringerSDR UPS04441911Frame · crackedINSPECTION TYPE:C M/D- BS 380 RT STR 25R FRAME FOUND CRACKED. REPAIRED FRAME PER RS 53-12-35103 AT BS 380 STR 25R AREA AND EO B747-5310-19928-A.Jan 21, 2004 · N672UP · Boeing 747123 · Fuselage Main, FrameSDR UPS04441909Stringer · crackedINSPECTION TYPE:C FWD CARGO COMPT- LT STA 820 - STA 840 STRINGER 47 FOUND CORROSION CRACKED. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.040 X 1 X 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. STRINGER TRIMMED OUT AS PER SRM 53-10-03 FIG 1. CIC APJan 21, 2004 · N672UP · Boeing 747123 · Fuselage Main, Longeron/StringerSDR UPS04441892Web · crackedINSPECTION TYPE: C, M/D - BS 270 LT STR 26L VERTICAL SUPPORT WEB FOUND CRACKED. REPAIRED VERTICAL SUPPORT WEB PER SRM 51-40-02 FIG 1.Jan 21, 2004 · N672UP · Boeing 747123 · Fuselage Miscellaneous StructureSDR UPS04441864Web · crackedINSPECTION TYPE: C, M/D- BS 270 RT STR 26R VERTICAL SUPPORT WEB FOUND CRACKED. REPAIRED VERTICAL SUPPORT WEB PER SRM 51-40-02 FIG 1.Jan 21, 2004 · N672UP · Boeing 747123 · Fuselage Miscellaneous StructureSDR UPS04441860Stringer · corrodedINSPECTION TYPE: C, FWD CARGO COMPT - RT STA 820 - STA 840 STRINGER 47 FOUND CORROSION CRACKED. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.040 X 1 X 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1. CIC APJan 21, 2004 · N672UP · Boeing 747123 · Fuselage Main, Longeron/StringerSDR UPS04441811Web · crackedINSPECTION TYPE: C, NR 2 PYLON - LWR WEB CRACKED THRU AFT RT LONGITUDINAL STIFFENER APPROX 15 INCHES FWD OF AFT MOUNT, CRACK RUNS LATERALLY. LWR SPAR WEB 5 LOCATIONS CRACK END BY STOP HOLE PRILLED AS PER SRM 54-10-03 FIG 2. NDT INSP NIL CRACKS AND PERFORMED Jan 21, 2004 · N672UP · Boeing 747123 · Nacelle/Pylon Miscellaneous StructureSDR UPS04441810Spar · crackedINSPECTION TYPE:C NR 2 PYLON - LWR WEB CRACKED THRU FASTENERS AFT OF PNEU DUCT CUTOUT APPROX 15 INCHES FWD OF AFT MOUNT, CRACK RUNS LONGITUDINALLY. LWR SPAR 5 LOCATIONS CRACK END BY STOP DRILLED HOLES PER SRM 54-10-03 FIG 2 NDT CONFIRMED NIL CRACKS AND PERFORJan 21, 2004 · N672UP · Boeing 747123 · Nacelle/Pylon, Main FrameSDR UPS03441269Module · inoperativeATB ON RETRACTION OF GEAR AFTER TAKEOFF THE RED GEAR AND DOOR OPEN LIGHTS WOULD NOT EXTINGUISH. THE RED GEAR LIGHT REMAINS ILLUM AND GEAR DOOR OPEN LIGHT ILLUM. BASED ON SOUND AND FEEL AT LEAST ONE DOOR AND OR GEAR WOULD NOT RETRACT. ACCOMPLISHED GEAR RETRASep 27, 2003 · N672UP · Boeing 747123 · Landing Gear Position and WarningSDR 03029Warning Light · illuminatedNR 4 ENGINE FIRE, AFTER SETTING CLIMB THRUST, NR 4 ENGINE FIRE LIGHT LIT AND BELL SOUNDED. CONFIRMED BOTH NR 4 NACELLE TEMP. INDICATORS PEGGED OUT HIGH. ACCOMPLISHED ENGINE FIRE SEVERE DAMAGE CHECKLIST WITH FIRE INDICATION OUT AFTER ONE BOTTLE. APPROXIMATELSep 26, 2003 · N673UP · Boeing 747123 · Fire DetectionSDR UPS03441156Engine · flamed outAT 1330Z INTO FLIGHT NR 4 ENG FLAMED OUT. COMPLY WITHIN FLIGHT ENGINE FAILURE/SHUTDOWN CK LIST. TRIED INFLIGHT START CK LIST AS THE ENG INDICATION WAS NORMAL WITH EXCEPTION OF NR 4 OIL TEMP BEING AROUND 100 DEG. REMOVED AND REPLACED MAIN FILTER, INSPECTED PAug 30, 2003 · N676UP · Boeing 747123 · Engine (Turbine/Turboprop)
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