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 UPS02439341Fitting · crackedINSPECTION TYPE:C LT BS 1480 BULKHEAD AREA HOLE NR 1 FOUND CRACK AT EXTENSION FITTING. LT BS 1480 BULKHEAD LONGERON EXTENSION FITTING NR 1 HOLE OVERSIZED AND CRACK FREE REPAIR BUSHING INSTALLED AS PER BS 747-53A2390 FIG 11.Aug 16, 2002 · N672UP · Boeing 747123 · Fuselage Miscellaneous StructureSDR UPS02439340Fitting · crackedINSPECTION TYPE:C LT BS 1480 BULKHEAD AREA HOLE NR 8 FOUND CRACK AT EXTENSION FITTING APPROX 0.06 INCH RUNNING FWD. LT BS 1480 BULKHEAD LONGERON EXTENSION FITTING NR 9 HOLE OVERSIZED AND CRACK FREE REPAIR BUSHING INSTALLED AS PER SB 747-53A2390 FIG 11.Aug 16, 2002 · N672UP · Boeing 747123 · Fuselage Miscellaneous StructureSDR UPS02439339Skin · crackedINSPECTION TYPE:C LT BS 1480 BULKHEAD HOLE NR 1 FOUND CRACK AT FUSE SKIN APPROX 0.06 INCH RUNNING FWD. LT BS 1480 BULKHEAD FUSE SKIN NR 1 BOLT HOLE OVERSIZED AND CRACK FREE REPAIR BUSHING INSTALLED AS PER SB 747-53A2390 FIG 11.Aug 16, 2002 · N672UP · Boeing 747123 · Fuselage Main, Plate/SkinSDR UPS02439338Splice · crackedINSPECTION TYPE:C LT BS 1480 BULKHEAD AREA HOLE NR 1 FOUND CRACK AT OUTER CHORD SPLICE FITTING, APPROX 0.04 INCH RUNNING FWD. LT BS 1480 BULKHEAD OUTER CHORD SPLICE FITTING NR 1 HOLE OVERSIZED AND CRACK FREE REPAIR BUSHING INSTALLED AS PER SB 747-53A2390 FIGAug 16, 2002 · N672UP · Boeing 747123 · Fuselage Main, BulkheadSDR UPS02439337Bulkhead · crackedINSPECTION TYPE:C LT BS 1480 BULKHEAD AREA HOLE NR 15 FOUND CRACK AT BULKHEAD WEB APPROX 0.03 INCH RUNNING O/B. LT BS 1480 BULKHEAD WEB NR 15 HOLE OVERSIZED AND CRACK FREE REPAIR BUSHING INSTALLED AS PER SB 747-53A2390 FIG 11.Aug 16, 2002 · N672UP · Boeing 747123 · Fuselage Main, BulkheadSDR UPS02439336Splice · crackedINSPECTION TYPE:C LT BS 1480 BULKHEAD AREA HOLE NR 16 FOUND CRACK AT WEB SPLICE PLATE, APPROX .125 INCH, RUNNING O/B. LT BS 1480 BULKHEAD WEB SPLICE PLATE NR 16 HOLE OVERSIZED AND CRACK FREE REPAIR BUSHING INSTALLED AS PER SB 747-3A2390 FIG 11.Aug 16, 2002 · N672UP · Boeing 747123 · Fuselage Main, BulkheadSDR UPS02439335Splice · crackedINSPECTION TYPE:C LT BS 1480 BULKHEAD AREA HOLE NR 15 FOUND CRACK AT OUTER CHORD SPLICE FITTING, APPROX 0.030 INCH. LT BS 1480 BULKHEAD OUTER CHORD SPLICE FITTING NR 15 HOLE OVERSIZED AND CRACK FREE REPAIR BUSHING INSTALLED AS PER SB 74753A2390 FIG 11.Aug 16, 2002 · N672UP · Boeing 747123 · Fuselage Main, BulkheadSDR UPS02439334Bulkhead · crackedINSPECTION TYPE:C LT BS 1480 BULKHEAD AREA HOLE NR 1 FOUND CRACK AT BULKHEAD CHORD, APPROX 0.06 INCH RUNNING FWD. LT BS 1480 BULKHEAD CHORD NR 1 HOLE OVERSIZED AND CRACK FREE REPAIR BUSHING INSTALLED AS PER SB 747-53A2390 FIG 11.Aug 16, 2002 · N672UP · Boeing 747123 · Fuselage Main, BulkheadSDR UPS02439333Splice · crackedINSPECTION TYPE:C LT BS 1480 BULKHEAD AREA HOLE NR 15 FOUND CRACK AT WEB SPLICE PLATE , APPROX 0.02 INCH RUNNING O/B. LT 1480 BULKHEAD WEB SPLICE PLATE NR 15 HOLE OVERSIZED AND CRACK FREE REPAIR BUSHING INSTALLED AS PER SB 747-53A2390 FIG11.Aug 16, 2002 · N672UP · Boeing 747123 · Fuselage Main, BulkheadSDR UPS02439268Pressure Panel · crackedINSPECTION TYPE:C RT LG W/W O/B PRESSURE DECK LWR FACE AT BS 1416 LATERAL O/B NR 2 RIVET HOLE AREA CRACKED TO EDGE. SECTION OF PRESSURE WEB AT RT LG W/W O/B FROM STA 1400 TO 1438 RBL 110 TO MOST O/B AREA REPLACED AS PER SRM 51-10-01 PG 8.Aug 16, 2002 · N672UP · Boeing 747123 · Fuselage Main, BulkheadSDR UPS02439210Floorbeam · corrodedINSPECTION TYPE:C, COCKPIT - BS 340 LBL 100 FLOORBEAM UPPER CHORD FOUND CORRODED. CORROSION REMOVED IAW 51-10-01, CORROSION BLEND OUT EXCEEDS SRM LIMIT. FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 53-10-07 FIG 23.Aug 16, 2002 · N672UP · Boeing 747123 · Fuselage Main, Floor BeamSDR UPS02439205Seat Track · corrodedINSPECTION TYPE:C UPPER DECK BS 550 LBL 50 SEAT TRACK CROWN FOUND CORRODED. CORROSION BLEND OUT EXCEEDS SRM LIMIT. SEAT TRACK REPLACED AS PER SRM 51-10-01 PG 8.Aug 16, 2002 · N672UP · Boeing 747123 · Fuselage, Seat/Cargo Attach FittingsSDR UPS02439203Floor Support · corrodedINSPECTION TYPE:C UPPER DECK STA 420-440 BL 0 FLOOR SUPPORT CORRODED. CORROSION BLEND OUT EXCEEDS SRM LIMIT. FLOOR SUPPORT REPLACED AS PER SRM 51-10-01 PG 8.Aug 16, 2002 · N672UP · Boeing 747123 · Fuselage Miscellaneous StructureSDR UPS02439188Seat Track · corrodedINSPECTION TYPE:C, UPPER DECK BS 560 - 580 LBL 30 SEAT TRACK CROWN FOUND CORROSION. CORROSION BLEND OUT EXCEEDS SRM LIMIT. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 6.Aug 16, 2002 · N672UP · Boeing 747123 · Fuselage, Seat/Cargo Attach FittingsSDR UPS02439183Seat Track · corrodedINSPECTION TYPE:C UPPER DECK BS 520 - 540 LBL 65 SEAT TRACK CROWN FOUND CORROSION. CORROSION BLEND OUT EXCEEDS SRM LIMIT. SEAT TRACK REPAIR AS PER SRM 53-10-05 FIG 6.Aug 16, 2002 · N672UP · Boeing 747123 · Fuselage, Seat/Cargo Attach FittingsSDR UPS02439181Floorbeam · crackedINSPECTION TYPE:C BS 360 UPPER DECK FLOORBEAM UPPER CHORD, 2 FASTENER HOLES CRACK REVEALED AT RBL 28 & RBL 43 RESPECTIVELY. UPPER DECK BS 360 RBL 28 CRACKED HOLE CRACK REMOVED AS PER EO B747-5320-12407-C APPENDIX D. NO NECESSARY REPAIR. RBL 43 CRACKED FASTEAug 16, 2002 · N672UP · Boeing 747123 · Fuselage Main, Floor BeamSDR UPS02439180Floorbeam · crackedINSPECTION TYPE:C BS 340 UPPER DECK FLOORBEAM UPPER CHORD, THREE FASTENER HOLES CRACKED, REVEALED AT LBL 18, RBL 15 & RBL 46 RESPECTIVELY. UPPER DECK BS 300 FLOORBEAM LBL 18 & RBL 15 CRACKED HOLE REF NRC 7305 SECTIONAL REPLACED FROM RBL 20 TO LBL 40 AS PER SRAug 16, 2002 · N672UP · Boeing 747123 · Fuselage Main, Floor BeamSDR UPS02439179Floorbeam · crackedINSPECTION TYPE:C BS 380 UPPER DECK FLOORBEAM UPPER CHORD, 1 FASTENER HOLE CRACK REVEALED AT RBL 60, RUNNING AFT APPROX .0625 INCH LENGTH. UPPER DECK BS 380 FLOORBEAM RBL 60 CRACKED HOLE REPAIRED AS PER EO B747-5320-12407-C APPENDIX D PLAN A.Aug 16, 2002 · N672UP · Boeing 747123 · Fuselage Main, Floor BeamSDR UPS02439161Attach Angle · crackedINSPECTION TYPE:C COCKPIT BS 340 - 360 CTR INTERCOSTAL WEB ATT ANGLE CRACKED. ATT ANGLE REPLACED AS PER SRM 51-10-01 PAGE 8.Aug 16, 2002 · N672UP · Boeing 747123 · Fuselage Miscellaneous StructureSDR UPS02439376Frame · corrodedINSPECTION TYPE:C LT LG W/W O/B BS 1438 WEB LWR END ADJACENT OVERWING LONGERON I/B AREA HEAVY CORROSION FOUND. CORROSION BLEND OUT EXCEEDED SRM LIMIT, FRAME WEB REPAIRED AS PER SRM 51-40-03 FIG 1.Aug 15, 2002 · N672UP · Boeing 747123 · Fuselage Main, FrameSDR UPS02439373Bulkhead · crackedINSPECTION TYPE:C CRACK FOUND ON NR 3 NACELLE STRUT REAR MOUNT BULKHEAD AFT O/B WEB APPROX .5 INCH LONG AND STOPPED AT FASTENER HOLE. NR 3 NACELLE STRUT REAR MOUNT BULKHEAD REPAIRED AS PER RS R54-53-34880 UPS EO NR 747-54-20029.Aug 15, 2002 · N672UP · Boeing 747123 · Nacelle/Pylon, Bulkhead/FirewallSDR UPS02439365Longeron · corrodedINSPECTION TYPE:C LT LG W/W O/B, OVERWING LONGERON BETWEEN BS 1436 AND 1446 I/B LWR SURFACE CORRODED AS MARKED. LONGERON FOUND CORRODED AT LOCATION BS 1436 TO 1445 LBL L118 TO L122 CORROSION BLEND OUT EXCEEDEDS SRM LIMIT REPLACED AS PER SRM 51-10-01. HX RSRS Aug 15, 2002 · N672UP · Boeing 747123 · Fuselage Main, Longeron/StringerSDR UPS02439353Splice · crackedINSPECTION TYPE:C RT BS 1480 BULKHEAD NR 24 HOLE FOUND CRACK AT WEB SPLICE PLATE RUNNING I/B APPROX 0.09 AND O/B APPROX .125. THE WEB SPLICE PL ATE CHANGED AS PER SB 747-53A2390. REFER HX RS R-53-43-34884 AND UPS EO B747-5310-17499-A.Aug 15, 2002 · N672UP · Boeing 747123 · Fuselage Main, BulkheadSDR UPS02439318Bulkhead · crackedINSPECTION TYPE:C CRACKS FOUND ON NR 4 NACELLE STRUT REAR MOUNT FWD AND AFT WEBS. NR 4 NACELLE STRUT REAR MOUNT BULKHEAD REPAIRED AS PER RS R54-53-34881 & UPS ENGINEERING FILE NUMBER 747-54-20030.Aug 15, 2002 · N672UP · Boeing 747123 · Nacelle/Pylon, Bulkhead/FirewallSDR UPS02439310Bulkhead · crackedINSPECTION TYPE:C FUSELAGE RT TUNNEL STA 260 CANTED BULKHEAD WEB RADIUS CRACKED AT WL 180 RBL 70. FUSELAGE RT TUNNEL STA 260 CANTED BULKHEAD WEB RADIUS CRACKED AREA REPAIRED AS PER SRM 53-10-04 FIG 6.Aug 15, 2002 · N672UP · Boeing 747123 · Fuselage Main, BulkheadSDR UPS02439374Reveal · crackedINSPECTION TYPE:C RT BS 2231 FRAME Y STR 24 & STR 25 FOUND 2EA FASTENER HOLES CRACKED AT REVEAL. RT BS 2231 FRAME BETWEEN STR 24R TO STR 25R 2EA FASTENER HOLES CRACKED AT REVEAL REPAIRED AS PER SRM 53-10-04 FIGURE 115.Aug 14, 2002 · N672UP · Boeing 747123 · Fuselage Miscellaneous StructureSDR UPS02439278Panel · wornINSPECTION TYPE:C NR 3 PYLON - O/B AFT UPPER MOUNT HALF MOON PANEL CUTOUT WORN AT FWD PORTION. NR 3 PYLON O/B AFT UPPER MOUNT HALF MOON PANEL CUTOUT REPAIRED AS PER SRM 54-30-03 FIG 35 AND FIG 36.Aug 14, 2002 · N672UP · Boeing 747123 · Nacelle/Pylon, Plate/SkinSDR UPS02439217Frame · crackedINSPECTION TYPE:C, M/D BS 540 S24L FRAME FOUND CRACKED. M/D BS 540 S24L FRAME REPAIRED AS PER SRM 53-10-04 FIGURE 15.Aug 14, 2002 · N672UP · Boeing 747123 · Fuselage Main, FrameSDR UPS02439212Floor Support · corrodedINSPECTION TYPE:C, M/D - FLOOR SUPPORT FOUND CORRODED AT STA 240 LBL 4 - LBL 5. CORROSION REMOVED IAW 51-10-01, CORROSION BLEND OUT EXCEEDS SRM LIMIT. FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 53-10-07 FIG 8.Aug 14, 2002 · N672UP · Boeing 747123 · Fuselage Miscellaneous StructureSDR UPS02439202Seat Track · corrodedINSPECTION TYPE:C M/D - STA 476-480 LBL 32 SEAT TRACK FLANGE FOUND CORRODED. CORROSION BLEND OUT EXCEEDS SRM LIMIT. BS 460-510 LBL 32 SEAT TRACK REPLACED AS PER SRM 51-10-01.Aug 14, 2002 · N672UP · Boeing 747123 · Fuselage, Seat/Cargo Attach FittingsSDR UPS02439201Seat Track · corrodedINSPECTION TYPE:C M/D - SEAT TRACK FLANGE FOUND CORRODED AT STA 480-500 RBL 85. CORROSION BLEND OUT EXCEEDS SRM LIMIT. SEAT TRACK REPLACED AS PER SRM 51-10-01 PG 8.Aug 14, 2002 · N672UP · Boeing 747123 · Fuselage, Seat/Cargo Attach FittingsSDR UPS02439193Seat Track · corrodedINSPECTION TYPE:C M/D - STA 506 LBL 70 SEAT TRACK FLANGE FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT EXCEEDS SRM LIMIT. O/B SPLICE ANGLE REPLACED AS PER SRM 51-10-01 PG 8.Aug 14, 2002 · N672UP · Boeing 747123 · Fuselage, Seat/Cargo Attach FittingsSDR UPS02439355Frame · crackedINSPECTION TYPE:C M/D - BS 360 S23R FRAME FOUND CRACKED. M/D BS 360 S23R FRAME REPAIR CARRIED OUT AS PER HX RS NR R53-12-34879 AND UPS EO B747-5310-17492-A.Aug 13, 2002 · N672UP · Boeing 747123 · Fuselage Main, FrameSDR UPS02439317Tie Clip · crackedINSPECTION TYPE:C M/D BS 320 S-13AL TIE CLIP FOUND CRACKED. CLIP REPLACED AS PER SRM 51-10-01 PG. 8.Aug 13, 2002 · N672UP · Boeing 747123 · Fuselage Miscellaneous StructureSDR UPS02439311Intercostal · crackedINSPECTION TYPE:C M/D - BS 1220 LBL 112 BELOW FLOOR, INTERCOSTAL WEB FOUND CRACKED. M/D - BS 1220 LBL 112 BELOW FLOOR INTERCOSTAL WEB CRACK STOP DRILLED AND REPAIRED AS PER SRM 51-40-02 FIG 1.Aug 13, 2002 · N672UP · Boeing 747123 · Fuselage Miscellaneous StructureSDR UPS02439273Web · crackedINSPECTION TYPE:C M/D - BS 390 S-14R WEB FOUND CRACKED. M/D BS 380-400 STR 14R WEB REPAIRED AS PER SRM 53-10-04 FIG 55.Aug 13, 2002 · N672UP · Boeing 747123 · Fuselage Miscellaneous StructureSDR UPS02439224Doubler · crackedINSPECTION TYPE:C, M/D BS 360 S-24A FRAME DOUBLER FOUND CRACKED. M/D BS 360 STR 24AL FRAME DOUBLER REPLACED AS PER SRM 51-10-01 PAGE 8.Aug 13, 2002 · N672UP · Boeing 747123 · Fuselage Miscellaneous StructureSDR UPS02439200Seat Track · corrodedINSPECTION TYPE:C M/D - BS 260 LBL 30 SEAT TRACK I/B FLANGE FOUND CORROSION. CORROSION BLEND OUT EXCEEDS SRM LIMIT. SEAT TRACK I/B FLANGE REPAIRED AS PER SRM 53-10-05 FIG 16.Aug 13, 2002 · N672UP · Boeing 747123 · Fuselage, Seat/Cargo Attach FittingsSDR UPS02439192Floor Support · corrodedINSPECTION TYPE:C M/D - FLOOR SUPPORT FOUND CORROSION. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT EXCEEDS SRM LIMIT. FLOOR SUPPORT REPAIRED AS PER SRM 51-40-04 FIG 4.Aug 13, 2002 · N672UP · Boeing 747123 · Fuselage Miscellaneous StructureSDR UPS02439379Skin · damagedINSPECTION TYPE:C FUSELAGE - AFT CARGO DOOR FWD CUTOUT SKIN PORTION TRIMMED OFF AT BS 1810 STR 39R-40R. FUSELAGE SKIN REPAIRED AS PER SRM 53-30-03 FIG 19.Aug 12, 2002 · N672UP · Boeing 747123 · Fuselage Main, Plate/SkinSDR UPS02439315Doubler · crackedINSPECTION TYPE:C M/D L1 DOOR UPPER HINGE SKIN DOUBLER FOUND CRACKED. DOOR SKIN REPAIRED AS PER SB B747-52-2144 FIG 3.Aug 12, 2002 · N672UP · Boeing 747123 · Passenger/Crew DoorsSDR UPS02439314Doubler · crackedINSPECTION TYPE:C M/D R1 DOOR LOWER HINGE SKIN DOUBLER FOUND CRACKED. SKIN REPAIRED AS PER SB 747-52-2144 FIG 4.Aug 12, 2002 · N672UP · Boeing 747123 · Passenger/Crew DoorsSDR UPS02439281Panel · damagedINSPECTION TYPE:C INSPECT SPEED TAPE TWO .25 INCH HOLES LOCATED O/B & FWD OF THE WATER SERVICING PANEL PER SRM 51-40-09 FIG 1 SHT 3. FIBERGLASS REPAIRED AS PER SRM 51-40-15 FIG 7 AT EXT SURFACE.Aug 7, 2002 · N672UP · Boeing 747123 · Fuselage Main, Plate/SkinSDR UPS02438877Engine · malfunctionedINSPECTION TYPE:N/A, WHEN PACK LAND 3 WAS TURNED ON AFTER TAKEOFF OILY SMOKE FILLED THE FLIGHT DECK. PACK 1 AND 3 WAS TURNED OFF AND PACK 2 TURNED ON. SMOKE CLEARED AND FLIGHT CONTINUED TO PHL. REMOVED AND CLEANED NR 1 PACK COALESCER BAG. RAN PACKS FROM APJul 20, 2002 · N674UP · Boeing 747123 · Engine (Turbine/Turboprop)SDR UPS02438859Wedge · crackedINSPECTION TYPE:PFLT LT INBOARD MID FLAP IS CRACKED IN TWO PLACES. REPAIRED DAMAGED AREAS OF MID FLAP T/E WEDGE IAW EO B747-5750-17190A. ACCOMPLISH PERM REPAIR OF PART REPLACEMENT NO LATER THAN C-CHECK.Jul 20, 2002 · N672UP · Boeing 747123 · Trailing Edge FlapsSDR UPS02438796Fire Warning · intermittentINSPECTION TYPE:N/A, ON CLIMBOUT GOT A BTB TRIP ON NR 2 WITH MOMENTARY FLASH OF FIRE WARNING HAD GCU LT ON GEN PARALLEL SHOWED MOMENTARY FLUX ON AC VOLT. RESET PWR AOM OPS NORMAL REMAINDER OF FLIGHT. NOTED TO MMOC INFM NR 2 BTB OK WITH APU PWR AND FIRE WARNIJul 13, 2002 · N675UP · Boeing 747123 · Fire DetectionSDR UPS02438716Light · dirtyINSPECTION TYPE:PFLT EMERGENCY LIGHT OVER CREW SERVICE DOOR BULB INOP. CLEANED AND RESEATED CP AT UPPER LIGHT ASSY OPS CK OK.Jun 28, 2002 · N674UP · Boeing 747123 · Emergency LightingSDR UPS02438693Fire Warning · false indicationINSPECTION TYPE:N/A AFTER APPROX 1 HOUR IN CRUISE FLIGHT. A RED WARNING LIGHT ON THE OVERHEAD ILLUMINATED FOR A SPLIT SECOND. RESEATED ALL THE FIRE DET CARDS. TESTED SYSTEMS IAW MM 26-10-00, ALL TEST CHECKS GOOD.Jun 20, 2002 · N673UP · Boeing 747123 · Fire DetectionSDR UPS02438355Light · inoperativeINSPECTION TYPE:N/A OVERHEAD EMERGENCY LIGHT STA 405 ONLY REMAINS ILLUMINATED FOR APPROX 5 SEC. REMOVED AND REPLACED LIGHT PACK ASSY, OPS NORMAL.May 21, 2002 · N675UP · Boeing 747123 · Emergency LightingSDR UPS02438184Switch · inoperativeINSPECTION TYPE:PFLT EMERGENCY EXIT LIGHT SWITCH INOP. REMOVED AND REPLACED EMERGENCY LIGHT SWITCH MODULE. OPS CHECK GOOD.May 8, 2002 · N677UP · Boeing 747123 · Emergency Lighting
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