Boeing 747-123

Service difficulty reports · 2,292

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Query with SQL
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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR P5CA9600258Panel · disbondingFOUND LEFT HAND OUTBOARD FOREFLAP UPPER SURFACE REPAIR DISBONDING ABOVE NR 1 FLAP TRACK. REPAIRED DAMAGED AREA IAW SRM 51-40-06.Jun 22, 1996 · N859FT · Boeing 747123 · Trailing Edge FlapsSDR P5CA9600257Panel · puncturedFOUND HOLE IN LEFT WING PANEL, FORWARD OF INBOARD AILERON, OUTBOARD OF NR 2 PYLON. REPAIRED IAW SRM 51-40-09.Jun 22, 1996 · N859FT · Boeing 747123 · Wing, Plate/SkinSDR P5CA9600256Te Panel · delaminatedFOUND LEFT WING TRAILING EDGE PANEL DELAMINATED AT OUTBOARD END OF INBOARD FLAP WELL. APPLIED FIBERGLASS REPAIR IAW SRM 51-40-15.Jun 22, 1996 · N859FT · Boeing 747123 · Wing, Plate/SkinSDR P5CA9600255Panel · puncturedFOUND HOLE IN LEFT WING LEADING EDGE, LOWER SURFACE AT OUTBOARD HINGE OF VARIABLE CAMBER FLAP. REPAIRED IAW SRM 51-24-11.Jun 22, 1996 · N859FT · Boeing 747123 · Wing, Plate/SkinSDR P5CA9600254Left Squib · no testNR 2 ENGINE LEFT HAND SQUIB WOULD NOT TEST. REPAIRED BROKEN WIRE, OPS CHECK GOOD IAW MM 26-10-00.Jun 22, 1996 · N859FT · Boeing 747123 · Fire DetectionSDR P5CA9600253Service Panel · crackedFOUND NOSE LANDING GEAR SERVICE PANEL CRACKED ALONG LOWER EDGE. SANDED DAMAGED AREA, APPLIED FIBERGLASS REPAIR IAW SRM 51-40-08.Jun 22, 1996 · N859FT · Boeing 747123 · Service DoorsSDR P5CA9600252Access Door · puncturedFOUND HOLE IN FUELING PANEL ACCESS DOOR, RIGHT WING. SANDED DAMAGED AREA, REPAIRED IAW SRM 51-40-08.Jun 22, 1996 · N859FT · Boeing 747123 · Fluid Service DoorsSDR UPS96420405Lights · inoperativeINSPECTION TYPE N/A REF D111137, EMERGENCY LIGHT AT STA 580 LT CEILING MAIN DECK DIM. REPLACED EMERGENCY LIGHT ASSM (P/N 1356837) (S/N 19732) ON, (P/N 1356-10A) (S/N UPS 5) OFF, ILLUMINATION CHECKS GOOD.Jun 21, 1996 · N676UP · Boeing 747123 · Emergency LightingSDR P5CA9600251Flow Contl Unit · leakingDURING MAINTENANCE, FOUND PASSENGER O2 LOW. FOUND ELECTRO-PNEUMATIC FLOW CONTROL UNIT LEAKING INTERNALLY. REPLACED SAME IAW MM 35-21-00. ALSO, REPLACED AFT PASSENGER O2 BOTTLE, (P/N 801307-00), (S/N 962110) NO LEAKS NOTED.Jun 20, 1996 · N858FT · Boeing 747123 · Passenger Oxygen SystemSDR P5CA9600246Fire Warning · activatedON CLIMBOUT, FL 28.0 IAS 320 KTS, APU FIRE WARNING LIGHT AND BELL CAME ON. ALSO, ON PILOT'S OVERHEAD PANEL. DISCHARGED APU FIRE BOTTLE, LIGHT WENT OUT IN APPROX 8 SECONDS. ON LANDING, NO EVIDENCE OF FIRE IN APU AREA. WIRES INSPECTED AND FIRE TEST NORMAL PEJun 17, 1996 · N858FT · Boeing 747123 · Fire DetectionSDR P5CA9600250Coupling · leakingDURING MAINTENANCE, FOUND LEAK IN PASSENGER OXYGEN SYSTEM. REMOVED AND REPLACED COUPLING IAW MM 35-21-00, LEAK CHECK NORMAL.Jun 15, 1996 · N858FT · Boeing 747123 · Passenger Oxygen SystemSDR P5CA9600249Oxy Control Unit · leakingDURING MAINTENANCE, DISCOVERED LEAK IN CREW OXYGEN SYSTEM. REMOVED AND REPLACED CONTROL UNIT IAW MM 35-11-00, LEAK CHECK OK.Jun 15, 1996 · N858FT · Boeing 747123 · Crew Oxygen SystemSDR P5CA9600245Duct · crackedON PUSHBACK, NOTED WING LEADING EDGE OVERHEAT ON LEFT WING. WHEN ADP NR 1 WAS SELECTED, LIGHT WENT OUT. RETURNED TO BLOCKS. FOUND DUCT CRACKED AT BOSS FOR NR 2 PYLON BLEED AIR SENSE LINE, BOSS BLOWN OUT. REMOVED AND REPLACED DUCT ASSY, LEAK CHECK NORMAL PEJun 14, 1996 · N859FT · Boeing 747123 · Pneumatic Distribution SystemSDR P5CA9600243Regulator · inoperativeSECOND OBSERVER'S O2 REGULATOR HAD NO FLOW. REMOVED AND REPLACED REGULATOR AS PER MM 35-11-07.Jun 7, 1996 · N859FT · Boeing 747123 · Crew Oxygen SystemSDR UPS96420227Seat Track · damagedINSPECTION TYPE: C. FOUND CROWN AREA FROM SEAT TRACK AT BSTA 1720 - 1740 LBL 25 DAMAGED. REPLACED SEAT TRACK IAW SRM 53-10-23 FIG 5/51-30-02.May 22, 1996 · N673UP · Boeing 747123 · Fuselage, Seat/Cargo Attach FittingsSDR UPS96420230Shear Tie · crackedINSPECTION TYPE: C. FOUND SHEAR TIE CRACKED AT STA 1740 RT SIDE BETWEEN STR 50 AND STR 51. REPAIRED SHEARED TIE IAW SRM 53-10-04, FIG 3.May 20, 1996 · N673UP · Boeing 747123 · Fuselage Miscellaneous StructureSDR P5CA9600232Comp Blades · bird strikeUPON INSPECTION OF NR 1 ENGINE DURING MAINTENANCE, FOUND EVIDENCE OF BIRD STRIKE ON FAN BLADES AND FAN EXIT DIAPHRAGM. COMPLIED WITH CONDITIONAL INSPECTION PER 5-51-14 AND BORESCOPE INSPECTION PER MM 72-00-00. FOUND 6 EACH 5TH STAGE COMPRESSOR BLADES BENT BEYMay 20, 1996 · N858FT · Boeing 747123 · Turbine Engine Compressor SectionSDR UPS96420237Frame · corrodedINSPECTION TYPE: C. AFT CARGO FRAME TOP CAP AT STA 1820, BBL 26L - 42L. REPAIRED IAW SRM 51-40-03.May 18, 1996 · N673UP · Boeing 747123 · Fuselage Main, FrameSDR UPS96420233Shear Tie · crackedINSPECTION TYPE: C. BULK CARGO COMPARTMENT FOUND CRACKED IN FRAME SHEAR TIE AT STRINGER CUTOUT AT BS 2160, S42/44 LT. REPAIRED SHEAR TIE IAW SRM 53-10-01.May 17, 1996 · N673UP · Boeing 747123 · Fuselage Miscellaneous StructureSDR UPS96420232Stringer · crackedINSPECTION TYPE: C. FOUND CRACK IN FRAME STRINGER CUT-OUT AT BS 2100 S29R. REPAIRED FRAME IAW SRM 53-10-04.May 17, 1996 · N673UP · Boeing 747123 · Fuselage Main, Longeron/StringerSDR UPS96420198Splice · corrodedINSPECTION TYPE-C, CORROSION ON STRINGER SPLICE END STRAP AT STA 2350, S-50 LT. REPLACED STRINGER SPLICE END STRAP IAW SRM 51-30-02.May 17, 1996 · N673UP · Boeing 747123 · Fuselage Miscellaneous StructureSDR UPS96420197Splice · corrodedINSPECTION TYPE-C, CORROSION ON STRINGER SPLICE END STRAP AT BS 2350 S-48R. STRINGER SPLICE END STRAP REPLACED IAW SRM 51-30-02.May 17, 1996 · N673UP · Boeing 747123 · Fuselage Miscellaneous StructureSDR UPS96420234Frame · crackedINSPECTION TYPE: C. FOUND CRACK IN FRAME INNER FLANGE AT BS 1960, S40L. REPAIRED FRAME INNER FLANGE IAW 53-10-04, FIG 66 DETAIL 3.May 16, 1996 · N673UP · Boeing 747123 · Fuselage Main, FrameSDR UPS96420231Bracket · crackedINSPECTION TYPE: C. AFT CARGO COMPAARTMENT ATTACHMENT BRACKET FOR LOWER SILL JOINT WITH FRAME AT BS 1760 IS CRACKED IN TOP. REPLACED BRACKET IAW SRM 51-30-02.May 16, 1996 · N673UP · Boeing 747123 · Fuselage Miscellaneous StructureSDR UPS96420228Torque Box · crackedINSPECTION TYPE: C. AFT CARGO COMP. WEB ON TOP OF TORQUE BOX IS CRACKED BETWEEN BS 1840/1860, LBL 63. WORKED OUT CRACK AND REPAIRED IAW SRM'S 51-40-02, 51-30-02.May 16, 1996 · N673UP · Boeing 747123 · Fuselage Miscellaneous StructureSDR UPS96420224Frame · crackedINSPECTION TYPE: C. AT BS 1740 RT STR 14, FRAME FORMED AND OLD FRAME REPAIR CRACKED. REPAIRED AT BS 1740 RT BETWEEN STR 12 AND STR 14 IAW ETN 747-53-0762.May 16, 1996 · N673UP · Boeing 747123 · Fuselage Main, FrameSDR UPS96420236Web · crackedINSPECTION TYPE: C. NLG WHEELWELL: WEB FROM PRESSURE PAN AT BULKHEAD STA 400 IS CRACKED. REPLACED WEB IAW SRM 51-30-02.May 15, 1996 · N673UP · Boeing 747123 · Fuselage Miscellaneous StructureSDR UPS96420235Frame · crackedINSPECTION TYPE: C. AFT CARGO COMPARTMENT, FOUND CRACK IN TOP OF FRAME BETWEEN STR 41/42 LBL 62 NEAR SIDE GUIDE BRACKET AT BS 1860. REPAIRED CRACK IN FRAME IAW SRM 51-40-03.May 15, 1996 · N673UP · Boeing 747123 · Fuselage Main, FrameSDR UPS96420229Stringer · corrdedINSPECTION TYPE: C. CORROSION FOUND DURING INSP. ON STR 46R BSTA 983 NEAR END FITTING. REPLACED CA. 1 FOOT OF STRINGER IAW SRM 53-10-01, FIG 1, DETAIL 1.May 15, 1996 · N673UP · Boeing 747123 · Fuselage Main, Longeron/StringerSDR UPS96420226Frame · crackedINSPECTION TYPE: C. FOUND CRACK IN TOP OF FRAME RT AT BSTA 1600 NEAR FLOOR STUD STR 34. DRILLED OFF CRACK IAW SRM 51-10-01 AND REPAIRED IAW SRM'S 51-40-03 AND 51-30-02.May 15, 1996 · N673UP · Boeing 747123 · Fuselage Main, FrameSDR UPS96420225Skin · corrodedINSPECTION TYPE: C. FOUND FUSELAGE SKIN CORRODED ON BSTA 987.5 STR 41L AND STR 42L. CUT OUT PIECE OF CORRODED SKIN AND REPAIRED IAW SRM 53-30-03.May 15, 1996 · N673UP · Boeing 747123 · Fuselage Main, Plate/SkinSDR UPS96420188Shear Tie · crackedINSPECTION TYPE-C, AFT CARGO COMPARTMENT FRAME SHEAR TIE CRACKED AT BS 1560, BETWEEN S-35/36 LT. REMOVED DAMAGED SHEAR TIE AND REPAIRED SHEAR TIE IAW SRM 53-10-04, FIG 4.May 15, 1996 · N673UP · Boeing 747123 · Fuselage Miscellaneous StructureSDR P5CA9600229Control Cable · wornDURING PRE-DEPARTURE CHECK, FOUND RIGHT WING GEAR SHELF AREA AILERON CONTROL CABLE FORWARD OF HYDRAULIC RETURN FILTER WORN BEYOND LIMITS. REMOVED AND REPLACED AB-10 CABLE PER MM 20-11-03. SWAGED NEW TERMINALS, INSTALLED, SAFETIED AND TENSIONED IAW MM 27-11-0May 15, 1996 · N859FT · Boeing 747123 · Aileron Control SystemSDR UPS96420196Frame · crackedINSPECTION TYPE-C, AFT CARGO COMP HAD CRACK IN FRAME INNER CHORD AT BS 1500 RT NEAR FLOOR. REMOVED DAMAGED SECTION OF FRAME INNER CHORD AND REPAIRED FRAME IAW SRM 51-40-03.May 14, 1996 · N673UP · Boeing 747123 · Fuselage Main, FrameSDR P5CA9600226Light Assy · inoperativeFOUND EMERGENCY LIGHT ABOVE CREDENZA LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT ASSY IAW MM 33-51-00, OPS CHECKS NORMAL.May 9, 1996 · N858FT · Boeing 747123 · Emergency LightingSDR P5CA9600225Light · malfunctionedEMERGENCY LIGHT ABOVE CREW SERVICE DOOR ILLUMINATES WITH EMERGENCY LIGHT SWITCH IN OFF POSITION. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY IAW MM 33-51-00, OPS CHECK NORMAL.May 9, 1996 · N858FT · Boeing 747123 · Emergency LightingSDR P5CA9600219Actuator · inoperativeON TAXI OUT DURING CONTROL CHECK, RIGHT OUTBOARD AILERON WOULD NOT UNLOCK WITH FLAPS IN TAKEOFF RANGE. REMOVED AND REPLACED LOCK-OUT ACTUATOR IAW MM 27-11-16. OPS CHECK NORMAL.May 2, 1996 · N859FT · Boeing 747123 · Aileron Control SystemSDR 96UAL900311Impeller · failedAFTER TAKEOFF, DETECTED LOW OIL PRESSURE NR 4 ENGINE. ENGINE SHUTDOWN, FLIGHT RETURNED TO HNL. *S/D* MAIN GEARBOX DE-AERATOR IMPELLER DRIVE FAILED. REPLACED MAIN GEARBOX ASSY.May 2, 1996 · N155UA · Boeing 747123 · Turbine Engine Accessory DriveSDR UPS96420101Blkhd Web · corrodedINSPECTION TYPE 'C', FOUND ON WEB EDGE FASTENER SEM AT LT AT STR 38L WL 225 AT BS 2360 REAR PRESS BULK. REPAIRED DAMAGE IAW SRM 51-10-04 FIG 86 BOEING TELEX UPS-AMS-96-012 3RE APP DOC DFX 96-104, EFN 747-0761.May 1, 1996 · N676UP · Boeing 747123 · Fuselage Main, BulkheadSDR P5CA9600209Flow Divider · malfunctionedNUMBER 2 ENGINE SURGE BLEED VALVE STUCK OPEN AT FLIGHT LEVEL 39, EGT 100 DEGREES CELSIUS HOTTER THAN OTHER ENGINES AND FUEL FLOW 500 LBS HIGHER. REMOVED AND REPLACED ENGINE FLOW DIVIDER IAW MM 75-32-05. REMOVED AND REPLACED TT2 SENSOR IAW MM 73-21-04 AS PRECApr 22, 1996 · N859FT · Boeing 747123 · Compressor Bleed ValveSDR UPS96420063Spar Web · corrodedINSPECTION TYPE 'C', LT WING REAR SPAR WEB OF LT WING REAR SPAR HAS CORROSION AT WS 550. REPAIRED CORROSION IAW UPS EFN 747-57-0323.Apr 19, 1996 · N676UP · Boeing 747123 · Wing SparSDR UPS96405958Stringer · corrosionWHILE IN AMS FOR C-CHECK, MAINTENANCE REPORTED AREA AFT OF BULK CARGO COMP. FOUND CORROSION ON STR FLANGE S-36 RT BETWEEN BS 2200-2220. REMOVED CORRODED SECTION OF STRINGER AND REPAIRED STRINGER IAW SRM 53-10-3.Apr 3, 1996 · N676UP · Boeing 747123 · Fuselage Main, Longeron/StringerSDR UPS96420100Skin · corrosionINSPECTION TYPE 'C', FOUND CORROSION AT BS 2360 AFT PRESSURE SKIN PLATES AND Y-CHORD BETWEEN STR 46R AND STR 46L. REPLACED AFT PRESSURE WEB SEGMENT, PARTLY REPLACED Y-CHORD BETWEEN LBL 44 TO RBL 55. INSTALLED FASTENERS IAW SRM 51-30-02, APPR EFN 747-53-0760.Apr 2, 1996 · N676UP · Boeing 747123 · Fuselage Main, Plate/SkinSDR UPS96406061Tube · wornWHILE IN AMS FOR C-CHECK, MAINTENANCE REPORTED LT L/E INTERIOR I/B OF PYLON NR 1 FOUND WEAR HOLE IN SUPPORT TUBE ON AISLES 1071.25. REMOVED TUBE IAW MM 20-50-03, INSTALLED BUSHINGS IAW OHM 20-50-03 AND INSTALLED NEW TUBE IAW MM 20-50-03.Apr 2, 1996 · N676UP · Boeing 747123 · Wing Miscellaneous StructureSDR UPS96405856Angle · crackedWHILE IN FOR C-CHECK AT AMS MAINTENANCE REPORTED - AREA AFT OF BULK CARGO COMP, FOUND CRACKED STIFFINER - ANGLE FROM INTERCOSTAL ON FORWARD SIDE OF FRAME BS 2200, S40R. REPLACED STIFFENER-ANGLE IAW SRM 51-30-02.Apr 1, 1996 · N676UP · Boeing 747123 · Fuselage Miscellaneous StructureSDR UPS96405959Bulkhead Web · damagedWHILE IN AMS FOR C-CHECK, MAINTENANCE REPORTED BULK CARGO COMP. FOUND SEVERAL HOLE DAMAGES ON BULKHEAD WEB AT BS 2160, LT OF ACCESS DR. REMOVED DAMAGED SECTION OF BULKHEAD WEB AND REPAIRED WEB ACCORDING TO SRM 51-40-02.Mar 28, 1996 · N676UP · Boeing 747123 · Fuselage Main, BulkheadSDR UPS96405892Frame · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED AFT CARGO COMP FOUND CRACKED IN FRAME UPPER FLANGE AT BS 1580 RT NEAR RT SIDE GUIDE. STOP DRILLED CRACK AND REPAIRED FRAME UPPER FLANGE ACC SRM 53-10-04, FIG 66.Mar 27, 1996 · N676UP · Boeing 747123 · Fuselage Main, FrameSDR UPS96420024Frame · corrodedINSPECTION TYPE: C. AREA AFT OF BULK CARGO COMPARTMENT, FOUND CORROSION ON INNER FLANGE OF FRAME AT BS 2220 NEAR RIGHT OUTFLOW VALVE. CORROSION DAMAGES OUT OF LIMITS IAW SRM 51-10-01. REPLACED FRAME AT BS 2220 IAW SRM 53-10-01.Mar 26, 1996 · N676UP · Boeing 747123 · Fuselage Main, FrameSDR UPS96420023Frame · crackedINSPECTION TYPE: C. AREA AFT OF BULK CARGO COMPARTMENT, FOUND CRACKS IN FRAME SHEAR TIE DUE TO CORROSION AT BS 2220 NEAR RIGHT OUTFLOW VALVE BETWEEN STR 40 AND STR 44R. REPLACED FRAME AT BS 2220 RIGHT BETWEEN STR 44 AND STR 36R IAW SRM 51-30-02.Mar 26, 1996 · N676UP · Boeing 747123 · Fuselage Main, FrameSDR P5CA9600166Position Ind · inoperativeTRAILING EDGE FLAPS SELECTED TO 30 DEGREES, THEY WOULD ONLY EXTEND TO 25 DEGREES. EXERCISED FLAP DOWN SWITCH FOR INBOARD FLAPS. REPLACED INBOARD FLAP POSITION INDICATOR AND SWITCH S938 ON FLAP POSITION LEVER. OPS CHECKS NORMAL IAW MM 27-51.Mar 26, 1996 · N859FT · Boeing 747123 · Trailing Flap Position Indicating System
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