Boeing 747-121

Service difficulty reports · 3,030

Newest first. General aviation reporting is voluntary.

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 = '747121'
  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 P5CA9500095Fairing · crackedNR 2 PYLON HAS CRACK WITH STOP HOLE ON LOWER SAIL BOAT AT NS. 286. DAMAGED SECTION REMOVED FROM SAIL BOAT, FOUND WITHIN LIMITS PER SRM 54-10-01.May 27, 1995 · N831FT · Boeing 747121 · Nacelle/Pylon StructureSDR P5CA9500093Panel · corrosionSURFACE CORROSION ON SCREW HEADS AND RIVETS NR 2 PYLON FAIRING TO WING LEFT SIDE, ALSO LOOSE RIVETS. REPLACED LOOSE RIVETS PER BOEING SRM 51-30-02 AND CLEANED SURFACE CORROSION PER BOEING SRM 51-10-01.May 27, 1995 · N831FT · Boeing 747121 · Nacelle/Pylon, Plate/SkinSDR P5CA9500092Strap · bentNR 2 PYLON STRAP VENT ON LOWER SPAR AT NS. 180. NEW STRAP FABRICATED PER SRM 54-30-03, INSTALLED PER SRM 51-30-02.May 27, 1995 · N831FT · Boeing 747121 · Nacelle/Pylon StructureSDR P5CA9500091Strap · damagedNR 2 PYLON RIGHT SIDE FORWARD LOWER STRAP IS DAMAGED AT NS. 128. NEW STRAP FABRICATED AS PER SRM 54-10-02 AND INSTALLED AS PER SRM 51-30-02.May 27, 1995 · N831FT · Boeing 747121 · Nacelle/Pylon StructureSDR P5CA9500089Angle · brokenNOSE LANDING GEAR WHEELWELL BS 400 LEFT SIDE ANGLE BRACKET IS BROKEN. MANUFACTURED NEW ANGLE BRACKET FROM 7075-T6 0.50 INCH MATERIAL PER BOEING SRM 53-10-20 AND INSTALLED PER BOEING SRM 51-30-02.May 27, 1995 · N831FT · Boeing 747121 · Fuselage Miscellaneous StructureSDR P5CA9500086Skin · corrodedFOUND CORROSION ON RIGHT WING UPPER SKIN AND AROUND FASTENERS BETWEEN WS 724 AND WS 972 AT THE MID SPAR AREA. REMOVED CORROSION PER SRM 51-10-01 AND FOUND WITHIN LIMITS PER SRM 53-10-01.May 27, 1995 · N831FT · Boeing 747121 · Wing, Plate/SkinSDR P5CA9500085Skin · corrodedRIGHT WING UPPER SKIN CORROSION ON SKIN AND AROUND FASTENERS BETWEEN WS 323 AND WS 586 AT THE MID SPAR. REMOVED CORROSION PER BOEING SRM 51-10-01 AND FOUND WITHIN LIMITS PER BOEING SRM 53-10-01.May 27, 1995 · N831FT · Boeing 747121 · Wing, Plate/SkinSDR P5CA9500084Skin · corrodedFOUND CORROSION ON RIGHT WING SKIN AND AROUND FASTENERS BETWEEN WS. 782 TO 1084 AT REAR SPAR. REMOVED CORROSION PER BOEING SRM 51-10-01, FOUND WITHIN LIMITS PER BOEING SRM 53-10-01.May 27, 1995 · N831FT · Boeing 747121 · Wing, Plate/SkinSDR P5CA9500083Skin · corrodedFOUND CORROSION ON RIGHT WING UPPER SKIN AND AROUND FASTENERS BETWEEN WS 528 AND 724 AT THE REAR SPAR. REMOVED CORROSION PER BOEING SRM 51-10-01 FOUND WITHIN LIMITS PER BOEING SRM 53-10-01.May 27, 1995 · N831FT · Boeing 747121 · Wing, Plate/SkinSDR P5CA9500082Skin · corrodedFOUND CORROSION ON RIGHT WING UPPER SKIN AND AROUND FASTENERS BETWEEN MID AND REAR SPAR AT THE WS. 586 AREA. REMOVED CORROSION PER BOEING SRM 51-10-01, AREA WITHIN LIMITS PER BOEING SRM 57-20-01.May 27, 1995 · N831FT · Boeing 747121 · Wing, Plate/SkinSDR P5CA9500081Skin · crackedCRACK ON NR 2 PYLON EXTERNAL SKIN ON RIGHT FORWARD LOWER SPAR EDGE. NEW STRAP FABRICATED PER BOEING SRM 54-10-02, INSTALLED PER BOEING SRM 51-30-02.May 27, 1995 · N831FT · Boeing 747121 · Nacelle/Pylon, Plate/SkinSDR P5CA9500080Panel · dentedNR 2 DAMAGE (DENT) AND RIVET IS PENETRATING SKIN ON RIGHT FAIRING PYLON TO WING. DENT HAS BEEN REMOVED AND RIVET REPLACED AS PER BOEING SRM 51-30-02.May 27, 1995 · N831FT · Boeing 747121 · Nacelle/Pylon, Plate/SkinSDR P5CA9500079Skin · corrodedCORROSION 3 POINTS ON LEFT WING UPPER SKIN BETWEEN WBL 832 AND 907 AT THE MID SPAR. CLEANED PER BOEING SRM 51-10-01 AND FOUND WITHIN LIMITS PER BOEING SRM 57-20-01.May 27, 1995 · N831FT · Boeing 747121 · Wing, Plate/SkinSDR P5CA9500077Skin · corrodedCORROSION ON LEFT WING UPPER SKIN BETWEEN MID AND REAR SPAR AT WBL 724. REMOVED CORROSION PER BOEING SRM 51-10-01, AREA IS WITHIN LIMITS PER BOEING SRM 57-20-01.May 27, 1995 · N831FT · Boeing 747121 · Wing, Plate/SkinSDR P5CA9500076Skin · corrodedCORROSION ON 3 POINTS ON LEFT WING UPPER SKIN BETWEEN MID AND AFT SPARS BETWEEN WBL. 586 AND 617 (LEVEL 1). CORROSION REMOVED PER BOEING SRM 51-10-01 AND FOUND WITHIN LIMITS PER BOEING SRM 57-20-01.May 27, 1995 · N831FT · Boeing 747121 · Wing, Plate/SkinSDR P5CA9500073Tension Tie · crackedUPPER DECK TENSION TIE AT STA. 760 LEFT AND RIGHT, FOUND CRACKED. MODIFIED PER BOEING SERVICE BULLETIN 53-2088.May 27, 1995 · N831FT · Boeing 747121 · Fuselage Miscellaneous StructureSDR P5CA9500072Tension Ties · crackedUPPER DECK TENSION TIE AT STA. 780, 800, 820, 860, 880, 900, 920, 940 LH AND RH, FOUND CRACKS. REPAIRED PER BOEING SERVICE BULLETIN 53-2371.May 27, 1995 · N831FT · Boeing 747121 · Fuselage Miscellaneous StructureSDR P5CA9500071Door Panel · delaminatedNR 3 HEAT EXCHANGER EXIT DOOR PANEL (AFT OF LOUVERS) DELAMINATED. REPAIRED PER BOEING SRM 51-40-09.May 27, 1995 · N831FT · Boeing 747121 · DoorsSDR P5CA9500070Door Panel · delaminatedNR 1 HEAT EXCHANGER EXIT DOOR PANEL (AFT OF LOUVERS) DELAMAINATED. REPAIRED PER BOEING SRM 51-40-09.May 27, 1995 · N831FT · Boeing 747121 · DoorsSDR P5CA9500069Mid Flap · damagedLEFT INBOARD TRAILING EDGE MID FLAP HAS 2 AREAS DAMAGED. REPAIRED PER BOEING SRM 51-40-09.May 27, 1995 · N831FT · Boeing 747121 · Wing, Control Surface Attach FittingsSDR UPS403283Eel Bulbs · failedMAINTENANCE REPORTED, CREW SVC DOORWAY EMERGENCY EXIT LIGHTS OUT. REPLACED LIGHT BULBS. OPS CHECKED OK.May 21, 1995 · N672UP · Boeing 747121 · Emergency LightingSDR P5CA9500120Fairing · delaminatedNR 5 FAIRING PANEL DELAMINATED ON OUTER SIDE. REPAIRED PER BOEING SRM 51-40-09.May 21, 1995 · N831FT · Boeing 747121 · Aerodynamic FairingsSDR P5CA9500119Seat Track · corrodedUPPER DECK SEAT TRACK CORRODED AT LBL 22 BETWEEN STA 620 TO 640. REMOVED CORROSION AS PER BOEING SRM 51-10-01.May 21, 1995 · N831FT · Boeing 747121 · Fuselage, Seat/Cargo Attach FittingsSDR P5CA9500118Angle · crackedUPPER DECK FLOORBEAM CHORD AT STA 580 RBL 45, FOUND CRACKED ANGLE. INSTALLED NEW ANGLE PER BOEING SRM 51-10-00.May 21, 1995 · N831FT · Boeing 747121 · Fuselage Miscellaneous StructureSDR P5CA9500117Support · corrodedCORROSION ON SUPPORT FAIRING STA 1660 BETWEEN STR 33 TO 46 LT AND RT. REPAIRED AS PER BOEING SRM 51-10-01.May 21, 1995 · N831FT · Boeing 747121 · Fuselage Miscellaneous StructureSDR P5CA9500116Support · corrodedCORROSION ON SUPPORT FAIRING STA 1580 BETWEEN STR 28 TO 50 RT AND LT. CORROSION REMOVED PER SRM 51-10-01.May 21, 1995 · N831FT · Boeing 747121 · Fuselage Miscellaneous StructureSDR P5CA9500115Support · corrodedCORROSION ON SUPPORT FAIRING STA 1540 BETWEEN STR 25 TO 50. CORROSION REMOVED AS PER BOEING SRM 51-10-01.May 21, 1995 · N831FT · Boeing 747121 · Fuselage Miscellaneous StructureSDR P5CA9500114Skin · corrodedCORROSION ON SKIN BETWEEN STR 40 TO 50 AND BETWEEN STA 1480 TO 1680 LT AND RT. REMOVED AS PER BOEING SRM 51-10-01.May 21, 1995 · N831FT · Boeing 747121 · Fuselage Main, Plate/SkinSDR P5CA9500113Support · corrosionCORROSION ON SUPPORT FAIRING AT THE CENTER LINE BETWEEN STATION 1480 TO 1620. CORROSION REMOVED PER BOEING SRM 51-10-01.May 21, 1995 · N831FT · Boeing 747121 · Fuselage Miscellaneous StructureSDR P5CA9500112Support · dentedDENT ON OMEGA SUPPORT BETWEEN STA 1620 TO 1660 STR 40 AREA. REPAIRED AS PER BOEING SRM 51-40-04.May 21, 1995 · N831FT · Boeing 747121 · Fuselage Miscellaneous StructureSDR P5CA9500109Skin · corrodedCORROSION ON FITTING SUPPORT FAIRING AT STA 1660 STR 49 AREA. REPAIRED PER BOEING SRM 51-40-04.May 21, 1995 · N831FT · Boeing 747121 · Fuselage Main, Plate/SkinSDR P5CA9500108Skin · corrodedCORROSION ON FUSELAGE SKIN AT THE CENTER LINE BETWEEN S50L AND S50R BETWEEN STA 1480 AND 1680. CORROSION REMOVED AS PER BOEING SRM 51-10-10.May 21, 1995 · N831FT · Boeing 747121 · Fuselage Main, Plate/SkinSDR P5CA9500107Fairing · corrosionCORROSION ON AFT FAIRING AT STA 1620 STRINGER 47 AREA. CORROSION REMOVED PER BOEING SRM 51-10-01.May 21, 1995 · N831FT · Boeing 747121 · Aerodynamic FairingsSDR P5CA9500103Te Fiber · deterioratedRIGHT WING LEADING EDGE FLAP NR 21 VARIABLE CAMBER TRAINING EDGE FIBER IS DETERIORATED. REPAIRED PER BOEING SRM 51-40-09.May 21, 1995 · N831FT · Boeing 747121 · Leading Edge DevicesSDR P5CA9500099Cover · delaminatedRIGHT WING LEADING EDGE WS. 1120 FIBER COVER ABOVE PYLON NR 4 COMING OFF. REPAIRED PER BOEING SRM 51-40-09.May 21, 1995 · N831FT · Boeing 747121 · Wing Miscellaneous StructureSDR P5CA9500094Seat Track · corrodedUPPER DECK SEAT TRACK LBL 6O BETWEEN STA. 530 TO 540 CORRODED. REMOVED CORROSION PER SRM 51-10-01 WITHIN LIMITS.May 21, 1995 · N831FT · Boeing 747121 · Fuselage, Seat/Cargo Attach FittingsSDR P5CA9500090Exhaust · crackedAPU EXHAUST AFT END AT 12 O'CLOCK IS CRACKED. TRIMMED AND SMOOTHED THE CRACK PER BOEING SRM 51-10-01.May 21, 1995 · N831FT · Boeing 747121 · APU Exhaust SystemSDR P5CA9500088Arm · corrodedNOSE LANDING GEAR ARM CONNECTED TO LANDING GEAR ACTUATOR IS CORRODED ON FORWARD SIDE. CORROSION REMOVED AND TREATED PER BOEING SRM 51-10-01.May 21, 1995 · N831FT · Boeing 747121 · Landing Gear Retraction/Extension SystemSDR P5CA9500087Skin · corrodedFOUND CORROSION ON RIGHT WING UPPER SKIN AND AROUND FASTENERS BETWEEN WBS 724 AND WS 972 AT THE FRONT SPAR AREA. CORROSION REMOVED PER BOEING SRM 51-10-01 AND FOUND WITHIN LIMITS PER BOEING SRM 53-10-01.May 21, 1995 · N831FT · Boeing 747121 · Wing, Plate/SkinSDR P5CA9500078Fasteners · corrodedCORROSION AROUND FASTENERS AT WBL 862 AND 1056 AT THE MID SPAR. CLEANED CORROSION AS PER BOEING SRM 51-10-01.May 21, 1995 · N831FT · Boeing 747121 · Wing Miscellaneous StructureSDR P5CA9500075Skin · delaminatingLEFT WING OUTBOARD FLAP AFT FLAP HAS LARGE REPAIR DELAMINATING. REPAIRED PER BOEING SRM 51-40-09.May 21, 1995 · N831FT · Boeing 747121 · Trailing Edge FlapsSDR P5CA9500067Aft Flap · damagedLEFT WING OUTBOARD FLAP AFT FLAP HAS LARGE REPAIR REQUIRING UPGRADE. REPAIRED PER BOEING SRM 51-40-09.May 21, 1995 · N831FT · Boeing 747121 · Wing, Control Surface Attach FittingsSDR P5CA9500066Skin Repair · peelingLEFT WING INBOARD MID FLAP LOWER SKIN HAS FIBERGLASS REPAIR PEELING OFF. REPAIRED PER BOEING SRM 51-40-09.May 21, 1995 · N831FT · Boeing 747121 · Leading Edge DevicesSDR UPS403282Eel Bulbs · failedMAINTENANCE REPORTED, CREW SVC DOOR SILL EMERGENCY EXIT LIGHTS OUT. REPLACED LIGHT BULBS. OPS CHECKED OK.May 20, 1995 · N672UP · Boeing 747121 · Emergency LightingSDR 95ZZZW769Door · delaminatedLEFT WING LANDING GEAR LOWER OUTBOARD STRUT DOOR DELAMINATED. REPAIRED IAW WITH BOEING SRM 51-40-09. TOTAL CYCLES 18,464.May 19, 1995 · N832FT · Boeing 747121 · Landing Gear DoorsSDR 95ZZZW768Door · delaminatedRIGHT WING LOWER OUTBOARD STRUT DOOR DELAMINATED. REPAIRED IAW BOEING SRM 51-40-02. TOTAL CYCLES 18,464.May 19, 1995 · N832FT · Boeing 747121 · Landing Gear DoorsSDR UPS403276Floor Beam · corrodedWHILE IN AMSTERDAM FOR C CHECK, MAINTENANCE FOUND CORROSION ON FLOOR BEAM, BS 640, RBL 99. INSTALLED REPAIR PER UPS EO FILE NR B747-53-0712.May 17, 1995 · N682UP · Boeing 747121 · Fuselage Main, Floor BeamSDR UPS403275Water Fill Panel · corrodedWHILE IN AMSTERDAM FOR C CHECK, MAINTENANCE FOUND CORROSION AT THE WATER FILL PANEL, STA 980, RT LOWER SIDE, FUSELAGE. INSTALLED REPAIR PER SRM 51-20-01, 53-10-01, 51-10-01.May 17, 1995 · N682UP · Boeing 747121 · Water and Waste SystemSDR UPS403274Floor Beam · corrodedWHILE IN AMSTERDAM FOR C CHECK, MAINTENANCE FOUND CORROSION ON FLOOR BEAM STA 640, RBL 99. INSTALLED REPAIR PER UPS EO FILE NR B747-53-0712.May 17, 1995 · N682UP · Boeing 747121 · Fuselage Main, Floor BeamSDR UPS403273Floor Beam · corrodedWHILE IN AMSTERDAM FOR C CHECK, MAINTENANCE FOUND CORROSION ON FLOOR BEAM UPPER CHORD AT BS 980, LBL80 AND 90. INSTALLED REPAIR PER SRM 51-40-04.May 17, 1995 · N682UP · Boeing 747121 · Fuselage Main, Floor Beam
Back to Boeing 747-121