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 P5CA9601076Strip · tornLEFT OUTBOARD AILERON UPPER OUTBOARD STRIP IS TORN. TORN STRIP REPLACED PER MM 57-51-00.Aug 12, 1996 · N832FT · Boeing 747121 · AileronsSDR P5CA9601075Restraint · damagedFWD CARGO COMPARTMENT FIXED RESTRAINT DAMAGED AT STA 780R. RESTRAINT REPLACED AS PER MM 25-50-00.Aug 12, 1996 · N832FT · Boeing 747121 · Cargo CompartmentsSDR P5CA9601074Skin · corrodedCORROSION ON THE SKIN BETWEEN STA 1820 TO 1840 RT SIDE AND BETWEEN STRINGER 45 TO 46. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.Aug 12, 1996 · N832FT · Boeing 747121 · Fuselage Main, Plate/SkinSDR P5CA9601073Window Frame · corrodedCORROSION WINDOW FRAME UNDER SEALANT AT STRINGER 22 BETWEEN STA 1940 TO 1960 RT. CORROSION REMOVED AND TREATED PER SRM 51-10-01.Aug 12, 1996 · N832FT · Boeing 747121 · Fuselage Miscellaneous StructureSDR P5CA9601072Angle · corrodedCORROSION AND LOOSE CLIPS ON FLOOR ANGLE BETWEEN STA 2280 TO 2360 LT SIDE. CLEANED CORROSION AND TREATED PER SRM 51-10-01 AND 51-30-02.Aug 12, 1996 · N832FT · Boeing 747121 · Fuselage Miscellaneous StructureSDR P5CA9601071Support · corrodedCORROSION FAIRING SUPPORT LWR FUS STA 1180 BETWEEN AREA RBL TO LBL 58. REPAIRED PER SRM 53-50-04.Aug 12, 1996 · N832FT · Boeing 747121 · Fuselage Miscellaneous StructureSDR P5CA9601070Support · crackedCRACKS ON FAIRING SUPPORT ANGLES LWR FUS LT SIDE STA 1480. REPAIRED PER SRM 53-50-04.Aug 12, 1996 · N832FT · Boeing 747121 · Fuselage Miscellaneous StructureSDR P5CA9601069Floorbeam · corrodedCORROSION INBOARD CHORD STA 2360 BETWEEN STRINGER 45 RT TO 45 LT. CORROSION REMOVED AND TREATED PER SRM 51-10-01.Aug 12, 1996 · N832FT · Boeing 747121 · Fuselage Main, Floor BeamSDR P5CA9601068Skin · corrodedSURFACE CORROSION ON THE SKIN BETWEEN STA 780 TO 1000 RT SIDE AND BETWEEN STRINGER 12 TO 18. CORROSION REMOVED AND TREATED PER SRM 51-10-01.Aug 12, 1996 · N832FT · Boeing 747121 · Fuselage Main, Plate/SkinSDR P5CA9601067Floor · crackedCRACK ON FLOOR SHEET METAL AT STRINGER 26 AREA NEAR STA 780 RT SIDE. FAB NEW PART PER SRM 53-10-21 AND 51-30-02.Aug 12, 1996 · N832FT · Boeing 747121 · Fuselage Floor PanelSDR P5CA9601066Dome Nuts · corrodedNR 3L MAIN ENTRY DOOR CORROSION ON DOME NUTS AT UPPER FRAME INNER SURFACE. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01 AND 51-30-02.Aug 12, 1996 · N832FT · Boeing 747121 · Passenger/Crew DoorsSDR P5CA9601065Stringer · corrodedCORROSION STRINGER 5 LT BETWEEN STA 1400 TO 1420. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.Aug 12, 1996 · N832FT · Boeing 747121 · Fuselage Main, Longeron/StringerSDR P5CA9601064Support · corrodedCORROSION FAIRING SUPPORT LWR FUS AT RBL 62 AREA STA 1160. CORROSION BLENDED OUT SURFACE, SMOOTH PER SRM 51-10-01 AND 51-40-03.Aug 12, 1996 · N832FT · Boeing 747121 · Fuselage Miscellaneous StructureSDR P5CA9601063Fairing · corrodedCORROSION FAIRING SUPPORT LWR FUS BETWEEN AREA RBL TO LBL 58 AND BETWEEN STA 1120 TO 1140. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.Aug 12, 1996 · N832FT · Boeing 747121 · Fuselage Miscellaneous StructureSDR P5CA9601062Stringer · corrodedCORROSION ON STRINGER 4 RT AT STA 1640. CORROSION REMOVED AND TREATED PER SRM 51-10-01.Aug 12, 1996 · N832FT · Boeing 747121 · Fuselage Main, Longeron/StringerSDR P5CA9601061Stringer · crackCRACK BEYOND EXISTING REPAIR ON STA 1900 LT SIDE ABOVE STRINGER 41 TO 42. REPAIRED PER SRM 53-10-04.Aug 12, 1996 · N832FT · Boeing 747121 · Fuselage Main, Longeron/StringerSDR P5CA9601060Chord · crackedCRACK WITH STOP HOLES ON UPPER CHORD STA 1800 LT SIDE ABOVE STRINGER 42. REPAIRED PER SRM 53-10-04 AND 51-30-02.Aug 12, 1996 · N832FT · Boeing 747121 · Fuselage Miscellaneous StructureSDR P5CA9601059Skin · corrodedSURFACE CORROSION ON THE SKIN BETWEEN STA 1372 TO 1740 AND BETWEEN STRINGER 12 TO 18 LT SIDE. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01, FOUND WITHIN THE LIMITS PER SRM 53-30-01.Aug 12, 1996 · N832FT · Boeing 747121 · Fuselage Main, Plate/SkinSDR P5CA9601058Web · tornTEAR ON THE WEB AT STA 1880 RT SIDE UNDER UPPER CHORD ABOVE STRINGER 48 TO 49. AREA REPAIRED PER SRM 51-40-02.Aug 12, 1996 · N832FT · Boeing 747121 · Fuselage Miscellaneous StructureSDR P5CA9601057Chord · crackedCRACK ON UPPER CHORD STA 1580 RT SIDE ABOVE STRINGER 39 TO 40. REPAIRED PER SRM 53-10-04.Aug 12, 1996 · N832FT · Boeing 747121 · Fuselage Miscellaneous StructureSDR P5CA9601056Stringer · crackedFOUND 2 CRACKS IN AFT ROW STA 460 BETWEEN STRINGER 14E AND 15 RT. REPAIRED IAW SB53-2289.Aug 12, 1996 · N832FT · Boeing 747121 · Fuselage Main, Longeron/StringerSDR P5CA9601055Beam · corrodedLEFT BODY LANDING GEAR WHEEL WELL AFTER REMOVAL OF SPLICE PLATES CORROSION FOUND IN LANDING GEAR BEAM LOWER CHORD HORIZONTAL FLANGE. ALSO, ON VERTICAL FLANGE INBOARD AFT SIDE. CORROSION REMOVED SB53-2310.Aug 12, 1996 · N832FT · Boeing 747121 · Fuselage, Landing Gear Attach FittingsSDR P5CA9601054Beam · corrodedRIGHT BODY LANDING GEAR WHEEL WELL AFTER REMOVAL OF SPLICE PLATES CORROSION FOUND ON L/G BEAM LWR CHORD HORIZ FLANGE. ALSO, SCRATCHES EXIST ON FLANGE AFT EDGE. CORROSION AND DAMAGE REMOVED PER SB53-2310.Aug 12, 1996 · N832FT · Boeing 747121 · Fuselage, Landing Gear Attach FittingsSDR P5CA9601053Intercostal · damagedDENT ON INTERCOSTAL AT STRINGER 35 BETWEEN STA 1920 TO 1940 LT SIDE. STRAIGHTEN SRM 51-40-01 AND TREATED PER SRM 51-10-01. VISUAL CHECK FOUND OK.Aug 12, 1996 · N832FT · Boeing 747121 · Fuselage Miscellaneous StructureSDR P5CA9601052Keel Beem · corrodedCORROSION SHEET METAL COVER AND BRACKET SUPPORTS AROUND TO KEEL BEAM CUTOUTS AT CENTER LWR FUS BETWEEN STA 1000 TO 1241. CORROSION REMOVED, AREA TREATED PER SRM 51-10-01.Aug 12, 1996 · N832FT · Boeing 747121 · Fuselage Main, KeelSDR P5CA9601051Frame · corrodedCORROSION FRAME LWR CHORD AT STA 1600 ABOVE STR 11, 12. CORROSION BLENDED OUT PER SRM 51-10-01 AND 51-10-02.Aug 12, 1996 · N832FT · Boeing 747121 · Fuselage Main, FrameSDR P5CA9601050Stringer · corrodedCORROSION STRINGER 7 TO 9 BETWEEN STA 1580 TO 1600 LT. CORROSION REMOVED AND AREA TREATED PER 51-10-01.Aug 12, 1996 · N832FT · Boeing 747121 · Fuselage Main, Longeron/StringerSDR P5CA9601049Stringer · corrodedCORROSION STRINGER 2 RT BETWEEN STA 1580 TO 1600. CORROSION BLENDED OUT SURFACE, SMOOTHED PER SRM 51-10-01 AND 51-10-02.Aug 12, 1996 · N832FT · Boeing 747121 · Fuselage Main, Longeron/StringerSDR P5CA9601048Stringer · corrodedCORROSION TIE CLIP AT STA 1520 NEAR STRINGER 2 RT. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.Aug 12, 1996 · N832FT · Boeing 747121 · Fuselage Main, Longeron/StringerSDR P5CA9601047Frame · corrodedCORROSION ON FRAME AT STA 1500 NEAR STRINGER 3 LT. CORROSION REMOVED AREA TREATED PER SRM 51-10-01.Aug 12, 1996 · N832FT · Boeing 747121 · Fuselage Main, FrameSDR P5CA9601046Skin · corrodedCORROSION ON THE SKIN UNDER SEALER AT STRINGER 12 LAP JOINT AREA BETWEEN STA 2120 TO 1960 RT SIDE. CORROSION REMOVED AND TREATED PER SRM 51-10-01.Aug 12, 1996 · N832FT · Boeing 747121 · Fuselage Main, Plate/SkinSDR P5CA9601045Stringer · corrodedCORROSION ON STRINGER 5 AT STA 1420. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.Aug 12, 1996 · N832FT · Boeing 747121 · Fuselage Main, Longeron/StringerSDR P5CA9601044Stringer · corrodedCORROSION ON STRINGER 8, 9, 10 LT BETWEEN STA 1380 TO 1400. CORROSION BLENDED OUT SURFACE, SMOOTHED PER SRM 51-10-01 AND 51-10-02.Aug 12, 1996 · N832FT · Boeing 747121 · Fuselage Main, Longeron/StringerSDR P5CA9601043Stringer · corrodedCORROSION ON STRINGER 7 LT AT STA 1420 TO 1440. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.Aug 12, 1996 · N832FT · Boeing 747121 · Fuselage Main, Longeron/StringerSDR P5CA9601042Stringer · corrodedCORROSION ON STRINGER 10 LT AND ON FRAME STA 1440. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.Aug 12, 1996 · N832FT · Boeing 747121 · Fuselage Main, Longeron/StringerSDR P5CA9601041Stringer · corrodedCORROSION ON STRINGER 1 BETWEEN STA 1260 TO 1320 LT. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.Aug 12, 1996 · N832FT · Boeing 747121 · Fuselage Main, Longeron/StringerSDR P5CA9601040Frame · corrodedCORROSION ON FRAME AT STA 1241 NEAR STRINGER 1 LT. CORROSION BLENDED OUT, SURFACE SMOOTHED PER SRM 51-10-01 AND 51-10-02.Aug 12, 1996 · N832FT · Boeing 747121 · Fuselage Main, FrameSDR P5CA9601039Skin · corrodedCORROSION ON INTERNAL SKIN BETWEEN STA 1420 TO 1400 AND BETWEEN STRINGER 1 TO 4 LT. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.Aug 12, 1996 · N832FT · Boeing 747121 · Fuselage Main, Plate/SkinSDR P5CA9601036Rivets · shearedSHEARED RIVETS ON UPPER WING SKIN RT AT STA WS 990 IN FRONT SPAR AREA. INSTALLED NEW RIVET .1875 PER SRM 51-30-02.Aug 12, 1996 · N832FT · Boeing 747121 · Wing Miscellaneous StructureSDR P5CA9601035Rivets · shearedSHEARED RIVETS ON UPPER WING SKIN RT AT STA 600 IN FRONT SPAR AREA. INSTALLED NEW RIVETS OBTAINED FROM STA STOCK BN 91662-25.Aug 12, 1996 · N832FT · Boeing 747121 · Wing Miscellaneous StructureSDR P5CA9601034Rivets · shearedSHEARED RIVETS ON UPPER WING SKIN RT AT STA 565 FRONT SPAR. NEW RIVETS PER SRM 51-30-02.Aug 12, 1996 · N832FT · Boeing 747121 · Wing Miscellaneous StructureSDR P5CA9601033Rivets · shearedSHEARED RIVETS ON UPPER WING SKIN RT AT STA 480 IN FRONT SPAR AREA. INSTALLED NEW RIVETS .1875 PER SRM 51-30-02.Aug 12, 1996 · N832FT · Boeing 747121 · Wing Miscellaneous StructureSDR P5CA9601032Hi-Lock Rivet · corrodedCORROSION ON HEAD OF HI-LOCK AND OPEN HOLE AT STA 1700 BETWEEN STRINGER 3 TO 5. CORROSION RIVETS TAKEN OUT AND OPEN HOLE AREA INSTALLED NEW HI-LOCKS PER SRM 51-30-02 OBTAINED FROM STA STOCK.Aug 12, 1996 · N832FT · Boeing 747121 · Fuselage Miscellaneous StructureSDR TWRA96268Slide Raft · deployedDURING B-CHECK, FOUND L2 DOOR WAS OPENED AFTER ARMING. SLIDE PARTIALLY DEPLOYED AND DOOR ASSIST BOTTLE FULLY DISCHARGED. REMOVED AND REPLACED ESCAPE SLIDE RAFT AND ACCESS ASSIST DOOR BOTTLE ON L2 DOOR AS PER MM 25-69-00. OPERATION CHECK NORMAL. (M)Aug 10, 1996 · N604FF · Boeing 747121 · Life RaftSDR TWRA96267Battery Pack · dischargedDURING DAILY CHECK, FOUND 3R DOOR UPPER EVAC LIGHT OUT. REMOVED AND REPLACED BATTERY PACK. OPS CHECKED OK AS PER MM 33-51-00. (M)Aug 8, 1996 · N609FF · Boeing 747121 · Emergency LightingSDR UPS96421184Web · crackedINSPECTION TYPE-C, NLG WHEEL WELL TOP PANEL WEB UNDERNEATH LT SPINBRAKE INTERCOSTAL IS CRACKED. REPAIRED WEB ACC SRM 53-30-03 FIG 1.Aug 6, 1996 · N683UP · Boeing 747121 · Fuselage Miscellaneous StructureSDR UPS96420825Light · inoperativeINSPECTION TYPE: DLY. EMERGENCY EXIT LIGHT ON CREW SERVICE DOOR INOP. EXIT DOOR LIGHT OPERATIONAL. OPS CHK GOOD.Aug 6, 1996 · N681UP · Boeing 747121 · Emergency LightingSDR TWRA96261Roller Crank · brokenON POST FLIGHT INSPECTION, FOUND L3 DOOR LIGHT ON IN COCKPIT WITH DOOR CLOSED. REMOVED UPPER GATE AND UPPER GATE CONTROL ROD. REMOVED TORQUE TUBE, LOWER GATE CONTROL ROD. REMOVED AND REPLACED LATCH ROLLER CRANKS PER MM 52-11-19. OPS CHECKED NORMAL. RIGGINAug 5, 1996 · N609FF · Boeing 747121 · Passenger/Crew DoorsSDR P5CA9601236Web · corrodedFOUND TWO AREAS ON THE WEB WITH CORROSION. CORROSION REMOVED, CHECKED AND FOUND LOSS OF 7 PERCENT OF MATERIAL ONLY PER SRM 57-10-01.Aug 5, 1996 · N832FT · Boeing 747121 · Fuselage Miscellaneous StructureSDR P5CA9601235Clip · brokenBROKEN CLIP ON STA 2020 LT SIDE ABOVE STRINGER 40 TO 41. NEW ANGLE CLIP INSTALLED PER SRM 51-40-03 AND RIVET PER SRM 51-30-02.Aug 5, 1996 · N832FT · Boeing 747121 · Fuselage Miscellaneous Structure
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