N482US, cancelled Mar 1, 2002

Service difficulty reports · 433

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N482US' AND deregistration_id = 'N482US-2002-03-01'
  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 QXEA0102018Rivet · missingPDX - TWO RIVET HEADS MISSING ON FUSELAGE SKIN AT FRAME 16060 NEAR STRINGER 55. REPAIRED IAW FOKKER SRM 51-31-01.Nov 29, 2001 · N482US · Fokker F28MK4000 · Fuselage Main, Plate/SkinSDR QXEA0102017Angle · damagedPDX - REMOVE DAMAGED LOWER THRESHOLD COAMING AND REPLACE WITH A34918-007. REPAIRED IAW HORIZON AIR EA 4-53-904A AND FOKKER MM 51-30-00, PAGE 701-706.Nov 28, 2001 · N482US · Fokker F28MK4000 · Fuselage Miscellaneous StructureSDR QXEA0102015Rivet · loosePDX - VERTICAL STABILIZER SMOKING RIVETS LT SIDE JUST BELOW RIB 5 ON 50 PERCENT SPAR. REPAIRED IAW HORIZON AIR EA 4-55-299.Nov 28, 2001 · N482US · Fokker F28MK4000 · Vertical Stabilizer, Plate/SkinSDR QXEA0102014Rivet · loosePDX - VERTICAL STABILIZER SMOKING RIVET JUST BELOW RIB 5 ON 50 PERCENT SPAR RT SIDE. REPAIRED IAW HORIZON AIR EA 4-55-299.Nov 28, 2001 · N482US · Fokker F28MK4000 · Vertical Stabilizer, Plate/SkinSDR QXEA0102012Shim · damagedPDX - LT WING FUEL ACCESS APERTURE 71A, SHIM HAS BEEN BLENDED COMPLETELY THROUGH AT SEVERAL SCREW HOLES. REPAIRED IAW HORIZON AIR EA 4-57-568.Nov 27, 2001 · N482US · Fokker F28MK4000 · Wing Miscellaneous StructureSDR QXEA0102016Floorbeam · crackedPDX - FLOORBEAM CRACKED 9 INCHES AFT OF FRAME 3450 AND APPROXIMATELY 30 INCHES FROM SERVICE/EMERGENCY DOOR. REPAIRED IAW HORIZON AIR EA 4-53-1525 AND FOKKER SRM 53-02-14.Nov 24, 2001 · N482US · Fokker F28MK4000 · Fuselage Main, Floor BeamSDR QXEA0102006Structure · chafedPDX - STRUCTURE IS CHAFED AT LOWER ATTACH POINT FOR LT WING ROOT FAIRING 91J. REPAIRED IAW HORIZON AIR EA 4-57-569.Nov 20, 2001 · N482US · Fokker F28MK4000 · Wing Main, Frame StructureSDR QXEA0102005Shear Tie · corrodedPDX - AFT CARGO BAY FRAME 15205 CASTELLATION TIE IN TO BELLY SKIN BETWEEN STRINGER 1 AND 2 HAS CORROSION ON TOP SURFACE WITH POSSIBLE CRACK AT VERTICAL FLANGE. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 6 AND SRM 51-10-04, PARAGRAPH 4 B AND C, PAGE 9.Nov 20, 2001 · N482US · Fokker F28MK4000 · Fuselage Main, StructureSDR QXEA0101974Shear Tie · corrodedPDX - ANGLED FRAME 15810 TIE IN CLIP TO FUSELAGE BELLY SKIN HAS CORROSION ON TOP SURFACE BETWEEN STRINGERS 73 AND 74. REPAIRED IAW FOKKER SRM 51-31-01.Nov 20, 2001 · N482US · Fokker F28MK4000 · Fuselage Main, StructureSDR QXEA0101976Shear Tie · corrodedPDX - FUSELAGE FRAME 15635 TIE IN CLIP TO BELLY SKIN HAS CORROSION ON TOP SURFACE AROUND RIVETS BETWEEN STRINGER 73 AND 74. REPAIRED IAW FOKKER SRM 51-31-01.Nov 20, 2001 · N482US · Fokker F28MK4000 · Fuselage Main, StructureSDR QXEA0101975Skin · corrodedPDX - FUSELAGE INTERIOR BELLY SKIN HAS CORROSION AROUND (8) RIVETS BETWEEN FRAMES 15635 AND 15810, FROM STRINGER 73 AND 74. REPAIRED IAW FOKKER SRM 51-10-04, PARAGRAPH 4B, C, PAGE 9 AND SRM 51-31-01.Nov 20, 2001 · N482US · Fokker F28MK4000 · Fuselage Main, Plate/SkinSDR QXEA0101973Frame · corrodedPDX - ANGLED FRAME 15810 HAS CORROSION ON FORWARD AND AFT SIDES AT CUTOUTS AROUND STRINGERS 1 AND 74. REPAIRED IAW FOKKER SRM 51-10-04, PARAGRAPH 4B, C, PAGE 9.Nov 20, 2001 · N482US · Fokker F28MK4000 · Fuselage Main, FrameSDR QXEA0101972Doubler · corrodedPDX - FUSELAGE INTERIOR BELLY SKIN DOUBLER HAS CORROSION AROUND (3) RIVETS AT AFT SIDE OF ANGLED FRAME 15810 BETWEEN STRINGERS 1 AND 2. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 6.Nov 20, 2001 · N482US · Fokker F28MK4000 · Fuselage Main, Plate/SkinSDR QXEA0101971Shear Tie · corrodedPDX - FUSELAGE FRAME 16060 TIE IN CLIP TO BELLY SKIN HAS CORROSION ON TOP SURFACE AROUND (3) RIVETS BETWEEN STRINGERS 2 AND 3. REPAIRED IAW FOKKER SRM 51-10-04, PARAGRAPH 4B, C, PAGE 9.Nov 20, 2001 · N482US · Fokker F28MK4000 · Fuselage Main, StructureSDR QXEA0101970Shear Tie · corrodedPDX - FUSELAGE FRAME 16060 TIE IN CLIP TO BELLY SKIN HAS CORROSION ON TOP SURFACE AROUND (3) RIVETS BETWEEN STRINGERS 1 AND 2. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2, PAGE 4.Nov 20, 2001 · N482US · Fokker F28MK4000 · Fuselage Main, StructureSDR QXEA0101969Skin · corrodedPDX - FUSELAGE INTERIOR BELLY SKIN AT AFT SIDE OF FRAME 16060 BETWEEN STRINGER 1 AND 2 HAS CORROSION. REPAIRED IAW FOKKER SRM 51-10-04, PARAGRAPH 4B, C, PAGE 9.Nov 20, 2001 · N482US · Fokker F28MK4000 · Fuselage Main, Plate/SkinSDR QXEA0101968Stringer · corrodedPDX - FUSELAGE BELLY STRINGER 1 HAS CORROSION AT TIE IN CLIP AREA AFT SIDE OF FRAME 16060. REPAIRED IAW FOKKER SRM 51-10-01, 4B, C, PAGE 9.Nov 20, 2001 · N482US · Fokker F28MK4000 · Fuselage Main, Longeron/StringerSDR QXEA0101967Shear Tie · corrodedPDX - FUSELAGE FRAME 16060 TIE IN CLIP TO BELLY SKIN HAS CORROSION ON TOP SURFACE ROUND RIVETS BETWEEN STRINGERS 1 AND 74. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 6 AND SRM 51-10-04, PARAGRAPH 4B, C, PAGE 9.Nov 20, 2001 · N482US · Fokker F28MK4000 · Fuselage Main, StructureSDR QXEA0101966Shear Tie · corrodedPDX - FUSELAGE FRAME 16060 TIE IN CLIP TO BELLY SKIN HAS CORROSION ON TOP SURFACE AROUND (3) RIVETS BETWEEN STRINGERS 73 AND 74. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2, PAGE 4.Nov 20, 2001 · N482US · Fokker F28MK4000 · Fuselage Main, StructureSDR QXEA0102008Doubler · chafedPDX - FRAME 11905 RT COLD SLEEVE REPAIR PLATE HAS 10/32 SCREW CHAFE DAMAGE AT .023 DEEP. REPAIRED IAW HORIZON AIR EA 4-53-1523.Nov 19, 2001 · N482US · Fokker F28MK4000 · Fuselage Main, FrameSDR QXEA0101995Frame · crackedPDX - FRAME 22293 CRACKED APPROXIMATELY 1.5 INCH IN OUTBOARD RADIUS AT AFT END OF STRINGER 53A. REPAIRED IAW HORIZON AIR EA 4-53-1524.Nov 19, 2001 · N482US · Fokker F28MK4000 · Fuselage Main, FrameSDR QXEA0101994Frame · crackedPDX - FRAME 22293 CRACKED APPROXIMATELY .5 INCH IN OUTBOARD RADIUS. REPAIRED IAW HORIZON AIR EA 4-53-1524.Nov 19, 2001 · N482US · Fokker F28MK4000 · Fuselage Main, FrameSDR QXEA0102009Clip · crackedPDX - CLIP CONNECTING LOWER WING TO FUSELAGE FAIRING SUPPORT AT FRAME 13815A AND CENTER RIB IS CRACKED. REPAIRED IAW FOKKER SRM 53-53-04, FIGURE 5, ITEM 190, SRM 51-30-01.Nov 18, 2001 · N482US · Fokker F28MK4000 · Fuselage Miscellaneous StructureSDR QXEA0101993Frame · crackedPDX - FRAME 22293 CRACKED APPROXIMATELY 1.25 INCH IN OUTBOARD RADIUS AT AFT END OF STRINGER 21A. REPAIRED IAW HORIZON AIR EA 4-53-1524.Nov 18, 2001 · N482US · Fokker F28MK4000 · Fuselage Main, FrameSDR QXEA0101985Seat Track · corrodedPDX - RT INBOARD SEAT TRACK HAS PITTING ON INBOARD FLANGE AT APPROXIMATELY STATION 306 - 327. REPAIRED IAW HORIZON AIR EA 4-53-1527.Nov 18, 2001 · N482US · Fokker F28MK4000 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA0101984Seat Track · corrodedPDX - RT INBOARD SEAT TRACK HAS PITTING ON INBOARD FLANGE AT APPROXIMATELY STATION 340-404. REPAIRED IAW HORIZON AIR EA 4-53-1527.Nov 18, 2001 · N482US · Fokker F28MK4000 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA0101983Seat Track · corrodedPDX - RT INBOARD SEAT TRACK IS PITTED ON INBOARD FLANGE AT APPROXIMATELY STATION 676 - 685. REPAIRED IAW HORIZON AIR EA 4-53-1527.Nov 18, 2001 · N482US · Fokker F28MK4000 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA0101982Seat Track · corrodedPDX - RT OUTBOARD SEAT TRACK HAS THREE PITS ON OUTBOARD FLANGE AT APPROXIMATELY STATION 232 - 234. REPAIRED IAW HORIZON AIR EA 4-53-1528.Nov 18, 2001 · N482US · Fokker F28MK4000 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA0101981Seat Track · corrodedPDX - RT OUTBOARD SEAT TRACK HAS PITTING ON OUTBOARD FLANGE AT APPROXIMATELY STATION 325 - 327. REPAIRED IAW HORIZON AIR EA 4-53-1528.Nov 18, 2001 · N482US · Fokker F28MK4000 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA0101980Seat Track · corrodedPDX - RT OUTBOARD SEAT TRACK HAS PITTING ON INBOARD FLANGE AT APPROXIMATELY STATION 349 - 357. REPAIRED IAW HORIZON AIR EA 4-53-1528.Nov 18, 2001 · N482US · Fokker F28MK4000 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA0101979Floorbeam · corrodedPDX - FLOORBEAM REPAIR BL 0 JUST FORWARD OF FRAME 4900 TOP TIE PLATE HAS LIGHT CORROSION. REPAIRED IAW HORIZON AIR EA 4-53-1526.Nov 18, 2001 · N482US · Fokker F28MK4000 · Fuselage Main, Floor BeamSDR QXEA0101917Stringer · chafedPDX - CLIP ON CASTELLATION, FRONT SIDE OF FRAME 50-2 IS CHAFING INTO STRINGER 27. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 5, PARAGRAPH 3E AND SRM 51-10-4.Nov 18, 2001 · N482US · Fokker F28MK4000 · Fuselage Main, Longeron/StringerSDR QXEA0101915Seat Track · corrodedPDX - RT INBOARD SEAT TRACK HAS LIGHT CORROSION ON OUTBOARD FLANGE AT APPROXIMATELY STATION 180.5 TO 191. REPAIRED IAW FOKKER SRM 51-31-01, SRM 51-11-4, AND SRM 51-30-02.Nov 17, 2001 · N482US · Fokker F28MK4000 · Fuselage, Seat/Cargo Attach FittingsSDR QXEA0101997Support · bentPDX - BENT FAIRING SUPPORT STRUCTURE IS BENT. REPAIRED IAW FOKKER SRM 53-53-11, PAGE 35, ITEM 265, SRM 51-10-4, PARAGRAPH 4 B AND C.Nov 16, 2001 · N482US · Fokker F28MK4000 · Aerodynamic FairingsSDR QXEA0102003Structure · dentedPDX - DENT 1.8 INCH LONG, 1.2 INCH WIDE, APPROXIMATELY .10 INCH DEEP ON TOP EDGE OF CENTER CARGO DOOR, 15INCHES AFT OF LEADING EDGE OF DOOR. REPAIRED IAW MM 51-00-00, PAGE 1 AND MM 51-30-02.Nov 15, 2001 · N482US · Fokker F28MK4000 · Cargo/Baggage DoorsSDR QXEA0101999Rib · crackedPDX - HORIZONTAL STABILIZER LEADING EDGE 51B THIRD RIB FROM INBOARD END CRACK TOP FORWARD. REPAIRED IAW FOKKER SRM 51-10-4, SRM 51-31-01, PAGE 13, PARAGRAPH 7B.Nov 15, 2001 · N482US · Fokker F28MK4000 · Horizontal Stabilizer, Spar/RibSDR QXEA0101991Frame · crackedPDX - CASTELLATION CRACKED AT LOWER RIVET ON FRAME 20075 ABOVE STRINGER 28. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 3, SRM 51-31-01 AND SRM 53-10-05.Nov 15, 2001 · N482US · Fokker F28MK4000 · Fuselage Main, FrameSDR QXEA0101990Strap · crackedPDX - SPEEDBRAKE ACCUMULATOR FORWARD MOUNT ASSEMBLY TOP FINGER STRAP CRACKED. REPAIRED IAW FOKKER SRM 51-31-01.Nov 15, 2001 · N482US · Fokker F28MK4000 · SpoilersSDR QXEA0101977Clip · crackedPDX - FRAME 16660 CLIP CRACKED AT INBOARD END IN RADIUS. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2, PAGE 4.Nov 15, 2001 · N482US · Fokker F28MK4000 · Fuselage Miscellaneous StructureSDR QXEA0101952Skin · corrodedPDX - CORROSION ON FUSELAGE SKIN CUTOUT NEXT TO RIVETS AND NUT PLATES WHERE AFT BLANKING PLATE ATTACHES FOR RADIO ALTIMETER ANTENNA. REPAIRED IAW HORIZON AIR EA 4-53-1521.Nov 15, 2001 · N482US · Fokker F28MK4000 · Fuselage Main, Plate/SkinSDR QXEA0101947Frame · crackedPDX - AFT CARGO BAY FRAME 15205 CASTELLATION TIE-IN TO BELLY SKIN AT STRINGER 4 IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.Nov 15, 2001 · N482US · Fokker F28MK4000 · Fuselage Main, FrameSDR QXEA0101946Frame · crackedPDX - AFT CARGO BAY FRAME 15205 CASTELLATION TIE-IN TO BELLY SKIN AT STRINGER 5 IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.Nov 15, 2001 · N482US · Fokker F28MK4000 · Fuselage Main, FrameSDR QXEA0101945Frame · crackedPDX - AFT CARGO BAY FRAME 15205 CASTELLATION TIE-IN TO BELLY SKIN AT STRINGER 6 IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.Nov 15, 2001 · N482US · Fokker F28MK4000 · Fuselage Main, FrameSDR QXEA0101944Frame · crackedPDX - AFT CARGO BAY FRAME 14755 CASTELLATION TIE-IN TO BELLY SKIN AT STRINGER 70 IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2.Nov 15, 2001 · N482US · Fokker F28MK4000 · Fuselage Main, FrameSDR QXEA0101940Doubler · tornPDX - BOTTOM TRAILING CORNER OF REPAIR DOUBLER TORN, CENTER CARGO DOOR INNER SKIN, 10 INCHES FORWARD OF TRAILING EDGE OF CENTER CARGO DOOR, ALONG BOTTOM OF DOOR. REPAIRED IAW HORIZON AIR EA 4-52-462 AND FOKKER MM 51-30-00 AND FOKKER SRM 51-31-01.Nov 15, 2001 · N482US · Fokker F28MK4000 · Cargo/Baggage DoorsSDR QXEA0101939Strap · damagedPDX - THREE RIVETS PULLED THROUGH STRAP ON BELLY SKIN JUST AFT OF RT MAIN LANDING GEAR DOOR. REPAIRED IAW FOKKER SRM 51-31-05.Nov 15, 2001 · N482US · Fokker F28MK4000 · Fuselage Main, Plate/SkinSDR QXEA0101938Vane · chafedPDX - LT WING INBOARD, TRAILING EDGE FLAP, VANE, LEADING EDGE IS CHAFED AT OUTBOARD END. REPAIRED IAW FOKKER SRM 51-10-4, SRM 57-01-01, PAGE 3 AND FOKKER MM 51-30-00.Nov 15, 2001 · N482US · Fokker F28MK4000 · Trailing Edge FlapsSDR QXEA0101922Frame · crackedPDX - CASTELLATION AT TOP OF OBLIQUE FRAME 41-2 AT STRINGER 43 IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 6, PAGE 8, SRM 51-10-4 AND 53-31-01.Nov 15, 2001 · N482US · Fokker F28MK4000 · Fuselage Main, FrameSDR QXEA0102011Frame · corrodedPDX - AFT CARGO BAY FRAME 14755 HAS CORROSION ON TOP SURFACE AND UNDER SIDE OF TOP FLANGE AT STRINGER 3. REPAIRED IAW FOKKER SRM 51-31-01.Nov 14, 2001 · N482US · Fokker F28MK4000 · Fuselage Main, FrameSDR QXEA0102007Frame · corrodedPDX - AFT CARGO BAY FRAME 14755 CORROSION TOP SURFACE AND UNDERSIDE OF TOP FLANGE AT STRINGER 72. REPAIRED IAW FOKKER SRM 53-01-01 AND SRM 51-10-04, PARAGRAPH 4 B AND C, PAGE 9.Nov 14, 2001 · N482US · Fokker F28MK4000 · Fuselage Main, Frame
Back to N482US, cancelled Mar 1, 2002