N16804, cancelled May 16, 2006

Service difficulty reports · 96

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 = 'N16804' AND deregistration_id = 'N16804-2006-05-16'
  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 CALA0000554Angle · crackedVERTICAL AND HORIZONTAL SUPPORT ANGLES AT CFS 1485 VENT BOX ARE CRACKED (2). REMOVED AND REPLACED SUPPORT ANGLES PER SRM 51-30-5.Apr 25, 2000 · N16804 · Doug DC982 · Fuselage Main, Attach FittingsSDR CALA0000553Bracket · crackedLEFT SIDE HEAT EXCHANGER SUPPORT BRACKET CRACKEDAT FS 1429 LONG. 4L (8). REMOVED AND REPLACED BRACKET PER SRM 51-30-1.Apr 25, 2000 · N16804 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000507Door Frame · corrodedINSPECTION FOUND AFT CARGO DOOR LOWER DOOR JAMB CORRODED BETWEEN STA 1156 AND 1212. A DOUBLER AND SPACER WERE INSTALLED IAW ECRA 5310-03027.Apr 20, 2000 · N16804 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000506Frame · corrodedINSPECTION FOUND AFT CARGO PIT MAIN FRAME CENTER FLOOR STA 1300 CORRODED. REMOVED AND REPLACED SPLICES IAW SRM 51-30-2 AND 51-30-5.Apr 19, 2000 · N16804 · Doug DC982 · Fuselage Main, FrameSDR CALA0000505Floor Support · corrodedINSPECTION FOUND MID CARGO COMPARTMENT FLOORBOARD SUPPORT CORRODED AT FS 598 - 636, RBL 20. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-1.Apr 19, 2000 · N16804 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000504Cargo Track · corrodedINSPECTION FOUND THE AFT CARGO PIT RT FLOOR TIE DOWN TRACK CORRODED AT STA 1211. THE TIE DOWN TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1.Apr 19, 2000 · N16804 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0000500Longeron · corrodedINSPECTION FOUND LONGERON 29L TO 29R HAD SEVERAL CORRODED FASTENERS IN LONGERONS AND SPLICES IN MID CARGO COMPARTMENT AT FS 579 - 598. THE LONGERON SPLICES WERE REMOVED AND REPLACED IAW SRM 51-30-5.Apr 17, 2000 · N16804 · Doug DC982 · Fuselage Main, Longeron/StringerSDR CALA0000499Skin · dentedINSPECTION FOUND LT WING NR 1 SLAT DENTED. THE DENTED AREA WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 57-06, FIGURE 1.Apr 17, 2000 · N16804 · Doug DC982 · Leading Edge DevicesSDR CALA0000498Floor Support · corrodedINSPECTION FOUND FORWARD CARGO COMPARTMENT FLOOR SUPPORT CORRODED AT STA 427 - 463. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-1.Apr 17, 2000 · N16804 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000497Door Frame · corrodedINSPECTION FOUND FORWARD CARGO DOOR JAMB AT O/B END OF TORQUE BOX CORRODED FROM STA 370 - 427. THE CORRODED AREA WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 44.Apr 17, 2000 · N16804 · Doug DC982 · Cargo/Baggage DoorsSDR CALA0000496Web · corrodedINSPECTION FOUND AFT CARGO DOOR AFT JAMB TORQUE BOX UPPER WEB CORRODED AT LONGERON 28R. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-30-5.Apr 17, 2000 · N16804 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000482Pan · wornINSPECTION FOUND AFT CARGO DOOR PAN STOP WORN. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-03, FIGURE 8 AND 51-10-3.Apr 15, 2000 · N16804 · Doug DC982 · Cargo/Baggage DoorsSDR CALA0000480Floor Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED IN AFT PIT AT STA 1117 FROM LONGERON 28L TO 28R. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-2.Apr 15, 2000 · N16804 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000479Angle · crackedINSPECTION FOUND A 1.5 INCH CRACK IN VERTICAL STABILIZER REAR SPAR LOWER ATTACH ANGLE ON LT SIDE. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-5 AND 51-30-2.Apr 15, 2000 · N16804 · Doug DC982 · Vertical Stabilizer, Attach FittingsSDR CALA0000478Skin · puncturedINSPECTION FOUND THREE HOLES PUNCTURED INTO RT I/B MLG DOOR OUTER SKIN UPPER BLOCK. THE DAMAGED SKIN WAS REMOVED AND REPLACED IAW SRM 51-30-2.Apr 15, 2000 · N16804 · Doug DC982 · Landing Gear DoorsSDR CALA0000477Bracket · crackedINSPECTION FOUND A 4 INCH CRACK IN TWO RT AFT LAV WALL ATTACH ANGLE BRACKETS. THE WALL ATTACH ANGLE BRACKETS WERE REMOVED AND REPLACED IAW MM 51-10-2.Apr 15, 2000 · N16804 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000476Cargo Track · corrodedINSPECTION FOUND FORWARD CARGO RT TIEDOWN TRACK CORRODED AT FS 229 - 370. THE TIEDOWN TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1.Apr 15, 2000 · N16804 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0000475Skin · dentedINSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT FS 1380 BETWEEN LONGERON 4L AND 6L. THE DENTED SECTION OF SKIN WAS CUTOUT IAW SRM 53-01, FIGURE 2. A REPAIR DOUBLER AND FILLER WERE INSTALLED IAW SRM 53-01, FIGURE 2, 51-30-02, AND 51-30-08.Apr 15, 2000 · N16804 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0000474Skin · damagedINSPECTION FOUND LT WING TIP UPPER T/E SCREW HOLES ELONGATED. THE ELONGATED HOLES WERE CUTOUT AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-01, FIGURE 5 AND 51-30-2.Apr 15, 2000 · N16804 · Doug DC982 · Wing, Plate/SkinSDR CALA0000473Skin · dentedINSPECTION FOUND LT HORIZONTAL STABILIZER O/B LEADING EDGE SKIN DENTED. DOUBLERS WERE INSTALLED IAW SRM 55-03, FIGURE 3.Apr 15, 2000 · N16804 · Doug DC982 · Horizontal Stabilizer, Plate/SkinSDR CALA0000472Fitting · corrodedINSPECTION FOUND SUPPORT FITTING CORRODED AT E & E COMPARTMENT INSIDE OF DOOR TORQUE BOX FS 148, LONGERON 28L. THE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-30-5.Apr 15, 2000 · N16804 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000483Pan · wornINSPECTION FOUND FORWARD CARGO DOOR PAN WORN. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-03, FIGURE 8 AND 51-10-3.Apr 14, 2000 · N16804 · Doug DC982 · Cargo/Baggage DoorsSDR CALA0000481Bracket · wornINSPECTION FOUND TWO FORWARD AND TWO AFT SUPPORT BRACKETS HAD WORN AND ELONGATED HOLES AT AFT CARGO DOOR HINGE. A DOUBLER WAS INSTALLED IAW SRM 53-05, FIGURE 16A.Apr 14, 2000 · N16804 · Doug DC982 · Cargo/Baggage DoorsSDR CALA0000471Skin · dentedINSPECTION FOUND EXTERNAL SKIN OF LT SIDE OF RUDDER DENTED BETWEEN CENTER AND LOWER HINGE POINT. A REPAIR DOUBLER WAS INSTALLED IAW SRM 55-01, FIGURE 10A, 51-10-4, 51-10-3, AND 51-30-6.Apr 14, 2000 · N16804 · Doug DC982 · Rudder, Plate/SkinSDR CALA0000470Cargo Track · corrodedINSPECTION FOUND RT TIEDOWN TRACK ATTACH FITTING CORRODED IN AFT CARGO PIT AT FS 1007. THE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-30-1, 51-10-4, AND 51-10-3.Apr 14, 2000 · N16804 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0000469Skin · chafedINSPECTION FOUND EXTERNAL FUSELAGE SKIN CHAFED AT AREA OF HOLD OPEN HOOK RECEPTACLE FOR FORWARD ENTRY DOOR. THE CHAFED AREA WAS BLENDED IAW SRM 53-01, FIGURE 1. A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 24.Apr 14, 2000 · N16804 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0000468Floor Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED IN AFT PIT AT STA 1155 FROM LONGERON 28L TO 28R. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-2.Apr 14, 2000 · N16804 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000467Floorbeam · corrodedINSPECTION FOUND R-1 DOOR FLOORBEAM CORRODED AT FS 160 - 200, RBL 48. THE FLOORBEAM WAS REMOVED AND A NEW FLOORBEAM WAS INSTALLED IAW SRM 51-30-2, 51-10-3 AND 51-30-1.Apr 14, 2000 · N16804 · Doug DC982 · Fuselage Main, Floor BeamSDR CALA0000466Doubler · crackedINSPECTION FOUND A 6 INCH CRACK IN LT MLG DOOR I/B LOWER AFT CORNER. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 28 AND 51-30-5.Apr 13, 2000 · N16804 · Doug DC982 · Landing Gear DoorsSDR CALA0000465Cargo Track · corrodedINSPECTION FOUND LT CARGO TIEDOWN TRACK CORRODED IN AFT PIT AT FS 1007 - 1360, LONGERON 27L. THE TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-3.Apr 13, 2000 · N16804 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0000464Angle · corrodedINSPECTION FOUND WEB AND ATTACH ANGLE CORRODED AT PAX DOOR JAMB AFT SIDE, FS 200, LBL 58. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-2, 51-10-3, 51-10-4, AND 51-30-5.Apr 13, 2000 · N16804 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000461Skin · gougedINSPECTION FOUND RT MLG DOOR LOWER SKIN, GOUGED ON O/B SIDE. THE GOUGED SKIN SECTION WAS REMOVED AND A NEW SKIN SECTION WAS INSTALLED IAW SRM 51-30-2.Apr 11, 2000 · N16804 · Doug DC982 · Landing Gear DoorsSDR CALA0000460Skin · chafedINSPECTION FOUND MID CARGO DOOR OUTER SKIN CHAFED AT LOWER AFT CORNER. A DOUBLER WAS INSTALLED IAW SRM 51-30-2.Apr 11, 2000 · N16804 · Doug DC982 · Cargo/Baggage DoorsSDR CALA0000458Stop · chafedINSPECTION FOUND AFT CARGO DOOR PAN STOP CHAFED. A DOUBLER REPAIR WAS INSTALLED IAW SRM 51-10-3, 51-30-1, 51-30-2, AND ECRA 5330-02189.Apr 11, 2000 · N16804 · Doug DC982 · Cargo/Baggage DoorsSDR CALA0000456Fitting · corrodedINSPECTION FOUND DOOR LATCH SUPPORT FITTING INSIDE OF E&E COMPARTMENT DOOR CORRODED AT FS 48, LONGERON 28 RT. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-30-5.Apr 11, 2000 · N16804 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000449Floorboard · crackedINSPECTION FOUND A 1 INCH CRACK IN CABIN LT FLOOR SKIN AT FS 218, LBL 54. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 2, 51-10-3, 51-10-4, 51-30-2, AND 51-30-5.Apr 8, 2000 · N16804 · Doug DC982 · Fuselage Floor PanelSDR CALA0000448Web · corrodedINSPECTION FOUND CUSP WEB CORRODED AT FS 200 - 218, LBL 54. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-10-3, 53-01, FIGURE 4, 51-01, 51-30-2, 51-30-5, AND 51-30-6.Apr 8, 2000 · N16804 · Doug DC982 · Fuselage Miscellaneous StructureSDR ALA0000447Bracket · crackedINSPECTION FOUND SUB FLOOR BRACKET CRACKED AT FS 200, LBL 58. A NEW BRACKET WAS INSTALLED IAW SRM 51-30-5.Apr 8, 2000 · N16804 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000446Floor Support · crackedINSPECTION FOUND A 4 INCH CRACK IN L-1 DOOR FLOOR SUPPORT AT FS 200. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-3 AND 51-30-5.Apr 8, 2000 · N16804 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000445Floorbeam · corrodedINSPECTION FOUND MID CARGO BAY FLOORBOARD SUPPORT CORRODED ON LOWER SIDE AT FS 636, LBL 15 TO RBL 15. THE FLOOR SUPPORT WAS REMOVEDAND REPLACED IAW SRM 51-30-2.Apr 8, 2000 · N16804 · Doug DC982 · Fuselage Main, Floor BeamSDR ALA0000444Angle · crackedINSPECTION FOUND A 6 CRACK IN CABIN RT SUPPORT ANGLE AT FS 1308, STRINGER 13 RT - 14 RT. THE FASTENER WAS REMOVED, THE CRACK WAS STOP DRILLED, AND A REPAIR ANGLE WAS INSTALLED IAW SRM 51-30-5 AND 51-30-2.Apr 8, 2000 · N16804 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000443Floorbeam · corrodedINSPECTION FOUND TOP T-CHORD OF FLOORBEAM CORRODED THE ENTIRE LENGTH AT STA 1322 LT, RT AND CENTER AISLE. THE FLOORBEAM WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 20A.Apr 8, 2000 · N16804 · Doug DC982 · Fuselage Main, Floor BeamSDR CALA0000442Cargo Track · corrodedINSPECTION FOUND RT CARGO TIE DOWN TRACK CORRODED IN AFT PIT AT FS 1007 - 1360. THE TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1 AND 51-30-2.Apr 8, 2000 · N16804 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0000441Skin · gougedINSPECTION FOUND EXTERNAL FUSELAGE SKIN GOUGED AT FS 487 BETWEEN LONGERON 23 RT AND 24 RT. A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38.Apr 8, 2000 · N16804 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0000440Floor Support · corrodedINSPECTION FOUND FLOOR SUPPORT AT RT AFT LAV CENTER AISLE, FS 1307 - 1338 CORRODED. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-01.Apr 8, 2000 · N16804 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000439Web · wornINSPECTION FOUND A HOLE WORN INTO CUSP WEB AT FS 220, RBL 54. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-01, PAGE 18, 53-11-3, PAGE 49, 51-30-08, AND 53-01, FIGURE 4.Apr 8, 2000 · N16804 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000438Web · crackedINSPECTION FOUND A 1 INCH CRACK IN L-1 DOOR CUSP WEB AT AFT END AND BULGING AT RIVETS, FS 198. FILLERS AND DOUBLERS WERE INSTALLED IAW ECRA 5320-01638 AND SRM 51-10-3.Apr 8, 2000 · N16804 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000452Cargo Track · corrodedINSPECTION FOUND MID CARGO BAY FLOOR, LT CARGO TRACK CORRODED AROUND CLIPNUT HOLES ON LOWER SURFACE, FS 579 - 676. THE CARGO TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1 AND 51-30-2.Apr 8, 2000 · N16804 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0000451Floor Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT RT FS 1007 IN AFT CARGO BAY. THE SUPPORT WAS REMOVED AND A NEW SUPPORT AND REPAIR DOUBLER WERE INSTALLED IAW SRM 51-30-2, 53-01, FIGURE 2, 51-10-3, AND 51-60, FIGURE 1.Apr 8, 2000 · N16804 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000450Floor Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED JUST INSIDE AFT CARGO BAY DOORWAY. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-1.Apr 8, 2000 · N16804 · Doug DC982 · Fuselage Miscellaneous Structure
Back to N16804, cancelled May 16, 2006