N33805, cancelled May 18, 2004

Service difficulty reports · 49

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 = 'N33805' AND deregistration_id = 'N33805-2004-05-18'
  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 CALA2000279Actuator · corrodedAFT VENTRAL STAIRS ACTUATOR LOWER TUBE, RT, IS CORRODED 2 INCHES. REPLACED RT LOWER STRUT ON VENTRAL STAIRS AND PERFORMED ADJUSTMENT AND TEST IAW MM 52-63-00.May 11, 2002 · N33805 · Doug DC982 · Entrance StairsSDR CALA0101000Battery Pack · dischargedTHE OVERWING EMERGENCY EXIT IDENTIFIERS ABOVE DOORS ON LT AND RT SIDE OF AIRCRAFT WERE FOUND INOPERATIVE. THE BATTERIES IN EMERGENCY BATTERY PACKS IN O/H BIN AT ROW 20DEF WERE REPLACED IAW MM 33-50-00.Nov 12, 2001 · N33805 · Doug DC982 · Emergency LightingSDR CALA0100958Power Supply · dischargedBOTH LEFT AND RIGHT OVERWING EVACUATION LIGHTS INOP. REMOVED AND REPLACED POWER SUPPLY PER MM 33-53-00 PAGE 407.Oct 17, 2001 · N33805 · Doug DC982 · Emergency LightingSDR CALA0100112Skin · dentedINSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT FS 275 BETWEEN LONGERON 22L AND 23L. THE DENT WAS COLD WORKED AND A DOUBLER WAS INSTALLED IAW SRM 53-04-38 AND 51-10-3.Feb 10, 2001 · N33805 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0100109Seat Track · corrodedINSPECTION FOUND CABIN LEFT I/B SEAT TRACK CORRODED AT FS 1031 - 1169. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-1 AND 53-05, FIGURE 4.Feb 9, 2001 · N33805 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0100098Cargo Track · corrodedINSPECTION FOUND MID CARGO LT TIE DOWN TRACK CORRODED AT FS 522 - 788. THE TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-2 AND 53-05, FIGURE 6.Feb 2, 2001 · N33805 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0100097Seat Track · corrodedINSPECTION FOUND CABIN LEFT O/B SEAT TRACK CORRODED AT FS 1117 - 1136. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SECTION OF TRACK WAS INSTALLED IAW SRM 53-05, FIGURE 4F.Feb 2, 2001 · N33805 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0100096Skin · gougedINSPECTION FOUND SKIN GOUGED AT AFT CARGO DOOR LOWER EDGE OF PAN. THE RIVETS WERE REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 51-30-2 AND EA 9-5230-2-A0832.Feb 2, 2001 · N33805 · Doug DC982 · Cargo/Baggage DoorsSDR CALA0100088Fitting · crackedINSPECTION FOUND A 1 INCH CRACK IN LEFT W/W FORWARD I/B (FWD OF MLG ATTACH) ANGLE T-FITTING. THE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-30-05 AND 51-30-3.Feb 1, 2001 · N33805 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0100083Skin · corrodedINSPECTION FOUND INNER SKIN DOUBLER CORRODED AT FS 1286 BETWEEN LONGERONS 21L AND 22L. THE INNER DOUBLER WAS REMOVED AND REPLACED IAW SRM 51-30-2, 51-30-5, AND ECRA 5332-01009.Jan 31, 2001 · N33805 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0100084Frame · crackedINSPECTION FOUND A 4 INCH CRACK IN AFT ACCESSORY COMPARTMENT FRAME UNDER RADIUS BLOCK AT LONGERON ATTACH POINT, FS 1446, LONGERON 5L. THE FRAME WAS REMOVED AND A NEW FRAME WAS INSTALLED IAW SRM 51-10-4, 53-03, FIGURE 30, AND 51-30-5.Jan 30, 2001 · N33805 · Doug DC982 · Fuselage Main, FrameSDR CALA0100080Pan · crackedINSPECTION FOUND A 1 INCH CRACK IN MID CARGO DOOR PAN. THE CRACK WAS STOP DRILLED IAW SRM 52-03, FIGURE 8. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-03, FIGURE 8, 51-10-3, AND 51-30-2.Jan 29, 2001 · N33805 · Doug DC982 · Cargo/Baggage DoorsSDR CALA0100079Floorbeam · corrodedINSPECTION FOUND AFT LT LAV FLOORBEAM CORRODED AT STA 1322, LBL 41. THE CORROSION WAS TRIMMED OUT AND A DOUBLER, REPAIR STRIP, AND SHIM WERE INSTALLED IAW SRM 53-05, FIGURE 20A, 51-30-2, AND 51-30-5.Jan 29, 2001 · N33805 · Doug DC982 · Fuselage Main, Floor BeamSDR CALA0100076Skin · dentedINSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT FS 275 BETWEEN LONGERONS 21L AND 22L. THE DENT WAS COLD WORKED IAW SRM 53-04-38. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-04-38, 51-10-3, AND 51-30-2.Jan 27, 2001 · N33805 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0100075Web · corrodedINSPECTION FOUND AFT CARGO DOOR WEB CORRODED AROUND ATTACH RIVNUT HOLES. THE CORROSION WAS REMOVED IAW SRM 51-10-3. THE CORRODED AREAS WERE REPAIRED IAW SRM 52-01, FIGURE 2 AND 51-10-3.Jan 27, 2001 · N33805 · Doug DC982 · Cargo/Baggage DoorsSDR CALA0100074Fitting · crackedINSPECTION FOUND A 2 INCH CRACK IN AFT CARGO DOOR LOWER FITTING. THE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-30-2, 51-10-4, 51-10-3, AND 51-30-1.Jan 26, 2001 · N33805 · Doug DC982 · Cargo/Baggage DoorsSDR CALA0100073Skin · dentedINSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT FS 237 BETWEEN LONGERONS 17L AND 18L. THE SKIN WAS REMOVED AND REPLACED IAW SRM 53-34-0, FIGURE 2, PAGE 7, 51-30-2, 51-30-5, AND 51-10-3.Jan 26, 2001 · N33805 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0100072Skin · crackedINSPECTION FOUND A 1 INCH CRACK IN LT FUSELAGE SKIN ABOVE NR 1 ENGINE PYLON AT STA 1401. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 2, SHEET 3, 53-10-3, AND 51-30-2.Jan 26, 2001 · N33805 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0100071Structure · crackedINSPECTION FOUND TWO 1 INCH CRACKS IN FORWARD LOWER CORNER OF LT MLG I/B DOOR. THE CRACKS WERE STOP DRILLED AND DOUBLERS WERE INSTALLED IAW SRM 51-10-4, 51-10-3, 51-30-2, 51-30-5, AND EA 9-5331-2-A0831.Jan 25, 2001 · N33805 · Doug DC982 · Landing Gear DoorsSDR CALA0100068Angle · corrodedINSPECTION FOUND CUSP ANGLE AT L-1 DOOR, FS 200, LBL 54 CORRODED. THE CUSP ANGLE WAS REMOVED AND REPLACED IAW EA 9-5310-2-A0829 AND ECRA 5310-04094.Jan 24, 2001 · N33805 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0100067Fitting · crackedINSPECTION FOUND A 1 INCH CRACK IN MID CARGO DOOR FITTING AND WITH UPPER INTERCOSTAL CLIP CRACKED. THE FITTING AND T-ANGLE WERE REMOVED AND A NEW FITTING AND ANGLE WERE INSTALLED IAW SRM 51-10-4, 51-30-2, AND 51-30-1.Jan 24, 2001 · N33805 · Doug DC982 · Cargo/Baggage DoorsSDR CALA0100065Skin · dentedINSPECTION FOUND LT FORWARD FUSELAGE SKIN DENTED AT FS 133, L10L. THE DENT WAS COLD WORKED AND A DOUBLER WAS INSTALLED IAW SRM 51-30-5, 51-30-2, 53-04, FIGURE 35, 51-10-3, AND EA 9-5331-2-A0835.Jan 23, 2001 · N33805 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0100064Skin · dentedINSPECTION FOUND FUSELAGE EXTERNAL SKIN AT FORWARD LT SIDE OF E AND E DOOR CUTOUT STA 145, L28L DENTED. THE SKIN WAS REPAIRED BY INSTALLING FILLER AND DOUBLERS IAW EA 9-5331-2-A0834 AND SRM 51-10-3.Jan 23, 2001 · N33805 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0100054Fitting · crackedINSPECTION FOUND A 3 INCH CRACK IN FORWARD CARGO DOOR FITTING I/B OF AFT HINGE. THE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-30-1, 51-30-2, 51-10-4, AND 51-10-3.Jan 22, 2001 · N33805 · Doug DC982 · Cargo/Baggage DoorsSDR CALA0100053Seat Track · corrodedINSPECTION FOUND CABIN LT CENTER SEAT TRACK CORRODED AT FS 1032 - 1184. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 4F.Jan 22, 2001 · N33805 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0100052Skin · dentedINSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT FS 230 BETWEEN LONGERON 19L AND 20L. THE DENTED AREA WAS CUT OUT IAW SRM 53-04, FIGURE 25. A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 25, 51-30-2, 51-30-4, AND 51-30-5.Jan 21, 2001 · N33805 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0100051Door Frame · crackedINSPECTION FOUND A 1 INCH CRACK (PAST STOP DRILL) IN RT MLG DOOR SUPPORT FRAME AT STA 946, RBL 10. THE EXISTING REPAIR DOUBLERS WERE REMOVED FOR ACCESS IAW SRM 51-30-2. THE CRACK WAS STOP DRILLED IAW SRM 51-10-4. THE REPAIR DOUBLERS WERE REINSTALLED IAW SRMJan 21, 2001 · N33805 · Doug DC982 · Fuselage Main, StructureSDR CALA0100044Skin · dentedINSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT FS 260 BETWEEN LONGERONS 24R AND 25R AND BETWEEN LONGERONS 27L AND 28L. A DOUBLER WAS INSTALLED AT EACH LOCATION IAW SRM 53-04, FIGURE 38, 51-10-4, 51-10-3, AND 51-30-2.Jan 17, 2001 · N33805 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0100043Skin · dentedINSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT FS 375 BETWEEN LONGERON 29L AND 30 AND AT FS 470, BETWEEN LONGERONS 20L AND 21L. A DOUBLER WAS INSTALLED AT EACH LOCATION IAW SRM 53-04, FIGURE 38, 51-10-4, 51-10-3, AND 51-30-2.Jan 17, 2001 · N33805 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0100038Skin · dentedINSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT FS 500 - 520 BETWEEN LONGERONS 20R AND 21R AND AT FS 550 - 560 BETWEEN LONGERONS 21L AND 22L. THE DENTS WERE COLD WORKED AND DOUBLERS WERE INSTALLED AT EACH LOCATION IAW SRM 53-04-38 AND 51-30-2.Jan 16, 2001 · N33805 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0100037Frame · crackedINSPECTION FOUND E&E COMPARTMENT FRAME CRACKED PAST STOP DRILL HOLE AT FS 150, L21R. THE EXISTING REPAIR WAS REMOVED, THE CRACK WAS STOP DRILLED, AND A REPAIR WAS INSTALLED IAW SRM 51-30-05 AND 51-10-4.Jan 16, 2001 · N33805 · Doug DC982 · Fuselage Main, FrameSDR CALA9901474Power Supply · inopINSPECTION FOUND EMERGENCY OVERHEAD LIGHTS INOPERATIVE AT ROWS 23-27. THE BATTERY POWER SUPPLY AT STATION 1150 IN RT OVERHEAD BIN WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD IAW MM 33-53-00.Nov 6, 1999 · N33805 · Doug DC982 · Emergency LightingSDR CALA9900117Skin · dentedINSPECTION FOUND THE FUSELAGE SKIN DENTED AT STA 218, LONGERON 17L. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5330-02766.Feb 5, 1999 · N33805 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA9900116Brace · crackedINSPECTION FOUND A CRACK OF UNSPECIFIED LENGTH IN THE LT GROUND SPOILER ACTUATOR I/B ATTACH BRACKET CROSS BRACE. A NEW CROSS BRACE WAS INSTALLED IAW SRM 51-30-5.Feb 5, 1999 · N33805 · Doug DC982 · SpoilersSDR CALA9900107Escape Line · frayedINSPECTION FOUND THE LT AND RT OVERWING EMERGENCY ESCAPE LINES FRAYED. NEW ESCAPE LINE WAS INSTALLED IAW SRM 51-30-1 AND MM 25-61-00, FIGURE 202.Feb 2, 1999 · N33805 · Doug DC982 · Emergency EquipmentSDR CALA9900095Beam · crackedINSPECTION FOUND A .5 INCH CRACK IN FORWARD SERVICE DOOR NR 4 HORIZONTAL BEAM. THE BEAM WAS REMOVED AND REPLACED IAW SRM 51-30.Jan 29, 1999 · N33805 · Doug DC982 · Service DoorsSDR CALA9900094Beam · crackedINSPECTION FOUND A .75 INCH CRACK IN OUTBOARD RADIUS OF MAIN CABIN DOOR TOP NR 1 HORIZONTAL BEAM. THE BEAM WAS REMOVED AND REPLACED IAW SRM 51-30-2.Jan 29, 1999 · N33805 · Doug DC982 · Passenger/Crew DoorsSDR CALA9701503Fcu · leakingWHILE OPERATING THE APU WITH THE NR 1 GENERATOR PLACARDED INOPERATIVE, THE APU AUTO SHUTDOWN WHEN CLIMBING THROUGH 28,000 FEET. THE APU WAS RESTARTED AT 26,000 FEET AND THE AIRCRAFT LANDED WITHOUT FURTHER PROBLEM. THE APU FCU WAS FOUND LEAKING. THE APU FCU Oct 24, 1997 · N33805 · Doug DC982 · APU Engine Fuel and ControlSDR CALA9700222Power Supply · inoperativeINSPECTION FOUND TWO EXTERIOR OVERWING EMERGENCY EVACUATION LIGHTS INOPERATIVE. MAINTENANCE FOUND THE POWER SUPPLY AT FAULT. THE POWER SUPPLY WAS REMOVED AND REPLACED.Feb 19, 1997 · N33805 · Doug DC982 · Emergency LightingSDR CALA9700152Door Pan · crackedINSPECTION FOUND A 3 INCH CRACK IN MAIN BAGGAGE BIN DOOR PAN AT LOCK AFT CAM AREA. THE PAN WAS REPAIRED IAW ECRA 5210-01283 AND SRM 52-05, FIGURE 26A.Jan 28, 1997 · N33805 · Doug DC982 · Cargo/Baggage DoorsSDR CALA9700147Door Pan · crackedINSPECTION FOUND A 3 INCH CRACK IN FORWARD BAGGAGE BIN DOOR PAN AT LOCK CAM AREA. THE PAN WAS REPAIRED IAW ECRA 5210-01283 AND SRM 52-05, FIGURE 26A.Jan 27, 1997 · N33805 · Doug DC982 · Cargo/Baggage DoorsSDR CALA9700154Fitting · crackedINSPECTION FOUND A 2.5 INCH CRACK IN UPPER RIGHT FITTING AND A 1.5 INCH CRACK IN UPPER LEFT FITTING AT MAIN BAGGAGE BIN STA 826. THE FITTINGS WERE REPLACED IAW SRM 51-30-5.Jan 22, 1997 · N33805 · Doug DC982 · Fuselage, Door HingeSDR CALA9700153Belt Frame · corrodedINSPECTION FOUND BELT FRAME LOWER CHANNEL CORRODED AT STA 1307, LONGERON 27R TO 27L. THE CORRODED SECTION OF BELT FRAME WAS CUT OUT, A NEW SEGMENT OF FRAME AND REPAIR DOUBLERS WERE INSTALLED IAW SRM 53-03, FIGURE 2A.Jan 22, 1997 · N33805 · Doug DC982 · Fuselage Main, FrameSDR CALA9700151Door Pan · crackedINSPECTION FOUND A 1.25 INCH CRACK AT LOWER HINGE CUTOUT OF MAIN CABIN DOOR PAN. THE PAN WAS REPLACED IAW SRM 52-11-0.Jan 21, 1997 · N33805 · Doug DC982 · Passenger/Crew DoorsSDR CALA9700150Angle · corrodedINSPECTION FOUND Z-ANGLE AND FLOOR MOUNTS CORRODED AT AFT SERVICE DOOR THRESHOLD. A NEW Z-ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-30-2.Jan 20, 1997 · N33805 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA9700149Rib · crackedINSPECTION FOUND A .5 INCH CRACK IN LT WING LEADING EDGE RIB JUST OUTBOARD OF 8L SLAT TRACK AT STA XRS 270. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5710-01776.Jan 20, 1997 · N33805 · Doug DC982 · Wing, Rib/BulkheadSDR CALA9700148Rib · crackedINSPECTION FOUND A .5 INCH CRACK IN RT WING LEADING EDGE RIB, TWO RIBS OUTBOARD OF 8R SLAT TRACK, STA XRS 277. A DOUBLER WAS INSTALLED IAW SRM 57-01.Jan 20, 1997 · N33805 · Doug DC982 · Wing, Rib/BulkheadSDR CALA9600647Actuator · inoperativeTHE NOSE GEAR WAS SLOW TO RETRACT AFTER TAKEOFF. THE RED LIGHT EXTINGUISHED AND DOORS CLOSED AFTER APPROXIMATELY 20 TO 25 SECONDS. THE FLIGHT WAS CONTINUED AND THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE FOUND THE NOSE GEAR RETRACT CYLINDER AT May 25, 1996 · N33805 · Doug DC982 · Landing Gear ActuatorSDR CAL950114Circuit Breaker · failedFLT NR 0246 - IAH - SEVERAL LEFT AC BUS CIRCUIT BREAKERS BEGAN POPPING AFTER TAKEOFF FROM IAH. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE B1-743 TO AMP 'C' PHASE CIRCUIT BREAKER ON LEFT GENERATOR PANEL AT FAULT. Feb 10, 1995 · N33805 · Doug DC982 · AC Power Distribution System
Back to N33805, cancelled May 18, 2004