N70542, cancelled Jul 14, 2000

Service difficulty reports · 47

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 = 'N70542' AND deregistration_id = 'N70542-2000-07-14'
  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 CALA9801853Vane · gougedINSPECTION FOUND RT WING UPPER MOVEABLE VANE LEADING EDGE GOUGED. A REPAIR WAS INSTALLED IAW SRM 57-01, FIGURE 1, 51-10-4, 51-10-3, 51-30-2, AND 51-10-2.Sep 22, 1998 · N70542 · Doug DC932 · Trailing Edge FlapsSDR CALA9801836Skin · dentedINSPECTION FOUND FUSELAGE SKIN DENTED AT STA 160, LONGERON 26R. THE DENTED AREA WAS CUT OUT IAW ECRA 5331-01030. DOUBLERS AND FILLER WERE INSTALLED IAW ECRA 5331-01030, SRM 51-10-3 AND 51-30-2.Sep 19, 1998 · N70542 · Doug DC932 · Fuselage Main, Plate/SkinSDR CALA9801813Skin · lightning strikeINSPECTION FOUND LIGHTNING STRIKE DAMAGE IN LT FUSELAGE SKIN AT STRINGER 25L, STA 246. THE DAMAGED AREA WAS CUT OUT, DOUBLER AND FILLER WERE INSTALLED IAW ECRA 5331-01031.Sep 17, 1998 · N70542 · Doug DC932 · Fuselage Main, Plate/SkinSDR CALA9801812Seat Track · corrodedINSPECTION FOUND FORWARD COCKPIT CO-PILOT'S SEAT TRACK CORRODED AT STA 203.9. THE SEAT TRACK WAS REMOVED AND REPLACED IAW MM 53-40-1.Sep 17, 1998 · N70542 · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR CALA9801778Skin · crackedINSPECTION FOUND TOP OF FUSELAGE AFT ADF LOOP ANTENNA MOUNTING SURFACE EXTERNAL SKIN CRACKED AT RT CENTER MOUNT HOLE, STA 259 LONGERON 1R, BL 0 AND AT RT MOUNT HOLE, STA 265, LONGERON 1R, BL 0. BOTH CRACKS WERE .375 INCH LONG. THE CRACKED AREAS OF SKIN WERE Sep 15, 1998 · N70542 · Doug DC932 · Fuselage Main, Plate/SkinSDR CALA9801752Fairing · delaminatedINSPECTION FOUND LT HORIZONTAL STABILIZER UPPER FAIRING DELAMINATED FROM AFT ATTACH POINT FORWARD. REMOVED PAN ON LOWER SURFACE AND REMOVED DELAMINATED HONEYCOMB. NEW HONEYCOMB WAS BONDED IN LOWER PAN AND THEN PAN WAS INSTALLED ON FAIRING AND BONDED IAW SRM 5Sep 14, 1998 · N70542 · Doug DC932 · Horizontal Stabilizer StructureSDR CALA9801751Fairing · delaminatedINSPECTION FOUND RT LOWER HORIZONTAL STABILIZER FAIRING DELAMINATED AT FWD END. THE DELAMINATED HONEYCOMB CORE, DOUBLER, AND PLATE WERE REMOVED. BONDED DOUBLER WITH HONEYCOMB CORE AND PLATE TO SKIN FAIRING IAW ECRA 5510-01317, SRM 51-70-2, 51-30-2.Sep 14, 1998 · N70542 · Doug DC932 · Horizontal Stabilizer StructureSDR CALA9801750Frame · gougedINSPECTION FOUND FRAME GOUGED AT STA 332, LONGERON 29L TO 30. A SPLICE AND PLATE REPAIR WAS INSTALLED IAW SRM 53-03, FIGURE 2A AND 51-10-2A.Sep 14, 1998 · N70542 · Doug DC932 · Fuselage Main, FrameSDR CALA9801749Fitting · gougedINSPECTION FOUND FLAP FITTING GOUGED AT AFT END OF LT WING AFT MOVEABLE VANE INBOARD TRACK STA XFLS 65.612 TO 69.125. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-30-2.Sep 14, 1998 · N70542 · Doug DC932 · Trailing Edge FlapsSDR CALA9801748Web · crackedINSPECTION FOUND THREE 2 INCH CRACKS ON NR 1 ENGINE PYLON INTERNAL WEB AT STA 1065. THE CRACKS WERE STOP DRILLED IAW SRM 51-10-1. A REPAIR WAS INSTALLED IAW SRM 51-10-3 AND 54-01, FIGURE 2.Sep 14, 1998 · N70542 · Doug DC932 · Nacelle/Pylon StructureSDR CALA9801747Tab · delaminatedINSPECTION FOUND TWO AREAS OF DELAMINATION ON UPPER SURFACE OF LT ELEVATOR CONTROL TAB BETWEEN THIRD AND OUTBOARD HINGES. THE DELAMINATED AREAS WERE TRIMMED OUT AND FILLER AND DOUBLER WERE INSTALLED IAW SRM 51-70-2.Sep 14, 1998 · N70542 · Doug DC932 · Elevator, Tab StructureSDR CALA9801746Skin · crackedINSPECTION FOUND A 1 INCH CRACK IN FUSELAGE SKIN AT STA 950, THREE INCHES BELOW LONGERON 14L. THE CRACKED AREA WAS REMOVED IAW SRM 53-04, FIGURE 38. A DOUBLER AND FILLER REPAIR WAS INSTALLED IAW SRM 51-10-3 AND 53-04, FIGURE 38.Sep 14, 1998 · N70542 · Doug DC932 · Fuselage Main, Plate/SkinSDR CALA9801686Bracket · corrodedINSPECTION FOUND SUPPORT BRACKET CORRODED AT STA 917, STRINGER 28L. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-10-3, 51-10-4, AND 51-30-1.Sep 9, 1998 · N70542 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9801685Hat Channel · crackedINSPECTION FOUND A 3 CRACK IN HAT CHANNEL AT FLOORBOARD PANEL, LT SIDE, STA 756. A NEW HAT CHANNEL SECTION WAS INSTALLED IAW SRM 53-05, PAGE 1 AND 51-30-2.Sep 9, 1998 · N70542 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9801659Fairing · crackedINSPECTION FOUND A 4.5 INCH CRACK IN LOWER AFT END OF RT HORIZONTAL STABILIZER LOWER FAIRING. THE CRACK WAS STOP DRILLED. A DOUBLER WAS INSTALLED IAW SRM 55-11-0 FIGURE 7, 55-01, FIGURE 2, 51-10-3, AND 51-30-2.Sep 8, 1998 · N70542 · Doug DC932 · Horizontal Stabilizer StructureSDR CALA9801654Doubler · crackedINSPECTION FOUND TWO 1 INCH CRACKS IN DOUBLER AT STA 945, LONGERON 14R. THE DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 53-03, FIGURE 28.Sep 8, 1998 · N70542 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9801653Floor · crackedINSPECTION FOUND 1 INCH CRACKS AT CLIP NUT HOLES IN FLOOR PANEL NR 47 FORWAD OF STA 756. A NEW FLOOR PANEL WAS INSTALLED IAW SRM 53-21, 51-30-2, AND 53-05, FIGURE 1.Sep 8, 1998 · N70542 · Doug DC932 · Fuselage Floor PanelSDR CALA9801636Frame · crackedINSPECTION FOUND A 1 INCH CRACK AT UPPER MOUNT HOLE OF FRAME AT STA 980, LONGERON 16R. THE CRACKED AREA WAS REMOVED. A REPAIR WAS INSTALLED IAW SRM 51-30-1.Sep 4, 1998 · N70542 · Doug DC932 · Fuselage Main, FrameSDR CALA9801621Web · corrodedINSPECTION FOUND WEB CORRODED AT FORWARD CARGO DOOR, STA 370, STRINGER 28R. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-01, FIGURE 2.Sep 2, 1998 · N70542 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9801620Skin · crackedINSPECTION FOUND A .25 INCH CRACK AT FASTENER IN TAIL SECTION SKIN AT STA 1062 APPROXIMATELY FOUR INCHES BELOW LONGERON 15L. THE FASTENER WAS REMOVED IAW SRM 51-30-2 AND THE CRACKED AREA WAS CUT OUT IAW SRM 53-04, FIGURE 28. A DOUBLER REPAIR WAS INSTALLED IASep 2, 1998 · N70542 · Doug DC932 · Fuselage Main, Plate/SkinSDR CALA9801619Bulkhead Strap · crackedINSPECTION FOUND A 1 INCH CRACK IN LOWER SUPPORT STRAP OF FORWARD BULKHEAD WALL IN AFT PIT, FS 737. THE SUPPORT STRAP WAS REMOVED AND A NEW SUPPORT STRAP WAS INSTALLED IAW SRM 51-10-2, 51-10-4, AND 51-10-3.Sep 2, 1998 · N70542 · Doug DC932 · Fuselage Main, BulkheadSDR CALA9801610Longeron · crackedINSPECTION FOUND A 2 INCH CRACK IN LONGERON 17L AT ANGLE MOUNT, STA 965. THE CRACKED SECTION OF LONGERON WAS CUT OUT IAW SRM 53-02, FIGURE 18. A NEW LONGERON SECTION AND SPLICE WERE INSTALLED IAW SRM 51-30-5.Sep 1, 1998 · N70542 · Doug DC932 · Fuselage Main, Longeron/StringerSDR CALA9801586Clip · crackedINSPECTION FOUND A 2 INCH CRACK IN SHEAR TIE CLIP AT LT AFT CABIN STA 965 UNDER LONGERON 13L. THE CRACK WAS REMOVED AND A CLIP REPAIR WAS INSTALLED IAW SRM 53-03, FIGURE 28.Aug 28, 1998 · N70542 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9801585Skin · crackedINSPECTION FOUND A 1 INCH CRACK IN FORWARD CARGO DOOR SKIN AT LOWER AFT CORNER. THE CRACKED AREA WAS CUT OUT AND A DOUBLER AND FILLER REPAIR WAS INSTALLED IAW SRM 52-01, FIGURE 4.Aug 28, 1998 · N70542 · Doug DC932 · Cargo/Baggage DoorsSDR CALA9601153Cables · out of adjustTAILCONE RELEASE USING INTERIOR HANDLE PULLED LOW AT 15 POUNDS. THE TAILCONE CABLES WERE ADJUSTED IAW MM 53-50-00.Aug 9, 1996 · N70542 · Doug DC932 · Aerodynamic FairingsSDR CALA9601194Skin · corrodedINSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 594, LONGERON 17R. THE CORROSION WAS REMOVED AND AN INTERNAL DOUBLER WAS INSTALLED IAW ECRA 5330-02427.Aug 6, 1996 · N70542 · Doug DC932 · Fuselage Main, Plate/SkinSDR CALA9601195Skin · crackedINSPECTION FOUND A 5 INCH CRACK IN RT ELEVATOR LOWER SKIN AT STA XHS 86.0. AN EXTERNAL DOUBLER WAS INSTALLED IAW ECRA 5530-01174 AND SRM 55-03, FIGURE 13.Aug 1, 1996 · N70542 · Doug DC932 · Elevator, Plate/SkinSDR CALA9601225Frame · crackedINSPECTION FOUND BELTFRAME CRACKED IN TWO PLACES AT STA 446, LONGERON 5L. THE CRACKS WERE 3 LONG. THE CRACKED SECTION OF FRAME WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 53-03, FIGURE 4.Jul 30, 1996 · N70542 · Doug DC932 · Fuselage Main, FrameSDR CALA9601224Frame · crackedINSPECTION FOUND BELTFRAME CRACKED IN TWO PLACES AT STA 446, LONGERON 5R. THE CRACKS WERE 2.5 LONG. THE CRACKED SECTION OF FRAME WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 53-03, FIGURE 4.Jul 30, 1996 · N70542 · Doug DC932 · Fuselage Main, FrameSDR CALA9601223Frame · crackedINSPECTION FOUND BELTFRAME CRACKED IN TWO PLACES AT STA 427, LONGERON 5R. THE CRACKS WERE 1.5 LONG. THE CRACKED SECTION OF FRAME WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 53-03, FIGURE 4.Jul 30, 1996 · N70542 · Doug DC932 · Fuselage Main, FrameSDR CALA9601222Frame · crackedINSPECTION FOUND BELTFRAME CRACKED IN TWO PLACES AT STA 427, LONGERON 5L. THE CRACKS WERE 3.5 LONG. THE CRACKED SECTION OF FRAME WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 53-03, FIGURE 4.Jul 30, 1996 · N70542 · Doug DC932 · Fuselage Main, FrameSDR CALA9601198Longeron · crackedINSPECTION FOUND LONGERON 5R CRACKED AT STA 737. A NEW SECTION OF LONGERON WAS SPLICED IN IAW SRM 53-02, FIGURE 2.Jul 30, 1996 · N70542 · Doug DC932 · Fuselage Main, Longeron/StringerSDR CALA9601192Longeron · crackedINSPECTION FOUND LONGERON 3L CRACKED AT STA 160. THE CRACKED SECTION OF LONGERON WAS REMOVED AND A NEW SECTION WAS SPLICED IN IAW SRM 53-02, FIGURE 2.Jul 30, 1996 · N70542 · Doug DC932 · Fuselage Main, Longeron/StringerSDR CALA9601191Longeron · crackedINSPECTION FOUND LONGERON 4L CRACKED AT STA 200. THE LONGERON WAS REMOVED AND REPLACED IAW SRM 53-02, FIGURE 2.Jul 30, 1996 · N70542 · Doug DC932 · Fuselage Main, Longeron/StringerSDR CALA9601190Longeron · crackedINSPECTION FOUND LONGERON 4L CRACKED AT STA 160. THE LONGERON WAS REMOVED AND REPLACED IAW SRM 53-02, FIGURE 2.Jul 30, 1996 · N70542 · Doug DC932 · Fuselage Main, Longeron/StringerSDR CALA9601144Spar · corrodedINSPECTION FOUND CORROSION ON UPPER SPAR CAP OF LT HORIZONTAL STABILIZER FORWARD SIDE OF REAR SPAR AT STA XHS 95. THE CORRODED SECTION OF SPAR CAP WAS CUT OUT AND A NEW SECTION WAS SPLICED IN IAW SRM 55-02, PAGES 85 TO 87.Jul 30, 1996 · N70542 · Doug DC932 · Horizontal Stabilizer, Spar/RibSDR CALA9601114Spar Nut · crackedINSPECTION FOUND, LT ELEVATOR MOST OUTBOARD BOTTOM NUT ON SPAR CRACKED. THE NUT WAS REMOVED AND REPLACED PER MM 20-16-0.Jul 30, 1996 · N70542 · Doug DC932 · Elevator, Spar/RibSDR CALA9601227Bulkhead Angle · crackedINSPECTION FOUND A 1 INCH CRACK IN FRONT SPAR TO PRESSURE BULKHEAD ATTACH ANGLE AT STA 598, LONGERON 24L. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-0.Jul 29, 1996 · N70542 · Doug DC932 · Fuselage Main, BulkheadSDR CALA9601226Bulkhead Angle · crackedINSPECTION FOUND A 3 INCH CRACK IN FRONT SPAR TO PRESSURE BULKHEAD ATTACH ANGLE AT STA 598, LONGERON 24R. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-0.Jul 29, 1996 · N70542 · Doug DC932 · Fuselage Main, BulkheadSDR CALA9601202Frame · crackedINSPECTION FOUND A CRACK IN FRAME JUST FORWARD OF RUDDER TRIM MOUNT AT TAIL COMPARTMENT STA 1143. A NEW ANGLE WAS INSTALLED ON FRAME IAW SRM 51-10-4.Jul 28, 1996 · N70542 · Doug DC932 · Fuselage Main, FrameSDR CALA9601193Support · crackedINSPECTION FOUND A .5 INCH CRACK ON FLOOR SUPPORT IN FORWARD CARGO COMPARTMENT AT STA 484, LONGERON 24R. A DOUBLER WAS INSTALLED IAW ECRA 5320C01263.Jul 28, 1996 · N70542 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9601201Rib · crackedINSPECTION FOUND A 1 INCH CRACK IN WING LEADING EDGE RIB AT NR 1 SLAT TRACK. THE RIB WAS REPAIRED IAW ECRA 5710-01751.Jul 27, 1996 · N70542 · Doug DC932 · Wing, Rib/BulkheadSDR CALA9601200Beam · crackedINSPECTION FOUND A .75 INCH CRACK IN FORWARD CARGO COMPARTMENT DOOR BEAM AT LOWER FORWARD STOP. A NEW PART WAS FABRICATED AND INSTALLED IAW SRM 51-30-3.Jul 27, 1996 · N70542 · Doug DC932 · Cargo/Baggage DoorsSDR CALA9601199Fitting · crackedINSPECTION FOUND A .375 INCH CRACK IN AFT CARGO COMPARTMENT DOOR FITTING INSIDE DOOR AT BOTTOM CENTER STOP. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-30-2.Jul 27, 1996 · N70542 · Doug DC932 · Cargo/Baggage DoorsSDR CALA9601197Beam · crackedINSPECTION FOUND A 1.5 INCH CRACK IN AFT CARGO COMPARTMENT DOOR BEAM AT UPPER FORWARD STOP. THE BEAM WAS REMOVED AND REPLACED IAW SRM 52-01, FIGURE 1.Jul 27, 1996 · N70542 · Doug DC932 · Cargo/Baggage DoorsSDR CALA9601196Beam · crackedINSPECTION FOUND A 1.5 INCH CRACK IN FORWARD CARGO COMPARTMENT DOOR BEAM AT UPPER FORWARD STOP. A REPAIR WAS DONE IAW SRM 51-30-2.Jul 27, 1996 · N70542 · Doug DC932 · Cargo/Baggage DoorsSDR CAL950783Fuel Coupling · leakingIAH - FLT 1230 - THE LEFT MAIN FUEL QUANTITY BEGAN TO DECREASE AS FUEL WAS TRANSFERRED FROM CENTER TANK AFTER TAKEOFF FROM IAH. THE LEFT FUEL QUANTITY STEADILY AND RAPIDLY DECREASED. THE CROSS-FEED WAS OPENED IN AN ATTEMPT TO BURN RT MAIN FUEL, BUT THE LT FUSep 2, 1995 · N70542 · Doug DC932 · Aircraft Fuel Distribution System
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