N35832, cancelled Apr 17, 2006

Service difficulty reports · 119

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 = 'N35832' AND deregistration_id = 'N35832-2006-04-17'
  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 CALA0400143Longeron · corrodedINSPECTION FOUND LONGERON 30 CORRODED FORWARD OF SPLICE IN FORWARD BAGGAGE BIN BETWEEN STA 484 AND 503. THE CORRODED SECTION OF LONGERON WAS REMOVED AND A SPLICE AND LONGERON SECTION WERE INSTALLED IAW SRM 53-02, FIGURE 18.Feb 20, 2004 · N35832 · Doug DC982 · Fuselage Main, Longeron/StringerSDR CALA0400130Cable · out of rigTHE TAIL CONE WOULD NOT DEPLOY USING AFT ENTRY DOOR HANDLE. THE TAIL CONE CABLES WERE RIGGED IAW MM 53-53-00.Feb 17, 2004 · N35832 · Doug DC982 · Emergency ExitsSDR CALA0300006Longeron · crackedINSPECTION FOUND A 1" CRACK IN LONGERON 2L AT AFT SIDE OF BELTFRAME, STA 1415. A LONGERON SPLICE WAS INSTALLED IAW SRM 53-02.Jan 9, 2003 · N35832 · Doug DC982 · Fuselage Main, Longeron/StringerSDR CALA0100990Intercostal · corrodedINSPECTION FOUND INTERCOSTAL CORRODED AT LOWER SECTION OF AFT BAGGAGE BIN DOOR CUTOUT, STA 1174. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 53-01, FIGURE 1 AND 51-30-2.Oct 30, 2001 · N35832 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0100985Skin · crackedINSPECTION FOUND A 1.5" CRACK IN R/H WING UPPER L/E SKIN BETWEEN #2 & #3 SLAT PANELS AT WS XOS 286. A SKIN DOUBLER REPAIR WAS INSTALLED IAW ECRA 5720-01731.Oct 29, 2001 · N35832 · Doug DC982 · Wing, Plate/SkinSDR CALA0001406Channel · corrodedINSPECTION FOUND DOME NUT GANG CHANNEL AND OUTER SHIM OF LT WING LOWER FUEL TANK OPENING (PANEL 1371C) CORRODED. THE RUB STRIP AND GANG CHANNEL WERE REMOVED AND REPLACED IAW SRM 51-22-2 AND ECRA 5100-02063.Sep 8, 2000 · N35832 · Doug DC982 · Wing Miscellaneous StructureSDR CALA0001405Access Panel · crackedINSPECTION FOUND A .5 INCH CRACK AT LAST RIVET HOLE IN THE FIXED SECTION ON O/B SIDE OF RT HORIZONTAL STABILIZER ELEVATOR ACCESS TO ELEVATOR GEAR TAB MECHANISM 3616A. THE PUSH ROD AND CONDUIT WERE REMOVED TO GAIN ACCESS IAW SRM 51-30-2. THE CRACK WAS STOP DSep 8, 2000 · N35832 · Doug DC982 · Horizontal Stabilizer, Plate/SkinSDR CALA0001404Skin · dentedINSPECTION FOUND THE LT NR 5 SLAT LEADING EDGE DENTED. THE SLAT WAS REMOVED, REPAIRED, AND REINSTALLED IAW MM 27-80-01, SRM 57-06, FIGURE 1, AND 51-30-2.Sep 8, 2000 · N35832 · Doug DC982 · Leading Edge DevicesSDR CALA0001393Floor Panel · corrodedINSPECTION FOUND R-1 ENTRYWAY FLOOR PANEL CORRODED AT FS 148 - 200. THE CORRODED FLOOR PANEL AREA WAS REPAIRED IAW SRM 53-24-0, FIGURE 3, 51-10-3, AND ECRA 5100-01844.Sep 4, 2000 · N35832 · Doug DC982 · Fuselage Floor PanelSDR CALA0001391Access Panel · corrodedINSPECTION FOUND LT WING FUEL ACCESS PANELS 1303C, 1355C, AND 1363C CORRODED AND GOUGED. THE FUEL PANELS WERE REMOVED AND REPLACED IAW ECRA 5730-01688.Sep 3, 2000 · N35832 · Doug DC982 · Wing, Plate/SkinSDR CALA0001390Access Panel · corrodedINSPECTION FOUND RT WING FUEL ACCESS PANELS 1410C, 1409C, AND 1436C CORRODED AND GOUGED. THE FUEL PANELS WERE REMOVED AND REPLACED IAW ECRA 5730-01688.Sep 3, 2000 · N35832 · Doug DC982 · Wing, Plate/SkinSDR CALA0001368Slat Track · gougedINSPECTION FOUND RT WING NR 5 SLAT TRACK GOUGED. THE SLAT TRACK WAS REMOVED AND REPLACED IAW MM 27-80-01.Sep 2, 2000 · N35832 · Doug DC982 · Leading Edge DevicesSDR CALA0001362Panel · gougedINSPECTION FOUND LT WING LOWER SURFACE FUEL ACCESS PANEL NR 2 GOUGED. THE PANEL WAS REPAIRED IAW SRM 5730-01688 AND SRM 51-30-2.Sep 1, 2000 · N35832 · Doug DC982 · Wing, Plate/SkinSDR CALA0001358Fitting · corrodedINSPECTION FOUND LEFT O/B FLIGHT SPOILER CENTER FITTING CORRODED. THE SPOILER WAS REMOVED IAW MM 27-62-01. THE HINGE FITTING WAS REMOVED AND REPLACED IAW OHM 27-61-10 AND THE SPOILER WAS REINSTALLED IAW MM 27-61-01.Sep 1, 2000 · N35832 · Doug DC982 · SpoilersSDR CALA0001357Access Panel · gougedINSPECTION FOUND FUEL ACCESS PANELS NR 1, 6 AND 7 GOUGED AND CORRODED ON RT WING LOWER SURFACE. THE PANELS WERE REPAIRED IAW ECRA 5730-01688 AND SRM 51-30-2.Sep 1, 2000 · N35832 · Doug DC982 · Wing, Plate/SkinSDR CALA0001356Fitting · crackedINSPECTION FOUND TWO 1 INCH CRACKS AT FASTENER HOLE OF RT WING NR 5 SLAT END FITTING. THE SEAL AND RETAINER ON END FITTING WERE REMOVED IAW SRM 51-30-3. THE CRACKS WERE WELDED IAW DPS 10.225. THE SEAL AND RETAINER WERE REINSTALLED IAW SRM 51-30-2.Sep 1, 2000 · N35832 · Doug DC982 · Leading Edge DevicesSDR CALA0001355Floor Panel · corrodedINSPECTION FOUND AFT CARGO FLOOR PANEL CORRODED AND DENTED AT STA 1211 - 1231. THE FLOOR PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW SRM 53-24-0, FIGURE 1A, 51-10-2, AND 51-60-0, PAGE 5.Sep 1, 2000 · N35832 · Doug DC982 · Fuselage Floor PanelSDR CALA0001350Floor Panel · corrodedINSPECTION FOUND AFT CARGO FLOOR PANEL CORRODED AT FS 1211 - 1231. THE FLOOR PANEL WAS REPLACED IAW SRM 53-24-0, FIGURE 11A, 51-10-2, AND 51-60-0, PAGE 5.Aug 30, 2000 · N35832 · Doug DC982 · Fuselage Floor PanelSDR CALA0001349Fitting · corrodedINSPECTION FOUND NR 4 GALLEY ATTACH MOUNT FITTINGS (2) CORRODED. THE FITTINGS WERE REMOVED AND REPLACED IAW ECRA 2530-01257.Aug 30, 2000 · N35832 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001342Floor Support · crackedINSPECTION FOUND A 6 INCH CRACK IN MID CARGO BAY FIBERGLASS FLOOR SUPPORT ANGLE AT STA 617, LONGERON 26R TO 27R. THE FLOOR SUPPORT ANGLE WAS REMOVED, REPAIRED WITH FIBERGLASS OVERLAY, AND REINSTALLED IAW SRM 51-70-1, FIGURE 4 AND 51-30-5.Aug 28, 2000 · N35832 · Doug DC982 · Fuselage Main, Attach FittingsSDR CALA0001341Web · crackedINSPECTION FOUND A 4.5 INCH CRACK IN AFT AIRSTAIR LT SIDE WEB. THE CRACKED AREA WAS CUT OUT IAW SRM 52-01, FIGURE 2. A DOUBLER AND FILLER REPAIR WAS INSTALLED IAW SRM 52-01, FIGURE 2, 51-30-2, AND 51-10-3.Aug 28, 2000 · N35832 · Doug DC982 · Entrance StairsSDR CALA0001334Fairing · gougedINSPECTION FOUND RT WING NR 3 AFT LOWER FLAP HINGE FAIRING GOUGED. A SPLICE REPAIR WAS INSTALLED IAW SRM 51-30-2 AND 57-50-14, FIGURE 4.Aug 27, 2000 · N35832 · Doug DC982 · Trailing Edge FlapsSDR CALA0001333Fairing · crackedINSPECTION FOUND A 4 INCH CRACK IN RT WING O/B FLAP HINGE FAIRING LOWER HALF. A DOUBLER REPAIR WAS INSTALLED IAW SRM 57-50-14 AND 51-30-2.Aug 27, 2000 · N35832 · Doug DC982 · Trailing Edge FlapsSDR CALA0001327Cargo Track · corrodedINSPECTION FOUND AFT CARGO TRACK CORRODED AT NUT CLIP HOLES. THE CARGO TRACK WAS REMOVED AND A NEW CARGO TRACK WAS INSTALLED IAW SRM 51-30-1 AND 53-24-0, FIGURE 11.Aug 25, 2000 · N35832 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0001326Frame · crackedINSPECTION FOUND A 1 INCH CRACK IN FORWARD END OF FRAME OF THE FORWARD LAV TOILET SERVICING UNIT AT STA 240, LT SIDE. A DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 2, 53-34-0, FIGURE 2, AND 51-30-1.Aug 25, 2000 · N35832 · Doug DC982 · Fuselage Main, FrameSDR CALA0001325Flap Track · corrodedINSPECTION FOUND RIGHT I/B FLAP TRACK UPPER ROLLER SURFACE CORRODED. THE RIGHT I/B FLAP TRACK WAS REMOVED AND REPLACED IAW MM 27-51-01.Aug 25, 2000 · N35832 · Doug DC982 · Trailing Edge FlapsSDR CALA0001324Vane · gougedINSPECTION FOUND RIGHT I/B FLAP MOVEABLE VANE GOUGED. THE GOUGED AREA OF SKIN WAS REMOVED AND REPAIR PARTS WERE INSTALLED IAW SRM 51-70-2, FIGURE 72 AND PARAGRAPH 22C.Aug 25, 2000 · N35832 · Doug DC982 · Trailing Edge FlapsSDR CALA0001323Angle · crackedINSPECTION FOUND FOUR INCH CRACKS IN TWO ANGLES ON I/B FAIRING OF NR 2 ENGINE UPPER T/R BUCKET. THE ANGLES WERE REMOVED AND NEW ANGLES WERE INSTALLED IAW SRM 51-30-1, 51-30-2, AND 51-10-2.Aug 25, 2000 · N35832 · Doug DC982 · Nacelle/Pylon, Attach FittingsSDR CALA0001322Flap Track · corrodedINSPECTION FOUND LEFT I/B FLAP TRACK UPPER ROLLER SURFACE CORRODED. THE LEFT I/B FLAP TRACK WAS REMOVED AND REPLACED IAW MM 27-51-01.Aug 25, 2000 · N35832 · Doug DC982 · Trailing Edge FlapsSDR CALA0001319Panel · corrodedINSPECTION FOUND RT WING FUEL PANEL 1414C CORRODED. THE PANEL WAS REMOVED AND REPLACED IAW SRM 51-30-2.Aug 25, 2000 · N35832 · Doug DC982 · Wing, Plate/SkinSDR CALA0001318Galley Track · corrodedINSPECTION FOUND FORWARD GALLEY I/B LOWER MOUNT FITTING CORRODED. A REPLACEMENT MOUNT FITTING WAS INSTALLED IAW ECRA 2530-01257.Aug 25, 2000 · N35832 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0001317Angle · crackedINSPECTION FOUND CRACKS IN FIRST AND THIRD ANGLES ON INBOARD T/R FAIRING ON UPPER BUCKET OF NR 1 ENGINE. THE CRACKS WERE APPROXIMATELY 3 INCHES LONG. THE ANGLES WERE REMOVED AND NEW ANGLES WERE INSTALLED IAW SRM 51-30-1, 51-30-2, AND 51-10-2.Aug 25, 2000 · N35832 · Doug DC982 · Nacelle/Pylon, Attach FittingsSDR CALA0001316Fitting · corrodedINSPECTION FOUND FORWARD ENTRY FLOOR SUPPORT FITTING CORRODED AT STA 160 - 196, LBL 55. THE FLOOR SUPPORT FITTING WAS REMOVED AND A NEW SUPPORT FITTING WAS INSTALLED IAW SRM 53-01, FIGURE 1, 53-15-1, AND 51-30-5.Aug 25, 2000 · N35832 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001315Attach Angle · crackedINSPECTION FOUND A 3 INCH CRACK IN MID CARGO LT SIDEWALL FORWARD ATTACH ANGLE AT STA 524. THE ATTACH ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2 AND 53-24-0, FIGURE 9.Aug 25, 2000 · N35832 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001314Skin · dentedINSPECTION FOUND THREE DENTS IN NR 1 SLAT T/E BETWEEN XOS 166 AND XOS 147. THE DENTED AREA WAS REMOVED AND A REPAIR WAS INSTALLED IAW ECRA 5750-03426.Aug 25, 2000 · N35832 · Doug DC982 · Leading Edge DevicesSDR CALA0001312Web · crackedINSPECTION FOUND A 6 INCH CRACK IN SUBFLOOR WEB AT STA 1170, LBL 56. THE CRACKED AREA OF WEB WAS REMOVED AND FILLER AND DOUBLER WERE INSTALLED IAW SRM 53-01, FIGURE 4, 53-14-3, FIGURE 12, AND 51-30-2.Aug 25, 2000 · N35832 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001311Panel · corrodedINSPECTION FOUND LT WING FUEL PANELS 1311C AND 1307C CORRODED. THE FUEL PANELS WERE REMOVED AND REPLACED IAW ECRA 5730-01688.Aug 25, 2000 · N35832 · Doug DC982 · Wing, Plate/SkinSDR CALA0001310Panel · gougedINSPECTION FOUND RT WING FUEL PANEL 1472C GOUGED. THE FUEL PANEL WAS REMOVED AND REPLACED IAW ECRA 5730-01688.Aug 25, 2000 · N35832 · Doug DC982 · Wing, Plate/SkinSDR CALA0001291Shim · corrodedINSPECTION FOUND SHIMS UNDER STRAPS OF DOOR STOP NUMBER 11 & 12 OF AFT CARGO DOOR CORRODED. THE SHIMS WERE REMOVED AND REPLACEMENT SHIMS WERE INSTALLED. THE STRAPS WERE REINSTALLED. WORK WAS PERFORMED IAW SRM 51-30-1, 51-30-2, AND 51-30-5.Aug 21, 2000 · N35832 · Doug DC982 · Cargo/Baggage DoorsSDR CALA0001290Cargo Track · corrodedINSPECTION FOUND THE UPPER FLANGE OF THE RIGHT CARGO TIE DOWN TRACK IN THE MID CARGO PIT CORRODED AROUND FASTENER HOLES ON UPPER AND LOWER SURFACES AT STA 579 - 598. THE TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 53-30-1, 53-05, FIGURE 4C, 51-30-Aug 21, 2000 · N35832 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0001289Vane · dentedINSPECTION FOUND LT WING O/B FLAP O/B NR 2 FIXED VANE DENTED ON LEADING EDGE. THE DENTED AREA WAS REMOVED AND REPAIR DOUBLERS WERE INSTALLED IAW SRM 57-50-14 AND 51-70-2.Aug 21, 2000 · N35832 · Doug DC982 · Trailing Edge FlapsSDR CALA0001288Floor Panel · corrodedINSPECTION FOUND FORWARD ENTRY FLOOR CORRODED AT STA 170 - 184, LBL 55. THE CORRODED AREA WAS CUT OUT IAW SRM 53-01. DOUBLER AND FILLER WERE INSTALLED IAW SRM 51-30-2.Aug 21, 2000 · N35832 · Doug DC982 · Fuselage Floor PanelSDR CALA0001287Skin · bulgedINSPECTION FOUND LOWER FUSELAGE SKIN BULGED AT STA 389, LONGERON 16L-17L. THE EXISTING REPAIR WAS REMOVED IAW SRM 51-30-2. AN EXTERNAL AND INTERNAL DOUBLER AND FILLER WERE INSTALLED IAW SRM 53-04, FIGURE 38, 51-30-2, 51-30-5, AND ECRA 5330-02944.Aug 21, 2000 · N35832 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0001281Panel · gougedINSPECTION FOUND RT WING LOWER PANEL NR 1222C GOUGED. THE PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW SRM 57-30-3, FIGURE 3 AND 51-10-3.Aug 20, 2000 · N35832 · Doug DC982 · Wing, Plate/SkinSDR CALA0001280Fitting · bentINSPECTION FOUND MID CARGO DOOR FRAME LOWER BEAM TEE FITTING BENT. THE TEE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-10-1, 51-30-5, AND 51-10-3.Aug 20, 2000 · N35832 · Doug DC982 · Cargo/Baggage DoorsSDR CALA0001279Panel · gougedINSPECTION FOUND RT WING LOWER FUEL PANEL NR 1244C GOUGED. A DOUBLER WAS INSTALLED IAW SRM 57-01, FIGURE 3, SHEET 2, 51-10-3, 51-30-2, AND DRAWING 9937483.Aug 20, 2000 · N35832 · Doug DC982 · Wing, Plate/SkinSDR CALA0001278Door Frame · corrodedINSPECTION FOUND AFT CARGO DOOR JAMB CENTER LOWER SECTION CORRODED. THE DOOR JAMB CENTER LOWER SECTION WAS REMOVED AND A NEW PART WAS INSTALLED IAW SRM 51-30-5, 53-05, FIGURE 63, 51-10-3, AND 51-30-4.Aug 19, 2000 · N35832 · Doug DC982 · Fuselage Main, StructureSDR CALA0001277Floor Support · corrodedINSPECTION FOUND AFT CARGO DOOR JAMB FLOOR SUPPORT CORRODED AT STA 1155 - 1211, RBL 24. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-1 AND 51-30-2.Aug 19, 2000 · N35832 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001276Web · corrodedINSPECTION FOUND FORWARD CARGO PIT FORWARD DOOR FRAME TORQUE BOX WEB CORRODED. A DOUBLER AND CONICAL WASHERS WERE INSTALLED IAW SRM 53-01, FIGURE 2, 51-30-1, 51-30-8, AND 51-30-2.Aug 19, 2000 · N35832 · Doug DC982 · Cargo/Baggage DoorsSDR CALA0001275Floor Support · crackedINSPECTION FOUND SUPPORT SPLICE UNDER CABIN FLOOR HAD 7 CRACKS AT STA 826 - 886. THE CRACKS WERE 4 - 6 INCHES LONG. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-3 AND 51-30-1.Aug 19, 2000 · N35832 · Doug DC982 · Fuselage Miscellaneous Structure
Back to N35832, cancelled Apr 17, 2006