N930CE

Service difficulty reports · 45

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 = 'N930CE' AND registry_match = 'registration'
  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 FXGA2018062700001Downlock Switch · wornGEAR DOWN FOR LANDING AT PANC, NO GEAR SAFE INDICATION FOR RIGHT MAIN GEAR.Jun 25, 2018 · N930CE · Doug DC933F · Landing Gear Position and WarningSDR FXGA201711211720Fitting · crackedFITTING AT BS 351 LONGERON 32L CRACKED. REPLACED THE DAMAGED FITTING IAW EA 25-2017-138Nov 21, 2017 · N930CE · Doug DC933F · Fuselage Main, Attach FittingsSDR FXGA20170215001Position Switch · stickingDURING GEAR RETRACTION, GEAR DOOR OPEN LIGHT AND GEAR RED UNSAFE LIGHTS FOR LEFT AND RIGHT MAIN GEAR ILLUMINATED WITH GEAR HANDLE IN UP POSITION.Feb 11, 2017 · N930CE · Doug DC933F · Landing Gear Door Retract SectionSDR FXGA201610261638Skin · crackedREPAIR OF CRACKS IN FUSELAGE SKIN FS 102.5 BELOW STRINGER R18. REPAIR CRACKS EXTENDING FROM RIVETS IN SKIN AT FS 102.5 STRUCTURAL REPAIR MANUAL 53-01 FIGURE 4 (SHEET 4).Oct 26, 2016 · N930CE · Doug DC933F · Fuselage Main, Plate/SkinSDR FXGA201610261637Structure · crackedREPAIR OF 4" CRACK IN FUSELAGE TAIL STA 1205 RT 3 O-CLOCK POSITION. MAJOR REPAIR OF CRACK PER SRM REFERENCE SRM 53-01 FIGURE 4.Oct 25, 2016 · N930CE · Doug DC933F · Fuselage Miscellaneous StructureSDR FXGA201610240001Support Bracket · crackedRIGHT FLAP I/B ACTUATOR SUPPORT BRACKET CRACKED.Oct 24, 2016 · N930CE · Doug DC933F · Trailing Edge Flap ActuatorSDR FXGA20160128001Strut · low pressureAFTER TAKEOFF COULD NOT RETRACT GEAR, HANDLE WOULD NOT MOVE TO UP POSITION. THE CAUSE WAS THE NLG STRUT WAS LOW ON PRESS.Jan 27, 2016 · N930CE · Doug DC933F · Nose/Tail Landing Gear Strut/AxleSDR FXGA201505061516Frame · crackedFRAME REPAIR, STATION 389, LONGERON 12R - 14R. MAJOR REPAIR. FUSELAGE FRAME INBD FLANGE CRACKED AT STATION 389 BETWEEN LONGERON 12R & 14R.May 6, 2015 · N930CE · Doug DC933F · Fuselage Main, FrameSDR FXGA201505061515Frame · corrodedFRAME REPAIR STA 180, L-28L TO L-28R. MAJOR REPAIR. FUSELAGE FRAME LOWER FLANGE CORRODED AT STATION 180 BTWN LONGERON 28 LEFT AND LONGERON 28 RIGHT.May 6, 2015 · N930CE · Doug DC933F · Fuselage Main, FrameSDR FXGA201505061517Skin · damagedLIGHTNING STRIKE REPAIR FUSELAGE SKIN BETWEEN STATION 101 - 110, LONGERON 17L & 18L. MAJOR REPAIR. TWO EACH LIGHTNING STRIKE DAMAGE TO FUSELAGE SKIN.May 6, 2015 · N930CE · Doug DC933F · Fuselage Main, Plate/SkinSDR FXGA201505061518Skin · damagedLIGHTNING STRIKE REPAIR FUSELAGE SKIN BETWEEN STATION 83.550 - 89.050, LONGERON 16R & 17R. MAJOR REPAIR, 3 EACH LIGHTNING STRIKE DAMAGE TO FUSELAGE SKIN.May 6, 2015 · N930CE · Doug DC933F · Fuselage Main, Plate/SkinSDR 7AHR2015043000420Frame · crackedFRAME AT BS 389 BETWEEN LONGERONS 12 - 14R IS CRACKED. REPAIRED SECTION OF FRAME IAW SRM 53-03, FIG 4.Apr 30, 2015 · N930CE · Doug DC933F · Fuselage Main, FrameSDR 7AHR2015043000371Frame · corrodedE & E BAY BILGE AREA FLOOR FRAME HAS CORRISON FROM LONGERON 28L-28R STA 180. R & R SECTION OF FRAME, STA 180, LONGERON 28L-28R IAW SRM 53-03, FIG 5.Apr 30, 2015 · N930CE · Doug DC933F · Fuselage Main, FrameSDR 7AHR2015043000346Seat Track · corrodedLIGHT SURFACE CORROSION ON SEAT TRACK, FLOOR ATTACHMENT AREAS IN VARIOUS LOCATIONS IN PASSENGER CABIN, STA 160-996, RBL5435 TO LBL 54.5. REMOVED LIGHT CORROSION AND TREATED AREAS. INSTALLED SEAT TRACK REPAIR STA 408-484, RBL 33 IAW SRM 53-05, FIG 4F AND 51-10Apr 30, 2015 · N930CE · Doug DC933F · Fuselage, Seat/Cargo Attach FittingsSDR 7AHR2015043000203Mount · crackedRT INBD SPOILER CONTROL MOUNT BRACKET CRACKED ON REAR SPAR. INSTALLED A REPAIR TO MOUNT BRACKET IAW SRM 51-10-3A, 51-30-2,51-10-2, 51-10-4 AND 51-30-5.Apr 30, 2015 · N930CE · Doug DC933F · SpoilersSDR 7AHR2015043000138Fitting · crackedWING TO FUSELAGE FITTING CRACKED LT SIDE BS 600, LONGERON 22L. R & R THE FITTING IAW SRM 51-30-1, 51-10-02, 51-10-4, 5110-2 AND 57-31-4.Apr 30, 2015 · N930CE · Doug DC933F · Fuselage, Wing Attach FittingsSDR 7AHR2015043000137Fitting · crackedRIGHT WING TO FUSELAGE FITTING IS CRACKED AT BS 600-LONGERON 22R. R & R THE FITTING IAW SRM 51-30-5, PGS 12-14, 51-30-01,51-10-4.51-10-2 AND 57-31-4.Apr 30, 2015 · N930CE · Doug DC933F · Fuselage, Wing Attach FittingsSDR 7AHR2015043000122Cargo Track · corrodedFORWARD LOWER CARGO COMPARTMENT CARGO TRACK SUPPORT HAS CORROSION FROM BS 427-513, RBL 14. REMOVED CORROSION FROM AREA. TRACK SUPPORT CHANNEL AND UPPER SUPPORT FLANGE OF INTERCOSTAL WERE REPAIRED/REINFORCED IAW SRM 51-70-5, FIG 1.Apr 30, 2015 · N930CE · Doug DC933F · Fuselage, Seat/Cargo Attach FittingsSDR 7AHR2015043000110Attach Angle · crackedRIGHT PLYON LOWER ATTACH ANGLE CRACKED AT 996. INSTALLED NEW SECTION OF RT PYLON LOWER ATTACH ANGLE IAW SRM 54-04, FIG 10.Apr 29, 2015 · N930CE · Doug DC933F · Nacelle/Pylon, Attach FittingsSDR FXGA20131023001Skin · damagedAIRCRAFT WAS STRUCK BY LIGHTNING DURING CLIMB. NO ABNORMAL INDICATIONS AFTER STRIKE. COMPLIED WITH LIGHTNING STRIKE INSPECTION PROCEDURES, IAW EAC POLICIES AND PROCEDURES. TWO BURNED RIVETS WERE FOUND AT LOWER FUSELAGE BS 434 CENTERLINE, INCLUDING CIRCULAR BOct 19, 2013 · N930CE · Doug DC933F · Fuselage Main, Plate/SkinSDR EE4Y201303270045Frame · damagedAFT CARGO COMPARTMENT BS 889 BETWEEN L27 AND 28L FRAME WITH AN ELONGATE HOLE. REPAIRED IAW SRM 53-03 PARA 1C, FIG 2A.Mar 27, 2013 · N930CE · Doug DC933F · Fuselage Main, FrameSDR EE4Y201303270042Shear Tie · crackedUPPER FUSELAGE, CARGO CABIN, AT BS 945 BETWEEN L15 TO 16R FRAME SHEAR TIE CRACKED. REPLACED SHEAR TIE IAW SRM 51-01, PARA 2D.Mar 27, 2013 · N930CE · Doug DC933F · Fuselage Internal Mounting StructureSDR EE4Y201303270041Bulkhead · corrodedLOWER FUSELAGE AFT CARGO COMPARTMENT AT BS 996 L23L AFT PRESSURE BULKHEAD WEB CORRODED. REPAIRED PRESSURE BULKHEAD WEB SECTION IAW SRM 53-03 PARA 17, FIG 23.Mar 27, 2013 · N930CE · Doug DC933F · Fuselage Main, BulkheadSDR EE4Y201303270038Skin · dentedLOWER FUSELAGE BS 248.5 BETWEEN L19 AND 20L SKIN DENTED. REPAIRED SKIN IAW SRM 53-01, FIG 1.Mar 27, 2013 · N930CE · Doug DC933F · Fuselage Main, Plate/SkinSDR EE4Y2013032700037Tee Fitting · crackedUPPER FUSELAGE AFT PRESSURE BULKHEAD TEE BETWEEN L15 AND 17L, AT Z=14 AND Z=24 TEE CRACKED. REPLACED PRESSURE BULKHEAD TEE SECTION IAW S/B A53-232 ACCOMPLISHMENT INSTRUCTIONS OPTION II CONDITION 2, FIG 4, REV 2, DATE APRIL 28,95.Mar 27, 2013 · N930CE · Doug DC933F · Fuselage Main, Attach FittingsSDR EE4Y2013032700036Frame · crackedCARGO CABIN AT BS 813, L17R, FRAME WEB WITH CRACK. REPAIRED CARGO CABIN FRAME SECTION BS 813 BETWEEN L16 AND 18R DUE TO CRACK IAW SRM 53-03, FIG 32, PARA 26.Mar 27, 2013 · N930CE · Doug DC933F · Fuselage Main, FrameSDR EE4Y2013032700035Fitting · crackedLOWER FUSELAGE, AFT CARGO COMPARTMENT DOOR AT BEAM NR 5, AFT BEAM END CRACKED. REPLACED NR 5 DOOR BEAM END FITTING IAW S/B DC-9-52-189 ACOMPLISMENT INSTRUCTIONS, WORK INSTRUCTIONS CONDITION 3, REV 3, DATE FEB 21,2008 AND DWG 5934142, REV H, DATED 12-21-06.Mar 27, 2013 · N930CE · Doug DC933F · Fuselage Main, StructureSDR EE4Y2013032700034Fitting · crackedLOWER FUSELAGE, AFT CARGO COMPARTMENT DOOR AT BEAM NR 3, FWD BEAM END CRACKED. REPLACED NR 3 DOOR BEAM END FITTING IAW S/B DC-9-52-189 ACOMPLISMENT INSTRUCTIONS, WORK INSTRUCTIONS CONDITION 3, REV 3, DATE FEB 21,2008 AND DWG 5934142, REV H, DATED 12-21-06.Mar 27, 2013 · N930CE · Doug DC933F · Fuselage Main, StructureSDR EE4Y2013032700033Fitting · crackedLOWER FUSELAGE, AFT CARGO COMPARTMENT DOOR AT BEAM NR 1, FWD BEAM END CRACKED. REPLACED DOOR BEAM FITTING IAW S/B DC-9-52-189 ACOMPLISMENT INSTRUCTIONS, WORK INSTRUCTIONS CONDITION 3, REV 3 DATE FEB 21,2008 AND DWG 5934142, REV H, DATED 12-21-06.Mar 27, 2013 · N930CE · Doug DC933F · Fuselage Main, StructureSDR EE4Y2013032700032Fitting · crackedLOWER FUSELAGE, AFT CARGO COMPARTMENT DOOR AT BEAM NR 2, AFT BEAM END CRACKED. REPLACED NR 2 DOOR BEAM IAW S/B DC-952-189 ACOMPLISMENT INSTRUCTIONS, WORK INSTRUCTIONS CONDITION 3 REV 3 DATE FEB 21, AND DWG 5934142, REV H, DATED12-21-062008.Mar 27, 2013 · N930CE · Doug DC933F · Fuselage Main, StructureSDR EE4Y201303270040Fitting · crackedLOWER FUSELAGE FWD CARGO COMPARTMENT, BS 237, ON L24R, FRAME AREA AFT FITTING CRACKED. REPLACED, FRAME FITTING IAW SRM 51-01 PARA 2D.Mar 26, 2013 · N930CE · Doug DC933F · Fuselage Main, Attach FittingsSDR EE4Y2013032000031Acoustic Liner · delaminatedENGINE NR 1 NOSE COWL ACOUSTIC INNER BARREL INNER SKIN WITH DELAMINATION. THE MENTION DAMAGE WAS REPAIRED UNDER NRI A1B089 4-3 AND EO# COO-CMP9-54-035-13.Mar 26, 2013 · N930CE · Doug DC933F · Turbine Engine Air Inlet SectionSDR EE4Y2013032000025Fitting · brokenDURING THE STRUCTURAL INSPECTION WAS FOUND ON FWD CARGO COMPARMENT STA 237, LONG 24 LEFT FITTING CRACKED. THE MENTIONED FITTING WAS REPLACED PER SRM GUIDELINES.Mar 22, 2013 · N930CE · Doug DC933F · Fuselage Miscellaneous StructureSDR EE4Y2013032000024Fitting · brokenDURING THE STRUCTURAL INSPECTION WAS FOUND ON FWD CARGO COMPARTMENT STA 256, LONG 24 LEFT FITTING CRACKED. THE MENTIONED FITTING WAS REPLACED PER SRM GUIDELINES UNDER WORK ORDER A1B089, SUBJOB: 1, ITEM 78.Mar 22, 2013 · N930CE · Doug DC933F · Fuselage Miscellaneous StructureSDR EE4Y2013032000023Fitting · crackedDURING THE STRUCTURAL INSPECTION WAS FOUND ON FWD CARGO COMPARTMENT STA 256, LONG 24 RIGHT FITTING CRACKED. THE MENTIONED FITTING WAS REPLACED PER SRM GUIDELINES.Mar 20, 2013 · N930CE · Doug DC933F · Fuselage Miscellaneous StructureSDR EE4Y2013032000022Fitting · crackedDURING THE STRUCTURAL INSPECTION WAS FOUND ON FWD CARGO COMPARTMENT STA 237, LONG 24 RIGHT FITTING CRACKED. THE MENTIONED FITTING WAS REPLACED PER SRM GUIDELINES.Mar 20, 2013 · N930CE · Doug DC933F · Fuselage Miscellaneous StructureSDR EE4Y201303270043Skin · crackedUPPER AFT FUSELAGE BS 1038 LONGERON 14 LT SIDE SKIN CRACKED. REPAIRED IAW SRM 53-04 FIG 18.Mar 18, 2013 · N930CE · Doug DC933F · Fuselage Main, Plate/SkinSDR EE4Y2013031500020Fitting · crackedDURING THE STRUCTURAL INSPECTION, "C1" SERVICE ON RT WING FRON SPAR SECTION AT XRS 204, FITTING CRACKED. THE FITTING WAS REPLACED IAW SRM GUIDELINES UNDER W/O A1B038, SUB JOB: 6, ITEM :3.Mar 15, 2013 · N930CE · Doug DC933F · Wing, Attach FittingsSDR EE4Y201303270044Skin · crackedUPPER AFT FUSELAGE BS 1038 L14R SKIN CRACKED. REPAIRED SKIN SECTION IAW SRM 53-04, FIG 18.Mar 13, 2013 · N930CE · Doug DC933F · Fuselage Main, Plate/SkinSDR EE4Y2013032600029Angle · crackedLOWER FUSELAGE AFT CARGO COMPARTMENT, BS 869 BETWEEN LONGERON 28-30L FRAME AREA, TITANIUM ANGLE WITH CRACK. DAMAGED ANGLE WAS REPAIRED IAW EO COO-9-53-039-13.Mar 10, 2013 · N930CE · Doug DC933F · Fuselage Miscellaneous StructureSDR EE4Y2013032200028Angle · crackedLOWER FUSELAGE AFT CARGO COMPARTMENT BS 889, BETWEEN LONGERON 28-29L, FRAME AREA TITANIUM ANGLE WITH CRACK. DAMAGED ANGLE WAS REPAIRED IAW THE EO COO-9-53-039-13.Mar 10, 2013 · N930CE · Doug DC933F · Fuselage Miscellaneous StructureSDR EE4Y2013032600030Angle · crackedLOWER FUSELAGE FWD CARGO COMPARTMENT, STA Y:427, BETWEEN LONGERON 24-26L FRAME AREA, TITANIUM ANGLE WITH CRACK. DAMAGED ANGLE WAS REPAIRED IAW E/O COO-9-53-039-13 REQUIREMENTS.Mar 9, 2013 · N930CE · Doug DC933F · Fuselage Miscellaneous StructureSDR EE4Y2013032600027Angle · crackedLOWER FUSELAGE FWD CARGO COMPARTMENT, BS 332 BETWEEN LONGERON 28R AND 28L FRAME AREA, STEEL ANGLE WITH CRACK. DAMAGED ANGLE WAS REPAIRED IAW THE EO COO-9-53-039-13, UNDER THE W/O: A1B089, SUBJOB: 1, ITEM: 91.Mar 9, 2013 · N930CE · Doug DC933F · Fuselage Miscellaneous StructureSDR EE4Y2013032600026Frame · crackedLOWER FUSELAGE FWD CARGO COMPARTMENT, BS 332, BETWEEN LONGERON 28R AND 28L, FRAME AREA, TITANIUM ANGLE WITH CRACK. DAMAGED ANGLE WAS REPAIRED IAW EO COO-9-53-039-13, UNDER THE W/O A1B089, SUBJOB 1, ITEM 91.Mar 9, 2013 · N930CE · Doug DC933F · Fuselage Main, FrameSDR FXGA201204251229Frame · gougedFWD CARGO DOOR FRAME WEB REPAIR AT FS 435, GOUGE APPROXIMATELY 2 INCHES ABOVE LONGERON L15 AT FS 435. REMOVE DAMAGE & FABRICATE FILLER FROM MATERIAL SAME AS PARENT 7075-T6 0.071INCHES. FABRICATE DOUBLER FROM 7075-T6 0.80 INCHES TO EXTEND A MINIMUM OF 6 FASTEApr 25, 2012 · N930CE · Doug DC933F · Fuselage Main, Frame
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