# Service difficulty reports: N930CE

A list on [N930CE](https://openairdocs.org/aircraft/N930CE.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR FXGA2018062700001](https://openairdocs.org/sdr/FXGA2018062700001.md): Downlock Switch · worn · Jun 25, 2018 · N930CE · Doug DC933F · Landing Gear Position and Warning
  > GEAR DOWN FOR LANDING AT PANC, NO GEAR SAFE INDICATION FOR RIGHT MAIN GEAR.
- [SDR FXGA201711211720](https://openairdocs.org/sdr/FXGA201711211720.md): Fitting · cracked · Nov 21, 2017 · N930CE · Doug DC933F · Fuselage Main, Attach Fittings
  > FITTING AT BS 351 LONGERON 32L CRACKED. REPLACED THE DAMAGED FITTING IAW EA 25-2017-138
- [SDR FXGA20170215001](https://openairdocs.org/sdr/FXGA20170215001.md): Position Switch · sticking · Feb 11, 2017 · N930CE · Doug DC933F · Landing Gear Door Retract Section
  > DURING GEAR RETRACTION, GEAR DOOR OPEN LIGHT AND GEAR RED UNSAFE LIGHTS FOR LEFT AND RIGHT MAIN GEAR ILLUMINATED WITH GEAR HANDLE IN UP POSITION.
- [SDR FXGA201610261638](https://openairdocs.org/sdr/FXGA201610261638.md): Skin · cracked · Oct 26, 2016 · N930CE · Doug DC933F · Fuselage Main, Plate/Skin
  > REPAIR 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).
- [SDR FXGA201610261637](https://openairdocs.org/sdr/FXGA201610261637.md): Structure · cracked · Oct 25, 2016 · N930CE · Doug DC933F · Fuselage Miscellaneous Structure
  > REPAIR 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.
- [SDR FXGA201610240001](https://openairdocs.org/sdr/FXGA201610240001.md): Support Bracket · cracked · Oct 24, 2016 · N930CE · Doug DC933F · Trailing Edge Flap Actuator
  > RIGHT FLAP I/B ACTUATOR SUPPORT BRACKET CRACKED.
- [SDR FXGA20160128001](https://openairdocs.org/sdr/FXGA20160128001.md): Strut · low pressure · Jan 27, 2016 · N930CE · Doug DC933F · Nose/Tail Landing Gear Strut/Axle
  > AFTER TAKEOFF COULD NOT RETRACT GEAR, HANDLE WOULD NOT MOVE TO UP POSITION. THE CAUSE WAS THE NLG STRUT WAS LOW ON PRESS.
- [SDR FXGA201505061516](https://openairdocs.org/sdr/FXGA201505061516.md): Frame · cracked · May 6, 2015 · N930CE · Doug DC933F · Fuselage Main, Frame
  > FRAME REPAIR, STATION 389, LONGERON 12R - 14R. MAJOR REPAIR. FUSELAGE FRAME INBD FLANGE CRACKED AT STATION 389 BETWEEN LONGERON 12R & 14R.
- [SDR FXGA201505061515](https://openairdocs.org/sdr/FXGA201505061515.md): Frame · corroded · May 6, 2015 · N930CE · Doug DC933F · Fuselage Main, Frame
  > FRAME 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.
- [SDR FXGA201505061517](https://openairdocs.org/sdr/FXGA201505061517.md): Skin · damaged · May 6, 2015 · N930CE · Doug DC933F · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE REPAIR FUSELAGE SKIN BETWEEN STATION 101 - 110, LONGERON 17L & 18L. MAJOR REPAIR. TWO EACH LIGHTNING STRIKE DAMAGE TO FUSELAGE SKIN.
- [SDR FXGA201505061518](https://openairdocs.org/sdr/FXGA201505061518.md): Skin · damaged · May 6, 2015 · N930CE · Doug DC933F · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE REPAIR FUSELAGE SKIN BETWEEN STATION 83.550 - 89.050, LONGERON 16R & 17R. MAJOR REPAIR, 3 EACH LIGHTNING STRIKE DAMAGE TO FUSELAGE SKIN.
- [SDR 7AHR2015043000420](https://openairdocs.org/sdr/7AHR2015043000420.md): Frame · cracked · Apr 30, 2015 · N930CE · Doug DC933F · Fuselage Main, Frame
  > FRAME AT BS 389 BETWEEN LONGERONS 12 - 14R IS CRACKED. REPAIRED SECTION OF FRAME IAW SRM 53-03, FIG 4.
- [SDR 7AHR2015043000371](https://openairdocs.org/sdr/7AHR2015043000371.md): Frame · corroded · Apr 30, 2015 · N930CE · Doug DC933F · Fuselage Main, Frame
  > E & 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.
- [SDR 7AHR2015043000346](https://openairdocs.org/sdr/7AHR2015043000346.md): Seat Track · corroded · Apr 30, 2015 · N930CE · Doug DC933F · Fuselage, Seat/Cargo Attach Fittings
  > LIGHT 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 51-10
- [SDR 7AHR2015043000203](https://openairdocs.org/sdr/7AHR2015043000203.md): Mount · cracked · Apr 30, 2015 · N930CE · Doug DC933F · Spoilers
  > RT 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.
- [SDR 7AHR2015043000138](https://openairdocs.org/sdr/7AHR2015043000138.md): Fitting · cracked · Apr 30, 2015 · N930CE · Doug DC933F · Fuselage, Wing Attach Fittings
  > WING 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.
- [SDR 7AHR2015043000137](https://openairdocs.org/sdr/7AHR2015043000137.md): Fitting · cracked · Apr 30, 2015 · N930CE · Doug DC933F · Fuselage, Wing Attach Fittings
  > RIGHT 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.
- [SDR 7AHR2015043000122](https://openairdocs.org/sdr/7AHR2015043000122.md): Cargo Track · corroded · Apr 30, 2015 · N930CE · Doug DC933F · Fuselage, Seat/Cargo Attach Fittings
  > FORWARD 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.
- [SDR 7AHR2015043000110](https://openairdocs.org/sdr/7AHR2015043000110.md): Attach Angle · cracked · Apr 29, 2015 · N930CE · Doug DC933F · Nacelle/Pylon, Attach Fittings
  > RIGHT PLYON LOWER ATTACH ANGLE CRACKED AT 996. INSTALLED NEW SECTION OF RT PYLON LOWER ATTACH ANGLE IAW SRM 54-04, FIG 10.
- [SDR FXGA20131023001](https://openairdocs.org/sdr/FXGA20131023001.md): Skin · damaged · Oct 19, 2013 · N930CE · Doug DC933F · Fuselage Main, Plate/Skin
  > AIRCRAFT 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 B
- [SDR EE4Y201303270045](https://openairdocs.org/sdr/EE4Y201303270045.md): Frame · damaged · Mar 27, 2013 · N930CE · Doug DC933F · Fuselage Main, Frame
  > AFT CARGO COMPARTMENT BS 889 BETWEEN L27 AND 28L FRAME WITH AN ELONGATE HOLE. REPAIRED IAW SRM 53-03 PARA 1C, FIG 2A.
- [SDR EE4Y201303270042](https://openairdocs.org/sdr/EE4Y201303270042.md): Shear Tie · cracked · Mar 27, 2013 · N930CE · Doug DC933F · Fuselage Internal Mounting Structure
  > UPPER FUSELAGE, CARGO CABIN, AT BS 945 BETWEEN L15 TO 16R FRAME SHEAR TIE CRACKED. REPLACED SHEAR TIE IAW SRM 51-01, PARA 2D.
- [SDR EE4Y201303270041](https://openairdocs.org/sdr/EE4Y201303270041.md): Bulkhead · corroded · Mar 27, 2013 · N930CE · Doug DC933F · Fuselage Main, Bulkhead
  > LOWER 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.
- [SDR EE4Y201303270038](https://openairdocs.org/sdr/EE4Y201303270038.md): Skin · dented · Mar 27, 2013 · N930CE · Doug DC933F · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE BS 248.5 BETWEEN L19 AND 20L SKIN DENTED. REPAIRED SKIN IAW SRM 53-01, FIG 1.
- [SDR EE4Y2013032700037](https://openairdocs.org/sdr/EE4Y2013032700037.md): Tee Fitting · cracked · Mar 27, 2013 · N930CE · Doug DC933F · Fuselage Main, Attach Fittings
  > UPPER 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.
- [SDR EE4Y2013032700036](https://openairdocs.org/sdr/EE4Y2013032700036.md): Frame · cracked · Mar 27, 2013 · N930CE · Doug DC933F · Fuselage Main, Frame
  > CARGO 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.
- [SDR EE4Y2013032700035](https://openairdocs.org/sdr/EE4Y2013032700035.md): Fitting · cracked · Mar 27, 2013 · N930CE · Doug DC933F · Fuselage Main, Structure
  > LOWER 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.
- [SDR EE4Y2013032700034](https://openairdocs.org/sdr/EE4Y2013032700034.md): Fitting · cracked · Mar 27, 2013 · N930CE · Doug DC933F · Fuselage Main, Structure
  > LOWER 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.
- [SDR EE4Y2013032700033](https://openairdocs.org/sdr/EE4Y2013032700033.md): Fitting · cracked · Mar 27, 2013 · N930CE · Doug DC933F · Fuselage Main, Structure
  > LOWER 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.
- [SDR EE4Y2013032700032](https://openairdocs.org/sdr/EE4Y2013032700032.md): Fitting · cracked · Mar 27, 2013 · N930CE · Doug DC933F · Fuselage Main, Structure
  > LOWER 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.
- [SDR EE4Y201303270040](https://openairdocs.org/sdr/EE4Y201303270040.md): Fitting · cracked · Mar 26, 2013 · N930CE · Doug DC933F · Fuselage Main, Attach Fittings
  > LOWER FUSELAGE FWD CARGO COMPARTMENT, BS 237, ON L24R, FRAME AREA AFT FITTING CRACKED. REPLACED, FRAME FITTING IAW SRM 51-01 PARA 2D.
- [SDR EE4Y2013032000031](https://openairdocs.org/sdr/EE4Y2013032000031.md): Acoustic Liner · delaminated · Mar 26, 2013 · N930CE · Doug DC933F · Turbine Engine Air Inlet Section
  > ENGINE 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.
- [SDR EE4Y2013032000025](https://openairdocs.org/sdr/EE4Y2013032000025.md): Fitting · broken · Mar 22, 2013 · N930CE · Doug DC933F · Fuselage Miscellaneous Structure
  > DURING THE STRUCTURAL INSPECTION WAS FOUND ON FWD CARGO COMPARMENT STA 237, LONG 24 LEFT FITTING CRACKED. THE MENTIONED FITTING WAS REPLACED PER SRM GUIDELINES.
- [SDR EE4Y2013032000024](https://openairdocs.org/sdr/EE4Y2013032000024.md): Fitting · broken · Mar 22, 2013 · N930CE · Doug DC933F · Fuselage Miscellaneous Structure
  > DURING 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.
- [SDR EE4Y2013032000023](https://openairdocs.org/sdr/EE4Y2013032000023.md): Fitting · cracked · Mar 20, 2013 · N930CE · Doug DC933F · Fuselage Miscellaneous Structure
  > DURING THE STRUCTURAL INSPECTION WAS FOUND ON FWD CARGO COMPARTMENT STA 256, LONG 24 RIGHT FITTING CRACKED. THE MENTIONED FITTING WAS REPLACED PER SRM GUIDELINES.
- [SDR EE4Y2013032000022](https://openairdocs.org/sdr/EE4Y2013032000022.md): Fitting · cracked · Mar 20, 2013 · N930CE · Doug DC933F · Fuselage Miscellaneous Structure
  > DURING THE STRUCTURAL INSPECTION WAS FOUND ON FWD CARGO COMPARTMENT STA 237, LONG 24 RIGHT FITTING CRACKED. THE MENTIONED FITTING WAS REPLACED PER SRM GUIDELINES.
- [SDR EE4Y201303270043](https://openairdocs.org/sdr/EE4Y201303270043.md): Skin · cracked · Mar 18, 2013 · N930CE · Doug DC933F · Fuselage Main, Plate/Skin
  > UPPER AFT FUSELAGE BS 1038 LONGERON 14 LT SIDE SKIN CRACKED. REPAIRED IAW SRM 53-04 FIG 18.
- [SDR EE4Y2013031500020](https://openairdocs.org/sdr/EE4Y2013031500020.md): Fitting · cracked · Mar 15, 2013 · N930CE · Doug DC933F · Wing, Attach Fittings
  > DURING 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.
- [SDR EE4Y201303270044](https://openairdocs.org/sdr/EE4Y201303270044.md): Skin · cracked · Mar 13, 2013 · N930CE · Doug DC933F · Fuselage Main, Plate/Skin
  > UPPER AFT FUSELAGE BS 1038 L14R SKIN CRACKED. REPAIRED SKIN SECTION IAW SRM 53-04, FIG 18.
- [SDR EE4Y2013032600029](https://openairdocs.org/sdr/EE4Y2013032600029.md): Angle · cracked · Mar 10, 2013 · N930CE · Doug DC933F · Fuselage Miscellaneous Structure
  > LOWER 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.
- [SDR EE4Y2013032200028](https://openairdocs.org/sdr/EE4Y2013032200028.md): Angle · cracked · Mar 10, 2013 · N930CE · Doug DC933F · Fuselage Miscellaneous Structure
  > LOWER 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.
- [SDR EE4Y2013032600030](https://openairdocs.org/sdr/EE4Y2013032600030.md): Angle · cracked · Mar 9, 2013 · N930CE · Doug DC933F · Fuselage Miscellaneous Structure
  > LOWER 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.
- [SDR EE4Y2013032600027](https://openairdocs.org/sdr/EE4Y2013032600027.md): Angle · cracked · Mar 9, 2013 · N930CE · Doug DC933F · Fuselage Miscellaneous Structure
  > LOWER 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.
- [SDR EE4Y2013032600026](https://openairdocs.org/sdr/EE4Y2013032600026.md): Frame · cracked · Mar 9, 2013 · N930CE · Doug DC933F · Fuselage Main, Frame
  > LOWER 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.
- [SDR FXGA201204251229](https://openairdocs.org/sdr/FXGA201204251229.md): Frame · gouged · Apr 25, 2012 · N930CE · Doug DC933F · Fuselage Main, Frame
  > FWD 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 FASTE

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/aircraft/N930CE/reports

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