# Service difficulty reports: N351CE

A list on [N351CE](https://openairdocs.org/aircraft/N351CE.md).

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

- [SDR FXGA201508071533](https://openairdocs.org/sdr/FXGA201508071533.md): Skin · corroded · Aug 7, 2015 · N351CE · Doug C118A · Fuselage Main, Plate/Skin
  > CORRODED SKIN AT FS 200, BETWEEN STRINGER 4L & 8L. REPAIRED CORRODED SKIN, PERFORMED SKIN SPLICE IAW EAC EO 05 21 & 0301.
- [SDR FXGA201508071532](https://openairdocs.org/sdr/FXGA201508071532.md): Skin · corroded · Aug 7, 2015 · N351CE · Doug C118A · Fuselage Main, Plate/Skin
  > TO REPAIR A CORRODED SKIN LAP JOINT AT FS 200, STRINGER 4L, PERFORMED SKIN LAP REPAIR IAW THE INSTRUCTIONS GIVEN IN EAC EO 0502.
- [SDR FXGA201508061531](https://openairdocs.org/sdr/FXGA201508061531.md): Skin · corroded · Aug 6, 2015 · N351CE · Doug C118A · Fuselage Main, Plate/Skin
  > TO REPAIR CORROSION DAMAGE ABOVE THE AFT EDGE OF THE FWD CARGO DOOR, AT WS 217, PERFORMED SKIN LAP REPAIR IAW THE INSTRUCTIONS GIVEN IN EAC EO 0502.
- [SDR FXGA201508051530](https://openairdocs.org/sdr/FXGA201508051530.md): Repair · cracked · Aug 5, 2015 · N351CE · Doug C118A · Fuselage Main, Bulkhead
  > REPAIR CRACKED WEB ON THE FUSELAGE BULKHEAD AT FS 600. PERFORM REPAIR IAW DC-6 A & B OVERHAUL MANUAL FIGURE 12-6.
- [SDR FXGA201507311529](https://openairdocs.org/sdr/FXGA201507311529.md): Skin · corroded · Jul 28, 2015 · N351CE · Doug C118A · Cargo/Baggage Doors
  > REPAIR A CORRODED SKIN ON THE UPPER AFT CORNER OF THE FWD CARGO DOOR. PERFORM CUT OUT OF CORRODED SKIN AT FS 200. REMOVE AFT SECTION OF SKIN AT EXISTING LAP AT SAME LEVEL OF FUSELAGE STRINGER 12L. LAYOUT NEW SEAM AT FS 200 IAW DWG 1529-01 & MANUFACTURE NEW
- [SDR FXGA201412041450](https://openairdocs.org/sdr/FXGA201412041450.md): Skin · worn · Dec 3, 2014 · N351CE · Doug C118A · Trailing Edge Flaps
  > REPLACE WORN RT FLAP LE SKIN FROM WING STATION 379.5 TO 421. THIS REPAIR WILL REMOVE WORN SKIN & USING OLD SKIN AS A TEMPLATE, MANUFACTURE NEW SKIN. TREAT & PRIME FOR CORROSION PROTECTION. INSTALL NEW SKIN WITH THE SAME SIZE & TYPE FASTENERS AS THE ORIGINAL
- [SDR FXGA201412041449](https://openairdocs.org/sdr/FXGA201412041449.md): Fitting · broken · Dec 3, 2014 · N351CE · Doug C118A · Wing Miscellaneous Structure
  > SUGAR SCOOP FITTING REPLACEMENT AT W STATION 60L STRINGER 20. TO REPLACE A BROKEN SUGAR SCOOP FITTING PN 4491280 WITH NEW ONE AT WING STATION 60L, STRINGER 20 USING TECHNICAL REFERENCES DC 6 A B OVERHAUL MANUAL & DWG 4491280.
- [SDR FXGA201408271432](https://openairdocs.org/sdr/FXGA201408271432.md): Skin · corroded · Aug 27, 2014 · N351CE · Doug C118A · Wing, Plate/Skin
  > LOWER WING SKIN REPAIR AT WS 347R STRINGER 25. REASON IS TO REPAIR A CORRODED WING SKIN BY PERFORMING A 1 INCH CIRCULAR CUT OUT & INSTALL A 2024-T3 0.071 DOUBLER IAW A B OHM FIGURE 13-30.
- [SDR FXGA20140227001](https://openairdocs.org/sdr/FXGA20140227001.md): Skin Panel · cracked · Feb 24, 2014 · N351CE · Doug C118A · Wing, Plate/Skin
  > ON PREFLIGHT WALK AROUND IN EMMONAK A FUEL LEAK WAS NOTED UNDER NR 2 NACELLE. THE WING SKIN HAD CRACKED AT APPROXIMATELY WS 176L, INSIDE THE NR 2 NACELLE. THE CRACK STARTS AT THE FRONT SPAR & GOES IN A STRAIGHT LINE AFT PAST STRINGER 19.
- [SDR FXGA20140110002](https://openairdocs.org/sdr/FXGA20140110002.md): Wire · damaged · Jan 9, 2014 · N351CE · Doug C118A · Fire Protection System Wiring
  > SMOKE INDICATION IN MAIN CABIN, CREWMEMBER INSPECTED WHILE WEARING PBE. TURNED TOWARD NEAREST SUITABLE AIRPORT. AFTER INSPECTION NO SMOKE NO FIRE & PROCEEDED TOWARDS ANC. CLEANED & SECURED NR 3 SMOKE DETECTOR GND. R & R 3 WIRES AT FS 470 FWD OF DOME LIGHT
- [SDR FXGA20140110001](https://openairdocs.org/sdr/FXGA20140110001.md): Wire · chafed · Jan 8, 2014 · N351CE · Doug C118A · Fire Protection System Wiring
  > SMOKE DETECTOR ACTIVATED IN FLIGHT. VISUAL INSPECTION OF CARGO COMPARTMENT SHOWED NO EVIDENCE OF SMOKE. ZONE NR 2 WOULD NOT TEST. REPAIRED CHAFFED WIRES AT NR 1 & NR 3 SMOKE DETECTOR. RELAMPED TEST LIGHT ON NR 2 SMOKE DETECTOR IAW DC6 MM 28-5-5 OPERATIONS C
- [SDR FXGA20140108001](https://openairdocs.org/sdr/FXGA20140108001.md): Wire · damaged · Jan 7, 2014 · N351CE · Doug C118A · Fire Protection System Wiring
  > NR 3 MAIN CABIN SMOKE DETECTOR GAVE FAULTY INDICATION, DIVERTED TO GAL AT 0405Z. DEFERRED NR 3 SMOKE DETECTOR IAW MEL 26-7. OFF LOADED CARGO & PROCEEDED TO ANC. AIRCRAFT WAS REPAIRED AT ANC, NR 3 SMOKE DETECTOR CONNECTOR WAS FOUND TO HAVE A DAMAGED WIRE THA
- [SDR FXGA2013020101](https://openairdocs.org/sdr/FXGA2013020101.md): Skin · cracked · Feb 1, 2013 · N351CE · Doug C118A · Nacelle/Pylon, Plate/Skin
  > THE NR 3 NACELLE LONGERON 11 Z ANGLE WAS FOUND CRACKED. THE STRINGER F WAS FOUND WORN THROUGH & THE NACELLE SKIN WAS FOUND CRACKED AT STATION 408, LONGERON 11. THE Z ANGLE & STRINGER WILL BE REPLACED WITH NEW PARTS MADE FROM THE SAME MATERIAL & THE SKIN WILL
- [SDR FXGA201212191296](https://openairdocs.org/sdr/FXGA201212191296.md): Stringer · cracked · Dec 12, 2012 · N351CE · Doug C118A · Wing, Longeron/Stringer
  > CRACK AT WING STRINGER 19L, WS 234L.
- [SDR FXGA201212061291](https://openairdocs.org/sdr/FXGA201212061291.md): Skin · corroded · Dec 9, 2012 · N351CE · Doug C118A · Fuselage Main, Plate/Skin
  > SKIN LAP CORRODED AT BS 122, STRINGER 17L. CUT CORRODED SKIN & INSTALL REPAIR DOUBLER & FILLERS IAW EAC EO 0502 - EO 1291.
- [SDR FXGA20120711001](https://openairdocs.org/sdr/FXGA20120711001.md): Fire Warning · illuminated · Jul 2, 2012 · N351CE · Doug C118A · Fire Detection
  > NR 1 ENGINE OBSERVED ZONE 1 FIRE INDICATION DURING TAKEOFF POWER.
- [SDR FXGA201205101231](https://openairdocs.org/sdr/FXGA201205101231.md): Skin · chafed · May 10, 2012 · N351CE · Doug C118A · Trailing Edge Flaps
  > APPROXIMATELY 8 INCHES OF CHAFING DAMAGE WAS FOUND ON RT FLAP LE. CUT OUT CHAFING DAMAGE. FABRICATE EXTERNAL PATCH FROM 0.020 INCHES 403 STAINLESS WITH ESTABLISHED RIVET PATTERN IAW DC-6A & B OVERHAUL MANUAL FIG 13-47. INSTALL DOUBLER & MS20470AD4 RIVETS W
- [SDR FXGA20111210006](https://openairdocs.org/sdr/FXGA20111210006.md): Skin · corroded · Dec 12, 2011 · N351CE · Doug C118A · Wing, Plate/Skin
  > DURING HEAVY MX, DISCOVERED CORRODED WING SKIN JUST OTBD OF NR 3 NACELLE BETWEEN CENTER AND REAR SPARS.
- [SDR FXGA20111210005](https://openairdocs.org/sdr/FXGA20111210005.md): Stringer · corroded · Dec 12, 2011 · N351CE · Doug C118A · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MX, DISCOVERED CORRODED FUSELAGE STRINGER 25L BETWEEN FUSELAGE STATIONS 440 AND 447.
- [SDR FXGA20111210004](https://openairdocs.org/sdr/FXGA20111210004.md): Frame · cracked · Dec 12, 2011 · N351CE · Doug C118A · Fuselage Main, Frame
  > DURING HEAVY MX, DISCOVERED CRACKED FUSELAGE FRAME AT FUSELAGE STATION 438 AT STRINGERS 27L AND 27R.
- [SDR FXGA20111210003](https://openairdocs.org/sdr/FXGA20111210003.md): Skin · cracked · Dec 12, 2011 · N351CE · Doug C118A · Wing, Center Box
  > DURING HEAVY MX DISCOVERED CRACKED CENTER WING SKIN, DOUBLER, AND REINFORCING RING AT RT WING STATION 17 FWD OF WING STRINGER 20 AND FOUND SAME DOUBLER AND REINFORCING RING CRACKED AT LT WING STA 17 FORWARD OF STRINGER 20.
- [SDR FXGA20111210002](https://openairdocs.org/sdr/FXGA20111210002.md): Stringer · cracked · Dec 12, 2011 · N351CE · Doug C118A · Wing, Longeron/Stringer
  > DURING HEAVY MX, DISCOVERED CRACKED WING STRINGER ON THE LT WING STRINGER 22 AT WING STA 240 ALONG WITH CRACKED WING SKIN AS A RESULT OF THE CRACKED STRINGER.
- [SDR FXGA20111210001](https://openairdocs.org/sdr/FXGA20111210001.md): Floor Panel · corroded · Dec 12, 2011 · N351CE · Doug C118A · Fuselage Floor Panel
  > DURING HEAVY MX, DISCOVERED 5 LARGE AERAS OF CORROSION ON THE CABIN FLOOR.
- [SDR FXGA2011120200005](https://openairdocs.org/sdr/FXGA2011120200005.md): Skin · corroded · Dec 2, 2011 · N351CE · Doug C118A · Wing, Plate/Skin
  > DURING HEAVY MX DISCOVERED CORRODED WING SKIN JUST OTBD OF NR 3 NACELLE BETWEEN CENTER AND REAR SPARS.
- [SDR FXGA2011120200004](https://openairdocs.org/sdr/FXGA2011120200004.md): Stringer · corroded · Dec 2, 2011 · N351CE · Doug C118A · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MX, DISCOVERED CORRODED FUSELAGE STRINGER 25L BETWEEN FUSELAGE STATIONS 440 AND 447.
- [SDR FXGA2011120200003](https://openairdocs.org/sdr/FXGA2011120200003.md): Frame · cracked · Dec 2, 2011 · N351CE · Doug C118A · Fuselage Main, Frame
  > DURING HEAVY MX DISCOVERED CRACKED FUSELAGE FRAME AT FUSELAGE STATION 438 AT STRINGERS 27L AND 27R.
- [SDR FXGA2001120200002](https://openairdocs.org/sdr/FXGA2001120200002.md): Stringer · cracked · Dec 2, 2011 · N351CE · Doug C118A · Wing, Longeron/Stringer
  > DURING HEAVY MX DISCOVERED CRACKED WING STRINGER ON THE LT WING STRINGER 22 AT WING STATION 240 ALONG WITH CRACKED WING SKIN AS A RESULT OF THE CRACKED STRINGER.
- [SDR FXGA2011202000001](https://openairdocs.org/sdr/FXGA2011202000001.md): Floor Panel · corroded · Dec 2, 2011 · N351CE · Doug C118A · Fuselage Floor Panel
  > DURING HEAVY MX DISCOVERED 5 LARGE AREAS OF CORROSION ON THE CABIN FLOOR.
- [SDR FXGA20110613001](https://openairdocs.org/sdr/FXGA20110613001.md): Tappet · stuck · Jun 13, 2011 · N351CE · Doug C118A · Reciprocating Engine Cylinder Section
  > AFTER LEAVING REVERSE NR 1 ENGINE BACK-FIRED AND CAUGHT FIRE THEN QUICKLY WENT OUT. REPLACED NR 1 ENGINE ASSY DUE TO FAILED NR 8 CYLINDER AND NR 13 CYLINDER EXHAUST TAPPET STUCK OPEN. ENGINE CHANGED IAW EAC DC-6MM 5.16, GROUND RUN CHECKS GOOD.
- [SDR FXGA351A](https://openairdocs.org/sdr/FXGA351A.md): Skin · cracked · Dec 7, 2010 · N351CE · Doug C118A · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CRACKED AT NR2 VHF COM ANTENNA DOUBLER. REPAIRED IAW EAC EO 1061 AND 8110-3 NR1032, DATED 12/07/2010.
- [SDR FXGAN351CE6](https://openairdocs.org/sdr/FXGAN351CE6.md): Skin · corroded · Aug 7, 2010 · N351CE · Doug C118A · Wing, Plate/Skin
  > CORROSION FOUND ON WING SKIN STA 167R TO 182R.
- [SDR FXGAN351CE5](https://openairdocs.org/sdr/FXGAN351CE5.md): Stringer · cracked · Aug 7, 2010 · N351CE · Doug C118A · Wing, Longeron/Stringer
  > STRINGERS 18L,19L AND 20L FOUND CRACKED.
- [SDR FXGAN351CE4](https://openairdocs.org/sdr/FXGAN351CE4.md): Doubler · cracked · Aug 7, 2010 · N351CE · Doug C118A · Wing, Plate/Skin
  > NR 2 ALTERNATE FUEL TANK ACCESS DOOR DOUBLER CRACKED.
- [SDR FXGAN351CE3](https://openairdocs.org/sdr/FXGAN351CE3.md): Fitting · corroded · Aug 7, 2010 · N351CE · Doug C118A · Wing, Longeron/Stringer
  > STRINGER 21R END FITTING AND SURROUNDING SKIN FOUND CORRODED.
- [SDR FXGAN351CE2](https://openairdocs.org/sdr/FXGAN351CE2.md): Skin · corroded · Aug 7, 2010 · N351CE · Doug C118A · Wing, Plate/Skin
  > CENTER WING END RIB SKIN AND LOWER ANGLE FOUND CORRODED.
- [SDR FXGAN351CE1](https://openairdocs.org/sdr/FXGAN351CE1.md): Fitting · cracked · Aug 7, 2010 · N351CE · Doug C118A · Wing Spar
  > CRACK DETECTED ON THE INBOARD CENTER SPAR UPPER FITTING.
- [SDR FXGAN351CE](https://openairdocs.org/sdr/FXGAN351CE.md): Fitting · corroded · Aug 7, 2010 · N351CE · Doug C118A · Wing, Longeron/Stringer
  > OUTBOARD WING STRINGER FITTING FOUND CORRODED.
- [SDR 2010F00099](https://openairdocs.org/sdr/2010F00099.md): Brush Block · worn · Mar 8, 2010 · N351CE · Doug C118A · Propeller/Rotor Anti-Ice/De-Ice System
  > DURING ICING THE NR (4) PROPELLER DEICE INDICATED 50 AMPS, SPARKS VISIBLE IN THE COWLING.
- [SDR 2005FA0000573](https://openairdocs.org/sdr/2005FA0000573.md): Bolt · broken · Mar 20, 2005 · N351CE · Doug C118A · Reciprocating Engine Power Section
  > CRANKSHAFT CONNECTING BOLT BROKE CAUSING LOSS OF ENGINE POWER. DAMAGE TO ENGINE INCLUDED REAR MAIN BEARING AND CRANKSHAFT ASSY. PROBABLE CAUSE COULD BE OVER TORQUE AT ASSY OR METAL FATIGUE. PREVIOUS OVERHAUL AGENCY UNKNOWN AT THIS TIME. (K)
- [SDR 97ZZZX3766](https://openairdocs.org/sdr/97ZZZX3766.md): Spar Cap · cracked · May 12, 1997 · N351CE · Doug C118A · Horizontal Stabilizer, Spar/Rib
  > HORIZONTAL SPAR CAP FITTING IS CRACKED.
- [SDR 96ZZZX3275](https://openairdocs.org/sdr/96ZZZX3275.md): Blower · worn · May 2, 1996 · N351CE · Doug C118A · Power Recovery Turbine
  > ABORTED TAKEOFF, NR 4 MANIFOLD PRESSURE ONLY 28 INCHES.
- [SDR 96ZZZX3276](https://openairdocs.org/sdr/96ZZZX3276.md): Distributor · malfunctioned · Apr 13, 1996 · N351CE · Doug C118A · Magneto/Distributor
  > SHUT DOWN NR 2 ENGINE DUE TO ROUGHNESS (21172).

## 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 = 'N351CE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N351CE/reports

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