# Service difficulty reports: N785NC, cancelled May 14, 2015

A list on [N785NC, cancelled May 14, 2015](https://openairdocs.org/deregistered/N785NC-2015-05-14.md).

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

Page 1 of 2 · 76 reports

- [SDR DALA1019909876](https://openairdocs.org/sdr/DALA1019909876.md): Attach Angle · cracked · Aug 21, 2010 · N785NC · Doug DC951 · Nacelle/Pylon, Attach Fittings
  > DURING LINE CHECK FOUND CRACK IN LT ENGINE PYLON INSP PANEL 8103 ATTACH ANGLE. REPAIRED IAW SRM 54-01.
- [SDR DALA1019899876](https://openairdocs.org/sdr/DALA1019899876.md): Attach Fitting · cracked · Aug 21, 2010 · N785NC · Doug DC951 · Nacelle/Pylon, Attach Fittings
  > DURING LINE CHECK FOUND CRACK IN LT PYLON CLOSURE WEB UPPER CLIP INBD SIDE. REPAIRED IAW SRM 54-20-0.
- [SDR DALA1019889876](https://openairdocs.org/sdr/DALA1019889876.md): Attach Angle · cracked · Aug 21, 2010 · N785NC · Doug DC951 · Nacelle/Pylon, Attach Fittings
  > DURING LINE CHECK FOUND CRACK IN LT PYLON FAIRING SUPPORT RIB ATTACH ANGLE. REPAIRED IAW DWG 9915500.
- [SDR DALA1018249876](https://openairdocs.org/sdr/DALA1018249876.md): Skin · damaged · Aug 3, 2010 · N785NC · Doug DC951 · Fuselage Main, Plate/Skin
  > DURING LINE CHECK FOUND DAMAGE TO FUSELAGE SKIN AT BS 427 AFT OF FORWARD CARGO DOOR AREA. REPAIRED PER SRM 53-05-82.
- [SDR DALA102609876](https://openairdocs.org/sdr/DALA102609876.md): Frame · cracked · Feb 2, 2010 · N785NC · Doug DC951 · Fuselage Main, Frame
  > DURING "H" CHECK FOUND CRACK IN FRAME AT BS 465 L26R. REPAIRED IAW 53-03-02 AND SRM 51-30-05.
- [SDR DALA102519876](https://openairdocs.org/sdr/DALA102519876.md): Pan · corroded · Feb 1, 2010 · N785NC · Doug DC951 · Fuselage Miscellaneous Structure
  > DURING "H" CHECK FOUND DOOR PAN CORRODED AT BS 1079. REPAIRED IAW SRM 51-30-2, 51-30-5.
- [SDR DALA102509876](https://openairdocs.org/sdr/DALA102509876.md): Frame · cracked · Feb 1, 2010 · N785NC · Doug DC951 · Fuselage Main, Frame
  > DURING "H" CHECK FOUND CRACK IN FRAME AT BS 465 L26R. REPAIRED IAW SRM 53-03,51-10-4,51-10-3,51-30-5,51-10-2.
- [SDR DALA102239876](https://openairdocs.org/sdr/DALA102239876.md): Structure · cracked · Jan 31, 2010 · N785NC · Doug DC951 · Fuselage Main, Structure
  > DURING "H" CHECK FOUND CRACK IN RT VERTICAL STRUT IN FWD CARGO BS 598. REPAIRED IAW SRM 51-30-2 & 53-01.
- [SDR DALA102229876](https://openairdocs.org/sdr/DALA102229876.md): Skin · corroded · Jan 31, 2010 · N785NC · Doug DC951 · Fuselage Main, Plate/Skin
  > DURING "H" CHECK FOUND CORROSION ON DOOR CUTOUT INNER SKIN. REPAIRED IAW SRM 51-30-2 & 51-30-5.
- [SDR DALA102249876](https://openairdocs.org/sdr/DALA102249876.md): Cargo Track · corroded · Jan 29, 2010 · N785NC · Doug DC951 · Fuselage, Seat/Cargo Attach Fittings
  > DURING "H" CHECK FOUND CORROSION ON CARGO TIEDOWN TRACK AT BS 1167 BETWEEN L27R AND L28R. REPAIRED IAW SRM 51-30-1.
- [SDR DALA102049876](https://openairdocs.org/sdr/DALA102049876.md): Floor Panel · corroded · Jan 28, 2010 · N785NC · Doug DC951 · Fuselage Floor Panel
  > DURING "H" CHECK FOUND COCKPIT FLOOR PANEL NR 15 BETWEEN STA 148 AND 160 HAS CORROSION. REPAIRED IAW SRM 51-10-04, SRM 51-30-01, AND SRM 51-30-02.
- [SDR DALA101989876](https://openairdocs.org/sdr/DALA101989876.md): Floor Panel · corroded · Jan 27, 2010 · N785NC · Airbus A330323 · Fuselage Floor Panel
  > DURING "H" CHECK FOUND CORROSION ON FLOOR PANEL NR 37. REPAIRED IAW SRM 51-30-2.
- [SDR DALA101749876](https://openairdocs.org/sdr/DALA101749876.md): Channel · cracked · Jan 26, 2010 · N785NC · Doug DC951 · Fuselage Miscellaneous Structure
  > DURING "H" CHECK FOUND FLOOR PANEL NR37 HAS A CRACKED HAT CHANNEL. REPAIRED IAW SRM 51-30-2.
- [SDR DALA101739876](https://openairdocs.org/sdr/DALA101739876.md): Floor Panel · corroded · Jan 26, 2010 · N785NC · Doug DC951 · Fuselage Floor Panel
  > DURING "H" CHECK FOUND COCKPIT FLOOR PANEL NR 13 HAS CORROSION AT STA 148 AND 160. REPAIRED IAW SRM 51-30-2, SRM 51-10-2, AND SRM 51-10-4.
- [SDR DALA101679876](https://openairdocs.org/sdr/DALA101679876.md): Intercostal · cracked · Jan 25, 2010 · N785NC · Doug DC951 · Fuselage Miscellaneous Structure
  > DURING "H" CHECK FOUND CRACK IN INTERCOSTAL AT BS 579-598 BL0. REPAIRED IAW SRM 51-30-1.
- [SDR DALA101669876](https://openairdocs.org/sdr/DALA101669876.md): Cusp Web · cracked · Jan 25, 2010 · N785NC · Doug DC951 · Fuselage Miscellaneous Structure
  > DURING H-CHECK FOUND CUSP WEB CRACKED AT BS 1135 RBL 54. REPAIRED PER SRM 53-10-16.
- [SDR DALA101659876](https://openairdocs.org/sdr/DALA101659876.md): Frame · cracked · Jan 25, 2010 · N785NC · Doug DC951 · Fuselage Main, Frame
  > DURING "H" CHECK FOUND FRAME CRACKED AT BS 332 L26L-L27L. REPAIRED IAW SRM 53-03-02.
- [SDR DALA101339876](https://openairdocs.org/sdr/DALA101339876.md): Attach Bracket · cracked · Jan 22, 2010 · N785NC · Doug DC951 · Fuselage, Seat/Cargo Attach Fittings
  > DURING H" CHECK FOUND CRACK IN LT TIE DOWN TRACK ATTACH BRACKET AT BS 427. REPAIRED IAW SRM 51-30-05.
- [SDR DALA100779876](https://openairdocs.org/sdr/DALA100779876.md): Stiffener · cracked · Jan 19, 2010 · N785NC · Doug DC951 · Fuselage Main, Bulkhead
  > DURING "H" CHECK FOUND CRACK IN AFT PRESSURE BULKHEAD NR 4 STIFFENER CLIP AT RT BS 1167. REPAIRED IAW SRM 51-30-5 & SRM 53-10-25.
- [SDR DALA100769876](https://openairdocs.org/sdr/DALA100769876.md): Stiffener · cracked · Jan 19, 2010 · N785NC · Doug DC951 · Fuselage Main, Bulkhead
  > DURING "H" CHECK FOUND CRACK IN AFT PRESSURE BULKHEAD NR 2 STIFFINER CLIP, AT LT BS 1167. REPAIRED IAW SRM 51-30-5, SRM 53-10-25, AND SRM 51-10-4.
- [SDR DALA100759876](https://openairdocs.org/sdr/DALA100759876.md): Stiffener · cracked · Jan 19, 2010 · N785NC · Doug DC951 · Fuselage Main, Bulkhead
  > DURING "H" CHECK FOUND CRACK IN AFT PRESSURE BULKHEAD NR 5 STIFFENER CLIP. REPAIRED IAW SRM 53-10-25.
- [SDR DALA100729876](https://openairdocs.org/sdr/DALA100729876.md): Floorbeam · damaged · Jan 18, 2010 · N785NC · Doug DC951 · Fuselage Main, Floor Beam
  > DURING "H" CHECK FOUND CHAFING DAMAGE TO FLOORBEAM AT BS 408, RBL 22 - BL 0. REPAIRED IAW SRM 53-01-20, SRM 51-10-4 & 51-10-3.
- [SDR DALA100709876](https://openairdocs.org/sdr/DALA100709876.md): Intercostal · cracked · Jan 18, 2010 · N785NC · Doug DC951 · Fuselage Miscellaneous Structure
  > DURING "H" CHECK FOUND CRACK ON INTERCOSTAL AT BS 408 BL 0. REPAIRED IAW SRM 51-10-2, SRM 51-10-3, SRM 51-10-4 AND SRM 51-30-5.
- [SDR DALA100689876](https://openairdocs.org/sdr/DALA100689876.md): Floorbeam · cracked · Jan 17, 2010 · N785NC · Doug DC951 · Fuselage Main, Floor Beam
  > DURING "H" CHECK FOUND CRACK IN ATTACH ANGLE AT BS 1167. REPAIRED IAW SRM 51-01.
- [SDR DALA100739876](https://openairdocs.org/sdr/DALA100739876.md): Stiffener · cracked · Jan 16, 2010 · N785NC · Doug DC951 · Fuselage Main, Bulkhead
  > DURING "H" CHECK FOUND 6 EACH BULKHEAD STIFFENERS, AND ATTACH CLIPS CRACKED, AT LT OTBD STA 1167. REPAIRED IAW SRM 53-10-25.
- [SDR DALA100719876](https://openairdocs.org/sdr/DALA100719876.md): Floor Support · cracked · Jan 16, 2010 · N785NC · Doug DC951 · Fuselage Miscellaneous Structure
  > DURING "H" CHECK FOUND CRACK IN FLOOR SUPPORT AT BS 1154, LBL 20. REPAIRED IAW SRM 51-72-01, SRM 51-10-2, SRM 51-10-4, AND SRM 51-10-3 & 51-30-2.
- [SDR DALA100699876](https://openairdocs.org/sdr/DALA100699876.md): Floor Panel · corroded · Jan 16, 2010 · N785NC · Doug DC951 · Fuselage Floor Panel
  > DURING "H" CHECK FOUND CORROSION ON FLOOR PANEL NR 26. REPAIRED IAW SRM 53-01, SRM 51-10-2, SRM 51-10-3, SRM 51-10-4 AND SRM 51-30-2.
- [SDR DALA100679876](https://openairdocs.org/sdr/DALA100679876.md): Cusp Web · cracked · Jan 16, 2010 · N785NC · Doug DC951 · Fuselage Miscellaneous Structure
  > DURING "H" CHECK FOUND CRACK IN LT CUSP WEB AT BS 1126. REPAIRED IAW SRM 53-13-3 AND SRM 53-10-16.
- [SDR DALA100669876](https://openairdocs.org/sdr/DALA100669876.md): Cusp Web · cracked · Jan 16, 2010 · N785NC · Doug DC951 · Fuselage Miscellaneous Structure
  > DURING "H" CHECK FOUND CRACK IN LT OTBD CUSP WEB AT BS 1102. REPAIRED IAW SRM 53-13-3 AND SRM 53-10-16.
- [SDR DALA100659876](https://openairdocs.org/sdr/DALA100659876.md): Cusp Web · cracked · Jan 16, 2010 · N785NC · Doug DC951 · Fuselage Miscellaneous Structure
  > DURING "H" CHECK FOUND CRACK IN RT OTBD CUSP WEB AT BS 1134. REPAIRED IAW SRM 53-10-16.
- [SDR DALA100649876](https://openairdocs.org/sdr/DALA100649876.md): Bulkhead · cracked · Jan 16, 2010 · N785NC · Doug DC951 · Fuselage Main, Bulkhead
  > DURING "H" CHECK FOUND CRACK IN BULKHEAD STRINGER NR 16 AT RT BS 1136. REPAIRED IAW SRM 51-30-2 AND SRM 51-30-5.
- [SDR DALA100399876](https://openairdocs.org/sdr/DALA100399876.md): Seat Track · corroded · Jan 14, 2010 · N785NC · Doug DC951 · Fuselage, Seat/Cargo Attach Fittings
  > DURING "H" CHECK FOUND LT INBD SEAT TRACK CLIP CORRODED AT BS 1136. REPAIRED IAW SRM 51-30-1.
- [SDR DALA100389876](https://openairdocs.org/sdr/DALA100389876.md): Floor Support · cracked · Jan 14, 2010 · N785NC · Doug DC951 · Fuselage Miscellaneous Structure
  > DURING "H" CHECK FOUND CRACK IN FLOOR SUPPORT HAT CHANNEL OTBD LEG AT BS 1136 RBL 20. REPAIRED IAW SRM 51-30-1, SRM 51-10-3, SRM 51-30-2.
- [SDR DALA100379876](https://openairdocs.org/sdr/DALA100379876.md): Floor Panel · cracked · Jan 14, 2010 · N785NC · Doug DC951 · Fuselage Floor Panel
  > DURING "H" CHECK FOUND CORROSION AND CRACKS IN FLOOR PANEL NR 16. FLOOR PANEL REPLACED IAW SRM 51-10-3, SRM 51-10-4 & 51-30-2.
- [SDR DALA100369876](https://openairdocs.org/sdr/DALA100369876.md): Floor Support · corroded · Jan 14, 2010 · N785NC · Doug DC951 · Fuselage Miscellaneous Structure
  > DURING "H" CHECK FOUND CORROSION ON FLOOR SUPPORT BETWEEN BS 218 TO 304 BL 0. REPAIRED IAW SRM 51-30-5,SRM 51-30-2 & SRM 51-10-4.
- [SDR DALA100359876](https://openairdocs.org/sdr/DALA100359876.md): Stringer · cracked · Jan 14, 2010 · N785NC · Doug DC951 · Fuselage Main, Longeron/Stringer
  > DURING "H" CHECK FOUND CRACK IN BULKHEAD STRINGER NR 17 AT BS 1136. REPAIRED IAW EA SRM 51-30-02.
- [SDR DALA100329876](https://openairdocs.org/sdr/DALA100329876.md): Floor Support · corroded · Jan 11, 2010 · N785NC · Doug DC951 · Fuselage Miscellaneous Structure
  > DURING "H" CHECK FOUND LEVEL 2 CORROSION AT RBL 44, BETWEEN STA 160 AND 200 FLOOR SUPPORT. REPAIRED IAW SRM 51-30.
- [SDR DALA109876032](https://openairdocs.org/sdr/DALA109876032.md): Floor Support · corroded · Jan 11, 2010 · N785NC · Doug DC951 · Fuselage Miscellaneous Structure
  > DURING "H" CHECK FOUND LEVEL 2 CORROSION AT RBL44, BETWEEN STA 160 AND 200 FLOOR SUPPORT. REPAIRED IAW SRM 51-30-5.
- [SDR DALA100299876](https://openairdocs.org/sdr/DALA100299876.md): Floor Support · corroded · Jan 11, 2010 · N785NC · Doug DC951 · Fuselage Miscellaneous Structure
  > DURING "H" CHECK FOUND CORROSION ON FLOOR SUPPORT BETWEEN BS 160 TO BS 200 RBL 44. REPAIRED IAW SRM 51-30-5.
- [SDR DALA100229876](https://openairdocs.org/sdr/DALA100229876.md): Floorbeam · corroded · Jan 9, 2010 · N785NC · Doug DC951 · Fuselage Main, Floor Beam
  > DURING "H" CHECK FOUND CORROSION ON FLOORBEAM AT BS 200 BL0-L20L. REPAIRED IAW SRM 51-10-03.
- [SDR DALA100219871](https://openairdocs.org/sdr/DALA100219871.md): Floorbeam · corroded · Jan 9, 2010 · N785NC · Doug DC951 · Fuselage Main, Floor Beam
  > DURING "H" CHECK FOUND CORROSION ON FLOORBEAM AT BS 237 L22L-L44L. REPAIRED IAW SRM 53-10-03.
- [SDR NWAA083429876](https://openairdocs.org/sdr/NWAA083429876.md): Battery · inoperative · Jul 26, 2008 · N785NC · Doug DC951 · Emergency Lighting
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 23-26 OF THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE ASSOCIATED FUSE AND INSTALLED NEW BATTERIES IN THE POWER SUPPLY. OPERATIONAL CHECK WAS GOOD. (A)
- [SDR NWAA082789876](https://openairdocs.org/sdr/NWAA082789876.md): Connector · disconnected · Jun 16, 2008 · N785NC · Doug DC951 · Light System Wiring
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGN LIGHT FOR THE FWD RT OVERWING HATCH WAS INOPERATIVE. MAINTENANCE FOUND THE WIRE RECEPTACLE UNPLUGGED. AFTER CONNECTOR WAS RE-SECURED THE LIGHTS FUNCTIONED WITHOUT PROBLEM. (A)
- [SDR NWAA081289876](https://openairdocs.org/sdr/NWAA081289876.md): Hose · separated · Mar 29, 2008 · N785NC · Doug DC951 · Cabin Cooling System
  > THE FLIGHT ATTENDANT REPORTED A THIN HAZE OF SMOKE AND A BURNING RUBBER SMELL IN THE CABIN. FLIGHT CREW NOTED THE SAME IN THE COCKPIT. THE SMOKE QUICKLY DISSIPATED SO THE FLIGHT CONTINUED TO SCHEDULED DESTINATION. LANDING AT DTW WAS NORMAL AND PASSENGERS DE
- [SDR 0203109876](https://openairdocs.org/sdr/0203109876.md): Duct · loose · Sep 22, 2002 · N785NC · Doug DC951 · Cabin Pressure Control System
  > LOST CABIN PRESSURE AT FL310 AND PERFORMED AN EMERGENCY DESCENT TO 10,000 FEET. THE OUTFLOW VALVE WAS FULLY CLOSED AND BOTH SUPPLY PRESSURES INDICATED 25 PSI. FLIGHT LANDED WITHOUT INCIDENT AT GFK. AFTER LANDING, THE CREW DETERMINED THERE WAS NO AIRFLOW FROM T
- [SDR 0202889876](https://openairdocs.org/sdr/0202889876.md): Control Valve · failed · Sep 12, 2002 · N785NC · Doug DC951 · Cabin Pressure Control System
  > DURING CRUISE AT FL330, THE MASTER WARNING AND RED CABIN PRESSURE LIGHTS ILLUMINATED AND CABIN PRESSURE INDICATED 1000 FEET. COMPLIED WITH COM PROCEDURES. AIRCRAFT DESCENDED TO 10,000 FEET BUT CREW COULD NOT CONTROL THE CABIN PRESSURE. MASKS DEPLOYED AUTOMA
- [SDR 0200199876](https://openairdocs.org/sdr/0200199876.md): Rod · broken · Jan 7, 2002 · N785NC · Doug DC951 · Leading Edge Slat Actuator
  > WHEN SLATS WERE EXTENDED, THE AIRCRAFT ROLLED TO THE RIGHT. SLAT DISAGREEMENT LIGHT ILLUMINATED AND BLUE SLAT EXTEND LIGHT DID NOT ILLUMINATE. COMPLIED WITH COM PROCEDURES AND AIRCRAFT LANDED UNEVENTFULLY WITH SLATS RETRACTED AND FLAPS EXTENDED. MAINTENANCE RE
- [SDR 0003689876](https://openairdocs.org/sdr/0003689876.md): Battery Pack · inoperative · Sep 27, 2000 · N785NC · Doug DC951 · Emergency Lighting
  > DURING LINE CHECK, FOUND FORWARD SECTION OF EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. OPERATIONAL CHECK NORMAL.
- [SDR 0001339973](https://openairdocs.org/sdr/0001339973.md): Battery Pack · discharged · Apr 7, 2000 · N785NC · Doug DC951 · Emergency Lighting
  > DURING LINE MAINTENANCE INSPECTION, FOUND TAIL COMPARTMENT EMERGENCY LIGHTS DIM. REPLACED BATTERY PACK.
- [SDR 9902859876](https://openairdocs.org/sdr/9902859876.md): Wire · crossed · Jul 14, 1999 · N785NC · Doug DC951 · Light System Wiring
  > DURING LINE MAINTENANCE INSPECTION, FORWARD COCKPIT AND FORWARD ENTRY CEILING EMERGENCY LIGHTS WOULD NOT SHUT OFF, NO OTHER POWER AVAILABLE. FOUND WIRES CROSSED AT TERMINALS 4 AND 7. REPAIRED WIRING, OPERATIONAL CHECK NORMAL.

Next page: https://openairdocs.org/deregistered/N785NC-2015-05-14/reports.md?page=2

## 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 = 'N785NC' AND deregistration_id = 'N785NC-2015-05-14'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N785NC-2015-05-14/reports

---
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