# Service difficulty reports: N19704, cancelled Nov 30, 1999

A list on [N19704, cancelled Nov 30, 1999](https://openairdocs.org/deregistered/N19704-1999-11-30.md).

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

- [SDR C2XA99IA482](https://openairdocs.org/sdr/C2XA99IA482.md): Stringer · cracked · Sep 18, 1999 · N19704 · Emb EMB120RT · Wing, Longeron/Stringer
  > DURING CONTINENTAL EXPRESS C-CHECK, FOUND LEFT WING LOWER SKIN 2ND STRINGER CRACKED AT PANEL 522EB. REMOVED DAMAGED SECTION OF STRINGER, SPLICED IN NEW SECTION IAW CONTINENTAL EXPRESS EC5710-01010 REV B. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA99IA481](https://openairdocs.org/sdr/C2XA99IA481.md): Stringer · cracked · Sep 18, 1999 · N19704 · Emb EMB120RT · Wing, Longeron/Stringer
  > DURING CONTINENTAL EXPRESS C-CHECK, FOUND LEFT WING LOWER SKIN 4TH STRINGER CRACKED AT PANEL 522EB. REMOVED DAMAGED SECTION OF STRINGER, SPLICED IN NEW SECTION IAW CONTINENTAL EXPRESS EC5710-01010 REV B. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA99IA480](https://openairdocs.org/sdr/C2XA99IA480.md): Stringer · cracked · Sep 18, 1999 · N19704 · Emb EMB120RT · Wing, Longeron/Stringer
  > DURING CONTINENTAL EXPRESS C-CHECK, FOUND RIGHT WING INTERNAL LOWER STRINGER CRACKED FORWARD OF PANEL 622EB. REMOVED EXISTING STRINGER SPLICE AND INSTALLED NEW SPLICE IAW CONTINENTAL EXPRESS EC5710-01010 REV B AND DER REPORT NR 99-150. AIRCRAFT APPROVED FOR
- [SDR C2XA99IA479](https://openairdocs.org/sdr/C2XA99IA479.md): Skin · cracked · Sep 18, 1999 · N19704 · Emb EMB120RT · Wing, Plate/Skin
  > DURING CONTINENTAL EXPRESS C-CHECK, FOUND RIGHT WING LOWER SKIN CRACKED AT REFUEL/DEFUEL ADAPTOR ACCESS PANELS. REMOVED AND REPLACED SKIN PANEL IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA99IA478](https://openairdocs.org/sdr/C2XA99IA478.md): Skin · cracked · Sep 18, 1999 · N19704 · Emb EMB120RT · Wing, Plate/Skin
  > DURING CONTINENTAL EXPRESS C-CHECK, FOUND RT WING LOWER SKIN CRACKED AT STATION YA2480 FORWARD OF PANEL 622EB. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW GRISWOLD ENGINEERING DER REPORT NR 99-150. AIRCRAFT APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA99IA477](https://openairdocs.org/sdr/C2XA99IA477.md): Skin · chafed · Sep 18, 1999 · N19704 · Emb EMB120RT · Fuselage Main, Plate/Skin
  > DURING CONTINENTAL EXPRESS C-CHECK, FOUND RT FUSELAGE SKIN CHAFFED BY A/C HEAT EXCHANGER AND DUCTS. BLENDED DAMAGE AND INSTALLED REPAIR DOUBLER IAW SRM 51-40-02 AND 51-21-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA97CL084](https://openairdocs.org/sdr/C2XA97CL084.md): Gcu · failed · Oct 24, 1997 · N19704 · Emb EMB120RT · AC Regulator
  > CLE - FLT 3266 - CREW REPORTED THAT THE RIGHT MAIN GENERATOR FAILED IN FLIGHT AND WOULD NOT RESET. AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND THEN REMOVED AND REPLACED THE RIGHT GENERATOR CONTROL UNIT IAW EMB-
- [SDR C2XA97IA064](https://openairdocs.org/sdr/C2XA97IA064.md): Skin · cracked · Feb 11, 1997 · N19704 · Emb EMB120RT · Wing, Plate/Skin
  > IAH - DURING C-CHECK INSPECTION, THE LEFT WING LOWER SKIN WAS FOUND TO BE CRACKED. MAINTENANCE REPAIRED THE LOWER SKIN USING A DOUBLER, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA97IA063](https://openairdocs.org/sdr/C2XA97IA063.md): Skin · cracked · Feb 11, 1997 · N19704 · Emb EMB120RT · Wing, Plate/Skin
  > IAH - DURING C-CHECK INSPECTION, THE RIGHT WING LOWER SKIN WAS FOUND TO BE CRACKED. MAINTENANCE REPAIRED THE SKIN USING A DOUBLER, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA97IA062](https://openairdocs.org/sdr/C2XA97IA062.md): Seat Track · corroded · Feb 11, 1997 · N19704 · Emb EMB120RT · Fuselage, Seat/Cargo Attach Fittings
  > IAH - DURING C-CHECK INSPECTION, THE RIGHT FLOOR SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PORTION OF SEAT TRACK AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA97IA061](https://openairdocs.org/sdr/C2XA97IA061.md): Seat Track · corroded · Feb 11, 1997 · N19704 · Emb EMB120RT · Fuselage, Seat/Cargo Attach Fittings
  > IAH - DURING C-CHECK INSPECTION, THE LEFT FORWARD FLOOR SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA97IA060](https://openairdocs.org/sdr/C2XA97IA060.md): Seat Track · corroded · Feb 11, 1997 · N19704 · Emb EMB120RT · Fuselage, Seat/Cargo Attach Fittings
  > IAH - DURING C-CHECK INSPECTION, THE LEFT AFT FLOOR SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PORTION OF SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA97IA059](https://openairdocs.org/sdr/C2XA97IA059.md): Seat Track · corroded · Feb 11, 1997 · N19704 · Emb EMB120RT · Fuselage, Seat/Cargo Attach Fittings
  > IAH - DURING C-CHECK INSPECTION, THE RIGHT FORWARD SIDEWALL SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PORTION OF SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA97IA058](https://openairdocs.org/sdr/C2XA97IA058.md): T-Profile · corroded · Feb 11, 1997 · N19704 · Emb EMB120RT · Fuselage Main, Frame
  > IAH - DURING C-CHECK INSEPCTION, THE RIGHT T-PROFILE WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED T-PROFILE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA97IA057](https://openairdocs.org/sdr/C2XA97IA057.md): T-Profile · corroded · Feb 11, 1997 · N19704 · Emb EMB120RT · Fuselage Main, Frame
  > IAH - DURING C-CHECK INSPECTION, THE RIGHT CENTER T-PROFILE AT FRAME 36 AND 38, WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED T-PROFILE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA97IA056](https://openairdocs.org/sdr/C2XA97IA056.md): T-Profile · corroded · Feb 11, 1997 · N19704 · Emb EMB120RT · Fuselage Miscellaneous Structure
  > IAH - DURING C-CHECK INSPECTION, THE T-PROFILER AT FRAME 38 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED T-PROFILE AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR C2XAIA142](https://openairdocs.org/sdr/C2XAIA142.md): Skin Support · cracked · Jul 25, 1995 · N19704 · Emb EMB120RT · Wing Miscellaneous Structure
  > IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB 21, NR 2 UPPER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA95IA147](https://openairdocs.org/sdr/C2XA95IA147.md): Stringer · cracked · Jul 25, 1995 · N19704 · Emb EMB120RT · Wing, Longeron/Stringer
  > IAH - DURING C-CHECK INSPECTION, THE RIGHT WING STRINGER NR 10, WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED THE AFFECTED PORTION OF THE STRINGER AND PERFORMED A SPLICE REPAIR IAW EMB FAX NR EST.234/95. THE AIRCRAFT WAS THE APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA95IA146](https://openairdocs.org/sdr/C2XA95IA146.md): Stringer · cracked · Jul 25, 1995 · N19704 · Emb EMB120RT · Wing, Longeron/Stringer
  > IAH - DURING C-CHECK INSPECTION, THE RIGHT WING STRINGER NR 8, WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND AFFECTED PORTION OF THE STRINGER AND PERFORMED A SPLICE REPAIR IAW EMB FAX NR EST.234/95. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA95IA145](https://openairdocs.org/sdr/C2XA95IA145.md): Support · cracked · Jul 25, 1995 · N19704 · Emb EMB120RT · Wing Miscellaneous Structure
  > IAH - DURING C-CHECK INSPECTION, THE RIGHT WING, PRESSURE REFUEL SHUTOFF VALVE SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA95IA144](https://openairdocs.org/sdr/C2XA95IA144.md): Seat Track · corroded · Jul 25, 1995 · N19704 · Emb EMB120RT · Fuselage, Seat/Cargo Attach Fittings
  > IAH - DURING C-CHECK INSPECTION, THE LEFT INBOARD AFT SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED TRACK SECTION, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA95IA143](https://openairdocs.org/sdr/C2XA95IA143.md): Skin Support · cracked · Jul 25, 1995 · N19704 · Emb EMB120RT · Wing Miscellaneous Structure
  > IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB 22, NR 4 UPPER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA95IA141](https://openairdocs.org/sdr/C2XA95IA141.md): Skin Support · cracked · Jul 25, 1995 · N19704 · Emb EMB120RT · Wing Miscellaneous Structure
  > IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB 21, NR 1 UPPER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA95IA140](https://openairdocs.org/sdr/C2XA95IA140.md): Skin Support · cracked · Jul 25, 1995 · N19704 · Emb EMB120RT · Wing Miscellaneous Structure
  > IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB 20, NR 2 UPPER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENACNE REMOVED AND REPLACED THE AFFECTED SUPPORT AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA95IA139](https://openairdocs.org/sdr/C2XA95IA139.md): Skin Support · cracked · Jul 25, 1995 · N19704 · Emb EMB120RT · Wing Miscellaneous Structure
  > IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB 20, NR 1 UPPER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA95IA138](https://openairdocs.org/sdr/C2XA95IA138.md): Skin Support · cracked · Jul 25, 1995 · N19704 · Emb EMB120RT · Wing Miscellaneous Structure
  > IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB 16, NR 4 LOWER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA95IA137](https://openairdocs.org/sdr/C2XA95IA137.md): Skin Support · cracked · Jul 25, 1995 · N19704 · Emb EMB120RT · Wing Miscellaneous Structure
  > IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB 16, NR 3 LOWER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA95IA136](https://openairdocs.org/sdr/C2XA95IA136.md): Skin Support · cracked · Jul 25, 1995 · N19704 · Emb EMB120RT · Wing Miscellaneous Structure
  > IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB 16, NR 2 UPPER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA95IA135](https://openairdocs.org/sdr/C2XA95IA135.md): Skin Support · cracked · Jul 25, 1995 · N19704 · Emb EMB120RT · Wing Miscellaneous Structure
  > IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 15, NR 2 LOWER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA95IA134](https://openairdocs.org/sdr/C2XA95IA134.md): Skin Support · cracked · Jul 25, 1995 · N19704 · Emb EMB120RT · Wing Miscellaneous Structure
  > IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB 15, NR 3 LOWER ATTACH ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA95IA133](https://openairdocs.org/sdr/C2XA95IA133.md): Skin Support · cracked · Jul 25, 1995 · N19704 · Emb EMB120RT · Wing Miscellaneous Structure
  > IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB 19, NR 5 UPPER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA95IA132](https://openairdocs.org/sdr/C2XA95IA132.md): Skin Support · cracked · Jul 25, 1995 · N19704 · Emb EMB120RT · Wing Miscellaneous Structure
  > IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB 21, NR 2 UPPER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA95IA131](https://openairdocs.org/sdr/C2XA95IA131.md): Skin Support · cracked · Jul 25, 1995 · N19704 · Emb EMB120RT · Wing Miscellaneous Structure
  > IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB 16, NR 2, NR 3, AND NR 4 UPPER SKIN SUPPORTS WERE FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA95IA130](https://openairdocs.org/sdr/C2XA95IA130.md): Skin Support · cracked · Jul 25, 1995 · N19704 · Emb EMB120RT · Wing Miscellaneous Structure
  > IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB 15, NR 3 LOWER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
- [SDR C2XA95IA129](https://openairdocs.org/sdr/C2XA95IA129.md): Skin Support · cracked · Jul 25, 1995 · N19704 · Emb EMB120RT · Wing Miscellaneous Structure
  > IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB 15, AND NR 4 LOWER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M0
- [SDR C2XA95CL085](https://openairdocs.org/sdr/C2XA95CL085.md): Annunciator · failed · May 18, 1995 · N19704 · Emb EMB120RT · Trailing Flap Position Indicating System
  > FLT 3335 - PIT-CLE - ON TAXI OUT, RECEIVED FLAP ASYMMETRY. BROUGHT FLAP LEVER UP AND ALL FLAPS CAME UP, HOWEVER, NO FLAP INDICATION ON OVERHEAD PANEL. FERRIED AIRCRAFT TO CLE. MAINTENANCE REMOVED AND REPLACED THE FLAP ANNUNCIATOR. OPS CHECKED GOOD. RETURN
- [SDR C2XA95CL030](https://openairdocs.org/sdr/C2XA95CL030.md): Actuator · intermittent · Feb 11, 1995 · N19704 · Emb EMB120RT · Trailing Edge Flap Actuator
  > FLT 3304 - TOL-CLE - FLAP DISAGREEMENT, LEFT AND RIGHT INBOARD SHOWING 10 DEGREES. MAINTENANCE REMOVED AND REPLACED OUTBOARD TRACKS ON INBOARD FLAPS. OPS CHECK GOOD. ON PREFLIGHT POWER UP RECEIVED FLAP CONTROL FAULT, WOULD NOT RESET. INBOARD SHOWED 10 DEGR

## 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 = 'N19704' AND deregistration_id = 'N19704-1999-11-30'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N19704-1999-11-30/reports

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