# Service difficulty reports: Boeing 737-230C

A list on [Boeing 737-230C](https://openairdocs.org/model/boeing-737-230c.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 4 · 193 reports

- [SDR 0711002](https://openairdocs.org/sdr/0711002.md): Position Sensor · malfunctioned · Nov 9, 2007 · N767TW · Boeing 737230C · Trailing Flap Position Indicating System
  > FLAP ASYMMETRY LOCKOUT AT 1 UNIT. DIVERTED FROM KLZU TO KATL (RUNWAY TOO SHORT FOR FLAPS 1 LANDING).
- [SDR 0701001](https://openairdocs.org/sdr/0701001.md): Lamp · loose · Jan 17, 2007 · N767TW · Boeing 737230C · Emergency Lighting
  > R1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE.
- [SDR 0601027](https://openairdocs.org/sdr/0601027.md): Skin · canning · Jan 6, 2006 · N767TW · Boeing 737230C · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN SECTION REPAIRED DUE TO OIL CANNING.
- [SDR 0601012](https://openairdocs.org/sdr/0601012.md): Frame · dented · Jan 6, 2006 · N767TW · Boeing 737230C · Fuselage Main, Frame
  > FUSELAGE FRAME SECTION REPAIRED DUE TO DENT OUT OF LIMITS.
- [SDR 0601011](https://openairdocs.org/sdr/0601011.md): Frame · dented · Jan 6, 2006 · N767TW · Boeing 737230C · Fuselage Main, Frame
  > FUSELAGE FRAME SECTION REPAIRED DUE TO DENT OUT OF LIMITS.
- [SDR 0601010](https://openairdocs.org/sdr/0601010.md): Frame · dented · Jan 6, 2006 · N767TW · Boeing 737230C · Fuselage Main, Frame
  > FUSELAGE FRAME SECTION REPAIRED DUE TO DENT OUT OF LIMITS.
- [SDR 0601026](https://openairdocs.org/sdr/0601026.md): Stringer · cracked · Jan 6, 2006 · N767TW · Boeing 737230C · Fuselage Main, Longeron/Stringer
  > FUSELAGE STRINGER REPAIRED DUE TO CRACK.
- [SDR 0601025](https://openairdocs.org/sdr/0601025.md): Stringer · corroded · Jan 6, 2006 · N767TW · Boeing 737230C · Fuselage Main, Longeron/Stringer
  > FUSELAGE STRINGER REPAIRED DUE TO CORROSION.
- [SDR 0601024](https://openairdocs.org/sdr/0601024.md): Shear Tie · corroded · Jan 6, 2006 · N767TW · Boeing 737230C · Fuselage Internal Mounting Structure
  > FUSELAGE FRAME SHEAR TIE REPAIRED DUE TO CORROSION.
- [SDR 0601009](https://openairdocs.org/sdr/0601009.md): Frame · dented · Jan 6, 2006 · N767TW · Boeing 737230C · Fuselage Main, Frame
  > FUSELAGE FRAME SECTION REPAIRED DUE TO DENT OUT OF LIMITS.
- [SDR 0601023](https://openairdocs.org/sdr/0601023.md): Skin · dented · Jan 6, 2006 · N767TW · Boeing 737230C · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN SECTION REPAIRED DUE TO DENT OUT OF LIMITS.
- [SDR 0601022](https://openairdocs.org/sdr/0601022.md): Skin · dented · Jan 6, 2006 · N767TW · Boeing 737230C · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN SECTION REPAIRED DUE TO DENT OUT OF LIMITS.
- [SDR MJYA0601021](https://openairdocs.org/sdr/MJYA0601021.md): Skin · dented · Jan 6, 2006 · N767TW · Boeing 737230C · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN SECTION REPAIRED DUE TO DENT OUT OF LIMITS.
- [SDR MJYA0601005](https://openairdocs.org/sdr/MJYA0601005.md): Frame · dented · Jan 6, 2006 · N767TW · Boeing 737230C · Fuselage Main, Frame
  > FRAME SECTION REPAIRED DUE TO DENT OUT OF LIMITS.
- [SDR MJYA0601015](https://openairdocs.org/sdr/MJYA0601015.md): Skin · out of limits · Jan 6, 2006 · N767TW · Boeing 737230C · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE E/E COMPARTMENT CUTOUT SKIN REPAIRED DUE TO SKIN HOLE EDGE DISTANCE OUT OF LIMITS.
- [SDR MJYA0601020](https://openairdocs.org/sdr/MJYA0601020.md): Skin · dented · Jan 6, 2006 · N767TW · Boeing 737230C · Cargo/Baggage Doors
  > FUSELAGE FORWARD CARGO COMPARTMENT DOOR EXTERNAL SKIN SECTION REPAIRED DUE TO DENT OUT OF LIMITS.
- [SDR MJYA0601008](https://openairdocs.org/sdr/MJYA0601008.md): Frame · dented · Jan 6, 2006 · N767TW · Boeing 737230C · Fuselage Main, Frame
  > FUSELAGE FRAME SECTION REPAIRED DUE TO DENT OUT OF LIMITS.
- [SDR MJYA0601004](https://openairdocs.org/sdr/MJYA0601004.md): Spar · corroded · Jan 6, 2006 · N767TW · Boeing 737230C · Wing Spar
  > WING CENTER SECTION REAR SPAR LOWER CHORD WAS REPAIRED DUE TO CORROSION.
- [SDR MJYA0601019](https://openairdocs.org/sdr/MJYA0601019.md): Floorbeam · cracked · Jan 6, 2006 · N767TW · Boeing 737230C · Fuselage Main, Floor Beam
  > FUSELAGE AFT CARGO COMPARTMENT DOOR LOWER BEAM REPAIRED DUE TO CRACK.
- [SDR MJYA0601017](https://openairdocs.org/sdr/MJYA0601017.md): Skin · dented · Jan 6, 2006 · N767TW · Boeing 737230C · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN SECTION REPAIRED DUE TO DENTS OUT OF LIMITS.
- [SDR MJYA0601016](https://openairdocs.org/sdr/MJYA0601016.md): Skin · dented · Jan 6, 2006 · N767TW · Boeing 737230C · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN SECTION REPAIRED DUE TO DENTS OUT OF LIMITS.
- [SDR MJYA0601013](https://openairdocs.org/sdr/MJYA0601013.md): Shear Beam · cracked · Jan 6, 2006 · N767TW · Boeing 737230C · Fuselage Miscellaneous Structure
  > RIGHT WHEEL WELL SHEAR BEAM REPAIRED DUE TO CRACK.
- [SDR MJYA0601007](https://openairdocs.org/sdr/MJYA0601007.md): Frame · dented · Jan 6, 2006 · N767TW · Boeing 737230C · Fuselage Main, Frame
  > FUSELAGE FRAME SECTION REPAIRED DUE TO DENT OUT OF LIMITS.
- [SDR MJYA0601018](https://openairdocs.org/sdr/MJYA0601018.md): Fairing · cracked · Jan 6, 2006 · N767TW · Boeing 737230C · Aerodynamic Fairings
  > FUSELAGE WING TO BODY FAIRING FORMER REPAIRED DUE TO CRACK.
- [SDR MJYA0601014](https://openairdocs.org/sdr/MJYA0601014.md): Skin · corroded · Jan 6, 2006 · N767TW · Boeing 737230C · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN SECTION REPAIRED DUE TO CORROSION.
- [SDR 0601030](https://openairdocs.org/sdr/0601030.md): Skin · cracked · Jan 6, 2006 · N767TW · Boeing 737230C · Fuselage Main, Plate/Skin
  > REPAIRED FUSELAGE SKIN SECTION DUE TO CRACK.
- [SDR MJYA0601041](https://openairdocs.org/sdr/MJYA0601041.md): Floorbeam · corroded · Jan 6, 2006 · N767TW · Boeing 737230C · Fuselage Main, Floor Beam
  > REPAIRED MAIN CARGO CABIN FLOORBEAM UPPER CHORD DUE TO CORROSION.
- [SDR 0601040](https://openairdocs.org/sdr/0601040.md): Floor Support · corroded · Jan 6, 2006 · N767TW · Boeing 737230C · Fuselage Miscellaneous Structure
  > REPAIRED MAIN CARGO CABIN FLOOR SUPPORT CHANNEL DUE TO CORROSION.
- [SDR 0601038](https://openairdocs.org/sdr/0601038.md): Fitting · damaged · Jan 6, 2006 · N767TW · Boeing 737230C · Fuselage Miscellaneous Structure
  > REPAIRED FUSELAGE MAIN CARGO CABIN FITTING UNDERNEATH LONGITUDINAL FLOOR BEAM DUE TO MISSING MATERIAL.
- [SDR 0601034](https://openairdocs.org/sdr/0601034.md): Web · corroded · Jan 6, 2006 · N767TW · Boeing 737230C · Fuselage Miscellaneous Structure
  > REPAIRED FUSELAGE MAIN CARGO CABIN LOWER JAMB FLOOR WEB DUE TO CORROSION.
- [SDR 0601033](https://openairdocs.org/sdr/0601033.md): Floorbeam · corroded · Jan 6, 2006 · N767TW · Boeing 737230C · Fuselage Main, Floor Beam
  > REPAIRED FUSELAGE MAIN CARGO CABIN FLOOR BEAM UPPER CHORD DUE TO CORROSION.
- [SDR 0601035](https://openairdocs.org/sdr/0601035.md): Skin · dented · Jan 6, 2006 · N767TW · Boeing 737230C · Fuselage Main, Plate/Skin
  > REPAIRED FUSELAGE SKIN SECTION DUE TO DENT OUT OF LIMITS.
- [SDR 0601032](https://openairdocs.org/sdr/0601032.md): Floorbeam · corroded · Jan 6, 2006 · N767TW · Boeing 737230C · Fuselage Main, Floor Beam
  > REPAIRED FUSELAGE MAIN CARGO CABIN FLOORBEAM UPPER CHORD DUE TO CORROSION.
- [SDR 0601048](https://openairdocs.org/sdr/0601048.md): Skin · elongated · Jan 6, 2006 · N767TW · Boeing 737230C · Nacelle/Pylon, Plate/Skin
  > REPLACED RT WING TO NR 2 ENGINE AFT FAIRING IB SKIN PANEL DUE TO ELONGATED HOLES.
- [SDR 0601047](https://openairdocs.org/sdr/0601047.md): Skin · dented · Jan 6, 2006 · N767TW · Boeing 737230C · Auxiliary Power Unit (APU) Doors
  > REPAIRED APU DOOR NONPRESSURIZED OUTER SKIN AT 2 LOCATIONS, FROM B/S 1098.5 TO 1108, AND FROM B/S 1113.5 TO B/S 1129.5 AT CENTER SECTION, DUE TO DENTS OUT OF LIMITS.
- [SDR 0601043](https://openairdocs.org/sdr/0601043.md): Skin · damaged · Jan 6, 2006 · N767TW · Boeing 737230C · Fuselage Main, Plate/Skin
  > REPAIRED FUSELAGE SKIN DUE TO SCRIBE LINES DAMAGE.
- [SDR 0601039](https://openairdocs.org/sdr/0601039.md): Window Frame · corroded · Jan 6, 2006 · N767TW · Boeing 737230C · Passenger Compartment Windows
  > REPAIRED FUSELAGE WINDOW FRAME AT TWO LOCATIONS, FROM B/S 688 TO 703.25, AND FROM B/S 727+3 TO 727+18.25, DUE TO CORROSION.
- [SDR 0601046](https://openairdocs.org/sdr/0601046.md): Skin · dented · Jan 6, 2006 · N767TW · Boeing 737230C · Fuselage Main, Plate/Skin
  > REPAIRED NONPRESSURIZED FUSELAGE SKIN SECTION DUE TO DENT OUT OF LIMITS.
- [SDR 0601042](https://openairdocs.org/sdr/0601042.md): Floorbeam · corroded · Jan 6, 2006 · N767TW · Boeing 737230C · Fuselage Main, Floor Beam
  > REPAIRED MAIN CARGO CABIN TRANSVERSAL BEAM DUE TO CORROSION.
- [SDR 0601044](https://openairdocs.org/sdr/0601044.md): Skin · damaged · Jan 6, 2006 · N767TW · Boeing 737230C · Fuselage Main, Plate/Skin
  > REPAIRED FUSELAGE SKIN DUE TO SCRIBE LINES DAMAGE.
- [SDR 0601049](https://openairdocs.org/sdr/0601049.md): Skin · damaged · Jan 6, 2006 · N767TW · Boeing 737230C · Trailing Edge Flaps
  > REPAIRED RIGHT WING OUTBOARD MID FLAP TRAILING EDGE LOWER SKIN DUE TO SHARP EDGE.
- [SDR 0601050](https://openairdocs.org/sdr/0601050.md): Skin Panel · delaminated · Jan 6, 2006 · N767TW · Boeing 737230C · Wing, Plate/Skin
  > REPAIRED RIGHT WING TRAILING EDGE LOWER FIXED PANEL DUE TO DELAMINATION.
- [SDR 0601045](https://openairdocs.org/sdr/0601045.md): Floorbeam · corroded · Jan 6, 2006 · N767TW · Boeing 737230C · Fuselage Main, Floor Beam
  > REPAIRED FUSELAGE MAIN CARGO CABIN FLOORBEAM WEB AND REPLACED PRODUCTION DOUBLER DUE TO CORROSION.
- [SDR 0601031](https://openairdocs.org/sdr/0601031.md): Door Frame · cracked · Jan 6, 2006 · N767TW · Boeing 737230C · Galley Doors
  > REPAIRED FUSELAGE FORWARD GALLEY DOOR, UPPER AFT FRAME, DUE TO CRACK.
- [SDR 0601006](https://openairdocs.org/sdr/0601006.md): Frame · dented · Jan 6, 2006 · N767TW · Boeing 737230C · Fuselage Main, Frame
  > FUSELAGE FRAME SECTION REPAIRED DUE TO DENT OUT OF LIMITS.
- [SDR 0601036](https://openairdocs.org/sdr/0601036.md): Skin · dented · Jan 6, 2006 · N767TW · Boeing 737230C · Fuselage Main, Plate/Skin
  > REPAIRED FUSELAGE SKIN SECTION DUE TO DENT OUT OF LIMITS.
- [SDR 0601029](https://openairdocs.org/sdr/0601029.md): Fitting · corroded · Jan 6, 2006 · N767TW · Boeing 737230C · Fuselage Main, Bulkhead
  > REPLACED FUSELAGE BULKHEAD LEFT FITTING DUE TO CORROSION. ALSO REPAIRED FUSELAGE SKIN AND DOUBLER DUE TO CRACK.
- [SDR 0601028](https://openairdocs.org/sdr/0601028.md): Stiffener · corroded · Jan 6, 2006 · N767TW · Boeing 737230C · Fuselage Main, Bulkhead
  > REPAIRED -579 STIFFENER AND PERFORMED BLEND OUT IN THE AFT PRESSURE BULKHEAD "Y" CHORD DUE TO CORROSION. REPAIRED AFT PRESSURE BULKHEAD WEB AND RADIAL STIFFENER AND REPAIRED FUSELAGE SKIN DUE TO ACCESS TO REPAIR AREA.
- [SDR 0601051](https://openairdocs.org/sdr/0601051.md): Spoiler · delaminated · Jan 6, 2006 · N767TW · Boeing 737230C · Spoilers
  > REPAIRED LEFT WING SPOILER #3 DUE TO DELAMINATION.
- [SDR 0601037](https://openairdocs.org/sdr/0601037.md): Bulkhead · cracked · Jan 6, 2006 · N767TW · Boeing 737230C · Fuselage Main, Bulkhead
  > REPAIRED FUSELAGE AFT PRESSURE BULKHEAD WEB DUE TO CRACK.

Next page: https://openairdocs.org/model/boeing-737-230c/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 aircraft_model_key = '737230C'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-737-230c/reports

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