# Service difficulty reports: Boeing 737-232

A list on [Boeing 737-232](https://openairdocs.org/model/boeing-737-232.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 34 · 1,700 reports

- [SDR ABXR2019071900294](https://openairdocs.org/sdr/ABXR2019071900294.md): Skin · corroded · Jul 19, 2019 · N316CM · Boeing 737232 · Wing, Plate/Skin
  > CORRODED
- [SDR NACA2019021200027](https://openairdocs.org/sdr/NACA2019021200027.md): Tee Fitting · cracked · Feb 4, 2019 · N321DL · Boeing 737232 · Nose/Tail Landing Gear
  > NOSE LANDING GEAR - CRACKS FOUND ON SUPPORT STRUCTURE FOR ACTUATOR ATTACH FITTING. REMOVED AND REPLACED TEE ANGLE PN: 65-45819-45 AND GUSSET 65-45819-45, REF BOEING DRAWING 65-45819 AND B737-200 SRM 51-10-1, 51-30-2, 3 AND 5. NDT OPEN HOLES REF NDT MANUAL PAR
- [SDR NACA2018082800067](https://openairdocs.org/sdr/NACA2018082800067.md): Skin · cracked · Aug 27, 2018 · N320DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN WAS CRACKED, BS 468, STRINGER 16R. A REPAIR WAS INSTALLED IAW SRM 53-30-03, FIG 48, DETAIL XI, PROCEDURE VII.
- [SDR NACA2018080600066](https://openairdocs.org/sdr/NACA2018080600066.md): Skin · cracked · Aug 6, 2018 · N321DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CRACKED AT STRINGER 16R JUST AFT OF BS 480. A DOUBLER AND TRIPLER WAS INSTALLED IAW SRM, 53-30-03, REPAIR 48, DETAIL VII.
- [SDR NACA2018071800002](https://openairdocs.org/sdr/NACA2018071800002.md): Skin · cracked · Jul 16, 2018 · N321DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > 3 INCH LONG CRACK FOUND IN FUSELAGE SKIN DIRECTLY BELOW S23R AT BS 344. CAT B REPAIR INSTALLED IAW SRM 53-30-3, FIGURE 48, DETAIL XVIII.
- [SDR NACA2018031400001](https://openairdocs.org/sdr/NACA2018031400001.md): Skin · cracked · Mar 12, 2018 · N321DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > SKIN CRACK FOUND ON RIGHT SIDE FUSELAGE S16R AND BS445 (VERIFIED WITH HFEC). DAMAGE REMOVED, DOUBLER INSTALLED REF SRM 53-30-3, FIG 48, REV SEP 2016. DETAIL XI AND III, PROCEDURE VII.
- [SDR NACA2017080900045](https://openairdocs.org/sdr/NACA2017080900045.md): Pump · weak · Aug 9, 2017 · N320DL · Boeing 737232 · Hydraulic Pump (Electric/Engine), Main
  > NR 2 ENGINE HYDRAULIC PUMP LOW PRESSURE LIGHT ILLUMINATED. RAN ENGINES, NO FAULTS. CLEANED SUMP TUBE AND DRAINED WATER. CHECKED RESERVOIR PRESSURE FILTER BOWL AND REMOVED WATER. CHECKED CASE DRAIN FILTERS FOR BOTH ENGINES. NO METAL FOUND IAW AMM 29-11-00,
- [SDR NACA2017072000044](https://openairdocs.org/sdr/NACA2017072000044.md): Engine · failed · Jul 18, 2017 · N321DL · Boeing 737232 · Engine (Turbine/Turboprop)
  > NR 2 ENGINE FAILED AT 2000 FEET ON TAKEOFF. MI AT 1705 FEET DURING CLIMB, LOUD NOISE FROM NR 2 ENGINE, NO EPR, SMOKE IN COCKPIT, AND ENGINE VIBRATION. NR 2 ENGINE HAD A FAILURE OF MULTIPLE STAGES OF THE TURBINE SECTION. THE ENGINE AND THRUST REVERSER WERE REM
- [SDR NACA2017022700018](https://openairdocs.org/sdr/NACA2017022700018.md): Floorbeam · corroded · Feb 26, 2017 · N321DL · Boeing 737232 · Fuselage Main, Floor Beam
  > CORROSION ON TOP SURFACE OF FLOORBEAM AT BS 827 LBL 49 - 56. CORROSION BLENDED OUT OF LIMITS IAW SRM 53-10-1, FIG 1, REV 113. REPAIRED THE FLOORBEAM IAW DWG R23093.1-053-023-001, REV NC.
- [SDR NACA2017022700016](https://openairdocs.org/sdr/NACA2017022700016.md): Frame · cracked · Feb 26, 2017 · N321DL · Boeing 737232 · Fuselage Main, Frame
  > CRACKED FRAME AT BS 787, RBL42, STRINGER 13R. REPAIRED IAW SR 4-3658265861, & 8100-9.
- [SDR NACA2017022700012](https://openairdocs.org/sdr/NACA2017022700012.md): Fitting · corroded · Feb 26, 2017 · N321DL · Boeing 737232 · Trailing Edge Flaps
  > RIGHT OUTBOARD FLAP, NR 7 CARRIAGE SUPPORT FITTING CORRODED ON THRUST BEARING SURFACE (IN MID FLAP). REPLACED WITH REPAIRED ASSY.
- [SDR NACA2017022700011](https://openairdocs.org/sdr/NACA2017022700011.md): Spindle · corroded · Feb 26, 2017 · N321DL · Boeing 737232 · Trailing Edge Flaps
  > LEFT OUTBOARD FLAP, NR 1 CARRIAGE SPINDLE CORRODED. THE CARRIAGE WAS REPLACED IAW MM 27-51-81, REV 123.
- [SDR NACA2017022700009](https://openairdocs.org/sdr/NACA2017022700009.md): Flap Track · damaged · Feb 26, 2017 · N321DL · Boeing 737232 · Trailing Edge Flaps
  > RIGHT INBOARD FLAP OUTBOARD TRACK REPAIR BUSHING CAD PLATING DETERIORATED. FLAP TRACK REPLACED IAW AMM 27-51-161, REV 12.
- [SDR NACA2017022700007](https://openairdocs.org/sdr/NACA2017022700007.md): Bulkhead Web · cracked · Feb 26, 2017 · N321DL · Boeing 737232 · Fuselage Main, Bulkhead
  > CRACKED RIVETS ON BS 1016 BULKHEAD WEB BETWEEN STRINGERS 5 - 7L. REPAIRED IAW SRM 113 53-10-4, FIGURE 15.
- [SDR NACA2017022700005](https://openairdocs.org/sdr/NACA2017022700005.md): Intercostal · cracked · Feb 26, 2017 · N321DL · Boeing 737232 · Fuselage Miscellaneous Structure
  > CRACK IN RADIUS OF INTERCOSTAL AT BS 294.5, STRINGER 14R. REPLACED THE INTERCOSTAL IAW SERVICE BULLETIN 737-53A1241 REV 1.
- [SDR NACA2017022700019](https://openairdocs.org/sdr/NACA2017022700019.md): Support Fitting · cracked · Feb 26, 2017 · N321DL · Boeing 737232 · Wing, Landing Gear Attach Fittings
  > CRACK FOUND IN RIGHT AFT SUPPORT FITTING FOR MAIN LANDING GEAR AT RSS 224. REPLACED THE SUPPORT FITTING IAW SERVICE BULLETIN 737-57-1216, REV 2, & SR 4-3648350626, AND 8100-9.
- [SDR NACA2017022700017](https://openairdocs.org/sdr/NACA2017022700017.md): Angle · cracked · Feb 26, 2017 · N321DL · Boeing 737232 · Fuselage Miscellaneous Structure
  > ANGLE CRACKED AT BS 663, LBL 24.82. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW DWG PL65-45410 REV DD, BSB 737-57A1296, SRM D6-15565 REV 113, AND 51-30-02.
- [SDR NACA2017022700015](https://openairdocs.org/sdr/NACA2017022700015.md): Stringer Clip · cracked · Feb 26, 2017 · N321DL · Boeing 737232 · Fuselage Main, Attach Fittings
  > CRACKED STRINGER CLIP BS 663, STRINGER 10R, REPLACED THE STRINGER CLIP IAW SRM 51-30-2, REV 113.
- [SDR NACA2017022700014](https://openairdocs.org/sdr/NACA2017022700014.md): Stringer Clip · cracked · Feb 26, 2017 · N321DL · Boeing 737232 · Fuselage Main, Attach Fittings
  > CRACKED STRINGER CLIP BS 663, STRINGER 10L, WL 256. REPLACED THE STRINGER CLIP IAW SRM 51-30-2 REV 113, & DWG 65-46541 REV H.
- [SDR NACA2017022700013](https://openairdocs.org/sdr/NACA2017022700013.md): Attach Fitting · corroded · Feb 26, 2017 · N321DL · Boeing 737232 · Wing, Control Surface Attach Fittings
  > RIGHT OUTBOARD FLAP, NR 8 TRACK FORWARD ATTACH FITTING (ON WING) HAS EVIDENCE OF CORROSION BETWEEN TRACK ATTACH BUSHINGS. REPLACED THE FWD ATTACH FITTING IAW BAC5047, AMM 20-50-11 REV 123, & DWG 65-45455 REV E.
- [SDR NACA2017022700010](https://openairdocs.org/sdr/NACA2017022700010.md): Flap Track · corroded · Feb 26, 2017 · N321DL · Boeing 737232 · Trailing Edge Flaps
  > LEFT OUTBOARD FLAP NR 1 TRACK CORRODED. REPLACED THE FLAP TRACK IAW AMM 27-51-151, REV 123.
- [SDR NACA2017022700008](https://openairdocs.org/sdr/NACA2017022700008.md): Bulkhead Web · cracked · Feb 26, 2017 · N321DL · Boeing 737232 · Fuselage Main, Bulkhead
  > ONE CRACK ON BS 1016 BULKHEAD WEB AT STRINGER 15R. REPAIREDTHE BULKHEAD WEB IAW SR 4-3633491853, & 8100-9.
- [SDR NACA2017022700006](https://openairdocs.org/sdr/NACA2017022700006.md): Intercostal · cracked · Feb 26, 2017 · N321DL · Boeing 737232 · Fuselage Miscellaneous Structure
  > CRACK IN RADIUS OF INTERCOSTAL BS 277 STRINGER 10R FORWARD OF R1 DOOR. REPLACED INTERCOSTAL ANGLE IAW SERVICE BULLETIN-737-53A1241 REV 1.
- [SDR NACA2017022700003](https://openairdocs.org/sdr/NACA2017022700003.md): Stringer Clip · cracked · Feb 26, 2017 · N321DL · Boeing 737232 · Fuselage Main, Attach Fittings
  > CRACKED STRINGER CLIP AT BS 967, STRINGER 22L. REPLACED IAW SRM 51-30-2 REV 113 AND DWG 65-46563 REV -.
- [SDR NACA2017022700002](https://openairdocs.org/sdr/NACA2017022700002.md): Tee Fitting · cracked · Feb 26, 2017 · N321DL · Boeing 737232 · Fuselage Main, Attach Fittings
  > CRACKED TEE ON FORWARD CARGO DOOR INTERNAL STRUCTURE AT BS 470. THE TEE WAS REPLACED IAW DWG 65-46921 REV M, AND SRM D6-15565 REV 113 51-30-02.
- [SDR NACA2017010300001](https://openairdocs.org/sdr/NACA2017010300001.md): Skin · cracked · Jan 1, 2017 · N322DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > A SKIN CRACK WAS FOUND AT BS727B, S19R WHILE PERFORMING THE AD 2005-13-30 ZONE 1 INSPECTION. THERE WAS AN EXISTING REPAIR IN THE AREA THAT HAD TO BE INCORPORATED; THE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3, FIGURE 48, DETAIL IX.
- [SDR NACA2016111400077](https://openairdocs.org/sdr/NACA2016111400077.md): Skin · cracked · Nov 13, 2016 · N320DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CRACKED AT BS 760, STRINGER 18L. REPAIRED IAW SRM 53-30-3, FIGURE 48, DETAIL X.
- [SDR NACA2016110900076](https://openairdocs.org/sdr/NACA2016110900076.md): Structure · cracked · Oct 2, 2016 · N320DL · Boeing 737232 · Fuselage Miscellaneous Structure
  > COMPRESSION CHORD AT BS 663.75 IN CABIN CRACKED BL0. COMPRESSION CHORD @ BS 663.75 IN CABIN @ BL 0 REPAIRED IAW AERONAUTICAL ENGINEERS INC # EO 2933
- [SDR NACA2016110900075](https://openairdocs.org/sdr/NACA2016110900075.md): Floor Support · cracked · Oct 2, 2016 · N320DL · Boeing 737232 · Fuselage Main, Floor Beam
  > FLOOR SUPPORT CRACKED AT BS 663, BL0. REPAIRED THE FLOOR SUPPORT IAW EO 2933 REV A.
- [SDR NACA2016110100073](https://openairdocs.org/sdr/NACA2016110100073.md): Skin · corroded · Oct 2, 2016 · N320DL · Boeing 737232 · Wing, Plate/Skin
  > CORROSION ON RIGHT HAND WING LOWER SURFACE AT WS 475 AFT SPAR. CORROSION ON RT WING LOWER SURFACE AT WS 500-510 REMOVED/BLENDED AND AREA REPAIRED IAW SERVICE REQUEST NUMBER 4-3237034623. RII COMPLETED.
- [SDR NACA2016110100072](https://openairdocs.org/sdr/NACA2016110100072.md): Skin · corroded · Oct 2, 2016 · N320DL · Boeing 737232 · Wing, Plate/Skin
  > CORROSION ON RIGHT HAND WING LOWER SURFACE AT WS 521 - WS552 AFT SPAR. CORROSION ON RT WING LOWER SURFACE AT WS 521-552 AT AFT SPAR REMOVED/BLENDED AND REPAIRED IAW SERVICE REQUEST NR 4-3237034632 REF NRC 15104120 FOR DOCUMENTATION. RII COMPLETED.
- [SDR NACA2016100200071](https://openairdocs.org/sdr/NACA2016100200071.md): Drag Angle · cracked · Oct 2, 2016 · N320DL · Boeing 737232 · Fuselage Miscellaneous Structure
  > CRACKED ANGLED STRAP BS 520 - BS 560 S23L UNDER WING TO BODY FAIRING. REPLACED CRACKED DRAG ANGLE AT STA 520 - 560 STR 23L UNDER WING TO BODY FAIRING IAW 2298 REV K & DWG R23092.1-053-021-001 REV NC.
- [SDR NACA2016081100070](https://openairdocs.org/sdr/NACA2016081100070.md): Frame · cracked · Aug 11, 2016 · N320DL · Boeing 737232 · Fuselage Main, Frame
  > CRACK FOUND ON INSULATION BLANKET STUD HOLE AT BS 360, STRINGERS 19 - 20R. REPAIRED THE FRAME IAW ST 4-3262647741..
- [SDR NACA2016081100069](https://openairdocs.org/sdr/NACA2016081100069.md): Door Sill · cracked · Aug 11, 2016 · N320DL · Boeing 737232 · Fuselage Miscellaneous Structure
  > R1 DOOR SILL CRACKED AT BS 291 - 297 RBL 60 STRINGER 17R. REPLACED THE DOOR SILL IAW DWG 141A8310-0007 REV.
- [SDR NACA2016081100068](https://openairdocs.org/sdr/NACA2016081100068.md): Frame · cracked · Aug 11, 2016 · N320DL · Boeing 737232 · Fuselage Main, Frame
  > COMPRESSION FRAME AT BS 663.75 IN CABIN CRACKED AT LBL 25 AND RBL 35. REPAIRED COMPRESSION CHORD AT BS 663.75 IN CABIN AT LBL 25 AND RBL 35 IAW SB B737-53-1184 MARCH 21, 1996.
- [SDR NACA2016081100067](https://openairdocs.org/sdr/NACA2016081100067.md): Stringer · corroded · Aug 11, 2016 · N320DL · Boeing 737232 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON STRINGER 26L, BS 1006. CORROSION FOUND TO BE BEYOND LIMITS IAW SRM 53-10-1 REV 110. REPAIRED THE STRINGER IAW SRM 53-10-3 FIG 1, REV 110.
- [SDR NACA2016081100066](https://openairdocs.org/sdr/NACA2016081100066.md): Frame · corroded · Aug 11, 2016 · N320DL · Boeing 737232 · Fuselage Main, Frame
  > CORROSION FOUND ON FRAME BS 927 BETWEEN STRINGER 26 & 27R. CORROSION IS BEYOND LIMITS IAW SRM 53-10-01, REV 110. REPAIRED IAW SRM 53-10-4 FIG 10, REV 110.
- [SDR NACA2016081100065](https://openairdocs.org/sdr/NACA2016081100065.md): Frame · corroded · Aug 11, 2016 · N320DL · Boeing 737232 · Fuselage Main, Frame
  > CORROSION FOUND ON FRAME BS 947 BETWEEN S27L & 27R. CORROSION FOUND BEYOND LIMITS IAW SRM 53-10-01, REV 110. REPAIRED IAW SRM 53-10-4 FIG 10, REV 110.
- [SDR NACA2016081100064](https://openairdocs.org/sdr/NACA2016081100064.md): Beltframe · corroded · Aug 11, 2016 · N320DL · Boeing 737232 · Fuselage Main, Frame
  > CORROSION ON BELTFRAME BS 360 S27 - 28R AFT OF E&E BAY DOOR CUT OUT. REPAIRED IAW SRM 53-10-4, REV 110.
- [SDR NACA2016081100063](https://openairdocs.org/sdr/NACA2016081100063.md): Beltframe · cracked · Aug 11, 2016 · N320DL · Boeing 737232 · Fuselage Main, Frame
  > CRACK IN BELTFRAME LOWER FLANGE BS 917 S21R. REPAIRED IAW SRM 53-10-4 FIGURE 10, REPAIR 1, REV 110.
- [SDR NACA2016081100062](https://openairdocs.org/sdr/NACA2016081100062.md): Bulkhead Web · cracked · Aug 11, 2016 · N320DL · Boeing 737232 · Fuselage Main, Bulkhead
  > FORWARD BS 178 PRESSURE BULKHEAD VERTICAL BEAM WEB CRACKED AT TOOLING HOLE AT WL 190 AND RBL 17. REPAIRED THE BULKHEAD WEB IAW SRM 53-10-11 FIG 11 REV 110..
- [SDR NACA2016081100061](https://openairdocs.org/sdr/NACA2016081100061.md): Floorbeam · cracked · Aug 11, 2016 · N320DL · Boeing 737232 · Fuselage Main, Floor Beam
  > FLOORBEAM WEB CRACKED AT BS 663 LBL 24.82. REPAIRED THE FLOORBEAM. REPAIRED IAW SERVICE REQUEST 3-363025-4704.
- [SDR NACA2016081100060](https://openairdocs.org/sdr/NACA2016081100060.md): Floorbeam · cracked · Aug 11, 2016 · N320DL · Boeing 737232 · Fuselage Main, Floor Beam
  > FLOORBEAM WEB CRACKED AT BS 663 RBL 24.82 LOWER CHORD. REPAIRED THE FLOORBEAM IAW SERVICE REQUEST 3-363254704.
- [SDR NACA2016081100059](https://openairdocs.org/sdr/NACA2016081100059.md): Doubler · corroded · Aug 11, 2016 · N320DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > CORRODED INTERNAL DOUBLER BETWEEN STA 967 TO 996 STR 25L. REPLACED WITH MADE REPAIR PART AND MAT IDENTIFIED IAW 65-45776 REV ER. DOUBLER INSTALLED WITH NEW SKIN REF NRC 1493466 AND NRC 1493379. RII COMPLETED.
- [SDR NACA2016081100058](https://openairdocs.org/sdr/NACA2016081100058.md): Shear Web · corroded · Aug 11, 2016 · N320DL · Boeing 737232 · Fuselage Miscellaneous Structure
  > CORROSION ON LEFT SHEAR WEB BS 711 TO 727 STRINGER 18A LT. REPAIRED THE SHEAR WEB.
- [SDR NACA2016081100057](https://openairdocs.org/sdr/NACA2016081100057.md): Skin · cracked · Aug 11, 2016 · N320DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > CRACKED FASTENER HOLES AT STA 303 JUST BELOW STR 13L AND AT STR 10L, UPPER AND LOWER DOOR HINGE CUT OUTS REPAIRED IAW SR 3-3626171693. RII COMPLETED.
- [SDR NACA2016081100056](https://openairdocs.org/sdr/NACA2016081100056.md): Skin · cracked · Aug 11, 2016 · N320DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > SKIN FOUND CRACKED DURING NDT, BS 291 JUST ABOVE STRINGER 10R. REPAIRED IAW BOEING SR 3-3628117058.
- [SDR NACA2016081100055](https://openairdocs.org/sdr/NACA2016081100055.md): Skin · corroded · Aug 11, 2016 · N320DL · Boeing 737232 · Horizontal Stabilizer, Plate/Skin
  > CORROSION ON TOP OF RT HORIZONTAL STAB BEAM AT ELEVATOR STA 149.12. FOUND TO BE BEYOND ALLOWABLE LIMITS IAW SRM REV 110 55-10-01 FIGURE 1. REPAIRED IAW SRM REV 110 55-10-7 FIGURE 1.
- [SDR NACA2016081100053](https://openairdocs.org/sdr/NACA2016081100053.md): Skin · cracked · Aug 11, 2016 · N320DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > SKIN CRACKED BS 259.5 STRINGER 22L. REPAIRED IAW SRM 53-30-3 FIG. 49 DETAIL V REV 101.
- [SDR NACA2016081100052](https://openairdocs.org/sdr/NACA2016081100052.md): Flap Track · corroded · Aug 11, 2016 · N320DL · Boeing 737232 · Trailing Edge Flaps
  > CORROSION ON NR 2 FLAP TRACK AT AFT SPAR ATTACH POINT. THE FLAP TRACK WAS REPLACED IAW AMM 27-51-151 REV. 122.

Next page: https://openairdocs.org/model/boeing-737-232/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 = '737232'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-737-232/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.