# Service difficulty reports: N320DL, cancelled Oct 30, 2018

A list on [N320DL, cancelled Oct 30, 2018](https://openairdocs.org/deregistered/N320DL-2018-10-30.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 5 · 219 reports

- [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 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 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.
- [SDR NACA2016081100051](https://openairdocs.org/sdr/NACA2016081100051.md): Flap Track · corroded · Aug 11, 2016 · N320DL · Boeing 737232 · Trailing Edge Flaps
  > CORROSION ON THE NR 1 FLAP TRACK AT AFT SPAR ATTACH POINT. REPLACED THE NR 1 FLAP TRACK IAW AMM 27-51-151 REV 122.
- [SDR NACA2016081100050](https://openairdocs.org/sdr/NACA2016081100050.md): Attach Bracket · cracked · Aug 11, 2016 · N320DL · Boeing 737232 · Fuselage Main, Attach Fittings
  > CRACKED LEFT WING TO BODY FAIRING BRACKET BS 540. REPAIRED THE BRACKET IAW SRM REV 112 SECTION 51-20-1 FIG 7.
- [SDR NACA2016081100049](https://openairdocs.org/sdr/NACA2016081100049.md): Frame · cracked · Aug 11, 2016 · N320DL · Boeing 737232 · Fuselage Main, Frame
  > CRACKED FRAME WEB BS 328 BETWEEN STRINGER 20 - 21R. REPAIRED THE FRAME IAW SB 737-53A1323 REV 00.
- [SDR NACA2016081100048](https://openairdocs.org/sdr/NACA2016081100048.md): Bulkhead Web · cracked · Aug 11, 2016 · N320DL · Boeing 737232 · Fuselage Main, Bulkhead
  > AFT PRESSURE DOME CAP AT CENTER ON PRESSURE BULKHEAD CRACKED AT BS 1016, STRINGERS 7 AND 23R. REPAIRED PRESSURE BULKHEAD IAW DRAWING 4-3234689378
- [SDR NACA2016081100047](https://openairdocs.org/sdr/NACA2016081100047.md): Frame · cracked · Aug 11, 2016 · N320DL · Boeing 737232 · Fuselage Main, Frame
  > CRACK INDICATION ON FRAME BS 727, STRINGER 18A LT. REPAIRED THE FRAME IAW SR 3-3621156580.
- [SDR NACA2016081100046](https://openairdocs.org/sdr/NACA2016081100046.md): Attach Bracket · corroded · Aug 11, 2016 · N320DL · Boeing 737232 · Fuselage Main, Attach Fittings
  > CORROSION ON STRINGER 25R, BS 540 STRINGER TO FRAME ATTACH BRACKET. CORROSION FOUND BEYOND LIMITS. ATTACH BRACKET REPLACED IAW SRM 51-25-01 PARA 7, FIG. 3, REV 110.
- [SDR NACA2016081100045](https://openairdocs.org/sdr/NACA2016081100045.md): Angle · cracked · Aug 11, 2016 · N320DL · Boeing 737232 · Fuselage Miscellaneous Structure
  > CRACKED LEFT FUSELAGE TO FUEL TANK ANGLE BS 540, STRINGERS 20 - 21L, IN THE FORWARD CARGO BAY. REPAIRED THE ANGLE IAW DWG 65-45401 REV D AND DWG 65-45767 REV H AND REV D.
- [SDR NACA2016081100044](https://openairdocs.org/sdr/NACA2016081100044.md): Floorbeam · corroded · Aug 11, 2016 · N320DL · Boeing 737232 · Fuselage Main, Floor Beam
  > CORRODED FLOORBEAM AT BS 520 LBL 26 AND RBL26. CHANNEL FOUND TO BE BEYOND ALLOWABLE LIMITS IAW SRM 53-10-1, REV 110. REPLACED THE CHANNEL IAW DWG 65-46803, REV E.
- [SDR NACA2016081100043](https://openairdocs.org/sdr/NACA2016081100043.md): Frame · damaged · Aug 11, 2016 · N320DL · Boeing 737232 · Fuselage Main, Frame
  > DOUBLE DRILLED HOLES IN FRAME AT BS 344 STRINGERS 7 - 14L. REPLACED THE FRAME IAW DWG 65-17685.
- [SDR NACA2016081100042](https://openairdocs.org/sdr/NACA2016081100042.md): Intercostal · cracked · Aug 11, 2016 · N320DL · Boeing 737232 · Fuselage Miscellaneous Structure
  > CRACK IN OUTER CHORD OF INTERCOSTAL BETWEEN STRINGERS 13-14R BS 290. REPLACED IAW SB 737-53A1241 REV 1.
- [SDR NACA2016081100041](https://openairdocs.org/sdr/NACA2016081100041.md): Skin · cracked · Aug 11, 2016 · N320DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > SKIN CRACKED AT RADIO ALTIMETER CUTOUT AT BS 410 BETWEEN STRINGERS 28L AND 28R. SKIN REPAIRED IAW SB 53-1230 FIG.10(A).
- [SDR NACA2016081100040](https://openairdocs.org/sdr/NACA2016081100040.md): Beltframe · corroded · Aug 11, 2016 · N320DL · Boeing 737232 · Fuselage Main, Frame
  > CORROSION ON BELTFRAME BS 1016 BETWEEN STRINGER 20 AND 21L. CORROSION FOUND TO BE BEYOND ALLOWABLE LIMITS IAW SRM 53-10-1, FIGURE 1, SHEET 11, REV 101. REPAIRED IAW SR 3-3612631720.
- [SDR NACA2016081100039](https://openairdocs.org/sdr/NACA2016081100039.md): Stringer Clip · cracked · Aug 11, 2016 · N320DL · Boeing 737232 · Fuselage Main, Attach Fittings
  > CRACKED STRINGER CLIP IN UPPER FUSELAGE BS 663 STRINGER 10R. THE STRINGER CLIP WAS REPLACED IAW SB 53-1268 REV.00.
- [SDR NACA2016081100038](https://openairdocs.org/sdr/NACA2016081100038.md): Floor Support · corroded · Aug 11, 2016 · N320DL · Boeing 737232 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORT BS 986 - 1016 RBL 40 JUST AFT OF R2 DOOR. CORROSION FOUND TO BE BEYOND ALLOWABLE LIMITS. REPLACED IAW SRM REV.110 53-10-2, ITEM 62.
- [SDR NACA2016081100037](https://openairdocs.org/sdr/NACA2016081100037.md): Keelbeam · corroded · Aug 11, 2016 · N320DL · Boeing 737232 · Fuselage Main, Keel
  > CORROSION ON LEFT KEEL BEAM AND ADJOINING STRUCTURE BETWEEN BS 616 TO 639. REPAIRED AT C CHECK. REPAIRED LT KEEL BEAM AND ADJOINING STRUCTURE BETWEEN STA 616 TO 639 DWG R23092.1-053-016-001 REV B.
- [SDR NACA2016081100036](https://openairdocs.org/sdr/NACA2016081100036.md): Keelbeam · corroded · Aug 11, 2016 · N320DL · Boeing 737232 · Fuselage Main, Keel
  > CORROSION ON RIGHT KEEL BEAM AND ADJOINING STRUCTURE BETWEEN BS 598 TO 578. REPAIRED AT C CHECK. REPAIRED RT KEELBEAM AND ADJOINING STRUCTURE BETWEEN 598 TO 578 IAW DWG R23092.1-053-013-001 REV A.
- [SDR NACA2016081100035](https://openairdocs.org/sdr/NACA2016081100035.md): Stringer Clip · cracked · Aug 11, 2016 · N320DL · Boeing 737232 · Fuselage Main, Attach Fittings
  > CRACK ON STRINGER CLIP BS 348.2, STRINGER 15L ATTACHED TO L1 DOOR FUSELAGE FRAME. REPLACED THE THE STRINGER CLIP IAW DWG 65-17685, AND SRM 51-30-2 REV 110.
- [SDR NACA2016081100034](https://openairdocs.org/sdr/NACA2016081100034.md): Stringer Clip · cracked · Aug 11, 2016 · N320DL · Boeing 737232 · Fuselage Main, Attach Fittings
  > CRACKED STRINGER CLIP BS277, STRINGER 15R. THE STRINGER CLIP WAS REPLACED IAW DWG 65-45805 REV K.
- [SDR NACA2016081100033](https://openairdocs.org/sdr/NACA2016081100033.md): Floorbeam · corroded · Aug 11, 2016 · N320DL · Boeing 737232 · Fuselage Main, Floor Beam
  > CORROSION ON UPPER AFT FLOORBEAM BS 480 BETWEEN RBL 24-45. REPAIRED THE FLOORBEAM IAW SRM REV 110, AND 53-10-9 FIG 7.
- [SDR NACA2016081100032](https://openairdocs.org/sdr/NACA2016081100032.md): Beltframe · cracked · Aug 11, 2016 · N320DL · Boeing 737232 · Fuselage Main, Frame
  > CRACK ON BELT FRAME BS 291 STRINGER 14R JUST FORWARD OF R1 DOOR. REPLACED BELTFRAME IAW DRAWING 65-45807 ID 0002 REV K.
- [SDR NACA2016081100031](https://openairdocs.org/sdr/NACA2016081100031.md): Floorbeam · corroded · Aug 11, 2016 · N320DL · Boeing 737232 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM UPPER FLANGE LOWER BS 480 LBL 21. FLOORBEAM REPAIRED IAW SRM 53-10-9 FIG.7, REV 110.
- [SDR NACA2016081100030](https://openairdocs.org/sdr/NACA2016081100030.md): Floorbeam · corroded · Aug 11, 2016 · N320DL · Boeing 737232 · Fuselage Main, Floor Beam
  > CORROSION ON LOWER FWD FLOORBEAM BS 500B LBL 23-20. FLOORBEAM REPLAIRED IAW SRM 53-10-09, REV 110.
- [SDR NACA2016081100029](https://openairdocs.org/sdr/NACA2016081100029.md): Stiffener · cracked · Aug 11, 2016 · N320DL · Boeing 737232 · Fuselage Main, Bulkhead
  > STIFFENER FLANGES ON AFT PRESSURE BULKHEAD DOME CAP CRACKED AT BS 1016 STRINGER 1, 8L, & 6R. REPAIRED THE STIFFENER IAW SERVICE REQUEST 4-3234689378, SERVICE BULLETIN 737-53A1214.
- [SDR NACA2016081100028](https://openairdocs.org/sdr/NACA2016081100028.md): Stringer Clip · cracked · Aug 11, 2016 · N320DL · Boeing 737232 · Fuselage Main, Attach Fittings
  > CRACKED STRINGER CLIP AT BS 616 STRINGER 5L. THE STRINGER CLIP WAS REPLACED IAW SB737-53-1268 REV 00.

Next page: https://openairdocs.org/deregistered/N320DL-2018-10-30/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 = 'N320DL' AND deregistration_id = 'N320DL-2018-10-30'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N320DL-2018-10-30/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.