# Service difficulty reports: N3159G

A list on [N3159G](https://openairdocs.org/aircraft/N3159G.md).

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

- [SDR NACA2026061300001](https://openairdocs.org/sdr/NACA2026061300001.md): Stringer · damaged · Jun 13, 2026 · N3159G · Boeing 737852 · Fuselage Main, Longeron/Stringer
  > AIRCRAFT SKIN DAMAGE UNDER CARGO DOOR DURING LOADING. STRINGER DAMAGED AT STR 17L, BS 445. REPAIRED DAMAGE BY INSTALLING DOUBLER REF AWATS EO 26-737-53-386 CLASSIFICATION MAJOR REPAIR.
- [SDR NACA2026021100001](https://openairdocs.org/sdr/NACA2026021100001.md): Brake Assy · faulted · Feb 11, 2026 · N3159G · Boeing 737852 · Landing Gear Brake System
  > NUMBER 4 BRAKE COOL TO THE TOUCH, REQUIRES EXCESSIVE PRESSURE TO STOP. BLED NR 4 BRAKE IAW AMM 32-41-00, OPS & LEAK CHECKED GOOD.
- [SDR NACA2026021000001](https://openairdocs.org/sdr/NACA2026021000001.md): Brake Fuse · faulted · Feb 10, 2026 · N3159G · Boeing 737852 · Landing Gear Brake System
  > AFTER LANDING IN PANC WITH AUTOBRAKE AT 3, NR 1 BRAKE COOL TO TOUCH. RESET NR 1 BRAKE HYDRAULIC FUSE & BLED NR 1 MLG BRAKE SYSTEM IAW AMM 32-41-00. GROUND TESTED NORMAL
- [SDR NACA2026020900001](https://openairdocs.org/sdr/NACA2026020900001.md): Brake Fuse · no test · Feb 9, 2026 · N3159G · Boeing 737852 · Landing Gear Brake System
  > EXCESSIVE BRAKE PRESSURE NEEDED TO SLOW ACFT, LT BRAKE APPEARS COOL TO THE TOUCH. BRAKE FUSE FAILED TEST IAW AMM 32-41-00-870-802. R & R NR 1 BRAKE FUSE IAW AMM 32-41-72, LEAK & OPS CHKD GOOD.
- [SDR NACA2026021000002](https://openairdocs.org/sdr/NACA2026021000002.md): Fuse · no test · Feb 6, 2026 · N3159G · Boeing 737852 · Landing Gear Brake System
  > AFTER A HIGH SPEED TAXI RUN AND MAX MANUAL BRAKES, THE NR 4 BRAKE IS COLD WHILE ALL OTHER BRAKES ARE VERY HOT. PERFORMED FUNCTIONAL TEST OF NR 4 BRAKE FUSE, OPS CHECK FAILED. IAW AMM TASK 32-41-00-870-804, REPLACED NR 4 BRAKE FUSE, OPS CHECKED GOOD.
- [SDR NACA202602100001](https://openairdocs.org/sdr/NACA202602100001.md): Brake Assy · weak · Feb 6, 2026 · N3159G · Boeing 737852 · Landing Gear Brake System
  > EXCESSIVE BRAKES NEEDED TO STOP AIRPLANE, UPON WALK AROUND FOUND RIGHT OUTBOARD MAIN BRAKE TO BE COLD TO THE TOUCH. PERFORMED MANUAL SYS B HYD BRAKE FUSE TEST, ALL 4 BRAKES FROM TEST PASS, REF AMM 32-41-00-870-804. BLED BRAKES, OPS CHECK GOOD REF AMM 32-41-00
- [SDR NACA2026020200001](https://openairdocs.org/sdr/NACA2026020200001.md): Brake Assy · faulted · Feb 2, 2026 · N3159G · Boeing 737852 · Landing Gear Brake System
  > EXCESSIVE BRAKE PRESSURE NEEDED TO SLOW AIRCRAFT. MX FOUND INBOARD BRAKES HOT, OUTBOARD BRAKES COLD AND OUTBOARD BRAKES WOULD NOT FUNCTION WHEN PUMPED. RESET ALL FOUR BRAKE FUSES AND 2 ALTERNATE FUSES, ALL BRAKES OPS CHECKED GOOD REF B737-800 32-41-00-870-802
- [SDR EE4Y2025092923243](https://openairdocs.org/sdr/EE4Y2025092923243.md): Frame · cracked · Sep 29, 2025 · N3159G · Boeing 737852 · Fuselage Main, Frame
  > DURING THE ACCOMPLISHMENT OF EO737-53-0388_P1 WAS FOUND IN THE LOWER FUSELAGE RH STA 727 FRAME INNER CHORD AND S-18A WEB AT LOWER OPEN FASTENERS HOLE WITH CRACK INDICATION. DUE TO IT, THE PART WAS REPLACED IAW NAC ENGINEERING ORDER #737-53-0403 REV. IR. UNDERJ
- [SDR EE4Y2025090423050](https://openairdocs.org/sdr/EE4Y2025090423050.md): Rib · worn · Sep 4, 2025 · N3159G · Boeing 737852 · Nacelle/Pylon, Main Frame
  > ENGINE #1 PYLON ACCESS PANEL 431CL O/B SUPPORT STRUCTURE WITH WEAR, THE RIB ASSY P/N: 116A5502-5 AND P/N: 116A5502-6 MUST BE FABRICATED PER THE APPLICABLE DWG116A5502 INSTRUCTIONS AND BCS COO-COO-25-0019-01B SMAL REQUESTED. HOWEVER, COOPESA DO NOTHAVE THE CAPA
- [SDR EE4Y2025090423049](https://openairdocs.org/sdr/EE4Y2025090423049.md): Rib · worn · Sep 4, 2025 · N3159G · Boeing 737852 · Nacelle/Pylon, Main Frame
  > RIB ASSY P/N: 116A5502-5 AND P/N: 116A5502-6 MUST BE FABRICATED PER THE APPLICABLE DWG 116A5502 INSTRUCTIONS AND BCS COO-COO-25-0019-01B SMAL REQUESTED. HOWEVER, COOPESA DO NOT HAVE THE CAPABILITIES TO COMPLY WITH THE CONVERSION COATING APPLICATION BY IMMERSIO
- [SDR EE4Y2025090423046](https://openairdocs.org/sdr/EE4Y2025090423046.md): Fan Cowl · damaged · Sep 4, 2025 · N3159G · Boeing 737852 · Nacelle/Pylon, Main Frame
  > DURING THE ACCOMPLISHMENT OF 737-70-812-02_P1-OP-UP-ENG NAC TASK CARD, IT WAS FOUND THE ENGINE #2, O/B FAN COWL P/N: 314-2200-18 BR, S/N: 9112001, WITH ELONGATED HOLES (2EA). COLLINS WAS CONTACTED ASKING FOR REPAIR INSTRUCTIONS AND FINAL APPROVAL. THE CONDITIO
- [SDR EE4Y2025090423045](https://openairdocs.org/sdr/EE4Y2025090423045.md): Door Sill · cracked · Sep 4, 2025 · N3159G · Boeing 737852 · Fuselage Main, Structure
  > DURING THE ACCOMPLISHMENT OF 737-53-360-00-01_P1-OP-UP-UF/001 NAC TASK CARD, WAS FOUND IN THE UPPER FUSELAGE FWD ENTRY DOOR, AT STA 303.9 LBL 55, WL208, LOWER SILL INNER CHORD WITH CRACK. THIS CONDITION WAS REPAIRED DUE TO CRACK IAW B737-800 SRM 53-10-15 REPAI
- [SDR EE4Y202509023040](https://openairdocs.org/sdr/EE4Y202509023040.md): Cargo Track · cracked · Sep 4, 2025 · N3159G · Boeing 737852 · Fuselage, Seat/Cargo Attach Fittings
  > DURING THE ACCOMPLISHMENT OF 737-53-250-00_P1-OP-UP-LF/001 NAC TASK CARD WAS FOUND AT AFT CARGO C/C TRACK WITH CRACKS, LOCATED AT STA 727C, STA 727G, STA 727J AND STA 767, LBL 17.24. THE CONDITION REPORTED WAS REPLACED THE TRACK AT LBL 17.24 FROM STA 727+4" TO
- [SDR EE4Y202509023039](https://openairdocs.org/sdr/EE4Y202509023039.md): Angle · cracked · Sep 4, 2025 · N3159G · Boeing 737852 · Fuselage Miscellaneous Structure
  > DURING THE ACCOMPLISHMENT OF 737-26-550-02_P1-VISUAL-INSP-LF/003 NAC TASK CARD, WAS FOUND IN THE BULKHEAD STA 663 AT RBL 7.25, WING CENTER SECTION LOWER REAR SPAR VAPOR BARRIER ATTACH ANGLE WITH CRACK. THE CONDITION REPORTED WAS REPAIRED AT STA 663 BTWN RBL 6
- [SDR EE4Y202509023037](https://openairdocs.org/sdr/EE4Y202509023037.md): Web · cracked · Sep 4, 2025 · N3159G · Boeing 737852 · Fuselage Miscellaneous Structure
  > DURING THE ACCOMPLISHMENT OF 737-26-550-02_P1-VISUAL-INSP-LF/002 NAC TASK CARD, WAS FOUND IN THE LOWER FUSELAGE L/H SIDE, CENTER WING REAR SPAR VAPOR BARRIER WEB WITH CRACKS, AT STA 663, BTWN LBL 15.54 AND LBL 54.21. THE CONDITION REPORTED WAS REPAIRED I//A/W
- [SDR EE4Y2025090423036](https://openairdocs.org/sdr/EE4Y2025090423036.md): Web · cracked · Sep 4, 2025 · N3159G · Boeing 737852 · Fuselage Miscellaneous Structure
  > DURING THE ACCOMPLISHMENT OF 737-26-550-02_P1-VISUAL-INSP-LF/001 NAC TASK CARD, WAS FOUND IN THE LOWER FUSELAGE R/H SIDE, CENTER WING REAR SPAR VAPOR BARRIER WEB WITH CRACKS, AT STA 663, BTWN RBL 31.83 AND RBL54.21. THE CONDITION REPORTED WAS REPAIRED I//A/W B
- [SDR EE4Y2025090323032](https://openairdocs.org/sdr/EE4Y2025090323032.md): Seat Track · worn · Sep 3, 2025 · N3159G · Boeing 737852 · Fuselage, Seat/Cargo Attach Fittings
  > REPAIRED SEAT TRACK SECTION AT MAIN CARGO CABIN LBL 45.5 BETWEEN STA 689 AND STA 703.5 DUE TO WEAR I/A/W B737-800 SRM 53-00-52 REPAIR 3 PARAGRAPH 4 FIGURE 202 DETAIL A. CATEGORY A REPAIR. REV 85 DATED 07-10-2025. UNDER JOB A1Q187 NRI 2-45
- [SDR EE4Y2025090323031](https://openairdocs.org/sdr/EE4Y2025090323031.md): Seat Track · worn · Sep 3, 2025 · N3159G · Boeing 737852 · Fuselage, Seat/Cargo Attach Fittings
  > DURING THE ACCOMPLISHMENT OF 737-AE-53-837_P1-OP-UP NAC TASK CARD, THERE WERE FOUND TWOSEAT TRACK CROWN AREAS DAMAGED, ONE CRACKED AT STA 520 LBL 24.75, AND THE OTHER ONE WITHWEAR AT STA 520 LBL 45.50. SINCE THE MENTIONED SEAT TRACK AREAS ARE AFFECTED BY AEI C
- [SDR EE4Y2025090323030](https://openairdocs.org/sdr/EE4Y2025090323030.md): Seat Track · cracked · Sep 3, 2025 · N3159G · Boeing 737852 · Fuselage, Seat/Cargo Attach Fittings
  > DURING THE ACCOMPLISHMENT OF 737-AE-53-837_P1-OP-UP NAC TASK CARD, THERE WERE FOUND TWO SEAT TRACK CROWN AREAS DAMAGED, ONE CRACKED AT STA 520 LBL 24.75, AND THE OTHER ONE WITH WEAR AT STA 520 LBL 45.50. SINCE THE MENTIONED SEAT TRACK AREAS ARE AFFECTED BY AEI
- [SDR EE4Y2025090323025](https://openairdocs.org/sdr/EE4Y2025090323025.md): Floorbeam · corroded · Sep 3, 2025 · N3159G · Boeing 737852 · Fuselage Main, Floor Beam
  > DURING THE ACCOMPLISHMENT OF 737-AE-53-837_P1-OP-UP NAC TASK CARD, IT WAS FOUND AT STA.767, THE FLOOR BEAM WITH SEVERAL CORROSION SPOTS BETWEEN LBL 60 AND RBL 60, SPECIFICALLYON UPPER CHORD, UPPER AND LOWER SURFACES. SINCE THE MENTIONED FLOOR BEAM IS AFFECTED
- [SDR EE4Y2025090323024](https://openairdocs.org/sdr/EE4Y2025090323024.md): Floorbeam · corroded · Sep 3, 2025 · N3159G · Boeing 737852 · Fuselage Main, Floor Beam
  > DURING THE ACCOMPLISHMENT OF 737-AE-53-837_P1-OP-UP NAC TASK CARD, IT WAS FOUND AT STA. 727J, THE FLOOR BEAM WITH SEVERAL CORROSION SPOTS BETWEEN LBL 60 AND RBL 60, SPECIFICALLY ON UPPER CHORD, UPPER AND LOWER SURFACES. SINCE THE MENTIONED FLOOR BEAM IS AFFECT
- [SDR EE4Y2025090323022](https://openairdocs.org/sdr/EE4Y2025090323022.md): Floorbeam · corroded · Sep 3, 2025 · N3159G · Boeing 737852 · Fuselage Main, Floor Beam
  > DURING THE ACCOMPLISHMENT OF 737-AE-53-837_P1-OP-UP NAC TASK CARD, IT WAS FOUND AT STA. 727F, THE FLOOR BEAM WITH SEVERAL CORROSION SPOTS BETWEEN LBL 60 AND RBL 60, SPECIFICALLY ON UPPER CHORD, UPPER AND LOWER SURFACES. SINCE THE MENTIONED FLOOR BEAM IS AFFECT
- [SDR NACA2023082803](https://openairdocs.org/sdr/NACA2023082803.md): Unknown · unknown · Aug 17, 2023 · N3159G · Boeing 7378 · Doors
  > FOUND MCD ACTUATOR FWD AND AFT MOUNT PLATES LOOSE. COMPLIED WITH AEI ENGINEERING ORDER E022458 REV 1R REMOVED AND REINSTALLED MCD FWD AND AFT ACTUATOR PLATES /FRAMES, SEE PROJECT WORKSHEET FOR DETAILS. FAA FORM 8110-3 AEI DATED 8/26/2023 AUTHORIZED.

## 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 = 'N3159G' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N3159G/reports

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