# Service difficulty reports: Boeing 727-30

A list on [Boeing 727-30](https://openairdocs.org/model/boeing-727-30.md).

Newest first. General aviation reporting is voluntary.

- [SDR FOTR2810812032012](https://openairdocs.org/sdr/FOTR2810812032012.md): Skin · corroded · Nov 20, 2012 · N606DH · Boeing 72730 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN HAS BULGE AT LAP SEAM, BS 259-264, S10L. REPAIRED ON FAS WO 22148.
- [SDR FOTR2812512032012](https://openairdocs.org/sdr/FOTR2812512032012.md): Skin · corroded · Nov 14, 2012 · N606DH · Boeing 72730 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN HAS AREAS OF CORROSION AT SKIN LAP SEAM, STR 4L, BS 259-360. REPAIRED ON FAS WO22148, NR 28125.
- [SDR FOTR2810912032012](https://openairdocs.org/sdr/FOTR2810912032012.md): Skin · corroded · Nov 8, 2012 · N606DH · Boeing 72730 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN HAS CORROSION AT LAP SEAM, BS 344-360, STR 10L. REPAIRED ON FAS NR 28109.
- [SDR FOTR3355612032012](https://openairdocs.org/sdr/FOTR3355612032012.md): Shear Tie · corroded · Nov 5, 2012 · N606DH · Boeing 72730 · Fuselage Internal Mounting Structure
  > BS 294.5 FRAME SHEAR TIE BETWEEN STRINGER 26-27L IS CORRODED. REPAIRED ON FAS WO 22148, NR 33556.
- [SDR FOTR2804512032012](https://openairdocs.org/sdr/FOTR2804512032012.md): Skin · bulged · Nov 4, 2012 · N606DH · Boeing 72730 · Fuselage Main, Plate/Skin
  > LEFT FUSELAGE SKIN BS 351.2 SKIN IS BULGING AND HAS POPPED RIVETS. REPAIRED ON FAS WO22148, NR28045.
- [SDR FOTR281612032012](https://openairdocs.org/sdr/FOTR281612032012.md): Skin · corroded · Nov 2, 2012 · N606DH · Boeing 72730 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN HAS CORROSION AROUND EXISTING DOUBLER STA 440, STR 26R. REPAIRED ON FAS WO 22148, NR 28161.
- [SDR FOTR3355512032012](https://openairdocs.org/sdr/FOTR3355512032012.md): Skin · gouged · Oct 31, 2012 · N606DH · Boeing 72730 · Fuselage Main, Plate/Skin
  > DEEP GOUGE FOUND FUSELAGE SKIN LT SIDE, STA 259, STR 27. REPAIRED ON FAS WO 22148, NR 33555.
- [SDR FOTR2819812032012](https://openairdocs.org/sdr/FOTR2819812032012.md): Skin · corroded · Oct 31, 2012 · N606DH · Boeing 72730 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN RT SIDE LAP JOINT AT STR 4R HAS CORROSION SPOTS BETWEEN BS 480 AND BS 620. REPAIRED ON FAS WO 22148, NR 28198.
- [SDR FOTR2815712032012](https://openairdocs.org/sdr/FOTR2815712032012.md): Skin · corroded · Oct 30, 2012 · N606DH · Boeing 72730 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN HAS CORROSION AT STRINGER 10R LAP SEAM, STA 480-600. REPAIRED ON FAS WO 22148, NR 28157.
- [SDR FOTR3348312032012](https://openairdocs.org/sdr/FOTR3348312032012.md): Seam · corroded · Oct 29, 2012 · N606DH · Boeing 72730 · Fuselage Main, Plate/Skin
  > SKIN LAP JOINT AT STR 4R HAS CORROSION SPOTS AROUND FASTENERS BETWEEN BS 620 AND 740. REPAIRED ON FAS WO 22148, NR 33483.
- [SDR FOTR2815512032012](https://openairdocs.org/sdr/FOTR2815512032012.md): Skin · corroded · Oct 29, 2012 · N606DH · Boeing 72730 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN HAS CORROSION BS 500, STRINGER 10R. REPAIRED ON FAS WO 22148, NR 28155.
- [SDR FOTR2801612032012](https://openairdocs.org/sdr/FOTR2801612032012.md): Skin · bulged · Oct 29, 2012 · N606DH · Boeing 72730 · Fuselage Main, Plate/Skin
  > RIGHT FWD FUSELAGE SKIN LAP SEAM FROM APPROX BS 441-522, STR 19R HAS NUMEROUS AREAS OF CORROSION, SHEARED FASTENERS AND BULGING SKIN. REPAIRED ON FAS WO 22148, NR28016.
- [SDR FOTR2805912032012](https://openairdocs.org/sdr/FOTR2805912032012.md): Skin · corroded · Oct 29, 2012 · N606DH · Boeing 72730 · Fuselage Main, Plate/Skin
  > STRINGER 14L, SKIN LAP SEAM HAS CORROSION EVIDENCE IN MULTIPLE AREAS BETWEEN BS 950-1183. REPAIRED ON FAS WO 22148, NR 28059.
- [SDR FOTR3352012032012](https://openairdocs.org/sdr/FOTR3352012032012.md): Skin · corroded · Oct 25, 2012 · N606DH · Boeing 72730 · Fuselage Main, Plate/Skin
  > SKIN LT SIDE LAP JOINT AT STR 4L HAS CORROSION SPOTS AND CORRODED FASTENERS BETWEEN BS 870-970. REPAIRED ON FAS WO 22148, NR 33521.
- [SDR FOTR2249812032012](https://openairdocs.org/sdr/FOTR2249812032012.md): Skin · corroded · Oct 24, 2012 · N606DH · Boeing 72730 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN RT SIDE LAP JOINT AT STR 4R HAS CORROSION SPOTS, ON SKIN AND AROUND FASTENERS HEAD, BETWEEN BS 950-1080. REPAIRED ON FAS WO 22148, NR 33498.
- [SDR 20000503SH005](https://openairdocs.org/sdr/20000503SH005.md): Hydraulic System · leaking · Feb 22, 2000 · N113 · Boeing 72730 · Hydraulic Power System
  > AIRCRAFT WAS ON A MAINTENANCE TEST FLIGHT FOLLOWING A C-CHECK INSPECTION, THE CREW REPORTED A LOSS OF HYDRAULIC FLUID IN THE A-SYSTEM. THE A-SYSTEM WAS SHUT DOWN AND THE AIRCRAFT LANDED WITHOUT ANY FURTHER INCIDENTS. (X)
- [SDR 97ZZZX4864](https://openairdocs.org/sdr/97ZZZX4864.md): Panel · leaking · Oct 1, 1997 · N113 · Boeing 72730 · Wing, Plate/Skin
  > DEFECT - IN-FLIGHT LEAK FROM LEFT WING. FOUND 9 LOOSE FASTENERS ON INBOARD END OF FUEL ACCESS PANEL NR 15 ON LEFT WING. SUSPECT IMPROPER TORQUE OF FASTENERS DURING LAST HEAVY MAINTENANCE VISIT. RE-TORQUED FASTENERS IAW BOEING MM 28-11-21. ADDITIONALLY, MAR
- [SDR 97ZZZX4361](https://openairdocs.org/sdr/97ZZZX4361.md): Skin · cracked · Sep 1, 1997 · N113 · Boeing 72730 · Fuselage Main, Plate/Skin
  > FOUND AND REPAIRED CRACKS IN THE FUSELAGE SKIN AT THE FOLLOWING LOCATIONS. STA 418, STR 21L, 2 EACH. STA 370 - STA 385, STR 22L, 5 EACH. STA 400 BELOW STR 23L, 1 EACH. STA 420, STR 20L, 2 EACH. STA 385, STR 23L, 1 EACH. REPAIRED CORROSION AT FS 415, STR
- [SDR 97ZZZX4362](https://openairdocs.org/sdr/97ZZZX4362.md): Casting · crack · Aug 26, 1997 · N113 · Boeing 72730 · Spoilers
  > RIGHT HAND INBOARD SPOILER CASTING CRACKED TOP INBOARD AFT ATTACH HOLE. REPAIRED PER APPROVED DATA BOEING AIRCRAFT COOPERATION ENGINEERING INSTRUCTIONS, REFERENCE TELEX NR 32-9430 AND BOEING AIRCRAFT DRAWING SKETCH NR 65-19222.
- [SDR 97ZZZX4363](https://openairdocs.org/sdr/97ZZZX4363.md): Skin · defective · Aug 25, 1997 · N113 · Boeing 72730 · Fuselage Main, Plate/Skin
  > AN EXISTING REPAIR HAS BEEN INSTALLED THE FULL LENGTH OF TH FUSELAGE FROM BS 360 TO BS 441 AT LONGERON 19R TO LONGERON 26R. THE EXISTING REPAIR WILL BE CHANGED BY DALFORT AVIATION UNDER XEA, NR X1-53-691. REVISION ONE. APPROVED DATA BOEING 727 SRM 53-30-3,
- [SDR 97ZZZX3066](https://openairdocs.org/sdr/97ZZZX3066.md): T Chord · corroded · Jun 1, 1997 · N357KP · Boeing 72730 · Fuselage Miscellaneous Structure
  > DURING C-CHECK INSPECTION, CORROSION NOTED ON T-CHORD BETWEEN STA 320 AND STA 350 AT S26R.
- [SDR 96ZZZX3831](https://openairdocs.org/sdr/96ZZZX3831.md): Check Valve · failed · Apr 29, 1996 · N727BE · Boeing 72730 · Aircraft Fuel Distribution System
  > CHECK VALVE FAILED IN OPEN POSITION. VALVE WAS INSTALLED IN AUXILIARY FUEL SYSTEM STC NR SA530NE CONFIGURATION NR 3. INSTALLED PER DWG NR 200-1-503 FUEL SYSTEM. AUXILARY FUEL KIT INSTALLED PER INSTALLATION MDL-200-1-141, REV. 1, DATED MAY 16, 1990.

## 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 = '72730'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-727-30/reports

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