Boeing 727-30

Service difficulty reports · 22

Newest first. General aviation reporting is voluntary.

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR FOTR2810812032012Skin · corrodedFUSELAGE SKIN HAS BULGE AT LAP SEAM, BS 259-264, S10L. REPAIRED ON FAS WO 22148.Nov 20, 2012 · N606DH · Boeing 72730 · Fuselage Main, Plate/SkinSDR FOTR2812512032012Skin · corrodedFUSELAGE SKIN HAS AREAS OF CORROSION AT SKIN LAP SEAM, STR 4L, BS 259-360. REPAIRED ON FAS WO22148, NR 28125.Nov 14, 2012 · N606DH · Boeing 72730 · Fuselage Main, Plate/SkinSDR FOTR2810912032012Skin · corrodedFUSELAGE SKIN HAS CORROSION AT LAP SEAM, BS 344-360, STR 10L. REPAIRED ON FAS NR 28109.Nov 8, 2012 · N606DH · Boeing 72730 · Fuselage Main, Plate/SkinSDR FOTR3355612032012Shear Tie · corrodedBS 294.5 FRAME SHEAR TIE BETWEEN STRINGER 26-27L IS CORRODED. REPAIRED ON FAS WO 22148, NR 33556.Nov 5, 2012 · N606DH · Boeing 72730 · Fuselage Internal Mounting StructureSDR FOTR2804512032012Skin · bulgedLEFT FUSELAGE SKIN BS 351.2 SKIN IS BULGING AND HAS POPPED RIVETS. REPAIRED ON FAS WO22148, NR28045.Nov 4, 2012 · N606DH · Boeing 72730 · Fuselage Main, Plate/SkinSDR FOTR281612032012Skin · corrodedFUSELAGE SKIN HAS CORROSION AROUND EXISTING DOUBLER STA 440, STR 26R. REPAIRED ON FAS WO 22148, NR 28161.Nov 2, 2012 · N606DH · Boeing 72730 · Fuselage Main, Plate/SkinSDR FOTR3355512032012Skin · gougedDEEP GOUGE FOUND FUSELAGE SKIN LT SIDE, STA 259, STR 27. REPAIRED ON FAS WO 22148, NR 33555.Oct 31, 2012 · N606DH · Boeing 72730 · Fuselage Main, Plate/SkinSDR FOTR2819812032012Skin · corrodedFUSELAGE SKIN RT SIDE LAP JOINT AT STR 4R HAS CORROSION SPOTS BETWEEN BS 480 AND BS 620. REPAIRED ON FAS WO 22148, NR 28198.Oct 31, 2012 · N606DH · Boeing 72730 · Fuselage Main, Plate/SkinSDR FOTR2815712032012Skin · corrodedFUSELAGE SKIN HAS CORROSION AT STRINGER 10R LAP SEAM, STA 480-600. REPAIRED ON FAS WO 22148, NR 28157.Oct 30, 2012 · N606DH · Boeing 72730 · Fuselage Main, Plate/SkinSDR FOTR3348312032012Seam · corrodedSKIN LAP JOINT AT STR 4R HAS CORROSION SPOTS AROUND FASTENERS BETWEEN BS 620 AND 740. REPAIRED ON FAS WO 22148, NR 33483.Oct 29, 2012 · N606DH · Boeing 72730 · Fuselage Main, Plate/SkinSDR FOTR2815512032012Skin · corrodedFUSELAGE SKIN HAS CORROSION BS 500, STRINGER 10R. REPAIRED ON FAS WO 22148, NR 28155.Oct 29, 2012 · N606DH · Boeing 72730 · Fuselage Main, Plate/SkinSDR FOTR2801612032012Skin · bulgedRIGHT 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.Oct 29, 2012 · N606DH · Boeing 72730 · Fuselage Main, Plate/SkinSDR FOTR2805912032012Skin · corrodedSTRINGER 14L, SKIN LAP SEAM HAS CORROSION EVIDENCE IN MULTIPLE AREAS BETWEEN BS 950-1183. REPAIRED ON FAS WO 22148, NR 28059.Oct 29, 2012 · N606DH · Boeing 72730 · Fuselage Main, Plate/SkinSDR FOTR3352012032012Skin · corrodedSKIN LT SIDE LAP JOINT AT STR 4L HAS CORROSION SPOTS AND CORRODED FASTENERS BETWEEN BS 870-970. REPAIRED ON FAS WO 22148, NR 33521.Oct 25, 2012 · N606DH · Boeing 72730 · Fuselage Main, Plate/SkinSDR FOTR2249812032012Skin · corrodedFUSELAGE 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.Oct 24, 2012 · N606DH · Boeing 72730 · Fuselage Main, Plate/SkinSDR 20000503SH005Hydraulic System · leakingAIRCRAFT 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)Feb 22, 2000 · N113 · Boeing 72730 · Hydraulic Power SystemSDR 97ZZZX4864Panel · leakingDEFECT - 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, MAROct 1, 1997 · N113 · Boeing 72730 · Wing, Plate/SkinSDR 97ZZZX4361Skin · crackedFOUND 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 Sep 1, 1997 · N113 · Boeing 72730 · Fuselage Main, Plate/SkinSDR 97ZZZX4362Casting · crackRIGHT 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.Aug 26, 1997 · N113 · Boeing 72730 · SpoilersSDR 97ZZZX4363Skin · defectiveAN 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, Aug 25, 1997 · N113 · Boeing 72730 · Fuselage Main, Plate/SkinSDR 97ZZZX3066T Chord · corrodedDURING C-CHECK INSPECTION, CORROSION NOTED ON T-CHORD BETWEEN STA 320 AND STA 350 AT S26R.Jun 1, 1997 · N357KP · Boeing 72730 · Fuselage Miscellaneous StructureSDR 96ZZZX3831Check Valve · failedCHECK 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.Apr 29, 1996 · N727BE · Boeing 72730 · Aircraft Fuel Distribution System
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