Boeing 727-82C

Service difficulty reports · 164

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 = '72782C'
  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 DHL9670901CSkin · bulgedAT C-CHECK, FOUND SKIN AT FS 1388 RIGHT SIDE AND FS 1400 RIGHT SIDE. CUT OUT SKIN 4 INCHES BY 4 INCHES, INSTALLED DOUBLER 6 INCHES BY 6 INCHES, FILLER 4 INCHES BY 4 INCHES PER SRM 54-10-1 AT STA 1388. CLEANED AREA AT FS 1400, NO CORROSION FOUND.May 6, 1996 · N709DH · Boeing 72782C · Fuselage Main, Plate/SkinSDR DHL9670920CSpar Forging · corrodedAT C-CHECK FOUND CORROSION ON VERTICAL FIN FRONT SPAR FORGING BELOW S-DUCT AND LEFT SIDE OF SPLICE PLATE. INSTALLED NEW MODIFIED FRONT SPAR FORGING UPPER SPLICE PLATE BELOW S-DUCT PER AVITAS EO 96PMSI 123D-1, REPAIR 10 BY 3.May 3, 1996 · N709DH · Boeing 72782C · Vertical StabilizerSDR DHL9670912CActuator Mount · crackedAT C-CHECK, FOUND NR 2 SLAT ACTUATOR MOUNT CRACKED. FABRICATED DOUBLER REPAIR PER S/B 57-130, DOUBLER 8 BY 3.May 3, 1996 · N709DH · Boeing 72782C · Leading Edge Slat ActuatorSDR DHL9670919CSkin · corrosionAT C-CHECK, FOUND SKIN BULGE AT STA 1166 BETWEEN STRINGER 21L AND 22L AT AFT LAVATORY SERVICE PANEL. REMOVED CORROSION, INSTALLED DOUBLER REPAIR AT AFT LAVATORY SERVICE PANEL PER AVITAS EO 96PMSI-123RO-5, FILLER PLATE 15.75 BY 14, BACKING PLATE 19 BY 21.May 2, 1996 · N709DH · Boeing 72782C · Fuselage Main, Plate/SkinSDR DHL9670918CDoor Frame · crackedAT C-CHECK, FOUND AFT CARGO DOOR HAS PRESSURIZATION LEAK AT UPPER AFT CORNER. STOP DRILLED CRACKS, INSTALLED REPAIR AT AFT CARGO DOOR FRAME PER AVITAS EO 96PMSI-RO-4, 3.5 BY 9.5.May 2, 1996 · N709DH · Boeing 72782C · Fuselage Miscellaneous StructureSDR DHL9670913CSkin · damagedAT C-CHECK, OB AILERON OF LEFT WING IB TRAILING EDGE CORNER IS BENT AND OIL CANNING. CUT OUT DAMAGED AREA, FABRICATED NEW SKIN, 14 BY 18 PER SRM 57-50-5. REBALANCED AILERON PER SRM 51-80-4.May 2, 1996 · N709DH · Boeing 72782C · AileronsSDR DHL9670910CDoubler · chafedAT C-CHECK, FOUND SKIN DOUBLER INSIDE B-SYSTEM HYDRAULIC COMPARTMENT, BETWEEN STA 990 AND 1010 CHAFED DEEPLY. INSTALLED DOUBLER PER SRM 53-30-3, 10 BY 6.May 2, 1996 · N709DH · Boeing 72782C · Fuselage Miscellaneous StructureSDR DHL9670904CSkin · corrodedAT C-CHECK, FOUND S-DUCT HAS CORROSION AROUND FASTENERS AND SKIN BULGE AT 12 O'CLOCK POSITION, 24 FWD OF PRODUCTION BREAK. CUT OUT DAMAGED AREA, INSTALLED DOUBLER 8.5 BY 9.5 PER SRM 54-10-3.May 2, 1996 · N709DH · Boeing 72782C · Nacelle/Pylon StructureSDR DHL9670903CSkin · crackedAT C-CHECK, RIGHT WING LEADING EDGE SLAT O/B HOOK SKIN CRACKED AT RIVET HOLES. REMOVED HOOK FOR ACCESS, FABRICATED AND INSTALLED REPAIR PLATE 4.5 X 3.5 PER SRM 57-30-3. INSTALLED HOOK AND FASTENERS PER SRM 51-30-2.May 2, 1996 · N709DH · Boeing 72782C · Leading Edge DevicesSDR DHL9670902CSkin · corrosionAT C-CHECK, FOUND SURFACE CORROSION AT STA 1080 BETWEEN STR 16R AND 18R AFT SKIN OF BUTT SEAM AND ALONG STR 17R STA 1080 TO 1090. REMOVED CORROSION ALONG STR 17R STA 1080 TO 1090, WITHIN LIMITS. INSTALLED FILLER AND EXTERNAL DOUBLER PER SRM 51-30-3 DOUBLER 8May 2, 1996 · N709DH · Boeing 72782C · Fuselage Main, Plate/SkinSDR 96DHL70901ASkin · bulgedDURING A11 CHECK, FUSELAGE SKIN BULGED UNDER RAIN GUTTER FS 1390 APPROXIMATELY JUST ABOVE NR 2 ENGINE LEFT FORWARD COWL. REMOVED FASTENERS, CUTOUT DAMAGED AREA, FABRICATED REPAIR PARTS 3.5 INCHES BY 5 INCHES. INSTALLED DOUBLER 8.5 INCHES BY 9.5 INCHES PER SRMar 2, 1996 · N709DH · Boeing 72782C · Fuselage Main, Plate/SkinSDR 95ZZZM664Fuel Control · failedON TAKEOFF AT 300 FT AGL, THE NR 1 ENGINE SHUT DOWN. FUEL FLOW WENT TO ZERO. ACCOMPLISHED APPROPRIATE CHECK LISTS AND LANDED WITHOUT INCIDENT. REPLACED FUEL CONTROL UNIT PER MM 73-21-1. REPLACED ENGINE DRIVEN FUEL PUMP PER 73-11-1 AS PRECAUTION. TRIMMED EOct 10, 1995 · N528PC · Boeing 72782C · Fuel Control/Turbine EnginesSDR 95ZZZW427Bulb · burned outRIGHT MAIN LANDING GEAR UNSAFE WARNING LIGHT CAME ON DURING GEAR EXTENSION. AIRCRAFT LANDED IN STL WITHOUT FURTHER INCIDENT. REPLACED THE RIGHT MAIN LANDING GEAR DOWN AND LOCKED INDICATION BULB. ALL INDICATIONS CHECK NORMAL. (W)Mar 28, 1995 · N528PC · Boeing 72782C · Landing Gear Position and WarningSDR 95ZZZW55Rub Block · out of adjustDURING CONTROL CHECK, MOVING WHEEL FROM FULL FWD TO AFT, THERE IS A VIBRATION AND A FEEL OF BINDING IN ELEVATORS. CAN FEEL SHAKING THROUGH FLOOR OF ACFT. RETURNED TO BLOCKS. ADJUSTED RUB BLOCK ON LT ELEVATOR. IAW BOEING MM 27-30-1. OPS CHECK OK.Jan 14, 1995 · N709DH · Boeing 72782C · Elevator Control System
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