Douglas DC-8-62F

Service difficulty reports · 1,163

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 = 'DC862F'
  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 AR022851Slot Door · corrodedDURING C-CHECK INSPECTION, FOUND RT WING OUTBOARD SLOT DOOR WITH LEVEL 2 CORROSION AT L/E, REF CPCP 031 116R0551. FABRICATED DOUBLER USING STAINLESS STEEL .040 301 1/2 HARD IAW EO NR 9503061 AND SRM 51-1-8. (X)Feb 28, 1995 · N791AL · Doug DC862F · Trailing Edge FlapsSDR 95ZZZX1510Slot Contl Valve · leakingKAUS/KDAY - FLT 107 - IN-FLIGHT LOST ALL HYDRAULIC PRESSURE AND QUANTITY DOWN TO AUX MARK ON QUANTITY INDICATOR. MAINTENANCE FOUND SLOT CONTROL VALVE LEAKING. REMOVED AND REPLACED SLOT CONTROL VALVE IAW MM 27-80-4. HYDRAULIC SYSTEM SERVICED. LEAK AND OPS CFeb 24, 1995 · N997CF · Doug DC862F · Trailing Edge Flap Control SystemSDR ARWA022051Support · crackedDURING C-CHECK, FOUND FLOOR SUPPORT CRACKED AT FS 600 BETWEEN L35L AND L36L. FABRICATED AND INSTALLED DOUBLER IAW SRM 53-20-0. ARROW AIR WORK ORDER NR 950007-5164 (0411). (M)Feb 20, 1995 · N791AL · Doug DC862F · Fuselage Miscellaneous StructureSDR 95ZZZX2492Skin · corrosionLEFT WING LEADING EDGE WS 69.500 AT FRONT SPAR, SMALL AREA AROUND SCREW, HAS CORROSION LEVEL II UPPER SURFACE. REMOVED CORROSION, FOUND AREA BEYOND LIMITS, FABRICATED DOUBLER AND FILLED REWORKED AREA IAW SRM 57-24. COMPLETED THICKNESS CHECK, TREATED, PRIMED,Feb 20, 1995 · N791AL · Doug DC862F · Wing, Plate/SkinSDR ARWA0927957Skin · corrodedDURING C-CHECK INSPECTION, FOUND LEVEL 2 CORROSION BEYOND LIMITS ON ELEVATOR STA XE 176.156. REMOVED DAMAGED SKIN. FABRICATED AND INSTALLED NEW SKIN IAW DER DRAWING ARW.950007-0169. REBALANCED ELEVATOR IAW SRM 51-4-0. (X)Feb 17, 1995 · N791AL · Doug DC862F · Elevator, Plate/SkinSDR ARWA021751Intercostal · crackedDURING C-CHECK, FOUND MAIN CARGO COMPARTMENT AFT BULKHEAD FS 1600 AT L28L HAD CRACKED INTERCOSTAL. REMOVED CRACKED INTERCOSTAL, FABRICATED AND INSTALLED NEW INTERCOSTAL IAW SRM 51-1-8, 51-1-20 AND 53-1-0. ARROW AIR WORK ORDER NR 950007-5110 (0249). (M)Feb 17, 1995 · N791AL · Doug DC862F · Fuselage Miscellaneous StructureSDR 95ZZZX2497Skin · corrosionCORROSION AT FS 857.0, LEFT, IN THE WING BOX AREA. PERFORMED REPAIRS PER E.O. 9502201, W/O 950040, ITEM 9026.Feb 17, 1995 · N791AL · Doug DC862F · Fuselage Main, Plate/SkinSDR 95ZZZX2496Skin · corrodedEXFOLIATING CORROSION AROUND PREVIOUS REPAIRS ON LEFT WING LEADING EDGE UPPER SURFACE, WS XFS 885, WS XFS 890, XFS 908, AND XFS 920. REMOVED SECTION OF THE LEADING EDGE, REMOVED CORROSION, FOUND BEYOND LIMITS. ACCOMPLISHED REPAIR PER SRM 57-2-1, SRM 51-1-6, Feb 17, 1995 · N791AL · Doug DC862F · Wing, Plate/SkinSDR 95ZZZX2494Intercostal · crackFS 1600, STR 28L, INTERCOSTAL IS CRACKED. REMOVED DAMAGED INTERCOSTAL, FABRICATED NEW INTERCOSTAL PER ORIGINAL HEAT TREATED TO 7075-T6 AND INSTALLED PER SRM 53-1-0. DOCUMENTED UNDER W/O 950007, ITEM 5110.Feb 17, 1995 · N791AL · Doug DC862F · Fuselage Miscellaneous StructureSDR ARWA0927958Skin · damagedDURING C-CHECK INSPECTION, FOUND RT WING OUTBOARD TRAILING EDGE UPPER SURFACE PANEL DAMAGED FROM STA XW 763.0 TO XW 636.0. REPAIRED PANEL IAW SRM 51-1-9 AND DER EO 950031-0024. (X)Feb 12, 1995 · N791AL · Doug DC862F · Wing, Plate/SkinSDR ARWA0927954Stress Plank · damagedDURING INCIDENT, INSPECTION FOUND NR 4 PYLON INBAORD STRESS PANEL (STATIONARY PLANK) BENT. REMOVED AND REPLACED NR 4 PYLON INBOARD STATIONARY STRESS PLANK PER DAC DRAWINGS NR 5753010 AND 5753000. (M)Feb 12, 1995 · N791AL · Doug DC862F · Nacelle/Pylon StructureSDR ARWA0927952Rib · bentDURING INCIDENT INSPECTION, FOUND RIGHT WING RIB SUPPORT FOR WING TIP AT STA XW 761.695 DAMAGED AT LEADING EDGE AREA. FABRICATED NOSE SECTION OF BULKHEAD FROM .071 INCH 7075-0, AND NOSE DOUBLER AND SPLICE DOUBLER FROM .080 INCH 7075-0. HEAT TREATED, PRIMED, Feb 12, 1995 · N791AL · Doug DC862F · Wing, Rib/BulkheadSDR EIAA9502Carbon Seal · leakingMZJ - ACCOMPLISHED PRECAUTIONARY SHUTDOWN OF NR 1 ENGINE DUE TO LOSS OF OIL QUANTITY. OIL PRESSURE REMAINED AT 32 PSI INITIALLY THE FLUCTUATED 15-30 PSI. OIL QUANTITY WAS AT 1.75 GALLONS WHEN ENGINE SHUTDOWN. PRESSURE AND TEMPERATURES NORMAL. OIL QUANTITY Jan 30, 1995 · N817EV · Doug DC862F · Turbine Engine Oil System
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