Douglas DC-8-62

Service difficulty reports · 2,778

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 = 'DC862'
  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 96ZZZX2721Fitting · corrodedDURING C-CHECK, FOUND LONGERON 30L BETWEEN FS 1530 TO FS 1670, HAS CORROSION, LEVEL 2. REMOVED AND REPLACED DAMAGED LONGERON AND FITTING IAW SRM 51-1-21 AND SRM 51-1-20D. TREATED AND PRIMED IAW SRM 51-1-8 AND SRM 53-10-0.Apr 26, 1996 · N8969U · Doug DC862 · Fuselage Miscellaneous StructureSDR 96ZZZX2720Longeron · corrodedDURING C-CHECK, FOUND LONGERON 30L BETWEEN FS 1530 TO FS 1670, HAS CORROSION, LEVEL 2. REMOVED AND REPLACED DAMAGED LONGERON AND FITTING IAW SRM 51-1-21 AND SRM 51-1-20D. TREATED AND PRIMED IAW SRM 51-1-8 AND SRM 53-10-0.Apr 26, 1996 · N8969U · Doug DC862 · Fuselage Main, Longeron/StringerSDR 96ZZZX2719Stiffener · corrodedDURING C-CHECK, FOUND A/C COMPARTMENT RT SIDE AT FS 208, BULKHEAD STIFFENER HAS EXFOLIATON CORROSION IN DIFFERENT LOCATION. REMOVED STIFFENER WITH CORROSION, FABRICATED NEW IAW SRM 53-2-0. TREATED, PRIMED, AND INSTALLED IAW SRM 51-1-8, SRM 51-1-21, AND SRM 5Apr 26, 1996 · N8969U · Doug DC862 · Fuselage Miscellaneous StructureSDR 96ZZZX2718Intercostal · corrodedDURING C-CHECK, FOUND FUSELAGE RT SIDE, INTERCOSTAL RT L28R BETWEEN FS 209 TO FS 225, HAS CORROSION. REMOVED INTERCOSTAL IAW SRM 53-2-0, SRM 5-1-21, AND SRM 51-1-20D.Apr 26, 1996 · N8969U · Doug DC862 · Fuselage Miscellaneous StructureSDR 96ZZZX2717Fitting · corrodedDURING C-CHECK, FOUND CABIN UPPER SURFACE OF THE RT SIDE CUSP AREA, FS 1260 AT FLOOR LEVEL, FITTING HAS CORROSION. REMOVED DAMAGED FITTING, REMOVED CORROSION AREA, FOUND WITHIN LIMITS. ALODINED AND PRIMED AREA. INSTALLED NEW FITTING, PN 4640162-1N, IAW SRM 5Apr 26, 1996 · N8969U · Doug DC862 · Fuselage Miscellaneous StructureSDR 96ZZZX2716Angle · crackedDURING C-CHECK, FOUND LOWER FUSELAGE LT ADF SENSE ANTENNA COMPARTMENT, FORWARD ATTACH ANGLE, CRACKED AT STA 834.500 BETWEEN XCW ZERO AND XCW 23. INSTALLED REPAIR ANGLE IAW SRM 53-2-0, SRM 53-2-0, AND SRM 51-1-20.Apr 26, 1996 · N8969U · Doug DC862 · Fuselage Miscellaneous StructureSDR 96ZZZX2715Skin · corrodedDURING C-CHECK, FOUND LT WING UPPER SKIN HAS CORROSION AT CTR SPAR AND XRS 22.750. REPAIRED SKIN IAW E.O. 961 ALE.005D-4.Apr 26, 1996 · N8969U · Doug DC862 · Wing, Plate/SkinSDR 96ZZZX2714Angle · corrodedDURING C-CHECK, FOUND LOWER AFT FUSELAGE COMPARTMENT AT STA 1606, ANGLE ATTACHED TO THE AFT BULKHEAD AT FLOOR LEVEL HAS CORROSION. FABRICATED NEW ANGLE AND INSTALLED IAW SRM 53-2-0, SRM 51-1-8, SRM 51-1-20D, SRM 51-1-21.Apr 26, 1996 · N8969U · Doug DC862 · Fuselage Miscellaneous StructureSDR 96ZZZX2713Skin · corrodedDURING C-CHECK, FOUND LT UPPER WING SKIN HAS CORROSION AT CTR SPAR AND XRS 45.000. REPAIRED SKIN IAW E.O. 96IALE.005D-4.Apr 26, 1996 · N8969U · Doug DC862 · Wing, Plate/SkinSDR 96ZZZX2712Longeron · corrodedDURING C-CHECK, FOUND LEVEL 2 CORROSION AT LONGERON L30R, FS 208.00 TO FS 270.00. REMOVED AND REPLACED LONGERON IAW SRM 53-2-0, SRM 51-1-21, AND SRM 51-1-20D.Apr 26, 1996 · N8969U · Doug DC862 · Fuselage Main, Longeron/StringerSDR 96ZZZX2711Longeron · corrodedDURING C-CHECK, FOUND LONGERON 36 BETWEEN FS 1530 TO FS 1670 WITH LEVEL 2 CORROSION. REMOVED AND REPLACED LONGERON IAW SRM 51-1-21 AND SRM 51-1-20D.Apr 26, 1996 · N8969U · Doug DC862 · Fuselage Main, Longeron/StringerSDR 96ZZZX2710Longeron · corrodedDURING C-CHECK, FOUND LONGERON 34L BETWEEN STA 1530 - STA 1670 HAS CORROSION, LEVEL 2. REMOVED AND REPLACED LONGERON IAW SRM 51-1-21, SRM 51-1-20D, AND SRM 51-1-8.Apr 26, 1996 · N8969U · Doug DC862 · Fuselage Main, Longeron/StringerSDR 96ZZZX2709Frame · corrodedCABIN WINDOW FRAME EXFOLIATED AROUND 1 BOLT HOLE. INSTALLED DOUBLER IAW DER NR SRO8530014 AND SRM 51-1-20D.Apr 26, 1996 · N8969U · Doug DC862 · Passenger Compartment WindowsSDR 96ZZZX2708Support Channel · corrodedCABIN, AFT LAVATORY AREA, FLOOR SUPPORT CHANNEL CORRODED. FABRICATED AND INSTALLED NEW CHANNEL IAW SRM 53-2-0, SRM 51-1-8, SRM 51-3-0.Apr 26, 1996 · N8969U · Doug DC862 · Fuselage Miscellaneous StructureSDR 96ZZZX2706Thrust Link · chafedNR 4 ENGINE PYLON THRUST LINK CHAFED. REMOVED AND REPLACED THRUST LINK IAW SB 54-92-00, SRM 51-1-20D.Apr 26, 1996 · N8969U · Doug DC862 · Nacelle/Pylon StructureSDR 96ZZZX2705Frame · corrodedCABIN WINDOW NR 28 LT, FRAME CORRODED. REPLACED WINDOW FRAME IAW SRM 51-1-20D, SRM 51-1-8.Apr 26, 1996 · N8969U · Doug DC862 · Passenger Compartment WindowsSDR 96ZZZX2704Frame · corrodedCABIN WINDOW, NR 30 LT, CORRODED. REPAIRED FRAME IAW DAC SRO 8530014.Apr 26, 1996 · N8969U · Doug DC862 · Fuselage Miscellaneous StructureSDR 96ZZZX2703Finger Doubler · corrodedFUSELAGE RT SIDE, L21R, HAS CORROSION AT INTERNAL FINGER DOUBLER BETWEEN STA 188 TO STA 270. REMOVED, FABRICATED, INSTALLED NEW FINGER DOUBLER IAW SRM 51-1-21, SRM 53-3-2, SRM 51-1-8.Apr 26, 1996 · N8969U · Doug DC862 · Fuselage Miscellaneous StructureSDR 96ZZZX2702Fitting · corrodedDURING C-CHECK, LEVEL 2 CORROSION ON FITTING AT FS 270.00, LONGERON 21R. REPAIRED IAW DAC FAX 287337, 288375, AND 251819/01, SRM 51-1-20D AND SRM 51-3-0.Apr 26, 1996 · N8969U · Doug DC862 · Fuselage Miscellaneous StructureSDR 96ZZZX2697Longeron · corrodedDURING C-CHECK, FOUND LONGERONS CRACKED AT FS 270.00, LONGERONS 8L AND 7L. REPAIRED IAW SRM 53-2-2.Apr 26, 1996 · N8969U · Doug DC862 · Fuselage Main, Longeron/StringerSDR 96ZZZX2696Longeron · corrodedDURING C-CHECK, FOUND CORROSION LEVEL 2 ON LONGERON 24R BETWEEN FS 208.00 AND FS 270.00. REMOVED AND REPLACED LONGERON IAW SRM 53-2-0, SRM 51-1-21, AND SRM 51-1-20D.Apr 26, 1996 · N8969U · Doug DC862 · Fuselage Main, Longeron/StringerSDR 96ZZZX2695T-Angle · crackedDURING C-CHECK, FOUND LEFT WING AUXILIARY SPAR AREA INBD LOWER VERTICAL SUPPORT T-ANGLE CRACKED AT STA XW 33.000. INSTALLED NEW VERTICAL SUPPORT T-ANGLE IAW SRM 51-1-20, SRM 53-1-0, AND SRM 51-1-8.Apr 26, 1996 · N8969U · Doug DC862 · Wing Miscellaneous StructureSDR 96ZZZX2694Longeron · corrodedDURING C-CHECK, FOUND CORROSION LEVEL 2 ON LONGERON 31R BETWEEN FS 208.00 AND FS 270.00. REMOVED AND REPLACED LONGERON IAW SRM 53-2-0, SRM 51-1-21, AND SRM 51-1-20D.Apr 26, 1996 · N8969U · Doug DC862 · Fuselage Main, Longeron/StringerSDR 96ZZZX2693Web · corrodedDURING C-CHECK, FOUND FUSELAGE RT SIDE, A/C COMPARTMENT AREA UNDER CABIN FLOOR PANEL AT FS 235 AND L21R INTERCOSTAL (WEB) HAS CORROSION. REMOVED, FABRICATED NEW WEB, AND INSTALLED IAW SRM 53-20-6 AND SRM 51-1-21.Apr 26, 1996 · N8969U · Doug DC862 · Fuselage Miscellaneous StructureSDR 96ZZZX2692Flange · corrodedDURING C-CHECK, FOUND FS 420 HAS CORROSION AT THE LOWER FLANGE BETWEEN L5R AND L6R. REMOVED CORROSION IAW SRM 51-1-8. FOUND OUT OF LIMITS IAW SRM 53-2-0. CUT OUT DAMAGED AREA, FABRICATED FILLER AND DOUBLER IAW 53-2-1. PARTS HEAT TREATED ATI P.O. 2407. TREAApr 26, 1996 · N8969U · Doug DC862 · Fuselage Miscellaneous StructureSDR 96ZZZX2691Angle · corrodedDURING C-CHECK, FOUND AFT BULKHEAD, FORWARD SIDE, FLOOR PANEL ATTACH ANGLE ON LEFT SIDE OF CENTER IS CORRODED. REMOVED ANGLE AND FABRICATED NEW ONE PER SRM 53-2-0. INSTALLED ANGLE PER SRM 51-1-21.Apr 26, 1996 · N8969U · Doug DC862 · Fuselage Miscellaneous StructureSDR 96ZZZX2690Intercostal · corrodedDURING C-CHECK, FOUND FS 822 L19L HAS CORROSION LEVEL 1 LOCAL TYPE. REMOVED INTERCOSTAL, FABRICATED NEW ONE, TREATED, ALODINED, AND PRIMED. INSTALLED NEW INTERCOSTAL IAW SRM 53-2-0 AND SRM 51-1-8.Apr 26, 1996 · N8969U · Doug DC862 · Fuselage Miscellaneous StructureSDR 96ZZZX2689Frame · corrodedDURING C-CHECK, FOUND FS 610 LT WINDOW FRAME HAS A CRACK AT LOWER SIDE FROM CORROSION LEVEL 1 LOCAL TYPE. BLENDED OUT AND REMOVED CORROSION. FOUND AREA BEYOND LIMITS IAW DAC SR.08530014 DRAWING. FABRICATED EXTERNAL DOUBLER FROM 7075.T6 .190 INCH. INSTALLEDApr 26, 1996 · N8969U · Doug DC862 · Fuselage Miscellaneous StructureSDR 96ZZZX2688Fitting · corrodedDURING C-CHECK, FOUND CORROSION FUSELAGE FITTING STA 1500.00 AT LONGERON 21R. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D, 51-1-8. 53-2-0, 51-1-21, AND 51-3-0.Apr 26, 1996 · N8969U · Doug DC862 · Fuselage Miscellaneous StructureSDR 96ZZZX2687Longeron · corrodedDURING C-CHECK, FOUND LONGERON 32R, BETWEEN STA 1530 AN STA 1670, WITH CORROSION, LEVEL 2. REMOVED AND REPLACED IAW 51-1-21, SRM 51-1-20D, SRM 51-1-8.Apr 26, 1996 · N8969U · Doug DC862 · Fuselage Main, Longeron/StringerSDR 96ZZZX2686Skin · corrodedDURING C-CHECK, FOUND LOWER AFT FUSELAGE SKIN AT STA 1420.00, LONGERON 30L, BULGING. REPAIRED IAW SRM 53-2-1 AND SRM 51-1-8.Apr 26, 1996 · N8969U · Doug DC862 · Fuselage Main, Plate/SkinSDR 96ZZZX2685Skin · corrodedDURING C-CHECK, FOUND RT OUTBOARD AILERON SKIN BULGING. CUT OUT DAMAGED AREA, REPAIRED IAW DER DRAWING ARW 950082-0289.Apr 26, 1996 · N8969U · Doug DC862 · AileronsSDR 96ZZZX2684Longeron · corrodedDURING C-CHECK, FOUND LEVEL 2 CORROSION ON LONGERON 29R, FS 208.00 TO FS 270.00. REMOVED AND REPLACED LONGERON IAW SRM 53-2-0, SRM 51-1-21, AND SRM 51-1-20D.Apr 26, 1996 · N8969U · Doug DC862 · Fuselage Main, Longeron/StringerSDR 96ZZZX2683Brace · damagedDURING C-CHECK, FOUND NR 2 INBOARD PYLON SIDE, BRACE DAMAGED AND GOUGED. REMOVED AND REPLACED NEW THRUST LINK BRACE IAW SB 54-90-00 AND SRM 51-1-20D.Apr 26, 1996 · N8969U · Doug DC862 · Nacelle/Pylon StructureSDR 96ZZZX2682Skin · rustedDURING C-CHECK, FOUND LEFT WING UPPER SKIN HAS BARE METAL AND RUSTED FASTENERS AT CTR SPAR AND XRS 22.750. REPAIRED UPPER SKIN IAW E.O. NR 961ALE.005D-4.Apr 26, 1996 · N8969U · Doug DC862 · Wing, Plate/SkinSDR 96ZZZX2681Strap · corrodedDURING C-CHECK, FOUND LEFT WING LEADING EDGE, INBOARD SLOT AREA OUTBOARD END HAS TWO AREAS OF EXFOLIATION WITH CORROSION ON STRAP. REMOVED CORROSION, FOUND BEYOND LIMITS IAW SRM 57-3-0. FABRICATED NEW STRAP IAW SRM 57-3-0. TREATED, PRIMED, AND INSTALLED IAWApr 26, 1996 · N8969U · Doug DC862 · Wing Miscellaneous StructureSDR 96ZZZX2680Door · corrodedDURING C-CHECK, FOUND FORWARD RT FUSELAGE LAVATORY SERVICE DOOR AND DOOR CUT-OUT HAVE CORROSION. REMOVED DOOR, FABRICATED NEW DOOR AND INSTALLED IAW SRM 51-1-0 AND SRM 53-4-1. REMOVED CORROSION ON CUT-OUT, TREATED AND PRIMED IAW SRM 51-1-8.Apr 26, 1996 · N8969U · Doug DC862 · Service DoorsSDR 96ZZZX2679Intercostal · corrodedDURING C-CHECK, FOUND FORWARD RT LOWER SIDE OF INTERNAL FUSELAGE BETWEN FS 168 TO FS 188, AND BETWEEN L27R AND L28R, SMALL INTERCOSTAL HAS CORROSION. REMOVED INTERCOSTAL WITH CORROSION, FABRICATED NEW INTERCOSTAL IAW SRM 53-2-0, TREATED, PRIMED, AND INSTALLEDApr 26, 1996 · N8969U · Doug DC862 · Fuselage Miscellaneous StructureSDR 96ZZZX2678Frame · corrodedDURING C-CHECK, FOUND FUSELAGE, RT SIDE FRAME FS 225, HAS CORROSION APPROXIMATELY BETWEEN L21R AND L36R. REMOVED SECTION OF FRAME WITH CORROSION FABRICATED NEW FRAME SECTION AND SPLICE IAW SRM 53-2-0, FIGURE 2, PAGE 5. TREATED, PRIMED, AND INSTALLED IAW SRM Apr 26, 1996 · N8969U · Doug DC862 · Fuselage Main, FrameSDR 96ZZZX2677Skin · corrodedDURING C-CHECK, FOUND LEFT WING UPPER SKIN HAS SEVERAL SPOTS WITH CORROSION BETWEEN FRONT SPAR AND CENTER SPAR BETWEEN XRS 238.000 AND XRS 255.000. REMOVED CORROSION, FOUND BEYOND LIMITS. FABRICATED DOUBLERS AND INSTALLED IAW DER NR 961ALE005 D-5.Apr 26, 1996 · N8969U · Doug DC862 · Wing, Plate/SkinSDR 96ZZZX2674Skin · corrodedRIGHT WING, UPPER SURFACE LEADING EDGE ASSY - TRAILING EDGE HAS CORROSION AT FS 329.000, APPROXIMATE. REMOVED CORROSION. AREA FOUND BEYOND LIMITS. REMOVED DAMAGED AREA, FABRICATED DOUBLER AND REPAIRS IAW 57-201. REPAIRED DAMAGE IAW SRM 5-1-8, SRM 57-2-0, SApr 26, 1996 · N8969U · Doug DC862 · Wing, Plate/SkinSDR 96ZZZX2673Floor Web · corrodedDURING C-CHECK, FOUND AT FS 1420, FLOOR WEB HAS CORROSION LEVEL 1 LOCAL/TYPE. REMOVED CORROSION IAW 51-1-8 AND TREATED AND PRIMED. REPAIRED DAMAGE IAW 53-2-0. INSTALLED DOUBLER IAW SRM 53-2-6.Apr 26, 1996 · N8969U · Doug DC862 · Fuselage Miscellaneous StructureSDR 96ZZZX2672Longeron · corrodedDURING C-CHECK, FOUND LONGERON 34R BETWEEN STA 1530 TO STA 1670 WITH CORROSION, LEVEL 2. REMOVED AND REPLACED LONGERON IAW SRM 51-1-21 AND SRM 51-1-8.Apr 26, 1996 · N8969U · Doug DC862 · Fuselage Main, Longeron/StringerSDR 96ZZZX2671Skin · corrodedDURING C-CHECK, FOUND LEVEL 2 CORROSION UPPER WING AT STA XRS 172.000. REPAIRED IAW DER DRAWING FROM AVITAS NR 961ALE.005D-6.Apr 26, 1996 · N8969U · Doug DC862 · Wing, Plate/SkinSDR 96ZZZX2669Skin · corrodedDURING C-CHECK, FOUND LEFT WING OUTBOARD AILERON, INBOARD LOWER SURFACE SKIN BULGED. REPAIRED AILERON IAW DER DRW 950082-4066.Apr 26, 1996 · N8969U · Doug DC862 · AileronsSDR 96ZZZX2668Skin · corrodedDURING C-CHECK, FOUND LT WING UPPER SKIN HAS CORROSION 10 INCHES AFT OF CENTER SPAR BETWEEN XRS 311.656 AND XRS 351.000. REPAIRED DAMAGED SKIN IAW DER NR 961 ALE.005D-3.Apr 26, 1996 · N8969U · Doug DC862 · Wing, Plate/SkinSDR 96ZZZX2667Skin · corrodedDURING C-CHECK, FOUND RT WING UPPER SURFACE HAS CORROSION FORWARD OF CENTER SPAR AND XRS 74.869 (APPROXIMATELY). REPAIRED RT WING UPPER SKIN AT APPROXIMATELY XRS 74.869 IAW DER 961ALE.005D-1.Apr 26, 1996 · N8969U · Doug DC862 · Wing, Plate/SkinSDR 96ZZZX2666Longeron · corrodedDURING C-CHECK, FOUND LOWER AFT FUSELAGE COMPARTMENT, FS 1380 AND 30R LONGERON HAS CORROSION. CUT OUT DAMAGED SECTION, FABRICATED REPAIR AND SPLICES IAW SRM 53-2-2, TREATED AND PRIMED IAW SRM 51-1-8. INSTALLED NEW LONGERON SECTION WITH FASTENERS IAW SRM 53-4Apr 26, 1996 · N8969U · Doug DC862 · Fuselage Main, Longeron/StringerSDR 96ZZZX2665Skin · dentedFOUND DURING C-CHECK, FUSELAGE AREA UNDER RUDDER HAS MAJOR DENTS IN SKIN. REMOVED AND REPLACED SKIN SEGMENT IAW DER 950087-0699.Apr 26, 1996 · N8969U · Doug DC862 · Fuselage Main, Plate/SkinSDR 96ZZZX2664Longeron · corrodedDURING C-CHECK, FOUND LONGERON 30R BETWEEN STATIONS 1530 TO 1606 HAS LEVEL 2 CORROSION. REMOVED AND REPLACED LONGERON IAW SRM 51-1-2, SRM 51-1-20D, SRM 51-1-8.Apr 26, 1996 · N8969U · Doug DC862 · Fuselage Main, Longeron/Stringer
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