Douglas DC-8-73F

Service difficulty reports · 15,471

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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 = 'DC873F'
  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 IXXA0500068SLongeron · corrodedDURING A ROUTINE C CHECK INSPECTION FOUND RT FUSELAGE LONGERON 24 CORROSION DAMAGE BETWEEN STA 920.00 AND STA 960.000. REPAIR ACCOMPLISHED REMOVAL OF CORROSION. FOUND OUT OF LIMITS. CLEANED, TREATED AND PRIMED. FABRICATED ANGLES. CLEANED, TREATED AND PRIMOct 11, 2004 · N606AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR IXXA0500067SFitting · corrodedDURING A ROUTINE C-CHECK INSPECTION FOUND RT FUSELAGE LONGERON 24 FITTING FRAME HAS CORROSION DAMAGE ON LOWER SIDE AT STA 960.000. REPAIR ACCOMPLISHED REMOVAL OF THE CORRODED AREA AND FOUND OUT OF LIMITS. FABRICATED NEW FITTING. FABRICATED SPLICES, DOUBLER Oct 11, 2004 · N606AL · Doug DC873F · Fuselage Main, Attach FittingsSDR IXXA0500066SPlate · damagedDURING A ROUTINE C CHECK INSPECTION, FOUND LT WING EXTENDED LEADING EDGE OUTBOARD VANE PLATING INTERIM REPAIR STA XOLDO 67.000. REPAIR ACCOMPLISHED REMOVAL OF FASTENERS AND EXISTING INTERIM REPAIR. REMOVED THE DAMAGED SKIN AREA AND PERFORMED NDT INSPECTION. Oct 11, 2004 · N606AL · Doug DC873F · Wing, Plate/SkinSDR IXXA0500065SPlate · damagedDURING A ROUTINE C CHECK INSPECTION, FOUND LT OUTER WING OUTBOARD EXTENDED LEADING EDGE PLATING WITH INTERIM REPAIR AT STA XFS 710.000. REPAIR ACCOMPLISHED REMOVAL OF ALL FASTENERS WITHIN THE REPAIR AREA AND THE EXISTION INTERIM REPAIR. REMOVED THE DAMAGED SOct 11, 2004 · N606AL · Doug DC873F · Wing, Plate/SkinSDR IXXA0500064SSkin · crackedDURING A ROUTINE C CHECK INSPECTION FOUND TAIL SECTION FUSELAGE EXTERNAL SKIN CRACKED .75 INCH STA 1755.000-L-13 TO L14. REPAIR ACCOMPLISHED REMOVAL OF FASTENERS WITH THE REPAIR AREA AND EXISTING REPAIR DOUBLER. REMOVED DAMAGED SECTION. PERFORMED NDT INSPECOct 11, 2004 · N606AL · Doug DC873F · Fuselage Main, Plate/SkinSDR IXXA0500060SFrame · crackedDURING A ROUTINE C CHECK INSPECTION, FOUND RT FUSELAGE STRUCTURE MAIN CARGO COMPARTMENT ZEE FRAME CRACK DAMAGE AROUND STA FS 260.000, L-20 RT. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED FRAME SEGMENT. CLEANED, TREATED AND PRIMED AREA. FABRICATED FRAME SEGMENT AOct 11, 2004 · N606AL · Doug DC873F · Fuselage Main, FrameSDR IXXA0500059SSkin · corrodedDURING A ROUTINE C CHECK INSPECTION, INTERIM REPAIR ON FUSELAGE EXTERIOR SKIN FROM FS 685.000 - 779.000 L-35 LT TO L-34 RT AND CORROSION DAMAGE. REPAIR ACCOMPLISHED REMOVAL OF ALL FASTENERS WITHIN THE REPAIR AREA. REMOVED CORROSION AND FOUND OUT OF LIMITS. Oct 11, 2004 · N606AL · Doug DC873F · Fuselage Main, Plate/SkinSDR IXXA0500058SLongeron · crackedDURING A ROUTINE C CHECK INSPECTION, FOUND CRACKED L-34 RT AFT CARGO COMPARTMENT STA FS1400.00 TO FS 1420.000. REPAIR ACCOMPLISHED REMOVAL OF CRACKED LONGERON SEGMENT. CLEANED, TREATED AND PRIMED AREA. FABRICATED SPLICE FILLING LONGERON. PERFORMED HEAT TREOct 11, 2004 · N606AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR IXXA0500057SFitting · damagedDURING A ROUTINE C CHECK INSPECTION, LT FUSELAGE LONGERON 24 FITTINGS FRAME REMOVED AND INSTALLED FOR NR 3484 AT STA 940.000. REPAIR ACCOMPLISHED REMOVAL OF FITTING IN ORDER TO GAIN ACCESS FOR REPAIR. FABRICATED SPLICES, DOUBLER AND FILLERS. HEAT TREATED DOOct 11, 2004 · N606AL · Doug DC873F · Fuselage Main, Attach FittingsSDR IXXA0500056SPressure Panel · corrodedDURING A ROUTINE C CHECK INSPECTION, FOUND CORROSION DAMAGE ON RT FUSELAGE NOSE SECTION PRESSURE PANEL BETWEEN STA FS 8.00 AND STA FS -67.00, RBL 28.78 TO RBL 56. REPAIR ACCOMPLISHED REMOVAL OF FASTENERS AND CORROSION. FOUND OUT OF LIMITS, REMOVED DAMAGED SEOct 11, 2004 · N606AL · Doug DC873F · Fuselage Main, BulkheadSDR IXXA0500055SWeb · crackedDURING A ROUTINE C CHECK, RT FUSELAGE WELL MLG WEB CRACK DAMAGE BETWEEN STA Y=857.125 AND XCW=25.000. REPAIR ACCOMPLISHED, REMOVED FASTENERS, REMOVED WEB DAMAGED SEGMENT. PERFORMED NDT INSPECTION. FABRICATED NEW WEB SEGEMENT AND EXTERNAL REPAIR DOUBLER AND Oct 11, 2004 · N606AL · Doug DC873F · Fuselage Miscellaneous StructureSDR IXXA0500054SSkin Panel · corrodedDURING A ROUTINE C CHECK INSPECTION, INTERIM REPAIR FOUND ON LOWER SURFACE OF LT OUTBOARD FLAP STA XF 420.000. REPAIR ACCOMPLISHED REMOVAL OF SKIN WITH THE INTERIM REPAIR ON IT. FABRICATED NEW SKIN PLUS FINGER DOUBLER. BONDED FINGER DOUBLER ON SKIN. CLEANEDOct 11, 2004 · N606AL · Doug DC873F · Trailing Edge FlapsSDR IXXA0500053SFloorbeam · crackedDURING A ROUTINE C CHECK INSPECTION, TEE CRACK DAMAGE WAS FOUND RT FUSELAGE STRUCTURE MLG COMPARTMENT AROUND STA 960.000. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED SECTION. FABRICATED TEE ANGLE, HEAT TREATED AND PERFORMED NDT INSPECTION. FABRICATED SPLICES. AOct 11, 2004 · N606AL · Doug DC873F · Fuselage Main, Floor BeamSDR IXXA0500052SFloorbeam · crackedDURING A ROUTINE C CHECK INSPECTION, CRACK DAMAGE WAS FOUND AT LT FUSELAGE STRUCTURE MAIN CARGO COMPARTMENT FLOORBEAM LOWER SIDE CRACK DAMAGE AT STA FS 980.000 LBL 40. REPAIR ACCOMPLISHED REMOVED OF "T" ANGLE SEGMENT, CLEANED, TREATED AND PRIMED AREA. FABRICAOct 11, 2004 · N606AL · Doug DC873F · Fuselage Main, Floor BeamSDR IXXA0500051SFrame · corrodedDURING A ROUTINE C CHECK INSPECTION, FOUND CORROSION DAMAGE ON RT FUSELAGE STRUCTURE MAIN CARGO COMPARTMENT ZEE FRAME AROUND STATION 240.000, L-33R AND L-34R. REPAIR ACCOMPLISHED THE REMOVAL OF THE CORRODED FRAME SEGMENT. FABRICATED NEW FRAME SEGMENT AND SPLOct 11, 2004 · N606AL · Doug DC873F · Fuselage Main, FrameSDR IXXA0500050SFloorbeam · crackedDURING A ROUTINE C CHECK INSPECTION MAIN CARGO COMP BEAM WEB CORROSION & 2 INCH CRACK STA 920.000 LBL 64-69". REPAIR ACCOMPLISHED REMOVAL OF CORROSION AND FOUND OUT OF LIMITS. REMOVED DAMAGED AREA ON BEAM. FABRICATED FILLER REPAIR AND REPAIR ANGLES. CLEANEOct 11, 2004 · N606AL · Doug DC873F · Fuselage Main, Floor BeamSDR IXXA0500049SSkin · damagedDURING A ROUTINE C CHECK INSPECTION, RT WING INBOARD VANE SLOT HAS INTERIM REPAIR AT STA XILD 7095.00. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED SECTION. PERFORMED NDT INSPECTION. FABRICATED EXTERNAL REPAIR DOUBLER, FILLER, AND INTERNAL DOUBLER. CLEANED, TREATOct 11, 2004 · N606AL · Doug DC873F · Wing, Plate/SkinSDR IXXA0500047SSkin · corrodedDURING A ROUTINE C-CHECK INSPECTION, FOUND RT FUSELAGE NOSE SECTION STRUCTURE FLIGHT COMPARTMENT HAS DAMAGE FROM CORROSION AT STA -67.000. REPAIR ACCOMPLISHED. REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED THE CORRODED FRAME SEGMENT AND FABRICATED A NEOct 11, 2004 · N606AL · Doug DC873F · Fuselage Main, Plate/SkinSDR IXXA0500046SPressure Panel · corrodedDURING A ROUTINE C CHECK INSPECTION, LT FUSELAGE NOSE SECTION PRESSURE PANEL CORROSION DAMAGE BETWEEN STA FS 8.00 AND STA FS -67.00 LBL 40.30 TO LBL 56.00. REPAIR ACCOMPLISHED. REMOVED FASTENERS WITHIN REPAIR AREA. REMOVED THE CORROSION AND FOUND OUT OF LIMOct 11, 2004 · N606AL · Doug DC873F · Fuselage Main, BulkheadSDR IXXA0500040SPlate · corrodedDURING A ROUTINE C CHECK INSPECTION, RT HORIZONTAL STAILIZER OUTBOARD LEADING EDGE UPPER PLATING CORROSION DAMAGE BETWEEN STA XFS 172.000 AND XFS 335.000. REPAIR ACCOMPLISHED. REMOVED FASTENERS AND CORROSION. FOUND OUT OF LIMITS, REMOVED CORROSION, CLEANEDOct 11, 2004 · N606AL · Doug DC873F · Horizontal Stabilizer, Tab StructureSDR UPS04843456Rib · crackedINSPECTION TYPE: C3, RIGHT CENTER L/E RIB (LOWER) CRACKED AT XFS 335. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW DC-8 SRM 57-3-0 AND 51-1-20D.Oct 11, 2004 · N755UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS04843348Eadi · failedELECTRICAL BURNING SMELL FROM F/O'S SIDE DURING APPROACH FOR APPROX 10 - 15 SECONDS. ALL FLUORESCENT LIGHTS WERE OFF. TURNED ON ALL LIGHTS, RAN BOTH PACKS, OPERATED ALL NAVIGATION COMPT, INSPECTED ALL WIRES AT F/O'S INSTRUMENT PANEL, NO ELECTRICAL BURNING SMOct 8, 2004 · N866UP · Doug DC873F · Magnetic CompassSDR DHL2004809008Engine · flamed outENGINE NR 4 FLAMED OUT AT FL 370, RAN ENGINE FAILURE EMERGENCY. CHECK LIST FOLLOWED BY THE ENGINE INFLIGHT START, BUT NO LIGHT OFF DESCENDED TO FL250 TRIED ANOTHER ATTEMPT TO START WITH NO LIGHT OFF. STILL NO LIGHT OFF. TROUBLESHOT PER CFM 71-00-00. PERFOROct 8, 2004 · N809DH · Doug DC873F · Engine (Turbine/Turboprop)SDR UPS04843311Battery Pack · inoperativeEMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK. OPS CHECK GOOD PER REF DC-8 MM CH 33.Oct 6, 2004 · N811UP · Doug DC873F · Emergency LightingSDR DHL2004801561Bracket · crackedLT WING NR 1 ALT TANK BOOSTER PUMP BRACKET CRACKED (FWD). PERFORMED MAJOR REPAIR IAW DWG W51-R11, FAA FORM 8110-3 DATED 10-04-04. REMOVED CRACKED BRACKET IAW SRM 57-1-0 PG.1, SRM 51-1-21 PG.1, SRM 51-1-20D PG.21, SRM 51-3-0 PG.1. FABRICATED NEW BRACKET (AL70Oct 5, 2004 · N801DH · Doug DC873F · Wing, Attach FittingsSDR UPS04843279Wire · damagedINSPECTION TYPE:N/A FLT DECK EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK AND REPAIRED WIRE TO PIN 9 OF CONNECTOR P1-1345, OP CHECK'S GOOD PER MM 33-50-01-2.Oct 5, 2004 · N802UP · Doug DC873F · Light System WiringSDR DHL2004801558Skin · corrodedAFT ACCY COMPT. INTERNAL SKIN CORRODED, STA 1640.000 TO STA. 1660.000, L-26 - L-27R PERFORMED MAJOR REPAIR IAW DWG W51-R04 FAA FORM 8110-3 DATED 10-01-04. REMOVED REPAIR DOUBLER IAW DWG W51-R04. REMOVED CORROSION IAW SRM 51-1-8 PAG. 17-18. FOUND OUT OF LIMITOct 3, 2004 · N801DH · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2004801550Skin · damagedITEM REF. NR. 2127: RT CTR L/E HAS INTERIM REPAIR AT XFS 304.000 (LWR. PART). PERFORMED MAJOR REPAIR IAW DWG W51-R10, FAA FORM 8110-3 DATED 09-28-2004. REMOVED INTERIM REPAIR IAW DC8 SRM 51-1-21 PG.1, SRM 51-1-20D PG.21, DC8 SRM 51-3-0 PG.1, DWG W51-R10. PERFOSep 30, 2004 · N801DH · Doug DC873F · Wing, Plate/SkinSDR DHL2004801551Skin · damagedCRT L/E HAS INTERIM REPAIR AT XFS 347.750 RT (LWR PART). PERFORMED MAJOR REPAIR IAW DWG W51-R09, FAA FORM 8110-3 DATED 09-28-2004. REMOVED INTERIM REPAIR IAW DWG W51-R09. CUT OUT DAMAGED SECTION IAW DWG W51-R09. PERFORMED NDT INSP IAW DC8 NDT SPM PART 06-1Sep 29, 2004 · N801DH · Doug DC873F · Wing, Plate/SkinSDR DHL2004801555Plate · wornRT OTBD FLAP L/E UPPER PLATING WORN AT XF 226.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG W51-R05 FAA FORM 8110-3 DATED 09-28-04. REMOVED DAMAGED SKIN SEGMENT IAW SRM 51-1-21, SRM 51-3-0. FABRICATED NEW SKIN SEGMENT (2024-T3AL 0.071) INTERNAL SPLICE Sep 29, 2004 · N801DH · Doug DC873F · Trailing Edge FlapsSDR DHL2004801559Skin · crackedDURING POSITIVE CHECK FOUND 1.000 CRACK IN NR 1 PYLON FRONT LWR SECTION (STA. XW 487.000 - 508.977 CANT, S-63) PERFORMED MAJOR REPAIR IAW MFG NR 1-OG81S, FAA FORM 8110-3 DATED 09-10-04. REPAIR SKETCH JCT03432. REMOVED FASTENERS IAW SRM 51-1-20D PG.21. CUT OUSep 29, 2004 · N801DH · Doug DC873F · Nacelle/Pylon, Plate/SkinSDR UPS04843219Pump · leakingNR 3 ENGINE HYDRAULIC LEAK. TROUBLESHOT & FOUND PT LEAKING IN NR 3 ENG PYLON & LEAKING INTO DRAIN LINES, TO DRAIN MAST. REMOVED AND REPLACED PART. OPS CK'D GOOD, LEAK CK'D GOOD, PERFORMED ENG RUN, & HYD SYS OP'S OF FLIGHT CONTROLS. SVC'D HYD RES PER MM 12-Sep 29, 2004 · N880UP · Doug DC873F · Hydraulic Pump (Electric/Engine), MainSDR IXXA0500037SRib · crackedDURING A ROUTINE C CHECK INSPECTION, FOUND LT STUB WING NR 1 STRUCTURE RIB WITH CRACK DAMAGE AT STA XS 520.000. REPAIR ACCOMPLISHED, REMOVED CRACKED RIB. FABRICATED RIB AND PERFORMED HEAT TREATMENT. PERFORMED NDT INSPECTION. CLEANED, TREATED AND PRIMED ARESep 27, 2004 · N606AL · Doug DC873F · Wing, Rib/BulkheadSDR IXXA0500036SFitting · crackedDURING A ROUTINE C CHECK INSPECTION, FOUND RT MAIN LANDING GEAR FRAME FITTING CRACK DAMAGE AT STA 98.000, BETWEEN L-19R AND L-24. REPAIR ACCOMPLISHED. REMOVED THE CRACKED FITTING, CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING PER DOUGLAS STRUCTURASep 27, 2004 · N606AL · Doug DC873F · Fuselage, Landing Gear Attach FittingsSDR DHL2004801556Fitting · crackedITEM REF. NR. 0988: AFT ACCY COMPARTMENT FLOORBEAM CEILING FITTING CRACKED 0.500 AT STA. 660.000. REMOVED CRACKED FITTING IAW SRM 51-3-0 PG.1. SRM 51-1-21 PG.1. FABRICATED NEW FITTING (AL7075-T7351) IAW DWG 4333996. PERFORMED NDT INSPECTION IAW NDT SPM PART 0Sep 27, 2004 · N801DH · Doug DC873F · Fuselage Main, Attach FittingsSDR DHL2004801553Skin · wornITEM REF. NR. 1130: LT OB FLAP L/E UPPER PART PLATING WORN, XF 345.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG R51-R08, FAA FORM 8110-3 DATED 09-24-2004. REMOVED FASTENERS IAW SRM 51-1-21. TRIMMED OUT DAMAGED SKIN SEGMENT IAW DWG W51-R08. FABRICATED NESep 27, 2004 · N801DH · Doug DC873F · Trailing Edge FlapsSDR DHL2004801544Fitting · crackedAFT CARGO COMPT STOP FITTING CRACKED 1.000, STA 1240.000, L-24L TO L-27L. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-21 PG 1, DC8 SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW FITTING IAW DC8 SRM 51-1-21 PG 1, DC8 SRMSep 27, 2004 · N801DH · Doug DC873F · Fuselage Main, Attach FittingsSDR DHL2004801554Plate · wornRT OTBD FLAP L/E UPPER PLATING WORN, XF 213.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG W51-R03, FAA FORM 8110-3 DATED 09-24-2004. REMOVED DAMAGED SKIN SEGMENT IAW SRM 51-1-21, DWG W51-R03. FABRICATED NEW SKIN SEGMENT (2024-T3AL 0.040), INTERNAL SPLISep 27, 2004 · N801DH · Doug DC873F · Trailing Edge FlapsSDR DHL2004801543Fitting · corrodedAFT CARGO COMPT FLOOR SUPPORT FITTING CORRODED, STA 1260.000, L-34R TO L-35R. REMOVED CORROSION FROM FLOOR SUPPORT FITTING IAW DC8 SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW DC8 SRM 53-2-0 PG 2P. REMOVED FLOOR SUPPORT FITTING IAW DC8 SRM 51-1-21 PG 1, DC8Sep 27, 2004 · N801DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2004801560Rib · crackedRUDDER RIB CRACKED 1.000 ZR 105.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 55-1-0 PG.1, DWG 5656226. REMOVED CRACKED RIB IAW SRM 51-1-21 PG. 1. FABRICATED NEW RIB IAW SRM 55-6-1 PG.4 FIG.2 SHEET 2 DWG 5656226, SRM 51-1-4 PG.1. DPS 3.69-4. PERFORMED HSep 27, 2004 · N801DH · Doug DC873F · Rudder Miscellaneous StructureSDR DHL2004801557Fitting · crackedAFT ACCY COMPT SPLICE FITTING HAS CRACKS 1.000, 0.500 STA. 640.000 TO STA. 660.000, L-32R. PERFORMED MAJOR REPAIR IAW SRM 53-2-0 PG.1, DWG 5800471. REMOVED CRACKED SPLICE FITTING IAW SRM 51-1-20D PG. 21. FABRICATED SPLICE FITTING (AL7075-T651) IAW DWG 580047Sep 27, 2004 · N801DH · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS04843200Battery Pack · inoperativeINSPECTION TYPE:N/A, EMERGENCY EXIT LIGHTS INOP. ALL SWITCHES & BREAKERS WERE OFF PRIOR TO TEST. REPLACED BATTERY PACK, OPS CHECK OK.Sep 27, 2004 · N812UP · Doug DC873F · Emergency LightingSDR DHL2004801552Doubler · damagedITEM REF. NR. 1131: LT IB FLAP L/E UPPER PLATING HAS INTERIM REPAIR, XW 85.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG W51-R07, FAA FORM 8110-3 DATED 09-24-2004. REMOVED INTERIM REPAIR IAW SRM 51-1-21. TRIMMED OUT DAMAGED AREA IAW DWG W51-R07. FABRICASep 26, 2004 · N801DH · Doug DC873F · Trailing Edge FlapsSDR IXXA0500039SFloorbeam · damagedDURING A ROUTINE C CHECK INSPECTION, FOUND LT FUSELAGE AFT CENTER SECTION FLOORBEAM INTERIM REPAIR STA 1560.000, LBL 45 INCH. REPAIR ACCOMPLISHED, REMOVED INTERIM REPAIR. PERFORMED BLEND OUT ON DAMAGE AREA, FOUND OUT OF LIMITS. FABRICATED FILLER AND REPAIR Sep 24, 2004 · N606AL · Doug DC873F · Fuselage Main, Floor BeamSDR IXXA0500038SFloorbeam · corrodedDURING A ROUTINE C CHECK INSPECTION, FOUND TH FUSELAGE FORWARD CENTER SECTION FLOORBEAM CAP UPPER CORROSION DAMAGE STA 857.000, LBL 32 INCH. REPAIR ACCOMPLISHED. REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED THE CORRODED AREA AND FABRICATED FILLER AND Sep 24, 2004 · N606AL · Doug DC873F · Fuselage Main, Floor BeamSDR DHL2004801541Fitting · crackedUPPER CUSP EXTRUSION FITTING CRACKED 1.000, STA 857.000 L-19R. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D PG 9.Sep 24, 2004 · N801DH · Doug DC873F · Fuselage Main, Attach FittingsSDR DHL2004801540Access Door · damagedLT WING ACCESS DOOR NR 583F HOLES ELONGATED. REMOVED ACCESS DOOR NR 583F IAW DC8 SRM 51-1-21 PG 1. FABRICATED NEW ACCESS DOOR (7075T6 0.080) IAW DC8 SRM 57-2-0 PG 1. CLEANED, TREATED AND PRIMED INNER SIDE OF ACCESS DOOR IAW DC8 SRM 51-1-8B. INSTALLED NEW ASep 23, 2004 · N801DH · Doug DC873F · Wing, Plate/SkinSDR DHL2004801539Bracket · crackedRT WING NR 4 ALT TANK BOOSTER PUMP BRACKET CRACKED (AFT) REF 505B ACCESS DOOR. REMOVED AND REPLACED CRACKED BRACKET ON RT WING NR 4 ALT TANK BOOSTER PUMP REF 505B ACCESS DOOR IAW SRM 51-1-20D PG 9, SRM 51-3-0 PG 1.Sep 23, 2004 · N801DH · Doug DC873F · Wing, Attach FittingsSDR DHL2004801538Doubler · crackedNR 4 ENGINE LT SIDE T/R INTERNAL STRUCTURE DOUBLER CRACKED 10.000 AT 3 O'CLOCK POSITION, STA 202.000. REMOVED CRACKED DOUBLER IAW SRM 51-1-21 PG 1. FABRICATED DOUBLER (AL2024-T3 0.050) IAW MM 78-30-00 PG 836 FIG 812. CLEANED, TREATED AND PRIMED IAW MM 78-30Sep 23, 2004 · N801DH · Doug DC873F · Engine Thrust ReverserSDR IXXA0500035SRib · wornDURING A ROUTINE C CHECK INSPECTION, FOUND RT STUB WING NR 4 STRUCTURE RIB WEAR DAMAGE AT STA XS 520.000. REPAIR ACCOMPLISHED, REMOVED WORN RIB. FABRICATED RIB AND PERFORMED HEAT TREATMENT. PERFORMED NDT INSPECTION. CLEANED, TREATED AND PRIMED. INSTALLED Sep 22, 2004 · N606AL · Doug DC873F · Wing, Rib/Bulkhead
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