Douglas DC-8-73F

Service difficulty reports · 15,471

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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"

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SDR DHL2003801003Seal1) SUBSTANTIAL FUEL LEAK FROM ACCESS PANEL INBOARD OF #1 PYLON.2) FOUND GAMMA SEAL TORN AT #1 MAIN FUEL MANIFOLD INBOARD OF #1 PYLON. REPLACED SEALS AND LEAK CHECKED OK PER M/M 28-20-0.Feb 27, 2003 · N801DH · Doug DC873F · Aircraft Fuel Distribution SystemSDR DHL2003873003Window · stuckF/O'S SLIDING WINDOW WILL NOT OPEN. FOUND WINDOW JAMMED. UNSTUCK WINDOW. OPS CHECKED GOOD PER M/M 56-10-3.Feb 27, 2003 · N873SJ · Doug DC873F · Flight Compartment WindowsSDR DHL2003873002Hose · kinkedFIRST OBSERVERS 02 MASK DOES NOT ALLOW O2 TO FLOW IN NORMAL ONLY IN EMERGENCY. FOUND O2 MASK HOSE KINKED BEHIND REGULATOR. UNKINKED AS REQUIRED. FIRST OBSERVERS 02 MASK OPS CHECKED NORMAL IAW DC8 M/M 35-10-8.Feb 26, 2003 · N873SJ · Doug DC873F · Crew Oxygen SystemSDR DHL2003806004Smoke Detector1) #4 SMOKE DETECTOR WON'T TEST.2) REMOVED AND REPLACED #4 SMOKE DETECTOR WITH SERVICEABLE ASSEMBLY IAW M/M 26-16-5. OPS CHECKED GOOD.Feb 26, 2003 · N806DH · Doug DC873F · Smoke DetectionSDR DHL2003805004Seat Belt1) F/O'S SEAT BELT WILL NOT UNLATCH.2) REMOVED AND REPLACED F/O'S LAP SEAT BELT PER M/M 25-11-1.Feb 26, 2003 · N805DH · Doug DC873F · Flight Compartment EquipmentSDR UPS03840238Slide · looseESCAPE SLIDE NOT SECURE AND GIRT BAR NOT TOTALLY IN SLIDE SLEEVE. SECURED ESCAPE SLIDE TO BRACKET WITH CAMLOCK FASTENER. REPOSITIONED GIRT BAR IN SLIDE SLEEVE. OK TO CONTINUE.Feb 25, 2003 · N866UP · Doug DC873F · Escape SlideSDR UPS03840237Wire · brokenEMERGENCY LIGHTS DISARMED LIGHT INOP WITH SWITCH DISARMED. REPAIRED BROKEN WIRE AT TERMINAL A2 ON SWITCH S1-327 REF WDM 33-50-01. OPS CHECK GOOD.Feb 25, 2003 · N808UP · Doug DC873F · Light System WiringSDR UPS03840236Battery Pack · inoperativeON PREFLIGHT EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY PACK IAW DC8 MM 33-50-01. EMERGENCY EXITS OPS CK NORMAL.Feb 24, 2003 · N803UP · Doug DC873F · Emergency LightingSDR IXXA0300018OConnector · looseDURING FINAL APPROACH FOR LANDING INTO PHIK. CREW NOTED NOSE LANDING GEAR DOWN AND LOCKED LIGHTS WERE NOT ILLUMINATED. USING VISUAL INDICATOR CREW VERIFIED GEAR WAS SAFE. ADDITIONALLY CREW PERFORMED FLY-BY OF CONTROL TOWER AND AGAIN CONFIRMED GEAR WAS IN SAFeb 23, 2003 · N605AL · Doug DC873F · Landing Gear Position and WarningSDR DHL2003604750Skin · damagedLT WING CTR. L/E VANE SLOT HOLES ELONGATED AT XOLDI 6.224 PERFORMED MAJOR REPAIR IAW EODHL-030544, ED-3301. REMOVED FASTENERS IAW SRM 51-1-21 PG.1, SRM 51-1-20D PG.21. TRIMMED OUT ELONGATED HOLES SKIN AREA IAW EODHL-030544, ED-3301. PERFORMED EDDY CURRENT INSPFeb 22, 2003 · N604AL · Doug DC873F · Wing, Plate/SkinSDR DHL2003805003Bulb1) #6 AND #8 SMOKE DETECTORS DO NOT TEST.2) SMOKE DETECTORS #6 AND #8 DEFERRED INOPERATIVE PER MEL 26-6-1 DMI #12078.3) REF. DMI #12078 SMOKE DETECTOR #6 AND #8 INOPERATIVE "DO NOT TEST".4) REMOVED AND REPLACED #6 AND #8 SMOKE DETECTOR LIGHT BULBS. OPS CHEFeb 22, 2003 · N805DH · Doug DC873F · Smoke DetectionSDR IXXA0300017OWarning Light · illuminatedAFTER DEPARTURE FROM TOL EN ROUTE TO LAX. DURING UPLATCH CHECK CREW NOTED DOORS NOT LATCHED LIGHT ILLUMINATED. CREW FOLLOWED PROCEDURE AND CYCLED LANDING GEAR. DOORS NOT LATCHED LIGHT REMAINED ILLUMINATED. APPROX 15 MINUTES LATER LIGHT EXTINGUSHED. FLIGHTFeb 21, 2003 · N606AL · Doug DC873F · Door Warning SystemSDR UPS03840213Spar · crackedINSPECTION TYPE: C3, PERFORM LT WING AND RT WING FWD SPAR INSPECTION OF LWR SPAR CAP PER EO DC8-5 710-14184-C AS REQUIRED. REAMED 1 DISCREPANT HOLE ON L/W TO .3230, PERFORMED HFEC AND NO CRACKS NOTED PER DAC SPM 06-10-01.003. CHECKED SPAR THICKNESS AT .689 Feb 21, 2003 · N805UP · Doug DC873F · Wing SparSDR IXXA0300016OLubrication Unit · faultyAFTER DEPARTURE FROM PDX DURING CRUISE EN ROUTE TO EWR CREW NOTED OIL PRESSURE INDICATION FLUCTUATING ON THE NR 2 ENGINE. POWER WAS RETARDED, OIL PRESSURE WARNING ILLUMINATED AND NR 2 ENGINE WAS SHUTDOWN. CREW ELECTED TO CONTINUE TO TOL AND MADE AN UNEVENTFUFeb 20, 2003 · N606AL · Doug DC873F · Turbine Engine Oil SystemSDR DHL2003804537Skin · crackedITEM REF N/R 2660; iterim repair on fwd lwr. corner of the aft pax entry door ref srm53-2-0 pgs. 125/126 fig. 18 sheet 2m (major repair) corr: performed major repair iaw srm53-2-0 fig 18 , removed interim repair from aft pax entry door fwd. lwr. corner iawFeb 19, 2003 · N804DH · Doug DC873F · Fuselage Structure (General)SDR UPS03840208Fitting · crackedINSPECTION TYPE: C3, O/B AFT STRINGER 51 END FT CRACKED AT XRS 74.000 NR 2 MAIN. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D AND 51-3-0. DRILLED LOCATED DEBURRED NEW FITTING IAW DC8 SRM 51-1-24. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D AND 51-3-0. LEAFeb 19, 2003 · N805UP · Doug DC873F · Stabilizer Control SystemSDR DHL2003804779Panel · delaminatedLT WING T/E LOWER PANEL EXTERNAL SKIN DELAMINATED 5.000 INCH AT STA. XW106.000. R & R LT WING T/E LOWER PANEL IAW SRM 51-3-0Feb 17, 2003 · N804DH · Doug DC873F · Wing, Plate/SkinSDR 2003804501Fitting · crackedITEM : REF. N/R 1557 AFT CARGO COMPT.: FITTING @ STA. 1240.000 WITH .5000 CRACK CORR: REMOVED DAMAGED FITTING IAW SRM 51-1-20D PG. 21 , FABRICATED NEW FITTING AND DOUBLERS (7075.T651) IAW SRM 53-2-0 FIG 2D , CLEANED ,TREATED , AND PRIMEDFITTING AND DOUBLERSIFeb 17, 2003 · N804DH · Doug DC873F · Fuselage Main, StructureSDR DHL2003804873Skin · delaminatedRT WING T/E UPPER PANEL SKIN DELAMINATED ( STA XW 5.000-47.000) R & R RT WING UPPER T/E PANEL (STA. XW5.000-47.000) IAW SRM 51-3-0 PG. 1Feb 16, 2003 · N804DH · Doug DC873F · Wing, Plate/SkinSDR DHL2003804906Panel · delaminatedLT WING - NR 728 CTR WING LOWER PANEL INNER SKIN DELAMINATED, STA 779.000 - STA 810.000. REMOVED AND REPLACED CTR WING LWR PANEL NR 728 IAW SRM 51-3-0 PG 1.Feb 15, 2003 · N804DH · Doug DC873F · Wing, Center BoxSDR DHL2003804890Skin · corrodedLT WING - L/E UPPER SKIN CORRODED AROUND STA XW 257.500 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EODHL-030108, ED-3214. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-0 PG 16. TRIMMED Feb 15, 2003 · N804DH · Doug DC873F · Wing, Plate/SkinSDR DHL2003804782Angle · crackedRT WING CENTER L/E FORMER AND ANGLE DOUBLER UPPER PART CRACKED.500 INCH. AT XFS 420.000. REMOVED CRACKED ANGLE DOUBLER IAW SRM 51-1-21 PG. 1 , SRM 51-1-20D PG. 21 STOP DRILLED FORMER CRACK IAW SRM 57-2-0 PG. 9-10 FERFORMED HEAT TREATMENT IAW SRM 51-1-1 PG. 1-Feb 15, 2003 · N804DH · Doug DC873F · Leading Edge DevicesSDR DHL2003804556Skin · corrodedLT WING L/E UPPER SKIN CORRODED BETWEEN STA. XFS291.5000 AND XFS 304.000 CORR: PERFORMED MAJOR REPAIR IAW EO DHL 030108 , ED-3214. REMOVED FASTNERS IAW SRM51-1-21 PG. 1 REMOVED CORROSION IAW SRM 51-1-8 PG. 17-18, FOUND OUT OF LIMITS IAW SRM57-2-0 PG 16 TRIMMEDFeb 15, 2003 · N804DH · Doug DC873F · Wing, Plate/SkinSDR DHL2003804896Longeron · crackedLWR FUSE INNER STRUCTURE, L-17L CRACKED 3.00, STA 1772.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, SRM 53-5-3, PG 16, FIG 5, SRM 51-2-0 FIG 50, DPS 4.710. REMOVED CRACKED LONGERON IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAWFeb 14, 2003 · N804DH · Doug DC873F · Fuselage Main, Longeron/StringerSDR DHL2003804908Frame · crackedFWD ACCY COMPT FRAME CRACKED 1.000 INCH, STA 55.000 L-23L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-0 PG 2U/2V FIG 2 (SHEET 2). REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. CUT OUT DAMAGED FRAME SEGMENT IAW SRM 53-2-0 PG 2U/2V FIG 2Feb 14, 2003 · N804DH · Doug DC873F · Fuselage Main, FrameSDR DHL2003804780Panel · delaminatedRT WING T/E UPPER PANEL EXTERNAL SKIN DELAMINATED STA. XW5.000-32.000. R & R RT WING T/E UPPER PANEL IAW SRM 51-3-0 PG. 1.Feb 14, 2003 · N804DH · Doug DC873F · Wing, Plate/SkinSDR DHL2003804778Frame · crackedFWD ACCESSORY BAY FRAME CRACKED 1.00 INCH, STA. 55.000 L23R. PERFORMED MAJOR REPAIR IAW 53-2-0 PG. 20/21 FIG. 2 (SHEET 2)., REMOVED FASTNERS IAW SRM 51-1-21 PG. 1 , SRM51-1-20D PG 21. CUT OUT DAMAGED FRAME SEGMENT IAW SRM 53-2-0 PG. 20/21 SHEET 2 . FABRICATEFeb 14, 2003 · N804DH · Doug DC873F · Fuselage Main, FrameSDR DHL2003804913Panel · delaminatedLT WING UPPER SURFACE T/E UPPER ACCESS PANEL 510 SHOWS EXTERNAL SKIN DELAMINATED STA XA 475.000- XA 507.000. REMOVED AND REPLACED T/E UPPER ACCESS PANEL 510 ON LT WING UPPER SURFACE, STA XA 475.000- XA 507.000 IAW SRM 51-3-0 PG 1.Feb 13, 2003 · N804DH · Doug DC873F · Wing, Plate/SkinSDR DHL2003804551Skin · damaged"C" CARGO DOOR LWR EXTERIOR SKIN WITH 2EACH INTERIM REPAIRS ON IT. (FS 1200.000-1260.000 PERFORMED MAJOR REPAIR IAW EO DHL 030111 , ED-3218. REMOVED FASTNERS IAW 51-1-21 PG. 1. TRIMMED OUT DAMAGED SKIN SEGMENT IAW EO DHL 030111, ED-3218. FABRICATED A REPAIR SKFeb 13, 2003 · N804DH · Doug DC873F · Cargo/Baggage DoorsSDR UPS03840231Skin · crackedINSPECTION TYPE: C1, AFTER REMOVAL OF LEAKING FASTENERS FOUND EXTERNAL DOUBLER AND UPPER WING SKIN CRACKED AT FASTENER HOLE AT XRS 22 AT STRINGER 5. REMOVED DOUBLER, OVERSIZED FASTENER HOLE, NDT VERIFIED NO CRACKS AT HOLE, FABRICATED FREEZE PLUG BUSHINGS, DOFeb 13, 2003 · N811UP · Doug DC873F · Wing, Plate/SkinSDR UPS03840172Connector · damagedRT MLG DOWNLOCK INDICATION INTERMITTENT. EMERGENCY DECLARED. TWO MINUTES RT MLG IND CAME ON ON ITS OWN. LANDED W/O INCIDENT, GEAR PINNED. REMOVED AND REPLACED RT MAIN LANDING GEAR DOWNLOCK SWITCH CONNECTOR PER MM CHAPTER 20, STANDARD PRACTICES CHECKS NORMAFeb 13, 2003 · N807UP · Doug DC873F · Landing Gear Position and WarningSDR DHL2003804888Skin · crackedRT WING T/E UPPER SKIN SURFACE WITH 0.500 INCH CRACK STA XRS.285.000- 305.000. CUT OUT DAMAGED AREA IAW SRM 57-2-0 FIG 2. FABRICATED FILLER (2024-T3 0.032) AND DOUBLER (2024-T3 0.050) IAW SRM 57-2-0 FIG 2. CLEANED, TREATED AND PRIMED FILLER AND DOUBLER IAW Feb 12, 2003 · N804DH · Doug DC873F · Wing, Plate/SkinSDR DHL2003804781Skin · delaminatedLT WING LOWER ACCESS DOOR NR 540 WITH EXTERNAL SKIN DELAMINATED. R & R LT LOWER EXTERNAL ACCESS DOOR NR 540 IAW SRM 51-3-0 PG. 1Feb 12, 2003 · N804DH · Doug DC873F · Wing, Plate/SkinSDR DHL2003804767Panel · crackedLT WING L/E OUTBD SLOT UPPER DOOOR SHOWS FOUR .250 CRACKS BTWN STA XS484.895 AND XS520.168 CORR: R & R LT WING OUTBD SLOT UPPER DOOR BETWEEN XS484.895 AND XS520.168 IAW MM.Feb 12, 2003 · N804DH · Doug DC873F · Wing, Plate/SkinSDR DHL2003804775Fillet · delaminatedLT WING, WING TO FUSELAGE FILLET INNER SKIN DELAMINATED , STA 826.000 - STA. 912.000. R & R PANEL ON LT WING, WING TO FUSELAGE STA. 826.000-STA. 912.000 IAW SRM 51-3-0 PG. 1Feb 12, 2003 · N804DH · Doug DC873F · Aerodynamic FairingsSDR DHL2003804661Skin · crackedFWD PASSENGER DOOR INTERIM REPAIR AT AFT LWR JAMB CORNER STA. 55.00 LT PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 15 REMOVED INTERIM REPAIR IAW SRM 51-1-21 PG. 1 CUT OUT DAMAGED AREA IAW SRM 53-2-0 FIG , FABRICATED FILLER & DOUBLER (7075 T6 0.63) & TRIPLER (7Feb 12, 2003 · N804DH · Doug DC873F · Passenger/Crew DoorsSDR DHL2003804552Skin · crackedRT WING T/E UPPER SKIN SURFACE WITH 1/2 INCH CRACK IN IT. (XRS285.000-305.000) CUT OUT DAMAGED AREA IAW SRM57-2-0 FIG. 2 FABRICATED FILLER (2024T3,032) & DOUBLER (2024T3.050) IAW SRM57-2-0 FIG. 2. CLEANED , TREATED AND PRIMED FILLER & DOUBLER INNER SURFACEFeb 12, 2003 · N804DH · Doug DC873F · Wing, Plate/SkinSDR DHL2003804536Rib · crackedITEM REF. N/R 1430 PERFORMED MAJOR REPAIR IAW SRM 55-1-0 PG.1 . REMOVED UPPER CAP-AFT DAMAGED RIB IAW SRM51-1-21 PG. 1 , FABRICATED UPPER CAP-AFT RIB (7075-T6)IAW ATM 5-19-00 , DWG. 5654192-1. CLEANED, TREATED AND PRIMED IAW SRM51-1-8B. INSTALLED NEW UPPER CAFeb 12, 2003 · N804DH · Doug DC873F · Horizontal Stabilizer Miscellaneous StructureSDR UPS03840232Floorbeam · corrodedINSPECTION TYPE: C1, FLOORBEAM UPPER FLANGE IS CORRODED BEYOND LIMITS AT STA 1580 AT LBL 5. CUT OUT DAMAGED AREA, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED ANGLE DOUBLER AND FILLER IAW SRM 53-2-0 FIG 1G.Feb 12, 2003 · N811UP · Doug DC873F · Fuselage Main, Floor BeamSDR DHL2003804898Angle · crackedRT WING- CTR L/E TO STUB WING JOINT ANGLE CRACKED 0.500. REMOVED CRACKED JOINT ANGLE IAW SRM 51-1-21 PG 1. FABRICATED JOINT ANGLE (7075-0-0.080) IAW SRM 57-2-0 PG 2. PERFORMED HEAT TREATMENT IAW SRM 51-1-4 PG 1-3, DPS 1-05.3, SRM 51-1-1 PG 1, 17. CLEANED, Feb 11, 2003 · N804DH · Doug DC873F · Wing Miscellaneous StructureSDR DHL2003804895Skin · damagedRT WING CTR L/E LWR PART SHOWS ELONGATED HOLES AROUND STA XS 521.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EODHL-030114, ED-3215. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. BLENDED OUT DAMAGED AREA IAW EODHL-30114,ED-3215. FABRICATED DOUBLER (7075-T6AL-0Feb 11, 2003 · N804DH · Doug DC873F · Wing, Plate/SkinSDR DHL2003804909Skin · crackedLT INBOARD AILERON L/E UPPER SKIN SURFACE WITH 0.500 INCH CRACK AT STA XA.502.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, SRM 57-8-1 PG 2. REMOVED UPPER SKIN ON LT INBOARD AILERON L/E STA XA. 502.000 IAW SRM 51-1-21 PG 1. FABRICATED NEW Feb 11, 2003 · N804DH · Doug DC873F · AileronsSDR DHL2003804776Skin · crackedFWD. SERVICE DOOR- AFT LOWER JAMB CORNER CRACKED 1.562 STA. 190.000. PERFORMED MAJOR REPAIR IAW SRO8530021 , REMOVED FASTNERS IAW SRM 51-1-20D PG. 21 CUT - OUT DAMAGED AREA IAW DWG SR8530021. FABRICATED FILLER AND DOUBLER (7075T6 .063 &TRIPLER (7075T6.080) IAWFeb 11, 2003 · N804DH · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2003804542Former · wornITEM REF. N/R 1727: RH WING L/E OUTBD STUB WING FORMER WORN OUT OF LIMITS XOLDO67.750 (MAJOR REPAIR) CORR: PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1 REMOVED WORN FORMER IAW SRM51-1-20DPG. 21 FABRICATED NEW FORMER (7075 "O" .090) IAW ATM5-19-00 & DRAWING 97532Feb 11, 2003 · N804DH · Doug DC873F · Wing, Rib/BulkheadSDR UPS03840214Doubler · corrodedINSPECTION TYPE: C3, LAP SPLICE BLENDED OUT OF LIMITS L21L/FS 1600. REMOVED DAMAGED SECTION OF CUSP DOUBLER 9750448-29. FAB REPLACEMENT PART, ALODINED, PRIMED & INSTALLED IAW TIMCO REO G09045. FAB FINGER DOUBLER IAW DAC DWG 9750448, ALODINED & PRIMED IAW DFeb 11, 2003 · N805UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS03840202Spar · crackedINSPECTION TYPE:C3 LT WING FRONT SPAR LOWER CAP XFS 7 HAS A CRACK INDICATION FOUND BY HFEC. STOP DRILLED CRACK, FABBED REPAIR ALODINED AND PRIMED INSTALLED REPAIR.Feb 11, 2003 · N805UP · Doug DC873F · Wing SparSDR DHL2003804880Angle · crackedLT STUB WING CTR L/E ATTACH ANGLE AT STA XS 515.750 WITH 2.000 INCH CRACK. REMOVED DAMAGED ANGLE IAW SRM 51-3-0 PAGE 1. FABRICATED ANGLE (7075-T6 AL 0.080) IAW SRM 57-2-0 FIG 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW ANGLE IAW SRM 51-3-Feb 10, 2003 · N804DH · Doug DC873F · Wing Miscellaneous StructureSDR DHL2003804877Skin · corrodedLT WING L/E UPPER SKIN CORRODED AT STA XFS 710.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EODHL 030103, ED-3213. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION ON LT WING L/E UPPER SKIN IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57Feb 10, 2003 · N804DH · Doug DC873F · Wing, Plate/SkinSDR DHL2003804662Vane · damagedLT WING OUTBOARD FLAP VANE SLOT UPPER SKIN HOLE ELONGATED XOLDO67.000. PERFORMED MAJOR REPAIR IAW EO DHL 030109 , ED-3222 REMOVED FASTNERS IAW SRM 51-1-21 PG. 1. TRIMMED OUT DAMAGED SKIN SEGMENT IAW EO DHL 030109 , ED-3222. FABRICATED AN EXTERNAL REPAIR DOUBLFeb 10, 2003 · N804DH · Doug DC873F · Wing, Plate/SkinSDR DHL2003804557Vane · damagedLT WING OUTBD VANE SLOT UPPER SKIN HOLE ELONGATED XOLDO58.000 PERFORMED MAJOR REPAIR IAW EO DHL 030109 ED-3222 . REMOVED FASTNERS IAW SRM 51-1-21 PG 1 TRIMMED OUT DAMAGED SKIN SEGMENT IAW EO DHL030109 , ED-3222. FABRICATED AN EXTERNAL REPAIR DOUBLER (7075T6AFeb 10, 2003 · N804DH · Doug DC873F · Wing Main, Frame Structure
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