Douglas DC-8-73F

Service difficulty reports · 15,471

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  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 UPS06846295Splice · crackedINSPECTION TYPE:C2 LONGERON 24L SPLICE FITTING AT STA 1690 IS CRACKED. REMOVED CRACKED FITTING AT STA 1690 L24L IAW SRM 51-3-0 AND SRM 51-1-21. LOCATED AND DRILLED REPLACEMENT SPLICE FITTING AND INSTALLED AT STA 1690 L24L IAW DWG 4641324, AND SRM 51-01-20D.Feb 11, 2006 · N814UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS06846243Fitting · crackedINSPECTION TYPE:C2 LONG 23R END FITTING AT STA 1698 CRACKED. REMOVED CRACKED END FITTING IAW SRM 51-1-21 AND SRM 51-3-0 LOCATED, DRILLED, AND DEBURRED REPLACEMENT END FITTING IAW DWG 4641324. INSTALLED REPLACEMENT FITTING AT STA 1698 L23R IAW SRM 51-1-20D ANFeb 11, 2006 · N814UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS06846241Fitting · crackedINSPECTION TYPE:C2 LONG END FITTING L30R END FITTING IS CRACKED AT STA 1690. REMOVED END FITTING IAW SRM 51-3-0, LOCATED, DRILLED AND DEBURRED REPLACEMENT END FITTING AT STA 1690 L30R IAW 51-03-02-0,51-01-20D AND SRM 51-03-01.Feb 11, 2006 · N814UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS06846239Splice · crackedINSPECTION TYPE:C2 LONGERON SPLCE FITTING L22L JUST AFT OF STA 1690 IS CRACKED. REMOVED SPLICE FITTING IAW SRM 51-1-21, LOCATED AND DRILLED AND REAMED REPLACEMENT FITTING IAW DWG 4641324. INSTALLED SPLICE FITTING IAW SRM 51-3-0, 51-1-21, 51-1-21D, AND DWG 46Feb 11, 2006 · N814UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS06846173Fitting · crackedFOUND L34L AFT OF STA 1690 HAS POSSIBLE CRACK ON INSIDE OF FITTING. REMOVED AND REPLACED FITTING IAW SRM 51-1-21 AND 51-1-20D.Feb 11, 2006 · N814UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS06846210Door Frame · crackedINSPECTION TYPE:C3 HFEC INSPECTION DETECTED A .500" CRACK ON THE D PIT UPPER AFT DOOR JAMB. CUT OUT DAMAGE AT AFT UPPER CORNER IAW SRM 53-02-00-0. FABRICATED AND INSTALLED REPAIR DOUBLER, TRIPLER, AND FILLERS IAW SRM 53-02-00-0 FIG 21, AND SRM 51-01-20D-0.Feb 10, 2006 · N814UP · Doug DC873F · Fuselage Main, StructureSDR DHL2006804540Skin · damagedINTERIM REPAIR ON FUSELAGE EXTERNAL SKIN STA 65.000 L-27R TO L-28R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-1 FIG. 7 SHEET 1-3. REMOVED EXISTING REPAIR IAW SRM 51-1-21. CUT OUT DAMAGED SECTION AND FABRICATED REPAIR DOUBLER (AL7075T6 0.071 INCH) AND Feb 10, 2006 · N804DH · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2006804541Skin · crackedRT WING LWR SKIN EXTERNAL FASTENER HOLE CRACKED 0.250 INCHES S-64 STA XRS 445.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SB 57-100 FIG. 5 SHEET 2. REMOVED FASTENERS IAW SRM 51-1-20D. CUT OUT DAMAGED SECTION IAW SB 57-100 FIG. 5 SHEET 2. FABRICATED REPAIR DFeb 10, 2006 · N804DH · Doug DC873F · Wing, Plate/SkinSDR UPS06846140Battery Pack · inoperativeEMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY PACK IAW MM 33-50-01-2. OPS CK NORMAL.Feb 10, 2006 · N867UP · Doug DC873F · Emergency LightingSDR DHL2006804543Bolt · crackedLT MLG UPPER TORQUE LINK BOLT THREADED AREA CRACKED 0.500". REMOVED AND REPLACED LT MLG UPPER TORQUE LINK BOLT IAW MM 32-11-4 PG 201. REFER TO JC 8-32-20-007 FOR OPS CHECK.Feb 9, 2006 · N804DH · Doug DC873F · Main Landing Gear Strut/Axle/TruckSDR DHL2006804542Bolt · crackedRT MLG UPPER TORQUE LINK BOLT THREADED AREA CRACKED 0.500". REMOVED AND REPLACED RT MLG UPPER TORQUE LINK BOLT IAW MM 32-11-4 PG. 201. REFER TO JC 8-32-20-007 FOR OPS CHECK.Feb 9, 2006 · N804DH · Doug DC873F · Main Landing Gear Strut/Axle/TruckSDR UPS06846298Spar · crackedINSPECTION TYPE:C2 CRACKS ON I/B WEB SUPPORT ANGLES ON LT HORIZ STAB FRONT SPAR. REMOVED CRACKED UPPER AND LWR T-CAP ANGLES IAW SRM 51-03-00-0. LOCATED AND DRILLED UP REPLACEMENT T-CAP ANGLES AND INSTALLED IAW SRM 51-3-0, 51-3-2, 51-01-21, AND SRM 51-01-20D.Feb 8, 2006 · N814UP · Doug DC873F · Horizontal Stabilizer, Spar/RibSDR UPS06846207Attach Fitting · crackedINSPECTION TYPE:C3 STA 834 L22L FWD ATTACH FITTING CRACKED 2" LONG REMOVED ATTACH FITTING AT STA 834 L22L IAW SRM 51-01-20D-0, REPLACED ATTACH FITTING AT STA 834 L22L FWD IAW DC8 SRM 51-3-2 AND SRM 51-1-20DFeb 8, 2006 · N814UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS06846174Finger Doubler · corrodedINSPECTION TYPE:C2 MAIN CABIN CENTER SUB FLOOR FINGER DOUBLER CORRODED AT STA 960 TO 980 RBL 65. REMOVED FINGER DOUBLER, FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW SRM 53-07-03 FIG 004, 51-01-21, 53-07-03 FIG 4.Feb 8, 2006 · N814UP · Doug DC873F · Fuselage Main, StructureSDR UPS06846158Finger Doubler · corrodedINSPECTION TYPE:C1 MAIN CABIN CENTER SUB FLOOR FINGER DOUBLER CORRODED AT STA 980 LBL 65. REMOVED FINGER DOUBLER IAW SRM 51-1-21, FABRICATED AND INSTALLED FINGER DOUBLER AT STA 980 LBL 65 IAW DWG 5645332, AND SRM 53-2-0 FIG 1F, 51-03-02,51-1-20D.Feb 8, 2006 · N814UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS06846153Angle · crackedINSPECTION TYPE:C1 CRACK AT STA 1766 LONG 4R ON "L" BRACKET. REMOVED DAMAGED ANGLE IAW 51-01-21, FABRICATED AND INSTALLED ANGLE ATTACHED TO AFT PRESS PANEL AT STA 1766, L4R IAW DWG 5773844, AND SRM 51-01-20D-0, 51-1-8.Feb 8, 2006 · N814UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS06846151Finger Doubler · crackedINSPECTION TYPE:C1 CORROSION AND CRACK ON FINGER DOUBLER AT STA -52 TO -64 LBL 17-23. REMOVED FINGER DOUBLER IAW SRM 51-1-21, FABRICATED AND INSTALLED FINGER DOUBLER AT STA -52 TO -64 LBL 17-23 IAW DWG 5612298, AND SRM51-1-21, 51-1-20D.Feb 8, 2006 · N814UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS06846149Finger Doubler · corrodedINSPECTION TYPE:C1 MAIN CABIN SUB FLOOR FINGER DOUBLER CORRODED AT STA 925 LBL65. REMOVED FINGER DOUBLER IAW SRM 51-1-21, FABRICATED AND INSTALLED FINGER DOUBLER AT STA 925 LBL65 IAW SRM 53-07-03,53-07-03-0 AND SRM 51-1-21Feb 8, 2006 · N814UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS06846383Spar Cap · crackedINSPECTION TYPE:C2 LT WHEEL WELL LOWER SPAR CAP HAS A 16 INCH CRACK. REPAIRED LT LWR SPAR CAP FS 857 IAW SRO 8570009.Feb 7, 2006 · N814UP · Doug DC873F · Wing SparSDR UPS06846208Attach Angle · crackedINSPECTION TYPE:C3 RT WW LWR SPAR ATTACH ANGLE CRACKED 1" LONG STA 857.125. MACHINED REPAIR ANGLE IAW DWG 5649893 AND INSTALLED REPAIR ANGLE AT RT WW STA 857.125 IAW SRM 51-1-21 AND SRO 8570009.Feb 7, 2006 · N814UP · Doug DC873F · Fuselage, Wing Attach FittingsSDR DHL2006804539Door · scheduled maintPERFORM PREVENTATIVE MODIFICATION TO FWD LOWER CORNER OF L1 DOOR IAW AD2000-20-08, SB DC8 53-075, SR 085300021. (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW AD2000-20-08, SB DC8 53-075, DOUGLAS DRAWING SR08530021, 5750776. REMOVED FASTENERS IAW SRM 51-1-21. Feb 7, 2006 · N804DH · Doug DC873F · Aircraft StructuresSDR DHL2006804530Angle · crackedRIGHT STUB WING ANGLE CRACKED 1 INCH XOLD 67.000. REMOVED CRACKED ANGLE IAW SRM 51-1-21. FABRICATED NEW ANGLE (AL7075"0" 0.080") IAW SRM 57-3-3 FIG 3. HEAT TREATED NEW ANGLE FROM 7075"0" TO 7075T6 IAW SRM 51-1-1 PG 1-13-17. CLEANED, TREATED AND PRIMED AREAFeb 6, 2006 · N804DH · Doug DC873F · Wing Miscellaneous StructureSDR DHL2006804538Cap · corrodedLT WING INBOARD L/E UPPER PART SLANT PANEL UPPER CAP CORRODED XFS 7.500 - XFS 26.250 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0, BOEING MESSAGE 1-156506024-2. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 FIG 37. Feb 6, 2006 · N804DH · Doug DC873F · Wing Main, Frame StructureSDR DHL2006804534Link · crackedRIGHT MLG LINK NR 7 CRACKED 3.250 INCH LENGTH. REMOVED AND REPLACED RIGHT MLG BRAKE LINK NR 7 IAW MM 32-11-1 PG 401.Feb 6, 2006 · N804DH · Doug DC873F · Main Landing Gear Strut/Axle/TruckSDR DHL2006804535Fitting · crackedMAIN CARGO COMPT FITTING CRACKED 1 INCH STA 680.000 LBL 25". REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-1 PG 2A (TORQUE). REFER TO JC EA53200017-001-D (WO 600Feb 6, 2006 · N804DH · Doug DC873F · Fuselage Main, Attach FittingsSDR DHL2006804536Door · nonePERFORM PREVENTATIVE MODIFICATION TO THE AFT UPPER L1 DOOR CORNER IAW AD2000-20-08, S/B 53-075 AND DWG SR085300021. PERFORMED MAJOR REPAIR IAW AD2000-20-08, SB 53-075, DOUGLAS DRAWING SR08530021, 5750776. REMOVED FASTENERS IAW SRM 51-1-21. FABRICATED REPAIRFeb 6, 2006 · N804DH · Doug DC873F · Aircraft StructuresSDR UPS06846382Spar Cap · crackedINSPECTION TYPE:C2 RT WW LWR SPAR CAP CRACKED 1 INCH LONG RBL 30. REPAIRED LWR SPAR CAP STA 857 RBL 30 IAW SRO 8570009.Feb 4, 2006 · N814UP · Doug DC873F · Wing SparSDR UPS06846157Rib · crackedRT WING OB LE UPPER RIB CRACKED 1/2" LONG XFS 693. STOP DRILLED CRACK IAW SRM 57-02-00, FABRICATED AND INSTALLED REPAIR ANGLE DOUBLER AT UPPER OB RIB RT WING STA XFS 693 IAW SRM 57-02-00, AND SRM 51-1-20D.Feb 3, 2006 · N814UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS06846155Rib · crackedINSPECTION TYPE:C1 RT WING LE UPPER RIB IS CRACKED AT XRS 636. STOP DRILLED CRACK IAW SRM 57-02-00, FABRICATED AND INSTALLED REPAIR ANGLES AND FILLER IAW SRM 57-02-00-0, AND SRM 57-02-00-0.Feb 3, 2006 · N814UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS06846147Rib · crackedINSPECTION TYPE:C1 RT WING OB FLAPWELL RIB IS CRACKED 1/2 INCH LONG STA XRS 204. CUT OUT DAMAGED AREA IAW 57-02-00-0, FABRICATED AND INSTALLED REPAIR ANGLE AND FILLER IAW SRM 57-02-00, 51-3-2 AND SRM 51-1-20DFeb 3, 2006 · N814UP · Doug DC873F · Wing, Rib/BulkheadSDR DHL2006804529Repair · misinstalledNOSE SECTION FUSELAGE EXTERNAL POWER RECEPTACLE ACCESS DOOR JAMB UPPER CORNER HAS NON STANDARD REPAIR STA 30.000 STA 36.000 L-31 L-32R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 01-31-06 DWG AA66-53-R03 REV IR DATED 01-16-06. REMOVED EXFeb 3, 2006 · N804DH · Doug DC873F · Aircraft StructuresSDR DHL2006804525Floorbeam · maint errorMAIN CARGO COMPT FLOORBEAM HOLE MISDRILLED STA 742.250 RBL 32.5 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 01-31-06, DWG AA66-53-R01 REV IR DATED 01-16-06. CUT OUT DAMAGED SECTION AND FABRICATED REPAIR ANGLE AND FILLER (EXTRUSION 7075T6Feb 3, 2006 · N804DH · Doug DC873F · Fuselage Main, Floor BeamSDR DHL2006804533Frame · maint errorMAIN CARGO COMPT FRAME 3EA MISDRILLED HOLES AT STA 220.000 L-10R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 01-31-06, DWG AA66-53-R04 REV IR DATED 01-16-06. CUT OUT DAMAGED SECTION AND FABRICATED REPAIR ANGLE (EXTRUSION BAC 1505-1006477Feb 3, 2006 · N804DH · Doug DC873F · Fuselage Main, FrameSDR DHL2006804532Frame · misdrilledMAIN CARGO COMPT FRAME 3EA MISDRILLED HOLES AT STA 260.000 L-10R. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 01-31-06, DWG AA66-53-R05 REV IR DATED 01-16-06. CUT OUT DAMAGED SECTION AND FABRICATED REPAIR ANGLE (EXTRUSION BAC1505-1006477075T6511) FILLERFeb 3, 2006 · N804DH · Doug DC873F · Fuselage Main, FrameSDR DHL2006804524Doubler · crackedPRIMARY HEAT EXCHANGER ACCESS DOOR JAMB AFT LWR CORNER ACS MODIFICATION DOUBLER CRACKED 0.75" STA -12.000 L-27R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 01-31-06 DWG AA66-53-R02 REV IR DATED 01-16-06. REMOVED FASTENERS IAW SRM 51-1-21Feb 3, 2006 · N804DH · Doug DC873F · Fuselage Main, StructureSDR UPS06846359Skin · crackedRT UPPER WING SKIN CRACKED 1/2" LONG, AT XCW69.500 REAR SPAR AREA. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED 2 DOUBLERS AND 1 FILLER IAW SRM 57-2-1 FIG 20.Feb 2, 2006 · N814UP · Doug DC873F · Wing, Plate/SkinSDR DHL2006804520Fitting · crackedNR 2 MAIN TANK FWD FITTING EXTERNAL PART CRACKED 1 INCH XRS 74.000 S-51 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND APPLIED POLYURETHANE YELLOW COATING IAW SRM 51-1-12 PG 7-12. Feb 2, 2006 · N804DH · Doug DC873F · Wing, Attach FittingsSDR DHL2006804511Fitting · crackedNR 2 MAIN TANK AFT FITTING CRACKED 3 INCHES XRS 74.000 S-51 (EXTERNAL PART) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND APPLIED POLYURETHANE YELLOW COATING IAW SRM 51-1-12 PG 7-12.Feb 2, 2006 · N804DH · Doug DC873F · Wing, Attach FittingsSDR DHL2006804513Fitting · crackedNR 2 MAIN TANK FWD FITTING CRACKED 2 INCHES XRS 74.000 S-51 MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND APPLIED COATING IAW SRM 51-1-12 PG 7-12. APPLIED SEALANT TO FAYING SURFFeb 2, 2006 · N804DH · Doug DC873F · Wing, Attach FittingsSDR DHL2006804509Fitting · crackedNR 2 MAIN TANK AFT FITTING CRACKED 2 INCHES XRS 74.000 S-51 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND APPLIED COATING IAW SRM 51-1-12 PG 7-12. APPLIED SEALANT TO FAYING SURFACFeb 2, 2006 · N804DH · Doug DC873F · Wing, Attach FittingsSDR DHL2006804527Web · crackedRUDDER L/E WEB CRACKED 0.500 INCH STA ZV 295.000. REMOVED CRACKED WEB IAW SRM 51-1-21. FABRICATED NEW WEB (AL2024"0" 0.050") IAW SRM 55-6-1 FIG 2. HEAT TREATED FROM 7075"0" TO 2024T4 IAW SRM 51-1-1 PG 1-13-17. CLEANED, TREATED AND PRIMED AREA AND WEB IAW SFeb 1, 2006 · N804DH · Doug DC873F · Rudder StructureSDR DHL2006804517Bolt · crackedNLG SIDE BRACE RT BOLT S/N 321626 CRACKED 2.000 INCH LENGTH. REMOVED AND REPLACED RT BOLT S/N 321626 ON NLG SIDE BRACE IAW MM 32-21-1 PG 409. REFER TO JC 8-32-20-007 FOR OPS CHECK (NEW BOLT S/N OII012).Feb 1, 2006 · N804DH · Doug DC873F · Nose/Tail Landing GearSDR DHL2006804514Fitting · crackedNR 3 MAIN TANK FITTING CRACKED 3 INCHES XRS 74.869 S-51 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND APPLIED POLYURETHANE YELLOW COATING TO AREA IAW SRM 51-1-12 PG 7-12. APPLIED Feb 1, 2006 · N804DH · Doug DC873F · Wing, Attach FittingsSDR DHL2006804516Splice · crackedMAIN CARGO COMPT LONGERON SPLICE FITTING CRACKED 1 INCH STA 857.125 L-3L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED BATHTUB FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. APPLIED SEALANT TO FAYIFeb 1, 2006 · N804DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2006804510Fitting · crackedNOSE SECTION FUSELAGE FWD FITTING END CRACKED STA 8.000 L-33L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-21, SRM 51-3-0. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFAFeb 1, 2006 · N804DH · Doug DC873F · Fuselage Main, Attach FittingsSDR DHL2006804523Fitting · crackedNR 1 ALT TANK (505B ACCESS DOOR) FITTING CRACKED 1 INCH XRS 428.000 - XRS 463.000 S-59 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 57-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND APPLIED YELLOW COATING TO AREA IAW SRM 51-1Feb 1, 2006 · N804DH · Doug DC873F · Wing, Attach FittingsSDR DHL2006804526Frame · crackedRUDDER L/E FORMER CRACKED 0.500" STA ZV 295.000 CANT. PERFORMED STOP HOLE AND FABRICATED ANGLE DOUBLER IAW SRM 55-2-0 PG 7-8. HEAT TREATED IAW SRM 51-1-1 PG 1-13-17. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLEFeb 1, 2006 · N804DH · Doug DC873F · Elevator StructureSDR UPS06846156Skin · corrodedINSPECTION TYPE:C1 INTERGRANULAR CORROSION 2 1/2" BY 2 1/2" AREA WHERE LWR VERT STAB L/E AND MIDDLE VERT L/E MATE. REMOVED CORROSION IAW SRM 55-02-00-0, CUT OUT AREA IAW SRM 55-02-01. FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 55--2-01-0 FIG 4 AND SJan 31, 2006 · N814UP · Doug DC873F · Vertical Stabilizer, Plate/SkinSDR DHL2006804522Skin · crackedRT RUDDER L/E PLATING CRACKED 3 INCHES STA ZR 257.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 55-6-1 FIG 1 PG 2. REMOVED DAMAGED PLATING IAW SRM 55-1-0, SRM 51-1-21. FABRICATED NEW PLATING (AL2024T3 0.040") IAW SRM 55-6-1 FIG 1 PG 2 ITEM C. CLEANED,Jan 31, 2006 · N804DH · Doug DC873F · Rudder, Plate/SkinSDR DHL2006804528Panel · delaminatedRIGHT WING TOP AND BOTTOM SURFACE WEAR AND INTERNAL PART DELAMINATED ON NR 3 SPOILER. REMOVED AND REPLACED NR 3 RT SPOILER PANEL IAW MM 027-61-1 PG 201-206. REFER TO NR 044174 FOR OPS CHECK.Jan 31, 2006 · N804DH · Doug DC873F · Spoilers
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