N803DH

Service difficulty reports · 573

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N803DH' AND registry_match = 'registration'
  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 DHL2005803522Floorbeam · misdrilledITEM REF. NR. 039049: MAIN CARGO COMPT. WING CTR SECTION FLOORBEAM UPPER FLANGE HOLE MISDRILLED STA 940.000 LBL 32.500 INCH (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 11/28/05, DWG AA33-53-R08 REV JR DATE 11/18/05. REMOVED FASTENERS IAW SRDec 3, 2005 · N803DH · Doug DC873 · Fuselage Main, Floor BeamSDR DHL2005803541Skin · crackedEXTERIOR FUSELAGE SKIN HAS THREE CRACKS OF 0.75 INCH APPROX AT STA 160.000 L-36 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-4-1 FIG. 5C, MFG DWG NR5779934. REMOVED CRACKED PLATING IAW SRM 51-1-21, SRM 51-1-20D. FABRICATED NEW PLATING (AL2014T6 0.050 INCNov 30, 2005 · N803DH · Doug DC873 · Fuselage Main, Plate/SkinSDR DHL2005803520Structure · crackedITEM REF. NR. 033485: LT OB SLAT UPPER DOOR CRACKED (CTR DOOR). REMOVED AND REPLACED CTR DOOR ON LT OB SLAT UPPER DOOR IAW MM 27-80-2 PG. 201-203. FOR OPS CHECK SEE NR 038928.Nov 29, 2005 · N803DH · Doug DC873 · Leading Edge DevicesSDR DHL2005803536Bracket · brokenITEM REF. NR. 033548: LT IB AILERON BRACKET BROKEN (NR 2 HINGE) (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PAGE 1. REMOVED DAMAGED BRACKET IAW SRM 51-1-21, SRM 51-3-0, SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW BRANov 28, 2005 · N803DH · Doug DC873 · AileronsSDR DHL2005803540Fitting · crackedITEM REF NR 039051: NR 4 ALT TANK S-64 END CRACKED 1 INCH STA XRS 445.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-2 FIG. 3D TR# 57-86. REMOVED FASTENERS IAW SRM 51-1-20D. FABRICATED REPAIR ANGLE (EXTRUSION AND 101342003 0.090") IAW SRM 57-2-2 FIG. Nov 28, 2005 · N803DH · Doug DC873 · Wing Miscellaneous StructureSDR DHL2005803521Channel · crackedITEM REF. NR. 033296: LT MLG W/W CHANNEL UPPER AFT CORNER CRACKED 0.250 INCH, FS 978.000. REMOVED CRACKED CHANNEL IAW SRM 51-1-21. FABRICATED NEW CHANNEL (AL 7075T6 0.063 INCH) IAW SRM 57-2-0 PG. 1. CLEANED, TREATED AND PRIMED AREA AND CHANNEL IAW SRM 51-1-8BNov 28, 2005 · N803DH · Doug DC873 · Fuselage Miscellaneous StructureSDR DHL2005803550Door Frame · misrepairedFWD PASSENGER DOOR FWD UPPER JAMB CORNER HAS A REPAIR NOT ACCORDING TO DWG NR SR08530021. PERFORMED MAJOR REPAIR IAW AD2000-20-08, S/B DC8 53-075, DOUGLAS DWG SR08530021, DOUGLAS DWG 5750776. REMOVED EXISTING REPAIR IAW SRM 51-1-21, SRM 51-1-20D, SRM 51-1-21Nov 25, 2005 · N803DH · Doug DC873 · Fuselage Main, StructureSDR DHL2005803552Door Frame · unknownACCOMPLISH REPAIR MODIFICATION ON FWD PASSENGER DOOR JAMB CORNERS IAW AD2000-20-08, SB 53-075, SERVICE REWORK DWG SR08530021. DOCUMENT ALL ACTIONS IN THE NR, AIRCRAFT LOG, 337 FORM (MAJOR REPAIR). PERFORMED MAJOR REPAIR ON JAMB CORNERS(4) OF FWD PASSENGER DONov 25, 2005 · N803DH · Doug DC873 · Fuselage Main, StructureSDR DHL2005803529Cap · crackedITEM REF. NR. 032491: ANTENNA DOPPLER COMPT. CAP 1 INCH CRACK AT STA -99.000. REMOVED CRACKED CAP IAW SRM 51-1-21 PAGE 1, SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW CAP IAW SRM 51-1-21, SRM 51-1-20D, SRM 51-3-1 PG. 2. FOR CANov 25, 2005 · N803DH · Doug DC873 · Fuselage Miscellaneous StructureSDR DHL2005803518Fitting · crackedITEM REF. NR 033026: AFT CARGO COMPT. SPLICE FITTING CRACKED 2 INCHES STA 1040.000 - STA 1060.000 L-31L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PAGE 1. REMOVED CRACKED SPLICE FITTING IAW SRM 51-1-21, SRM 51-1-20D. CLEANED, TREATED AND PRIMED ARENov 24, 2005 · N803DH · Doug DC873 · Fuselage Miscellaneous StructureSDR DHL2005803519Fitting · crackedITEM REF. NR. 038721: EMPENNAGE SPLICE FITTING CRACKED 1 INCH STA 1766.000 L-17 RT (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG. 1. REMOVED CRACKED SPLICE FITTING IAW SRM 51-1-21, SRM 51-3-0. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTANov 21, 2005 · N803DH · Doug DC873 · Fuselage Miscellaneous StructureSDR DHL2005803516Fitting · crackedMAIN CARGO COMPT L-10L SPLICE FITTING CRACKED 3 INCHES STA 902.000 - 909.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED SPLICE FITTING IAW SRM 51-1-20D, SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLNov 21, 2005 · N803DH · Doug DC873 · Fuselage Miscellaneous StructureSDR DHL2005803517Repair · crackedRT WING OB STUB WING LWR EXTERNAL SKIN REPAIR DOUBLER CRACKED 0.500 IN XW 485.000. PERFORMED MAJOR REPAIR IAW SRM 57-2-1A FIG. 1 PG. 3. REMOVED EXTERNAL REPAIR DOUBLER AND INTERNAL REPAIR DOUBLER IAW SRM 51-1-21, SRM 51-1-20D. FABRICATED EXTERNAL REPAIR DOUBLENov 20, 2005 · N803DH · Doug DC873 · Wing, Plate/SkinSDR DHL2005803513Seat Track · damagedCOCKPIT F/E'S AFT SEAT TRACK HAS ELONGATED HOLES. REMOVED AND REPLACED F/E'S AFT SEAT TRACK IAW SRM 51-3-0 PG 1, SRM 51-3-1 PG 2A (TORQUE). REFER TO JC 8-25-40-002 FOR OPS CHECK.Nov 20, 2005 · N803DH · Doug DC873 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2005803506Angle · crackedITEM REF NR 033540: RT WING CTR L/E INTERCOSTAL JOINT ANGLE TO FORMER CRACKED XS 454.976. REMOVED CRACKED ANGLE IAW SRM 51-3-0. FABRICATED NEW ANGLE (AL7075T6 0.063") IAW SRM 57-2-0 PG. 1. CLEANED, TREATED AND PRIMED AREA AND ANGLE IAW SRM 51-1-8B. INSTALLED NNov 18, 2005 · N803DH · Doug DC873 · Wing Miscellaneous StructureSDR DHL2005803514Panel · wornLT INBOARD FLAP UPPER PANEL PLATING WORN 2 INCHES APPROX, STA XW 104.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-7-1 FIG 1. REMOVED DAMAGED PANEL PLATING IAW SRM 57-1-0, SRM 51-1-21. FABRICATED NEW PLATING (AL 2024T3 0.025) AND BONDED FINGER DOUBLNov 17, 2005 · N803DH · Doug DC873 · Trailing Edge FlapsSDR DHL2005803511Stiffener · crackedITEM REF NR 033271: FWD ACCY COMPT LT FWD PRESSURE BULKHEAD STIFFENER CRACKED 1 INCH STA 8.000. REMOVED CRACKED STIFFENER IAW SRM 51-1-21, SRM 51-1-20D. FABRICATED NEW STIFFENER (ALCLAD 7075"0" 0.071") IAW SRM 53-3-3 PG. 11. HEAT TREATED FROM 7075"0" TO 7075T6Nov 17, 2005 · N803DH · Doug DC873 · Fuselage Miscellaneous StructureSDR DHL2005803509Skin · corrodedITEM REF NR 033464: RUDDER SKIN DELAMINATED AT STA ZR 166.656 AND LEVEL 2 CORROSION (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 55-6-1 FIG. 1. REMOVED DAMAGED PANEL PLATING IAW SRM 55-1-0, SRM 51-1-21. REMOVED CORROSION FROM RUDDER SKIN AT ZR 166.656 IAW SRNov 17, 2005 · N803DH · Doug DC873 · Rudder, Plate/SkinSDR DHL2005803508Stiffener · crackedITEM REF NR 033272: FWD ACCY COMPT RT FWD PRESSURE BULKHEAD STIFFENER CRACKED 1.500 INCHES STA 8.000. REMOVED CRACKED STIFFENER IAW SRM 51-1-21, SRM 51-1-20D. FABRICATED NEW STIFFENER (ALCLAD 7075"0" 0.071") IAW SRM 53-3-3 PG. 11. HEAT TREATED FROM 70750" TO 7Nov 17, 2005 · N803DH · Doug DC873 · Fuselage Miscellaneous StructureSDR DHL2005803504Frame · crackedITEM REF NR 033451: RT WING CTR LE LWR FORMER CRACKED 1 INCH XFS 347.750. PERFORMED STOP HOLE ON CRACK END AND FABRICATED ANGLE DOUBLER (AL7075T6 0.040") IAW SRM 57-2-0 PG. 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANNov 17, 2005 · N803DH · Doug DC873 · Wing, Longeron/StringerSDR DHL2005803512Drive Link · crackedRIGHT OUTBOARD FLAP DRIVE LINK ASSY AT STA XF 219.498 HAS THREE CRACKS: I/B LUG J-POINT 3.500 INCH LENGTH CRACK, O/B LUG J-POINT 0.500 INCH LENGTH CRACK AND REAR LUG J-POINT 3.000 INCH LENGTH CRACK. REMOVED AND REPLACED RT OUTBOARD FLAP DRIVE LINK ASSY AT STNov 16, 2005 · N803DH · Doug DC873 · Trailing Edge Flap Control SystemSDR DHL2005803510Fitting · crackedITEM REF NR 033357: MAIN CARGO COMPT FITTING CRACKED 3.500 INCHES STA 680.000 L-11R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG.1. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IANov 16, 2005 · N803DH · Doug DC873 · Fuselage Miscellaneous StructureSDR DHL2005803507Skin · wornITEM REF NR 038897: LT WING INBD FLAP PLATING UPPER PART WORN 1" XW 104.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG. 1. REMOVED DAMAGED PLATING IAW SRM 51-1-21. FABRICATED NEW PLATING (AL 2024T3 0.040") IAW SRM 57-7-1 FIG. 1 ITEM D. CLEANED, TNov 16, 2005 · N803DH · Doug DC873 · Trailing Edge FlapsSDR DHL2005803505Skin · wornITEM REF NR 032704: RT OUTBD FLAP UPPER SURFACE WORN (STA XF 203.000-210.000) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 57-7-1 FIG. 4, TR 57-94. REMOVED DAMAGED PLATING IAW SRM 57-1-0 PG. 1, SRM 51-1-21. FABRICATED NEW PLATING (AL 2024T3 0.040") IAW SRM 57-Nov 16, 2005 · N803DH · Doug DC873 · Trailing Edge FlapsSDR DHL2005803502Floor Panel · corrodedITEM REF. NR. 033228: MAIN CARGO COMPT INTERIOR FLOOR PANEL SUPPORT CORRODED, STA 1726.000 RBL 30. REMOVED CORROSION IAW SRM 51-1-8 PG. 17-18. MEASURED THICKNESS 0.090". BLEND OUT 0.024", REMAINING MATERIAL 0.066". FOUND OUT OF ALLOWABLE LIMITS IAW SRM 53-2-0 Nov 16, 2005 · N803DH · Doug DC873 · Fuselage Floor PanelSDR DHL2005803503Fitting · crackedITEM REF. NR. 033307: MAIN CARGO COMPT SPLICE FITTING CRACKED 5.500 INCHES, STA 857.000 L-1 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG. 1. REMOVED CRACKED SPLICE FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLENov 14, 2005 · N803DH · Doug DC873 · Fuselage Miscellaneous StructureSDR DHL2005803500Floor Panel · corrodedITEM REF. NR. 033352: MAIN CARGO COMPT. FLOOR PANEL CORRODED, STA 0440.000 LBL 56. REMOVED CORROSION FROM FLOOR PANEL STA 1440.000 LBL 56" IAW SRM 51-1-8 PG. 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG. 2P. CUT OUT DAMAGED SECTION AND FABRICATED DOUBLER (7075Nov 11, 2005 · N803DH · Doug DC873 · Fuselage Floor PanelSDR DHL2005803501Floor Panel · corrodedITEM REF NR 033351: MAIN CARGO COMPT. FLOOR PANEL CORRODED, STA 1360.000 LBL 56". REMOVED CORROSION IAW SRM 51-1-8 PG. 17-18 FLOOR PANEL THICKNESS 0.071". BLEND OUT 0.035", REMAINING MATERIAL 0.036". FOUND OUT OF ALLOWABLE LIMITS IAW SRM 53-2-0 PG. 2P. TRIMMEDNov 10, 2005 · N803DH · Doug DC873 · Fuselage Floor PanelSDR DHL2005803515Fitting · crackedMAIN CARGO COMPT INTERIOR SPLICE FITTING CRACKED 2 INCHES STA 902.000 - STA 909.000 L-6R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED SPLICE FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. INSTNov 7, 2005 · N803DH · Doug DC873 · Fuselage Main, Attach FittingsSDR DHL2005803002Proximity Sensor · malfunctionedDURING PREFLIGHT PERFORMED GEAR UNSAFE LIGHT CHECK LEFT DOOR UNSAFE LIGHT WOULD NOT ILLUMINATE DURING CHECK. ITEM TRANSF TO DMI NR 21967 IAW MEL 32-14 CAT "A"3.) REF DMI #21967 DURING PREFLIGHT PERFORMED GEAR UNSAFE LIGHT CHECK LEFT DOOR UNSAFE LIGHT WOULD NAug 6, 2005 · N803DH · Doug DC873 · Landing Gear Position and WarningSDR DHL2005803001Shutoff Valve · failedSTART VALVE OPEN LIGHT ILLUMINATED NEAR TOP OF CLIMB, OIL PRESSURE LIGHT ILLUMINATED AND ENGINE WAS SHUTDOWN WITH 10 PSI OF OIL PRESSURE ON GAUGE AND 0 OIL QUANTITY SHUTDOWN NR 3 ENGINE AT 22:05. FOUND STARTER FAILED WHICH CAUSED OIL LOSS. REMOVED AND REPLACJan 15, 2005 · N803DH · Doug DC873 · Engine StarterSDR DHL2004803001Engine · malfunctionedSHUTDOWN NR 4 ENG DUE TO LOSS OF OIL QUANTITY NOTE PSI WAS 28 OIL QUANTITY WAS .5 QUART ENG OIL TEMP WAS 85 ENG WINDMILLED FOR APPROX 25 MINS COMPLETED ABNORMAL PROCEDURES NOTE AFTER ENG WAS SHUT DOWN OIL QUANTITY. REMOVED AND REPLACED NR 4 ENG PER DC-8 TASK Nov 19, 2004 · N803DH · Doug DC873 · Engine (Turbine/Turboprop)SDR DHL2004803551Clip · crackedNR 2 MAIN TANK CLIP CRACK 2.000, STA XRS 22.750 S-1. REMOVED CRACKED CLIP IAW DC8 SRM 51-1-20D PG 21. FABRICATED NEW CLIP (7075-T651) IAW EA 5740-018, DWG 4647424. HEAT TREATED IAW DC8 SRM 51-1-1 PG 13-17. PERFORMED NDT INSP IAW NDT SPM PART 08-00.02.07. May 19, 2004 · N803DH · Doug DC873 · Wing Miscellaneous StructureSDR DHL2004803552Angle · corrodedLEFT WING REAR SPAR L-ANGLE CORRODED, STA XCW 46.000. REMOVED CORRODED L-ANGLE IAW DC8 SRM 51-1-20D PG 21, DC8 SRM 51-3-0 PG 1-3. REMOVED CORROSION IAW DC8 SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW DC8 SRM 57-2-0 PG 16. FABRICATED NEW L-ANGLE (7075-T651May 19, 2004 · N803DH · Doug DC873 · Wing Miscellaneous StructureSDR DHL2004803547Clip · crackedNR 2 MAIN TANK LWR SPAR CLIP CRACKED 1.500 AT STA XW -6.000. REMOVED AND REPLACED CRACKED CLIP ON NR 2 MAIN TANK LWR SPAR, XW -6.000 IAW DC8 SRM 51-1-20D PG 9-21.May 16, 2004 · N803DH · Doug DC873 · Wing Miscellaneous StructureSDR DHL2004803548Spar Cap · crackedBOLT HOLE OUTBD END OF LT WING INBD LWR AUX SPAR CAP WITH 1.000 AND 2.250 LENGTH CRACKS IN IT (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 57-1-0 PG 1. REMOVED CRACKED LT INBD LWR AUX SPAR CAP IAW DC8 SRM 51-1-20D PG 21, DC8 SRM 51-3-0 PG 1. CLEANED, May 16, 2004 · N803DH · Doug DC873 · Wing SparSDR DHL2004803550Fitting · crackedLOWER AUX SPAR CAP, FITTING CRACKED 2.000 P/N 4778052-1 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 57-1-0 PG 1, EA 5320-014, DWG 4778052. REMOVED CRACKED FITTING IAW SRM 51-3-0 PG 1. FABRICATED NEW FITTING (7075-T6 51) IAW EA 5320-014, DWG 4778052. May 15, 2004 · N803DH · Doug DC873 · Wing SparSDR DHL2004803553Splice · crackedLT WING LWR REAR SPAR CAP SPLICE TEE 1.000 CRACK, STA XRS 74.869 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 57-1-0 PG 1, EA 5710-13, DWG 5640364. REMOVED CRACKED SPLICE TEE IAW DC8 SRM 51-1-20D PG 21, DC8 SRM 51-3-0 PG 1. FABRICATED NEW SPLICE TEE, May 15, 2004 · N803DH · Doug DC873 · Wing Miscellaneous StructureSDR DHL2004803546Panel · delaminatedLT WING T/E LWR HONEYCOMB PANEL INTERIOR AND EXTERIOR SKIN DELAMINATED (STA XF 219.000-339.000). REMOVED AND REPLACED HONEYCOMB PANEL TO LT WING INBD T/E (STA XF 219.000-339.000) IAW DC8 SRM 51-3-0 PG 1.May 12, 2004 · N803DH · Doug DC873 · Wing, Plate/SkinSDR DHL2004803545Fitting · crackedFWD ACCESSORY COMPT END FITTING CRACKED 2.000 AT STA 8.000, L-33R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 53-1-0 PG 1. REMOVED CRACKED END FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED END FITTING (NMay 12, 2004 · N803DH · Doug DC873 · Fuselage Miscellaneous StructureSDR DHL2004803549Angle · corrodedMAIN CARGO COMPT PRESSURE PANEL ATTACH ANGLE CORRODED AT STA 857.125 RBL 29 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 51-2-1 PG 8-14. REMOVED CORROSION FROM PRESSURE PANEL ATTACH ANGLE AT STA 857.125 RBL 29 IAW DC8 SRM 51-1-8 PG 17-18. FOUND OUT OFMay 5, 2004 · N803DH · Doug DC873 · Fuselage Miscellaneous StructureSDR DHL2004803544Skin · corrodedLT WING OUTBOARD L/E INNER SECTION CORRODED, STA XFS 710.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 PG 11. TRIMMED OUT DAMAGED SECTION IAW ED EDV43-1, DWG V4Apr 22, 2004 · N803DH · Doug DC873 · Wing, Plate/SkinSDR DHL2004803540Skin · corrodedOUTER PLATING CORROSION DAMAGE TO RT INNER WING CENTER L/E SLOT UPPER SIDE AROUND STA XFS 422.750 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 PG 11. TRIMMED OUT DApr 22, 2004 · N803DH · Doug DC873 · Wing, Plate/SkinSDR DHL2004803543Skin · corrodedLT WING OUTBOARD L/E INNER SECTION CORRODED, STA XW 485.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 PG 11. TRIMMED OUT DAMAGED SECTION IAW ED EDV43-6, DWG V43Apr 22, 2004 · N803DH · Doug DC873 · Wing, Plate/SkinSDR DHL2004803542Skin · corrodedRIGHT WING CTR L/E UPPER SURFACE SHOWS CORROSION AT STA XW 257.500 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW ED EDV43-7, DWG V43-R07. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D, SRM 51-3-0 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18, FOUND OUApr 22, 2004 · N803DH · Doug DC873 · Wing, Plate/SkinSDR DHL2004803541Skin · corrodedRT WING INBOARD SLOT L/E UPPER SKIN CORRODED AT XILD 42.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG V43-R03, ED EDV43-3. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21, SRM 51-3-0 PG 1. TRIMMED OUT DAMAGED AREA IAW DWG V43-R03, ED EDV43-3Apr 22, 2004 · N803DH · Doug DC873 · Leading Edge DevicesSDR DHL2004803539Skin · wornFUSELAGE EXTERIOR SKIN SURFACE WORN (STA FS. 314.000-327.000, L-31R TO L-32R) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW ED EDV43-4, DWG V43-R04. REMOVED FASTENERS IAW SRM 51-1-21 PG.1, SRM 51-1-20D PG. 21, SRM 51-3-0 PG.1. TRIMMED OUT DAMAGED SECTION IAW ED EDApr 22, 2004 · N803DH · Doug DC873 · Fuselage Main, Plate/SkinSDR DHL2004803538Vane · elongatedLT WING IB. VANE SLOR HOLES ELONGATED STA XS 247.000. PERFORMED MAJOR REPAIR IAW ED EDV43-9, DWG V43-R09. REMOVED FASTENERS IAW SRM 51-1-21 PG.1, SRM 51-3-0 PG.1, SRM 51-1-20D PG.21. TRIMMED OUT DAMAGED SECTION IAW ED ECV43-9, DWG V43-R09. PERFORMED NDT INSP.Apr 22, 2004 · N803DH · Doug DC873 · Leading Edge DevicesSDR DHL2004803537Skin · corrodedRT WING CTR L/E EXTERIOR SURFACE SHOWS CORROSION AT STA. XW 257.500. PERFORMED MAJOR REPAIR IAW ED NR EDV43-5, DWG V43-R05. REMOVED FASTENERS IAW SRM 51-1-21 PG.1, SRM 51-3-0 PG.1. REMOVED CORROSION IAW SRM 51-1-8 PG. 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-Apr 22, 2004 · N803DH · Doug DC873 · Wing, Plate/SkinSDR DHL2004803536Skin · corrodedLT WING OB L/E OUTER SECTION CORRODED, STA. XFS 710.000. REMOVED FASTENERS IAW SRM 51-1-21 PG.1, SRM 51-1-20D PG. 9, SRM 51-3-0 PG.1. REMOVED CORROSION IAW SRM 51-1-8 PG. 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 PG.9. TRIMMED OUT DAMAGED SECTION IAW ED EDV4Apr 22, 2004 · N803DH · Doug DC873 · Wing, Plate/Skin
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