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 DHL2003803001B-Nut · crackedNR 4 ENGINE LOST 4 QUARTS OF OIL IN FLIGHT FROM MEX APPROXIMATELY 1/2 QUART EVERY HALF HOUR. FOUND OIL TUBE SUPPLY TGB CRACKED AT B-NUT. REMOVED FOR FABRICATION. NR 4 ENGINE QUIT ON DESCENT. OIL PRESSURE AND TEMPERATURE NORMAL. ENGINE CONTINUED WINDMILLINJan 24, 2003 · N803DH · Doug DC873 · Turbine Engine Oil SystemSDR DHL2002803013Warning Light · false indicationNR 3 FUEL BYPASS LIGHT KEEPS ILLUMINATING IN FLIGHT. RESETS OK, BUT RE-ILLUMINATES WITHIN ONE MINUTE. DEFERRED NR 3 FUEL BYPASS LIGHT PER MEL 73-2-2. REMOVED AND REPLACED NR 3 FUEL FILTER. NO CONTAMINATION PRESENT. DMI 11188 ASSIGNED. SPECIAL PROCEDURE COMPLDec 10, 2002 · N803DH · Doug DC873 · Engine Fuel DistributionSDR DHL2002803012Fuel Filter1) #3 FUEL BYPASS LIGHT ILLUMINATED IN FLIGHT. PERFORMED ABNORMAL PROCEEDURE AND LIGHT EXTINGUISHED. BYPASS LIGHT ILLUMINATED A SECOND TIME AND WOULD NOT EXTINGUISH. FUEL FILTER BYPASS RESET LIGHT INOPERATIVE.2) FOUND #3 ENGINE FUEL FILTER CONTAMINATED. REMODec 7, 2002 · N803DH · Doug DC873 · Engine Fuel PumpSDR DHL2002803011Lamp1) #13 SMOKE DETECTOR WILL NOT TEST.2) DEFERRED PER MEL 26-6-1 DMI #11131.3) RE: DMI #11131 - #13 SMOKE DETECTOR WILL NOT TEST.4) REMOVED AND REPLACED BOTH LAMPS IN #13 SMOKE DETECTOR. SYSTEM CHECKED GOOD PER 26-10-0. CLEARED DMI #11131. PLACARD REMOVED.Dec 4, 2002 · N803DH · Doug DC873 · Smoke DetectionSDR DHL2002803010Seat · damagedFIRST OFFICER'S SEAT UNABLE TO MOVE FORE AND AFT. REPLACED COTTER PIN TO FORE AND AFT ADJUSTMENT ON RT SIDE. OPS CHECKED NORMAL PER M/M 25-11-1.Nov 26, 2002 · N803DH · Doug DC873 · Flight Compartment EquipmentSDR DHL2002803539Panel · delaminatedITEM REF. N/R 0409 : LOWER FUS.- #715 LH LOWER ACCESS PANEL INNER SKIN FLANGE UNBONDEDCORR: R/R #715 LH LOWER ACCESS PANEL ON LOWER FUS. , CTR. WING IAW 51-3-0 PG. 1Oct 28, 2002 · N803DH · Doug DC873 · Fuselage Structure (General)SDR DHL2002803535Panel · delaminatedIITEM REF N/R: 0108 : RH WING LOWER SURFACE T/E LOWER PANEL EXTERNAL SLIN DELAMINATED XRS 162.000 TO XF 219.000 CORR: removed and replaced panel iaw srm 51-1-3Oct 28, 2002 · N803DH · Doug DC873 · Wing, Plate/SkinSDR DHL2002803541Longeron · crackedAFT OF PRESSURE DOME AREA, INTERIOR LONGERON 17 LT AT FS 1766.000 WITH 2 INCH CRACK IN IT PERFORMED MAJOR REPAIR IAW SRM53-1-10. REMOVED DAMAGED LONGERON IAW SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM51-1-8B. INSTALLED NEW LONGERON IAW SRM51-1-21 Oct 23, 2002 · N803DH · Doug DC873 · Fuselage Main, Longeron/StringerSDR DHL2002803540Longeron · crackedITEM REF. N/R: 1842: FUS. AFT OF PRESSURE DOME AREA- INTERIOR-LONGERON 17R@FUS.STA. 1766.000 WITH 1" CRACK IN IT. (MAJOR REPAIR)Oct 23, 2002 · N803DH · Doug DC873 · Fuselage Structure (General)SDR DHL2002803536Fitting · crackedITEM REF N/R: 0470 MAIN CARGO COMPT. - SPLICE FITTING CRACKED .500 @ STA. 759.000 RBL 23 ( MAJOR REPAIR)CORR:PERFORMED MAJOR REPAIR IAW ATM# po111892 , drawing 5750549.REMOVED SPLICE FITTING CRACKED IAW SRM 51-1-20D PG. 21. CLEANED , TREATED , AND PRIMED AREA Oct 20, 2002 · N803DH · Doug DC873 · Fuselage Main, StructureSDR DHL2002803543Skin · corrodedFUSELAGE SKIN CORRODED BETWEEN STA 78.000 AND STA 82.000 , L32 LT TO L33 LT. PERFORMED MAJOR REPAIR IAW EO DHL021002 , ED-3136 , REMOVED FASTNERS IAW SRM51-1-21. REMOVED CORROSION IAW SRM51-1-8, OUT OF LIMITS IAW SRM53-2-0. TRIMMED OUT DAMAGED AREA SKIN SEGMOct 13, 2002 · N803DH · Doug DC873 · Fuselage Main, Plate/SkinSDR DHL2002803547Plate · crackedRT INBD SLOT LE INTERNAL PLATE WITH 2 INCH CRACK IN IT STA XFS 218.000. REMOVED DAMAGED PLATE IAW SRM 57-2-0 FIG 2 FABRICATED NEW PLATE IAW SRM57-2-0 FIG. 2. CLEANED ,TREATED AND PRIMED AREA IAW SRM 51-1-8B INSTALLED NEW PLATE IAW SRM 57-2-0 FIG. 2Oct 12, 2002 · N803DH · Doug DC873 · Leading Edge DevicesSDR DHL2002803542Former · crackedITEM REF. LH WING FORMER CENTRAL LEADING EDGE CRACKED 3" @ STA. XFS347.000 (MAJOR REPAIR).PERFORMED MAJOR REPAIR IAW SRM57-2-20 D PG. 21 STOP DRILLED CRACK IAW SRM 57-2-0 PG. 1-10 FABRICATED DOUBLERS (02EA.)(7075T6AL .071) IAW SRM 57-2-0 PG 9-10 CLEANED , TREOct 10, 2002 · N803DH · Doug DC873 · Fuselage Structure (General)SDR DHL2002803537Skin · dentedITEM REF. N/R: 0179: FUS. EXT. EXTERNAL SKIN DENTED 30.0000 " LONG NEAR L14R STA. 35.000 - STA. -12.000 ( MAJOR REPAIR) CORR: PERFORMED MAJOR REPAIR IAW FAX BOEING DHL-CVG-02-00057H; ED-3135 & ED-3142. REMOVED FASTNERSIAW SRM 51-1-21 PG. 1 , CLEANED , TREATED Oct 10, 2002 · N803DH · Doug DC873 · Fuselage Structure (General)SDR DHL2002803546Fitting · crackedITEM REF. N/R 0819: AFT ACCY COMPT. - FITTING 2" CRACKED, STA. 1766.000 L28L (MAJOR REPAIR)CORR: PERFORMED MAJOR REPAIR IAW SRM53-1-0 PG. 1 REMOVED DAMAGED FITTING IAW SRM51-1-20D PG. 21CLEANED , TREATED , AND AREA IAW SRM51-1-8B. INSTALLED NEW FITTING IAW SRMOct 6, 2002 · N803DH · Doug DC873 · Fuselage Main, Longeron/StringerSDR DHL2002803545Rib · crackedLT WING OUTBD LE FORMER AT STA XRS 597.000 WITH 1/2 INCH CRACK IN IT. STOP DRILLED CRACK IAW SRM 57-2-0 PG. 9-10 FABRICATED RE-INFORCING ANGLE IAW SRM 57-2-0 PG 9-10 CLEANED , TREATED AND PRIMED IAW SRM 51-1-8B INSTALLED REINFORCING ANGLE IAW SRM 57-2-0 PG. 9Sep 29, 2002 · N803DH · Doug DC873 · Wing, Rib/BulkheadSDR DHL2002803525Frame · crackedRT WING L/E FRAME UPPER PART AT STA 680.000 WITH 1/2 INCH CRACK IN IT. REMOVED FASTENERS PER SRM 51-1-21 PG 1. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED REINFORCING ANGLE (2024.T3 AL0.032) PER SRM 57-2-0 PG9-10. CLEANED TREATED AND PRIMED PER SSep 29, 2002 · N803DH · Doug DC873 · Leading Edge DevicesSDR DHL2002803505Frame · crackedRT WING L/E UPPER PART FRAME CRACKED 1/2 IN AT STA 649.000. REMOVED FASTNERS PER SRM 51-121 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED REINFORCING ANGLE (2024.T3 AL 0.32) PER SRM 57-2-0 PG 9-10,51-1-21 PG 1. CLEANED TREATED AND PRIMED PER SRM Sep 29, 2002 · N803DH · Doug DC873 · Leading Edge DevicesSDR DHL2002803531Frame · crackedLT WING CENTRAL L/E FRAME CRACKED 1 INCH AT STA XFS 422.000. REMOVED FASTNERS PER SRM 51-1-20D PG 21. STOP DRILLED 1 INCH CRACK PER SRM 57-20 PG 9-10.FABRICATED A DOUBLER ANGLE (2024T3AL0.032) PER SRM 57-2-0 PG 9-10. CLEANED TREATED AND PRIMED PER SRM 51-1-Sep 27, 2002 · N803DH · Doug DC873 · Leading Edge DevicesSDR DHL2002803530Frame · crackedLT WING CENTRAL L/E FRAME CRACKED AT STA XFS 471.000. REMOVED FASTNERS PER SRM 51-1-20 PG 21. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED DOUBLER ANGLE (2024 T3 AL 0.032) PER SRM 57-2-0 PG 9-10. CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLEDSep 27, 2002 · N803DH · Doug DC873 · Leading Edge DevicesSDR DHL2002803526Frame · crackedRT WING L/E FRAME LOWER PART AT STA 643.000 WITH 1/2 INCH CRACK IN IT. REMOVED FASTNERS PER SRM 51-1-21 PG 1. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED REINFOCING ANGLE (2024.T3 AL0.032) PER SRM 57-2-0 PG9-10. CLEANED TREATED AND PRIMED PER SRSep 27, 2002 · N803DH · Doug DC873 · Leading Edge DevicesSDR DHL2002803524Frame · crackedRT WING L/E FRAME UPPER PART AT STA 649.000 WITH 1/2 INCH CRACK IN IT. REMOVED FASTNESS PER SRM 51-1-21 PG 1. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED REINFORCING ANGLE (2024.T3 AL0.032) PER SRM 57-2-0 PG9-10. CLEANED TREATED AND PRIMED PER SRMSep 27, 2002 · N803DH · Doug DC873 · Leading Edge DevicesSDR DHL2002803523Frame · crackedRT WING L/E FRAME PART AT STA 607.000 WITH 1/2 INCH CRACK IN IT. REMOVED FASTNERS PER SRM 51-1-21 PG 1. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED REINFORCING ANGLE (2024.T3 AL 0.032) PER SRM 57-2-0 PG 9-10. CLEANED TREATED AND PRIMED PER SRM 51-Sep 27, 2002 · N803DH · Doug DC873 · Leading Edge DevicesSDR DHL2002803516Doubler · crackedLT WING CENTER L/E INNER DOUBLER AT STA XFS 435.000 WITH 2 INCH CRACK IN IT. REMOVED DAMAGED DOUBLER PER SRM 51-1-21 PG 1. FABRICATED NEW DOUBLER (7075.T6 AL0.080) PER SRM57-2-0 FIG 2. CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED DOUBLER PER SRM 5Sep 27, 2002 · N803DH · Doug DC873 · Wing Miscellaneous StructureSDR DHL2002803504Frame · crackedRT WING L/E FRAME UPPER PART AT STA 661.000 WITH 1/2 IN CRACK IN IT. REMOVED FASTNERS PER SRM 51-1-21 PG 1. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED REINFOCING ANGLES PER IAW SRM 57-2-0 PG 9-10. CLEANED TREATED AND PRIMED PER SRM 51-1-8B .INSTALSep 27, 2002 · N803DH · Doug DC873 · Leading Edge DevicesSDR DHL2002803503Frame · crackedRT WING L/E FRAME UPPER PART AT STA 620.000, WITH 1/2 IN CRACK IN IT. REMOVED FASTNERS PER SRM 51-1-21 PG 1. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10.FABRICATED REINFOCING ANGLES IAW SRM 57-2-0 PG 9-10.CLEANED TREATED AND PRIMED PER SRM 51-1-8B.INSTALLED NESep 27, 2002 · N803DH · Doug DC873 · Leading Edge DevicesSDR DHL2002803534Frame · crackedLT WING O/B L/E FRAME AT STA XRS 603.750 WITH A 1/2 IN CRACK IN IT. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED REINFORCING ANGLE (2024T3 AL0.032) PER SRM 57-2-0 PG 9-10. CLEAND TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED ANGLE PER SRM 57-2-0 Sep 26, 2002 · N803DH · Doug DC873 · Leading Edge DevicesSDR DHL2002803533Frame · crackedLT WING O/B L/E FRAME AT STA XRS 660.000 WITH A 1 IN CRACK IN IT. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED REINFORCING ANGLE (2024T3 AL0.032) PER SRM 57-2-0 PG 9-10. CLEAND TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED ANGLE PER SRM 57-2-0 PG9-Sep 26, 2002 · N803DH · Doug DC873 · Leading Edge DevicesSDR DHL2002803532Frame · crackedLT WING O/B L/E FRAME AT STA XRS 616.250 WITH A 1/2 INCH CRACK IN IT. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED REINFORCING ANGLE (2024-T3 AL 0.032) PER SRM 57-2-0 PG9-10. CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED REINFORCING ANGLE PESep 26, 2002 · N803DH · Doug DC873 · Leading Edge DevicesSDR DHL2002803529Doubler · brokenLT WING CENTER L/E INTERNAL PART SHOWS DOUBLER BROKEN (2IN) AT XFS 521.250. REMOVED DAMAGED DOUBLER PER SRM 57-2-0 FIG 2. FABRICATED NEW DOUBLER (7075T6AL0.050) PER SRM 57-2-0. CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED DOUBLER PER SRM 57-2-0 ANDSep 26, 2002 · N803DH · Doug DC873 · Wing Miscellaneous StructureSDR DHL2002803527Frame · crackedLT WING O/B L/E FRAME UPPER PART AT STA 635.000 WITH 1/2 INCH CRACK IN IT. REMOVED FASTNERS PER SRM 51-1-21 PG 1. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED REINFORCING ANGLE (2024.T3 AL0.032) PER SRM 57-2-0 PG9-10. CLEANED TREATED AND PRIMED PERSep 26, 2002 · N803DH · Doug DC873 · Leading Edge DevicesSDR DHL2002803522Fitting · crackedAFT CARGO COMPT.SPLICE FITTING WITH 3" CRACK IN IT AT STA 1040.000-1060.000.PREFORMED MAJOR REPAIR PER SRM 53-1-0 PG1.REMOVED DAMAGED FITTING PER SRM51-1-20D PG 21.CLEANED TREATED AND PRIMED PER SRM 51-1-8B.INSTALLED NEW FITTING PER SRM 51-1-20D PG 9 AND 51-1-Sep 26, 2002 · N803DH · Doug DC873 · Cargo CompartmentsSDR DHL2002803521Support · crackedAFT CARGO BAY PRESSURE WALL VERTICAL LINING SUPPORT CRACKED 1/2 INCH AT STA 980.000 L-27H. STOP DRILLED CRACK PER SRM 53-2-0 FIG 7B. FABRICATED DOUBLER (2024 T3 AL0.040) PER SRM 53-2-0 FIG 7B. CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED DOUBLER PSep 26, 2002 · N803DH · Doug DC873 · Fuselage Miscellaneous StructureSDR DHL2002803528Frame · crackedLT WING O/B L/E FRAME UPPER PART AT STA XRS 591.250 WITH 1/2 INCH CRACK IN IT. REMOVED FASTNERS PER SRM 51-1-21 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED REINFOCING ANGLE (2024.T3 AL0.032) PER SRM 57-2-0 PG9-10.CLEANED TREATED AND PRIMED PERSep 26, 2002 · N803DH · Doug DC873 · Leading Edge DevicesSDR DHL2002803517Frame · crackedLT WING O/B L/E FRAME AT STA XRS 610.000 WITH 1/2 INCH. REMOVED FASTNERS PER SRM 51-1-21 PG 9-10. FABRICATED SUPPORT ANGLE (21024 T3 AL0.032) PER SRM 57-2-0 PG 9-10. CLEANED TERATED AND PRIMED PER SRM 51-1-8B. INSTALLED SUPPORT ANGLE WITH NEW FASTNERS PERSep 26, 2002 · N803DH · Doug DC873 · Leading Edge DevicesSDR DHL2002803515Frame · crackedLT WING O/B L/E FRAME AT STA XRS 672.000 WITH 1/2 INCH CRACK IN IT. REMOVED FASTNERS PER SRM 57-2-0 PG 9-10. FABRICATED SUPPORT ANGLE (2024 T3 AL0.032) PER SRM 57-2-0 PG 9-10. CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED ANGLE WITH NEW FASTNERS PSep 26, 2002 · N803DH · Doug DC873 · Leading Edge DevicesSDR DHL2002803514Frame · crackedLT WING O/B L/E FRAME AT STA XRS 622.500 WITH 1/2 INCH CRACK. STOP DRILLED CRACK PER SRM 57-1-0 PG 9-10. FABRICATED REINFOCING ANGLE (2024 T3 0.032) PER SRM 57-2-0 PG 9-10. CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED REINFOCING ANGLE PER SRM 57-Sep 26, 2002 · N803DH · Doug DC873 · Leading Edge DevicesSDR DHL2002803513Skin · crackedRT WING O/B FLAP UPPER SKIN CRACKED 1/2 INCH AT XW 212. PREFORMED MAJOR REPAIR PER SRM 57-1-0 PG 1. REMOVED DAMAGED SKIN PER SRM 51-1-21 PG 7. FABRICATED NEW SKIN (2024.T3.AL 0.40) PER SRM57-7-1 PG 2. CLEANED TREATED AND PRIMED PER SRM 51-1-8B.INSTALLED NEWSep 26, 2002 · N803DH · Doug DC873 · Trailing Edge FlapsSDR DHL2002803512Frame · crackedLT WING CENTER L/E INTERNAL PART SHOWS FRAME CRACKED 1 INCH AT XFS 385.250. REMOVED FASTNERS PER SRM 51-1-20D PG 21. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED NEW DOUBLER ANGLE (2024T3AL0.032)PER SRM 57-2-0 PG 9-10.CLEANED TREATED NAD PRIMED IAWSep 26, 2002 · N803DH · Doug DC873 · Leading Edge DevicesSDR DHL2002803511Frame · crackedLT WING CENTER L/E INTERNAL PART SHOWS FRAME WITH 2 EA CRACKS 3/4 INCH AT XFS 454.000. STOP DRILLED CRACK PER SRM57-2-0 PG 9-10. FABRICATED DOUBLER ANGLE (2024 T3 AL0.040) PER SRM 57-2-0 PG 9-10.CLEANED TERATED AND PRIMED PER SRM 51-1-8B. INSTALLED DOUBLERSep 26, 2002 · N803DH · Doug DC873 · Leading Edge DevicesSDR DHL2002803510Frame · crackedLT WING CENTER L/E INTERNAL PART SHOWS FRAME CRACKED 1 INCH AT XFS 447.350. REMOVED FASTNERS PER SRM 51-1-20 D PG 21.STOP DRILLED CRACKED FRAME XFS 447.750 PER SRM 57-2-0 PG 9-10.FABRICATED DOUBLER ANGLE (2024 T3 ALO 032")PER SRM 57-20 PG 9-10.CLEANED,TREATEDSep 26, 2002 · N803DH · Doug DC873 · Leading Edge DevicesSDR DHL2002803508Frame · crackedLT WING O/B L/E FRAME AT STA XRS 641.250 WITH 1/2 IN CRACK IN IT. REMOVED FASTNERS PER SRM 51-1-21 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG9-10. FABRICATED SUPPORT ANGLE (2024.T3 AL 0.032) PER SRM 57-2-0 PG 9-10.CLEANED ,TREATED AND PRIMED PER SRM 51-1-8B. Sep 26, 2002 · N803DH · Doug DC873 · Leading Edge DevicesSDR DHL2002803507Stiffener · crackedAFT CARGO COMPARTMENT LT PRESSURE WALL VERTICAL STIFFENER CRACKED 1 IN AT STA 1540.00. STOP DRILLED CRACK PER SRM 53-2-0 FIG 1F. FABRICATED DOUBLER (2024.T3AL 0.050)PER SRM 53-2-0 FIG 1B.CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED DOUBLER PER SRM 51Sep 26, 2002 · N803DH · Doug DC873 · Fuselage Main, BulkheadSDR DHL2002803501Structure · dentedLT WING OUTBOARD AILERON TRAILING EDGE, SHOWS 3 DENTS (1/2 IN) BETWEEN XRS 624.000 AND XRS 693.000. REMOVED DAMAGED O/B AILERON T/E PER SRM 51-1-21 PG 1.FABRICATED NEW T/E (2024T3AL 0.030) PER SRM 57-8-1 PG 8.CLEANED TERATED AND PRIMED PER SRM 51-1-8B.INSTASep 26, 2002 · N803DH · Doug DC873 · AileronsSDR DHL2002803500Support Bracket · crackedRT INBOARD FLAP CANOE FITTING LWR SUPPORT ANGLE AT STA. 97.000 WITH CRACK IN IT.R&R SUPPORT ANGLE PER M/M 27-51-12 PG 201-204, SRM51-3-1 PG A.Sep 26, 2002 · N803DH · Doug DC873 · Trailing Edge FlapsSDR DHL2002803519Clip · crackedAFT ACCESSORY BAY, FRAME JOINT CLIP ATTACHED TO FUSELAGE CRACKED 2 INCH, STA 640.000 L-26 AND L-27R. REMOVED FASTENERS PER SRM 51-1-20D PG 21. STOP DRILLED CRACK PER SRM 53-2-0 FIG 1B. FABRICATED REINFORCING ANGLE (2024T3AL0.050) PER SRM 53-2-0 FIG 1B. CSep 25, 2002 · N803DH · Doug DC873 · Fuselage Miscellaneous StructureSDR DHL2002803509Clip · crackedRT MLG DOOR REINFORCING CLIP LOWER PORTION CRACKED 1/2 INCH STA 902.000. REMOVED CRACKED CLIP PER SRM 51-1-21 PG 1. FABRICATED NEW CLIP (STEEL 301 1/4 H 0.032)PER SRM53-2-0 FIG 1F. INSTALLED NEW CLIP PER SRM 51-1-21 PG 1.Sep 25, 2002 · N803DH · Doug DC873 · Landing Gear DoorsSDR DHL2002803520Skin · crackedFUSELAGE EXTERIOR RT FWD SERVICE DOOR FWD UPPER CORNER CRACKED 1/4 INCH AT STA 160.000. PERFORMED MAJOR REPAIR PER SRM 53-2-0 PG 87-88 FIG 14. CUT OUT DAMAGED AREA PER SRM 53-2-0 PG 87-88 FIG 14. FABRICATED FILLER (7075T60.063) PER SRM 53-2-0 PG 87-88 FIG 1Sep 24, 2002 · N803DH · Doug DC873 · Service DoorsSDR DHL2002803518Pan · crackedRT WING L/E PAN UPPER PART CRACKED 2 INCH, XFS 327.000. REMOVED ZEE PAN PER SRM 51 1 20D.CLEANED TREATED AND PRIMED AREA PER SRM 51-1-8B.INSTALLED NEW ZEE PAN FITTING PER SRM 51-1-20D PG 9.Sep 24, 2002 · N803DH · Doug DC873 · Wing Miscellaneous StructureSDR DHL2002803506PanR/H WING L/E ZEE PAN UPPER PART CRACKED 2 IN AT STA XFS 245.000.REMOVED ZEE PAN PER SRM 51-1-21 PG 1.CLEANED TREATED AND PRIMED AREA PER SRM 51-1-8B.INSTALLED NEW ZEE PAN PER SRM 51-1-21 PG 2,51-3-0 PG 1Sep 24, 2002 · N803DH · Doug DC873 · Wing Structure
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