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 DHL2007803522Fitting · crackedRT WING T/E UPPER FITTING 0.250" CRACK STA XRS 421.000. 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. TORQUED IAW SRM 51-3-1 PG 2A.Jun 2, 2007 · N803DH · Doug DC873 · Wing, Attach FittingsSDR DHL2007803525Attach Angle · crackedRT WING CTR L/E OUTBD VANE SLOT ATTACH ANGLE CRACKED 1/2" STA XOLDI 6.225. REMOVED CRACKED ANGLE IAW SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW ANGLE IAW SRM 51-1-21. REFER TO JC EC-00372-001 (WO 1028) FOR ANGLE FABRICATIOJun 1, 2007 · N803DH · Doug DC873 · Wing, Attach FittingsSDR DHL2007803515Skin · delaminatedLT WING T/E LWR PANEL SKIN DELAMINATED (STA XF 339.000 - 409.000). REMOVED AND REPLACED DELAMINATED LT WING T/E LWR PANEL IAW SRM 51-3-0, SRM 51-3-1 (TORQUE).May 31, 2007 · N803DH · Doug DC873 · Wing, Plate/SkinSDR DHL2007803516Cargo Track · wornUPPER CARGO COMPT NR 6 TRACK LUGS WORN (STA 135.000 - 270.000). CUT OUT DAMAGED SEGMENT OF TRACK NR 6 AND FABRICATED SPLICES (AL7075T6 0.100"/ 0.125"/ 0.160") IAW SRM 53-2-3 PG 49-50. CLEANED, TREATED AND PRIMED AREA AND SPLICES IAW SRM 51-1-8B. INSTALLED NMay 30, 2007 · N803DH · Doug DC873 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2007803514Angle · crackedRT MLG W/W ANGLE CRACKED 1" STA 950.000. REMOVED CRACKED ANGLE IAW SRM 51-1-20D. FABRICATED NEW ANGLE (EXTRUSION 2616279) IAW SRM 53-2-0 PG 1, SRM 51-2-0 FIG 50. CLEANED, TREATED AND PRIMED AREA AND ANGLE IAW SRM 51-1-8B. INSTALLED NEW ANGLE IAW SRM 51-1-2May 28, 2007 · N803DH · Doug DC873 · Fuselage Miscellaneous StructureSDR DHL2007803513Angle · crackedLT MLG W/W UPPER ANGLE CRACKED STA XFS 920.000 LBL 44". REMOVED CRACKED ANGLE IAW SRM 51-1-21. FABRICATED NEW ANGLE (AL2024T3 0.050") IAW SRM 53-2-0 PG 1. CLEANED, TREATED AND PRIMED AREA AND NEW ANGLE IAW SRM 51-1-8B. INSTALLED NEW ANGLE IAW SRM 51-1-21May 28, 2007 · N803DH · Doug DC873 · Fuselage Miscellaneous StructureSDR DHL2007803512Angle · crackedRT MLG W/W ANGLE CRACKED 1" STA 940.000. REMOVED CRACKED ANGLE IAW SRM 51-1-20D. FABRICATED NEW ANGLE (EXTRUSION 2616279) IAW SRM 53-2-0 PG 1, SRM 51-2-0 FIG 50. CLEANED, TREATED AND PRIMED AREA AND NEW ANGLE IAW SRM 51-1-8B. INSTALLED NEW ANGLE IAW SRM 51May 28, 2007 · N803DH · Doug DC873 · Fuselage Miscellaneous StructureSDR DHL2007803518Skin · misrepaired"B" CARGO DOOR SKIN REPAIR RIVETS EDGE DISTANCE NOT IN ACCORDANCE WITH SRM (UPPER PORTION) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 52-2-0 FIG 4 SHEET 3. REMOVED EXISTING REPAIR IAW SRM 51-1-21. FABRICATED REPAIR DOUBLER AND FILLER (AL7075T6 0.063")IAW May 27, 2007 · N803DH · Doug DC873 · Cargo/Baggage DoorsSDR DHL2007803508Frame · crackedRT WING OUTBD L/E INNER SECTION FORMER CRACKED 0.250", STA XFS 635.000. REMOVED FASTENERS IAW SRM 51-1-21. FABRICATED (2EA) ANGLE DOUBLERS AL7075T6 0.032" IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLERS IAW SRM 51-1-8B. INSTALLEMay 27, 2007 · N803DH · Doug DC873 · Wing SparSDR DHL2007803505Frame · crackedRT WING CTR L/E LWR FORMER CRACKED 0.250" STA XFS 466.615. REMOVED FASTENERS IAW SRM 51-1-21. FABRICATED (2EA) DOUBLER (AL7075T6 0.040") IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 51-1-21May 26, 2007 · N803DH · Doug DC873 · Wing SparSDR DHL2007803507Frame · crackedRT WING CTR L/E UPPER FORMER CRACKED, STA XFS 397.750. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-1-20D. PERFORMED STOP HOLE AND FABRICATED (2EA) DOUBLERS (AL7075T6 0.032" / 0.040") IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND DOUBLERS IAW SRMay 26, 2007 · N803DH · Doug DC873 · Wing SparSDR DHL2007803509Skin · crackedUPPER FUSELAGE EXT SKIN CRACKED 0.500" APPROX, STA 580.000 L-4R TO L-5R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-1 FIG 7 SHEET 1, 3. REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT DAMAGED AREA AND FABRICATED REPAIR DOUBLER (AL7075T6 0.100") (2EA) INTMay 25, 2007 · N803DH · Doug DC873 · Fuselage Main, Plate/SkinSDR DHL2007803501Frame · crackedRT WING OUTBD L/E INNER SECTION LWR FORMER CRACKED 0.500" AT STA XFS 653.750. REMOVED FASTENERS IAW SRM 51-1-21. FABRICATED 2EA ANGLES DOUBLERS (AL7075T6 0.032") IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLES IAW SRM 51-1-8B. INSTALLEDMay 23, 2007 · N803DH · Doug DC873 · Wing SparSDR DHL2007803503Frame · crackedRT WING OUTBD L/E INNER SECTION LWR FORMER CRACKED 0.500" AT STA XFS 616.250. REMOVED FASTENERS IAW SRM 51-1-21. FABRICATED 2 ANGLE DOUBLERS AL7075T6 0.032" IAW SRM 57-2-0 PG 9-10. CLEANED,TREATED AND PRIMED AREA AND ANGLE DOUBLERS IAW SRM 51-1-8B. INSTALLMay 23, 2007 · N803DH · Doug DC873 · Wing SparSDR DHL2007803500Frame · crackedRT WING OUTBD L/E INNER SECTION LWR FORMER CRACKED 0.500" AT STA XFS 660.000. REMOVED FASTENERS IAW SRM 51-1-21. FABRICATED ANGLES (2EA) DOUBLERS AL7075T6 0.032" IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLERS IAW SRM 51-1-8B. IMay 23, 2007 · N803DH · Doug DC873 · Wing SparSDR DHL2007803506Doubler · crackedRT WING CTR L/E LWR SKIN INTERNAL DOUBLER CRACKED 0.500" STA XFS 428.000. REMOVED CRACKED INTERNAL DOUBLER IAW SRM 51-1-21, SRM 51-1-20D. FABRICATED NEW INTERNAL DOUBLER (AL7075T6 0.090") IAW SRM 57-2-0 PG 1 AND CLEANED, TREATED AND PRIMED AREA AND INTERNAL May 23, 2007 · N803DH · Doug DC873 · Wing, Plate/SkinSDR DHL2007803504Skin · wornRT OUTBD FLAP UPPER SKIN WORN STA XF 207.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-7-1 FIG 4, TR NR 57-94 DATED 10-01-02. REMOVED DAMAGED PLATING IAW SRM 57-1-0 PG 1, SRM 51-1-21. FABRICATED NEW PLATING (AL2024T3 0.040") IAW SRM 57-7-1 FIG 4, TRMay 23, 2007 · N803DH · Doug DC873 · Trailing Edge FlapsSDR DHL2007803510Skin · crackedUPPER FUSELAGE SKIN CRACKED 0.500" STA 510.000 L-5R TO L-6R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-1 FIG 7 SHEET 1-3. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-1-20D. CUT OUT DAMAGED SECTION AND FABRICATED REPAIR DOUBLER (AL7075T6 0.090") (2EA)May 23, 2007 · N803DH · Doug DC873 · Fuselage Main, Plate/SkinSDR DHL2007803502Frame · crackedRT WING OUTBD L/E INNER SECTION LWR FORMER CRACKED 0.500" AT STA 622.250. REMOVED FASTENERS IAW SRM 51-1-21. FABRICATED TWO ANGLES DOUBLERS (AL7075T6 0.032") IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLES IAW SRM 51-1-8B. INSTALLED ANGMay 23, 2007 · N803DH · Doug DC873 · Wing SparSDR DHL2006803002Filter · contaminatedAT 1000FT AGL, NR 3 OIL QUANTITY DROPPED FROM 12 QUARTS TO 2 QUARTS OIL PRESSURE NORMAL NR 3 ENGINE SHUTDOWN AFTER LANDING OIL QUANTITY RETURNED TO 12 QUARTS, ENGINE SHUTDOWN BY FLIGHT CREW. INSPECTED LUB AND SCAVENGE CHIP DETECTORS, NO DEBRIS FOUND. REMOVNov 1, 2006 · N803DH · Doug DC873 · Turbine Engine Oil SystemSDR DHL2006803001Odor · detectedSTRONG SMELL OFF SOMETHING HOT OR OVER HEATING IN A/C STRONGER IN LAV IT GOES AWAY WITH LT PACK OFF. OPERATED LT AND RT PACKS FULL COLD TO FULL HOT IAW MM 21-20-0 BOTH PACK OPERATE NORMAL NO DEFECTS NOTEDSep 7, 2006 · N803DH · Doug DC873 · Air Distribution SystemSDR DHL2005803554Fitting · crackedITEM REF. NR. 039052: AFT CARGO COMPT. FITTING CRACKED 1.500 INCH STA 1080.000 L-21R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PAGE 1. REMOVED CRACKED FITTING IAW SRM 51-3-0 AND SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTADec 16, 2005 · N803DH · Doug DC873 · Fuselage Main, Attach FittingsSDR DHL2005803556Skin · crackedPERFORM PREVENTATIVE MODIFICATION IAW SB 57-88 REV. 3 ON LT WING LOWER SKIN CRACK AT STA 69.5 REF. SB AND DRAWING JO 60095-506. PERFORMED PREVENTATIVE MODIFICATION IAW AD80-22-01, SB 57-88 REV. 3 DWG NR JO60095-506. REMOVED FASTENERS AND SKI FITTING IAW DWG JODec 16, 2005 · N803DH · Doug DC873 · Wing, Plate/SkinSDR DHL2005803557Skin · crackedPERFORM PREVENTATIVE MODIFICATION IAW SB 57-88 REV. 3 ON RT WING LOWER SKIN CRACK AT STA 69.5 REF. SB AND DRAWING J060095-505. PERFORMED PREVENTATIVE MODIFICATION IAW AD80-22-01, SB 57-88 REV. 3 DWG NRJO60095-505. REMOVED FASTENERS AND SKI FITTING IAW DWG JO6Dec 16, 2005 · N803DH · Doug DC873 · Fuselage Main, Plate/SkinSDR DHL2005803543Fitting · crackedITEM REF. NR. 032512: NR3 ENG RT T/R RAIL FITTING CRACKED, STA YN 254.000 AT 12 O'CLOCK POSITION. FABRICATED REINFORCING SPLICE (17-4 PH STAINLESS FLAT BAR) IAW MM 78-31-41 PG.1. APPLIED SILICONE TO AREA AND INSTALLED REINFORCING SPLICE MM 78-31-41 FIG. 902, Dec 15, 2005 · N803DH · Doug DC873 · Engine Thrust ReverserSDR DHL2005803551Door Frame · unknownCOMPLY WITH REPAIR MODIFICATION ON "D" BELLY DOOR AFT LWR JAMB CORNER IAW AD2005-18-07 SB DC8 53-078, SERVICE REWORK DRAWING SR 08530019. PERFORMED MAJOR REPAIR IAW FAA FORM 8100-9, AD2005-18-07, SB DC8 53-078, SERVICE REWORK DWG SR08530019, BOEING MESSAGE NRDec 14, 2005 · N803DH · Doug DC873 · Fuselage Main, StructureSDR DHL2005803538Channel · crackedLT MLG INBD DOOR ZEE CHANNEL UPPER AFTER CORNER CRACKED 0.500", STA 970.000. REMOVED FASTENERS IAW SRM 51-1-21. PERFORMED STOP HOLE ON CRACK END AND FABRICATED DOUBLER REPAIR (AL7075T6 0.040") IAW SRM 52-2-0, SRM 52-6-1 PAGE 2. CLEANED, TREATED AND PRIMED ADec 12, 2005 · N803DH · Doug DC873 · Fuselage Miscellaneous StructureSDR DHL2005803555Fitting · crackedMLG SUPPORT FITTING (TRAPEZOIDAL) RT HAS 2 CRACKS 0.750" AFTER STOP HOLE OF 0.562" AT STA 863.25 AND 4" CRACK AT STA 870.000. PERFORMED MAJOR REPAIR IAW DOUGLAS DWG 5750127, SRM 53-1-0 PG 1. REMOVED SUPPORT FITTING (TRAPEZOIDAL) AND 2 FITTINGS IAW SRM 53-1-0Dec 12, 2005 · N803DH · Doug DC873 · Wing, Landing Gear Attach FittingsSDR DHL2005803549Door Frame · unknownCOMPLY WITH REPAIR MODIFICATION ON "A" BELLY DOOR JAMB CORNER IAW SERV REWORK DRAWING SR 08530019. PERFORMED MAJOR REPAIR IAW FAA FORM 8100-9, AD2005-18-07, SB DC8 53078, SERVICE REWORK DWG SR 08530019, BOEING MESSAGES NR 1-145489684-5, SEMAN DWG ED-4113, 1-1Dec 12, 2005 · N803DH · Doug DC873 · Fuselage Main, StructureSDR DHL2005803547Fitting · crackedFWD CARGO COMPT BILGE FITTING CRACKED STA 300.000 BETWEEN L-35L AND L-36. REMOVED CRACKED FITTING IAW SRM 51-1-20D. FABRICATED ANGLE DOUBLER (2EA) (7075-0 0.125") TO INSTALL FITTING IAW SRM 53-2-0. PERFORMED HEAT TREATMENT TO ANGLE DOUBLER FROM 7075-0 TO 70Dec 11, 2005 · N803DH · Doug DC873 · Fuselage Main, Attach FittingsSDR DHL2005803542Fitting · crackedITEM REF NR. 033356: MAIN CARGO COMPT FITTING CRACKED 1 INCH STA 834.500 L-13R (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 IAW SRDec 11, 2005 · N803DH · Doug DC873 · Fuselage Main, Attach FittingsSDR DHL2005803553Skin · crackedITEM REF. NR. 038581: RT WING LWR SKIN OB FASTENER HOLE CRACKED 0.250 INCH S-64 (MAJOR REPAIR). PERFORMED MAJOR REPAIR AND REMOVED FASTENERS IAW SRM 51-1-20D. TRIMMED OUT DAMAGED AREA IAW SB 57/100 FIG. 5 SHEET 2 OF 5. FABRICATED DOUBLERS (7075T6 AL 0.125 INCHDec 9, 2005 · N803DH · Doug DC873 · Wing, Plate/SkinSDR DHL2005803530Clip · brokenRT WING NR3 MAIN TANK INTERNAL STRUCTURE CLIP BROKEN XRS 22.000 S-63. REMOVED AND REPLACED CLIP ON RT WING NR3 MAIN TANK INTERNAL STRUCTURE XRS 22.000 S-63 IAW SRM 51-1-20D, SRM 51-3-1. FOR LEAK CHECK SEE NR 039053.Dec 8, 2005 · N803DH · Doug DC873 · Wing, Attach FittingsSDR DHL2005803545Fitting · crackedITEM REF. NR. 038748: WING CTR. SECTION FITTING CRACKED STA 781.000 (NR5 TRACK). 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. TORQUED IAW SRM 51-3-1 PG. 2A. FOR FITTING FABRDec 8, 2005 · N803DH · Doug DC873 · Fuselage Main, Attach FittingsSDR DHL2005803544Fitting · crackedITEM REF. NR. 038465: WING CTR SECTION FITTING CRACKED 1 INCH STA 798.000 RBL 22 INCH (MAIN CARGO COMPT). REMOVED CRACKED FITTING AT STA 798.000 RBL 22 INCH IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-Dec 8, 2005 · N803DH · Doug DC873 · Fuselage Main, Attach FittingsSDR DHL2005803548Plate · elongatedLT WING OTBD FLAP LWR PLATING RIVETS HOLES ELONGATED BETWEEN XF 210.000 AND XF 247.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 12-06-2005, DWG AA33-53-R10 REV IR DATE 11-22-05. REMOVED DAMAGED EXISTING SOLID PLATING, FABRICATED NEW PLATING (2024T3 0Dec 7, 2005 · N803DH · Doug DC873 · Trailing Edge FlapsSDR DHL2005803546Doubler · crackedNR 2 ACCESS DOOR FRAME INTERNAL DOUBLER 0.75" CRACKED WORN & BROKEN (STA -156.000 TO -165.000). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 12/06/05, DWG AA33-53-R09 REV IR DATE 11/22/05 REMOVED LT/RT NOSE AIR SCOOP IAW SRM 51-3-0. REMOVED EXISTING EXTERDec 7, 2005 · N803DH · Doug DC873 · Standard Practices/StructuresSDR DHL2005803533Fitting · crackedITEM REF. NR. 039057: AFT CARGO COMPT. FITTING CRACKED 2 INCHES AT STA 1075.000 L-21R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0. REMOVED CRACKED FITTING IAW SRM 51-3-0, SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. APPLIED SEALANTDec 5, 2005 · N803DH · Doug DC873 · Fuselage Main, Attach FittingsSDR DHL2005803532Fitting · brokenLT IB FLAP OB FITTING BROKEN STA 97.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0. REMOVED BROKEN FITTING IAW SRM 51-1-21, SRM 51-1-20D, SRM 51-3-0. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-1Dec 5, 2005 · N803DH · Doug DC873 · Trailing Edge FlapsSDR DHL2005803535Fitting · crackedNR 2 MAIN TANK OB FWD FITTING CRACKED XRS 74.000 S-51 (LWR PART) (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND APPLIED COATING MATERIAL TO AREA IAW SRM 51-1-12 PG. 7. APPLIED SEALANT TO FADec 5, 2005 · N803DH · Doug DC873 · Wing, Attach FittingsSDR DHL2005803526Doubler · crackedMODIFICATION DOUBLER (ACS) CRACKED 0.500" ON AFT LWR CORNER OF LT PRIMARY HEAT EXCHANGER STA -12.000 L-27L. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 12/02/05, DWG AA33-53-R02 REV TR DATE 11/08/05. REMOVED FASTENERS IAW SRM 51-1-21. TRIMMED OUT DAMAGEDec 4, 2005 · N803DH · Doug DC873 · Fuselage Main, StructureSDR DHL2005803527Frame · crackedMAIN CARGO COMPT FRAME CRACKED 0.500" STA 320.000 L-20L TO L-21L. PERFORMED MAJOR REPAIR IAW SRM. TRIMMED OUT DAMAGED FRAME SEGMENT IAW SRM 53-2-0 FIG 2 SHEET 2. PREPARED NEW FRAME SEGMENT, HEAT TREATED FROM 7075T651 TO 7075-0, FORMED AND HEAT TREATED FROM Dec 4, 2005 · N803DH · Doug DC873 · Fuselage Main, FrameSDR DHL2005803537Floorbeam · misdrilledWING CTR SECTION FLOORBEAM HOLES (2EA) MISDRILLED, STA 834.500 RBL 32" RBL 37.750 (MAIN CARGO COMPT.) PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 11-28-05, DWG NR AA33-53-R06 REV IR DATE 11-16-05. REMOVED FASTENERS IAW SRM 51-1-21. TRIMMED OUT DAMAGED SEDec 3, 2005 · N803DH · Doug DC873 · Fuselage Main, Floor BeamSDR DHL2005803525Doubler · crackedMODIFICATION DOUBLER (ACS) CRACKED 0.500" ON AFT LWR CORNER OF RT PRIMARY HEAT EXCHANGER, STA -12.00. L-27R. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 12-02-05, DWG AA33-53-R01 REV A DATE 12-02-05. REMOVED FASTENERS IAW SRM 51-1-21. TRIMMED OUT DAMAGEDec 3, 2005 · N803DH · Doug DC873 · Fuselage Main, StructureSDR DHL2005803531Frame · crackedMAIN CARGO COMPT FRAME CRACKED 0.250" STA 1580.000 L-20 - L-21R. PERFORMED MAJOR REPAIR IAW SRM. TRIMMED OUT DAMAGED FRAME SEGMENT, FABRICATED NEW FRAME SEGMENT IAW SRM. TWO ANGLES IAW SRM. HEAT TREATED NEW FRAME SEGMENT AND ANGLES FROM 70750 TO 7075T6 IAW Dec 3, 2005 · N803DH · Doug DC873 · Fuselage Main, FrameSDR DHL2005803534Floorbeam · misdrilledWING CTR SECTION FLOORBEAM HOLES (2EA) MISDRILLED STA 960.000 LBL 9.625 INCH, LBL 15.250 INCH(MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 11-30-05 DWG AA33-53-R05 REV JR DATE 11-22-05. DRILLED MISDRILLED HOLES (2EA) TO 0.250 INCH AND 0.290 IDec 3, 2005 · N803DH · Doug DC873 · Fuselage Main, Floor BeamSDR DHL2005803528Panel · wornLT IB FLAP UPPER PANEL PLATING WORN 1 INCH APPROX AT STA XW 92.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 12-02-05, DWG AA33-53-R03 REV. JR DATE 11-11-05. REMOVED DAMAGED EXISTING SOLID SEGMENT PLATING IAW SRM 51-1-21. FABRICATED NEW SDec 3, 2005 · N803DH · Doug DC873 · Trailing Edge FlapsSDR DHL2005803524Channel · crackedNR. 033035: AFT CARGO COMPT. (D) BELLY DOOR JAMB CHANNEL CRACKED 0.250 INCH, STA 1420.000, STA 1460.000. REMOVED CRACKED CHANNEL IAW SRM 51-1-21, SRM 51-3-0. FABRICATED NEW CHANNEL (2024T3 AL 0.050 INCH) IAW SRM 53-2-0. CLEANED, TREATED AND PRIMED AREA AND CHADec 3, 2005 · N803DH · Doug DC873 · Fuselage Miscellaneous StructureSDR DHL2005803523Skin · crackedNR. 032564: LT WING CTR LE UPPER SKIN HAS 2 CRACKS 0.250 INCH (STA XFS 285.250 - 291.500) (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 11-30-05, DWG AA33-53-R04 REV JR DATE 11-14-05. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-1-20D. TRIMMED ODec 3, 2005 · N803DH · Doug DC873 · Leading Edge DevicesSDR DHL2005803539Floorbeam · misdrilledITEM REF NR 038741: WING CTR SECTION FLOORBEAM HOLE MISDRILLED STA 980.000 RBL 93750 (MAIN CARGO COMPT.) (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 11/28/05, DWG AA33-53-R07 REV IR DATE 11/11/05. REMOVED FASTENERS IAW SRM 51-1-21. TRIMMED Dec 3, 2005 · N803DH · Doug DC873 · Fuselage Main, Floor Beam
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