Douglas DC-8-73

Service difficulty reports · 821

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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 aircraft_model_key = 'DC873'
  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 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 BeamSDR 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 DHL2005802011Bulb · inoperativeEMERGENCY LIGHTS DISARM LIGHT INOP. REMOVED AND REPLACED EMER LIGHTS DISARM BULB. OPS CHECK OK IAW MM 33-50-0. P/N 313.Nov 23, 2005 · N802DH · Doug DC873 · Emergency LightingSDR 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 DHL2005802010Door · damagedFOUND L1 DOOR DAMAGED BY STAIRS. REMOVED DAMAGED AREA FROM BTM FWD LWR AREA OF DOOR STRUCTURE. FABRICATED DOOR FRAME SEGMENT DOUBLER FROM 2024-T3, .070. INSTALLED REPAIR USING EXSISTING RIVET SPACING AND SECOND ROW SPACING PER SRM.Nov 16, 2005 · N802DH · Doug DC873 · Passenger/Crew DoorsSDR 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 System
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