N802DH

Service difficulty reports · 511

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 = 'N802DH' 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 DHL99802002Oxygen Sys · leakingLOST O2 PRESSURE FROM 1600 TO 200 PSI. SERVICED AND LEAK CHECKED CREW O2 PER MM 35-10-00. OK FOR SERVICE.Oct 14, 1999 · N802DH · Doug DC873F · Crew Oxygen SystemSDR DHL99802001Static Wicks · damagedIN PRECIP BOTH VHF AND HF WILL TRANSMIT BUT NOT RECEIVE. REPLACED 10 STATIC WICKS AND NR 1 VHF ANTENNA PER MM 23-60-0 AND 23-10-0.Aug 18, 1999 · N802DH · Doug DC873F · Static Discharge SystemSDR DHL9980204CFitting · crackedC-CHECK NON-ROUTINE ENG NR 4 RT AT 12 O'CLOCK FWD CORE COWL CLOSE TO PRECOOLER SCOOP AREA HAD CRACK DAMAGE ON SURFACE. THRUST REVERSER RT HALF NR 4 ENG IAW MM. FACILITY S/M WORK REMOVED CRACKED FITTING FROM FWD CORE COWL IAW DC-8 SRM 51-1-21 PAR 5, 51-3-0 PARMay 25, 1999 · N802DH · Doug DC873F · Engine Cowling SystemSDR DHL9980251CSkin · delaminatedC-CHECK, FLAP VANE NR 3 DELAMINATED LEFT WING DOT 38255. REMOVED I/W NR 3 VANE IAW DC-8 27-51-14 ROUTE TO STORES TO BE SENT OUT FOR REPAIR. INSTALLED I/H NR 3 FLAP VANE IAW DC-8 MM 27-51-14 PG 201. PENDING RIG & OPS CHK ACCOMP. RIG & OPS CHK NORMAL IAW DC-May 21, 1999 · N802DH · Doug DC873F · Trailing Edge FlapsSDR DHL9980211CFrame · crackedC-CHECK, UPPER CARGO COMPT AT STA 1600 CIRCUMFERENTIAL FRAME AT CUSP LINE WAS CRACKED RT SIDE. CUT OUT CRACKED SECTION OF FRAME AT FS 1580 RT M CARGO CABIN IAW DC-8 SRM 53-2-0 FIG 2. FABRICATED NEW SECTION OF FRAME: 6 X 2.5 AND 2 SPLICES 10 X 2.5 IAW MHA ENMay 21, 1999 · N802DH · Doug DC873F · Fuselage Main, FrameSDR DHL9980214CBracket · crackedC-CHECK, MAIN CARGO COMPARTMENT MAIN CARGO DOOR INTERIOR CENTER AREA DOOR LATCH ACTUATOR UPPER ATTACH BRACKET MOUNT BOLTS LOOSE AND SMALL ANGLE BRACKET WAS CRACKED D20CD1. REMOVED DAMAGED BRACKET AT MAIN CARGO COMPT CARGO DOOR INTERIOR CENTER ARA DOOR LATCH AMay 11, 1999 · N802DH · Doug DC873F · Cargo/Baggage DoorsSDR DHL9980216CSeat Track · damagedC-CHECK, SEAT TRACK NR 4 BETWEEN STA 151-171 2 PLUG REPAIRS NOT PER SRM. CUT OUT DAMAGED SECTION OF SEAT TRACK NR 4 BETWEEN STA 130 TO 170 & PREPAIRED NEW SECTION FROM APPROPRIATED MATCHING SECTION OF TRACK AND FABRICATED SPLICES FROM 7075-T6 IAW DC-8 SRM 53-May 8, 1999 · N802DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL9980215CBulkhead · crackedC-CHECK, AFT PRESSURE BULKHEAD, REAR FACE, CENTER SECTION, ATTACHING ANGLE WAS CRACKED AT BEND RADIUS. BEHIND PULLEY BRACKET ASSY. CLEANED CRACKED AREA AT ANGLE ON PRESSURE BULKHEAD REAR FACE, CENTER SECTION PER SRM 51-1-8, PARA 6A. STOP DRILLED CRACK, DYE May 7, 1999 · N802DH · Doug DC873F · Fuselage Main, BulkheadSDR DHL9980220CFitting · crackedC-CHECK, MCC LT CUSP LINE AREA AT STA 700.000 LOWER FITTING IS CRACKED. D 20C01. REMOVED CRACKED FITTING FROM MCC LT CUSP LINE AREA AT STA 700.000 IAW DC-8 SRM 51-1-20D PAR 8, 51-3-0 PAR 1 & 2. FABRICATED NEW FITTING FROM ALUMINUM PLATE 7075-T6 IAW MHA ENGIMay 4, 1999 · N802DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL9980218CScuff Plate · crackedC-CHECK, FWD PIT (C-1) CARGO SCUFF HAD A CRACK, 13 FASTENERS DAMAGED AND SPARK BURN AT LOWER LT AREA. DOT 3822. STOP DRILLED CRACK AND REMOVED DAMAGED FASTENERS AT FWD PIT (C1) CARGO SCUFF AT LOWER LT AREA IAW DC-8 SRM 51-1-21 PG 1. TREATED, PRIMED DOUBLER May 4, 1999 · N802DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL9980217CLongeron · crackedC-CHECK, AT STA IS 1220, LONGERON, 26L IS CRACKED AT CARGO PIT NR 3 LT SIDE. FABRICATED DOUBLER REPAIR 2024 T3 032 14 X 4 IAW DC-8 SRM 51-1-4 PG 1 PAR 1. TREATED AND PRIMED PER DC-8 SRM 51-1-8 PG 16 & 13 PAR 6 6F. INSTALLED REPAIR PER DC-8 SRM 51-1-21 PG 1 May 4, 1999 · N802DH · Doug DC873F · Fuselage Main, Longeron/StringerSDR DHL9980229CAngle · crackedC-CHECK, RT WING AT NR 1 HINGE AREA XW 5 & FS 980 APPROX CRACKED ANGLE. DOT 641.59. REMOVED DAMAGED ANGLE AT RT WING NR 1 HINGE AREA XW 5 FS 940 IAW DC-8 51-1-21 PG 1 PAR 1. FABRICATED NEW ANGLE PER DC-8 SRM 53-8-3 PG 5/6 FIG 1 2024-T3 050 14X3. TREATED & May 3, 1999 · N802DH · Doug DC873F · Wing Miscellaneous StructureSDR DHL9980228CAngle · crackedC-CHECK, FWD LOWER CARGO COMPARTMENT LONG 31R STA 420 CIRCUMFERENTIAL HAS ATTACHED ANGLE WITH CRACK ON SURFACE. DOT 13919. CLEANED CRACKED AREA AT ANGLE AT FWD LOWER CARGO IS 420 LONG 31R IAW DC-8 SRM 53-2-0 FIG 13 (SHEET 3). TREATED & PRIMED REWORKED AREA May 3, 1999 · N802DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL9980226CFitting · crackedC-CHECK, LT WING, I/B FLAP, I/B HINGE, 2 INCH CRACK UNDER FLAP FITTING ATTACH POINT WING STA XW 5.000. STOP DRILLED END CRACK .25 AT LT WING I/B FLAP I/B HINGE UNDER FLAP FITTING ATTACH POINT IAW DC-8 SRM 51-3-2 PG 1 PAR 1. FABRICATED ANGLE REPAIR 2024-T3 05May 3, 1999 · N802DH · Doug DC873F · Wing Miscellaneous StructureSDR DHL9980225CCircumferntial · crackedC-CHECK, AFT LOWER CARGO COMPT CIRCUMFERENTIAL AT FS 1380 BTW LONG 33R IS CRACKED. REF 344013. STOP DRILLED END CRACK AREA AT AFT CARGO COMPT CIRCUMFERENTIAL STA 1380 BTWN LONG 34R IAW DC-8 SRM 53-2-0 PG 2E FIG 1B. FABRICATED ANGLE REPAIR 301 STAINLESS .25 May 3, 1999 · N802DH · Doug DC873F · Fuselage Main, FrameSDR DHL9980224CAngle · crackedC-CHECK, RT WING AT NR 1 HINGE AREA XW 5 & 980 APPROX CRACKED ANGLE DOT 641-59. REMOVED DAMAGED ANGLE AT RT WING NR 1 HINGE AREA XW 5 FS 940 PER DC-8 SRM 51-1-21 PG 1 PAR 1. FABRICATED NEW ANGLE PER DC-8 SRM 53-8-3 PG 5/6 FIG 1 2024-T3 050 14 X 3. TREATED &May 3, 1999 · N802DH · Doug DC873F · Wing Miscellaneous StructureSDR DHL9980223CCircumferential · crackedC-CHECK, AFT LOWER CARGO COMPT CIRCUMFERENTIAL AT FS 1420 BTW LONG 36 & 33R IS CRACKED. REF 344015. STOP DRILLED END CRACK AREA AT AFT CC FS 1420 BETWEEN LONG 36 & 33R IAW DC-8 SRM 53-2-0 PG 2E FIG 1B. INSTALLED ANGLE REPAIR PER DC-8 SRM 51-1-21 PG 1 PAR A6May 3, 1999 · N802DH · Doug DC873F · Fuselage Main, FrameSDR DHL9980221CCircumferential · crackedC-CHECK, AFT LOWER CARGO COMPT CIRCUMFERENTIAL AT FS 1380 BTW LONG 34R IS CRACKED. REF 34403. STOP DRILLED END CRACK AREA AT AFT CARGO COMPT CIRCUMFERENTIAL STA 1380 BETWEEN LONG 34R TO 33R IAW DC-8 SRM 53-2-0 PG 2E FIG 1B. FABRICATED ANGLE REPAIR 301 STAINMay 3, 1999 · N802DH · Doug DC873F · Fuselage Main, FrameSDR DHL9980219CFitting · crackedC-CHECK, LT WING, L/B HINGE, 2 INCH CRACK UNDER FLAP FITTING ATTCH POINT WING STA: XW 5.000. STOP DRILLED END CRACK .25 AT LT WING L/B FLAP L/B HINGE UNDER FLAP FITTING ATTACH POINT IAW DC-8 SRM 51-3-2 PG 1 PAR 1. FABRICATED ANGLE REPAIR 2024-T3 050. 6 X 3 IMay 3, 1999 · N802DH · Doug DC873F · Wing Miscellaneous StructureSDR DHL9980230CAngle · crackedC-CHECK, RT WING LOWER TO FUSELAGE FS 640 & XW 0 CRACKED ANGLE. DOT 64157. REMOVED CRACKED ANGLE FROM RT WING LWR TO FUSELAGE STA 640 & XWO PER SRM 51-1-21 PAR 1. FABRICATED NEW ANGLE SAME MATERIAL & THICKNESS 2024-T3 0.050 (14 X 1.15 X 1) IAW DC-8 SRM 53-8May 2, 1999 · N802DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL9980227CRib · crackedC-CHECK, LT WING CENTER I/E I/B AREA AT STA 255.00 LOWER RIB IS CRACKED. DOT 38138. STOP DRILLED END CRACK AT LT WING CENTER SECTION 4E STA 255.000 LOWR RIB IAW DC-8 SRM 57-2-0 PG 9 FIG 2. FABRICATED ANGLE REPAIR 8 X 4 063 7075T6 IAW DC-8 SRM 57-2-0 PG 10 FMay 2, 1999 · N802DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL9980202CAngle · crackedAT C-CHECK, RT WING TO FUSELAGE FS 640 & XW 0 CRACKED ANGLE. REMOVED CRACKED ANGLE FROM RT WING LWR TO FUSELAGE STA 640 AND XWO PER SRM. FABRICATED NEW ANGLE SAME MATERIAL AND THICKNESS 2023-T3 0.050. CLEANED ANGLE AREA PER SRM. TREATED, PRIMED AREA AND NEMay 2, 1999 · N802DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL9980201CSeat Track · corrodedAT C-CHECK, FWD LOWER CARGO COMPARTMENT HAS SECTION OF CHANNEL TRACK WITH EVIDENCE OF CORROSION AND SEVERAL CRACKS ON SURFACE. REMOVED CRACKED SECT OF TRACK CHANNEL IAW, CLEANED TRACK CHANNEL AREA PER SRM. OK TO TREAT, PRIME AREA AND NEW CHANNEL. TREATED, PMay 2, 1999 · N802DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL9980233CFitting · crackedC-CHECK, CENTER TANK AREA UPPER FUELAGE STA 760 O/B RT OF SEAT TRACK NR 6 FITTING CRACKED BETWEEN FASTENERS. REMOVED CRACKED FITTING FROM CENTER TANK AREA UPPER FUSELAGE STA 760 IAW DC-8 SRM 51-1-20D, PAR 8, 51-1-21, PAR 1, FIG 32. DRILLED NEW FITTING PER SRMay 1, 1999 · N802DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL9980232CFitting · crackedC-CHECK, UPPER CARGO COMPT CENTER TANK AREA STA 780 FITTING ON FLOORBEAM REFERENCE SEAT TRACK NR 4 & NR 5 IS CRACKED FITTING NEED MIRROR & FLASHLIGHT. REMOVED CRACKED FITTING AT MCC TANK AREA STA 780 FLOORBEAM IAW DC-8 SRM 51-1-21D PG 1 PAR 1. DRILLED NEW FIMay 1, 1999 · N802DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL9980231CBracket · crackedC-CHECK, LT WING STA SRS 693 THRU PLATE DOOR NR 518B BRACKET CRACKED. DOT 381. STOP DRILLED END CRACK AT LT WING I/E RIB STA WRS 693 IAW DC-8 SRM 57-2-0 PG 9 FIG 2. FABRICATED ANGLE REPAIR 2024 T3.050 3 X 1 X 4 IAW DC-8 SRM 57-2-0 PG 10 FIG 2. TREATED & PRMay 1, 1999 · N802DH · Doug DC873F · Wing Miscellaneous StructureSDR DHL9980203CFitting · crackedAT C-CHECK, CENTER TANK AREA UPPER FUSELAGE STA 760 O/B RT OF SET TRACK NR 6 FITTING CRACKED BETWEEN FASTENERS. REMOVED CRACKED FITTING FROM CENTER TANK AREA UPPER FUSELAGE. DRILLED NEW FITTING PER SRM. CLEANED FITTING AREA PER SRM. OK TO TREAT, PRIME AREAMay 1, 1999 · N802DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL9980269CSkin · crackedC-CHECK, RT WING T/E LOWER PANEL HAS CRACK STA XRS 240 IS ABOUT 4 LONG DOT 64109. CUT OUT CRACKED AREA AT RT WING T/E LWR PANEL ST XRS 240 IAW DC-8 SRM 51-1-9A PG 1 THRU 69, FABRICATED FILLER FROM 2024-T3 0.020 (3 X 6) & DOUBLER REPAIR FROM 2024-T3 0.020 (7 XApr 30, 1999 · N802DH · Doug DC873F · Wing, Plate/SkinSDR DHL9980268CRib · crackedC-CHECK, RT WING O/B L/E INT THRU ACCES PANEL 517B RIB CRACK AT UPPER END XFS 848 DOT 64118. STOP DRILLED END CRACK AT RT WING O/B L/E RIBS STA XFS 848 & IAW DC-8 SRM 57-2-0 PG 9 FIG 2. FABRICATED ANGLE REPAIR 2024 T3 050 .75 X 1.25 X 5 IAW DC-8 SRM 57-2-0 PApr 30, 1999 · N802DH · Doug DC873F · Wing, Plate/SkinSDR DHL9980267CRib · crackedC-CHECK, RT WING O/B L/E INT THRU ACCESS PANEL 517B RIB CRACK AT UPPER END XFS 828 DOT 64119. STOP DRILLED END CRACK AT RT WING O/B L/E RIBS STA XFS 828 IAW DC-8 SRM 57-2-0 PG 9 FIG 2. FABRICATED ANGLE REPAIR 2024 T3 050 .75 X 1.25 X 4 IAW DC8 SRM 57-2-0 PG Apr 30, 1999 · N802DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL9980266CRib · crackedC-CHECK, RT WING O/B L/E INT THRU ACCESS PANEL 518A RIBS CRACKED AT UPPER END 3 XFS 822; XFS 815 & XFS 809 DOT 64120-64122-64121. STOP DRILLED END CRACK AT RT WING O/B L/E RIBS STA XFS 822 XFS 815 XFS 809 IAW DC-8 SRM 57-2-0 PG 9 FIG 2. STOP DRILLED END CRACApr 30, 1999 · N802DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL9980265CRib · crackedC-CHECK, RT WING O/B L/E INT THRU ACCESS PANEL 518A RIB CRACK AT UPPER END XFS 797 DOT 64123. STOP DRILLED END CRACK AT RT WING O/B L/E RIB STA XFS 797.000 IAW DC-8 SRM 57-2-0 PG 9 FIG 2. FABRICATED ANGLE REPAIR 2024 T3 .050 .75 X 1.25 X 5 IAW DC-8 SRM 57-2-Apr 30, 1999 · N802DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL9980264CRib · crackedC-CHECK, RT WING O/B L/E INT THRU ACCES PANEL 518B CRACKED RIBS AT THE UPPER END XFS 772; XFS 779 & XFS 785 DOT 64124-64125-64126. STOP DRILLED END CRACK AT RT WING O/B L/E RIBS STA XFS 772, XFS 779 & XFS 785 IAW DC-8 SRM 51-3-2 PG 1 PAR 1 & SRM 57-2-0 PG 9/1Apr 30, 1999 · N802DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL9980257CSeat Track · crackedC-CHECK, SEAT TRACK NR 2 BETWEEN STA 240-260 PLUG NO GOOD. REMOVED (1) DAMAGED (4) FOUR HOLES CARGO TRACK REPAIR FROM NR 2 SEAT TRACK STA 240-260 IAW DC-8 SRM 51-3-0 PAR 1 & 2 FIG. CLEANED REPAIRED AREA PER SRM 51-1-8 PAR 6A. TREATED & PRIMED AREA IAW DC-8 Apr 30, 1999 · N802DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL9980256CRib · crackedC-CHECK, RT WING OUTB L/E INT THRU ACCESS PANEL 518B CRACKED RIBS AT UPPER END XFS 766.25 & XFS 760 DOT 64127-64128. STOPPED DRILLED END CRACK AT RT WING O/B L/E RIB STA XFS 766.250 & 760 IAW DC-8 SRM 57-2-0 PG 10 FIG 2. TREATED & PRIMED PER DC-8 SRM 51-1-8 Apr 30, 1999 · N802DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL9980255CRib · crackedC-CHECK, RT WING O/B L/E INTO THRU ACCESS PANEL 519C CRACKED RIBS TO UPPER END XFS 622 AND XFS 644 DOT 64131-64132. STOP DRILLED END CRACK AT RT WING O/B L/E RIBS STA XFS 641 & 622 IAW DC-8 SRM 57-2-0 PG 9 FIG 2. FABRICATED ANGLE REPAIR 2024 T3 050 .75 X 1.2Apr 30, 1999 · N802DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL9980254CRib · crackedC-CHECK, RT WING O/B L/E INT THRU ACCESS PANEL S/B CRACKED RIBS AT UPPER END XFS 728 & XFS 747 DOT 64129-64130. STOP DRILLED END CRACK AT RT WING O/B L/E RIBS STA XFS 728 &747 IAW DC-8 SRM 57-2-0 PG 9 FIG 2. FABRICATED ANGLE REPAIR 2024T3 050 .75 X 1.25 X 5 Apr 30, 1999 · N802DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL9980252CSeat Track · wornC-CHECK, SEAT TRACK NR 2 BETWEEN STA 1560-1610 TRACK WORN/CHIPPED. CUT OUT DAMAGED SECTION OF SEAT TRACK NR 2 BETWEEN STA 1560 TO 1650 & PREPARED NEW SECTION FROM: APPROPPIATE MATCHING SECTION OF TRACK & FABRICATED SPLICES FROM:7075-T6 0.100 (1 X 13) 0.125 (1Apr 30, 1999 · N802DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL9980237CSeat Track · crackedC-CHECK, SEAT TRACK NR 1 BETWEEN STA 480-580 TRACK HAS CORRODED SPOTS. CUT OUT DAMAGED SECTIONS OF TRACK NR 1 STA 520 IAW DC-8 SRM 53-2-3 FIG 6D SHEET 1-3. CLEANED REWORKED AREA PER SRM 51-1-8 PAR 6. TREATED & PRIMED REWORKED AREA IAW DC-8 SRM 51-1-8 PG 13 Apr 30, 1999 · N802DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL9980236CSeat Track · crackedC-CHECK, SEAT TRACK NR 1 BETWEEN STA 329 TO 380 TRACK HAS CORROSION. CUT OUT DAMAGED SECTION OF TRACK NR 1 AT STA 329 & CLEANED AREA OF SEAT TRACK BETWEEN STA 329 TO 380 IAW DC-8 SRM 53-2-3 FIG 6D SHEET 1 & 51-1-8 PAR 6A. FOUR HOLES CARGO TRACK REPAIR INSTALApr 30, 1999 · N802DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL9980235CSpar · crackedC-CHECK, RT WING AT REAR SPAR AREA XW 5 WEB PANEL IS CRACK 3 LONG DOT 64101. STOP DRILLED END CRACK AT RT WING, REAR SPAR ARA XW5 WEB PANEL IAW DC-8 SRM 51-3-2. FABRICATED DOUBLER REPAIR AS PER SRM 57-2-0 PAR 2 E 6 X 6 .090-2024T3. TREATED & PRIMED AS PER SApr 30, 1999 · N802DH · Doug DC873F · Wing SparSDR DHL9980234CFitting · crackedC-CHECK, LT STA 97 FLAP HINGE SUPPORT FITTING HAS TWO CRACK INDICATION, ONE IN LT SIDE NR 2 HOLE & ONE IN RT SIDE NR 1 HOLE MARKED. ENLARGED CRACKED HOLES TO THE LIMITATIONS CONTAINED ON SR DRAWING 5894377 & CRACK WAS NOT REMOVED. REMOVED O/B FITTING STA 97 Apr 30, 1999 · N802DH · Doug DC873F · Trailing Edge FlapsSDR DHL9980209CSeat Track · corrodedC-CHECK, SEAT TRACK NR 1 STA 980-1080 TRACK IS CORRODED. CUT OUT DAMAGED SECTIONS OF TRACK NR 1 STA 1100 IAW DC-8 SRM 53-2-3 FIG 6D SHEET 1-3. CLEANED REWORKED AREA PER SRM 51-1-8 PAR 6A. TREATED & PRIMED REWORKED AREA IAW DC-8 SRM 51-1-8 PG 13 & 16. INSTAApr 30, 1999 · N802DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL9980208CSeat Track · corrodedC-CHECK, SEAT TRACK NR 1 BETWEEN STA 880-980 TRACK WAS CORRODED. CUT OUT DAMAGED SECTION OF TRACK NR 1 AT STA 920 AND CLEANED AREA OF TRACK BETWEEN STA 880-980 IAW DC-8 SRM 53-2-3 FIG 6D SHEET 1 & 51-1-8 PARA 6A. OK TO TREAT AND PRIME REWORKED AREA IAW DC-8 Apr 30, 1999 · N802DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL9980205CSkin · crackedC CHECK, NONROUTE ENG #4 INSIDE CENTER PYLON SECTION GENERATOR FEEDER CABLE SUPPORT HAD CRACK DAMAGE ON SURFACE. REMOVED GENERATOR FEEDER CABLE SUPPORT AS PER DC8 MM 20-50-1. CUT OUT CRACKED AREAS FROM PANEL AT NR 4 PYLON CENTER AREA IAW DC8 SRM 3-2-0 FIG 23Apr 30, 1999 · N802DH · Doug DC873F · Nacelle/Pylon, Plate/SkinSDR DHL9980263CSeat Track · wornC-CHECK, SEAT TRACK NR 3 BETWEEN STA 400-440 TRACK WORN. REMOVED (2) DAMAGED, FOUR HOLES CARGO TRACK REPAIR FROM NR 3 SEAT TRACK STA 400-440 IAW DC-8 SRM 51-3-0 PAR 1 & 2. CLEANED REPAIRED AREA PER SRM 51-1-8 PAR 6A. TREATED & PRIMED AREA IAW DC8 SRM 51-1-8Apr 29, 1999 · N802DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL9980262CSeat Track · wornC-CHECK, SEAT TRACK NR 3 BETWEEN STA 320-340 TRACK WORN. CUT OUT DAMAGED SECTION OF SEAT TRACK NR 3 BETWEEN STA 310 TO 370 & PREPARED NEW SECTION FROM APPROPIATED MATCHING SECTION OF TRACK & FABRICATED SPLICE FROM 7075-T6 0.100 (1 X 13) 0.125 (1 X 7) 0.160 (1Apr 29, 1999 · N802DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL9980261CSeat Track · wornC-CHECK, SEAT TRACK NR 4 BETWEEN STA 1300-1320 TRACK WORN. CUT OUT DAMAGED SECTION OF SEAT TRACK NUMBER 4 BETWEEN STA 1290-1350 & PREPARED NEW SECTION FROM APPROPRIATED MATCHING SECTION OF TRACK & FABRICATED SPLICES FROM: 7075-T6 0.100 (1 X 7) 0.160 (1 X 8) IApr 29, 1999 · N802DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL9980260CSeat Track · wornC-CHECK, SEAT TRACK NR 4 BETWEEN STA 221-260 TRACK WORN. CUT OUT DAMAGED SECTION OF SEAT TRACK NR 4 BETWEEN STA 210-250 & PREPARED NEW SECTION FROM APROPRIATE MATCHING SECTION OF TRACK & FABRICATED SPLICES FROM 7075-T6 1000 (1 X 13) 0.125 (1 X 7) 0.160 (1 X 8Apr 29, 1999 · N802DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL9980259CSeat Track · wornC-CHECK, SEAT TRACK NR 4 BETWEEN STA 270-290 TRACK WORN. CUT OUT DAMAGED SECTIONS OF TRACK NR 4 STA 280-290 IAW DC-8 SRM 53-2-3 FIG 6D SHEET 1-3. CLEANED REWORKED AREA PER SRM 51-1-8 PAR 6A. TREATED & PRIMED REWORKED AREA IAW DC-8 SRM 51-1-8 PG 13 & 16. INApr 29, 1999 · N802DH · Doug DC873F · Fuselage, Seat/Cargo Attach Fittings
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