Douglas DC-8-73F

Service difficulty reports · 15,471

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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 = 'DC873F'
  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 RRXA991610Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, AFT PIT FRAME AT STA 1500 AND LONGERON 26 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FRAME REPAIR IAW DC8 SRM 53-2-0. (CORROSMay 20, 1999 · N604AL · Doug DC873F · Fuselage Main, FrameSDR RRXA991622Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, LEFT WING, UPPER SURFACE (SKIN) CENTER L/E AT STA XFS 450.000 AT FRONT SPAR. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FILLER AND DOUBLER IAW May 19, 1999 · N604AL · Doug DC873F · Wing, Plate/SkinSDR UPS99829635Window · out of adjustINSPECTION TYPE:N/A, F/O SLIDE WINDOW WILL ONY OPEN INTERMITTENTLY. ADJUSTED F/O CLEARVIEW WINDOW PER MM 56-10-03, OPS CHECK GOOD.May 18, 1999 · N805UP · Doug DC873F · Flight Compartment WindowsSDR RRXA991608Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, AFT LWR CARGO COMPT AT STA 1540 AND LONGERON 33 RIGHT, CRACKED AND CORRODED 2 FTY AFT OF BULKHEAD. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND IMay 18, 1999 · N604AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS99829725Frame · damagedINSPECTION TYPE:C1, MAIN CABIN FRAME STA 480 L10R HAS HOLE FABBED REPAIR ANGLE IAW REO-06496. FABBED FILLER IAW REO-06496, ALODINED AND PRIMED REPAIR ANGLE AND FILLER IAW DC8 SRM 51-1-8, INSTALLED REPAIR WITH HI-LOKS IAW DC8 SRM 51-1-20D.May 17, 1999 · N851UP · Doug DC873F · Fuselage Main, FrameSDR UPS99829620Battery Pack · dischargedINSPECTION TYPE:N/A, EMERGENCY LIGHTS WILL NOT TEST. REMOVED AND REPLACED BATTERY PACK IAW M/M 33-50-01, OPS CHK GOOD. (P/N 5708458-503), (S/N 1132) ON, (P/N 10382) OFF.May 17, 1999 · N809UP · Doug DC873F · Emergency LightingSDR RRXA991599Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, LWR FUSELAGE KEEL PANEL NR 161CC, HAD CORROSION BLISTERS, BARE METAL LIGHT CORROSION, AT STA 960 AND LONGERON 36. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FMay 16, 1999 · N604AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA991605Door Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, AFT LWR CARGO COMPT AFT DOOR FRAME FOR THRESHHOLD AND CRACKED AT STA 1440 AND LONGERON 30 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM.. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INMay 15, 1999 · N604AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA991604Seat Track · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, AFT LWR CARGO COMPT BETWEEN STA 1240 AND STA 1320, AT LONGERON 36 FLOOR TRACK. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SECTIONMay 15, 1999 · N604AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA991349Doubler · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FINGER DOUBLER, B-PIT, LEFT FWD BETWEEN STA 460 AND STA 480 AT LONGERON 31 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FINGER DOMay 15, 1999 · N606AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA991607Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, AFT LWR CARGO COMPT BETWEEN STA 1500 AND STA 1504 AT LONGERON 26 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED NEW SECTION OF LONGERON AND SPLICMay 14, 1999 · N604AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR RRXA991606Bracket · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, AFT LWR CARGO COMPT AT STA 1395 AND LONGERON 33 RIGHT INSIDE LIGHT HOLE PIECE OF METAL MISSING AND LIGHT CORROSION. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. May 14, 1999 · N604AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA991594Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, INTERNAL SKIN SECTION, BETWEEN STA 49.5 AND STA 64, AND BETWEEN LONGERONS 33 RIGHT AND LONGERON 35 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATEMay 14, 1999 · N604AL · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS99829780Frame · corrodedINSPECTION TYPE:C1, FWD PIT FS 640 L33L CORROSION ON WALL TO FRAME AND ATTACH ANGLE DOT N 619. CLEANED CORROSION, CORROSION BEYOND LIMITS, FABRICATED REPAIR ANGLE PER DC8 DWG 56104-16 ANGLE PER DC8 SRM 51-1-20D.May 13, 1999 · N851UP · Doug DC873F · Fuselage Main, FrameSDR UPS99829775Skin · corrodedINSPECTION TYPE:C1, FWD PIT FS 600 L36 CORROSION ON SKIN DOT 0441. REMOVED FASTENERS FOR ACCESS, REMOVED CORROSION, ALODINED AND PRIMED IAW UPS DC8 SRM 51-1-8. FASTENERS TO BE INSTALLED ON UPS N/R 936077.May 13, 1999 · N851UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS99829777Longeron · corrodedINSPECTION TYPE:C1, CORROSION ON LONGERON 31R ACCESSORY COMPARTMENT STA 660. FABRICATED REPAIR ANGLE IAW REO 06502, ALODINED AND PRIMED IAW DC8 S RM 51-1-8, INSTALLED REPAIRED ANGLE IAW DC8 SRM 51-1-20D.May 12, 1999 · N851UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS99829613Seat Track · corrodedINSPECTION TYPE:C3, FS 1300, 1310, 1320 AND 1340, RBL 45 THE SEAT TRACK HAS HEAVY CORROSION. CUT OUT DAMAGED SECTION, FABRICATED AND REPLACED SEAT TRACK IAW SRM 53-2-3.May 11, 1999 · N840UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS99829563Battery Pack · dischargedINSPECTION TYPE:N/A, EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHTS BATT PACK, OPS CHECK GOOD. (P/N 60-1223-5), (S/N 339) ON, (S/N 337) OFF.May 11, 1999 · N803UP · Doug DC873F · Emergency LightingSDR RRXA991596Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO EXTERNAL SKIN SECTION BETWEEN STA 25 AND STA 55 BETWEEN LONGERONS 23 RIGHT AND LONGERON 25 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED ANDMay 11, 1999 · N604AL · Doug DC873F · Fuselage Main, Plate/SkinSDR 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 UPS99829636Frame · crackedINSPECTION TYPE:C3, FS 55 FRAME IS CRACKED AT LONG 24R. REPAIRED FRAME IAW SRM 53-2-0 FIG 2.May 10, 1999 · N840UP · Doug DC873F · Fuselage Main, FrameSDR RRXA991362Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FLOOR TRACK NR 4 SUPPORT FITTING AT STA 1700, BL 35 LEFT, LONGERON 21 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FITTING IAW DAMay 10, 1999 · N606AL · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99829590Floorbeam · corrodedINSPECTION TYPE:C3, FS 70 FLOORBEAM AT RBL 48 IS CORRODED BEYOND LIMITS. REPAIRED FLOORBEAM IAW DHC SK840-349.May 8, 1999 · N840UP · Doug DC873F · Fuselage Main, Floor BeamSDR 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 DHL99873004Transducer · failedUNCOMMANDED RUDDER INPUTS, TURNED YAW DAMPER OFF AND NO SIGNIFICANT CHANGE. INSPECTED AND FOUND YAW CHANNEL COMPUTER FAILED SEVERAL TESTS. REMOVED AND REPLACED YAW COMP PER MM 22-11-1. ALSO, REMOVED AND REPLACED RUDDER POSITION TRANSDUCER TRANSFORMER PER MMay 5, 1999 · N873SJ · Doug DC873F · Autopilot SystemSDR UPS99829581Fitting · corrodedINSPECTION TYPE:C2 FITTING AT FS 280 AND LONGERON 34L IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW SRM 51-3-0.May 4, 1999 · N880UP · Doug DC873F · Fuselage Miscellaneous StructureSDR 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 UPS99829654Longeron · corrodedINSPECTION TYPE:C2, LONG 28L FS 1160 TO 1180 IS CORRODED BEYOND LIMITS. REPAIRED IAW DH SK880-651.May 3, 1999 · N880UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS99829543Skin · crackedINSPECTION TYPE:C2, RT O/B LEADING EDGE SKIN IS CRACKED BETWEEN FASTENERS AT XW 761. REPAIRED SKIN IAW SRM 57-2-1 FIG 2H.May 3, 1999 · N880UP · Doug DC873F · Wing, Plate/SkinSDR UPS99829533Strap · corrodedINSPECTION TYPE:C2 FS 610, LONGERON 31L TO 31R, THE STRAP IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND INSTALLED STRAP IAW DWG 5779913 CPCP.May 3, 1999 · N880UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99829528Doubler · corrodedINSPECTION TYPE:C2 FS 610, LONGERON 31L TO 31R, THE FINGER DOUBLER IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND INSTALLED FINGER DOUBLER IAW DWG 5779913 AND SRM 51-1-21. CPCPMay 3, 1999 · N880UP · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA991364Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, MID AC COMPARTMENT ACCESS DOOR FRAME, FWD SIDE AROUND CAM LOCK HOLES, AT STA 640, BETWEEN BL 12 RIGHT AND BL 24 RIGHT, AT WL 45 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IMay 3, 1999 · N606AL · Doug DC873F · Fuselage Main, FrameSDR 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 Structure
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