Douglas DC-8-71F

Service difficulty reports · 8,938

Newest first. General aviation reporting is voluntary.

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 = 'DC871F'
  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 RRXA002769Frame · tornDURING A MAINTENANCE VISIT FOUND A TEAR TO THE FWD FRAME FOR CARGO DOOR UPPER CORNER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-0 AND 51-1-21.May 12, 2000 · N8084U · Doug DC871F · Fuselage Main, FrameSDR RRXA002763Intercostal · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE INTERCOSTAL AT STA 1100 TO 1120 AND L27R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-0 AND May 12, 2000 · N8084U · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA002753Intercostal · crackedDURING A MAINTENANCE VISIT FOUND CRACKED AND BENT BRACES ON THE FWD LOWER BILGE LEFT SIDE OF BULKHEAD AT STA 70, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SMay 12, 2000 · N8084U · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA002751Retainer · crackedDURING A MAINTENANCE VISIT FOUND A BENT FWD DOOR SEAT RETAINER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 51-1-4, 51-1-24 AND 51-1-21.May 12, 2000 · N8084U · Doug DC871F · Passenger/Crew DoorsSDR RRXA002747Web · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE CUSP WEB AT STA 980 TO 1000 LT SIDE AND L24L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-0, 51-1-4 AMay 12, 2000 · N8084U · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA002736Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE 3RD LOWER RIB ON THE RT WING MIDDLE L/E AT STA XFS 304, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57-2-0May 12, 2000 · N8084U · Doug DC871F · Wing, Rib/BulkheadSDR RRXA002735Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE 4TH RIB LOWER SURFACE ON THE RT WING MIDDLE L/E AT STA XFS 310, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRMay 12, 2000 · N8084U · Doug DC871F · Wing, Rib/BulkheadSDR RRXA002731Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE UPPER RIB ON THE RT WING O/B LEADING EDGE AT STA XFS 752, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57-2May 12, 2000 · N8084U · Doug DC871F · Wing, Rib/BulkheadSDR RRXA002730Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE UPPER RIB ON THE RT WING O/B LEADING EDGE AT STA XFS 748, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57-2May 12, 2000 · N8084U · Doug DC871F · Wing, Rib/BulkheadSDR RRXA002729Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK AT END OF UPPER RIB ON RT WING OUTBOARD L/E AT STA XFS 741, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57-2-0, 5May 12, 2000 · N8084U · Doug DC871F · Wing, Rib/BulkheadSDR RRXA002728Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACKED NR 12 UPPER RIB ON THE RT WING L/E MIDDLE SECTION AT STA XFS 408, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 5May 12, 2000 · N8084U · Doug DC871F · Wing, Rib/BulkheadSDR RRXA002727Gusset · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE LOWER RIB INTERCOSTAL GUSSET ON THE RT WING L/E MIDDLE SECTION AT STA XFS 350, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPMay 12, 2000 · N8084U · Doug DC871F · Wing Miscellaneous StructureSDR RRXA002725Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE NR 11 UPPER RIB ON THE RT WING LEADING EDGE MIDDLE SECTION AT STA XFS 408, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR May 12, 2000 · N8084U · Doug DC871F · Wing, Rib/BulkheadSDR RRXA002724Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE NR 8 UPPER RIB ON THE RT WING LEADING EDGE MIDDLE SECTION AT STA XFS 408, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IMay 12, 2000 · N8084U · Doug DC871F · Wing, Rib/BulkheadSDR RRXA002723Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE NR 7 UPPER RIB ON THE RT WING MIDDLE L/E AT STA XFS 407, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-7 SRM 57-2-May 12, 2000 · N8084U · Doug DC871F · Wing, Rib/BulkheadSDR RRXA002722Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE NR 5 UPPER RIB ON RT WING LEADING EDGE MID SECTION AT STA XFS 408, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8May 12, 2000 · N8084U · Doug DC871F · Wing, Rib/BulkheadSDR RRXA002712Stiffener · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE RT WING NR 4 STUB WING RT SIDE VERTICAL STIFFENER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 51-1-4 AND May 12, 2000 · N8084U · Doug DC871F · Wing Miscellaneous StructureSDR RRXA002709Baffle · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE LOWER SURFACE OF THE RT WING O/B LEADING EDGE DUCTED SKIN BAFFLE AT STA 678, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRMay 12, 2000 · N8084U · Doug DC871F · Wing Miscellaneous StructureSDR RRXA002702Skin · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE NOSE WHEEL WELL AFT RT CORNER OF CUTOUT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-1 AND 51-1-21.May 12, 2000 · N8084U · Doug DC871F · Fuselage Main, Plate/SkinSDR RRXA002682Frame · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE CENTER L/E UPPER FORMER AT TRAILING EDGE AT STA XFS 372, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57-2-May 12, 2000 · N8084U · Doug DC871F · Wing SparSDR RRXA002680Frame · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE CENTER L/E UPPER FORMER AT TRAILING EDGE AT STA XFS 366, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57-2-May 12, 2000 · N8084U · Doug DC871F · Wing SparSDR RRXA002679Frame · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE CENTER L/E UPPER FORMER AT TRAILING EDGE AT STA XFS 354, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57-2-May 12, 2000 · N8084U · Doug DC871F · Wing SparSDR RRXA002678Frame · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE CENTER L/E UPPER FORMER AT TRAILING EDGE AT STA XFS 348, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57-2-May 12, 2000 · N8084U · Doug DC871F · Wing SparSDR RRXA002677Frame · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE CENTER L/E UPPER FORMER AT TRAILING EDGE AT XFS 328, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57-2-0 ANMay 12, 2000 · N8084U · Doug DC871F · Wing SparSDR RRXA002674Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE UPPER RIB AT TRAILING EDGE I/B ON CENTER L/E AT XFS 477, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57-2-May 12, 2000 · N8084U · Doug DC871F · Wing, Rib/BulkheadSDR RRXA002670Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACKS TO THE DE-ICER BLEED HOLES ON THE LEADING EDGE O/B OF NR 1 PYLON, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57-2May 12, 2000 · N8084U · Doug DC871F · Wing, Plate/SkinSDR RRXA002658Brace · crackedDURING A MAINTENANCE VISIT FOUND A CRACK IN THE FIRST OVERHEAD BRACE LT SIDE AT STA 1916, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 5-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-0 AND 51-1-21.May 12, 2000 · N8084U · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA002758Longeron · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE LONGERON AT THE FWD LWR CARGO BILGE AT STA 560 TO 550 AND L33R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 53-2-0.May 10, 2000 · N8084U · Doug DC871F · Fuselage Main, Longeron/StringerSDR RRXA002708Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE RT WING NR 3 STUB WING NR 12 RIB UPPER T/E, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57-2-1, 57-2-0, 51May 10, 2000 · N8084U · Doug DC871F · Wing, Rib/BulkheadSDR RRXA002705Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE RT WING NR 3 STUB WING NR 6 RIB UPPER END, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57-2-0, 51-1-21 ANDMay 10, 2000 · N8084U · Doug DC871F · Wing, Rib/BulkheadSDR UPS00832551Panel · inoperativeINSPECTION TYPE:N/A, ATB- NR 4 GEN LOW VOLTAGE, CREW REPORTED SMOKE IN COCKPIT (DFW. *S/D* REMOVED AND REPLACED BUS PROTECTION PANEL.May 10, 2000 · N798UP · Doug DC871F · AC Generation SystemSDR RRXA003498Sill · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE R1 DOOR AFT SILL AT FR 600 AND L21R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PART IAW DC-8 SRM 51-1-4. (CORROSMay 5, 2000 · N8084U · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA003702Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FLOOR PANEL AT STA 50-70 X-50 Z-0, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PART IAW DC-8 SRM 51-1-4. (CORROSION DAMAGE RECOMay 4, 2000 · N8084U · Doug DC871F · Fuselage Floor PanelSDR RRXA003493Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE COCKPIT FLOOR PANEL AT SCREW HOLES AT STA -12, +32 TO -32, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW PANEL IAWMay 4, 2000 · N8084U · Doug DC871F · Fuselage Floor PanelSDR RRXA003492Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMMAGE TO THE COCKPIT PANEL 676B ALONG EDGE & SCREW HOLES AT FR -52X-20,Z0, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SKIN IMay 4, 2000 · N8084U · Doug DC871F · Fuselage Main, Plate/SkinSDR RRXA003488Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMGE TO THE LAV FLOOR PANEL FWD. CARGO COMPT. AT STA 220-240 AND X-40, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PANEL IAW DC-8 May 4, 2000 · N8084U · Doug DC871F · Fuselage Floor PanelSDR RRXA003699Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE AFT SIDE FRAME AT STA 1140 AND L36, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-0. (CORROSION DAMAGE RMay 3, 2000 · N8084U · Doug DC871F · Fuselage Main, FrameSDR RRXA003497Intercostal · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE CABIN FLOOR RT INTERCOSTAL AT STA 660, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW PART IAW DC-8 SRM 51-1-21. (CMay 3, 2000 · N8084U · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA002756Skin · bulgedDURING A MAINTENANCE VISIT FOUND A BULGE TO THE SKIN IN THE FWD LWR CARGO BILGE AT STA 622 AND L36 TO L35L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW EO NR 00-107 May 2, 2000 · N8084U · Doug DC871F · Fuselage Main, Plate/SkinSDR RRXA002733Skin · dentedDURING A MAINTENANCE VISIT FOUND A PREVIOUS DENT REPAIR FILLER DETERIORATED AND DEBONDING ON THE RT WING EXTERIOR L/E AT STA XFS 737, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAMay 2, 2000 · N8084U · Doug DC871F · Wing, Plate/SkinSDR UPS00832543Pressure Panel · corrodedINSPECTION TYPE:C2, LT WHEEL WELL PRESSURE PANEL IS CORRODED OUT OF LIMITS AT STA 970, LBL8. REPAIRED AREA IAW SRM 53-2-0.May 2, 2000 · N700UP · Doug DC871F · Fuselage Main, StructureSDR RRXA002657Skin · dentedDURING A MAINTENANCE VISIT FOUND 2 DENTS IN SKIN BELOW GROUND POWER RECPT PLATE AT NOSE GEAR/FWD DOOR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-0,May 1, 2000 · N8084U · Doug DC871F · Landing Gear DoorsSDR RRXA000447Fitting · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO Z FITTING AT STA 1160 AND LONGERON 36L - 35L. DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED AND REPLACED Z FITTING IAW DC8 SRM 53-1-2 FIG 1. TREATED AREA IAW DC8 SRM 51-1-8. CORROSION DAMAGE RECORDEDMay 1, 2000 · N8177U · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA000415Fitting · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FWD CARGO DOOR FRAME FITTING AND FASTENER AT STA 315 AND STR 32L, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED AND REPLACED CORRODED FITTING IAW DC8 SRM 53-1-02 AND MM 20-16-0 FIG 1. TREATED AREA IAW May 1, 2000 · N8177U · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA000412Frame · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FWD CARGO FRAME AT STA 120 AND STR 30R AND 27R, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED AND REPLACED DAMAGED FRAME, TREATED AREA IAW DC8 SRM 51-1-8, INSTALLED IAW DC8 SRM 53-2-0 FIG 1. CORROSIONMay 1, 2000 · N8177U · Doug DC871F · Fuselage Main, FrameSDR RRXA000411Frame · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FRAME, FWD CARGO AT STA 100 AND STR 35L - 35R, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC8 SRM 51-1-8, RECEIVED PART AND INSTALLED IAW DC8 SRM 53-1-2. CORROSION DAMAGE REMay 1, 2000 · N8177U · Doug DC871F · Fuselage Main, FrameSDR RRXA000397Frame · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MID CARGO AT STA 607 AND STR 34L AND 35R, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED DAMAGE DOUBLER, TREATED AREA IAW DC8 SRM 51-1-8, FABRICATE PART AND INSTALLED IAW DC8 SRM DC8 SRM 51-1-9 & SRM 5May 1, 2000 · N8177U · Doug DC871F · Fuselage Main, FrameSDR UPS00832583Cap · crackedINSPECTION TYPE:C-2, STA 857 CENTER WING TANK UPPER CHORD CRACKED AND CORRODED BEYOND LIMITS. REMOVED AND INSTALLED NEW SPAR CAP IAW SRM 51-1-20D & 51-1-21.May 1, 2000 · N700UP · Doug DC871F · Wing, Center BoxSDR UPS00832470Rib · crackedINSPECTION TYPE:N/A, LEFT WING INBOARD SPOILER OUT HINGE POINT ATTACH FRAME APPEARS TO HAVE A CRACK. *S/D* REMOVED CRACKED FRAME BPT 92716 4-30-00, FABRICATED NEW FRAME PER SRM 57-5-1. NEEDS HEAT TREAT BPT 5-2-00 RB 09282 MF 33016, INSTALLED NEW FRAME AND IApr 30, 2000 · N707UP · Doug DC871F · SpoilersSDR RRXA002668Skin · crackedDURING A MAINTENANCE VISIT FOUND A CRACK FROM SCREW HOLE ON THE LEFT L/E LWR SURFACE AT STA XFS 710, 26 INCHES FROM FRONT SPAR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REApr 29, 2000 · N8084U · Doug DC871F · Wing, Plate/Skin
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