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 RRXA002661Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE SKIN ON THE LT UPPER SURFACE L/E BETWEEN STA XFS 666 & 672, 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 DCApr 29, 2000 · N8084U · Doug DC871F · Wing, Plate/SkinSDR RRXA002660Skin · damagedDURING A MAINTENANCE VISIT FOUND A SCREW PULLING THROUGH SKIN ON THE FWD FRONT SPAR AT STA XFS 710, 26 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.Apr 29, 2000 · N8084U · Doug DC871F · Wing, Plate/SkinSDR RRXA003491Doubler · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE DOUBLER BETWEEN FRAMES -12&8, +X=58 INCHES, -Z=11 INCHES, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. REMAINING THICKNESS IS WITHIN LIMITS.Apr 28, 2000 · N8084U · Doug DC871F · Fuselage Main, Plate/SkinSDR RRXA003490Doubler · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE UNDER THE FINGER DOUBLER AND POPPED RIVET HEADS AT STA -32+-52, X-15" TO 21", DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8.Apr 28, 2000 · N8084U · Doug DC871F · Fuselage Main, Plate/SkinSDR RRXA003489Finger Doubler · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FINGER DOUBLER AT STA -32, -X=20 TO 22 INCH RT -Z-11, 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 Apr 28, 2000 · N8084U · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00832446Doubler · crackedINSPECTION TYPE:C123, STA 690 LONG 34L TIE-END DOUBLER IS CRACKED. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5755058 AND SRM 51-1-20D.Apr 28, 2000 · N709UP · Doug DC871F · Fuselage Main, Plate/SkinSDR RRXA000441Fitting · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO ''Z'' FITTING AFT BAGGAGE AT STA 1220 AND LONGERON 36R - 35R , DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED AND REPLACED FITTING IAW DC8 SRM 53-2-0 FIG 2D. TREATED AREA IAW DC8 SRM 51-1-8. CORROSION Apr 27, 2000 · N8177U · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA000433Cargo Track · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO RT CARGO TIE DOWN AT STA 365 AND LONGERON 33R, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED AND REPLACED TRACK IAW DC8 SRM 51-1-24, 51-1-8, 51-3-2, 53-2-3 FIG 12. TREATED AREA IAW DC8 SRM 51-1-8. CORApr 27, 2000 · N8177U · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA000428Longeron · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LONGERON AT STA 216 - 220 AND LONGERON STR 36, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED AND REPLACED LONGERON IAW DC8 SRM 53-2-2 FIG 4A & 52-2-0 FIG 1F. TREATED AREA IAW DC8 SRM 51-1-8. CORROSIOApr 27, 2000 · N8177U · Doug DC871F · Fuselage Main, Longeron/StringerSDR RRXA000426Skin · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO INNER SKIN FWD, BELOW AND AFT OF NR 1 CARGO DOOR. DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED DAMAGED DOUBLER, TREATED AREA IAW DC8 SRM 51-1-8, FABRICATE PART AND INSTALLED IAW DC8 SRM 51-1-20 & 53-2Apr 27, 2000 · N8177U · Doug DC871F · Cargo/Baggage DoorsSDR RRXA000424Fitting · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA 420 AND LONGERON 33R - 34R, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED AND REPLACED FITTING IAW DC8 SRM 53-01-0, 53-2-0 FIG 2A, 53-02-0 FIG 1F. TREATED AREA IAW DC8 SRM 51-1-8. CORRApr 27, 2000 · N8177U · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA000414Fitting · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO DOOR FRAME FITTING FWD CARGO AT STA 320 AND STR 32R, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED AND REPLACED DOOR FRAME FITTING IAW DC8 SRM 53-2-0 FIG 1F, TREATED AREA IAW DC8 SRM 51-1-8. CORROSIONApr 27, 2000 · N8177U · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA000410Cap · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FWD CARGO END CAP AT STA 60 AND STR 36, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED DAMAGED END CAP, TREATED AREA IAW DC8 SRM 51-1-8, RECEIVED PART AND INSTALLED IAW DC8 SRM 53-01-0 AND 53-2-0 FIG 1FApr 27, 2000 · N8177U · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA000403Angle · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FLOOR SUPPORT ANGLE AT STA 25 - 55 AND LONGERON RBL 62, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED DAMAGED SUPPORT ANGLE, TREATED AREA IAW DC8 SRM 51-1-8, FABRICATE PART AND INSTALLED IAW DC8 SRM 53-Apr 27, 2000 · N8177U · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA000402Plate · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO SUPPORT PLATE FOR TOILET DRAINS AT STA 35 & 50 AND LONGERON RBL 50, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED DAMAGED SUPPORT PLATE, TREATED AREA IAW DC8 SRM 51-1-8, FABRICATE PART AND INSTALLED IAApr 27, 2000 · N8177U · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA000399Angle · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO CUSP ANGLE AT STA 25 - 55 AND LONGERON RBL 62, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC8 SRM 51-1-8, FABRICATED PART AND INSTALLED IAW DC8 SRM 51-1-1, 51-1-8, 51-1-20D Apr 27, 2000 · N8177U · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00832607Doubler · corrodedINSPECTION TYPE:C2, COCKPIT SUBFLOOR CAN DOUBLER AND FINGER DOUBLER ARE CORRODED BEYOND LIMITS AT STA -18 AT RBL 8. REMOVED, FABRICATED AND REPLACED DOUBLERS IAW DWG 5612298, SRO8530026 AND SRM 51-1-21, 51-1-20D.Apr 27, 2000 · N700UP · Doug DC871F · Fuselage Main, StructureSDR UPS00832581Fitting · crackedINSPECTION TYPE:C-2, LT HORIZ STAB I/B FWD UPPER T-ANGLE FITTING CRACKED STA XFS 60.00. REMOVED, FAB AND INSTALLED FITTING IAW SRM 51-1-20D & 51-1-11.Apr 27, 2000 · N700UP · Doug DC871F · Horizontal Stabilizer StructureSDR UPS00832562Attach Angle · crackedINSPECTION TYPE:C-2 WING BOX TO FLOORBEAM ATTACH ANGLE CRACKED STA 798 RBL-50. REMOVED, FAB AND INSTALLED ATTACH ANGLE IAW DWG NR 3643112 & SRM 51-1-20D.Apr 27, 2000 · N700UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00832559Attach Angle · crackedINSPECTION TYPE:C-2, WING BOX TO FLOORBEAM ATTACH ANGLE CRACKED STA 798 LBL-50. REMOVED AND REPLACED ATTACH ANGLE IAW SRM 51-1-20D & 51-1-21.Apr 27, 2000 · N700UP · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA003704Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON 33R AT STA 580, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORRApr 26, 2000 · N8084U · Doug DC871F · Fuselage Main, Longeron/StringerSDR RRXA000454Splice · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO SPLICE AT STA 1050 AND LONGERON 36, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED AND REPLACED SPLICE IAW DC8 SRM 53-2-0 AND 53-2-2 FIG 10. TREATED AREA IAW DC8 SRM 51-1-8. CORROSION DAMAGE RECORDED IApr 26, 2000 · N8177U · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA000451Fitting · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO Z FITTING AT STA 1220 AND LONGERON 36R - 35R, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED AND REPLACED Z FITTING IAW DC8 SRM 53-2-0 FIG 2D. TREATED AREA IAW DC8 SRM 51-1-8. CORROSION DAMAGE RECORDEDApr 26, 2000 · N8177U · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA000449Longeron · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LONGERON AT STA 1380 AND LONGERON 36L, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC8 SRM 51-1-8, FABRICATED PART AND INSTALLED IAW DC8 SRM 51-1-8 & 53-2-2 FIG 11. CORROSIOApr 26, 2000 · N8177U · Doug DC871F · Fuselage Main, Longeron/StringerSDR RRXA000446Fitting · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO Z FITTING AFT BAGGAGE AT STA 1160 AND LONGERON 35R-34R, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED AND REPLACED Z FITTING IAW DC8 SRM 53-2-0 FIG 2D. TREATED AREA IAW DC8 SRM 51-1-8. CORROSION DAMAGApr 26, 2000 · N8177U · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA000443Fitting · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO Z FITTING AFT BAGGAGE AT STA 1200 AND LONGERON 36L-35L, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED AND REPLACED Z FITTING IAW DC8 SRM 53-2-0 FIG 2D. TREATED AREA IAW DC8 SRM 51-1-8. CORROSION DAMAGApr 26, 2000 · N8177U · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA000439Clip · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO AFT CARGO SKIN CLIP AT STA 1240 AND LONGERON 34L TO 33R, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC8 SRM 51-1-8, FABRICATED PART AND INSTALLED IAW DC8 SRM 53-4-0 FIG 7 & Apr 26, 2000 · N8177U · Doug DC871F · Fuselage Main, StructureSDR RRXA000438Clip · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO AFT CARGO SKIN CLIP AT STA 1260 AND LONGERON 36L - 35L, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC8 SRM 51-1-8, FABRICATED PART AND INSTALLED IAW DC8 SRM 51-1-4 AND 51-1-Apr 26, 2000 · N8177U · Doug DC871F · Fuselage Main, StructureSDR RRXA000434Pressure Panel · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CABIN SHEAR WEB AND PRESSURE PANEL AT STA 848 AND LONGERON LEFT BL 44, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC8 SRM 51-1-8, REPLACED DOUBLER AND ANGLES IAW DC8 SRMApr 26, 2000 · N8177U · Doug DC871F · Fuselage Main, BulkheadSDR RRXA000420Stiffener · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO PRESSURE PANEL STIFFENER AT STA 960 - 980. DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC8 SRM 51-1-8, FABRICATE PART AND INSTALLED IAW DC8 SRM 51-1-8, 51-1-2 AND 53-2-0 FIGApr 26, 2000 · N8177U · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00832561Seat Track · crackedINSPECTION TYPE:C-2, STA 680 LBL -24 SEAT TRACK SUPPORT FITTING CRACKED. REMOVED, FAB AND INSTALLED SEAT TRACK SUPPORT FITTING IAW DWG NR 5773275 AND SRM 51-1-20D.Apr 26, 2000 · N700UP · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR UPS00832540Doubler · corrodedINSPECTION TYPE:C2, STA 730 - 780 ,LBL 8 -RBL 8, THE CENTER WING UPPER EXTERNAL DOUBLER HAS HEAVY CORROSION IN SEVERAL PLACES. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5643130.Apr 26, 2000 · N700UP · Doug DC871F · Wing, Center BoxSDR UPS00832533Fitting · corrodedINSPECTION TYPE:C2, STA 960 - 980, LBL 8 ON THE SUB FLOOR, THE FRAME TO WEB TIE FITTING HAS HEAVY CORROSION ON THE MATING FLANGE. REMOVED AND REPLACED FITTING IAW DWG 3640887U AND SRM 51-1-20D.Apr 26, 2000 · N700UP · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA003500Seat Track · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE ON SEAT TRACK 2ND FROM O/B RT SIDE FRAME AT STA 1120+X-48, Z-0, 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-Apr 25, 2000 · N8084U · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA003486Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE SKIN AT STA 700 TO 781 AND L35L TO L35R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-0 AND E.O. 00-107.Apr 25, 2000 · N8084U · Doug DC871F · Fuselage Main, Plate/SkinSDR RRXA000452Bracket · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO Z BRACKET AT STA 1220 AND LONGERON 36L-35L, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED AND REPLACED Z BRACKET IAW DC8 SRM 53-2-0 FIG 2D. TREATED AREA IAW DC8 SRM 51-1-8. CORROSION DAMAGE RECORDED Apr 25, 2000 · N8177U · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA000448Clip · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO SKIN CLIP AT STA 1260 AND LONGERON 36R - 35R, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC8 SRM 51-1-8, FABRICATE PART AND INSTALLED IAW DC8 SRM 51-1-4 & 51-1-8 FIG 7 & 8. Apr 25, 2000 · N8177U · Doug DC871F · Fuselage Main, StructureSDR RRXA000442Fitting · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO Z FITTING AT STA 1180 AND LONGERON 36L - 35L, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED AND REPLACED Z FITTING IAW DC8 SRM 51-1-24, 51-1-8 AND 53-2-0 FIG 2D. TREATED AREA IAW DC8 SRM 51-1-8. CORROApr 25, 2000 · N8177U · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA000440Structure · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO AFT CARGO RIB AT STA 1400 AND LONGERON 35L TO 35R, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC8 SRM 51-1-8, FABRICATE PART AND INSTALLED IAW DC8 SRM 53-04-1 AND 51-1-4 FIGApr 25, 2000 · N8177U · Doug DC871F · Fuselage Main, StructureSDR RRXA000429Longeron · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LONGERON AT STA 343 AND LONGERON 36, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED AND REPLACED LONGERON IAW DC8 SRM 53-2-0 FIG 1F. TREATED AREA IAW DC8 SRM 51-1-8. CORROSION DAMAGE RECORDED IN EWA CApr 25, 2000 · N8177U · Doug DC871F · Fuselage Main, Longeron/StringerSDR RRXA000427Finger Doubler · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FINGER DOUBLER AT STA 190 - 220 AND 240 - 450 AND LONGERON 31L , DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC8 SRM 51-1-8, FABRICATE PART AND INSTALLED IAW DC8 SRM 51-1-20 Apr 25, 2000 · N8177U · Doug DC871F · Fuselage Main, StructureSDR RRXA000425Finger Doubler · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FINGER DOUBLER AT SKIN SPLICE AT STA 190 AND LONGERON 30R TO 31R, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED AND REPLACED DOUBLER IAW DC8 SRM 53-4-0 AND 51-1-21. TREATED AREA IAW DC8 SRM 51-1-8. COApr 25, 2000 · N8177U · Doug DC871F · Fuselage Main, StructureSDR RRXA000423Strap · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO TIE STRAP AND FITTINGS AT STA 190 - 224 AND LONGERON 36, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-2, 53-2-2 FIG 4C, 51-1-20 FIG 2D, AND 53-2-0 FIG 1F. TREATEDApr 25, 2000 · N8177U · Doug DC871F · Fuselage Main, StructureSDR RRXA000419Finger Doubler · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FINGER DOUBLER AT STA 190 - 220, 240 - 450 AND LONGERON 31L, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED AND REPLACED DOUBLER IAW DC8 SRM 51-1-20 AND 53-2-1 FIG 7 & 8. TREATED AREA IAW DC8 SRM 51-1-8Apr 25, 2000 · N8177U · Doug DC871F · Fuselage Main, StructureSDR RRXA000417Fitting · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FRAME FITTING AT STA 260 AND STR 35L AND 36L, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED AND REPLACED FITTING IAW DC8 SRM 53-2-0 FIG 2D, TREATED AREA IAW DC8 SRM 51-1-8. CORROSION DAMAGE RECORDED INApr 25, 2000 · N8177U · Doug DC871F · Fuselage Main, Attach FittingsSDR RRXA000413Finger Doubler · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FINGER DOUBLER AT SKIN SPLICE FWD CARGO COMP AT STA 180 - 220 AND STR 31R TO 27R, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED AND REPLACED DOUBLER AND SPLICE IAW SRM 51-1-0, 51-1-21 AND 53-2-1 FIG 7 &Apr 25, 2000 · N8177U · Doug DC871F · Fuselage Main, StructureSDR RRXA000400Splice · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO SKIN SPLICE AT STA 1340 & 1360 AND LONGERON 35L & 35R, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC8 SRM 51-1-8, FABRICATED PART AND INSTALLED IAW DC8 SRM 53-2-2 AND 53-2-1 Apr 25, 2000 · N8177U · Doug DC871F · Fuselage Main, StructureSDR RRXA000396Finger Doubler · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FINGER DOUBLER IN SKIN SPLICE AT STA 1500 - 1520 AND LONGERON 27L TO 31L, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REPLACED DOUBLER IAW DC8 SRM 53-2-0 AND 53-04-1 FIG 7 & 8. CORROSION DAMAGE RECORDED IN EApr 25, 2000 · N8177U · Doug DC871F · Fuselage Main, StructureSDR UPS00832604Rib · chafedINSPECTION TYPE:C2, RIGHT WING L/E RIB HAS HOLE CHAFED IN IT AT XS 503.379. REPAIRED IAW SRM 57-2-0 FIG 2.Apr 25, 2000 · N700UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS00832571Stiffener · crackedINSPECTION TYPE:C-2, LEFT WING NUMBER 2 STUB WING VERTICAL STIFFENER CRACKED APPROX STA XS256. REMOVED, FAB AND INSTALLED IAW DWG NR 9753294 AND SRM 51-1-8, 51-1-20D.Apr 25, 2000 · N700UP · Doug DC871F · Wing Miscellaneous Structure
Back to Douglas DC-8-71F