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 RRXA002767Plate · gougedDURING A MAINTENANCE VISIT FOUND SEVERAL DENTS/GOUGES AROUND D PIT DOOR EXTERNAL, 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 AND 51-1-21.Jun 8, 2000 · N8084U · Doug DC871F · Cargo/Baggage DoorsSDR RRXA002715Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE CANOE FITTING ON THE RT WING AT STA 410, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8 AND EO NR 00-107 WITH APPROVED 8110-3 DATED 6-6-00. (CORROJun 8, 2000 · N8084U · Doug DC871F · Wing, Attach FittingsSDR RRXA002710Vane · damagedDURING A MAINTENANCE VISIT FOUND ENLARGED SCREW HOLES ON THE NR 2 RT FLAP VANE, 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 51-3-2 AND EO NR 00-107 WITH APPROVED 8110-Jun 8, 2000 · N8084U · Doug DC871F · Trailing Edge FlapsSDR RRXA002690Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE CANOE FITTING AT STA 410 LT WING, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8 AND EO NR 00-107 WITH APPROVED 8110-3 DATED 6-6-00. (CORROSION DAJun 8, 2000 · N8084U · Doug DC871F · Wing, Attach FittingsSDR UPS00833392Web · corrodedINSPECTION TYPE:C123, CORROSION ON MEMBRANE AND CUSP UNDER SIDE RT STA 37 SPLICED IN NEW SECTION OF CUSP IAW REO-G07444.Jun 8, 2000 · N708UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00833389Floorbeam · crackedINSPECTION TYPE:C123, FWD LWR CARGO PIT AT FS 340, FLOORBEAM AT RBL 40 IS CRACKED. REPAIRED PER TIMCO REO G07463, ALODINED AND PRIMED PER DC8 SRM 51-1-8. INSTALLED PER DC8 SRM 51-3-0, TIMCO REO-G07463.Jun 8, 2000 · N708UP · Doug DC871F · Fuselage Main, Floor BeamSDR UPS00833364Skin · crackedINSPECTION TYPE:C123, LWR FUSELAGE SKIN AT STA 120 ANTENNA MOUNTING AREA HAS CRACKED HOLE. FABBED REPAIR IAW DC8 SRM 53-2-1 FIG 7, ALODINED AND PRIMED REPAIR PER DC8 SRM 51-1-8, INSTALLED REPAIR PER DC8 SRM 51-1-21 AND DC8 SRM 51-1- 20D.Jun 8, 2000 · N708UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS00833362Attach Angle · corrodedINSPECTION TYPE:C123, FWD LWR CARGO PIT AT FS 300 - 320 LONG 35 FITTING ATTACH ANGLE CORRODED IN DOORWAY. REMOVED ZEE FITTING AT FS 320 LONGERON SECTION FS 310 - 330 L35R IAW DC8 SRM 51-1-24, FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. FABBED ZEE ANGLE REPJun 8, 2000 · N708UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00833314Fitting · corrodedINSPECTION TYPE:C123, LONG AND SPLICE FITTING ARE CORRODED. REMOVED A OLD FITTING. RECEIVED NEW FITTING IAW P/N 379919-501U. LOCATED, DRILLED AND DEBURRED IAW DC8 SRM 51-1-24. INSTALLED FITTING IAW DC8 SRM 51-1-20D.Jun 8, 2000 · N708UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00833312Splice · crackedINSPECTION TYPE:C123, SPLICE FITTING IS CRACKED. REMOVED CRACKED SPLICE FITTING. RECEIVED NEW FITTING. LOCATED, DRILLED AND DEBURRED FITTING IAW DC8 SRM 51-1-24B. INSTALLED FITTING IAW DC8 SRM 51-1-24.Jun 8, 2000 · N708UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00833310Splice · crackedINSPECTION TYPE:C123, SPLICE FITTING IS CRACKED. REMOVED AND REPLACED SPLICE FITTING IAW DC8 SRM 51-1-20D, 51-1-24.Jun 8, 2000 · N708UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00833058Rib · crackedINSPECTION TYPE: C123. LT WING CENTER L/E UPPER RIB CRACKED AT STA XFS 518 STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 57-2-0.Jun 8, 2000 · N708UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS00833057Longeron · corrodedINSPECTION TYPE: C123. LONGERON IS CORRODED UNDER SPLICE FITTING. REMOVED SPLICE FITTING TO ACCESS TO CORROSION. FOUND TO BE OUT OF LIMITS IAW DC8 53-2-0. REMOVED DAMAGED SECTION IAW DC8 SRM 53-2-2. FABRICATED NEW SECTION & INSTALLED NEW SECTION & SPLIJun 8, 2000 · N708UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR RRXA002776Skin · cutDURING A MAINTENANCE VISIT FOUND SEVERAL CUTS IN NR 4 ENG O/B T/R INTER RING COWL, 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 WITH APPROVED 8110-3 DATEJun 7, 2000 · N8084U · Doug DC871F · Nacelle/Pylon, Plate/SkinSDR RRXA002714Skin · damagedDURING A MAINTENANCE VISIT FOUND OVERSIZED ATTACH HOLES TO THE STUB WING OVER NR 3 ENG O/B UPPER SURFACE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW EO NR 00-107 WITH APPROVEDJun 7, 2000 · N8084U · Doug DC871F · Wing, Plate/SkinSDR RRXA002707Angle · crackedDURING A MAINTENANCE VISIT FOUND A CRACKED NR 11 RIB ON THE RT WING NR 3 STUB LWR LT RIB ANGLE AT STA XS 246, 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 EO NR 00-Jun 7, 2000 · N8084U · Doug DC871F · Wing Miscellaneous StructureSDR RRXA002691Skin · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE SCREW HOLE 33 INCHES FROM LEADING FROM SPAR LWR, ON LT CENTER SECTION L/E AT STA 520, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALJun 7, 2000 · N8084U · Doug DC871F · Wing, Plate/SkinSDR RRXA002662Skin · damagedDURING A MAINTENANCE VISIT FOUND LOOSE SCREWS ON THE LEFT O/B SLOT L/E AT STA 520 33 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 REPAIR IAW EO NR 00-1Jun 7, 2000 · N8084U · Doug DC871F · Fuselage Main, Plate/SkinSDR RRXA002656Panel · bulgedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE T/E UPPER SURFACE AT STA XE 245, 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 51-1-21 AND EO NR 00-107 WITH APPROJun 7, 2000 · N8084U · Doug DC871F · Wing, Plate/SkinSDR UPS00833311Fitting · crackedINSPECTION TYPE:C123, AIR COND COMPT RT SIDE L31 FITTING TO FS 70 CRACKED. REMOVED CRACKED FITTING RT L31 FS 70 IAW DC8 SRM 51-1-20D, LOCATED, DRILLED NEW FITTING IAW DC8 SRM 51-1-24 AND INSTALLED FITTING IAW DC8 SRM 51-1-20D.Jun 7, 2000 · N708UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00833055Structure · corrodedINSPECTION TYPE: C123. FLCP AT FS 260 FRAME HAS CORROSION & BAREMETAL FROM LONGERON 35LT - 33 RT. REMOVED CORROSION IAW DC8 SRM 51-1-8, WITHIN LIMITS IAW DC8 SRM 53-2-0. ALODINED & PRIMED IAW DC8 SRM 51-1-8.Jun 7, 2000 · N708UP · Doug DC871F · Fuselage Main, StructureSDR UPS00833054Longeron · corrodedINSPECTION TYPE: C123. FWD LWR CARGO PIT AT BS 180 - 200, LONGERON 36 IS CORRODED ON BOTH SIDES. REMOVED CORROSION IAW DC8 SRM 51-1-8 WITHIN LIMITS IAW DC8 SRM 53-2-0. ALODINED & PRIMED IAW DC8 SRM 51-1-8.Jun 7, 2000 · N708UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR RRXA002759Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE TOP OF CIRCUMFERENTIAL FRAME AT STA 1400 AND L36, 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-Jun 6, 2000 · N8084U · Doug DC871F · Fuselage Main, FrameSDR UPS00833053Door Frame · crackedINSPECTION TYPE: C123. RT AFT SERVICE DOOR, AFT DOOR FRAME WEB CRACKED AT LIGHTNING HOLE FOR DOOR WARNING SWITCH. ROUTED OUT DAMAGE IAW DC8 SRM 53-2-0. ALODINED & PRIMED IAW DC8 SRM 51-1-8.Jun 6, 2000 · N708UP · Doug DC871F · Fuselage Main, StructureSDR RRXA002752Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FWD LWR CARGO BILGE AT STA 350 AND L35R LT SIDE, 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 53-2Jun 5, 2000 · N8084U · Doug DC871F · Fuselage Main, Longeron/StringerSDR RRXA002726Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK THROUGH UNDER GUSSET ON THE NR 11 LOWER RIB 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 INSTAJun 5, 2000 · N8084U · Doug DC871F · Wing, Rib/BulkheadSDR UPS00833056Rib · crackedINSPECTION TYPE: C123. LT WING, CENTER L/E UPPER RIB CRACKED AT STA XFS 404 . STOP DRILLED CRACK IAW DC8 SRM 57-3-3. FAB REPAIR ANGLE FROM MAT .0 71 EXT. 7075 T6 PO NR 316089 IAW DC8 SRM 57-3-3. ALODINED, PRIMED & I NSTALLED IAW DC8 SRM 51-1-8, 51-1-20D,Jun 5, 2000 · N708UP · Doug DC871F · Wing, Rib/BulkheadSDR RRXA002701Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE AND CRACK TO LONGERON 31R AT STA 8 TO -67, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW PART IAW DC-8 SRM 51-1-0 AND 51-1-2Jun 2, 2000 · N8084U · Doug DC871F · Fuselage Main, Longeron/StringerSDR RRXA002790Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE INSIDE LONGERON UNDER CIRCUMFERENTIAL FRAME AT STA 600 AND L35R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Jun 1, 2000 · N8084U · Doug DC871F · Fuselage Main, Longeron/StringerSDR RRXA002770Frame · brokenDURING A MAINTENANCE VISIT FOUND A BROKEN FRAME AND SEAT TRACK AT STA 240 3RD SEAT TRACK FROM LT SIDE OF CABIN, 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 EO NR 0Jun 1, 2000 · N8084U · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA002766Rib · damagedDURING A MAINTENANCE VISIT FOUND DAMAGE TO THE LT SIDE L2 DOOR LWR RIB FWD NUT PLATE, 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 EO NR 00-107 WITH APPROVED 8110-3Jun 1, 2000 · N8084U · Doug DC871F · Passenger/Crew DoorsSDR RRXA002671Bracket · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE BRACKET AT BOTTOM ON THE L/E SECTION ABOVE NR 1 PYLON I/B AT STA 526, 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 DJun 1, 2000 · N8084U · Doug DC871F · Wing, Attach FittingsSDR RRXA002765Frame · damagedDURING A MAINTENANCE VISIT FOUND A HOLE IN FLANGE AT STA 1400 AND L35R, 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 EO NR 00-107 WITH APPROVED 8110-3 DATED 5-24-00May 31, 2000 · N8084U · Doug DC871F · Fuselage Main, FrameSDR RRXA002748Intercostal · tornDURING A MAINTENANCE VISIT FOUND A TORN SIDEWALL ATTACH FRAME IN CARGO PIT (INTERCOSTAL) AT FS 500 - 520 RT, 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 31, 2000 · N8084U · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00832893Frame · corrodedINSPECTION TYPE:C123, STA 1746 FRAME IS CORRODED BEYOND LIMITS BETWEEN LONG 29L AND 30L. REPAIRED FRAME IAW EO DC8-5310-11728-A AND DC8-53A-010.May 31, 2000 · N730UP · Doug DC871F · Fuselage Main, FrameSDR RRXA002667Skin · damagedDURING A MAINTENANCE VISIT FOUND TOO LONG OF SCREWS AND SCREWS PULLING THROUGH SKIN ON THE LEFT I/B SLOT L/E AT STA XS 250 46.5 INCHES FROM FRONT SPAR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE. FABRICATED AND INSTALLED REPAIR IAW EO 00-107 WITMay 30, 2000 · N8084U · Doug DC871F · Leading Edge DevicesSDR RRXA005667Skin · damagedDURING A MAINTENANCE VISIT FOUND TOO LONG OF SCREWS AND SCREWS PULLING THROUGH SKIN ON THE LEFT I/B SLOT L/E AT STA XS 250 46 .5 INCHES FROM FRONT SPAR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FAMay 30, 2000 · N8084U · Doug DC871F · Fuselage Main, Plate/SkinSDR RRXA003700Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FWD SIDE OF FRAME AT STA 20 AND L21R, 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 51-1-20D AND 53-2-0. (CORMay 26, 2000 · N8084U · Doug DC871F · Fuselage Main, FrameSDR RRXA002703Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE UNDER FINGER DOUBLER COCKPIT FLOOR FRAME AT STA -67 + X -17 -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 REPAIR IAW EMay 26, 2000 · N8084U · Doug DC871F · Fuselage Main, Plate/SkinSDR RRXA002746Longeron · damagedDURING A MAINTENANCE VISIT FOUND THAT THE PREVIOUS BLEND OUT NEEDS THICKNESS CHECKED AT STA 1690 TO 1700 AND L10L, 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 25, 2000 · N8084U · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS00832892Doubler · corrodedINSPECTION TYPE:C123, INTERNAL DOUBLER IS CORRODED BEYOND LIMITS AT STA 380 LONG 36. REPAIRED DOUBLER IAW 8110-3 APPROVED DH SK 730-429.May 25, 2000 · N730UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS00832823Fitting · corrodedINSPECTION TYPE:C123, STA 390 LONG 35R SPLICE FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 3754026 AND SRM 51-1-20D.May 25, 2000 · N730UP · Doug DC871F · Fuselage Main, StructureSDR UPS00832821Rib · crackedINSPECTION TYPE:C123, LEFT WING L/E UPPER SPLICE PAN IS CRACKED AT XS 250. REMOVED, FABRICATED AND REPLACED SPLICE PAN IAW DWG 5769859 AND SRM 51-1-21.May 25, 2000 · N730UP · Doug DC871F · Wing, Rib/BulkheadSDR RRXA003495Finger Doubler · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FINGER DOUBLER FROM STA -57 TO -70, -X 59, -Z-10 RT SIDE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. ORIGINAL MATERIAL REMAINING IS WITHIN ALMay 24, 2000 · N8084U · Doug DC871F · Fuselage Main, Plate/SkinSDR RRXA002778Skin · dentedDURING A MAINTENANCE VISIT FOUND 2 DENTS BEHIND JACK PAD AT STA 280 AND BETWEEN L36 - L35L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.May 24, 2000 · N8084U · Doug DC871F · Fuselage Main, Plate/SkinSDR RRXA002761Finger Doubler · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FINGER DOUBLER AT STA 1514 BETWEEN L27L AND L28L, 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 WMay 24, 2000 · N8084U · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA002706Angle · crackedDURING A MAINTENANCE VISIT FOUND A CRACKED RT SIDE ON THE RT WING NR 3 STUB WING NR 11 RIB LOWER ANGLE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW ANGLE IAW DC-8 SRM 51-1-May 24, 2000 · N8084U · Doug DC871F · Wing Miscellaneous StructureSDR RRXA002744Angle · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE LT AFT ENTRY DOOR/PLATE ABOUT 1.5 INCH AT LWR DOOR HINGE INSIDE LIGHTENING HOLE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED RMay 23, 2000 · N8084U · Doug DC871F · Passenger/Crew DoorsSDR RRXA002672Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK ABOUT 9 INCHES LONG ON THE UPPER RIB ON THE L/E SECTION ABOVE NR 2 PYLON AT STA 250, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAMay 23, 2000 · N8084U · Doug DC871F · Wing, Rib/BulkheadSDR RRXA002666Skin · crackedDURING A MAINTENANCE VISIT FOUND A CRACK LEADING FROM SCREW HOLE ON THE LEFT I/B LEADING EDGE AT STA XS 515, 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 EO NR 00-1May 23, 2000 · N8084U · Doug DC871F · Fuselage Main, Plate/Skin
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