Mcdonnell Douglas DC-8-71

Service difficulty reports · 341

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 = 'DC871'
  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 RRXA002791Door Frame · damagedDURING A MAINTENANCE VISIT FOUND A LARGE TEAR IN STRUCTURE ABOVE MAIN CARGO DOOR CENTER (DOOR JAM) AT STA 210-220 AND L6 L AND L7L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DAug 11, 2000 · N811AL · Doug DC871 · Fuselage Main, StructureSDR RRXA003820Spar · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO RT CENTER AUX. TANK AFT LT INNER ACCESS HOLE UPPER REAR SPAR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW EO 00-196 WITH APPROVAug 10, 2000 · N811AL · Doug DC871 · Wing SparSDR RRXA002794Frame · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE FORMER ON THE LT WING CENTER L/E BOTTOM T/E AT STA XFS 322.750, 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 51-1-4, 51-1Aug 10, 2000 · N811AL · Doug DC871 · Trailing Edge FlapsSDR RRXA002793Skin · puncturedDURING A MAINTENANCE VISIT FOUND A PUNCTURE TO THE STRUCTURE AT O/B END OF NR 2 GROUND SPOILER LT WING AT STA XRS 162.263 (NOT SPOILER), DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLEAug 10, 2000 · N811AL · Doug DC871 · Wing, Plate/SkinSDR RRXA002792Fitting · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE "C" PIT DOOR T-LOCK SUPPORT FITTING INSIDE DOOR WELL AT STA 1180 AND L33R, 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 5Aug 10, 2000 · N811AL · Doug DC871 · Fuselage Miscellaneous StructureSDR RRXA003821Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO SKIN DOUBLER AT GROUND PNEUMATIC CONNECTOR DOOR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRMAug 9, 2000 · N811AL · Doug DC871 · Fuselage Structure (General)SDR RRXA002797Skin · damagedDURING A MAINTENANCE VISIT FOUND 2 OBLONG HOLES ON THE RT O/B FLAP VANE NR 4 O/B EDGE, 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 57-3-0, AND EO#00-196 WITH APPROVED 8Aug 8, 2000 · N811AL · Doug DC871 · Trailing Edge FlapsSDR RRXA002796Spar · crackedDURING A MAINTENANCE VISIT FOUND A SMALL CRACK INSIDE OF HOLE EDGE ON THE RT CENTER AUX TANK AFT LT INNER ACCESS HOLE UPPER REAR SPAR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAug 8, 2000 · N811AL · Doug DC871 · Wing SparSDR RRXA002795Skin · crackedDURING A MAINTENANCE VISIT FOUND A 1 1/4 INCH CRACK IN L/E AT LT CHIN SCOOP, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK. WELDED CRACK TO MIL-STD-2219 USING TYPE 4043 WELD FILLER ROD IAW EO#00Aug 8, 2000 · N811AL · Doug DC871 · Fuselage Main, Plate/SkinSDR RRXA003823Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO L/H SIDE VERTICAL STAB. BASE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 55-2-Aug 4, 2000 · N811AL · Doug DC871 · Vertical StabilizerSDR RRXA003818Link · chafedDURING A MAINTENANCE VISIT FOUND CHAFF DAMAGE TO LT WING FLAP AFT LINK O/B SIDE AT STA. 98, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. BLENDED AREA AND RETURNED TO SERVICE IAW EO#00-196 WITH APPROVED 8110-3 DATEAug 4, 2000 · N811AL · Doug DC871 · Trailing Edge FlapsSDR RRXA003784Floorbeam · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FLOOR BEAM AT STA 1320 AND L36R, 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 DC-8 SRM 51-1-21, 53-2-0 FIG 1FAug 4, 2000 · N811AL · Doug DC871 · Fuselage, Seat/Cargo Attach FittingsSDR RRXA003817Fitting · gougedDURING A MAINTENANCE VISIT FOUND GOUGED DAMAGE TO LT. O/B FLAP O/B CANOE FITTING AT O/B AFT END BY SLIDING HINGE COVER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW EO#00-196 WIAug 3, 2000 · N811AL · Doug DC871 · Trailing Edge FlapsSDR RRXA002804Skin · damagedDURING A MAINTENANCE VISIT FOUND DAMAGE TO THEINSIDE OF THRUST REVERSER ON THE NR 2 ENGINE I/B THRUST REVERSER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW EO#00-196 WITH APPRAug 3, 2000 · N811AL · Doug DC871 · Engine Thrust ReverserSDR RRXA002803Fitting · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE LONGERON NR 1 FITTING JUST FWD OF STA 857, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. (NO CRACK FOUND)Aug 3, 2000 · N811AL · Doug DC871 · Fuselage Miscellaneous StructureSDR RRXA002802Skin · bulgedDURING A MAINTENANCE VISIT FOUND BULGED SKIN AND FASTENERS PULLING THROUGH SKIN AT THE RT WING UPPER SKIN AT STA 727 STR. 2, 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 SRMAug 3, 2000 · N811AL · Doug DC871 · Wing, Plate/SkinSDR RRXA002800Angle · misdrilledDURING A MAINTENANCE VISIT FOUND DOUBLE DRILLED & IMPROPER FASTENERS INSTALLED ON THE CLIP ANGLE AT STA 160 UPPER CROWN +0 AND LONGERON 1, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLEAug 3, 2000 · N811AL · Doug DC871 · Fuselage Miscellaneous StructureSDR RRXA002807Former · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE FORMER AT T/E AT STA XFS 803, 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 57-2-2 AND 51-1-21.Aug 3, 2000 · N811AL · Doug DC871 · Trailing Edge FlapsSDR RRXA002806Former · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE FORMER AT T/E AT STA XFS 778, 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 57-2-2 AND 51-1-21.Aug 3, 2000 · N811AL · Doug DC871 · Trailing Edge FlapsSDR RRXA002805Former · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE FORMER T/E AT STA XFS 766, 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 57-2-2 AND 51-1-21.Aug 3, 2000 · N811AL · Doug DC871 · Trailing Edge FlapsSDR RRXA002801Former · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE FORMER AT T/E AT STA XFS 766, 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 57-2-2 AND 51-1-21.Aug 3, 2000 · N811AL · Doug DC871 · Trailing Edge FlapsSDR RRXA002799Former · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE FORMER AT T/E AT STA XFS 803, 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 57-2-2 AND 51-1-21.Aug 3, 2000 · N811AL · Doug DC871 · Trailing Edge FlapsSDR RRXA002798Former · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE FORMER AT T/E AT STA XFS 778, 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 57-2-2 AND 51-1-21.Aug 3, 2000 · N811AL · Doug DC871 · Wing Miscellaneous StructureSDR RRXA002810Fitting · chafedDURING A MAINTENANCE VISIT FOUND A CHAFED FLAP SUPPORT FITTING O/B END ON THE RT WING AT STA 98, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. BLENDED AREA AND FOUND TO BE WITHIN LIMITS, RETURNED TO SERVICE IAW EOAug 1, 2000 · N811AL · Doug DC871 · Trailing Edge FlapsSDR RRXA003777Bulkhead · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE 9G BULKHEAD PANEL AT STA 70, X=25, Z=15, DAAMGE 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 SRM 53-2-0, 51-1-Jul 31, 2000 · N811AL · Doug DC871 · Fuselage Main, BulkheadSDR RRXA003773Vane · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE RT INBD FLAP VANE UPPER SURFACE AT STA XW 90 3 AFT OF L/E, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRJul 31, 2000 · N811AL · Doug DC871 · Trailing Edge FlapsSDR RRXA002817Skin · crackedDURING A MAINTENANCE VISIT FOUND A 2 INCH CRACK AT CUT OUT ON THE NR 3 STUB WING RT I/B BOTTOM INNER SKIN DOUBLER AT STA 258, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW EO#00-2Jul 31, 2000 · N811AL · Doug DC871 · Trailing Edge FlapsSDR RRXA002816Bracket · crackedDURING A MAINTENANCE VISIT FOUND A CRACKED BRACKET INSIDE OF BOTTOM ACCESS PANEL ON NR 3 STUB WING RT I/B AT STA XS 254, 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 51-Jul 31, 2000 · N811AL · Doug DC871 · Trailing Edge FlapsSDR RRXA002815Doubler · crackedDURING A MAINTENANCE VISIT FOUND A 10 INCH LONG CRACK TO THE NR 3 STUB WING RT I/B TOP INNER DOUBLER AT STA 254, 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 51-1-21, 57Jul 31, 2000 · N811AL · Doug DC871 · Trailing Edge FlapsSDR RRXA002814Frame · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP FORMER AT T/E OF NR 3 STUB WING RT I/B AT STA XS 213, 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 51-1-21.Jul 31, 2000 · N811AL · Doug DC871 · Trailing Edge FlapsSDR RRXA002813Frame · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP FORMER AT T/E ON NR 3 STUB WING RT I/B AT STA XS 254, 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 51-1-21, 57-2-0.Jul 31, 2000 · N811AL · Doug DC871 · Wing Miscellaneous StructureSDR RRXA002812Spar · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE AFT SURFACE REAR SPAR LWR. CAP AT STA XRS 578, 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 51-1-4 AND EO 00-196Jul 31, 2000 · N811AL · Doug DC871 · Wing SparSDR RRXA002811Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE EXTERIOR SKIN AT STA 1440 AND L21R, 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 51-1-20D, 52-1-4 AND EO 00-196 Jul 31, 2000 · N811AL · Doug DC871 · Fuselage Main, Plate/SkinSDR RRXA003783Attach Angle · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LONGERON ATTACH ANGLE AT STA 1180 AND L28L, 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 FIJul 29, 2000 · N811AL · Doug DC871 · Fuselage Main, Attach FittingsSDR RRXA003769Plate · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMGE TO PANEL 505G LT UPPER CENTER AUX TANK PLATE BETWEEN STA'S 717-442 X=+25 TO +45 Z+-9, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INJul 29, 2000 · N811AL · Doug DC871 · Wing, Plate/SkinSDR RRXA003815Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO NR 2 STUB WING L/E 7 INCHES AND BOTTOM RIB AT STA. XS250.089, 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 51-1-4, 51-1-2Jul 28, 2000 · N811AL · Doug DC871 · Wing, Rib/BulkheadSDR RRXA003814Angle · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO NR 2 STUB WING L/E ANGLE INSIDE BOTTOM ACCESS PANEL AT STA. XS250.089, 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 51-1-Jul 28, 2000 · N811AL · Doug DC871 · Wing Miscellaneous StructureSDR RRXA003813Former · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO NR 2 STUB WING L/E AT STA. XS227.335 AND UPPER T/E, 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 51-1-4, 51-1-20D.Jul 28, 2000 · N811AL · Doug DC871 · Wing Miscellaneous StructureSDR RRXA003812Bracket · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO NR 2 STUB WING L/E AT STA. XS255 AND BULKHEAD WEB, 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 51-1-20D, 51-3-2, 51-1-4.Jul 28, 2000 · N811AL · Doug DC871 · Wing Miscellaneous StructureSDR RRXA003768Rib · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE I/B END OF LT I/B L/E ON RIB AT STA 1.250, 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 51-1-21D, Jul 28, 2000 · N811AL · Doug DC871 · Wing, Rib/BulkheadSDR RRXA002828Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE SKIN BETWEEN STA 8 TO -12 AND L31L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW EO00-196 WITH APPROVED 8110-3 DATED 08/1Jul 28, 2000 · N811AL · Doug DC871 · Fuselage Main, Plate/SkinSDR RRXA002821Skin · crackedDURING A MAINTENANCE VSIIT FOUND A 1 1/2 INCH CRACK TO THE BOTTOM SKIN AT STA XFS 747, 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 51-1-21, 57-2-1.Jul 28, 2000 · N811AL · Doug DC871 · Fuselage Main, Plate/SkinSDR RRXA002819Frame · crackedDURING A MAINTENANCE VISIT FOUND A CRACK AT TOP T/E OF FORMER AT STA XFS 766, 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 51-1-21, 57-2-0.Jul 28, 2000 · N811AL · Doug DC871 · Trailing Edge FlapsSDR RRXA003822Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO BASE OF VERTICAL STAB. R/H SIDE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 55Jul 27, 2000 · N811AL · Doug DC871 · Vertical StabilizerSDR RRXA003816Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO LT WING CENTER L/E BOTTOM SKIN AT STA. XFS422.750, 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 51-1-21, 57-2-0.Jul 27, 2000 · N811AL · Doug DC871 · Wing, Plate/SkinSDR RRXA003782Attach Angle · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LWR CARGO PIT CEILING SUPPORT AT STA 1390, X=+41 TO -41, Z+-6, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICJul 27, 2000 · N811AL · Doug DC871 · Fuselage Main, Attach FittingsSDR RRXA003781Stiffener · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE D-PIT DOOR STIFFNER AT STA 1394 L24R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DD-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 51-1-21 AND 53Jul 27, 2000 · N811AL · Doug DC871 · Fuselage Miscellaneous StructureSDR RRXA003780Attach Angle · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE AFT LWR CARGO COMPT FLOOR ATTACH STRAP AT STA 1390 AND L35L TO L35R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. Jul 27, 2000 · N811AL · Doug DC871 · Fuselage Main, Attach FittingsSDR RRXA002829Frame · crackedDURING A MAINTENANCE VISIT FOUND A CRACK AT T/E TO THE BOTTOM FORMER ON LT WING CENTER L/E AT STA XS 467.323, 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 51-1-21, 51-1-Jul 27, 2000 · N811AL · Doug DC871 · Trailing Edge FlapsSDR RRXA002827Frame · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP FORMER AT T/E ON THE LT WING CENTER L/E AT STA XS 467, 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 51-1-21, 57-2-0.Jul 27, 2000 · N811AL · Doug DC871 · Trailing Edge Flaps
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