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 RRXA991462Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RT WING L/E UPPER SKIN AT STA XFS 423.25 AT 2 RIVET HOLES, ALSO HAS 12 RIVET HEAT CRACKED. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW FAAug 20, 1999 · N8087U · Doug DC871F · Wing, Plate/SkinSDR RRXA991439Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, LT WING, L/E AUX TANK UPPER AFT MOUNTING CHORD BETWEEN STA XFS 7.50 AND XFS 20.0. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED THE CHORD IAW DC8 Aug 20, 1999 · N8087U · Doug DC871F · Wing SparSDR RRXA991436Web · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, NLG UPPER PRESSURE PANEL JUST AFT OF AIR CONDITIONING UNIT BETWEEN STA -32 AND STA -12, AND BETWEEN BL 5 RIGHT AND BL 10 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SAug 20, 1999 · N8087U · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA991637Web · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, WEB, BETWEEN STA 920 AND STA 940, AT LONGERON 22 RIGHT AND RIGHT BL 60. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR WEB IAW FAAAug 19, 1999 · N8087U · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA991633Floorbeam · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FLOOR SUPPORT AT STA 600, BETWEEN LONGERON 33 RIGHT AND LONGERON 36. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FLOOR SUPPORT IAW DACAug 19, 1999 · N8087U · Doug DC871F · Fuselage Main, Floor BeamSDR RRXA991438Web · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, WEB, BETWEEN STA Y920 AND SAT Y940, AT LONGERON 22 RIGHT, BL 60 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED WEB IAW FAA APPROVED DER ENGIAug 19, 1999 · N8087U · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA991431Support · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION, FUSELAGE, FLOOR SUPPORT, AT LOCATION Y600, BETWEEN LONGERONS 33 RIGHT AND LONGERON 36. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FLOOR SUPPOAug 19, 1999 · N8087U · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS99830464Landing Gear · collapsedINSPECTION TYPE:N/A, AFTER LANDING AND COMING TO A STOP ON RUNWAY 32R, THE NOSE GEAR COLLAPSED INTO THE WHEEL WELL. *S/D* ALL REQUIRED EO'S IE DC8-5300-11498A HAVE BEEN C/W BY TIMCO. PER FERRY FLIGHT PERMIT NR 9086 ALL FERRY FLIGHT PROCEDURES HAVE BEEN ACCOAug 17, 1999 · N797UP · Doug DC871F · Nose/Tail Landing GearSDR UPS99830353Girt Bar · failedINSPECTION TYPE:N/A, ESCAPE SLIDE GIRT BAR RETAINER FAILED UPON EGRESS OF A/C, SLIDE SEPARATED FROM A/C. STILL I/W ON LOG PAGE 208929/2. FOLLOW UP ACTION SCHEDULED FOR REMAINDER OF DC-8 FLEET. *S/D* INSTALLED HARDWARE IAW EO DC-8-2560-11700, OPS CK NORMAL Aug 17, 1999 · N797UP · Doug DC871F · Emergency EquipmentSDR RRXA991666Fitting · crackedDURING A MAINTENANCE VISIT FOUND CRACK, FLOORBEAM SUPPORT STRUT LOWER FITTING CRACKED AT AFT SIDE OF TEE AT STA 1160, TOP OF LONGERON 29 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED Aug 17, 1999 · N8087U · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA991665Fitting · crackedDURING A MAINTENANCE VISIT FOUND CRACK, LONGERON SPLICE FITTING CRACKED AT LONGERON 31 LEFT, AT STA 1260. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW MFG DWG 4753059 AND DCAug 17, 1999 · N8087U · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA991654Intercostal · crackedDURING A MAINTENANCE VISIT FOUND CRACK, INTERCOSTAL BETWEEN STA 580 AND STA 600 AT LONGERON 33 LEFT, 2 CRACKS FWD OF STA 600. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED INTERCOSTAL IAW MFAug 17, 1999 · N8087U · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA991632Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, INTERNAL DOUBLER AND INNER SUFRACE OF OUTER SKIN BETWEEN LONGERONS 31 LEFT AND LONGERON 31 RIGHT AND BETWEEN STA 350 AND STA 370. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-Aug 17, 1999 · N8087U · Doug DC871F · Fuselage Main, Plate/SkinSDR RRXA991631Finger Doubler · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FINGER DOUBLER AT LONGERON 31 RIGHT, AT STA 100. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FINGER DOUBLER IAW DAC DWG 5779917 AND DCAug 17, 1999 · N8087U · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA991519Fitting · crackedDURING A MAINTENANCE VISIT FOUND CRACK, FLOOR BEAM SUPPORT STRUT LOWER FITTING, CRACKED AT AFT SIDE OF TEE, AT STA 1160, TOP OF LONGERON 29 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLAug 17, 1999 · N8087U · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA991517Fitting · crackedDURING A MAINTENANCE VISIT FOUND CRACK, LONGERON SPLICE FITTING CRACKED AT LONGERON 31 LEFT, STA 1260. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DAC DWG NR 470359 AND DC8Aug 17, 1999 · N8087U · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA991455Intercostal · crackedDURING A MAINTENANCE VISIT FOUND CRACK, INTERCOSTAL BETWEEN STA FS 580 AND FS 600 AT LONGERON 33 LEFT, FWD OF STA FS 600. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED INTERCOSTAL PER DAC DWAug 17, 1999 · N8087U · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA991434Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, INTERNAL DOUBLER AND INNER SURFACE OF OUTER SKIN, BETWEEN LONGERONS 31 LEFT AND LONGERON 31 RIGHT, AND BETWEEN STATIONS Y350 AND STA Y370. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREAug 17, 1999 · N8087U · Doug DC871F · Fuselage Main, Plate/SkinSDR RRXA991433Finger Doubler · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FINGER DOUBLER, AT STA Y100, LONGERON 31 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FINGER DOUBLER IAW DAC DWG NR 5779917 AND Aug 17, 1999 · N8087U · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS99830349Doubler · corrodedINSPECTION TYPE:SV, CORROSION BETWEEN SKIN AND DOUBLER FS 1620 L26R DOT E253. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR IAW UPS DC8 SRM 53-4 -1, 53-2-1 FIG 7, 51-120D.Aug 16, 1999 · N752UP · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA991664Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, L/E RIB AT STA XFS 163.75, CRACKED AT THE AFT LWR END. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 57-2-0 FIGAug 16, 1999 · N8087U · Doug DC871F · Wing, Rib/BulkheadSDR RRXA991657Angle · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, L/E AT STA XW 0.00, THE UPPER AFT L/E ATTACH ANGLE CRACKED. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED ANGLE IAW MFG DWG 5613646 AND DCAug 16, 1999 · N8087U · Doug DC871F · Wing Miscellaneous StructureSDR RRXA991656Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, L/E LWR SKIN INTERNAL TRIPLER AT STA XFS 430 AT THE SPAR, CRACKED IN TWO. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. F8 REPAIR IAW MFG DWG 5769891 AND DC8 SRM 5Aug 16, 1999 · N8087U · Doug DC871F · Wing, Plate/SkinSDR RRXA991647Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RT WING, L/E RIB AT STA XFS 385.25, 17 FWD OF THE SPAR. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK AND REPAIRED IAW DC8 SRM 57-2-0 FIG 2.Aug 16, 1999 · N8087U · Doug DC871F · Wing, Rib/BulkheadSDR RRXA991644Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RT WING, L/E RIB AT STA XFS 354, CRACKED AT THE AFT UPPER END. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK AND REPAIRED IAW DC8 SRM 57-2-0 FIG 2.Aug 16, 1999 · N8087U · Doug DC871F · Wing Miscellaneous StructureSDR RRXA991643Intercostal · crackedDURING A MAINTENANCE VISIT FOUND CRACK, WING, RIGHT, L/E RIB AT STA XFS 335.25, 17 FWD OF THE SPAR, AT THE INTERCOSTAL GUSSET AFT FASTENERS IS CRACKED. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACAug 16, 1999 · N8087U · Doug DC871F · Wing Miscellaneous StructureSDR RRXA991642Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RT WING, L/E LWR SKIN AT STA XFS 301.25, 14 FWD OF THE SPAR IS CRACKED AT A RIVET HOLE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK AND REPAIRED IAW DC8 SAug 16, 1999 · N8087U · Doug DC871F · Wing, Plate/SkinSDR RRXA991641Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, WING, RIGHT L/E RIB AT STA XFS 163.75, CRACKED AT THE AFT LOWER END. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK AND REPAIRED IAW DC8 SRM 57-2-0 FIG 2.Aug 16, 1999 · N8087U · Doug DC871F · Wing, Rib/BulkheadSDR RRXA991640Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACK, WING, RIGHT, L/E, LWR SKIN AT STA XS 208, 31 FWD OF THE SPAR. THE CRACK IS APPROX 2 INCHES LONG. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK AND REPAIREDAug 16, 1999 · N8087U · Doug DC871F · Wing, Plate/SkinSDR RRXA991470Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RT WING L/E EDGE RIB AT STA XFS 163.75 AT THE AFT LOWER END. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACKED, FABRICATED AND INSTALLED REPAIR DOUBLER IAW DCAug 16, 1999 · N8087U · Doug DC871F · Wing, Rib/BulkheadSDR RRXA991466Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, L/E RIB, AT STA XFS 163.75, AT THE AFT LOWER END. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK AND REPAIRED IAW DC8 SRM 57-2-0, FIG 2.Aug 16, 1999 · N8087U · Doug DC871F · Wing, Rib/BulkheadSDR RRXA991458Angle · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RT WING L/E AT STA XW 0.00, THE UPPER AFT L/E ATTACH ANGLE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR ANGLE IAW DAC DWG NR 5613646 AND DC8 Aug 16, 1999 · N8087U · Doug DC871F · Wing Miscellaneous StructureSDR RRXA991457Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RT WING, L/E LWR SKIN INTERNAL TRIPLER AT STA XFS 430 AT THE SPAR, CRACKED IN TWO. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DAC DWG NRAug 16, 1999 · N8087U · Doug DC871F · Wing, Plate/SkinSDR RRXA991448Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RT WING L/E RIB AT STA XFS 385.25, 17 FWD OF THE SPAR. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 57Aug 16, 1999 · N8087U · Doug DC871F · Wing, Rib/BulkheadSDR RRXA991447Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RT WING LE RIB AT STA XFS 354 AT THE AFT UPPER END. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER PER DC8 SRM 57-2-Aug 16, 1999 · N8087U · Doug DC871F · Wing, Rib/BulkheadSDR RRXA991446Intercostal · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RT WING L/E RIB AT STA XFS 335.25, 17 FWD OF THE SPAR, AT THE INTERCOSTAL GUSSET AFT FASTENERS. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK, FABRICATED ANAug 16, 1999 · N8087U · Doug DC871F · Wing Miscellaneous StructureSDR RRXA991445Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACKED RT WING L/E LWR SKIN AT STA XFS 301.25, 14 FWD OF THE SPAR AT A RIVET HOLE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR Aug 16, 1999 · N8087U · Doug DC871F · Wing, Plate/SkinSDR RRXA991444Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RT WING L/E LWR SKIN AT STA XS 208, 31 FWD OF THE SPAR. THE CRACK IS APPROXIMATELY 2 INCHES LONG. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK, FABRICATEDAug 16, 1999 · N8087U · Doug DC871F · Wing, Plate/SkinSDR RRXA991669Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, LEFT WING, LEADING EDGE, EXTERNAL SKIN BETWEEN XFS 7.5 AND XFS 20. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 57-2-1Aug 15, 1999 · N8087U · Doug DC871F · Wing, Plate/SkinSDR RRXA991668Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, LEFT WING, LEADING EDGE SKIN BETWEEN XFS 250 AND XFS 250.89. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 57-2-0 FIG 2Aug 15, 1999 · N8087U · Doug DC871F · Wing, Plate/SkinSDR RRXA991667Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACK, FUSELAGE, EXTERIOR FUSELAGE SKIN CRACKED AND CORROSION AT STA 1755, LONGERON 31 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED SKIN AREA IAW DC8Aug 15, 1999 · N8087U · Doug DC871F · Fuselage Main, Plate/SkinSDR RRXA991663Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACK, LEFT WING, CENTER L/E UPPER SKIN CRACKED AT STA XFS 316.5 AT FRONT SPAR. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC8 SRM 57-2-1.Aug 15, 1999 · N8087U · Doug DC871F · Wing, Plate/SkinSDR RRXA991660Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, L/E LWR SKIN AT STA XFS 630, 3 FWD OF THE SPAR, CRACKED AT A RIVET HEAD. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK AND REPAIRED IAW DC8 SRM Aug 15, 1999 · N8087U · Doug DC871F · Wing, Plate/SkinSDR RRXA991659Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, LT L/E LOWER RIB CRACKED AT FASTENER END AT STA XFS 622.5 AND STA XFS 628.750 FWD OF ACCESS PANEL 519C OPENING. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACAug 15, 1999 · N8087U · Doug DC871F · Wing, Rib/BulkheadSDR RRXA991658Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING L/E UPPER RIB AT STA XFS 521.168, CRACKED 6 FWD OF THE SPAR. THE CRACK IS APPROX 2.5 INCHES LONG. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED RIB ANAug 15, 1999 · N8087U · Doug DC871F · Wing, Rib/BulkheadSDR RRXA991655Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, LT O/B L/E UPPER RIB CRACKED AT FASTNER END OF STA XFS 585. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK AND REPAIRED IAW DC8 SRM 57-2-0 FIG 2.Aug 15, 1999 · N8087U · Doug DC871F · Wing, Rib/BulkheadSDR RRXA991653Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, WING, LEFT, LOWER L/E RIB, CRACKED AT FASTENER END AT STA XFS 653.75 FWD OF ACCESS PANEL 519C OPENING. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK AND REAug 15, 1999 · N8087U · Doug DC871F · Wing, Rib/BulkheadSDR RRXA991652Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, L/E RIB AT STA XFS 616.25, CRACKED AT THE LWR FASTENER. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK AND REPAIRED IAW DC8 SRM 57-2-0 FIB 2.Aug 15, 1999 · N8087U · Doug DC871F · Wing, Rib/BulkheadSDR RRXA991651Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, L/E LWR SKIN INTERNAL DOUBLER AT STA XFS 597.5, CRACKED AT THE DRAIN HOLE, CRACK RUNS AFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DAug 15, 1999 · N8087U · Doug DC871F · Wing, Plate/SkinSDR RRXA991650Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, L/E RIB AT STA XFS 735.00, CRACKED AT THE AFT LOWER END. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK AND REPAIRED IAW DC8 SRM 57-2-0 FIG 2.Aug 15, 1999 · N8087U · Doug DC871F · Wing, Rib/Bulkhead
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