N961R, cancelled Jul 5, 2002

Service difficulty reports · 331

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N961R' AND deregistration_id = 'N961R-2002-07-05'
  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 2003F00055Floorbeam · corrodedFOUND DURING DOUGLAS D-CHECK INSPECTION, AT STATION 1600 LBL 42 INCH FLOORBEAM UPPER FLANGE LOWER SURFACE HAS 1 INCH BY 2 INCH CORRODED BEYOND LIMITS. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABRICATED REPAIR DOUBLER, FILLER IAW EO NR 02-039. TREATED, PRIMEDJun 17, 2002 · N961R · Doug DC873F · Fuselage Main, Floor BeamSDR 2002F01102Web · crackedFOUND DURING DOUGLAS D-CHECK INSPECTION, RIGHT INBOARD FLAP INBOARD WEB HAS PREVIOUS REPAIR CRACK EXTENDS TO NEW STOP DRILL AT END OF CRACK BEYOND REPAIR DOUBLER. STOP DRILLED END OF CRACK IAW DC-8 SRM 57-2-0. FABRICATED DOUBLER IAW DC-8 SRM 57-2-0, FIG 2. Jun 11, 2002 · N961R · Doug DC873F · Trailing Edge FlapsSDR 2002F01101Spar Cap · crackedFOUND DURING DOUGLAS D-CHECK INSPECTION, RIGHT WING LOWER FRONT SPAR CAP FORWARD TANG APPROXIMATELY STATION 520 SPAR CAP HAS CRACK. REMOVED INTERNAL REPAIR ANGLE FOR EVALUATION IAW DC-8 SRM 51-1-20D. REPAIR IS ACCEPTABLE AS TEMP REPAIR PER BOEING LETTER TEK-Jun 11, 2002 · N961R · Doug DC873F · Wing SparSDR 2002F01100Longeron · crackedFOUND DURING DOUGLAS D-CHECK INSPECTION, REPAIR AT STATION 55 LEFT LONGERON 31 HAS NO SUPPORTING DOCUMENTATION. REMOVED DOUBLER IAW DC-8 SRM 51-1-21. CRACK HAD EXTENDED .5 BEYOND STOP DRILL. STOP DRILLED CRACK IAW DC-8 SRM 53-2-0. FABRICATED REPAIR DOUBLERJun 11, 2002 · N961R · Doug DC873F · Fuselage Main, Longeron/StringerSDR 2002FA0000724Longeron · damaged(LONGERON 24/ FITTING) FOUND DURING (D) CHECK INSPECTION, STA 960 AND LONGERON 24L HOLES ELONGATED IN FITTING AND LONGERON 24 TWO FORWARD.Jun 8, 2002 · N961R · Doug DC873F · Fuselage Main, Longeron/StringerSDR 2002FA0000723Panel · corroded(BULKHEAD PANELS) FOUND DURING (D) CHECK INSPECTION. RIGHT W/W STA. 980 CNAT BULKHEAD PANELS HAVE CORROSION SPOTS FROM LONG 24R TO LONGERON 25R.Jun 8, 2002 · N961R · Doug DC873F · Fuselage Miscellaneous StructureSDR 2002F01098Fitting · corrodedFOUND DURING DOUGLAS D-CHECK INSPECTION, RIGHT LONGERON AND BATHTUB FITTING STATION 960 AFT SIDE HAS SPOT OF SURFACE CORROSION. REMOVED CORROSION FROM LONGERON 24R AND BATHTUB FITTING IAW DC-8 SRM 51-1-8. LONGERON 24 REPAIRED. REMOVED AND REPLACED BATHTUB FJun 7, 2002 · N961R · Doug DC873F · Fuselage Miscellaneous StructureSDR 2002F01104Skin · damagedFOUND DURING DOUGLAS D-CHECK INSPECTION, REPAIR AT STATION 275 RIGHT 31 AND 32 HAS NO SUPPORTING DOCUMENTATION. REMOVED REPAIR IAW DC-8 SRM 51-1-20D. FABRICATED FILLER, DOUBLER. TREATED AND PRIMED AND INSTALLED REPAIR PER EO NR 02-039, WITH APPROVED 8110-3 Jun 5, 2002 · N961R · Doug DC873F · Fuselage Main, Plate/SkinSDR 2002F01103Longeron · crackedFOUND DURING DOUGLAS D-CHECK INSPECTION, REPAIR AT STATION 300 RIGHT LONGERON 33 HAS NO SUPPORT DOCUMENTATION. REMOVED DOUBLER IAW DC-8 SRM 51-1-21. IT IS ACCEPTABLE TO USE EXISTING FILLER. FABRICATED NEW DOUBLER. TREATED AND PRIMED ALL PARTS AND INSTALLED Jun 5, 2002 · N961R · Doug DC873F · Fuselage Main, Longeron/StringerSDR 2002F01105Frame · corrodedFOUND DURING DOUGLAS D-CHECK INSPECTION, STATION 460 HAS CORROSION ON FRAME BETWEEN STRINGERS 2/3 LEFT. REMOVED CORROSION. FOUND OUT OF LIMITS. FABRICATED REPAIR DOUBLER. TREATED, PRIMED AND INSTALLED DOUBLER IAW DC-8 SRM 51-1-4, 53-2-0 AND 53-2-0, FIG 1F.Jun 4, 2002 · N961R · Doug DC873F · Fuselage Main, FrameSDR 2002F01095Fitting · corrodedFOUND DURING DOUGLAS D-CHECK INSPECTION, LONGERON 24L SURFACE CORROSION ON BOTH SIDES OF BATHTUB FITTING STATION 940 AT LONGERON ATTACH. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED AND REPLACED BATHTUB FITTING STATION 940 IAW DC-8 SRM 51-1-24, 51-3-0. Jun 3, 2002 · N961R · Doug DC873F · Fuselage Miscellaneous StructureSDR 2002F01094Skin · corrodedFOUND DURING DOUGLAS D-CHECK INSPECTION, LIGHT SURFACE CORROSION ON LOWER CENTER FUSELAGE AREA BETWEEN CENTER WING STRINGERS 67 AND 68 5 INCHES RIGHT OF ECWO. CORROSION OUT OF LIMITS STATION 759-768, 6 INCHES RIGHT OF CENTER LINE, ITEM 4 ON FORM 84. REMOVED Jun 3, 2002 · N961R · Doug DC873F · Fuselage Main, Plate/SkinSDR 2002FA0000720Longeron · corroded(LONGERON/BATHTUB FITTING) FOUND DURING (D) CHECK INSPECTION, LEFT LONGERON, LEFT LONGERON, 24 STA. 960.Jun 2, 2002 · N961R · Doug DC873F · Fuselage Main, Longeron/StringerSDR 2002FA0000725Longeron · corroded(LONGERON) FOUND DURING (D) CHECK INSPECTION, STA960 AND LONGERON 24L AFTER FITTING REMOVAL, FOUND CORROSION ON LONGERON 24 AT FASTENER HOLES.May 8, 2002 · N961R · Doug DC873F · Fuselage Main, Longeron/StringerSDR 2002FA0000722Web · corroded(WEB SKIN) FOUND DURING (D) CHECK INSPECTION, RIGHT W/W STA. 980 CNAT BULKHEAD WEB SKIN AND ANGLES HAS SURFACE CORROSION FROM LONGERON 24 TO LONGERON 27R.May 8, 2002 · N961R · Doug DC873F · Fuselage Miscellaneous StructureSDR 2002FA0000721Longeron · corroded(LONGERON 24) FOUND DURING (D) CHECK INSPECTION, LEFT WHEEL WELL STA. 902 FITTING AND LONGERON 24 CORROSION EMINATING FROM BETWEEN FITTING AND LONGERON LOWER SURFACE.May 8, 2002 · N961R · Doug DC873F · Fuselage Main, Longeron/StringerSDR 2002FA0000726Floorbeam · corroded(FLOORBEAM) FOUND DURING (D) CHECK INSPECTION. CORROSION AT STA 920. 63 INCHES LEFT OF CENTER, FLOORBEAM.May 6, 2002 · N961R · Doug DC873F · Fuselage Main, Floor BeamSDR 2002FA0000719Stringer · corroded(STRINGER) FOUND DURING (D) CHECK INSPECTION, STRINGER 31R HAS CORROSION AT STA 680.May 3, 2002 · N961R · Doug DC873F · Fuselage Main, Longeron/StringerSDR RRXA010060Gyro · failedCAPT'S VG FAILURE AFTER TAKEOFF. R&R CAPT'S VG IAW DC8 MM 34-25-0. OPS CHECKS GOOD.REMOVED & REPLACED CAPTS. ADI SYSTEM CHECKS GOOD IAW DC-8 MM 34-25-0 NO DEFECTS NOTEDAug 9, 2001 · N961R · Doug DC873F · Attitude Gyro and Indicating SystemSDR RRXA010009Light · malfunctionedNR 3 ENGINE OIL PRESSURE LIGHT ILLUMINATED IN FLIGHT 3900 FEET, M.8 249 KIAS OIL PRESS 42, PSI IDLE 32 PSI. LIGHT REMAINED ILLUMINATED AS POWER REDUCED FROM CRUISE TO IDLE POWER. INFLIGHT SHUTDOWN PERFORMED IAW QRH. AFTER SHUTDOWN OIL PRESSURE LIGHT REMAINEFeb 11, 2001 · N961R · Doug DC873F · Engine Oil PressureSDR RRXA001077Flow Valve · failedON CLIMBOUT WITH RT PACK AT MAX FLOW COULD NOT MAINTAIN CABIN ALTITUDE BELOW 10,000 FT. RETURNED TO AIRPORT. REMOVED AND REPLACED FLOW CONTROL VALVE. RAN ENGS AND PRESSURIZED IAW 21-31-0, OPS CHECK GOOD.Oct 27, 2000 · N961R · Doug DC873F · Cabin Cooling SystemSDR RRXA003427Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE 'B' PIT DOOR FRAME AT STA 520 AND L30R TO L29R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW E.O. L40-R01.Sep 2, 2000 · N961R · Doug DC873F · Fuselage Main, FrameSDR RRXA001052Structure · corrodedHEAVY CORROSION AT FRAME STA 520 BETWEEN LONGERONS 30R & 29 R,CARGO LIGHT SWITCH AREA. REPAIRED STA 250, L30R AND L29R, FRAME REF: ENG DRAWING NR L40-R01. MAT USED 7075-0, .090. HEAT TREATED REF DC-8 SRM 51-1-1.Aug 31, 2000 · N961R · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA003730Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE RIGHT AFT LOWER STAB WIPER PANEL AT STA 1723-1849, L15R, 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 , Jul 3, 2000 · N961R · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA001002Structure · crackedLT GEAR DOOR CRACKED IN TWO PLACES (MAIN LANDING). PERFORMED PLATING REPAIR IAW DC-8 SRM CHAP 52-2-0 FIG 2.Jun 20, 2000 · N961R · Doug DC873F · Landing Gear DoorsSDR RRXA000296Harness · corrodedNR 1 ENGINE INFLIGHT SHUT DOWN DUE TO ERRATIC -OFF SCALE EGT INDICATION FOR BOTH ANALOG AND DIGITAL EGT READOUT. TESTED NR 1 EGT SYSTEM IAW M/M 77-20-4, FOUND ALL TO BE WITHIN LIMITS. USED WHEATSTONE BRIDGE (TT1000A) TEST BOX TO VERIFY EGT GAUGE AND EGT HARNMay 14, 2000 · N961R · Doug DC873F · Engine EGT/TIT Indicating SystemSDR RRXA002020Retainer · inadequateDURING A MAINTENANCE VISIT FOUND ALL 4 AFT MOUNT BOLT RETAINERS ARE TOO SHORT AND DO NOT FIT OVER BOLT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED BOLTS IAW DC-8 SRM 51-3-0,Apr 27, 2000 · N961R · Doug DC873F · Engine Mount SectionSDR RRXA001886Retainer · wrong partDURING A MAINTENANCE VISIT FOUND THE AFT MOUNT BOLT RETAINERS ARE TOO SHORT (DO NOT FIT OVER BOLT), DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW MOUNT BOLT IAW DC-8 SRM 51-3-0, 72-22Apr 27, 2000 · N961R · Doug DC873F · Engine Mount SectionSDR RRXA002026Doubler · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE EXISTING DOUBLER AT BOTTOM OF A-PIT DOOR EXTERNAL SKIN, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED REPAIR IAW EO NR 00-055 WITH APPROVED 8Apr 25, 2000 · N961R · Doug DC873F · Cargo/Baggage DoorsSDR RRXA001892Doubler · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE EXISTING DOUBLER ON THE BOTTOM OF A-PIT DOOR EXTERNAL SKIN, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED DOUBLER IAW EO NR 00-055Apr 25, 2000 · N961R · Doug DC873F · Cargo/Baggage DoorsSDR RRXA001910Panel · crackedDURING A MAINTENANCE VISIT FOUND A 2.5 INCH CRACK ON THE RT WING I/B SLOT PANEL, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED PANEL IAW DC-8 SRM 51-3-0 AND MM 27-80-1.Apr 20, 2000 · N961R · Doug DC873F · Wing, Plate/SkinSDR RRXA001774Panel · crackedDURING A MAINTENANCE VISIT, FOUND A 2 1/2 INCH CRACK ON THE RT WING IB SLOT PANEL, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW PANEL IAW DC-8 SRM 51-3-0 AND DC-8 MM 27-80-1.Apr 20, 2000 · N961R · Doug DC873F · Nacelle/Pylon StructureSDR RRXA001948Boss · corrodedDURING A MAINTENANCE VISIT FOUND THE MLG STRUT ASSY RETRACT PIN BOSS AND RETRACT PIN NEEDED REWORK PER MA-AI-3210-01:03, 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 00-05Apr 15, 2000 · N961R · Doug DC873F · Main Landing Gear Attach SectionSDR RRXA001813Strut · corrodedDURING A MAINTENANCE VISIT MLG STRUT ASSY RETRACT PIN BOSS AND RETRACT PIN NEED REWORK PER MA-AI-3210-01:03, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED, REWORKED AND INSTALLED RETRACT PIN IAW EWA MA-AIApr 15, 2000 · N961R · Doug DC873F · Main Landing Gear Strut/Axle/TruckSDR RRXA001947Outflow Valve · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE RETANGULAR OUTFLOW VALVE (SUGAR SCOOP) IN THE AFT ACCESSORY COMPT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED REPAIR IApr 14, 2000 · N961R · Doug DC873F · Pressure Regulator/Outflow ValveSDR RRXA001946Web · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE IN THE LWR PIT C ON WEB AT STA 1200 BETWEEN L34R AND L35R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED REPAIR IAW DC-8 SRM 53-Apr 14, 2000 · N961R · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA001945Web · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE AREA BETWEEN STA 1120 TO 1160 AND BETWEEN L26L TO ''C'' PIT DOOR SILL L32R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLEDApr 14, 2000 · N961R · Doug DC873F · Cargo/Baggage DoorsSDR RRXA001812Outflow Valve · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE AFT ACCESSORY COMPT RETANGULAR OUTFLOW VALVE BETWEEN STA 1670 TO 1690, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED, PRIMED AND BLENDED AREA IAW DC-8 SRM 51-1-8. RETURNED TO SERVIApr 14, 2000 · N961R · Doug DC873F · Pressure Regulator/Outflow ValveSDR RRXA001811Web · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE IN LWR PIT C ON WEB AT STA 1200 AND BETWEEN L34R AND L35R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. AREA IS ACCEPTABLE AND RETURNED TO SERVICE IAWApr 14, 2000 · N961R · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA001810Web · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO AREA BETWEEN STA 1120 TO 1160 AND BETWEEN L26L TO ''C'' PIT DOOR SILL L32R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. AREA IS ACCEPTABLE AND RETApr 14, 2000 · N961R · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA002135Intercostal · misdrilledDURING A MAINTENANCE VISIT FOUND HOLES TO THE INTERCOSTAL IN THE UPPER CARGO COMPT. AT FS 798 TO 822 AND L5L, 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, 51-1Apr 13, 2000 · N961R · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA002040Angle · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE "L" ANGLE AT STA 1120 AND L27L, 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, 51-1-20D.Apr 13, 2000 · N961R · Doug DC873F · Fuselage Main, Attach FittingsSDR RRXA002019Frame · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE C PIT CROSS SLIDE DOOR AFT FR ON FUSELAGE AT FRAME 1260 AND LONGERON 36, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED REPAIR IAW Apr 13, 2000 · N961R · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA001944Angle · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE L ANGLE AT STA 1120 AND L27L, 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 51-1-20D AND 53-2-0. (Apr 13, 2000 · N961R · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA001914Spar Cap · damagedDURING A MAINTENANCE VISIT FOUND GOUGED HOLES AND ELONGATED UPPER SPAR CAP ON RT WING FRONT SPAR AT STA XFS 454, 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 EO NR 00-055 WApr 13, 2000 · N961R · Doug DC873F · Wing SparSDR RRXA001885Frame · crackedDURING A MAINTENANCE VISIT FOUND A CRACK AT THE C'' PIT CROSS SLIDE DOOR AFT FR ON FUSELAGE AT FRAME 1260 AND LONGERON 36, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED ANApr 13, 2000 · N961R · Doug DC873F · Fuselage Main, FrameSDR RRXA001809Angle · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE L ANGLE AT STA 1120 AND L27L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW ANGLE IAW DC-8 SRM 51-1-20D AND 53-2-0.Apr 13, 2000 · N961R · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA001778Spar Cap · damagedDURING A MAINTENANCE VISIT, FOUND GOUGED AND ELONGATED HOLES IN THE RT WING UPPER SPAR CAP AT STA XFS 454, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. OVERSIZED FASTENER HOLES & RE-COUNTER SUNK AND INSTALLApr 13, 2000 · N961R · Doug DC873F · Wing SparSDR RRXA001921Skin · crackedDURING A MAINTENANCE VISIT FOUND DENTED AND CRACKED THE LEFT O/B STUB WING, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW EO NR 00-055 WITH APPROVED 8110-3 DATED 3-Apr 12, 2000 · N961R · Doug DC873F · Wing, Plate/SkinSDR RRXA001902Panel · delaminatedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE, RIVETS PULLING THROUGH AND RIVET HEADS SHEARING OFF ON THE RT FLAP SCISSORS PANEL, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW PANELApr 12, 2000 · N961R · Doug DC873F · Trailing Edge Flaps
Back to N961R, cancelled Jul 5, 2002