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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
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, PRIMEDSDR 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. SDR 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-SDR 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 DOUBLERSDR 2002FA0000724Longeron · damaged(LONGERON 24/ FITTING) FOUND DURING (D) CHECK INSPECTION, STA 960 AND LONGERON 24L HOLES ELONGATED IN FITTING AND LONGERON 24 TWO FORWARD.SDR 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.SDR 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 FSDR 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 SDR 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 SDR 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.SDR 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. SDR 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 SDR 2002FA0000720Longeron · corroded(LONGERON/BATHTUB FITTING) FOUND DURING (D) CHECK INSPECTION, LEFT LONGERON, LEFT LONGERON, 24 STA. 960.SDR 2002FA0000725Longeron · corroded(LONGERON) FOUND DURING (D) CHECK INSPECTION, STA960 AND LONGERON 24L AFTER FITTING REMOVAL, FOUND CORROSION ON LONGERON 24 AT FASTENER HOLES.SDR 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.SDR 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.SDR 2002FA0000726Floorbeam · corroded(FLOORBEAM) FOUND DURING (D) CHECK INSPECTION. CORROSION AT STA 920. 63 INCHES LEFT OF CENTER, FLOORBEAM.SDR 2002FA0000719Stringer · corroded(STRINGER) FOUND DURING (D) CHECK INSPECTION, STRINGER 31R HAS CORROSION AT STA 680.SDR 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 NOTEDSDR 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 REMAINESDR 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.SDR 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.SDR 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.SDR 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 , SDR RRXA001002Structure · crackedLT GEAR DOOR CRACKED IN TWO PLACES (MAIN LANDING). PERFORMED PLATING REPAIR IAW DC-8 SRM CHAP 52-2-0 FIG 2.SDR 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 HARNSDR 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,SDR 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, 72-22SDR 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 8SDR 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 00-055SDR 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.SDR 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.SDR 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 00-05SDR 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-AISDR 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 ISDR 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-SDR 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 INSTALLEDSDR 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 SERVISDR 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 IAWSDR 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 RETSDR 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, 51-1SDR 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.SDR 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 SDR 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. (SDR 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 WSDR 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 ANSDR 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.SDR 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 INSTALLSDR 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-SDR 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 PANEL
Back to N961R, cancelled Jul 5, 2002