N950R, cancelled Sep 17, 2013

Service difficulty reports · 49

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 = 'N950R' AND deregistration_id = 'N950R-2013-09-17'
  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 2002F01099Wire · damagedRED ' GEAR NOT LATCHED' LIGHT ON FORWARD INSTRUMENT PANEL ILLUMINATED. ABNORMAL PROCEDURE COMPLETED. REPAIRED WIRE BY REPINNING ON LEFT UPLATCH SWITCH CONNECTOR IAW DC-8 MM 20-50-1. ACCOMPLISHED NORMAL UPLATCH CHECK AND EMERGENCY EXTENSION. OPS CHECKS GOODJun 10, 2002 · N950R · Doug DC863 · Landing Gear System WiringSDR 2002F01097Warning Light · illuminatedRED 'GEAR NOT LATCHED' LIGHT ON FORWARD INSTRUMENT PANEL ILLUMINATED. ABNORMAL PROCEDURE COMPLETED. (M)Jun 7, 2002 · N950R · Doug DC863 · Landing Gear Position and WarningSDR COOSDR02050Floorbeam · corrodedMAIN CARGO COMPONENT, STA 1680, Z0, +X7 INCHES AND X 15 INCHES, FLOOR BEAM UPPER CHORD CORRODED.Apr 1, 2002 · N950R · Doug DC863 · Fuselage Main, Floor BeamSDR COOSDR02051Frame · corrodedAFT CARGO COMPONENT STA 1600 BETWEEN LONG 34 LEFT AND 34 RIGHT FRAME, CORRODED.Apr 1, 2002 · N950R · Doug DC863 · Fuselage Main, FrameSDR COOSDR02012Floorbeam · crackedMAIN CARGO COMPARTMENT. Y STA 1580, Z0, +49.0 AND +X56.0, FLOORBEAM UPPER CHORD WITH CRACK.Mar 8, 2002 · N950R · Doug DC863 · Fuselage Main, Floor BeamSDR COOSDR02044Floorbeam · crackedMAIN CARGO CABIN - STA Y=1600-FLOOR BEAM UPPER CHORD CRACKED.Mar 1, 2002 · N950R · Doug DC863 · Fuselage Main, Floor BeamSDR COOSDR02045Doubler · crackedSECTION 43 - CARGO DOOR DOUBLER CRACKED, AT STA Y=270.000, LONG 21L.Mar 1, 2002 · N950R · Doug DC863 · Cargo/Baggage DoorsSDR COOSDR020001Floorbeam · crackedFRAME TO FLOORBEARM STRUT, CRACKED.Mar 1, 2002 · N950R · Doug DC863 · Fuselage Main, Floor BeamSDR COOSDR02010Fitting · corrodedNET SUPPORT FITTING (PN 5711283516) CORRODED LOCATED AT AFT CARGO COMPARTMENT STA 1145 LONG 31R.Mar 1, 2002 · N950R · Doug DC863 · Fuselage Main, Attach FittingsSDR COOSDR020007Doubler · corrodedRIGHT LOWER WING EXTERNAL (BEAVER TAIL) DOUBLER WITH CORROSION.Mar 1, 2002 · N950R · Doug DC863 · Wing Miscellaneous StructureSDR COOSDR020006Doubler · corrodedLEFT LOWER WING EXTERNAL (BEAVER TAIL) DOUBLER WITH CORROSION.Mar 1, 2002 · N950R · Doug DC863 · Wing Miscellaneous StructureSDR COOSDR02005Skin · dentedRIGHT WING, INBOARD AILERON-CONTROL TAB (PN 5642831502, SN 60023311) LOWER AND UPPER SKIN WITH DENT.Mar 1, 2002 · N950R · Doug DC863 · AileronsSDR COOSDR020008Frame · crackedNOSE SECTION - WHEEL WELL FRAME CRACKED AT STA Y = 19,000 =X 23,000.Mar 1, 2002 · N950R · Doug DC863 · Fuselage Main, FrameSDR COOSDR020009Frame · crackedNOSE SECTION, WHEEL WELL FRAME CRACKED AT STA Y 19,000, -X 23,000.Mar 1, 2002 · N950R · Doug DC863 · Fuselage Main, FrameSDR COOSDR02011Floorbeam · corrodedMAIN CARGO COMPARTMENT Y STA 1680, Z0, -X10, FLOOR BEAM WITH CORROSION.Mar 1, 2002 · N950R · Doug DC863 · Fuselage Main, Floor BeamSDR COOSDR02013Longeron · corrodedFORWARD CARGO COMPT. Y STA 570.0, LONGERON 31R WITH CORROSION.Mar 1, 2002 · N950R · Doug DC863 · Fuselage Main, Longeron/StringerSDR RRXA001098Ring · damagedNR 2 T/R TRANSLATING RING DAMAGED. REMOVED AND REPLACED NR 2 ENG T/R TRANSLATING RING IAW DC-8 MM 78-30-0, OPS CHECK GOOD.Dec 22, 2000 · N950R · Doug DC863 · Engine Thrust ReverserSDR RRXA001091Compressor · stalledON CLIMBOUT WITH ENGINE ANTI-ICE ON NR 3 ENG COMPRESSOR STALLED, OIL PRESSURE WAS 59 PSI. DURING B-CHECK INSP FOUND PRBC LOCKED UP. REMOVED AND REPLACED PRBC IAW 75-30-3. BORESCOPE NR 3 ENG IAW DC-8 MM 72-00 431453082, PRBC CHECKS GOOD, NO COMPR STALL ON ENDec 12, 2000 · N950R · Doug DC863F · Turbine Engine Compressor SectionSDR RRXA001083Thrust Reverser · brokenTOWER REPORTED SOMETHING FELL OFF ON LANDING. FOUND NR 3 ENGINE THRUST REVERSER BROKEN IN SEVERAL PLACES ON TRANSLATING RING. REMOVED AND REPLACED NR 3 ENGINE TRANSLATING RING AND DOOR ASSY IAW DC-8 MM 78-30-1 OPS CHECK GOOD AT THIS TIME.Dec 3, 2000 · N950R · Doug DC863 · Engine Thrust ReverserSDR RRXA001057Fire Loop · false activationFIRE WARNING NR 1 ENG SECURED PER QRH, RETURNED TO ATL. REMOVED AND REPLACED FIRE LOOP AT NR 1 ENG IAW DC-8 MM 26-10-1, OK FOR SERVICE.Sep 23, 2000 · N950R · Doug DC863 · Fire DetectionSDR RRXA001051Engine · malfunctionedAT FL 290 NR 4 ENG COMPRESSOR STALLED. INSURED ENG HAD POSITIVE FUEL FLOW AND IGNITION. EGT STARTED TO RISE TOWARD CAUTION ZONE, THEN ENGINE WAS SHUT DOWN. EGT CONTINUED TO RISE TO ABOVE RED LINE BEFORE COOLING. MAX EGT WAS 600 DEG FOR A SEC OR SO. REMOVEAug 22, 2000 · N950R · Doug DC863 · Engine (Turbine/Turboprop)SDR RRXA003017Skin · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE SKIN ON THE R/H UPPER WING REAR SPAR AT STA XCW 69.5, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLEAug 19, 2000 · N950R · Doug DC863 · Wing, Plate/SkinSDR RRXA003429Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE RT HORZ. STAB LWR FWD PANEL ABOUT 8 INCHES FROM FRONT SPAR AT STA XE 29.812, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Aug 18, 2000 · N950R · Doug DC863 · Horizontal Stabilizer StructureSDR RRXA003428Skin · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE R/H UPPER WING SKIN AND REAR SPAR AT STA XCW 69.5, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////OPEN/////Aug 18, 2000 · N950R · Doug DC863 · Wing, Plate/SkinSDR RRXA003018Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE R/H HORIZ. STAB LWR FWD PANEL ABOUT 8" FROM FRONT SPAR AT STA XE 29.812, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-Aug 18, 2000 · N950R · Doug DC863 · Horizontal Stabilizer StructureSDR RRXA000197Line · rupturedHYD FLUID MAIN RES LOSS TO AUX LEVEL; USED AUX PUMP FOR NORM SYSTEM OPS. AFTER BY-PASS MAIN SYS & PUMPS. DISCOVERED RT ENG DRIVEN HYD PUMP MAIN PRESSURE SUPPLY LINE RUPTURED FABRICATED AND INSTALLED LIKE HYDRAULIC LINE ASSY. RESECURED HYD RESERVOIR, LK CK Mar 31, 2000 · N950R · Doug DC863 · Hydraulic System, MainSDR 99ZZZX3985Keel Beam · corrodedKEEL BEAM HAS SURFACE CORROSION, STA 730 AND STA 742 WHERE SKIN WAS OPENED FOR INSPECTION OF AREA. FOUND DURING SCHEDULED C MAINTENANCE CHECK. AREA EXPOSED TO ENVIRONMENTAL CHANGES.Sep 8, 1999 · N950R · Doug DC863 · Fuselage Main, KeelSDR RRXA98440Pin · shearedLEFT MAIN GEAR WOULD NOT RETRACT. MAINTENANCE FOUND PIN ATTACHING RETRACT CYLINDER TO GEAR WAS SHEARED OFF.Oct 8, 1998 · N950R · Doug DC863 · Landing Gear Retraction/Extension SystemSDR RRXA98239Structure · damagedEXTENSIVE DAMAGE TO LEFT WING EXTENDED LEADING EDGE INTO NR 1 ALT FUEL TANK. AIRCRAFT STRUCK BY GROUND HANDLERS FORK LIFT. AIRCRAFT FERRIED FROM KMSP TO KGSO.Jun 17, 1998 · N950R · Doug DC863 · Wing Miscellaneous StructureSDR RRXA98013Check Valve · malfunctionedA/C DEPRESSURIZED AT 33,000 DESCEND TO 17,000 TO HOLD 12,000 FT CABIN. NR 1 T/C INOP. INSTALLED SERVICEABLE WARM AIR CK VALVE ON LT PNEU MANIFOLD. SECURED LOOSE DUCTING, A/C PRESSURIZATION AND LEAK CK GOOD, NR 1 T/C GRD CKS GOOD.Feb 3, 1998 · N950R · Doug DC863 · Pneumatic Distribution SystemSDR RRXA97215Press Dome Web · crackedDURING A MAINTENANCE VISIT, FOUND PRESSURE DOME WEB CRACKED, AT STA 680 AND LONGERON 31 LEFT. *S/D* FABRICATED AND INSTALLED REPAIR ON PRESSURE WEB IAW DC-8 SRM 53-2-5, FIGURE 14.Aug 5, 1997 · N950R · Doug DC863 · Fuselage Main, BulkheadSDR RRXA97208Longeron · crackedDURING MAINTENANCE VISIT, FOUND LONGERON 34 LEFT CRACKED, BETWEEN STA 605 AND STA 607. REMOVED DAMAGED LONGERON 34L, FABRICATED AND INSTALLED NEW LONGERON IAW DC-8 SRM 53-2-0.Jul 22, 1997 · N950R · Doug DC863 · Fuselage Main, Longeron/StringerSDR RRXA97207Longeron · crackedDURING A MAINTENANCE VISIT, FOUND LONGERON 34 RIGHT CRACKED, BETWEEN STA 602 AND STA 607. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED NEW LONGERON 34R IAW FAA DER APPROVED ENGINEERING SKETCH C76-R09.Jul 22, 1997 · N950R · Doug DC863 · Fuselage Main, Longeron/StringerSDR RRXA97206Skin · corrosionDURING MAINTENANCE VISIT, FOUND CORROSION DAMAGE ON INTERIOR SKIN AT, STA 610, BETWEEN LONGERONS 36 AND 35R. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA DER APPROVED COTNEY ENGINEERING SKETCH C76-R08. TREATED AREA IAW DC-8 SRM 51-1-8.Jul 16, 1997 · N950R · Doug DC863 · Fuselage Main, Plate/SkinSDR RRXA97204Skin · crackedDURING A MAINTENANCE VISIT, FOUND RIGHT LOWER FLAP SKIN CRACKED AT XF=219. *S/D* REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED FILLER AND DOUBLER REPAIR IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH C76-R07 AND DC-8 SRM 51-1-8 AND 51-1-21A.Jul 10, 1997 · N950R · Doug DC863 · Trailing Edge FlapsSDR RRXA97203Skin · chafedDURING MAINTENANCE VISIT, INSPECTION FOUND RT WING OUTBOARD FLAP UPPER SKIN STA 230 CHAFFED.Jul 8, 1997 · N950R · Doug DC863 · Trailing Edge FlapsSDR RRXA97202Skin · chafedDURING MAINTENANCE VISIT, INSPECTION FOUND RT WING OUTBOARD FLAP AFT UPPER SKIN AT STA 210 IS CHAFFED.Jul 8, 1997 · N950R · Doug DC863 · Trailing Edge FlapsSDR RRXA97201Frame · gougedDURING MAINTENANCE VISIT, INSPECTION FOUND FRAME GOUGED AT STA 1080 LT AT CUSP ATTACH POINT, 13 ABOVE FLOOR.Jul 8, 1997 · N950R · Doug DC863 · Fuselage Main, FrameSDR RRXA97200Skin · gougedDURING MAINTENANCE VISIT, INSPECTION FOUND RT WING OUTBOARD FLAP LOWER SKIN GOUGED FWD OF EXHAUST GATE STA 258.Jul 8, 1997 · N950R · Doug DC863 · Trailing Edge FlapsSDR RRXA97199Longeron · crackedDURING MAINTENANCE VISIT, INSPECTION FOUND LONGERON 35 LT CRACKED ON INBOARD UPPER LEG FROM STA 1270 TO STA 1280.Jul 8, 1997 · N950R · Doug DC863 · Fuselage Main, Longeron/StringerSDR RRXA97198Longeron · crackedDURING A MAINTENANCE VISIT, INSPECTION FOUND LONGERON 35 RT CRACKED AT SPLICE STA 1270.Jul 8, 1997 · N950R · Doug DC863 · Fuselage Main, Longeron/StringerSDR RRXA97197Longeron · crackedDURING A MAINTENANCE VISIT, INSPECTION FOUND LONGERON 33 LT CRACKED AT SPLICE, STA 1270.Jul 8, 1997 · N950R · Doug DC863 · Fuselage Main, Longeron/StringerSDR RRXA97193Skin · corrodedDURING MAINTENANCE VISIT, INSPECTION FOUND LT HORIZONTAL STAB, LOWER TRAILING EDGE SKIN CORRODED AT STA 231, 2 TO 16 AFT OF REAR SPAR. FABRICATED AND INSTALLED NEW HORIZONTAL STABILIZER TRAILING EDGE PANEL IAW FAA DER APPROVED COTNEY ENGINEERING SKETCH C84-R0Jul 3, 1997 · N950R · Doug DC863 · Horizontal Stabilizer, Plate/SkinSDR RRXA97192Air Shroud · crackedDURING A MAINTENANCE VISIT, FOUND NR 1 ENGINE EXHAUST NOZZLE AFT FAN AIR SHOUD CRACKED IN TWO AREAS. ONE CRACK AT 5:30 AND 1 CRACK AT 8:30 POSITION.Jul 2, 1997 · N950R · Doug DC863 · Engine Collector/Tailpipe/NozzleSDR RRXA97191Longeron · crackedDURING A MAINTENANCE VISIT, FOUND BOLT HOLE CRACKED AT LONGERON 24 RIGHT AND STA 900.Jul 2, 1997 · N950R · Doug DC863 · Fuselage Main, Longeron/StringerSDR RRXA97190Longeron · crackedDURING A MAINTENANCE VISIT, FOUND LONGERON 24 LEFT CRACKED, BETWEEN STA 880 AND STA 900.Jul 2, 1997 · N950R · Doug DC863 · Fuselage Main, Longeron/StringerSDR RRXA96040Duct Clamp · missingKDAY - FLT 27 - DURING CLIMB-OUT, NUMEROUS WARNING LIGHTS AND INDICATORS FOR NR 2 ENG CAME ON. GEN DRIVE OIL LIGHT, NR 2 START VLV OPEN LIGHT, GEN FAIL LIGHT, GEN UNPARALLED LIGHT, ENG OIL PRESS FRONT AND BACK AND CB'S OPENED ALL PERTAINING TO NR 2 ENG, OIL PJul 16, 1996 · N950R · Doug DC863 · Pneumatic Distribution SystemSDR 95ZZZM656Uplatch Pin · shearedFLT NR 021 - KDFW-KDAY - AFTER TAKEOFF UPLATCH CHECK WAS NOT GOOD. GEAR UNSAFE LIGHT ON. EXTENDED GEAR AND RETRACTED GEAR. WHEN UPLATCH CHECK WAS ATTEMPTED AGAIN, THE GEAR HANDLE WOULD NOT MOVE. UNABLE TO MOVE LONG HANDLE, SHORT HANDLE WAS PUT DOWN AND GEAOct 13, 1995 · N950R · Doug DC863 · Landing Gear Retraction/Extension SystemSDR 95ZZZM561Actuator · out of adjustFLT 212 - KDAY-KMCI - DURING CLIMB, GEAR NOT LATCHED AND DOOR NOT LATCHED LIGHTS AND RIGHT ALT LIGHT ON AFTER RETACTION AND UPLATCH CHECK. EXTENDED GEAR, GOT 3 GREEN, NO ABNORMALITIES. CYCLED GEAR SEVERAL TIMES AND GOT ORIGINAL INDICATIONS. FOLLOWED ABNORMAAug 19, 1995 · N950R · Doug DC863 · Landing Gear Retraction/Extension System
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