Sabreliner NA-265-80

Service difficulty reports · 33

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 = 'NA26580'
  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 2021FA0000004Panel · damagedCABIN FLOOR PANEL IS DAMAGED.Nov 4, 2021 · N171AT · Rkwell NA26580 · Fuselage Main, Plate/SkinSDR BTA2003F00001Engine · flamed outAIRCRAFT IN FLIGHT AT HIGH ALTITUDE (FL410) AIRCRAFT GOT SLOW (APPROXIMATELY 165 KNOTS). RIGHT ENGINE FLAMED OUT. ADVISE ATC THAT WE HAD ENGINE PROBLEM AND REQUEST TO GO DOWN TO FL270 TO RESTART ENGINE. DESCENDED TO FL270 AND RESTARTED ENGINE. NO OTHER ABNFeb 12, 2003 · N382LS · Rkwell NA26580 · Engine (Turbine/Turboprop)SDR BTA2003F00000Engine · flamed outAIRCRAFT IN FLIGHT AT HIGH ALTITUDE (FL410) AIRCRAFT GOT SLOW (APPROX. 165 KNTS). RIGHT ENGINE FLAMED OUT. ADVISE ATC THAT WE HAD ENGINE PROBLEM AND REQUEST TO GO DOWN TO FL270 TO RESTART ENGINE. DECENDED TO FL270 AND RESTARTED ENGINE. NO OTHER ABNORMALITIFeb 12, 2003 · N382LS · Rkwell NA26580 · Engine (Turbine/Turboprop)SDR UVV2002F00000Panel · corrodedFOUND OVER FLAP PANEL UNDERSIDE CORRODED COMPLETELY THROUGH SKIN TO HONEYCOMB SUBSTRUCTURE. AREA NOT READILY INSPECTABLE DUE TO VELCRO APPLIED OVER AREA TO ACT AS CHAFE STRIPS FOR FLAP UPPER SURFACE. RECOMMEND CLOSE VISUAL INSPECTION OF AREA DURING 150 HOUR Apr 19, 2002 · N910BH · Rkwell NA26580 · Wing, Plate/SkinSDR 2001FA0000393Support · brokenDURING SCHEDULED INSPCTION FOUND SMALL PIECE OF A BEARING BOSS IN HELL HOLE. UPON INVESTIGATION FOUND ELEVATOR TORQUE TUBE SUPPORT MISSING PIECE. ALSO FOUND RT SUPPORT CRACKED IN THE SAME POSITION. REPLACED BOTH RT AND LT ELEVATOR SUPPORT BRACKETS.Sep 27, 2001 · N380GK · Rkwell NA26580 · Elevator Control SystemSDR 20010510AP001Lever · mismanufacturedON 8/9/99 1EA. P/N232-20258-511 WAS INSTALLED ON LT T/R. 2EA. P/N 232-20258-513 AND 2EA. 232-20258-514 LEVERS WERE INSTALLED ON RT T/R DURING REPAIR OF THESE T/R''''S. IN JAN. 2001 THE CUSTOMER REPORTED PROBLEMS WITH THE LT T/R. INSPECTION OF BOTH T/RS REVEALApr 24, 2001 · N316EC · Rkwell NA26580 · Engine Thrust ReverserSDR 20010501AP004Lever · mismanufacturedON 8/9/99 1EA. P/N232-20258-511 WAS INSTALLED ON L/H T/R. 2EA. P/N 232-20258-513 AND 2EA. 232-20258-514 LEVERS WERE INSTALLED ON R/H T/R DURING REPAIR OF THESE T/RS. IN JAN. 2001 THE CUSTOMER REPORTED PROBLEMS WITH THE LT T/R. INSPECTION OF BOTH T/RS REVEALEDApr 24, 2001 · N316EC · Rkwell NA26580 · Engine Thrust ReverserSDR 20000508SH006Rib · crackedWHILE DOING HARD LANDING INSPECTION, THE RIB ASSEMBLY IN THE RT MAIN LANDING GEAR WHEELWELL WAS FOUND CRACKED. THIS POSSIBLE HARD LANDING WAS REPORTED TO MAINTENANCE ON THE RETURN OF AIRCRAFT, 4-10-00. NO OTHER DISCREPANCY WAS NOTED IN THIS AREA. THIS RIB ASApr 10, 2000 · N7148J · Rkwell NA26580 · Fuselage Miscellaneous StructureSDR 20000504SH029Rib · crackedDUE TO SUSPECTED HARD LANDING, AIRCRAFT WAS INSPECTED AND MAINTENANCE DISCOVERED A 1.50 INCH CRACK IN THE LOWER RADIUS OF THE RT MAIN LANDING GEAR ACTUATOR ATTACHMENT RIB ASSEMBLY. RIB REPLACED AND NO FURTHER DEFECTS NOTED. THIS SAME RIB WAS FOUND CRACKED DUApr 10, 2000 · N7148J · Rkwell NA26580 · Landing Gear ActuatorSDR 20000505SH021Thrust Reverser · malfunctionedLEFT THRUST REVERSER FAILED TO RETURN TO STOW POSITION AFTER LANDING. CONNECTED EXTERNAL AIR SUPPLY TO THRUST REVERSER AIR SUPPLY MANIFOLD AND CLOSED THRUST REVERSER. PINNED, DEFERRED THRUST REVERSER IAW MEL. (X)Mar 2, 2000 · N265KC · Rkwell NA26580 · Engine Thrust ReverserSDR 20000504SH028Switch · failedTHE AIRCRAFT RETURNED TO THE USMS RAMP WITH A LOG ENTRY STATING THE GEAR WILL NOT LOCK NORMAL, FREE FELL GEAR ALL GREEN. THE AIRCRAFT WAS PLACED ON JACKS AND THE GEAR SYSTEM WAS INSPECTED. (X)Dec 27, 1999 · N71460 · Rkwell NA26580 · Landing Gear Retraction/Extension SystemSDR 20000503SH008Wheel · failedTHE AIRCRAFT RETURNED TO THE USMS RAMP WITH A DISCREPANCY ON THE NR 3 TIRE BEING FLAT. THE NR 3 WHEEL ASSY WAS REMOVED AND THE RIM HAD A 6-10 INCH SECTION OF THE INBOARD RIM LIP BROKEN OFF. (X)Aug 24, 1999 · N7148J · Rkwell NA26580 · Wheel/Ski/FloatSDR RU3A99004Valve · malfunctionedOK - STRONG ODOR OF BURNING RUBBER COCKPIT IMMEDIATELY AFTER TAKEOFF. RIGHT ENGINE FIRE WARNING LIGHT ILLUMINATED IMMEDIATELY AFTER TAKEOFF. ENGINE SHUT DOWN AND RETURN SAFELY TO LAND. (M)May 24, 1999 · N58 · Rkwell NA26580 · Pneumatic Distribution SystemSDR 99ZZZX1969Support · crackedDURING THE COURSE OF A ROUTINE ELEVATOR BALANCE INSPECTION, BOTH LEFT AND RIGHT ELEVATOR INBOARD HINGE BEARING SUPPORTS WERE FOUND CRACKED THROUGH THE BEARING SUPPORT RING AREA OF THE CASTING. BOTH LEFT AND RIGHT SUPPORTS WERE REMOVED AND REPLACED WITH NEW PAMar 12, 1999 · N424R · Rkwell NA26580 · Elevator StructureSDR RU3A9805Fire Loop · malfunctionedRIGHT ENGINE FIRE LIGHT ILLUMINATED IN FLIGHT. ENGINE POWER LEVER WAS BROUGHT BACK TO IDLE AND LIGHT EXTINGUISHED. RETURN TO STATION WITHOUT FURTHER INCIDENT. (M)Oct 6, 1998 · N58 · Rkwell NA26580 · Detection SystemSDR 98ZZZX3333Wheel Rim · damagedAFTER AIRCRAFT TAXIED TO PARKING, THE TIRE WAS FOUND FLAT. INSPECTION DISCOVERED THE INBOARD SIDE OF RIM BROKEN. THE MISSING PART WAS FOUND ON THE TAXIWAY. THE RIM/TIRE ASSY WAS INSTALLED ON THE AIRCRAFT ON 5-29-98.Aug 26, 1998 · N7148J · Rkwell NA26580 · Wheel/Ski/FloatSDR 98ZZZX3594Web · crackedWHILE PERFORMING A VISUAL INSPECTION OF THE NOSE GEAR WHEEL WELL DURING A SCHEDULED 150 HOUR INSPECTION, CRACKS WERE DISCOVERED INSIDE THE NOSE GEAR WELL AT THE LANDING GEAR WEB AREA. THESE CRACKS ARE LOCATED ON BOTH THE LT AND RT SIDE OF THE WHEEL WELL BETWEAug 12, 1998 · N12659 · Rkwell NA26580 · Fuselage Miscellaneous StructureSDR 98ZZZX3593Web · crackedWHILE PERFORMING A VISUAL INSPECTION OF THE NOSE GEAR WHEEL WELL DURING A SCHEDULED 150 HOUR INSPECTION, CRACKS WERE DISCOVERED INSIDE THE NOSE GEAR WELL AT THE LANDING GEAR WEB AREA. THESE CRACKS ARE LOCATED ON BOTH THE LT AND RT SIDE OF THE WHEEL WELL BETWEAug 12, 1998 · N71460 · Rkwell NA26580 · Fuselage Main, BulkheadSDR 98ZZZX3592Web · crackedWHILE PERFORMING A VISUAL INSPECTION OF THE NOSE GEAR WHEEL WELL DURING A SCHEDULED 150 HOUR INSPECTION, CRACKS WERE DISCOVERED INSIDE THE NOSE GEAR WELL AT THE LANDING GEAR WEB AREA. THESE CRACKS ARE LOCATED ON BOTH THE LT AND RT SIDE OF THE WHEEL WELL BETWEAug 12, 1998 · N7148J · Rkwell NA26580 · Fuselage Miscellaneous StructureSDR 98ZZZX3591Web · crackedWHILE PERFORMING A VISUAL INSPECTION OF THE NOSE GEAR WHEEL WELL DURING A SCHEDULED 150 HOUR INSPECTION, CRACKS WERE DISCOVERED INSIDE THE NOSE GEAR WELL AT THE LANDING GEAR WEB AREA. THESE CRACKS ARE LOCATED ON BOTH THE LT AND RT SIDE OF THE WHEEL WELL BETWEAug 12, 1998 · N2200A · Rkwell NA26580 · Fuselage Miscellaneous StructureSDR 98ZZZX3341Slat · separatedON POST-FLIGHT INSPECTION, LT INBD SLAT WAS DISCOVERED MISSING (38) RIVETS ON THE UNDERSIDE AND BOTH INBD RIBS CRACKED AND BROKEN, HOLES VERY ELONGATED. ALSO, WING LEADING EDGE SKIN IMMEDIATELY AFT, MISSING (5) RIVETS, RIBS CRACKED (OLD CRACKS). 1ST STAGE COAug 5, 1998 · N773W · Rkwell NA26580 · Leading Edge DevicesSDR HAIHEEA9853Actuator · leaksACTUATOR LEAKS.May 13, 1997 · N221PH · Rkwell NA26580 · Autopilot SystemSDR HAIHEEA9287Transponder · inoperativeTRANSPONDER COMPLETELY DEAD.Mar 31, 1997 · N221PH · Rkwell NA26580 · ATC Transponder SystemSDR 97ZZZX1077Brake Valve · malfunctionedAIRCRAFT LANDED AT PTK AND DURING BRAKING, WENT OFF THE RIGHT SIDE OF RUNWAY. PILOTS STATED ACFT WAS PULLING TO THE RIGHT AND WAS NOT SLOWING DOWN FAST ENOUGH TO KEEP IT ON THE RUNWAY. DURING TROUBLESHOOTING, PRESSURE GAUGES INSTALLED AT EACH WHEEL BRAKE ANDFeb 5, 1997 · N383CF · Rkwell NA26580 · Landing Gear Brake SystemSDR HEEA978878Engine · oil leakLEAKING OIL FROM FAN SPLIT LINE.Jan 14, 1997 · N221PH · Rkwell NA26580 · Turbine Engine Compressor SectionSDR 96ZZZX4696Skin · crackedWHILE PERFORMING PRE-FLIGHT INSP, MECH NOTICED PAINT CRACKED AND CHIPPED ON L/E OF WING ABOUT SS 236.9. UPON FURTHER INSP FOUND A CRACK, ABOUT 8.5 INCHES, THROUGH FIRST STIFFENER AND 4.0 INCHES AND 5.0 INCHES THROUGH SECOND STIFFENER ON BOTTOM OF L/E UNDER DEAug 20, 1996 · N7148J · Rkwell NA26580 · Wing, Plate/SkinSDR 96ZZZX1345Skin · corrodedDURING REPAINT OF AIRCRAFT WITH SUPER CRITICAL WING, FOUND EXISTING SEALANT CRACKED AND DETERIORATED. AT CUSTOMER REQUEST, REMOVED SEALANT AND FOUND ALUMINUM SKIN SURFACE AT EDGE OF OVERLAY CORRODED BEYOND MANUFACTURER'S ALLOWABLE LIMITS. ONE AREA APPEARED TJan 30, 1996 · N221PH · Rkwell NA26580 · Wing, Plate/SkinSDR 96ZZZX1344Skin · corrodedDURING REPAINT OF AIRCRAFT WITH SUPER CRITICAL WING, FOUND EXISTING SEALANT CRACKED AND DETERIORATED. AT CUSTOMER REQUEST, REMOVED SEALANT AND FOUND ALUMINUM SKIN SURFACE AT EDGE OF OVERLAY CORRODED BEYOND MANUFACTURER'S ALLOWABLE LIMITS. ONE AREA APPEARED TJan 30, 1996 · N221PH · Rkwell NA26580 · Wing, Plate/SkinSDR 95ZZZX6840Support · crackedSUPPORT CRACKED AT END WHERE ELEVATOR ATTACHES. THIS CAUSES HINGE BEARINGS, PN BR4, TO BE LOOSE. THIS PART CAN ONLY BE SEEN BY REMOVING HINGE SUPPORT, PN 285-220401-7. RIGHT SUPPORT WAS FOUND BROKEN AND AS A PRECAUTION, LEFT SIDE WAS INSPECTED AND FOUND CRAOct 16, 1995 · N66ED · Rkwell NA26580 · Horizontal Stabilizer StructureSDR 95ZZZX5705Support Assy · crackedDEFECTS WERE FOUND DURING ROUTINE MAINTENANCE INSPECTION PER CAMP CARD NR 27013, ATA 274006, LT, AND ATA 274007, RT. THE LT INBD HORIZ SUPPORT WAS FOUND BROKEN AT THE BEARING (PN BR4) AND THE RT INBD HORIZ SUPPORT WAS CRACKED AT THE BEARING (PN BR4). THE BEAAug 23, 1995 · N66ED · Rkwell NA26580 · Horizontal Stabilizer StructureSDR 95ZZZX5704Support Assy · crackedDEFECTS WERE FOUND DURING ROUTINE MAINTENANCE INSPECTION PER CAMP CARD NR 27013, ATA 274006, LT, AND ATA 274007, RT. THE LT INBD HORIZ SUPPORT WAS FOUND BROKEN AT THE BEARING (PN BR4) AND THE RT INBD HORIZ SUPPORT WAS CRACKED AT THE BEARING (PN BR4). THE BEAAug 23, 1995 · N66ED · Rkwell NA26580 · Horizontal Stabilizer StructureSDR 95ZZZX1488Inner Arm · mismanufacturedARMS ARE MANUFACTURED BY LEARJET UNDER PMA. BIZJET RECEIVED AND PUT IN STOCK 1 EACH DASH 511 ARM AND 6 EACH DASH 512 ARMS. ONE EACH DASH 511 ARM AND 2 EACH DASH 512 ARMS WERE INSTALLED ON A CUSTOMER'S AIRCRAFT. BIZJET'S PURCHASING AGENT WAS NOTIFIED BY A LEMar 6, 1995 · N80LX · Rkwell NA26580 · Engine Thrust ReverserSDR 95ZZZX1487Inner Arm · mismanufacturedARMS ARE MANUFACTURED BY LEARJET UNDER PMA. BIZJET RECEIVED AND PUT IN STOCK 1 EACH DASH 511 ARM AND 6 EACH DASH 512 ARMS. ONE EACH DASH 511 ARM AND 2 EACH DASH 512 ARMS WERE INSTALLED ON A CUSTOMER'S AIRCRAFT. BIZJET'S PURCHASING AGENT WAS NOTIFIED BY A LEMar 6, 1995 · N80LX · Rkwell NA26580 · Engine Thrust Reverser
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