# Service difficulty reports: Sabreliner NA-265-80

A list on [Sabreliner NA-265-80](https://openairdocs.org/model/sabreliner-na-265-80.md).

Newest first. General aviation reporting is voluntary.

- [SDR 2021FA0000004](https://openairdocs.org/sdr/2021FA0000004.md): Panel · damaged · Nov 4, 2021 · N171AT · Rkwell NA26580 · Fuselage Main, Plate/Skin
  > CABIN FLOOR PANEL IS DAMAGED.
- [SDR BTA2003F00001](https://openairdocs.org/sdr/BTA2003F00001.md): Engine · flamed out · Feb 12, 2003 · N382LS · Rkwell NA26580 · Engine (Turbine/Turboprop)
  > AIRCRAFT 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 ABN
- [SDR BTA2003F00000](https://openairdocs.org/sdr/BTA2003F00000.md): Engine · flamed out · Feb 12, 2003 · N382LS · Rkwell NA26580 · Engine (Turbine/Turboprop)
  > AIRCRAFT 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 ABNORMALITI
- [SDR UVV2002F00000](https://openairdocs.org/sdr/UVV2002F00000.md): Panel · corroded · Apr 19, 2002 · N910BH · Rkwell NA26580 · Wing, Plate/Skin
  > FOUND 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
- [SDR 2001FA0000393](https://openairdocs.org/sdr/2001FA0000393.md): Support · broken · Sep 27, 2001 · N380GK · Rkwell NA26580 · Elevator Control System
  > DURING 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.
- [SDR 20010510AP001](https://openairdocs.org/sdr/20010510AP001.md): Lever · mismanufactured · Apr 24, 2001 · N316EC · Rkwell NA26580 · Engine Thrust Reverser
  > ON 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 REVEAL
- [SDR 20010501AP004](https://openairdocs.org/sdr/20010501AP004.md): Lever · mismanufactured · Apr 24, 2001 · N316EC · Rkwell NA26580 · Engine Thrust Reverser
  > ON 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 REVEALED
- [SDR 20000508SH006](https://openairdocs.org/sdr/20000508SH006.md): Rib · cracked · Apr 10, 2000 · N7148J · Rkwell NA26580 · Fuselage Miscellaneous Structure
  > WHILE 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 AS
- [SDR 20000504SH029](https://openairdocs.org/sdr/20000504SH029.md): Rib · cracked · Apr 10, 2000 · N7148J · Rkwell NA26580 · Landing Gear Actuator
  > DUE 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 DU
- [SDR 20000505SH021](https://openairdocs.org/sdr/20000505SH021.md): Thrust Reverser · malfunctioned · Mar 2, 2000 · N265KC · Rkwell NA26580 · Engine Thrust Reverser
  > LEFT 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)
- [SDR 20000504SH028](https://openairdocs.org/sdr/20000504SH028.md): Switch · failed · Dec 27, 1999 · N71460 · Rkwell NA26580 · Landing Gear Retraction/Extension System
  > THE 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)
- [SDR 20000503SH008](https://openairdocs.org/sdr/20000503SH008.md): Wheel · failed · Aug 24, 1999 · N7148J · Rkwell NA26580 · Wheel/Ski/Float
  > THE 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)
- [SDR RU3A99004](https://openairdocs.org/sdr/RU3A99004.md): Valve · malfunctioned · May 24, 1999 · N58 · Rkwell NA26580 · Pneumatic Distribution System
  > OK - 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)
- [SDR 99ZZZX1969](https://openairdocs.org/sdr/99ZZZX1969.md): Support · cracked · Mar 12, 1999 · N424R · Rkwell NA26580 · Elevator Structure
  > DURING 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 PA
- [SDR RU3A9805](https://openairdocs.org/sdr/RU3A9805.md): Fire Loop · malfunctioned · Oct 6, 1998 · N58 · Rkwell NA26580 · Detection System
  > RIGHT ENGINE FIRE LIGHT ILLUMINATED IN FLIGHT. ENGINE POWER LEVER WAS BROUGHT BACK TO IDLE AND LIGHT EXTINGUISHED. RETURN TO STATION WITHOUT FURTHER INCIDENT. (M)
- [SDR 98ZZZX3333](https://openairdocs.org/sdr/98ZZZX3333.md): Wheel Rim · damaged · Aug 26, 1998 · N7148J · Rkwell NA26580 · Wheel/Ski/Float
  > AFTER 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.
- [SDR 98ZZZX3594](https://openairdocs.org/sdr/98ZZZX3594.md): Web · cracked · Aug 12, 1998 · N12659 · Rkwell NA26580 · Fuselage Miscellaneous Structure
  > WHILE 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 BETWE
- [SDR 98ZZZX3593](https://openairdocs.org/sdr/98ZZZX3593.md): Web · cracked · Aug 12, 1998 · N71460 · Rkwell NA26580 · Fuselage Main, Bulkhead
  > WHILE 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 BETWE
- [SDR 98ZZZX3592](https://openairdocs.org/sdr/98ZZZX3592.md): Web · cracked · Aug 12, 1998 · N7148J · Rkwell NA26580 · Fuselage Miscellaneous Structure
  > WHILE 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 BETWE
- [SDR 98ZZZX3591](https://openairdocs.org/sdr/98ZZZX3591.md): Web · cracked · Aug 12, 1998 · N2200A · Rkwell NA26580 · Fuselage Miscellaneous Structure
  > WHILE 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 BETWE
- [SDR 98ZZZX3341](https://openairdocs.org/sdr/98ZZZX3341.md): Slat · separated · Aug 5, 1998 · N773W · Rkwell NA26580 · Leading Edge Devices
  > ON 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 CO
- [SDR HAIHEEA9853](https://openairdocs.org/sdr/HAIHEEA9853.md): Actuator · leaks · May 13, 1997 · N221PH · Rkwell NA26580 · Autopilot System
  > ACTUATOR LEAKS.
- [SDR HAIHEEA9287](https://openairdocs.org/sdr/HAIHEEA9287.md): Transponder · inoperative · Mar 31, 1997 · N221PH · Rkwell NA26580 · ATC Transponder System
  > TRANSPONDER COMPLETELY DEAD.
- [SDR 97ZZZX1077](https://openairdocs.org/sdr/97ZZZX1077.md): Brake Valve · malfunctioned · Feb 5, 1997 · N383CF · Rkwell NA26580 · Landing Gear Brake System
  > AIRCRAFT 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 AND
- [SDR HEEA978878](https://openairdocs.org/sdr/HEEA978878.md): Engine · oil leak · Jan 14, 1997 · N221PH · Rkwell NA26580 · Turbine Engine Compressor Section
  > LEAKING OIL FROM FAN SPLIT LINE.
- [SDR 96ZZZX4696](https://openairdocs.org/sdr/96ZZZX4696.md): Skin · cracked · Aug 20, 1996 · N7148J · Rkwell NA26580 · Wing, Plate/Skin
  > WHILE 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 DE
- [SDR 96ZZZX1345](https://openairdocs.org/sdr/96ZZZX1345.md): Skin · corroded · Jan 30, 1996 · N221PH · Rkwell NA26580 · Wing, Plate/Skin
  > DURING 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 T
- [SDR 96ZZZX1344](https://openairdocs.org/sdr/96ZZZX1344.md): Skin · corroded · Jan 30, 1996 · N221PH · Rkwell NA26580 · Wing, Plate/Skin
  > DURING 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 T
- [SDR 95ZZZX6840](https://openairdocs.org/sdr/95ZZZX6840.md): Support · cracked · Oct 16, 1995 · N66ED · Rkwell NA26580 · Horizontal Stabilizer Structure
  > SUPPORT 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 CRA
- [SDR 95ZZZX5705](https://openairdocs.org/sdr/95ZZZX5705.md): Support Assy · cracked · Aug 23, 1995 · N66ED · Rkwell NA26580 · Horizontal Stabilizer Structure
  > DEFECTS 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 BEA
- [SDR 95ZZZX5704](https://openairdocs.org/sdr/95ZZZX5704.md): Support Assy · cracked · Aug 23, 1995 · N66ED · Rkwell NA26580 · Horizontal Stabilizer Structure
  > DEFECTS 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 BEA
- [SDR 95ZZZX1488](https://openairdocs.org/sdr/95ZZZX1488.md): Inner Arm · mismanufactured · Mar 6, 1995 · N80LX · Rkwell NA26580 · Engine Thrust Reverser
  > ARMS 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 LE
- [SDR 95ZZZX1487](https://openairdocs.org/sdr/95ZZZX1487.md): Inner Arm · mismanufactured · Mar 6, 1995 · N80LX · Rkwell NA26580 · Engine Thrust Reverser
  > ARMS 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 LE

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/model/sabreliner-na-265-80/reports

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