# Service difficulty reports: Slingsby T67M-260

A list on [Slingsby T67M-260](https://openairdocs.org/model/slingsby-t67m-260.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 76 reports

- [SDR 98ZZZX3142](https://openairdocs.org/sdr/98ZZZX3142.md): Fuel Hose · loose · Jul 1, 1998 · N3045S · Slnsby T67M260 · Aircraft Fuel Distribution System
  > THE ENGINE QUIT WHILE PERFORMING AN ENGINE GROUND RUN-UP. DEFUELED AIRCRAFT AND OPENED FUEL TANK FOR INSPECTION. THE FUEL FLAP TUB WAS REMOVED FOR INSPECTION AND AN AIR PRESSURE CHECK WAS PERFORMED. FOUND AN AIR LEAK AT THE SCREW CLAMP SECURING THE FUEL HOS
- [SDR 97ZZZX5178](https://openairdocs.org/sdr/97ZZZX5178.md): Oil Filter · cracked · Dec 11, 1997 · Slnsby T67M260 · Reciprocating Engine Oil System
  > CRACKS WERE FOUND ON ENGINE OIL FILTERS (NEW FILTERS). THIS CRACK IS ON THE BASE FLANGE INSIDE OF BASE SEAL AND OUTBOARD OF INLET HOLES. SUSPECT CAUSE MIGHT BE ASSEMBLY DEFECT. SUBMITTER RECOMMENDED EMERGENCY AD ISSUE ON THIS OIL FILTER AND REPLACE IF FOUND
- [SDR 97ZZZX3924](https://openairdocs.org/sdr/97ZZZX3924.md): Steering Collar · cracked · Aug 11, 1997 · Slnsby T67M260 · Landing Gear Steering System
  > DURING 100-HOUR INSPECTION, THE NOSE STEERING COLLAR ON NOSE STRUT WAS FOUND CRACKED. A ONE-TIME INSPECTION WAS PERFORMED FOR THE REST OF THE FLEET (57). EIGHTEEN AIRCRAFT WERE FOUND WITH NOSE WHEEL STEERING COLLAR CRACKED. UNKNOWN CAUSE AND NO RECOMMENDATI
- [SDR 97ZZZX3414](https://openairdocs.org/sdr/97ZZZX3414.md): Blade · loose · Jul 15, 1997 · N3037C · Slnsby T67M260 · Propeller Blade Section
  > AFTER AEROBATICS, EXCESSIVE NOSE/PROPELLER VIBRATION WAS FELT, VERY ROUGH AND LOW AIRSPEED. ACFT LANDED SAFELY. FOUND NR 1 PROPELLER BLADE HAD EXCESSIVE PLAY. REMOVED AND REPLACED THE PROPELLER. PROPELLER WAS SENT TO MANUFACTURER FOR INSPECTION AND REPAIR.
- [SDR 97ZZZX2885](https://openairdocs.org/sdr/97ZZZX2885.md): Sump · cracked · Jun 13, 1997 · N3188R · Slnsby T67M260 · Reciprocating Engine Oil System
  > AFTER A PHASE INSPECTION AND AFTER ENGINE RUN-UP, THE ENGINE WAS CHECKED FOR OIL LEAKS BEFORE COWLING INSTALLED. A LEAK WAS NOTED BEHIND THE RIGHT REAR ENGINE MOUNT BRACKET. A CLOSER LOOK WAS MADE AND A CRACK WAS FOUND (ABOUT 2.50 INCHES LONG). OIL SUMP WAS
- [SDR 97ZZZX2891](https://openairdocs.org/sdr/97ZZZX2891.md): G Switch · failed · May 28, 1997 · N7020D · Slnsby T67M260 · Emergency Locator Beacon
  > WHILE PERFORMING AN ANNUAL ELT INSPECTION, ELT SENSOR DID NOT COME ON. DORNE AND MARGOLIN, ELT NR TSOC91.
- [SDR 97ZZZX4299](https://openairdocs.org/sdr/97ZZZX4299.md): Switch · malfunction · May 27, 1997 · N3045H · Slnsby T67M260 · Emergency Locator Beacon
  > WHILE PERFORMING AN ANNUAL ELT INSPECTION, FOUND THE ELT SENSOR DID NOT COME ON.
- [SDR 97ZZZX970](https://openairdocs.org/sdr/97ZZZX970.md): Tank · cracked · Feb 13, 1997 · N3045H · Slnsby T67M260 · Fuel Storage
  > ON A PRE-FLIGHT INSPECTION, A FUEL STAIN WAS NOTICED ON BOTTOM OF LEFT WING. FURTHER INSPECTION FOUND A CRACK ON THE FWD INBOARD SIDE OF THE FUEL TANK. SUBMITTER SUSPECTS POSSIBLE STRESS CRACK. AWATING REPAIR FROM MANUFACTURER.
- [SDR 97ZZZX969](https://openairdocs.org/sdr/97ZZZX969.md): Blade · delamination · Feb 13, 1997 · N31909 · Slnsby T67M260 · Propeller Blade Section
  > INSPECTION OF PROPELLER FOUND A PROPELLER BLADE WITH DELAMINATION AT BASE OF BLADE. (ONE INCH WIDE BY FOUR INCHES LONG). CAUSE UNKNOWN. AWAITING INFORMATION FROM HOFFMAN PROPELLER.
- [SDR 97ZZZX753](https://openairdocs.org/sdr/97ZZZX753.md): Wire · chafed · Feb 4, 1997 · N3045S · Slnsby T67M260 · Communications System Wiring
  > WIRE BUNDLE CHAFING ON INSTRUMENT MOUNT BRACKET BEHIND RADIOS. DISCREPANCY IS THE INTERCOM DOES NOT TRANSMIT CLEARLY. CUTS IN AND OUT. INSPECTED, FOUND A WIRE CHAFE THROUGH DUE TO THE WIRE BUNDLE ON THE RADIO MOUNT BRACKET. RECOMMEND RE-ROUTING OF THE WIRE
- [SDR 97ZZZX893](https://openairdocs.org/sdr/97ZZZX893.md): Blade · delaminated · Jan 1, 1997 · N7020D · Slnsby T67M260 · Propeller Blade Section
  > INSPECTION FOUND DELAMINATION AT BASE OF BLADE. SUBMITTER STATED CAUSE UNKNOWN. AWAITING INFORMATION FROM MANUFACTURER.
- [SDR 97ZZZX887](https://openairdocs.org/sdr/97ZZZX887.md): Blade · delaminated · Jan 1, 1997 · N3004H · Slnsby T67M260 · Propeller Blade Section
  > INSPECTION FOUND DELAMINATION AT BASE OF BLADE. SUBMITTER STATED CAUSE UNKNOWN. AWAITING INFORMATION FROM MANUFACTURER.
- [SDR 96ZZZX5907](https://openairdocs.org/sdr/96ZZZX5907.md): Support Bracket · cracked · Nov 7, 1996 · N31917 · Slnsby T67M260 · Rudder Control System
  > ON ANNUAL INSPECTION THE INBD STBD RUDDER BAR SUPPORT BRACKET WAS FOUND CRACKED. PRESSURE APPLIED TO RUDDER PEDAL PUTS PRESSURE ON BRACKET CAUSING IT TO CRACK. SUBMITTER RECOMMENDS A HEAVIER DUTY BRACKET.
- [SDR 96ZZZX5906](https://openairdocs.org/sdr/96ZZZX5906.md): Muffler · chafed · Nov 7, 1996 · N3004H · Slnsby T67M260 · Engine Collector/Tailpipe/Nozzle
  > ON ANNUAL INSPECTION THE MUFFLER TAILPIPE WAS FOUND CHAFING ON FRAME NR 1 (FIREWALL). THE HEAT EXPANDS THE TAILPIPE WHICH CAUSED IT TO HIT THE BOTTOM OF FRAME NR 1.
- [SDR 96ZZZX5293](https://openairdocs.org/sdr/96ZZZX5293.md): Crank · chafing · Oct 3, 1996 · N3189N · Slnsby T67M260 · Rudder Control System
  > WHILE PERFORMING AN ANNUAL INSPECTION, NOTICED LT RUDDER BAR CRANK WAS CHAFING ON RUDDER BAR WHEN BRAKE WAS APPLIED. SUSPECT RUDDER BAR CRANK WAS IMPROPERLY INSTALLED IN PRODUCTION. SLINGSBY IPC CHAPTER 19, PAGES 19, 20, ITEMS 5 AND 2.
- [SDR 96ZZZX5294](https://openairdocs.org/sdr/96ZZZX5294.md): Brake Caliper · leaking · Sep 7, 1996 · N3192X · Slnsby T67M260 · Brake
  > DURING 100-HOUR INSPECTION, RT BRAKE CALIPER FOUND LEAKING THROUGH CASE, WHEN BRAKE WAS APPLIED. HYDRAULIC FLUID WAS SEEN LEAKING FROM CASE. SUBMITTER SUSPECTS POSSIBLE IMPURITIES IN MOLD WHEN BEING MADE. THIS IS THE SECOND OCCURRENCE.
- [SDR 96ZZZX4867](https://openairdocs.org/sdr/96ZZZX4867.md): Sender · failed · Sep 5, 1996 · N3064Q · Slnsby T67M260 · Engine Oil Pressure
  > AIRCREWS REPORT ENGINE OIL PRESSURE TOO LOW OR TOO HIGH DURING GROUND AND FLIGHT OPERATIONS. ERRONEOUS OIL PRESSURE GAUGE NEEDLE INDICATIONS HAVE CAUSED EMERGENCY LANDINGS. THE OIL PRESSURE SENDER/TRANSDUCER IS MANUFACTURED BY VDO IN GERMANY AND DISTRIBUTED
- [SDR 96ZZZX4836](https://openairdocs.org/sdr/96ZZZX4836.md): Brake Disc · warped · Aug 29, 1996 · N31398 · Slnsby T67M260 · Brake
  > THE AIR CREW REPORTED THE AIRCRAFT BRAKES WERE SPONGY DURING BRAKING APPLICATION. THERE HAVE BEEN MANY REPORTS BY USAF PILOTS IN THE T-3A PROGRAM PERTAINING TO SPONGY OR DEFECTIVE BRAKES. A DETAILED INSPECTION OF THIS AIRCRAFT'S BRAKING SYSTEM REVEALED A WAR
- [SDR 96ZZZX4835](https://openairdocs.org/sdr/96ZZZX4835.md): Brake Disc · warped · Aug 29, 1996 · N3102J · Slnsby T67M260 · Brake
  > THE AIR CREW REPORTED THE ACFT BRAKES WERE SPONGY DURING BRAKING APPLICATION. THERE HAVE BEEN MANY REPORTS BY USAF PILOTS IN THE T-3A PROGRAM PERTAINING TO SPONGY OR DEFECTIVE BRAKES. A DETAILED INSPECTION OF THIS AIRCRAFT'S BRAKING SYSTEM REVEALED A WARPED
- [SDR 96ZZZX4834](https://openairdocs.org/sdr/96ZZZX4834.md): Fuel Pump · failed · Aug 29, 1996 · N30723 · Slnsby T67M260 · Fuel Boost Pump
  > THE AIR CREW REPORTED LOW OR NO FUEL PRESSURE INDICATION/RISE DURING PRE-FLIGHT CHECK. FURTHER INSPECTION BY UNC MAINTENANCE TECHNICIANS REVEALED THE FUEL PUMP DID NOT PRODUCE ANY NOISE WHEN THE FUEL PUMP BOOST SWITCH WAS TURNED ON. THERE HAVE BEEN 6 AIRBORN
- [SDR 96ZZZX4298](https://openairdocs.org/sdr/96ZZZX4298.md): Push Rod · broken · Aug 15, 1996 · N3104L · Slnsby T67M260 · Power Lever
  > THE AIRCREW DECLARED AN IN-FLIGHT EMERGENCY AFTER ACFT ENGINE WOULD NOT RESPOND TO THROTTLE APPLICATION FROM IP'S REMOTE THROTTLE HANDLE AND LINKAGE LOCATED ON LT SIDE OF COCKPIT. REMOTE THROTTLE LEVER/HANDLE IS ATTACHED TO LT SIDE OF AIRFRAME. IT IS ATTACHE
- [SDR 96ZZZX4299](https://openairdocs.org/sdr/96ZZZX4299.md): Push Rod · broken · Jul 10, 1996 · N3172R · Slnsby T67M260 · Power Lever
  > THE AIRCREW DECLARED AN IN-FLIGHT EMERGENCY AFTER ACFT ENGINE WOULD NOT RESPOND TO THROTTLE APPLICATION FROM IP'S REMOTE THROTTLE HANDLE AND LINKAGE LOCATED ON LT SIDE OF COCKPIT. REMOTE THROTTLE LEVER/HANDLE IS ATTACHED TO LT SIDE OF AIRFRAME. IT IS ATTACHE
- [SDR 96ZZZX4833](https://openairdocs.org/sdr/96ZZZX4833.md): Master Cylinders · failed · Jul 9, 1996 · N3102J · Slnsby T67M260 · Master Cylinder/Brake Valve
  > AIR CREWS HAVE REPORTED AIRCRAFT BRAKE PEDALS WERE SPONGY OR HAVE FADED/FAILED DURING BRAKING APPLICATIONS. AFTER 20,000 HOURS OF OPERATION AT THE USAFA, BRAKE SYSTEMS STARTED TO DEVELOP PROBLEMS. REVISED BRAKE BLEEDING PROCEDURES WERE DEVELOPED, OPERATOR BR
- [SDR 96ZZZX3810](https://openairdocs.org/sdr/96ZZZX3810.md): Engine · stoppage · Jun 25, 1996 · N3192E · Slnsby T67M260 · Engine (Reciprocating)
  > ENGINE STOPPED. DURING TRAFFIC PATTERN STALL MANEUVERS WITH THE ENGINE AT APPROXIMATELY IDLE. STARTER WAS ENGAGED FOR A SUCCESSFUL RESTART. DURING LANDING THE ENGINE STALLED AGAIN, NO RESTART WAS ATTEMPTED. AIRCRAFT LANDED WITHOUT INCIDENT. ALL OTHER INDI
- [SDR 96ZZZX3001](https://openairdocs.org/sdr/96ZZZX3001.md): Cooler · leak · May 28, 1996 · N3192F · Slnsby T67M260 · Engine Oil Cooler
  > AFTER FIRST FLIGHT OF THE DAY, AIR CREW NOTICED OIL ON WING WALK. COWLING WAS REMOVED AND OIL WAS SEEN DRIPPING FROM OIL COOLER FINS. REMOVED AND REPLACED OIL COOLER.
- [SDR 96ZZZX2985](https://openairdocs.org/sdr/96ZZZX2985.md): Blower Motor · failed · May 20, 1996 · Slnsby T67M260 · Cabin Cooling System
  > SUBMITTER REPORTS SEVERAL CONDENSER BLOWER MOTORS QUIT. SEVEN INSPECTED MOTORS FOUND BRUSHES COMPLETELY WORN. SUBMITTER STATES NO RECOMMENDATIONS AT THIS TIME. (ALL HAVE HAD LESS THAN 100 HRS, TT).
- [SDR 96ZZZX3811](https://openairdocs.org/sdr/96ZZZX3811.md): Engine · stoppage · May 15, 1996 · N3193K · Slnsby T67M260 · Engine (Reciprocating)
  > ENGINE STOPPED AFTER PILOT REDUCED POWER IN SPIN. SUCCESSFUL RESTART AND RETURN TO BASE WITHOUT FURTHER INCIDENT. ALL INDICATIONS NORMAL. USAF CONDUCTING INVESTIGATION. MAINTENANCE IS IN PROCESS OF COMPLETING ENGINE STOPPAGE CHECK LIST. AIRCRAFT HAS 101.9
- [SDR 96ZZZX3808](https://openairdocs.org/sdr/96ZZZX3808.md): Engine · stoppage · May 10, 1996 · N3037C · Slnsby T67M260 · Engine (Reciprocating)
  > ENGINE STOPPED DURING AEROBATIC MANEUVER. SUCCESSFUL RESTART AND RETURN TO BASE WITHOUT FURTHER INCIDENT. ALL INDICATIONS NORMAL. PRELIMINARY ASSESSMENT IS THAT AIRCRAFT WAS PUT IN CONDITION KNOWN TO INDUCE ENGINE STOPPAGE.
- [SDR 96ZZZX2887](https://openairdocs.org/sdr/96ZZZX2887.md): Engine · failed · May 1, 1996 · N3193K · Slnsby T67M260 · Engine (Reciprocating)
  > ENGINE STOPPED IN-FLIGHT AFTER POWER REDUCTION IN SPIN DURING POWER ON OF THE SPIN DEMONSTRATION SORTIE. ENGINE RESTARTED WITH START BUTTON.
- [SDR 96ZZZX3809](https://openairdocs.org/sdr/96ZZZX3809.md): Sender · failed · Apr 25, 1996 · N3037X · Slnsby T67M260 · Engine Oil Pressure
  > PILOT MADE AN EMERGENCY LANDING AT A SMALL AIRSTRIP. THE PILOT REPORTED LOW OIL PRESSURE AND RAISING OIL TEMPERATURE. A DOSS MAINTENANCE TEAM WAS SENT TO THE AIRSTRIP TO RECOVER THE AIRCRAFT. THE MAINTENANCE PERSONNEL REMOVED AND REPLACED THE OIL PRESSURE SE
- [SDR CA960222039](https://openairdocs.org/sdr/CA960222039.md): Control Cable · frayed · Feb 13, 1996 · Slnsby T67M260 · Rudder Control System
  > (CAN)THE NEW CABLES WERE INSPECTED UNDER THE INSPECTION SCHEDULE OF 500 HOURS OR 12 MONTHS WHICHEVER COMES FIRST AS DIRECTED IN SERVICE BULLETIN 78. THE TWO AIRCRAFT INSPECTED HAD ONE FRAYED CABLE EACH. RE FERENCE ADDITIOINAL SDR 960222016. CANADA REVIEWING PO
- [SDR CA960222016](https://openairdocs.org/sdr/CA960222016.md): Cable · frayed · Feb 13, 1996 · Slnsby T67M260 · Rudder Control System
  > (CAN)THE NEW CABLES WERE INSPECTED UNDER THE INSPECATION SCHEDULE OF 500 HOURS OR 12 MONTHS WHICHEVER COMES FIRST AS DIRECTED IN SERVICE BULLETIN 78. THE TWO AIRCRAFT INSPECTED HAD ONE FRAYED CABLE EACH. R EFERENCE ADDITIONAL SDR 96022039. CANADA REVIEWING POS
- [SDR 95ZZZX7029](https://openairdocs.org/sdr/95ZZZX7029.md): Hose · detached · Nov 30, 1995 · N31880 · Slnsby T67M260 · Engine Oil Distribution (Airframe Furnished)
  > PARTIAL ENGINE FAILURE, RPM DROPPED FROM 2700 RPM TO 2100 RPM AND BACK TO 27 RPM FOLLOWED BY LOSS OF OIL PRESSURE. ENGINE RAN FOR APPROXIMATELY 4 TO 5 MINUTES WITH VIBRATIONS AND DETERIORATING POWER LOSS FOLLOWED BY TOTAL POWER LOSS. ACFT LANDED SAFELY. INS
- [SDR 95ZZZX6608](https://openairdocs.org/sdr/95ZZZX6608.md): Canopy · failed · Oct 18, 1995 · N3047K · Slnsby T67M260 · Flight Compartment Windows
  > EIGHTEEN MINUTES INTO FLIGHT THE CANOPY OPENED AND SHATTERED. OTHER THAN CANOPY, VERY MINOR DAMAGE DONE TO AIRFRAME. 15MM HOLE - STAB, RT SIDE TOP. 15MM HOLE - ELEV RT SIDE TOP. 10MM SCRATCH RT SIDE, MID-RUDDER CANOPY DECK FAIRING CHIPPED. AIRFRAME CHIPPE
- [SDR 95ZZZX6005](https://openairdocs.org/sdr/95ZZZX6005.md): Alternator · defective · Oct 5, 1995 · N3190H · Slnsby T67M260 · DC Generator-Alternator
  > ALTERNATOR LIGHT CAME ON DURING FLIGHT. TESTED AND FOUND DEFECTIVE.
- [SDR 95ZZZX6004](https://openairdocs.org/sdr/95ZZZX6004.md): Alternator · defective · Oct 5, 1995 · N3189W · Slnsby T67M260 · DC Generator-Alternator
  > ALTERNATOR LIGHT CAME ON DURING FLIGHT. TESTED AND FOUND DEFECTIVE.
- [SDR 95ZZZX6003](https://openairdocs.org/sdr/95ZZZX6003.md): Aternator · defective · Oct 5, 1995 · N3189K · Slnsby T67M260 · DC Generator-Alternator
  > ALTERNATOR LIGHT CAME ON DURING FLIGHT. TESTED ALTERNATOR AND FOUND TO BE DEFECTIVE.
- [SDR 95ZZZX6002](https://openairdocs.org/sdr/95ZZZX6002.md): Vent Line · fuel fumes · Sep 28, 1995 · N3037T · Slnsby T67M260 · Aircraft Fuel Distribution System
  > AIR CREW REPORTED A STRONG SMELL OF FUEL WHEN FULL POWER WAS SET FOR TAKEOFF. FUEL TANK VENT LINES ARE ROUTED IN COCKPIT AND OUT THROUGH BELLY OF AIRCRAFT. SUSPECT FUEL FUMES COMING IN FROM AROUND VENT LINES.
- [SDR 95ZZZX6001](https://openairdocs.org/sdr/95ZZZX6001.md): Vent Line · fuel fumes · Sep 28, 1995 · N3047K · Slnsby T67M260 · Aircraft Fuel Distribution System
  > AIR CREW REPORTED A STRONG SMELL OF FUEL WHEN FULL POWER WAS SET FOR TAKEOFF. FUEL TANK VENT LINES ARE ROUTED IN COCKPIT AND OUT THROUGH BELLY OF AIRCRAFT. SUSPECT FUEL FUMES COMING IN FROM AROUND VENT LINES.
- [SDR 95ZZZX5944](https://openairdocs.org/sdr/95ZZZX5944.md): Muffler · chafed · Sep 1, 1995 · N3154Z · Slnsby T67M260 · Engine Noise Suppressor
  > THE MUFFLER TAILPIPE IS CHAFING ON THE FIREWALL. A WEAR SPOT WAS FOUND ON INSPECTION. THE ENGINE WAS GROUND RUN AT OPERATING TEMPERATURE WHICH CAUSED THE MUFFLER TAILPIPE TO EXPAND UP TO 13 MM CAUSING IT TO TOUCH FIREWALL AT FRAME NR 1. SUBMITTER RECOMMENDS
- [SDR 95ZZZX5943](https://openairdocs.org/sdr/95ZZZX5943.md): Muffler · chafed · Sep 1, 1995 · N3004H · Slnsby T67M260 · Engine Noise Suppressor
  > THE MUFFLER TAILPIPE IS CHAFING ON THE FIREWALL. A WEAR SPOT WAS FOUND ON INSPECTION. THE ENGINE WAS GROUND RUN AT AN OPERATING TEMPERATURE WHICH CAUSED THE MUFFLER TAILPIPE TO EXPAND UP TO 13 MM CAUSING IT TO TOUCH FIREWALL AT FRAME NR 1. SUBMITTER RECOMME
- [SDR 95ZZZX4557](https://openairdocs.org/sdr/95ZZZX4557.md): Valve · loose nut · Aug 23, 1995 · N3094T · Slnsby T67M260 · Engine Oil Temperature Regulator
  > AIRCRAFT DEVELOPED HIGH OIL TEMPERATURE (120 DEGREES CELSIUS) AND LOW OIL PRESSURE (60 PSI) DURING ROUTINE TRAINING MISSION. SEVERAL AIRCRAFT IN THE FLEET HAD SIMILAR PROBLEMS WHICH WERE RESOLVED BY CHANGING DEFECTIVE THERMOSTATIC BYPASS VALVES. WHEN THIS VA
- [SDR 95ZZZX4558](https://openairdocs.org/sdr/95ZZZX4558.md): Valve · malfunctioning · Aug 21, 1995 · N3079Q · Slnsby T67M260 · Engine Oil Temperature Regulator
  > AIRCRAFT DEVELOPED HIGH OIL TEMPERATURE (120 DEGREES CELSIUS) AND LOW OIL PRESSURE (60 PSI) DURING A ROUTINE TRAINING MISSION. OUTSIDE AIR TEMPERATURE WAS ABOVE 80 DEGREES FAHRENHEIT. AIRCRAFT PILOT MADE ATTEMPT TO COOL ENGINE DURING RETURN FLIGHT TO THE AIR
- [SDR 95ZZZX4483](https://openairdocs.org/sdr/95ZZZX4483.md): Sensor · defective · Aug 15, 1995 · N3037T · Slnsby T67M260 · Engine Oil Pressure
  > OIL PRESSURE SENDING UNIT FAILING TO GIVE CORRECT READINGS. SUBMITTER RECOMMENDS TRYING A DIFFERENT MANUFACTURER. SLINGSBY IPC, CHAPTER 55, FIGURE 5, ITEM NR 3.
- [SDR 95ZZZX4482](https://openairdocs.org/sdr/95ZZZX4482.md): Control Cable · frayed · Aug 15, 1995 · N7020D · Slnsby T67M260 · Rudder Control System
  > DURING AN ANNUAL INSPECTION, THE RT RUDDER CABLE WAS FOUND FRAYED BY AFT PULLEY. FRAYED AREA RUNS BACK AND FORTH ON PULLEY. NO RECOMMENDATION AT THIS TIME. SLINGSBY IPC, CHAPTER 19, FIGURE 9, ITEM NR 24.
- [SDR 95ZZZX4556](https://openairdocs.org/sdr/95ZZZX4556.md): Valve · malfunctioning · Aug 7, 1995 · N3064Q · Slnsby T67M260 · Engine Oil Temperature Regulator
  > AIRCRAFT DEVELOPED HIGH OIL TEMPERATURE (120 DEGREES CELSIUS) AND LOW OIL PRESSURE (60 PSI) DURING A ROUTINE TRAINING MISSION. OUTSIDE AIR TEMPERATURE WAS ABOVE 80 DEGREES FAHRENHEIT. AIRCRAFT PILOT MADE ATTEMPT TO COOL ENGINE DURING THE RETURN FLIGHT TO AIR
- [SDR 95ZZZX4555](https://openairdocs.org/sdr/95ZZZX4555.md): Valve · malfunctioning · Aug 7, 1995 · N3107K · Slnsby T67M260 · Engine Oil Temperature Regulator
  > AIRCRAFT DEVELOPED HIGH OIL TEMPERATURE (120 DEGREES CELSIUS) AND LOW OIL PRESSURE (60 PSI) DURING A ROUTINE TRAINING MISSION. OUTSIDE AIR TEMPERATURE WAS ABOVE 80 DEGREES FAHRENHEIT. AIRCRAFT PILOT MADE AN ATTEMPT TO COOL ENGINE DURING RETURN FLIGHT TO AIRF
- [SDR 95ZZZX4494](https://openairdocs.org/sdr/95ZZZX4494.md): Sensor · defective · Aug 1, 1995 · N7020D · Slnsby T67M260 · Engine Oil Pressure
  > OIL PRESSURE SENDING UNIT GIVES FALSE READINGS ON INSTRUMENT GAUGE. READINGS ARE ALSO DIFFERENT WHEN TESTING WHILE UNIT IS OFF THE ENGINE. SUBMITTER RECOMMENDS TRYING A DIFFERENT TYPE OIL PRESSURE SENDING UNIT.
- [SDR 95ZZZX3272](https://openairdocs.org/sdr/95ZZZX3272.md): Skin · debonded · Jun 23, 1995 · N3037H · Slnsby T67M260 · Wing, Plate/Skin
  > A ONE-TIME INSPECTION FOUND LT AND RT WING SKIN DEBONDING FROM NR 2 RIB, 31 INCHES FROM CENTER LINE.
- [SDR 95ZZZX3271](https://openairdocs.org/sdr/95ZZZX3271.md): Skin · debonded · Jun 23, 1995 · N3037H · Slnsby T67M260 · Wing, Plate/Skin
  > A ONE-TIME INSPECTION FOUND LT AND RT WING SKIN DEBONDING FROM NR 2 RIB, 31 INCHES FROM CENTER LINE.

Next page: https://openairdocs.org/model/slingsby-t67m-260/reports.md?page=2

## 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 = 'T67M260'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/slingsby-t67m-260/reports

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