# Service difficulty reports: Lycoming T5317A

A list on [Lycoming T5317A](https://openairdocs.org/engine/lycoming-t5317a.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 91 reports

- [SDR CA150818010](https://openairdocs.org/sdr/CA150818010.md): Shaft · sheared · Aug 14, 2015 · Bell 212 · Windshield/Door Rain/Ice Removal
  > (CAN) SHAFT SHEARED DURING FLIGHT. MOTOR ASSEMBLY REPLACED.
- [SDR CA150713024](https://openairdocs.org/sdr/CA150713024.md): Hydraulic Line · ruptured · Jul 11, 2015 · Bell 205A1 · Hydraulic System, Main
  > (CAN) DURING FLIGHT THE PILOT EXPERIENCED A LOSS OF NR 2 HYD PRESS. PILOT RETURN TO THE BASE AFTER ISOLATING THE SYS. ONCE THE ACFT LANDED SAFELY, THE INVESTIGATION REVEALED THE LINE TO THE PRESS SIDE OF HYD PUMP NR 2 HAD RUPTURED AT THE 90 DEGREE FITTING.
- [SDR CA150316004](https://openairdocs.org/sdr/CA150316004.md): Blade · cracked · Mar 15, 2015 · Bell 205A1 · Turbine Engine Compressor Section
  > (CAN) DURING INSPECTION OF ACFT BLOWER FAN, IT WAS NOTED THAT 4 OF THE FAN BLADES WERE CRACKED AT THE BASE.
- [SDR CA150225006](https://openairdocs.org/sdr/CA150225006.md): Shield · leaking · Feb 23, 2015 · Bell 205A1 · Tail Rotor Drive System
  > (CAN) DURING DAILY INSPECTION, NOTICED THAT THE HANGER BEARING ASSEMBLY GREASE SHIELD WAS LEAKING. UNIT WAS REPLACED WITH SERVICEABLE, GND RUN CARRIED OUT & NO FURTHER FAULTS. ACFT RELEASED.
- [SDR CA131009002](https://openairdocs.org/sdr/CA131009002.md): Blade · separated · Aug 24, 2013 · Bell 205A1 · Tail Rotor Blades
  > (CAN) A SUDDEN MEDIUM FREQUENCY VIBRATION WAS FELT IN FLIGHT. A PRECAUTIONARY LANDING WAS CARRIED OUT. AFTER VISUAL INSPECTION, IT WAS DISCOVERED THAT THE TIP CAP FILLER HAD SEPARATED CAUSING THE VIBRATION. BOTH BLADES WERE REPLACED, THE TAIL ROTOR WAS BALA
- [SDR CA130705006](https://openairdocs.org/sdr/CA130705006.md): Fitting · cracked · Jul 3, 2013 · Bell 205A1 · Tail Rotor Drive Shaft
  > (CAN) AME WAS PERFORMING POST FLIGHT/DAILY INSPECTION FOLLOWING LAST FLIGHT OF DAY. DURING INSPECTION, A SMALL VERTICAL LINE WAS NOTED ON THE LT LUG OF THE FITTING THROUGH WHICH THE BOLT SECURING THE TAIL ROTOR DRIVE SHAFT FLEXIBLE COUPLING ASSY TO THE F1TTING
- [SDR CA130116020](https://openairdocs.org/sdr/CA130116020.md): Panel · inoperative · Jan 16, 2013 · Kaman K1200 · Instrument Panel
  > (CAN) DURING TROUBLESHOOTING OF THE FUEL QTY INDICATING SYS FOR A CALIBRATION DEFECT. THE ACFT WAS SUBSEQUENTLY DEFUELED AND THE AME NOTICED THAT THERE WAS NO LOW FUEL LIGHT INDICATION ON THE MASTER CAUTION PANEL. THE PRESS TO TEST FUNCTION FOR THE FUEL LOW L
- [SDR CA121206010](https://openairdocs.org/sdr/CA121206010.md): Mount · loose · Dec 3, 2012 · Bell 212 · Engine Mount Section
  > (CAN) FOUND DURING INSPECTION, THAT ATTACHMENT BOLTS, HAD COME LOOSE. THE INSPECTION WAS CARRIED OUT IAW INSTRUCTIONS FOR AIRWORTHINESS STC SH08-8. ALSO, THE HOLES HAD ELONGATED CAUSING THE FITTING TO MOVE INSIDE THE STRUT ASSEMBLY. MFG DART AEROSPACE, WAS N
- [SDR CA120817001](https://openairdocs.org/sdr/CA120817001.md): Longeron · cracked · Aug 7, 2012 · Bell 205A1 · Fuselage Main, Longeron/Stringer
  > (CAN) TOP LT LONGERON ON ACFT LOCATED IN AFT COMPARTMENT WAS CRACKED BEHIND DOUBLER ON TOP LT TAILBOOM ATTACHMENT. CRACK WAS FOUND DURING DAILY INSPECTION, MACHINE WAS FLOWN TO ACFT SERVICE CENTER WERE LONGERON WAS REPLACED.
- [SDR CA120817004](https://openairdocs.org/sdr/CA120817004.md): Tachometer · failed · Jun 6, 2012 · Bell 205A1 · Engine RPM Indicating System
  > (CAN) CO-PILOT DUAL TACH N2 ENGINE RPM NEEDLE, FLUCUATES FROM 0 TO 50 PERCENT THEN STICKS.
- [SDR CA120223006](https://openairdocs.org/sdr/CA120223006.md): Cap · fractured · Jan 28, 2012 · Bell 205A1 · Rotorcraft Tail Boom
  > (CAN) FAILURE OF CAP, IN ORDER TO EXAMINE THE FRACTURE SURFACE OF A STRUCTURAL LONGERON, HERE-IN REFERRED TO AS A CAP. THE CAP, PN 205-030-207-005 AND THE ASSOCIATED TAILBOOM ATTACHMENT FITTING, PN 205-030-767-005, WERE SUBSEQUENTLY SENT TO FOR EXAMINATION AND
- [SDR CA120116003](https://openairdocs.org/sdr/CA120116003.md): Gimbal Ring · damaged · Jan 16, 2012 · Bell 205A1 · Main Rotor Mast/Swashplate
  > (CAN) DURING 100 HRS INSPECTION, 2 SMALL DAMAGED SCREWS WHERE FOUND IN THE BOTTOM OF THE MAIN TRANSMISSION BAY STILL ATTACHED WITH LOCKING WIRE. FURTHER INSPECTION REVEALED THAT THE SCREW BELONGED TO 1 OF THE 4 SWASHPLATE GIMBAL RING ATTACHEMENT POINTS. SWAS
- [SDR CA111220005](https://openairdocs.org/sdr/CA111220005.md): Blade · cracked · Dec 20, 2011 · Bell 205A1 · Main Rotor Blades
  > (CAN) 3 CRACKS DEVELOPED ON BOTTOM SIDE OF BLADE SKIN, PN 212-015-501-115, SN A6009 (TSN) 3521.9, 1 CRACK 5.5", THE OTHER 2 CRACKS ARE 2.5" - 3.5" RESPECTIVELY. MEASURING FROM TRIM TAB EDGE INBD 41.5" IS THE LONG, 5.5. THE OTHER 2 CRACKS ARE OTBD A FEW INCHE
- [SDR CA110909011](https://openairdocs.org/sdr/CA110909011.md): Governor · failed · Aug 14, 2011 · Bell 205A1 · Turbine Governor
  > (CAN) ACFT LEVELED OFF AFTER CLIMB, A BANG WAS HEARD THEN ACFT YAWED, ROTOR LOW HORN AND LIGHT SOUNDED. ENGINE FAILURE WAS CONFIRMED- N1 WAS AT 25 PERCENT AND TORQUE WAS READING 0. ACFT AUTOROTATED TO GROUND. FUEL CELLS AND AIRFRAME FILTER ON BOARD INSPECTE
- [SDR CA111222011](https://openairdocs.org/sdr/CA111222011.md): Diffuser · used · Mar 6, 2011 · Bell 205A1 · Engine Collector/Tailpipe/Nozzle
  > (CAN) UPON LANDING AND PERFORMING A POST FLIGHT VISUAL INSPECTION THE AME FOUND THE BOTTOM STRUT ON THE EXHAUST DIFFUSER CRACKED WITH A SECTION OF MATERIAL MISSING. THE EXHAUST DIFFUSER SERVES AS THE REAR BEARING SUPPORT. AS A RESULT OF THIS DEFECT THE POWER
- [SDR CA101122028](https://openairdocs.org/sdr/CA101122028.md): Baffle · detached · Nov 22, 2010 · Bell 205A1 · Fuel Storage
  > BAFFLE DIVIDING FORWARD AND AFT SECTIONS OF FUEL CELL, FOUND DETACHED. FUEL IS ABLE TO MOVE AROUND POTENTIALLY CAUSING C OF G ISSUES. IN LOW FUEL SITUATIONS, SLOSHING FUEL MAY CAUSE SUPPLY TO THE PUMPS TO DIMINISH, POTENTIALLY CAUSING ENGINE FUEL STARVATION.
- [SDR CA090806005](https://openairdocs.org/sdr/CA090806005.md): Governor · unknown · Jul 30, 2009 · Bell 205A1 · Turbine Governor
  > EXCESSIVE ENGINE DROOP.
- [SDR CA090702013](https://openairdocs.org/sdr/CA090702013.md): Fitting · cracked · Jul 1, 2009 · Bell 205A1 · Tail Rotor Drive System
  > DURING A POST FLIGHT INSP, THE TAIL ROTOR DRIVE FITTING WAS FOUND CRACKED. TIME ON THE FITTING IS UNKNOWN. CRACK WAS FOUND RADIATING FROM THE BORE OF THE BARREL NUT ATTACHMENT. UNSURE IT THIS MAYBE THE CAUSE OF OVER TORQUING OF THE BOLT. NUT WAS REPLACED W
- [SDR CA090619003](https://openairdocs.org/sdr/CA090619003.md): Quill Assy · sheared · Jun 16, 2009 · Bell 205A1 · Starter-Generator
  > ACFT WOULD NOT START, UPON FURTHER INVESTIGATION THE QUILL DRIVE FROM STARTER/GENERATOR TO ENGINE FOUND SHEARED.
- [SDR CA090126003](https://openairdocs.org/sdr/CA090126003.md): O-Ring · leaking · Jan 25, 2009 · Bell 205A1 · Fuel Boost Pump
  > (CAN) REPORTS OF A LOW FUEL CAUTION LIGHT COMING ON EARLY AND SMALL FUEL DRIP PROMPTED MX TO REMOVE THE LT FUEL CELL SUMP PLATE TO INSPECT THE LOW LEVEL FUEL SWITCH/BOOST PUMP AREA AND FACILITATE AN O-RING REPLACEMENT. UPON REMOVAL OF THE SUMP PLATE A T-SHIRT/
- [SDR CA081120004](https://openairdocs.org/sdr/CA081120004.md): Mount · cracked · Nov 16, 2008 · Kaman K1200 · Main Rotor Head
  > (CAN) CRACK DISCOVERED ON LT FWD STRUT MOUNT FITTING.
- [SDR CA080731002](https://openairdocs.org/sdr/CA080731002.md): Bearing · rough · Jul 29, 2008 · Bell 205A1 · Main Rotor Gearbox
  > (CAN) UPON A SCHEDULED INSPECTION OF THE TRANSMISSION WAFFER FILTER AN EXCESSIVE AMOUNT OF FERROUS METAL WAS FOUND. THERE HAD BEEN NO METAL FOUND ON THE CHIP DETECTOR OR IN THE COURSE INLET SCREEN. A SWEEP OF THE SUMP WITH A MAGNET FOUND NO METAL. AFTER DISSAS
- [SDR CA081023005](https://openairdocs.org/sdr/CA081023005.md): Fitting · cracked · Jul 27, 2008 · Bell 205A1 · Rotorcraft Tail Boom
  > (CAN) WHILE CONDUCTING 100 HR INSP NOTED AREA IN LT LOWER TAIL BOOM LONGERON AT FWD FITTING TO BE CRACKED. NDT CONFIRMED A CRACK INDCATION OF 1.5 INCHES LONG IN THE FITTING.
- [SDR CA080604011](https://openairdocs.org/sdr/CA080604011.md): Attach Fitting · cracked · May 28, 2008 · Bell 205A1 · Fuselage Main, Attach Fittings
  > (CAN) WHILE CONDUCTING A 25 HR INSP, A CRACK WAS NOTED ON THE LIFT LINK BEAM LUG. THE PART WAS REMOVED AND TT OF THE BEAM IS UNKNOWN AT THIS TIME. CRACK WAS FOUND ON THE AFT EAR OF LUG RT SIDE.
- [SDR CA080326001](https://openairdocs.org/sdr/CA080326001.md): Wire · chafed · Mar 25, 2008 · Bell 205A1 · Engine Starting System Wiring
  > (CAN) DURING START UP THE STARTER RELAY CIRCUIT BREAKER WAS POPPING NOT ALLOWING THE STARTER TO START. IT WAS FOUND THAT THERE WERE 2 WIRES LABELED K2D20 AND K3C20 CHAFFED INSIDE THE CO-PILOTS COLLECTIVE. K3C20 HAD BEEN SOLDER SPLICED AND CHAFED AT THE SPLICE
- [SDR CA080117002](https://openairdocs.org/sdr/CA080117002.md): Bearing · unserviceable · Jan 17, 2008 · Bell 205A1 · Tail Rotor Head
  > (CAN) FOUND TAIL ROTOR HUB ASSY OB BEARING CAGE INSERT OUT OF IS SOCKET. ASSY SEND FOR O/H. (TC NR 20080117002)
- [SDR CA080124003](https://openairdocs.org/sdr/CA080124003.md): Crosstube · cracked · Jan 17, 2008 · Bell 205A1 · Main Landing Gear
  > (CAN) WHILE THE ENGINEER WAS CONDUCTING THE DI, A CRACK IN THE AFT DART CROSSTUBE WAS DISCOVERED. THE DART CROSSTUBE FOLLOWS 300/600 HR INSP CYCLE. CROSSTUBE WAS 60.7 FROM 300 HR INSP, AND 360.7 FROM THE 600 HR. CROSSTUBE WAS CHECKED FOR EXCESSIVE DEFLECTION,
- [SDR CA071214009](https://openairdocs.org/sdr/CA071214009.md): Mount · cracked · Dec 10, 2007 · Bell 205A1 · Engine Mount Section
  > (CAN) RT ENGINE BIPOD INSPECTED FOR SUSPICIOUS CRACK IN FRONT TUBING DURING 100 HRS INSPECTION. NDT REVEALED CRACK MOUNT AT WELDED JOINT. NOTE: THIS MOUNT WAS MODIFIED IAW STC SH99-11, DART ADJUSTABLE MOUNT. (TC NR 20071214009)
- [SDR CA071127011](https://openairdocs.org/sdr/CA071127011.md): Fitting · cracked · Nov 5, 2007 · Bell 205A1 · Main Rotor Gearbox
  > (CAN) ON ROUTINE INSPECTION, A CRACK WAS NOTED IN THE LIFT LINK FITTING. TRANSMISSION WAS REMOVED AND SENT FOR REPAIR. THE TSO FOR THE COMPLETE TRANSMISSION WAS AT 785.1 AND TT 19803.1. NO AVAILABLE INFORMATION FOR TT ON THE SUMP ASSY CASE. (TC NR 20071127011)
- [SDR CA070724005](https://openairdocs.org/sdr/CA070724005.md): Control Lever · broken · Jul 23, 2007 · Bell 205A1 · Turbine Governor
  > (CAN) THIS IS THE INITIAL REPORT. INFORMATION NOT HERE YET. THE PILOT COULD ONLY GET 92 PERCENT NR RP, LANDED THE AIRCRAFT NO INCIDENT, AFTER SHUTDOWN THE ENGINEER OPENED THE GOVERNOR SIDE ENGINE COWLING AND FOUND THE THE GOVERNOR LEVER BROKEN BOTH ENDS OF THE
- [SDR CA070807005](https://openairdocs.org/sdr/CA070807005.md): Connector · burned · Jul 17, 2007 · Bell 205A1 · Communications System Wiring
  > (CAN) TRAINING FLIGHT, NOTICED SMOKE COMING UP FROM CENTER CONSOLE BEHIND VHF NR 2 RADIO. PUT DOWN, A/C ON GROUND. CO-PILOT JUMPED OUT TO CHECK IN BATT COMPARTMENT. NO ANOMALIES FOUND. FORCE TRIM CB POPPED. CARGO RELEASE LIGHT CAME ON AND STAYED ON. VHF RADI
- [SDR CA070524001](https://openairdocs.org/sdr/CA070524001.md): Pump · failed · May 17, 2007 · Bell 205A1 · Engine Fuel Pump
  > (CAN) DURING HELI-PORTABLE SEISMIC DRILLING OPERATIONS, UPON DESCENT WITH AN EXTERNAL LOAD: THE MASTER CAUTION WARNING INDICATION WAS ILLUMINATED. THE LOAD WAS SET AND RELEASED. THE CAUTION PANEL OBSERVED TO REVEAL THAT THE ENGINE DRIVEN FUEL PUMP WARNING LIG
- [SDR CA070412004](https://openairdocs.org/sdr/CA070412004.md): Governor · damaged · Mar 30, 2007 · Bell 205A1 · Turbine Governor
  > (CAN) DURING THE DAILY INSPECTION PERFORMED BY THE ENGINEER, THE SCREW HOLDING THE GOV SERVO LEVER PLATE IN PLACE WAS ENTIRELY BACKED OUT OF THE HOLE. THIS PART HAD BEEN REPLACED, TESTED AND ADJUSTED AT TSN 2346.3 FOR LOOSE SCREWS. THE SCREWS ARE STAKED IN P
- [SDR CA070418003](https://openairdocs.org/sdr/CA070418003.md): Mount · cracked · Mar 21, 2007 · Bell 205A1 · Engine Mount Section
  > (CAN) ENGINE MOUNT WAS INSTALLED NEW IAW STC SH99-11. POWER PLANT WAS ALIGNED IAW MM SUPPLEMENT. THE MM SUPPLEMENT INCLUDES AN INSP EVERY 100 HRS OR ANNUALLY. NOTE TO INSPECT ENGINE MOUNTS FOR CRACKS, DAMAGE, CORROSION AND SECURITY. THE CRACK STARTED BELOW TH
- [SDR CA061222004](https://openairdocs.org/sdr/CA061222004.md): Nut · cracked · Dec 4, 2006 · Bell 205B · Main Rotor Head
  > (CAN) THE ACORN NUTS WERE SENT OUT FOR NDT IAW THE REQUIREMENT OF THE OVERHAUL OF THE M/R HEAD ASSY. THE NDT SHOP FOUND A CRACK DEVELOPING NEAR THE BASE IN THE TRANSITION AREA OR CURL OF THE DOME AND THE GEAR PART OF THE ACORN NUTS. THE ESTIMATED TIME ON THE
- [SDR CA060907005](https://openairdocs.org/sdr/CA060907005.md): Actuator · failed · Aug 30, 2006 · Bell 205A1 · Rotorcraft Servo System
  > (CAN) DURING LONG LINE SLINGING OPERATIONS, UPON APPROACHING A DROP ZONE WITH A LOAD. THE COLLECTIVE WAS RAISED TO CUSHION LANDING OF THE LOAD, THEN LOWERED TO TAKE TENSION OFF OF THE LINE. THE HELICOPTER TURNED TO THE LT AND THE RT TAIL ROTOR PEDAL WAS FOUND
- [SDR CA060727001](https://openairdocs.org/sdr/CA060727001.md): Nut · cracked · Jul 27, 2006 · Bell 205A1 · Main Rotor Head
  > (CAN) THIS IS AN ON CONDITION ITEM. SO HISTORY MAY NOT BE ACCURATE. M/R HUB ASSY HAS 18437.6 TIME SINCE NEW. M/R HEAD ASSY WAS IN FOR O/H AND REQUIRES ACORN NUTS TO BE NDT. THIS ONE WAS FOUND CRACKED. (TC NR 20060727001)
- [SDR CA060602004](https://openairdocs.org/sdr/CA060602004.md): Drag Brace · cracked · May 29, 2006 · Bell 205A1 · Main Rotor Head
  > (CAN) THE DRAG BRACE WAS IN THE COMPONENT SHOP GETTING ITS 1200 HR INSPECTION/24 MONTH INSPECTION. THE DRAG BRACE ASSEMBLY WAS PREPARED FOR NDT MAGNETIC PARTICLE INSPECTION. THE NDT SHOP FOUND THIS FITTING WAS CRACKED ON THE IB CURVE. (TC NR 20060602004)
- [SDR CA060524001](https://openairdocs.org/sdr/CA060524001.md): Fitting · cracked · May 19, 2006 · Bell 205A1 · Main Rotor Gearbox
  > AIRCRAFT WAS ON SEISMIC DRILL MOVE JOB. THE ENGINEER WAS DOING HIS DAILY INSPECTION WHEN NOTICED THAT ONE EAR OF THE LIFT LINK FITTING WAS APPEARED CRACKED. A CLOSER VISUAL LOOK CONFIRMED IT WAS CRACKED. INVESTIGATING IF THE BUSHING WAS WRONG FOR THIS INST
- [SDR CA060331005](https://openairdocs.org/sdr/CA060331005.md): Saddle · cracked · Mar 27, 2006 · Bell 205A1 · Wheel/Ski/Float
  > CRACK WAS FOUND ON SKID TUBE AT FORWARD CROSSTUBE MOUNTING SADDLE. THERE WAS NO REPORT OF A HARD LANDING WITH THIS AIRCRAFT AT THIS TIME. TIMES FOR THESE SKID TUBES WERE NOT AVAILABLE.
- [SDR CA050816005](https://openairdocs.org/sdr/CA050816005.md): Mount · cracked · Aug 12, 2005 · Bell 205A1 · Engine Mount Section
  > (CAN) THE ENGINE MOUNT WAS MODIFIED BY STC SH99-11 WHICH ALLOWS THE MOUNT TO BECOME ADJUSTABLE. THE ADJUSTABLE PORTION OF THE MOUNT IS RIVETED TO ONE LEG AND IT CRACKED FROM ONE OF RIVET HOLES SECURING THE ADJUSTABLE TURN BARREL TO THE MOUNT LEG.
- [SDR CA050816006](https://openairdocs.org/sdr/CA050816006.md): Mount · cracked · Aug 12, 2005 · Bell 205A1 · Engine Mount Section
  > (CAN) THE ENGINE MOUNT WAS MODIFIED BY STC SH99-11 WHICH ALLOWS THE MOUNT TO BECOME ADJUSTABLE. THE ADJUSTABLE PORTION OF THE MOUNT IS RIVETED TO ONE LEG AND IT CRACKED FROM ONE OF RIVET HOLES SECURING THE ADJUSTABLE TURNBARREL TO THE MOUNT LEG.
- [SDR CA050707005](https://openairdocs.org/sdr/CA050707005.md): Hub · worn · Jun 24, 2005 · Kaman K1200 · Main Rotor Head
  > (CAN) DURING LAG PIN REPLACEMENT BLADE WAS REMOVED. UPON REMOVAL OF BLADE HUB WAS INSPECTED AND THE PROBLEM WAS FOUND. THE UPPER SURFACE OF THE LOWER HUB HALF KRON BEARING SURFACE WAS WORN THROUGH TO METAL IN APPROXIMATELY 1/5 OF ITS CIRCUMFERENCE. NO INSPE
- [SDR CA051115006](https://openairdocs.org/sdr/CA051115006.md): Structure · cracked · Jul 5, 2004 · Kaman K1200 · Cargo/Baggage Doors
  > ON MAINTENANCE SHUTDOWN DURING A NORMAL HELI LOGGING DAY, DURING INSP OF FLIGHT CONTROLS THE APPRENTICE NOTICED SOME SMOKING COMING FROM THE BOTTOM CORNER OF THE STBD OCTAGONAL CARGO DOOR. UPON FURTHER INSP IT WAS DETERMINED TO BE A CRACK.
- [SDR 2004FA0000423](https://openairdocs.org/sdr/2004FA0000423.md): Pin · unserviceable · Mar 25, 2004 · N358KA · Kaman K1200 · Main Rotor Head
  > THE LEADING EDGE OF THE LT SIDE TEETER PIN WAS DAMAGED (MUSHROOMED). FURTHER INSPECTION SHOWED THAT THE HEAD SIDE OF THE INSIDE DIAMETER OF THE LINER THAT THE TEETER PIN SITS IN IS ALSO DAMAGED. THE LINER IS DEFORMED AND PROTRUDES IN AN IRREGULAR MANNER ON T
- [SDR CA040127014](https://openairdocs.org/sdr/CA040127014.md): Pump · failed · Dec 28, 2003 · Bell 205A1 · Fuel Control/Reciprocating Engines
  > (CAN) WHILE HELICOPTER WAS CONDUCTING AERIAL LIFT WORK THE PILOT NOTED THE ENGINE FUEL PUMP LIGHT CAME ON. HE RETURNED TO THE STAGING AREA AND LANDED UNEVENTFULLY. THROUGH TROUBLESHOOTING ON THE GROUND IT WAS DISCOVERED THAT ONE ELEMENT OF A DUAL ELEMENT PUMP
- [SDR CA040128006](https://openairdocs.org/sdr/CA040128006.md): Pump · worn · Dec 28, 2003 · Bell 205A1 · Fuel Control/Reciprocating Engines
  > (CAN) FUEL CONTROL P/N 1-170-240-93, S/N 5ADS1907 WAS RECEIVED DUE TO DAMAGED MAIN DRIVE SHAFT SPLINE. DISASSEMBLED AND INSPECTED FCU AND FOUND DAMAGED PUMP ASSEMBLY. RECORD OF INSPECTION IAW SB73-39. FCU S 91 AND 93 HAVE TIP SEAL PUMP, AND THEY CAN BE INS
- [SDR AUS20031090](https://openairdocs.org/sdr/AUS20031090.md): Compressor · unserviceable · Oct 10, 2003 · Turbine Engine Compressor Section
  > (AUS) ENGINE COMPRESSOR SECTION CONTAINED COMPONENTS FROM AN ENGINE INVOLVED IN AN AIRCRAFT CRASH. ENGINE HAD BEEN ASSEMBLED FROM COMPONENTS FROM FIVE DIFFERENT ENGINES. NO HISTORY CARDS WERE SUPPLIED FOR THE COMPRESSOR MODULE BUT INVESTIGATION FOUND THAT THE
- [SDR CA040204006](https://openairdocs.org/sdr/CA040204006.md): Fuel Control · failed · Sep 11, 2003 · Bell 205A1 · Fuel Controlling System
  > (CAN) ENGINE STOPPED IN-FLIGHT.
- [SDR FZO2003F00000](https://openairdocs.org/sdr/FZO2003F00000.md): Drive Shaft · chafed · Jul 18, 2003 · N6288Y · Bell 205A1 · Tail Rotor Drive Shaft
  > PILOT FELT HARMONIC VIBRATION DURING REDUCE POWER DECENT INTO DIP SITE. FOUND T/R DRIVE SHAFT PN 204-040-623-011 RUBBING ON 205-060-923-001 BOOT ASSY. BOOT SEAL ECE-300-3/3 OIL SOAKED AND DEBONDED FROM BOOT LETTING BOOT SIDE. DOWN AND AMAKING CONTACT WITH T

Next page: https://openairdocs.org/engine/lycoming-t5317a/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 engine_model_key = 'T5317A'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/lycoming-t5317a/reports

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