# Service difficulty reports: Erickson S64E

A list on [Erickson S64E](https://openairdocs.org/model/erickson-s64e.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 3 · 145 reports

- [SDR JYDR20260203027](https://openairdocs.org/sdr/JYDR20260203027.md): Piston Rod · broken · Feb 3, 2026 · N173AC · Skrsky S64E · Main Rotor Head
  > AIRCRAFT HAD JUST SHUT DOWN FOR A 3HR BIM INSPECTION. (REQUIRED AD) MAINTENANCE PERSONAL NOTICED A DAMPER ASSEMBLY BROKEN AT THE ATTACHMENT TO THE HORIZONTAL HINGE PIN. THIS REPORT IS PRELIMINARY BECAUSE THIS REPAIR STATION HAS NOT YET RECIEVED THE MRH.
- [SDR JYDR20231019286](https://openairdocs.org/sdr/JYDR20231019286.md): Blade · broken · Oct 18, 2023 · Skrsky S64E · Turbine Section
  > AIRCRAFT WAS FIREFIGHTING WHEN PILOTS HEARD A LOW FREQUENCY RUMBLE. AIRCRAFT RETURNED TO BASE FOR TROUBLESHOOTING. AFTER TROUBLESHOOTING AMTS FOUND 1 EA. 2ND STAGE N1 BLADE HAD BROKEN OFF AT THE ROOT. ENGINE IS BEING RETURNED TO THIS REPAIR STATION FOR FURTHER
- [SDR JYDR20230607155](https://openairdocs.org/sdr/JYDR20230607155.md): Flange · broken · Jun 4, 2023 · Skrsky S64E · Main Landing Gear Attach Section
  > UPON RETURN TO SERVICE AT COMPLETION OF LOGGING CYCLE AT 250-FOOT HOVER (GRAPPLE PLACED ON GROUND) R/H MLG STRUT AND WHEEL ASSY DETACHED. THIS IS A PRELIMINARY REPORT TO MEET REPORTING REQUIREMENTS. ONCE MLG IS RECEIVED BY THIS REPAIR STATION AND ANALYZED REP
- [SDR JYDR20230413094](https://openairdocs.org/sdr/JYDR20230413094.md): Bevel Gear · cracked · Apr 12, 2023 · Skrsky S64E · Main Rotor Gearbox
  > MAIN GEAR BOX RECEIVED AT THIS REPAIR STATION FOR OVERHAUL. DURING THE OVERHAUL PROCESS THE MAIN BEVEL GEAR WAS FOUND TO HAVE A TOTAL OF 18 CRACKS. CRACKS FOUND BY MAGNETIC PARTIAL INSPECTION. THIS IS THE FIRST TIME THIS REPAIR STATION HAS FOUND CRACKS IN THIS
- [SDR JYDR20230125233](https://openairdocs.org/sdr/JYDR20230125233.md): Lock Tab · broken · Jan 25, 2023 · Skrsky S64E · Engine (Turbine/Turboprop)
  > AIRCRAFT HAD JUST LANDED WHEN ENGINE WENT HOT AND STOPPED. ENGINE REMOVED AND SENT TO THIS REPAIR STATION. UPON DISASSEMBLY OF ENGINE A 4TH STAGE TABLOCK HAD FAILED ALLOWING THE 4TH STAGE COMPRESSOR BLADE TO MOVE AND CAUSE DAMAGE TO THE REST OF THE ENGINE. DAM
- [SDR JYDR20220406093](https://openairdocs.org/sdr/JYDR20220406093.md): None · broken · Apr 4, 2022 · Skrsky S64E · Turbine Section
  > AIRCRAFT WAS ON FERRY FLIGHT WHEN PILOT NOTICED LOSS OF OIL PRESSURE ON NUMBER 2 ENGINE. LARGE AMOUNT OF OIL ON RIGHT SIDE OF AIRCRAFT. ENGINE SHUT DOWN IN FLIGHT AND AIRCRAFT WAS LANDED AT CLOSEST AIRPORT. UPON INSPECTION BY MAINTENANCE AN 2ND STAGE N1 BLADE
- [SDR JYDR20220214044](https://openairdocs.org/sdr/JYDR20220214044.md): Turbine Blades · broken · Feb 13, 2022 · Skrsky S64E · Turbine Section
  > AIRCRAFT WAS LOGGING. PILOTS FELT VIBRATION FROM #2 ENGINE AND RETURNED TO SERVICE LANDING. WHEN SHUT DOWN ENGINE CAME TO A SUDDEN STOP AND LOCKED UP. WHEN FREE TURBINE WAS SEPARATED, A 2ND STAGE N1 BLADE WAS FOUND TO BE BROKEN AT THE ROOT. ENGINE IS BEING SEN
- [SDR JYDR20220209040](https://openairdocs.org/sdr/JYDR20220209040.md): None · broken · Feb 9, 2022 · Skrsky S64E · Engine (Turbine/Turboprop)
  > ENGINE WAS AT REPAIR STATION FOR SCHEDULED OVERHAUL. UPON DISASSEMBLY 1 EACH TAB LOCK WAS FOUND BROKEN AT THE FORWARD SECTION. AFT SECTION OF TAB LOCK WAS STILL INSTALLED AND BLADE HAD NOT SHIFTED IN THE DISK SLOT. DOWN STREAM DAMAGE TO BLADES AND STATORS WAS
- [SDR JYDR20220120016](https://openairdocs.org/sdr/JYDR20220120016.md): None · broken · Jan 19, 2022 · Skrsky S64E · Engine/Transmission Coupling
  > WHILE LANDING FROM A HOVER, AS THE WHEELS TOUCHED DOWN A VIBRATION WAS FELT. PILOTS PULLED EACH ENGINE BACK SEPARATELY AND FOUND VIBRATION COMING FROM #2 ENGINE. AFTER AIRCRAFT SECURE MECHANICS FOUND A PIECE MISSING FROM #2 ENGINE TO MAIN GEAR BOX DRIVE SHAFT
- [SDR JYDR20210715194](https://openairdocs.org/sdr/JYDR20210715194.md): Engine · overtemp · Jul 14, 2021 · N154AC · Skrsky S64E · Engine (Turbine/Turboprop)
  > SHORT FINAL FOR WATER DROP. PILOT HEARD LOUD WOOSH SOUND FOLLOWED BY ROLLBACK CONDITIONS, 65% CHIME, 60% WARNING T5 RISING, N1 DROPPING. AIRCRAFT LANDED AT FIRST AVAILABLE LANDING AREA. THIS IS A PRELIMINARY REPORT TO MEET REPORTING TIME LIMITS.
- [SDR JYDR20210715184](https://openairdocs.org/sdr/JYDR20210715184.md): Engine · overtemp · Jul 13, 2021 · N217AC · Skrsky S64E · Engine (Turbine/Turboprop)
  > SHORT FINAL FOR WATER DROP. PILOT RECEIVED 65% CHIME THEN 60% WARNING. ENGINE SECURED AND AIRCRAFT RETURNED TO BASE SINGLE ENGINE. THIS IS A PRELIMINARY REPORT TO MEET REPORTING TIME LIMITS.
- [SDR JYDR20210615165](https://openairdocs.org/sdr/JYDR20210615165.md): Blade · broken · Jun 14, 2021 · N176AC · Skrsky S64E · Turbine Section
  > AIRCRAFT PERFORMING LOGGING OPERATIONS. PILOTS FELT VIBRATION AND NOISE. ENGINE SHUT DOWN IN FLIGHT, AIRCRAFT RETURNED TO LANDING AREA. MAINTENANCE FOUND DEBRIS IN TAIL PIPE. ENGINE REMOVED, FOUND 2ND STAGE N1 BLADE BROKEN, CAUSING EXTENSIVE DAMAGE THROUGH THE
- [SDR JYDR20210429](https://openairdocs.org/sdr/JYDR20210429.md): Blade · broken · Apr 29, 2021 · N6962R · Skrsky S64E · Turbine Section
  > AT SHUTDOWN PILOTS FELT VIBRATION AND HEARD NOISE. UPON INSPECTION MAINTENANCE FOUND INTERNAL FOD IN TAILPIPE. AFTER REMOVING ENGINE, MAINTENANCE FOUND 2ND STAGE N1 TURBINE BLADE HAD FAILED. ENGINE WAS SENT TO THIS REPAIR STATION FOR REPAIR. ENGINE TC HOLDER N
- [SDR JYDR20201008272](https://openairdocs.org/sdr/JYDR20201008272.md): Blades · broken · Oct 7, 2020 · N176AC · Skrsky S64E · Turbine Section
  > PILOTS HEARD A NOISE COMING FROM NR 2 ENGINE AND RETURNED TO SERVICE LANDING. MAINTENANCE FOUND DEBRIS IN TAIL PIPE. ENGINE REMOVED AND IS BEING SHIPPED BACK TO THIS REPAIR STATION FOR INVESTIGATION. THIS IS A PRELIMINARY REPORT FOR REPORTING. ONCE ENGINE
- [SDR JYDR20200702181](https://openairdocs.org/sdr/JYDR20200702181.md): Stabilizer · cracked · Jul 1, 2020 · Skrsky S64E · Horizontal Stabilizer Structure
  > DURING ROUTINE MAINTENANCE/INSPECTION THE STRUCTURE UNDER THE AFT FITTING WAS FOUND CRACKED/BROKEN. STABILIZER WAS REMOVED FROM SERVICE. THIS IS A PRELIMINARY REPORT TO SATISFY REPORTING REQUIREMENTS. AIRCRAFT WAS OPERATING UNDER A NATO FIREFIGHTING CONTRAC
- [SDR JYDR20200625174](https://openairdocs.org/sdr/JYDR20200625174.md): Hinge · cracked · Jun 24, 2020 · Skrsky S64E · Main Rotor Head
  > MAIN ROTOR HEAD WAS BEING OVERHAULED. DURING OVERHAUL MAGNETIC PARTICLE INSPECTION TWO VERTICAL HINGES HAD CRACKS IN PIN HOLES. VERTICAL HINGE SN F-1608 AND F-1768.
- [SDR JYDR20200420109](https://openairdocs.org/sdr/JYDR20200420109.md): Turbine Blades · broken · Apr 19, 2020 · N176AC · Skrsky S64E · Turbine Section
  > DURING RE-FUELING PILOT REPORTED A STRANGE ENGINE NOISE. AFTER SHUTDOWN MECHANICS FOUND A SECOND STAGE N1 BLADE HAD BROKEN AND EXITED THROUGH THE FREE TURBINE. THIS IS A PRELIMINARY REPORT FOR MEETING REPORTING DEADLINE. ENGINE HAS NOT ARRIVED AT THIS REPAIR S
- [SDR JYDR20200408092](https://openairdocs.org/sdr/JYDR20200408092.md): Hinge · cracked · Apr 7, 2020 · N243AC · Skrsky S64E · Main Rotor Head
  > DURING OVERHAUL, AFTER REACHING TBO A CRACK WAS FOUND IN THE EAR DURING NDT PROCEDURE. PART SUBMITTED TO ENGINEERING FOR EVALUATION.
- [SDR JYDR20190423081](https://openairdocs.org/sdr/JYDR20190423081.md): Turbine Blades · broken · Apr 22, 2019 · Skrsky S64E · Turbine Section
  > ENGINE RECEIVED AT REPAIR STATION FOR REPAIR. FOUND 1 EACH 2ND STAGE N1 BLADE BROKEN AT ROOT. UNKNOWN CAUSE AT THIS TIME BECAUSE THIS REPORT MUST BE SUBMITTED FOR REPORTING TIME LIMITS.
- [SDR JYDR20190124023](https://openairdocs.org/sdr/JYDR20190124023.md): Disk · cracked · Jan 23, 2019 · Skrsky S64E · Turbine Engine Compressor Section
  > ENGINE WAS AT REPAIR STATION FOR OVERHAUL. NDT WAS COMPLIED WITH ON THE 3RD STAGE DISK REFERENCE OIS 352 REV N, 3/3/2015. 7EA. CRACK INDICATIONS WERE FOUND FROM A TIE-ROD HOLES USING EDDY CURRENT (REF SPM 585005 REV 143, 01/JUN/2018). THERE WERE 0 CRACK INDI
- [SDR JYDR20190107007](https://openairdocs.org/sdr/JYDR20190107007.md): Tab · broken · Jan 7, 2019 · Skrsky S64E · Turbine Engine Compressor Section
  > ENGINE WAS AT REPAIR STATION FOR SCHEDULED OVERHAUL. DURING TEAR DOWN A BROKEN TAB LOCK WAS DISCOVERED ON THE 4TH STAGE COMPRESSOR DISK. THIS CAUSED THE 4TH STAGE BLADE TO SHIFT AND RUB ON THE 4TH STAGE STATOR. THIS REPAIR STATION PREVIOUSLY SUBMITTED AN SDR,
- [SDR JYDR20181214347](https://openairdocs.org/sdr/JYDR20181214347.md): Disk · cracked · Dec 13, 2018 · N172AC · Skrsky S64E · Turbine Engine Compressor Section
  > ENGINE WAS RECEIVED AT REPAIR STATION FOR HOT SECTION AND AIRWORTHINESS COMPLIANCE (AD) UNDER WO 164822. DURING COMPLIANCE WITH AD 97-02-13 NDT INSPECTION, 2 EACH CRACKS WERE FOUND AT TIE ROD HOLES. AD CALLS FOR FIRST INSPECTION AT 3000 HOURS AND 1500 HOURS TH
- [SDR JYDR20181130332](https://openairdocs.org/sdr/JYDR20181130332.md): Blades · broken · Nov 28, 2018 · N247AC · Skrsky S64E · Turbine Section
  > THIS IS A PRELIMINARY REPORT TO MEET REPORTING REQUIREMENTS. THE ENGINE IS CURRENTLY BEING SHIPPED TO THIS REPAIR STATION FROM CANADA. MORE INFORMATION WILL BE PROVIDED AFTER TEAR DOWN. PILOTS REPORTED VISUAL LOSS OF OIL ON AIRCRAFT RIGHT HAND LANDING GEAR LEG
- [SDR JYDR20180724204](https://openairdocs.org/sdr/JYDR20180724204.md): Strut · broken · Jul 23, 2018 · Skrsky S64E · Fuselage Miscellaneous Structure
  > SEA SNORKELING IN ROUGH SEAS OFF THE COAST OF GREECE. SEA SNORKEL STRUT BROKE OFF AT WELD AREA JUST ABOVE BOOM COUPLING. THIS IS A PRELIMINARY REPORT TO FULFILL 96 HR REPORTING REQUIREMENT. UPPER PORTION OF BOOM IS BEING SHIPPED TO REPAIR STATION FROM GREECE F
- [SDR JYDR20180524141](https://openairdocs.org/sdr/JYDR20180524141.md): Spacer · cracked · May 23, 2018 · Skrsky S64E · Main Rotor Head
  > ALL SIX SPACERS WERE FOUND CRACKED. AFTER VISUAL INDICATIONS WERE FOUND, FPI CONFIRMED THEY WERE CRACKED.
- [SDR JYDR20170817227](https://openairdocs.org/sdr/JYDR20170817227.md): Gearbox · overserviced · Aug 15, 2017 · N176AC · Skrsky S64E · Tail Rotor Gearbox
  > INTERMEDIATE GEAR BOX CHIP LIGHT WHILE FIGHTING FIRE. PILOTS IMMEDIATELY RETURNED TO BASE. GEAR BOX REMOVED FROM AIRCRAFT. INTERMEDIATE GEAR BOX OIL WAS DRAINED AND CAPTURED. THE IGB WAS FOUND TO HAVE ALMOST 3 US GALLONS OF OIL. THIS DOES NOT TAKE INTO ACCOU
- [SDR JYDR20170811215](https://openairdocs.org/sdr/JYDR20170811215.md): Servo · locked · Aug 10, 2017 · Skrsky S64E · Tail Rotor Control System
  > TAIL ROTOR GEAR BOX & SERVO ASSY RECEIVED WITH A WRITE-UP OF UNABLE TO CHANGE PITCH OF BLADES BY HAND DURING INSPECTION.. UPON RECEIPT IN SHOP PITCH CHANGE SHAFT MOVED FREELY BY HAND. T/R G/B WAS DISASSEMBLED AND FOUND OK. T/R G/B SERVO WAS CHECKED AND FOUND B
- [SDR JYDR20170810191](https://openairdocs.org/sdr/JYDR20170810191.md): Pilot Valve · scored · Aug 9, 2017 · Skrsky S64E · Main Rotor Control
  > RIGHT LATERAL SERVO RECEIVED WITH A WHITE-UP OF "RIGHT LATERAL SECOND STAGE PILOT VALVE STUCK". CONFIRMED SECOND STAGE PILOT VALVE STUCK. DISASSEMBLED PILOT VALVE AND FOUND SCORING. HYDRAULIC OIL SAMPLE WILL BE SENT OUT TO DETERMINE WHAT CAUSED SCORING OF PILO
- [SDR JYDR20170727207](https://openairdocs.org/sdr/JYDR20170727207.md): Tie Bolt · broken · Jul 26, 2017 · Skrsky S64E · Main Rotor Head
  > DURING A POST FLIGHT, TIE BOLT WAS FOUND BROKEN. NUT AND WASHER WERE FOUND ON AIRCRAFT UPPER DECK. REPAIR STATION DISPATCHED TASK QUALIFIED PERSON TO CHANGE ALL 3 TIE BOLTS IN THIS AREA. THE TECHNICIAN WILL RETURN WITH THE BROKEN BOLT AND IT WILL BE GIVEN TO
- [SDR JYDR20170628176](https://openairdocs.org/sdr/JYDR20170628176.md): Turbine Blades · missing · Jun 27, 2017 · Skrsky S64E · Turbine Engine Combustion Section
  > PILOT RETURNED TO LANDING REPORTING NOISE AND VIBRATION IN NR 1 ENGINE. AFTER SEPARATING FREE TURBINE FROM ENGINE DISCOVERED ONE EACH SECOND STAGE N1 TURBINE BLADE MISSING FROM ROOT OUT. DOWNSTREAM DAMAGE IN FREE TURBINE. BOTH COMPRESSOR AND FREE TURBINE REPLA
- [SDR JYDR20170428115](https://openairdocs.org/sdr/JYDR20170428115.md): Blade · cracked · Apr 28, 2017 · Skrsky S64E · Turbine Engine Compressor Section
  > ENGINE AT REPAIR STATION FOR OVERHAUL. DURING FPI INSPECTION A CRACK WAS DETECTED ON INBOARD SIDE OF PLATFORM ON DOVE TAIL. CRACK WAS APPROXIMATELY.025 INCH IN LENGTH AXIALLY. AFTER OVERHAULING HUNDREDS OF THESE MODEL ENGINES, THIS IS THE FIRST TIME THIS REPA
- [SDR JYDR20170324075](https://openairdocs.org/sdr/JYDR20170324075.md): Gear · spalled · Mar 23, 2017 · Skrsky S64E · Main Rotor Gearbox
  > DURING DISASSEMBLY FOR MINI OVERHAUL LARGE AMOUNTS OF FERROUS MATERIAL WAS NOTICED IN OIL SUMP. FURTHER TEARDOWN REVEALED 2ND STAGE PLANETARY GEARS WERE HEAVILY SPALLED.
- [SDR JYDR20170324074](https://openairdocs.org/sdr/JYDR20170324074.md): Bracket · missing · Mar 22, 2017 · Skrsky S64E · Tail Rotor Head
  > WHILE CONDUCTING A TAIL ROTOR BALANCE SESSION, BALANCE CHANGED. VISUAL INSPECTION OF THE TAIL ROTOR HEAD SHOWED AN VERNIER BRACKET HAD FALLEN OFF. VISUAL INSPECTION OF THE AREA SHOWED NO OTHER DAMAGE. TAIL ROTOR BALANCED TO WITHIN LIMITS.
- [SDR JYDR20170306065](https://openairdocs.org/sdr/JYDR20170306065.md): Bolt · broken · Mar 6, 2017 · N176AC · Skrsky S64E · Rotorcraft Tail Boom
  > DURING POST FLIGHT, MECHANIC FOUND A DING IN THE LEADING EDGE OF 1 TAIL ROTOR BLADE. FURTHER INSPECTION REVEALED A BROKEN STABILIZER BOLT HEAD. TRB WAS REPLACED. AIRCRAFT MANUFACTURE WAS CONTACTED FOR AN DER APPROVED REPAIR. AFTER AUTHORIZED REPAIR WAS PERFOR
- [SDR JYDR20170321001](https://openairdocs.org/sdr/JYDR20170321001.md): Gearbox · failed · Jan 1, 2017 · N217AC · Skrsky S64E · Main Rotor Gearbox
  > DURING A NORMAL START PROCEDURE, WITH THE NR 1 ENGINE AT GROUND IDLE AND JUST PRIOR TO THE ROTOR BRAKE BEING RELEASED, A FAILURE OCCURRED IN THE MAIN GEARBOX THAT ALLOWED MOMENTARY ROTATION AND SUBSEQUENT LOCKING OF THE MGB. THE ROTOR SYSTEM BARELY MOVED BEFOR
- [SDR JYDR20161128318](https://openairdocs.org/sdr/JYDR20161128318.md): Blade · unbonded · Nov 28, 2016 · N247AC · Skrsky S64E · Tail Rotor Blades
  > TAIL ROTOR BLADE CAUSED VIBRATION ON AIRCRAFT. UPON DISASSEMBLY AT REPAIR STATION, A LARGE AMOUNT OF WATER WAS FOUND IN THE FAIRING. THE WATER WAS ALLOWED ENTRY BECAUSE OF A FAILURE IN A BOND LINE.
- [SDR JYDR20150814209](https://openairdocs.org/sdr/JYDR20150814209.md): Lock Tab · missing · Aug 13, 2015 · Skrsky S64E · Turbine Engine Compressor Section
  > DURING INSPECTION OF COMPRESSOR CORE IT WAS NOTED THAT ONE 5TH STAGE BLADE TAB LOCK WAS MISSING AND THAT BLADE HAD MOVED AFT IN THE DISK MAKING CONTACT WITH THE FORWARD FACE OF THE 5TH STAGE STATOR. A PORTION OF THE MISSING TAB LOCK WAS LATER FOUND AFT IN THE
- [SDR JYDR20150611153](https://openairdocs.org/sdr/JYDR20150611153.md): Ring Gear · loose · Jun 11, 2015 · N247AC · Skrsky S64E · Main Rotor Gearbox
  > MAIN GEAR BOX WAS RECEIVED FOR OVERHAUL. DURING DISASSEMBLY IT WAS FOUND THAT 1EA NUT, MS14182P06 HAD BACKED OFF OF 1EA BOLT MS14181-06010P THAT HOLDS THE SECOND STAGE RING GEAR TO THE SHAFT. THE NUT DID NOT COME OFF THE BOLT. THIS CAUSED DAMAGE TO THE INTE
- [SDR JYDR20150408085](https://openairdocs.org/sdr/JYDR20150408085.md): Turbine · loose · Apr 7, 2015 · N172AC · Skrsky S64E · Turbine Section
  > FREE TURBINE ASSY WAS AT REPAIR STATION FOR A LEAK REPAIR. DURING DISASSEMBLY THE NUT THAT HOLDS THE 6435-20072-101 DRIVE FLANGE WAS FOUND TO BE LOOSE. FURTHER INVESTIGATION SHOWED THAT THE FLANGE HAD PAINT ON THE MATING SURFACES. TORQUEING THE NUT AGAINST PA
- [SDR JYDR2014030600439](https://openairdocs.org/sdr/JYDR2014030600439.md): Bearing · spalled · Mar 6, 2014 · N247AC · Skrsky S64E · Main Rotor Gearbox
  > MAIN GEAR BOX WAS REMOVED FROM ACFT, DUE TO MAKING METAL AFTER A CHIP LIGHT DURING FLIGHT. DISASSEMBLY OF MGB AT REPAIR STATION REVEALED THAT LT (NR 1) 2ND STAGE INPUT ALIGNMENT BEARING HAD FAILED. THIS BEARING IS NORMALLY NOT A RECURRING PROBLEM.
- [SDR JYDR2013FA0000586](https://openairdocs.org/sdr/JYDR2013FA0000586.md): Lock Tab · broken · Oct 3, 2013 · N957AC · Skrsky S64E · Turbine Engine Compressor Section
  > DURING TEARDOWN OF THE COMPRESSOR CORE THERE WAS EXTENSIVE DAMAGE TO BLADES AND VANES FROM THE 3RD STAGE AFT. THE DAMAGE OCCURED WHEN THE AFT END OF A 3RD STAGE TABLOCK BROKE ALLOWING THE 3RD STAGE BLADE TO MOVE AFT CONTACTING THE 4TH STAGE STATOR. THE BLADE T
- [SDR JYDR2013FA0000421](https://openairdocs.org/sdr/JYDR2013FA0000421.md): Compressor Wheel · cracked · Jul 26, 2013 · N154AC · Skrsky S64E · Turbine Engine Compressor Section
  > COMPRESSOR WAS BEING OVERHAULED. DURING NDT CRACKS WERE FOUND AT THE TIE ROD HOLES.
- [SDR JYDR2013FA0000420](https://openairdocs.org/sdr/JYDR2013FA0000420.md): Compressor Wheel · cracked · Jul 26, 2013 · N229AC · Skrsky S64E · Turbine Engine Compressor Section
  > COMPRESSOR WAS BEING OVERHAULED. DURING NDT CRACKS WERE FOUND AT THE TIE ROD HOLES.
- [SDR 2013FA0000416](https://openairdocs.org/sdr/2013FA0000416.md): Lock · broken · Jul 18, 2013 · N218AC · Skrsky S64E · Turbine Engine Compressor Section
  > ENGINE REMOVED, DURING DISASSEMBLY MINOR DAMAGE WAS NOTED ON THE BLADES AND VANES AFT IF 5TH STAGE. THE DAMAGE WAS CAUSED BY A 5TH STAGE DISK TAB LOCK THAT HAD BROKEN AND ALLOWED THE BLADE TO MOVE AFT IN THE DISK MAKING CONTACT WITH THE 6TH STAGE STATOR.
- [SDR 2011FA0000703](https://openairdocs.org/sdr/2011FA0000703.md): Blade · cracked · Aug 29, 2011 · N194AC · Skrsky S64E · Main Rotor Blades
  > AT FIRST BIM CHECK, PILOTS REPORTED HEARING A CHIRPING NOISE COMING FROM THE MAIN ROTOR BLADES. INSPECTED BLADES. FOUND THE TIP WEIGHT ON MAIN ROTOR BLADE PROTRUDING THROUGH THE TIP CAP. BLADE WAS REPLACED. OPEN
- [SDR 2011FA0000704](https://openairdocs.org/sdr/2011FA0000704.md): Blades · fractured · Jun 10, 2011 · N172AC · Skrsky S64E · Turbine Engine Compressor Section
  > AFTER ABOUT 1.5 HRS OF FLIGHT, THE PILOTS RETURNED TO LANDING AND SAID THAT THE NR1 ENGINE HAD A HIGH FREQUENCY RUMBLE AND JUST BEFORE LANDING, THE TQ AND EPR GAUGES DECRESED RAPIDLY, WHILE THE ENGINE TEMP AND OIL IND WERE STILL GREEN. AFTER SHUTDOWN, THE INLE
- [SDR CA100323004](https://openairdocs.org/sdr/CA100323004.md): Engine · failed · Mar 8, 2010 · Skrsky S64E · Engine (Turbine/Turboprop)
  > ACFT WAS INVOLVED IN AERIAL TIMBER HARVESTING OPERATIONS. WHILE THE ACFT WAS DESCENDING TO THE LOG LANDING AT A RATE OF 200 TO 300 FT PER MINUTE AND AN AIRPSEED OF 20 KNOTS THE FLIGHT CREW HEARD A "SWOOSH" SOUND AND THEN WERE ALTERTED BY AN ENGINE LOW N1 RPM
- [SDR CA100119008](https://openairdocs.org/sdr/CA100119008.md): Blade · dislodged · Jan 15, 2010 · Skrsky S64E · Turbine Engine Compressor Section
  > (CAN) COMPRESSOR WAS REMOVED FROM ACFT FOR HIGH VIBRATION. COMPRESSOR HAD 20.3 HOURS SINCE INSTALL AND LAST HOT SECTION INSP. UPON DISASSEMBLY, DAMAGE WAS FOUND TO VARIOUS STATORS, BLADES, BLEED BAND, AND OTHER PARTS. THE DAMAGE WAS CUASED BY A 4TH STAGE COMP
- [SDR CA081105002](https://openairdocs.org/sdr/CA081105002.md): Engine · overtemp · Sep 8, 2008 · Skrsky S64E · Engine (Turbine/Turboprop)
  > (CAN) WHILE DEPARTING AREA WITH AN AIRSPEED OF 30 TO 40 KNOTS AND A 500 FT PER MINUTE RATE OF DESCENT, NR 2 ENG N1 LOW RPM AUDIO HORN SOUNDED ALONG WITH ILLUMINATION OF NR 2 ENG LOW OIL PRESSURE LIGHT. A SCAN OF ENG GAUGES REVEALED NR 2 ENG HAD LOW N1 RPM WIT
- [SDR CA080925007](https://openairdocs.org/sdr/CA080925007.md): Fuel Control · failed · Sep 8, 2008 · Skrsky S64E · Fuel Control/Turbine Engines
  > (CAN) LIGHT A SCAN OF THE ENG GAUGES REVEALED THE NR 2 ENGINE HAD LOW N1 RPM WITH A CLIMBING T5 TEMP. FLIGHT CREW IDENTIFIED THE PROBLEM AS AN ENG ROLL BACK AND ONCE THE LOAD WAS SAFELY JETTISONED A SHUTDOWN OF THE NR (2) ENGINE WAS CARRIED OUT. THE ACFT THE

Next page: https://openairdocs.org/model/erickson-s64e/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 = 'S64E'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/erickson-s64e/reports

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