# Service difficulty reports: JASC 6140

A list on [JASC 6140](https://openairdocs.org/jasc/6140.md).

Reports filed under 6140 · Propeller Indication System, newest first.

Page 1 of 6 · 292 reports

- [SDR 2026FA0000059](https://openairdocs.org/sdr/2026FA0000059.md): Tach Generator · loose · Dec 25, 2025 · N971LA · Textrn 408
  > ON 12/25/25, WE HAD AN INFLIGHT EMERGENCY DECLARED BY THE FLIGHT CREW FOR #1 ENGINE PROP SPEED ERRATIC. THE CREW REPORTED THE #1 ENGINE PROPELLER SPEED WAS JUMPING AROUND BETWEEN 1400 AND 1900 IN CLIMB SHORTLY AFTER TAKEOFF. THE CREW SAID ALL OTHER ENGINE INDI
- [SDR OZCA90130MAR21](https://openairdocs.org/sdr/OZCA90130MAR21.md): Propeller · low pressure · Mar 30, 2021 · N901BC · Saab SF340A
  > DURING CRUISE FLIGHT AT 13000, WE HAD PROP OIL PRESSURE LOW ON #1 ENGINE. PROCEEDED ACCORDING TO QRH PG E3-6
- [SDR RU3A20190827044](https://openairdocs.org/sdr/RU3A20190827044.md): Proximity Switch · failed · Aug 27, 2019 · N79 · Beech 300BEECH
  > RT PROP PITCH ANNUNCIATOR ON INTERMITTENTLY IN FLIGHT. ISSUE RESOLVED BY REPLACEMENT OF THE RIGHT PROXIMITY SWITCH.
- [SDR RU3A201908197040](https://openairdocs.org/sdr/RU3A201908197040.md): Proximity Switch · failed · Aug 16, 2019 · N75 · Beech 300BEECH
  > RT PROP PITCH LIGHT FAST FLICKERS AND COMES ON BEFORE LEFT. FLICKERS ON SHUTDOWN AS WELL. R/H ENGINE PROXIMITY SWITCH WAS FOUND TO HAVE FAILED. REPLACED SWITCH. NO FURTHER ACTION REQUIRED.
- [SDR RU3A20190326010](https://openairdocs.org/sdr/RU3A20190326010.md): Proximity Switch · out of adjust · Mar 22, 2019 · N69 · Beech 300BEECH
  > LEFT PROP PITCH LIGHT ILLUMINATED IN FLIGHT. LASTED APPROX 10 MIN. ISSUE WAS CLEARED FOLLOWING THE CLEANING AND ADJUSTMENT OF PROXIMITY SWITCH.
- [SDR QXEA2019031300115](https://openairdocs.org/sdr/QXEA2019031300115.md): Warning System · activated · Mar 12, 2019 · N444QX · Bombdr DHC8402
  > NR 1 PROP SPEEC 1070 WITH ASSOICATED NR 1 PEC CAUTION AND POWERPLANT MESSAGE. SHUTDOWN ENGINE IN FLIGHT AND RETURND TO FIELD. LANDING UNEVENTFUL, NOT OVERWEIGHT. AIRCRAFT OUT OF SERVICE FOR REPAIRS.
- [SDR RU3A20181204049](https://openairdocs.org/sdr/RU3A20181204049.md): Proximity Switch · out of adjust · Dec 4, 2018 · N72 · Beech 300BEECH
  > RIGHT PROP PITCH ANNUNCIATOR ILLUMINATED IN FLIGHT. THE PROBLEM WAS SOLVED BY ADJUSTING THE PROXIMITY SWITCH. NO FURTHER ACTION REQUIRED.
- [SDR RU3A2018F00127](https://openairdocs.org/sdr/RU3A2018F00127.md): Proximity Switch · faulty · Oct 1, 2018 · N69 · Beech 300BEECH
  > L PROP PITCH CAUTION LIGHT ILLUMINATED IN FLIGHT (CRUISE, 200 KTS, 5000') CAUSED BY FAULTY PROX SWITCH. INSTALLED NEW PROX SWITCH. OPERATIONAL CHECK SATISFACTORY.
- [SDR RU3A2018092119041](https://openairdocs.org/sdr/RU3A2018092119041.md): Proximity Switch · broken · Sep 19, 2018 · N72 · Beech 300BEECH
  > RT PROP PITCH LIGHT ILLUMINATED IN FLIGHT CAUSED BY A FAULTY PROXIMITY SWITCH. PROXIMITY SWITCH WAS REPLACED. OPERATIONAL CHECK WAS GOOD.
- [SDR 2019F00058](https://openairdocs.org/sdr/2019F00058.md): Signal Cond Unit · failed · Aug 12, 2018 · Dhav DHC8202
  > PROPELLER OVERSPEED INDICATION ENG#1. AIRCRAFT TURN BACK TO AIRPORT AFTER SHUTTING DOWN AFFECTED ENGINE ACCORDING TO PROCEDURE. CORRECTIVE ACTION: SIGNAL CONDITIONER UNITS SWAPPED BETWEEN ENG#1 AND ENG #2. CLEANED OVERSPEED GOVERNOR SOLENOID VALVE CONNECTOR. E
- [SDR RU3A201805216018](https://openairdocs.org/sdr/RU3A201805216018.md): Switch · failed · May 16, 2018 · N72 · Beech 300BEECH
  > RIGHT PROPELLER PITCH LIGHT ILLUMINATED AFTER TAKEOFF. REPLACED A FAULTY PROPELLER SWITCH. NO FURTHER ACTION REQUIRED.
- [SDR CA180423014](https://openairdocs.org/sdr/CA180423014.md): Gear · damaged · Apr 19, 2018 · Mtsbsi MU2B60
  > (CAN) AFTER LANDING THE PILOT WENT TO SPIN THE PROPELLER, PER ROUTINE PROCEDURES, AND FOUND THAT THE ENGINE WOULD NOT TURN. AFTER SEVERAL ATTEMPTS THE ENGINE DID ROTATE, BUT A REASON FOR THE PROBLEM COULD NOT BE DETERMINED. THE ENGINE WAS REPLACED AND IS NOW
- [SDR VGCA20161114001](https://openairdocs.org/sdr/VGCA20161114001.md): Tachometer · false indication · Nov 14, 2016 · N361FL · Cvac STC3405800
  > NR 2 ENGINE EXPERIENCED A PROP OVERSPEED CONDITION. PRECAUTIONARY ENGINE SHUTDOWN. TACHOMETER FOUND TO BE GIVING A FALSE INDICATION.
- [SDR HNAA2016071100213](https://openairdocs.org/sdr/HNAA2016071100213.md): Indicator · inoperative · Jul 9, 2016 · N814EX · Dhav DHC8102
  > NR 2 PROPELLER N/P INDICATOR ANALOG NEEDLE WILL NOT TEST. STUCK AT ZERO. RETURN TO GATE. R & R THE NR 2 PROPELLER INDICATOR. OPS CHECKED GOOD IAW AMM 61-44-00. OKAY FOR SERVICE.
- [SDR CA151224002](https://openairdocs.org/sdr/CA151224002.md): Switch · faulty · Dec 21, 2015 · Dhav DHC8311
  > (CAN) FLIGHT CREW REPORTED THAT THE BETA WARNING SOUNDED AT APPROX FL40, AT 1200 RMP AND C/L AT MAX. CONTINUOUS. AIRCRAFT RETURNED TO DEPARTURE AIRPORT. MAINTENANCE ACTION, BETA WARNING MICRO SWITCH ACTUATOR REPLACED, ADJUSTED, AND TESTED SERVICEABLE AS PER A
- [SDR CA150714013](https://openairdocs.org/sdr/CA150714013.md): Switch · shorted · Jul 12, 2015 · Dhav DHC8102
  > (CAN) FLIGHT CREW REPORTED THAT DURING TAKEOFF THE NR 1 ENG HAD TORQUE & PROP FLUCTUATIONS & AS A RESULT THEY DID A PRECAUTIONARY SHUTDOWN OF THE NR 1 ENG. THE ACFT RETURNED TO THE DEPARTURE AIRPORT. TROUBLESHOOTING DETERMINED THAT THE ENG PARAMETER FLUCTUAT
- [SDR HNAA2015062400206](https://openairdocs.org/sdr/HNAA2015062400206.md): Relay · no test · Jun 24, 2015 · N814EX · Dhav DHC8102
  > BETA LOCKOUT WILL NOT TEST. R & R RELAY 3313-K1 IAW WIRING MANUAL 32-42-00. OPS CHECKED GOOD IAW MM 61-42-00. PERFORMED WC 61-20-10Q. OK FOR SERVICE.
- [SDR O2GA2015052280201](https://openairdocs.org/sdr/O2GA2015052280201.md): Proximity Switch · defective · May 18, 2015 · N802UP · Beech B300
  > ON CLIMB OUT THE RT PROPELLER PITCH ANNUNCIATOR ILLUMINATED. ACFT WAS DIVERTED BACK FOR MX. TROUBLE SHOT THE DISCREPANCY & FOUND A DEFECTIVE RT PROXIMITY SWITCH. ENG RUNS WERE PERFORMED & SYS OPERATIONAL CHECKS WERE GOOD. ACFT WAS RETURNED TO SERVICE.
- [SDR HNAA2015020600034](https://openairdocs.org/sdr/HNAA2015020600034.md): Indicator · malfunctioned · Feb 5, 2015 · N934HA · Dhav DHC8102
  > REJECTED T/O DUE TO NR 2 PROPELLER REACHED 1243 RPM FOR APPROX 5-10 SEC. R &R NR 2 PROP INDICATOR & NR 2 NP PROBE AS REQUIRED. R & R NR 2 HORSECOLLAR PANEL. RAN ENGINES PERFORMED ALL REQUIRED OPS CHECKS. OPS CHECK GOOD AT THIS TIME.
- [SDR O2GA2014071582701](https://openairdocs.org/sdr/O2GA2014071582701.md): Switch · intermittent · Jul 7, 2014 · N827UP · Beech B300
  > PROP GND SOL ANNUCIATOR ILLUMINATED IN FLIGHT. COMPLIED WITH CHECKLIST & ANNUNCIATOR EXTINGUISHED. REPLACED THE PROPELLER GND FINE SWITCH IN THE PEDESTAL & PERFORMED A SUCCESSFUL OPERATIONAL CHECK. ACFT RETURNED TO SERVICE.
- [SDR JJBA20140622011](https://openairdocs.org/sdr/JJBA20140622011.md): Unknown · malfunctioned · Jun 22, 2014 · N838CA · Bombdr DHC8400
  > NUMBER 2 PROP DID NOT COME OUT OF 900 RPM WHEN CREW TRIED TO INCREASE TO 1200 RPM ON LANDING. GND RAN ACFT, INSPECTED NR 2 ENG PUSHRODS TO PCU & NO DEFECTS FOUND. OCF REQUIRED.
- [SDR 29GA2014060900001](https://openairdocs.org/sdr/29GA2014060900001.md): Sensor · malfunctioned · Jun 6, 2014 · N347AG · Saab 340B
  > DURING CRUISE, LEFT PROPELLER DROPPED FROM 1230-1100 RPM, FOLLOWED BY A DROP FROM 1230-800 RPM TWICE WAS NOT AN INDICATION EVENT, RETURNED TO DEPARTURE, LANDED WITHOUT INCIDENT. REPLACED PROPELLER SPEED INDICATOR AND SPEED SENSOR.
- [SDR ERAA20140022](https://openairdocs.org/sdr/ERAA20140022.md): Indicator · inoperative · Apr 18, 2014 · N972EA · Beech 1900D
  > LEFT PROP GAUGE INOPERATIVE ON TAKEOFF ROLL. R & R PROP INDICATOR, OPERATIONS CHECKED GOOD IAW MM 31-10-00.
- [SDR RU3A20140131002](https://openairdocs.org/sdr/RU3A20140131002.md): Warning Light · illuminated · Jan 28, 2014 · N80 · Beech 300BEECH
  > NUMBER 2 RT PROP PITCH LIGHT ILLUMINATED ON APPROACH TO LANDING & REMAINED ON UNTIL SHUTDOWN.
- [SDR HNAA2013122300627](https://openairdocs.org/sdr/HNAA2013122300627.md): Warning Horn · false activation · Dec 23, 2013 · N809EX · Dhav DHC8102
  > BETA LOCKOUT HORN CAME ON AFTER 50 FEET CONTINUOUSLY. RETURN TO FIELD, FUNCTION CHECKED SYSTEM. OPS CHECKED OK IAW 61-20-10.
- [SDR GLBA2013102200342](https://openairdocs.org/sdr/GLBA2013102200342.md): Indicator · malfunctioned · Oct 21, 2013 · N202UX · Beech 1900D
  > PILOT REPORTED AFTER TAKE OFF, LT PROP RPM ROSE TO 1730 FOR 15 SECS, PULLED BACK PROP LEVERS AND CONTINUED TO CLIMB, LEVELED OFF AND TRIED TO SYNC PROPS, RECEIVED A VIBRATION, TURNED OFF PROP SYNC AND SYNC'D, NR 1 AT 1400 AND NR 2 AT 1550, STARTED LOSING PROP
- [SDR HNAA2013032900187](https://openairdocs.org/sdr/HNAA2013032900187.md): Lockout · intermittent · Mar 29, 2013 · N808EX · Dhav DHC8102
  > DURING NR 2 BETA LOCKOUT TEST, WITH BETA TEST SWITCH AT LOCKOUT AND NR 2 PROP INDICATOR BETA LOCK TEST BUTTON PRESSED, NR 2 PROPELLER GROUND RANGE LIGHT ILLUMINATED. PROBLEM IS INTERMITTENT. BETA LOCKOUT SYS WITH CR AND MOD DEACTIVATED IAW APPENDIX 1,61-4.
- [SDR RNVA20130325005](https://openairdocs.org/sdr/RNVA20130325005.md): Indicator · faulty · Feb 5, 2013 · N308PW · Cessna 208B
  > ON 2/05/2013 PILOT REPORTED THAT PROP RPM EXCEEDED 1900 RPM, MAINTENANCE PERFORMED GROUND RUN AND COULD NOT DUPLICATE PROBLEM. THE AIRCRAFT WAS FLOWN BY OTHER PILOTS WITHOUT ANY PROP OVERSPEED ISSUE. ON 2/15/2013 PILOT REPORTED AGAIN THAT HE HAD A PROP OVERS
- [SDR HNAA2012080600899](https://openairdocs.org/sdr/HNAA2012080600899.md): Warning Horn · false activation · Aug 6, 2012 · N814EX · Dhav DHC8102
  > BETA LOCKOUT WARNING HORN SOUNDED AFTER TAKEOFF AND BECAME SILENT AFTER LANDING. RETURNED TO FIELD. BETA LOOCKOUT SYS WITH CR AND MOD COMPLIED WITH APPENDIX 1 /61-4.
- [SDR HNAA2012080600898](https://openairdocs.org/sdr/HNAA2012080600898.md): Warning Horn · false activation · Aug 6, 2012 · N814EX · Dhav DHC8102
  > BETA WARNING HORN SOUNDED ON TAKEOFF AFTER 50 FT, CONTINUED TO SOUND UNTIL RETURN TO FIELD, SILENCED AFTER 50 FT WAS REACHED. BETA WARNING HORN SYS WITH MOD PULLED AND COLLARED CIRCUIT BREAKER C8 LEFT MAIN BUSS.
- [SDR II9A20120719001](https://openairdocs.org/sdr/II9A20120719001.md): Tach Generator · defective · Jul 19, 2012 · N228ST · Dorner DO228212
  > RPM DECREASED AND FLUCTUATING LEFT ENGINE. SHUT ENGINE DOWN AS PRECAUTION.
- [SDR NSVA20120421521](https://openairdocs.org/sdr/NSVA20120421521.md): Transducer · faulty · Apr 21, 2012 · N187WQ · Bombdr DHC8402
  > GATE RETURN DUE TO MX (POWERPLANT MESSAGE). MX REQUESTED EMU DOWNLOAD DUE TO REPEAT WRITE UP. FAULT CODE SHOWS CLEAR FAULT WITH NR 2 BFT CHANNEL. REMOVED AND REPLACED BETA FEEDBACK TRANSDUCER OPS CHECK GOOD.
- [SDR HNAA2012022100599](https://openairdocs.org/sdr/HNAA2012022100599.md): Switch · inoperative · Feb 20, 2012 · N335EN · Dhav DHC8311
  > NR 2 BETA LOCKOUT FAILED AFTER TAKE OFF. RETURNED TO FIELD. R & R BETA LOCKOUT SWITCH 6141-S6, NO FIX. R & R PLA SWITCH 6141-S4. OPS CHECKED GOOD. PERFORMED BETA LOCKOUT TEST FUNCTION, CHECK IAW RUN MANUAL. OPS CHECK GOOD.
- [SDR HNAA2012012600506](https://openairdocs.org/sdr/HNAA2012012600506.md): Indicator · erratic · Jan 27, 2012 · N837EX · Dhav DHC8102
  > NR 1 N/P INDICATOR VERY ERRATIC DIGITAL AND ANALOG AT 1050 RPM NR 1 PROP SOUNDED ERRATIC. SMOOTHED OUT AT 900 RPM. R & R INDICATOR IAW CHAPTER 20.
- [SDR HNAA2011090100264](https://openairdocs.org/sdr/HNAA2011090100264.md): Pcu · failed · Aug 21, 2011 · N936HA · Dhav DHC8102
  > ON CLIMB OUT, NR 2 NP REACHED 1245 AND DROPPED TO 1236, THEN CREW RETARDED TO 1050 AND RETURNED TO FIELD. PROP OVERSPEED WITHIN LIMITS OF MM 61-10-00. R & R NR 2 PCU IAW WC 61-10-10. OPS CHECKED GOOD.
- [SDR HNAA2011081700258](https://openairdocs.org/sdr/HNAA2011081700258.md): Electronic Unit · failed · Aug 14, 2011 · N931HA · Dhav DHC8102
  > AUTOFEATHER ARM LIGHT REMAINED ILLUMINATED INFLIGHT UNTIL TORQUE REDUCED BELOW 80 PERCENT, NR 1 TORQUE INDICATOR ERRATIC AND STICKS. R & R TSEU USING RETAINED HARDWARE AND RESECURED ALL CONNECTOR PLUGS AND BONDING WIRE. GROUND RAN ACFT WITH OPS CHECKS. OPS CH
- [SDR CA110804008](https://openairdocs.org/sdr/CA110804008.md): Tach Generator · failed · Jul 28, 2011 · Beech B200
  > ACFT WAS ON A ROUTINE FLIGHT. WHEN THE NP (PROP SPEED) INDICATION WENT TO ZERO. THE TACH GENERATOR WAS REPLACED WITH AN O/H UNIT WITH OUT FURTHER INCIDENT.
- [SDR RU3A1113](https://openairdocs.org/sdr/RU3A1113.md): Proximity Switch · defective · Apr 5, 2011 · N76 · Beech 300BEECH
  > IN CRUISE FLIGHT AT 16000 MSL, RIGHT PROP PITCH ANNUNCIATOR ILLUMINATED. NO OTHER INDICATIONS ON INSTRUMENTS. NO AFFECTS ON AIRCRAFT HANDLING WERE DETECTED IN FLIGHT. CREW ELECTED TO RETURN TO HOME BASE. IN ANTICIPATION OF POSSIBLE ASYMMETRIC THRUST ON LAN
- [SDR CA101216002](https://openairdocs.org/sdr/CA101216002.md): Drive Shaft · unserviceable · Dec 15, 2010 · Beech 1900D
  > (CAN) THE PROP INDICATION WENT TO "0" IN FLIGHT - THE DRIVE SHAFT ON THE TACH GENERATOR WAS FOUND TO BE WORN TO THE POINT WHERE IT WAS SPINNING INSIDE THE ENGINE DRIVE.
- [SDR NSVA2010116](https://openairdocs.org/sdr/NSVA2010116.md): Warning System · malfunctioned · Jul 7, 2010 · N362PX · Saab 340B
  > ABORTED TAKEOFF FOR AUTO COARSEN LIGHT. PERFORMED AUTO COARSEN TEST, OPS CHECKED GOOD.
- [SDR CA100528005](https://openairdocs.org/sdr/CA100528005.md): Beta Switch · unserviceable · May 25, 2010 · Frchld SA227DC
  > LT BETA LIGHT CAME ON DURING TAKEOFF ROLL. PILOT ABORTED TAKEOFF - MX REPLACED BETA LIGHT SWITCH AND ACFT RETURNED TO SERVICE AFTER SERVICEABLE GROUND RUN.
- [SDR GLBA200911221](https://openairdocs.org/sdr/GLBA200911221.md): Indicator · inoperative · Nov 22, 2009 · N231YV · Beech 1900D
  > UPON APPLICATION OF TAKEOFF POWER ON RUNWAY, THE NR 2 PROP GAUGE WENT TO ZERO.
- [SDR GLBA20091120A](https://openairdocs.org/sdr/GLBA20091120A.md): Gauge · inoperative · Nov 20, 2009 · N96ZK · Beech 1900D
  > ABORTED TAKEOFF - UPON APPLYING TAKEOFF POWER ON THE RUNWAY, PILOTS REPORTED THAT THE NR 2 PROPELLER GAUGE WENT TO ZERO. MX REMOVED AND REPLACED THE NR 2 PROPELLER GAUGE IAW MM 31-10-00 AND OPERATIONALLY CHECKED THE SYS WHICH WAS GOOD.
- [SDR SWIA200922647](https://openairdocs.org/sdr/SWIA200922647.md): Warning System · malfunctioned · Sep 16, 2009 · N216SW · Emb EMB120
  > TRIPLE CHIME "TAKEOFF, AUTO FEATHER" WARNING. (FLT 7779) AUTO FEATHER TEST AND ENGINE RUNS NORMAL.
- [SDR GLBA20090703A](https://openairdocs.org/sdr/GLBA20090703A.md): Tach Generator · deteriorated · Jul 3, 2009 · N195GL · Beech 1900D
  > ABORTED TAKEOFF, PILOTS REPORTED THAT AT TAKEOFF POWER THE PROPELLER RPM ON THE LT SIDE EXCEEDED 2000 RPM AND THE TAKEOFF WAS ABORTED. MX REMOVED AND REPLACED NR 1 PROPELLER TACH GENERATOR IAW 67D MM 70-00-00. OPS AND LEAK CHECKS WERE GOOD IAW MM 77-10-00.
- [SDR JJBA200972549](https://openairdocs.org/sdr/JJBA200972549.md): Torque Sensor · false activation · Jun 22, 2009 · N374PH · Dhav DHC8202
  > AFTER T/O AT 700 FT NR 2 PROP WENT INTO FEATHER. PILOT SHUTDOWN NR 2 ENGINE, DECLARED EMERGENCY, RETURNED TO FIELD (PIT) SAFELY. MAINT CREW FOUND THAT NR 2 TORQUE SIGNAL CONDITIONER FAILED. REMOVED AND REPLACED NR 2 TSCU. PERFORMED A TEST FLIGHT. TEST FLI
- [SDR GLBA20090520F](https://openairdocs.org/sdr/GLBA20090520F.md): Circuit Board · failed · May 18, 2009 · N237YV · Beech 1900D
  > PILOTS REPORTED THAT THE AFX ANNUNCIATORS AND REPEATER LIGHTS EXTINGUISHED AFTER V. THE AFX FAULT ANNUNCIATOR DID NOT ILLUMINATE. MAINT REMOVED AND REPLACED THE PRINTED CIRCUIT BOARD A123 IAW 1900D MM 61-20-00. MAINT ADDTIONALLY COMPLIED WITH FLEET CAMPAIGN DI
- [SDR GLBA200904191](https://openairdocs.org/sdr/GLBA200904191.md): Gasket · damaged · Apr 19, 2009 · N153GL · Beech 1900D
  > AFTER TAKEOFF, PROP GAUGE FOR NR 1 ENGINE DROPPED TO 0 RPM AND REMAINED THERE FOR THE REMAINDER OF THE FLIGHT AND TAXI. MAINTENANCE R & R NR 1 ENGINE TACH GENERATOR. MAINTENANCE THEN INSTALLED A GASKET, TACH GEN, AND GROUND RAN NR 1 ENGINE WHICH OPERATIONALL
- [SDR COEA2009012301700](https://openairdocs.org/sdr/COEA2009012301700.md): Indicator · malfunctioned · Jan 22, 2009 · N700FX · Cessna 208B
  > ABORTED TAKEOFF. DURING TAKEOFF ROLL, THE PROPELLER SPEED CAME UP TO ONLY 1300 RPM. NORMAL RPM IS 1900. THE PILOT ABORTED TAKEOFF AND THE ACFT SAFELY RETURNED TO THE RAMP. REPLACED NP (PROPELLER RPM) INDICATOR.
- [SDR SWIA200820505](https://openairdocs.org/sdr/SWIA200820505.md): Propeller · surges · Nov 23, 2008 · N561SW · Emb EMB120ER
  > FLT 7802 - RIGHT PROP NP ABOVE TOLERANCES ON CLIMB-OUT. RAN ENGINES, UNABLE TO DUPLICATE.

Next page: https://openairdocs.org/jasc/6140/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 jasc_code = '6140'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/jasc/6140/reports

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