# Service difficulty reports: JASC 6340

A list on [JASC 6340](https://openairdocs.org/jasc/6340.md).

Reports filed under 6340 · Rotor Drive Indicating System, newest first.

Page 1 of 6 · 265 reports

- [SDR QR9R2026091000001](https://openairdocs.org/sdr/QR9R2026091000001.md): Transducer · fluctuates · Sep 10, 2026 · Bolkms BK117C2
  > #2 XMSN PRESSURE INDICATION ON CPDS ERRATIC DURING GROUND RUN. INDICATION FLUCTUATED BETWEEN 0.0 AND 5.0 BAR RANDOMLY. REMOVED AND REPLACED #2 XMSN OIL PRESSURE TRANSDUCER IAW AMM 63-41-00, 4-1.
- [SDR QR9R2026082400001](https://openairdocs.org/sdr/QR9R2026082400001.md): Transmitter · faulted · Aug 24, 2026 · Bolkms BK117C2
  > NO OIL PRESSURE OBSERVED ON TRANSMISSION NR 2 AFTER REACHING STABILIZED GROUND IDLE AFTER START OF ENGINE NR1. ABORTED THE START IAW CL. AVIONICS PERSONNEL PERFORMED BATTERY DISCONNECT/RESET. ATTEMPTED A START ON ENGINE NR 2, STILL NO OIL PRESSURE ON TRANSMISS
- [SDR QR9R2026060400001](https://openairdocs.org/sdr/QR9R2026060400001.md): Indicator · stuck · Jun 4, 2026 · Bolkms BK117C2
  > TRIPLE TACH WOULD NOT MOVE AT IDLE DURING START RUN-UP. REMOVED AND REPLACED TRIPLE TACH IAW AMM 62-41-00, 4-3; MOC SUCCESSFULLY COMPLETED.
- [SDR QR9R2026052900001](https://openairdocs.org/sdr/QR9R2026052900001.md): Transducer · faulty · May 29, 2026 · Bolkms BK117C2
  > NO RISE IN #1 TRANSMISSION OIL PRESSURE AFTER STARTING. ONLY DISPLAYED STATIC INDICATION OF.2. REMOVED AND REPLACED #1 TRANSMISSION OIL PRESSURE TRANSDUCER IAW 63-41-00, 4-4. MOC SUCCESSFULLY COMPLETED.
- [SDR QR9R2026043000001](https://openairdocs.org/sdr/QR9R2026043000001.md): Transducer · faulted · Apr 30, 2026 · Bolkms BK117C2
  > NR 1 TRANSMISSION OIL PRESSURE.4 BAR, RESET, INDICATED 1.4 AND IMMEDIATELY DROPPED DOWN TO.4 AGAIN DURING START RUN-UP. REMOVED AND REPLACED #1 TRANSMISSION OIL PRESSURE TRANSDUCER IAW AMM 63-41-00, 4-4. T/P MOC SUCCESSFULLY COMPLETED.
- [SDR QR9R2025121700001](https://openairdocs.org/sdr/QR9R2025121700001.md): Transmitter · failed · Dec 17, 2025 · Bolkms BK117C2
  > PILOT REPORTED MAST MOMENT EXCEEDANCE ABOVE 90% WHILE IN LEVEL FLIGHT AND STEADY SPEED. REPORTED MM MONITORING SYSTEM JUMPED BETWEEN VECTORIAL AND LINEAR WHILE IN FLIGHT ACCOMPANIED WITH A GONG. REMOVED AND REPLACED SENSOR SIGNAL TRANSMITTING UNIT IAW AMM 63-4
- [SDR QR9R2025112500001](https://openairdocs.org/sdr/QR9R2025112500001.md): Transmitter · failed · Nov 25, 2025 · Bolkms BK117C2
  > DURING ENG #1 START, MM INDICATION BEGAN TO MOVE PAST 77% REACHING THE MM EXCEEDANCE ONCE THE ENG REACHED IDLE. A TEST FLIGHT EVAL FOUND DURING TWO CONSECUTIVE STARTS OF #1 ENG; MAST MOMENT GAVE 3-4 AND 2 ERRONEOUS DEVIATIONS ABOVE 90%. ADDITIONAL 2 DEVIATIONS
- [SDR QR9R2025101700001](https://openairdocs.org/sdr/QR9R2025101700001.md): Spu · unreliable · Oct 17, 2025 · Bolkms BK117C2
  > MAST MOMENT INDICATION UNRELIABLE DURING START RUN-UP. UNABLE TO REDUCE BELOW 8% WHEN CENTERED, ALSO JUMPED AROUND WHEN CYCLIC WAS NOT BEING MOVED. DURING TROUBLESHOOTING OF MAST MOMENT SYS, UPEAK, UPEAK1, AND UPEAK2 VOLTAGES WERE OUT OF TOLERANCE. SUBBED IN S
- [SDR QR9R2025070200001](https://openairdocs.org/sdr/QR9R2025070200001.md): Indicator · stuck · Jul 2, 2025 · Bolkms BK117C2
  > TRIPLE TAC FAILED IN FLIGHT. NR STUCK IN POSITION AND WOULD NOT MOVE. BOTH N2 NEEDLES DID MOVE. REMOVED AND REPLACED TRIPLE INDICATO RPM IAW AMM 62-41-00, 4-3. MOC SUCCESSFULLY COMPLETED.
- [SDR QR9R2025052900002](https://openairdocs.org/sdr/QR9R2025052900002.md): Transducer · failed · May 29, 2025 · Bolkms BK117C2
  > #2 TRANSMISSION OIL PRESSURE GUAGE REDUCED TO 1.0 IN FLIGHT. REMOVED AND REPLACED #2 PRESSURE TRANSDUCER IAW AMM 63-41-00, 4-4; MOC COMPLETED IAW RFM.
- [SDR QR9R2025052000001](https://openairdocs.org/sdr/QR9R2025052000001.md): Indicator · stuck · May 20, 2025 · Bolkms BK117C2
  > #1 ENGINE N2 STUCK AT 96%. SHUTDOWN ENGINES AFTER LANDING AND THE NEEDLE REMAINED AT 96%. ALL OTHER ENGINE INDICATIONS WERE NORMAL. A TEST FLIGHT EVAL FOUND BOTH NR AND #1 N2 NEEDLES ON TRIPLE TACH WERE INTERMITTENT. REMOVED AND REPLACED TRIPLE INDICATOR IAW A
- [SDR QR9R2025043000001](https://openairdocs.org/sdr/QR9R2025043000001.md): Indicator · stuck · Apr 30, 2025 · Bolkms BK117C2
  > #1 ENGINE TRIPLE TAC POINTER STUCK IN POSITION AT ABOUT 101%. REMOVED AND REPLACED TRIPLE INDICATOR RPM IAW AMM 62-41-00, 4-3. MTP MOC SUCCESSFULLY COMPLETED.
- [SDR QR9R2025040900002](https://openairdocs.org/sdr/QR9R2025040900002.md): Transducer · faulty · Apr 9, 2025 · Bolkms BK117C2
  > #1 TRANSMISSION OIL PRESSURE DROPPED BELOW 1.0 BAR DURING TAKEOFF. REMOVED AND REPLACED TRANSDUCER IAW AMM 63-41-00, 4-4. MOC COMPLETED, NO FLUCTUATIONS OR ANOMALIES NOTED.
- [SDR QMLA2025032120038](https://openairdocs.org/sdr/QMLA2025032120038.md): Warning Light · illuminated · Mar 21, 2025 · N775AL · Bell 407
  > TRANSMISSION CHIP LIGHT ILLUMINATED
- [SDR QR9R2025031400004](https://openairdocs.org/sdr/QR9R2025031400004.md): Transducer · faulty · Mar 14, 2025 · Bolkms BK117C2
  > #1 TRANSMISSION OIL PRESSURE DROPPED TO ZERO IN FLIGHT. REMOVED AND REPLACED TRANSDUCER IAW AMM 63-41-00, 4-4; MOC SUCCESSFULLY COMPLETED.
- [SDR QR9R2025031100002](https://openairdocs.org/sdr/QR9R2025031100002.md): Transducer · faulty · Mar 11, 2025 · Bolkms BK117C2
  > AT IIDLE (70% N1 + - 2) #2 TRANSMISSION OIL PSI WAS LESS THAN 1.0 BAR. TROUBLESHOOTING REVEALED #2 TRANSMISSION OIL PRESSURE TRANSDUCER BAD. REMOVED AND REPLACED TRANSDUCER IAW AMM 63-41-00, 4-4.
- [SDR QR9R2025030700002](https://openairdocs.org/sdr/QR9R2025030700002.md): Transmitter · failed · Mar 7, 2025 · Bolkms BK117C2
  > MAST MOMENT READING ON VEMD LANE 1 INOP DURING START RUN-UP. TROUBLESHOOTING FOUND THE SSTU FAILED DYN.KAL ON FUNCTIONAL TEST. REMOVED AND REPLACED SENSOR SIGNAL TRANSMITTING UNIT IAW AMM 63-42-00, 4-2.
- [SDR QR9R2025011700001](https://openairdocs.org/sdr/QR9R2025011700001.md): Transducer · fluctuates · Jan 17, 2025 · Bolkms BK117C2
  > FOUR SEPARATE EVENTS OF #2 XMSN OIL PRESSURE FLUCTUATION IN FLIGHT BELOW 1.5 BAR AND AS LOW AS 0.7. NO ASSOCIATED WARNING OR CAUTION LIGHTS. REMOVED AND REPLACED #2 TRANSMISSION PRESSURE TRANSDUCER IAW AMM 63-41-00, 4-4.
- [SDR QR9R2024101000004](https://openairdocs.org/sdr/QR9R2024101000004.md): Transducer · fluctuates · Oct 10, 2024 · Bolkms BK117C2
  > IN FLIGHT, #2 TRANSMISSION OIL PUMP PRESSURE FLUCTUATED DOWN TO.3 BAR AND THEN BACK TO NORMAL. FLUCTUATED MULTIPLE TIMES IN FLIGHT. REMOVED AND REPLACED #2 TRANSMISSION OIL TRANSDUCER IAW AMM 63-41-00, 4-4. T/F COMPLETD IAW AMM 05-60-00, 6-12.
- [SDR QR9R2024071600001](https://openairdocs.org/sdr/QR9R2024071600001.md): Transmitter · failed · Jul 16, 2024 · Bolkms BK117C2
  > SENSOR SIGNAL TRANSMITTING UNIT WAS RECEIVED NEW FROM AIRBUS. DURING MAST MOMENT PART 2 ADJUSTMENT- UNABLE TO MAINTAIN MAST MOMENT MINIMIZED BELOW 10%. MAST MOMENT FLUCTUATES MORE THAN 10% AFTER BEING MINIMIZED AS LOW AS 3% ON THE GROUND AT FLIGHT IDLE. SUBBED
- [SDR QR9R2024020600001](https://openairdocs.org/sdr/QR9R2024020600001.md): Pickup · failed · Feb 6, 2024 · Bolkms BK117C2
  > TRIPLE TACH ROTOR INDICATED 0% RPM AFTER REACHING GROUND IDLE CONDITIONS. REMOVED AND REPLACED SPEED PICK-UP. MOC COMPLETED IAW AMM 62-41-00, 4-1.
- [SDR QR9R2023092000001](https://openairdocs.org/sdr/QR9R2023092000001.md): Transducer · fluctuates · Sep 20, 2023 · Bolkms BK117C2
  > IN FLIGHT, #2 TRANSMISSION OIL PRESSURE WILL FLUCTUATE BETWEEN NORMAL, DOWN TO LESS THAN 1.5 BAR, THEN RETURN TO NORMAL. REMOVED AND REPLACED #2 TRANSMISSION PRESSURE TRANSDUCER, MOC SUCCESSFULLY COMPLETED.
- [SDR QR9R20220914002](https://openairdocs.org/sdr/QR9R20220914002.md): None · fluctuates · Sep 14, 2022 · Bolkms BK117C2
  > #2 TRANSMISSION OIL PRESSURE SYSTEM FAILED DURING FLIGHT. DISCONNECTED, INSPECTED, CLEANED AND RESEATED TRANSMISSION PRESSURE TRANSMITTER IAW AMM 70-43-00-110-801-A01. DURING TEST FLIGHT EVALUATION, #2 XMSN OIL PRESSURE FLUCTUATED FROM 2.0 TO.9. REMOVED AND R
- [SDR JBZA20220801001](https://openairdocs.org/sdr/JBZA20220801001.md): Transmitter · inoperative · Jul 29, 2022 · N315RX · Urocop EC135P2
  > CRUISE FLIGHT 1500' MSL MAIN TRANSMISSION OIL PRESSURE STARTED FLUCTUATING BETWEEN 1.1 & 2.8, MOMENTS LATER PRESSURE DROPPED TO ZERO, TRANSMISSION TEMPERATURE REMAINED NORMAL. ALL ENGINE INDICATIONS REMAINED NORMAL. MADE LANDING IN FIELD 6.5 NM SOUTHWEST OF K
- [SDR QR9R20220629001](https://openairdocs.org/sdr/QR9R20220629001.md): Transducer · low pressure · Jun 29, 2022 · Bolkms BK117C2
  > NO POSITIVE TRANSMISSION OIL PRESSURE AT GROUND IDLE ON ENGINE NUMBER 1. REMOVED AND REPLACED PRESSURE TRANSDUCER IAW AMM 63-41-00, 4-4. MOC SUCCESSFULLY COMPLETED.
- [SDR QR9R20220428002](https://openairdocs.org/sdr/QR9R20220428002.md): None · failed · Apr 28, 2022 · Bolkms BK117C2
  > DURING AVIONICS CONFIGURATION OF THE RUN-UP PROCEDURES, WITH ENGINES AT IDLE, THE MAST MOMENT INDICATOR DRIFTED OFF THE CIRCULAR SCALE 2 TIMES AND THEN THE CIRCULAR SCALE DISAPPEARED COMPLETELY, IMMEDIATELY NOTIFIED MAINTENANCE, THE AIRCRAFT WAS SHUT DOWN, THE
- [SDR QR9R20220422001](https://openairdocs.org/sdr/QR9R20220422001.md): None · pressure loss · Apr 22, 2022 · Bolkms BK117C2
  > START ABORTED DUE TO TRANSMISSION OIL PRESSURE WAS AT 0.0 BARS AFTER STARTING #1 ENGINE. REMOVED AND INSTALLED NEW PRESSURE TRANSDUCER IAW 63-41-00, 4-4. TEST FLIGHT SUCCESSFULLY COMPLETED.
- [SDR QR9R20220401001](https://openairdocs.org/sdr/QR9R20220401001.md): Transducer · pressure loss · Apr 1, 2022 · Bolkms BK117C2
  > #2 TRANSMISSION OIL PRESSURE REMAINED AT ZERO AFTER ENGINE START. REMOVED AND REPLACED #2 TRANSMISSION OIL PRESSURE TRANSDUCER. T/F MOC COMPLETED IAW RFM.
- [SDR QR9R20220223001](https://openairdocs.org/sdr/QR9R20220223001.md): Transducer · failed · Feb 23, 2022 · Bolkms BK117C2
  > DURING FLIGHT, # 2 XMSN OIL PRESSURE WENT TO ZERO. REMOVED AND REPLACED NO. 2 TRANSMISSION OIL PRESSURE TRANSDUCER. MOC AND LEAK CHECK SUCCESSFULLY COMPLETED IAW 05-60-00 6-12.
- [SDR QR9R20211029008](https://openairdocs.org/sdr/QR9R20211029008.md): None · fault message · Oct 29, 2021 · Bolkms BK117C2
  > FLT #1, WHILE CONDUCTING NORMAL HOVER FLIGHT ON HOVER TAXI LANE, MAST MOMENT EXCEEDANCE MESSAGE RECEIVED. MM INDICATED VISUALLY ON CAD SCREEN 71% AT THE 7 O'CLOCK POSITION. WITH MM EXCEED CAD CAUTION MESSAGE, THEN RETURNED TO NORMAL FOR ABOUT 2 SECONDS THEN MM
- [SDR QR9R20211021002](https://openairdocs.org/sdr/QR9R20211021002.md): Chip Detector · fault message · Oct 21, 2021 · Bolkms BK117C2
  > TRANSMISSION CHIP CAUTION LIGHT ILLUMINATED IN FLIGHT. MAINTENANCE REPLACED MAIN TRANSMISSION RH CHIP DETECTOR IAW AMM 63-41-00, 6-2.
- [SDR QR9R20210930003](https://openairdocs.org/sdr/QR9R20210930003.md): Transducer · faulty · Sep 30, 2021 · Bolkms BK117C2
  > #2 XMSN PRESSURE INDICATION STAYED AT 0.0 ONCE ENGINE WAS STARTED RESULTING IN AN ABORTED TAKEOFF. #2 PRESSURE TRANSDUCER REPLACED IAW AMM 63-41-00, 4-4; GROUND RUN SUCCESSFULLY COMPLETED.
- [SDR 8HBR20211012033](https://openairdocs.org/sdr/8HBR20211012033.md): Dual Tachometer · fluctuates · Sep 29, 2021 · N8340S · Robsin R22BETA
  > ENGINE SIDE OF DUAL TACHOMETER HAD INTERMITTENT INDICATION ISSUES.
- [SDR 8HBR20210920027](https://openairdocs.org/sdr/8HBR20210920027.md): Dual Tachometer · fluctuates · Sep 11, 2021 · N7155W · Robsin R22BETA
  > ENGINE SIDE OF DUAL TACHOMETER HAD INTERMITTENT INDICATION ISSUES.
- [SDR 8HBR20210920029](https://openairdocs.org/sdr/8HBR20210920029.md): Dual Tachometer · fluctuates · Sep 9, 2021 · N351JD · Robsin R22BETA
  > ENGINE SIDE OF DUAL TACHOMETER HAD INTERMITTENT INDICATION ISSUES.
- [SDR 8HBR20210920028](https://openairdocs.org/sdr/8HBR20210920028.md): Dual Tachometer · fluctuates · Sep 8, 2021 · N779SH · Robsin R22BETA
  > ENGINE SIDE OF DUAL TACHOMETER HAD INTERMITTENT INDICATION ISSUES.
- [SDR YV3R2020111900392](https://openairdocs.org/sdr/YV3R2020111900392.md): Horn · inoperative · Nov 13, 2020 · Robsin R44
  > CUSTOMER REPORTED HORN ASSEMBLY P/N: B320-6 IS INOPERATIVE.
- [SDR FKEA202008040353](https://openairdocs.org/sdr/FKEA202008040353.md): Indicator · inoperative · Jul 31, 2020 · N240SF · Bolkms BK117C2
  > AIRCRAFT WAS HOVERING WHEN PILOT NOTICED THERE WAS NO ROTOR RPM INDICATION WITH NO WARNING INDICATION AIRCRAFT WAS LANDED AND FLIGHT WAS ABORTED.
- [SDR 2020F00343](https://openairdocs.org/sdr/2020F00343.md): Indicator · inoperative · Jul 17, 2020 · N440SF · Bolkms BK117C2
  > AIRCRAFT WAS PULLED INTO A HOVER AND THE LOW ROTOR WARNING SOUNDED AND THE ROTOR RPM READ ZERO. AIRCRAFT LANDED AND FLIGHT WAS CANCELLED.
- [SDR HEER20200604815](https://openairdocs.org/sdr/HEER20200604815.md): Chip Detector · activated · Jun 3, 2020 · N935PH · Skrsky S92A
  > CHIP SYSTEM FAULT CAUTION LIGHT ILLUMINATED IN FLIGHT. CHECKED DRIVE TRAIN HUMS NR 2 INPUT CHIP.
- [SDR YV3R2020051800260](https://openairdocs.org/sdr/YV3R2020051800260.md): Horn · inoperative · May 1, 2020 · N888SN · Robsin R44
  > CUSTOMER REPORTED HORN ASSEMBLY P/N: B320-6 IN INOPERATIVE.
- [SDR YV3R2020052000263](https://openairdocs.org/sdr/YV3R2020052000263.md): Warning Horn · inoperative · Apr 29, 2020 · N888SN · Robsin R44
  > CUSTOMER REPORTED LOW WARNING R.P.M WARNING HORN P/N: B320-6 WAS INOPERATIVE.
- [SDR M3XA2020042303](https://openairdocs.org/sdr/M3XA2020042303.md): Sensor · dirty · Apr 22, 2020 · N456MT · Urocop EC135P2
  > PILOT REPORTED DURING CRUISE FLIGHT MAIN GEARBOX OIL PRESSURE INDICATED 0.1 BAR. MECHANIC TROUBLESHOT SYSTEM, CLEANED OIL PRESSURE SENSOR, INSPECTED AND CLEANED CONNECTOR TO SENSOR. PERFORMED OIL PRESSURE SENSOR FUNCTION CHECK WITH NO DEFECTS AND PERFORMED
- [SDR YV3R2020052000261](https://openairdocs.org/sdr/YV3R2020052000261.md): Warning Horn · inoperative · Apr 21, 2020 · N888SN · Robsin R44
  > CUSTOMER REPORTED LOW R.P.M WARNING HORN P/N: B320-6 WAS INOPERATIVE.
- [SDR AC2A2020012483901](https://openairdocs.org/sdr/AC2A2020012483901.md): Ring · unstaked · Jan 18, 2020 · N139FW · Agusta AB139
  > DURING DAILY INSPECTION, NOTICED RIGHT SIDE MAIN GEARBOX CHIP DETECTOR NOT FULLY ENGAGED. UPON INVESTIGATION, FOUND RETENTION RING FOR CHIP DETECTOR HAD BECOME UN-STAKED FROM CHIP DETECTOR BODY.
- [SDR QMLA2019091019074](https://openairdocs.org/sdr/QMLA2019091019074.md): Chip Detector · contaminated · Sep 10, 2019 · N135AN · Urocop EC135P2
  > SUPPLEMENTAL INFORMATION. WHILE ENROUTE TO HOSPITAL THE TRANSMISSION CHIP LIGHT CAME ON. A LANDING WAS CONDUCTED WITHOUT INCIDENT. VERY SMALL CHIP NOTED, DOCUMENTED AND SENT IN FOR ANALYSIS. THIS WAS THE FIRST FLIGHT SINCE THE AIR CONDITIONING DRIVE ADAPTER WA
- [SDR YV3R2019032300054](https://openairdocs.org/sdr/YV3R2019032300054.md): Warning Horn · defective · Mar 12, 2019 · Robsin R44RAVENII
  > CUSTOMER REPORTED LOW RPM WARNING HORN P/N: B320-6 WILL NOT WORK UNTIL TAPPED WHEN TESTING.
- [SDR O84A2018F00155](https://openairdocs.org/sdr/O84A2018F00155.md): Chip Detector · contaminated · Dec 3, 2018 · N240SF · Bolkms BK117C2
  > M/R GEARBOX CHIP LIGHT ILLUMINATED DURING HOVER. MECHANIC INSPECTED CHIP PLUGS AND FOUND NORMAL FUZZ PER MM. CLEANED CHIP PLUGS AND PERFORMED 10 MINUTE HOVER CHECK AND FOUND NO DEBRIS ON CHIP PLUGS. RETURNED AIRCRAFT TO SERVICE.
- [SDR M3XA2017092210](https://openairdocs.org/sdr/M3XA2017092210.md): Warning Light · false activation · Sep 22, 2017 · N242MT · Bell 407
  > PL FOR TRANSMISSION CHIP LIGHT INDICATION. REMOVED, CLEANED, AND INSPECTED. ALL TRANSMISSION CHIP DETECTORS, NO CHIPS FOUND. REMOVED AND INSPECTED THE TRANSMISSION OIL FILTER, NO EVIDENCE OF DEBRIS, REINSTALLED FILTER. PERFORMED 20 MINUTE GROUND RUN. NO DE
- [SDR M3XA2017081205](https://openairdocs.org/sdr/M3XA2017081205.md): Pressure Switch · defective · Aug 12, 2017 · N762MT · Bell 407
  > ON SHORT FINAL TO THE HOSPITAL THE PILOT HAD A TRANSMISSION OIL PRESSURE WARNING LIGHT ILLUMINATE ON THE CAUTION WARNING PANEL. HE DECIDED TO DIVERT TO THE LOCAL AIRPORT, WHERE HE LANDED WITHOUT INCIDENT WITH A PATIENT ONBOARD, WHICH WAS TRANSPORTED BY GROUND

Next page: https://openairdocs.org/jasc/6340/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 = '6340'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/jasc/6340/reports

---
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