# Service difficulty reports: Pratt & Whitney Canada PW207E

A list on [Pratt & Whitney Canada PW207E](https://openairdocs.org/engine/pratt-whitney-canada-pw207e.md).

Newest first. General aviation reporting is voluntary.

- [SDR CA160121022](https://openairdocs.org/sdr/CA160121022.md): Hose · cracked · Jan 21, 2016 · Doug MD900 · Engine Oil Cooler
  > (CAN) AFTER SHUT DOWN FOLLOWING A SHORT UNRELATED TEST FLIGHT, TRANSMISSION OIL WAS DISCOVERED COVERING THE TRANSMISSION DECK AND FLOWING DOWN THE SIDES OF THE FORWARD FUSELAGE. APPROXIMATELY 5 QUARTS OF THE 10 QUART CAPACITY IN THE MAIN TRANSMISSION HAD LEAKE
- [SDR CA151007018](https://openairdocs.org/sdr/CA151007018.md): Compressor · leaking · Sep 30, 2015 · Doug MD900 · Turbine Engine Compressor Section
  > (CAN) THE CREW OF THE HELICOPTER WAS FORCED TO MAKE AN EMERGENCY LANDING ON THE OUTSKIRTS OF PARIS DUE TO LEFT ENGINE LOW OIL PRESSURE AND SMOKE IN THE CABIN. TROUBLESHOOTING FOUND THE COMPRESSOR WET WITH OIL (POSSIBLY LEAKING FROM THE NR 3 BEARING CAVITY) AND
- [SDR CA150911004](https://openairdocs.org/sdr/CA150911004.md): Engine · power loss · Sep 5, 2015 · Engine (Turbine/Turboprop)
  > (CAN) DURING A FLIGHT TEST, AFTER ANNUAL CHECK, THE NR 1 ENGINE EXPERIENCED A LOSS OF TORQUE. NO OTHER DETAILS ARE AVAILABLE ON THE CIRCUMSTANCES. THE OPERATOR IS CURRENTLY DOWNLOADING ENGINE AND AIRFRAME DATA, TROUBLESHOOTING IS ON-GOING.
- [SDR CA141008011](https://openairdocs.org/sdr/CA141008011.md): Throttle · malfunctioned · Sep 21, 2014 · Doug MD900 · Power Lever
  > (CAN) UPON LANDING, THE PILOT LOWERED THE COLLECTIVE AND 1 ENGINE BEGAN TO ACCELERATE. THE PILOT RAISED THE COLLECTIVE TO APPLY TORQUE TO REDUCE ENGINE SPEED. THIS SEEMED TO LOWER THE SPEED MOMENTARILY. THE ENGINE THEN BEGAN TO ACCELERATE AGAIN, THE PILOT TU
- [SDR QMLA2014012214010](https://openairdocs.org/sdr/QMLA2014012214010.md): Transmission · making metal · Jan 22, 2014 · N902LC · Doug MD900 · Engine/Transmission Coupling
  > MULTIPLE MAIN TRANSMISSION CHIP LIGHTS, AFTER FOLLOWING CSP 900RMM 2 CHAPTER 63-20-00 & TABLE 601. CHIPS INDICATED ALL UNDER THE LIMITS OF THE CHAPTER BUT COME ON EACH AIRCRAFT RUN UP.
- [SDR CA130729002](https://openairdocs.org/sdr/CA130729002.md): Engine · power loss · Jul 15, 2013 · Doug MD900 · Engine (Turbine/Turboprop)
  > (CAN) AFTER DROPPING A SLINGED LOAD, THE NR 2 ENGINE FROZE AT HIGH TORQUE FOR 20 SEC. THE NR 1 ENGINE REDUCED POWER ACCORDINGLY BUT THE MAIN ROTOR OVERSPED TO 104 PERCENT. TROUBLESHOOTING IS ON-GOING.
- [SDR CA130617002](https://openairdocs.org/sdr/CA130617002.md): Engine · shutdown · Jun 10, 2013 · Doug MD900 · Engine (Turbine/Turboprop)
  > (CAN) THE PILOT REPORTED AN ELECTRONIC ENGINE CONTROL SHUTDOWN FROM THE LT ENGINE. THE PILOT REQUESTED MORE POWER FROM RT ENGINE TO FLY OVER THE CABLES IN FRONT OF HIM. THE PILOT COMPLETED AN UNEVENTFUL LANDING AND SHUTDOWN THE ENGINES.
- [SDR CA130508014](https://openairdocs.org/sdr/CA130508014.md): Screw · missing · May 3, 2013 · Doug MD900 · Tail Rotor System
  > (CAN) FOD DAMAGE TO NOTAR FAN. STATOR BLADE RETAINER SCREW FOUND MISSING.
- [SDR CA121211003](https://openairdocs.org/sdr/CA121211003.md): Compressor · seized · Dec 3, 2012 · Doug MD900 · Turbine Engine Compressor Section
  > (CAN) CREW COMPLAINED OF POPPING NOISE WHEN GOING FROM IDLE TO FLY CONDITION. MECHANIC CONFIRMED NOISE AND COMMENCED COMPRESSOR WASHES AND RINSES. DURING THE RINSE CYCLE SPOOL DOWN THE MECHANIC NOTED A LOUD AND ABRUPT GRINDING NOISE. HE TRIED TO ROTATE THE C
- [SDR CA120716009](https://openairdocs.org/sdr/CA120716009.md): Blade · fractured · Jul 8, 2012 · Doug MD900 · Turbine Section
  > (CAN) AFTER TAKINGOFF FROM THE ROOF OF A HOSPITAL, DURING THE TRANSITION PHASE, THE CREW HEARD A LOUD NOISE FOLLOWED BY A POWER LOSS AND NR 1 ENGINE SHUTDOWN. THE CREW FLEW THE ACFT SINGLE ENGINE (OEI) AND PERFORMED AN UNEVENTFUL RUN-ON LANDING AT AIRPORT.
- [SDR QMLA2011050911056](https://openairdocs.org/sdr/QMLA2011050911056.md): Impeller · damaged · May 9, 2011 · N902LC · Doug MD900 · Turbine Engine Compressor Section
  > PART OF THE GASKET OF THE INLET SCREEN CAME LOOSE AND WAS INGESTED INTO THE ENGINE. ONE BLADE ON THE COMPRESSOR HAD DAMAGE THAT CAUSED A LOUD WHINING NOISE WHEN THE ENGINE WAS OPERATED. THE ONLY DAMAGE THAT CAN BE OBSERVED IS THE COMPRESSOR BLADES. IT IS BE
- [SDR 2009FA0000440](https://openairdocs.org/sdr/2009FA0000440.md): Drive Shaft · corroded · Jan 30, 2009 · N902PD · Doug MD900 · Engine/Transmission Coupling
  > DURING AN ANNUAL INSP THE MAIN ROTOR DRIVE SHAFT AND DRIVE PLATE WHERE REMOVED TO SATISFY THE 12 MONTH REQUIREMENT. WHILE REMOVING THE DRIVE SHAFT IT WAS FOUND THAT THE GREASE COATING ON LWR DRIVE SPLINE WAS DISCOLORED AND DEGRADED. FURTHER INSP SHOWED MOIS
- [SDR 2006FA0000620](https://openairdocs.org/sdr/2006FA0000620.md): Hose · cracked · Jun 8, 2006 · N902PD · Doug MD900 · Main Rotor Mast/Swashplate
  > PILOT NOTICED TRANSMISSION OIL PRESSURE INDICATION DROPPED FROM GREEN TO YELLOW TO RED. MADE UNSCHEDULED LANDING. FOUND FWD LT TRANSMISSION OIL COOLER HOSE LEAKING. HOSE IS A FLEXIBLE STAINLESS STEEL HOSE WITH A STAINLESS STEEL OUTER BRAID. HOSE WAS INSPECTED
- [SDR 2006FA0000503](https://openairdocs.org/sdr/2006FA0000503.md): Hose · cracked · May 16, 2006 · N902PD · Doug MD900 · Main Rotor Gearbox
  > DISCOVERED MAIN TRANSMISSION OIL HOSE FROM OIL COOLER TO MAIN TRANSMISSION LEAKING FROM STEEL BRAIDING. PULLED BACK BRAIDING AND FOUND HOSE TO BE CRACKED. REPLACED LINE WITH NEW. LEAK CHECK OF NEW LINE WAS SATISFACTORY, P/N 900D3409526-105.
- [SDR 2006FA0000506](https://openairdocs.org/sdr/2006FA0000506.md): Hose · cracked · May 16, 2006 · N902PD · Doug MD900 · Main Rotor Gearbox
  > DISCOVERED MAIN TRANSMISSION OIL HOSE FROM OIL COOLER TO MAIN TRANSMISSION LEAKING FROM STEEL BRAIDING. PULLED BACK BRAIDING AND FOUND HOSE TO BE CRACKED. REPLACED LINE WITH NEW. LEAK CHECK OF NEW LINE WAS SATISFACTORY. P/N 900D3409526-105.
- [SDR 2006FA0000507](https://openairdocs.org/sdr/2006FA0000507.md): Beam · cracked · May 16, 2006 · N902PD · Doug MD900 · Main Rotor Head
  > DURING SCHEDULED INSPECTION FOUND FLEXBEAM CRACKED IN LEG OF FLEXBEAM. REJECTED FLEXBEAM IAW INSPECTION CRITERIA IN MAINTENANCE MANUAL. REPLACED WITH NEW FLEXBEAM.
- [SDR 2006FA0000508](https://openairdocs.org/sdr/2006FA0000508.md): Beam · cracked · May 16, 2006 · N902PD · Doug MD900 · Main Rotor Head
  > DURING SCHEDULED INSPECTION FOUND FLEXBEAM CRACKED IN LEG OF FLEXBEAM. REJECTED FLEXBEAM IAW INSPECTION CRITERIA IN MM. REPLACED WITH NEW FLEXBEAM.
- [SDR 2006FA0000501](https://openairdocs.org/sdr/2006FA0000501.md): Oil Cooler · leaking · May 16, 2006 · N902PD · Doug MD900 · Engine Oil Cooler
  > FOUND WETTING OIL MAIN TRANSMISSION/ENGINE OIL COOLER CORE. REMOVED AND SENT OUT FOR EVALUATION. COOLER FOUND TO HAVE INTERNAL CORROSION THAT CAUSED MATERIAL LOSS AND SUBSEQUENT LEAKING. REPLACED COOLER WITH NEW. LEAK CHECK WAS SATISFACTORY.
- [SDR L192006F00000](https://openairdocs.org/sdr/L192006F00000.md): Line · worn · Apr 14, 2006 · N911AC · Doug MD900 · Engine Bleed Air System
  > ON TRAINING FLIGHT, RT ENG FIRELIGHT CAME ON. PILOT COMPLIED WITH EMERGENCY PROCEDURES, THEN SHUT RT ENG DOWN AND DISCHARGED RT ENG FIRE BOTTLE, LANDED AC AND FIRE LIGHT WENT OUT. AC WAS CHECKED FOR FIRE IN ENG COMPT, NONE WAS FOUND. NO EVIDENCE OF FLAMES I
- [SDR 2006FA0000274](https://openairdocs.org/sdr/2006FA0000274.md): Hose · cracked · Mar 1, 2006 · N902PD · Doug MD900 · Main Rotor Gearbox
  > HOSE IS INSTALLED ON MD902 HELICOPTERS. MD P/N IS 900D3409526-105. HOSE IS USED FOR MAIN TRANSMISSION OIL COOLING. FOUND LARGE ACCUMULATION OF OIL ON TRANSMISSION DECK AFTER FLIGHT. HOSE WAS FOUND TO BE CRACKED IN ONE OF THE BELLOWS. (CORE OF HOSE IS STAIN
- [SDR 2005FA0000816](https://openairdocs.org/sdr/2005FA0000816.md): Hub · cracked · Jun 8, 2005 · N3PD · Doug MD900 · Main Rotor Head
  > DURING ACCOMPLISHMENT OF AD 2002-10-05- MAIN ROTOR UPPER HUB INSP FOUND (2) BOLT HOLES CRACKED AS DEPICTED IN MD HELICOPTERS SERVICE BULLETIN 900-072. CRACKS WERE FOUND USING MAGNIFIED VISUAL METHOD. HUB WAS SUBSEQUENTLY INSPECTED BY EDDY CURRENT METHOD TO V
- [SDR 2004FA0000938](https://openairdocs.org/sdr/2004FA0000938.md): Hub · cracked · Dec 16, 2004 · Doug MD900 · Main Rotor Head
  > DURING ACCOMPLISHMENT OF AD 2002-10-05 "MAIN ROTOR UPPER HUB INSP" FOUND BOLT HOLES CRACKED AS DEPICTED IN MD HELICOPTERS SERVICE BULLETIN 900-072. PART TOTAL TIME: 1852 HRS
- [SDR 2004FA0000940](https://openairdocs.org/sdr/2004FA0000940.md): Hub · cracked · Dec 16, 2004 · N902PD · Doug MD900 · Main Rotor Head
  > DURING ACCOMPLISHMENT OF A.D. 2002-10-05 " MAIN ROTOR UPPER HUB INSP." FOUND (3) OUT OF (10) BOLT HOLES CRACKED AS DEPICTED IN MD HELICOPTERS SERVICE BULLETIN 900-072. PART TOTAL TIME: 292 HRS
- [SDR 2004FA0000939](https://openairdocs.org/sdr/2004FA0000939.md): Beam · cracked · Dec 16, 2004 · N902PD · Doug MD900 · Main Rotor Head
  > DURING 100 HOUR INSPECTION, FOUND FLEX BEAM CRACKED IN AREA OF LEG GOING INTO UPPER HUB. REPLACED PART WITH UPDATED SERVICEABLE PART.
- [SDR 2004FA0000934](https://openairdocs.org/sdr/2004FA0000934.md): Fuel Cell · leaking · Dec 16, 2004 · N902PD · Doug MD900 · Fuel Storage
  > DURING TROUBLESHOOTING A FUEL LEAK FOUND THAT WHEN THE FUEL CELL WAS FLEXED, FUEL WOULD WEEP FROM EXTERIOR SURFACE. REMOVED FUEL CELL AND SENT OUT FOR TEST AND REPAIR. EVALUATION RESULTS SHOWED WEEPING/ POROUS CONDITION OVER 80 PERCENT OF THE CELL AND CELL TO
- [SDR PG9R097903](https://openairdocs.org/sdr/PG9R097903.md): Line · leaking · Oct 21, 2004 · N368PA · Doug MD900 · Turbine Engine Oil System
  > FOUND TO BE LEAKING A SMALL QUANTITY OF OIL/REPLACED OIL HOSE ASSY.
- [SDR PG9R97903](https://openairdocs.org/sdr/PG9R97903.md): Line · leaking · Oct 21, 2004 · N368PA · Doug MD900 · Hoses and Tubes
  > FOUND TO BE LEAKING A SMALL QUANTITY OF OIL/ REPLACED OIL HOSE ASSY. (K)
- [SDR 2004FA0000877](https://openairdocs.org/sdr/2004FA0000877.md): Rotor Head · cracked · Oct 12, 2004 · N3PD · Doug MD900 · Main Rotor Head
  > HAD VIBRATION (.7 IPS) CAUTION ON IDS DURING FLIGHT AND HIGH VIBRATION ON SHUT DOWN BETWEEN 30-40 PERCENT NR. INSPECTED MAIN ROTOR SYSTEM IAW MAINTENANCE MANUAL AND FOUND (3) OUT OF (5) FLEXBEAMS CRACKED. REPLACING FLEXBEAMS WITH NEW UPDATED FLEXBEAMS.
- [SDR 2004FA0000802](https://openairdocs.org/sdr/2004FA0000802.md): Drive Shaft · worn · Oct 12, 2004 · N3PD · Doug MD900 · Main Rotor Mast/Swashplate
  > DURING ACCOMPLISHMENT OF A 300 HR INSPECTION FOUND MAIN ROTOR DRIVE SHAFT UPPER DRIVE SPLINES WORN BEYOND MAINTENANCE MANUAL LIMITS. PART TOTAL TIME: 1478.9 HRS. REPLACED DRIVE SHAFT WITH NEW PART.
- [SDR 2004FA0000578](https://openairdocs.org/sdr/2004FA0000578.md): Hub · cracked · Jul 19, 2004 · N3PD · Doug MD900 · Main Rotor Head
  > DURING ACCOMPLISHMENT OF A.D. 2002-10-05, (MAIN ROTOR UPPER HUB INSP.) FOUND (2) OUT OF (10) HOLES CRACKED IN UPPER HUB FLANGE AS DEPICTED IN MFG SERVICE BULLETIN 900-072.
- [SDR 2004FA0000876](https://openairdocs.org/sdr/2004FA0000876.md): Rotor Head · cracked · Jul 19, 2004 · N3PD · Doug MD900 · Main Rotor Head
  > DURING ACCOMPLISHMENT OF AD 2002-10-05, "MAIN ROTOR UPPER HUB INSP", FOUND (2) OUT OF (10) HOLES CRACKED IN UPPER HUB FLANGE AS DEPICTED IN MD HELICOPTERS SERVICE BULLETIN 900-072 PART TOTAL TIME: 91.23 HRS.
- [SDR 2004FA0000324](https://openairdocs.org/sdr/2004FA0000324.md): Hub · cracked · Apr 21, 2004 · N3PD · Doug MD900 · Main Rotor Head
  > DURING ACCOMPLISHMENT OF AD 2002-10-05 (MAIN ROTOR UPPER HUB INSPECTION), FOUND (3) OUT OF (10) BOLT HOLES TO BE CRACKED AS DEPICTED IN MFG SERVICE BULLETIN 900-072. CRACKS START IN BOLT HOLE CHAMFER. PART TOTAL TIME: 102.0HOURS. REMOVED AND REPLACED UPPER HUB
- [SDR 2004FA0000322](https://openairdocs.org/sdr/2004FA0000322.md): Hub · cracked · Apr 13, 2004 · N3PD · Doug MD900 · Main Rotor Head
  > DURING ACCOMPLISHMENT OF AD2002-10-05 (MAIN ROTOR UPPER HUB INSP.) FOUND (3) OUT OF (10) BOLT HOLES CRACKED AS DEPICTED IN MFG SERVICE BULLETIN 900-072. CRACKS START IN BOLT HOLE CHAMFER. PART TOTAL TIME: 102.0 HRS.
- [SDR 2004FA0000323](https://openairdocs.org/sdr/2004FA0000323.md): Hub · cracked · Apr 13, 2004 · N3PD · Doug MD900 · Main Rotor Head
  > DURING ACCOMPLISHMENT OF AD2002-10-05 (MAINROTOR UPPER HUB INSP.) FOUND (3) OUT OF (10) BOLT HOLES CRACKED AS DEPICTED IN MFG SERVICE BULLETIN 900-072. CRACKS START IN BOLT HOLE CHAMFER. PART TOTAL TIME: 102.0 HRS.
- [SDR 2004FA0000332](https://openairdocs.org/sdr/2004FA0000332.md): Hub · cracked · Apr 13, 2004 · N3PD · Doug MD900 · Main Rotor Head
  > DURING ACCOMPLISHMENT OF AD2002-10-05 (MAINROTOR UPPER HUB INSP.) FOUND (3) OUT OF (10) BOLT HOLES CRACKED AS DEPICTED IN MFG SERVICE BULLETIN 900-072. CRACKS START IN BOLT HOLE CHAMFER. PART TOTAL TIME: 102.0 HRS.
- [SDR 2004FA0000331](https://openairdocs.org/sdr/2004FA0000331.md): Hub · cracked · Apr 13, 2004 · N3PD · Doug MD900 · Main Rotor Head
  > DURING ACCOMPLISHMENT OF AD 2002-10-05 (MAIN ROTOR UPPER HUB INSP.) FOUND (3) OUT OF (10) BOLT HOLES CRACKED AS DEPICTED IN SERVICE BULLETIN 900-072. CRACKS START IN BOLT HOLE CHAMFER. PART TOTAL TIME: 102 HRS.
- [SDR 2004FA0000801](https://openairdocs.org/sdr/2004FA0000801.md): Hub · cracked · Apr 13, 2004 · N3PD · Doug MD900 · Main Rotor Head
  > DURING ACCOMPLISHMENT OF AD 2002-10-05, MAIN ROTOR UPPER HUB INSP. FOUND (3) OUT OF (10) BOLT HOLES CRACKED AS DEPICTED IN SB 900-072. CRACKS START IN BOLT HOLE CHAMFER. PART TOTAL TIME: 102.0 HRS.
- [SDR 2004FA0000330](https://openairdocs.org/sdr/2004FA0000330.md): Hub · cracked · Mar 3, 2004 · N902PD · Doug MD900 · Main Rotor Head
  > DURING ACCOMPLISHMENT OF AD 2002-10-05 INSP. (MAIN ROTOR UPPER HUB INSP.) FOUND (2) OUT OF (10) FLANGE BOLT HOLES WITH CRACKS AS DEPICTED IN MFG SERVICE BULLETIN 900-072. CRACKS RUN RADIALLY FROM BOLT HOLE INWARD TO FLANGE EDGE. PART TOTAL TIME WAS 399.65 HRS.
- [SDR 2004FA0000163](https://openairdocs.org/sdr/2004FA0000163.md): Line · cracked · Feb 4, 2004 · N902PD · Doug MD900 · Main Rotor Gearbox
  > AIRCRAFT EXPERIENCED LOW TRANSMISSION OIL PRESSURE. DURING RUN-UP AND LEAK CHECK FOUND TRANSMISSION OIL COOLER LINE P/N 900D3409526105 TO BE LEAKING FROM UNDER STEEL BRADE. REPLACED OIL COOLER LINE, OPS AND LEAK CHECK WERE GOOD. CUT BACK STEEL BRADE ON OLD
- [SDR 2004FA0000095](https://openairdocs.org/sdr/2004FA0000095.md): Hub · cracked · Jan 8, 2004 · N3PD · Doug MD900 · Main Rotor Head
  > DURING ACCOMPLISHMENT OF A.D. 2002-10-05(MAIN ROTOR UPPER HUB INSPECTION)FOUND (6) OUT OF (10) UPPER FLANGE BOLT HOLES TO BE CRACKED. CRACKS RUN RADIALLY FROM BOLT HOLE TO INNER EDGE AS DEPICTED IN SB 900-072. PART TOTAL TIME: 435 HRS SINCE NEW. REPLACED UP
- [SDR 2003FA0000190](https://openairdocs.org/sdr/2003FA0000190.md): Filter · contaminated · Sep 17, 2001 · N902PD · Doug MD900 · Hydraulic System, Main
  > BYPASS PIN POPPED ON NR 1 HYDRAULIC RETURN FILTER. REMOVED FILTER AND INSPECTED FOR CONTAMINATION. REPLACED FILTER. OPS AND LEAK CHECK GOOD.
- [SDR 2003FA0000188](https://openairdocs.org/sdr/2003FA0000188.md): Indicator · defective · Sep 6, 2001 · N3PD · Doug MD900 · Hydraulic System, Main
  > AFTER INSTALLING NEW HYDRAULIC FILTER, THE RETURN SIDE BYPASS INDICATOR POPPED WITH NO PRESSURE APPLIED. AFTER RESETTING THE INDICATOR, INDICATOR POPPED AGAIN. REPLACED IMPENDING BY-PASS INDICATOR PN 071142-258. OPS CHECK GOOD.
- [SDR 2003FA0000187](https://openairdocs.org/sdr/2003FA0000187.md): Drive Link · worn · Jul 26, 2001 · N902PD · Doug MD900 · Main Rotor Head
  > MAIN ROTOR UPPER DRIVE LINK BEARING PLAY EXCEEDS MAINTENANCE MANUAL LIMITS.
- [SDR 2003FA0000186](https://openairdocs.org/sdr/2003FA0000186.md): Drive Link · worn · Jul 24, 2001 · N3PD · Doug MD900 · Main Rotor Head
  > MAIN ROTOR UPPER DRIVE LINK BEARING PLAY EXCEEDS MAINTENANCE MANUAL LIMITS.
- [SDR 2003FA0000184](https://openairdocs.org/sdr/2003FA0000184.md): Transmission · making metal · Jun 23, 2001 · N3PD · Doug MD900 · Main Rotor Gearbox
  > MAIN TRANSMISSION PRODUCING METAL CHIPS. CHIP SIZE EXCEED MAINTENANCE MANUAL LIMITS.

## 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 = 'PW207E'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/pratt-whitney-canada-pw207e/reports

---
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