# M1 Support Services: FAA repair station QR9R369D

- Type: FAA-certificated repair station (14 CFR Part 145)
- Certificate number: QR9R369D
- Designator: QR9R
- Name on the FAA list: M1 SUPPORT SERVICES
- Address: CAIRNS ARMY AIRFIELD, 30300 SPECKER STREET, FORT NOVOSEL, AL 36322
- Phone: (334) 598-0421
- Accountable manager: WOOD, BILL
- Liaison: WOODS, BILL, (334) 503-3278, woodb@frmaint.com
- On the FAA list: On the list of October 26, 2026; listed since October 26, 2026 or earlier (OpenAirDocs’ first copy)
- Service difficulty reports filed: 975
- Source: FAA Find a Facility dashboard, https://www.faa.gov/av-info/facility-dashboard
- Page: https://openairdocs.org/faa-repair-station/QR9R369D/m1-support-services

The FAA writes names in capitals; the mixed case here is OpenAirDocs'. The dashboard has no certificate dates, and nothing on it shows whether a certificate is in good standing.

## Ratings

- Airframe: Limited
- Powerplant: Limited
- Radio: Class 1 (Communication equipment); Class 2 (Navigational equipment); Limited
- Instrument: Class 1 (Mechanical); Class 2 (Electrical); Class 3 (Gyroscopic); Class 4 (Electronic)
- Accessory: Class 1 (Mechanical accessories); Class 2 (Electrical accessories); Class 3 (Electronic accessories)
- Limited: Nondestructive testing (Nondestructive inspection, testing and processing)

A Limited class covers only the makes and models in the station's operations specifications (14 CFR 145.61), which the FAA doesn't publish.

## Service difficulty reports (975, newest 50)

Filed under designator QR9R by a repair station (submitter type B).

- [SDR QR9R2026110900001](https://openairdocs.org/sdr/QR9R2026110900001), Nov 9, 2026: Bolkms BK117C2. SENSOR. OUT OF LIMITS. GENERATOR SPLIT PRIOR TO TAKEOFF. GEN1 READ 40, GEN 2 READ 125. A TEST FLIGHT EVAL FOUND #2 AMP JUMPED UP FROM 40 AMP TO
- [SDR QR9R2026110500004](https://openairdocs.org/sdr/QR9R2026110500004), Nov 5, 2026: Bolkms BK117C2. TRANSDUCER. FAULTY. XMSN PSI ON #2 SIDE WAS IN THE CAUTION RANGE AT 1.3 PSI. IT OCCURED AT 2500 FT APPROXIMATELY .7 INTO FLIGHT. TROUBLESHOO
- [SDR QR9R2026110500003](https://openairdocs.org/sdr/QR9R2026110500003), Nov 5, 2026: Bolkms BK117C2. SENSOR. OUT OF LIMITS. GEN AMPS SYSTEM 1 WOULD NOT STABILIZE DURING START RUN-UP. TROUBLESHOOTING REVEALED #1 HALL SENSOR WAS BAD. 15 AMP DIFFE
- [SDR QR9R2026110500002](https://openairdocs.org/sdr/QR9R2026110500002), Nov 5, 2026: Bolkms BK117C2. ACTUATOR. FAILED. A/C FAILED AP TEST DURING START RUN-UP. TROUBLESHOOTING FOUND PITCH 2 SEMA BAD. AP2 FAULT WHEN POWER APPLIED AND FAILS A
- [SDR QR9R2026110500001](https://openairdocs.org/sdr/QR9R2026110500001), Nov 5, 2026: Bolkms BK117C2. DISPLAY. FAULTY. #1 GENERATOR AMPS FLUCTUATING, EVEN GOING TO ZERO DURING START RUN-UP. TROUBLESHOOTING FOUND VEMD BAD CAUSING #1 GEN AMP
- [SDR QR9R2026110400003](https://openairdocs.org/sdr/QR9R2026110400003), Nov 4, 2026: Bolkms BK117C2. TRIM MOTOR. FAILED. AP TEST FAILED MULTIPLE TIMES. TROUBLESHOOTING DETECTED YAW TRIM MOTOR MOVES INTERMITTENTLY. REMOVED AND REPLACED YAW TR
- [SDR QR9R2026110400002](https://openairdocs.org/sdr/QR9R2026110400002), Nov 4, 2026: Bolkms BK117C2. ACTUATOR. FAULTY. ACTUATOR CAUTION ILLUMINATED DURING FLIGHT. DURING TEST FLIGHT RECOVERY, ACTUATOR CAUTION AND "Y" ON BOTH PFDS APPEARED.
- [SDR QR9R2026110400001](https://openairdocs.org/sdr/QR9R2026110400001), Nov 4, 2026: Bolkms BK117C2. GYRO. FAULTED. DURING RUN-UP, YAW SAS AND BACKUP SAS CAUTION ILLUMINATED AND DISAPPEARED MULTIPLE TIMES. SAS/AP CUT DID NOT RESOLVE. AV
- [SDR QR9R2026110200002](https://openairdocs.org/sdr/QR9R2026110200002), Nov 2, 2026: Bolkms BK117C2. ACTUATOR. FAILED. AUTOPILOT ACTUATOR FAIL AND FORCE TRIM RELEASE STUCK DURING INFLIGHT. TROUBLESHOOTING FOUND YAW SEMA ACTUATOR TO BE BAD.
- [SDR QR9R2026110200001](https://openairdocs.org/sdr/QR9R2026110200001), Nov 2, 2026: Bolkms BK117C2. BLEED VALVE. NO INDICATION. #2 BLEED VALVE FLAG NOT INDICATED PRIOR TO TAKEOFF IAW AIRCRAFT CL. A TEST FLIGHT EVAL FOUND #2 BLEED VALVE FLAG FAILED 
- [SDR QR9R2026102800003](https://openairdocs.org/sdr/QR9R2026102800003), Oct 28, 2026: Bolkms BK117C2. ACTUATOR. FAILED. AP TEST FAILED, PITCH ACTUATOR DURING PREFLIGHT. TROUBLESHOOTING REVEALED THE PITCH 2 SEMA HAD A VALID SIGNAL IN BUT NO 
- [SDR QR9R2026102800002](https://openairdocs.org/sdr/QR9R2026102800002), Oct 28, 2026: Bolkms BK117C2. DISPLAY. FAILED. INTERMITTENT MASTER CAUTION ON ENGINE 2 IN FLIGHT JUST AFTER TAKEOFF. NO CAD INDICATIONS. TROUBLESHOOTING FOUND THE VEMD
- [SDR QR9R2026102800001](https://openairdocs.org/sdr/QR9R2026102800001), Oct 28, 2026: Bolkms BK117C2. ACTUATOR. FAILED. WHILE LIFTING OFF PAD THE YAW ACTUATOR FAILED. MAINTENANCE ATTEMPTED TO TROUBLESHOOT BUT FAILURE REMAINED. REMOVED AND R
- [SDR QR9R2026102700001](https://openairdocs.org/sdr/QR9R2026102700001), Oct 27, 2026: Bolkms BK117C2. AIR DATA MODULE. OUT OF LIMITS. NR 1 & 2 AIRSPEED TAPES WILL INDICATE UP TO A 25 KIAS SPLIT WHILE IN FLIGHT. THE TAPES WILL OCCASIONALLY MATCH THEN SPLI
- [SDR QR9R2026102200003](https://openairdocs.org/sdr/QR9R2026102200003), Oct 22, 2026: Bolkms BK117C2. SENSOR. FAILED. NR NEEDLE DROPPED TO ZERO INTERMITTENTLY AFTER 1.5 HRS OF FLIGHT. REMOVED AND REPLACED #1 XMSN SPEED PICK UP SENSOR IAW 
- [SDR QR9R2026102200002](https://openairdocs.org/sdr/QR9R2026102200002), Oct 22, 2026: Bolkms BK117C2. BLEED VALVE. NO INDICATION. NO BLEED VALVE FLAG INDICATED ON ENG 1. A TEST FLIGHT EVAL FOUND #1 BLEED VALVE FLAG INDICATES IN REVERSE OF WHAT CONFIG
- [SDR QR9R2026102200001](https://openairdocs.org/sdr/QR9R2026102200001), Oct 22, 2026: Bolkms BK117C2. BRACKET. BROKEN. PRIOR TO TAKEOFF, CO-PILOT DOOR STRUT SEPERATED FROM DOOR END. MOUNT ON DOOR WAS FOUND TO BE BROKEN. REMOVED AND REPLACE (N895AE)
- [SDR QR9R2026101900001](https://openairdocs.org/sdr/QR9R2026101900001), Oct 19, 2026: Bolkms BK117C2. TRANSCEIVER. INOPERATIVE. RADIO NR 4 INOPERATIVE, DURING START RUN-UP. REMOVED AND REPLACED TRANSCEIVER RT5000/P25; MOC SUCCESSFULLY COMPLETED.
- [SDR QR9R2026101400001](https://openairdocs.org/sdr/QR9R2026101400001), Oct 14, 2026: Bolkms BK117C2. HEADREST. BROKEN. DURING POSTFLIGHT INSPECTION, PILOT HEAD REST WAS FOUND TO BE BROKEN AT BASE. REPLACED HEAD REST ASSEMBLY IAW CMM 25-10-
- [SDR QR9R2026100700001](https://openairdocs.org/sdr/QR9R2026100700001), Oct 7, 2026: Bolkms BK117C2. ACTUATOR. FAILED. CYCLIC TRIM FAILED MULTIPLE TIMES WHILE AT A HOVER. REMOVED AND REPLACED DUPLEX TRIM ACTUATOR IAW AMM 22-10-00, 4-8; MOC
- [SDR QR9R2026100600001](https://openairdocs.org/sdr/QR9R2026100600001), Oct 6, 2026: Bolkms BK117C2. SKID SHOE. MISALIGNED. MOUNTING HOLES ON FWD END OF SKID SHOE ARE OUT OF ALIGNMENT BY 1/4".
- [SDR QR9R2026100500001](https://openairdocs.org/sdr/QR9R2026100500001), Oct 5, 2026: Bolkms BK117C2. ACTUATOR. FAILED. A/C FAILED AUTOPILOT TEST; YAW SAS AND BACKUP SAS ACTUATORS. A TEST FLIGHT EVAL FOUND AUTOPILOT FAILS SELFTEST. INDICATE
- [SDR QR9R2026093000002](https://openairdocs.org/sdr/QR9R2026093000002), Sep 30, 2026: Bolkms BK117C2. WARNING UNIT. MALFUNCTIONED. UNKNOWN MALFUNCTION 1 MASTER CAUTION (RIGHT SIDE) WITH NO INDICATION ON CAD. AIRBUS RESET DONE WITH SOME RESULT UPON LEV
- [SDR QR9R2026093000001](https://openairdocs.org/sdr/QR9R2026093000001), Sep 30, 2026: Bolkms BK117C2. ACTUATOR. FAILED. SAS A/P CUT FAILURE; YAW SAS AND BACKUP SAS ACTUATOR FAILURE DURING START RUNUP. A TEST FLIGHT EVAL FOUND DURING AUTOPIL
- [SDR QR9R2026092900001](https://openairdocs.org/sdr/QR9R2026092900001), Sep 29, 2026: Bolkms BK117C2. DISPLAY. INTERMITTENT. FLT 2: ON START UP, PILOT SIDE ND DISPLAY FLICKERING AND UNREADABLE. REMOVED AND REPLACED SMD 45 IAW AMM 31-60-00, 4-2.
- [SDR QR9R2026092500001](https://openairdocs.org/sdr/QR9R2026092500001), Sep 25, 2026: Bolkms BK117C2. ACTUATOR. FAILED. IN FLIGHT TRIM ACTUATOR FAIL MESSAGE WITH BACK UP SAS AND YAW TRIM CIRCUIT BREAKER POP. UNABLE TO RESET. DURING RECOVERY
- [SDR QR9R2026092400001](https://openairdocs.org/sdr/QR9R2026092400001), Sep 24, 2026: Bolkms BK117C2. CONTROL LEVER. GOUGED. CONTROL LEVER ASSEMBLY WAS RECEIVED FROM SUPPLY WITH 2 GOUGES IN FLOATIND BUSHING BORE.
- [SDR QR9R2026092300001](https://openairdocs.org/sdr/QR9R2026092300001), Sep 23, 2026: Bolkms BK117C2. BLADE. FAILED. M/R BLADE WAS RECEIVED FROM SUPPLY AND FAILED RESISTANCE CHECK.
- [SDR QR9R2026092200002](https://openairdocs.org/sdr/QR9R2026092200002), Sep 22, 2026: Bolkms BK117C2. ACTUATOR. FAILED. ACTUATOR CAUTION LIGHT ILLUMINATED CENTER POSITION ON THE CAD WITH CORRESPONDING AMBER Y ON PFD. TROUBLESHOOTING REVEALE
- [SDR QR9R2026092200001](https://openairdocs.org/sdr/QR9R2026092200001), Sep 22, 2026: Bolkms BK117C2. FUEL CONTROL. FLUCTUATES. CONTINUAL NEEDLE SPLIT GREATER THAN 15% CAUSING VAR NR CAUTION TO COME ON DURING HOVERING FLIGHT. A TEST FLIGHT EVAL FOU
- [SDR QR9R2026091800001](https://openairdocs.org/sdr/QR9R2026091800001), Sep 18, 2026: Bolkms BK117C2. ACTUATOR. FAILED. ACTUATOR CAUTION ILLUMINATED AND WAS STILL PRESENT AFTER SHUTTING DOWN THE ACFT AND RE-STARTING. DURING TEST FLIGHT EVAL
- [SDR QR9R2026091600002](https://openairdocs.org/sdr/QR9R2026091600002), Sep 16, 2026: Bolkms BK117C2. AIR DATA MODULE. INACCURATE. RIGHT AIRSPEED INDICATOR INDICATED 30+ KNOTS CONSISTENTLY, ALL OTHER AIRSPEED INDICATORS INDICATED 0. MAINTENANCE ATTEMP
- [SDR QR9R2026091600001](https://openairdocs.org/sdr/QR9R2026091600001), Sep 16, 2026: Bolkms BK117C2. SENSOR. INTERMITTENT. LOW ROTOR RPM LT AND AUDIO INTERMITTENTLY ACTIVE WHILE HOVER TAXIING, ALL OTHER INDICATIONS WERE NORMAL. A TESTFLIGHT EV
- [SDR QR9R2026091500001](https://openairdocs.org/sdr/QR9R2026091500001), Sep 15, 2026: Bolkms BK117C2. WINDSHIELD WIPER. STUCK. WINDSHIELD WIPER STUCK IN FAR RIGHT POSITION OBSTRUCTING CO-PILOTS VIEW. REMOVED AND REPLACED WIPER ARM IAW AMM 30-40-00
- [SDR QR9R2026091100002](https://openairdocs.org/sdr/QR9R2026091100002), Sep 11, 2026: Bolkms BK117C2. CONTROL BOX. FAULTY. ROTOR RPM REMAINED IN LOW RED RANGE (95%) IN FLIGHT. LOW ROTOR RPM LIGHT AND HORN CAME ON INTERMITTENTLY. REMOVED AND RE
- [SDR QR9R2026091100001](https://openairdocs.org/sdr/QR9R2026091100001), Sep 11, 2026: Bolkms BK117C2. ACTUATOR. STICKING. ON LIFTOFF, ACTUATOR CAUTION CAME ON. WHEN TRYING TO BUILD BACK UP, THE YAW CAUTION ON THE PFD WAS ILLUMINATED, HOWEVER,
- [SDR QR9R2026091000002](https://openairdocs.org/sdr/QR9R2026091000002), Sep 10, 2026: Bolkms BK117C2. AIR DATA MODULE. OUT OF TOLERANCE. #2 ADC FAILURE INDICATION DURING TAKEOFF. TROUBLESHOOTING REVEALED #2 ADC TO BE OUT OF TOLERANCE. REMOVED AND REPLACED A
- [SDR QR9R2026091000001](https://openairdocs.org/sdr/QR9R2026091000001), Sep 10, 2026: Bolkms BK117C2. TRANSDUCER. FLUCTUATES. #2 XMSN PRESSURE INDICATION ON CPDS ERRATIC DURING GROUND RUN. INDICATION FLUCTUATED BETWEEN 0.0 AND 5.0 BAR RANDOMLY. R
- [SDR QR9R2026090900001](https://openairdocs.org/sdr/QR9R2026090900001), Sep 9, 2026: Bolkms BK117C2. TRANSMITTER. FAILED. DURING RUN UP, FUEL QUANTITY DEGRADED, CAUTION LIGHT WAS ON AND COULD NOT BE RESET. FWD FUEL QUANTITY TRANSMITTER IN FWD
- [SDR QR9R2026090300002](https://openairdocs.org/sdr/QR9R2026090300002), Sep 3, 2026: Bolkms BK117C2. GCU. FAILED. ON APPROACH, GEN DISCON ON CAD AND GEN AMPS DROPPED TO 0.0 ON SYSTEM #2. TROUBLESHOOTING CONFIRMED THE #2 GCU TO BE BAD.
- [SDR QR9R2026090300001](https://openairdocs.org/sdr/QR9R2026090300001), Sep 3, 2026: Bolkms BK117C2. TRANSCEIVER. FAULTY. DURING FLIGHT, #4 RADIO COULD RECEIVE BUT WAS INTERMITTENT ON TRANSMIT. REMOVED AND REPLACED TRANSCEIVER IAW CMM BK 117 
- [SDR QR9R2026090200001](https://openairdocs.org/sdr/QR9R2026090200001), Sep 2, 2026: Bolkms BK117C2. SENSOR. FAULTY. GEN SPLIT +10 LOW ON #2. A TEST FLIGHT EVAL FOUND #2 GEN AMPS DISPLAY 10 AMPS IN COCKPIT WHILE AMP CLAMP SHOWS 40 AMPS. 
- [SDR QR9R2026090100001](https://openairdocs.org/sdr/QR9R2026090100001), Sep 1, 2026: Bolkms BK117C2. ACTUATOR. FAILED. AP1/TRIM FAIL DURING AUTOPILOT TEST, WITH "P" INDICATOR. REMOVED AND REPLACED DUPLEX TRIM ACTUATOR IAW AMM 67-14-00, 4-1
- [SDR QR9R2026082800001](https://openairdocs.org/sdr/QR9R2026082800001), Aug 28, 2026: Bolkms BK117C2. REU. FAILED. WHILE AT HOVER, COMM #2 WOULD NOT TRANSMIT FROM COPILOTS STATION, NO SIDE TONE OR TX INDICATED PILOTS STATION COULD XMIT
- [SDR QR9R2026082600003](https://openairdocs.org/sdr/QR9R2026082600003), Aug 26, 2026: Bolkms BK117C2. SENSOR. OUT OF LIMITS. GEN AMP DIFFERENCE OF 25 AMPS DURING PRE TAKEOFF CHECKS, ENGINES AT FLIGHT. AVIONICS TROUBLESHOT, BUT PROBLEM REMAINED, 
- [SDR QR9R2026082600002](https://openairdocs.org/sdr/QR9R2026082600002), Aug 26, 2026: Bolkms BK117C2. AHRS. FAILED. AHRS FAIL FLT 1. TEST FLIGHT EVAL FOUND AHRS DISC APPEARED MULTIPLE TIMES DURING A 0.2 HOVER FLIGHT. OTHER INDICATIONS W
- [SDR QR9R2026082600001](https://openairdocs.org/sdr/QR9R2026082600001), Aug 26, 2026: Bolkms BK117C2. CARTRIDGE. INOPERATIVE. F PUMP AFT CIRCUIT BREAKER POPPED TWICE DURING RUN-UP. REMOVED AND REPLACED FUEL PUMP CARTRIDGE IAW AMM 28-11-01, 4-5. M
- [SDR QR9R2026082400001](https://openairdocs.org/sdr/QR9R2026082400001), Aug 24, 2026: Bolkms BK117C2. TRANSMITTER. FAULTED. NO OIL PRESSURE OBSERVED ON TRANSMISSION NR 2 AFTER REACHING STABILIZED GROUND IDLE AFTER START OF ENGINE NR1. ABORTED T
- [SDR QR9R2026082100001](https://openairdocs.org/sdr/QR9R2026082100001), Aug 21, 2026: Bolkms BK117C2. SENSOR. FAILED. IN FLIGHT NR NEEDLE ON TRIPLE TAC FAILED. IN FLIGHT NR FLUCTUATED CONTINUOUSLY BETWEEN NORMAL RANGE AND 0 WITH ASSOCIATE
- [SDR QR9R2026082000001](https://openairdocs.org/sdr/QR9R2026082000001), Aug 20, 2026: Bolkms BK117C2. CABLE. BINDING. DURING INSTALLATION OF NEW N2 CABLE (NR 1 ENGINE) COULD NOT ACHIEVE SMOOTH CABLE MOVEMENT AFTER CABLE WAS ROUTED. REMOVE

All 975: https://openairdocs.org/faa-repair-station/QR9R369D/m1-support-services/reports.md

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