# Service difficulty reports: GE CF-34-1A

A list on [GE CF-34-1A](https://openairdocs.org/engine/ge-cf-34-1a.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 3 · 115 reports

- [SDR ASOA201001969](https://openairdocs.org/sdr/ASOA201001969.md): Smoke Detector · false indication · Dec 15, 2010 · N861AS · Cndair CL6002B19 · Smoke Detection
  > SMOKE TOILET CAUTION MSG ILLUMATED MOMENTARLY IN FLIGHT. R & R LAV SMOKE DETECTOR, OPS CK GOOD REF AMM 26-16-01.
- [SDR ASOA201001532](https://openairdocs.org/sdr/ASOA201001532.md): Lamp · burned out · Oct 10, 2010 · N859AS · Cndair CL6002B19 · Emergency Lighting
  > NR 4 POSITION EXTERIOR EMERGENCY LIGHT INOP. RELAMPED NR4 POSITION EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21.
- [SDR ASOA201001020](https://openairdocs.org/sdr/ASOA201001020.md): Attach Fitting · cracked · Jul 18, 2010 · N861AS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > FOUND ENGINE SUPPORT BEAM FWD CLIP AT LBL 9.5 HAS A CRACK APPROX.5" IN LENGTH NEAR LOWER FASTENER. R & R CLIP AT ESB AT LBL 9.5 FWD WEB IAW SRM 51-42-06 AND 51-42-22.
- [SDR ASOA201000332](https://openairdocs.org/sdr/ASOA201000332.md): Bulkhead · cracked · Feb 27, 2010 · N861AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > COMPLIED WITH A SPECIAL DETAILED INSP OF FS559.0 PRESSURE BULKHEAD WEB AND CAP ANGLE LOCAL TO BL9.0 AND BL18.0 LT AND RT IAW NDT MANUAL, PART 6, 53-41-201. (3) CRACKS NOTED LBL18 APPROX.2500" IN THE FRAME RADIUS, RBL18 APPROX.5" IN THE FRAME RADIUS AND RBL1
- [SDR CA090831001](https://openairdocs.org/sdr/CA090831001.md): Signal Cond Unit · faulty · Aug 18, 2009 · Cndair CL600* · Engine Oil Quantity
  > RT LOW OIL PRESSURE ON CLIMB-OUT, AFTER LANDING, RT ENGINE WAS DOWN 5 LITRES. OIL LEVEL RETURNED TO NORMAL (5 LITRES ADDED) AND NO FURTHER INCIDENTS. OIL LEVEL SIGNAL CONTROL UNIT WAS FOUND TO BE FAULTY, THERE FORE INDICATING FULL ALL THE TIME, SO NO OIL WAS
- [SDR DJFA2007133](https://openairdocs.org/sdr/DJFA2007133.md): Adg · burned · Nov 2, 2007 · N664CW · Cndair CL6012A12 · DC Generating System
  > DURING POST MAINTENANCE CHECK FLIGHT, CREW TESTED THE AIR DRIVEN GENERATOR SYSTEM (ADG). DURING THE TEST THE ADG FAILED LEAVING THE CREW IN COMPLETE ELECTRICAL BLACKOUT. ENGINE DRIVEN SYSTEM WAS BROUGHT BACK ON-LINE AND AIRCRAFT LANDED SAFELY. MAINTENANCE F
- [SDR WWQ2007F00001](https://openairdocs.org/sdr/WWQ2007F00001.md): Wire Harness · shorted · Aug 5, 2007 · N39CD · Cndair CL6002A12 · Landing Gear System Wiring
  > DURING APPROACH, THE CREW EXTENDED THE LANDING GEAR (NORMAL PROCEDURE). SEVERAL SECONDS AFTER THE GEAR EXTENSION THE NOSE LANDING GEAR DOWN AND LOCKED GREEN LIGHT EXTINGUISHED AND THE NOSE GEAR DOORS OPENED AND CLOSED. A FEW SECONDS LATER THE DOORS CYCLED AG
- [SDR 2007FA0000000](https://openairdocs.org/sdr/2007FA0000000.md): Engine · failed · Dec 1, 2006 · N388DB · Cndair CL6002A12 · Engine (Turbine/Turboprop)
  > RT ENGINE FAILURE AT T/O. ALL INDICATIONS WERE NORMAL ON ENGINE START AND TAXI. UPON THRUST ADVANCEMENT FOR TAKEOFF, AT APPROXIMATELY 60 PERCENT N1 WE HEARD AND FELT A COMPRESSOR STALL. THE THRUST LEVER WAS IMMEDIATELY RETARDED TO IDLE AND TEMPERATURES WERE NO
- [SDR 2006FA0000835](https://openairdocs.org/sdr/2006FA0000835.md): Inverter · misinstalled · Aug 11, 2006 · N372G · Cndair CL6002B16 · Cabin Equipment/Furnishings
  > THIS STATIC FREQUENCY INVERTER WAS INSTALLED IN THE STATED AIRCRAFT ON JUNE 2, 2006. AT THE TIME OF INSTALLATION, THE PART HAD BEEN OVERHAULED BY CONSOLIDATED AC SUPPLY CO, INC. UNDER WO NR 7314, DATED MAR 14,2006. THE STATIC FREQUENCY INVERTER FAILED ON AU
- [SDR CA060515002](https://openairdocs.org/sdr/CA060515002.md): Vent Line · corroded · May 3, 2006 · Cndair CL600* · Fuel Storage
  > (CAN) MASTER REFUEL PANEL CHECK TO CHECK VALVE FOR OP, FUEL CAME OUT OF LT NACA SCOOP APPROX 2 GALLON, THEN STOP. MAINT WAS ADVISE THIS WAS ONLY HAPPEN WHEN AC WAS PARKED OVERNIGHT. FIGURED THERE WAS A BAD O-RING IN VENT SYS. FUEL WAS DRAINED, FUEL PANELS REMO
- [SDR CA060515003](https://openairdocs.org/sdr/CA060515003.md): Vent Line · corroded · May 3, 2006 · Cndair CL6012A12 · Fuel Storage
  > (CAN) REFUELLING WAS C/O, MASTER REFUEL PANEL CHECK C/O TO CHECK VALVE FOR OPERATION, WHAT WAS NOTICED, FUEL CAME OUT OUT OF THE LT NACA SCOOP APPROXIMATE 2 GALLON, THEN STOP. MAINT WAS ADVISED,THIS WAS ONLY HAPPENING WHEN A/C WAS PARK OVERNIGHT. SO MAINT CREW
- [SDR CA051121001](https://openairdocs.org/sdr/CA051121001.md): Fuel Heater · cracked · Nov 21, 2005 · Cndair CL6012A12 · Fuel Heater
  > (CAN) FUEL LEAK AS BEEN FOUND ON SEVEN DAYS INSPECTION, TECHNICIAN HAS FOUND A CRACK IN A SOLDERED JOINT ON FUEL HEATER. THE FUEL HEATER HAS BEEN REPLACED AND THE AIRCRAFT RETURNED TO SERVICE.
- [SDR DJFA2005159](https://openairdocs.org/sdr/DJFA2005159.md): Bulkhead · cracked · Oct 19, 2005 · N627CW · Cndair CL6012A12 · Fuselage Main, Bulkhead
  > DURING A ROUTINE MAINTENANCE VISIT, A CRACK WAS DISCOVERED IN THE PRESSURE BULKHEAD WEB AT FUSELAGE STATION 409.00 WHILE PERFORMING AD 97-24-02. THE CRACK WAS REPAIRED IAW EO NR 601-53-10-266, AND IN CONJUNCTION WITH DRAWING K600-31904. THE AIRCRAFT WAS RETU
- [SDR COMA0560558](https://openairdocs.org/sdr/COMA0560558.md): Actuator · malfunctioned · Oct 17, 2005 · N804CA · Cndair CL6002B19 · Trailing Edge Flap Actuator
  > FLIGHT 5814 - FLAPS FAIL. REPLACED THE RT OB FLAP ACTUATOR.
- [SDR MASA200500354](https://openairdocs.org/sdr/MASA200500354.md): Oil System · low · May 14, 2005 · N652ML · Cndair CL6002B19 · Turbine Engine Oil System
  > CREW RETURNED TO FIELD FOR RT ENGINE OIL LOW PRESSURE. CREW DID NOT SHUT DOWN ENGINE. MX SERVICED ENGINE OIL.
- [SDR CA050413003](https://openairdocs.org/sdr/CA050413003.md): Element · broken · Apr 13, 2005 · Cndair CL6012A12 · Autopilot System
  > (CAN) DURING A SCHEDULED 1200-HOUR CHECK, A FUNCTIONAL TEST OF THE RIGHT THRUST REVERSER AUTO THROTTLE RETARDER WAS CARRIED OUT. THE RIGHT THROTTLE FAILED TO RETURN TO IDLE POSITION WITH THE THRUST REVERSERMANUAL DEPLOYMENT. UPON INVESTIGATION IT WAS DISCOVERE
- [SDR CA050406005](https://openairdocs.org/sdr/CA050406005.md): Actuator · leaking · Apr 6, 2005 · Cndair CL6012A12 · Landing Gear Actuator
  > (CAN) NOSE LANDING GEAR ACTUATOR LEAKING AT ROD END PISTON. LIFE LIMITED PART AT 19480 CYCLES. A/C RETURN TO BASE ON SPECIAL FLIGHT PERMIT WITH GEAR DOWN.
- [SDR CA050215012](https://openairdocs.org/sdr/CA050215012.md): Connector · loose · Feb 10, 2005 · Cndair CL6012A12 · Landing Gear Retraction/Extension System
  > (CAN) ON APPROACH, NLG WOULD NOT DEPLOY UPON NORMAL SELECTION OF LANDING GEAR DOWN. EMER EXTENSION WAS COMPLETED, AC LANDED WITHOUT FURTHER INCIDENT, FOUND THAT (NLG) SELECTOR VALVE WAS AT FAULT. PINS IN CONNECTION TO EXTEND SOLENOID WHICH CONTROLS DOWN SELE
- [SDR CA050125008](https://openairdocs.org/sdr/CA050125008.md): Access Door · distorted · Jan 19, 2005 · Cndair CL6012A12 · Electrical/Electronic Compartment Doors
  > (CAN) THIS AIRCRAFT WAS INSPECTED AND TESTED AND FOUND TO EXHIBIT UNACCEPTABLE NOSE AVIONICS ACCESS DOOR DEFORMATION IN EXTREME COLD CONDITIONS. THE DEGREE OF DOOR CORNER CURLING EXCEEDS THE MANUFACTURERS LIMITS FOR SKIN WAVINESS FOR RVSM CERTIFICATION. (THIS
- [SDR COMA0460445](https://openairdocs.org/sdr/COMA0460445.md): Outflow Valve · obstructed · Aug 3, 2004 · N804CA · Cndair CL6002B19 · Pressure Regulator/Outflow Valve
  > FLIGHT 4952 AIRCRAFT WILL NOT PRESSURIZE. FOUND SAFETY WIRE IN OUTFLOW VALVE. REMOVED WIRE AND PRESSURE CHECK WAS NORMAL.
- [SDR CA040729002](https://openairdocs.org/sdr/CA040729002.md): Generator · failed · Jul 27, 2004 · Cndair CL6012A12 · AC Generation System
  > DURING A ROUTINE POST MAJOR MAINTENANCE FLIGHT CHECK OF THE AIR DRIVEN TURBINE GENERATOR SYSTEM, THE SYSTEM FAILED TO TAKE THE ELECTRICAL LOAD, AS INDICATED BY THE AMMETER AND THE VOLTMETER, WHEN THE TURBINE WAS MANUALLY DEPLOYED. MAINTENANCE FINDINGS:- ADG O
- [SDR CA040603004](https://openairdocs.org/sdr/CA040603004.md): Aileron · mismanufactured · Jun 3, 2004 · Cndair CL6012A12 · Autopilot System
  > (CAN) WHILE INVESTIGATING A SNAG, DISCOVERED AN AILERON A/P QUADRANT ASSEMBLY P/N 40E22-84-1069-1 WHICH DID NOT MEET THE MANUFACTURER'S DRAWING IN THE INSTALLATION OF THE NR 1 COLLINS A/P SERVO, LOCATED IN THE LT MLG WHEEL WELL. FOR THE DISABLING OF THE NR1
- [SDR REX2004F00001](https://openairdocs.org/sdr/REX2004F00001.md): Apu · odor · Jun 1, 2004 · N8444F · Cndair CL6002B19 · Airborne Auxiliary Power Unit (APU) System
  > ELECTRICAL/AC SMOKE IN CABIN. EVACUATED AIRCRAFT-MECHANIC NOTIFIED. PERFORMED ENG RUNS/BLEED AIR CHECKS IAW. NO SMOKE NOTED. OK FOR SERVICE. SMOKE IN CABIN ON APU START WITH PACKS ON APU. DEFERRED APU IAW MEL, CAT C AUTHORIZATION NR 48877. DM48877 IS DU
- [SDR CA040423007](https://openairdocs.org/sdr/CA040423007.md): Potentiometer · intermittent · Apr 16, 2004 · Cndair CL6012A12 · Stall Warning System
  > (CAN) DURING TAKEOFF ROTATION, THE STICK SHAKER ACTIVATED ON THE LOW LEVEL, THE STALL PROTECT SYSTEM (SPS) WARBLER SOUNDED, THE SPS FAIL LIGHTS WENT TO A FLASH CYCLE AND THE STALL PUSH LIGHTS ACTIVATED. THE LT SPS NEEDLE WAS SWINGING BACK AND FORTH INTO THE S
- [SDR REXA04003](https://openairdocs.org/sdr/REXA04003.md): Oil System · low · Jan 31, 2004 · N8444F · Cndair CL6002B19 · Turbine Engine Oil System
  > FLIGHT CREW RECEIVED AN AURAL OIL PRESSURE WARNING FOR THE LEFT ENGINE. OIL PRESSURE WAS OBSERVED TO BE FLUCTUATING BETWEEN 25-30 PSI. FLIGHT CREW PERFORMED AN INFLIGHT SHUTDOWN, DECLARED AN EMERGENCY AND WAS DIVERTED TO TULSA. AN OTHERWISE UNEVENTFUL APPRO
- [SDR CA040321003](https://openairdocs.org/sdr/CA040321003.md): Window · failed · Jan 13, 2004 · Cndair CL6002B19 · Flight Compartment Windows
  > (CAN) THE LEFT SIDE WINDOW HAD SHATTERED. AN EMERGENCY DESCENT WAS TAKEN.THE REMAINDER OF THE FLIGHT, APPROACH AND LANDING WERE UNEVENTFUL. THE WINDOW WAS REPLACED. THE WINDOW IS OLDER VERSION.
- [SDR MASA200300509](https://openairdocs.org/sdr/MASA200300509.md): Light · inoperative · Dec 23, 2003 · N87353 · Cndair CL6002B19 · Emergency Lighting
  > CAPTAIN REPORTED A CABIN CEILING EMERGENCY LIGHT INOPERATIVE. MECHANIC RELAMPED. OP CHECKS GOOD
- [SDR CA031205003](https://openairdocs.org/sdr/CA031205003.md): Skin · damaged · Dec 1, 2003 · Cndair CL6002B19 · Wing, Plate/Skin
  > (CAN) DURING FTP STALLS, BUFFET WAS EXPERIENCED JUST PRIOR TO PUSHER ACTIVATION FOR BOTH THE CLEAN AND F20 STALLS. ADDITIONALLY A MILD LT WING DROP WAS EXPERIENCED ON THE F20 STALL. AFTER LANDING, SEALANT WAS OBSERVED TO HAVE SPREAD OUT OF THE LT WING LEADING
- [SDR CA031113001](https://openairdocs.org/sdr/CA031113001.md): Engine · shutdown · Oct 14, 2003 · Cndair CL6012A12 · Engine (Turbine/Turboprop)
  > (CAN) DURING CRUISE AT FL 390, THE RT ENGINE SHUTDOWN. THE CREW REPORTED ALL ENGINE PARAMETERS WERE NORMAL AT THE TIME AND NO MESSAGES OR CAUTIONS WERE POSTED. THE CREW DECENDED AND PERFORMED A SUCCESSFUL WINDMILL RELIGHT AT 10,000 FT. FOLLOWED BY AN UNEVENT
- [SDR JBXA03017](https://openairdocs.org/sdr/JBXA03017.md): Aileron · frozen · Sep 23, 2003 · N652ML · Cndair CL6002B19 · Aileron Control System
  > FLIGHT 5119 FROM PWM TO DCA PILOT REPORTED LT AILERON WAS FROZEN. PERFORMED DISCONNECT. ON DESCENT PILOTS RECONNECTED AND NO FURTHER PROBLEMS WERE REPORTED. PROBABILITY OF ICE ON CONTROL SURFACE OR CABLES. AIRCRAFT LANDED UNEVENTFULLY. MX PREFORMED FUNC
- [SDR CA030903006](https://openairdocs.org/sdr/CA030903006.md): Actuator · failed · Aug 27, 2003 · Cndair CL6012A12 · Elevator Tab Control System
  > (CAN) ATTEMPT TO TRIM AIRCRAFT NOSE UP OR NOSE DOWN CAUSED BOTH PITCH TRIM CHANNELS TO INDICATE (OFF). THUS HORIZONTAL PITCH TRIM SYSTEM DE-ACTIVATED.
- [SDR CA030122001](https://openairdocs.org/sdr/CA030122001.md): Fitting · broken · Jan 19, 2003 · Cndair CL6012A12 · Passenger/Crew Doors
  > (CAN) DOOR TENSION FITTING (UPPER FORWARD) BROKEN IN FLIGHT.
- [SDR CA021125002](https://openairdocs.org/sdr/CA021125002.md): Bearing · broken · Nov 11, 2002 · Cndair CL6012A12 · Aileron Control System
  > (CAN) DURING 300-600 HOURS INSPECTION AILERON PCU OPERATION TEST, FOUND AILERON QUADRANT IN RT WHEEL WELL IS NOISY (SNAPPING).AFTER REMOVING RT/ AILERON QUADRANT ASSEMBLY FOR INVESTIGATION, FOUND RT/ QUADRANT, BEARING IS DAMAGED (RACES HALF WAY ROUND). CHANGE
- [SDR CA021217006](https://openairdocs.org/sdr/CA021217006.md): Bearing · broken · Nov 11, 2002 · Cndair CL6012A12 · Aileron Control System
  > (CAN) DURING 300-600 HOUR INSPECTION AILERON PCU OPERATION TEST. FOUND AILERON QUADRANT IN RT WHEEL WELL IS NOISY (SNAPPING). AFTER REMOVING RT AILERON QUADRANT ASS FOR INVESTIGATION, FOUND RT QUADRANT ITEM 57 PAGE 27-11-00 FGURE 3 IN IPC BEARING IS DAMAGE (RA
- [SDR CA020925003](https://openairdocs.org/sdr/CA020925003.md): Wire Harness · exposed · Sep 18, 2002 · Cndair CL6012A12 · Fire Protection System Wiring
  > (CAN) WIRING HARNESS FOR THE ENGINE FIRE BOTTLE SQUIBS LOCATED IN THE APU AREA HAD EXPOSED WIRES WHERE THEHARNESS ENTERS THE CONNECTOR PLUG FOR THE SQUIB.
- [SDR SWIA200211107](https://openairdocs.org/sdr/SWIA200211107.md): Engine · overtemp · Aug 1, 2002 · N588SW · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > DURING TAKEOFF, LEFT ENGINE ITT WENT TO 907 DEGREES, FLASHING RED. ABORTED TAKEOFF. REMOVED AND REPLACED LEFT ENGINE IAW MM 71-00-00.
- [SDR CA020806002](https://openairdocs.org/sdr/CA020806002.md): Connector · failed · Jul 19, 2002 · Cndair CL6012A12 · Fuel Boost Pump
  > (CAN) AS A RESULT OF REPORTED "PUMP INOP" LIGHT AND ADAPTER OIL "HI TEMP" LIGHT, REPLACED THE APU BOOST PUMP. OPERATED NORMALLY FOR THE FIRST FEW TESTS BUT QUIT AGAIN. DISCOVERED NO POWER AT THE CONNECTOR INSIDE THE BOOST PUMP CANNISTER. THE FUEL WAS DRAIN
- [SDR CA020220012](https://openairdocs.org/sdr/CA020220012.md): Outflow Valve · failed · Feb 15, 2002 · Cndair CL6012A12 · Pressure Regulator/Outflow Valve
  > (CAN) OVERHAULED SECONDARY OUTFLOW VALVE FOR PRESSURIZATION SYSTEM WAS INSTALLED TO RECTIFY A POPPED CIRCUIT BREAKER. SYSTEM GROUND RUN CARRIED OUT AND AIRCRAFT DEPARTED A FEW DAYS LATER. UPON REACHING FL 230 FT PNF NOTICED CABIN PRESSURIZATION WAS AT MAX CABI
- [SDR M02023](https://openairdocs.org/sdr/M02023.md): Bulb · burned out · Feb 11, 2002 · N87353 · Cndair CL6002B19 · Emergency Lighting
  > DURING OVERNIGHT MAINTENANCE, IT WAS DISCOVERED THAT THE RIGHT FORWARD EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MECHANIC REMOVED AND REPLACED THE LIGHTS. OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (SW072002B1585)
- [SDR CA020207004](https://openairdocs.org/sdr/CA020207004.md): Bellcrank · Feb 6, 2002 · Cndair CL6012A12 · Passenger/Crew Doors
  > (CAN) DOOR HARD TO OPEN: INSPECTION FOUND CRANK ASSY CRACKED (P/N 600-31890-21) - PART CRACKED DUE TO IMPROPER INSTALLATION OF SB 601-0192 - DOGS OF LOST MOTION CRANK NOT CONTACTING DRIVE CRANK AND COLLAR SIMULTANIOUSLY. THIS CAUSED STRESS ON OPPOSITE EARS C
- [SDR CA020308012](https://openairdocs.org/sdr/CA020308012.md): Engine · failed · Jan 30, 2002 · Cndair CL6012A12 · Engine (Turbine/Turboprop)
  > (CAN) DURING FLIGHT INSPECTION OF ILS CLEARANCE ORBIT OF AIRFIELD IN SLIGHT BANK & 10-20 KTS TAILWIND NR 2 ENGINE SUDDENLY SHUTDOWN. A/C RETURNED & LANDED. ENGINEER TOOK LOOK AT ENGINE NOTHING SEEN ABNORMAL. OIL SYS CHECKED BECAUSE OF PREVIOUS EXPERIENCE WIT
- [SDR CA020207003](https://openairdocs.org/sdr/CA020207003.md): Brake · malfunctioned · Jan 18, 2002 · Cndair CL6012A12 · Brake Anti-Skid Section
  > (CAN) DURING TAXI- ANTI-SKID TEST FAILURE - WIRES BG15B20BLU & GB30B20WHT - SUSPECT CYCLIC FAILURE.
- [SDR CA011217020](https://openairdocs.org/sdr/CA011217020.md): Controller · burned · Dec 17, 2001 · Cndair CL6012A12 · Flight Environment Data
  > (CAN) AS AIRCRAFT WAS SITTING IN THE HANGER WITH POWER ON ADS HEATER CONTROL TURNED OFF SMOKE STARTED COMING OUT FROM CONTROLLER POWER WAS SHUT DOWN. C/B DID NOT POP I T ALSO TOOK OUT SOME DIMMING MODUALS.
- [SDR CA011113013](https://openairdocs.org/sdr/CA011113013.md): Contactor · burned · Nov 6, 2001 · Cndair CL6012A12 · AC Generation System
  > (CAN) AFTER STARTING ENGINES WENT AND TRANSFERED GENRATORS. TURNED ON NR 3A HYD PUMP LARGE POWER SURGE ABOUT 34KVA NR 3A HYD BREAKER POPPED. TURNED ON NR 1 HYD PUMP, HYD BREAKER POPPED, R/H SIDE WINDOW FAILED. ANY HEAVY LOAD ON RT BUS CREATED FAILERS. ALSO
- [SDR CA011101018](https://openairdocs.org/sdr/CA011101018.md): Indicator · failed · Sep 29, 2001 · Cndair CL6012A12 · Attitude and Direction Data System
  > (CAN) SMOKE IN CABIN WHEN AIRCRAFT IS PARKED AT BAGOTVILLE AIRPORT. A FAIL RESISTANCE HAS BEEN FOUND ON THE CABIN DISPLAY ALTITUDE REPORTER WHICH IS USED BY MEDICAL PERSONNEL FOR MEDEVAC PURPOSE ONLY.
- [SDR M01091](https://openairdocs.org/sdr/M01091.md): Light · inoperative · Aug 15, 2001 · N17175 · Cndair CL6002B19 · Lighting System
  > DURING A PREFLIGHT INSPECTION, THE CREW FOUND THE FIRST THREE SECTIONS OF THE FLOOR TRACK LIGHTING INOPERATIVE. MAINTENANCE CLEANED THE CONNECTIONS. OPS CHECKED GOOD AND THE AIRCRAFT RETURNED TO SERVICE.
- [SDR 2001FA0000174](https://openairdocs.org/sdr/2001FA0000174.md): Check Valve · damaged · Jun 1, 2001 · N604MU · Cndair CL6002B16 · APU Core Engine
  > DURING REPLACEMENT OF THE CHECK VALVE, FOUND PIECES OF CHECK VALVE FLAPPERS, REPLACED WITH PN 320-2832-1-1 SN 635 OPERATIONAL CHECKED SATISFACTORY. NOTE: ALL PIECES REMOVED.
- [SDR CA010403003](https://openairdocs.org/sdr/CA010403003.md): Beam · cracked · Mar 13, 2001 · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > (CAN) DURING C-CHECK A CRACK WAS FOUND IN THE ENGINE SUPPORT BEAM LOWER WEB BETWEEN FS 625.30 AND FS 640.00 NEAR LBL 36.20. THE CRACK WAS LOCATED IN THE CORNER OF ACCESS PANEL (P/N 601-35006-39) LANDING AND ENDED NEAR THE PANEL EDGE.
- [SDR COMA0160234](https://openairdocs.org/sdr/COMA0160234.md): Warning System · illuminated · Feb 10, 2001 · N958CA · Cndair CL6002B19 · Turbine Engine Bypass Section
  > RT ENGINE FAN VIB ICON ON EICAS. INSPECTED ENGINE AND FOUND NO DEFECTS. COULD NOT DUPLICATE.
- [SDR CA010213019](https://openairdocs.org/sdr/CA010213019.md): Smoke Detector · faulty · Jan 24, 2001 · Cndair CL6002B19 · Smoke Detection
  > (CAN) ON SHORT FINAL, SMOKE TOILET CAUTION MESSAGE CAME ON. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT ANY FURTHER EVENT.LAV SMOKE DETECTOR FOUND FAULTY & REPLACED.

Next page: https://openairdocs.org/engine/ge-cf-34-1a/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 engine_model_key = 'CF341A'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/ge-cf-34-1a/reports

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