# Service difficulty reports: GE CF34-8E5A1

A list on [GE CF34-8E5A1](https://openairdocs.org/engine/ge-cf34-8e5a1.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 4 · 194 reports

- [SDR CA190809017](https://openairdocs.org/sdr/CA190809017.md): Bushing · worn · Jun 11, 2019 · Emb ERJ170200SU · Turbine Engine Air Inlet Section
  > (CAN) FLIGHT CREW ADVISED MTCE THE THE #1 ENGINE WAS PERSISTENTLY APPROACHING (BUT NOT EXCEEDING) ITT LIMITS DURING STARTS. MOC REQUESTED AN INSPECTION OF THE VGV SYSTEM. AN UNUSUAL AMOUNT OF PLAY WAS FOUND IN ONE OF THE ACTUATORS (MASTER) ON REMOVAL THE ATTA
- [SDR CA190604019](https://openairdocs.org/sdr/CA190604019.md): Pcu · corroded · May 30, 2019 · Emb ERJ170200SU · Drag Control System
  > (CAN) SPOILER FAULT EICAS MESSAGE AFTER TOUCH DOWN,FLIGHT CONTROL NO DISPATCH MESSAGE FOLLOWED SHORTLY AFTER. AIRCRAFT OUT OF SERVICE, AOG. WAS TOWED TO HANGAR DURING T/S FOUND L/H WING O/B PCU CONNECTOR HEAVILY CORRODED AND ALSO CONNECTOR AIRFRAME SIDE MFS
- [SDR CA190502003](https://openairdocs.org/sdr/CA190502003.md): Rod · broken · Apr 22, 2019 · Emb ERJ170200SU · Trailing Edge Flap Control System
  > (CAN) DURING SERVICE CHECK, LEFT WING INB FLAP WAS FOUND LOWER THAN OTHER FLAP. INB AFT FLAP OUTB ROD WAS FOUND SHORTER THAN THE INB ROD. ROD WAS FOUND BROKEN IN HALF. REF: AIPC: 57-54-00-10 P/N: 171-03779-901. TRAX DEFECT 145287. THIS IS NOT THE FIRST TIME TH
- [SDR CA190304017](https://openairdocs.org/sdr/CA190304017.md): Duct · failed · Mar 1, 2019 · Emb ERJ170200SU · Pneumatic Distribution System
  > (CAN) #1 ENGINE PRE-COOLER INLET DUCT ASSY PART NUMBER 171-03352-405 FOUND CRACKED AND BLOWN OUT DURING A SCHEDULED INSPECTION. COMPOSITE PANEL FOUND BRITTLE DUE TO AGE, PANEL 170-03352-405 HAS BEEN REPLACED AND AC HAS BEEN RETURNED TO SERVICE.
- [SDR CA160215001](https://openairdocs.org/sdr/CA160215001.md): Bracket · out of alignment · Feb 14, 2016 · Cndair CL600* · Door Warning System
  > (CAN) DURING CLIMB OUT THE "DOOR UNLOCKED" LIGHT ILLUMINATED AT 1500 AGL. RETURN TO BASE AND UNEVENTFUL LANDING COMPLETED. DOOR UNLOCK ANNUNCIATION EXTINGUISHED DURING DESCENT. MAINTENANCE WAS NOT ABLE TO DUPLICATE CONDITION. MOST SUSPECT PART REPLACED - EXTER
- [SDR CA160205010](https://openairdocs.org/sdr/CA160205010.md): Line · leaking · Feb 3, 2016 · Emb ERJ170200SU · Turbine Engine Oil System
  > (CAN) AFTER ENGINE SHUTDOWN CREW REPORTED THAT NR 2 ENGINE OIL QUANTITY READS 4.1. THE CREW CARRIED OUT A WALK AROUND FOUND A PUDDLE OF OIL UNDER NR 2 ENGINE. MAINTENANCE WAS ADVISED AND ASKED TO INVESTIGATE/SERVICE OIL AS REQUIRED. CONTRACT MAINTENANCE FOUND
- [SDR CA151203005](https://openairdocs.org/sdr/CA151203005.md): Wire Harness · damaged · Nov 28, 2015 · Emb ERJ170200SU · Fire Protection System Wiring
  > (CAN) ON CLIMB OUT AT APPROXIMATELY 15000 FEET THE ENGINE NR 1 FIRE EICAS MESSAGE CAME ON ALONG WITH THE ALARM. #1 ENGINE SET TO IDLE AND MAYDAY DECLARED. CHECKLIST PERFORMED AND ENGINE WAS SHUT DOWN. BOTH EXTINGUISHERS WERE DISCHARGED. MAINTENANCE CARRIED OUT
- [SDR CA150731006](https://openairdocs.org/sdr/CA150731006.md): Brake · failed · Jul 31, 2015 · Emb ERJ170200SU · Brake
  > (CAN) DISPATCH REPORTED A FLIGHT INCIDENT THAT ON LANDING THE RT OUTBOARD BRAKE SHATTERED. ON TAXI IN TO GATE THE RT INBOARD BRAKE OVERHEATED. MAINTENANCE FOUND THE NR 4 BRAKE SHATTERED WITH SIGNIFICANT DAMAGE TO THE PISTONS AND LARGE SECTIONS OF A ROTOR AND P
- [SDR CA150703007](https://openairdocs.org/sdr/CA150703007.md): Wire · shorted · Jul 2, 2015 · Emb ERJ170200SU · Fuel System Wiring
  > (CAN) PILOT REPORTED THAT FUEL 2 LOW LEVEL - EICAS WARNING MESSAGE CAME ON. MEL 28-44-00 APPLIED ALLOWED THE AIRCRAFT TO RETURN TO SERVICE PROVIDED THAT ASSOCIATED FUEL QUANTITY INDICATIONS ON EICAS AND MFD ARE AVAILABLE AND ARE MONITORED THROUGHOUT FLIGHT.
- [SDR CA150616008](https://openairdocs.org/sdr/CA150616008.md): Insulation · unsecure · Jun 11, 2015 · Emb ERJ170200SU · Passenger Compartment Equipment
  > (CAN) AFTER B CHECK, DURING A FLIGHT, THERE WAS A PRESS AUTO FAULT MSG. THIS WAS RESET IAW THE FAULT ISOLATION MANUAL. DURING A FLIGHT THERE WAS ANOTHER PRESS AUTO FAIL MSG. WHILE TROUBLESHOOTING & INSPECTING, AN INSULATION BLANKET WAS FOUND STUCK IN THE OU
- [SDR CA150312004](https://openairdocs.org/sdr/CA150312004.md): Stop · cracked · Mar 10, 2015 · Emb ERJ170200SU · Aileron Control System
  > (CAN) WHILE DOING SCHEDULED INSPECTION TASKS ON "B" CHECK, A CRACK WAS FOUND IN THE RT AILERON UPPER TORQUE TUBE BEARING STOP. REPLACED WITH A NEW ONE.
- [SDR CA150209008](https://openairdocs.org/sdr/CA150209008.md): Wire Harness · failed · Jan 22, 2015 · Emb ERJ170200SU · Landing Gear System Wiring
  > (CAN) THE LANDING GEAR WOULD NOT RETRACT. CREW USED THE DOWNLOCK RELEASE BUTTON TO RETRACT THE GEAR AND THEN RETURNED FOR MAINTENANCE TO TROUBLESHOOT. THE FAULT CODE 32612301PSS DIRECTED MAINTENANCE TO THE RT MLG NR 2 WEIGHT ON WHEEL (WOW) SENSOR. THE SENSOR H
- [SDR CA150207002](https://openairdocs.org/sdr/CA150207002.md): Bearing · damaged · Jan 11, 2015 · Emb ERJ170200SU · Aileron Control System
  > (CAN) CREW REPORTED AILERONS STIFF. UPON FURTHER INSPECTION, MAINTENANCE FOUND UPPER BEARING REF IPC 27-11-07-06 ON LH FUSELAGE SECTOR TORQUE TUBE BEARING ASSY STIFF (METAL TO METAL CONTACT) REF IPC 27-11-07-01. MAINTENACE ALSO FOUND LH WING STUB AILERON FEEL
- [SDR CA141007006](https://openairdocs.org/sdr/CA141007006.md): Relay · burned · Sep 29, 2014 · Emb ERJ170200SU · Buffet/Galleys
  > (CAN) 1 COFFEMAKER IN THE FWD GALLEY HAD ELECTRICAL FLASHES AND ARCING EMANATING FOR THE RELAY AT THE BACK OF THE UNIT. A CLOUD OF BLACK SMOKE AND A BIG BLUE/YELLOW FLASH WAS SEEN BY THE CABIN CREW. THEY DISCHARGED A FIRE EXTINGUISHER ON BOTH COFFEMAKERS AND
- [SDR CA140916004](https://openairdocs.org/sdr/CA140916004.md): Connector · broken · Sep 11, 2014 · Emb ERJ170200SU · Ice/Rain Protection System Wiring
  > (CAN) THIS AIRCRAFT HAS HAD NUMEROUS REPORTS OF WING ANTI-ICE LEAK FROM THE LTSLAT 2 SENSOR CAUSING MANY OPERATIONAL INTERRUPTIONS AND DELAYS. ALL THE RECOMMENDED TROUBLESHOOTING WAS CARRIED OUT IAW THE FAULT ISOLATION MANUAL (FIM) WITHOUT ANY SUCCESS. BECAUSE
- [SDR CA140710004](https://openairdocs.org/sdr/CA140710004.md): Line · chafed · Jul 1, 2014 · Emb ERJ170200SU · Hydraulic System, Main
  > (CAN) FLIGHT CREW REPORTED NR 1 HYDRAULIC SYSTEM FLUID QUANTITY DEPLETING IN FLIGHT. AN EMERGENCY WAS DECLARED AND AIRCRAFT HAD AN UNEVENTFULL LANDING. POST LANDING INSPECTION BY MAINTENANCE FOUND CUSHION CLAMP MIGRATED AND CHAFFED SMALL PIN HOLE IN PRESSURE
- [SDR CA140508002](https://openairdocs.org/sdr/CA140508002.md): Sensor · failed · May 3, 2014 · Emb ERJ170200SU · Leading Edge Slat Position Indicating System
  > (CAN) A "SLAT FAIL" EICAS MESSAGE ON THE GROUND. ON THE 3RD A LT WING OTBD SLAT SKEW SENSOR WAS REPLACED. ALSO, RIGGING CHECKS WERE CARRIED OUT AND FAULT CLEARED. THE FOLLOWING DAY FLYING THE SAME MESSAGE APPEARED AND MAINTENANCE WAS SENT TO FIX THE FAULT.
- [SDR CA140421006](https://openairdocs.org/sdr/CA140421006.md): Pump · damaged · Apr 16, 2014 · Emb ERJ170200SU · Fuel Boost Pump
  > (CAN) FUEL 2 LO LEVEL WARNING EICAS MESSAGE WITTH LOTS OF FUEL IN TANK. EJECTOR ENGINE FEED PUMP REMOVED TO INSPECT FOR DEFECTS. CLAMP FLANGE ON FORWARD SIDE FOUND DAMAGED. IAW FIM TASK 28-21-00-810-8B-A, FUEL MAIN EJECTOR PUMP REPLACED IAW AMM 28-21-13-400
- [SDR CA140423001](https://openairdocs.org/sdr/CA140423001.md): Wire Harness · chafed · Apr 16, 2014 · Emb ERJ170200SU · Landing Gear System Wiring
  > (CAN) A "LANDING GEAR NO DISPATCH" MESSAGE WAS DISPLAYED. IT HAD OCCURRED EARLIER THAT DAY BUT WAS RESETTABLE IAW THE FIM 32-00-00-810-801-A. ANOTHER RESET WAS ATTEMPTED BUT THE CONDITION RETURNED SHORTLY AFTER PUSHBACK. TROUBLESHOOTING REVEALED A WIRE BROK
- [SDR CA140421003](https://openairdocs.org/sdr/CA140421003.md): Duct · cracked · Apr 14, 2014 · Emb ERJ170200SU · Pneumatic Distribution System
  > (CAN) AFTER T/O BLEED 2 OVERPRESS AMBER EICAS ALERT. CHECKLIST PROCEDURE CARRIED OUT WITH NO RELIEF. EMERGENCY DECLARED AND ACFT RETURNED TO DEPARTURE IAW CHECKLIST. MECHANIC ON RAMP DISCOVERED CRACKED T-DUCT. NR 2 ENGINE BLEED "T-DUCT" REPLACED IAW AMM 36
- [SDR CA140421005](https://openairdocs.org/sdr/CA140421005.md): Duct · cracked · Apr 12, 2014 · Emb ERJ170200SU · Pneumatic Distribution System
  > (CAN) RT ENGINE T-DUCT FOUND CRACKED, PN 170-14806-401, MECHANIC ON RAMP NOTED SOUND OF BLEED AIR LEAK DURING REGULAR SCHEDULED ENGINE OIL SERVICE CHECK. RT ENG T-DUCT, BLEED, REPLACED IAW AMM 36-11-04. OPS CHECK SERVICEABLE.
- [SDR CA140331008](https://openairdocs.org/sdr/CA140331008.md): Sensor · failed · Mar 18, 2014 · Emb ERJ170200SU · Leading Edge Slat Position Indicating System
  > (CAN) DURING CRUISE A "SLAT FAIL" FAILURE WARNING OCCURRED. BECAUSE OF THE ABNORMAL LANDING CONFIGURATION, SLATS UP, AN EMERGENCY WAS DECLARED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE FAULT IAW THE FIM 27-83-00-810-814-A AND FOUND THE
- [SDR CA140227002](https://openairdocs.org/sdr/CA140227002.md): Attach Fitting · broken · Feb 24, 2014 · Emb ERJ170200SU · Rudder/Tab, Attach Fittings
  > (CAN) RUDDER LOWER ATTACHMENT FITTING BROKEN, DISCOVERED DURING ROUTINE INSPECTION. CAUSE OF DAMAGE UNKNOWN AT THIS TIME.
- [SDR CA140225009](https://openairdocs.org/sdr/CA140225009.md): Sensor · failed · Feb 21, 2014 · Emb ERJ170200SU · Landing Gear Position and Warning
  > (CAN) AFTER TAKEOFF THE LANDING GEAR LEVER WOULD NOT GO UP. RETURNED FOR LANDING. CONTRACT MAINTENANCE DISCOVERED A FAULTY NLG WOW SENSOR. THIS WAS REPLACED AND ADJUSTED IAW AMM 32-62-01AND THE GEAR SWUNG SEVERAL TIMES SUCCESSFULLY. ACFT RELEASED FOR SERVICE
- [SDR CA140128011](https://openairdocs.org/sdr/CA140128011.md): Sensor · failed · Jan 24, 2014 · Emb ERJ170200SU · Landing Gear Position and Warning
  > (CAN) AFTER T/O DEPARTING, THE LANDING GEAR COULD NOT BE SELECTED UP. CREW PERFORMED THE CHECKLIST AND RETURNED. MOC WAS CONTACTED AND A SPECIAL FERRY PERMIT WAS APPLIED FOR AND GRANTED FOR A GEAR DOWN, NON-STOP FERRY FLIGHT. MAINTENANCE FOUND A DEFECTIVE NL
- [SDR CA140121002](https://openairdocs.org/sdr/CA140121002.md): Landing Gear · lack of lube · Jan 15, 2014 · Emb ERJ170200SU · Landing Gear Retraction/Extension System
  > (CAN) AFTER T/O THE LT MLG WOULD NOT RETRACT. THE ACFT RETURNED. MAINTENANCE FOUND THE MID PIVOT POINT OF THE SIDE BRACE STIFF AND NEEDING LUBRICATION. AFTER LUBRICATION THE RETRACTION WAS TESTED SERVICEABLE. SINCE THIS IS A KNOWN HISTORICAL PROBLEM ON THE
- [SDR CA131231001](https://openairdocs.org/sdr/CA131231001.md): Landing Gear · frozen · Dec 26, 2013 · Emb ERJ170200SU · Landing Gear Retraction/Extension System
  > (CAN) INSTANCES OF LANDING GEAR DISAGREE LIGHTS AFTER TAKEOFF ON 17TH, 25TH AND 26TH OF DECEMBER 2013. ON THE 17TH A LOT OF ICING ACCUMULATION WAS FOUND, CLEANED AND GEAR SWINGS CARRIED OUT SUCCESSFULLY. NO FURTHER OCCURRENCES UNTIL THE 25TH DECEMBER ON THE
- [SDR CA131001005](https://openairdocs.org/sdr/CA131001005.md): Wire · chafed · Sep 20, 2013 · Emb ERJ170200SU · Equipment/Furnishings Wiring
  > (CAN) SMOKE ODOR IN CABIN IN INITIAL CRUISE. ACFT DIVERTED FOR INVESTIGATION. POWER CONTROL BOARD FOUND BURNED. AFFECTED SEAT AND OTHERS, AS A PRECAUTION, PUT ON MEL. ON A SUBSEQUENT FLIGHT THE CHIMES WERE GOING OFF AGAIN SO DUE TO HISTORY OF CHIMES AND BUR
- [SDR CA130805018](https://openairdocs.org/sdr/CA130805018.md): Module · failed · Aug 3, 2013 · Emb ERJ170200SU · Central Computers
  > (CAN) MAYDAY DECLARED FOR A MAU 1 FAULT. MAYDAY DECLARED. MAU 1 POWER, MOD 1 REPLACED IAW AMM 31-41-02 PB401. MAU 1 NIC-PROCESSOR 1 REPLACED IAW AMM 31-41-04, PB401. MAU 1 MAIN BRAKE CONTROL MOD 1 REPLACED IAW AMM 32-41-07, PB401. CHECKED SERVICEABLE. REM
- [SDR CA131125014](https://openairdocs.org/sdr/CA131125014.md): Torque Tube · chafed · Jul 14, 2013 · Emb ERJ170200SU · Rudder Control System
  > (CAN) RUDDER PEDAL TORQUE TUBE GOUGED FROM PANEL COVER. TORQUE TUBE REPLACED, COVER PANELS REWORKED OR VERIFIED CLEARANCE.
- [SDR CA130625005](https://openairdocs.org/sdr/CA130625005.md): Panel · out of position · Jun 24, 2013 · Emb ERJ170200SU · Flight Compartment Equipment
  > (CAN) DURING PRIMARY INSPECTION, IT WAS NOTED THAT PANEL 221 EZ WAS CHAFING AGAINST THE PILOTS RT RUDDER PEDAL TORQUE TUBE.
- [SDR CA130524007](https://openairdocs.org/sdr/CA130524007.md): Module · overheated · May 14, 2013 · Emb ERJ170200SU · External Power System
  > (CAN) ON ARRIVAL, APU WAS IN OPERATION WHEN CREW SELECTED APU GENERATOR AND BLEED THERE WAS A BURNING ELECTRICAL SMELL, GPU WAS HOOKED UP BUT FAILED SHORTLY THEREAFTER, CREW THEN NOTICED A BLUISH HAZE THROUGHOUT THE CABIN AND THE BURNING SMELL WAS STRONGER.
- [SDR CA130411001](https://openairdocs.org/sdr/CA130411001.md): Shroud · corroded · Apr 10, 2013 · Cndair CL6002B19 · Aircraft Fuel Distribution System
  > (CAN) AFTER FINDING CORROSION ON 2 OTHER AIRCRAFT. THE FUEL SHROUDS AND FUEL LINES WERE REMOVED FORM THIS ACFT, CURRENTLY BEING PARTED OUT, TO SERVICE THE FIRST ACFT. THE INSIDES OF THESE COMPONENTS WERE COVERED WITH A BLACK SUBSTANCE, ONCE CLEANED OFF THE C
- [SDR CA130409002](https://openairdocs.org/sdr/CA130409002.md): Flap System · failed · Apr 6, 2013 · Emb ERJ170200SU · Trailing Edge Flap Control System
  > (CAN) ON APPROACH THE CREW REPORTED THE FLAPS HAD FAILED. AN EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITHOUT FURTHER COMPLICATIONS. BY CMC FAULT CODE - 27512014ACE. FIM TASK- 27-51-00-810-802-A. FAULT ISOLATION PROCEDURE CARRIED OUT. TRANSITORY CONDI
- [SDR CA130318018](https://openairdocs.org/sdr/CA130318018.md): Actuator · leaking · Mar 16, 2013 · Emb ERJ170200SU · Rudder Actuator
  > (CAN) OVERWEIGHT LANDING DUE TO AIRBORNE RETURN ACCOUNT OF STRONG IRRITATING DIRTY SOCK ODOR EMANATING THROUGHOUT CABIN/FLIGHT DECK. SEQUENCED PACKS, UNABLE TO ELIMINATE ODOR. ACFT LANDED APPROXIMATELY 600 KGS OVER MAXIMUM LANDING WEIGHT. BOROSCOPE INSP C/O
- [SDR CA130204001](https://openairdocs.org/sdr/CA130204001.md): Duct · punctured · Feb 1, 2013 · Emb ERJ170200SU · Air Distribution System
  > (CAN) UNABLE TO PRESSURIZE AIRCRAFT. RETURNING TO DEPARTURE. NO EMERGENCY DECLARED BY CREW. CABIN ALT HI EICAS WARNING MESSAGE ON WHILE CLIMBING THROUGH FL250, PACK 2 APPEARED NORMAL, OFV SHOWING FULLY CLOSED. PACK NR 2 AIR SUPPLY DUCT FOUND WITH HOLE IN
- [SDR CA130129005](https://openairdocs.org/sdr/CA130129005.md): Gasket · leaking · Jan 29, 2013 · Emb ERJ170200SU · Pneumatic Distribution System
  > (CAN) WHEN FLIGHT WAS ENROUTE, ACFT EXPERIENCED A NR 1 BLEED FAILURE FOLLOWED BY NR 1 BLEED LEAK MESSAGE. WITH THUNDERSHOWERS FORECAST, THE CREW ELECTED TO RETURN. NR 1 ENGINE PRECOOLER AFT INTERFACE GASKET REPLACED IAW AMM 36-11-08 PB401.
- [SDR CA130114009](https://openairdocs.org/sdr/CA130114009.md): Filter · failed · Jan 8, 2013 · Emb ERJ170200SU · Air Distribution System
  > (CAN) THE FLIGHT CREW ENCOUNTERED FUMES IN THE COCKPIT AFTER TAKEOFF. THERE WAS ALSO A POSSIBLE HAZE ASSOCIATED. THERE WERE SIMILAR FUMES REPORTED IN THE FWD & AFT CABIN. THE FLIGHT CREW DIVERTED BACK AND DID DECLARE AN EMERGENCY AND LANDED RUNWAY WITHOUT F
- [SDR CA121217004](https://openairdocs.org/sdr/CA121217004.md): Control Valve · failed · Dec 15, 2012 · Emb ERJ170200SU · Landing Gear Brake System
  > (CAN) ENCOUNTERED HOT BRAKES AT THE THRESHOLD OF R23 WARNING AMBER, REQUESTED TO BE TOWED TO GATE. REPLACED INBD MAIN BRAKE CONTROL VALVE IAW AMM 32-41-09 PB 401. OPS TEST SERVICABLE.
- [SDR CA121211015](https://openairdocs.org/sdr/CA121211015.md): Fitting · collapsed · Nov 28, 2012 · Emb ERJ170200SU · Pneumatic Distribution System
  > (CAN) BOTH LT AND RT PYLON TORQUE MOTOR CONTROLLER FITTING AIR FILTERS HAVE COLLAPSED. ACFT WAS DUE FOR N1 VISIT, AND TASK CARD 37-36-11-06-001AC-01 CALLED FOR THE CLEANING OF BOTH FILTERS. UPON DISCOVERING THEIR CONDITIONS, THEY WERE BOTH REPLACED. THESE F
- [SDR CA121128001](https://openairdocs.org/sdr/CA121128001.md): Engine · power loss · Nov 25, 2012 · Emb ERJ170200SU · Engine (Turbine/Turboprop)
  > (CAN) ENGINE SHUTDOWN AFTER T/O, RETURNED TO DEPARTURE. NR 2 ENGINE SUFFERED AN IFSD SHORTLY AFTER TAKEOFF. AT THE TIME, THE THROTTLES WERE AT HIGH POWER SETTING WHILE CLIMBING THROUGH 15,000 FT, A LOUD AUDIBLE BANG WAS REPORTED BY THE CREW, FOLLOWED SHORTL
- [SDR CA121009006](https://openairdocs.org/sdr/CA121009006.md): Flap System · failed · Oct 8, 2012 · Emb ERJ170200SU · Trailing Edge Flap Control System
  > (CAN) ON, SHORT FINAL, THE FLIGHT CREW RECEIVED A FLAP DISAGREE MESSAGE. A GO-AROUND WAS INITIATED. DURING THE SECOND APPROACH, NO MESSAGES WERE RECEIVED AND THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. AS A PRECAUTION, CFR WAS CALLED AND MET THE FLIGHT ON A
- [SDR CA121009005](https://openairdocs.org/sdr/CA121009005.md): Transponder · failed · Oct 7, 2012 · Emb ERJ170200SU · Independent Position Determining System
  > (CAN) AFTER TAKEOFF THE CREW WAS ADVISED BY ATC THEY WERE NOT RECEIVING TRANSPONDER INFO FROM THE FLIGHT. THE FLIGHT RETURNED AND LANDED NORMALLY. THE CREW DID NOT DECLARE ANY EMERGENCY BUT THE EMERGENCY RESPONSE VEHICLES ATTENDED THE LANDING. MRC1 NIM REP
- [SDR CA121009002](https://openairdocs.org/sdr/CA121009002.md): Duct · cracked · Oct 6, 2012 · Emb ERJ170200SU · Vacuum Distribution System
  > (CAN) FOUND DURING SCHEDULED MAINTENANCE, T-DUCT BELOW PRE-COOLER ON RT PYLON SIDE IS CRACKED. IPC ATTACHED, PN 170-14806-401.
- [SDR CA120921003](https://openairdocs.org/sdr/CA120921003.md): Shutoff Valve · failed · Sep 20, 2012 · Emb ERJ170200SU · Cabin Pressure Control System
  > (CAN) ON DEPARTURE PASSING 14,000 FT THE SERVICE DIRECTOR REPORTED AN ODOR RESEMBLING DIRTY SOCKS THROUGHOUT THE CABIN. THE FLIGHT CREW SWITCHED OFF THE NR 1 PACK AND THE ODOR DISSIPATED. TROUBLESHOOTING COMPLETED IAW FMR M2028728. NO FAULTS FOUND. IAW FMR
- [SDR CA120914006](https://openairdocs.org/sdr/CA120914006.md): Indicator · malfunctioned · Sep 13, 2012 · Emb ERJ170200SU · Engine Temperature Indicating System
  > (CAN) DEPARTING ON THE TAKE OF ROLL, THE FLIGHT EXPERIENCED AN EGT EXCEEDENCE ON THE NR 1 ENGINE AT 110 KNOTS FOLLOWED BY A REJECTED TAKEOFF AT 120 KNOTS. THE ACFT PULLED OF THE RUNWAY AND STOPPED TO ENSURE BRAKE TEMPERATURES DIDN`T EXCEED LIMITS. ONCE THE B
- [SDR CA120911004](https://openairdocs.org/sdr/CA120911004.md): Flap System · failed · Sep 8, 2012 · Emb ERJ170200SU · Trailing Edge Flap Control System
  > (CAN) DURING THE APPROACH, IN SHORT FINAL WHEN SELECTING FULL FLAPS FROM FLAPS 3 CONFIGURATION THE CREW RECEIVED A FLAPS FAIL INDICATION. THEY EXECUTED A GO- AROUND, AND TRIED A RE-SET. THE SECOND APPROACH WAS THE SAME INDICATION BUT THEY WERE ABLE TO CONIT
- [SDR CA120904009](https://openairdocs.org/sdr/CA120904009.md): Sensor · failed · Aug 30, 2012 · Emb ERJ170200SU · Engine Oil Temperature
  > (CAN) ON DEPARTURE, ACFT YAWED TO THE LT, NUMBER 1 SIDE, CREW ELECTED TO LEAVE GEAR DOWN AS THEY THOUGHT POSSIBLE BLOWN TIRE. ATC HAD THEM CLIMB TO 7000FT, AT THAT TIME THE NR 1 ENGINE HAD HIGH OIL TEMP 180C. THE CREW THEN ELECTED TO RETURN. WITH THE TEMP T
- [SDR CA120828007](https://openairdocs.org/sdr/CA120828007.md): Circuit Card · failed · Aug 27, 2012 · Emb ERJ170200SU · Autopilot System
  > (CAN) AIRCRAFT WAS OSCILLATING WHILE THE AUTOPILOT WAS ENGAGED AT APPROXIMATELY 10000 FT, AUTOPILOT WAS DISENGAGED, THE OSCILLATING WENT AWAY FLT RETURNED. THE ACFT CONDUCTED AN OVERWEIGHT LANDING. PILOT TALKED WITH MTCE AFTER THE LANDING. CAPTAIN WILL FIL
- [SDR CA120828008](https://openairdocs.org/sdr/CA120828008.md): Oil System · low pressure · Aug 26, 2012 · Emb ERJ170200SU · Engine Oil Indicating System
  > (CAN) ENGINE 2 LOW OIL PRESSURE, ENGINE 2 SHUTDOWN, DIVERTED, EMERGENCY DECLARED.

Next page: https://openairdocs.org/engine/ge-cf34-8e5a1/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 = 'CF348E5A1'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/ge-cf34-8e5a1/reports

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