# Service difficulty reports: GE CF34-10E5A1

A list on [GE CF34-10E5A1](https://openairdocs.org/engine/ge-cf34-10e5a1.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 10 · 476 reports

- [SDR BAGA2026042700005](https://openairdocs.org/sdr/BAGA2026042700005.md): Oil System · low pressure · Apr 24, 2026 · N120BZ · Emb ERJ190100IGW · Engine Oil Indicating System
  > DURING FLIGHT ENGINE OIL 2 PRESSURE DECREASED WENT TO APPROX 20 RED INDICATION, RAN QRH AND SHUT ENGINE DOWN. NO FURTHER INCIDENT.
- [SDR BAGA2024082800662](https://openairdocs.org/sdr/BAGA2024082800662.md): Engine · vibration · Aug 28, 2024 · N126BZ · Emb ERJ190100IGW · Engine (Turbine/Turboprop)
  > ENGINE 2 VIBRATION ON HIGH PASS DURRING TAXI, AND THERE WAS A SLIGHT HAZE AND UNUSUAL SMELL. NO FIRE INDICATIONS NOR SMOKE IN THE COCKPIT OCCURED. AIRCRAFT RETURNED TO THE GATE. ENGINE R/R IN PROCESS FOR CORRECTIVE ACTION.
- [SDR BAGA2024073000004](https://openairdocs.org/sdr/BAGA2024073000004.md): Bleed Valve · failed · Jul 29, 2024 · N145BZ · Emb ERJ190200IGW · Compressor Bleed Valve
  > ENGINE 1 BLEED ON MEL, ENGINE 2 BLEED FAULED. BLEED 2 FAIL EICAS ENROUTE JUST AFTER ICING CONDITIONS EICAS MESSAGE APPEARED. PERFORMED QRH. BLEED 2 FAIL MESSAGE CONTINUED. MOC NOTIFIED. REMOVED AND REPLACED NAPROV PER AMM 36-11-03/400, LEAK CHECK GOOD. PERFORM
- [SDR CA190812014](https://openairdocs.org/sdr/CA190812014.md): Engine · power loss · Aug 4, 2019 · Emb ERJ190100IGW · Engine (Turbine/Turboprop)
  > (CAN) AFTER DEPARTURE THROUGH 15000 FEET CREW NOTICED SMALL DROP IN N1 AND HAD SHUTTERING AND VIBRATIONS FROM NUMBER 2 ENGINE. AFTER LOSING POWER ON THE NUMBER 2,FLIGHT CREW BROUGHT THROTTLES BACK TO IDLE THAT STOPPED THE CONTINUOUS VIBRATIONS. THEY DECLARED A
- [SDR CA190605001](https://openairdocs.org/sdr/CA190605001.md): Control Panel · failed · Jun 4, 2019 · Emb ERJ190100IGW · Autopilot Computer
  > (CAN) FLIGHT DECLARED `MAYDAY` DUE INSTRUMENTATION FAILURE. FLIGHT DIVERTING. RESOLUTION GUIDANCE PANEL REPLACED IAW AMM 22-11-01. OPS CHK SERVICEABLE. (TC# 20190605001)
- [SDR CA190527023](https://openairdocs.org/sdr/CA190527023.md): Proximity Sensor · failed · May 25, 2019 · Emb ERJ190100IGW · Landing Gear Position and Warning
  > (CAN) SHORTLY AFTER DEPARTURE THE CREW REPORTED A WEIGHT ON WHEELS FAIL MESSAGE. THE FLIGHT RETURNED AND LANDED APPROXIMATELY 400KG OVERWEIGHT. NO EMERGENCY WAS DECLARED. RESOLUTION CARRIED OUT THE WIRING CHECK TO ASCB TERMINATORS AS PER FIM 31-42-00-815-A.
- [SDR CA190523005](https://openairdocs.org/sdr/CA190523005.md): Processor · failed · May 22, 2019 · Emb ERJ190100IGW · Central Computers
  > (CAN) DECLARED A PAN PAN WITH ATC DUE TO A MAU 1 FAILURE. POSSIBLE LOSS OF SPOILERS, NOSEWHEEL STEERING. AIRCRAFT WAS ABLE TO CLEAR THE RWY WITHOUT A TOW. RESOLUTION CMC INTERROGATED, AVNX MAU 1A FAIL MSG + F.C. 45452143CMC. REPLACED MAU1 + NIC1 PROC MODULE
- [SDR CA190510002](https://openairdocs.org/sdr/CA190510002.md): Processing Unit · failed · May 9, 2019 · Emb ERJ190100IGW · Central Computers
  > (CAN) AIRCRAFT RECEIVED ANVX MAU 2B FAULT MESSAGE. DUE TO THIS SYSTEM AFFECTING THE BRAKES THE CREW DECLARED A PAN PAN TO HAVE FIRE TRUCKS TO DO A BRAKE INSPECTION ON ARRIVAL. FLIGHT TAXIED INTO GATE SHORTLY AFTER LANDING. RESOLUTION REF FIM 45-45-00-810-942
- [SDR CA190429010](https://openairdocs.org/sdr/CA190429010.md): Trans Rectifier · arced · Apr 29, 2019 · Emb ERJ190100IGW · DC Rectifier/Converter
  > (CAN) UPON ARRIVAL AIRCRAFT EICAS MESSAGES AC STBY BUS OFF, FL CTRL NO DISPATCH AND ELECTRONIC CB`S EMRG FAN EBAY MID AND EMRG FAN EBAY FWD ARE POPPED OUT, WITH FWD EBAY FANS FAIL AND CENTER EBAY FANS FAIL EICAS MESSAGES. RESOLUTION TRU #1 REPLACED AS PER
- [SDR CA190425010](https://openairdocs.org/sdr/CA190425010.md): Processor · failed · Apr 22, 2019 · Emb ERJ190100IGW · Central Computers
  > (CAN) CREW GOT AN AVIONICS MAU 1A FAIL. ALONG WITH THIS MESSAGE, THE QRH STATES THAT THEY MAY HAVE PRESSURE ISSUES THAT MAY AFFECT NOSE WHEEL STEERING, OUTBOARD BRAKING. WE HAVE CONFIRMED WITH THE CREW THAT THEY WILL NOT DECLARE A PAN PAN OR MAYDAY, BUT CREW A
- [SDR CA190304003](https://openairdocs.org/sdr/CA190304003.md): Bleed Valve · failed · Mar 1, 2019 · Emb ERJ190100IGW · Pneumatic Distribution System
  > (CAN) LEFT WITH ONE BLEED AIR SYSTEM UNDER MEL. ENROUTE, THE OTHER BLEED AIR SYSTEM FAILED. MTC SUGGESTED THAT THE AIRCRAFT SHOULD RETURN RESOLUTION REPLACED NAPRSOV AS PER AMM 36-11-03-000-801-A ON LEAK CHK FOUND LOWER SEALS LEAKING INSTALLED NEW SEALS. REPL
- [SDR CA190225007](https://openairdocs.org/sdr/CA190225007.md): Motor · failed · Feb 24, 2019 · Emb ERJ190100IGW · Windshield/Door Rain/Ice Removal
  > (CAN) CREW CONTACTED MOC CONCERNING A WIPER PROBLEM. MOC GAVE CREW CB RESET AND CREW DID THE RESET AND TRIED THE WIPERS AGAIN. THE MOTOR STARTED BUT THE WIPERS DID NOT MOVE. THE CAPTAIN SAID HE SMELLED AN ODOUR AS DID THE F/O. THE FIRST OFFICER SAID THAT HE SA
- [SDR CA190225009](https://openairdocs.org/sdr/CA190225009.md): Flight Dir · failed · Feb 24, 2019 · Emb ERJ190100IGW · Flight Management Computing Hardware System
  > (CAN) FLIGHT REJECTED TAKE-OFF AT 20KTS DUE TO AN AUTO THROTTLE FAIL/FLIGHT DIRECTOR FAIL MESSAGE. RESOLUTION AFTER CONSULTING MOC AND RE-ENGAGING AT SYSTEM THE SYSTEM WORKED CORRECTLY. (EICAS HAD CLEARED AFTER T/O REJECTED). (TC# 20190225009)
- [SDR 7AHR2018092500000](https://openairdocs.org/sdr/7AHR2018092500000.md): Nut · cracked · Sep 25, 2018 · Emb ERJ190100IGW · Nacelle/Pylon Miscellaneous Structure
  > REPLACED CRACKED NUT ON NR 2 PYLON PER AMM 54-50-00-000-803-A. OPENED NR 2 RT PYLON ACCESS PANEL. INSTALLED NR 2 RT PYLON PANEL.
- [SDR CA180223004](https://openairdocs.org/sdr/CA180223004.md): Sensor · failed · Feb 22, 2018 · Emb ERJ190100IGW · Trailing Flap Position Indicating System
  > (CAN) IN CRUISE CREW HAD FLAP LOW RATE ON EICAS. RESOLUTION CMC INTERROGATED & FOUND FAULT CODE 27534019ACE AND 27512009ACE C/O FIM TASK 27-53-00-810-840-A. REPLACED LT WING OUTBOARD FLAP SKEW SENSOR (POS NR 4) IAW AMM 27-53-06/401. FLAP LOW RATE MSG CLEARE
- [SDR CA160317007](https://openairdocs.org/sdr/CA160317007.md): Skin · cracked · Mar 16, 2016 · Emb ERJ190100IGW · Wing, Plate/Skin
  > (CAN) DURING SURFACE PREPARATION FOR TREATMENT, A CRACK WAS FOUND ON RT WING LOWER TRAILING EDGE SKIN INBOARD OF RIB 4 AFT OF SPAR II.
- [SDR CA160310010](https://openairdocs.org/sdr/CA160310010.md): Sensor · failed · Mar 10, 2016 · Emb ERJ190100IGW · Leading Edge Slat Position Indicating System
  > (CAN) CREW REPORTED THEY HAD A SLAT FAIL ON APPROACH. RESOLUTION FIM TASK 27-83-00-810-814-A CARRIED OUT. FOUND SLAT SKEW SENSOR (OUTBOARD) 2/3 RESISTANCE OUT OF LIMIT. REPLACED IAW AMM 27-83-01 PB 401. SLAT SYSTEM CHECK SERVICEABLE.
- [SDR CA160229002](https://openairdocs.org/sdr/CA160229002.md): Actuator · failed · Feb 27, 2016 · Emb ERJ190100IGW · Trailing Edge Flap Actuator
  > (CAN) DECLARED A PAN PAN DUE TO A FLAP ISSUE. RT I/B FLAP ACTUATORS 1R AND 2R FOUND TRIPPED. RESET OPERATED WITH NO FAULTS. MOC REQUEST TO REPLACE BOTH ACTUATORS. RT I/B CANOE REMOVED FLAP DRIVE 2R REPLACED IAW AMM 27-51-01 PB 401 AND ADJUSTED IAW AMM 27-50-0
- [SDR CA160120020](https://openairdocs.org/sdr/CA160120020.md): Warning System · false activation · Jan 20, 2016 · Emb ERJ190100IGW · Engine Vibration Analyzer
  > (CAN) DURING DEPARTURE CREW RECEIVED ENGINE VIBRATION WARNING IN CLIMB. IN CRUISE THE WARNING CONTINUED. AFTER CONSULTATION WITH MOC AND DISPATCH IT WAS DECIDED TO DIVERT. NR 2 ENGINE GND RUN TO T/O POWER ENGINE VIBRATION TEST COMPLETED IAW EMM 72-00-00-760-1
- [SDR CA160119019](https://openairdocs.org/sdr/CA160119019.md): Window · cracked · Jan 19, 2016 · Emb ERJ190100IGW · Flight Compartment Windows
  > (CAN) AFTER DEPARTURE CREW REPORTED FIRST OFFICERS WINDOW HAD CRACKED. THE CREW ELECTED TO RETURN TO DEPARTURE AIRPORT. NO EMERGENCY WAS DECLARED TO ATC. FLIGHT LANDED WITHOUT FURTHER INCIDENT. RESOLUTION RT WINDSHIELD REPLACED ON J/C IAW 39-56-01-00-001AC-02
- [SDR CA160118007](https://openairdocs.org/sdr/CA160118007.md): Uplock · failed · Jan 17, 2016 · Emb ERJ190100IGW · Landing Gear Retraction/Extension System
  > (CAN) AFTER GEAR RETRACTION THE CREW REPORTED A BANGING NOISE FROM THE NOSE GEAR AREA AND THE GEAR WOULD MOMENTARILY INDICATE IN TRANSIT. THE CREW DID NOT DECLARE ANY LEVEL OF EMERGENCY BUT REQUESTED THE FIRE TRUCKS ATTEND AS A PRECAUTION. AIRCRAFT WAS APPROXI
- [SDR CA160118006](https://openairdocs.org/sdr/CA160118006.md): Oxygen Mask · unwanted deploy · Jan 16, 2016 · Emb ERJ190100IGW · Passenger Oxygen System
  > (CAN) WHILE IN CRUISE, BOTH F/A OXYGEN MASKS DEPLOYED WITH A FAULT LIGHT ON THE F/A PANEL. NO PRESSURIZATION ISSUES OR TURBULENCE REPORTED AT THE TIME. RESOLUTION RESEATED&STOWED F/A`S L2&R2 MASK.OP`S OK PER AMM 35-20-07.
- [SDR CA160111002](https://openairdocs.org/sdr/CA160111002.md): Heat Exchanger · contaminated · Jan 9, 2016 · Emb ERJ190100IGW · Cabin Cooling System
  > (CAN) FLIGHT DEPARTED, AT 1500FT CABIN AND COCKPIT HAD A STRONG SMOKE ODOUR IN THE FORM OF A WHITE POWDER COME THROUGH THE VENTS. PASSENGERS AND CREW EXPERIENCED EYE AND THROAT IRRITATION. COCKPIT CREW DONNED OXYGEN MASKS AND DECLARED A MAYDAY WITH ATC. FLIGHT
- [SDR CA151210003](https://openairdocs.org/sdr/CA151210003.md): Sensor · failed · Dec 10, 2015 · Emb ERJ190100IGW · Leading Edge Slat Position Indicating System
  > (CAN) ON APPROACH CREW HAD A SLAT FAIL. FLIGHT DECLARED A PAN PAN WITH ATC FLIGHT LANDED AND WAS MET BY CFR. FLIGHT TAXIED TO GATE WITH NO FURTHER INCIDENT. RESOLUTION C/O FIM 27-80-00-810-802-A AND FIM 27-83-00-810-814-A. REPLACED RT SLAT POSITION SENSOR UNI
- [SDR CA151214009](https://openairdocs.org/sdr/CA151214009.md): Link · worn · Dec 8, 2015 · Emb ERJ190100IGW · Engine Mount Section
  > (CAN) FORWARD MOUNT LINK SPHERICAL BEARING FOUND WORN DURING ENGINE CHANGE.
- [SDR CA151214005](https://openairdocs.org/sdr/CA151214005.md): Link · worn · Dec 6, 2015 · Emb ERJ190100IGW · Engine Mount Section
  > (CAN) FORWARD MOUNT LINK SPHERICAL BEARING FOUND WORN DURING ENGINE CHANGE.
- [SDR CA151127013](https://openairdocs.org/sdr/CA151127013.md): Proximity Sensor · failed · Nov 27, 2015 · Emb ERJ190100IGW · Landing Gear Position and Warning
  > (CAN) AFTER DEPARTURE THE FLIGHT CREW WERE UNABLE TO RAISE THE LANDING GEAR. THE FLIGHT CREW RETURNED AND THERE WAS NIL ADVERSE PASSENGER REACTION. RESOLUTION FIM 32-61-00-810-840A CARRIED OUT. NLG WOFW PROX SENSOR P36 REPLACED PER AMM 32-61-01 PB401. LANDING
- [SDR CA151118003](https://openairdocs.org/sdr/CA151118003.md): Loop · failed · Nov 17, 2015 · Emb ERJ190100IGW · Pneumatic Indicating System
  > (CAN) DEPARTING, CLIMBING THROUGH 8000`, THE CREW RECEIVED AN ALERT, BLEED 2 LEAK. WHILE PERFORMING THE CHECKLIST FOR THAT FAILURE, THEY RECEIVED A SECOND ALERT, WING ANTI ICE FAIL THROUGH 13,000`. THE DECISION WAS MADE TO RETURN AS THEY WERE CLIMBING INTO ICI
- [SDR CA151116006](https://openairdocs.org/sdr/CA151116006.md): Control Valve · failed · Nov 14, 2015 · Emb ERJ190100IGW · Cabin Cooling System
  > (CAN) ON TAKEOFF AND LANDING THERE WAS A BURNING ODOR DETECTED BY THE CREW. NO SIGN OF VISIBLE SMOKE. A PAN PAN WAS DECLARED. LOCAL MTCE IS INVESTIGATING. RT PACK FLOW CONTROL VALVE, RT PACK BYPASS VALVE FILTERS REPLACED AS PER AMM 21-51-01 AND 21-51-00 RESPE
- [SDR CA151210007](https://openairdocs.org/sdr/CA151210007.md): Mount · worn · Oct 22, 2015 · Emb ERJ190100IGW · Engine Mount Section
  > (CAN) FORWARD MOUNT LINK SPHERICAL BEARING FOUND WORN DURING ENGINE CHANGE.
- [SDR CA151022003](https://openairdocs.org/sdr/CA151022003.md): Deflector · failed · Oct 21, 2015 · Emb ERJ190100IGW · Passenger/Crew Doors
  > (CAN) SHORTLY AFTER TAKEOFF THE CREW CREW REPORTED A BANG AND SOME VIBRATION FELT THROUGH THE AIRCRAFT. THE FLIGHT CONTINUED AT 10000FT AS A PRECAUTION AGAINST A POSSIBLE DOOR/PRESSURIZATION ISSUE. FORWARD PASSENGER DOOR DEFLECTOR REPLACED IAW AMM 52-11-28.
- [SDR CA151001009](https://openairdocs.org/sdr/CA151001009.md): Sensor · failed · Oct 1, 2015 · Emb ERJ190100IGW · Landing Gear Steering System
  > (CAN) LANDING GEAR WILL NOT GO UP. RETURNING TO DEPARTURE AIRPORT. RESOLUTION T/S IAW FIM TASK 32-61-00-810-840-A AND REPLACED STEERING FEEDBACK SENSOR IAW AMM 32-00-01-000-801B AND PROXIMITY SENSOR IAW AMM 32-62-01-400-801A. OPS CHECK NORMAL. OK FOR SERVICE
- [SDR CA150925011](https://openairdocs.org/sdr/CA150925011.md): Module · failed · Sep 25, 2015 · Emb ERJ190100IGW · Central Computers
  > (CAN) ON APPROACH TO RWY AT 700 AGL AIRCRAFT HAD MULTIPLE AMBER WARNINGS SPOILER FAULT STICK SHAKER ANTICIPATED AOA FAIL RESOLUTION GENERIC I/O MODULE MAU NR 1 SLOT 11/12 REPLACED IAW AMM 31-41-06 PS401.
- [SDR CA150909008](https://openairdocs.org/sdr/CA150909008.md): Indicator · malfunctioned · Sep 7, 2015 · Emb ERJ190100IGW · Leading Edge Slat Position Indicating System
  > (CAN) AIRCRAFT WAS INTERCEPTING FINAL AND HAD SELECTED FLAPS 0 TO 1 AT WHICH POINT THE CREW GOT A SLAT FAIL MESSAGE. THE CREW USED THEIR QRH AND CLEARED THE FAULT WHILE THEY LEVELED OFF. ONCE FAULT WAS CLEARED THEY CAME AROUND AND DID THE VISUAL TO RWY 14R. R
- [SDR CA150821007](https://openairdocs.org/sdr/CA150821007.md): Wire Harness · loose · Aug 21, 2015 · Emb ERJ190100IGW · Landing Gear System Wiring
  > (CAN) ON DEPARTURE THE GEAR FAILED TO RETRACT. THE CREW CONSULTED WITH MTCE AND ELECTED TO RETURN. AN UNEVENTFUL LANDING WAS CONDUCTED. FOUND NLG PROX HARNESS P41 IN WHEEL WELL LOOSE. RETIGHTENED CANON PLUG. PROX SENSORS CHECKED IAW 32-62-01-820-801-A & AIR/
- [SDR CA150819001](https://openairdocs.org/sdr/CA150819001.md): Unknown · odor · Aug 18, 2015 · Emb ERJ190100IGW · Air Distribution System
  > (CAN) SHORTLY AFTER DEPARTURE BACK END CREW REPORT AN ELECTRICAL ODOR, CAPT ELECTED TO DIVERT AND LANDED WITHOUT FURTHER INCIDENT...NO EMERGENCY DECLARED WITH ATC. TAXIED TO THE GATE UNDER OWN POWER. RESOLUTION NO ODOUR OF SMOKE OR ABNORMAL SMELL IN CABIN UP
- [SDR CA150819003](https://openairdocs.org/sdr/CA150819003.md): Flap System · malfunctioned · Aug 18, 2015 · Emb ERJ190100IGW · Trailing Edge Flap Control System
  > (CAN) ON FINAL FOR RWY CREW EXPERIENCED A FLAP ISSUE AND INITIATED A GO AROUND, CREW CARRIED OUT QRH CHECKLIST AND ISSUE WAS RESOLVED. CAME BACK AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED WITH ATC. FIM22-31-00-810-806A(AT-INVALID DATA-FLAP
- [SDR CA150814003](https://openairdocs.org/sdr/CA150814003.md): Motor · failed · Aug 13, 2015 · Emb ERJ190100IGW · Trailing Edge Flap Actuator
  > (CAN) PAN PAN DECLARED WITH ATC DUE TO FLAP FAIL. FAULT CODE 27512014ACE RETRIVED FROM CMC FIM PROCEEDURE 27-51-00 COMPLETED TO BOX NR 8 NIL FAULTS R/H FPDU MOTOR REPLACED AS PER AMM 27-53-03 SYST OPS OK NORMAL.
- [SDR CA150805006](https://openairdocs.org/sdr/CA150805006.md): Pump · failed · Aug 5, 2015 · Emb ERJ190100IGW · Hydraulic Pump (Electric/Engine), Main
  > (CAN) AIR RETURN DUE TO HYDRAULIC 2 SHOWING 0 QTY,NO PRESSURIZATION., REQUIRING TOW OFF,PAN PAN DECLARED. NR 2 ENG EDP REPLACED AS PER AMM 29-11-01-401. NR 2 SYSTEM MANIFOLD PRESSURE AND CASE DRAIN FILTERS REPLACED AS PER AMM 29-11-05-401 OPS CHECK AND LEAK C
- [SDR CA150806003](https://openairdocs.org/sdr/CA150806003.md): Processor · failed · Aug 5, 2015 · Emb ERJ190100IGW · Cabin Pressure Control System
  > (CAN) DUEL BLEED FAILURE ENROUTE, MADE AN EMERGENCY DESCENT TO F200,DIVERTING MASKS DID DROP AT CABIN ALTITUDE 14400FT. AMS CONTROLLER PROCESSOR MODULE SLOT 25 FROM SPDA2 REPLACED IAW 21-00-01-000/400-801-A TESTED NFF.
- [SDR CA150805002](https://openairdocs.org/sdr/CA150805002.md): Processor · failed · Aug 4, 2015 · Emb ERJ190100IGW · Central Computers
  > (CAN) STEERING FAIL ON APPROACH. GO-AROUND INITIATED. IAW FC- 45452145CMC AND FIM 45-45-00-810-941-A. FAULT ISOLATION PROCEDURE C/OUT. NIC + PROCESSOR MODULE NR 3 (MAU NR 2, NIC NR 1) REPLACED IAW AMM TASK- 31-41-04-000/400-801-A.
- [SDR CA150803003](https://openairdocs.org/sdr/CA150803003.md): Pump · failed · Aug 2, 2015 · Emb ERJ190100IGW · Hydraulic Pump (Electric/Engine), Main
  > (CAN) AT APPROX 2315Z AC PATCHED THROUGH TO MOC VIA DISPATCH REGARDING LOSS OF THEIR NR 2 HYDRAULICS, WILL CONTINUE BUT WILL DECLARE AN EMERGENCY THROUGH ATC FOR THE ARRIVAL...TOWER CONTACTED AND STATION ORGANIZED A TOW TO GET AIRCRAFT OFF THE RUNWAY. NR 2 HY
- [SDR CA150731008](https://openairdocs.org/sdr/CA150731008.md): Pump · failed · Jul 31, 2015 · Emb ERJ190100IGW · Hydraulic Pump (Electric/Engine), Main
  > (CAN) AT CRUISE AIRCRAFT EXPERIENCED HYDRAULIC SYSTEM 1 FAILURE MESSAGE, ALONG WITH A LOW PRESSURE AND LOW QUANTITY INDICATION. DECLARED PAN PAN WITH ATC, AFTER LANDING AIRCRAFT TAXIED TO THE GATE UNDER OWN POWER. CRF WAS ADVISED AND PRESENT. EDP REMOVED PER
- [SDR CA150720011](https://openairdocs.org/sdr/CA150720011.md): Windshield · cracked · Jul 19, 2015 · Emb ERJ190100IGW · Flight Compartment Windows
  > (CAN) DURING CRUISE THE CAPTAINS WINDSCREEN CRACKED. THE FLIGHT RETURNED. CAPT WINDSHIELD REPLACED IAW TASK CARD 39-56-01-00-001AC-01.
- [SDR CA150716001](https://openairdocs.org/sdr/CA150716001.md): Io Card · failed · Jul 16, 2015 · Emb ERJ190100IGW · Central Computers
  > (CAN) FLIGHT TAXIED TO GATE. WHILE ENGS WERE OFF AT GATE, CREW OBSERVED A 3S FIRE INDICATION. THIS OCCURRED 3 TIMES, DURING 3RD EVENT, CREW WAS PREPARED TO FIRE THE BOTTLE. CREW OBSERVED NO PHYSICAL SMOKE OR FIRE FROM NR 1 ENG, NO BOTTLE WAS FIRED. PAX DIS
- [SDR CA150714002](https://openairdocs.org/sdr/CA150714002.md): Shutoff Valve · failed · Jul 11, 2015 · Emb ERJ190100IGW · Pneumatic Distribution System
  > (CAN) FLIGHT DEPARTED WITH LT ENG BLEED INOPERATIVE. AFTER DEPARTURE THE RT ENG BLEED FAILED, ATTEMPTS TO RESET WERE UNSUCCESSFUL. FLIGHT DIVERTED FOR MX. LANDING WEIGHT WAS BELOW MAXIMUM LANDING WEIGHT. RESOLUTION NR 2 ENG PRSOV REPLACED IAW AMM 36-11-01
- [SDR CA150702001](https://openairdocs.org/sdr/CA150702001.md): Control Lever · failed · Jun 30, 2015 · Emb ERJ190100IGW · Landing Gear Selector
  > (CAN) ON DEPARTURE THE CREW WAS UNABLE TO SELECT GEAR UP. THEY WERE UNABLE TO MOVE THE LANDING GEAR LEVER. AFTER COMPLETING THEIR QRH AND CONSULTING WITH MTCE THE CREW ELECTED TO RETURN. THE AIRCRAFT WAS 200KGS ABOVE MAX LANDING WEIGHT AND LANDED WITHOUT FURTH
- [SDR CA150702002](https://openairdocs.org/sdr/CA150702002.md): Valve · failed · Jun 30, 2015 · Emb ERJ190100IGW · Landing Gear Brake System
  > (CAN) DURING CRUISE THE PARKING BRAKE ON LIGHT ILLUMINATED. AFTER CONSULTATION WITH MTCE THE LIGHT WENT OUT. AS A PRECAUTION THE CREW ELECTED TO DECLARE A PAN PAN AND HAVE CFR ON STAND BY FOR THEIR ARRIVAL. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. RESOLUTI
- [SDR CA150629020](https://openairdocs.org/sdr/CA150629020.md): Actuator · failed · Jun 28, 2015 · Emb ERJ190100IGW · Leading Edge Slat Actuator
  > (CAN) ON APPROACH TO AIRPORT THE CREW DID A GO AROUND DUE TO A SLAT FAIL. THE CREW COMPLETED THE CHECKLIST & CONDUCTED AN UNEVENTFUL LANDING. RESOLUTION COMPLIED WITH FIM TASK 27-81-00-810-802-A. FOUND RT NR 8 SLAT ACTUATOR TORQUE LIMITER INDICATOR TRIPPED.
- [SDR CA150623010](https://openairdocs.org/sdr/CA150623010.md): Controller · failed · Jun 23, 2015 · Emb ERJ190100IGW · Windshield/Door Rain/Ice Removal
  > (CAN) AFTER TAKEOFF CREW REPORTED A WINDSHIELD HEAT FAILURE. DUE TO CONVECTIVE ACTIVITY EN ROUTE & FORECAST THE FLIGHT IS RETURNING. LANDING WEIGHT WILL BE BELOW MAXIMUM. RESOLUTION IAW FAULT CODE 30420030AI1, WINDSHIELD HEATER CONTROL REPLACED IAW AMM 30-4

Next page: https://openairdocs.org/engine/ge-cf34-10e5a1/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 = 'CF3410E5A1'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/ge-cf34-10e5a1/reports

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