# Service difficulty reports: GE CF34-8C5

A list on [GE CF34-8C5](https://openairdocs.org/engine/ge-cf34-8c5.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 16 · 772 reports

- [SDR VNAA2026090924601](https://openairdocs.org/sdr/VNAA2026090924601.md): Start Valve · open · Sep 8, 2026 · N562NN · Cndair CL6002D24 · Engine Start Valves/Controls
  > R START VLV OPEN IN FLIGHT C/A REMOVED AND REPLACED STARTER AND STARTER CONTROL VALVE IAW AMM 80-11-01-000/400-801-AO1-PSA
- [SDR VNAA2026073121902](https://openairdocs.org/sdr/VNAA2026073121902.md): Engine · vibration · Jul 30, 2026 · N556NN · Cndair CL6002D24 · Engine (Turbine/Turboprop)
  > RIGHT ENGINE N1 FAN VIB UPTO 2.2 / PERFORMED STIFFNESS CHECK AND VIBE CHECK PER AMM 72-21-02-200-803-A01-PSA AND PPGRM 71-00-00-720-806-A01. NO DEFECTS NOTED.
- [SDR SWIA2026071177738](https://openairdocs.org/sdr/SWIA2026071177738.md): Stand Off · cracked · Jul 11, 2026 · N822SK · Cndair CL6002D24 · Engine Thrust Reverser
  > UPON REMOVAL OF INBD A BRACKET STANDOFF, FOUND THAT STANDOFF SCOOP ANGLE IS CRACKED AT FASTENER HOLE. REMOVED DAMAGE FROM INBD STANDOFF SCOOP ANGLE FROM RT UPPER TRANSCOWL ENSURING COMPLETE DAMAGE REMOVAL, FABRICATED REPAIR ANGLE, WET INSTALLED FABRICATED RE
- [SDR REXA2026062400975](https://openairdocs.org/sdr/REXA2026062400975.md): Engine · bird ingestion · Jun 18, 2026 · N934XJ · Cndair CL6002D24 · Turbine Engine Air Inlet Section
  > BIRD INGESTED ON CLIMB OUT R ENG DEGRADED FAN VIB 9.9 FOLLOWED QRH VIB CONTINUED EVENTUALLY R ENG FLAME OUT RAN EMER CHECK FOR SEVERE ENGINE DAMAGE. REMOVED AND REPLACED RT ENG ASSY IAW JOBCARD 900-72-430-902 OPS CHECK GOOD
- [SDR SWIA2026061877714](https://openairdocs.org/sdr/SWIA2026061877714.md): Angle · cracked · Jun 18, 2026 · N822SK · Cndair CL6002D24 · Engine Thrust Reverser
  > LEFT UPPER TRANSCOWL HAD A CRACKED CLOSING ANGLE UNDER INBD A BRACKET, FOUND AFTER REMOVAL. LT UPPER TRANSCOWL SCOOP ANGLE REPAIRED IAW REO 690-54-21-644, REV -, COMPLIED WITH SKYCARD 51-900-1002-SKY.
- [SDR SWIA2026060277630](https://openairdocs.org/sdr/SWIA2026060277630.md): Stand Off · cracked · Jun 2, 2026 · N822SK · Cndair CL6002D24 · Engine Thrust Reverser
  > RIGHT UPPER TRANSCOWL INBD -A- BRACKET CRACKED. REMOVED THE CRACKED BRACKET STANDOFF FROM RT UPPER TRANSCOWL AND INSTALLED ONE NEW INBD A BRACKET STANDOFF ONTO RT UPPER TRANSCOWL, IAW GREO 670-54-21-971, REV -B, STEP 1-3. COMPLIED WITH SKY CARD 51-900-1002
- [SDR SWIA2026060277650](https://openairdocs.org/sdr/SWIA2026060277650.md): Coaming · chafed · Jun 2, 2026 · N822SK · Cndair CL6002D24 · Engine Thrust Reverser
  > RH LWR TRANSCOWL INNER COAMING IS CHAFED FWD LATCH C-CHECK RO 10132026REPLACED INNER LATCH DOOR COAMING PN CN624-2060-209 AND REPAIRED CRACK FROM EDGE OF OUTER SKIN TO FASTENER HOLE COMMON TO FWD LATCH OF RH LOWER TRANSCOWL, REF REO 690-54-21-647, REV --, 2
- [SDR SWIA2026060277651](https://openairdocs.org/sdr/SWIA2026060277651.md): Stand Off · cracked · Jun 2, 2026 · N822SK · Cndair CL6002D24 · Engine Thrust Reverser
  > RH LWR TRANSCOWL INBD A BRACKET STANDOFF IS CRACKED C-CHECK RO 10132026REMOVED AND REPLACED IB STAND-OFF ANGLE PN CN624-2082-S2901 ON RH LOWER TRANSCOWL, REF EO CN624-2005 SNIEO S28 AND REO 670-54-21-971, REV B, 2023-11-28 COMPLIED WITH MAJOR REPAIR M-337 A
- [SDR SWIA2026060277652](https://openairdocs.org/sdr/SWIA2026060277652.md): Bracket · cracked · Jun 2, 2026 · N822SK · Cndair CL6002D24 · Engine Thrust Reverser
  > RH LWR TRANSCOWL OTBD A BRACKET IS CRACKED C-CHECK RO 10132026REMOVED AND REPLACED OB STAND-OFF ANGLE PN CN624-2082-S2901 ON RH LOWER TRANSCOWL, REF EO CN624-2005 SNIEO S28 AND REO 670-54-21-971, REV B, 2023-11-28 COMPLIED WITH MAJOR REPAIR M-337 AND SKY CA
- [SDR SWIA2026060277653](https://openairdocs.org/sdr/SWIA2026060277653.md): Coaming · worn · Jun 2, 2026 · N822SK · Cndair CL6002D24 · Engine Thrust Reverser
  > LH LWR TRANSCOWL INNER COAMING IS WORN THIN ON LOWER AFT SIDE C-CHECK RO 10132026REPAIRED LH LWR TRANSCOWL INNER COAMING REF REO 690-54-21-646, REV--, DATED 72226 AND REO 670-54-21-1207 REV A DATED 08-27-15 REFER TO CONTINUATION SHEET FOR DETAILSCOMPLIED WI
- [SDR SWIA2026060277685](https://openairdocs.org/sdr/SWIA2026060277685.md): Stiffener · sheared · Jun 2, 2026 · N822SK · Cndair CL6002D24 · Engine Thrust Reverser
  > RT UPPER TRANSCOWL Z STIFFINER RIVETS SHEARED. REMOVED AFFECTED Z STIFFENER FROM RT UPPER TRANSCOWL, CUT OUT DAMAGE FROM INNER PERFORATED SKIN, ENSURED DAMAGE REMOVAL, REMOVED ALL BURRS & SHARP EDGES, UNDERCUT THE HONEYCOMB CORE BY 025 ALL AROUND THE PERIPHER
- [SDR SWIA2026060277687](https://openairdocs.org/sdr/SWIA2026060277687.md): Stand Off · cracked · Jun 2, 2026 · N822SK · Cndair CL6002D24 · Engine Thrust Reverser
  > LH UPPER TRANSCOWL INBD A BRACKET STANDOFF IS CRACKED C-CHECK RO 10132026INSTALLED NEW LH UPPER TRANSCOWL IB A BRACKET PN CN624-2082-201 REF REO 670-54-21-971, REV -B, DATED 112823, SNIEO CN624-2005, S21, STEPS 1, INSTALLED STANDOFF, 2, ENSURED ALL REQUIREME
- [SDR SWIA2026060277688](https://openairdocs.org/sdr/SWIA2026060277688.md): Stand Off · cracked · Jun 2, 2026 · N822SK · Cndair CL6002D24 · Engine Thrust Reverser
  > LH LWR TRANSCOWL OTBD A BRACKET STANDOFF IS CRACKED C-CHECK RO 10132026INSTALLED A NEW LH LWR TRTANSCOWL OB A BRACKET PN CN624-2082-201 REF REO 670-54-21-971, REV -B, DATED 112823 AND SNIEO CN624-2005, S22 STEPS 1, INSTALLED STANDOFF, 2, ENSURED ALL REQUIREM
- [SDR SWIA2026060277689](https://openairdocs.org/sdr/SWIA2026060277689.md): Stand Off · cracked · Jun 2, 2026 · N822SK · Cndair CL6002D24 · Engine Thrust Reverser
  > LH LWR TRANSCOWL INBD A BRACKET STANDOFF IS CRACKED C-CHECK RO 10132026INSTALLED NEW LH LWR TRANSCOWL IB A BRACKET PN CN624-2082-201 REF REO 670-54-21-971, REV B, DATED 112823 REFER TO CONTINUATION SHEET FOR DETAILS COMPLIED FULLY WSKYCARD 51-900-1002-SKY
- [SDR VNAA2026050417002](https://openairdocs.org/sdr/VNAA2026050417002.md): Pin · loose · Apr 24, 2026 · N587NN · Cndair CL6002D24 · Engine Mount Section
  > RIGHT ENG VIBE BETWEEN 1.5-1.9 CONTINUOUSLY. RAN QRH PROCEEDURE 3 TIMES. WHEN WE DECREASED POWER VIBES INCREASED TO 1.9; IN CLIMB DETENT VIBES DECREASED. REMOVED AND REPLACED RH ENGINE FAN BLADE PINS IAW CRJ 900 AMM 12-20-72-640-803-A01. PERFORMED VIBRATION R
- [SDR VNAA2026032414601](https://openairdocs.org/sdr/VNAA2026032414601.md): O-Ring · leaking · Mar 22, 2026 · N560NN · Cndair CL6002D24 · Turbine Engine Oil System
  > R ENG OIL PRESSURE WARNING ON CLIMB OUT FOLLOWED QRH / REMOVED RH ATS IAW CRJ 900 AMM 80-11-01-000-801-A01 AND FOUND O-RING ON SPLINED SHAFT TO BE INSTALLED INCORRECTLY, FOUND OIL ON UNDERSWIDE OF THE HOUSING SEEPING OUT FROM THE GEAR BOX. REMOVED AND REINSTA
- [SDR VNAA2026032414803](https://openairdocs.org/sdr/VNAA2026032414803.md): Engine · vibration · Mar 22, 2026 · N549NN · Cndair CL6002D24 · Engine (Turbine/Turboprop)
  > N1 VIB AT 1.7 IN FLT, QRH C/W. VIBE REACHED 2.4 ON #2 ENG. / DURING BLADE SHAKE FOUND RH FWD SPINNER TO NOT BE COMPLETELY CLOCKED. RE-CLOCKED FWD SPINNER IAW CRJ 900 AMM 72-21-02-400-801-A01-PSA. PERFORMED BLADE SHAKE IAW CRJ 900 AMM 72-21-02-200-803-A01-PSA W
- [SDR REXA2026032600265](https://openairdocs.org/sdr/REXA2026032600265.md): Engine · odor · Mar 11, 2026 · N293PQ · Cndair CL6002D24 · Engine (Turbine/Turboprop)
  > FA REPORTED ODOR IN CABIN FORWARD TO AFT WHICH LED TO AIR RETURN. R & R RIGHT ENG PER JC 900-72-430-902. OPS/LEAK CHECKS GOOD.
- [SDR SWIA2026022675356](https://openairdocs.org/sdr/SWIA2026022675356.md): Engine · odor · Feb 26, 2026 · N821SK · Cndair CL6002D24 · Humidity Control System
  > IN FLIGHT FA REPORTED STRONG EXHAUST ODOR IN THE CABIN CAUSING HER THROAT AND HEAD TO HURT. DESCENDED TO FL240 AND SWAPPED TO THE APU BLEED. FA INITIALLY NOTED THAT THE SMELL IMPROVED BUT LATER CALLED US SAYING THE ODOR WAS BACK. PILOTS CONFIRMED THERE WAS A
- [SDR REXA2026031300237](https://openairdocs.org/sdr/REXA2026031300237.md): Seal · leaking · Feb 20, 2026 · N348PQ · Cndair CL6002D24 · Turbine Engine Oil System
  > WHILE AT FL 310 I NOTICED L OIL LOW. BEGAN MONITORING OIL INIDCATIONS. EVENTUALLY RECEIVED A L ENG OIL PRESS WARNING MESSAGE. FOLLOWED CRJ 900 QRH 1-20 AND 1-22 AS DIRECTED. SHUTDOWN LEFT ENGINE IN FLIGHT AS DIRECTED BY QRH. REPLACEED OF LT ENGINE C SUMP IN
- [SDR REXA2026020500041](https://openairdocs.org/sdr/REXA2026020500041.md): Packing · missing · Jan 24, 2026 · N337PQ · Cndair CL6002D24 · Turbine Engine Oil System
  > DURING CLIMB THRU FL250, RT OIL LEVEL LOW STATUS MESSAGE, 15% OIL LEVEL NO ACTION REQUIRED IAW QRH 0-23, OIL PRESSURE 80 PSI AT FL250, 67 PSI AT FL270, 55 PSI AT FL300, 30 PSI AT FL330, FOLLOWED BY RT ENG LOW WARNING, RAN QRH 1-20, RT ENG OIL PRESS. COMPLE
- [SDR VNAA202512020036](https://openairdocs.org/sdr/VNAA202512020036.md): Ring · corroded · Dec 4, 2025 · N515AE · Cndair CL6002C10 · Engine (Turbine/Turboprop)
  > CORROSION FOUND IN RT ENGINE RING AT A4 ATTACHMENT BOLT HOLE (1EA) MARKED WITH ZIP TIE THROUGH DISCREPANT BOLT HOLE.
- [SDR REXA2025102900968](https://openairdocs.org/sdr/REXA2025102900968.md): Engine · contaminated · Oct 15, 2025 · N272PQ · Cndair CL6002D24 · Engine (Turbine/Turboprop)
  > AFTER ROTATION CA AND FO STARTED TO SMELL SMOKE. VERY FAINT WHITE SMOKE SEEN BY PILOTS AND FAS WITH CHEMICAL ODOR. RAN CHECKING CARD AND QRH SMOKE AND FUMES REMOVAL PROCEDURE. TURNING PACKS AND RECIRC FAN OFF REDUCED ODOR SIGNIFICANTLY. FIRE RESCUE DID NOT N
- [SDR VNAA2025091711103](https://openairdocs.org/sdr/VNAA2025091711103.md): Fmu · unserviceable · Sep 16, 2025 · N575NN · Cndair CL6002D24 · Fuel Controlling System
  > R FADEC CAUTION AT CRUISE. / REMOVED AND REPLACED RH ENGINE FMU IAW CRJ900 AMM 73€“21€“03€“000/400€“801. OPS CHECK AND LEAKS CHECK GOOD.
- [SDR VNAA2025091111101](https://openairdocs.org/sdr/VNAA2025091111101.md): Fmu · faulted · Sep 7, 2025 · N568NN · Cndair CL6002D24 · Fuel Controlling System
  > L FADEC MSG IN FLIGHT. / REMOVED AND REPLACED R FADEC IAW AMM 73-21-01-000/400-801. REMOVED AND REPLACED LH ENGINE FMU IAW CRJ 900 AMM 73-21-03-000/400-801.OPS CHECK AND LEAK CHECK GOOD. PERFORMED HIGH POWER RUN IAW CRJ 900 AMM 71-00-00-866-806-A02-PSA. ALL P
- [SDR VNAA2025031411103](https://openairdocs.org/sdr/VNAA2025031411103.md): Pin · faulted · Mar 12, 2025 · N630NN · Cndair CL6002D24 · Turbine Engine Air Inlet Section
  > EXCESSIVE N1 VIBRATION ON RH ENG. RAN QRH PROCEDURE. DID NOT CORRECT ISSUE AT NORMAL POWER SETTINGS. HAD TO REDUCE RH THRUST TO 72-73% TO KEEP VIB BELOW 1.7. / REMOVED AND REPLACED RH ENGINE FAN BLADE PINS IAW CRJ900 AMM 72-21-02-400-801-A01-PSA. PERFORMED VIB
- [SDR VNAA2025022111102](https://openairdocs.org/sdr/VNAA2025022111102.md): Fadec · unserviceable · Feb 20, 2025 · N613NN · Cndair CL6002D24 · Fuel Controlling System
  > L FADEC FAULT CAUTION MSG ABOVE 80 KNOTS / INTERROGATED MDC AND FOUND FAULT CODE B1 006562. SUSPECT LH ENGINE FADEC TO BE FAULTING. REMOVED AND REPLACED LH ENGINE FADEC IAW CRJ 900 AMM 73-21-01-000/400-801-A01. OPS CHECK GOOD.
- [SDR VNAA2025021011104](https://openairdocs.org/sdr/VNAA2025021011104.md): Fadec · unserviceable · Feb 8, 2025 · N602NN · Cndair CL6002D24 · Fuel Controlling System
  > R FADEC CAUTION MSG. NO ABNORMAL ENGINE INDICATIONS / REMOVED AND REPLACED RH ENG FADEC IAW AMM 73-21-01-000/400-801-A01, OPS TEST GOOD.
- [SDR REXA2025011300045](https://openairdocs.org/sdr/REXA2025011300045.md): Engine · damaged · Jan 4, 2025 · N909XJ · Cndair CL6002D24 · Engine (Turbine/Turboprop)
  > ON INITIAL CLIMB OUT HEARD VIBRATION FOLLOWED BY A LOUD BANG, SAW OBJECT FLY BY FO WINDOW EMERGENCY DECLARED WITH ATC, RETURNED TO LAND IN ATL, NO ABNORMAL INDICATIONS ON EICAS ON POST FLIGHT WALK AROUND, A PIECE OF HEAD SET JACK WAS DISCOVERED STILL CONNECTED
- [SDR VNAA2024090911101](https://openairdocs.org/sdr/VNAA2024090911101.md): Pin · unserviceable · Sep 5, 2024 · N609NN · Cndair CL6002D24 · Turbine Engine Air Inlet Section
  > ENGINE FAN "LEFT" VIB 2.9 AT FL330 RAN QRH VIB DID NOT DECREASE BELOW 1.8 UNTIL AT FL250 WITH REDUCED THRUST / REMOVED BLADE PINS IN LH ENG DUE TO HIGH VIBES. REPLACED LH ENG BLADE RETAINING PINS IAW CRJ 900 AMM 72-21-02-000/400-801-A01-PSA. PERFORMED LH ENGIN
- [SDR VNAA2024072411101](https://openairdocs.org/sdr/VNAA2024072411101.md): Engine · vibration · Jul 22, 2024 · N578NN · Cndair CL6002D24 · Engine (Turbine/Turboprop)
  > AT FL 350 R ENG VIB FOR APPROX 3-5 SECS. SHORTLY AFTER N1 ROLL BACK ITT SPIKE +1000 DEGREES AND ENG OIL DECREASED. DESCENDED AND ENGINE RETURNED R PACK FAULT STATUS MSG. R ENG BLEED CAUTION MSG / REMOVED AND REPLACED RH ENGINE ASSEMBLY IAW CRJ900 AMM 71-00-00-
- [SDR VNAA2024053111101](https://openairdocs.org/sdr/VNAA2024053111101.md): Blade · unserviceable · May 30, 2024 · N569NN · Cndair CL6002D24 · Turbine Engine Air Inlet Section
  > LEFT ENGINE HIGH VIBES ON TAKEOFF. 2.0 MAX. COULDNT ADVANCE THRUST ABOVE IDLE WITHOUIT HIGH VIBES RETURN TO FIELD / REMOVED AND REPLACED FAN BLADE PINS FOR LH ENG IAW CRJ 900 AMM 72-21-02-000/400-801-A01-PSA. OPS CHECK GOOD
- [SDR SWIA20240523](https://openairdocs.org/sdr/SWIA20240523.md): Engine · flamed out · May 23, 2024 · N800SK · Cndair CL6002D24 · Engine (Turbine/Turboprop)
  > R ENG FLAMEOUT WARNING MESSAGE ON CLIMB AROUND 28,000 FEET. ALL RIGHT ENGINE GAUGES WENT TO NEARLY IDLE. WE RAN THE QRC/QRH, DIVERTED TO KGRR AND PERFORMED A SINGLE ENGINE LANDING. (FLIGHT 4055 FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 2827909
- [SDR VNAA2024021211101](https://openairdocs.org/sdr/VNAA2024021211101.md): Pin · unserviceable · Feb 8, 2024 · N585NN · Cndair CL6002D24 · Turbine Engine Air Inlet Section
  > INSPECTED LH FAN BLADES FOR STIFFNESS, NO DEFECTS FOUND, VIBE CHECK GOOD IAW CRJ 900 AMM 72-21-02-200-803-A01. HIGH TORQUE PIN T/S DUE WITHIN 15 CYCLES. / REMOVED AND REPLACED LH ENGINE FAN BLADE PINS IAW CRJ 900 AMM 72-21-02-000/400-801-A01-PSA. PERFORMED VIB
- [SDR VNAA202302271113](https://openairdocs.org/sdr/VNAA202302271113.md): None · none · Feb 24, 2023 · N576NN · Cndair CL6002D24 · Engine (Turbine/Turboprop)
  > POSSIBLE ENGINE 1 FLAMEOUT ON TAKE OFF. ENGINE FLAMEOUT/ REJECT REPORTED BY AIRCRAFT BEHIND-NO EICAS FLAMEOUT REPORTED CREW NOTED SLIGHT JERK AND THEN AIRCRAFT RECOVERED, INDICATIONS LOOKED NORMAL / RTO WAS 70 KTS OR LESS / REMOVED AND REPLACED LH ENGINE IAW C
- [SDR VNAA202212221111](https://openairdocs.org/sdr/VNAA202212221111.md): Blades · damaged · Dec 19, 2022 · N600NN · Cndair CL6002D24 · Turbine Engine Air Inlet Section
  > BIRD STRIKE AND BIRD INGESTION ON RH ENG. FOUND 5 DAMAGED FAN BLADES AND REMOVED AND REPLACED 5 SETS OF BLADES IAW CRJ 900 AMM 72-21-02-000-801-A01.
- [SDR REXA2022091602101](https://openairdocs.org/sdr/REXA2022091602101.md): Panel · chafed · Sep 7, 2022 · N919XJ · Cndair CL2151A10 · Engine Thrust Reverser
  > TRANSCOWL PANEL 443BT IS CHAFED REPLACED PANEL PER CRJ900 SRM 51-12-00-001-001-A01
- [SDR VNAA202209081111](https://openairdocs.org/sdr/VNAA202209081111.md): Fadec · unserviceable · Sep 5, 2022 · N565NN · Cndair CL2151A10 · Engine (Turbine/Turboprop)
  > DUAL R ENG FADEC FAULT RESULTING IN R ENG FLAMEOUT DURING CLIMB. HAD SUCCESSFUL AUTO RE-LIGHT. PREFORMED A VISUALLY CHECK OF RH FADEC AND MADE SURE ALL CONNECTORS ARE SECURED, NO DEFECTS NOTED. PERFORMED A POWER ON BUILT IN TEST IAW CRJ900 AMM 71-00-00-710-801
- [SDR VNAA202207071111](https://openairdocs.org/sdr/VNAA202207071111.md): Engine · noise · Jul 5, 2022 · N548NN · Cndair CL6002D24 · Engine (Turbine/Turboprop)
  > A/C WAS FLYING AT FL340 AT.81MACH FOR ABOUT 30MIN AND HEARD A LOUD BANG. IMMEDIATELY NOTICED HI ENG VIB AND ITT IN LFT ENG. PROCEEDED TO RUN THE QRH FOR A LFT ENG SHUTDOWN. NO FIRE WAS DETECTED. THE CREW DECLARED AN EMERGENCY AND CONTINUED ONTO CLT. PIC MADE
- [SDR REXA2022082501956](https://openairdocs.org/sdr/REXA2022082501956.md): Door · chafed · Jul 1, 2022 · N937XJ · Cndair CL6002D24 · Engine Thrust Reverser
  > LH LOWER TRANSCOWL LATCH DOOR CHAFED. 1.5" X.50" X.025" DEEP REPLACED DOOR
- [SDR REXA2022060201044](https://openairdocs.org/sdr/REXA2022060201044.md): Fairing · cracked · May 27, 2022 · N135EV · Cndair CL6002D24 · Engine Cowling System
  > RH ENGINE UPPER COWL HINGE LINE FAIRING 443BT CRACKED PERFORMED REPAIR ON RH ENGINE UPPER COWL HINGE LINE FAIRING PER EA CRJ954-12492 REV D DATED 05/24/2022
- [SDR REXA2022053100964](https://openairdocs.org/sdr/REXA2022053100964.md): Mount · chafed · May 3, 2022 · N176PQ · Cndair CL6002D24 · Engine Mount Section
  > R/H ENGINE YOKE MOUNT IS CHAFED AT 2 LOCATIONS. REPAIRED R/H ENGINE YOKE IAW MHIRJ REO 690-71-21-041 REV -- DATED 2022-04-23 AND BOMBARDIER REO 670-71-21-057 EV -- DATED 2013-09-13.
- [SDR VNAA202205041111](https://openairdocs.org/sdr/VNAA202205041111.md): None · none · May 1, 2022 · N594NN · Cndair CL6002D24 · Engine (Turbine/Turboprop)
  > DURING CLIMB CREW NOTICED HIGH VIBS BUT NEEDLE STILL IN GREEN. AT FL290 NEEDLE MOVED TO YELLOW CREW RAN THROUGH CHECK LIST AND PULL THE POWER BACK AND CONTINUE TO CLIMB TO FL310 THE NEEDLE CAME BACK TO GREEN FOR FEW MIN. THEN NEEDLE WENT INTO YELLOW AGAIN. CRE
- [SDR REXA2022062801407](https://openairdocs.org/sdr/REXA2022062801407.md): Latch · worn · Apr 24, 2022 · N917XJ · Cndair CL6002D24 · Engine Cowling System
  > RH UPPER FWD CORE COWL BLOW OFF DOOR 444CT LATCH PLATE WORN WITH 100% MATERIAL LOSS. REPLACED RH UPPER FWD CORE COWL LATCH PLATE
- [SDR REXA2022060600972](https://openairdocs.org/sdr/REXA2022060600972.md): Plate · cracked · Apr 18, 2022 · N676CA · Cndair CL6002D24 · Engine Thrust Reverser
  > LH ENGINE LOWER TRANSCOWL BIFURCATION PANEL NYLON PLATE BROKEN MANUFACTURED NEW PLATE PER EA# CRJ954-13327.
- [SDR MASA20220413203](https://openairdocs.org/sdr/MASA20220413203.md): Transcowl · cracked · Apr 13, 2022 · N904FJ · Cndair CL6002D24 · Engine Thrust Reverser
  > THE RH UPPER TRANSCOWL WAS FOUND TO HAVE CRACK DAMAGE TO THE OUTER SKIN. PERFORMED PERM REPAIR IAW CRJ?00/900 STRUCTURAL REPAIR MANUAL (SRM) 54-21-05, FIGURE 54-21-05-991-801, ITEM 1 (REV.38 DATED JUL. 25, 2020).
- [SDR REXA2022050300812](https://openairdocs.org/sdr/REXA2022050300812.md): Yoke · chafed · Apr 10, 2022 · N232PQ · Cndair CL6002D24 · Engine Mount Section
  > RH FORWARD ENGINE MOUNT HAS CHAFFING. CA: REPAIRED IAW BOMBARDIER REO 670-71-21-057 REV-- DATED 2013-09-13 AND MHIRJ REO 690-71-21-039 REV A DATED 2022-04-01.
- [SDR REXA2022050900820](https://openairdocs.org/sdr/REXA2022050900820.md): None · worn · Apr 8, 2022 · N135EV · Cndair CL6002D24 · Engine Cowling System
  > RH ENGINE LOWER CORE COWL RUB STRIP HAS HEAVY WEAR REMOVED WORN RH ENG. LOWER CORE COWL RUB STRIP AND REPLACED WITH NEW RUB STRIP PER EA CRJ954-13184 REV A DATED: 4/5/2022.
- [SDR VNAA202204051112](https://openairdocs.org/sdr/VNAA202204051112.md): Pin · worn · Apr 2, 2022 · N571NN · Cndair CL6002D24 · Engine (Turbine/Turboprop)
  > SHORTLY AFTER TAKEOFF FROM DCA, THE CREW NOTICED THAT THE R ENGINE VIBE WENT INTO THE AMBER. THEY CONTINUED MONITORING IT AND SAW IT GO UP TO 2.6 AT ONE POINT. THEY SAID THE FAS STATED THEY COULDN'T HEAR ANYTHING IN THE CABIN OVER THE VIBRATIONS AND THE PILOTS
- [SDR MASA20220401162](https://openairdocs.org/sdr/MASA20220401162.md): None · none · Apr 1, 2022 · N904FJ · Cndair CL6002D24 · Engine Thrust Reverser
  > THE RH ENGINE UPPER TRANSCOWL LATCH DOOR (PN-CN624-2021-901) WAS FOUND TO HAVE WEAR ON THE SURROUND LANDING AT THE FREE EDGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 (SRM) TASK 54-21-05-003-A01, (REV. 38 DATED 9JUL2021). (SUPPLEMENTAL)

Next page: https://openairdocs.org/engine/ge-cf34-8c5/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 = 'CF348C5'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/ge-cf34-8c5/reports

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