GE CF34 series

Service difficulty reports · 1,368

Newest first. General aviation reporting is voluntary.

Query with SQL
duckdb -csv -c "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 = 'CF34'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR ASOA201001732Seat Track · corrodedSEAT TRACK 9R AT FS 581 TO FS 677 HAS MINOR SURFACE CORROSION. REMOVED SEAT TRACK AT 9R, FS 581 TO FS 697 IAW SRM51-41-02-001-001-A01. INSTALLED NEW SEAT TRACK. FABRICATED NEW SEAT TRACK USING SEAT TRACK EXTRUSTION PN N126-2075 6, TRIMED BACK UPPER FLANGE Oct 11, 2010 · N709EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201001529Stringer Splice · corrodedFACTORY STRINGER SPLICE AT FS 333 CORRODED. REMOVED FACTORY STRINGER SPLICE AT FS 333 AND DRILLED SERVICEABLE STRINGER SPLICE ALL WORK DONE IAW SRM 51-42-06-001-001-A01. INSTALLED STRINGER SPLICE IAW SRM 51-42-06-001-001-A01. FILLET SEALED IAW SRM 51-223-00Oct 10, 2010 · N750EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA201001530Stringer · corrodedSTRINGER 25R JUST AFT OF FS 280 HAS CORROSION AROUND FASTENERS. INSTALLED STRINGER IAW SRM 51-42-06-001-001.Oct 10, 2010 · N750EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA201001531Lamp · burned outEXTERIOR EMERGENCY LIGHT(MIDDLE) ON LT & RT SIDE INOP. RELAMPED LT & RT MIDDLE EXTERIOR EMERGENCY LIGHTS IAW AMM 33-51-21. OPS CK GOOD. (CLOSED)Oct 10, 2010 · N850AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201001533Placard · missingEXIT PLACARD ON ASD MISSING. INSTALLED EXIT PLACARD ON AIR STAIR DOOR IAW AMM 11-30-00. CLEARED PLACARD REMOVED.Oct 10, 2010 · N879AS · Cndair CL6002B19 · Placards and MarkingsSDR ASOA201001534Terminal · damagedDURING TAXI NOTICED STRONG ELECTRICAL BURNING ODOR ON FLT DECK. CHANGING PACKS AND BLEED SOURCE HAD NO EFFECT. STRONGEST SMELL IN NR 2 CBP AREA AND RT GALLEY AREA BY SERVICE DOOR. (GATE RETURN) ( HYD AC MOTOR PUMPS (ACMP) (SYS 1 AND 2) ACMP 1B ) ( HYD AC MOOct 10, 2010 · N970EV · Cndair CL6002B19 · Electrical Power System WiringSDR QXEA2010101000610Wire Harness · malfunctionedPROX SYS FAULT NR 2 STATUS. RETURNED TO FIELD. LANDING UNEVENTFUL. INTERROGATED MDC AND FOUND AFT BAGGAGE DOOR PROX SENSOR PX102 UNREASONABLE FAR/OPEN, ALSO FOUND BAGGAGE DOOR HARNESS TO HAVE NO CONTINUITY ON 1 WIRE , REPLACED HARNESS AND PX102 SENSOR IAW AMM Oct 10, 2010 · N601QX · Cndair CL6002C10 · Door System WiringSDR QXEA2010101000611Warning Message · false activationAFT CARGO DOOR CAUTION MESSAGE WITH PROXIMITY SYS FAULT 2 STATUS MGS DURING CLIMB. RETURNED. LANDING WT 66,800 LBS. PERFORMED ADJUSTMENT OF AFT BAGGAGE BAY DOOR PROXIMITY SENSOR PX102. IAW AMM TASK 52-70-02-820-802. SENSOR PLACED AT .025 IN. CLEARENCE. NO FUROct 10, 2010 · N601QX · Cndair CL6002C10 · Door Warning SystemSDR A6WA201040763Ring · damagedCONTAINMENT RING AT 5 O`CLOCK POSITION APPROX 1 IN LONG BY .2500 IN DEEP. REPLACED CONTAINMENT CASE IAW AMM 72-20-00. ALL CKS GOOD AT THIS TIME.Oct 10, 2010 · N446AW · Cndair CL6002B19 · Turbine Engine Reduction GearSDR A6WA201040772Bulkhead · crackedCRACK INDICATION AT WL 58.70 AND RBL9 REO601R5341260 REV E TO BE ACCOMPLISHED IAW AWAC JC 4MFG50672 AND 601R5341609 REV B AS NEEDED. REPAIRED CRACK ON FS 559 BULKHEAD AT WL 58.70 AND RBL 9 BY INCOPR OF REO 601R-53-41-260 REV E AND REO 601R-53-41-609, REV B7 DOct 10, 2010 · N423AW · Cndair CL6002B19 · Wing, Rib/BulkheadSDR A6WA201040832Skin · crackedPAX DOOR INNER SKIN EDGE MEMBER CRACKED UNDER TOP STEP NEXT TO BENDING JUMPER, AFT CORNER. REPAIRED PAX DOOR INNER SKIN EDGE MEMBER UNDER TOP STEP NEXT TO BONDING JUMPER AFT CORNER. IAW REO 601R-52-11-279, REV NC.Oct 10, 2010 · N450AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201040833Panel · crackedPAX DOOR STAIR STRUCTURE CRACKED ON 3RD STEP FROM TOP BOTTOM AFT CORNER ON THE STAIRFACE ZONE 3. REMOVED CRACK ON 3RD STEP FROM BTM AFT CORNER OF STAIR FACE IAW REO 601R-52-11-702, REV C, ZONE 4, TYPE 1 PG 8.Oct 10, 2010 · N450AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201040834Bracket · crackedPAX DOOR STAIR STRUCTURE IS CRACKED NEXT TO AFT HAND RAIL BRACKET ZONE 2. REPAIRED PAX DOOR STAIR STRUCTURE NEXT TO HAND RAIL BRACKET IAW REO 601R-52-11702, REV C.Oct 10, 2010 · N450AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201040829Bracket · wornSTUB FAIRING (RT) ATTACH BRACKET ON WING IS WORN. R & R RT STUB FAIRING ATTACH BRACKET ON WING IAW SRM 51-42-21.Oct 9, 2010 · N423AW · Cndair CL6002B19 · Wing Miscellaneous StructureSDR A6WA201040839Skin · chafedRT MLG DOOR CHAFED L/E R & R FILLER PN 601R-52-82-034-2 PREVIOUSLY INSTALLED IAW REO 601R-52-82-034, REV NC.Oct 9, 2010 · N450AW · Cndair CL6002B19 · Landing Gear DoorsSDR A6WA201040831Bracket · crackedGROUND POWER RECEPTICAL MOUNTING BRACKET CRACKED AT BOLT HOLES REMOVED DAMAGED BRACKET AND REPLACED WITH NEW SERVICEABLE PART, PN 600-33283-33.Oct 8, 2010 · N450AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201040842Vane · chafedLT INBD FLAP VANE (MOVEABLE) IS CHAFED IN 3 LOCATIONS ON L/E CHAFED AREAS WERE BLENDED, TREATED AND FOUND TO BE WITHIN ALLOWABLE LIMITS IAW REO 601R-57-52-004.Oct 7, 2010 · N450AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201040843Fitting · chafedRT OTBD FLAP ALIGNMENT FITTING CHAFED, C/W REO 601-57-51-143, REV NC.Oct 6, 2010 · N450AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201040841Guide · chafedRT OTBD FLAP ALIGNMENT GUIDE (FLAP SIDE CHAFED) AND ROLLER IS STIFF AND CRUNCHY C/W REO 601R-57-53-832.Oct 6, 2010 · N450AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201040844Guide · chafedLT WING OTBD FLAP ROLLER GUIDE CHAFED. C/W REO 601R-57-51-143, REV NC.Oct 6, 2010 · N450AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201040845Strip · chafedLT ENGINE UPPER NOSE COWL AFT EDGE STRIP IS CHAFED. REPAIRED LT ENGINE UPPER NOSE COWL BY FULLY INCORPORATING CMM 71-14-01, SRS 091.Oct 6, 2010 · N450AW · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR A6WA201040820Attach Fitting · crackedCLIP INBD RBL 9.00 AT FS 280.00 CRACKED. REMOVED CRACKED CLIP FS 280.00 INBD, RBL 9.00. DUPLICATED AND INSTALLED NEW CLIP AT FS 280.00, INBD RBL 9.00.Oct 5, 2010 · N450AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA201040837Structure · chafedMLG DOOR FWD LWR L/E CHAFED (LOWER). DAMAGED AREA WAS TRIMMED OUT AND REPLACED IAW REO 601R-52-82-034, REV NC.Oct 4, 2010 · N450AW · Cndair CL6002B19 · Landing Gear DoorsSDR A6WA201040846Intercostal · crackedOTBD CLIP ON INTERCOSTAL AT FS 484.00 AT LBL 36.00 IS CRACKED. REMOVED CRACKED CLIP, DUPLICATED AND INSTALLED NEW SERVICEABLE CLIP IAW REO 601R-53-41-059.Oct 4, 2010 · N450AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201040838Structure · chafedMLG DOOR FWD AND LWR L/E CHAFED (LOWER). BLENDED DAMAGED AREA AND WAS FOUND TO BE WITHIN ALLOWABLE LIMITS .020 MATERIAL LOSS, UP TO .030 IS ACCEPTABLE IAW REO 601R-52-82-033, REV A.Oct 4, 2010 · N450AW · Cndair CL6002B19 · Landing Gear DoorsSDR ASOA201001493Light · inoperativeFWD EMERGENCY LIGHTS WILL NOT ILLUMINATE. ITEM TRANSFERRED TO ASA DMIL NR 568377-2 IAW CUSTOMER.Oct 3, 2010 · N740EV · Cndair CL6002C10 · Emergency LightingSDR UIEA2010100100170Cadc · inoperativeAT FL 33.0 CAPT'S ALTIMETER READS 33,020. F/O ALTIMETER 32,520. AT FL 28.0 CAPT'S ALTIMETER READS 28000 F/O 27660. UNABLE TO CONTINUE INTO RVSM AIRSPACE. IAW ATC, CAPT'S & NBSP; ALTIMETER READS CORRECTLY. (FOUND NR 2 CADC AT FAULT. REPLACED NR2 CADC IAW MM 3Oct 1, 2010 · N517MC · Boeing 747243B · Air Data ComputerSDR ASOA201001453Lamp · burned outFLOOR LEVEL EMERGENCY FLOODLIGHT AFT OF SERVICE DOOR INOP. RELAMPED FLOOR LEVEL EMERGENCY FLOODLIGHT AFT OF SERVICE DOOR IAW AMM 33-51-11. RELAMPED FLOOR LEVEL EMERGENCY FLOODLIGHT AFT OF SERCICE DOOR IAW AMM 33-51-11. (CLOSED)Sep 27, 2010 · N744EV · Cndair CL6002C10 · Emergency LightingSDR A6WA201040849Bulkhead · crackedPARKING BRAKE FEED THROUGH AT FS 202 IS CRACKED. REPAIRED FS 202.75 BULKHEAD AT LBL 23.71, WL 69.795 IAW REO 601R-53-11-1982.Sep 26, 2010 · N451AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA201001450Placard · wornCREW REPORTED ASD EXIT PLACARD WORN. REMOVED TEMP PLACARD AND INSTALLED NEW PLACARD IAW AMM 11-30-02 DEFER CLEARED.Sep 25, 2010 · N719EV · Cndair CL6002C10 · Placards and MarkingsSDR QXEA2010092700565Regulator Valve · malfunctionedON TAXI OUT, ODOR OF SMOKE NOTICED. RETURNED TO THE GATE. REPLACED NR 2 ENGINE SEAL PRESSURE REGULATOR VALVE OP CHECK GOOD NO ODOR OF SMOKE. RETURNED TO SERVICE.Sep 22, 2010 · N606QX · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR A6WA201040851Support · crackedCARGO DOOR CAM TRACK SUPPORT CRACKED. R & R SUPPORT CHANNEL ON CARGO DOOR CAM TRACK IAW SRM 51-42-06.Sep 21, 2010 · N451AW · Cndair CL6002B19 · Cargo/Baggage DoorsSDR ASOA201001415Stringer · corrodedSTR 25R FS 280 HAS CORROSION AROUND FASTENERS KC161770. REMOVED STRINGER AND DRILLED UP NEW STRINGER IAW SRM 51-40-11-001-001.Sep 20, 2010 · N750EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA201001416Stringer · corrodedSTRINGER 26R, JUST AFT OF FS 280 HAS CORROSION AROUND FASTENERS. DRILLED NEW STRINGER AND FABRICATED SPLICE PIECES DRILLED ALL PARTS TO SIZE ALODINED & PRIMED PARTS REF SRM 53-00-03-991-803. INSTALLED SPLICE REPAIR & SEALED SPLICE, & APPLIED CIC OUTER SKIN Sep 20, 2010 · N750EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA201001418Cargo Track · corrodedCARGO BAY SEAT TRACK ARE CORRODED. APPLIED DINITROL ON FS 409+16 FRAME SECTOR IAW SRM 51-21-11.Sep 20, 2010 · N823AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201001419Placard · deterioratedPAX DOOR "EXIT" PLACARD IS DETERIORATED. R & R PAX DOOR EXIT PLACARD IAW AMM 11-30-00-000-801 AND 11-30-00-400-801.Sep 20, 2010 · N823AS · Cndair CL6002B19 · Placards and MarkingsSDR ASOA201001421Structure · crackedFOUND CRACK INDICATION APPROX .2500" IN LENGTH AT WL 58.7 AND RBL 9. COMPLIED WITH EC/TC REO 601R-53-41-260 AND REO 601R-53-41-260 REV E AND COMPLIED WITH EC/TC REO 601R-53-41-609 OR AND MET ALL THE REQUIREMENTS OF REO 601R-53-41-609 REV B (SHEET 3 TO 11 REV Sep 20, 2010 · N925EV · Cndair CL6002B19 · Fuselage Main, StructureSDR ASOA201001422Skin · crackedPAX DOOR INNER SKIN TO STAIR SUPPORT AFT DRAG ANGLE IS CRACKED. REPAIRED AFT DRAG ANGLE IAW REO 601R-52-11-513. C/W ASA EC/TC REO 601R-52-11-513.Sep 20, 2010 · N925EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201001423Rib · crackedBATTERY RIB IN LT W/W IS CRACKED. REPAIRED BATTERY RIB IN LT W/W WHICH WAS CRACKED IAW REO 601R-57-51-046, REPAIR NR 2.Sep 20, 2010 · N925EV · Cndair CL6002B19 · Wing, Rib/BulkheadSDR ASOA201001424Rib · crackedBATTERY RIB IN RT W/W IS CRACKED. REPAIRED BATTERY BIB RT IAW REO 601R-57-51-046, REV B. AND EC/TC 601R-57-51-046.Sep 20, 2010 · N925EV · Cndair CL6002B19 · Wing, Rib/BulkheadSDR QXEA2010092400553Sensor · malfunctionedRT ENG DEGRADE CAUTION MESSAGE AFTER COWL ANTIICE SELECTED ON DIVERED FOR OVER WEIGHT LANDING. DESCENT RATE AT 300 FT PER MIN UPON TOUCHDOWN. REPORTED CODE 351B,BIT 19, CW FIM TASK 72-00-00-810-804-A01. R & R T2 SENSORS K20 & K22 IAW TASK 24-05-07-000-801-ANSep 20, 2010 · N617QX · Cndair CL6002C10 · Power Indicating SystemSDR ASOA201001417Circuit Breaker · trippedFLAPS FAIL 30 CAUTION, EMERGENCY DECLARED. FLAPS FAIL RESET RESET IAW AMM 05-51-51-970-801-A01 RESET PROCEDURES. AS PER MCC, NO FURTHER ACTION IS REQUIRED.Sep 20, 2010 · N761ND · Cndair CL6002C10 · Trailing Edge Flap Control SystemSDR ASOA201001374Seat Track · corrodedONE SEAT TRACK AT RBL 9, FS 350.00 TO 485.00 CORRODED BEYOND LIMITS. REMOVED SEAT TRACK AT LBL 9 FS 350.00 TO FS 485.00 IAW AMM 53-00-49-000-801. FIT & DRILLED SEAT TRACK NR N126-2075 PO T-3525 IAW SRM 51-42-11-001-001-A01. ET INSP REF NDTM 51-20-006, NO DSep 17, 2010 · N740EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201001351Seat Track · corrodedSEAT TRACK 9R AT FS 485 TO FS581 SEVERELY CORRODED. SEAT TRACK 9A AT FS 485 TO 581 REMOVED IAW AMM 53-00-49-000-801. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801.Sep 16, 2010 · N750EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201001356Light · inoperativeTHE SERVICE DOOR EXTERIOR LIGHT IS INOP. REPLACED THE SERVICE DOOR EXTERIOR EMERGENCY LIGHT. DONE IAW THE AMM CHAPTER 33-51-21. (CLOSED)Sep 16, 2010 · N870AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201001357Battery Pack · inoperativeEXTERIOR EMERGENCY LIGHTS 7 AND 8 INOP. R & R NR4 EMERGENCY BATTERY PACK FOR LIGHTS IAW AMM 33-51-04. OPS CHECKS GOOD. NO DEFECTS NOTED. PLACARD REMOVED. DMIL CLEARED. (CLOSED)Sep 16, 2010 · N902EV · Cndair CL6002B19 · Emergency LightingSDR ASOA201001360Drag Angle · crackedPOSSIBLE CRACK ON AFT PAX DOOR DRAG ANGLE. REMOVED DAMAGED DRAG ANGLE AND INSTALLED A NEW DRAG ANGLE IAW SRM 51-42-06 AND 51-42-13.Sep 16, 2010 · N970EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201001361Floorbeam · crackedCABIN FLOORBEAM STRUCTURE HAS A CRACK AT FS 280.0 LBL 9.0 INBD CLIP. UPON FURTHER INVESTIGATION FOUND ADDITIONAL DAMAGE AT FS 280 BETWEEN RBL 9 AND LBL 9.Sep 16, 2010 · N970EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201001414Seat Track · corrodedLIGHT CORROSION LT SIDE SIDESEAT RAIL ROW 12 TO 17. R & R WITH SERVICEABLE SEAT TRACK IAW AMM TASK 53-00-49-400-801 AND TASK 53-00-49-000-801. INSTALL SCREWS RETAINED BY NUTS AND WASHERS IAWTASK 53-00-49-400-801. INSTALLED SCREWS WASHERS AND NUTS AS REQUIRESep 16, 2010 · N750EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201001433Seat Track · corrodedSEAT TRACK 9L AT FS269 AND FS613 AND FS 645 4EA MINOR CORROSION SPOTS. R & R SEAT TRACK 9L AT FS 589 TO FS 677 IAW AMM TASK 53-00-49-000-801 AND TASK 53-00-49-400-801.Sep 16, 2010 · N750EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
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