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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR ASOA201001096Bulkhead · crackedFOUND FS 559 LT CAP ANGLE AT LBL 18.0 HAS INDICATION NOTED APPROX .2" IN LENGTH 80 PERCENT FSH AND FS 559 RT BULKHEAD WEB AT WL 59.10 INBD OF RBL 18.0 HAS INDICATION NOTED APPROX .2" IN LENGTH 60 PERCENT FSH, FAILED NDT INSPECTION. COMPLIED WITH EC/TC REO 601SDR ASOA201001170Frame · corrodedTHERE IS AN AREA OF LIGHT SURFACE CORROSION ON AFT FACE OF FS 349 JUST LT OF 6 O'CLOCK POSITION INTERNALLY. UPON ASSESSING THE DAMAGE, FOUND THE CORROSION ON AFT FACE OF FS 349.00 BOTTOM FRAME SECTION TO BE BEYOND ALLOWABLE LIMITS IAW SRM 53-00-00, FIG 102 (SDR A6WA201040586Skin · chafedRUDDER L/E SKIN IS CHAFED. REPAIRED DAMAGE ON RUDDER L/E SKINS IAW SRM 55-40-00.SDR ASOA201001082Engine · failedON FINAL APPROACH INTO NR 2 ENGINE HAD EXCESS VIBRATION AND THEN FAILED. HAD DETAILS OF OTHER SYMPTOMS. EMERGENCY DECLARED. (N2 WENT TO 0) (N2 TO 0) RT ENG WAS CHANGED REF WO 170440 FOR ALL WORK PERFORMED.SDR ASOA201001081Angle · crackedAFT EQUIPMENT COMPARTMENT FS 621.00 TO 625.00 OBLIQUE ANGLES LT AND RT SIDES ARE CRACKED .5" LONG IN AFT RADIUS. REMOVED CRACKED OBLIQUE ANGLES ON AFT EQUIPMENT COMPARTMENT AT LT AND RT SIDES OF FS 621 TO 625 IAW SRM 51-42-21. INSTALLED NEW SERVICEABLE OBLISDR ASOA201001076Computer · failedABNORMAL INCREASE OF FUEL IN CTR TANK. FUEL IMBALANCE MESSAGE. (ENROUTE, ACFT DIVERTED DUE TO MX -- EMERGENCY DECLARED) R & R FUEL COMPUTER AND REFUEL/DEFUEL PANEL IAW AMM 28-41-16, OPS CHECK GOOD AND 28-25-16 OPS CHECK GOOD. (CLOSED)SDR QXEA2010080200456Light · malfunctionedEMERGENCY LIGHTS ARE INOP. PERFORMED OPS CHECK OF LIGHTS WITH NO DEFECTS NOTED. COULD NOT DUPLICATE. IAW AMM 33-51-00-710-801-A01. NO PARTS REPLACED.SDR MALA100103Proximity Sensor · out of toleranceAFTER SELECTING GEAR UP ON TAKEOFF, RECEIVED A GEAR DISAGREE AURAL WARNING AND TRIPLE CHIME ON EICAS MSG. RAN POM CHECKLIST AND PULLED EMERGENCY GEAR EXTENSION HANDLE. NOSE GEAR INDICATION WAS RED BOX. AFTER RUNNING CHECKLIST WE GOT 3 GREEN LIGHTS. FOUND NLSDR QXEA2010071600418Stringer Clip · corrodedC-CHECK - FOUND CORROSION ON ATTACH ANGLE FOR STRINGER 26R AT FS 333.00. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. CORROSION FOUND TO EXCEED ALLOWABLE LIMITS IAW SRM 53-21-003-101-002-A01. REMOVED ATTACH ANGLE IAW SRM 51-42-06-001-001-A01. LOCATED FASSDR QXEA2010070800388Seat Track · corrodedC-CHECK - RT SIDE SEAT TRACK HAS CORROSION PRESENT BETWEEN FS814 AND FS863. BLENDED CORROSION ON RT SIDE SEAT TRACK, ORIGINAL THICKNESS .260, REMOVED .040, MAX ALLOWABLE IS .035, REMAINING MATERIAL IS .220. BLEND IS OUT OF LIMITS IAW REO 670-53-00-013. REMOSDR ASOA201000984Bulb · inoperativeRT OVERWING EMERGENCY LIGHT INOP. R & R EMERGENCY LIGHT BULB IAW AMM 33-51-21 OP CK GOOD. ITEM: 1, R & R EMERGENCY LIGHT BULB IAW AMM 33-51-21. OPS CK GOOD.SDR ASOA201000986Bulb · burned outLT OVERWING EMERGENCY LIGHT BULB INOP. R & R LT OVERWING EMERGENCY LIGHT BULB IAW AMM 33-51-21. OPS CHECK GOOD. ITEM: 1 R & R LT OVERWING EMERGENCY LIGHT BULB IAW AMM 33-51-21. OPS CHECK GOOD.SDR ASOA201000963Relay · failedDURING CRUISE, RECEIVED A SPOILERONS CAUTION MESSAGE ,FOLLOWED BY A FLT SPOILERS CAUTION MESSAGE FOLLOWED BY AN INBD GROUND SPOILER FAULT STATUS MESSAGE (EMERGENCY DECLARED) R & R RELAY K3CN FOR SECU POWER SUPPLY IAW ESPM 20-22-00 OPS CHECK GOOD JB-10 RETESTSDR ASOA201000916Seat Track · corrodedLEFT WALL SEAT TRACK AT FS 559+75 IS CORRODED. REMOVED CORRODED SEAT RAIL SECTION ON LT WALL IAW AMM 53-01-11-000-802. INSTALLED NEW RAIL SECTION IAW AMM 53-01-11-400-802.SDR ASOA201000917Sill · crackedSUPPORT ANGLE AT FS 589.00, LBL 36 UNDER CARGO DOOR FLOOR SILL IS CRACKED. LOCATED & INSTALLED NEW SUPPORT ANGLE IAW SRM 51-42-06 & 51-42-21.SDR ASOA201000919Pressure Panel · corrodedLEFT PRESSURE FLOOR SKIN OTBD OF LBL 36 HAS AREAS OF CORROSION. C/W REO 601R-53-41-666, REV A.SDR ASOA201000920Frame · corrodedLEFT FRAME 513.00 HAS CORROSION AT PRESSURE FLOOR. COMPLIED WITH STEP 2 OF REO 601R-53-41-1241. PERFORMED EDDY CURRENT OF LT FRAME 513 AT PRESSURE FLOOR REPAIR IAW NDTM 51-20-06. NO INDICATIONS NOTED AT THIS TIME. COMPLIED WITH STEPS 3, 4 AND 5 OF REO 601R-SDR ASOA201000921Bulb · inoperativeRT FWD EXTERNAL EMERGENCY LIGHT INOP. REPLACED EMERGENCY LIGHT BULB IAW AMM 33-51-21.SDR ASOA201000914Intercostal · crackedFS 625 INTERCOSTAL CLIP AT LBL 45 WL 97.5 IS CRACKED. R & R INTERCOSTAL CLIP IAW REO 601R-53-61-422. REPAIRED INTERCOSTAL CLIP IAW ECTC 601R-53-61-422.SDR ASOA201000915Flashlight · inoperativeCAPT'S FLASHLIGHT INOP. REPLACED CAPT'S FLASHLIGHT. OPS CHECK GOOD. REF AMM 25-60-00.SDR ASOA201000925Attach Fitting · crackedFS 484, LBL 36 INTERCOSTAL CLIP IS CRACKED. REMOVED DAMAGED REPAIR ANGLE IAW SRM 51-42-21. FABRICATED NEW SERVICEABLE REPAIR ANGLE IAW REO 601R-53-41-059, STEP 13. C/W LPIP OF FS 484, LBL 36 FABBED CLIP IAW NDTM PT 1 51-20-08. NO INDICATIONS NOTED AT THISSDR ASOA201000913Battery Pack · inoperativeMAIN CABIN EMERGENCY LIGHTING , NR 2 BATTERY PACK INOP. REPLACED EMERGENCY LIGHT BATTERY PACK NR 2, OPS CHECKED IAW MM 33-51-00. OPS CHECK GOOD.SDR ASOA201000912Lens · crackedMAIN CABIN PASSENGER CABIN G1 GALLEY EMERGENCY EXIT LIGHT LENS CRACKED. R & R EMERGENCY EXIT SIGN LENS IAW AMM 33-51-10. DEFER CLEARED. PLACARD REMOVED.SDR ASOA201000910Sign · inoperativeMAIN CABIN BOTH EMERGENCY EXIT SIGNS AT RT SIDE CLASS DIVIDER INOP. COMPLIED WITH RIL NR 2029 707 LETTER FOR INSTALLING WIRES FOR EMERGENCY EXIT SIGNS AT RT SIDE CLASS DIVIDER AND PERFORMED SUCCESSFUL OPS TEST OF EMERGENCY LIGHT IAW AMM 33-51-00-710-801-A01 ASDR ASOA201000923Detector · failedFLAPS FAIL AT FL 350 LANDED IN ATL WITH FLAPS 1 DEGREE IAW QRH. (EMERGENCY DECLARED) R & R LT OTBD SKEW DETECTOR AS REQUIRED IAW AMM 27-50-01, TRIED TO RIG SKEW DETECTOR MDC SHOWED SFECU 2 NO COMM REFER TO AFDL NR 535400-2 FOR CONTINUATION. (CLOSED)SDR ASOA201000906Lamp · inoperativeEMERGENCY LIGHT ON SIDEWALL AT SEAT 12CD HAS INOP LAMPS. R & R FLOOR LEVEL EMERGENCY FLOOD LIGHTS AS REQUIRED IAW AMM 33-51-05. OPS CHECK GOOD.SDR ASOA201000922Flap System · failedFLAPS FAIL CAUTION IN CRUISE FLIGHT. (EMERGENCY TRUCKS REQUESTED AS A PRECAUTION - EMERGENCY DECLARED BY TOWER) T/S IAW FIM 27-52-45. PERFORMED CLEAR INHIBITS AND LRU TEST. FLAP FAIL MSG CLEARED. FLAPS AND SLATS OPS CHECK GOOD. (CLOSED)SDR ASOA201000924Reservoir · wornRECEIVED NOSE GEAR DISAGREE WARNING MSG AFTER T/O, CYCLED GEAR AND GOT GEAR DISAGREE MSG AND NOSE DOOR WARNING MSG. (EMERGENCY EQUIPMENT REQUESTED AS A PRECAUTION) (LANDING GEAR RETRACTION SYS ) REFER TO LOG PAGE 532717-3 HYD RESERVOIR, REPLACED. PERFORMEDSDR ASOA201000908Intercostal · crackedAFT EQUIPMENT COMPARTMENT FS 621.00 TO 625.00 ANGLE AT STR 14R IS CRACKED. REMOVED DAMAGED ANGLE AT FS 621.00 - 625.00 AT STR 14R AND INSTALLED SERVICEABLE ANGLE (INTERCOSTAL) IAW SRM 51-42-21.SDR ASOA201000856Bulkhead · corrodedFS 280.00 BULKHEAD LT SIDE LOWER WEB HAS CORROSION DAMAGE. REMOVED LT SIDE FS280 BULKHEAD LOWER WEB IAW SRM 51-42-06-001-001-A01. DRILLED ALL HOLES IN LT SIDE 280 LOWER PANEL, FASTENER HOLES DRILLED IAW SRM 51-40-11-001-001-A01. INSTALLED ALL FASTENERS IN LSDR ASOA201000853Unknown · smokeFLT U:7135--PASSENGERS IN 10 A&B COMPLAINED OF SMOKE ON SHORT FINAL (EMERGENCY DECLARED - TRUCKS STANDING BY AS A PRECAUTION) PERFORMED SYS CKS AND INSP OF BOTH ENG'S BOTH PACK SYS AND APU NO FAULTS FOUND NO LEAKS NO SMOKE OR SMELL. LT & RT PACK ACM SERVICEDSDR ASOA201000854Manifold · intermittentSTEERING INOP CAUTION MSG AFTER GEAR EXTENSION COMPLIED WITH QRH, MSG CLEARED, EXTENDED GEAR AGAIN, MSG REAPPEARED 1 MINUTE LATER. CONTINUED WITH QRH, TURNED OFF NWS AND LT IT OFF, MSG CLEARED (EMERGENCY DECLARED -- TRUCKS STANDING BY AS A PRECAUTION) TS AND SDR ASOA201000907Floor Support · corrodedCARGO BAY FLOORBEAM CAP AT LBL 27 HAS MINOR CORROSION AROUND FASTENER HOLES FOR FLOORBOARD ON OTBD SIDE OF CAP FROM FS 621.0+0 TO FS 574.0. REPAIRED IAW REO 601R-53-61-3400 AND 601R-53-61-3688SDR SWIA201024262Engine · failedLEFT ENGINE VIBRATION, ITT OVERTEMP, AND LOSS OF OIL PRESSURE ON CLIMBOUT. (FLT 6641) REPLACED THE LEFT ENGINE ASSEMBLY. P/N ON (ENGINE) CF34-3B1 S/N OFF 873779.SDR N6WA20100407Light · inoperativeCEILING EMERGENCY FLOODLIGHT AT ROW 7 INOP. DEFERRED CEILING EMERGENCY FLOODLIGHT AT ROW 7 ON DMI NR 12725 IAW MEL 33-51-01B CAT C.SDR N6WA20100401Light · missingFLOOR EMERGENCY LIGHTING STRIP MISSING AT EXIT ROW 12C. MOVED LIGHT STRIP FROM ROW 2C TO ROW 12C. DEFERRED FLOOR PATH LIGHTING AT ROW 2C IAW MEL 33-51-01G CAT C.SDR QXEA2010032900205Flap System · failedON TAXI IN THE FLAPS FAIL CAUTION ILLUMINATED. ACFT DOWN FOR REPAIRS.SDR QXEA2010032900206Slat System · failedSLATS FAIL. MDC INDICATED SLAT SYS MECHANICAL JAM IN FAULT HISTORY CW OPS TEST OF THE FLAP AND SLAT SYS IAW AMM TASK 27-50-00-710-801 NO DEFECTS NOTED CW VISUAL INSP OF SLATS AND SLAT TRACK ASSYS WITH SLATS EXTENDED AND RETRACTED NO DEFECTS NOTED. RETURNED TOSDR A6WA201040232Apu · odorAFTER APU START-UP, JET A SMELL IN COCKPIT. R & R NR 1 PACK COALESCER IAW AMM 21-51-13. OPS CK GOOD, SUSPECT APU OIL OVERSERVICED, CLEANED UP OIL, NO LEAKS NOTED.SDR ASOA201000292Floorbeam · corrodedUPON INSP, FOUND CORROSION AT FWD END OF FLOOR SUPPORT BEAM LBL 9 AT 280 ATTACH BRACKET UNDER FLOOR BEAM CAP. REMOVED RIVETS TO SEPARATE CAP FROM FLOORBEAM AT FS 280, LBL 9 BLENDED CORROSSION REMOVED DAMAGE REF. 51-42-06-001-001-A01 & 51-21-06-001-001-A01 SUBSDR 2010FA0000200Frame · crackedFWD FUSELAGE FRAME AT FS 235 ABOVE FLOOR, PILOTS AND COPILOTS SIDE, FOUND CRACKED DURING 240 MONTH INSP.SDR SWIA201023414Mount · corrodedLEFT ENGINE FORWARD LINK AND BUSHING PITTED. (ENG CHANGE) REPLACED YOKE LINK AND BUSHING.SDR SWIA200923362Fuel Control · failedENGINE OIL WARNING WITH ENGINE SPOOLING DOWN. (FLT 6044) REPLACED FUEL CONTROL AND FUEL PUMP.SDR ASOA20100001Ecu · failedIAW FIM 32-50-00 R & R NWS ECU IAW AMM 32-51-10. OPS CHECK GOOD. (CLOSED)SDR 2009FA0001063Bushing · crackedPROBLEM FOUND ON THRUST REVERSER REMOVED FROM ACFT. UPON PRELIMINARY INSP AT APPLIED COMPOSITES ENGINEERING (ACE) IT WAS DISCOVERED THAT ONE FWD HINGE BUSHING PN 14G0311-203 WAS CRACKED ACROSS THE SHOULDER AND AROUND THE TRANSITION FROM THE RADIAL TO THE FLANSDR SWIA200923301Mount · corrodedRIGHT ENGINE FORWARD MOUNT, BEARING SURFACES ARE CORRODED. (ENG CHG) REPLACED RIGHT ENGINE FORWARD MOUNT.SDR SWIA200923300Module · crackedRIGHT ENGINE LPT MODULE CRACKED. (FLT 6458) REPLACED RIGHT ENGINE.SDR 2009F00146Megaphone · weakTHE ACFT WAS IN THE PROCESS OF A INSP AN A-CHECK AND THE MEGA PHONE IS ONE OF THE INSP AND IT WAS DISCOVERED THAT THE MEGA PHONE WAS WEAK FUNCTIONING AND THE BATTERY WAS REPLACED AND THE MEGA PHONE OPS CHECK WAS GOOD AND THE ACFT WILL BE PUT BACK IN SERVICE FSDR 2009F00134Push-Pull Rod · brokenACFT CABIN WOULD NOT PRESSURIZE. PERFORM GROUND CHECK AND FOUND CABIN DOOR PRESSURE VALVE IN THE OPEN POSITION. INSP FOUND THE PUSH-PULL ROD WAS BROKEN AND NOT ALLOWING THE DOOR PRESSURE VENT FLAP, PN: 601R38634-7, TO CLOSE.SDR CHQA200900250Windshield · delaminatedDURING CRUISE THE FLIGHT CREW REPORTED THAT THE WINDSHIELD WAS BEGINNING TO DELAMINATE. IT WAS DECIDED TO DIVERT TO KSDF DUE TO PARTS AND MAINTENANCE ON SITE. THE AIRCRAFT DIVERTED TO KSDF AND LANDED WITHOUT INCIDENT. MAINTENANCE IS CURRENTLY IN THE PROCESS
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