GE CF6-80 series
Service difficulty reports · 1,092
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 = 'CF680' 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 = 'CF680' 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 FDEA201008173032Starter · failedWITH 40 PERCENT N1 STABLE SELECTED TO GO NR2 ENGINE DID NOT ACCELERATE LOW SPEED REJECT DUE TO YAW, ON SECOND ATTEMPT STABLE AT 50 PERCENT N1 ROLLING T/O SELECTED TO GO AND HAD NORMAL ACELERATION. STARTER FAILED ON ENG START BY MX-- SUSPECT STARTER, STAYEDSDR FDEA201008163008Skin · misrepairedPREVIOUS EXTERNAL LAP SEAM REPAIR LOCATED AT LOWER FUSELAGE SKIN AT FRAME 66 AND BETWEEN STRINGERS 54 LT TO 56 RT. THE REPAIR FILLER MEASURES 19.3 IN X 11 IN AND THE REPAIR DOUBLER MEASURES 17.5 IN X 12.9 IN. AGING ACFT. PREVIOUSLY INSTALLED REPAIR LOCATED AT SDR FDEA201008163009Heat Exchanger · failedPASSING FL200, RECEIVED LEVEL 2 "ENG 1 OIL TEMP HI" FOLLOWED BY DECREASING OIL QUANTITY AND DECREASING PRESSURE. NR1 ENGINE WAS SHUTDOWN IAW CHECKLIST AFTER OIL QUANTITY REACHED ZERO. OIL TEMP PEAKED AT 167 DEG. AFTER SHUTDOWN NOTICED OIL QUANTITY INCREASINSDR HALA2010081400366Coupler · damagedETOPS SIGNIFICANT SYS - LT HF INOP (VOICE AND DATA MODES). REPLACED LT COUPLER, OPS CHECK OK IAW MM23-11-01.SDR HALA2010081300364Fcu · failedETOPS SIGNIFICANT SYS - APU FAILED TO START AT GATE. R & R APU FCU IAW AMM 49-31-01. R & R APU BATT IAW AMM 24-31-04. OPS & LK CK GOOD.SDR HALA2010081300369Igniter · failedETOPS SIGNIFICANT SYS - LT ENG EGT FAILED TO RISE W/IGN 2 SELECTED. RESTART NORMAL W/SW IN BOTH. R & R LT ENGINE NR 2 IGNITER IAW AMM 74-21-02/401. STARTED ENGINE USING NR 2 IGNITION SYS. OPS NORMAL.SDR FDEA201008122943Seat Track · damagedMDCC SEAT TRACK 4L HAS 2 LOCK TABS GOUGED AT FRAMES 54.3-55. BLENDED GOUGES ON SEAT TRACK IAW SRM 51-74-10. CHECKED LIMITS IAW SRM 53-10-16, FIG 101 AND FOUND OUT OF LIMITS. R & R SEAT TRACK 4L BETWEEN FRAMES 54.3 AND 55 IAW SRM 51-40-21.SDR HALA2010080900358Actuator · inoperativeETOPS SIGNIFICANT SYS - EICAS AILERON LOCKOUT CAME ON AT 300KTS. C/W R & R LT AILERON LOCKOUT ACTUATOR IAW TASK 27-11-44-022-004. OPS CHECK GOOD.SDR HALA2010080900359Transmitter · failedETOPS SIGNIFICANT SYS - NR 2 ENG OIL PRESS PEGGED OUT W/ENG SHUTDOWN. R & R NR 2 ENG OIL PRESSURE TRANSMITTER IAW AMM79-32-01. OPS & LEAK CK GOOD.SDR HALA2010080500357Computer · malfunctionedETOPS SIGNIFICANT SYS - R EICAS COMPUTER EICAS DISAGREE. REPLACED RT EICAS COMPUTER GROUND CHECK OK IAW MM 31-41-02.SDR HALA2010080400353Processor · malfunctionedETOPS SIGNIFICANT SYS - LT FUEL TANK QTY BLANK ON FLIGHT AND WING GAUGES DURING FUELING, CAME BACK AFTER AT 5 MINUTES THEN BLANK AGAIN FOR A FEW MINUTES CYCLE REPEATS FREQUENTLY. ACCOMPLISHED FIM 28-41-00-1, TABLE 151 NO FAULTS FOUND. ACCOMPLISHED DRY CAP TESDR DALA1019131612Light · inoperativeRED SEAT MOUNTED EMERGENCY LIGHTS ARE INOPERATIVE AT SEAT 19FG. MX REPLACED LIGHT ASSY AND THE SYS. OPS RETURNED TO NORMAL.SDR DALA1018641609Power Supply · inoperativeMX FOUND THE EMERGENCY PATH LIGHTS BETWEEN 24F AND 32F INOPERATIVE AND REPLACED M732 POWER SUPPLY. SYS OPS IS NORMAL.SDR FDEA201007292721Hmu · failedAT APPROX 300 FT INSIDE OF 1 MILE, NR 1 ENG SPOOLED DOWN.NO INDICATIONS OR WARNINGS ON ECAM OR OTHERWISE ENT BY: 110437 RPT BY: 115143 30JUL10 03:18 MEM R POWERPLANT ENGR REQUESTS T/SHOOT NR 1 ENGINE PER TSM 72-00-30 FIG.108; STEPS 1-4 COMPLIED WITH. STESDR UIEA2010072900129Doubler · crackedDURING D-CHECK INSP OF DATUM ACFT, EGAT FOUND THE REVEAL DOUBLER CRACK ABOUT 2.5 INCHES AT MAIN ENTRY DOOR NR 5 NEAR STA 2231 BETWEEN S-21L AND 22L. (REPAIR WAS ACCOMPLISHED IAW EGAT EI T2010A53B-1512 AND APPROVED BY MFG SR 1-1634841517 AND FAA 8100-9 DATED 0SDR UIEA2010072700120Skin · damagedDURING D-CHECK, A DENT THAT HAD INTERIM APPROVAL AND WAS CHECKED AT EVERY "A" CHECK UNTIL A PERMANENT REPAIR COULD BE ACCOMPLISHED, WAS LOCATED AT BS 682 AND STR 37R. (DAMAGE WAS TRIMMED OUT AND A DOUBLER AND FILLER WERE INSTALLED IAW SRM 53-00-01, REPAIR NR SDR ZI3R20100909Fuel Nozzle · leaking(ZI3R) A FUEL SPRAY NOZZLE REMOVED FROM ENGINE DURING A SERVICE CHANGE-OUT OF A NON-RELATED COMPONENT(FUEL FILTER). ONCE COMPONENT REPLACED & SYSTEM TESTED, NOTED FUEL EMITTING FROM A FSN IN AN AREA THAT NORMALLY DOES NOT SEE FUEL. THAT PARTICULAR NOZZLE WASSDR HALA2010072500325Warning Light · false activationETOPS SIGNIFICANT SYS - LT EEC LIGHT CAME "ON" ON ENGINE START. PERFORMED BIT ON EEC MONITOR. NO FAULTS NOTED. RESET SAME PERFORMED IDLE RUN. ALL CHECK GOOD.SDR HALA2010072500326Electrical Box · malfunctionedETOPS SIGNIFICANT SYS - NR 2 EGT DROPPED TO 16 DEG IN CLIMP, WITH ALL OTHER ENGINE READINGS NORMAL (BOTH EICAS AND STBY ENGINE GAUGES) EGT RESUMED NORMAL DISPLAY ABOUT AFTER TAKEOFF. PERFORMED FIM 77-21-00, FIG 103 INSPECTED THERMOCOUPLE PROBES NO DEFECTS NOTSDR FDEA201007252663Seat Track · crackedMAIN DECK - SEAT TRACK AT STA 6-70 X= 46 FOUND CRACKED. REMOVED AND FABRICATED NEW SEAT TRACK AND INSTALLED AS PER SRM 51-33-01 REV. 43 AND DWG AGA7082 REV. A. THIS REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 110.SDR FDEA201007252664Seat Track · gougedMAIN DECK - SEAT TRACK AT STATION 1293 X= 8.5 FOUND GOUGES ON FLANGE AREA. REPAIRED AS PER SRM 53-00-52 FIG. 201 REV. 43. THIS REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 110.SDR FDEA201007252666Longeron · crackedCTR CARGO COMPARTMENT RT TUNNEL AREA - STA 1673, LONGERON 30R, CRACKED. DAMAGED LONGERON REMOVED AS PER SRM 51-33-01 REVISION 43. CUTOUT CARRIED OUT AS PER SRM 53-00-05 FIGURE 201 REVISION 43. NEW LONGERON REWORKED AS PER DWG AFA7797 REVISION A AND NEW LONGESDR UIEA2010072400118Compressor · stalledCLIMBING OUT OF APPROX 3500' NR 4 ENG EMITTED 2 LOUD COMPRESSOR STALLS WITH ASSOCIATED SURGES IN N1, N2 AND EGT. SHUTDOWN NR 4 ENG SHUTDOWN ENG AT APPROX 2210Z. DUE TO SIGNIFICANT COMPRESSOR STALL, ELECTED TO COMPLETE THE "SEVERE ENG DAMAGE CHECKLIST", SO FIRESDR HALA2010072300336Engine · noneETOPS SIGNIFICANT SYS - BOTH ENG EGT WENT TO RED RANGE ON TAKEOFF EEC WAS OFF. LT ENG TEMP 941 DEG; RT ENG TEMP 956 DEG FOR 3 MIN OAT 33 DEG N1'S 108.0. IAW AMM TASK 71-00-00-862-002-G00 & SUB TASK 71-00-00-282-150-600. BOTH ENG EGT EXCEEDANCE TEMPS WITHIN LISDR UIEA2010072200116Seat Track · damagedDURING DAILY CHECK INSP, DAMAGE TO THE LWR AFT CARGO COMPARTMENT - BS 1880, RBL 46.0 SEAT TRACK - CRACKED / DAMAGE WAS FOUND (ACCOMPLISH REPAIR TO THE LOWER AFT CARGO COMPARTMENT. REMOVE/TRIM OUT THE SEAT TRACK DAMAGED SECTION IAW THE SRM 51-10-02. APPLED A SDR UIEA2010071700114Structure · damagedDURING SPECIAL CHECK (TLW); A STORM DRAGGED A MX STAND IMPACTING THE LT WING - OTBD L/E AT OLES1580.95, OLES1606.95 & OLES1625.951. DENT AT OLES 1580.95 (11.0 IN. LONG X 1.750 IN. WIDE X 0.187 IN. DEEP) REFERENCE FIG 1. EXCEEDS THE LIMITS IAW SRM 57-41-01 FIGSDR IPXA10661155Floor Panel · damagedMAIN DECK FLOOR PANEL POS 4L HAS A .5" HOLE. IDENTIFIED AS MAJOR REPAIR. INSTALLED FLOOR PANEL, SEALANT & TAPE REF MM 53-01-06-4, THIS CLEARS D411572.SDR FDEA201007162570Skin · corrodedRT WING UPPER SKIN SURFACE 8 INCH AFT OF REAR SPAR AND RIB 4 HAS 4 SQ INCH OF CORROSION COMMON TO FASTNER HEAD. REPAIR ACCOMPLISHED IAW EA 6-5730-135225 IAW APPROVED DATA REF 6, RAS/BAE/1013408/2010, ISSUE A. THE REPAIR IS IAW THE A/B REPAIR RECOMMENDATIOSDR FDEA201007152569Wire Harness · failedON CLIMB OUT PASSING FL 290, NR 2 ENGINE EGT COMPLETELY FAILED ( BOTH DIGITIAL AND ANALOG ) WITH - 2 PERCENT N1 AND N2 FLUX WITH - 200 POUNDS FUEL FLOW FLUX. UPON LANDING AT MEM - BOTH EGT'S WORKED NORMAL. R & R NR 2 ENG LOWER AND UPPER EGT HARNESSES IAW ASDR TAMF20100043SKeelbeam · corrodedDURING SC4 CHECKS INSP, FOUND FUSELAGE KEELBEAM WITH CORROSION AT LOWER CHORD STA 1010-1020 RT. REPAIR ACCOMPLISHED IAW EWO 767 53-101R0 AND SR 1-1624511669.SDR AALA20100714SJU01Fan Blade · bentPOS - CREW REPORTED BIRD STRIKE TO LEFT ENGINE ON TAKEOFF. VIBRATION ON LEFT ENGINE WENT TO MAXIMUM. EMERGENCY DECLARED RETURNED POS LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED DAMAGED FAN BLADES NUMBER 32 AND 33. SYSTEM GROUND CHECK SDR IPXA10661260Skin · misrepairedINSPECTION TYPE:C, SURVEY SEQUENCE NR 330-F1-01 THE EXISTING REPAIR DOES NOT CORRELATE TO A SRM JUST AT BS 143 TO BS 164 BETWEEN S21R AND S27R SURVEY SEQ 330-F1-01 FX SKIN REPAIRED IAW R53-11-36792 & EO B767-5330-38856 JUST AT BS143 TO BS164 BTN STR21R & SSDR FDEA201007092461Rib · corrodedFOUND CORROSION DURING A RIB 5 MOD INSP ON RT SIDE MLG SUPPORT RIB AFT PINTLE BEARING FWD LUG BORE AND FACES. THIS CORROSION WAS REMOVED BY OVERSIZING THE BORE AND SPOTFACING THE LUG FACES, NDT INSP (NO FINDINGS), AND INSTALLING OVERSIZE BUSHES IAW REPAIR INSDR FDEA201007082406Spar · corrodedVERTICAL STAB T/E PANEL ATTACH ANGLEAT RT SIDE HAS APPROX 2 SQ INCH OF VISIBLE CORROSION BETWEEN RIB 9 AND AT RIB 10 AT STA 286 AND 309 (2 EA LOCATIONS) BETWEEN RIB. REMOVED CORROSION FROM VERTICAL STAB T/E PANEL ATTACH ANGLE RT SIDE BETWEEN RIB 9 AND RSDR FDEA201007082421Rib · damagedRT WING KRUEGER FLAP FWD OTBD CORNER HAS IMPACT DAMAGE TO THE EXTERIOR SKIN & CLOSE OUT RIB. FOUND DAMAGE BEYOND ALLOWABLE LIMITS IAW SRM 57-41-11. REMOVED DAMAGED END CAP AND FABRICATED REPLACEMENT PART, END CAP, AND INSTALLED ON RT WING KRUEGER FLAP IAW SRSDR FDEA201007082422Skin · damagedFWD CARGO DOOR HAS DAMAGE STRUCTURE WEB AND HOLE BETWEEN FR 22A AND FR 23 AT BEAM 2. REMOVED DAMAGED AREA OF DOOR SKIN BY CUT OUT OF APPROX 2 IN X 3 IN AND INSTALLED FRAME, STRINGER AND SKIN REPAIR FILLERS AND DOUBLER BETWEEN FR 22 AND FR 23 AT BEAM NR 2 IAW SDR FDEA201007082425Rib · gougedLT WING L/E KRUEGER FLAP LOWER LIP OTBD L/E GOUGED, 2 SQ INCHES FOUND DAMAGE BEYOND ALLOWABLE LIMITS IAW SRM 57-41-11. REMOVED DAMAGED END CAP AND FABRICATED REPLACEMENT PART, END CAP, IAW DWG A57843755 AND INSTALLED ON LT WING KRUEGER FLAP OTBD L/E IAW SDR FDEA201007072394Floor Panel · corrodedFRAME 26 SEAT TRACK 4 LT OTBD JUST AFT OF CLS, FOUND CORROSION IN FLOOR PANEL, APPROX 1 SQ INCH REMOVED LEVEL 1 CORROSION. MATERIAL LOSS OUT OF LIMITS IAW SRM 53-10-00, FIG 102. R & R SHEAR PLATE BETWEEN FR 26/32 AND FR 36 AND SEAT TRACK 4LT AND SEAT TRACK 5SDR FDEA201007072395Floorbeam · corrodedMAIN DECK CARGO COMPT FLOORBEAM CORRODED ON UPPER SURFACE,FR 14 AT SEAT TRACK 3 LT REMOVED LEVEL 1CORROSION. REMOVED, FABRICATED REPLACEMENT TRACK SECTION AND REPLACED DAMAGED SECTION OF TRACK NR3 LT BETWEEN FR 10 AND FR 15A IAW SRM 51-72-10 AND SRM 53-12-15.SDR FDEA201007042344Skin · dentedRT WING INBD FLAP OTBD LOWER SURFACE FOUND WITH DENTS AT STA XIFH 293.910 TO XIFH 299.680. REPAIR CARRIED OUT AT RT WING INBOARD FLAP OUTBOARD LOWER SEGMENT AS PER SRM 57-50-01 FIG 201 REV 43. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100 REV 110.SDR FDEA201007022324Plate · corrodedSUB FLOOR CORRODED APPROX 1 SQ IN AFT OF FR 25 BETWEEN SEAT TRACKS 4 LT AND TRACK 3 LT REMOVED LEVEL 1 CORROSION. R & R SUB FLOOR THRUST PLATE BETWEEN FR 25 AND FR 26/32 AND BETWEEN SEAT TRACKS 3 LT AND 4 LT IAW SRM 51-72-10.SDR FDEA201007022327Floorbeam · corrodedMAIN DECK CARGO COMPT CROSSOVER BEAM HAS CORROSION ON UPPER SURFACE FR 14, BETWEEN SEAT TRACKS 3 LT AND 4 LT. REMOVED LEVEL 1 CORROSION. REMOVED DAMAGED BEAM, FABRICATED REPLACEMENT BEAM IAW DWG A53611789 AND INSTALLED REPLACEMENT BEAM IAW SRM 51-75-10.SDR FDEA201007022328Web · damagedWEB BETWEEN FRAME 12A AND 14, BENEATH TRACK 3 LT, IS DAMAGED. REMOVED DAMAGED WEB, FABRICATED REPLACEMENT WEB IAW DWG A53610800 AND INSTALLED REPLACEMENT WEB BETWEEN FR 12A AND FR 14 AT SEAT TRACK 3 LT IAW SRM 51-75-10.SDR FDEA201007022329Web · damagedWEB HAS DAMAGED HOLES AT FR 10 AND FR 12A SEAT TRACK 3 LT REMOVED DAMAGED WEB, FABRICATED REPLACEMENT WEB IAW DWG A53610800 AND INSTALLED REPLACEMENT WEB BETWEEN FR 10 AND FR 112A AT SEAT TRACK 3 LT IAW SRM 51-75-10.SDR P5CA2010070101644Thrust Reverser · damagedLOWER BALLSCREW REMOVED FROM LEFT SLEEVE OF THE NR 2 THRUST REVERSER. TIME LIMITED REPAIR ACCOMPLISHED PER AMM 78-31-00-& NBSP; EO 4478A133 AND FAA 8110-3 DATED 27 JUNE 2010. NOTE: DETAILED VISUAL INSPECTION IS DUE EVERY FLIGHT CYCLE UNTIL PERMANENT REPAIR SDR DALA1019070662Bulkhead · chafedNR 1 PYLON AFT BULKHEAD OTBD SIDE LWR AREA CHAFED. ACCOMPLISHED ER/A 483508-14AD, REV ORIG AT SAA DURING HMV ON N/R CARD 174462.SDR FDEA201006302227Proximity Sensor · malfunctionedLANDING GEAR HANDLE WOULD NOT RAISE BEYOND NEUTRAL ON POSITION DETECTOR SYSTEM 2. SYSTEM 1 WAS DEFERRED. RETURN TO LAND ACCOMPLISHED. R & R 55GB PROX SENSOR IAW 32-00-00-4. NO HELP. OHMD WIRES FROM PDU TO 55GB. ALL WIRES CHECKED GOOD. SWAPPED 55GB AND SDR IPXA10660741Floor Panel · damagedREF D 427434, P2 LT AFT HAS INTERIM REPAIR TO HOLE 1.75 DIA. (STA 390, LBL 62) REPLACED FLOOR PANEL IAW EO B767-5320-09793-G.SDR FDEA201006252147Wire Harness · failedAT APPROX 100 KTS TAKEOFF ROLE ENG NR 1 OIL QUANTITY INDICATED 0. TAKEOFF REJECTED AT 118 KTS. QRH PROCEDURES ACCOMPLISHED. RELEASED FOR SERVICE IAW MEL: 79-31-01 CATEGORY: B EXPIRATION: 28JUN10 "MEL 79-31-01: ENG NR 1, OIL QTY INDICATION - INOP. BEFORE EACSDR IPXA10661036Skin · misrepairedRT WING INBD AILERON EXISTING REPAIR PATCH NOT IAW SRM 57-60-01-2R1, TABLE 3 NOTE G. COMPOSITE WET LAY UP REPAIR CARRIED OUT AT EXISTING REPAIR PATCH AREA IAW EO B767-5750-38681 AND RS R57-60-36772.
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