GE CF6-80C2D1F
Service difficulty reports · 536
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 = 'CF680C2D1F' 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 = 'CF680C2D1F' 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 FDEA201007272675Skin · crackedLT WING DROOP L/E UPPER OTBD SKIN CRACKED. REPAIR CARRIED OUT AT LT WING DROOP L/E UPPER OTBD SKIN IAW SRM 57-40-01, FIG 201, REV 43. FABRICATED REPAIR DOUBLER AND INSTALLED IAW SRM 57-40-01, FIG 201, REV 43. THIS REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-1SDR IPXA10M61557Skin · chafedINSPECTION TYPE:1C, RT WING TELESCOPIC DUCT CUTOUT DOUBLER CHAFED. REMOVED DOUBLER, CUTOUT DAMAGE,FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBLERS IAW SRM 57-40-01, REPAIR 10.SDR FDEA201006262190Vane · delaminatedDELAMINATION - LT WING INBD FLAP VANE LOWER SURFACE. REMOVED AND REPLACED AS PER AMM 27-50-22 REV 66 ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-50-22-830-801 REV 66.SDR FDEA201006212084Seat Track · corrodedMAIN DECK CARGO - FLOOR UNDERFLOOR SEAT TRACK INBD FLANGE STA 1199-1229 X=-8. FOUND MULTIPLE SURFACE CORROSION. SEAT TRACK REPAIRED IAW SRM 53-00-52, FIG 201. REPAIR 1, REV 43 THIS REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.SDR FDEA201006212087Seat Track · corrodedMAIN DECK CARGO - UPON REMOVAL OF FLOOR PANEL NR 281JF FOR SEAT TRACK ACCESS. FOUND SEAT TRACK STA 1741 X=75 OTBD FLANGE CORROSION. MAIN DECK CARGO CORRODED SEAT TRACK AT STA 1740-1 X= 75 O/B FLANGE REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 16SDR FDEA201006212081Skin · cracked01 EA FASTENER HOLE FOUND CRACK INDICATION DURING HFEC HOLE INSP AT LT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS=690 AND STA XORS=700. REPAIR CARRIED OUT AS PER EA 1-5710-140364. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100 REV 110.SDR IPXA0M60487Skin · puncturedINSP RT AIR COND BAY DOOR HAS A HOLE APPROX 2 INCH X 1.5 INCH D427388. DMI OPENED. C/O TIME LIMITED REPAIR IAW EO MD11-5240-31630-B APPENDIX A. ITEM DEF ERRED IAW EO MD11-5240-31630-B. PERMANENT REPAIR (IAW SRM VOL 1 52-10-00, FIG 1) OR REPLACEMENT AT OR ON SDR IPXA10M60326Engine · failedATB - NR 3 ENGINE FIRE WARNING SOUNDED FOR 5 SECONDS. THIS WAS ACCOMPANIED BY NR3 HYD FAIL AND NR 3 ENG FADEC MAIN ALERT. WE DUMPED ABOUT 85,000 LBS OF FUEL AND RETURNED TO ANC. ACFT OOS FOR REPAIR. REPLACED NR 3 RT ENG ON LP 381588/1. THIS DEFERRED ITEM TRANSDR FDEA201006021780Adc · malfunctionedDURING CRUISE FLIGHT AUTOPILOT CONNECTED RECEIVED STALL INDICATION (STICKSHAKER) AND RED IAS. IAS ON BOTH AIRSPEED TAPE READ APPROX 280KTS. STANBY AIRSPEED WAS 220 KTS. ACCOMPLISHED ERRACTIC AIRSPEED CHECKLIST AND FADEC ALT. CDG U PERFORMED STICK SHAKER ASDR FDEA201006021760Longeron Splice · crackedCABIN - 1 OFF LONGERON SPLICE AT STA 1511-1531 LONGERON 15R CRACK AT TOP CORNER AREA. REMOVED AND REPLACED AS PER SRM 51-31-01 REV. 43. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV.110SDR FDEA201006021761Seat Track · corrodedMAIN DECK CARGO COMPARTMENT SEAT TRACK AT STA. 1341 X= 8.5 FOUND WITH CORROSION. REPAIR CARRIED OUT FROM STA. 1331 TO 1371 X= 8.5 AS PER SRM 53-00-52 FIG. 201 REPAIR I REV. 43. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 110.SDR FDEA201005291714Seat Track · corrodedMAIN DECK CARGO SEAT TRACK INBD FLANGE FROM STA 1501 TO 5-0 X= 107 FOUND W/ SURFACE CORROSION. MAIN DECK CARGO CORRODED SEAT TRACK INBD FLANGE FROM STA 1501 TO 5-0 X= 107. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 1471 TO 1531 / 5-0 X= 107 IAW SSDR FDEA201005291715Seat Track · corrodedMAIN DECK CARGO SEAT TRACK INBD FLANGE AT STA 1481 X= 107 FOUND W/ SURFACE CORROSION. MAIN DECK CARGO CORRODED SEAT TRACK INBD FLANGE AT STA 1481 X= 107, REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 1471 TO STA 1531/5-0 X= 107 IAW SRM 53-00-52, FIG SDR FDEA201005291717Seat Track · corrodedMAIN DECK CARGO SEAT TRACK INBD FLANGE STA 1501-1521 X=-8 FOUND W/ SURFACE CORROSION. MAIN DECK CARGO CORRODED SEAT TRACK AT STA 1501 TO STA 1521 X=-8, REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 1491 TO STA 1531 X=-8 IAW SRM 53-00-52, FIG 201. REPASDR FDEA201005291719Seat Track · corrodedMAIN DECK CARGO SEAT TRACK CROWN STA 755 X=-47 FOUND W/ SURFACE CORROSION. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 725 TO STA 765 X=-47 IAW SRM 53-00-52, FIG 201. REPAIR REV 43. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.SDR FDEA201005291725Skin · bulgedSKIN BULGE ALONG FR STA 5-70 BETWEEN LONG 51R - 52R APPROX 4" LENGTH. BULGE SKIN AT FR STA 5-70 BETWEEN LONG 51R - 52R APROX 4" LENGTH TRIMMED OUT AND CARRIED REPAIR IAW SRM 53-00-01, FIG 201, REV 43. HFEC INSP CARRIED OUT IAW NDT SPM REV 13, 06-10-01.001SDR FDEA201005291726Skin · deformedSKIN DEFORMATION AT FR STA 5-70, BETWEEN LONG 49R - 50R. SKIN DEFORMED AT FR STA 5-70 BETWEEN LONG 49R -50R TRIMMED OUT AND CARRIED OUT REPAIR AS PER SRM 53-00-01 FIG 201 REV 43. HFEC INSP CARRIED OUT IAW DAC NDT SPM REV 13, 06-10-01.001 ON TRIMMED OUT ARESDR FDEA201005271680Wedge · delaminatedRT WING - OTBD FLAP T/E WEDGE INBD EDGE FOUND DELAMINATION. COMPLIED WITH EA 1-5750-140479.SDR FDEA201005271681Rib · crackedLT WING - NR 1 L/E SLAT INBD EDGE RIB FOUND CRACKED. LT WING NR1 L/E SLAT INBD EDGE RIB FABRICATED IAW DWG ARB 7128 REV L. RIB R & R IAW SRM 51-53-01, REV 43, LT NR1 SLAT ADJUSTMENT AND TEST CARRIED OUT IAW AMM 27-80-20-5, REV 66. FOUND SATISFACTORY. REPAISDR FDEA201005271682Support Fitting · crackedLT WING - NR 1 L/E SLAT INBD EDGE FWD LOWER FASTENER SUPPORT FITTING FOUND CRACKED AFTER REMOVAL. LW NR1 L/E SLAT INBD EDGE FWD FASTENER SUPPORT FITTING R & R IAW SRM 51-33-01, REV 43. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.SDR FDEA201005261656Skin · dentedRT WING - NR 4 SLAT L/E SURFACE FOUND DENT. RT WING NR 4 SLAT L/E SURFACE DENT EVALUATED AND FOUND WITHIN LIMIT IAW SRM 57-40-02, FIG 201. REPAIR G REV. 43. DEPTH OF DENT 0.032" DIA. OF DENT 1" AFFIXED A CLEAR DOT ADJACENT TO THE DENT AREA IAW GMM 6-3-101, REVSDR FDEA201005261655Skin · crackedLT WING - L/E LOWER ACCESS PANEL 519CB CUT-OUT FWN INBD CORNER FOUND CRACK. LT WING L/E LOWER ACCESS PNL 519CB CUTOUT FWD INBD CRACK CORNER TRIMMED OFF AND REPAIR CARRIED OUT IAW SRM 57-40-02, FIG 201, REPAIR 7, REV 43. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-SDR FDEA201005261657Skin · crackedRT WING - NR 6 L/E SLAT INBD TRACK CUT-OUT OTBD CORNER FOUND CRACKED. RT WING L/E SLAT NR6 INBD TRACK CUTOUT OTBD CRACK CORNER TRIMMED OFF AND REPAIR CARRIED OUT IAW ARM 57-40-02, FIG 201, REPAIR 7, REV 43. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.SDR FDEA201005251628Vane · delaminatedRT WING - INBD FLAP VANE LOWER SURFACE FOUND DELAMINATED. RT WING INBD FLAP VANE R & R IAW AMM 27-50-22-4, REV 66. FLAP VANE ADJUSTMENT AND TEST CARRIED OUT IAW AMM 27-50-22-5, REV 66 FOUND SATISFACTORY.SDR FDEA201005231618Relay · inoperativeIN LEVEL FLIGHT AT FL330, RECEIVED A LEVEL 1 BAT DISCHARGING ALERT. IT STAYED ON FOR ABOUT 3 MIN, WENT OUT FOR ABOUT 1 MIN, THEN REMAINED ON FOR THE REMAINDER OF THE FLIGHT. R & R R2-17 RELAY IAW SWP 24-31-00, OPS CHECK OF ELECTRICAL BATTERY IAW AMM 24-32-SDR FDEA201005161550Connector · corrodedAFTER T/O OAK GEAR SHOWED RED LT MAIN PRIMARY SECONDARY. COMPLED WITH CHECK LIST, RECKED GEAR PRIMARY SECONDARY BOTH SHOW GREEN LANDED MEM WITHOUT INCIDENT. INTERROGATED PSEU AND FOUND NO FAULTS ON SYS. TEST IAW AMM ATA 31-71-01-2. CHECKED D1-81 AND FOUNDSDR IPXA10M60180Vane · chafedINSPECTION TYPE:4C, LT WING OTBD FLAP VANE OTBD LOWER EDGE HAS CONTACT DAMAGE. REPAIRED FLAP VANE REF SRM 57-50-80 REPAIR 2 PARAGRAPH 2.A.(2)(A)SDR IPXA10M59840Fire Loop · false activationENGINE 3 FIRE WARNING ON DECENT. INTERMITTENT 3 TIMES EMERGENCY DECLARED IAW FIM 26-11-00-1-1. PERFORMED TESTS. R & R LOWER TURBINE FIRE LOOP WRT AMM 26-11-03-4 & 26-11-02-700-801. R & R GEARBOX FIRE LOOP WRT AMM 26-11-03-4 & 26-11-02-700-801. OPS CHECK GOOD.SDR FDEA201005131526Frame · misrepairedMAIN DECK CARGO - EXISTING REPAIR FOUND AT LT STA 535 FRAME ADJACENT TO 9G NET YOKE UPPER AND LOWER FITTINGS. EXISTING REPAIR AT MAIN DECK CARGO LT STA 535 FRAME ADJACENT TO 9G NET YOKE UPPER AND LOWER FITTINGS EVALUATED FOUND REPAIR NOT IAW ANY SRM REPAIR SDR FDEA201005131527Frame · misrepairedMAIN DECK CARGO - EXISTING REPAIR FOUND AT RT STA 535 FRAME ADJACENT TO 9G NET YOKE UPPER AND LOWER FITTINGS. EXISTING REPAIR AT MAIN DECK CARGO RT STA 535 FRAME ADJACENT TO 9G NET YOKE UPPER AND LOWER FITTINGS EVALUATED FOUND REPAIR NOT IAW ANY SRM REPAIR SCSDR IPXA10M59862Skin · puncturedINSPECTION TYPE:1C, RT WING FIXED L/E SKIN PUNCTURED BETWEEN STA XOS437 & XOS443. FABRICATED & INSTALLED REPAIR REF SRM 57-40-02 FIG 201 REPAIR 4 SHEET 4.SDR IPXA10M60184Longeron Splice · crackedINSPECTION TYPE:4C, CTR CARGO, BILGE, LONGERON SPLICE CRACKED AT L51L STA.5-113 TO 1541. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SPLICE REF DWG A5A7114 & SRM 51-31-01, 51-33-01SDR IPXA10M60048Skin · crackedINSPECTION TYPE:4C, LT WING L/E TELESCOPIC DUCT INBD CUTOUT FIXED L/E SKIN CRACKED AT RADIUS, GAINED ACCESS TO AREA. FABRICATED AND INSTALLED REPAIR REF MD1 SRM 57-40-01 REPAIR 10 FIG 201. RESTORED AREA.SDR IPXA10M59920Vane · damagedINSPECTION TYPE:4C, RT OTBD FLAP VANE DAMAGED AT EDGE OTBD END. FABRICATED AND INSTALLED REPAIR REF SRM 57-50-80. REPAIR 2 FIG 201 AND SRM 51-62-01.SDR IPXA10M60303Skin · delaminatedINSPECTION TYPE:4C, LT WING OTBD FLAP T/E INBD LOWER SURFACE, TAP TESTED AREA HAS DEAD SPOT, POSSIBLE DELAMINATION. REMOVED DAMGE, FABRICATED AND INSTALLED REPAIR PLYS IAW STA SA EA 011-5750-01-A2343 I/R AND UPS EO MD11-5750-38061-A.SDR FDEA201005061471Skin · crackedCRACK FASTENER HOLE (07 EACH) FOUND BETWEEN XORS 690 TO XORS 700 AT RT WING LOWER SKIN ACCESS DOOR CUTOUT. REPAIR CARRIED OUT IAW EA 5710-140304. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 110.SDR FDEA201005061472Skin · crackedCRACK FASTENER HOLE (09 EACH) FOUND BETWEEN XORS690 TO XORS700 AT LT WING LOWER SKIN ACCESS DOOR CUTOUT. REPAIR CARRIED-OUT IAW EA 1-5710-140305. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 110.SDR IPXA10M60293Spar Cap · corrodedINSPECTION TYPE:4C, EVIDENCE OF CORROSION UNDER WING SKIN AT LT WING REAR SPAR, SKIN BULGING NEAR STA XORS.650. GAINED ACCESS, REMOVED CORROSION, REPAIRED LT UPPER SPAR REF STA SA EA NR 011-5710-01-A2346 REV IR AND UPS EO MD11-5710-38030-A.SDR FDEA201005051461Skin · misrepairedAGING INSP - EXISTING REPAIR ON RT WING SLAT ASSY NR 6 LOWER SURFACE. EXISTING REPAIR ON RT WING SLAT ASSY NR 6 LOWER SURFACE EVALUATED, FOUND NOT IAW SRM. SLAT ASSY NR 6 R & R IAW AMM 27-80-30. OPERATION TEST CARRIED IAW AMM 27-80-30 FOUND SATISFACTORY. EOSDR IPXA10M59921Skin · crackedINSPECTION TYPE:4C, CRACK FOUND AS MARKED NEAR PREVIOUS REPAIR AT UPPER SKIN OF LT OTBD L/E COMPT STA XOS678. REMOVED EXISTING REPAIR DOUBLER, FABRICATED AND INSTALLED REPAIR REF SRM 57-40-02, REPAIR 9, FIG 203.SDR IPXA10M60045Skin · crackedINSPECTION TYPE:4C, CRACK FOUND AT UPPER SKIN WEB OF LT WING OTBD L/E COMPT STA XOS653-658 ON TOP OF WHEEL CABLE THRU ACCESS PANEL 519CB GAINED ACCESS TO AREA. FABRICATED AND INSTALLED REPAIR REF SRM 57-40-02, FIG 203, REPAIR 9, RESTORED AREA.SDR IPXA10M59663Power Supply · inoperativeDURING EMERGENCY LIGHT TEST LO BAT 1 MSG. REPLACED AND OPERATIONAL TESTED EMERGENCY LIGHT SYS IAW MM CH AP 33-51-01-04 AND 33-51-04-5. PN OFF AND ON 60-4411 SN OFF 33 SN ON35.SDR FDEA201005041443Skin · chafedEXISTING REPAIR DOUBLER FOUND AT APPROX STA 999 LONGERON 40 RT AT FWD CARGO DOOR JAMB LOWER AFT. EXISTING REPAIR DOUBLER AT STA 999 LONGERON 40 RT EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED IAW SRM 53-00-15, FIG 202 REPAIR 8, REVISION 43. CHAFED DOUBLER ON SDR FDEA201005041445Skin · chafedEXISTING REPAIR DOUBLER FOUND AT STA 2140, LONGERON 41 LT FUSELAGE SKIN. EXISTING REPAIR DOUBLER AT STA 2140 LONGERON 41 LT, FUSELAGE SKIN EVALUATED AND FOUND DOES NOT CORRELATE WITH ANY SRM. EXISTING REPAIR REACCOMPLISHED EA 1-5330-138496, TITLE: FUSELAGE -SDR FDEA201005041446Skin · damagedEXISTING REPAIR DOUBLER FOUND AT RT FUSELAGE STA 392 LONGERON 25 RT. EXISTING REPAIR DOUBLER AT RT FUSELAGE STA 392 LONGERON 25 RT, EVALUATED AND FOUND DOES NOT CORRELATE WITH ANY SRM. EXISTING REPAIR DOUBLER REMOVED IAW SRM 53-00-01 FIG 201, REV 43. DUE TO CASDR FDEA201005041452Frame · misrepairedEXISTING REPAIR (2 EACH) FOUND AT MAIN DECK FRAME STA 535 BETWEEN LONGERON 20 LT AND LONGERON 26 LT. EXISTING REPAIR (2 EACH) AT MAIN DECK FRAME STA 535 BETWEEN LONGERON 20 LT AND LONGERON 26 LT EVALUATED AND FOUND NOT IAW SRM. STA 535 MAIN DECK FRAME BETWEESDR IPXA10M60185Fairing · delaminatedINSPECTION TYPE:4C, LT WING INBD SLAT NR1 CRUISE PERFORMANCE FILLET L/E ERODED, DELAMINATED. REPAIRED CRUISE FAIRING REF SRM 51-62-01.SDR FDEA201005011409Rib · crackedLT WING - NR1 SLAT INBD EDGE RIB FOUND CRACKED. R & R IAW SRM 51-31-01 REV 43. OPERATION AND ADJUSTMENT TEST CARRIED OUT IAW AMM 27-80-20-4 REVISION 64 FOUND SATISFACTORY. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100, REV 110.SDR FDEA201005011421Seat Track · corrodedCORROSION - CABIN FLOOR SEAT TRACK, STA 2007, X = -47", IN AFT CARGO WASTE TANK COMPARTMENT CEILING. REPAIRED AS IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 43 AND EA 1-5310-138498. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.SDR FDEA201005011422Seat Track · corrodedCORROSION - CABIN FLOOR SEAT TRACK, STA 2007, X = 47", IN AFT CARGO WASTE TANK COMPARTMENT CEILING. REPAIRED IAW SRM 53-00-52 FIG. 201 REPAIR 1, REV 43 AND EA 1-5310-138498. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.
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