GE CF6-80C2B1F
Service difficulty reports · 768
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 = 'CF680C2B1F' 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 = 'CF680C2B1F' 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 IPXA10B63027Skin · misrepairedINSPECTION TYPE:C, SURVEY SEQ NR580-F1-11, FUSELAGE SKIN AT BETWEEN BS1697 TO BS 1723 AND STR 44R-47R EXISTING REPAIR DOES NOT CORRELATE TO EFN 58020071001. SKIN REPAIRED IAW RS R53-00-36836 & EO B747-5330-4005-A. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR. SDR IPXA10B61886Floor Panel · damagedFLOOR PANEL, POS 5L, DAMAGED. REPAIRED IAW SRM 53-00-50-2R-1, PARA 4 C.SDR IPXA10162096Skin · gougedINSPECTION TYPE:4C, REPAIR SURVEY NR 135-W3-01, LT WING CTR FLAP UPPER SKIN REPAIR DOUBLER IS GOUGED. ACCOMPLISHED REPAIR IAW SRM 57-50-00, PB 201 PARA E AND FIG 205 AND SRM 57-51-12-201, PARA 4 AND FIG 209.SDR IPXA10B62625Fairing · delaminatedINSPECTION TYPE:C, RT WING OTBD MID FLAP L/E FAIRING PUNCTURE. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5C, FIG 2, REV 57.SDR IPXA10B62732Panel · crackedINSPECTION TYPE:C, LT WING LG INBD STRUT DOOR LOWER FAIRING FWD CUTUT PANEL FOUND CRACKED. LT WING LANDING GEAR W/W FWD CUTOUT FAIRING PNL SKIN REPAIRED IAW HX RS NR R-53-27-36808, REV A & EO B747-5320-39567-A. THIS REPAIR IS CLASSIFIED AS MINOR REPAIR. 3" SKSDR IPXA10B61902Skin · damagedINSPECTION TYPE:C, CARGO DOOR DAMAGE IAW SRM (REF DI 431689). FWD CARGO DOOR AFT LOWER CORNER EXT SKIN ASSY REPAIRED IAW RS52-34-36802 & EO B747-5230-39172-A JUST BETWEEN BS 650-670 & STR38R - 39R, ORG MATL IS CLAD2024-T3 0.062" AS SKIN & 2024-T3 0.190" (CHESDR IPXA10B61910Skin · misrepairedINSPECTION TYPE:C, SURVEY SEQUENCE NR 581-F1-05 FWD CARGO DOOR SKIN AND LOWER BEAM AT BETWEEN BS 653-670 AND STR 38R-40R AREA EXISTING REPAIR DOES NOT CORRELATE TO EFN 58120041002. BS653-BS670 & STR 38R-40R AREA REPAIRED & ACCEPTABLE RESPECTIVELY IAW HX RS R5SDR UIEA2010072700125Stiffener · crackedDURING D-CHECK INSP OF DATUM ACFT, SEVERAL LIGHT CORROSIONS WERE FOUND ON STIFFENERS AND PANELS UNDER KEEL TORQUE BOX AT STA 1265 TO STA 1480, RBL 9 TO LBL 9 (REF FIG 1). (THE CORROSION AREAS WERE BLENDED OUT, TRIMMED IAW EGAT EI T2010A53B-1516 AND APPROVED BSDR UIEA2010072700126Web · gougedDURING D02/C03 CHECK, GOUGE DAMAGE WAS FOUND TO THE MAIN DECK BS 1917, RBL 49 WEB OF LATERAL GUIDE SUPPORT (REF FIG 1 THRU 3, PN 65B20024-65). GOUGE WAS CLEANED, BLENDED OUT AND REWORKED IAW EGAT EI T2010A53B-1513 ON WEB IAW THE SRM 53-60-53 WITHIN ALLOWABLESDR UIEA2010082200142Nozzle · crackedDURING MX WALK AROUND, MX FOUND (1EA) CRACK ON THE EXHAUST NOZZLE OUTER SLEEVE, STARTING AT APPROX THE 11 O'CLOCK POSITION. THE CIRCUMFERENTIAL CRACK IS APPROX 35.0 IN. LONG. IAW SRM 54-41-30 THE LENGTH OF THE CRACK IS OUT OF LIMITS. DISPOSITION IS TO STOP DRSDR UIEA2010082600122Stiffener · crackedDURING D-CHECK, THE NR2 STRUT WAS FOUND TO HAVE A CRACK IN A STIFFENER TEE ANGLE ON THE INBD SIDE NEAR NAC STA 377 AND NAC WL 155. SEE FIG 1 FOR DAMAGE LOCATION AND REPAIR DETAILS. (THE DAMAGE WAS CUT OUT WITH AN ANGLE AND FILLERS BEING INSTALLED AS SHOWN IN FSDR IPXA10B61586Wedge · misrepairedINSPECTION TYPE:C, LT WING OTBD AILERON T/E WEDGE UPPER SURFACE EXISTING REPAIR (NO REPAIR RECORD). FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A(1) FIG 5, REV 57.SDR IPXA10B61587Panel · unknownINSPECTION TYPE:C, LT WING OTBD AILERON UPPER PANEL EXISTING REPAIR (REDO) SURVEY SEQ NR 581-W3-74 (NO REPAIR RECORD). FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A(1) FIG 5, REV 57.SDR IPXA10B61589Panel · unknownINSPECTION TYPE:C, LT WING OTBD AILERON UPPER PANEL EXISTING REPAIR (REDO) NO REPAIR RECORD. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5A(1), FIG 5, REV 57.SDR IPXA10B61590Panel · unknownINSPECTION TYPE:C, LT WING OTBD AILERON UPPER PANEL EXISTING REPAIR (REDO) SURVEY SEQ NR 581-W3-04. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A(1) FIG 5, REV 57.SDR IPXA10B61592Panel · noneINSPECTION TYPE:C, LT WING OTBD AILERON T/E WEDGE UPPER SURFACE EXISTING REPAIR (REDO) REF SURVEY SEQ NO 581-W3-09 (NO REPAIR RECORD). FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5A(1) FIG 5, REV 57.SDR IPXA10B61515Skin · dentedINSPECTION TYPE:C, LT WING NR6 SPOILER UPPER SURFACE FOUND DENTED. METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10-2R, REPAIR 4, FIG 201, SHEET 1, REV 56.SDR IPXA10B61585Panel · noneINSPECTION TYPE:C, LT WING OTBD AILERON T/E WEDGE LWR SURFACE EXISTING REPAIR. (NO REPAIR RECORD) FIBERGLASS PREPREG LAYUP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5A(1) FIG 5, REV.57.SDR IPXA10B61597Wedge · misrepairedINSPECTION TYPE:C LT WING INBD FORE FLAP T/E WEDGE LWR SURFACE EXISTING REPAIR NON-STANDARD. REPAIR FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5C, FIG 2, REV 57.SDR IPXA10B61598Wedge · misrepairedINSPECTION TYPE:C, LT WING INB FORE FLAP T/E WEDGE LWR SURFACE EXISTING REPAIR NON-STANDARD. REPAIR FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5 C, FIG 2, REV 57.SDR IPXA10B61600Wedge · misrepairedINSPECTION TYPE:C LH WING I/B FORE FLAP T/E WEDGE LWR SURFACE EXISTING REPAIR NON-STANDARD REPAIR FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-07 PAR 5.C FIG.2 REV 57.SDR IPXA10B61601Wedge · misrepairedINSPECTION TYPE:C LT WING INBD FORE FLAP T/E WEDGE LWR SURFACE EXISTING REPAIR NON-STANDARD. REPAIR FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5 C, FIG 2, REV 57.SDR IPXA10B61602Wedge · misrepairedINSPECTION TYPE:C, LT WING INBD FORE FLAP T/E WEDGE LWR SURFACE EXISTING REPAIR NON-STANDARD REPAIR. FIBERGLASS PREPREG LAYUP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5.C, FIG.2, REV.57.SDR IPXA10B61603Wedge · misrepairedINSPECTION TYPE:C, LT WING INBD FORE FLAP T/E WEDGE LWR SURFACE EXISTING REPAIR NO-STANDARD. REPAIR FIBERGLASS PREPREG LAY UP. REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5C, FIG 2, REV 57.SDR IPXA10B61502Wedge · delaminatedINSPECTION TYPE:C, LT WING OTBD AFT FLAP T/E WEDGE LWR SURFACE DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SEM 51-70-07, PAR 5A (1) FIG 5, REV 56.SDR IPXA10B61505Wedge · delaminatedINSPECTION TYPE:C, LT WING OTBD FORE FLAP T/E WEDGE UPPER SURFACE DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5A(1) FIG 5, REV 56.SDR IPXA10B61514Wedge · delaminatedINSPECTION TYPE:C, LT WING OTBD AFT FLAP T/E WEDGE LWR SURFACE DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5A(1) FIG 5, REV 56.SDR IPXA10B61593Wedge · delaminatedINSPECTION TYPE:C, LT WING OTBD AFT FLAP T/E WEDGE LWR SURFACE DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5A(1) FIG 5, REV 56.SDR IPXA10B61501Panel · delaminatedINSPECTION TYPE:C, LT WING OTBD MID FLAP T/E COVE PANEL UPPER SURFACE DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A(1) FIG 5, REV 56.SDR IPXA0B61955Skin · dentedINSPECTION TYPE:C, LT WING INBD AFT FLAP LWR SKIN FOUND SEVERAL DENTS. SKIN METAL HOT BOND INTERIM REPAIRED IAW HX RS R57-51-36778 REV A AND EO B747-5750-39125-A. THIS IS A MAJOR REPAIR WITH ALUMINUM SHEET: 2024T3-0020IN. REPAIR PATCH SIZE: 36.5" X 19". FINSDR IPXA0B61956Skin · dentedINSPECTION TYPE:C, RT WING INBD AFT FLAP LWR SKIN FOUND DENTS. SKIN METAL HOT BOND INTERIM REPAIRED IAW HX RS NR R57-51-36778, REV A AND EO B747-5750-39125-A. THIS IS A MAJOR REPAIR WITH ALUMINUM SHEET : 2024T3-0020IN. REPAIR PATCH SIZE: 51.5" X 19". FINAL CUSDR IPXA10B61423Fairing · puncturedINSPECTION TYPE:C, LT WING INBOARD FORE FLAP L/E FAIRING PUNCTURE. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR. 5A (1) FIG 5, REV 56.SDR IPXA10B61491Panel · delaminatedINSPECTION TYPE:C, LT WING OTBD MID FLAP T/E COVE PANEL UPPER SURFACE DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5A(1), FIG 5, REV 56.SDR IPXA10B61507Panel · delaminatedINSPECTION TYPE:C, LT WING OTBD MID FLAP T/E COVE PANEL UPPER SURFACE DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5A(1) FIG 5, REV 56.SDR IPXA10B61510Wedge · delaminatedINSPECTION TYPE:C LT WING INBD FORE FLAP T/E WEDGE LWR SURFACE INBD AREA DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-50-07 PAR 5A(1) FIG 5, REV 56.SDR IPXA10B61513Wedge · delaminatedINSPECTION TYPE:C RT WING INBD FORE T/E WEDGE LWR SURFACE DELAMINATION FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5A(1) FIG 5, REV 56.SDR IPXA10B61891Frame · crackedINSPECTION TYPE:C EMP- TAIL COMPT STA 2598 LT BHD INNER CHORD CRACK AT LWR TORSION BOX AREA AS MARKED. (CHORD CRACK LENGTH 0.915"), ( WEB CRACK LENGTH 0.030" ) CHORD & WEB REPAIRED IAW HX RS R53-80-36775, REV A AND EO 747- 5310-38966-A, ORG MAT'L:BAC1505-1008SDR IPXA10B61909Skin · crackedINSPECTION TYPE:C, EMP LT OTBD ELEVATOR LWR SURFACE L/E FIXED PANEL CRACK AT ELE STA 281.8, CRACK LENGTH 2.3". STA 273-290 AREA L/E FIXED PNL REPAIRED IAW HX RS R55-20-36774, REV A & EO B747-5520-38940-A, ORG. MAT'L 0.032IN 6061-T6 CRACK LENGTH 2.3", FINAL CUSDR IPXA10B61489Fairing · delaminatedINSPECTION TYPE:C, RT WING OTBD MID FLAP L/E FAIRING DELAMINATION. FIBERGLASS PERPREG LAYUP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A (1) FIG 5 REV 56.SDR IPXA10B61490Fairing · delaminatedINSPECTION TYPE:C, RT WING OTBD MID FLAP L/E FAIRING DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM51-70-07 PAR 5A(1) FIG(5), REV 56.SDR IPXA10B61503Wedge · delaminatedINSPECTION TYPE:C, RT WING OTBD FORE FLAP T/E WEDGE LWR SURFACE DELAMINATION. FIBERGLASS PREPREG LAY REPAIR CARRIED OUT IAW SRM 57-70-07 PAR 5A (1) FIG 5, REV 56.SDR IPXA10B61509Panel · delaminatedINSPECTION TYPE:C EMP RT INBD ELEVATOR LWR PANEL DELAMINATION FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5A(1) FIG 5, REV 56.SDR UIEA2010062600035Tire · failedDURING WALKAROUND INSP, MX FOUND THE LT MAIN BODY GEAR NR 8 WHEEL SEVERED; DUE TO TIRE DAMAGED/BURST.SDR IPXA0B60653Skin · dentedLT WING INBD AFT FLAP LWR SKIN DENT REPAIR WBL 208.2 REF EO B747-5750- 37247-A. REPAIRED IAW EO B747-5750-37247-B.SDR IPXA10B60462Skin · puncturedRT INBD AFT FLAP T/E .7500" PUNCTURE. REPAIRED IAW E0 B747-5750-38155-A.SDR IPXA10B60464Skin · damagedLT OTBD AFT FLAP DAMAGED BOTTOM SIDE. REPAIRED IAW EO B747-5750-38156-A.SDR IPXA10B60477Panel · puncturedINSPECTION TYPE:C, DMI D421159 - LT WING INBD MID FLAP T/E COVE PANEL LOWER SURFACE PUNCTURE. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5A FIG 5, REV 56.SDR IPXA10B60478Wedge · dentedINSPECTION TYPE:C, DMI D423196 - LT WING INBD FORE FLAP T/E WEDGE UPPER SURFACE CRACK /DENT. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5A FIG 5 REV 56.SDR IPXA10B60299Floor Panel · damagedMCD FLOOR PANEL STA 1620 DAMAGED. REPAIRED IAW OE B747-5320-35924-C.SDR UIEA2010060200023Skin · damagedDURING D-CHECK IN TPE, WRINKLES WERE FOUND IN THE 65B02697-122, BS 2360-2484, S-23L TO -46L SKIN (SEE FIG 1 AND 2) WHILE THE TAIL WAS UNSUPPORTED. (FASTENERS WERE REMOVED FROM THE WRINKLED AREA AND SHIMS WERE INSTALLED TO REMOVE THE WRINKLES.)
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