GE CFM56 series
Service difficulty reports · 5,028
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 = 'CFM56' 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 = 'CFM56' 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 DALA1050163705Threshold · corrodedFWD CARGO FS 440-492, RBL23-29, DOOR THRESHOLD WEB CORRODED. REPLACED WEB IAW SRM 51-40-02.SDR F3LA2010111400550Battery Pack · dischargedBATTERY PACK 12W FAILED CAPACITY CHECK IAW TASK CARD A332204-02. REPLACED ESPU 12WL IAW AMM 33-51-38, PB 401.SDR F3LA2010111800552Link · buckledPILOT REPORT, LP 551794 ITEAM P-1, ECAM MESSAGE ON FLIGHT, FO PROPES FAULT, LP 551794 ITEAM P-2, ECAM MESSAGE IN FLIGHT REVERSER NR 1 FAULT. LP 551795 ITEM P-1, ECAM MESSAGE AFTER LANDING, LANDING GEAR SYS DISAGREE FAULT LP 551795 P-2, ECAM MESSAGE AFTER LANDISDR DALA1030883142Connector · looseDURING A NON-ROUTINE CHECK, THE EMERGENCY LIGHT SYS FAILED A EPSU LOAD TEST. MX FOUND A LOOSE CONNECTOR AT AFT LT SLIDE. RE-SEATED CONNECTOR AND FUNCTIONAL CHECK WAS NORMAL. ACFT RETURNED TO SERVICE.SDR DALA1031303715Shutoff Valve · malfunctionedTHE NR 2 ENGINE BLEED TRIPPED AT 39,000 FT. THE CABIN CLIMBED TO ABOVE 10,000 FT WITH AN INTERMITTENT CABIN ALTITUDE WARNING HORN SOUNDING. CREW EXECUTED AN EMERGENCY DESCENT, COMPLIED WITH QRH PROCEDURES, AND CONTINUED TO DESTINATION. MX REPLACED THE NR2 ENGSDR DALA1030843210Profile · crackedDURING L-CHECK FOUND CRACK IN AFT RT OVERWING EMERGENCY EXIT DOOR LT LOAD TRANSMITTING PROFILE. REPAIRED IAW SRM 51-44-11, SRM 51-42-1 & SRM 51-75-12.SDR DALA1030853210Profile · crackedDURING L-CHECK FOUND CRACK IN AFT RT OVERWING EMERGENCY EXIT DOOR RT LOAD TRANSMITTING PROFILE. REPAIRED IAW SRM 51-44-11, SRM 51-42-1 & SRM 51-75-12.SDR DHLA201000133Finger Doubler · corrodedMAIN CARGO COMPT- FINGER DOUBLER CORRODED, STA 879.000 RB 1. 65" REMOVED CORROSION IAW SRM 51-1-8, PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0, PG 2P. REMOVED FINGER DOUBLER IAW SRM 51-1-21, FABRICATED FINGER DOUBLER (AL7075T6 0.050") IAW SRM 53-7-3 FIG 4, SDR DHLA201000143Seat Track · wornCOCKPIT.- F/E'S FWD SEAT TRACK HOLES ELONGATED. CORRECTIVE ACTION: REMOVED F/E'S FWD SEAT TRACK IAW SRM 51-3-0. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW SEAT TRACK IAW SRM 51-3-0, SRM 51-3-1. OPS CHECKED GOOD IAW MMS 25-11-02 PG 501.SDR DHLA201000144Frame · wornNR 4 ENG LT T/R STRUCTURE FWD FRAME HAS EXISTING WEAR DAMAGE AT STA YN 202.000, BETWEEN 7 AND 8 O'CLOCK POS. PERFORMED MAJOR REPAIR IAW FORM 8110-3. REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT DAMAGED AREA + FABRICATED FRAME SEGMENT (AL6061T6 0.071") IAW DWG ESDR DHLA2010000149Frame · wornNR2 ENG LT T/R STRUCTURE FWD FRAME HAS EXISTING WEAR DAMAGE AT STA YN 202.000, BETWEEN 7 AND 8 O'CLOCK POS. C/A PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 11-29-10, EVA D878-00380, REV IR DATED 11-09-10. REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT DAMAGEDSDR DHLA201000132Blades · damagedREF LOG A022635, ITEM 2M: DURING POST MX RUN, WALK AROUND, FOUND HEAVY FOD DAMAGE TO NR4 ENGINE INLET FAN BLADES AND INLET COWLING. NR4 ENGINE WAS REPLACED AS A RESULT OF THE DAMAGE.SDR KNNA201000002Fire Loop · false activationON FINAL APPROACH, STARTED THE APU. THE APU FIRE WARNING LIGHT AND BELL ACTIVATED. PROCEEDED WITH THE APU FIRE IMMEDIATE ACTION ITEMS. THE FIRE WARNING LIGHT EXTINGUISHED. COMPLETED THE APU NON-NORMAL CHECKLIST AND NOTIFIED THE TOWER. REQUESTED A FIRE TRUCK SDR ASMF201010006Actuator · leakingCAPTAIN REPORTED THAT DURING CRUISE AND DESCENT, THE CONTROL COLUMN WITH AFT AND FWD MOVEMENT ABOUT 2 INCHES. ACFT WAS SENT TO THE HANGAR AND MX PERFORMED A CONTROL COLUMN POWER FORCE TEST AND ELEVATOR MECHANISM CONDITION INSP IAW 27-31-00; ELEVATOR PITOT SYS SDR DHLA201000105Pan · crackedINNER PAN AT AIR START DOOR ACCESS IS DAMAGED FS. -156.000. R & R DAMAGED INNER PAN AT AIR START ACCESS DOOR IAW SRM 51-1-21 AND DWG ED-4985 DTD 09/05/09 AND IAW ASTAR EVA D853-00376 DTD 09/21/2010.SDR DALA1024683735Skin · gougedGOUGE ON LOWER FUSELAGE SKIN APPROX STA.807 BETWEEN STR 25L AND 26L. DAMAGE REPAIRED IAW ERA-486014-14.SDR IXXA10SMN094SSkin · crackedDURING ROUTINE C-CHECK INSP, FOUND LT WING OUTER WING OTBD L/E LOWER SKIN CRACKED AT STA XFS 847.500. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. PERFORMED NDT INSP. NO CRACKS OR CORROSION NOTED. FABRICATED NEW SKIN, FILLERS AND DOUBSDR IXXA10SMN092SSkin · damagedDURING ROUTINE C-CHECK INSP, FOUND LT WING NR 2 STUB WING LOWER SKIN ELONGATED HOLES AT STA XFS 247.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED SPLICE DOUBLER AND NEW SKIN. PERFORMED NDT INSP. NO CRACKS OR CORROSION NOTSDR IXXA10SMN091SSkin · crackedDURING ROUTINE C-CHECK INSP FOUND LT WING NR 2 STUB WING LOWER SKIN CRACKED AT STA XFS 200.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED SPLICE DOUBLER AND NEW SKIN. PERFORMED NDT INSP. NO CRACKS OR CORROSION NOTED. SDR IXXA10SMN090SFitting · crackedDURING ROUTINE C-CHECK INSP, FOUND AFT CARGO COMPARTMENT SPLICE FITTING CRACKED AT STA 1390.000 LONGERON 30 LT. REMOVED CRACKED FITTING. FABRICATED NEW SPLICE FITTING. CLEANED, TREATED, PRIMED AREA AND SPLICE FITTING. INSTALLED NEW SPLICE FITTING IAW SRM 53-SDR ASMF201009007Warning Light · illuminatedACFT REJECTED TAKEOFF AT LESS THAN 80 KNOTS AND GROSS WEIGHT 61267 KG DUE AFT SERVICE DOOR LIGHT TURNED ON. DURING MX REVISION, THE PSEU AND AFT SERVICE DOOR WERE CHECKED IAW FIM PROCEDURE 52-10 TASK 801 AND MM 52-13-00, THE LIGHT TURNED OFF. THE HIGH ENERGYSDR DHLA201000130Skin · damagedEXISTING REPAIR LOCATED ON LOWER BELLY AT FS 1400.000 L36 IN POOR CONDITION. R & R. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 10-04-10, EVA D853-00378 REV IR DATED 09-22-10. REMOVED EXISTING REPAIR IAW SRM 51-1-21, SRM 51-1-20D. CUT OUT DAMAGED AREA ANDSDR IXXA10SMN077SSkin · wornDURING ROUTINE C-CHECK INSP, FOUND RT INBD FLAP SKIN WORN AT STA XW 104.000 - 115.0000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED, AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND RESDR IXXA10SMN076SSkin · corrodedDURING ROUTINE C-CHECK INSP, FOUND EXTERNAL FUSELAGE LOWER PART BUTT JOINT SKIN CORRODED AT STA 1690.000 BETWEEN LONGERON 34 RT- LONGERON 34 LT. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED NEW SKIN, DOUBLERS, FINGER DOUBLERS AND FISDR DALA1021733102Attach Fitting · corrodedDURING M-CHECK FOUND CORROSION ON FRAME CLIP IN FWD CARGO COMPARTMENT AT FR30 BETWEEN STRINGER 41R AND STRINGER 42R. REPAIRED IAW SRM 51-44-11, SRM 51-21-11 & SRM 51-42-11.SDR DHLA201000098Intercostal · crackedNOSE SECTION.- INTERCOSTAL CRACKED 1" APPROX, STA - 2.000 L-30 - 33RT. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-3-0 CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B PERFORMED STOP HOLE + FABRICATED DOUBLER ( AL 2024 B 0.050") IAW SRM 53-2-0 FIG 23 SHEET 1 TRSDR DHLA201000129Intercostal · crackedNOSE SECTION.- INTERCOSTAL CRACKED 1" APPROX, STA - 2.000 L-30 - 33RT. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-3-0 CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B PERFORMED STOP HOLE + FABRICATED DOUBLER (AL 2024 B 0.050") IAW SRM 53-2-0 FIG 23, SHEET 1 TR SDR DALA1021233102Floor Support · corrodedDURING M-CHECK FOUND CORROSION ON RT FLOOR SUPPORT AT Y254 FR20. REPAIRED IAW SRM 51-44-11, SRM 51-42-11.SDR DALA1021173101Support · corrodedDURING M-CHECK FOUND CORROSION ON RT SHEAR PLATE SUPPORT AT FR69-FR70. REPAIRED IAW SRM 51-42-11, SRM 51-44-11.SDR DALA1021183274Floor Panel · damagedDURING LINE CHECK FOUND FWD CARGO FLOOR PANEL 131AF WITH SEVERAL SCREWS PULLED THROUGH. REPLACED FLOOR PANEL IAW SRM 53-22-14 PAGE 401.SDR DALA1021193274Floor Panel · damagedDURING LINE CHECK FOUND FWD CARGO FLOOR PANEL 131EF WITH SEVERAL SCREWS PULLED THROUGH. REPLACED FLOOR PANEL IAW SRM 53-22-14, PAGE 401.SDR DALA1021163101Floor Panel · dentedDURING M-CHECK, FOUND DENTS ON FLOOR PANEL 151ZG. REPLACED FLOOR PANEL IAW DWG 3D25-40532.SDR DALA1021213102Support · corrodedDURING M-CHECK FOUND CORROSION ON R2 DOOR LOWER SILL SUPPORT AT Y1732 FR66. REPAIRED IAW SRM 51-42-11, SRM 51-44-11.SDR DALA1021503155Connector · unsecureDURING EMERGENCY LIGHT TEST FOUND ROW 11 ESCAPE PATH LIGHT INOP, SECURED WIRE CONNECTOR AND TESTED OK.SDR DALA1021693739Power Supply · inoperativeEMERGENCY EGRESS AISLE LIGHTS INOPERATIVE AT ROWS 11DEF THROUGH 16DEF. REPAIRED HARNESS CONNECTOR AT ROW 16, REPLACED POWER SUPPLY ADJACENT TO ROWS 10/11. CHECKS OK.SDR DALA1021223102Support · corrodedDURING M-CHECK FOUND CORROSION ON L2 DOOR LOWER SILL SUPPORT AT Y1732 FR 66. REPAIRED IAW SRM 51-42-11, SRM 51-44-11.SDR DALA1021093101Floor Panel · dentedAFT CARGO COMPARTMENT FLOOR PANEL NR 161NF HAS SEVERAL DENTS. RII: N FABRICATED NEW PANEL ON STAM TRAVELER T10/848970 IAW DWG 3D25-40532.SDR DALA1021103101Floor Panel · dentedFWD CARGO FLOOR PANEL NR 131AF HAVE MULTIPLE DENTS. FABRICATED NEW PANEL ON STAM TRAVELER T10/848915 IAW DWG 3D25-40532.SDR DALA1021123101Floorboard · debondedAFT CARGO COMPARTMENT FLOORBOARD NR151PE HAS DEBONDED DAMAGE ALONG AFT EDGE. FABRICATED NEW PANEL ON STAM TRAVELER NR T10/848917 IAW DWG 3D25-40532.SDR DALA1021133101Floor Panel · dentedAFT CARGO COMPARTMENT FLOOR PANEL NR 161PF HAS SEVERAL DENTS. FABRICATED NEW PANEL ON STAM TRAVELER NR T10/848931 IAW DWG 3D25-40532.SDR DALA1021143102Seat Track · corrodedFWD CABIN RT SEAT TRACK -Y765 CORRODED FR20-21. REMOVED CORROSION IAW SRM 51-74-00, ORIGINAL THICKNESS .087 MAT LOSS .070, L=1.5" W=1" D=.065" IS OUT OF LIMITS IAW TRM 53-00-15. R & R SEAT TRACK IAW SRM 51-42-11.SDR DHLA201000096Skin · deformedLT OTBD AIL LWR PLATING DEFORMED STA XA 741.000 PERFORMED MAJOR REPAIR IAW SRM 57-8-1 FIG 4. REMOVED DEFORMED NOSE PLATING IAW SRM 57-1-0 PG 1, SRM 51-1-21, SRM 51-3-0. FABRICATED NEW NOSE PLATING (AL2024T3 0.032") IAW SRM 57-8-1 FIG. 4 ITEM "H". CLEANED, TRESDR DHLA201000126Skin · deformedLEFT OTBD AILERON LOWER PLATING DEFORMED STA XA 741.000. PERFORMED MAJOR REPAIR IAW SRM 57-8-1 FIG 4. REMOVED DEFORMED NOSE PLATING IAW SRM 57-1-0 PG 1, SRM 51-1-21, SRM 51-3-0. FABRICATED NEW NOSE PLATING IAW SRM 57-8-1 FIG. 4 ITEM "H". CLEANED, TREATED AND PSDR DHLA201000127Cargo Track · wornUPPER CARGO COMPT.- NR4 TRACK LUG WORN (STA 57.000 - 110.000). PERFORMED MAJOR REPAIR IAW SRM 53-2-3 FIG 12, SHEET 1, PG 49-50. REMOVED WORN TRACK SEGMENT AND EXISTING SPLICES IAW SRM 53-1-0 PG 1, SRM 51-3-0. FABRICATED NEW TRACK SEGMENT EXTRUSION PN S2772660 SDR DHLA201000128Cargo Track · wornUPPER CARGO COMPT.-NR3 TRACK LUGS WORN (STA 1670.000 - 1702.000). PERFORMED MAJOR REPAIR IAW SRM 53-2-3, FIG 12, SHEET 1, PG 49-50. REMOVED WORN TRACK SEGMENT AND EXISTING SPLICES IAW SRM 53-1-0 PG 1, SRM 51-3-0. FABRICATED NEW TRACK SEGMENT EXTRUSION PN S277SDR DHLA201000131Skin · corrodedFUS LWR SKIN CORRODED, STA 160.000 L-35R - L-36 PERFORMED MAJOR REPAIR IAW SRM 53-2-1 FIG 7, SHEET 25,23,24 TR 53-203, DATED JAN 21-2008. REMOVED CORROSION IAW SRM 51-1-8, PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0, PG 2P. REMOVED EXISTING REPAIR NEAR CORROSDR F3LA2010090100491Transmitter · erraticPILOT REPORT ERMENGENCY DECLARED. AIR TURN BACK, NR 1 ENGINE LOW OIL QUANTITY. PLACED NR 1 ENGINE OIL QUANTITY ON MEL 79-31-01A. R & R NR 1 ENGINE OIL QUANTITY TRANSMITTER. REF 79-31-15 PG BLOCK 401. OPS AND LEAK CHECK NORMAL.SDR DHLA2010000100Skin · misrepairedREMOVED EXISTING NON STANDARD REPAIR IAW SRM 51-1-21. FABRICATED REPAIR DOUBLER IAW SRM 53-2-0 FIG. 1D SHEET 3, SRM 53-3-3 FIG. 1 ITEM "A" SRM 51-9-0 FIG 68A. CLEANED, TREATED AND PRIMED AREA & REPAIR PARTS IAW SRM 51-1-8B. INSTALLED REPAIR DOUBLER IAW SRM 53-SDR DHLA201000101Skin · dentedRT INBD FLAP UPPER PLATING DENTED STA XW 68 PERFORMED MAJOR REPAIR IAW SRM 57-7-1 FIG 1. REMOVED DENTED PANEL PLATING IAW SRM 57-1-0 PG 1, SRM 51-1-21. FABRICATED PLATING & BONDED DOUBLER IAW SRM 57-7-1 FIG 1, ITEM "A" & "L". BONDED BOTH PARTS WITH HYSOL IAW SDR 2010F00223Skin · damagedINSPECT EXISTING REPAIR ON FUS STA -156 FOR CONFORMITY WITH SRM, CONDITION AND SECURITY. IF REPAIR COMPLIES, NOTE DETAILS ON NON ROUTINE. IF REPAIR DOES NOT CONFORM, R & R UTILIZING APPROVED DATA. REF REPAIR REPORT (F011). STRIPPED REPAIR AREA IAW MM 51-20-0
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