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 DHLA201000125Skin · 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 (AL2024T3 0.025") & BONDED DOUBLER (AL2024T3 0.020") IAW SRM 57-7-1 FIG 1 ITEM "A" & "L"SDR MYWA100094RWarning Light · illuminatedETOPS SIGNIFICANT SYS: INFLIGHT APU FAULT LIGHT ON WITH APU AUTO SHUTDOWN.SDR DALA1019923210Skin · damagedDURING FWD A&G ANTENNA INSTALLATION SKIN BETWEEN FR25 & FR26 AND BETWEEN STRINGER 43L & STRINGER 42L HAD (2) .7500 HOLES AND (6) NR10 HOLES DRILLED IN WRONG LOCATION DUE TO INCORRECT MANUFACTURED DOUBLER. REPAIRED IAW SRM 53-21-11, FIG 214, SHEET 1.SDR DALA1019523270Support · gougedDURING M-CHECK, WHILE PERFORMING LT INBD FLAP AND TRUNNION INSP, FOUND GOUGE DAMAGE ON LT INBD FLAP TRUNNION SUPPORT ASSY. REPLACED TRUNNION SUPPORT ASSY IAW SRM 57-51-21 & ERA 484244-14.SDR MYWA100094Apu · shutdownETOPS SIGNIFICANT SYS: IN FLIGHT, APU FAULT LIGHT AND AUTO SHUTDOWN.SDR DALA1019443727Skin · damagedTHE ACFT SKIN WAS DAMAGED BY TIRE DEBRIS AFTER THE NOSE WHEEL TIRE CAP SEPARATED DURING TAKEOFF.SDR DALA1019483758Battery Pack · inoperativeEMERGENCY EGRESS LIGHTS ARE INOPERATIVE IN THE AFT LT GALLEY. REPLACED BATTERY PACK, CHECKS GOOD.SDR DALA1018313124Floor Panel · damagedDURING L-CHECK, FOUND DAMAGE TO FWD CARGO COMPARTMENT PANEL 131CG. REPLACED FLOOR PANEL IAW SRM 53-02-00, FIG 209.SDR DALA1018583714Battery Pack · inoperativeDURING OPS CHECK OF EMERGENCY LIGHTS, FOUND RT AFT EMERGENCY OVERWING EXIT DOOR LIGHT INOPERATIVE. REPLACED BOTH CHARGER BATTERY PACKS FOR EQUIPMENT M1671.SDR DALA1018593714Battery Pack · inoperativeDURING OPS CHECK OF EMERGENCY LIGHTS, FOUND SEAT MOUNTED LIGHTS INOPERATIVE FROM ROW 23 UP TO RT GALLEY AREA. REPLACED THE BATTERY PACK.SDR IPXA10562045Seat Track · corrodedINSPECTION TYPE:C3, SEAT TRACK INBD AND OTBD FLANGE IS CORRODED BS1319 LBL45, WL208. REMOVED, FABRICATED REPLACEMENT, INSTALLED REPLACEMENT SEAT TRACK SRM 51-40-02-0G.SDR IPXA10562306Seat Track · corrodedINSPECTION TYPE:C3, UPPER LOBE, CORROSION ON SEAT TRACK RT FLANGE, BS 618 AND 608, LBL 44, WL 208. REPAIRED IAW ATS ER 10-3980, DATED 8-31-10.SDR IPXA10562291Frame · damagedINSPECTION TYPE:C3, MCB FRAME INBD FLANGE HAS A MECHANICAL DAMAGE AT BS 900 BETWEEN S-15R AND S-16R. REPAIR IAW ATS ER 10-4009.SDR IPXA10562043Skin Panel · damagedINSPECTION TYPE:C3, EXTERNAL FUSELAGE SKIN SURFACE HAS MECHANICAL DAMAGE AT BS 1534-1564 STR - 22R. REPAIRED IAW ATS ER10-3824 DATED 8/19/10 AND EO B757-5330-39251-A, DATED 8-20-10.SDR IPXA10562256Skin · chafedINSPECTION TYPE:C3, FUSE EXTERNAL SKIN IS CHAFED AT BS 1862.7 - 1871.7 BELOW RT HORIZONTAL STAB. REPAIR IAW ER 10-3787.SDR IPXA10562293Frame · damagedINSPECTION TYPE:C3, ACCOMPLISH EO B757-5310-25199B. REPLACED INNER CHORD OF FUSELAGE FRAME REPAIR AT BS 940, S-14L TO S-16L. REPAIRED IAW EO B757-5310-25199B.SDR DHLA201000075Doubler · crackedNOSE SECTION ACCESS DOOR 2 INTERNAL DOUBLER CRACKED STA-156.0000. PERFORMED MAJOR REPAIR IAW EVA D853-00350, REV IR DATED 07-15-10. REMOVED EXISTING REPAIR IAW SRM 51-1-20D, SRM 51-1-21. VISUALLY INSPECTED REWORKED AREA. NO CRACK, NO CORROSION FOUND. FABRICATSDR DHLA201000076Skin · wornRIGHT INBD AILERON UPPER PLATING WORN STA XA 474.000 PERFORMED MAJOR REPAIR IAW SRM 57-8-1 FIG 1. REMOVED WORN PLATING IAW SRM 57-1-0, SRM 51-1-21. FABRICATED NEW PLATING (AL2024T3 0.040") IAW SRM 57-8-1 FIG. 1 ITEM "E". CLEANED, TREATED AND PRIMED AREA + NEWSDR DHLA201000080Longeron Fitting · crackedLONGERON END FITTING BATHTUB FITTING CRACK 3.5" STA 902.125, L-4L PERFORMED MAJOR REPAIR IAW SRM 53-1-0, PG 1. REMOVED CRACKED BATHTUB FITTING IAW SRM 53-1-0 PG 1, SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW BATHTUB FITTING ISDR DHLA201000073Rib · crackedRIGHT INBD FLAP T/E RIB CRACKED 1", STA XW -5.000 REMOVED FASTENERS IAW SRM 51-1-21. PERFORMED STOPHOLE AND FABRICATED REPAIR ANGLE (AL2024T3 0.071") IAW SRM 57-2-0 PG 9-10, SRM 57-5-2 FIG. 5 SHEET 1, SRM 51-9-0 FIG 68A. CLEANED, TREATED AND PRIMED AREA + REPASDR DHLA201000078Cargo Track · wornUPPER CARGO COMPT.- NR 6 TRACK LUGS WORN (STA 560.000 - 610.000) PERFORMED MAJOR REPAIR IAW SRM 53-2-3 FIG 14, SHEET 1, PG 49-50. REMOVED EXISTING SPLICES AND CUT OUT TRACK DAMAGED SEGMENT IAW SRM 53-2-3 FIG. 14 SHEET 1, SRM 53-1-0 PG 1, SRM 51-3-0. FABRICATEDSDR CA100714001Skin · debonded(CAN) TOP AND BOTTOM SKINS DISBONDED. 21 INCH BY 6.5 INCH. 21 INCHES INBOARD OF OUTBOARD EDGE DUE TO WATER INGRESS THROUGH THE BOND LINE BETWEEN THE TRAILING EDGE SKINS AND THE SPAR. UNIT REPAIRED WITH STANDARD HOT BOND TECHNIQUES PER MANUFACTURER RECOMMENDASDR DHLA201000081Skin · damagedRT OTBD FLAP UPPER SKIN HOLE ELONGATED AND WORN STA XF 203.000 - 213.000 PERFORMED MAJOR REPAIR IAW SRM 57-7-1 FIG 4, TR 57-94 DATED 10-01-02. REMOVED DAMAGED PLATING IAW SRM 57-1-0 PG 1, SRM 51-1-21. FABRICATED NEW PLATING IAW SRM 57-7-1 FIG 4, TR 57-94 ITEM SDR DHLA201000085Skin · crackedRT WING TOP AFT PANEL PLATING CRACKED 4" STA XCW 69.500 PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 20, SHEET 1. REMOVED FASTENERS IAW SRM 51-3-0, SRM 51-1-20D. CUT OUT DAMAGED AREA + FABRICATED (-5) DOUBLER (7075"0" 0.160") + (-7) TRIPLER (7075"0" 0.125") + FISDR USAA20100629SB107Indicator · faultyMIA - CLIMBING THROUGH 11,000 FEET OUT OF MIA, CREW REPORTED THE NR 2 ENGINE EGT WENT TO 1250 DEGREES. CREW ACCOMPLISHED QRH PROCEDURES AND RETARDED NR 2 THROTTLE TO IDLE. EGT REMAINED AT 1250 DEGREES. JUST AS CREW WAS ABOUT TO SHUT DOWN THE NR 2 ENGINE, THSDR IPXA0560647Floor Panel · damagedFLOOR PANEL NR STA 8 AFT HAS DAMAGE CORNER MFG NEW FLOOR PANEL IAW EO B757-5320-9692.SDR DALA1012273252Power Supply · inoperativeDURING A NON ROUTINE CHECK, THE EMERGENCY POWER SUPPLY UNIT FAILED TEST. REPLACED EPSU AND CHECK WAS NORMAL. ACFT RETURNED TO SERVICE.SDR DALA1011153266Floor Panel · damagedDURING M-CHECK FOUND DAMAGE TO FLOOR PANEL 261PF. REPAIRED IAW SRM 53-02-00 FIG 209.SDR DL738101256Power Supply · inoperativeEMERGENCY EGRESS LIGHTING INOP AT LT & RT FWD OVERWING EXIT SIGNS. REPLACED POWER SUPPLY M1894, OPS CHECKS NORMAL.SDR DL738101249Battery Pack · inoperativeEMERGENCY EGRESS LIGHTING, OVERWING EXIT SIGNS INOP. REPLACED BATTERY PACK AND CHARGER M1694, CHECKS OK.SDR F3LA2010033000378Proximity Sensor · inoperativeREF LOG PAGE NRS 537910 AND 537923. CAPTAIN NOTED RT OVERWING EXIT SLIDE NOT SHOWING ARMED. MX ISSUED MEL 25-60-04C, CONTROL NR 1074315, TO THE RT OVERWING SLIDE, REF LOG PAGE NR 537910. MX R & R PROXIMITY DETECTOR IAW AMM 52-73-11-400-004A. OPS CHECK GOOD,SDR USAA20100329SB040Engine · leakingYYZ - CREW REPORTED NO ODORS DURING TAXI-OUT. ON TAKEOFF THRUST OUT OF CLT, AN ODOR LIKE DIRTY SOCKS WAS NOTED. AFTER THRUST REDUCTION, NO ODORS WERE PRESENT IN COCKPIT. IN CRUISE AFTER TWENTY MINUTES, FLIGHT ATTENDANT REPORTED A FOUL SMELL IN AFT CABIN (ROSDR DHLA201000037Structure · damagedNR 2 ENG T/R TRANSLATING COWL HOLES ELONGATED STA 240.000 BETWEEN 6 AND 7 O'CLOCK POS. PERFORMED MAJOR REPAIR IAW FORM 8110-3 DATED 04-20-10, EVA D878-00324 REV IR DATED 04-02-10. REMOVED FASTENERS IAW SRM 51-1-21A. CUT OUT DAMAGED AREA AND FABRICATED (2EA) FSDR SWAA101192Compressor Blade · damagedAIR TURNBACK / DECLARED EMERGENCY / ENGINE SHUTDOWN. LOUD "POPPING" NOISES FROM NR 1 ENGINE DURING ROTATION. ENGINE INDICATIONS NORMAL. PUSHED THRUST LEVERS UP & NOISES CEASED FOR 6-7 SECONDS. THEN RESUMED. INDICATIONS STILL NORMAL. DECLARED EMERGENCY, TSDR CA091202016Scuff Plate · damaged(CAN) AFTER DEPARTURE FROM YEG, CREW REPORTED DIFFICULTY PRESSURIZING THE AIRCRAFT AND THE LT SLIDING WINDOW APPEAR TO BE NOT CLOSED PROPERLY. AIRCRAFT RETURNED TURNED BACK FROM FLIGHT AND LANDED SAFELY IN YEG. ON INVESTIGATION, FOUND THE SCUFF PLATE ON LT CDSDR CA091202002Bolt · dirty(CAN) F/CREW NOTED A LOSS OF YELLOW HYD FLUID DURING FLIGHT MCO TO YYZ. MAINTENANCE IN YYZ NOTED EVIDENCE OF HEAVY BUILD-UP ON THE RUDDER. FURTHER INVESTIGATION FOUND TWO OF THREE ATTACH BOLTS FOR ONE OF THE ACTUATOR RODS SHEARED. BOLTS SHANKS REMAINED BUT SDR F3LA2009110200222Floor Support · corrodedREFERENCE NON ROUTINE C073186. DURING DEN C3 C-CHECK, INSP NOTED CORROSION ON THE FLOOR SUPPORT NUT CLIP HOLES LOCATED AT STATION Y1292 BETWEEN FRAMES 66 AND 68. MX REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-44-11, 51-42-11 AND 51-72-11.SDR F3LA2009103000220Anti-Ice Valve · faultyPILOT MADE AN AIR TURN BACK TO DEN DUE TO A WARNING ON THE ELECTRONIC CENTRALIZED ACFT MONITORING SYS FOR 'WING ANTI-ICE LT AND RT VALVE OPEN'. MX REMOVED AND REPLACED THE LT WING ANTI-ICE VALVE AND PERFORMED AN OPS TEST IAW AMM 30-11-51-000-001, 30-11-51-400SDR IXXA090057OFuel Filter · cloggedDURING CLIMB OUT NR 1 ENGINE FLAMED OUT. THE CREW ACCOMPLISHED FLAME OUT IN FLIGHT START CHECKLIST. THE NR 1 ENGINE STARTED ALL PARAMETER NORMAL. CREW LANDED WITHOUT FURTHER INCIDENT. MX PERFORMED TROUBLESHOOTING FAULT 51 AND REPLACED ENGINE FUEL FILTER. OPSDR F3LA2009101600202Support · crackedREFERENCE NON-ROUTINE C071806. DURING DEN C3 C-CHECK, INSP NOTED THE NR 2 ENG OTBD PYLON RIB SUPPORT WAS CRACKED ABOUT RIB 7. MX REMOVED AND REPLACED SUPPORT IAW SRM 51-42-11, SRM 51-44-11, SRM 51-26-00, SRM 54-52-12 AND SRM 51-42-00.SDR IXXA090046OFire Loop · defectiveDURING CLIMB OUT, NR 4 FIRE WARNING HORN SOUNDED, THEN SILENCED AND SOUNDED AGAIN. THE CREW DISCHARGED BOTH BOTTLES AND SHUTDOWN NR 4 ENGINE. CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX REPLACED CORE FIRE LOOP, CORE LOOP CONNECTORS AND BOTH FIRESDR IXXA090042OFuel Control · out of rigDURING TAKEOFF, NR 4 ENG WOULD NOT MAKE PWR. ONCE AIRBORNE HAD TO PUSH THROTTLE PAST OTHER THROTTLES NR 4 EGT WENT TO 907 DEGREE. THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX INSPECTED NR 4 ENG AND FOUND VSV'S AND VBV OUT OF RIG. MX ACCOMPLISSDR BJ6A2009082612701Window · failedNR3 RT WINDOW SHATTERED IN FLIGHT. FOUND THAT THE FRACTURE OF WINDOW INITIATED IN THE STRUCTURAL GLASS PANE AT THE EDGE OF THE SOLDER TAB. THERE WAS NO EVIDENCE OF ARCING OR ELECTRICAL DAMAGE. THE MOST LIKELY CAUSE IS THAT A TINY PIECE OF THE BUSS BAR WAS PSDR DU4R2009392Stringer Clip · crackedDURING SCHEDULED INSPECTION, FOUND CRACKED STRINGER CLIP ATTACHED TO FRAME AT BS 867 AND STR 1, AFT CABIN CEILING.SDR F3LA2009082500139Shear Plate · corrodedDURING C3 C-CHECK, INSP NOTED THE LT SHEAR PLATE BETWEEN FRAME 69 AND FRAME 70 HAS CORROSION AROUND NUTPLATES. MX REMOVED AND REPLACED THE LT SHEAR PLATE IAW SRM 52-41-11, 52-42-21 AND EA A0-53T-31040.SDR F3LA2009082500140Floor Support · corrodedDURING C3 C-CHECK, INSP NOTED THE LONGITUDINAL FLOORBEAM Y1292 AND FRAME 68 HAS CORROSION AROUND FLOOR PANEL NUTPLATES. MX REMOVED AND REPLACED FLOORBEAM IAW SRM 53-41-14, 51-42-11 AND DRAWING D53472780.SDR DU4R2009393Skin · gougedDURING SCHEDULED INSP, FOUND DEEP GOUGE ON FUSELAGE SKIN AT BS 867, STR 1.SDR F3LA2009082500142Sill · corrodedDURING C3 C-CHECK, INSP NOTED THE L2 DOOR SILL PLATE HAS CORROSION AT FRAME 68. MX REMOVED CORROSION DAMAGE, FABRICATED REPAIR DOUBLER AND INSTALLED IAW EA A9-53R-31275.SDR F3LA2009082500143Floor Support · corrodedDURING C3 C-CHECK, INSP NOTED THE L2 DOOR LONGITUDINAL FLOORBEAM Y1292 AT FRAME 66 HAS CORROSION AROUND FLOOR PANEL NUTPLATES. MX REMOVED CORROSION AND PERFORMED REPAIR IAW EA A9-53R-31266.SDR F3LA2009082500144Floor Support · corrodedDURING C3 C-CHECK, INSP NOTED THE R2 DOOR LONGITUDINAL FLOORBEAM -Y1292 AFT OF FRAME 66 HAS CORROSION AROUND NUTPLATES. MAINT REMOVED CORROSION AND PERFORMED REPAIR IAW EA A9-53R-31267.
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