GE CFM56 series

Service difficulty reports · 5,028

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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.

SDR 2004UALA00765Trunnion · damagedLEFT MLG TRUNNION LINK WAS DAMAGED BY IMPROPER CORROSION REMOVAL. REPLACED LINK.Aug 8, 2004 · N395UA · Boeing 737322 · Main Landing Gear Attach SectionSDR 2004UALA00764Skin · dentedFUSELAGE SKIN HAS TWO DENTS AT STA 393 AND STR 16L. CUT-OUT DAMAGE AND INSTALLED DOUBLER AND TRIPLER.Aug 8, 2004 · N395UA · Boeing 737322 · Fuselage Main, Plate/SkinSDR 2004UALA00782Generator · malfunctionedAPU GEN ON LINE, FOUND VOLTAGE TO INDICATE 127VAC, WITH COCKPIT PANEL LIGHTS DIM, E&E LIGHTS VERY DIM AND FLUCTUATING, EXHAUST FAN NORMAL CB POPS. APU POWER IS NO GOOD. APU GEN C-B (C899) CONTACT B2 TERMINAL LUG & 3EA WIRES INSULATION BURNT 8 INCHES FROM B2 LAug 8, 2004 · N362UA · Boeing 737322 · AC Generation SystemSDR 2004UALA00768Link Assy · failedRIGHT MLG WAS DAMAGED BY IMPROPER CORROSION REMOVAL. MAJOR REPAIR ACCOMPLISHED. REPLACED LINK.Aug 8, 2004 · N395UA · Boeing 737322 · Main Landing Gear Attach SectionSDR 2004UALA00733Csd · failedRETURNED TO ORD DUE TO A NR 1 ENGINE GENERATOR DRIVE LIGHT. NR 1 CSD FAILED. OIL LOSS EVIDENT ON COWL, CSD EXTREMELY HOT ON ARRIVAL, SUSPECT INTERNAL FAILURE. REPLACED THE NR 1 CSD, EXCESSIVE METAL FOUND ON CHIP DETECTOR. SHOP FOUND EXTENSIVE INTERNAL CSD FAILAug 7, 2004 · N352UA · Boeing 737322 · AC Generation SystemSDR 2004UALA00746Light · inoperativeEMERGENCY EXIT LIGHT INOPERATIVE AT LEFT OVERWING EXIT. REPLACED LAMP.Aug 7, 2004 · N919UA · Boeing 737522 · Emergency LightingSDR 2004UALA00745Light · inoperativeFWD GALLEY EEL FLOOR LIGHT INOPERATIVE. REPLACED EEL GALLEY FLOOR STRIP.Aug 6, 2004 · N343UA · Boeing 737322 · Emergency LightingSDR IXXA0400101OSmoke Detector · brokenDURING ROUTINE TAKEOFF FROM MIAMI LOWER CARGO COMPT FIRE LIGHT ILLUMINATED. AFTER SHUTDOWN, MECHANIC DISPLAY SHOWED FALSE ALARM. FIRE DEPARTMENT VERIFIED NO HEAT IN (D) PIT. DOOR OPENED AND NOTHING FOUND. OVERWEIGHT INSPECTION REQUIRED. T/S SMOKE SYSTEM AND Aug 4, 2004 · N830BX · Doug DC871F · Smoke DetectionSDR CALA0400591Angle · corrodedINSPECTION FOUND L-2 DOOR ZEE ANGLE CORRODED IN SEVERAL AREAS FROM BS 910-1016. THE ZEE ANGLE WAS REPLACED IAW SRM 51-10-2.Aug 4, 2004 · N69603 · Boeing 737524 · Fuselage Miscellaneous StructureSDR AWXA200400850Wire · looseDURING 4-DAY CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 23 LT WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED A LOOSE WIRE AT SPLICE SEAT ROW 23 LT, OPERATIONAL CHECK WAS GOOD.Aug 4, 2004 · N174AW · Boeing 73733A · Light System WiringSDR 2004UALA00719Warning Light · illuminatedDIVERTED TO JFK DUE TO NOSE GEAR RED LIGHT INDICATION. PERFORMED GEAR SWING AND NOTED NOSE GEAR LOCK ACTUATOR WOULD NOT LOCK IN RETRACT POSITION WITH GEAR LEVER IN OFF POSITION. REPLACED NOSE GEAR LOCK ACTUATOR AND ACCOMPLISHED SEVERAL GEAR SWING AND MANUAL EAug 3, 2004 · N350UA · Boeing 737322 · Landing Gear Position and WarningSDR 2004UALA00716Seal · misinstalledABORTED TAKEOFF AT VERY LOW SPEED DUE TO A REPORT OF FLAMES COMING FROM THE TAILPIPE OF THE NR 2 ENGINE. FLT RETURNED TO THE GATE UNDER IT'S OWN POWER. TEARDOWN OF THE ENGINE REVEALED THAT AN HPC STAGE 6 HONEYCOMB HAD FAILED. THIS FAILURE MODE IS AN INDUSTRAug 2, 2004 · N393UA · Boeing 737322 · Engine (Turbine/Turboprop)SDR 2004UALA00717Warning Light · illuminatedABORTED TAKEOFF AT 110 KNOTS DUE TO A WING BODY OVERHEAT MESSAGE. LEFT WING BODY OVERHEAT LIGHT COME ON AT TAKE-OFF ROLL. MAINTENACE CHECKED LEFT PACK AREA FOR PNEUMATIC LEAK. NO LEAKS WERE FOUND. REPOSITIONED OVERHEAT SENSING ELEMENT GROMMETS. RAN LEFT PACKAug 2, 2004 · N329UA · Boeing 737322 · Overheat DetectionSDR 2004UALA00763Skin · dentedFUSELAGE SKIN IS DENTED AT STA 357, 3 INCHES BELOW STR 20R AND NEXT TO A BUTT JOINT. INSTALLED DOUBLER AND TRIPLER.Aug 2, 2004 · N395UA · Boeing 737322 · Fuselage Main, Plate/SkinSDR 2004UALA00715Cable · damagedLAST 18 FEET OF EEL LIGHTING INOP. REPLACED FEEDER CABLE.Aug 1, 2004 · N351UA · Boeing 737322 · Light System WiringSDR 2004UALA00762Clip · crackedSTA 500D STR 8R HAS CRACKED CLIP. REPLACED STRINGER CLIP.Aug 1, 2004 · N395UA · Boeing 737322 · Fuselage Miscellaneous StructureSDR 2004UALA00761Frame · crackedCABIN OVERWING FRAME BODY STA 616L CRACKED AT BOTTOM FASTENER BELOW FLOOR LEVEL. REMOVED CRACKED AREA, FABRICATED AND INSTALLED ANGLE.Jul 31, 2004 · N395UA · Boeing 737322 · Fuselage Main, FrameSDR 2004UALA00744Light · inoperativeAFT SECTION OF EEL LIGHT IS INOPERATIVE. REPLACE DEFECTIVE RIBBON.Jul 30, 2004 · N907UA · Boeing 737522 · Emergency LightingSDR 2004UALA00759Frame · crackedR1 DOOR CUT-OUT FWD FRAME CRACKED JUST ABOVE STR 17R AT STA 294. MAJOR REPAIR ACCOMPLISHED. REMOVED THE CRACKED FRAME AND FABRICATED A REPAIR.Jul 30, 2004 · N395UA · Boeing 737322 · Fuselage Main, FrameSDR 2004UALA00760Intercostal · crackedMID CABIN HAS A CRACKED INTERCOSTAL AT STA 540 RBL 2 AND LBL 2. REPAIRED THE FLOOR INTERCOSTALS.Jul 30, 2004 · N395UA · Boeing 737322 · Fuselage Miscellaneous StructureSDR IXXA060110SFrame · corrodedDURING ROUTINE C CHECK FOUND CORRODED FRAME AT STATION 220 LONGERON 36. REMOVED CORROSION,. ORIGINAL THICKNESS .100 REMOVED .040 MATERIAL, OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTAJul 30, 2004 · N605AL · Doug DC873F · Fuselage Main, FrameSDR CALA0400592Skin · crackedMAINTENANCE FOUND THE FUSELAGE SKIN DENTED AND CRACKED BETWEEN STA 500D + 10 AND 520, S12L. THE CRACK WAS 1.4 INCHES LONG. AN INTERIM REPAIR WAS INSTALLED IAW ECRA 5330-03361. A DIP WAS ISSUED TO PERFORM A PERMANENT REPAIR WITHIN 12 MONTHS.Jul 29, 2004 · N19357 · Boeing 7373T0 · Fuselage Main, Plate/SkinSDR F3LA200400075Computer · failedAIR TURN BACK. FLIGHT CREW REPORTED NUMEROUS SYSTEM FAILURES (GPS, GPWS, NR 1 RA, NR 1 ILS, NR 1 ENGINE REVERSER, NR 1 FADEC). CHECKED LAST LEG ECAM REPORT AND WAS UNABLE TO VERIFY FAULTS WITH CREW OR AIRCRAFT. CREW STATED ALL (FAULTED) SYSTEMS OPERATED NORJul 27, 2004 · N909FR · Airbus A319111 · Central WarningSDR U30A200400009Glowstrip · crackedAFTER FLT 609, RSW-ORD, DURING MAINTENANCE, THE EMERGENCY FLOOR PATHWAY LIGHTING PHOTO LUMINESCENT STRIP BETWEEN SEAT ROWS 2 DEF AND 5 DEF WAS IDENTIFIED AS DAMAGED. MAINTENANCE REPLACED THE PHOTO LUMINESCENT STRIP BETWEEN ROWS 2 DEF AND 5 DEF IAW AMM 33-51-21Jul 26, 2004 · N262AV · Airbus A320214 · Emergency EquipmentSDR 2004UALA00743Skin · damagedDAMAGED AREA EIGHT INCHES LONG ON FUSELAGE AFT OF REAR CARGO DOOR TEN INCHES FROM AFT DOOR FRAME. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER/TRIPLER REPAIR.Jul 26, 2004 · N926UA · Boeing 737522 · Fuselage Main, Plate/SkinSDR DHL2004804531Skin · wornLT WING IB FLAP UPPER SKIN WORN XW 91.000 (MAJOR REPAIR). CORR.: PERFORMED MAJOR REPAIR IAW ED EDW 27-4, DWG W27-R04 REV. IR. REMOVED FASTENERS IAW SRM 51-1-21 PG.1. TRIMMED OUT DAMAGED PLATING SEGMENT IAW ED EDW 27-4, DWG W27-R04. FABRICATED NEW PLATING SEGMEJul 25, 2004 · N804DH · Doug DC873F · Trailing Edge FlapsSDR 2004UALA00702Light · inoperativeFOUND EMERGENCY LIGHTS FROM ROW 10 UP TO LAST ROW, INOP. SPLICED HARNESS AT ROW 10 AND REPLACED WIRE FEED HARNESS FROM ROW 12 AFT.Jul 25, 2004 · N938UA · Boeing 737522 · Emergency LightingSDR F3LA200400072Adc · inoperativeABORTED TAKEOFF. FLIGHT CREW REPORTED THERE WAS NO AIRSPEED INDICATION ON CAPT'S SIDE. FIRST OFFICER'S AIRSPEED WAS 110 KIAS. BRAKE TEMP ACHIEVED 550 DEG. TROUBLESHOT LACK OF AIRSPEED INDICATION. PERFORMED EFCS GND SCAN IAW AMM 27-96-00-740-001 AND IRU-1 GJul 23, 2004 · N906FR · Airbus A319111 · Air Data ComputerSDR F3LA200400073Probe · inoperativeABORTED TAKEOFF. FLIGHT CREW REPORTED THERE WAS NO AIRSPEED INDICATION ON CAPT'S SIDE. FO'S AIRSPEED WAS 80 KTS. FOUND CAPTAIN'S PITOT PROBE 9DA1 BAD. REPLACED PITOT PROBE IAW AMM 34-11-15-400-001. PERFORMED OPS AND LEAK CHECK AND AIRSPEED INDICATION TESJul 23, 2004 · N906FR · Airbus A319111 · Pitot/Static SystemSDR TSAA0452055Relay · failedTHE LT OVER-WING EXIT LIGHT ILLUMINATED DURING TAKE-OFF AT 15 KTS. REJECTED TAKE-OFF AND RETURNED TO GATE. VERIFIED THAT THE LT OVER-WING EXIT DOOR WAS CLOSED AND LOCKED. CONFORMED WITH PSEU BITE CHECK, NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. ETOPSJul 22, 2004 · N739AL · Boeing 73773A · Passenger/Crew DoorsSDR UPS04842795Fitting · crackedINSPECTION TYPE: C1, HFEC INSPECTION DETECTED A CRACK IN FITTING AT STA 1150, FWD SIDE AT LONGERON 33 RT. REMOVED AND REPLACED FITTING AT STA 1150, LONGERON 33 RT IAW SRM 51-3-2, 51-1-8, 51-1-21, 51-1-20D.Jul 22, 2004 · N802UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS04842804Doubler · corrodedINSPECTION TYPE: C1, RT WING INTERIOR DOUBLER CORRODED AT STALL WARNING VANE, STA XFS371- 376. REMOVED CORRODED INTERNAL DOUBLERS SRM51-1-21. FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW DWG5769589, AND SRM 51-1-21, & 51-1-8.Jul 22, 2004 · N802UP · Doug DC873F · Wing, Plate/SkinSDR 2004UALA00696Stringer · damagedSTRINGER 21R DAMAGED BETWEEN STA 867 AND 887. MAJOR REPAIR ACCOMPLISHED. REPAIRED DAMAGED STRINGER 21R.Jul 21, 2004 · N926UA · Boeing 737522 · Fuselage Main, Longeron/StringerSDR IXXA0400098OSeal · damagedDURING TAKE OFF, ON GEAR RETRACTION, CREW HEARD NOISE AND VIBRATION IN THE NOSE GEAR AREA UNTIL GEAR WAS LOWERED. CREW CYCLED GEAR, RETURNED AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND LT NOSE LANDING GEAR DOOR SEAL PARTIALLY HANGING OUT. THE DAMAGED SEAL Jul 20, 2004 · N823BX · Doug DC871F · Nose/Tail Landing GearSDR AWXA200400797Connector · damagedDURING 4-DAY CHECK EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 11 THRU 17 LT WERE FOUND INOPERATIVE. MAINTENANCE REPAIRED DAMAGED PIN ON CONNECTOR FOR EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROW 12 LT; OPERATIONAL CHECK WAS GOOD.Jul 20, 2004 · N324AW · Boeing 737301 · Light System WiringSDR IXXA0400099OLink · brokenDURING TAKE OFF, ON GEAR RETRACTION, CREW HEARD NOISE AND VIBRATION IN NOSE GEAR AREA UNTIL GEAR WAS LOWERED. CREW CYCLED GEAR, RETURNED AND LANDED WITHOUT INCIDENT. AN INSPECTION IS ONGOING. AS SOON AS INFORMATION BECOMES AVAILABLE IT WILL BE PROVIDED. MAINTJul 20, 2004 · N823BX · Doug DC871F · Nose/Tail Landing GearSDR UPS04842801Intercostal · crackedINSPECTION TYPE: C1, INTERCOSTAL CRACKED IN MAIN CABIN SUBFLOOR, STA 1726, LBL 35. REMOVED, FABBED, AND REPLACED INTERCOSTAL IAW DWG 5755032, SRM 51-1-21, 51-1-8, 51-1-20D.Jul 20, 2004 · N802UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS04842805Longeron · crackedINSPECTION TYPE: C1, LONGERON 28L CRACKED AT FRAME INTERSECTION STA 1400, CUT OUT DAMAGED LONGERON SECTION FROM 1390 TO 1410. FABRICATED REPLACEMENT LONGERON. SECTION SRM53-2-2 FIG10 AND SRO853009 AND 53-4-1 FIG44. INSTALLED 2 SPLICE FITTINGS AND LONGERON SJul 20, 2004 · N802UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR F3LA200400071Computer · inoperativeON CLIMB OUT, FLIGHT CREW REPORTED ECAM: FLT CNT. FLT CTR 1 NR 2. RAN ECAM. RETURNED TO DEN WITHOUT INCIDENT AND LANDED OVERWEIGHT. TROUBLESHOT FLT CONT 1 AND 2 IAW TSM 27-93-00-810-949. REPLACED ELAC 1 IAW AMM 27-93-34-000-001. ELAC NR 1 OPS CHECKED NJul 19, 2004 · N804FR · Airbus A318111 · Flight Management Computing Hardware SystemSDR UPS04842794Web · corrodedINSPECTION TYPE: C1, CORROSION ON SUBFLOOR BETWEEN WEB AND CHANNEL, MAIN CABIN STA 857 AT FUEL DUMP TORQUE TUBE. REMOVED UPPER CHANNEL IAW SRM 51-1-21. CUT OUT DAMAGED AREA. FABBED AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM53-2-0 FIG23, DWG 5645332, 51Jul 19, 2004 · N802UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS04842796Finger Doubler · corrodedINSPECTION TYPE:C1 CORROSION ON/AROUND MAIN CABIN SUBFLOOR FINGER DOUBLER STA 880 TO 900 RBL60-64 FINGER DOUBLER CORRODED BEYOND LIMITS. UNDERLYING STRUCTURE OK. FABBED AND INSTALLED REPLACEMENT FINGER DOUBLER IAW DWG 5645332, SRM 53-2-0 FIG1F, 51-1-8, 51Jul 19, 2004 · N802UP · Doug DC873F · Fuselage Miscellaneous StructureSDR 2004UALA00675Skin · dentedRIGHT HORIZONTAL STABILIZER DENTED ON THE FIXED LEADING EDGE TWELVE INCHES FROM INBOARD EDGE. *S/D* DURING AIRCRAFT MAINTENANCE VISIT, AN INTERIM REPAIR WAS FOUND ON THE RIGHT HORIZONTAL STABILIZER LEADING EDGE AT STA 75. THE INTERIM REPAIR WAS CHANGED TO AJul 19, 2004 · N394UA · Boeing 737322 · Horizontal Stabilizer, Plate/SkinSDR 2004UALA00676Stringer Clip · crackedSTRINGER 23R CLIP AT STA 727C CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED CLIP.Jul 19, 2004 · N394UA · Boeing 737322 · Fuselage Main, Attach FittingsSDR AWXA200400828Skin · corrodedDURING 4-DAY CHECK CORROSION WAS FOUND ON SKIN AT AFT AIR PHONE ANTENNA UNDER AFT CARGO DOOR AT BS 794.6, BETWEEN STR 27 LT AND STR 27 RT. MAINTENANCE CUTOUT DAMAGED SKIN AT AFT AIR PHONE ANTENNA BS 794.6, BETWEEN STR 27 LT AND STR 27 RT AND PERFORMED A HFEC IJul 18, 2004 · N328AW · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR UPS04842798Fitting · crackedINSPECTION TYPE: C1, LONGERON 31 LT SPLICE FITTING CRACKED AT STA 450. REMOVED AND REPLACED SPLICE FITTING IAW SRM 51-1-11, 51-1-20D.Jul 18, 2004 · N802UP · Doug DC873F · Fuselage Miscellaneous StructureSDR 2004UALA00674Lamp · inoperativeAFT GALLEY EEL STRIP INOPERATIVE. REPLACED EEL STRIP.Jul 18, 2004 · N323UA · Boeing 737322 · Emergency LightingSDR 2004UALA00694Skin · damagedON SKIN DAMAGE AT STA 360, A DENT IN STRINGER 20R SKIN FLANGE. MAJOR REPAIR ACCOMPLISHED. SKIN REPAIRED. REPLACED STRINGER SPLICE FITTING.Jul 18, 2004 · N367UA · Boeing 737322 · Fuselage Main, Plate/SkinSDR UPS04842800Finger Doubler · corrodedINSPECTION TYPE: C1, FINGER DOUBLER CORRODED IN COCKPIT SUBFLOOR. STA.-75 AT LT CUSP REMOVED, FABRICATED, AND REPLACED CORRODED EDGE DOUBLER IAW SRM 53-3-3 FIG.6, 51-1-8, 51-1-21, AND DWG5612298.Jul 17, 2004 · N802UP · Doug DC873F · Fuselage Main, Plate/SkinSDR 2004UALA00704Bear Strap · damagedPREVIOUS BEAR STRAP REPAIR NEEDED TO BE REPLACED DUE TO SIDE SKIN REPLACEMENT FOR AFT CARGO. THE PREVIOUS REPAIR IS LOCATED ON THE AFT PIT DOOR CUT OUT ON THE AFT SIDE. INSTALLED QUADRUPLER.Jul 17, 2004 · N394UA · Boeing 737322 · Fuselage Main, Plate/SkinSDR UPS04842793Attach Angle · crackedINSPECTION TYPE: C1, VERTICAL FIN TO FUSELAGE ATTACH ANGLE HAS POPPED RIVET, LT SIDE, STA 1766. REMOVED PAINT IAW SRM 51-20-00. FOUND CRACK, NDT VERIFIED. FABBED REPAIR ANGLE IAW SRM 53-2-5 FIG16A. REMOVED AND REPLACED ANGLE IAW SRM 51-1-20D, 51-1-26, 51-1Jul 15, 2004 · N802UP · Doug DC873F · Vertical Stabilizer, Attach Fittings
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