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 2006UALA00759Frame · gougedFWD ENTRY DOOR SN 392 METAL GOUGED ON UPPER FWD FRAME OF THE DOOR BY LATCH BEARING HOUSING.SDR 2006UALA00760Skin · tool damageAFTER REMOVAL OF BOTTOM AIRFONE ANTENNA FOUND DRILL START NEXT TO MOUNT HOLE. REMOVED DAMAGE FABRICATED FILLER AND DOUBLER AND INSTALLED PER EA I060196 AND EA I06089 AND UAL EVA UA-EVA-60250SDR 2006UALA00761Frame · crackedFOUND FRAME BS 727 HAS A CRACK LOCATED JUST BELOW STRINGER 14L. REMOVED DAMAGE, FABRICATED FILLER AND SPLICE ANGLE AND INSTALLED PER AAR EA I060181 AND UAL EVA UA-EVA-60252.SDR 2006UALA00765Stiffener · crackedRT NR 6 FLAP TRACK FAIRING AFT INBD STIFFENER CRACKED IN UPPER RADIUS THRU FASTENER HOLE AND CRACKED IN HALF, THRU CENTER OF PART. REMOVED AND REPLACED THE STIFFENER REF SRM 51-40-02SDR 2006UALA00766Attach Bracket · crackedFOUND STA 440 BETWEEN STRINGERS 7 AND 8 CRACK AT PSU ATTACH BRACKET. REMOVED DAMAGE REF MM 53-10-84 NDT VERIFIED CRACK TERMINATION B737 NDT PT 6. INSTALLED NEW ANGLES PER SRM 53-10-84 REPAIR III.SDR 2006UALA00767Frame · crackedFWD GALLEY DOOR AFT FRAME IS CRACKED AT LWR STOP FITTING ATTACH FASTENER HOLE.SDR 2006UALA00768Frame · crackedFOUND FWD GALLEY DOOR FWD FRAME IS CRACKED AT LOWER STOP FITTING ATTACH FASTENER HOLE.SDR 2006UALA00769Shear Tie · damagedFOUND SHEAR TIE DAMAGED AT STA 727B AFT SIDE OF FRAME BETWEEN STR 21 AND STR 22 LT SIDE. REPLACED SHEAR TIE STA 727B STR 21 - 22 LT REF SRM 51-40-02 AND BOAC DRAWING 65-46569 PAGE 2.SDR 2006UALA00776Warning Light · malfunctionedFOUND RED LIGHT ON NOSE GEAR AND INT GREEN LIGHT FLASHING.SDR AMTA200600281Hmu · fluctuatesAFTER 10 MINUTES OF NORMAL GROUND OPS NR 1 ENG WOULD NOT ACCELERATE WITH THROTTLE MOVEMENT AND FLAME OUT. REMOVED AND REPLACED HMU IAW AMM. LEAK CHECK NORMAL. OPS CHECK NORMAL.SDR AMTA200600277Hmu · unserviceableENGINE NR 2 FLAMEOUT ON TAXI, ENGINE RE-START NOT OK. REMOVED AND REPLACED HMU IAW MM AND PERFORMED TEST 2, 3A, 12 AND 13 OF MM. OPS CHECK GOOD. (K)SDR AMTA200600276Module · malfunctionedLT SIDE WINDOW HEAT (OFF) LIGHT WILL NOT EXTINGUISH. REMOVED AND REPLACED D WINDOW/ PITOT HEAT MODULE IAW. AMM 30-41-41-4, INSTALLATION TEST GOOD. (K)SDR 2006UALA00654Bulkhead · damagedFOUND LT AC BAY OB SIDE OF DOOR CUTOUT 22" FROM AFT END. BULKHEAD WEB DAMAGED FROM CONTACT WITH DOOR LATCH. DAMAGE AREA TRIMMED OUT REF MM51-20-01 & EA I060153.SDR 2006UALA00656Skin · crackedFOUND HORIZONTAL STAB LOWER SURFACE AFT SPAR SKIN CRACKED AT THIRD BAY FROM I-B END. REMOVED DAMAGE AND ACP NDT FOR CRACKS. FABRICATED AND INSTALLED REPAIR DOUBLER WITH TWO EACH CUT-OUT ACCESS HOLES REF SRM 55-10-01.SDR 2006UALA00657Frame · crackedROUND OVERWING FRAME STA 616 RT SIDE IS CRACKED. INSTALLED STIFFENING ANGLE PER MM53-11-89.SDR 2006UALA00655Skin · crackedFOUND STA 296.5 STR 10L UPPER FLANGE CUTOUTS CRACKED. REMOVED CRACK, INSTALLED STRAP INSTALLED STRINGER CLIP PER AAR EA I060145 AND UAL UA-EVA-60211.SDR SB06033Cable · faultyDURING CRUISE AT FL340, CREW REPORTED ENGINES WERE FLUCTUATING 0.4% N1 FUEL FLOW FROM 2,600 TO 2,630 LBS. ALL GAUGES FLUCTUATING. ENGINES WOULD NOT STAY IN SYNC. PMC ON OR OFF MADE NO DIFFERENCE. AUTOTHROTTLES OFF FLUCTUATED AT 0.6%. DURING A TURN, FLUCTUSDR 2006UALA00613Frame · crackedFOUND FUSELAGE FRAME AT STA 440 CRACKED BETWEEN STR 8R AND 9R CRACK RADIATING FROM INBD RIVET OF FRAME. DAMAGE & CHECK FOR CRACK CONTAINMENT WITH NDT. FABRICATED & INSTALLED NESTED ANGLE DOUBLER REPAIR REF MM53-10-84. RPR 3.SDR 2006UALA00620Frame · crackedFOUND CABIN BODY FRAME WEB IS CRACKED AT STRINGER CUT OUT BS 727 STR 14R. TRIMED OUT DAMAGE FABRICATED DOUBLER AND FILLER AND INSTALLED THE REPAIR PER AAR EAI060128 AND UNITED EVA-60171.SDR 2006UALA00622Bushing · damagedFOUND VERTICAL STAB LT PRIMARY FWD LUG BUSHING SPUN WHILE MACHINING. DAMAGE REMOVED AND A NEW REPAIR BUSHING WAS INSTALLED PER AAR EA I060151. RESULTING BORE SIZE WAS 1.6048 IN.SDR 2006UALA00933Connector · burnedLEFT AFT BOOST PUMP CONNECTOR BURNED TO PUMP ASSEMBLY. THE LEAKAGE OBSERVED WAS VERIFIED AND CAUSED BY A LOCALIZED OVERHEATING OF THE CONNECTOR PINS THAT RESULTED IN DAMAGE TO THE SEAL AROUND PIN 2. THE CAUSE FOR THE EXCESSIVE OVERHEATING IN THE CONNECTOR SDR 2006UALA00610Frame · crackedBS 727 BULKHEAD FRAME WAS FOUND CRACKED AT THE STR 15L CUT-OUT EMANATING UPWARD FROM THE STRINGER CUT-OUT. REMOVED DAMAGE & VERIFIED CRACK CONTAINMENT WITH NDT. FABRICATED & INSTALLED NESTED ANGLE REPAIR & STRUCTURAL FILLERS REF. AAR ENGINEERING AUTHORIZATIONSDR 2006UALA00611Frame · crackedFRAME STA 927 IS CRACKED BETWEEN STR 8L AND 9L AT THE INBD RIVET OF THE PSU RAIL SUPPORT BRACKET. REMOVED DAMAGE & CHECK FOR CRACK CONTAINMENT USING NDT. FABRICATED & INSTALLED NESTED ANGLE DOUBLER REPAIRS REF SRM 53-00-07-201.SDR 2006UALA00612Frame · crackedFOUND FUSELAGE FRAME AT STA 440 CRACKED BETWEEN STR 8L AND 9L PSU RAIL ATTACH BRACKET. REMOVED DAMAGE & CHECK FOR CRACK CONTAINMENT USING NDT. FABRICATED & INSTALLED NESTED ANGLE DOUBLER REPAIR REF MM53-10-84 RPR NR 3.SDR 2006UALA00605Web · crackedFOUND CABIN STR 7L WEB CRACKED STA 294.5 IN RADIUS, AFT SIDE OF FRAME. MAJOR REPAIR ACP'D, INSTALLED REPLACEMENT INTERCOSTAL PER AAR EA-I060121 & UA EVA-60168.SDR 2006UALA00607Intercostal · crackedFOUND FWD CABIN BS 303 INTERCOSTAL ANGLE IS CRACKED AT STR 11R. MAJOR REPAIR ACP'D, INST'D TEE CHORD REPAIR PER BACO DRAWING 65-17684 & AAR EA-I060138 ON NR11079-2000-0047.SDR 2006UALA00594Power Supply · inoperativeFOUND EEL LIGHTS FROM ROW 3-9 INOP.SDR 2006UALA00595Power Supply · inoperativeEMERGENCY EXIT SIGNS ABOVE LT OVERWING HATCH AND LOWER FWD CORNER OF LT OVERWING HATCH INOP.SDR 2006UALA00596Wire · damagedEEL LIGHTS INOP FROM ROW 15 AFT TO AND INCLUDING EEL STRIP IN FRONT OF AFT GALLEY CART STOWAGE COMPARTMENT.SDR 2006UALA00584Door Frame · crackedFWD CARGO DOOR CUTOUT SURROUND AFT FRAME STA 452.4 HAS CRACK IN WEB AT UPPER IB CORNER OF LOWER STOP STR 24R. REMOVED AND REPLACED FRAME REF SRM 51-40-02 AND BACO DWG 65-20723.SDR F3LA200600011Engine · bird ingestionBIRD STRIKE TO NR 2 ENGINE ON APPROACH TO MKE. DUE TO N1/N2 ROLLBACK, DAMAGE WAS SUSPECTED AND AGENT NR 1 FIRE BOTTLE WAS DISCHARGED. AN EMERGENCY WAS DECLARED AND AIRCRAFT LANDED WITHOUT INCIDENT. A BORESCOPE OF THE NR 2 ENGINE WAS PERFORMED AND MAJOR DAMASDR CA060324002Wire Harness · damagedA/C HAS NR 2 AFT FUEL PUMP LOW PRESSURE LIGHT ILLUMINATE ON TAXI. A/C RETURNED TO GATE AND IT WAS DISCOVERED THAT ASSOCIATED CIRCUIT BREAKER WAS TRIPPED. FURTHER INVESTIGATION REVEALED WIRE W1134-3601-18 HAD SHORTED TO GROUND. MOC CONSULTED WITH BOEING ENGISDR SWAA060817Engine · failedAIR TURNBACK / IN FLT SHUTDOWN / DECLARED EMERGENCY. NR 1 ENG FAILURE AT 10,500 FT DURING CLIMB, EGT IND 830 DEGS AND RISING. REMOVED AND REPLACED NR 1 ENG PER MT.SDR AMTA200600150Unknown · unknownLT ENGINE CONTROL LIGHT ILLUMINATED DURING TAXI. IAW FIM FAULT 75-10581 DISPLAYED IAW 71-00-00-700-807-FOO PERFORMED ACTUATOR TEST. TEST PASSED. NO FURTHER FAULTS RECORDED. (K)SDR 2006UALA00367Pin · damagedFOUND RT MLG TRUNNION LINK PIN HAS PLATING MISSING IN SHANK AREA. PIN REPLACED ON JC I3576 WO NR 11070-7500-0009. BY AAR-IND MECH 11708 AND INSP 050 ON AAR WO NR 11071-7500-0007.SDR 2006UALA00368Clip · crackedFOUND CRACKED SHEAR CLIP IN LOWER RADIUS JUST ABOVE DOOR L2 UPPER SILL, STA 967. FABRICATED CLIP PER 53-00- 07 AND INSTALLED PER SRM 51-40-02SDR 2006UALA00362Attach Angle · crackedFOUND RT CABIN STA 294, SILL CHORD ANGLE HAS CRACKED ATTACH ANGLE. REMOVED SILL ANGLE. DRILLED NEW ONE AND INSTALLED REF 51-40-02 SRM.SDR 2006UALA00363Intercostal · crackedFOUND LT CABIN STA 312 INTERCOSTAL AT STR 4 IS CRACKED. REMOVED INTERCOSTAL REF SRM 51-40-02. PICKED UP FASTENER HOLES REF SRM 51-40-02, INSTALL REF SRM 51-40-02.SDR 2006UALA00365Intercostal · crackedSTATION 305 STR 8R INTERCOSTAL WEB TO FUSELAGE SKIN ANGLE IS CRACKED IN THE RADIUS. REPLACED ANGLE PER SRM 51-40-02.SDR 2006UALA00366Stringer Clip · crackedFOUND AFT PIT STA 727A RBL 24" STRINGER CLIP CRACKED AT STR 25R. INSTALLED NEW STRINGER CLIP REF SRM 51-40-02.SDR 2006UALA00352Floorbeam · corrodedAFT CABIN FLOORBEAM CORRODED AROUND NUT CLIP HOLES BS 986.5 RBL 23-45 WL 208. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, INSTALLED REPAIR REF MM 53-10-95.SDR 2006UALA00358Attach Angle · crackedFOUND FWD CABIN BS 305 STR 10R WEB TO SKIN ATTACH ANGLE CRACKED IN RADIUS. MANUFACTURED AND INSTALLED NEW ANGLE PER SRM 51-40-02.SDR 2006UALA00359Splice · crackedFOUND STRINGER SPLICE CRACKED AT STA 907 L4 AT 2 FASTENERS. REPLACED SPLICE PER SRM 51-40-02.SDR 2006UALA00360Intercostal · crackedFOUND INTERCOSTAL WEB STR 16 BETWEEN STA 294.5 & 303.9 IS CRACKED. FABRICATED NEW WEB PER SRM 51-30-01, INSTALLED WEB PER SRM51-40-02.SDR 2006UALA00361Door · dentedFOUND E/E DOOR DENT, OUT OF LIMITS. INSTALLED DOUBLER REPAIR PER SRM 52-00-01. NO FURTHER FINDINGS, O.K. FOR SERVICE.SDR 2006UALA00364Frame · dentedAFT CARGO COMPARTMENT STA 727B AT S22L FRAME DENTED. REPAIRED FRAME AT STA 727B AT STRINGER 22L WITH REF TO MM CHAPTER 53-11-99. REPLACED STRINGER CLIP ON FRAME 727B AND STRINGER 22L DUE TO REPAIR WITH REF TO SRM 51-40-02.SDR 2006UALA00351Shear Tie · crackedFOUND STA 360 STR 14R SHEAR TIE IS CRACKED. REPLACED SHEAR TIE PER SRM 53-00-07.SDR 2006UALA00339Frame · gougedFOUND FUSELAGE BODY FRAME WEB IS GOUGED NEAR BLEED AIR CUTOUT BS 1040, STR 26L - 27L. CUT OUT DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED REPAIR REF MM 53-11-86. REPAIR SCHEME DOUBLER AND TRIPLER.SDR 2006UALA00340Skin · damagedLT FUSELAGE SKIN AT 1" FWD OF FRAME STA 727A STR 25L HAS TOOLING DAMAGE. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED REF SRM 53-60-01 REPAIR 31 PG 338. ADD REPAIR DOUBLER AND STRUCTURAL FILLER.SDR 2006UALA00341Floorbeam · corrodedCABIN FLOORBEAM UPPER FLG IS CORRODED BS 947 LBL 4-20, WL 208. REPAIRED WITH ANGLE (REF MM 53-10-95-801) REPAIR #VII. TREATED, PRIMED AND PAINTED. INSTALLED NESTED ANGLE.
Back to GE CFM56 series