IAE V2527-A5

Service difficulty reports · 8,007

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 = 'V2527A5'
  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 CALA2016101795814Power Supply · inoperativeMID L EMERGENCY LIGHT INOP. REPLACED POWER SUPPLY AND BATTERY, OPS CHECK NORMAL.Oct 15, 2016 · N436UA · Airbus A320232 · Emergency LightingSDR CALA2016101795815Power Supply · inoperativePROXIMITY EMERGENCY AISLE LIGHTS AT ROWS 10 AND 11 INOP. REPLACED MID LEFT POWER SUPPLY AND BATTERY.Oct 15, 2016 · N497UA · Airbus A320232 · Emergency LightingSDR CALA2016101995822Skin · damagedLT FUSE AT FR 35 STR 30 HOLE MARKED AS 2 IS CRACKED IN SIDESHELL AND FRAME FLANGE. INTERIM RPR ACP IAW ECRA 5330-05797 PART1ACP PERM RPR OF THE FASTENER HOLES AT FR 35 STR 30L, 30R ON OR BEFORE MARCH 26 2017.Oct 15, 2016 · N406UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2016101995823Skin · damagedLT FUSE AT FR35 STR 30 HOLE MARKED AS 1 IS CRACKED IN SKIN AND SIDESHELL. INTERIM RP ACP IAW ECRA 5330- 05797 PART1 ACP PERM RPR OF THE FASTENER HOLES AT FR35 STR 30L, 30R ON OR BEFORE MARCH 26 2017.Oct 15, 2016 · N406UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2016101995824Skin · damagedLT FUSE AT FR35 STR30 HOLE MARKED AS 4 IS OUT OF ROUND. INTERIM RPR ACP IAW ECRA5330-05797 PART1 ACP PERM RPR OF THE FASTENER HOLES AT FR35 STR 30L, 30R ON OR BEFORE MARCH 26 2017.Oct 15, 2016 · N406UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2016101995825Skin · damagedLT FUSE AT FR35 STR30 HOLE MARKED 3 IS OUT OF ROUND. INTERIM RPR ACP IAW ECRA5330-05797 PART1 ACP PERM RPR OF THE FASTENER HOLES AT FR35 STR 30L, 30R ON OR BEFORE MARCH 26 2017.Oct 15, 2016 · N406UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2016101995826Skin · damagedRT FUSE AT FR35 STR 30 HOLE MARKED 3 IS OUT OF ROUND. INTERIM RPR ACP IAW ECRA5330-05797 PART1 ACP PERM RPR OF THE FASTENER HOLES AT FR35 STR 30L 30R ON OR BEFORE MARCH 26 2017.Oct 15, 2016 · N406UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2016101995827Skin · dentedAFT CARGO DOOR SKIN DENT FR54A+5. INSTALLED DOUBLER IAW SRM 52-32-00 FIG 205.Oct 15, 2016 · N406UA · Airbus A320232 · Cargo/Baggage DoorsSDR CALA2016101995828Skin · dentedAFT CARGO DOOR SKIN DENT FR55. INSTALLED DOUBLER IAW SRM 52-32-00 FIG 205.Oct 15, 2016 · N406UA · Airbus A320232 · Cargo/Baggage DoorsSDR CALA2016101995830Tail Cone · crackedWHILE WORKING FCD 7811-01330 FOUND NR 1 ENG TAIL CONE WITH WELDS AND CRACKS AT 11:00 AND 5:00 POSITION. REPLACED TAIL CONE PER MM 78-30-00.Oct 15, 2016 · N414UA · Airbus A320232 · Engine Thrust ReverserSDR CALA2016101995819Cleat · corrodedFWD CARGO CLEAT AT FR27 AND STR 43R HAS CORROSION. REMOVED AND REPLACED CLEAT AT FR27 AT STR 43R IAW SRM 51-72-11.Oct 14, 2016 · N402UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2016101995820Skin · corrodedFUSELAGE EXT SKIN AT WASTE VENT HAS MINOR CORROSION FR 69-FR 70, STR 28R. DAMAGED FOUND TO BE OUT OF LIMITS IAW SRM 53-41-11 TABLE 108. INSTALLED REPAIR DOUBLER AT FR69-FR70 STR 28R EXT SKIN AT WASTE VENT, IAW SRM 53-41-11 PARA 5 D.Oct 14, 2016 · N406UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2016101995821Tail Cone · crackedWHILE ACCOMPLISHING FCD 7811-01330, FOUND TWO .5 CRACKS IN THE NR 2 ENGINE TAIL CONE. REPLACED TAIL CONE PER MM 78-11-12-000-010-A 13.Oct 14, 2016 · N414UA · Airbus A320232 · Engine Thrust ReverserSDR CALA2016101795811Door Sill · corrodedAFT CARGO PIT INNER DOOR SILL WEB HAS AREAS OF CORROSION FR52-FR56. REMOVED AND REPLACED AFT CARGO DOOR SILL WEB FR52-FR56 IAW SRM 51-72-11.Oct 13, 2016 · N404UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2016101795806Angle · corrodedCORROSION ON LEFT AFT EMERGENCY EXIT LOWER FRAME NEXT TO DRAIN HOLE. REMOVED AND REPLACED T-ANGLE FWD AND LEFT LOWER CORNER CURVED WEBS IAW SRM 51-42-11.Oct 12, 2016 · N406UA · Airbus A320232 · Emergency ExitsSDR CALA2016101395797Skin · dentedFUSELAGE EXTERNAL DENT FR3, 11" ABOVE LOWER LAP SEAM. ACCOMPLISHED REPAIR IAW SRM 53-00-11, PAR 4 W FIG 240.Oct 10, 2016 · N406UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2016101395803Stringer · corrodedAFT PIT STRINGER 42L BETWEEN FR 58-59 HAS CORROSION. REMOVED & REPLACED STRINGER AND FACTORY SPLICE PLATES IAW SRM 51-42-11.Oct 10, 2016 · N404UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2016101395804Stringer · corrodedFWD PIT FR 28-FR 33 STRINGER 40 RT HAS CORROSION. REMOVED & REPLACED STRINGER AND SPLICE PLATES IAW SRM 51-42-11.Oct 10, 2016 · N404UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2016101395801Connector · unsecureFOUND SEAT 7 & 8 EEL LIGHTS INOP DURING 2 SVC CHECK. SECURED CONNECTOR AT SIDE WALL, OPS CK OK.Oct 9, 2016 · N487UA · Airbus A320232 · Light System WiringSDR CALA2016101395802Cleat · corrodedFWD CARGO FR 31 STR 43L-43R CLEAT HAS CORROSION. REMOVED AND REPLACED FWD CARGO FR31 STR 43L-43R CLEAT SRM 51-42-11.Oct 9, 2016 · N406UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2016101395798Skin · dentedFUSE EXTERIOR HAS DENT AT LT SIDE FR 30-31 STR 38. FOUND DENT TO BE OUT OF LIMITS, CUTOUT OUT DAMAGE AREA AND FAB REPAIR DOUBLER FORM 2024-T3-.063 SKIN THICKNESS IN THIS AREA IS .047 AND INSTALLED REPAIR IAW SRM 53-00-11 FIG220. THIS IS A CAT B REPAIR.Oct 8, 2016 · N404UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2016093095786Cleat · corrodedFWD CARGO FR33 STR 42-43R CLEAT HAS CORRSION. REMOVED AND REPLACED FWD CARGO FR33 STR 42-43R CLEAT IAW SRM51-42-11.Sep 30, 2016 · N406UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2016093095789Cleat · corrodedFWD CARGO PIT FR33 STR40R-41R CORROSION ON CLEAT. R&R CLEAT IAW SRM 51-42-11.Sep 30, 2016 · N406UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2016093095790Cleat · corrodedFWD CARGO PIT FR33 STR43R-43L CLEAT IS CORRODED. R&R CLEAT IAW SRM 51-42-11.Sep 30, 2016 · N406UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2016093095791Cleat · corrodedFWD CARGO PIT FR32 STR 40R-41R CLEAT HAS CORROSION. R&R CLEAT IAW SRM 51-42-11.Sep 30, 2016 · N406UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2016092995783Stringer · corrodedCORROSION ON STRINGER 23L. AFT ENTRY DOOR SILL FRAME 67. REMOVED AND REPLACED DOOR SILL IAW A320 51-22-11Sep 27, 2016 · N404UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2016092995784Uplock · out of positionVERY LOUD WIND RUSH, WITH COCKPIT FLOOR VIBRATION, DOES NOT CHANGE WITH SPEED DEREASED. WITH ALT INCREASE. WIND NOISE AND VIBRATION AT ROW 1, ALL NORMAL AFT OF ROW2. ALL GEAR DOORS SHOWED CLOSED AFTER TAKE OFF. NLD INDICATION IS NOW XX. ALSO, AFTER LANDINGSep 27, 2016 · N409UA · Airbus A320232 · Landing Gear Door Retract SectionSDR CALA2016092795763Shear Tie · corrodedFWD CARGO BAY FRAME 28 STRINGERS 41-40L SHEAR TIE HAS CORROSION. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 53-42-11.Sep 26, 2016 · N406UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2016092795779Shear Tie · corrodedFWD CARGO FR28, STR 43R - 44R CLEAT HAS CORROSION. REMOVED & REPLACED IAW A320 SRM 51-42-11.Sep 26, 2016 · N406UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2016092795780Shear Tie · corrodedFWD CARGO FR30 CLEATS HAVE CORROSION AT STR'S 42L - 43L AND 44 - 43R. REPLACED 2 EA CLEATS IAW A320 SRM 51-42-1 1.Sep 26, 2016 · N406UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR GTIA2016092601606Engine · failedNR 2 ENGINE EGT OVERLIMIT DURING FLIGHT, FOLLOWD BY A NR 2 ENGINE STALL ECAM. F/A REPORTED FLAMES ON RIGHT SIDE OF AIRCRAFT. AN EMERGENCY WAS DELARED.Sep 26, 2016 · N602NK · Airbus A320232 · Engine (Turbine/Turboprop)SDR CALA2016092995785Hydraulic System · lowGREEN SYSTEM HYDRAULIC LOSS. EMERGENCY DECLARED, DIVERTED. SERVICED GREEN HYDRAULIC SYSTEM IAW AMM 12-12-29-611-001-A. NO LEAKS NOTED, AIRCRAFT RETURNED TO SERVICESep 25, 2016 · N415UA · Airbus A320232 · Hydraulic System, MainSDR CALA2016092795764Shear Tie · corrodedFWD CARGO BAY FRAME 28 STRINGERS 42-43L SHEAR TIE HAS CORROSION. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 53-42-11.Sep 24, 2016 · N406UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2016092795765Shear Tie · corrodedFWD CARGO BAY FRAME 28 STRINGERS 41-42L SHEAR TIE HAS CORROSION. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 53-42-11.Sep 24, 2016 · N406UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2016092795766Shear Tie · corrodedFWD CARGO BAY FRAME 28 STRINGERS 41-42R SHEAR TIE HAS CORROSION. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 53-42-11.Sep 24, 2016 · N406UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2016092795767Shear Tie · corrodedFWD CARGO BAY FRAME 28 STRINGERS 42-43R SHEAR TIE HAS CORROSION, REMOVED AND REPLACED THE SHEAR TIE IAW SRM 53-42-11.Sep 24, 2016 · N406UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2016092795768Shear Tie · corrodedFWD CARGO BAY FRAME 33 STRINGERS 42-43L SHEAR TIE HAS CORROSION. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 53-42-11.Sep 24, 2016 · N406UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2016092795769Shear Tie · corrodedFWD CARGO BAY FRAME 33 STRINGERS 40-41L HAS CORROSION. REMOVED AND REPLACED THE SHEART TIE IAW SRM 53-42-11.Sep 24, 2016 · N406UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2016092795770Shear Tie · corrodedFWD CARGO BAY FRAME 34 STRINGERS 42-43L SHEAR TIE HAS CORROSION. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 53-42-11.Sep 24, 2016 · N406UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2016092795771Shear Tie · corrodedFWD CARGO BAY FRAME 27 STRINGERS 42-41 SHEAR TIE HAS CORROSION. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 53-42-11.Sep 24, 2016 · N406UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2016092795772Probe · malfunctionedNR 2 ENGINE OVERSPEED FAULT DURING ROLLOUT. REPLACED N1 SENSOR PROBE.Sep 24, 2016 · N465UA · Airbus A320232 · Power Indicating SystemSDR CALA2016092795781Shear Tie · corrodedFWD CARGO FRAME 27 STRINGERS 43L - 42L AND 43L - 43R CLEATS HAVE CORROSION. REPLACED THE CLEATS IAW SRM 51-42-1 1.Sep 24, 2016 · N406UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2016092795782Shear Tie · corrodedFWD CARGO BAY, FRAME 30 STRINGERS 40, 41, 42, 43R CLEATS HAVE CORROSION. REPLACED THE CLEATS IAW SRM 51-42-1 1.Sep 24, 2016 · N406UA · Airbus A320232 · Fuselage Structure (General)SDR CALA2016092795773Skin · contaminatedLEFT ELEVATOR UPPER SKIN PANEL HAS A TRAPPED WATER INDICATION, 47.5" FROM INBOARD, 5" FROM TE, 3 X 2.5 DIA . REPAIRED IAW SRM 55-21-11 PAR. 5.E.Sep 22, 2016 · N406UA · Airbus A320232 · Horizontal Stabilizer, Plate/SkinSDR CALA2016092795774Skin · contaminatedRIGHT ELEVATOR UPPER SKIN PANEL HAS TRAPPED WATER INDICATIONS 186" FROM INBOARD, 9" FROM TE, 4 X 5.5 DIA A ND 150" FROM INBOARD, 14" FROM TE, 4.5 X 6.0 DIA. REPAIRED IAW SRM 55-21-11 PAR. 5.N.Sep 22, 2016 · N406UA · Airbus A320232 · Horizontal Stabilizer StructureSDR CALA2016092795775Skin · dentedEXTERIOR FUSELAGE SKIN HAS DENT FRAME 7 8.5 INCH ABOVE LOWER LAP SEAM. FOUND TO BE OUT OF LIMITS. CUT OUT THE DAMAGED AREA & FABRICATED A REPAIR DOUBLER AND INSTALLED IAW SRM53-00-11 FIG 239.Sep 22, 2016 · N406UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2016091995746Battery Pack · inoperativeEMERGENCY LIGHT TEST FAULTED. REPLACED EPSU BATTERY, OPS TESTED GOOD.Sep 16, 2016 · N491UA · Airbus A320232 · Emergency LightingSDR CALA2016092095756Strut · dischargedAIR RETURN DUE TO LANDING GEAR FAILING TO RETRACT. EMERGENCY DECLARED. SERVICED STRUT, SECURED LOOSE NLG PROXIMITY TARGET, REPLACED MLG SENSOR. SYSTEM GOOD, OK TO CONTINUESep 16, 2016 · N465UA · Airbus A320232 · Nose/Tail Landing GearSDR CALA2016091995741Support Fitting · corrodedAFT CARGO FRAME 51, STRINGER 37R SUPPORT FITTING COMMON TO PROFILE PANEL WAS FOUND CORRODED. FITTING WAS REPLACED IAW SRM51-42-11.Sep 11, 2016 · N401UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2016091995743Frame · damagedFRAME 51 INNER FLANGE DAMAGED BETWEEN STRINGERS 37 - 38R. REPAIRED IAW SRM53-00-12 TBL 201, PARA 4.A. FIG 201.Sep 11, 2016 · N401UA · Airbus A320232 · Fuselage Main, Frame
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