IAE V2527-A5
Service difficulty reports · 8,009
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.
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
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 CALA2014101692432Door Sill · corrodedMAJOR REPAIR & SDR L2 DOOR SILL HAS CORROSION AROUND TWO EACH NUTPLATES AT FRAME 66 & STRINGER 23L. CUT OUT THE DAMAGED AREA IAW SRM 53-41-14 PG 205. FABRICATED ONE EACH REPAIR ANGLE IAW SRM 53-41-14 PGS 215 - 216 PRINCIPLE 1 & INSTALLED. RESTORED THE AREA.SDR CALA2014100792376Stringer · corrodedAFT PIT STRINGER 41R BETWEEN FRAME 59 - 64 HAS CORROSION. REPLACED FACTORY STRINGER SECTION IAW SRM 51-42-11.SDR CALA2014100792377Stringer · corrodedAFT CARGO COMPARTMENT STRINGER 42R HAS CORROSION FRAME 63 - 64. REPAIRED STRINGER 42R IN AFT PIT FROM FRAME 62.5 - 64 IAW SRM 53-00-13 PARA 4 A FIG 201.SDR CALA2014100792368Bleed Valve · malfunctionedNUMBER 2 ENG SN V12 083 HAD TWO EACH COMPRESSOR STALLS AFTER TAKEOFF. FOLLOWED FM PROCEDURE, THROTTLE BACK TO IDLE, CURRENTLY ENG PARAMETERS NORMAL. RETURNING BACK TO FIELD. CFDS SHOWS ENG 2 STALL 2 TIMES IN CRUISE, WITH VSV BLD VLV LP C2 ALONG WITH ENG 2 FSDR CALA2014100792366Doubler · damagedLEFT WING TE & RIB 8 SKIN DOUBLER PLATE HAS ELONGATED HOLES. R & R LT WING TE & RIB 8 LOWER SKIN DOUBLER PLATE IAW SRM 57-21-11 FIG 205. CAT A REPAIR IAW SRM 57-21-11 TBL 202.SDR CALA2014092992325Stringer · corrodedMAJOR REPAIR & SDR STRINGER 42R IS CORRODED BETWEEN FRAME 33 & 34 AROUND FASTENER IN FWD PIT. AFTER BLENDING CORROSION FOUND THE REPAIRED AREA TO BE OUT OF LIMITS IAW SRM 53-21-13 FIG 101. R & R STRINGER 42R FROM FRAME 31 TO 34 IAW SRM 51-42-11. NO REQUIREMSDR CALA2014092992323Stringer · corrodedCORROSION IN FWD CARGO ON AFT BILGE AREA STRINGER 43R BETWEEN FRAME 33 & 34 AROUND FASTENER. REMOVED CORROSION & FOUND TO BE OUT OF LIMITS IAW SRM 53-21-13 FIG 101. R & R IAW SRM 51-42-11 PGS 7 -10, 23, 24 & 30 - 32.SDR CALA2014092992349Longeron · corrodedMAJOR REPAIR & SDR LONGERON SUPPORT IS CORRODED AT FRAME 70 ON RT SIDE OF AFT CABIN. AFTER BLENDING CORROSION LONGERON WAS FOUND TO BE OUT OF LIMITS IAW SRM 51-73-11. R & R IAW SRM 51-72-11.SDR CALA2014092292255Switch · faultyALL EMER LIGHTS IN THE CABIN CAME ON FOR ABOUT 10 SECONDS IN FLIGHT. REPLACED SWITCH 4WL IAW TSM 33-51-00-810-881-A. OPERATIONS CHECKED OK IAW AMM 33-51-00710-004-A.SDR CALA2014092292272Epsu · failed2 SERVICE EMER LIGHT TEST FAILED. REPLACED 12WL EPSU & BATTERY IAW MM 33-51-38.SDR CALA2014092292274Battery · faultedOVERHEAD EMER LIGHTS INOPERATIVE. OVERWING EMER EXIT LIGHTS CAME ON SOMETIME AFTER TAKEOFF RECYCLED SWITCH. ACCOMPLISHED TEST OF THE EMER LIGHTS IAW MM 33-51-00 HAD 2 FAULTS EPSU BATTERY RT & EPSU BATTERY AFT LT. REPLACED BATTERY IN POWER SUPPLY UNITS RT & SDR CALA2014091892243Door Sill · corrodedCORROSION PRESENT ON R2 DOOR AFT GIRT BAR PLATE DOOR SILL. REMOVED CORROSION & FOUND OUT OF LIMITS IAW SRM 53-41-14 FIG 101. R & R R2 DOOR SILL IAW SRM 51-42-11 PARA 5, 6 & 7. NO REQUIREMENT FOR SRI INSPECTIONS.SDR CALA2014091892244Stringer · corrodedSTRINGER 43L HAS CORROSION BETWEEN FRAME 53 & 59. FOUND NO ALLOWABLE DAMAGE LIMITS IAW SRM 53-41-13 PAGE 101. REMOVED STRINGER 43L BETWEEN FRAME 54 - 60 & ONE EACH FACTORY SPLICE & REPLACED WITH NEW STRINGER & SPLICE IAW SRM 51-42-11 PGS 7 - 24. NO SRI INSPSDR CALA2014111092671Spar · mechanic errorNUMBER 2 PYLON LOWER SPAR WEB MIS-DRILLED DURING ACCOMPLISHMENT OF SRM 54-51-12. INTERIM REPAIR ACCOMPLISHED IAW ECRA 5450-02258. REPAIR HAS BEEN APPROVED AS INTERIM FOR 1 MONTH IAW RDAS 80003171-003-2014 DATED 9-10-14. A NEW RDAS THAT PROVIDES THE INSPECTSDR CALA2014091892237Slide · defectiveDURING EMER LIGHT TEST, GOT EPSU EXT LOAD FWD LT MSG. REPLACED DOOR SLIDES L1 & R1 IAW AMM 25-62-44-400. EMER LIGHT TEST PASSED.SDR CALA2014091892238Slide · deployedDOOR 1R SLIDE DEPLOYED. REPLACED 1R DOOR SLIDE IAW AMM 25-62-44-000-002, CHECKED OK.SDR CALA2014091892227Spar · mechanic errorNUMBER 2 PYLON LOWER SPAR WEB MIS-DRILLED DURING ACCOMPLISHMENT OF SRM 54-51-12. INTERIM REPAIR ACCOMPLISHED IAW ECRA 5450-02258. REPAIR APPROVED FOR 1 MONTH IAW RDAS 80003171-003-2014 DATED 9-10-14. A NEW RDAS THAT PROVIDES THE INSPECTION & THRESHOLD MUSTSDR CALA2014091892229Stringer · corrodedSTRINGER 41R HAS CORROSION BETWEEN FRAME 63 & 64. FOUND NO ALLOWABLE LIMITS FOR STRINGER DAMAGE IN SRM 53-41-13 PG ,101. REMOVED STRINGER 41R FROM FRAME 58 TO 64 & SPLICE AT FRAME 58. REPLACED WITH NEW STRINGER & FACTORY SPLICE BETWEEN FRAME 58 & 64.SDR CALA2014091892231Stringer · corrodedSTRINGER 40L HAS CORROSION BETWEEN FRAME 63 & 64. FOUND NO ALLOWABLE LIMITS FOR STRINGER DAMAGE IN SRM 53-41-13 PG 101. REMOVED STRINGER 40L BETWEEN FRAME 60 & 64. REPLACED IT IAW SRM 51-42-11 PG 24 SRI INSPECTION NOT REQUIRED.SDR USAA2014090900007Actuator · malfunctionedRETURNED TO FIELD FOR ENG NR 2 COMPRESSOR VANE FAULT ON TAKEOFF ROLL. REPLACED ENG 22 VSV ACTUATOR IAW JOB CARD 26T40075005. LEAK CHECKED GOOD.SDR USAA2014091000006Valve · inoperativeRETURN TO FIELD DUE TO NR 2 ENG BEARING 4 OIL SYS HIGH PRESS INDICATION DURING CRUISE. SWAPPED NR 4 BEARING SCAVENGE VLV TO ENG NR 1, NO HELP. REPLACED NR 4 BEARING SCAVENGE VLV ON ENG NR 1.SDR CALA2014091292106Battery · dischargedEPSU BATTERY EMER LIGHT MSG ON PTP PANEL AFTER EMER LIGHT OPERATIONAL TEST. REPLACED BATTERY IAW AMM 33-51-38. OPERATIONS CHECKED OK.SDR CALA2014090992105Slide · damagedRIGHT OVERWING SLIDE PACK SKIN PEELING OFF. HONEYCOMB STRUCTURE VISIBLE. AREA APPROX 6 INCHES X 6 INCHES, SIGNS OF CORROSION. REPLACED RT OVERWING ESCAPE SLIDE IAW AMM 25-62-42. TESTED OK.SDR CALA2014090992097Skin · damagedLEFT ELEVATOR UPPER SURFACE HAD A 2.0 INCH BY 1.5 INCH AREA OF WATER INGRESS, 30 INCHES FROM THE OTBD END OF THE ELEVATOR & 13 INCHES FWD OF THE TE, ZONE 1. DAMAGE WAS R & R ACP IAW SRM 55-21-11 PARA 5 E FIG 205 CONFIG 1. REPAIR REQUIRES INSPECTION IAW SRI55SDR CALA2014090992098Skin · damagedRIGHT ELEVATOR UPPER SURFACE HAD A 1.5 INCH X 1.5 INCH AREA OF WATER INGRESS, 26 INCHES FROM THE INBD END OF THE ELEVATOR & 26 INCHES FWD OF THE TE ZONE 1. DAMAGE WAS R & R ACP IAW SRM 55-21-11 PARA 5 E FIG 205 CONFIG 1. REPAIR REQUIRES INSPECTION IAW SRI55-SDR CALA2014090392057Threshold · corrodedR2 DOOR THRESHOLD BEAM CORRODED AT FRAME 68 IN AFT CABIN. MATERIAL LOSS WAS 100% AT FRAME 68 NUTPLATE. OUT OF LIMITS IAW SRM 53-41-14 FIG 101. FABRICATED REPAIR ANGLE & FILLER & INSTALLED IAW SRM 53- 41-14 FIG 201 & MT.SDR CALA2014090392049Battery · dischargedEMERGENCY LIGHT FAIL LT EPSM. REPLACED LT ESPM BATTERY, CHECKED OK.SDR CALA2014090392054Threshold · corrodedL2 DOOR THRESHOLD BEAM CORRODED AT FRAME 68 IN AFT CABIN. CORROSION AROUND 2 NUTPLATES WAS EXFOLIATED. CUT OUT DAMAGED PART & INSTALLED REPAIR PARTS IAW SRM 53-11-14 PG 203 PARA 5 FIG 201.SDR CALA2014090392055Stringer · corrodedSTRINGER 42L IS CORRODED BETWEEN FRAME 63 - 64 IN AFT CARGO PIT. REMOVED DAMAGED PART. FABRICATED & INSTALLED NEW STRINGER & REPAIR SPLICE IAW SRM 53-00-13 FIG 201.SDR CALA2014090392056Stringer · corrodedSTRINGER 41L IS CORRODED BETWEEN FRAME 63 - 64 IN AFT CARGO PIT. REMOVED DAMAGED SECTION. FABRICATED & INSTALLED STRINGER & REPAIR SPLICE IAW SRM 53-00-13 FIG 201. REPAIR REQUIRES SRI INSPECTIONS IAW SRI 53-00-13-2-001-00 TABLE 205. 1ST INSPECTION DUE AT 6SDR CALA2014091892239Stringer · corrodedSTRINGER 41L IS CORRODED BETWEEN FRAME 63 - 64 IN AFT CARGO PIT. REMOVED DAMAGED SECTION. FABRICATED & INSTALLED STRINGER & REPAIR SPLICE IAW SRM 53-00-13 FIG 201. REPAIR REQUIRES SRI INSPECTIONS IAW SRI 53-00-13-2-001-00 TABLE 205. 1ST INSPECTION DUE AT 6SDR USAA2014082700001Warning System · false activationEN ROUTE CREW RECEIVED STATUS MSG INOP SYS. REVERSER 1 ENG 1 THRUST, FLIGHT DIVERTED. FOUND NO FAULTS ON PFR OR MSG. PERFORMED OPERATIONAL TEST OF NR 1 ENG THRUST REVERSER IAW AMM 78-31-00-710-041-A 13, TESTED OK. PERFORMED TSM 76-00-00-810-803-A WITH NR 1 SDR CALA2014082692019Structure · damagedDAMAGE TO ACFT, BELOW AFT LOWER CORNER OF DOOR 2L. DAMAGE IS APPROX 9 INCHES LONG & 2 INCHES WIDE BURNISH AREA IAW SRM 53-41 -11. WILL REQUIRE REPETITIVE INSPECTION IAW SR I53-41-11, TABLE 10 4, BLOCK SSI53-41-31. MUST BE ACCOMPLISHED WITHIN 23,800 FC OR 4SDR CALA2014082592016Battery · faultedEXT LOADS FWD LT & BATTERY EMER LT FAULTS WHEN PERFORMING EMER LIGHTS TEST. AFTER RESETTING BREAKERS ONLY GETTING EXT LOAD FWD LT FAULT TRIED NEW POWER SUPPLY, NO HELP. REINSTALLED ORIGINAL, FAULT CLEARS WHEN SLIDE AT DOOR 1L CONNECTOR IS TESTED WITH TEST LASDR CALA2014082692021Skin · dentedSKIN DENT AT FRAME 71 STRINGER 31R OUT OF LIMITS OF SRM 53-51-11. SKIN REPAIRED IAW SRM 53-00-11 PAR 4 W FIG 240, REQUIRES IIR 53-00-11-2-017-00 PAR 3L TBL 226, SKIN THICKNESS .071 AT FRAME.SDR CALA2014082692023Skin · damagedUPPER FUSELAGE SKIN FRAME 60 STRINGER 2L - 3L HAS EXISTING EXT REPAIR IN AREA OF WIFI DOUBLER INSTALLATION. INT SKIN IN SAME AREA HAS EXISTING SCRIBE MARKS AROUND SHEAR TIES & DRILL START. REPLACED EXISTING DOUBLER IAW ECRA 5340-01571 & REO-L01421. BLENDED SDR CALA201409039058Seal · leakingNUMBER 1 ENGINE HAD DECREASING OIL QTY, LANDED WITH 4.5 QTS. NO LOSS OF OIL PRESSURE. LANDED WITH ENGINE AT IDLE. FOUND NR 5 BEARING COVER SEAL DAMAGED. REPLACED SEAL IAW MM 72-51-41-400-010B. CLEANED OUTSIDE BEARING AREA OF HEAVY COKE RESIDUE. INSPECTEDSDR USAA2014081900003Warning System · false activationIN CRUISE FLIGHT AT FL 350 STATUS MSG APPEARED. WHEN SLATS OUT ENG 1 AT IDLE ON GND ENG 1 MAX PWR, IDLE " $ INOP SYS REVERSER NR 1 ENG 1 THRUST. PERFORMED BITE TEST OF NR 1 ENG FADEC IAW AMM 73-22-00-710-040-A, TEST PASSED. PERFORMED BITE TEST OF ENG 1 INTESDR CALA2014082192008Stringer · corrodedSTRINGER 43R BETWEEN FRAMES 27 & 28 CORRODED. FOUND NO ALLOWABLE LIMITS FOR STRINGER 43R SPLICE IAW SRM 53-00-13 PG 101. R & R THE STRINGER IAW SRM 51-42-11 P 1- 5.SDR YENA20140814155Seal · leakingFLT 3, PRECAUTIONARY AIR RETURN TO DEPARTURE FOR NR 1 ENGINE LOW OIL QUANTITY AND HIGH TRENDING OIL CONSUMPTION. INSPECTED NR 1 ENGINE FOR OIL LEAKS, FOUND DEOILER BREATHER WORN. R & R DEOILER SEAL ASSY IAW MM 72-60-31. ACCOMPLISHED ENGINE RUN TO INSPECT SESDR CALA2014081591991Stringer · corrodedSTRINGER 42R FOUND CORRODED BEYOND LIMITS FRAME 60 TO 64. R & R STRINGER 42R FROM FRAME 60 TO 64 PND53470418219 IAW SRM 51-42-11.SDR CALA2014081591992Skin · scratchedSCRATCHES NOTED 7 INCHES BELOW R1 DOOR CUT OUT 10 INCHES & 16 INCHES OF BUTT SPLICE AT FRAME 20. BLEND MEASURES 1.5 INCHES X 1 INCHES .091 IS LOWEST REMAINING SPOT.SDR CALA2014081491989Door Sill · corrodedCORROSION FOUND BEYOND LIMITS AT R2 DOOR SILL UNDER GIRT BAR FITTINGS. R & R PN D5348004320701 IAW A320SRM51-42-11 PARA 5 & 6.SDR CALA2014081491990Stringer · corrodedSTRINGER 41R FOUND CORRODED BEYOND LIMITS AT FRAME 63 - 64. R & R STRINGER 41R FROM SPLICE FRAME 68 TO 63 IAW SRM 51-42-11.SDR CALA2014081491987Slide · faultyEMERGENCY LIGHT TEST FAILS. MSG EPSU EXT LOAD AFT LT. R & R L2 DOOR ESCAPE SLIDE PACK ASSEMBLY IAW AMM 25-62-44. PLACARD REMOVED.SDR CALA2014081391979Wire · damagedCODE, EXTERNAL LOADS FWD LEFT 33-51-38. FOUND EMER LIGHT CHECK DURING 2 SVC. REPLACED WIRE NR 5109 FROM CONNECTOR 2819VC PINK TO CONNECTOR 2871VC PIN B IAW WDM33-51-04. PERFORMED OPERATIONAL TEST OF THE EMER LIGHTS IAW MM33-51-00. OPERATIONS TESTED GOOD, NOSDR CALA2014081391980Wire · damagedFOUND WIRE 5109 INTERMITTENT BY WIGGLING HARNESS IN DOOR AT SOFT CONDUIT. REPLACED WIRE NR 5109 FROM CONNECTOR 2819VC PIN K TO CONNECTOR 2871VC PIN B IAW WDM33-51-04. PERFORMED OPERATIONAL TEST OF THE EMER LIGHTS IAW MM33-51-00. OPERATIONS TESTED GOOD, NO FASDR SOKF20140812006Computer · faultyDURING CLIMB THE ACFT RETURNED DUE ELAC 2 FAULT. IAW TSM 27-93-00-810-967-A PERFORMED R & R OF ELAC 2 IAW AMM 27-93-34-000-001 & AMM 27-93-34-400-001. PERFORMED OPERATIONAL TEST IAW AMM 27-93-00-710-001 & LAND CAT III CAPABILITY TEST IAW AMM TASK 22-97-00-71SDR CALA2014081391960Stringer Splice · corrodedFORWARD CARGO PIT STRINGER SPLICE ON STRINGER 41R BETWEEN FRAME 30 - 31 CORRODED. STRINGER SPLICE REPLACED IAW SRM 51-42-11 & 51-44-11.SDR CALA2014081191932Landing Gear · low pressureLANDING GEAR WOULD NOT RETRACT WHEN HANDLE SELECTED UP. FAULTING NLG EXTEND PROX SENSORS 24GA & 25GA. CHARGED NLG NITROGEN PRESS IAW AMM 12-14-614-004A.
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