IAE V2522-A5
Service difficulty reports · 3,463
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 = 'V2522A5' 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 = 'V2522A5' 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 CALA2014081891999Battery · dischargedFAILED EMER LIGHT TEST FWD FLIGHT ATTENDANT PANEL. EPSU BATTERY EMER LIGHT REPLACED BOTH LT & AFT LT BATTERIES AMM 33-51. TEST NOW OK.SDR CALA2014081891997Door Sill · corrodedL2 DOOR SILL HAS SPOTS OF CORROSION BETWEEN FRAME 66 & 68. BLENDED CORROSION, AFTER BLENDING ALL AREAS WERE WITHIN LIMITS EXCEPT FOR NUTPLATE AT INBD FLANGE ON FRAME 68 IAW SRM 53-41-14 FIG 101.SDR CALA2014081891995Stringer · corrodedCORROSION FOUND ON STRINGER 42R AT FRAME 60 IN AFT PIT. UPON FURTHER EVALUATION FOUND STRINGER 42R CORRODED BEYOND LIMITS. REMOVED CORRODED SECTION OF STRINGER & SPLICED IN NEW SECTION OF STRINGER BETWEEN FRAME 59.5 & 60.5 IAW SRM 53-00-13 FIG 201.SDR CALA2014081391982Door Sill · corrodedL2 DOOR SILL FWD & AFT HAS CORROSION FRAME 68 - 68, STRINGER 22L - 23L. FABRICATED & INSTALLED REPAIR IAW SRM 53-41-14 REPAIR PRINCIPLE 5 FIG 201 SHEET 3 AREA K.SDR CALA2014081391976Door Sill · corrodedR2 DOOR SILL WAS FOUND CORRODED. SILL REPLACED IAW SRM 51-42-11.SDR CALA2014081391956Plate · damagedFOUND BURN MARK ON LOWER RT CORNER OF STATIC PORT AREA. STBY LT STATIC PORT. DISCONNECTED STBY STATIC PORT & REMOVED FROM INSIDE SURFACE. REMOVED STATIC PORT BLANKING PLATE IAW AMM 53-19-42. INSTALLED IAW AMM 53-19-42-400-001-A TO STEP 3F 7. VERIFIED ZONSDR CALA2014081391975Stringer · corrodedAFT PIT STRINGER 31R CORRODED BETWEEN FRAME 65 & 66. STRINGER SECTION WAS REPLACED FROM FRAME 65 - 69 IAW SRM 53-00-13.SDR CALA2014081191928Door Sill · corrodedR2 DOOR SILL FRAME 66 - 68 CORROSION FOUND OUT OF LIMITS. REPAIRED IAW SRM53-41-14 PARA 5A FIG 201.SDR CALA2014081191931Chiller · overheatedAFT GALLEY CHILLER OVERHEATED IAW CREW VERBAL. CB'S PULLED THE CB PANEL AT GALLEY & COFFEE MAKERS WERE HOT & DID NOT COOL DOWN. EVENTUALLY CREW DESELECTED THE COMMERCIAL SWITCH & STILL DID NOT COOL. DEFERRED IAW MEL. DEACTIVATED CHILLER, PULLED & COLLARED SDR CALA2014081391963Fitting · corrodedRIGHT MLG UPPER SIDE STAY BUSHING HAS EVIDENCE OF ROTATION. SEALANT FOUND SPLIT. REMOVED CORROSION BY OVER SIZING SIDE STAY FITTING LUG & INSTALLING HIGH INTERFERENCE FIT BUSHINGS IAW SRM 57-26-13 PARAGRAPH 5 E FIG 206. ACID ETCHED & FPI IAW 57-00-0PR8 & NTSDR CALA2014081391964Fitting · corrodedLEFT MLG UPPER SIDE STAY BUSHING SHOWS EVIDENCE OF ROTATION. SEALANT IS SPLIT. CORROSION FOUND. REMOVED CORROSION BY OVER SIZING SIDE STAY FITTING LUG & INSTALLING HIGH INTERFERENCE FIT BUSHINGS IAW SRM 57-26-13 PARAGRAPH 5 E FIG 206. ACID ETCH & FIP IAW 5SDR CALA2014081391967Skin · corrodedLEFT WING LOWER FUEL TANK LANDING 540HB HOLE B & 540KB HOLE D WERE FOUND CORRODED. HOLES WERE REAMED TO 0.363 & REPAIRED IAW SRM 57-21-11 PARA 5 B FIG 202.SDR CALA2014081391968Skin · corrodedLEFT WING LOWER FUEL TANK LANDING 540HB HOLE AE & 540KB HOLE H WERE FOUND CORRODED. HOLES WERE REAMED TO 0.391 & 0.406 & REPAIRED IAW ECRA 5721-01374.SDR CALA2014081391969Skin · corrodedLEFT WING LOWER FUEL TANK LANDING 540HB HOLE B & 540KB HOLE D WERE FOUND CORRODED. HOLES WERE REAMED TO 0.363 & REPAIRED IAW SRM 57-21-11 PARA 5 B FIG 202.7.SDR CALA2014081391970Skin · corrodedLEFT WING LOWER FUEL TANK LANDING 540HB HOLE AE & 540KB HOLE H WERE FOUND CORRODED. HOLES WERE REAMED TO 0.391 & 0.406 & REPAIRED IAW ECRA 5721-01374.SDR CALA2014081191949Door Frame · corrodedDETAILED INSPECTION, ROTO OF AFT PAX CREW DOOR CUT OUT. DOOR STOP FITTINGS HOLES, AT FRAME 68 WEB, LT & RT IAW AMM 53-41-00-220-813. CORROSION DMG NOTED AT R2 POS 1, 2, 3 & 6. L2 NR 2. CLEANED & RESCANNED, NO INDICATIONS.SDR CALA2014081391958Light · malfunctionedOVERHEAD EMER LIGHTS INOPERATIVE. OVERWING EMER EXIT LIGHTS ON CONTINUOUSLY RESET. CIDS EMER LIGHTS IN CABIN, OPERATIONS CHECKED GOOD.SDR CALA2014080691736Skin · dentedEXTERNAL FUSELAGE SKIN DENTED AT THREE EACH LOCATIONS FRAME 23 & 24, STRINGER 23L & 24L. FOUND DENTS TO BE OUT OF LIMITS IAW SRM 53-11-11 FIG 115. FABRICATED REPAIR DOUBLER & INSTALLED IAW SRM 53-00-11 FIG 232 PG 505 - 506.SDR CALA2014080691738Slide · faultedEPSU EXT LOAD FWD L FAULT WHEN EMER LIGHTS TEST PERFORMED. REPLACED SLIDE ASSEMBLY DUE TO EXTERNAL LOAD FAULT DOOR 1R IAW 25-62-44.SDR CALA2014080691735Skin · dentedSMALL DENT FOUND ON ARRIVAL ON RT FUSELAGE, 1 FT ABOVE UPPER WINDOW LINE & 7 WINDOWS FT OF OVERWING EXIT. DENT WAS OUT OF LIMITS IAW SRM 53-41-11. FABRICATED REPAIR DOUBLER 7 INSTALLED IAW SRM 53-00-11.SDR CALA2014080191589Door Sill · corrodedL2 DOOR SILL HAS CORROSION AT 7 E. LOCATIONS BETWEEN FRAME 66 & 68. REPAIRED THE AREA IAW SRM 53-41-14.SDR CALA2014080191586Skin · damagedLEFT AIRFONE ANTENNA AREA NEEDS REPAIRED AT FRAME 63 - 64 STRINGER 41 - 42LT VARIANT 002. REPAIRED IAW SRM 53-00-11 PARAGRAPH 4S FIG 230.SDR CALA2014080191588Door Sill · corrodedR2 DOOR SILL FRAME 66 - 68 CORROSION FOUND OUT OF LIMITS. REPAIRED IAW SRM 53-41-14 PARA 5A FIG 201.SDR CALA2014072891547Skin · dentedFUSELAGE SKIN RT DENT FOUND OUT OF LIMITS AT FRAME 1 - 28 + WL. INSTALLED A 7 X 7 REPAIR IAW SRM 53-00-11 4S-230 PRINCIPLE 2. FIRST INSPECTION REQUIRED AT 77452 PTC. R & R IAW SRM 53-00-11-PH4S FIG 230. REINSPECT IAW SRI53-00-11-2-017-00.SDR CALA2014072891546Shear Web · corrodedRIGHT FRAME SUPPORT FOR SHEAR WEB FOUND CORRODED FRAME 69 - 70R PN 5347112320300. R & R SHEAR WEB IAW SRM 51-42-11.SDR CALA2014072591512Door Sill · corrodedMAJOR REPAIR. R2 DOOR SILL HAS CORROSION AT GIRT BAR ATTACHMENT BETWEEN FRAME 66 & 68 AT STRINGER 43. AFTER REMOVING CORROSION, MATERIAL LOSS WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-41-14 FIG 101. R & R RT 2 DOOR SILL.SDR CALA2014072291496Light · inoperativeEMERGENCY LIGHTS FAILED TEST IAW NR 2 SERVICE. FOUND OVERWING EMER SLIDE LIGHT INOPERATIVE. RELAMPED IAW MM 33-51-15 EMER LIGHT TEST DID NOT PASS.SDR CALA2014072991571Sensor · faultyAT CRUISE NOSE WHEEL STEERING & BRAKE SYS 2 FAULT. IAW FLIGHT MANUAL & QRH, RESET WAS ATTEMPTED WITH THE ANTI-SKID SWITCH & MALFUNCTION RETURNED EXCEPT BRAKE SYS FAULT WAS NOW THE NR 1 SYS. R & R SENSOR 3GC IAW AMM 32-51-19. OPERATIONS CHECKED OK.SDR CALA2014071591468Control Unit · malfunctionedSYSTEM 1 FAULT DISPLAYED ON UPPER ECAM SCREEN. INFLIGHT RESET NO HELP. BSCU REPLACEMENT. SYS 1 FAULT ON ECAM WENT AWAY UPON LANDING NO HISTORY.SDR CALA2014071191441Actuator · malfunctionedCOMPRESSOR VANE DISPLAYED ON UPPER ECAM SCREEN. ENG PARAMETERS NORMAL. R & R VSV ACTUATOR IAW AMM 75-32-41. LEAK & OPERATIONS CHECK WERE GOOD OK TO CONTINUE.SDR CALA2014071191440Hydraulic System · lowFLIGHT DIVERTED DUE TO LOSS OF YELLOW HYDS. SERVICED HYDS TO FULL LEVEL.SDR CALA2014071191412Panel · damagedON ARRIVAL PANEL 192MB FOUND OPENED & DAMAGED. ALSO DAMAGED PANEL 192FB AC BAY RT. TWO PUNCTURES DIRECTLY BELOW PANEL 192MB. REPLACED PANEL 192MB.SDR CALA2014070191392Computer · malfunctionedFLIGHT CONTROL FLAP 1 FAULT. REPLACED NR 1 SFCC IAW AMM 27-51-34. TESTED OK ALSO CLEANED CONNECTOR ON FLAP PCU VLV BLOCK NR 1 & 2. OPERATIONS CHECK FLAPS RAN UP & DOWN 4 TIMES NO MSG NOTED.SDR CALA2014063091365Warning System · false indicationCREW REPORTS WHILE ATTEMPTING NR 1 ENG START RECEIVED ENG 1 START FAULT WITH EGT OVER LIMIT. CHECKED EXCEEDANCE PAGE & NO OVERTEMP OCCURRED. CHECKED INLET & EXHAUST, NO DEFECTS NOTED. APU BLEED SYS INOPERATIVE.SDR CALA2014062091307Power Supply · faultedEMERGENCY LIGHTS TEST FAULTS EPSU INT LOAD EMER RT. REPLACED EPSU POWER SUPPLY AT BELOW RT EMER EXIT DOOR 12WL.SDR CALA2014062091306Slide · defectiveEMERGENCY LIGHT TEST FAILS WITH EPSU EXT LOAD FWD LT IAW TSM 33-51-00-810-808. FOUND 1R SLIDE BAD.SDR CALA2014062091310Door Sill · corrodedCORROSION ON L2 DOOR SILL AT FRAME 66 - 68 IN AFT WET AREA. A 1 SECTION OF THE FLANGE WAS CUT OUT & A REPAIR INSTALLED IAW SRM 53-41-14 PARA 5 A FIG 201, REPAIR PRINCIPAL 5.SDR CALA2014061791298Warning System · faultyRIGHT WING OVERWING EXIT NOT SHOWING ARMED. PLACED ON MEL, DDP COMPLIED WITH.SDR CALA2014062091305Warning System · false activationCOMPRESSOR VANE DISPLAYED ON UPPER ECAM SCREEN, ENG PARAMETERS NORMAL. OCCURRED DURING CLIMB OUT WAS JUST MOMENTARY. THEN REOCCURRED DURING TAXI-IN & REMAINED DISPLAYED. WORKED WITH LOCAL MAINTENANCE & FOUND FAULT ACRONYM B25TK IN FADEC. TROUBLESHOOTING ONSDR CALA2014062091308Spar · chafedNUMBER 2 PYLON LOWER SPAR FOUND CHAFED AT LOWER SPAR RIB 5. REPAIR ACCOMPLISHED. THIS IS A CAT B REPAIR & REQUIRES SUBSEQUENT INSPECTIONS.SDR CALA2014062091309Door Sill · corrodedR2 DOOR SILL INBD FLANGE WAS FOUND CORRODED AT FRAME 68. A 1 SECTION OF THE FLANGE WAS CUT OUT & A REPAIR INSTALLED. REPAIR REQUIRES INSPECTION IAW SRI53-41-14-2-001-00 PARA 3 A TBL 202.SDR CALA2014061791297Spar · chafedNUMBER 2 PYLON SHOWS SIGNS OF CHAFING AT FIREWALL SEAL LOWER SPAR RIB 5. ACCOMPLISHED REPAIR TO NR 5 RIB SPAR ON NR 2 PYLON IAW SRM54-51-12 FIG 202. SRI INSPECTIONS WILL BE ACCOMPLISHED AS REQUIRED.SDR CALA2014061691281Slat · lockedFLIGHT CONTROL SLATS LOCKED. WING TIP BREAKER ON SLAT SYS 2 FAULT CYCLED CB & PERFORMED BITE CHECK. NO FAULTS FOUND, NO MSGS. OPERATIONS CHECKED WITH CREW PRESENT. OPERATIONS CHECKED GOOD IAW AMM 27-51-00.SDR CALA2014061691278Wire · damagedFORWARD CABIN EWIS RED & BLACK WIRES DAMAGED AT SEAT TRACK ROW 12 LT. REPAIRED RED & BLACK EMER LIGHT WIRES DAMAGED AT SEAT ROW 12 LT IAW ESPM 20- 53-21. INSULATION WAS DAMAGED ON WIRES FROM CONNECTOR 7260VC5-A 3330-0872-1673-18N & 3330-08702-1673-18.SDR CALA2014061391256Hydraulic Line · chafedFOUND HYD LEAK COMING FROM RT LG UPPER FWD BEHIND BEAM FOUND YELLOW SYS PRESS LINE LEAKING CHAFED ON SUCTION LINE IAW IPC 29-13-05-04C ITEM 23 & 24. ALL LINE CLAMPS REMOVED STOWED IN PART BAGS AT POSITIONS REMOVED YELLOW SYS HEAD PRESS REMOVED. INSTALLED & SSDR CALA2014061691284Mmr · faultedGPWS GLIDESLOPE DEVIATION, MODE 5, HAS BEEN DEFERRED IAW MEL CARD 34335. TROUBLE SHOT IAW TSM34-48- 00-810-815-A. ACCOMPLISHED OPERATIONAL TEST OF THE ENHANCED GPWS GND SELF-TEST FUNCTION, OPERATIONS CHECKED GOOD. NO FAULTS DURING EPGWS FAULT REVIEW, NR 1 MSDR CALA2014061391268Anti-Ice System · failedFLIGHT HAD WINDOW HEAT FAIL EN-ROUTE.SDR CALA2014060991240Stringer · corrodedSTRINGER 44 BETWEEN FRAME 64 - 65 HAS CORROSION. REMOVED CORROSION & INSTALLED REPAIR ANGLE IAW SRM 53-00-13 FIGURE 202 SHEET 2. NO SRI REQUIRED.SDR CALA2014060991229Angle · crackedNR 2 PYLON HAS A CRACKED ANGLE OTBD SIDE NEAR RIB 6. CUT OUT CRACKED SPAR OTBD SIDE NEAR RIB 6 IAW SRM 54-52-12 FIG 211 SH 2. FABRICATED REPAIR SPLICE & INSTALLED SPLICE REPAIR IAW SRM 54-52-12. THIS REPAIR DOES NOT REQUIRE SRI INSPECTIONS IAW ABOVE SRM.SDR CALA2014060991230Stringer · corrodedSTRINGER 33R BETWEEN FRAME 59 & 60 HAS LIGHT CORROSION. REMOVED CORROSION IAW SRM 51-73-11. THICKNESS OF THE FLANGE IS 0.063. LOW READING AFTER BLENDING IS 0.037. MAX LOSS ALLOWED IS 0.0315, 0.5 X TC. WITHIN LIMITS IAW SRM 53-00- 13 FIG 202 SH 4 PG 231.
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