# IAE V2522-A5

- Type: Engine model (FAA registry)
- Registry codes: 34607, 34612
- Manufacturer (registry): IAE
- Model: V2522-A5
- Engine type: Turbo-fan
- Power: 23,040 lb thrust
- Data sheet: [TCDS E40NE](https://openairdocs.org/tcds/E40NE) (OpenAirDocs)
- Holder: International Aero Engines AG (IAE)
- Installed in: 2 registered aircraft
- Page: https://openairdocs.org/engine/iae-v2522-a5

Model codes come from the FAA registry's reference file. The FAA lists this model under more than one registry code, usually for different spellings of the maker. This page covers them all.

## ADs that may apply (OpenAirDocs)

Matched to this engine model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment.

- [AD 2026-17-03](https://openairdocs.org/ad/2026-17-03): Turbine Engine Compressor Section · International Aero Engines V2522-A5, V2524-A5, V2525-D5 and 7 more. Effective Sep 24, 2026
- [AD 2025-19-13](https://openairdocs.org/ad/2025-19-13): Turbine Section · International Aero Engines V2522-A5, V2524-A5, V2525-D5 and 7 more. Effective Oct 29, 2025
- [AD 2025-17-16](https://openairdocs.org/ad/2025-17-16): Turbine Engine Compressor Sections · International Aero Engines V2522-A5, V2524-A5, V2525-D5 and 7 more. Effective Oct 10, 2025
- [AD 2024-11-03](https://openairdocs.org/ad/2024-11-03): Turbine Engine · International Aero Engines V2522-A5, V2524-A5, V2525-D5 and 7 more. Effective Jun 26, 2024
- [AD 2022-02-09](https://openairdocs.org/ad/2022-02-09): Turbine Section · International Aero Engines V2522-A5, V2524-A5, V2525-D5 and 7 more. Effective Mar 15, 2022
- [AD 2021-14-19](https://openairdocs.org/ad/2021-14-19): Turbine Section · International Aero Engines V2522-A5, V2524-A5, V2525-D5 and 7 more. Effective Aug 5, 2021
- [AD 2021-11-51](https://openairdocs.org/ad/2021-11-51): Turbine Section · International Aero Engines V2522-A5, V2524-A5, V2527-A5 and 4 more. Effective Jul 19, 2021
- [AD 2021-05-18](https://openairdocs.org/ad/2021-05-18): Turbine Section · International Aero Engines V2500-A1, V2522-A5, V2524-A5 and 8 more. Effective Apr 29, 2021
- [AD 2021-01-03](https://openairdocs.org/ad/2021-01-03): Turbine Section · International Aero Engines V2500-A1, V2522-A5, V2524-A5 and 8 more. Effective Jan 21, 2021
- [AD 2020-09-03](https://openairdocs.org/ad/2020-09-03): Turbine Engine Compressor Section · International Aero Engines V2500-A1, V2522-A5, V2524-A5 and 8 more. Effective May 29, 2020
- [AD 2020-07-51](https://openairdocs.org/ad/2020-07-51): Turbine Section · International Aero Engines V2522-A5, V2524-A5, V2525-D5 and 6 more. Effective Apr 28, 2020
- [AD 2019-18-01](https://openairdocs.org/ad/2019-18-01): Turbine Section · International Aero Engines V2522-A5, V2524-A5, V2527-A5 and 4 more. Effective Oct 15, 2019
- [AD 2017-14-07](https://openairdocs.org/ad/2017-14-07): Turbine Engine · International Aero Engines V2522-A5, V2524-A5, V2525-D5 and 7 more. Effective Aug 21, 2017
- [AD 2016-25-11](https://openairdocs.org/ad/2016-25-11): No. 3 bearing · International Aero Engines V2522-A5, V2524-A5, V2525-D5 and 7 more. Effective Jan 20, 2017
- [AD 2016-18-10](https://openairdocs.org/ad/2016-18-10): High- pressure turbine (HPT) stage 2 hub · International Aero Engines V2522-A5, V2524-A5, V2525-D5 and 6 more. Effective Oct 7, 2016
- [AD 2015-10-04](https://openairdocs.org/ad/2015-10-04): HPC stage 3 to 8 drum · International Aero Engines V2500-A1, V2522-A5, V2524-A5 and 7 more. Effective Jul 1, 2015
- [AD 2011-25-08](https://openairdocs.org/ad/2011-25-08): High- pressure turbine (HPT) case burn-through events · International Aero Engines V2500-A1, V2522-A5, V2524-A5 and 7 more. Effective Jan 17, 2012
- [AD 2010-06-18](https://openairdocs.org/ad/2010-06-18): Vortex reducers · International Aero Engines V2500-A1, V2522-A5, V2524-A5 and 7 more. Effective Apr 22, 2010
- [AD 2008-14-15](https://openairdocs.org/ad/2008-14-15): No. 4 bearing oil system components · International Aero Engines V2500-A1, V2522-A5, V2524-A5 and 7 more. Effective Aug 20, 2008
- [AD 2007-21-05](https://openairdocs.org/ad/2007-21-05): Monitoring of N2 vibration on all IAE V2500 series engines · International Aero Engines V2500-A1, V2522-A5, V2524-A5 and 7 more. Effective Nov 15, 2007
- [AD 2006-25-01](https://openairdocs.org/ad/2006-25-01): Master magnetic chip detector (MCD) · International Aero Engines V2522-A5, V2524-A5, V2527-A5 and 4 more. Effective Jan 8, 2007
- [AD 2004-12-08](https://openairdocs.org/ad/2004-12-08): Airworthiness Limitations Section (ALS) · International Aero Engines V2500-A1, V2522-A5, V2524-A5 and 7 more. Effective Jul 23, 2004
- [AD 2000-22-07](https://openairdocs.org/ad/2000-22-07): High Pressure Turbine (HPT) · International Aero Engines V2522-A5, V2524-A5, V2525-D5 and 6 more. Effective Dec 6, 2000
- [AD 99-13-01](https://openairdocs.org/ad/99-13-01): High Pressure Turbine (HPT) Stage 1 Inner Rotating Airseal (TOBI ID seal) · International Aero Engines V2500-A1, V2522-A5, V2524-A5 and 4 more. Effective Jun 25, 1999
- [AD 99-04-03](https://openairdocs.org/ad/99-04-03): High Pressure Compressor (HPC) Stage 9-12 Drum · International Aero Engines V2522-A5, V2524-A5, V2525-D5 and 5 more. Effective Apr 12, 1999

Historical (superseded or no longer in force):

- [AD 2021-11-15](https://openairdocs.org/ad/2021-11-15) (historical): Turbine Section · International Aero Engines V2522-A5, V2524-A5, V2525-D5 and 7 more. Effective Jul 13, 2021
- [AD 2019-06-06](https://openairdocs.org/ad/2019-06-06) (historical): Turbine Engine Combustion Section · International Aero Engines V2500-A1, V2522-A5, V2524-A5 and 7 more. Effective Apr 12, 2019
- [AD 2012-09-09](https://openairdocs.org/ad/2012-09-09) (historical): High-pressure compressor (HPC) stage 3 to 8 drums · International Aero Engines V2500-A1, V2522-A5, V2524-A5 and 7 more. Effective Jun 27, 2012
- [AD 2010-20-07](https://openairdocs.org/ad/2010-20-07) (historical): Initial and repetitive on-wing ultrasonic inspections · International Aero Engines V2500-A1, V2522-A5, V2524-A5 and 7 more. Effective Nov 1, 2010
- [AD 2003-11-23](https://openairdocs.org/ad/2003-11-23) (historical): Master magnetic chip detector (MCD) · International Aero Engines V2522-A5, V2524-A5, V2527-A5 and 3 more. Effective Jun 20, 2003
- [AD 99-08-11](https://openairdocs.org/ad/99-08-11) (historical): International Aero Engines V2500-A1, V2522-A5, V2524-A5 and 7 more. Effective May 13, 1999

## Information bulletins (advisory) (1)

- [SAIB 2026-11](https://openairdocs.org/saib/2026-11): Theft of Turbofan Engine Parts before Mutilation. Issued Jun 8, 2026

## Registered aircraft (2)

- [N606NK](https://openairdocs.org/aircraft/N606NK): [Wells Fargo Trust Co Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20TRUST%20CO%20NA%20TRUSTEE), [Columbia, MD](https://openairdocs.org/faa-place/MD/Columbia), built 2011, S/N 4592
- [N817UA](https://openairdocs.org/aircraft/N817UA): [United Airlines Inc](https://openairdocs.org/faa-owner/UNITED%20AIRLINES%20INC), [Chicago, IL](https://openairdocs.org/faa-place/IL/Chicago), built 1998, S/N 0873

## NTSB investigations

None matched to aircraft with this engine model.

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20090522009219I](https://openairdocs.org/incident/20090522009219I), May 22, 2009: Airbus A319131 (N817UA), Pittsburgh, PA, No damage. (-23) Event summary - at approximately 1612 greenwich mean time (gmt), while climbing through 24,000 feet, the flight crew observed a message for the green…

## Service difficulty reports (3,460, newest 50)

As reported by operators and repair stations, by the model named in the report.

- [SDR CALA2026102220518](https://openairdocs.org/sdr/CALA2026102220518), Oct 22, 2026: ELEC CONNECTOR. FOD. BRAKES AUTO BRK FAULT ECAM ON FINAL APPROACH, DID CHECKLIST, CYCLED LANDING GEAR, NORMAL LANDING AND BRAKES POST FLT FAULTING BRK SELECTOR VALVE (23GG) ON BSCU 
- [SDR CALA2026102220526](https://openairdocs.org/sdr/CALA2026102220526), Oct 20, 2026: FLOOR SUPPORT. CRACKED. FWD CARGO, FRMS 28 - 34, STR 35R. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11/001 2E, SRM 51-44-11/001, SRM 51-46-11/00 1, & SRM 51-75-12-911-002.
- [SDR CALA2026102120482](https://openairdocs.org/sdr/CALA2026102120482), Oct 19, 2026: UNKNOWN. ODOR. FUMES THROUGHOUT ACFT AFTER SHUTDOWN OF NR 2 ENGINE AND OPENING APU BLEED. RAN APU & BLEED TO VERIFY ODOR IN CABIN, ACCOMPLISHED INSPECTION IAW AMM 05-50-00-810
- [SDR CALA2026102120493](https://openairdocs.org/sdr/CALA2026102120493), Oct 17, 2026: FLASHLIGHT. NO DISCREPANCY. AFT FLASHLIGHT NEAR FLIGHT ATTENDANT JUMPSEAT BATTERY FLASHING RED INOP STICKER INSTALLED ON THE AFFECTED FLASHLIGHT BY THE CAPTAIN. AFT OTBD FLASHLIGHT WORKING
- [SDR CALA2026101920451](https://openairdocs.org/sdr/CALA2026101920451), Oct 15, 2026: HYDRAULIC LINE. LEAKING. GREEN HYD SYS LOW PRESSURE. ECAM RUN MANUAL GEAR EXTENSION. FOUND HYD LINE LEAKING IN LEFT WING BETWEEN RIB 1 AND RIB 2. REMOVED LINE #30 REF IPC 29-11-05-02. R
- [SDR CALA2026101620404](https://openairdocs.org/sdr/CALA2026101620404), Oct 14, 2026: PUMP. LEAKING. HYD G ENG 1 PUMP LO PR, HYD G SYS LO PR, GREEN SYS DEPLETED SDR INFO ADDED FOUND AN ACTIVE LEAK WITH HYD PRESSURE OFF ON LINE AT THE TOP OF NR 1 ENGINE OTBD SID
- [SDR CALA2026101320358](https://openairdocs.org/sdr/CALA2026101320358), Oct 12, 2026: POWER SUPPLY. FAULTED. TEST OF THE EMERGENCY LIGHTS FAILS WITH EPSU INT LOAD EMER R, EPSU BATTERY AFT L AND EPSU UNIT EMER L MESSAGES. R&R RIGHT OVER WING EPSU REF AMM 33-51-400-001-A
- [SDR CALA2026101320357](https://openairdocs.org/sdr/CALA2026101320357), Oct 11, 2026: LIGHT. INOPERATIVE. AISLE SEAT 8C EMERGENCY LIGHT INOP. REMOVED AND REPLACED PATHWAY ILLUMINATION LIGHT ON SEAT 8C IN REFERENCE TO AMM 33-51-19. OPS CHECK GOOD. PARTS USED: BR9644-
- [SDR CALA2026101320315](https://openairdocs.org/sdr/CALA2026101320315), Oct 10, 2026: FLOOR SUPPORT. CORRODED. AFT CARGO COMPARTMENT FLOORBOARD PROFILE AT FR 58-59 STR 38L, FLOORBOARD RISER/RAMP CORRODED. REMOVED AND REPLACED AFT CARGO FLOORBOARD RISER AT FR 58-59 STR 38
- [SDR CALA2026100920246](https://openairdocs.org/sdr/CALA2026100920246), Oct 8, 2026: FRAME. CRACKED. RIGHT FRAME 16 DOUBLE JOGGLE AREA HOLE 5, HAS A CRACK INDICATION IN CORNER DOUBLER LAYER AT 6 OCLOCK DIRECTION 100%. ACCOMPLISHED A REPAIR IAW REO L26059, REV I
- [SDR CALA2026100820218](https://openairdocs.org/sdr/CALA2026100820218), Oct 7, 2026: ACCESS PANEL. DAMAGED. DURING REMOVAL OF ACCESS PANEL 540KB, ACFT SKIN WAS DAMAGED. EXCEEDED LIMITS OF SRM 57-21-11-300-002, INTERIM REPAIR PERFORMED TO FUEL ACCESS PANEL 540KB IAW PA
- [SDR CALA2026100720173](https://openairdocs.org/sdr/CALA2026100720173), Oct 5, 2026: SEAT TRACK. CORRODED. CORROSION LOCATED AT SEAT TRACK Y-1292 AND FRAME 20. REMOVED SEAT TRACK Y-1292 FR12-FR24 IAW A319 SRM 51-42-11/001 RE V 159 PAR 2.F, REPLACED SEAT TRACK Y-1292 
- [SDR CALA2026100720181](https://openairdocs.org/sdr/CALA2026100720181), Oct 5, 2026: SEAT TRACK. CORRODED. CORROSION ON SEAT TRACK Y-765 AND FRAME 20 2 AEREAS. REMOVED AND REPLACED SEAT TRACK 765 IAW A319 SRM 51-42-11 FROM F R12-FR24.
- [SDR CALA2026100520102](https://openairdocs.org/sdr/CALA2026100520102), Oct 3, 2026: FUEL CAP. MISSING. MISSING FUEL CAP UPON ARRIVAL. INSTALLED A FUEL CAP.
- [SDR CALA2026100620130](https://openairdocs.org/sdr/CALA2026100620130), Oct 3, 2026: FLOORBEAM. CORRODED. AFT WET AREA, LT FLOOR BEAM Y160.5, BARREL NUT CORRODED IN LAV MOUNT FITTING, JUST AFT OF FR 68. REMOVED AND REPLACED L/H FLOOR BEAM Y160.5 FR68-70 IAW A319 SRM
- [SDR CALA2026100620132](https://openairdocs.org/sdr/CALA2026100620132), Oct 3, 2026: WINDOW FRAME. CRACKED. RIGHT WINDSHIELD FRAME CONTINUITY FITTING AREA ROTO TEST INSPECTIO N FOUND CRACK INDICATION IN MOST I/B HOLE GEN BY V929087 ON AAR LCQ NR 9298821/26821 UP DATED
- [SDR CALA2026100520071](https://openairdocs.org/sdr/CALA2026100520071), Oct 2, 2026: LIGHT. DISCONNECTED. EMERGENCY LIGHTS AT SEATS 27C AND 28C WILL NOT ILLUMINATE. FOUND LIGHT ASSEMBLIES AT SEATS 27C AND 28C TO BE DISCONNECTED. CONNECTED LIGHTING ASSEMBLIES AND PER
- [SDR CALA2026092920000](https://openairdocs.org/sdr/CALA2026092920000), Sep 29, 2026: FLOOR SUPPORT. CORRODED. AFT CARGO BAY FLOOR SUPPORT, FR 52-56, STR38L HAD MULTIPLE SPOTS OF CORROSION. REMOVED AND REPLACED AFT CARGO COMPARTMENT FLOOR SUPPORT IAW SRM 51-41-4.
- [SDR CALA2026092920004](https://openairdocs.org/sdr/CALA2026092920004), Sep 29, 2026: FLOOR SUPPORT. CORRODED. AFT CARGO COMPARTMENT FLOOR BOARD PROFILE AT FR 56-58 STR38L HAS MULTIPLE SPOTS OF CORROSION. REMOVED AND REPLACED AFT CARGO COMPARTMENT FLOOR BOARD PROFILE A T
- [SDR CALA2026101320340](https://openairdocs.org/sdr/CALA2026101320340), Sep 27, 2026: FEEDER CABLE. DAMAGED. DURING ALI VISIT, FOUND RT PYLON IDG FEEDER CABLE WIRE 2422-4519 INSULATION DAMAGED UNDER PANEL 521BT BETWEEN RIB 5A & PS 6480/RIB09 STA MLB. PERFORMED DAMAGE A
- [SDR CALA2026092819919](https://openairdocs.org/sdr/CALA2026092819919), Sep 25, 2026: SKIN. DAMAGED. LEFT TOP & BOTTOM SKIN PANEL FOUND LIQUID ENGRESS INDICATION AT 160" FROM INBD EDGE, AND 9 1/2" FROM T/E. DEFECT IS 2 INCHES IN SIZE. REPAIRED THE LT ELEVATOR T
- [SDR CALA2026092819921](https://openairdocs.org/sdr/CALA2026092819921), Sep 25, 2026: SKIN. DAMAGED. LEFT TOP SKIN PANEL FOUND LIQUID ENGRESS INDICATION AT 146 INCHES FROM INBD EDGE AND 12 1/2 INCHES FROM T/E. DEFECT IS 1 3/4 INCH IN SIZE. REPAIRED THE LT ELEVA
- [SDR CALA2026092519834](https://openairdocs.org/sdr/CALA2026092519834), Sep 24, 2026: PANEL. CORRODED. AFT CARGO COMPARTMENT SLOPING PANEL PROFILE AT FR 54-56, STR 35R HAD MULTIPLE SPOTS OF CORROSION. REMOVED AND REPLACED AFT CARGO SLOPING PANEL PROFILE IAW SRM 5
- [SDR CALA2026092519836](https://openairdocs.org/sdr/CALA2026092519836), Sep 24, 2026: FLOOR SUPPORT. CORRODED. AFT CARGO BAY FLOOR SUPPORT AT FR 59-63, STR 38L HAS MULTIPLE SPOTS OF CORROSION. REMOVED AND REPLACED THE AFT CARGO PROFILE PANEL IAW SRM 51-42-11.
- [SDR CALA2026092519838](https://openairdocs.org/sdr/CALA2026092519838), Sep 24, 2026: FLOORBEAM. DAMAGED. FWD CARGO FLOORBEAM, FR28, STR 38R-38L HAD MULTIPLE ELONGATED HOLES . REMOVED AND REPLACED FLOORBEAM IAW SRM 51-42-11-001A,
- [SDR CALA2026092819854](https://openairdocs.org/sdr/CALA2026092819854), Sep 24, 2026: OIL SYSTEM. LOW. ENG 1 LOW OIL, AFTER ROTATIONIND 4.5 QT AFTER LEVEL OFF 6-8 QT ENGINE 1 FAN COWLS AND THRUST REVERSERS OPENED TO PERFORM VISUAL INSP OF ENGINE. NO LEAKS NOTED. 
- [SDR CALA2026092519805](https://openairdocs.org/sdr/CALA2026092519805), Sep 23, 2026: FITTING. CORRODED. L2 DOOR CUTOUT, AFT CORNER FITTING CORRODED. REMOVED AFT CORNER ON L2 DOOR IAW SRM 51-42-11/001, REV 159, PAR 2.G, 2.F. REPLACED THE AFT CORNER ON L2 DOOR IAW S
- [SDR CALA2026092819868](https://openairdocs.org/sdr/CALA2026092819868), Sep 23, 2026: PROFILE. CORRODED. FWD PIT PROFILE AT FR 27, S38L WAS CORRODED. REMOVED AND REPLACED FWD PIT PROFILE IAW SRM 5 1-42-11.
- [SDR CALA2026092419768](https://openairdocs.org/sdr/CALA2026092419768), Sep 21, 2026: FITTING. CORRODED. FRAME 68 HAS A DRILLED OUT FASTENER WITH CORROSION AROUND IT AFT CABIN. REMOVED AND REPLACED FITTING AT AFT CABIN FLOOR IAW SRM 51-42-11.
- [SDR CALA2026092519801](https://openairdocs.org/sdr/CALA2026092519801), Sep 21, 2026: PANEL. MISSING. FOUND NR 1 PYLON SECTION PANEL MISSING, REF IPC 54-57-22-07A, ITEM 90, DETERMINED TO BE CATEGORY 2 50.75 SQ-IN R & R THE PYLON TO NACELLE PROFILE PANEL INBD IAW
- [SDR CALA2026092219660](https://openairdocs.org/sdr/CALA2026092219660), Sep 19, 2026: PANEL. CRACKED. FWD CARGO LT BOTTOM SLANT FLOOR PROFILE HAD MULTIPLE CRACKS AROUND FASTENER HOLES AT FR 28 +10 IAW AAR LCQ N/R 9298507/26507. REMOVED AND REPLACED FWD CARGO PRO
- [SDR CALA2026092219662](https://openairdocs.org/sdr/CALA2026092219662), Sep 19, 2026: SEAL. CRACKED. RIGHT PYLON FWD INBD BLADE SEAL CRACKED. REMOVED AND REPLACED BLADE SEAL AT RT PYLON FWD INBD IAW SRM 51-42-11.
- [SDR CALA2026092219664](https://openairdocs.org/sdr/CALA2026092219664), Sep 19, 2026: PANEL. CRACKED. FWD CARGO RT BOTTOM SLANT TO FLOOR PROFILE STR 38 HAD A CRACK AT FR 28 +1. REMOVED AND REPLACED PROFILE PANEL ON FWD CARGO BAY IAW SRM 51-42-11-001.
- [SDR CALA2026092219666](https://openairdocs.org/sdr/CALA2026092219666), Sep 19, 2026: FLOORBOARD. CORRODED. AFT CARGO BAY CENTER FLOORBOARD AT FR 51 HAD MULTIPLE SPOTS OF CORROSION. REMOVED AND REPLACED AFT CARGO PROFILE PANEL AT FR57 IAW SRM 51-42-11.
- [SDR CALA2026092219668](https://openairdocs.org/sdr/CALA2026092219668), Sep 19, 2026: FLOORBOARD. CORRODED. AFT CARGO COMPARTMENT FLOORBOARD AT FR 59 - 63, STR 38R HAD MULTIPLE SPOTS OF CORROSION. REMOVED AND REPLACED AFT CARGO FLOORBOARD IAW SRM 51-42-11.
- [SDR CALA2026092219670](https://openairdocs.org/sdr/CALA2026092219670), Sep 19, 2026: FLOORBOARD. CORRODED. AFT CARGO BAY, FLOORBOARD AT FR 51-52, STR 38R HAD MULTIPLE SPOTS OF CORROSION. REMOVED AND REPLACED THE FLOORBOARD IAW SRM 51-42-11.
- [SDR CALA2026092219672](https://openairdocs.org/sdr/CALA2026092219672), Sep 19, 2026: FLOORBOARD. CORRODED. AFT CARGO BAY FLOORBOARD AT FR 52-56, STR 38R HAD MULTIPLE SPOTS OF CORROSION. REMOVED AND REPLACED FLOORBOARD IAW SRM 51-42-11.
- [SDR CALA2026092119613](https://openairdocs.org/sdr/CALA2026092119613), Sep 18, 2026: WIRE HARNESS. FAULTED. NORMAL START ON NUMBER 1 ENGINE. REJECTED TAKEOFF APPROX 60 KNOTS DUE TO NR 1 EGT READING 162 DEGREES. OTHERWISE NORMAL ENGINE INSTRUMENTS AND ACCELERATION NO S
- [SDR CALA2026092119615](https://openairdocs.org/sdr/CALA2026092119615), Sep 18, 2026: PANEL. CORRODED. FWD CARGO SLOPING PANEL VERTICAL PROFILE 10" FWD OF FR30, STR 38R CORRODED. REMOVED AND REPLACED FWD CARGO PROFILE PANEL AT FR 30, STR 38R IAW SRM 51-42-11.
- [SDR CALA2026092119617](https://openairdocs.org/sdr/CALA2026092119617), Sep 18, 2026: SUPPORT. CORRODED. AFT WET AREA, LT FR 69 - 70, SHEAR PLATE SUPPORT CORRODED. REMOVED AND REPLACED SHEAR PLATE SUPPORT ON AFT WET AREA BTW FR 70 -FR 69 LT STR 23 IAW SRM 51-42-11.
- [SDR CALA2026092119626](https://openairdocs.org/sdr/CALA2026092119626), Sep 18, 2026: FRAME. CORRODED. AFT CARGO FR 59 HAD CORROSION AT FASTENER HOLES. PERFORMED PERMANENT A REPAIR AT FR 59 IAW EC/RA 5341-01583.
- [SDR CALA2026101220280](https://openairdocs.org/sdr/CALA2026101220280), Sep 18, 2026: GUSSET. CRACKED. FRAME 66, STRINGER 14R, GUSSET PLATE MIDDLE HOLE IS VISIBLY ELONGATED IN GUSSET PLATE LAYER. THE GUSSET PLATE WAS R & R IAW SRM 53-41-12-300-018, FIGURE 1.
- [SDR CALA2026091819548](https://openairdocs.org/sdr/CALA2026091819548), Sep 17, 2026: DOOR FRAME. CRACKED. RIGHT EMERGENCY EXIT, FWD LOAD TRANSMITTING PROFILE SHOWS SIGNS OF CRACKING. REMOVED & REPLACED THE FRAME SEGMENT IAW SRM 51-72-11-911-001, & SRM 51-42-11-001.
- [SDR CALA2026092219642](https://openairdocs.org/sdr/CALA2026092219642), Sep 17, 2026: SHEAR PLATE. CORRODED. AFT WET AREA, RT FR 69 - 70,SHEAR PLATE CORRODED. REMOVED AND REPLACED SHEAR PLATE IAW SRM 51-42-11/001 AND 5 1-72-11-911-002.
- [SDR CALA2026092219644](https://openairdocs.org/sdr/CALA2026092219644), Sep 17, 2026: DOOR SILL. CORRODED. L2 DOOR SILL HAS CORROSION JUST INBD OF AFT GIRT BAR FITTING. EVALUATED & REPAIRED L-2 DOORSILL JUST INBD OF AFT GIRT BAR FITTING, REPAIR/EVAL FOUND TO BE CATEG
- [SDR CALA2026101220271](https://openairdocs.org/sdr/CALA2026101220271), Sep 17, 2026: GUSSET. CRACKED. FR 66, STR 16L GUSSET PLATE TOP HOLE HA S A REJECTABLE INDICATION. GUSSET PLATE REMOVED AND REPLACED IAW SRM 53-41-12-300-018, FIGURE 1. FLOWCHART SOLUTION 1. G
- [SDR CALA2026101220275](https://openairdocs.org/sdr/CALA2026101220275), Sep 17, 2026: GUSSET. CRACKED. FRAME 68, STRINGER 12R, GUSSET PLATE MIDDLE HOLE IS VISIBLY ELONGATED IN GUSSET PLATE LAYER. GUSSET PLATE R & R IAW SRM 53-41-12-300-018, FIGURE 1.
- [SDR CALA2026101220277](https://openairdocs.org/sdr/CALA2026101220277), Sep 17, 2026: GUSSET. CRACKED. FRAME 68, STRINGER 14L GUSSET PLATE 2ND HOLE FROM BOTTOM IS VISIBLY OUT OF ROUND. THE GUSSET PLATE WAS R & R IAW SRM 53-41-12-300-018, FIGURE 1.
- [SDR CALA2026091719510](https://openairdocs.org/sdr/CALA2026091719510), Sep 13, 2026: FUEL CAP. MISSING. FUEL CAP MISSING, CAP FOUND MISSING UPON ARRIVAL. EWR WAS PREVIOUS STATION THEY DID NOT FIND THE CAP AT THIS TIME. INSTALLED A NEW FUEL CAP IAW AMM 28-25-41-400
- [SDR CALA2026091519458](https://openairdocs.org/sdr/CALA2026091519458), Sep 10, 2026: FUEL CAP. MISSING. PDA 2 FUELER REPORTING FUEL CAP MISSING REPLACED MISSING FUEL CAP P/N 0727540 PER AMM 28-25-41-00 PARTS USED: 31-2825-9-0001,QTY :1 MFG PN ON - 0727540 MFG SN O

All 3,460: https://openairdocs.org/engine/iae-v2522-a5/reports.md

## STCs that may be installed (OpenAirDocs) (1)

Approved for this engine model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has.

- [STC SE1091NE](https://openairdocs.org/stc/SE1091NE): Installation of thrust reverser/exhaust system. Rohr Inc

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