# SDR SWAA2026072396220

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: July 19, 2026
- Submitted: July 24, 2026
- Operation: Air carrier
- Aircraft: [N291WN](https://openairdocs.org/aircraft/N291WN), registered now
- Make and model: Boeing 737-7H4
- Registry model: [Boeing 737-7H4](https://openairdocs.org/model/boeing-737-7h4) (OpenAirDocs)
- Aircraft serial: 32539
- Aircraft time: 58,109 hours, 33,532 cycles
- Engine: Cfmint CFM567B242
- System (JASC): [7230 · Turbine Engine Compressor Section](https://openairdocs.org/jasc/7230)
- Part: Stator Vane
- Condition: Leaking
- Location: Nr 2 Engine
- Stage of operation: NR
- How discovered: O
- Nature of condition: K
- Precautionary procedure: O
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/SWAA2026072396220

## Discrepancy

OTS-#2 ENGINE FUEL LEAK_ REMOVED AND REPLACED THE ENG 2 RH VSV IAW AMM 75-31-01. PERFORMED POWER PLANT TEST IAW AMM 71-00-00 TEST 3A. IDLE LEAK CHECK FAILED. E 202957 C/W RII OF #2 ENG RH VSV INSTALL PER AMM 75-31-01. TEST 3A IDLE LEAK CHECK FAILED. C/W #2 ENGINE RH VSV ACTUATOR LEAK CHECK IAW AMM 75-31-01-790-801-F00.  NO LEAKS NOTED. FOUND HEAD-END COUPLING NUT LOOSE RESECURED HEAD-END COUPLING NUT AND VERIFIED INSTALLATION OF ROD END COUPLING NUT SHROUDS AND DRAIN MANIFOLDS REF AMM 75-31-01. NO LEAKS NOTED AND OPS TEST GOOD REF AMM 71-00-00 COMPLIED WITH RII INSPECTION OF THE FOLLOWING ON THE #2 ENGINE RH VSV ACTUATOR: TORQUE AND SECURITY OF INSTALLATION OF THE HEAD/ ROD END NIPPLES/ NUTS AND DRAIN MANIFOLD IAW AMM 75-31-01 AND A VSV ACTUATOR LEAK CHECK IAW AMM 75-31-01. PER AMM 71-00-00: TEST 3A IDLE POWER LEAK CHECK PASSED AND TEST 12 ACTUATORS TEST PASSED.

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