20260528006419I

Incident · Minor damage

FAA incident report · Embraer ERJ-170-200SU · Columbus, OH · May 28, 2026

Date: May 28, 2026 · 15:10 local
Place: Columbus, OH
Airport: John Glenn Columbus International
Phase of flight: Landing: Approach
Operating rules: Foreign air carrier (Part 129)
Operator: NZAF
Damage: Minor damage
Aircraft: C-FEKH
Reported as: Embraer ERJ-170-200SU
People aboard: 21
Fatal injuries: 0
Other injuries: 0

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry 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.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

Crew turned base and reduced speed towards 190KTS and pf requested FLAP2. Approximately 10 seconds later, the “flap fail” message appeared on the iecas. Crew determined that the flaps were jammed at 1 and the slats at 3 and that crew would land under these conditions. The remainder of the flight was completed without further issues.

(Resolved on w/o: 962522 taskcard: NR-00002 )

In fim 27-51-00-810-802-A, e. faults isolation procedures step 1 carried out. In step 2, lh&rh flap track fairing 2, 3, 4 removed iaw amm 27-50-00-820-801, subtask 940-022-A (4)(5)(6). Hg 816558

LH flap actuator #2 found with torque limit indicator tripped. Actuator replaced iaw amm task 27-51-01-400-801-A with no faults found. Operational test of the flap control system carried out iaw amm task 27-50-00-710-801-A with no faults found.

As the FAA filed it

CREW TURNED BASE AND REDUCED SPEED TOWARDS 190KTS AND PF REQUESTED FLAP2. APPROXIMATELY 10 SECONDS LATER, THE “FLAP FAIL” MESSAGE APPEARED ON THE IECAS. CREW DETERMINED THAT THE FLAPS WERE JAMMED AT 1 AND THE SLATS AT 3 AND THAT CREW WOULD LAND UNDER THESE CONDITIONS. THE REMAINDER OF THE FLIGHT WAS COMPLETED WITHOUT FURTHER ISSUES.

(RESOLVED ON W/O: 962522 TASKCARD: NR-00002 )

IN FIM 27-51-00-810-802-A, E. FAULTS ISOLATION PROCEDURES STEP 1 CARRIED OUT. IN STEP 2, LH&RH FLAP TRACK FAIRING 2, 3, 4 REMOVED IAW AMM 27-50-00-820-801, SUBTASK 940-022-A (4)(5)(6). HG 816558

LH FLAP ACTUATOR #2 FOUND WITH TORQUE LIMIT INDICATOR TRIPPED. ACTUATOR REPLACED IAW AMM TASK 27-51-01-400-801-A WITH NO FAULTS FOUND. OPERATIONAL TEST OF THE FLAP CONTROL SYSTEM CARRIED OUT IAW AMM TASK 27-50-00-710-801-A WITH NO FAULTS FOUND.