REPUBLIC AIRWAYS INC.

Operated by Republic Airways (per NTSB report)

The captain’s decision to continue the landing after the bounce and the subsequent misapplication of pitch controls. Contributing to the accident was the ongoing “land and hold short” operations that may have created an urgency to land.

Operated by Republic Airways Holdings (per NTSB report)

an inadvertent encounter with turbulence.

Part: SKIN — DENTED (ZONE 100) · airframe 6,269 hrs · 4,956 cycles

DENT DAMAGE BETWEEN FR6-FR7 AND STGR23L-STGR24L INSTALLED REPAIR DOUBLER AND FILLER IAW ETD2026-170-014095

Part: SKIN PANEL — DAMAGED (ZONE 600) · airframe 43,535 hrs · 33,126 cycles

WING LEADING EDGE - RH FIXED LE SKIN #4 SLAT TRACK CUTOUT TOP SIDE - CRACK - PERMANENT REPAIR-

Part: POWER SUPPLY — NO TEST (ZONE 200) · airframe 6,238 hrs · 4,935 cycles

DURING A FUNCTIONAL CHECK OF THE EMERGENCY LIGHTS, SOME EMERGENCY LIGHTS FAILED. R&R ELPU 3.

Part: DOUBLER — CRACKED (ZONE 100) · airframe 52,073 hrs · 32,826 cycles

DURING TWO DAY INSPECTION FOUND CRACK UNDER LEFT WING NEAR DOUBLER OF MLG, MAJOR, INSTALLED REPAIR DOUBLER PARTS AND ORIGINAL INTERNAL SPLICE IAW ETD2026-170-013770 AND SRIIM CH51.INSPECTOR VERIFIED INSTALLATION OF REPAIR PARTS AND ORIGINAL INTERNAL SPLICE PER ETD2026-170-013770 AND SRIIM CH51.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 28,538 hrs · 19,663 cycles

COCKPIT FLOOR STRUCTURE UPPER SURFACE HAS AREAS OF LIGHT CORROSION.PERFORMED REPAIR ON LT COCKPIT FLOOR STRUCTURE UPPER SURFACE (LT COCKPIT FLOOR DOUBLER) BETWEEN FR6 - 12 REF SRM 53-10-10/ REPAIR 07P AND SRIIM 51

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 28,538 hrs · 19,663 cycles

COCKPIT FLOOR STRUCTURE UPPER SURFACE RIGHT SIDE HAS AREAS OF LIGHT CORROSION AT AND BETWEEN FRS 10 - 12 PERFORMED REPAIR IAW SRM 53-10-10, REPAIR 07P AND SRIIM CHAPTER 51

Part: SLIDE — PARTIAL DEPLOY (ZONE 800) · airframe 35,856 hrs · 27,298 cycles

R1 DOOR SLIDE PARTIALLY DEPLOYED WHILE OPENING FROM THE OUTSIDE. R & R R1 DOOR SLIDE.

Part: SKIN — DAMAGED (ZONE 600) · airframe 28,007 hrs · 19,147 cycles

RIGHT WING FIXED LEADING EDGE IS DAMAGED BETWEEN RIBS 20-22

Part: PROCESSOR — FAILED (MAU) · airframe 47,124 hrs · 35,544 cycles

AVNX MAU FAIL ON APPROACH. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. R & R NIC PROC 5

Part: SKIN — DENTED (ZONE 300 ELEV) · airframe 13,653 hrs · 12,375 cycles

WHILE PERFORMING HEAVY CHECK FOUND THE HORIZONTAL STABILIZER - RH LOWER SKIN AT RIB 3 AND STRINGER 02L - DENT PERFORMED TEMPORARY REPAIR AS PER ETD2026-170-012588 AND TEMP. NON-MEL-DMI AS PER THE ETD FOR 12 MONTHS

Part: BATTERY — NO TEST (ZONE 200) · airframe 52,326 hrs · 33,668 cycles

DURING RETURN TO SERVICE PROCEDURES FROM A PARKING PROGRAM, AFT RT EMERGENCY LIGHT BATTERY INOPERATIVE. R & R EMERGENCY THE RT AFT EMERGENCY BATTERY.

Part: SKIN — DENTED (ZONE 100) · airframe 31,375 hrs · 21,691 cycles

DENT DAMAGE BETWEEN FR02 AND FR03, STGR 26R AND 28R. INSTALLED REPAIR DOUBLER AND FILLER PER ETD2026-170-13177. REFERENCE NRWC'S VP-035609-2026/1-1, -2,-3, -4, AND -5 FOR WORK PERFORMED

Part: SKIN — CRACKED (ZONE 600) · airframe 35,801 hrs · 27,255 cycles

FOUND CRACK ON RH WING MAIN BOX, LOWER SKIN, INBOARD OF RIB 17. MAJOR REPAIR, MECHANIC PERFORMED REPAIR TO RT WING MAIN BOX IAW WITH ETD2026-170-012770 AND SRIIM CHAPTER 51INSPECTOR PERFORMED RII INSPECTION OF MAJOR REPAIR IAW ETD2026-170-012770 AND SRIIM TASK 51

Part: MAU — FAULTED (ZONE 100) · airframe 44,501 hrs · 29,255 cycles

CARGO FWD SMOKE WILL NOT EXTINGUISH MESSAGE. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. R&R MAU 1 CUSTOM I/O SLOT 13/14. ALL FAULTS CLEARED.

Part: CHECK VALVE — FAULTED (ZONE 100) · airframe 1,825 hrs · 1,402 cycles

IN FLIGHT, GOT 'CABIN ALTITUDE HI' MSG. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. R&R LOW PRESSURE GROUND CONNECTION CHECK VALVE.

Part: REGULATOR VALVE — FAILED (ZONE 400) · airframe 29,677 hrs · 20,435 cycles

BLEED 2 OVERPRESSURE ON DEPARTURE. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. R&R E2 NAPRSOV.

Part: BEAM — CORRODED (ZONE 800) · airframe 51,261 hrs · 32,787 cycles

FWD CARGO DOOR LOWER CENTER BEAM HAS CORROSION. MECHANIC PERFORMED PERMANENT REWORK REPAIR AT FWD CARGO DOOR, LOWER CENTER BEAM, REF.ETD2026-170-012650.

Part: RADOME — DAMAGED (ZONE 100)

DROP IN - DAMAGE TO NOSE AT RADOME. REPLACED FR 1 AND GUTTER SRM 51-40-08 AND COMPLIED WITH ETD2026-170-012441 AND ETD2026-170-012474 FOR PERMANENT REPAIR OF NOSE DAMAGE ON RH SIDE AT RADOME

Part: CONTROL LEVER — FAILED (ZONE 700) · airframe 24,447 hrs · 17,431 cycles

LANDING GEAR STUCK IN DOWN POSITION AFTER TAKEOFF. RETURNED TO DEPARTING AIRPORT, DECLARED EMERGENCY, AND LANDED WITHOUT INCIDENT. R&R LANDING GEAR CONTROL LEVER.

Part: SKIN — DENTED (ZONE 200) · airframe 6,692 hrs · 5,325 cycles

MAJOR REPAIR, DENT ON PREVIOUS ANTENNA DOUBLER AREA CF111 FUSE LT BTWN FR 89-90 AND STGR 10L-11L. MX, DENT WAS REPAIRED IAR EMB ETD2026-170-011924 REV B. SEE AAR NRC 4502648-7000-0017.

Part: BATTERY — NO TEST (ZONE 200) · airframe 50,542 hrs · 32,297 cycles

DURING RETURN TO SERVICE PROCEDURES FROM A PARKING PROGRAM, FWD RT LIGHTS NOT HOLDING A CHARGE. R & R FWD RT EMERGENCY LIGHT BATTERIES.

Part: BATTERY — NO TEST (ZONE 200) · airframe 50,542 hrs · 32,297 cycles

DURING RETURN TO SERVICE PROCEDURES FROM A PARKING PROGRAM, AFT RT LIGHTS NOT HOLDING A CHARGE. R & R AFT RT EMERGENCY LIGHT BATTERIES.

Part: DOOR — GROUND DAMAGE (ZOEN 800) · airframe 39,232 hrs · 28,963 cycles

AIRCRAFT STRUCK BY AIRSTAIRS BELOW L1 DOOR LOWER DOOR AFT CORNER, PERFORMED TRIPLER REPAIR AT FUSLAGE SKIN FR19 AND STGR18L IAW ETD2026-107-012344 REV B

Part: SHEAR TIE — GOUGED (ZONE 200) · corrosion level 2 · airframe 51,261 hrs · 32,787 cycles

SHEAR CLIP GOUGED IN RADIUS AT FR 12 STRS 6R - 7R. FABRICATED AND INSTALLED NEW SHEAR CLIP IAW SRM 51-40-08.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 43,692 hrs · 28,451 cycles

BLEED 2 OVERPRESSURE RIGHT AFTER TAKE OFF. MAX OBSERVED PSI 110. FOLLOWED QRH PROCEDURE. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. PERFORMED EMB FIM TASK 36-11-00-810-812-A AND 36-14-00-810-818-A. NO DEFECTS NOTED. PERFORMED ENGINE PNEUMATIC BLEED SYSTEM OPS CHECK, OPS CHECK GOOD.

Part: SKIN — DAMAGED (ZONE 100) · airframe 51,261 hrs · 32,787 cycles

LIGHTNING STRIKE FWD FUSELAGE BETWEEN FRAMES 3-4 STRINGERS 22R-24R.MECHANIC CUT OUT LIGHTNING STRIKE DAMAGE,FABRICATED, DRILLED AND INSTALLED PERMANENT REINFORCING REPAIR AT FWD FUSELAGE BETWEEN FRAMES 3-4 AND STRINGERS 22R-24R IAW ETD2026-170-012124

Part: SKIN — DAMAGED (ZONE 200) · airframe 51,261 hrs · 32,787 cycles

LIGHTNING STRIKE FWD FUSELAGE BETWEEN FRAMES 11-12 STRINGERS 24R-23R.MECHANIC REMOVED DAMAGE AND PERFORMED PERMANENT REINFORCING REPAIR AT FWD FUSELAGE BETWEEN FRAMES 11-12 STRINGERS 24R-23R IAW ETD2026-170-012519 REV. A

Part: DOUBLER — CORRODED (ZONE 100) · airframe 43,848 hrs · 33,458 cycles

DOUBLER AT FR82-83 STGR28R-29R - LFEC INSPECTION DETECTED POSSIBLE CORROSION IN FASTENERS OR BETWEEN SKIN AND DOUBLER, AS MARKED EXTERNALLY. UPON VISUAL INSPECTION FROM INSIDE AFT CARGO. CORROSION NOTED AROUND ADDITIONAL FASTENERS OF DOUBLER REPAIR.

Part: DOUBLER — DAMAGED (ZONE 100) · airframe 43,848 hrs · 33,458 cycles

FORWARD FUSELAGE - EXTERNAL GPU DOOR MID LATCH BRACKET FASTENER HOLE AND STRUCTURE DAMAGED - PERMANENT REPAIR - PERMANENT COMPOSITE REPAIR

Part: FIRE BOTTLE — FAILED (ZONE 100) · airframe 44,057 hrs · 29,010 cycles

CARGO FIRE SYSTEM FAIL MSG IN FLIGHT. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REMOVED AND REPLACED FWD CARGO FIRE BOTTLE.

Part: CROSSBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 28,725 hrs · 19,791 cycles

AFTER REMOVAL OF DOUBLER , CORROSION WAS FOUND ON FR 84 CROSSBEAM AT OUTBOARD EDGE OF RT INBD SEAT TRACK BEAM. MECHANIC PERFORMED PERMANENT REINFORCING REPAIR TO FR 84 CROSSBEAM AT OUTBOARD EDGE OF RH INBOARD SEAT TRACK. REF ETD2026-170-011708 AND SRIIM CHAPTER 51

Part: CONTROL VALVE — FAULTED (ZONE 700) · airframe 43,913 hrs · 33,087 cycles

BRAKE RT FAULT EICAS MESSAGE DISPLAYED AFTER LANDING GEAR EXTENSION. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. LANDING GEAR NO DISPATCH AFTER LANDING. R & R OTBD MAIN BRAKE CONTROL VALVE.

Part: BCU — FAULTED (ZONE 700) · airframe 43,913 hrs · 33,087 cycles

RIGHT BRAKE FAULT EICAS MSG DISPLAYED ON LANDING GEAR EXTENSION, RAN QRH FOR RH BRK FAULT. LG NO DISPATCH AFTER LANDING. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REPLACED IN NEW BCU #1.

Part: MAU — FAULTED (ZONE 100) · airframe 43,400 hrs · 33,025 cycles

AVNX MAU 3A FAULT WHILE CRUISING AT 23,000 FT. ASSOCIATED AP AND ALT FAIL CAUTION MESSAGES. BOTH FMS NAV FELL OFF PFD. MULTIPLE FLIGHT INSTRUMENTS FAILED. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. PERFORMED POWER RESET FOR 15 MINS. FAULT DID NOT RETURN.

Part: SEAL REST — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,874 hrs · 29,102 cycles

DURING HEAVY CHECK FWD CARGO DOOR CUTOUT CENTER LOWER SEAL REST FOUND WITH CORROSION. REMOVED AND REPLACED SEAL REST IAW EMB 170/175 SRM 51-41-01

Part: SEAL REST — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,874 hrs · 29,102 cycles

DURING HEAVY CHECK FWD CARGO DOOR CUTOUT AFT LOWER SEAL REST FOUND WITH CORROSION. REMOVED AND REPLACED SEAL REST IAW EMB 170/175 SRM 51-41-01

Part: BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,874 hrs · 29,102 cycles

DURING HEAVY CHECK FWD CARGO DOOR CUTOUT LOWER BEAM UNDER DOOR FITTINGS FOUND CORROSION. REMOVED AND REPLACED LOWER BEAM IAW EMB 170/175 SRM 51-41-01

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,874 hrs · 29,102 cycles

DURING HEAVY CHECK CF III RT FLOOR SUPPORT PANEL BETWEEN FR 88-FR 90 RBL 40 FOUND CORRODED. REMOVED AND REPLACED SUPPORT PANEL IAW 170/175 SRM 51-43-03

Part: CROSSBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,874 hrs · 29,102 cycles

DURING HEAVY CHECK CF III FR 84 RBL 30 FOUND CORRODED UPPER FLANGE CROSSBEAM. REPAIRED CROSSBEAM IAW EMB ETD 2026-170-011629 REV. B

Part: CROSSBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,874 hrs · 29,102 cycles

DURING HEAVY CHECK CF III FR 84 RBL 30 FOUND CORRODED UPPER FLANGE CROSSBEAM. REPAIRED CROSSBEAM IAW EMB ETD 2026-170-011629 REV. B

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,874 hrs · 29,102 cycles

DURING HEAVY CHECK FWD FUSELAGE L/H SEAT TRACK BETWEEN FR 12 - FR 20 FOUND WITH SPOTS OF CORROSION. REMOVED AND REPLACED SEAT TRACK IAW EMB 170/175 SRM 51-43-03

Part: SKIN — CRACKED (ZONE 600) · airframe 45,390 hrs · 30,105 cycles

CRACKED LEFT WING FWD WHEEL WELL EDGE AT RIB 3A. PERFORMED DOUBLER REPAIR IAW ETD2026-170-010629-A.

Part: SKIN — CRACKED (ZONE 600) · airframe 39,984 hrs · 30,080 cycles

WING MAIN BOX - RH LOWER SKIN AT SPAR II RIB 4A - CRACK - PERMANENT REINFORCING REPAIR PER ETD2026-170-011524 REV. A

Part: SLAT TRACK — CRACKED (ZONE 500) · airframe 39,874 hrs · 29,102 cycles

DURING HEAVY CHECK LT FIXED LEADING EDGE WING SLAT #2 INBOARD TRACK CUTOUT FOUND WITH CRACK. REPAIRED IAW ETD 2026-170-012048

Part: SLAT TRACK — CRACKED (ZONE 500) · airframe 39,874 hrs · 29,102 cycles

DURING HEAVY CHECK L/H FIXED LEADING EDGE WING SLAT #2 OUTBOARD TRACK CUTOUT FOUND WITH CRACK. REPAIRED IAW EMB ETD 2026-170-012049

Part: SLAT TRACK — CRACKED (ZONE 600) · airframe 39,874 hrs · 29,102 cycles

DURING HEAVY CHECK RT FIXED LEADING EDGE WING SLAT #2 INBOARD TRACK CUTOUT FOUND WITH CRACK. REPAIRED IAW EMB ETD 2026-170-012050

Part: BATTERY — NO TEST (ZONE 100) · airframe 46,833 hrs · 35,232 cycles

EMERGENCY LIGHT BATTERY FAILED FUNCTIONAL CHECK. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY.

Part: POWER SUPPLY — INOPERATIVE (ZONE 200) · airframe 20,090 hrs · 14,506 cycles

CREW REPORTS 2 EMERGENCY LIGHTS INOP. REMOVED AND REPLACED ELPU #2.

Part: DOUBLER — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,874 hrs · 29,102 cycles

DURING HEAVY CHECK CF III WASTE SERVICE PANEL CUTOUT INTERNAL DOUBLER FOUND CORRODED. REMOVED AND REPLACED INTERNAL DOUBLER IAW EMB 170/175 SRM 51-41-02

Part: DOOR — CORRODED (ZONE 800) · corrosion level 2 · airframe 39,874 hrs · 29,102 cycles

DURING HEAVY CHECK WASTE ACCESS DOOR FOUND WITH CORROSION. REMOVED AND REPLACED WASTE ACCESS DOOR IAW EMB 170/175 AMM 53-03-60