N164HQ
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| REPUBLIC AIRLINES INC | Operator | on 2013-02-24 | Operator named in NTSB report |
Accident & incident history
Operated by Republic Airlines (per NTSB report)
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
41 reports on file, 2009-12-23 – 2015-10-01.
Part: FRAME — DAMAGED (FRM 15) · airframe 13,492 hrs · 8,377 cycles
WHILE ACFT WAS IN FOR HEAVY CHECK, FOUND TOOL DAMAGED, UNDER WATER SUPPLY LINE BRACKET ON FRAME 15, STRINGERS 22-23L. REPAIRED IAW RTD2015-190-092206.
Part: BEAM — CORRODED (CARGO BAY) · corrosion level 2 · airframe 13,492 hrs · 8,377 cycles
DURING HEAVY CHECK, FOUND FWD CARGO LOWER BEAM CORRODED BEHIND AFT FITTING. MAINTENANCE BLENDED IAW ETD2015-190089744.
Part: CASTING — CRACKED (SPOILER ACTUATOR) · airframe 13,492 hrs · 8,377 cycles
WHILE ACFT WAS IN FOR HEAVY CHECK, FOUND LT WING SPOILER NR 3 INBD ACTUATOR CASTING CRACKED. DATS REMOVED DAMAGES SECTION IAW ETD2015-190-095553, TEMPORARY REPAIR UNTILL NEW PART CAN BE PROCURED THEN CASTING WILL BE REPLACED. PN 19129941-401, REPLACEMENT IS ON NON-MEL DMI 443316-2 WITHIN 750 FC.
Part: SEAL REST — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 13,492 hrs · 8,377 cycles
DURING HEAVY CHECK, FOUND FORWARD CARGO DOOR SURROUND, LOWER REINFORING ANGLES, X3 CORRODED. MAINTENANCE R & R ANGLES IAW SRM 51-41-01, AMM 20-10-01 SEAL REST, PN 170-66804-401.
Part: SEAT TRACK — CORRODED (FRAMES 51-56) · corrosion level 2 · airframe 13,492 hrs · 8,377 cycles
WHILE ACFT WAS IN FOR HEAVY CHECK, FOUND RT INBD TRACK FLANGE CORRODED BETWEEN FRAME 51, FRAME 56. MAINTENANCE FOUND BEAM TO BE OUT OF LIMITS, SPLICED BEAM PN PE1156-F2C AT FRAME 51 AND FRAME 54 IAW SRM 53-00-10. REPAIR 51P, AND SRM 51-23-00 REF DATS WP 483, JC 1042 FOR WORK PERFORMED.
Earlier reports · 2009–2014 · 36 reports
2014
Part: DOUBLER — CORRODED (WASTE SERVICE PA) · corrosion level 2 · airframe 11,905 hrs · 7,147 cycles
DURING HEAVY CHECK, WASTE SERVICE BOX DOULBER FRAME 87 INBD FWD CORNER IS CORRODED. MX R & R IAW S/B 190-53-0056. NO FURTHER ACTION REQUIRED.
Part: UPPER SHEET — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,905 hrs · 7,147 cycles
DURING HEAVY CHECK, AFT FUSELAGE LT UPPER SHEET GUSSET FRAME 84-85 IS CORRODED. MX R & R AFT FUSELAGE LT UPPER SHEET GUSSET FRAME 84-85 IAW SRM 51-41-01, 51-43-03. PN 170-86101-001 UPPER SHEET.
Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,905 hrs · 7,147 cycles
DURING HEAVY CHECK, AFT FUSELAGE RT SEAT TRACK EXTENSION BEAM HAS CORROSION. MAINTENANCE R & R AFT FUSELAGE RT SEAT TRACK EXTENSION BEAM IAW SRM 51-40-02, 51-41-01, 51-43-01, PN 170-65669-004, BEAM.
Part: SHEAR PLATE — CORRODED (FRAMES 12-14) · corrosion level 2 · airframe 11,905 hrs · 7,147 cycles
DURING HEAVY CHECK RT FWD WALL SHEAR PLATE AT FRAMES 12-14 IS CORRODED. MAINTENANCE R & R SHEAR PLATE IAW SRM 51-40-02, 51-40-04, 51-41-02, 51-43-04.
Part: SEAT TRACK — CORRODED (FRAMES 12-17) · corrosion level 2 · airframe 11,905 hrs · 7,147 cycles
DURING HEAVY CHECK, RT FWD SEAT TRACK FROM FRAMES 12-17 CORRODED. MX R & R SEAT TRACK IAW SRM 51-41-02, 51-41-02, 51-43-04.
Part: SHEAR PLATE — CORRODED (FRAME 17) · corrosion level 2 · airframe 11,905 hrs · 7,147 cycles
DURING HEAVY CHECK, FOUND CORRODED SHEAR PLATE JUST AFT OF R1 DOOR AT FR STA 17 AGAINST THE WALL. MX R & R SHEAR PLATE IAW CPM 51-25-00-910-001-A.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 11,905 hrs · 71 cycles
DURING HEAVY CHECK, AFT FUSELAGE LT SEAT TRACK EXTENSION BEAM IS CORRODED. MAINTENANCE R & R AFT FUSELAGE LT SEAT TRACK EXTENSION BEAM IAW SRM 51-41-01,51-43-03.
Part: SEAT TRACK — CORRODED (FRAMES 17-19) · corrosion level 2 · airframe 11,905 hrs · 7,147 cycles
DURING HEAVY CHECK, FOUND LT FWD SEAT TRACK CORRODED AT FRAMES 17-19. MX R & R SEAT TRACK IAW SRM 51-41-01, 51-41-02, 51-43-03, 51-43-04, 51-40-02, 51-40-04, 51-43-01, & 51-43-02.
Part: SHEAR PLATE — CORRODED (FRAME 16) · corrosion level 2 · airframe 11,905 hrs · 7,147 cycles
DURING HEAVY CHECK, FWD SHEAR PLATE AT FRAME 16 NEAR L1 DOOR IS CORRODED. MX R & R THE SHEAR PLATE IAW SRM 51-41-02, 51-43-04.
Part: SHEAR WEB — CORRODED (FRAME 16) · corrosion level 2 · airframe 11,905 hrs · 7,147 cycles
DURING HEAVY CHECK, FOUND LT SHEAR WEB CORRODED AT FRAME 16 FROM L1 DOOR TO FWD SEAT TRACK BEAM. MX R & R WITH NEW SHEAR WEB DOUBLER, PN 170-121118-001, LT AT FR 16 IAW SRM 51-40-02, 51-41-02.
Part: SHEAR PLATE — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 11,905 hrs · 7,147 cycles
DURING HEAVY CHECK, AFT FUSELAGE CENTER SHEAR PLATE FRAME 87-88 IS CORRODED. R & R AFT FUSELAGE CENTER SHEAR PLATE IAW SRM 51-42-01, 51-43-01.
Part: FLOOR SUPPORT — CORRODED (FRAMES 88-90) · corrosion level 2 · airframe 11,905 hrs · 7,147 cycles
DURING HEAVY CHECK, FOUND LT AFT OTBD FLOOR SUPPORT AT FRAMES 88 - 90 CORRODED. MX R & R LT AFT OTBD FLOOR SUPPORT IAW SRM 51-41-01, 51-41-02, 51-42-02, & 51-43-03.
Part: SCREW — CORRODED (HARNESS CLAMP) · corrosion level 2 · airframe 11,905 hrs · 7,147 cycles
DURING HEAVY CHECK, HARDWARE ON ADEL CLAMP FOR ELECTRICAL HARNESS CORRODED. MX R & R HARDWARE ON ADEL CLAMP IAW SWPM 20-51-00.
Part: BOLT — CORRODED (ZONE 600) · corrosion level 2 · airframe 11,905 hrs · 7,147 cycles
DURING HEAVY CHECK, RT WING TRACK SUPPORT FORWARD ATTACHMENT TO WING FLAP FAIRING HARDWARE IS CORRODED. MX R & R RT WING TRACK SUPPORT FORWARD ATTACHMENT TO WING FLAP FAIRING HARDWARE IAW AMM 57-54-21.
Part: SHEAR PLATE — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 11,905 hrs · 7,147 cycles
DURING HEAVY CHECK, AFT GALLEY FRAME SHEAR PLATE FRAMES 87-88 HAS CORROSION. MAINTENANCE R & R AFT GALLEY FRAME SHEAR PLATE FRAME, STATION 87-88 IAW SRM 51-42-01, 51-42-02, 51-43-03. PN 170-91919-001 SHEAR PLATE.
Part: DAMPENER — CORRODED (R1 DOOR) · corrosion level 2 · airframe 11,905 hrs · 7,147 cycles
DURING HEAVY CHECK, R1 DOOR DAMPENER ASSY IS CORRODED. MX R & R R1 DOOR DAMPENER ASSY IAW AMM 52-41-27, PN SP-21619A DAMPENER.
Part: DAMPENER — CORRODED (L1 DOOR) · corrosion level 2 · airframe 11,905 hrs · 714 cycles
DURING HEAVY CHECK, L1 DOOR DAMPENER ASSY IS RUSTY AND CORRODED. MX R & R L1 DOOR DAMPENER ASSY PERFORMED DAMPENER ADJUSTMENT IAW AMM 52-11-27, PN SP-21619A DAMPENER.
Part: SUPPORT BRACKET — CRACKED (ZONE 100) · airframe 11,905 hrs · 7,147 cycles
DURING HEAVY CHECK, LT RAM AIR DUCT SUPPORT BRACKET IS CRACKED. MAINTENANCE R & R LT RAM AIR DUCT SUPPORT BRACKET IAW SRM 51-41-01, PN 190-27133-003, SUPPORT.
2013
Part: SLIDE — PARTIAL DEPLOY (L1 DOOR) · airframe 11,014 hrs · 6,485 cycles
CREW REPORTED THE L1 DOOR GIRT BAR WOULD NOT DISARM. FOUND SLIDE PARTIALLY DEPLOYED. REPLACED SLIDE IAW AMM AND OPS CHECKED GOOD.
Part: GRILL — CRACKED (NR 1 PYLON) · airframe 10,465 hrs · 6,022 cycles
WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE REPLACED THE NUMBER ONE ENGINE PYLON INBOARD EXHAUST GRILL. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE ENGINE PYLON INBOARD EXHAUST GRILL IAW EMB ETD2013-190-004333. THE AIRCRAFT WAS RETURNED TO SERVICE 3/14/2013.
Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 10,268 hrs · 5,855 cycles
FIRST OFFICERS FLASHLIGHT WAS INOP. REMOVED AND REPLACED PER EMB AMM.
Part: SPINNER — CRACKED (RT ENGINE) · airframe 10,253 hrs · 5,838 cycles
WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE RIGHT ENGINE SPINNER CRACKED. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE SPINNER IAW GE 34-10E MM 72-00-00 AND SB 72-0201. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.
2012
Part: MOUNT — DAMAGED (COCKPIT) · airframe 9,112 hrs · 4,983 cycles
CREW REPORTED THE CRASH AXE BRACKET WON'T OPEN DUE TO SNAP BEING BROKEN. MAINTENANCE REPLACED CRUSH MOUNT PER EMB AMM.
Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 7,771 hrs · 4,096 cycles
CREW REPORTED 3 EMERGENCY LIGHTS IN CABIN WOULDN'T ILLUMINATE. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY NR 2 PER AMM, OPS CHECK GOOD.
2011
Part: DOOR — LACK OF LUBE (L2) · airframe 7,060 hrs · 3,643 cycles
CREW REPORTED L-2 DOOR DIFFICULT TO ARM. MAINTENANCE INSPECTED AND LUBRICATED L-2 DOOR PER EMB AMM, OPS CHECK GOOD.
Part: DOOR — LACK OF LUBE (L2) · airframe 6,873 hrs · 3,545 cycles
CREW REPORTED L-2 DOOR DIFFICULT TO ARM/DISARM. MAINTENANCE LUBED AND PERFORMED OPS CHECK OF L-2 DOOR PER EMB AMM, OPS CHECK GOOD.
Part: DOOR — DIRTY (L2) · airframe 6,770 hrs · 3,489 cycles
CREW REPORTED L2 DOOR WAS HARD TO OPEN. MAINTENANCE CLEANED AND LUBED DOOR PER EMB AMM, OPS CHECK GOOD.
Part: DOOR — OUT OF ADJUST (CABIN) · airframe 6,636 hrs · 3,420 cycles
CREW REPORTED L2 DOOR HARD TO CLOSE. MAINTENANCE ADJUSTED L2 DOOR AND FLAP PER EMB AMM, OPS CHECK GOOD.
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 5,818 hrs · 2,940 cycles
CREW REPORTED LT EMERGENCY DOOR OPEN MSG DURING CLIMB, NO EMERGENCY DECLARED, LANDED WITHOUT INCIDENT AT MCI. MAINTENANCE PERFORMED OPS CHECK OF LT OWE DOOR PER EMB AMM, OPS CHECK GOOD.
Part: DOOR — UNSECURE (OVERWING EXIT) · airframe 5,502 hrs · 2,778 cycles
CREW REPORTED DOOR EMER LT OPEN MSG ON EICAS IN FLIGHT, FLIGHT CONTINUED ON NORMALLY WITHOUT ANY INCIDENTS, AN EMERGENCY WAS NOT DECLARED. MAINTENANCE RE-SECURED LT OVERWING DOOR PER EMB AMM, OPS CHECK GOOD.
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 5,067 hrs · 2,567 cycles
CREW REPORTED SLAT FAIL ON APPROACH INTO OMA, DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED OPS CHECKS PER EMB AMM, AND COULDN'T DUPLICATE FAULT. A/C WAS THEN RETURNED TO SERVICE.
2010
Part: BATTERY PACK — DISCHARGED (COCKPIT) · airframe 4,193 hrs · 2,129 cycles
CREW REPORTED COCKPIT EMERGENCY LIGHTS WERE NOT WORKING. MX REPLACED BATTERY PACK PER EMB AMM, OPS CHECK GOOD.
Part: ARMING LEVER — BINDS (R2 DOOR) · airframe 6,380 hrs · 4,427 cycles
CREW REPORTED THE R-2 DOOR ARMING LEVER WAS HARD TO OPERATE. MAINTENANCE PERFORMED OPS CHECK OF R-2 DOOR ARMING LEVER PER EMB AMM, AND REPORTED EVERYTHING WAS OPERATING NORMALLY.
Part: LEVER — BINDING (R2 DOOR) · airframe 6,380 hrs · 4,427 cycles
CREW REPORTED THE R-2 DOOR ARMING LEVER WAS HARD TO OPERATE. MAINTENANCE PERFORMED OPS CHECK OF R-2 DOOR ARMING LEVER PER EMB AMM, AND REPORTED EVERYTHING WAS OPERATING NORMALLY.
Part: BATTERY PACK — DISCHARGED (CABIN)
CREW REPORTED OVERWING EXIT LIGHT WAS INOP. MAINTENANCE REMOVED AND REPLACED CABIN BATTERY PACK PER EMB AMM, THE A/C WAS THEN RETURNED TO SERVICE.
2009
Part: DOOR — UNSECURE (LT OVERWING EXIT) · airframe 1,081 hrs · 480 cycles
CREW REPORTED LT OVERWING EXIT INDICATION OPEN IN FLIGHT, RETURNED TO FIELD. NO EMERGENCY WAS DECLARED. MX RE-SECURED O.W.E. PER EMB AMM, A/C WAS RETURNED TO SERVICE.