# N175HQ: 2008 Embraer ERJ 190-100 IGW, registration cancelled 2014-06-03

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: June 3, 2014
- Exported to: Mexico
- Status when cancelled: Valid registration
- Airframe: [Embraer ERJ 190-100 IGW](https://openairdocs.org/model/embraer-erj-190-100-igw) (registry code 3260408)
- Engine: [GE CF34-10E6](https://openairdocs.org/engine/ge-cf34-10e6) (registry code 30023)
- Data sheets: [TCDS A57NM](https://openairdocs.org/tcds/A57NM), [TCDS E00070EN](https://openairdocs.org/tcds/E00070EN) (OpenAirDocs)
- Serial number: 19000216
- Year built: 2008
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 10, 2008
- Certificate issued: October 28, 2009
- Last registry action: July 12, 2012
- Mode S code: A12C7E
- Owner when cancelled: [Republic Airline Inc](https://openairdocs.org/faa-owner/REPUBLIC%20AIRLINE%20INC)
- Location: [Indianapolis, IN](https://openairdocs.org/faa-place/IN/Indianapolis)
- Owner type: Corporation
- Owner's area on the map: 39.8974° N, 86.2333° W: Placed by OpenAirDocs at the center of ZIP code 46268, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N175HQ
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=175HQ
- Page: https://openairdocs.org/deregistered/N175HQ-2014-06-03

From the FAA registry file of November 4, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Embraer ERJ 190-100 IGW: https://openairdocs.org/model/embraer-erj-190-100-igw.md

## Service difficulty reports (53, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR R61A201403180398](https://openairdocs.org/sdr/R61A201403180398), Mar 18, 2014: INSERT. CORRODED. DURING HEAVY CHECK, FOUND AFT CARGO CENTER FLOORBOARD HAS SEVERAL POTTED INSERTS WITH CORROSION. MX R & R INSERTS IAW AMM 25-00-23.
- [SDR R61A201403140395](https://openairdocs.org/sdr/R61A201403140395), Mar 14, 2014: BOLT. CORRODED. DURING HEAVY CHECK, L2 SERVICE DOOR LOWER FRAME AFT ESCAPE SLIDE FITTING ASSY HAS 2 BOLTS CORRODED. MX R & R L2 SERVICE DOOR LOWER FRAME AFT ESCAPE SLIDE FITTIN
- [SDR R61A201403130403](https://openairdocs.org/sdr/R61A201403130403), Mar 13, 2014: RUB STRIP. CORRODED. DURING FOR HEAVY CHECK, FOUND RT ENGINE OTBD HALF COWLING FAN ON FWD/AFT METALIC STRIP WORN AND CORRODED. MX R & R RT ENGINE OTBD HALF COWNING FAN ON FWD/AFT ME
- [SDR R61A201403130394](https://openairdocs.org/sdr/R61A201403130394), Mar 13, 2014: SKIN. CORRODED. DURING HEAVY CHECK, CENTER FUSELAGE II LOWER SKIN BETWEEN FRAME 67-73 AND STRINGER 24L-24R ON FIXING FLANGE WING TO FUSELAGE AFT WITH FRETTING CORROSION. MAINTE
- [SDR R61A201403120389](https://openairdocs.org/sdr/R61A201403120389), Mar 12, 2014: SEAL SEAT. CORRODED. DURING HEAVY CHECK, FWD CARGO DOOR CUT OUT LOWER SEAL REST CENTER HAS CORROSION AROUND NUT PLATE. MAINTENANCE R & R FWD CARGO DOOR CUT OUT LOWER SEAL REST CENTE
- [SDR R61A201403120371](https://openairdocs.org/sdr/R61A201403120371), Mar 12, 2014: SEAL SEAT. CORRODED. DURING HEAVY CHECK, FWD CARGO DOOR CUT OUT LOWER SEAL REST CENTER HAS CORROSION AROUND NUTPLATE. MAINTENANCE R & R FWD CARGO DOOR CUT OUT LOWER SEAL REST CENTER
- [SDR R61A201403110388](https://openairdocs.org/sdr/R61A201403110388), Mar 11, 2014: STRUCTURE. CORRODED. DURING HEAVY CHECK, RT FRAME CAP BETWEEN FRAME 84-85 CORRODED. MX R & R RT FRAME CAP IAW SRM 51-41-02.
- [SDR R61A201403110387](https://openairdocs.org/sdr/R61A201403110387), Mar 11, 2014: SILL. CORRODED. DURING HEAVY CHECK, RT SILL AT FRAME 84 IS CORRODED. MX R & R RT SILL IAW SRM 51-40-02, 51-41-02, 51-43-04.
- [SDR R61A201403110372](https://openairdocs.org/sdr/R61A201403110372), Mar 11, 2014: FRAME. CORRODED. DURING HEAVY CHECK, RT FRAME CAP BETWEEN FRAME 84-85 HAS CORROSION. MAINTENANCE R & R RT FRAME CAP BETWEEN FRAME 84-85 IAW SRM 51-41-02. PN 170-86101-001, SHEET
- [SDR R61A201403090393](https://openairdocs.org/sdr/R61A201403090393), Mar 9, 2014: DAMPENER. CORRODED. DURING HEAVY CHECK, L2 DOOR DAMPENER HAS SURFACE CORROSION. MAINTENANCE R & R L2 DOOR DAMPENER IAW AMM 52-12-27.
- [SDR R61A201403090392](https://openairdocs.org/sdr/R61A201403090392), Mar 9, 2014: BOLT. CORRODED. DURING HEAVY CHECK, L1 DOOR GIRT BAR SLIDE ATTACH FITTING BOLTS HAVE CORROSION. MX R & R L1 DOOR GIRT BAR SLIDE ATTACH FITTING BOLTS IAW AMM 2558 52-11-41, PN N
- [SDR R61A201403090386](https://openairdocs.org/sdr/R61A201403090386), Mar 9, 2014: BOLT. CORRODED. DURING HEAVY CHECK, L2 DOOR LOWER EMERGENCY SLIDE MOUNTING HARDWARE IS CORRODED. MAINTENANCE R & R L2 DOOR LOWER EMERGENCY SLIDE MOUNTING HARDWARE IAW AMM 2558 
- [SDR R61A201403090385](https://openairdocs.org/sdr/R61A201403090385), Mar 9, 2014: BOLT. CORRODED. DURING HEAVY CHECK, L1 DOOR LOWER EMERGENCY SLIDE MOUNTING HARDWARE IS CORRODED. MAINTENANCE R & R L1 DOOR LOWER EMERGENCY SLIDE MOUNTING HARDWARE IAW AMM 2558 
- [SDR R61A201403090384](https://openairdocs.org/sdr/R61A201403090384), Mar 9, 2014: BOLT. CORRODED. DURING HEAVY CHECK, R2 DOOR SLIDE GIRT BAR ATTACHING BOLTS ARE CORRODED. MX R & R R2 DOOR SLIDE GIRT BAR ATTACHING BOLTS IAW AMM 2558, AMM 52-42-41.
- [SDR R61A201403090383](https://openairdocs.org/sdr/R61A201403090383), Mar 9, 2014: BOLT. CORRODED. DURING HEAVY CHECK, R1 DOOR GIRT BAR ATTACH FITTING BOLTS ARE CORRODED. MX R & R R1 DOOR GIRT BAR ATTACH FITTING BOLTS IAW EMB 190 2558 52-41-41, PN NAS6604-14,
- [SDR R61A201403090382](https://openairdocs.org/sdr/R61A201403090382), Mar 9, 2014: BOLT. CORRODED. DURING HEAVY CHECK, L2 DOOR GIRT BAR ATTACH FITTING BOLTS ARE CORRODED. MX R & R L2 DOOR GIRT BAR ATTACH FITTING BOLTS IAW AMM 2558 52-12-41.
- [SDR R61A201403090381](https://openairdocs.org/sdr/R61A201403090381), Mar 9, 2014: BOLT. CORRODED. DURING HEAVY CHECK, L2 DOOR GIRT BAR ATTACH FITTING BOLTS ARE CORRODED. MX R & R L2 DOOR GIRT BAR ATTACH FITTING BOLTS IAW AMM 2558 52-12-41, PN NAS6604-14, BOL
- [SDR R61A201403080369](https://openairdocs.org/sdr/R61A201403080369), Mar 8, 2014: SPLICE. CORRODED. DURING HEAVY CHECK, RT GUSS PLATE, RT CENTER GUSS PLATE, FRAME 90 HAS CORROSION. MX R & R RT GUSS PLATE, RT CENTER GUSS PLATE, FRAME 90 IAW SRM 51-41-02, 51-43-
- [SDR R61A201403080368](https://openairdocs.org/sdr/R61A201403080368), Mar 8, 2014: PANEL. CORRODED. DURING HEAVY CHECK, LEFT SUPPORT PANEL BETWEEN FRAMES 89-90 CROSS FRAMES HAS CORROSION. MX R & R PANEL IAW SRM 51-41-01, 51-42-02, 51-42-02,51-43-03.
- [SDR R61A201403080367](https://openairdocs.org/sdr/R61A201403080367), Mar 8, 2014: FLOORBEAM. CORRODED. DURING HEAVY CHECK, LT SIDE OF THE FRAME 88 FLOORBEAM HAS CORROSION. MX R & R IAW SRM 1-43-04.
- [SDR R61A201403070370](https://openairdocs.org/sdr/R61A201403070370), Mar 7, 2014: BRACKET. CRACKED. DURING HEAVY CHECK, STEERING MANIFOLD BRACKET IS CRACKED IN 3 OF 4 RADIUS. MAINTENANCE R & R STEERING MANIFOLD BRACKET IAW SRM 51-42-02, P/N 170-10788-401 BRACK
- [SDR R61A201403060381](https://openairdocs.org/sdr/R61A201403060381), Mar 6, 2014: PAN. CRACKED. DURING HEAVY CHECK, SEAT PAN 26F IS CRACKED. MAINTENANCE R & R SEAT PAN 26F IAW SRM 51-42-00, PN 41191032-8, SEAT PAN.
- [SDR R61A201312041295](https://openairdocs.org/sdr/R61A201312041295), Dec 4, 2013: DOOR. OUT OF ADJUST. CREW REPORTED THAT THE L2 DOOR IS HARD TO CLOSE. MAINTENANCE ADJUSTED THE L2 DOOR SUPPORT ARMS IAW AMM AND OPS CHECKED GOOD. ACFT IS GOOD FOR SERVICE.
- [SDR R61A201307150608](https://openairdocs.org/sdr/R61A201307150608), Jul 15, 2013: BOTTLE. LOW PRESSURE. CREW REPORTED THE L2 DOOR SLIDE PRESSURE IS LOW. ON CALL MX CONFIRMED THE L2 DOOR SLIDE DISCHARGE BOTTLE IS LOW AT 500 POUNDS. ACFT WAS FLOWN VIA MX FERRY TO PI
- [SDR R61A201305120458](https://openairdocs.org/sdr/R61A201305120458), May 12, 2013: INDICATOR. OUT OF ADJUST. CREW REPORTED THAT THE R1 DOOR RED ARMED INDICATION IS PARTIALLY IN VIEW. MAINTENANCE ADJUSTED R1 DOOR INDICATION PER EMB AMM 52-41-00. OPS CHECKED GOOD.
- [SDR R61A201212020690](https://openairdocs.org/sdr/R61A201212020690), Dec 2, 2012: SKIN. DENTED. AIRCRAFT WAS OUT OF SERVICE FOR MAJOR REPAIR LEFT FORWARD FUSELAGE SKIN REPLACEMENT, RVSM AREA ADSP NUMBER ONE. MAINTENANCE REMOVED AND REPLACED FF LOWER SKIN P
- [SDR R61A201211230688](https://openairdocs.org/sdr/R61A201211230688), Nov 23, 2012: FITTING. DAMAGED. WHILE AIRCRAFT WAS OUT OF SERVICE AND IN REPAIR, MAINTENANCE FOUND SHEAR CLIP BELOW STRINGER 22R ON FRAME 3 HAS TOOLING MARKS. MAINTENANCE REMOVED AND REPLACED 
- [SDR R61A201211230689](https://openairdocs.org/sdr/R61A201211230689), Nov 23, 2012: FRAME. DAMAGED. WHILE AIRCRAFT WAS OUT OF SERVICE AND DURING ACCOMPLISHMENT OF A REPAIR, MAINTENANCE MISDRILLED RIVET HOLE IN FRAME 1, 5TH HOLE OUTBOARD OF STRINGER 28R. MAINTE
- [SDR R61A201211220676](https://openairdocs.org/sdr/R61A201211220676), Nov 22, 2012: VENT. CRACKED. WHILE AIRCRAFT WAS OUT OF SERVICE IN CMH MAINTENANCE WORKED DEFERRED MAINTENANCE ITEM NUMBER TWO ENGINE OUTBOARD AFT PYLON VENT IS CRACKED. MAINTENANCE REMOVED 
- [SDR R61A201211220675](https://openairdocs.org/sdr/R61A201211220675), Nov 22, 2012: HEAT SHIELD. CRACKED. WHILE AIRCRAFT WAS OUT OF SERVICE IN CMH MAINTENANCE WORKED DEFERRED MAINTENANCE ITEM NUMBER TWO ENGINE PYLON HEAT SHIELD AFT INBOARD GRILL CRACKED. MAINTENANCE
- [SDR R61A201211220674](https://openairdocs.org/sdr/R61A201211220674), Nov 22, 2012: HEAT SHIELD. CRACKED. WHILE AIRCRAFT WAS OUT OF SERVICE CMH MAINTENANCE WORKED DEFERRED MAINTENANCE ITEM, NUMBER ONE ENGINE PYLON HEAT SHIELD AFT INBOARD GRILL SKIN CRACKED. MAINTENA
- [SDR R61A201207100373](https://openairdocs.org/sdr/R61A201207100373), Jul 10, 2012: SEAT TRACK. CORRODED. WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE RIGHT FORWARD FUSELAGE SEAT TRACK CORRODED FROM FRAME 13 TO 20. MAINTENANCE REMOVED AND REPLACED THE RIG
- [SDR R61A201207100356](https://openairdocs.org/sdr/R61A201207100356), Jul 10, 2012: PLATE. CORRODED. WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE FORWARD RIGHT SILL PLATE AT DOOR R1 CORRODED. MAINTENANCE REMOVED AND REPLACED THE FORWARD RIGHT SILL PL
- [SDR R61A201207060372](https://openairdocs.org/sdr/R61A201207060372), Jul 6, 2012: PIN. CORRODED. WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND CORROSION AROUND THE BOLT HOLES FOR THE LEFT MAIN GEAR FORWARD PINTLE PIN. MAINTENANCE REMOVED AND REPLACED 
- [SDR R61A201207050344](https://openairdocs.org/sdr/R61A201207050344), Jul 5, 2012: DAMPER. CORRODED. WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE L1 DOOR DAMPER HAS CORROSION. MAINTENANCE REMOVED AND REPLACED THE L1 DOOR DAMPER IAW EMB 190 AMM 52-11-
- [SDR R61A201207040345](https://openairdocs.org/sdr/R61A201207040345), Jul 4, 2012: DAMPER. CORRODED. WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE R1 DOOR DAMPER CORRODED. MAINTENANCE REMOVED AND REPLACED THE R1 DOOR DAMPER IAW EMB 190 AMM 52-41-27. T
- [SDR R61A201207040339](https://openairdocs.org/sdr/R61A201207040339), Jul 4, 2012: SHEAR PLATE. CORRODED. WHILE AIRCRAFT WAS IN FOR HEAVY CHECK, LEVEL 2 CORROSION WAS FOUND ON THE LEFT SHEAR PLATE BETWEEN FRAME 87 & 88, IN AFT LAV AREA. MAINTENANCE REMOVED AND REPLA
- [SDR R61A201207030360](https://openairdocs.org/sdr/R61A201207030360), Jul 3, 2012: SKIN PANEL. DENTED. WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE WORKED DMI 344190/1 TICKET/CONTROL#06429, DENT ON LEFT FORWARD FUSELAGE BY ADSP NR 1. MAINTENANCE REMOVED DAMAGED 
- [SDR R61A201207030341](https://openairdocs.org/sdr/R61A201207030341), Jul 3, 2012: GUSSET. CORRODED. WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE RIGHT GUSSET AT FRAME 90 OUTBOARD SIDE CORRODED. MAINTENANCE REMOVED AND REPLACED THE RIGHT GUSSET AT FR
- [SDR R61A201207030338](https://openairdocs.org/sdr/R61A201207030338), Jul 3, 2012: STRUCTURE. CORRODED. WHILE AIRCRAFT WAS IN FOR HEAVY CHECK, LEVEL 2 CORROSION WAS FOUND ON THE LEFT UPPER SHEET AT FRAME 85 TO 86. MAINTENANCE REMOVED AND REPLACED THE LEFT UPPER SH
- [SDR R61A201207030337](https://openairdocs.org/sdr/R61A201207030337), Jul 3, 2012: GUSSET. CORRODED. WHILE AIRCRAFT WAS IN FOR HEAVY CHECK, LEVEL 2 CORROSION WAS FOUND ON THE LEFT & RIGHT GUSSETS AT FRAME 90. MAINTENANCE REMOVED AND REPLACED BOTH LEFT & RIGHT G
- [SDR R61A201207030336](https://openairdocs.org/sdr/R61A201207030336), Jul 3, 2012: PANEL. CORRODED. WHILE AIRCRAFT WAS IN FOR HEAVY CHECK, LEVEL 2 CORROSION WAS FOUND ON THE RIGHT SHEAR PANEL AT FRAME 87R TO 88R. MAINTENANCE REMOVED AND REPLACED RIGHT SHEAR PA
- [SDR R61A201207030335](https://openairdocs.org/sdr/R61A201207030335), Jul 3, 2012: STRUCTURE. CORRODED. WHILE AIRCRAFT WAS IN FOR HEAVY CHECK, LEVEL 2 CORROSION WAS FOUND ON THE RIGHT UPPER SHEET AT FRAME 85R TO 86R ON THE UPPER SURFACE. MAINTENANCE REMOVED AND RE
- [SDR R61A201207030334](https://openairdocs.org/sdr/R61A201207030334), Jul 3, 2012: SEAT TRACK. CORRODED. WHILE AIRCRAFT WAS IN FOR HEAVY CHECK, LEVEL 2 CORROSION WAS FOUND ON THE RIGHT SEAT TRACK UPPER SERVICE AT FRAME 87. MAINTENANCE REMOVED AND REPLACED THE RIGHT
- [SDR R61A201207030333](https://openairdocs.org/sdr/R61A201207030333), Jul 3, 2012: PANEL. CORRODED. WHILE AIRCRAFT WAS IN FOR HEAVY CHECK, LEVEL 2 CORROSION WAS FOUND ON FLOORBEAM LOCATED IN AFT GALLEY WET AREA. MAINTENANCE REMOVED AND REPLACED THE LEFT FLOORB
- [SDR R61A201207030332](https://openairdocs.org/sdr/R61A201207030332), Jul 3, 2012: FLOORBEAM. CORRODED. WHILE AIRCRAFT WAS IN FOR HEAVY CHECK, LEVEL 2 CORROSION WAS FOUND ON FLOORBEAM LOCATED IN AFT GALLEY WET AREA. MAINTENANCE REMOVED AND REPLACED THE LT FLOORBEA
- [SDR R61A201207030329](https://openairdocs.org/sdr/R61A201207030329), Jul 3, 2012: BRACKET. CRACKED. WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE BRACKET ON FLOORBEAM UNDER PANEL 251HLF, AFT GALLEY AT L2 DOOR LOCATION CRACKED. MAINTENANCE REMOVED AND
- [SDR R61A20110221](https://openairdocs.org/sdr/R61A20110221), Aug 16, 2011: UNKNOWN. MALFUNCTIONED. CREW REPORTED L-1 DOOR WAS DIFFICULT TO ARM/DISARM. MAINTENANCE PERFORMED FUNCTIONAL CHECK OF L-1 DOOR PER EMB AMM, AND REPORTED NO DISCREPANCIES WERE FOUND.
- [SDR R61A20110137](https://openairdocs.org/sdr/R61A20110137), Jun 6, 2011: DOOR. BINDS. CREW REPORTED L-1 DOOR WAS DIFFICULT TO OPEN FROM THE OUTSIDE. MAINTENANCE PERFORMED OPS TEST OF L-1 DOOR PER EMB AMM, OPS CHECK GOOD.
- [SDR R61A20110041](https://openairdocs.org/sdr/R61A20110041), Feb 16, 2011: GIRT BAR. OUT OF ADJUST. MAINTENANCE REPORTED L1 DOOR SLIDE WILL NOT ARM. MX ADJUSTED L1 GIRT BAR IAW EMB AMM, OPS CHECK GOOD.

All 53: https://openairdocs.org/deregistered/N175HQ-2014-06-03/reports.md

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