N175HQ

No registry detail on file · not in current registry

Operators of this aircraft

Who operated this tail, and how firmly we know it.

No operator established for this aircraft.

Accident & incident history

No NTSB accidents or incidents on file for this aircraft.

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.

53 reports on file, 2010-06-10 – 2014-03-18.

OTHER · 2014-03-18 Matched by certificate designator
ATA 5321

Part: INSERT — CORRODED (FLOORBOARD) · corrosion level 2 · airframe 13,387 hrs · 8,833 cycles

DURING HEAVY CHECK, FOUND AFT CARGO CENTER FLOORBOARD HAS SEVERAL POTTED INSERTS WITH CORROSION. MX R & R INSERTS IAW AMM 25-00-23.

Source: SDR R61A201403180398
OTHER · 2014-03-14 Matched by certificate designator
ATA 2565

Part: BOLT — CORRODED (ESCAPE SLIDE) · corrosion level 2 · airframe 13,388 hrs · 8,833 cycles

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 FITTING ASSY TWO BOLTS IAW AMM 2558 53-23-21, PN NAS6603-10, BOLT.

Source: SDR R61A201403140395
OTHER · 2014-03-13 Matched by certificate designator
ATA 5330

Part: SKIN — CORRODED (FRAMES 67-73) · airframe 13,388 hrs · 8,833 cycles

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. MAINTENANCE REPRIMED FUSELAGE II LOWER SKIN BETWEEN FRAME 67-73 AND STRINGER 24L-24R ON FIXING FLANGE WING TO FUSELAGE AFT IAW SRM 51-23-04.

Source: SDR R61A201403130394
OTHER · 2014-03-13 Matched by certificate designator
ATA 5420

Part: RUB STRIP — CORRODED (RT NACELLE) · corrosion level 2 · airframe 13,387 hrs · 8,833 cycles

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 METALIC STRIP, PN 341-2221-503, AMM 71-11-02.

Source: SDR R61A201403130403
OTHER · 2014-03-12 Matched by certificate designator
ATA 5320

Part: SEAL SEAT — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,388 hrs · 8,833 cycles

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 IAW SRM 51-41-01. MAJOR REPAIR.

Source: SDR R61A201403120371
OTHER · 2014-03-12 Matched by certificate designator
ATA 2530

Part: SEAL SEAT — CORRODED (ZONE 800) · corrosion level 2 · airframe 13,388 hrs · 8,833 cycles

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 CENTER IAW SRM 51-41-01. MAJOR REPAIR.

Source: SDR R61A201403120389
OTHER · 2014-03-11 Matched by certificate designator
ATA 5320

Part: STRUCTURE — CORRODED (FRAMES 84-85) · corrosion level 2 · airframe 13,388 hrs · 8,833 cycles

DURING HEAVY CHECK, RT FRAME CAP BETWEEN FRAME 84-85 CORRODED. MX R & R RT FRAME CAP IAW SRM 51-41-02.

Source: SDR R61A201403110388
OTHER · 2014-03-11 Matched by certificate designator
ATA 5311

Part: FRAME — CORRODED (ZONE 200) · corrosion level 2 · airframe 13,388 hrs · 8,833 cycles

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.

Source: SDR R61A201403110372
OTHER · 2014-03-11 Matched by certificate designator
ATA 5320

Part: SILL — CORRODED (FRAME 84) · corrosion level 2 · airframe 13,388 hrs · 8,833 cycles

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.

Source: SDR R61A201403110387
OTHER · 2014-03-09 Matched by certificate designator
ATA 2560

Part: BOLT — CORRODED (GIRT BAR) · corrosion level 2 · airframe 13,388 hrs · 8,833 cycles

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, BOLT.

Source: SDR R61A201403090381
OTHER · 2014-03-09 Matched by certificate designator
ATA 2560

Part: BOLT — CORRODED (L1 DOOR GIRT BAR) · corrosion level 2 · airframe 13,388 hrs · 8,833 cycles

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 NAS6604-14, BOLT.

Source: SDR R61A201403090392
OTHER · 2014-03-09 Matched by certificate designator
ATA 2560

Part: BOLT — CORRODED (R1 GIRT BAR) · corrosion level 2 · airframe 13,388 hrs · 8,833 cycles

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, BOLT.

Source: SDR R61A201403090383
OTHER · 2014-03-09 Matched by certificate designator
ATA 5210

Part: DAMPENER — CORRODED (L2 DOOR) · corrosion level 2 · airframe 13,388 hrs · 8,833 cycles

DURING HEAVY CHECK, L2 DOOR DAMPENER HAS SURFACE CORROSION. MAINTENANCE R & R L2 DOOR DAMPENER IAW AMM 52-12-27.

Source: SDR R61A201403090393
OTHER · 2014-03-09 Matched by certificate designator
ATA 2560

Part: BOLT — CORRODED (R2 GIRT BAR) · corrosion level 2 · airframe 13,388 hrs · 8,833 cycles

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.

Source: SDR R61A201403090384
OTHER · 2014-03-09 Matched by certificate designator
ATA 2565

Part: BOLT — CORRODED (L2 DOOR SLIDE) · corrosion level 2 · airframe 13,388 hrs · 8,833 cycles

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 52-12-40.

Source: SDR R61A201403090386
OTHER · 2014-03-09 Matched by certificate designator
ATA 2565

Part: BOLT — CORRODED (L1 DOOR SLIDE) · corrosion level 2 · airframe 13,388 hrs · 8,833 cycles

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 52-11-40.

Source: SDR R61A201403090385
OTHER · 2014-03-09 Matched by certificate designator
ATA 2560

Part: BOLT — CORRODED (L2 DOOR GIRT BAR) · corrosion level 2 · airframe 13,388 hrs · 8,833 cycles

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.

Source: SDR R61A201403090382
OTHER · 2014-03-08 Matched by certificate designator
ATA 5320

Part: SPLICE — CORRODED (FRAME 90) · corrosion level 2 · airframe 13,388 hrs · 8,833 cycles

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, 51-43-03, PN 170-86119-005 SPLICE, 170-60259-001 GUSS PLATE.

Source: SDR R61A201403080369
OTHER · 2014-03-08 Matched by certificate designator
ATA 5315

Part: FLOORBEAM — CORRODED (FRAME 88) · corrosion level 2 · airframe 13,388 hrs · 8,833 cycles

DURING HEAVY CHECK, LT SIDE OF THE FRAME 88 FLOORBEAM HAS CORROSION. MX R & R IAW SRM 1-43-04.

Source: SDR R61A201403080367
OTHER · 2014-03-08 Matched by certificate designator
ATA 5320

Part: PANEL — CORRODED (FRAMES 89-90) · corrosion level 2 · airframe 13,388 hrs · 8,833 cycles

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.

Source: SDR R61A201403080368
OTHER · 2014-03-07 Matched by certificate designator
ATA 5340

Part: BRACKET — CRACKED (FUSELAGE) · airframe 13,388 hrs · 8,833 cycles

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 BRACKET.

Source: SDR R61A201403070370
OTHER · 2014-03-06 Matched by certificate designator
ATA 2520

Part: PAN — CRACKED (SEAT 26F) · airframe 13,388 hrs · 8,833 cycles

DURING HEAVY CHECK, SEAT PAN 26F IS CRACKED. MAINTENANCE R & R SEAT PAN 26F IAW SRM 51-42-00, PN 41191032-8, SEAT PAN.

Source: SDR R61A201403060381
Earlier reports · 2010–2013 · 31 reports

2013

OTHER · 2013-12-04 Matched by certificate designator
ATA 5210

Part: DOOR — OUT OF ADJUST (L2 DOOR) · airframe 12,994 hrs · 8,588 cycles

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.

Source: SDR R61A201312041295
OTHER · 2013-07-15 Matched by certificate designator
ATA 2565

Part: BOTTLE — LOW PRESSURE (L2 DOOR SLIDE) · airframe 12,363 hrs · 8,270 cycles

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 PIT WHERE THE L2 DOOR EMERGENCY SLIDE WAS R & R IAW AMM. OPS CHECKED GOOD.

Source: SDR R61A201307150608
OTHER · 2013-05-12 Matched by certificate designator
ATA 5240

Part: INDICATOR — OUT OF ADJUST (R1 DOOR) · airframe 12,115 hrs · 8,121 cycles

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.

Source: SDR R61A201305120458

2012

OTHER · 2012-12-02 Matched by certificate designator
ATA 5330

Part: SKIN — DENTED (FUSELAGE) · airframe 10,974 hrs · 7,390 cycles

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 PANEL IAW EMB 190 SRM 51-40-02, 51-40-04, AND 51-41-02. (MAJOR REPAIR) THE AIRCRAFT IS OUT OF SERVICE IN CMH.

Source: SDR R61A201212020690
OTHER · 2012-11-23 Matched by certificate designator
ATA 5311

Part: FRAME — DAMAGED (FUSELAGE) · airframe 10,974 hrs · 7,390 cycles

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. MAINTENANCE REPAIRED MISDRILLED HOLE IAW ETD 2012-190-017046. (MAJOR REPAIR) THE AIRCRAFT IS OUT OF SERVICE IN CMH.

Source: SDR R61A201211230689
OTHER · 2012-11-23 Matched by certificate designator
ATA 5320

Part: FITTING — DAMAGED (FUSELAGE) · airframe 10,974 hrs · 7,390 cycles

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 THE SHEAR CLIP BELOW STRINGER 22R FRAME 3 IAW EMB 190 SRM 51-40-02, AND 51-41-01. (MAJOR REPAIR)

Source: SDR R61A201211230688
OTHER · 2012-11-22 Matched by certificate designator
ATA 5420

Part: VENT — CRACKED (NR 2 PYLON) · airframe 10,974 hrs · 7,390 cycles

WHILE AIRCRAFT WAS OUT OF SERVICE IN CMH MAINTENANCE WORKED DEFERRED MAINTENANCE ITEM NUMBER TWO ENGINE OUTBOARD AFT PYLON VENT IS CRACKED. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO ENGINE OUTBOARD AFT PYLON VENT IAW ETD 2012-190-017052. THE AIRCRAFT IS OUT OF SERVICE IN CMH.

Source: SDR R61A201211220676
OTHER · 2012-11-22 Matched by certificate designator
ATA 5412

Part: HEAT SHIELD — CRACKED (NR 2 PYLON) · airframe 10,974 hrs · 7,390 cycles

WHILE AIRCRAFT WAS OUT OF SERVICE IN CMH MAINTENANCE WORKED DEFERRED MAINTENANCE ITEM NUMBER TWO ENGINE PYLON HEAT SHIELD AFT INBOARD GRILL CRACKED. MAINTENANCE REMOVED AND REPLACED THE NUMBER 2 ENGINE PYLON HEAT SHIELD AFT INBOARD GRILL IAW ETD 2012-190-011983-A REV A. THE AIRCRAFT IS OUT OF SERVICE IN CMH.

Source: SDR R61A201211220675
OTHER · 2012-11-22 Matched by certificate designator
ATA 5412

Part: HEAT SHIELD — CRACKED (NR 1 PLYON) · airframe 10,975 hrs · 7,390 cycles

WHILE AIRCRAFT WAS OUT OF SERVICE CMH MAINTENANCE WORKED DEFERRED MAINTENANCE ITEM, NUMBER ONE ENGINE PYLON HEAT SHIELD AFT INBOARD GRILL SKIN CRACKED. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE ENGINE AFT INBOARD HEAT SHIELD GRILL IAW ETD 2012-190-011983-A REV A. THE AIRCRAFT REMAINS OUT OF SERVICE IN CMH.

Source: SDR R61A201211220674
OTHER · 2012-07-10 Matched by certificate designator
ATA 5320

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,161 hrs · 6,783 cycles

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 PLATE AT DOOR R1 IAW EMB 190 SRM 51-40-02, 51-43-02, 51-41-02, AND 51-43-02. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.

Source: SDR R61A201207100356
OTHER · 2012-07-10 Matched by certificate designator
ATA 5347

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,161 hrs · 6,783 cycles

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 RIGHT FORWARD SEAT TRACK IAW EMB 190 SRM 51-43-01, 51-40-02, 51-43-02. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.

Source: SDR R61A201207100373
OTHER · 2012-07-06 Matched by certificate designator
ATA 3211

Part: PIN — CORRODED (LT MLG) · corrosion level 2 · airframe 10,161 hrs · 6,783 cycles

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 THE LEFT MAIN LANDING GEAR FORWARD PINTLE PIN IAW EMB 190 AMM 32-11-01. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.

Source: SDR R61A201207060372
OTHER · 2012-07-05 Matched by certificate designator
ATA 5210

Part: DAMPER — CORRODED (L1 DOOR) · corrosion level 2 · airframe 10,161 hrs · 6,783 cycles

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 52-11-27. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.

Source: SDR R61A201207050344
OTHER · 2012-07-04 Matched by certificate designator
ATA 5240

Part: DAMPER — CORRODED (R1 DOOR) · corrosion level 2 · airframe 10,161 hrs · 6,783 cycles

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. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.

Source: SDR R61A201207040345
OTHER · 2012-07-04 Matched by certificate designator
ATA 5320

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,161 hrs · 6,783 cycles

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 REPLACED THE LEFT SHEAR PLATE AT FRAME 87 TO 88 IAW EMB 190 SRM 51-42-01. AIRCRAFT IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Source: SDR R61A201207040339
OTHER · 2012-07-03 Matched by certificate designator
ATA 5320

Part: BRACKET — CRACKED (FUSELAGE) · airframe 10,161 hrs · 6,783 cycles

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 REPLACED CRACKED BRACKET LOCATED UNDER PANEL 251HLF IAW EMB SRM 51-40-02, AND 51-41-01. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.

Source: SDR R61A201207030329
OTHER · 2012-07-03 Matched by certificate designator
ATA 5320

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,161 hrs · 6,783 cycles

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 PANEL IAW EMB 190 SRM 51-40-02 AND 51-42-00. AIRCRAFT IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Source: SDR R61A201207030336
OTHER · 2012-07-03 Matched by certificate designator
ATA 5347

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,161 hrs · 6,783 cycles

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 SEAT TRACK AT FRAME 87 IAW EMB 190 SRM 51-40-02, 51-41-01 & 51-43-03. AIRCRAFT IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Source: SDR R61A201207030334
OTHER · 2012-07-03 Matched by certificate designator
ATA 5320

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,161 hrs · 6,783 cycles

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 GUSSETS (SAME P/N'S 170-60257-001) AT FRAME 90 IAW EMB 190 SRM 51-41-02, 51-40-02, 51-40-04 & 51-21-01. AIRCRAFT IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Source: SDR R61A201207030337
OTHER · 2012-07-03 Matched by certificate designator
ATA 5320

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,161 hrs · 6,783 cycles

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 REPLACED THE RIGHT UPPER SHEET IAW EMB 190 SRM 51-41-00, 51-40-02 & 51-43-01. AIRCRAFT IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Source: SDR R61A201207030335
OTHER · 2012-07-03 Matched by certificate designator
ATA 5320

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,161 hrs · 6,783 cycles

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 FRAME 90 OUTBOARD SIDE IAW EMB 190 SRM 51-41-02, 51-40-02, 51-21-01, AND 51-41-02. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.

Source: SDR R61A201207030341
OTHER · 2012-07-03 Matched by certificate designator
ATA 5330

Part: SKIN PANEL — DENTED (FUSELAGE) · airframe 10,161 hrs · 6,783 cycles

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 AREA BY CUTOUT IAW ETD 2012-190-009748. MAINTENANCE INSTALLED FABRICATED DOUBLER AND FILLER IAW ETD 2012-190-009748. FABRICATED DOUBLER FROM 2024T3, AND FILLER FROM 2024T3. THIS IS CLASSIFIED AS A MAJOR REPAIR. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.

Source: SDR R61A201207030360
OTHER · 2012-07-03 Matched by certificate designator
ATA 5320

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,161 hrs · 6,783 cycles

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 SHEET IAW EMB 190 SRM 51-40-02, 51-41-00 & 51-43-01. AIRCRAFT IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Source: SDR R61A201207030338
OTHER · 2012-07-03 Matched by certificate designator
ATA 5320

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,161 hrs · 6,783 cycles

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 FLOORBEAM AND CENTER SHEAR PLATE IAW EMB 190 SRM 51-40-02, 51-41-01, 51-43-01 AND 51-42-00. REF P/N'S 170-65669-003 (BEAM) & 170-65928-001 (SHEAR PANEL). AIRCRAFT IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Source: SDR R61A201207030333
OTHER · 2012-07-03 Matched by certificate designator
ATA 5315

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,161 hrs · 6,783 cycles

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 FLOORBEAM AND CENTER SHEAR PLATE IAW EMB 190 SRM 51-40-02, 51-41-01, 51-43-01 AND 51-42-00. REF P/N'S 170-65669-003 (BEAM) & 170-65928-001 (SHEAR PANEL). AIRCRAFT IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Source: SDR R61A201207030332

2011

OTHER · 2011-08-16 Matched by certificate designator
ATA 5210

Part: UNKNOWN — MALFUNCTIONED (L1 DOOR) · airframe 7,639 hrs · 5,200 cycles

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.

Source: SDR R61A20110221
OTHER · 2011-06-06 Matched by certificate designator
ATA 5210

Part: DOOR — BINDS (L1) · airframe 7,015 hrs · 4,848 cycles

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.

Source: SDR R61A20110137
OTHER · 2011-02-16 Matched by certificate designator
ATA 2560

Part: GIRT BAR — OUT OF ADJUST (L1 DOOR) · airframe 5,992 hrs · 4,365 cycles

MAINTENANCE REPORTED L1 DOOR SLIDE WILL NOT ARM. MX ADJUSTED L1 GIRT BAR IAW EMB AMM, OPS CHECK GOOD.

Source: SDR R61A20110041

2010

WARNING INDICATION · 2010-07-26 Matched by certificate designator
ATA 2780

Part: SLAT — MALFUNCTIONED (WING) · airframe 4,311 hrs · 3,419 cycles

CREW REPORTED SLAT FAIL ON APPROACH AFTER SELECTING SLAT/FLAP LEVER TO 1, DECLARED AN EMERGENCY AND LANDED AT DEN WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT PER EMB AMM AND CLEARED INHIBITS AND RESET SYSTEM, A/C WAS THEN RELEASED INTO SERVICE.

Source: SDR R61A20100359
FALSE WARNING · 2010-07-26 Matched by certificate designator
ATA 2781

Part: SENSOR — FAULTY (LE SLAT) · airframe 4,311 hrs · 3,419 cycles

CREW REPORTED SLAT FAIL ON APPROACH AND DECLARED AN EMERGENCY INTO DEN, AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT OUTBOARD SLAT SKEW SENSORS PER EMB AMM, A/C WAS THEN RETURNED TO SERVICE.

Source: SDR R61A20100360
OTHER · 2010-06-10 Matched by certificate designator
ATA 2565

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 3,900 hrs · 3,194 cycles

CREW REPORTED L-1 DOOR SLIDE WAS OUT OF BUSTLE. MAINTENANCE REMOVED AND REPLACED L-1 DOOR SLIDE PER EMB AMM, A/C WAS THEN RETURNED TO SERVICE.

Source: SDR R61A20100249