N208JQ
Registered owner: REPUBLIC AIRWAYS INC, IN (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| SHUTTLE AMERICA CORP | Operator | on 2013-05-11 | Operator named in NTSB report |
Accident & incident history
Operated by SHUTTLE AMERICA CORP (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.
128 reports on file, 2010-01-27 – 2026-08-20.
Part: POWER SUPPLY — NO TEST (ZONE 200) · airframe 39,426 hrs · 29,130 cycles
DURING A FUNCTIONAL CHECK, FWD LH EMERGENCY LIGHT POWER UNIT FAILED. R&R FWD LH EMERGENCY LIGHT POWER UNIT.
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: FMU — FAILED (NR 2) · airframe 38,125 hrs · 28,164 cycles
ENG 2 FUEL IMPENDING BYPASS MSG. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. INSPECTED ENG 2 FUEL FILTER DIFF PRESS SENSOR. REMOVED AND REPLACED FMU 2.
Earlier reports · 2010–2024 · 125 reports
2024
Part: CONTROL LEVER — FAULTED (ZONE 700) · airframe 35,686 hrs · 26,222 cycles
LANDING GEAR WILL NOT RETRACT. NOT OVERWEIGHT AND HANDLE WOULD NOT MOVE. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. R&R LANDING GEAR CONTROL LEVER.
2023
Part: DOOR — CORRODED (ZONE 100) · corrosion level 2 · airframe 31,798 hrs · 22,984 cycles
AFT WASTE SERVICE PANEL DOOR CORRODED AT FWD EDGE. MX REPLACED WASTE DOOR PN 170-86668-403 IAW 53-03-60-040-801-A
Part: PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 31,798 hrs · 22,984 cycles
CF3 RH OB FLOOR PANEL SUPPORT FOUND CORRODED UPPER SURFACE FR83-84. MX REPLACED SUPPORT PN 170-92908-001, IAW SRM 51-*41-01, 51-41-02, 51-43-02.
Part: PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 31,798 hrs · 22,984 cycles
CF3 LH OB FLOOR PANEL SUPPORT FOUND TO HAVE CORROSION ON UPPER SURFACE AT FR 83-84. MX REPLACED PANEL PN 170-92907-001 IAW SRM 51-41-01, 51-41-02.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 31,798 hrs · 22,984 cycles
R/H O/B FLOOR PNL UPPER SURFACE AT FR 83 - 84 CORRODED. R&R IAW 51-41-02, 5141-01 AND 51-43-02.
Part: RIB — CORRODED (ZONE 600) · airframe 31,798 hrs · 22,984 cycles
DENT FOUND ON RH WING LEADING EDGE AT SLAT 3 OB TRACK AT RIB 19. RIB 19 PN 170-01421-011 PERM ALLOWED DAMAGE IAW ETD2023-170-002278.
Part: DOUBLER — CORRODED (ZONE 100) · corrosion level 2 · airframe 31,798 hrs · 22,984 cycles
WASTE SERVICE DOOR CUTOUT DOUBLER HAS CORROSION AT THE INBD FWD CORNER. REPLACED DOUBLER PN 170-66931-001 IAW SRM 51-41-01, 51-21-02.
Part: SPLICE PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 31,798 hrs · 22,984 cycles
SPLICE PLATE AT FR 90, BL 0 UPPER SURFACE CORRODED. R&R IAW SRM 51-43-03.
Part: GUSSET — CORRODED (ZONE 100) · corrosion level 2 · airframe 31,798 hrs · 22,984 cycles
AFT WET AREA TOP SURFACE OF FLOOR BEAM AT FR 90+2 INCHES. CORRODED. MX REPLACED GUSSETT PN 170-60259-001 IAW SRM 51-41-02.
Part: SHEAR PANEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 31,798 hrs · 22,984 cycles
CENTER SHEAR PNL AT FR 88-89 UPPER SURFSCE CORRODED. R&R IAW SRM 51-42-01.
Part: RIB — CORRODED (ZONE 100) · airframe 31,798 hrs · 22,984 cycles
SUSPECTED CRACK ON LH H-STAB RIB 7A. REPAIRED LH H-STAB RIB 7A UPPER AFT FLANGE IAW ETD2023-170-002311.
Part: RIB — CORRODED (ZONE 100) · airframe 31,798 hrs · 22,984 cycles
SUSPECTED CRACK ON LH H-STAB RIB 7A. MX REPAIRED RIB 7A IAW ETD2023-170-002311.
Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 31,798 hrs · 22,984 cycles
AFT WET AREA GUSSET PLATE AT FR 90, LBL8 IS CORRODED. R&R IAW SRM 51-41-02.
Part: UPPER SHEET — CORRODED (ZONE 200) · corrosion level 2 · airframe 31,798 hrs · 22,984 cycles
UPPER SHEET AT FR 85, AFT RH I/B SEAT TRACK AREA TOP SURFACE CORRODED. R&R IAW SRM 51-43-03 AND 51-41-01.
Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 31,798 hrs · 22,984 cycles
AFT WET AREA RH OB PANEL SUPPORT AT FR 88-90 FOUND TO HAVE CORROSION ON UPPER SURFACE. MX REPLACED SUPPORT PN 170-86787-003 IAW SRM 51-41-01, 51-43-03.
Part: STRAP — CORRODED (ZONE 100) · corrosion level 2 · airframe 31,798 hrs · 22,984 cycles
AFT WING TO BODY FAIRING SUPPORT STRUCTURE HAS CORROSION BTWN STR 19R-STR 19L.MX REPLACED STRAPS IAW SRM 51-41-02
Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 31,798 hrs · 22,984 cycles
AFT WING TO BODY FAIRING SUPPORT STRUCTURE HAS CORROSION BTWN STR 19R-STR 19L.MX REPLACED STRAPS IAW SRM 51-41-02
Part: NONE — CORRODED (ZONE 100) · corrosion level 2 · airframe 31,798 hrs · 22,984 cycles
UPPER SHEET AT FR 85, JUST AFT OF LH INBD SEAT TRACK FOUND CORROSION TOP SURFACE. REPLACED UPPER SHEET PN 170-86101-001 IAW SRM 51-41-01, 51-43-01.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 31,798 hrs · 22,984 cycles
AFT WET AREA LH O/B PNL SUPPORT AT FR 88-90 UPPER SURFACE CORRODED. R&R IAW SRM 51-41-01 AND 51-43-03.
Part: SHEAR WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 31,798 hrs · 22,984 cycles
SHEAR CLIP AT FR 76, BTWN STR 28L - 29L CORRODED. R&R IAW SRM 51-41-01 AND 51-41-02.
Part: RIB — CRACKED (ZONE 300) · airframe 31,798 hrs · 22,984 cycles
***MAJOR***RH H-STAB RIBS 10A AN 11A FOUND CRACKED. MX PEPAIRED IAW REPUBLIC JC 170EO-55-10-004_1. AAR ROUTINE CARD 4501315-3000-0071***MAJOR***
Part: BONDING — CORRODED (ZONE 100) · corrosion level 2 · airframe 31,798 hrs · 22,984 cycles
CF3 AVIONICS BONDING BRACKET BTWN FR 85-86 AT STR 29R FOUND CORRODED. MX REPLACED BONDING ASSY PN PE29075A-1 IAW SRM 51-41-01
Part: SHEAR PANEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 31,798 hrs · 22,984 cycles
SHEAR CLIP AT FR 75 BTWN STR 28L - 29L CORRODED. R&R IAW SRM 51-41-01 AND 51-41-02.
Part: SHEAR PANEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 31,798 hrs · 22,984 cycles
SHEAR CLIP AT FR 75 BTWN STR 28R - 29R CORRODED. R&R IAW SRM 51-41-01 AND 51-41-02.
Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 31,798 hrs · 22,984 cycles
DRAIN MAST SUPPORT BRKT AND CLIP AT FR 86-87, BTWN STR 27R-28R CORRODED. R&R IAW SRM 51-41-01.
Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 31,798 hrs · 22,984 cycles
CF3 SHEAR CLIP AT FR 76 BTWN STR 28R-STR 29R FOUND CORRODED. REPLACED CF3 CORRODED SHEAR CLIP PN 170-66664-001 AT FR 76 BTWN STR 28R-29R IAW SRM 51-41-02.
Part: SHEAR WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 31,798 hrs · 22,984 cycles
SHEAR CLIP FR 85 BTWN STR 28L-27L AFT OF WATER BOX CORRODED. R&R IAW SRM 51-41-02 AND 51-43-01.
Part: SHEAR PANEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 31,798 hrs · 22,984 cycles
CF III SHEAR CLIP AT FR 84, BTWN STR 28R - 29R CORRODED. R&R IAW SRM 51-41-01 AND 51-41-02.
Part: SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 31,798 hrs · 22,984 cycles
BAGGAGE SUPPORT AT FR 75 STR 29L CORRODED. R&R IAW SRM 51-41-01.
2021
Part: HANDLE — LACK OF LUBE (L1 DOOR) · airframe 28,156 hrs · 20,226 cycles
L1 DOOR HANDLE HARD TO OPERATE. LUBED L1 DOOR MECHANISM IAW AMM 52-11-00.
2020
Part: ANGLE — CRACKED (FRAME 12) · airframe 26,941 hrs · 19,131 cycles
DURING HEAVY CHECK MAINTENANCE FOUND CRACK FOUND ON FWD FUSELAGE COCKPIT UNDER FLOOR CONSOLE ANGLE AT FR 12 AND BL 0. FWD FUSELAGE COCKPIT UNDER FLOOR CONSOLE ANGLE AT FR 12 AND BL 0 REPLACED, IAW SRM 51-41-01. A/C REMAINS IN CHECK.
Part: RIB — CRACKED (VERTICAL STAB) · airframe 26,941 hrs · 19,131 cycles
DURING HEAVY CHECK MAINTENANCE FOUND CRACK FOUND ON VERTICAL STABILIZER TRAILING EDGE RIB 9/10. VERTICAL STABILIZER TRAILING EDGE RIB 9/10 REPLACED WITH NEW, IAW EMB 170 SRM 51-41-01 AND 51-41-02. A/C REMAINS IN CHECK.
Part: COVER — CRACKED (CARGO DOOR) · airframe 26,941 hrs · 19,131 cycles
DURING HEAVY CHECK MAINTENANCE FOUND FWD CARGO DOOR SPRING COVER CRACKED. SPRING COVER ON FWD CARGO DOOR REPLACED, AS PER EMB AMM 20-10-01 AND SRM 53-21-29 AND SRM 51-21-02. A/C REMAINS IN CHECK.
Part: DOOR SILL — CORRODED (R2 DOORWAY) · corrosion level 2 · airframe 26,941 hrs · 19,131 cycles
DURING HEAVY CHECK MAINTENANCE FOUND CORROSION FOUND ON PREVIOUSLY BLENDED AREA ON AFT SERVICE DOOR(R2) LOWER SILL BEAM. AFT SERVICE DOOR (R2) LOWER SILL BEAM REMOVED AND REPLACED, IAW EMB 170 SRM 51-43-02 AND 51-43-01. A/C REMAINS IN CHECK.
Part: SHEAR PANEL — CORRODED (FRAME 87) · corrosion level 2 · airframe 26,941 hrs · 19,131 cycles
DURING HEAVY CHECK MAINTENANCE FOUND CORROSION ON CENTER FUSELAGE III FLOOR STRUCTURE RT SHEAR PANEL AT FR 87. FLOOR STRUCTURE RT SHEAR PANEL AT FR 87 REMOVED AND REPLACED, IAW EMB 170 SRM 51-42-01. A/C REMAINS IN CHECK.
Part: SHEAR PANEL — CORRODED (FRAME 87) · corrosion level 2 · airframe 26,941 hrs · 19,131 cycles
DURING HEAVY CHECK MAINTENANCE FOUND CORROSION ON CENTER FUSELAGE III FLOOR STRUCTURE MID SHEAR PANEL AT FR 87. MID SHEAR PANEL AT FR 87 AND FLOOR STRUCTURE REMOVED AND REPLACED, IAW EMB 170 SRM 51-42-01. A/C REMAINS IN CHECK.
Part: BEAM — CORRODED (L2 DOOR SILL) · corrosion level 2 · airframe 26,941 hrs · 19,131 cycles
DURING HEAVY CHECK MAINTENANCE FOUND CORROSION ON PREVIOUSLY BLENDED AREA AT CENTER FUSELAGE III AFT PASSENGER DOOR (L2) LOWER SILL BEAM. AFT PASSENGER DOOR (L2) LOWER SILL BEAM REMOVED AND REPLACED, IAW EMB 170 SRM 51-43-02 AND SRM 51-43-01. A/C REMAINS IN CHECK.
Part: SHEAR PANEL — CORRODED (FRAME 87) · corrosion level 2 · airframe 26,941 hrs · 19,131 cycles
DURING HEAVY CHECK MAINTENANCE FOUND CORROSION ON CENTER FUSELAGE III FLOOR STRUCTURE, LT SHEAR PANEL AT FR 87. LT SHEAR PANEL AT FR 87 REMOVED AND REPLACED, IAW EMB 170 SRM 51-42-01. A/C REMAINS IN CHECK.
Part: SEAT TRACK — CORRODED (FRAME 17) · corrosion level 2 · airframe 26,941 hrs · 19,131 cycles
DURING HEAVY CHECK MAINTENANCE FOUND CORROSION ON FWD FUSELAGE FLOOR STRUCTURE, RT INBOARD SEAT TRACK BEAM AT FR 17. FUSELAGE FLOOR STRUCTURE RT INBOARD SEAT TRACK BEAM AT FR 17 REPLACED, IAW EMB SRM 51-43-01 AND SRM 51-41-02. A/C REMAINS IN CHECK.
Part: DOOR — CORRODED (WASTE SERVICE) · corrosion level 2 · airframe 26,941 hrs · 19,131 cycles
DURING HEAVY CHECK MAINTENANCE FOUND CORROSION ON AFT FUSELAGE WASTE SERVICE PANEL. AFT FUSELAGE WASTE SERVICE PANEL REPLACED, IAW AMM 20-10-01-910-001-A. A/C REMAINS IN CHECK.
2018
Part: ACM — DAMAGED (NR 1) · airframe 23,230 hrs · 16,263 cycles
SMOKE IN COCKPIT AND CABIN AROUND 9000FT WITH ASSOCIATED GRINDING NOISE THAT DISSIPATED. NO INDICATION ON EICAS, SMOKE AND SMELL DISSIPATED ON APPROACH. R&R ACM PACK #1 IAW AMM 21-51-05, OPS CHECK GOOD.
Part: CONNECTOR — DIRTY (NR 2 ACCEROMETER) · airframe 22,401 hrs · 15,706 cycles
NR 2 ENGINE LP VIBRATION AT 4.0, DURING CRUISE, BUT ONLY FOR 5 SECONDS. THIS HAPPENED SEVERAL TIMES WHILE AT CRUISE. DURING DESCENT, VIBRATION WENT TO 4 WITH DESCENT POWER. AT 8,000 FEET, NR 2 ENGINE LP VIBRATION WHEN TO 4.1 AND PEAKED AT 4.4 BY THE TIME THE ENGINE WAS SHUTDOWN. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. INSPECTED THE NR 2 ENGINE, DISCOVERED AFT ACCELEROMETER DIRTY. CLEANED THE CONNECTOR PLUG IAW MM 77-00-00.
Part: ANGLE — CORRODED (FRAME 52) · corrosion level 2 · airframe 21,202 hrs · 14,977 cycles
SURFACE CORRROSION ON TWO ANGLES ON PANEL 1431DL. REMOVED AND REPLACED THE ANGLES IAW AMM 20-10-07, AND SRM 51-40-02.
Part: SEAT TRACK — CORRODED (FRAME 84) · corrosion level 2 · airframe 21,202 hrs · 14,977 cycles
RT SEAT TRACK FRAME 84 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW ETD2018-170-013113.
Part: SHEAR PANEL — CORRODED (FRAMES 88-88) · corrosion level 2 · airframe 21,202 hrs · 14,977 cycles
CENTER SHEAR PANEL CORRODED. REMOVED AND REPLACED THE SHEAR PLATE IAW SRM 51-40-08, 51-23-04, 51-23-05, AND 51-23-06.
Part: THRESHOLD — CORRODED (CARGO BAY) · corrosion level 2 · airframe 21,202 hrs · 14,977 cycles
CORROISON ON THE COVER PLATE ATTACH POINT ON THE FWD CARGO THRESHOLD. REMOVED AND REPLACED THE THRESHOLD AND APPLIED SURFACE PROTECTION IAW SRM 51-40-08, 51-23-04,51-23-05, AND 51-23-06.
Part: SEAT TRACK — CORRODED (FRAMES 14-18) · corrosion level 2 · airframe 21,202 hrs · 14,977 cycles
CORROSION ON THE RT CENTER SEAT TRACK, FRAMES 14 - 18. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-08.
Part: CLOSEOUT PANEL — CORRODED (FRAMES 77-80) · corrosion level 2 · airframe 21,202 hrs · 14,977 cycles
SURFACE CORROSION ON AFT CARGO CLOSE OUT PANEL. REMOVED AND REPLACED THE CLOSE OUT PANEL IAW SRM 51-40-02, 51- 23-04, 51-23-05, AND 51-23-06.
Part: UPPER SHEET — CORRODED (FRAMES 85-86) · corrosion level 2 · airframe 21,202 hrs · 14,977 cycles
RIGHT UPPERSHEET FRAMES 85 - 86. REMOVED AND REPLACED THE UPPERSHEET IAW SRM 51-41-01, 51-43-03, AND SRM 51-40-08.
Part: SKIN — CORRODED (NR 4 SLAT) · corrosion level 2 · airframe 21,202 hrs · 14,977 cycles
LEFT NR 4 SLAT INTERNAL SKIN CORRODED AT INBD END. REMOVED AND REPLACED THE LT WING SLAT PANEL IAW AMM 27-81-08.
Part: SPLICE — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 21,202 hrs · 14,977 cycles
LEFT OTBD SPLICE FRAMES 87 - 88 CORRODED. REMOVED AND REPLACED THE SPLICE IAW SRM 51-23-04, SRM 51-40-02, AND SRM 51-40-08.
Part: DOUBLER — CORRODED (FRAME 16) · corrosion level 2 · airframe 21,202 hrs · 14,977 cycles
FWD LT FLOOR DOUBLER CORRODED AT FR 16. LOCATED, DRILLED, COUNTERSANK, AND ALODINED A NEW FLOOR DOUBLER IAW SRM 51-45-00, SRM 51-41-02, SRM 51-40-02, AND SRM 51-23-04.
Part: CLOSEOUT PANEL — CORRODED (FRAMES 24-27) · corrosion level 2 · airframe 21,202 hrs · 14,977 cycles
SURFACE CORROSION ON FWD CARGO CLOSE OUT PANEL. REMOVED AND REPLACED FWD CARGO CLOSE OUT PANEL REF SRM 51-40-02, 51-23-04, 51-23-05, AND 51-23-06.
Part: BEAM — CORRODED (FRAMES 87-94) · corrosion level 2 · airframe 21,202 hrs · 14,977 cycles
CORROSION ON THE RT BEAM Y +10.748. REMOVED AND REPLACED THE BEAM IAW SRM 51-40-08.
Part: SEAT TRACK — CORRODED (FRAMES 14-19) · corrosion level 2 · airframe 21,202 hrs · 14,977 cycles
CORROSION ON THE LT CENTER SEAT TRACK, FRAMES 14 - 19. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-08, SRM 51-23-06, AND CPM 51-25-00.
Part: SPLICE — CORRODED (FRAME 90) · corrosion level 2 · airframe 21,202 hrs · 14,977 cycles
RIGHT SPLICE FRAME 90 CORRODED. REPLACED THE SPLICE.
Part: BEAM — CORRODED (FRAMES 87-94) · corrosion level 2 · airframe 21,202 hrs · 14,977 cycles
CORROSION CENTER FUSELAGE WET AREA 53-23 RT BEAM Y +10.748. REMOVED DAMAGED BEAM IAW SRM 51-40-08. LOCATED & DRILLED A NEW BEAM, INSTALLED THE BEAM IAW SRM 51-40-08.
Part: GUSSET — CORRODED (FRAME 90) · corrosion level 2 · airframe 21,202 hrs · 14,977 cycles
CORROSION ON THE GUSSET FRAME 90. REMOVED THE GUSSET AND INSTALLED A NEW GUSSET IAW SRM 51-40-08.
Part: SPLICE — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 21,202 hrs · 14,977 cycles
RT, OTBD SPLICE FRAMES 87 - 88 CORRODED. REMOVED AND REPLACED THE SPLICE IAW SRM 51-40-02.
Part: FLOOR SUPPORT — CORRODED (FRAME 16) · corrosion level 2 · airframe 21,202 hrs · 14,977 cycles
LEFT OTBD FLOOR SUPPORT CORRODED, FRAME 16. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-41-02, 51-43-04, AND 51-45-00.
Part: SHEAR PANEL — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 21,202 hrs · 14,977 cycles
CORROSION ON THE RT SHEAR PLATE, FRAMES 87 - 88. REMOVED AND REPLACED THE SHEAR PLATE IAW SRM 51-40-08, SRM 51-40-02, AND 51-23-04.
Part: SEAT TRACK — CORRODED (FRAME 84) · corrosion level 2 · airframe 21,202 hrs · 14,977 cycles
LEFT SEAT TRACK FRAME 84 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 53-00-10, REPAIR 01, ETD2018-170-013185, AND NTM 51-00-00-918-803-A.
Part: FLOOR SUPPORT — CORRODED (FRAME 16) · corrosion level 2 · airframe 21,202 hrs · 14,977 cycles
FWD LEFT FLOOR SUPPORT CORRODED, FRAME 16. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-08, AND SRM 51-23-06.
Part: FINGER DOUBLER — CHAFED (DOOR FRAME) · airframe 21,202 hrs · 14,977 cycles
FWD CARGO DOOR CUTOUT, LOWER HORIZONTAL BEAM, FWD FINGER DOUBLER IS CHAFED. REMOVED AND REPLACED THE BEAM FWD FINGER DOUBLER IAW SRM 51-40-08.
Part: UPPER SHEET — CORRODED (FRAMES 85-86) · corrosion level 2 · airframe 21,202 hrs · 14,977 cycles
LEFT UPPERSHEET, FRAMES 85 - 86. REMOVED AND REPLACED THE UPPERSHEET IAW SRM 51-41-01, 51-43-03, AND SRM 51-40-08.
Part: ANGLE — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 21,202 hrs · 14,977 cycles
CORROSION BOTH BOTTOM ANGLE ON PANEL 1441FR. REMOVED AND REPLACED THE ANGEL IAW SRM 51-45-00.
2017
Part: SKIN — GOUGED (FRAMES 3-4) · airframe 20,659 hrs · 14,625 cycles
MAINTENANCE FOUND A GOUGE ON THE FWD FUSELAGE SKIN. MAINTENANCE REPAIRED THE SKIN IAW ETD2017-170-091330. AIRCRAFT WAS RETURNED TO SERVICE.
Part: BATTERY — FAULTED (EMERGENCY LIGHT) · airframe 20,473 hrs · 14,499 cycles
EMERGENCY LIGHT BATTERY FAULTED. FAULT CODE 33500004UT1. R & R THE RT AFT EMERGENCY LIGHT POWER SUPPLY.
Part: SENSOR — MALFUNCTIONED (L2 DOOR) · airframe 19,080 hrs · 13,559 cycles
CREW RECEIVED AN L2 DOOR OPEN MESSAGE. AN EMERGENCY WAS NOT DECLARED AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE CLOSED DOOR SENSOR IAW AMM. OPS CHECKED GOOD.
2016
Part: LIGHT — NO TEST (CABIN) · airframe 18,323 hrs · 13,106 cycles
EMERGENCY LIGHTS FAILED OPERATIONAL TEST. R & R THE LIGHT IAW AMM.
Part: DETECTOR — DEFECTIVE (ZONE 800) · airframe 17,766 hrs · 12,738 cycles
L2 DOOR SHOWING OPEN ON MFD IN FLIGHT. ALL PHYSICAL DOOR INDICATIONS NORMAL. R & R ROLLER DETECTOR SHAFT IAW 53-23-25.
Part: WARNING MESSAGE — FALSE ACTIVATION (L2 DOOR) · airframe 17,695 hrs · 12,694 cycles
MASTER WARNING FOR L2 DOOR OPEN DURING FLIGHT. IT STAYED ON FOR 40 MINUTES, ALL INDICATORS ON DOOR WERE NORMAL.
Part: GIRT BAR — STUCK (L1 DOOR) · airframe 17,661 hrs · 12,673 cycles
L1 DOOR WON'T ARM. GIRT BAR STUCK. INSPECTED AND FOUND L1 DOOR GIRT BAR NOT SNAPPED IN PLACE. RESECURED GIRT BAR IAW MM 52-11-41 AND NO DEFECTS NOTED. CHECKS GOOD IAW MM 52-11-20.
Part: INDICATOR — OUT OF ADJUST (L2 DOOR) · airframe 17,372 hrs · 12,486 cycles
DOOR L2 INDICATOR LATCH MISSING. -ADJUSTED THE L2 DOOR INDICATOR IAW AMM 52-42-00. OPS CHECK GOOD.
2015
Part: SKIN — DENTED (FRAMES 10-11) · airframe 15,808 hrs · 11,509 cycles
FOUND DENT BELOW CAPTAIN'S DV WINDOW BETWEEN STR 17-18 AND FR 10-11. REPAIRED LT FORWARD FUSELAGE SKIN AT FR 10-FR 11 BETWEEN STR 17L-18L IAW ETD2015-170-070243, REV C.
Part: GUST LOCK — INOPERATIVE (L1 DOOR) · airframe 14,477 hrs · 10,714 cycles
L1 DOOR GUST LOCK DOES NOT HOLD DOOR OPEN. R & R L1 DOOR HINGE COVER REF AMM 25-23-04. OPS CHECK GOOD.
Part: GUST LOCK — INOPERATIVE (L1 DOOR) · airframe 14,469 hrs · 10,709 cycles
L1 DOOR GUST LOCK DOES NOT WORK. DOOR DOES NOT LOCK IN ON OPEN POSITION. CLEANED GUST LOCK AND PERFORMED OPS CHECK ON L1 DOOR IAW AMM 52-11-00. OPS CHECK NORMAL.
2013
Part: HANDLE — MALFUNCTIONED (MLG) · airframe 11,331 hrs · 8,722 cycles
GEAR HANDLE WOULD NOT MOVE IN UP POSITION ON TAKEOFF, DOWNLOCK RELEASE BUTTON PRESSED, GEAR RETRACTED. LANDING GEAR RETRACTED BUT REMAINED IN TRANSIENT FOR A LONG PERIOD. NO EMERGENCY DECLARED, LANDED WITHOUT INCIDENT. R & R LANDING GEAR LEVER, PSEM 1, NIM 2, AND SPDA 1 DC POWER MODULE SLOT 13, PEFORMED MULTIPLE GEAR SWINGS, OPS CHECKED GOOD.
Part: SENSOR — MALFUNCTIONED (WOW) · airframe 11,327 hrs · 8,720 cycles
LANDING GEAR HANDLE WOULD NOT RAISE GEAR AFTER TAKEOFF, LANDING INDICATING DOWN AND THREE GREEN, NO EICAS MESSAGE. DECLARED EMERGENCY AND RETURNED TO FIELD, LANDED WITHOUT INCIDENT. R & R NR 1 NLG WOW SENSOR AND WOW SENSOR HARNESS, PERFORMED MULTIPLE GEAR SWINGS IAW AMM 32-33-00, OPS CHECKED GOOD.
Part: CLOSEOUT PANEL — CORRODED (CARGO BAY) · airframe 11,324 hrs · 8,717 cycles
CORROSION FOUND ON FWD CARGO BAY LOWER HORIZONTAL BEAM CLOSE OUT PANEL IN THREE PLACES. REMOVED FWD CARGO CLOSE OUT PANEL.
Part: DOUBLER — CORRODED (ZONE 100) · airframe 11,324 hrs · 8,717 cycles
CORROSION ON DOUBLER. R & R DOUBLER.
Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,324 hrs · 8,717 cycles
CORROSION FOUND ON AFT RT DOOR SILL CORRODED AT FRAME 17. R & R SILL.
Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,324 hrs · 8,717 cycles
CORROSION FOUND ON FLOORBEAM AT FRAME 84. R & R FLOORBEAM.
Part: UPPER SHEET — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,324 hrs · 8,717 cycles
CORROSION FOUND ON RT UPPER SHEET AT FRAMES 85-86. R & R UPPER SHEET.
Part: GUSSET — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,324 hrs · 8,717 cycles
CORROSION FOUND ON LT GUSSET AT FRAME 90. R & R LT GUSSET.
Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,324 hrs · 8,717 cycles
CORROSION FOUND ON LT SEAT TRACK CORRODED AT FRAME 19. FABRICATED DOUBLER AND FILLER AND INSTALLED REPAIR IAW SRM 53-10-10.
Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,324 hrs · 8,717 cycles
CORROSION FOUND ON RT FWD FLOOR SUPPORT FRAME 84. R & R RT FWD FLOOR SUPPORT.
Part: GUSSET — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,324 hrs · 8,717 cycles
CORROSION FOUND ON RT GUSSET PLATE FRAME 90. R & R GUSSET.
Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,324 hrs · 8,717 cycles
CORROSION FOUND ON FLOOR SUPPORT AT FRAME 16. REMOVED AND REPLACED FLOOR SUPPORT.
Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,324 hrs · 8,717 cycles
CORROSION FOUND ON SHEAR TIE FRAME 88, STRINGERS 26-27R. R & R SHEAR TIE.
Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,324 hrs · 8,717 cycles
CORROSION FOUND ON LT FWD DOOR SILL AT FRAME 16. R & R SILL.
Part: BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,324 hrs · 8,717 cycles
CORROSION FOUND ON RT BEAM BETWEEN FRAMES 86-89. R & R RT AFT BEAM.
Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,324 hrs · 8,717 cycles
CORROSION FOUND ON FWD RT DOOR SILL CORRODED AT FRAMES 13-14. R & R SILL.
Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,324 hrs · 8,717 cycles
CORROSION FOUND ON LT AFT FLOOR SUPPORT FRAMES 88-90. R & R LT AFT FLOOR SSUPPORT.
Part: SHEAR PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,324 hrs · 8,717 cycles
CORROSION FOUND ON LT SHEAR PLATE SPLICE FRAMES 87-88. R & R SHEAR PLATE.
Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,324 hrs · 8,717 cycles
CORROSION FOUND ON LT SEAT TRACK AT FRAME 17. FABRICATED DOUBLER AND FILLER AND INSTALLED IAW SRM 53-10-10.
Part: SHEAR PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,324 hrs · 8,717 cycles
CORROSION FOUND ON RT SHEAR PLATE FRAMES 87-88. R & R SHEAR PLATE.
Part: DOUBLER — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,324 hrs · 8,717 cycles
CORROSION FOUND ON DOUBLER. R & R DOUBLER.
Part: UPPER SHEET — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,324 hrs · 8,717 cycles
CORROSION FOUND ON LT UPPER SHEET AT FRAMES 85-86. R & R UPPER SHEET.
Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,324 hrs · 8,717 cycles
CORROSION FOUND ON LT SEAT TRACK FRAMES 84-85. FABRICATED AND INSTALLED DOUBLER IAW ETD2013-170-052232.
Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,324 hrs · 8,717 cycles
CORROSION FOUND ON RT SEAT TRACK CORRODED AT FRAMES 15-17. REMOVED CORROSION AND INSTALLED FASTENERS IAW SRM 53-10-10.
Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,324 hrs · 8,717 cycles
CORROSION FOUND ON INTERCOSTAL BETWEEN FRAMES 89-90. R & R INTERCOSTAL.
Part: SHEAR PLATE — CORRODED (ZONE 100) · airframe 11,324 hrs · 8,717 cycles
CORROSION FOUND ON LEFT SHEAR PLATE, FRAMES 87-88. R & R SHEAR PLATE.
Part: SHEAR PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,324 hrs · 8,717 cycles
CORROSION FOUND ON CENTER SHEAR PLATE FRAMES 87-88. R & R SHEAR PLATE.
Part: SEAT TRACK — CORRODED (FRAMES 15-17) · airframe 11,324 hrs · 8,717 cycles
CORROSION FOUND ON RT SEAT TRACK AT FRAMES 15-17. REMOVED CORROSION AND INSTALLED FASTENERS.
Part: GUSSET — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,324 hrs · 8,717 cycles
CORROSION FOUND ON RT GUSSET PLATE FRAME 90. R & R GUSSET.
Part: WARNING LIGHT — ILLUMINATED (EMERGENCY LIGHTS) · airframe 11,246 hrs · 8,669 cycles
EMERGENCY LIGHTS FAULT ON EICAS. PERFORMED POWER RESET IAW AMM 24-42-02. MESSAGE CLEARED.
Part: GLOWSTRIP — LOOSE (CABIN) · airframe 10,224 hrs · 7,933 cycles
EMERGENCY PHOTO LUMINESCENT STRIP BY FWD COAT CLOSET LOOSE. RE-SECURED EMERGENCY PHOTO LUMINESCENT STRIP IAW AMM 33-50-21.
Part: BATTERY — FAULTY (CABIN) · airframe 9,731 hrs · 7,531 cycles
EMERGENCY BATTERY FWD L FAULT ON EICAS. REPLACED BOTH FWD EMERGENCY BATTERIES IAW MM 33-50-01-800-806-A20.
Part: WARNING SYSTEM — FALSE ACTIVATION (EMERGENCY LIGHTS) · airframe 9,629 hrs · 7,446 cycles
EMERGENCY LIGHT BATTERY FAULT. PERFORMED OPS CHECK OF EMERGENCY LIGHTS IAW AMM 33-50-00, OPS CHECK GOOD.
2012
Part: ROLLER PIN — DEFECTIVE (PAX DOOR) · airframe 9,183 hrs · 7,125 cycles
"DOOR PAX FWD OPEN" ANNUN LIGHT ON AT FL350, CABIN PRESSURE HOLDING AT 7.5PSI. REMOVED AND REPLACED ROLLER PIN SHAFT ON LATCH POSITION INDICATOR IAW AMM 53-10-21, OPS CHECK GOOD.
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 9,174 hrs · 7,119 cycles
DOOR PAX FWD OPEN MESSAGE IN FLIGHT. OPS CHECK GOOD IAW AMM 52-11-00-05, COULD NOT DUPLICATE.
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 9,175 hrs · 7,120 cycles
DOOR PAX FWD MESSAGE IN FLIGHT AT FL180, EXTINGUISHED 13,000FT. NO FAULT FOUND, COULD NOT RECREATE ON GROUND, INSPECTED DOOR IAW AMM 52-72-20.
Part: TRACK — DIRTY (PAX DOOR) · airframe 9,154 hrs · 7,100 cycles
AT FL370 "DOOR PAX FWD OPEN" EICAS MESSAGE ILLUMINATED. COMPLETED QRH PROCEDURE, PRESSURIZATION NORMAL, MESSAGE CLEARED DESCENDING THROUGH FL180. FOUND MIXTURE OF DEICE FLUID AND FOD, CLEANED DOOR TRACKS AND MECHANISM. NO DEFECTS NOTED IAW AMM 52-11-2.
Part: GLOWSTRIP — DETACHED (CABIN) · airframe 8,393 hrs · 6,490 cycles
FORWARD MOST PHOTO LUMINESCENT FLOOR TRIM ON A/C RIGHT NEEDS TO BE RE-ATTACHED. RE-SECURED FWD PHOTO LUMINESCENT FLOOR TRIM IAW EMB 170 MM 33-50-21.
Part: LIGHT — LOOSE (CABIN) · airframe 8,275 hrs · 6,408 cycles
ILLUMINATION STRIP IN FRONT OF FWD CLOSET CAME OFF. RE-SECURED ILLUMINATION STRIP IN FRONT OF FWD CLOSET IAW EMB 170 MM 33-50-2.
Part: GIRT BAR — DISCONNECTED (L2 DOOR) · airframe 8,043 hrs · 6,224 cycles
NO GIRT BAR INDICATION ON L2 SERVICE DOOR WHEN DOOR IS CLOSED. DOOR INDICATES CLOSED ON STATUS PAGE, BUT NO RED FLAG IN BOTTOM LEFT WINDOW OF DOOR. FOUND GIRT BAR ON L2 DOOR DISCONNECTED. RECONNECTED GIRT BAR IAW EMB 170 AMM 25-65-01. OPS CHECK GOOD.
Part: GIRT BAR — DETACHED (CABIN DOOR) · airframe 7,370 hrs · 5,660 cycles
MAIN CABIN DOOR GIRT BAR INDICATOION IS NOT SHOWING PROPER ROD INDICATION. RE-ATTACHED GIRT BAR TO AFT HINGE.
Part: GIRT BAR — DETACHED (L1 DOOR) · airframe 7,315 hrs · 5,610 cycles
L1 DOOR SLIDE WILL NOT ARM, HANDLE WILL NOT MOVE DOWN. RE-ATTACHED GIRT BAR ASSY ON DOOR IAW EMB 170 MM 52-11-41. DOOR ARMS NORMALLY AT THIS TIME.
2011
Part: BATTERY — DISCHARGED (CABIN) · airframe 7,245 hrs · 5,534 cycles
EMERGENCY LIGHTS STUCK ON. RESET EMERGENCY LIGHT POWER UNIT AND CHARGED BATTERIES IAW AMM 33-50-01. MESSAGE CLEARED, LIGHTS OFF.
Part: GIRT BAR — OUT OF ADJUST (L1 DOOR) · airframe 6,705 hrs · 5,152 cycles
L1 DOOR WILL NOT ARM. INSPECTED L1 DOOR AND ADJUSTED DOOR GIRT BAR IAW EMB 170 AMM 52-11-41. OPS CHECK GOOD.
Part: COFFEEMAKER — ODOR (GALLEY) · airframe 5,719 hrs · 4,455 cycles
ON CLIMBOUT, PASSING THROUGH 20,000 FEET, F/A CALLED FLIGHT DECK REPORTING A SMOKY ODOR IN THE AFT GALLEY. THERE WAS NO VISIBLE SMOKE. LEVELED OFF AT FL240, DIVERTED. ATC DECLARED AN EMERGENCY. WHILE STARTING DESCENT, F/A REPORTED THE ODOR HAD DISSIPATED AND THE SOURCE APPEARED TO BE THE AFT COFFEEMAKER WHICH WAS SPILLING COFFEE ONTO THE HOT BURNER PLATE. LANDED WITHOUT INCIDENT. MX RAN BOTH ENGINES WITH APU BLEED OFF AND BOTH PACKS RUNNING TO TAKEOFF POWER AND BACK TO IDLE, THEN ISOLATED THE ENGINE BLEEDS AND RAN PACKS WITH APU BLEED ON FOR 20 MINUTES. NO ODOR NOTED, PLACED COFFEEMAKER ON NEF. THE NEF WAS CLEARED THAT NIGHT WITH AN OPS CHECK GOOD.
2010
Part: SKIN — DENTED (ZONE 200) · airframe 4,637 hrs · 3,674 cycles
DURING BIRD STRIKE INSPECTION FOUND DENT ON NOSE AREA BETWEEN FR1 AND FR2, STR 6L AND STR 2L. CUT OUT DAMAGE AND INSTALLED FILLER AND DOUBLER IAW ETD 2010-170/10396 REV B.
Part: SKIN — CRACKED (VERTICAL STAB) · airframe 3,253 hrs · 2,618 cycles
MAJOR REPAIR - CRACK IN VERTICAL STAB JUST AFT OF RT UPPER HOIST POINT. STOP DRILLED CRACK TIPS AND PERFORMED NDI HFEC INSPECTION TO LOCATE CRACK TIPS IAW EMB 175 SRM 51-10-04. ACCOMPLISHED FINAL REPAIR TO RT SKIN OF VERTICAL STAB IAW ETD 2010-170/02797 REV C.
Part: BATTERY — DISCHARGED (CABIN) · airframe 2,766 hrs · 2,199 cycles
EMERGENCY LIGHT FAULT MESSAGE. MAINTENANCE RESET EMERGENCY LIGHT, OPS TEST GOOD IAW EMB FIM 33-50-00-810-803A. MAINTENANCE LATER REMOVED AND REPLACED THE NR 3 ELPU IAW MM 33-50-01.