N245NN
Registered owner: AMERICAN AIRLINES INC, TX (owner ≠ operator)
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.
56 reports on file, 2017-06-14 – 2026-08-08.
Part: ENGINE — VIBRATION (NR 2) · airframe 24,898 hrs · 16,719 cycles
NR 2 ENG HIGH VIBRATION AT 4.0. NOTICED AFTER 80KTS. STAYED AT 4.0 IN AMBER. LEVELED AT 12000FT TO RUN QRH. AFTER RUNNING QRH STEPS ENG REMAINED 4.O - 4.2 AS WELL AS BEING ABLE TO FEEL A VIBRATION FROM THE ENG2 SIDE. ENG 2 DID RETURN TO GREEN WITH REDUCED THRUST SO WE KEPT IT REDUCED AND RETURNED TO DFW. DURING TAXI IN WE DID SEE A BRIEF RETURN TO 4.1 VIB IN ENG 2. TRANSFERRED TO NRWC 045-DFW-05383 ITEM-1. EMERGENCY DECLARED C/W E2 FAN BLADES AND PINS TROUBLESHOOTING IAW EA72-00-00-012 FOUND PINS NEEDED CHANGED REF NRWC 045-DFW-05384 FOR RAR OF PINS OPC CHECK GOOD HIGHEST VIB WAS 0.3AU @70% N1
Part: DOOR — NO DISCREPANCY (ZONE 800) · airframe 24,105 hrs · 16,110 cycles
GATE AGENT REPORTED L1 DOOR EXTREMELY DIFFICULT TO OPEN PERFORMED INSPECTION OF FORWARD PASSENGER DOOR SUPPORT ARM IAW AMM 52-11-30. NO DEFECTS NOTED. OPERATED DOORS FOR NORMAL FUNCTIONS. OPS CHECK GOOD.
Earlier reports · 2017–2025 · 54 reports
2025
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 22,191 hrs · 14,758 cycles
AFT END OF SEAT TRACK PN 170-99451-003 FOUND TO CORRODED OUT OF LIMITS. (MAJOR REPAIR) (LEVEL 2 CORROSION). REMOVED AND REPLACED DAMAGED SECTION OF RH INBD SEAT TRACK BTW FR 57-60 IAW ERJ 175 SRM 53-00-10 ITEM 6.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 22,191 hrs · 14,758 cycles
GALLEY LH SEAT TRACK CORRODED AT FRAME 16. (MAJOR REPAIR) (LEVEL 2 CORROSION). INSTALLED FABRICATED REPAIR DOUBLER & FILLER ON FWD GALLEY LH SEAT TRACK BEAM AT FR.16 IAW ENVOY ERS-EJ-53MR-5227
Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 22,191 hrs · 14,758 cycles
SHEAR CLIP AT FR 88 STGR 28R-29R CORRODED. R & R SHEAR CLIP AT FR 88 BTW STGR 28R-29R IAW ERJ 175 SRM 51-40-08.
Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 22,191 hrs · 14,758 cycles
FRAME 82 SHEAR CLIP BETWEEN STRINGERS 27-28R IS CORRODED. REMOVED AND REPLACED SHEAR CLIP AT FR 82 BTW STGR 27R-28R IAW SRM 51- 40-08.
Part: SHEAR PANEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 22,191 hrs · 14,758 cycles
AFT GALLEY FLOOR STRUCTURE, THE RH SHEAR PANEL HAS CORROSION AT MULTIPLE LOCATIONS. FR 87-88. SSI 53-23-005.(LEVEL 2 CORROSION). RAR THE AFT GALLEY FLOOR STRUCTURE RH SHEAR PANEL BETWEEN FR 87-88 IAW ERJ 175 SRM 51- 40-08
Part: SHEAR TIE — CORRODED (ZONE 200) · corrosion level 2 · airframe 22,191 hrs · 14,758 cycles
FRAME 82 SHEAR CLIP BETWEEN STRINGERS 28-29R IS CORRODED. REMOVED AND REPLACED SHEAR CLIP AT FR 82 BTW STGR 28R-29R IAW ERJ 175 SRM 51- 40-08
Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 22,191 hrs · 14,758 cycles
FRAME 74 SHEAR CLIP BETWEEN STRINGERS 29R-29L IS CORRODED. REMOVED AND REPLACED SHEAR CLIP AT FR 74 BTW STGR 29R-29L IAW SRM 51- 40-08.
Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 22,191 hrs · 14,758 cycles
AFT GALLEY FLOOR STRUCTURE, THE RH FLOOR BEAM GUSSET HAS CORROSION AT FR 89-90. SSI 53-23-005. (MAJOR REPAIR) (LEVEL 2 CORROSION). RAR THE AFT GALLEY FLOOR STRUCTURE, RH FLOOR BEAM GUSSET AT FR 89-90 IAW ERJ 175 SRM 51-40-08
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 22,191 hrs · 14,758 cycles
AFT GALLEY FLOOR STRUCTURE, THE RH FLOOR SILL HAS CORROSION AT MULTIPLE LOCATIONS. FR 88-90. PREVIOUSLY BLUE PAINTED AREA. SSI 53-23-005. (LEVEL 2 CORROSION). BLENDED TO REMOVE CORROSION ON AFT GALLEY FLOOR STRUCTURE RH FLOOR SILL AT FR 88-90 IAW ERJ 175 SRM 51-10-03. THE CORROSION IS SEVERE AND PART REQUIRES REPLACEMENT. RAR AFT GALLEY FLOOR STRUCTURE, RH FLOOR SILL FR 88-90 IAW ERJ 175 SRM 51-40-08.
Part: SHEAR PANEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 22,191 hrs · 14,758 cycles
AFT GALLEY FLOOR STRUCTURE, THE CENTER SHEAR PANEL HAS CORROSION AT MULTIPLE LOCATIONS. FR 87-88. PREVIOUSLY BLUE PAINTED AREA. SSI 53-23-005. (LEVEL 2 CORROSION). BLENDED TO REMOVE CORROSION ON AFT GALLEY FLOOR STRUCTURE CENTER SHEAR PANEL AT FR 87-88 IAW ERJ 175 SRM 51-10-03. THE CORROSION IS SEVERE AND AND REQUIRES REPLACEMENT. RAR THE AFT GALLEY FLOOR STRUCTURE CENTER SHEAR PANEL BETWEEN FR 87-88 IAW ERJ 175 SRM 51-40-08
Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 22,191 hrs · 14,758 cycles
SSI 53-23-003: FRAME 87 SHEAR CLIP BETWEEN STRINGERS 27-28R IS CORRODED. (LEVEL 2 CORROSION) REMOVED AND REPLACED SHEAR CLIP AT FR 87 STGR 27R-28R IAW ERJ 175 SRM 51-40-08.
Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 22,191 hrs · 14,758 cycles
FRAME 88 IS CORRODED AT STRINGERS 27-28R. (MAJOR REPAIR) REMOVED AND REPLACED FR 88 LOWER SECTION BTW STGR 25R-23L IAW ERJ 175 SRM 51- 40-08.
Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 22,191 hrs · 14,758 cycles
FRAME 84 SHEAR CLIP BETWEEN STRINGERS 27-28R IS CORRODED. REMOVED AND REPLACED SHEAR CLIP AT FR 84 BTW STGR 27R-28R IAW SRM 51- 40-08.
Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 22,191 hrs · 14,758 cycles
SSI 53-23-003: FRAME 87 IS CORRODED AT STRINGERS 27-28R. (MAJOR REPAIR) (LEVEL 2 CORROSION). REMOVED AND REPLACED FR 87 LOWER SECTION BTW STGR 23L-25R IAW ERJ 175 SRM 51-- 40-08
Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 22,191 hrs · 14,758 cycles
AFT GALLEY FLOOR STRUCTURE, THE RH CROSS-BEAM GUSSET HAS CORROSION AT FR90. PREVIOUSLY BLUE PAINTED AREA. SSI 53-23-005. (LEVEL 2 CORROSION). BLENDED TO REMOVE CORROSION ON AFT GALLEY FLOOR STRUCTURE RH CROSS-BEAM GUSSET AT FR90 IAW ERJ 175 SRM 51-10-03. THE CORROSION IS SEVERE, AND PART REQUIRES REPLACEMENT. REMOVED AND REPLACED THE AFT GALLEY FLOOR STRUCTURE RH CROSS- BEAM GUSSET AT FR90 IAW ERJ 175 SRM 51-- 40-08.
Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 22,191 hrs · 14,758 cycles
FRAME 76 SHEAR CLIP BETWEEN STRINGERS 29R-29L IS CORRODED. REMOVED AND REPLACED SHEAR CLIP AT FR 76 BTW STGR 29R-29L IAW SRM 51- 40-08.
Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 22,191 hrs · 14,758 cycles
AFT GALLEY FLOOR STRUCTURE, THE LH FLOOR BEAM HAS CORROSION AT FR 87. SSI 53-23-005. (MAJOR REPAIR) (LEVEL 2 CORROSION). RAR THE AFT GALLEY FLOOR STRUCTURE LH FLOOR BEAM BETWEEN FR 86-89 IAW ERJ 175 SRM 51-40-08
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 22,191 hrs · 14,758 cycles
AFT GALLEY FLOOR STRUCTURE, THE RH FLOOR BEAM HAS CORROSION AT FR 88-- 89. SSI 53-23-005. (MAJOR REPAIR) (LEVEL 2 CORROSION). RAR THE AFT GALLEY FLOOR STRUCTURE RH FLOOR BEAM BETWEEN FR 86-89 IAW ERJ 175 SRM 51-40-08
Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 22,191 hrs · 14,758 cycles
FRAME 86 SHEAR CLIP BETWEEN STRINGERS 27-28R IS CORRODED. REMOVED AND REPLACED SHEAR CLIP AT FR 86 BTW STGR 27R-28R IAW ERJ 175 SRM 51- 40-08.
Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 22,191 hrs · 14,758 cycles
FRAME 85 SHEAR CLIP BETWEEN STRINGERS 27-28R IS CORRODED. REMOVED AND REPLACED SHEAR CLIP AT FR 85 BTW STGR 27R-28R IAW ERJ 175 SRM 51- 40-08.
Part: SHEAR BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 22,191 hrs · 14,758 cycles
AFT GALLEY FLOOR STRUCTURE, THE LH SHEAR PANEL HAS CORROSION AT MULTIPLE LOCATIONS. FR 87-88. PREVIOUSLY BLUE PAINTED AREA. SSI 53-23-005. (LEVEL 2 CORROSION). BLENDED TO REMOVE CORROSION ON AFT GALLEY FLOOR STRUCTURE LH SHEAR PANEL AT FR 87-88 IAW ERJ 175 SRM 51-10-03. THE CORROSION IS SEVERE AND PART REQUIRES REPLACEMENT. RAR THE AFT GALLEY FLOOR STRUCTURE LH SHEAR PANEL BETWEEN FR 87-88 IAW ERJ 175 SRM 51-40-08.
Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 22,191 hrs · 14,758 cycles
SSI 53-23-003: STRINGER 27R HAS CORROSION AT FWD SIDE OF FRAME 87. (MAJOR REPAIR) (LEVEL 2 CORROSION) REMOVED AND REPLACED STGR 27R BTW FR 80-88 IAW ERJ 175 SRM 51-40-08
Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 22,191 hrs · 14,758 cycles
INTERNAL FUSELAGE SKIN DOUBLER IS CORRODED AT INBD SIDE OF WASTE SERVICE BUCKET. REMOVED AND REPLACED INTERNAL FUSELAGE SKIN DOUBLER AT WASTE SERVICE BUCKET IAW SRM 51-40-08.
Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 22,191 hrs · 14,758 cycles
SSI 53-23-003: FRAME 88 SHEAR CLIP BETWEEN STRINGERS 27-28R IS CORRODED. REMOVED AND REPLACED SHEAR CLIP AT FR 88 STGR 27R-28R IAW ERJ 175 SRM 51-40-08.
Part: SEAL REST — CORRODED (ZONE 200) · corrosion level 2 · airframe 22,191 hrs · 14,758 cycles
SSI# 53-21-009 FWD CARGO DOOR CUTOUT FWD CORNER SEAL DEPRESSOR IS GOUGED ON EDGES AND HAS CORROSION AT NUT PLATE HOLE. (MAJOR REPAIR) (LEVEL 2 CORROSION). RAR THE FWD CARGO DOOR CUTOUT FWD CORNER SEAL DEPRESSOR IAW ERJ 175 AMM 20-10-01.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 22,191 hrs · 14,758 cycles
SSI 53-22-012: RH FLOOR BEAM SEAT TRACK OTBD FLANGE HAS MULTIPLE CORROSION SPOTS BETWEEN FR#59-73. (MAJOR REPAIR) (LEVEL 2 CORROSION). RAR RH FLOOR BEAM SEAT TRACK BETWEEN FR#59-73 IAW ERJ 175 SRM 51-40-08
Part: SKIN — GOUGED (WING) · airframe 22,191 hrs · 14,758 cycles
RH & LH WING FIXED L/E SKIN IS GOUGED UPPER SIDE BETWEEN SLAT 2 ; 3 AND 4. (MAJOR REPAIR) REPAIRED RH & LH WING FIXED LEADING EDGE SKIN BETWEEN SLAT 2; 3 AND 4 AND # IAW ERS-EJ-57MR-1718
Part: SEAL REST — CORRODED (ZONE 200) · corrosion level 2 · airframe 22,191 hrs · 14,758 cycles
SSI 53-21-009: FWD CARGO DOOR FUSELAGE CUTOUT LOWER EDGE IS CORRODED AT 2 HOLES. (MAJOR REPAIR) (LEVEL 2 CORROSION). RAR FWD CARGO DOOR FUSELAGE CUTOUT LOWER EDGE (SEAL REST) IAW ERJ 175 SRM 51-40-08.
2022
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 15,339 hrs · 9,946 cycles
FWD PAX DOOR EXIT EMERGENCY LIGHT INOPERATIVE. FOUND FWD PAX DOOR EMERGENCY LIGHT NOT ILLUMINATING AND PASSAGE WAY LIGHTS DIM, RAR ELPU #2 IAW AMM 33-50-01, NO DEFECTS NOTED, OPERATIONAL TEST GOOD.
Part: NONE — CORRODED (FR 86-88) · corrosion level 2 · airframe 14,713 hrs · 9,516 cycles
RH FLOOR BEAM IN AFT GALLEY CORRODED FWD OF FRAME 87.(LEVEL 2 CORROSION)C-C/A-REMOVED AND REPLACED RH FLOOR BEAM IN AFT GALLEY IAW EMB 175 SRM 51-40-08.
Part: NONE — CORRODED (FR19-20) · corrosion level 2 · airframe 14,713 hrs · 9,516 cycles
FWD GALLEY CENTER LOWER SEAT TRACK CORRODED AT FWD END. (LEVEL 2 CORROSION) (MAJOR REPAIR) -C/A-PERFORMED PERMANENT REPAIR TO FWD GALLEY CENTER LOWER SEAT TRACK AT FWD END IAW ERS-EJ-53MR-4635.
Part: SEAT TRACK — CORRODED (FR 84) · corrosion level 2 · airframe 14,713 hrs · 9,516 cycles
AFT GALLEY LH FLOOR BEAM CORRODED AT FRAME 84. (LEVEL 2 CORROSION) (MAJOR REPAIR) -C/A-PERFORMED PERMANENT REPAIR TO AFT GALLEY LH FLOOR BEAM IAW EMB 175 SRM 53-23-10/ REPAIR 04P.
Part: NONE — CORRODED (FR86-88) · corrosion level 2 · airframe 14,713 hrs · 9,516 cycles
AFT GALLEY RH FLOOR SHEAR PANEL CORRODED. (LEVEL 2 CORROSION)-C/A-REMOVED AND REPLACED AFT GALLEY RH FLOOR SHEAR PANEL IAW EMB 175 SRM 51-40-08.
Part: NONE — CORRODED (FR 17-18) · corrosion level 2 · airframe 14,713 hrs · 9,516 cycles
FWD GALLEY RH LOWER SEAT TRACK CORRODED FWD END. (LEVEL 2 CORROSION) -C/A-PERFORMED PERMANENT REPAIR TO FWD GALLEY RH LOWER SEAT TRACK IAW ERS-EJ-5300-4626.
Part: NONE — CORRODED (FR12-14) · corrosion level 2 · airframe 14,713 hrs · 9,516 cycles
RH FLOOR SILL IN FWD GALLEY CORRODED AT FR 13, 14. (LEVEL 2 CORROSION)-C/A-REMOVED AND REPLACED RH FLOOR SILL IN FWD GALLEY IAW EMB 175 SRM 51-40-08
Part: UPPER SHEET — CORRODED (TOP OF SHEET FR) · corrosion level 2 · airframe 14,713 hrs · 9,516 cycles
AFT GALLEY FLOOR RH UPPER SHEET AT FRAM 86 IS CORRODED. (LEVEL 2 CORROSION) -C/A-REMOVED AND REPLACED AFT GALLEY FLOOR RH UPPER SHEET AT FR 86 IAW EMB 175 SRM 51-40-08.
Part: NONE — CORRODED (FR 84-85) · corrosion level 2 · airframe 14,713 hrs · 9,516 cycles
RH SEAT TRACK IN AFT GALLEY FRAME 84 IS CORRODED. (LEVEL 2 CORROSION) -C/A- PERFORMED PERMANENT REPAIR TO RH SEAT TRACK IN AFT GALLEY FRAME 84 IAW ERS-EJ-5300-4628.
Part: NONE — NONE (FR 19) · airframe 14,713 hrs · 9,516 cycles
FWD PAX DOOR CUTOUT CHAFED IN 3 PLACES ON AFT EDGE. (LEVEL 2 CORROSION) ( MAJOR REPAIR) -C/A-PERFORMED PERMANENT REPAIR TO FWD PAX DOOR CUTOUT AFT EDGE IAW EMB 175 SRM 53-10-21/REPAIR 01P.
Part: NONE — CRACKED (RH) · airframe 14,713 hrs · 9,516 cycles
RH WING SPAR 1 OUTBD END CRACKED. (MAJOR REPAIR) -C/A-REMOVED AND REPLACED RIGHT WING SPAR 1 OUTBD END IAW EMB 175 SRM
Part: NONE — CRACKED (L/H) · airframe 14,713 hrs · 9,516 cycles
LH WING SPAR 1 OUTBD END CRACKED.(MAJOR REPAIR) -C/A-REMOVED AND REPLACED LEFT WING SPAR 1 OUTBD END IAW EMB 175 SRM 51-40-08
Part: LIGHT — DAMAGED (CABIN) · airframe 14,713 hrs · 9,516 cycles
LH #3 PHOTO LUMINESCENT EMERGENCY FLOOR STRIP DAMAGED-C/A-COMPLETE:RAR LH #3 PHOTO LUMINESCENT STRIP IAW EMB 175 AMM 33-50-21
2021
Part: LIGHT — WORN (CABIN) · airframe 12,083 hrs · 7,810 cycles
FIRST FWD LH EMERGENCXY PHOTOLUMINESCENT STRIP WORN-C/A-RAR WORN FIRST FWD LH EMERGENCY PHOTOLUMINESCENT STRIP IAW AMM 33-50-21. NO FURTHER DEFECT NOTED
Part: RADIO ALTIMETER — MALFUNCTIONED (NR 1) · airframe 11,030 hrs · 7,131 cycles
AT 11000 FT. LANDING GEAR AURAL WARNING CONTINOUS COULD NOT BECANCELED CAS RADIO ALTIMETER SHOWED ZERO FT PUT GEAR DOWN TO SILENCE NO AURAL ALT ALERTS ON FINAL.-C/A-NO.1 RAD ALT DEFERRED PER MEL 34-15 AUTHNO. 040621M-C M PROCEDURED CW
Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 10,401 hrs · 6,765 cycles
ROW 3 EMERGENCY LIGHTS INOPERABLE. C/A: R & R EMERGENCY LIGHT POWER UNIT 2, IAW AMM 33-50-01. OPERATIONS CHECK GOOD. NO FURTHER DEFECT NOTED.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,318 hrs · 6,715 cycles
FIRST FWD EMERGENCY LIGHT INOPERABLE. C/A: FOUND FIRST FWD EMERGENCY LIGHT INOPERABLE. R & R LIGHT IAW AMM 33-50-13. NO FURTHER DEFECTS NOTED.
2020
Part: WARNING MESSAGE — FALSE ACTIVATION (MLG) · airframe 9,983 hrs · 6,516 cycles
LG LEVER DISAGREE MESSAGE ON APPROACH GEAR THEN CAME DOWN, FOLLOWED QRH AND CYCLED LANDING GEAR LEVER, GEAR CYCLED NORMALLY DECLARED EMERGENCY. CFR RESPONDED. C/A: R & R LANDING GEAR LEVER, IAW E175 AMM 32-33-01. PERFORMED OPERATIONAL CHECK, IAW E175 AMM 32-33-00. OPERATIONAL CHECK GOOD, NO DEFECTS FOUND.
2019
Part: ARMING LEVER — LACK OF LUBE (R2 DOOR SLIDE) · airframe 7,950 hrs · 5,214 cycles
DOOR 2R ESCAPE SLIDE WINDOW DOES NOT INDICATE "ARMED" WHEN THE HANDLE IS IN THE ARMED POSITION.-C/A-PERFORMED GVI OF DOOR LINKAGE. NO DEFECTS NOTED . LUBED ARMING LEVER LINKAGE , OPENED AND CLOSED DOOR. OPS CHECKS GOOD. REF. AMM 52-41-22
Part: GIRT BAR — BINDING (R1 DOOR SLIDE) · airframe 7,952 hrs · 5,216 cycles
THE SLIDE ARMING LEVER ON DOOR1R IS DIFFICULT TO MOVE INTO THE ARMED POSITION-C/A-INSPECTED FOUND DEBRIS IN GIRT BAR CATCH ON THE FLOOR CLEANNED AND REMOVED DEBRIS, PERFORMED OPERATIONAL CHECK OF THE R1 DOOR IAW SDS 52-41-00
Part: ATTACH FITTING — CRACKED (LT WING) · airframe 7,496 hrs · 4,916 cycles
LT ENHACED WINGTIP SPAR 1 ATTACHMENT FITTING CRACKED. FOUND ON OPEN UP. C/A-REMOVED AND REPLACED LT ENHANCED WINGTIP SPAR 1 ATTACHMENT FITTING IAW ERS-EJ-57MR-1151 PART A.
Part: ATTACH FITTING — CRACKED (RT WING) · airframe 7,496 hrs · 4,916 cycles
RT ENHANCED WINGTIP SPAR 1 ATTACHMENT FITTING CRACKED. FOUND ON OPEN UP. C/A-REMOVED AND REPLACED RT ENHANCED WINGTIP SPAR1 ATTACHMENT FITTING IAW ERS-EJ-57MR-1151 PART B.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,496 hrs · 4,916 cycles
CABIN FWD 2 EMERGENCY LIGHT STRIPS REQUIRE REPLACEMENT-C/A-COMPLETE:REMOVED REPLACED CABIN FWD W EMERGENCY LIGHT STRIPS IAW EMB 175 AMM 33-50-21. OPS CHECK GOOD.
Part: SLIDE — DISLODGED (L1 DOOR) · airframe 6,925 hrs · 4,540 cycles
MAIN PAX DOOR OPEN PRIOR TO THE DOOR BEING DISARM /SLIDE DID NOT DEPLOY BUT WAS POPPED OUT OF DOOR HANGING DOWN. DEPLOYED L1 DOOR SLIDE REMOVED FROM AIRCRAFT DEFLATE SLIDE PRESSURE IAW EMB-175 AMM 25-65-01 SEE ITEM 3 FOR FERRY FLIGHT
2018
Part: ROD — BROKEN (FLAP SYSTEM) · airframe 3,767 hrs · 2,450 cycles
EXCESSIVE RIGHT AILERON INPUT REQUIRED WITH FLAPS EXTENDED. MORE INPUT REQUIRED AS MORE FLAPS DEPLOYED. ON INSPECTION OF FLIGHT CONTROLS IAW AMM 57-00-00-06, FOUND THE LT FLAP (INBD AND OTBD) TUBE ASSYS BROKEN. REPLACED SCREW IAW SMP 20-10-07. FOUND THE LT OTBD FLAP INBD UPPER AND OTBD UPPER ROD ASSY BROKEN IN HALF. REMOVED AND REPLACED THE ROD ASSY IAW AMM 57-57-40. OPS CHECKED GOOD IAW AMM 27-50-000. NO OTHER DEFECTS FOUND
2017
Part: BLADE — DAMAGED (ENGINE) · airframe 1,423 hrs · 915 cycles
NR 2 ENGINE LP VIBRATION WENT AMBER AT 4.0 AND 34000FT. COMPLIED WITH N1 VIBRATION WORKSCOPE ON RT ENGINE IAW MM 72-00-00 SPECIAL PROCEDURE 097. MAX LP VIBRATION LEVEL NOW 1.5 AU. DURING ACCOMPLISHEMENT OF N1 VIBRATION WORKSCOPE ON RT ENGINE, FOUND BASE COAT MISSING FROM ID OF FAN BLADE RETAINING PIN HOLES ON NUMEROUS BLADES. PERFORMED REPLACEMENT OF ENTIRE RT ENGINE FAN BLADE SET IAW MM 72-00-00 SPECIAL PROCEDURE 094.