N273NN
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.
23 reports on file, 2019-10-31 – 2026-08-04.
Part: ENGINE — POWER LOSS (NR 1) · airframe 19,558 hrs · 13,119 cycles
REJECTED T/O DUE TO ASYMMETRIC THRUST. TAKEOFF THRUST WAS SET AT TOGA TO START ROLL. NR 1 THRUST LEVER WAS SUBSEQUENTLY PUSHED THROUGH THE DETENT INADVERTENTLY. TO1 RSV WAS ACTIVATED. THRUST DIFFERENTIAL OF AROUND 7% N1 OBSERVED. DECISION MADE TO REJECT AS PM CALLED 80. NO ABNORMAL BRAKE INDICATIONS. MAX SPEED APPROX 83 KIAS. ENG TLA NOT TOGA EICAS MESSAGE ANNUNCIATED AND CLEARED. MAINTENANCE REQUEST ETN-EJ-72-001 APR EVENT DATA COLLECTION & ENGINE LIFING UPDATE BE COMPLETED. C/W ETN-EJ-72-001 NO ENGINE EXCEEDANCE RECORDED OK FOR SERVICE.
Part: SIGN — INOPERATIVE (ZONE 200) · airframe 18,861 hrs · 12,639 cycles
AFT SERVICE DOOR LOWER EMERGENCY EXIT LIGHT INOP RAR AFT SERVICE DOOR LOWER EXIT IDENTIFIER SIGN IAW AMM 33-50-15. OPC GOOD. NO FURTHER DEFECTS NOTED
Part: SIGN — INOPERATIVE (ZONE 200) · airframe 18,187 hrs · 12,182 cycles
R2 DOOR BOTTOM EMERGENCY INDICATOR EXIT LIGHT IS INOPERATIVE. REMOVED R2 EMERGENCY INDICATOR EXIT SIGN FROM MOUNT AND CHECKED CONNECTORS. OPS TESTED OK. REINSTALLED EXIT SIGN IAW AMM 33-50-15.
Part: SLAT SYSTEM — MULTIPLE FAIL · airframe 17,997 hrs · 12,059 cycles
SHAKER ANTICIPATED, AOA LIMIT FAIL, SLAT FAIL, SPDBRK FAIL EICAS MESSAGES APPEARED DURING APPROACH. QRH PROCEDURE FOLLOWED. MESSAGES CLEARED. WORK SCOPE FOR SLAT FAIL EVENT PER FIM 27-81-00-810-802-A BLOCK DIAGRAM 2 EXTENDED SLATS/FLAPS TO POSITION 4 AND DEACTIVED IAW AMM 27-53-01 FOR FERRY FLIGHT. REVERSED M PRECEDURES.PERFORMED OPS CHECK OF THE SLAT CONTROL SYSTEM CHECKED GOOD IAW AMM 27-80-00-710-801-A. C/W WORKSCOPE. PERFORMED INSPECTION OF EACH SLAT ACTUATORS TORQUE LIMITER TRIP INDICATORS.NO TRIPPED INDICATORS FOUND.IAW ERJ AMM 27-81-01-210-801-A.
Earlier reports · 2019–2025 · 19 reports
2025
Part: BATTERY — INOPERATIVE (ZONE 200) · airframe 16,936 hrs · 11,320 cycles
INTERIOR COCKPIT EMERGENCY LIGHTS INOP REMOVED AND REPLACED EMERGENCY LIGHT POWER UNIT IAW EMB 175 AMM 33-50-01. OPS CHK PASS. MEL RESTORED.
Part: UNKNOWN — ODOR (CABIN) · airframe 15,130 hrs · 10,048 cycles
FLIGHT ATTENDANT REPORTS BURNING ELECTRICAL SMELL FROM THE AFT GALLEY AREA; RETURNED TO GATE. COULD NOT DETECT SMELL AFTER RETURN TO GATE. PROCEEDED TO PERFORM HIGH POWER ENGINES WITH BOTH BLEEDS AND PACKS ON. COULD NOT DETECT SMELL. INSPECTED AFT GALLEY AREA, NO DEFECTS NOTED. AFTER ENGINE RUNS PERFORMED FIM TASK 21-20-00-810-801-A FOR ABNORMAL SMELL IN CABIN AS APPLICABLE. NO DEFECTS NOTED. RETURNING AIRCRAFT TO SERVICE. - SEE ALSO AML 114500215 ITEM 1
2024
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 14,675 hrs · 9,731 cycles
RH SEAT TRACK, BETWEEN FR84 AND FR85, @ STGR 17, Y=+10.748? IS CORRODED. (LEVEL 2 CORROSION). RH SEAT TRACK BETWEEN FR84 AND FR85 AT STGR 17, Y+10.748? CORROSION FOUND TO BE OUT OF ALLOWABLE LIMITS PER EMB175 SRM 53-23-10. CUT AND REMOVED DAMAGED PORTION OF RH AFT SEAT TRACK BETWEEN FR84 AND FR85 IAW EMB175 SRM 53-00-10. LOCATED, DRILLED, AND FABRICATED 4EA DOUBLERS FOR REPAIR SPLICE FOR RH SEAT TRACK BETWEEN FR84 AND FR85 PER EMB175 SRM 53-00-10. LOCATED, DRILLED, DEBURRED, TREATED AND PRIMED FASTENER HOLES ON NEW REPAIR SPLICE SEGMENT OF NEW RH SEAT TRACK PN 170-86082-005 PER EMB175 SRM 53-00-10, 51-23-04, AND 51-23-05. RESTORED FINISH ON RH SEAT TRACK REPAIR AS REQUIRED PER EMB175 SRM 51-53-06, ETN EJ-51-015, AND CPM 51-25-00
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 14,675 hrs · 9,731 cycles
RH SEAT TRACK, BETWEEN FR84 AND FR85, @ STGR 17, Y=+10.748? IS CORRODED (MAJOR REPAIR) (LEVEL 2 CORROSION). RH SEAT TRACK BETWEEN FR84 AND FR85 AT STGR 17, Y+10.748? CORROSION FOUND TO BE OUT OF ALLOWABLE LIMITS PER EMB175 SRM 53-23-10. CUT AND REMOVED DAMAGED PORTION OF RH AFT SEAT TRACK BETWEEN FR84 AND FR85 IAW EMB175 SRM 53-00-10. LOCATED, DRILLED, AND FABRICATED 4EA DOUBLERS FOR REPAIR SPLICE FOR RH SEAT TRACK BETWEEN FR84 AND FR85 PER EMB175 SRM 53-00-10. LOCATED, DRILLED, DEBURRED, TREATED AND PRIMED FASTENER HOLES ON NEW REPAIR SPLICE SEGMENT OF NEW RH SEAT TRACK PN 170-86082-005 PER EMB175 SRM 53-00-10, 51-23-04, AND 51-23-05. RESTORED FINISH ON RH SEAT TRACK REPAIR AS REQUIRED PER EMB175 SRM 51-53-06, ETN EJ-51-015, AND CPM 51-25-00
Part: SEAT TRACK — CORRODED (RH SEAT TRACK) · corrosion level 2 · airframe 14,675 hrs · 9,731 cycles
RH SEAT TRACK, BETWEEN FR84 AND FR85, @ STGR 17, Y=+10.748? IS CORRODED. (MAJOR REPAIR) (LEVEL 2 CORROSION). RH SEAT TRACK BETWEEN FR84 AND FR85 AT STGR 17, Y+10.748? CORROSION FOUND TO BE OUT OF ALLOWABLE LIMITS PER EMB175 SRM 53-23-10. CUT AND REMOVED DAMAGED PORTION OF RH AFT SEAT TRACK BETWEEN FR84 AND FR85 IAW EMB175 SRM 53-00-10. LOCATED, DRILLED, AND FABRICATED 4EA DOUBLERS FOR REPAIR SPLICE FOR RH SEAT TRACK BETWEEN FR84 AND FR85 PER EMB175 SRM 53-00-10. LOCATED, DRILLED, DEBURRED, TREATED AND PRIMED FASTENER HOLES ON NEW REPAIR SPLICE SEGMENT OF NEW RH SEAT TRACK PN 170-86082-005 PER EMB175 SRM 53-00-10, 51-23-04, AND 51-23-05. RESTORED FINISH ON RH SEAT TRACK REPAIR AS REQUIRED PER EMB175 SRM 51-53-06, ETN EJ-51-015, AND CPM 51-25-00.
Part: CONTROL CABLE — DAMAGED (ZONE 800 SLIDE) · airframe 14,675 hrs · 9,731 cycles
L2 DOOR EMERGENCY SLIDE MECHANISM CABLE IS DAMAGED AND MIGRATING REMOVED AND REPLACED WITH NEW L2 DOOR EMERGENCY SLIDE MECHANISM CABLE AND ADJUSTED CABLE IAW EMB175 AMM 52-12-40. EMERGENCY OPENING SYSTEM ADJUSTMENT CHECKED GOOD IAW EMB175 AMM 52-12-52
Part: CONTROL CABLE — DAMAGED (ZONE 800) · airframe 14,675 hrs · 9,731 cycles
R2 DOOR EMERGENCY SLIDE MECHANISM CABLE IS DAMAGED AND IS MIGRATING REMOVED AND REPLACED R2 DOOR EMERGENCY SLIDE MECHANISM CABLE PN 170-84631-403 IAW EMB175 AMM 52-42-40. EMERGENCY DOOR OPENING SYSTEM CHECKED GOOD PER EMB175 AMM 52-42-40.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 14,675 hrs · 9,731 cycles
RH SEAT TRACK, BETWEEN FR84 AND FR85, @ STGR 17, Y=+10.748? IS CORRODED. (LEVEL 2 CORROSION) RH SEAT TRACK BETWEEN FR84 AND FR85 AT STGR 17, Y+10.748? CORROSION FOUND TO BE OUT OF ALLOWABLE LIMITS PER EMB175 SRM 53-23-10. CUT AND REMOVED DAMAGED PORTION OF RH AFT SEAT TRACK BETWEEN FR84 AND FR85 IAW EMB175 SRM 53-00-10. LOCATED, DRILLED, AND FABRICATED 4EA DOUBLERS FOR REPAIR SPLICE FOR RH SEAT TRACK BETWEEN FR84 AND FR85 PER EMB175 SRM 53-00-10. LOCATED, DRILLED, DEBURRED, TREATED AND PRIMED FASTENER HOLES ON NEW REPAIR SPLICE SEGMENT OF NEW RH SEAT TRACK PN 170-86082-005 PER EMB175 SRM 53-00-10, 51-23-04, AND 51-23-05. RESTORED FINISH ON RH SEAT TRACK REPAIR AS REQUIRED PER EMB175 SRM 51-53-06, ETN EJ-51-015, AND CPM 51-25-00.
Part: CONTROL CABLE — DAMAGED (R1 SLIDE) · airframe 14,675 hrs · 9,731 cycles
R1 DOOR EMERGENCY SLIDE MECHANISM CABLE IS DAMAGED AND IS MIGRATING. REMOVED, REPLACED AND ADJUSTED R1 DOOR EMERGENCY SLIDE MECHANISM CABLE PN 170-84031-403 IAW EMB175 AMM 52-41-40. DOOR OPENING CHECKED GOOD IAW EMB175 AMM 52-41-52
Part: FLAP SYSTEM — FAULTED · airframe 12,952 hrs · 8,512 cycles
FLAP OVRSPEED. FLAPS 1 EXCEEDANCE + 3 KNOTS MAX 2 SECONDS DURATION DURING LLWS CONDITIONS ON APPROACH PERFORMED INITIAL EVALUATION OF FLAP CW TASK CARD 05-50-07-200-801 SUBTASK 710-004-A. NO ACTIVE MESSAGES ON EICAS. AIRCRAFT OK FOR SERVICE. NO DAMAGE NOTED.
2023
Part: WIRE HARNESS — DAMAGED (SLAT SYS) · airframe 9,776 hrs · 6,251 cycles
DECLARED AN EMERGENCY INTO ORD FOR A SLAT ISSUE. FLT LANDED SAFELY -C/A-RAR RH WING #4 SLAT HARNESS IAW ERJ 175 AMM 27-83-07. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED.
2022
Part: SPAR — CRACKED (LH) · airframe 7,493 hrs · 4,722 cycles
LEFT WINGLET IS CRACKED ON THE FWD SPAR RADIUS.-C/A-COMPLETE:INSTALLED SERVICEABLE RH WINLET IAW AMM 57-30-00. REF NRTC:E910621
Part: SPAR — CRACKED (RH) · airframe 7,493 hrs · 4,722 cycles
RIGHT WINGLET IS CRACKED ON THE FWD SPAR RADIUS-C/A-COMPLETE:INSTALLED SERVICEABLE RH WINLET IAW AMM 57-30-00. REF NRTC:E910621
Part: SPAR — CRACKED (LH) · airframe 7,493 hrs · 4,722 cycles
LEFT WINGLET IS CRACKED ON THE FWD SPAR RADIUS.-C/A-COMPLETE:REF BOW360562 FOR REPAIR OF LH WINGLET FWD SPAR. INSTALLED SERVICEABLE LH WINLET IAW AMM 57-30-00. REF NRTC:E910621 FOR AERODYNAMIC SEALANT.
Part: SPAR — CRACKED (RH) · airframe 7,493 hrs · 4,722 cycles
RIGHT WINGLET IS CRACKED ON THE FWD SPAR RADIUS.-C/A-COMPLETE:INSTALLED SERVICEABLE RH WINLET IAW AMM 57-30-00. REF NRTC:E910621
Part: NONE — NONE · airframe 7,043 hrs · 4,431 cycles
AFT FLIGHT ATTENDENT FLASHLIGHT INOP-C/A-RAR FLASHLIGHT ASSEMBLY PER AMM 33-51-01. OPC GOOD. NO FURTHER DEFECT NOTED
2021
Part: NONE — NONE · airframe 6,913 hrs · 4,357 cycles
RIGHT INBOARD BRAKE OVERHEAT 450 DECLARED EMERGENCY CFR INSPECTED AIRCRAFT.-C/A-RAR RIGHT INBOARD BRAKE TEMPRATURE SENSOR IAW ERJ-175 AMM 32-47-01. AND FIM32-40-00-810-A00. OPC GOOD. NO FUTHER DEFECT NOTED.
Part: NONE — NONE · airframe 6,491 hrs · 4,099 cycles
FOUND BOTH EMERGENCY PHOTOLUMINESCENT STRIPS IN FRONT OF WARDROBE WORN-C/A-RAR WORN EMERGENCY PHOTOLUMINESCENT STRIPS IAW AMM 33-50-21. NO FURTHER DEFECTS NOTED
2019
Part: POWER UNIT — INOPERATIVE (CABIN) · airframe 1,823 hrs · 1,187 cycles
FOUND EMERGENCY LIGHT ABOVE SEAT 2A INOP-C/A-REMOVED AND REPLACED EMERGENCY LIGHT POWER UNIT #2 IAW AMM 33-50-01,NO FURTHER DEFECTS NOTED, OPERATIONAL TEST GOOD.