N298FR
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.
10 reports on file, 2022-01-23 – 2026-08-02.
Part: SKIN — DENTED (ZONE 200) · airframe 15,609 hrs · 10,731 cycles
FUSELAGE DENT AFT OF FWD PASSENGER DOOR BETWEEN FRAMES 20 AND 21, BETWEEN STGRS 11L AND 12L. (MJOR REPAIR) COMPLIED WITH HIDDEN DAMAGE INSPECTION OF AREA IAW EAMS QCM 1.16 REV 50. NO ADDITIONAL DEFECTS NOTED. CUT & REMOVED DAMAGE SPOT IN THE SKIN AT FR 20 - FR 21 STR 11L - 12L REF ETD2026-170-013290 REV . LOCATED DRILLED, DEBURRED & COUNTERSUNK REPAIR DOUBLER AND FILLER REF ETD2026-170-013290 REV.: A. TREATED REPAIR DOUBLER AND FILLER AND CUTOUT OF SKIN IAW SRM 51- 23-04 AND ETD2026-170-013290 REV.: A, PRIMED REPAIR DOUBLER AND FILLER AND CUT OUT OF SKIN IAW SRM 51-23-05, ETN-EJ-051-025 & ETD2029-170-013290 REV.A. FILLET SEALED AROUND REPAIR DOUBLER IAW ETD2026-170-13290 REV B. CLEANED, PREPPED, PRIMED AND RESTORED FINISH IAW SRM 51-23-06, ETN-EJ-51-015. INSTALLED FUSELAGE REPAIR DOUBLER AT FR 20 - FR21 AT STRG 11L - 12L REF ETD2026-170-013290 REV.: B.
Part: CROSSBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,408 hrs · 10,582 cycles
LEVEL 2 CORROSION FRAME 87 CROSS BEAM HAS CORROSION AROUND 1EA FASTENER HOLE. (LVL 2 CORROSION) (MAJOR REPAIR) BLENDED CORROSION ON FRAME 87 CROSS BEAM IAW E-175 SRM 51-10-03. ORIGINAL THICKNESS .098" IAW EMBRAER DRAWING #170-86056-003. MATERIAL REMOVED .055" MATERIAL REMAINING .043" FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRM 51-75-16. CUT AND REMOVED DAMAGE OF CROSS BEAM FR 87 REF ETD2026-170-010539 REV.: A. FABRACATED, DRILLED AND DEBURED REPAIR DOUBER L ANGLE REPAIR FILLERS AND REPAIR SHIM REF ETD2026-170-00539 RE V.: B. TREATED ALL REPAIR SHIMS. DOUBLER, ANGLE, FILLER, AND CROSS BEAM CUT OUT REF ETD2026-170-00539 REV.: B. PRIMED ALL REPAIR SHIMS, DOUBLER, ANGLE, FILLE R, AND CROSS BEAM CUT OUT REF ETD2026- 170-00539 REV.: B USING TOP COATED ALL REPAIR SHIMS, DOUBLER, ANGLE, FILLER, AND CROSS BEAM CUTOUT REF2026-170-00539 REV.: B. INSTALLED REPAIR PER: ETD2026-170-00539 REV.: B. APPLIED TOPCOAT PER: SRM 51-23- 06 AND ETN-EJ-51-003. APPLIED CIC PER: CPM PART1-51-25-00-910-001-A. TOPCOAT: P/N EC L-G-46. REPAIRED FRAME 87 CROSS BEAM LT SIDE REF ETD2026-170-00539 REV: B. (LEVEL 2 CORROSION) (MAJOR REPAIR)
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,408 hrs · 10,582 cycles
SSI 53-10-027-0392 LEVEL 2 CORROSION CORROSION AT FWD PASSENGER FLOOR STRUCTURE WET AREAS RH SEAT TRACK FROM FR 16 TO FR 18 Y = +273. (LVL 2 CORROSION) (MAJOR REPAIR) BLENDED CORROSION AT FWD PASSENGER FLOOR STRUCTURE WET AREAS RH TRACK FROM FR 16 TO FR 18 Y = +273 PER EMB 175 SRM 51-10-03, FOUND AREA DEPTH TO MEASURE .120" ORIGINAL MATERIAL THICKNESS IS .295" REMAINING MATERIAL IS .175? MAXIMUM ALLOWED IS .007? AND IS OUT OF LIMITS PER EMB 175 SRM 53-10-10/AD01. LOCATED, DRILLED, DEBURRED AND COUNTERSUNK R/H FWD SEAT TRACK FROM FR 16 TO FR 18 Y+273" IAW EMB 175 SRM 51-40-02 AND EMB 175 SRM 51-40-04. P/N170-03263-001. APPLIED TOPCOAT PER: EMB 175 SRM 51-23-06 AND ETN-EJ-51-003. APPLIED CIC PER: EMB 175 CPM PART1-51-25-00-910-001-A. REMOVED AND REPLACED FWD PASSENGER FLOOR STUCTURE RH SEAT TRACK FR12 - FR20 @Y=+273 IAW E175-SRM 51-40-08. (LEVEL 2 CORROSION) (MAJOR REPAIR)
Part: BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,408 hrs · 10,582 cycles
LEVEL 2 CORROSION RH BEAM HAS CORROSION AT FR 87 Y + 13. (LVL 2 CORROSION) (MAJOR REPAIR) RT BEAM HAS CORROSION AT FR 87 Y + 13 BLENDED CORROSION ON RH BEAM AT FR 87 Y+ 13" IAW E-175 SRM 51-10-03. MATERIAL REMOVED .070" MATERIAL REMAINING .0" OUT OF ALLOWABLE LIMITS IAW E-175 SRM 51-75-16. PN 170-65669-004 LOCATED, DRILLED, DEBURED, TREATED AND PRIMED NEW RH BEAM IAW E-175 SRM 51-40-02 SRM 51-23-04 SRM 51-23-05 AND ETN-EJ-51-025. RESTORED FINISH IAW SRM 51-23-06, ETN-EJ-51-015. APPLIED CIC IAW CPM 51-25-00. REMOVED AND REPLACED RT BEAM AT FR 87 Y+13" IAW E-175 SRM 51-40-08. LEVEL 2 CORROSION
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,408 hrs · 10,582 cycles
LEVEL 2 CORROSION RH SEAT TRACK HAS CORROSION ON AFT END BETWEEN FR 84 - 85 AND Y + 11? (LVL 2 CORROSION) (MAJOR REPAIR) CORROSION ON RH SEAT TRACK AFT END BETWEEN FR 84 - 85 AND Y + 11" 100% MATERIAL LOSS REMOVED DAMAGED SEAT TRACK SEGMENT FROM AFT R/H SEAT TRACK BETWEEN FR-83 AND FR-84 PER EMB-175 SRM 53-00- 10/REPAIR01 AND ETN-EJ-53-012. FABRICATED, LOCATED, AND DRILLED 4EA REPAIR DOUBLERS FOR AFT R/H SEAT TRACK SPLICE PER EMB-175 SRM 53-00-10/REPAIR 01 AND ETN-EJ-53-012. FABRICATED, LOCATED, DRILLED, AND DEBURRED FASTENER HOLES ON NEW R/H SEAT TRACK SEGMENT PER EMB-175 SRM 53- 00-10/REPAIR01 AND ETN-EJ-53-012. RESTORED FINISH TO AFT R/H SEAT TRACK SPLICE AND REPAIR PARTS PER EMB-175 SRM 51-23-04, 51-23-05, 51-23-06, ETN-EJ-51- 015, AND ETN EJ-51-025. INSTALLED NEW R/H SEAT TRACK SEGMENT AND REPAIR PARTS PER EMB-175 SRM 53-00-10/REPAIR01 AND ETN-EJ-53-012, SRM 51-40-08. REPAIRED RH SEAT TRACK AT FR 84 - 85 AND Y + 11" EMB-175 SRM 53-00-10/REPAIR 01 AND ETN-EJ-53-012.
Part: DISCONNECT UNIT — FAILED (ZONE 100) · airframe 15,168 hrs · 10,410 cycles
AOA PITCH TRIM DISCONNECT. FELT SPRING AND HEARD SPRINGS POP FOLLOWED BY AOA LIMIT FAIL CAUTION MESSAGE.EMERGENCY DECLARED. LANDED NO ISSUES. RAR CONTROL COLUMN DISCONNECT DEVICE IAW AMM 27-11-01. OPS CHECK GOOD.
Part: POWER SUPPLY — INOPERATIVE (ZONE 200) · airframe 14,745 hrs · 10,102 cycles
WHILE PERFORMING EMERGENCY LIGHTS POWER UNIT OPPS CHECK, FOUND UNIT TWO NOT HOLDING CHARGE FOR 15 MINUTES. RAR ELPU #2 (FWD LH) IAW AMM 33-50-01. OPS CHECK OF EMERGENCY LIGHTS GOOD IAW AMM 33-50-00. REFER TO NRWC 098-CMH-03074 FOR PARTS TRANSACTION.
Part: LIGHT — DAMAGED (CABIN) · airframe 7,497 hrs · 5,042 cycles
CABIN FLOOR LH EMERGENCY PHOTOLUMINESCENT INDICATOR STRIP BETWEEN FM 19 AND FM 29 ARE DAMAGED (DOES NOT ILLUMINATE IN PLACES)-C/A-COMPLETE:RAR EMERGENCY CABIN FLOOR LH PHOTOLUMINESCENT INDICATOR STRIP BETWEEN FM 19 AND FM 29 IAW ERJ175 AMM 33-50-21.
Part: LIGHT — DAMAGED (CABIN) · airframe 7,497 hrs · 5,042 cycles
CABIN FLOOR RH EMEREGENCY PHOTOLUMINESCENT INDICATOR STRIP BETWEEN FM 17 AND FM 19 ARE DAMAGED (DOES NOT ILLUMINATE IN PLACES)-C/A-COMPLETE:RAR CABIN FLOOR RH EMEREGENCY PHOTOLUMINESCENT INDICATOR STRIP BETWEEN FM 17 AND FM 19 IAW ERJ175 AMM 33-50-21.
Part: NONE — NONE · airframe 3,135 hrs · 2,024 cycles
LAV SMOKE EICAS MSG AT GATE NO PAX IN LAV-C/A-PERFORMED OPS TEST OF FWD AND AFT LAV SMOKE DETECTORS OPS CHECK GOOD IAW ERJ175 AMM 26-14-01 A/C OK FOR SERVICE