N220NN
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, 2018-06-27 – 2024-07-06.
Part: SENSOR — FAILED (NLG STEERING) · airframe 21,446 hrs · 14,502 cycles
STEER FAIL CAUTION/QRH NO CLEAR/ EMERGENCY DECLARED NML LDING TOWED NO STEERING. REMOVED AND REPLACED NWS FB SENSOR 1 IAW AMM CH 32-53-09, RIG/ OPS CHK OK IAW 32-53-09
Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,019 hrs · 14,212 cycles
EMERGENCY PHOTOLUMINESCENT FLOOR STRIPS 1 AND 2 ON RH SIDE OF PASSENGER CABIN INOP RAR PHOTOLUMINESCENT EMERGENCY FLOOR STRIPS 1 AND 2 ON RH SIDE OF PASSENGER CABIN IAW AMM 33-50-21, SEE NRWC E032276 FOR EMERGENCY FLOOR STRIPS INSTALLATION.
Earlier reports · 2018–2022 · 21 reports
2022
Part: NONE — LOOSE (FA) · airframe 17,127 hrs · 11,418 cycles
F/A #1 JUMPSEAT EMERGENCYFLASHLIGHT HOLDER LOOSE-C/A-RAR FA EMERGENCY #1 FLASHLIGHT ASSY. IAW AMM 33-51-01, OPS. CHECK GOOD
2021
Part: SHEAR PANEL — CORRODED (FRMS 87-88) · airframe 13,798 hrs · 9,270 cycles
SSI# 53-23-005 R/H SHEAR PANEL IN AFT GALLEY AT FRAMES 87 AND 88 CORRODED (LEVEL 2 CORROSION) -C/A-REMOVED AND INSTALLED SERVICEABLE RH FR 87-88 SHEAR PANEL IAW EMB 175 SRM 51-40-08 AND 51-40-02
Part: FLOORBEAM — CORRODED (FRM 89) · airframe 13,798 hrs · 9,270 cycles
SSI 53-23-005 R/H OUTBD FLOOR BOARD SUPPORT IN AFT GALLEY AT FRAME 89 CORRODED BY DRAIN LINES (LEVEL 2 CORROSION)-C/A-RAR R/H OUTBD FLOOR BOARD SUPPORT IN AFT GALLEY AT FRAME 89 IAW ERJ 175 SRM 51-40-08, 51-43-01 & 51-40-02
Part: SEAT TRACK — CORRODED (FRM 29) · corrosion level 2 · airframe 13,798 hrs · 9,270 cycles
SSI 53-21-005: RH FLOOR SEAT TRACK CORRODED AT FR 29 (MARKED) (LEVEL 2 CORROSION) (MAJOR REPAIR)-C/A-PERFORMED REPAIR OF RH FLOOR SEAT TRACK DUE TO CORROSION AT FRAME 29 IAW ERS-EJ-53MR-4377
Part: SEAT TRACK — CORRODED (FRMS 83-84) · airframe 13,798 hrs · 9,270 cycles
SSI 53-23-005: RH FLOOR SEAT TRACK HAVE SEVERAL AREAS OF CORROSION BETWEEN FR 80-84 (MARKED) (LEVEL2 CORROSION)-C/A-REMOVED AND REPLACED RH FLOOR SEAT TRACK AT FR 80-84 IAW ERJ 175 SRM 51-40-02, 51-40-08. SEE WIPS AND TASK FOR DETAILS
Part: SHEAR PANEL — CORRODED (FRMS 87-88) · airframe 13,798 hrs · 9,270 cycles
SSI# 53-23-005 CENTER SHEAR PANEL IN AFT GALLEY AT FRAMES 87 AND 88 CORRODED (LEVEL2 CORROSION)-C/A-RAR CENTER SHEAR PANEL IN AFT GALLEY AT FRAMES 87 AND 88 IAW EMB 175 SRM 51-40-08
Part: FLOOR SUPPORT — CORRODED (FRM 90) · corrosion level 2 · airframe 13,798 hrs · 9,270 cycles
SSI# 53-23-005 R/H FLOOR BOARD SUPPORT GUSSET IN AFT GALLEY AT FRAME 90 JUST FWD OF AVIONICS RACK CORRODED (LEVEL 2 CORROSION)-C/A-RAR R/H FLOOR BOARD SUPPORT GUSSET IN AFT GALLEY AT FRAME 90 JUST FWD OF AVIONICS RACK IAW EMB 175 SRM 51-40-08.
Part: SEAT TRACK — CHAFED (FRMS 32-33) · airframe 13,798 hrs · 9,270 cycles
LH FLOOR SEAT TRACK CHAFED BETWEEN FR 32-33 (MARKED)-C/A-PERFORMED REPAIR OF LH FLOOR SEAT TRACK DUE TO BEING CHAFED OUT OF LIMITS AT FRAMES 32-33 IAW ERS-EJ-53MR-4377
Part: FLOOR SUPPORT — CORRODED (FRMS 13-14) · airframe 13,798 hrs · 9,270 cycles
SSI 53-10-027 THE RH FLOOR SILL IS CORRODED BETWEEN FRAMES 13 AND 14 (AS MARKED) (LEVEL2 CORROSION)-C/A-RAR RH FLOOR SILL BETWEEN FRAMES 13 AND 14 IAW EMB 175 SRM 51-40-08, 51-43-01 AND 51-40-02
Part: SEAT TRACK — CORRODED (FRMS 80-84) · airframe 13,798 hrs · 9,270 cycles
SSI 53-23-005: LH FLOOR SEAT TRACK HAVE SEVERAL AREAS OF CORROSION BETWEEN FR 80-84 (MARKED) (LEVEL 2 CORROSION)-C/A-BLENDED AREAS ON LH FLOOR SEAT TRACK BTW FR 80-83 AND FOUND TO BE WITHIN ALLOWABLE LIMITS IAW EMB 175 SRM 53-23-10. BLEND AT FR 84 BEYOND LIMITS .035 IAW EMB 175 SRM 53-23-10. TRIMMED OUT RELATED TEETH ON LH FLOOR SEAT TRACK AT FR 84 IAW EMB 175 SRM 51-10-03 AND 53-00-10.PERFORMED SPLICE DEVICE REPAIR AT FR 84 IAW EMB 175 SRM 53-00-10 AND AMM 25-21-11.
Part: SPAR — CRACKED (LT WING) · airframe 13,798 hrs · 9,270 cycles
LH WING OUTBD SPAR 1 CRACKED AT AFT OUTB SIDE-C/A-RAR LH WING OUTBD SPAR 1 IAW EMB 175 SRM51-40-02, 51-45-00, AND 51-40-08.
Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 13,798 hrs · 9,270 cycles
L/H AND R/H EMERGENCY SERVICE DOOR EXIT LIGHT LENS CRACKED-C/A-REMOVED AND REPLACED L/H AND R/H EMERGENCY SERVICE DOOR EXIT IDENTIFIER SIGNS IAW EMB 175 AMM 33-50-15. OPS CHK GOOD
Part: SPAR — CRACKED (RH WING TIP) · airframe 13,798 hrs · 9,270 cycles
RH WING TIP INBD SPAR 1 CRACKED-C/A-COMPLETE:SEE NRTC E870481 FOR REPLACEMENT OF RH WING TIP INBD SPAR 1.
2019
Part: WARNING MESSAGE — ILLUMINATED (AFT PAX DOOR) · airframe 8,968 hrs · 6,160 cycles
DURING CLIMB CREW RECEIVED PAX AFT DOOR MESSAGE. CREW COMPLIED WITH QRH AND RETURNED TO SHV-C/A-NO CREW RIGHT UP AS PER MEL 52-23 REF LGPG 4339488 ITEM 1 L2 DOOR INDICATOR INOP ITEM IS ALREADY BEEN DOCUMENTED PREVIOUSLY.
Part: WARNING LIGHT — ILLUMINATED (PAX DOOR) · airframe 8,953 hrs · 6,151 cycles
ON TAKEOFF AT 8,500 FT WE GOT AT MASTER WARNING DOOR PAX AFT OPEN ONE DOOR INDICATOR WAS NOT INDICATING PROPERT WHEN FA CALLED LIGHT CLEARED AT 500 FT-C/A-AS PER MEL 52-23 REF LGPG 4339488 ITEM 1 L2 DOOR INDICATOR INOP ITEM IS ALREADY BEEN DOCUMENTED PREVIOUSLY
Part: DOOR — OUT OF RIG (PAX DOOR) · airframe 8,908 hrs · 6,125 cycles
ON DEP MASTER WARING EICAS MESSAGE DOOR PAX AFT OPEN MSG PER ORH DOOR LOCK INDICATION SHOWED GREEN DOOR LATCH INDICATION 1 GREEN 1 WHITE-C/A-REINSPECTED DOOR ALL CHECKS GOOD CHANGED MEL FROM 52-22 TO 52-23 AUTHRIZATION NUMBER REMAINS THE SAME M PROC C/W. VERIFIED VISUAL INDICATOR DOES SHOW GREEN. M PROCEDURES FOR MEL 52-23 MEETS PROVISOS. REMOVED AND REPLACED THE POSITION INDICATOR SPRING IAW AMM 53-23-21, FURTHER TROUBLESHOOTING REQUIRES. MEL ITEM REMAINS OPEN. PERFORMED ADJUSTMENT OF AFT PASSENGER DOOR TO GET W GAP FOR LATCH SENSOR PER EMB MM 52-12-00-820-059-A. UNABLE TO ADJUST FOR W GAP. RIGGED DOOR TO PROPER Z MEASUREMENT AS PER EMB MM 52-12-00-820-059-A. MEL REMAINS OPEN. ADJUSTED AFT PAX DOOR COMMAND RAMP IAW EMB 175 AMM 52-12-00 OPS CHECKS GOOD. REINSTALLED AFT PASSENGER DOOR SURROUND IAW EMB 175 AMM 25-23-09. AND REINSTALLED AFT PASSENGER DOOR LINER IAW EMB 175 AMM 25-23-05.
Part: WARNING MESSAGE — FALSE ACTIVATION (PAX DOOR) · airframe 8,907 hrs · 6,124 cycles
ON DEP AFTER GEAR RETRACTION MASTER WARINING FOR DOOR PAX AFT OPEN RAN APPR CHECK LIST QRH DECLARED EMERGENCY RETURNED TO AIRPORT KELP LANDED UNDER MAX LANDING WIGHT-C/A-PERFORMED OPS CHECK AFT PAX DOOR IAW EMB 175 AMM 52-12-00 ALL CHECKS GOOD DEFERRED WARING SYSTEM
2018
Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,235 hrs · 5,066 cycles
EMERGENCY LIGHT STRIP INOP FWD CABIN AFT OF FLOOR PANEL 226BRF. C/A-REMOVED AND REPLACED EMERGENCY LIGHT STRIP FWD CABIN AFT OF 226BRF IAW AMM 33-50-21. OPS CHECK GOOD.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 7,235 hrs · 5,066 cycles
HOLE FOUND IN FUSELAGE ALONG STRINGER 28L BETWEEN FRAMES 19 AND 20 ON BOTTOM OF FUSELAGE. C/A-INSTALLED REPAIR DOUBLER, TRIPLER & FILLER IAW SRM 53-10-01.
Part: SKIN — DAMAGED (FRAMES 18-19) · airframe 7,235 hrs · 5,066 cycles
INVESTIGATE POSSIABLE BURN MARK BW FR 18-19/ STGR 27R-28R.-C/A-COMPLETE:UPON FURTHER INVESTIGATION ON DAMAGE WAS NOTED TO FUSELAGE SKIN,BTW FR 18-19/ STGR 27R-28R. IAW EMB 175 SRM 51-10-02. SEE WIPS FOR FURTHER DETAILS
Part: POWER UNIT — FAILED (CABIN) · airframe 6,456 hrs · 4,552 cycles
EMERGENCY LIGHT ON CEILING PANEL BETWEEN OVERHEAD BIN 12 AND 13 INOP. FOUND EMERGENCY LIGHT AT CEILING PANEL BETWEEN OVHD BIN 12 AND 13 INOP. REMOVED AND REPLACED EMERGENCY LIGHT LAMP IAW AMM 33-50-13. OPS CHK NO GOOD IAW AMM 33-50-00. REINSTALLED ORIGINAL EMERGENCY LIGHT LAMP IAW AMM 33-50-13. REMOVED AND REPLACED EMERGENCY LIGHT POWER UNIT NR 4 IAW AMM 33-50-01. OPS CHK GOOD IAW AMM 33-50-01 AND 33-50-00. BONDING CHK GOOD IAW AMM 20-13-21.