N244NN
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
FA AND GATE AGENT REPORT ISSUES OPENING/CLOSING F1 MAIN CABIN DOOR. "STICKY" LUBRICATED THE L1 FORWARD-PASSENGER-DOOR COMMAND-RAMP ROLLER-SHAFT AND ITS BUSHING IAW AMM 53-10-21. OPC GOOD.
EMERGENCY PHOTOLUMINESCENT STRIP IN FRONT OF WARDROBE FADED RAR EMERGENCY PHOTOLUMINESCENT STRIP IN FRONT OF WARDROBE IAW ERJ 175 AMM 33-50-21/400. NO FURTHER DEFECTS NOTED.
1L DOOR IS HARD TO OPEN. HAPPENED TWICE. ONCE IN NASSAU AND IN MIAMI. GATE AGENTS HAVE A HARD TIME OPENING 1L DOOR. GET STUCK AT THE TOP. LUBRICATED L1 DOOR OPEN/CLOSE MECHANISM AND OPS CHECKED IAW AMM 52-11-23 OPS CHK GOOD.
FWD FA EMERGENCY FLASHLIGHT MISSING RAR FA FWD EMERGENCY FLASHLIGHT AT FA# 1 STATION AND DEFERRED ORIGINAL FLASHLIGHT. AUTH# 011341D-C REF# 25-51
GATE AGENT STATES THAT THE L1 CABIN DOOR HANDLE IS VERY HARD TO LIFT UP AND OPEN FROM THE OUTSIDE WHEN OPENING THE DOOR PERFORM OPC OF L1 DOOR IAW:AMM 52-11-00 OPC GOOD
RT FLOOR SUPPORT HAS CORROSION BETWEEN FR86 AND 87 @ Y+276 (LEVEL 2 CORROSION) (MAJOR REPAIR) REMOVED CORROSION FROM RT FLOOR SUPPORT BETWEEN FR 86 AND 87 @ +276MM PER SRM 51-10-03. BLENDED AREA MEASURES L= 1.6", W= 1.5", H= 0.060.? ORIGINAL MATERIAL THICKNESS IS 0.073", MATERIAL REMOVED 0.060", MATERIAL REMAINING IS 0.- 013", AND IS FOUND TO BE OUT OF LIMITS IAW SRM 51-75-16. LOCATED, DRILLED & DEBURED NEW RT FLOOR SUPPORT IAW SRM 51-40-02. TOPCOATED FASTENERS ON RH FLOOR SUPPORT IAW SRM 51-23-06 AND ETN-EJ-51-015. APPLIED CIC TO RH FLOOR SUPPORT IAW CPM 51-25-00 PART 1. R & R RT FLOOR SUPPORT IAW SRM 51-40-08.
CORROSION FOUND ON R/H SIDE IB SEAT TRACK BETWEEN FR 81 AND 82 Y= +276 (LEVEL 2 CORROSION) (MAJOR REPAIR) CORROSION ON INBOARD SEAT TRACK MEASURED .025", FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-23-10 AD01. REMOVED RT SIDE IB SEAT TRACK BETWEEN FR 73 TO 88 IAW SRM 51-40-08. LOCATED & DRILLED NEW AFT RH IB SEAT TRACK IAW SRM 51-40-02. INSTALLED SEAT TRACK IAW SRM 51-40-08. RESTORED FINISH TO SEAT TRACK IAW SRM 51-23-06, ETN-EJ-51-015. APPLIED CIC PER EMB-175 CPM-51-25-00.
CORROSION FOUND AT CLIP SHEAR ZONE 152 FR 88 STGR 29R (INTERNAL FWD WASTE WATER PANEL) (LEVEL 2 CORROSION) (MAJOR REPAIR) LOCATED AND DRILLED NEW SHEAR CLIP PN# 170-66531-001 IAW EMBRAER 175 SRM 51-40-02. INSTALLED NEW SHEAR CLIP LOCATED AT FR88 AND STR29R IAW EMBRAER 175 SRM 51-40-08. RESTORED FINISH TO SHEAR CLIP LOCATED AT FR88 AND STR29R. IAW ENVOY ETN-EJ-51-015 AND EMBRAER 175 SRM 51-23-06. APPLIED CIC IAW EMBRAER 175 CPM 51-27-00-910-001-A. REMOVED AND REPLACED SHEAR CLIP LOCATED AT FR88 AND STR29R IAW EMBRAER 175 SRM 51-40-08. LEVEL 2 CORROSION
LH DV WINDOW BOTTOM ROD HAS GOUGE (MAJOR REPAIR) BLENDED GOUGED AREA ON LH DV WINDOW BOTTOM ROD PER EMB-175 SRM 51-10-03. BLENDED AREA MEASURES (L=1.4?, W=.3?, H=.017?). DIAMETER REMAINING IS .692? AND IS FOUND TO BE OUT OF ALLOWABLE LIMITS PER EMB-175 AMM MPP 56-12-00-350-801-A. REMOVED LOWER ROD ON LH DV WINDOW, ADJUSTED NEW ROD TO OLD ROD LENGTH, INSTALLED NEW ROD ON LH DV WINDOWS REF EMB 175 AMM 56-12-00. REMOVED AND REPLACED LOWER ROD ON BOTTOM OF DV WINDOW AS REQUIRED REF EMB 175 AMM 56-12-00
EMERGENCY DECLARED TRU 1 FAIL ON EICAS-C/A-AT THIS TIME RESETED TRU 1 IAW AMM 24-31-00.OPS. CK FOUND OK.
DURING APPROACH, FLAP FAIL CAUTION APPEARED ON EICAS AFTER FLAPS EXTENDED TO 1. COMPLETED QRH PROCEDURE AND LANDED AS PER QRH. DECLARED EMERGENCY. RAR LH AND RH INBOARD FLAP OUTBOARD FLAP ACTUATOR IAW AMM 27-51-01 OPS CHECK GOOD.
FLAPS EICAS FAIL. DIVERTED TO SMF. DECLARED EMERGENCY. FLAP FAIL EICAS UPON SELECTING POSITION 1 SLATS 3 FLAPS 0 AMBER INDICATED QRH C/W MESSAGE REMAINED-C/A-T/S FAULT CODE 27512014ACE BLOCK 1 AND BLOCK 2 FOUND TO BE TRANSITORY CONDITION CLEAR INHIBITS PERFORMED FLAPS OPS CHECK IAW ERJ-175 AMM 27-50-00 FIM TASK 27-51-00-810-802-A PERFORMED GVI NO DAMAGE NOTED A/C OK FOR SERVICE
FLAPS FAIL ON APPROACH EMERGENCY DECLARED. CLEARED INHIBITS AND PERFORMED FLAPS OPS CHECK IAW AMM 27-50-00-710-801-A. OPS CHECK GOOD.
ABORTED TAKEOFF ROLL N1 ON #2 NEVER CAME UP. PERFORMED HIGH POWER GROUND ENGINE RUN IAW GHC AND MONITORED N1 FOR CORRECT RESPONSE. OBSERVED N1 INCREASE AS THROTTLE LEVERS WERE ADVANCED. ALSO PERFORMED OPC OF AUTOTHROTTLE IAW AMM 22-31-00-710-801 WITH NO DEFECTS NOTED.
LH HORIZONTAL STAB RIB 14 IS CRACKED (MAJOR REPAIR) -C/A-RAR LH HORIZONTAL STAB RIB 14 IAW EMB 175 SRM 51-40-08.
SSI 53-23-005- RH OUTBD FLOOR PANEL SUPPORT AT FR 89 IS CORRODED (LEVEL 2 CORROSION)-C/A-RAR RH OTBD FLOOR PANEL SUPPORT AT FR 89 IAW EMB 175 SRM 51-40-08.
RH FLOOR SILL BETWEEN FRAMES 12-14 IS CORRODED IN MULTIPLE SPOTS. (LEVEL 2 CORROSION) -C/A-REMOVED AND REPLACED RH FLOOR SILL BETWEEN FR 12-14 IAW EMB 175 SRM 51-40-02 AND 51-40-08.
SSI 53-10-027 - RH CENTER FLOOR SEAT TRACK IS CORRODED IN 2 SPOTS BETWEEN FR 17-18. (LEVEL 2 CORROSION) (MAJOR REPAIR). -C/A-PERFORMED CUTOUT OF CORROSION AT FR 17 AND REMOVED CROWN TEETH AND CORROSION ON FWD END OF RH SEAT TRACK BTW FR 17-18 AND FABRICATED AND INSTALLED DOUBLER AND FILLER IAW ERS-EJ-53MR-4638.
LH CENTER FLOOR BEAM IS CORRODED AT FR 17 (LEVEL 2 CORROSION) (MAJOR REPAIR)-C/A-ACCOMPLISHED A PERMANENT REPAIR ON LH CENTER FLOOR BEAM CORRODED AT FRAME 17 IAW ERS-EJ-53MR-4641.
CENTER FLOOR CROSS BEAM IS CORRODED AT FRAME 17 (LEVEL 2 CORROSION) (MAJOR REPAIR)-C/A-ACCOMPLISHED PERMANENT REPAIR ON CENTER FLOOR CROSS BEAM AT FR 17 IAW EMB 175 SRM 53-00-10 REPAIR 03P AND ERS-EJ-53MR-4642
SSI 53-23-005. RH SHEAR PANEL IS CORRODED-C/A-RAR RH SHEAR PANEL IAW EMB 175 SRM 51-40-08 (LEVEL 2 CORROSION)
SSI 53-23-005. AFT GALLEY RH UPPER SHEET IS CORRODED AFT OF FRAME 85. (LEVEL 2 CORROSION)-C/A- RAR AFT GALLEY R/H UPPER SHEET AFT OF FR 85 IAW EMB 175 SRM 51-40-08.
EMER BRK FAULT-C/A-FOUND #2 BRAKE ASSY BROKEN RAR #2 BRAKE ASSY IAW WC 32-49-11-000-801-A OPS CHECK OF EMER PARK BRAKE SYS IAW AMM 32-44-00 SATISFACTORY
SUPPLEMNTAL FOR DIVR TUL ACCT E2 VIBE 4.0 / DECLARED EMERGENCY FLIGHT CONT. -C/A-ANALYSIS PREFORMED TDMI ITEM RESTORED PER EHM-2022-03-16 044-RH-0030
SUPPLEMENTAL CA FOR UNABLE TO KEEP E2 VIBRATION IN GREEN. DECLARED EMERGENCY---E2---HAD TO ADJUST THROTTLE TO KEEP VIBE IN GREEN.CONTINUED TO MIA - ON CLIMBOUT #2 ENG LP INDICATED 4.0. FOLLOWED PROCEDURE AND WHEN POWER WAS REDUCED INDICATION REDUCED TO 3.5. INCREASING POWER INDICATION AT 4.0 BUT NEVER ABOVE. SLIGHT VIBRATION FELT MOMENTARILY. REQUESTED A GRADUAL CONTINUOUS DESCENT TO THE AIRPORT WITH #2 ENGINE POWER AT IDLE IDICATION WAS 1.5 OR LESS AND NO VIBRATION. LANDING WITHOUT ANY FURTHUR ISSUES REMAINING ENG INDICATIONS NORMAL.-C/A-REFERENCE PSR ALERT NOTICE EHM-2022-03-11-044-RH-0029. THE ENGINE GROUP HAS ANALIZED THE TRENDS AND NO ACTION IS REQUIRED AT THIS TIME REF ETN-EJ -72-009. THIS CLEARS TDMI
UPON TAXING FROM RAMP AREA RECEIVED STRONG SMOKE SMELL. EICAS MESSAGE PACK 2 FAIL ANNUNCIATED.DISCREPANCY: 21-50 AIR CONDITIONINGCABIN/COCKPIT COOLING SYSTEM (ACM PACK, HEAT EXCHANGE)PERFORMED QRH CHECKLIST & MESSAGE REANNUNCIATED."TRANSFERRED TO NRWC 044-DFW-02289"-C/A-RAR RH ACM IAW AMM 21-51-05 THROUGH STEP 3.H(25) WITH THE EXCEPTION OF 3 CONDENSER/REHEATER COUPLINGS.
PAX DOOR L1 DIFFICULT TO OPEN FROM OUTSIDE AIRCRAFT-C/A-REMOVED ICE FROM L1 DOOR AND OPENED AND CLOSED NUMEROUS TIMES IAW EMB 175 SDS 52-11-00. NO DISCREPANCIES NOTED
FLAP FAIL ON EICAS INITIAL FLAP EXTENSION ATTEMPT AT 210 KTS SLATS EXTENDED TO FULL WHEN COMMANDED WHENEVER SLATS EXTENDED "TRANSFERRED TO NRWC 044-DFW-01403"-C/A-REMOVED AND REPLACED RH INBOARD FLAP #2 ACTUATOR IAW EMB 175 AMM 27-51-01. FLAP SYSTEM OPERATIONAL CHECK GOOD.
LEFT ENHANCED WINGTIP SPAR 1 ATTACH FITTING CRACKED. REMOVED AND REPLACED SPAR ATTACH FITTING IAW ERS-EJ-57MR-1151 01, PART A. EASI 8945.
RT ENHANCED WINGTIP SPAR 1 ATTACHMENT FITTING CRACKED. FOUND ON OPEN UP. REMOVED AND REPLACED THE SPAR ATTACHMENT FITTING IAW ERS-EJ-57MR-1151 01 PART B. EASI 8945.
RH FUSELAGE SKIN DENT AT FR 28-29 PERMANENT REPAIR-C/A-ACCOMPLISHED PERMANENT REPAIR TO RH FUSELAGE SKIN DENT AT FR 28-29 IAW ERS-EJ-53MR-3866
LT ENHACED WINGTIP SPAR 1 ATTACHMENT FITTING CRACKED. TRANSFERRED TO NRTC E732621. C/A-R&R LT ENHANCED WINGTIP SPAR 1 ATTACHMENT FITTING IAW ERS-EJ-57MR-1151 01 PART A.
RT ENHANCED WINGTIP SPAR 1 ATTACHMENT FITTING CRACKED. TRANSFERRED TO NRTC E732622 C.OAKLEY 657866. C/A-REMOIVED AND REPLACED RT ENHANCED WINGTIP SPAR 1 ATTACHMENT FITTING IAW ERS-EJ-57MR-1151 01 PART B. EASI# 8945. SEE NRTC E732622 FOR DETAILS.
FLOOR EMERGENCY LIGHT STRIP IN FRONT OF FWD CLOSET DO NOT ILLUMINATE. C/A-REMOVED AND REPLACED PHOTOLUMNESCENT INDICATOR STRIP NEXT TO FWD CLOSET IAW MM 33-50-21 OPS CHECK GOOD.
EMERGENCY LIGHT BATTERY FAULT EICAS ILLUMINATED. C/A-RAN OPS CHECK IAW AMM 33-50-01. OPS CHECK GOOD. NO EICAS MSG OR FAULTS AT THIS TIME.
ENG TLA NOT TOGA ABORTED TAKE OFF AT 50 KTS. TROUBLESHOT IAW FIM 22-31-00. FOUND TO BE TRANSITORY CONDITION. OPS CHK GOOD IAW AMM 45-45-00 AND 22-31-00.
LG NO DISPATCH AFTER BRAKE TEMPS LEFT BRAKE TEMPS 46/34 RIGHT BRAKE TEMPS 219/89. FOUND LG NO DISPATCH MESSAGE ON EICAS AND RT IB BRAKE TEMP HIGH AFTER LANDING. FAULT CLEARED AFTER BRAKES RETURNED TO NORMAL TEMP. ACCOMPLISHED MAIN BRAKE ADJUSTMENT/TEST IAW AMM 32-41-00-710-801. NO FAULTS NOTED. INTERROGATED CMC AND FOUND FAULT CODE 36112200AM. TROUBLE SHOT IAW FIM 36-11-00 AND DISCOVERED PRECOOLER OUTLET GASKET MISSING CHUNKS. RAR GASKET IAW AMM 36-11-08-04. PERFORMED ENGINE BLEED OPS CHK IAW AMM 36-11-00. NO DEFECTS NOTED.
FAINT BURNING SMELL W/NO VISIBLE SMOKE B/W ROW 13-16. SMELL MOSTLY DISSAPATED. RT RECIRC FAN DEFERRED. MTX ITEMS C/W. REFERENCE TURNOVER FOR WORKED PERFORMED IAW AMM 21-20-00. UPON ADDITIONAL GVI FOUND FWD DRAIN MAST WITH STAINS STREAKING COFFEE AND ON NR 2 PACK FOUND EVIDENCE OF STREAKS OF COFFEE INTO THE NR 2 RAM INLET. CLEANED THE AREA. NO FURTHER DEFECTS NOTED AT THIS TIME. PERFORMED OPC RT PACK SYSTEM IAW AMM 21-00-00-860-801-A. OPC GOOD.
DURING CRUISE FLIGHT LG WOW SYS FAIL EICAS MESSAGE "TRANSFERRED TO NRWC 044-ORD-00174". TRANSFERRED FROM NRWC 004-ORD-00174. REMOVED AND REPLACED PSEM 1 IAW AMM 32-61-01-000/400-801. PERFORMED FLT CRTL NO DISPATCH RTS CHECK.
PASSING THROUGH APPROXIMATELY 27000 FT WHILE CLIMBING, THE NR 2 LP VIBRATION INDICATOR WAS AT 4.0 IN THE CAUTION RANGE. REDUCED N1 TO 77% BEFORE INDICATION WENT GREEN. RAN CHECKLIST AND PERFORMED A PERCAUTIONARY ENGINE SHUTDOWN IAW ENGINE ABNORMAL VIBRATION CHECKLIST. PERFORMED ENGINE VIBRATION IAW FIM 72-00-00 THRU BLOCK E OF FIGURE 109. PERFORMED E2 VIBRATION CHECK IAW MM 72-00-00. ALL PARAMETERS WITHIN LIMITS. REMOVED AND CLEANED THE RT ENGINE FAN BLADES, REMOVED AND REPLACED THE RT ENGINE FAN BLADE PINS AND BUMPER BAND, REINSTALLED FAN BLADES IAW ESM 72-00-00-800-915 SPECIAL PROCEDURES 097, VIBRATION RUN 0.3 TDMI RESTORED.
CLIMBING THRU FL 29.0 "DOOR PAX AFT OPEN" WARNING ON EICAS MSG EXTINGUISHED DESCENDING THRU FL 18.4. DEFERRED DOOR PAX AFT OPEN WARNING MSG. REMOVED AND REPLACED AFT PAX DOOR CLOSED SENSOR IAW AMM 52-72-21 OPS CHECK GOOD IAW AMM 52-70-00.
EICAS MSG IN FLIGHT FL310 DOOR PAX AFT OPEN. FLIGHT CREW PLACARDED AFT PAX DOOR IND M PROCEDURE. READJUSTED AFT PASSENGER DOOR WARNING SENSOR IAW AMM 52-72-21 OPS CHECK GOOD. PRESSURIZED AIRCRAFT, AFT PASSENGER DOOR SHOWED ON EICAS GREEN LIGHT MEL RESTORED