N211FR
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.
14 reports on file, 2011-06-01 – 2023-02-21.
Part: BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 40,208 hrs · 16,814 cycles
DISCREPANCY: REFERENCE AIRBORNE/PEMCO N/R 13579.0412 FR 66 LH SIDE DUMMY BEAM CORRODED CORRECTIVE ACTION: REMOVED AND REPLACED FR 66 L/H SIDE DUMMYH BEAM IAW A320 SRM 53-00-14-283-002 FIG 001 SHEET 2. 51-72-11//END//
Part: BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 40,208 hrs · 16,814 cycles
DISCREPANCY: REFERENCE AIRBORNE/PEMCO N/R 13579.0410 FR 66 BEAM Y512.5 CORRODED CORRECTIVE ACTION: REMOVED AND REPLACED FR66 FLOORBEAM Y512.5 IAW A320 SRM 51-72-11-911-002//END//
Earlier reports · 2011–2022 · 12 reports
2022
Part: NONE — NONE (NONE) · airframe 39,015 hrs · 16,303 cycles
POSSIBLE FUME EVENT. BURNT SMELL STRONGER IN THE BACK OF AIRPLANE DISCOVERED AT THE GATE WILL ALL THE DOORS CLOSED APU BLEED ON PACKS ON. FWD AFT PAX DOORS WERE OPEN WHEN FA REPORTED THE ODOR. AN EXTERNAL POWER CART WAS NEAR ACFT RUNNING. IT IS BELIEVED THE ODOR IF FRON OUTSIDE OF ACFT.PERFORMED PACK AS A PRECAUTION NO ODOR AT THIS TIME IAW TSM 05-50-00-810-831-LEVEL A DECOMINATION PERFORMED. NOT AN SDR. :
Part: SLIDE — DAMAGED (R1 DOOR) · airframe 38,940 hrs · 16,272 cycles
DISCREPANCY: PERFORMING TC FFT A25200-A0-3, R1 DOOR WAS UNABLE TO PIN THE BOTTLE. R1 SLIDE REQUIRES REPLACEMENT. CORRECVTIVE ACTION: INSTALLED NEW R1 DOOR SLIDE IAW AMM 25-62-44-400-803-A OPS GOOD .
2021
Part: LANDING GEAR — VIBRATION (NOSE) · airframe 35,780 hrs · 14,770 cycles
EXCESSIVE NOSEWHELL VIBRATION AFTER SELECTING GEARUP. LASTED OVER 6 SECONDS. IAW AMM 32-20-00-810-802-A STEP 4.B.1.AV1 WE GREASED AL JOINTS OF THE NLGIAW STEP 4.B.1.A.V11 CLEANED AND INSPECTED NLG TORQUE LINK AND CENTER BOLT. NO DEFECTS NOTED. IAW STEP 4.B.1.B.1V INSPECTED THE GAP OF THE 2 SMALL NLG AFT DOORS. THE PLAY WAS WITHIN. (CORRECTIVE ACTION ITEM 2)-- THE 5 MM PLAY LIMITNLG TIRES HAVE ALREADY BEEN REPLACED AND INSPECTED ON LP185654NO NEW DEFECTS HAVE BEEN FOUND AT THE MOMENT. IAW AMM 32-20-00-810803-A ACFT OK FOR SERVICE.
Part: BOLT — FAILED (DOOR SLIDE) · airframe 34,467 hrs · 14,121 cycles
FORWARD LEFT DOOR SLIDE FELL OFF DOOR PRIOR TO PUSH. CORRECTIVE ACTION: REPLACED L1 DOOR SLIDE ATTACH BOLTS OPS CK'S GOOD REF. AMM 25-62-44-400-007A T/W F9TAB2198C DUE 12-21.
2019
Part: A/C PACK — ODOR (NR 1) · airframe 30,726 hrs · 12,440 cycles
MULTIPLE ODOR EVENTS , FIRST IN CRUISE FL360 OCCASSIONAL DIRTY SOCK SMELL IN COCKPIT. FOLLOWED QRH AFTER 5 MIN AND NO ODOR NOTED . AFTER CHECKING W /FA'S NO ODORS NOTED AT TIME. PERFPORMED TSM INSPECTION FOR CABIN ODORS , IDENTIFIED CAUSE OF ODOR TO BE PACK . TSM 05-50-00-810-831-A, AFTER TOP OF DESCENT FA B CALLED TO TELL OF AN ODOR AND TASTE AFTER PARKING FA C SAID SHE NOTED ODOR MID CABIN DURING FIANL COMPLIANCE . CORRECTIVE ACTION -- PERFORMED TSM INSPECTION FOR CABIN ODOR , IDENTIFIED CAUSE OF ODOR TO BE PACK 1. TSM 05-50-00-810-831-A. FOUND PACK 1 TO SOURCE OF ODOR.
2018
Part: BATTERY — FAILED (CABIN) · airframe 27,108 hrs · 10,888 cycles
BATTERY 10WL FAILED EPSU TEST. REPLACED BATTERY AT EPSU 10WL IAW AMM 33-51-38 PB401. OPS NORMAL NO FAULTS NOTED.
Part: UNKNOWN — ODOR (CABIN) · airframe 26,789 hrs · 10,753 cycles
FA IN THE AFT CABIN REPORTED A POSSIBLE FUME EVENT. SOUR BODY ODOR DURING TAXI, A MUSTY ODOR DURING TAKEOFF AND ODOR OF PENCIL SHAVINGS DURING CRUISE. FEELING OF HEAVY AIR IN AFT CABIN. APU ECS NOT DE-ENERGIZED IN FLIGHT. PERFORMED TSM 71-00-00-810-802-A THRU STEP 4A(4). NO OIL WETTING PRESENT IN THE NR 1 & 2 ENGINES. PERFORMED AN IDLE ENGINE LEAK CHECK IAW AMM 71-00-00-710-006. NO LEAKS FOUND. NO ODOR NOTED IN THE CABIN.
Part: UNKNOWN — ODOR (CABIN) · airframe 26,437 hrs · 10,598 cycles
DIRTY SOCKS/OILY/METALLIC ODOR NOTED BY ALL FLIGHT ATTENDANTS PRIMARILY IN THE GALLEYS NEARING TOP OF CLIMB. APPLIED ELIMINATION OF ODOR PROCEDURE AND IT DIDN'T DISSIPATE THE ODOR. EMERGENCY DECLARED. PERFORMED IDLE RUNS OF BOTH NR 1 AND NR 2 ENGINES PER AMM 71-00-00-710-006. NO EVIDENCE OF OIL DROPS OR SMOKE FROM DRAIN MAST. ISOLATED BLEED SOURCES AND PACKS WHILE RUNNING ENGINES. NO FAULTS/ODORS IN ANY CONFIGURATION. NO EVIDENCE OF HYDRAULIC LEAKS PER AMM 29-00-00-790-001. BORESCOPED ENGINE NR 1 AND NR 2 PER AMM 72-31-00-290-002-A FOR EVIDENCE OF OIL WETTING. NO DEFECTS WERE FOUND. AC WAS RELEASED FOR SERVICE.
2017
Part: DOOR SILL — CORRODED (R2 DOORWAY) · corrosion level 2 · airframe 20,763 hrs · 8,406 cycles
R2 DOOR SILL PLATE FLOORBOARD HOLE HAS CORROSION LOCATED AT FRAME 66. REMOVED AND REPLACED R2 DOOR SILL IAW SRM 51-72-11-911-001.
2013
Part: PROXIMITY SENSOR — INOPERATIVE (CARGO DOOR) · airframe 5,641 hrs · 2,236 cycles
FWD CARGO DOOR ECAM CLIMBING OUT OF 2000' WITH INITIAL PRESSURIZATION FLUCTUATIONS. AIR TURNBACK AT L416. PERFORMED PRESSURLZATION TEST IAW AMM 05-53-00-860/780. NO FLUCTUATION OF PRESSURIZATION NOTED. FWD CARGO DOOR INDICATED OPEN INDICATION AT 1.6 PSI. FWD CARGO DOOR DID PASS ELECTRICAL INDICATION TEST LAW AMM 52-35-00-710 ONLY WITH NO PRESSURE. DEFERRED FWD CARGO DOOR INDICATLON IAW MEL 52-70-01I CONTROL NR 1096312 DD 2-25-13. CLEARED MEL 52-70-01-I. REPLACED PROXIMITY SWITCH AND ADJUSTED AS REQUIRED REF AMM 52-71-12-400-001-A, AMM 52-71-12-820-050-B MDDR 1096312. MEL REMOVED.
2012
Part: TIRE — FAILED (NLG) · airframe 3,639 hrs · 1,457 cycles
FOUND RT NOSE TIRE WITH TREAD SEPARATION. REPLACED RT NOSE TIRE LAW AMM32-41-12-PB40 1.
2011
Part: SKIN — PUNCTURED (ZONE 300) · airframe 128 hrs · 50 cycles
ACFT LP 605289: DURING OPERATIONS, ACFT WAS CAUGHT IN A SEVER HAIL STORMS. THE STORM RESULTED IN PENETRATING DAMAGE TO THE LT ELEVATOR IN (3) LOCATIONS. NR L - A 172.4 INCHES FROM THE INBD EDGE. 10.25 INCHES FROM THE T/E, .9 INCHES WIDE. NR 2 - A 125.0 INCHES FROM THE INBD EDGE. 13.5 INCHES FROM THE T/E, .95 INCHES WIDE. NR3 - A 72.0 INCHES FROM THE INBD EDGE. 13.5 INCHES FROM THE T/E, .9 INCHES WIDE. DAMAGE WAS REPARED IAW SRM 55-21-11, FIG 204, CONF 1 (COMPOSITE REPAIR) AUTHORIZED BY EA A2-55R-32086.