N210FR
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.
24 reports on file, 2014-12-09 – 2023-04-21.
Part: PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 40,972 hrs · 17,273 cycles
DISCREPANCY: REFERENCE AIRBORNE/PEMCO N/R 13425.1281 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX-FD/CR PII ROW 330 PASSENGER CABIN FLOOR STRUCTURE TRACK-Y1292 AT FR 66 CORRODED. CHECK FOR SERVICEABILITY. CORRECTIVE ACTION: REOMVED AND REPLACED PASSENGER CABIN FLOOR STRUCTURE TRACK-T1292 AT FR66 IAW A320 SRM 51-72-11-911-001. MX ACTION IS ACCETABLE./END/
Part: BEAM — CORRODED (ZONE 200) · airframe 40,972 hrs · 17,273 cycles
DISCREPANCY: REFERENCE AIRBORNE/PEMCO N/R 13425.0785 FLOOR SUPPORT AT L-2 DOOR SILL STA C68 T CAP CORRODED DOT 921-4 CORRECTIVE ACTION: REMOVED AND INSTALLED NEW FLOOR SUPPORT AT L-2 DOOR SILL STA FROM FR 68 TO FR 70 IAW A320 SRM 51-72-11 ///END//
Part: PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 40,972 hrs · 17,273 cycles
DISCREPANCY: REFERENCE AIRBORNE/PEMCO N/R 13425.0587. AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. AFT CABIN-WET AREA-LATERAL SHEAR PLATE BETWEEN FLOOR BEAMS C69 TO C70 HAS CORROSION - REF:RBL 48.00 DOT#997-162. CORRECTIVE ACTION: REMOVED AND REPLACED L/H SHEAR PLATE IAW A320 SRM 51-42-11, SRM 51-44-11 AND ESPM 20-33-20-02. RECONNECTED 7102VC AND RESECURED IAW ESPM 20-33-20-02. BITE CHECK OF VOR/MKR PERFORMED ON LEAK & FUNC (13424.0913) ITEM 51. SEE COPY ATTACHED. MX ACTION IS ACCEPTABLE. /END/
Part: BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 40,972 hrs · 17,273 cycles
DISCREPANCY: REFERENCE AIRBORNE/PEMCO N/R 13425.0588 AFT CABIN WET AREA TOP BEAM ON FLOOR BEAM C66 HAS CORROSION REF: LBL 19.00 DOT#997-163 CORRECTIVE ACTION: EVALUATED REMOVED AND REPLACED BEAM P/N D5347209400800 FR 66 LBL 19.00 IAW A 320 SRM 51-44-11, SRM 53-00-14-283-002, SRM 51-72-911-001//END//
Part: FITTING — CORRODED (ZONE 200) · corrosion level 2 · airframe 40,972 hrs · 17,273 cycles
DISCREPANCY: REFERENCE AIRBORNE/PEMCO NR 13425.0576 FWD WET AREA L1 DOOR THRESHOLD SUPPORT STRUCTUTRE CORRODED AROUND FASTNER HOLES. CORRECTIVE ACTION: REMOVED AND REPLACED L1 DOOR SILL BOX CENTER FITTING IAW A320 SRM 51-4-11, 51-44-11//END//
Part: BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 40,972 hrs · 17,273 cycles
DISCREPANCY: REFERENCE AIRBORNE/PEMCO N/R 13425.0575 FWD WET AREA RH BEAM -Y1292 CORRODED FRAME 15-18 CORRECTIVE ACTION: REMOVED & REPLACED FWD WET AREA RH BEAM-Y1292 FRAME 15-18 PER A320 SRM 51-42-11 ///END//
Part: BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 40,972 hrs · 17,273 cycles
DISCREPANCY: REFERENCE AIRBORNE/PEMCO N/R 13425.0591 AFT CABIN-WET AREA TOP BEAM BETWEEN FLOOR BEAMS C67 TO C68 HAS CORROSION- REF: LBL 30.00DOT #997-166 CORRECTIVE ACTION: REMOVED AND REINSTALLED NEW BEAM FROM FR 67 TO FR 68 LBL 30.00 IAW A320 SRM 51-72-11 ///END//
Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 40,972 hrs · 17,273 cycles
AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. AFT CABIN - WET AREA - TOP BEAM BETWEEN FLOOR BEAMS C66 TO C68 HAS CORROSION - REF RBL 30.00. FLOORBEAM FR 66 TO 68 RBL 30 AFTER EVALUATION FOUND TO BE OUT OF LIMITS IAW A320 SRM 53-00-14-283-002 AND REMOVED FOR REPLACED FOR NEW FLOORBEAM, LOCATE AND DRILL AND INSTALLED IAW A320 SRM 51-44-11. MX ACTION IS ACCEPTABLE.
Part: BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 40,972 hrs · 17,273 cycles
DISCREPANCY: REFERENCE AIRBORNE/PEMCO N/R 13425.0590 AFT CABIN-WET AREA TOP BEAM BETWEEN FLOOR BEAMS C66 TO C67 HAS CORROSION- REF: LBL 36.00DOT #997-165 CORRECTIVE ACTION: REMOVED AND REPLACED FLOOR BEAMS C66 TO C67 IAW A320 SRM 51-72-11, SRM 53-00-14-283-002 ///END//
Part: PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 40,972 hrs · 17,273 cycles
REFENENCE AIRBORNE/PEMCO N/R 13425.0589 AIRCRAFT WS NOT GROUNDED AND IS IN CHEKF FOR SCHEDULE MX-AFT CABIN-WET AREA-LATERAL SHEAR PLATE BETWEEN FLOOR BEAMS C69 TO C70 HAS CORROSION- REF: RBL 48. REMOVED AND REPLACED FLOOR STRUCTURE R/H FR6970 SHEAR PLATE IAW A320 SRM 51-72-11 AND 51-44-11//END//
Earlier reports · 2014–2022 · 14 reports
2022
Part: APU — LEAKING (ZONE 200) · airframe 39,391 hrs · 16,584 cycles
DISCREPANCY: LOWER ALTITUDES < 10000FF MODERATE ODOR PRESENT. CORRECTIVE ACTION: PERFORMED TSM 05-50-00-810-831-A APU FOUND PREVIOUSLY PLACED ON MEL CTL#1186539 TSM REQJUIRES LEVEL A DECONTAMINATION OF ECS PERFORMED IAW AMM 21-00-00-615-802-A NO ODORS NOTED NR125726 ATTACHED REF LP224177 ITEM#3 FOR REQUIRED TSM 71-00-00-810-802-A INCLUDING ENG#1 AND ENG#2 BORESCOPE WORK PERFORMED. ORIGINAL SUBMISSION DATE: 09/21/2022
Part: OIL SYSTEM — LEAKING (APU) · airframe 39,388 hrs · 16,582 cycles
DUE TO SEVERAL ODOR EVENTS AND OIL FOUND IN APU DUCTS, INLET,AND DOOR,APU NEEDS MEL. PLACED ON MEL 49-10-01 CONTROL # 1186539 DUE DATE09-29-2022 MCC ABM 430781 MX ACTIONS CW - PLACARDS INSTALLED.
Part: APU — ODOR (ZONE 100) · airframe 39,382 hrs · 16,580 cycles
REFERENCE LP 224157 BTB FOR FUMES IN THE CABIN OUT 0652 IN 0725 FLIGHT ATTENDANTS REPORTED STRONG ODOR IN AFT CABIN AREA. PERFORMED IDENTIFICATION OF CAUSE FOR CABIN ODOR SMOKE OR FUMES IAW AMM 05-50-00-810-831-A DECISION TABLE 05-50-00-991-01200-00-A TYPE 3 (B) THE LEVEL C PERFORMED THE BLEED AIR DUCTS AMM 36-10-00-615-804 NO CONTAMINATION FOUND, RAN #2 ENG FOR 20MIN PACK ON NO SMELL NOTED AC OK FOR SERVICE // LP224158; DUE TO MULTIPLE ODOR EVENTS APU NEEDS TO BE PLACED ON MEL - PLACED ON MEL 49-10-01A CTRL#1186244 DD 9/21/2022 WITH MCC AB 434922 PLACARDS INSTALLED MX ACTIONS C/W
Part: APU — FUMES (ZONE 100) · airframe 39,365 hrs · 16,574 cycles
DISCREPANCY: REFERENCE LP 224151 POSSIBLE FUME EVENT IN CABIN. REPORTED BY 2 PEOPLE. CORRECTIVE ACTION: PERFORMED INSPECTION OF THE APU UPON ODOR IN THE CABIN/FUMES IN THE CABIN/OIL SMOKE, LEVEL B. NO LEAKS NOTED. REPLACED RECIRCULATION FILTER CARTRIDGES. T/W NO. F9TAB2940C D/D 07/23. AMM 21-21-41-000-001-A, AMM 21-21-41-400-001-A, AMM 49-00-00-200-811-A
2021
Part: ACTUATOR — FAILED (ZONE 300) · airframe 34,875 hrs · 14,418 cycles
THSA FAILED TEST OF THE NO-BACK DEVICE. THSA REMOVED AND REPLACED ON PEMCO NR 10682-0363. IAW A320 AMM 27-44-51-400-001-A. OPS CHECK GOOD.
Part: BOTTLE — LEAKING (RT OVERWING EXIT) · airframe 34,825 hrs · 14,934 cycles
LP1212072 ITEM 1 -- ENROUTE , RIGHT AFT OVERWING EXIT CHECK SLIDE PRESSURE LIGHT ILLUMINATED ON FA PANEL -- CORRECTIVE ACTION ITEM 1 -- REMOVED THE INFLATION RESERVOIR FOR RIGHT OVERWING ESCAPE SLIDE IAW AMM 25-62-46-000-001-A. P/N 60592-101 S/N 81911466 CONT LP 12212072 ITEM 3 -- ITEM 3 -- REMOVAL COMPLETED ON LP1212072-1 . INSTALLED RH OVERWING SLIDE RESEVOIR BOTTLE IAW AMM 25-62-46-400-001-A
2019
Part: WARNING SYSTEM — FALSE ACTIVATION (CABIN PRESSURE) · airframe 30,665 hrs · 12,534 cycles
LP1207623 ITEM#3 - AFTER TAKEOFF SKIN VALVE FAULT FOLLOWED QRH TO DEPRESSURIZE CABIN AND RETURNED TO KAUS CORRECTIVE ACTION - PERFORMED OPS CHECK OF AEVC SYSTEM, OPS CHECK NORMAL. PERFORMED PRESSURIZATION OF FUSELAGE, NO DEFECTS NOTED, AC OK TO CONTINUE. AMM 21-26-00-710-001A, AMM 05-53-00-PB601 CONF 00.
2018
Part: ADIRU — MALFUNCTIONED · airframe 27,958 hrs · 11,412 cycles
NAV IAS DISCREPANCY. FO'S IAS SHOWED 30% LESS SPEED THAN CAPT'S AND STANDBY IAS DISPLAYED. DEFERRED ADR2 PER MEL 34-10-01I CONTROL 1143664, DUE DATE 10/24/2018. SWAPPED ADIRU 1 AND 2, FAULT CLEARED. ADIRU 1, 2, AND 3 TESTED GOOD IAW AMM 34-12-34 PB 401 OPS CHECK GOOD. MEL CLEARED.
Part: ELECTRICAL BOX — INOPERATIVE (NLG STEERING) · airframe 27,654 hrs · 11,281 cycles
ECAM BRAKES SYS 1 FAULT (IN FLIGHT) & ECAM WHEEL NLG STEERING FAULT (IN FLIGHT) WITH ASSOCIATED INOP SYS MESSAGE NLG STEERING. RESET BSCU AND PERFORMED BITE TEST IAW AMM 32-46-00-740-005-A. MESSAGE CLEARED. NO FAULTS NOTED. RESET BSCU AND PERFORMED OPS CHECK IAW AMM 32-51-00-720-A AND FUNCTIONAL CHECK IAW AMM 32-51-00-720-003-A. NOSE WHEEL STEERING OPERATES NORMALLY WITH NO FAULTS. REMOVED AND REPLACED NOSE WHEEL STEERING DEACTIVATION ELECTRICAL BOX IAW AMM 32-51-12 PAGE BLOCK 401. OPS NORMAL IAW TSM 32-51-00-810-823-A. NOSE WHEEL STEERING OPS NORMAL.
Part: SLIDE — FAILED (L1 DOOR) · airframe 25,522 hrs · 10,360 cycles
L1 DOOR SLIDE FOUND BAD DURING AN EPSU TEST. REMOVED AND REPLACED THE DOOR SLIDE IAW AMM 25-62-44-PB401. OPS CHECKED GOOD.
2017
Part: DOOR SILL — CORRODED (FRAMES 65-66) · corrosion level 2 · airframe 21,602 hrs · 8,841 cycles
FOUND DOOR SILL CORROSION TO BE OUT OF LIMITS IN FASTENER HOLE. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-72-11-911-001.
2015
Part: INTERFACE UNIT — FAULTY (ZONE 100) · airframe 16,803 hrs · 6,968 cycles
AFTER TAKEOFF, LG FAILED TO RETRACT. NUMEROUS ASSOCIATED ECAMS. PRECAUTIONARY AIR TURN BACK. R & R LG CONTROL INTERFACE UNIT NR 2. REFERENCE AMM 32-31-71 PAGE BLOCK 401. BITE TESTED GOOD, REFERENCE LP 9955448.
Part: CABLE — LACK OF LUBE (R1 DOOR) · airframe 12,887 hrs · 5,421 cycles
FORWARD R1 DOOR WILL NOT ARM. REMOVED DOOR TRIM, GREASED GIRT BAR TELEFLEX CABLE & SECURED DOOR TRIM. INSTALLED SLIDE RAFT IAW AMM 25-62-44-400-007A. ALL INDICATIONS NORMAL.
2014
Part: FAN — MALFUNCTIONED (E&E BAY) · airframe 12,543 hrs · 5,283 cycles
CLIMBING OUT OF 15,000 SMELLED SMOKE IN COCKPIT & CABIN. REFERENCE MDDR 109218, R & R EXTRACT FAN IAW AMM 21-26-51 PB 401. OPERATIONS TESTED GOOD.