N216FR
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.
29 reports on file, 2012-04-03 – 2023-07-21.
Part: FITTING — CORRODED (ZONE 200) · airframe 39,913 hrs · 16,686 cycles
DISCREPANCY: REFERENCE AIRBORNE/PEMCO N/R 13876.0555. AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. L1 DOOR SCUFF PLATE TRIM CORRODED CORRECTIVE ACTION: REMOVED AND REPLACED L1 DOOR SCUFF PLATE FITTING IAW A320 SRM 51-11-00, 51-72-11, 51-42-11. MX ACTION IS ACCEPTABLE./END/
Part: PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,913 hrs · 16,686 cycles
DISCREPANCY: REFERENCE AIRBORNE/PEMCO N/R 13876.0604 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SHCEDULED MX. LH SHEAR PLATE FR70 CORRODED CORRECTIVE ACTION: AFT FUSELAGE MAIN CABIN L/H SHEAR PLATE AT FR 70 REMOVED AND REPLACED IAW A320 SRM 51-42-11; APPLIED TEMPORARY PROTECTION SYSTEM CIC IAW A320 AMM 51-78-00. OPERATIONAL TEST OF THE VOR CABLE TRANSFERED TO THE LEAK AND FUNCTIONAL BOOK 13875.0786 PG 10 ITEM 39 MX ACTION IS ACCEPTABLE. /END/
Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,913 hrs · 16,686 cycles
REFERENCE AIRBORNE/PEMCO N/R 13876.0609 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SHCEDULED MX. FLOORBEAM Y765 AT FR66-FR68 CORRODED. REMOVED AND REPLACED FLOORBEAM Y765 AT FR64-FR70 PER A320 SRM 51-42-11. MX ACTION IS ACCEPTABLE. /END/
Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,913 hrs · 16,686 cycles
DISCREPANCY: REFERENCE AIRBORNE/PEMCO N/R 13876.0610 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SHCEDULED MX. FLOORBEAM Y512.5 AT FR64-FR68 CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED FLOORBEAM Y512.5 AT FR64-FR70 PER A320 SRM 51-42-11.MX ACTION IS ACCEPTABLE. /END/
Part: DOOR SILL — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,913 hrs · 16,686 cycles
AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SHCEDULED MX. L2 DOOR SILL OUTER TRIM CORRODED. EVALUATED REMOVED AND REPLACED L2 CENTER SHAPE FITTING IAW A320 SRM51-72-11. MX ACTION IS ACCEPTABLE.
Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,913 hrs · 16,686 cycles
AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SHCEDULED MX. FLOORBEAM-Y969 AT FR66-68 CORRODED. REMOVED AND REPLACED WITH NEW FLOORBEAM FROM FR64-70 P/N D5347219320400 AND P/N D5347209001500 IAW A320 SRM 51-44-11, 53-41-14-283-009, 51-72-11-911-001, 51-42-11. MX ACTION IS ACCEPTABLE.
Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,913 hrs · 16,686 cycles
DISCREPANCY: REFERENCE AIRBORNE/PEMCO N/R 13876.0607 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SHCEDULED MX. FLOORBEAM Y1292 AT FR68 CORRECTIVE ACTION: REMOVED AND REPLACED FLOORBEAM-Y1292 @FR68 PER A320 SRM 51-42-11. MX ACTION IS ACCEPTABLE. /END/
Part: PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,913 hrs · 16,686 cycles
DISCREPANCY: REFERENCE AIRBORNE/PEMCO N/R 13876.0606 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SHCEDULED MX. RH SHEAR PLATE FR70 CORRODED CORRECTIVE ACTION: REMOVED AND REPLACED RH SHEAR PLATE FR70 PER A320 SRM 51-72-11 MX ACTION IS ACCEPTABLE. /END/
Part: FITTING — CORRODED (ZONE 200) · airframe 39,913 hrs · 16,686 cycles
DISCREPANCY: REFERENCE AIRBORNE/PEMCO N/R 13876.0556 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SHCEDULED MX. R1 DOOR SCUFF PLATE TRIM CORRODED CORRECTIVE ACTION: EVALUATED REMOVED AND REPLACED R1 DOOR SCUFF PLATE FITTING IAW A320 SRM 51-42-11, 51-44-11, 51-72-11/END/
Part: DOOR SILL — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,913 hrs · 16,686 cycles
DISCREPANCY: REFERENCE AIRBORNE/PEMCO N/R 13876.0611 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SHCEDULED MX. R2 DOR SILL FWD ARES CORRODED 3 PLCS CORRECTIVE ACTION: REMOVED AND REPLACED WITH NEW R2 DOOR SILL P/N D5348004320701 IAW A320 SRM 53-41-14-300-001, 51-74-00, 53-41-14-283-002, 51-72-11-911-001, 51-44-11, 51-46-11, 51-42-11, 51-75-12-911-001, A320 AMM 52-13-31-400-002A, 20-21-11-911001-A. APPLIED TEMPORARY PROTECTIONSYSTEM CIC IAW A320 AMM 51-78-00, OPERTAIONAL TEST OF THE VOR CABLE TRANSFERED TO THE LEAK & FUNCTIONAL BOOK 13875.0786 PG 10 ITEM 39. MX ACTION IS ACCEPTABLE. /END/
Earlier reports · 2012–2022 · 19 reports
2022
Part: APU — LEAKING (ZONE 100) · airframe 37,862 hrs · 15,768 cycles
DISCREPANCY: REFERENCE LP279524 #1 WHEN APU BLEED WAS USED FOR PACK 1&2 DIRTY SOCK SMELL WAS NOTED THROUGHTOUT WHOLE AC. CORRECTIVE ACTION: PERFORMED INSPECTION OF CABIN ODOR REF 05-50-810-085-A ISOLATED ODOR TO APU INSPECTED APU PER AMM 49-00-00-200-811-A PLACED APU ON MEL 49-10-01A C/N 1184122 DD 7-20-22 WITH MCC AB 434922 PLACARDS INSTALLED MX ACTIONS C/W
Part: APU — ODOR · airframe 37,614 hrs · 15,654 cycles
DISCREPANCY: REFERENCE LP228413 DIRTY SOCK SMELL DECENDING THROUGH 10000 FEET FOR SJU FORWARD AND AFT F/A REPORT SMELL AND LIGHT HEADEDNESS EVENT LASTED APPROXIMATLY 5 MINUTES F/O REPORTS OIL NEAR PACK 2 INLET ON POST FLIGHT CABIN SMELL VERIFIED BY CAPT AND F/O ON GROUND AT GATE W/PACK 2 RUNNING ON APU. CORRECTIVE ACTION: PERFORMED IDENTIFICATIONS OF CABIN ODOR FOUND PACK 2 TO BE CAUSE OF ODOR SEE LP228414 ITEM NO 1 FOR PACK 2 DEFERRAL NO OTHER FAULTS NOTED AIRCRAFT OK FOR SERVICE//END
Part: NONE — NONE · airframe 36,869 hrs · 15,313 cycles
DISCREPANCY: REFERENCE LP1276686 ITEM: DIRTY SOCK ODOR IN FLIGHT DECK AT 5000 FEET ON DESCENT BURNT RUBBER ODOR IN AFT GALLEY AT 3000 FEET CORRECTIVE ACTION REFERENCE LP1276686 ISOLATED PROBLEM TO PACKS. PERFORMED PACK BURNOUT PROCEDURE IAW AMM 21-00-00-615-802-A. NO ODOR/SMELL AT THIS TIME.
2020
Part: OIL SYSTEM — OVERSERVICED (APU) · airframe 32,674 hrs · 13,323 cycles
ONCOMING CREW REPORTED TO MX THERE WAS A SMELLY SOCK ODOR WHEN THEY TURNED ON APU BLEED. MX TROUBLESHOT AND FOUND THE APU TO BE OVERSERVICED. MX RAN BLEEDS TO BURN OUT PACKS AND BLEED LINES NO ODOR REMAINED. PERFORMED TSM FOR ODOR EVENT, FOUND APU OVER SERVICED. CLEANED UP OIL IN INTAKE, NO OTHER DEFECTS FOUND AT THE TIME. REF: TSM 05-50-00-810-831-A
2018
Part: A/C PACK — ODOR (AC BAY) · airframe 27,074 hrs · 10,944 cycles
DISCREPANCY: REFERENCE LP1133373 ITEM 2 AND 3, ODOR EVENT INFLIGHT INITIALLY NOTICED AT 9000 FT IN CLIMB. RAN QRH PROC AND ISOLATED WITH NR 2 PACK OFF. AFTER SPEAKING WITH AFT FLIGHT ATTENDANT ODOR DISSIPATED. LEFT NR 2 PACK OFF. AT TOP OF DESCENT THE FLIGHT ATTENDANT CALLED TO REPORT THAT THE ODOR WAS PERCEPTIBLE AGAIN. WE DID NOT NOTICE AGAIN UNTIL A LEVEL OFF AT 14000 FT IT WAS FAINT AND DID NOT REOCCUR AFTER. ODOR SMELLED LIKE OILY CRAYON. CORRECTIVE ACTION: DURING TROUBLE SHOOTING CONFIRMED ODOR COMING FROM PACK NR 2 AND PACK IS LOCKED OUT PER AMM 21-51-00-040-002-A. PLACED PACK 2 ON MEL 21-52-01F CONT 1143867 DUE DATE 10/29/18./END/
Part: PROXIMITY SWITCH — DEFECTIVE (R4 DOOR) · airframe 26,882 hrs · 10,863 cycles
DISCREPANCY: REFERENCE LP 1160067-3, DOOR 4R WILL NOT STAYED ARMED INFLIGHT. BOTH DOORS PAGE LOWER ECAM AND FAP SHOWED DOOR 4R DISARMED INFLIGHT. CORRECTIVE ACTION: REF N/R 2129N1, REMOVED AND REPLACED 4R DOOR PROXIMITY SWITCH PAX IAW AMM 52-71-11-000-001, 52-71-11-400-001-A OPS CHECK GOOD IAW AMM 52-71-00-710-001, TSM 52-13-00-810-805-A, AMM 52-71-00-820-002-A AND AMM 52-10-00-860-002./END/
Part: UNKNOWN — ODOR (COCKPIT) · airframe 26,855 hrs · 10,851 cycles
DISCREPANCY: REFERENCE LP1160063-1, DISCREPANCY STRONG DIRTY SOCKS SMELL IN THE COCKPIT AND AFT GALLEY ON APPROACH DURING LEVEL OFF AND ENGINE SPOOL. FA'S SMELLED ODOR FROM THE AFT GALLEY TO THE EMERGENCY EXITS OVER THE WINGS. NO ODOR IN THE FWD GALLEY. CORRECTIVE ACTION: LP1160063-1 2ND OCCURRENCE COMPLIED WITH EA# A0-21T-34386. 1ST OCCURRENCE ON LP1160061-1. NO ODORS NOTED - A/C WAS RELEASED FOR SERVICE./END/
Part: UNKNOWN — ODOR (CABIN & COCKPIT) · airframe 26,847 hrs · 10,848 cycles
ODOR EVENT DURING BASE TURN TO LAND. CABIN AND COCKPIT CREW NOTICED A BURNING WAX SMELL. SMELL DISSIPATED AFTER LANDING. NO PACKS WERE TURNED OFF. PER EA A0-21T-34386 TSM TASK 05-50-00-810-831-A, PLACED ON TDI 1142918 DUE:60 FLT CYCLES. AC WAS RELEASED FOR SERVICE.
Part: UNKNOWN — ODOR (CABIN) · airframe 26,401 hrs · 10,653 cycles
DIRTY SOCK ODOR DETECTED BY THE FLIGHT CREW AND FLIGHT ATTENDANTS. ORIGINATED IN AFT CABIN. THE ACFT WAS AT FL360. NO POWER CHANGE WAS MADE. PACK 2 WAS TURNED OFF AND THE ODOR DISAPATED, SUSPECT PACK 2 CONTAMINATION. AT TOP OF DESCENT, POWER REDUCTION, THE ODOR RETURNED WHILE USING THE NR 1 PACK. PERFORMED TSM 71-00-00-810-802-A, FOUND NO FUMES, SMOKE OR ODOR. PERFORMED A BORESCOPE OF THE STAGE 1 AND 2 BLADES (S1 AND S2). NO OIL WETTING NOTED AT THIS TIME ON THE NR 1 ENGINE IAW AMM 72-31-00-290-002.
Part: APU — ODOR · airframe 26,337 hrs · 10,626 cycles
DIRTY SOCK OR BURNING OIL ODOR NOTICED BY ALL CREW MEMEBERS WHEN BOARDING THE ACFT. ODOR NOTICED IN COCKPIT AND ENTIRE CABIN. BLEED CONFIGURATION, APU BLEED ON, NR 2 PACK ON, NR 1 PACK OFF. PERFORMED TSM 05-50-00-810-831-A. CAUSE INDICATED TO BE APU AND PERFORMED ENGINE RUN. ODOR ONLY PRESENT WITH APU RUNNING.
Part: DIAPHRAGM — DAMAGED (R1 DOOR BOTTLE) · airframe 24,814 hrs · 10,002 cycles
FWD SERVICE DOOR ASSIST BOTTLE WILL NOT HOLD PRESSURE. REMOVED AND REPLACED THE ASSIST BOOTLE DIAPHRAGM. OPS TESTED GOOD. R1 DOOR SERVICED TO 1700 PSI IAW AMM 52-10-00-420-061A, AND 52-10-00, PB 301, CONF 00. AIRCRAFT OK TO CONTINUE.
Part: STARTER — ARCED (APU) · airframe 24,415 hrs · 9,844 cycles
ECB FAULT ACTIVATED. REMOVED AND REPLACED ECB IAW AMM-49-61-34-000-003-A. FAULT CLEAR, APU START MOTOR REMAINS FAULTED. REMOVED AND REPLACED APU STARTER ASSY 8KA IAW AMM 49-42-51 AND REPLACED MONITORING WIRE RING TERMINAL. REMOVED AND REPLACED POSITIVE LEAD TERMINAL END IAW ESPM 20-48-11. OPERATIONAL CHECKED GOOD.
2017
Part: TUBE — LEAKING (APU OIL SYS) · airframe 22,705 hrs · 9,170 cycles
REPORTS OF AN ODOR IN THE COCKPIT AND CABIN BY THE FLIGHT CREW. FOUND HEAVY OIL LEACKAGE AND POOLING IN THE APU COMPARTMENT. LEAK SOURCE FOUND TO BE APU OIL COOLER FEED AND RETURN LINES. REMOVED AND REPLACED FEED AND RETURN LINES IAW AMM 20-21-11-991, AND AMM 49-91-44-400-802A. LEAK AND OPS CHECKED GOOD.
Part: TUBE — BENT (APU OIL) · airframe 22,705 hrs · 9,170 cycles
DISCREPANCY: REFERENCE LOG PAGES 9044632, 9044633 AND PEMCO NR 1781N1 REPETITIVE REPORTS OF ODOR IN THE COCKPIT AND CABIN BY THE FLIGHT CREW. FOUND HEAVY OIL LEACKAGE AND POOLING IN THE APU COMPARTMENT. LEAK SOURCE FOUND TO BE APU OIL COOLER FEED AND RETURN LINES. REMOVED AND REPLACED FEED AND RETURN LINES IAW AMM 20-21-11-991, AND AMM 49-91-44-400-802A. LEAK AND OPS CHECKED GOOD, ECS DECONTAMINATION ACCOMPLISHED ON TASK CARD 21-00-00-615-002-A.
Part: LINE — LEAKING (APU OIL SYS) · airframe 22,693 hrs · 9,164 cycles
ODOR IN CABIN. FOUND OIL SUPPLY LINE LEAKING. REMOVED AND REPLACED THE O-RING AND SECURED IAW AMM 49-99-44-400-802-A. PERFORMED OPERATIONAL CHECK FLIGHT. NO ODOR NOTED.
Part: DOOR SILL — CORRODED (FRAMES 66-68) · corrosion level 2 · airframe 20,733 hrs · 8,403 cycles
R2 DOOR SILL CORRODED AT NUTPLATE HOLES. FOUND THE R2 DOOR SILL NUT PLATE HOLES EXCEEDED ALLOWABLE LIMITS IAW SRM 53-41-14-283-002. REPAIRED THE AREA IAW SRM 51-41-14-300-001, REPAIR 5. RESTORED SURFACE PROTECTION IAW SRM 51-75-12 AND 51-23-12.
2012
Part: SKIN — DAMAGED (ZONE 200) · airframe 2,290 hrs · 927 cycles
RIGHT SKIN PANEL FROM FRAME 1 TO FRAME 12, RT WINDSHIELD LOWER SECTION TO RT SIDE STRINGER, DAMAGED .
Part: SKIN — DAMAGED (ZONE 100) · airframe 2,290 hrs · 927 cycles
RIGHT SKIN PANEL FROM FRAME 1 TO FRAME 24, STRINGER 29 TO STRINGER 37 RT, DAMAGED.
Part: BULKHEAD — DAMAGED (ZONE 100) · airframe 2,290 hrs · 927 cycles
FUSELAGE FWD BULKHEAD RT SIDE HAS DAMAGED.