N221FR
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.
32 reports on file, 2014-06-13 – 2019-07-30.
Part: STRINGER — CORRODED (FRAMES 64-65) · airframe 40,712 hrs · 19,839 cycles
AFT WET AREA CORRODED BETWEEN FRAMES 64-65, STRINGER 26R. REPAIRED STR 26R SECTION BETWEEN FR64 AND FR65 IAW DOSSIER 80662279 AND EA A2-53R-34906.
Part: FITTING — CORRODED (R2 DOOR SILL) · airframe 40,712 hrs · 19,839 cycles
AFTER REMOVAL OF R2 DOOR SILL, FWD CORNER FOUND TO BE CORRODED. REMOVED AND REPLACED R-2 DOOR SILL FWD CORNER FITTING IAW SRM 51-72-11-911-001 .
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,712 hrs · 19,839 cycles
DISCREPANCY : REFERENCE NR #2577N735 FUSELAGE TOP SIDE ADF 1 ANTENNA ATTACH FASTNER HOLES ARE CORRODED. CORRECTIVE ACTION: PERFORMED ADF 1 ANTENNA REPAIR ON THE SKIN BETWEEN FR44 AND FR45 STR 2R IAW T/D 80667193/005/2019 #A (SEE DETAILS BACK ). OP TEST OF ADF SYS PASSED IAW AMM 34-53-00-710-002-A
Part: SUPPORT FRAME — CORRODED (FRAME 69-70) · airframe 40,712 hrs · 19,839 cycles
AFTER REMOVAL OF RT SHEAR-PLATE FOUND FRAME SUPPORT CORRODED. REMOVED AND INSTALLED NEW SUPPORT FRAME AT R/H FRAME 69TO 70 IAW SRM 51-42-11
Part: FRAME ANGLE — CORRODED (ZONE 100) · airframe 40,712 hrs · 19,839 cycles
AFTER REMOVAL OF LT SHEAR PLATE FOUND FRAME SUPPORT CORRODED. REMOVED AND REPLACED CORRODED FRAME SUPPORT IAW SRM 51 -42-1 1, SRM 51-44-11 & SRM 51-23-11.
Part: DOOR SILL — CORRODED (FRAME 68) · airframe 14,712 hrs · 19,839 cycles
L2 DOOR SILL CORRODED AT Y1732 FR 68. REMOVED AND REPLACED L2 DOOR SILL IAW SRM 51 -42-11 AND 51 -72-11 .
Part: SHEAR WEB — CORRODED (FRAMES 68-70) · airframe 40,712 hrs · 19,839 cycles
AFT GALLEY AFT LT SHEAR WEB AT FR 70 TO FR 68 CORRODED. REMOVED AND REPLACED THE SHEAR WEB IAW AMM 51-74-11.
Part: FITTING — CORRODED (L2 DOOR SILL) · airframe 40,712 hrs · 19,839 cycles
L2 DOOR SILL FWD CORNER SHAPE CORRODED. REMOVED AND REPLACED L2 DOOR SILL FWD CORNER FITTING IAW A320 SRM 51 -42-11 AND 51-72-11
Part: FLOOR SUPPORT — CORRODED (FRAME 66) · airframe 40,712 hrs · 19,839 cycles
AFT CABIN FLOOR SUPPORT AT FRAME 66, Y765 HAD CORROSION ON TOP SURFACE NEAR ATTACHMENT HOLES. REMOVED AND REPLACED FLOOR SUPPORT FROM FRAMES 64 TO 66, IAW SRM 51-72-11.
Part: DOOR SILL — CORRODED (L2 DOOR AREA) · airframe 40,712 hrs · 19,839 cycles
L2 DOOR SILL CORRODED AT FWD SPLICE FRAME 66. REMOVED AND REPLACED FWD SPLICE IAW SRM 51-72-11-911-001.
Part: DOOR SILL — CORRODED (R2 DOOR AREA) · airframe 40,712 hrs · 19,839 cycles
R2 DOOR SILL CORNER SHAPE CORRODED. REMOVED AND REPLACED R2 DOOR SILL AFT CORNER SHAPE SILL IAW A320 SRM 51-42-11, A320 SRM 51-44-11 AND A320 SRM 51 -72-11-911-002.
Part: FLOOR SUPPORT — CORRODED (FRAME 68) · airframe 40,712 hrs · 19,839 cycles
AFT CABIN FLOOR SUPPORT AT FR 68, Y765 HAD CORROSION ON TOP SURFACE NEAR ATTACHMENT HOLES. REMOVED AND REPLACED FLOORBEAM AT FRAMES 66 - 70, Y765 IAW SRM 51-72-11, AND 51-44-11.
Part: FLOORBEAM — CORRODED (FRAME 68) · airframe 40,712 hrs · 19,839 cycles
AFT CABIN FLOOR BEAM AT FR 68 (-YL 292) HAS CORROSION ON TOP SURFACE NEAR ATTACHMENT HOLES. MAX. ALLOWABLE MATERIAL LOSS .016" MAT LOSS .050, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14-283-02 AND REMOVED AND REPLACED NEW FLOORBEAM IAW SRM 51-44-11
Part: FLOORBEAM — CORRODED (FRAME 66) · airframe 40,712 hrs · 19,839 cycles
AFT CABIN FLOOR BEAM AT FR66 (-Y765) HAS CORROSION ON TOP SURFACE NEAR ATTACHMENT HOLES. REMOVED AND INSTALLED NEW FLOOR BEAM IAW SRM 51-72-11 AND SRM 51-42-11
Part: FLOORBEAM — CORRODED (FRAME 66) · airframe 40,712 hrs · 19,839 cycles
AFT CABIN FLOORBEAM AT FR 66, YSL 2. HAD CORROSION ON TOP SURFACE NEAR ATTACHMENT HOLES. DAMAGE LOCATED AT HARDPOINT. FOUND TO BE OUT OF LIMITS IAW 53-00-14-283-002. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-72-11, AND 51-42-11.
Part: DOOR SILL — CORRODED (FRAME 68) · airframe 40,712 hrs · 19,839 cycles
R2 DOOR SILL CORRODED AT Y1732, FRAME 68. CORROSION ON R2 DOOR SILL EXCEEDS ALLOWABLE DAMAGE LIMITS OF SRM 53-41-14-283-002. REMOVED AND REPLACED R2 DOOR SILL IAW SRM 51-72-11-911 -001.
Part: FITTING — CORRODED (L2 DOOR SILL) · airframe 40,712 hrs · 19,839 cycles
AFTER REMOVAL OF L2 DOOR SILL, AFT CORNER FOUND TO BE CORRODED. REMOVED AND REPLACED L2 DOOR AFT CORNER FITTING IAW SRM 51-42-11 AND 51-72-11-911-001 .
Part: DOOR SILL — CORRODED (R2 DOOR) · airframe 40,712 hrs · 19,839 cycles
R2 DOOR SILL CENTER SHAPE SILL CORRODED. REMOVED AND REPLACED R2 DOOR SILL CENTER SHAPE SILL IAW SRM 51-42-11, SRM 51-44-11, AND SRM 51-72-11-911-002.
Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 40,712 hrs · 19,839 cycles
DISCREPANCY: REFERENCE N/R# 2577N447 AFT GALLEY AFT R/H SHEAR WEB AT FR70 TO FR68 CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED RT SHEAR WEB AT FR70 TO FR68 IAW SRM 51-42-11, 51-44-11. AMM 38-31-36-400-001-A, AND 38-31-36-710-050-A.
Part: FLOORBEAM — CORRODED (FRAME 68) · airframe 40,712 hrs · 19,839 cycles
AFT CABIN FLOORBEAM FR 68, -Y765, HAD CORROSION ON TOP SURFACE NEAR ATTACHMENT HOLES. REMOVED AND REPLACED FLOORBEAM AT FR68 -Y765 IAW SRM 51-72-11-911-001
Part: FLOORBEAM — CORRODED (FRAME 16) · airframe 40,712 hrs · 19,839 cycles
FWD CABIN FLOORBEAM CORRODED AT 7087, FRAME 16, Y290. REMOVED CORROSION AND EVALUATED THE FLOORBEAM. ORIGINAL MATTHICKNESS IS .149'~ REMOVED .D70 MAT., MAX ALLOWED REMOVED IS .047" FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14-283-004. REMOVED AND REPLACED THE FLOORBEAM IAW IAW SRM 51-42-11.
Part: DOOR FRAME — CRACKED (EMERGENCY EXIT) · airframe 40,712 hrs · 19,839 cycles
R/H AFT EMERGENCY OVERWING EXIT HAS INDICATIONS OF CRACKING IN THE AFT I/B FRAME. REPAIRED FRAME AT R/H AFT EMERGENCY OVERWING EXIT IAW A320 EA# A2-52R-34616
Part: DOOR FRAME — CRACKED (EMERGENCY EXIT) · airframe 40,712 hrs · 19,839 cycles
L/H AFT EMERGENCY OVERWING EXIT HAS INDICATIONS OF CRACKING IN THE FWD 1/B FRAME. REPAIRED FRAME AT L/H AFT EMERGENCY OVERWING EXIT IAW A320 EA# A2-52R-34616
Part: DOOR FRAME — CRACKED (EMERGENCY EXIT) · airframe 40,712 hrs · 19,839 cycles
RT AFT EMERGENCY OVERWING EXIT HAS INDICATIONS OF CRACKING IN THE FWD 1/B FRAME. REPAIRED FWD 1/B FRAMER/HAFT EMERGENCY DOOR JAW EA# A2-52R-34616
Part: BATTERY — FAILED (CABIN) · airframe 40,117 hrs · 19,582 cycles
DISCREPANCY: REFERENCE LOG PAGE LP1111414 ITEM 1, EMERGENCY BATTERY UNITS FAILED BITE TEST AT FIN #10WL AND 13WL. CORRECTIVE ACTION: REFERENCE LOG PAGE LP1111414 ITEM 1(LAS), PLACED ON MEL 33-50-09A, CONTROL NUMBER 1149938, DUE 5-14-19. CORRECTIVE ACTION: REFERENCE LOG PAGE LP1111416 ITEM 3(DEN), REFERENCE MEL 33-50-09A EMERGENCY BATTERY UNITS FAILED TEST. REFERENCE ASM 33-51-02 P0051 SHEET 3, RECONNECTED AFT RIGHT DOOR SLIDE, OPS CHECK GOOD REFERENCE AMM 33-51-00-710-001 AND 33-51-00-720-001-A. CONTROL NUMBER 1149938 REMOVED./END/
Part: DOOR FRAME — CRACKED (EMERGENCY EXIT) · airframe 39,218 hrs · 19,214 cycles
L/H FWD EMERGENCY EXIT HATCH, AFT INBD FRAME HAS A CRACK INDICATION. REPAIRED L/H FWD EMERGENCY EXIT HATCH AFT INBOARD FRAME IAW E.A. # A2-52R-34616.
Part: DOOR FRAME — CRACKED (EMERGENCY EXIT) · airframe 39,218 hrs · 19,214 cycles
R/H AFT EMERGENCY EXIT HATCH, FWD INBD FRAME HAS A CRACK INDICATION. REPAIRED R/H AFT EMERGENCY EXIT HATCH FWD INBOARD FRAME IAW FRONTIER E.A. # A2-52R-34616./END/
Part: THRESHOLD — CORRODED (FWD CARGO) · corrosion level 2 · airframe 39,218 hrs · 19,214 cycles
FWD CARGO DOOR THRESHHOLD CORRODED OUTER EDGE. EVALUATED AND REPAIRED FWD CARGO DOOR THRESHOLD IAW A320 SRM 51-74-00, 51-42-11 AND AMM 53-22-14-400-001-A.
Earlier reports · 2014–2018 · 4 reports
2018
Part: HYDRAULIC SYSTEM — OVERSERVICED (GREEN) · airframe 37,663 hrs · 18,537 cycles
DURING CRUISE FLIGHT, THE FLIGHT ATTENDANTS IN BACK OF ACFT NOTICED AN ODOR OF DIRTY SOCKS, BURNING FUMES. AFTER TURNING OFF THE NR 2 PACK, THE ODOR DISSIPATED. PERFORMED IDENTIFICATION OF CAUSE OF CABIN ODOR IAW TSM 05-50-00-810-831-A. FOUND GREEN HYDRAULICS OVERSERVICED AND ECO BOTTLE FULL. ODOR CAUSED BY APU INLET INGESTING HYDRAULICS. CLEANED AND EMPTIED THE BOTTLE AND AREA. RAN THE NR 1 & 2 PACKS WITH APU FOR 20 MINUTES. NO ODORS DETECTED. AIRCRAFT RETURNED TO SERVICE.
2014
Part: WIRE — LOOSE (CABIN) · airframe 21,567 hrs · 12,098 cycles
EMERGENCY LIGHTS SEAT ROW 10, 11 & 12 INOPERATIVE. TERMINATED WIRING AT TERMINAL BLOCK 7225VT NR 12. OPERATIONAL CHECK OF EMER LIGHTS NORMAL IAW AMM 33-51-00-710-001.
Part: HYDRAULIC LINE — CHAFED (HYDRAULIC SYS) · airframe 21,264 hrs · 11,959 cycles
HYD Y RSVR LO LVL ON CLIMB OUT. YELLOW HYD QTY SHOWED ZERO. ACCUMULATOR PRESS REMAINED NORMAL. REPLACED RT ENG HYD HOSE. OPERATIONS & LEAK CHECKED GOOD IAW AMM 29-13-49-000-002 & 29-13-49-400-002. TORQUE WRENCH F9TAB2197C DUE 03-14 & F9TAB0435C DUE 06-14.
Part: COMPUTER — FAILED (ZONE 100) · airframe 21,257 hrs · 11,956 cycles
UPON THRUST REDUCTION AFTER TAKEOFF ACFT ENTERED ALT LAW & END. R & R NR 1 ELAC. OPERATIONS TESTED GOOD IAW MM 278-93-34 PB 401. PERFORMED LAND CAT 3 CAPABILITY TEST. OPERATIONS TESTED GOOD IAW AMM 22-97-00-710-001. ACFT RETAINS CAT IIIB STATUS.