N219FR

No registry detail on file · not in current registry

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.

41 reports on file, 2015-09-12 – 2018-04-02.

OTHER · 2018-04-02 Matched by certificate designator
ATA 5340

Part: FITTING — CORRODED (L1 GIRT BAR) · corrosion level 2 · airframe 48,192 hrs · 19,632 cycles

L1 DOOR LOWER SILL HAS CORROSION UNDER FWD AND AFT GIRT BAR FITTING PLATE ASSBLIES. REPAIRED THE DOOR SILL GIRT BAR FITTING PLATES IAW SRM 53-11-14-283-005.

Source: SDR F3LA2018043000333
OTHER · 2018-03-05 Matched by certificate designator
ATA 5330

Part: SKIN — CRACKED (ZONE 100) · airframe 48,192 hrs · 19,632 cycles

FRAME 35, STRINGER 30L, OPEN HOLE INSPECTION IN THE SKIN REVEALED AFT LOWER HOLE WITH CRACK INDICATION. REPAIRED THE SKIN IAW SRM 51-43-00, 51-44-11, 51-42-11, 51-21-11, 51-75-12, 51-73-12, 51-24-00, 51-23-11, NTM 51-10-01, AMM 21-21-860-050-A, TDI 80434805, AND EA A2-53R-34200.

Source: SDR F3LA2018051800339
OTHER · 2018-02-28 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (FRAMES 65-66) · corrosion level 2 · airframe 48,192 hrs · 19,632 cycles

MAIN CABIN FLOOR SUPPORT, Y521.5, FRAMES 65 - 66 CORRODED. FOUND OUT OF LIMITS IAW SRM 53-00-14, REMOVED FOR REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11.

Source: SDR F3LA2018040200303
OTHER · 2018-02-28 Matched by certificate designator
ATA 5315

Part: FLOORBEAM — CORRODED (FRAME 16) · corrosion level 2 · airframe 48,192 hrs · 19,632 cycles

CABIN FLOORBEAM FWD WET AREA FRAME 16, -Y765, CORRODED. CLEANED AND EVALUATED THE AREA AND FOUND OUT OF LIMITS IAW SRM 53-11-14-283-004, LOCATED AND DRILLED NEW FLOORBEAM IAW SRM 51-42-11, TREATED AND PRIMED IAW SRM 51-21-11 AND INSTALLED THE FLOORBEAM IAW SRM 51-42-11, AND SRM 51-72-11.

Source: SDR F3LA2018040300305
OTHER · 2018-02-27 Matched by certificate designator
ATA 5320

Part: STRAP — CORRODED (DOOR SILL) · corrosion level 2 · airframe 48,192 hrs · 19,632 cycles

FWD CARGO DOOR HAS CORROSION BELOW LOWER SILL. REMOVED AND REPLACED THE STRAP ON FWD CARGO LOWER DOOR SILL IAW SRM 51-72-11, SRM 53-21-29-283-001, SRM 51-42-11, AND SRM 51-44-11.

Source: SDR F3LA2018042600327
OTHER · 2018-02-27 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (FRAME 66) · corrosion level 2 · airframe 48,192 hrs · 19,632 cycles

MAIN CABIN AFT WET AREA FLOOR SUPPORT -Y1292 AT FRAME 66 HAS CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14. REMOVED AND REPLACED THE FLOOR SUPPORT FROM FRAMES 64 - 66 IAW SRM 51-44-11, AND 51-42-11.

Source: SDR F3LA2018040200300
OTHER · 2018-02-27 Matched by certificate designator
ATA 5315

Part: FLOORBEAM — CORRODED (FRAME 66) · corrosion level 2 · airframe 48,192 hrs · 19,632 cycles

FLOORBEAM -Y765 AT FRAME 66 CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-11.

Source: SDR F3LA2018040300304
OTHER · 2018-02-27 Matched by certificate designator
ATA 5315

Part: FLOORBEAM — CORRODED (FRAME 66) · corrosion level 2 · airframe 48,192 hrs · 19,632 cycles

FLOORBEAM, Y1292 AT FRAME 66 CORRODED. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-72-11, AND SRM 53-00-14.

Source: SDR F3LA2018040300302
WARNING INDICATION · 2018-01-07 Matched by certificate designator
ATA 3230

Part: COMPUTER — FAULTY (MLG) · airframe 47,727 hrs · 19,446 cycles

LANDING GEAR SYSTEM DISAGREE. REMOVED AND REPLACED LGCIU 2, IAW AMM 32-31-71 PB401. OPS CHECKED GOOD.

Source: SDR F3LA2018010800275
Earlier reports · 2015–2017 · 32 reports

2017

FLUID LOSS; WARNING INDICATION · 2017-10-31 Matched by certificate designator
ATA 2910

Part: LINE — CHAFED (HYD SYSTEM) · airframe 46,999 hrs · 19,161 cycles

DIVERT DUE TO A GREEN HYD SYSTEM LOW LEVEL, NR 1 ENGINE PUMP PRODUCED LOW PRESSURE. REMOVED AND REPLACED THE LEFT ENGINE HYDRAULIC CONTROL UNIT PIPE IAW AMM 29-11-49-400-049-A. OPS AND LEAK CHECKED GOOD.

Source: SDR F3LA2017110200244
OTHER · 2017-05-17 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,194 hrs · 18,470 cycles

FLOOR SUPPORT Y1292 CORRODED AT FRAME 16. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11-911-001, 53-11-14-283-001, 53-00-14-283-002, 51-44-11, AND AMM 53-12-11-420-051-B.

Source: SDR F3LA2017053100157
OTHER · 2017-05-17 Matched by certificate designator
ATA 5315

Part: FLOORBEAM — CORRODED (FRAME 16) · corrosion level 2 · airframe 45,194 hrs · 18,470 cycles

FLOORBEAM Y765 CORRODED AT FRAME 16. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-72-11-911-001, 53-11-14-283-001, AND 53-00-14-283-002.

Source: SDR F3LA2017052200145
OTHER · 2017-05-15 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (FRAMES 16-20) · corrosion level 2 · airframe 45,194 hrs · 18,470 cycles

SURFACE CORROSION ON FLOOR SUPPORT Y254 FRAMES 16 - 20. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11-911-001, 53-00-14-283-002, AND 51-44-11.

Source: SDR F3LA2017053100159
OTHER · 2017-05-15 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (FRAMES 16-20) · corrosion level 2 · airframe 45,194 hrs · 18,470 cycles

SURFACE CORROSION ON THE FLOOR SUPPORT -Y254, FRAMES 16 - 20. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 53-00-14-283-002, 51-72-11-911-001, 51-44-11, 51-21-00, AND 51-23-11.

Source: SDR F3LA2017053100170
OTHER · 2017-05-15 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,194 hrs · 18,470 cycles

CORROSION FOUND ON THE FLOOR SUPPORT -765 FWD OF FR66. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11-911-001, 53-00-14-283-002, 51-42-11, AND 51-44-11.

Source: SDR F3LA2017053100160
OTHER · 2017-05-14 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (FRAME 68) · corrosion level 2 · airframe 45,194 hrs · 18,470 cycles

FLOOR SUPPORT +Y254 AFT OF FRAME 68 CORRODED. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-72-11-911-001, 53-00-14-283-002, AND 51-44-11.

Source: SDR F3LA2017053100166
OTHER · 2017-05-14 Matched by certificate designator
ATA 5315

Part: FLOORBEAM — CORRODED (FRAME 68) · corrosion level 2 · airframe 45,194 hrs · 18,470 cycles

FLOORBEAM AFT OF FRAME 68 CORRODED. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-72-11-911-001.

Source: SDR F3LA2017052300151
OTHER · 2017-05-14 Matched by certificate designator
ATA 5315

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,194 hrs · 18,470 cycles

FLOORBEAM +Y765 FWD OF FR66 CORRODED. REMOVED AND REPLACED + Y765 FLOORBEAM FWD OF FR66 IAW SRM 51-72-11, SRM 51-44-11 AND SRM 53-00-14-283-002.

Source: SDR F3LA2017052300148
OTHER · 2017-05-14 Matched by certificate designator
ATA 5320

Part: DOOR SILL — CORRODED (FRAME 66) · corrosion level 2 · airframe 45,194 hrs · 18,470 cycles

L2 DOOR SILL SPLICE PLATE FWD OF FRAME 66 CORRODED. REPLACED THE DOOR SILL IAW SRM 51-42-11, 51-72-11-911-001, 53-00-14-283-002, 51-44-11, 51-75-12, AND 51-21-11.

Source: SDR F3LA2017053100158
OTHER · 2017-05-14 Matched by certificate designator
ATA 5315

Part: FLOORBEAM — CORRODED (FRAMES 66) · corrosion level 2 · airframe 45,194 hrs · 18,470 cycles

FLOORBEAM BETWEEN Y1292 AND Y765 FOWARD OF FRAME 66 CORRODED. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-72-11, SRM 53-00-14-283-002 AND SRM 51-23-11.

Source: SDR F3LA2017052200147
OTHER · 2017-05-14 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-66) · corrosion level 2 · airframe 45,194 hrs · 18,470 cycles

FLOOR SUPPORT -Y254 BETWEEN FRAMES 64 TO 66 CORRODED AT NUTPLATES. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, 51.42-11, 53-00-14-283-002, 51-44-11, 51-21-11, AND 51-23-11.

Source: SDR F3LA2017053100168
OTHER · 2017-05-14 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (FRAME 68) · corrosion level 2 · airframe 45,194 hrs · 18,470 cycles

FLOOR SUPPORT +Y1292 AFT OF FRAME 68 CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11-911-001, 53-00-14-283-002, AND 51-44-11.

Source: SDR F3LA2017053100165
OTHER · 2017-05-14 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (FRAME 68) · corrosion level 2 · airframe 45,194 hrs · 18,470 cycles

FLOOR SUPPORT -Y254 AFT OF FRAME 68 CORRODED AT NUTPLATES. REMOVED AND INSTALLED A NEW FLOOR SUPPORT IAW SRM 51-42-11, AND 51-72-11-911-001 AND 53-00-14-283-002./END/

Source: SDR F3LA2017053100155
OTHER · 2017-05-14 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,194 hrs · 18,470 cycles

MAIN CABIN FLOOR SUPPORT -Y1292 CORRODED AFT OF FRAME 68. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11-911-001, 53-00-14-283-002, 51-21-11, AND 51-23-11.

Source: SDR F3LA2017053100156
OTHER · 2017-05-14 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 45,194 hrs · 18,470 cycles

FLOOR SUPPORT +Y1292 FWD OF FRAME 66 CORRODED. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-72-11-911-001, 53-00-14-283-002, 51-44-11, AND 51-75-12.

Source: SDR F3LA2017053100162
OTHER · 2017-05-12 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-68) · corrosion level 2 · airframe 45,194 hrs · 18,470 cycles

MAIN CABIN FLOOR SUPPORT BETWEEN FLOORBEAMS -Y765 CORRODED BETWEEN FRAMES 66 AND 68. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 53-00-14-283-002, 51-42-11, 51-72-11-911-001, 51-44-11, AND ESPM 20-33-40.

Source: SDR F3LA2017053100169
OTHER · 2017-05-12 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-68) · corrosion level 2 · airframe 45,194 hrs · 18,470 cycles

MAIN CABIN FLOOR SUPPORT Y1292 CORRODED BETWEEN FRAMES 66 AND 68. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11-911-001, 53-00-14-283-002, AND 51-44-11.

Source: SDR F3LA2017053100167
OTHER · 2017-05-12 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-68) · corrosion level 2 · airframe 45,194 hrs · 18,470 cycles

MAIN CABIN FLOOR SUPPORT -Y765 CORRODED BETWEEN FRAMES 66 AND 68. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11-911-001, 53-00-14-283-002, 51-42-11, AND 51-44-11.

Source: SDR F3LA2017053100163
OTHER · 2017-05-12 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-68) · corrosion level 2 · airframe 45,194 hrs · 18,470 cycles

MAIN CABIN FLOOR SUPPORT OTBD -Y254 CORRODED BETWEEN FRAMES 66 - 68. REMOVED AND REPLACED THE FLOOR SUPPORT IAW 51-72-11, AND SRM 53-00-14-283-002.

Source: SDR F3LA2017052200142
OTHER · 2017-05-12 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-24) · corrosion level 2 · airframe 45,194 hrs · 18,470 cycles

MAIN CABIN FLOOR SUPPORT Y254 FROM FRAMES 12 - 24 CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11-911-001, 51-44-11. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14-283-002.

Source: SDR F3LA2017053100171
OTHER · 2017-05-12 Matched by certificate designator
ATA 5315

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,194 hrs · 18,470 cycles

MAIN CABIN FLOORBEAM Y765 CORRODED BETWEEN FR66 AND FR68. REMOVED AND REPLACED Y765 BETWEEN FR66-68 IAW SRM 51-72-11, SRM 51-44-11 AND SRM 53-00-14-183-002.

Source: SDR F3LA2017052300149
OTHER · 2017-05-12 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-68) · corrosion level 2 · airframe 45,194 hrs · 18,470 cycles

MAIN CABIN FLOOR SUPPORT BETWEEN Y254 AND Y765 CORRODED BETWEEN FRAMES 66 AND 68. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11, 51-72-11-911-001, AND 53-00-14-283-002.

Source: SDR F3LA2017052200146
OTHER · 2017-05-12 Matched by certificate designator
ATA 5320

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,194 hrs · 18,470 cycles

R2 DOOR SILL PLATE CORRODED AT NUT PLATES. REMOVED AND REPLACED R2 DOOR SILL IAW A320 SRM 51-72-11 AND SRM 51-42-11.

Source: SDR F3LA2017052300150
OTHER · 2017-05-12 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (FRAMES 67-68) · corrosion level 2 · airframe 45,194 hrs · 18,470 cycles

FLOOR SUPPORT -Y1292 CORRODED BETWEEN FRAMES 67 AND 68. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 53-00-14-283-002, 51-44-11, AND 51-72-11-911-001.

Source: SDR F3LA2017053100161
OTHER · 2017-05-12 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-68) · corrosion level 2 · airframe 45,194 hrs · 18,470 cycles

MAIN CABIN FLOOR SUPPORT -Y254 CORRODED BETWEEN FRAMES 66 AND 68. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11, 51-72-11-911-001, 53-00-14-283-002, AND 51-44-11.

Source: SDR F3LA2017053100164

2016

WARNING INDICATION · 2016-05-25 Matched by certificate designator
ATA 3222

Part: STRUT — UNDERSERVICED (NLG) · airframe 41,254 hrs · 16,929 cycles

AFTER TAKEOFF, RECEIVED AN ECAM MSG, THE MLG SHOCK ABSORBER FAULT. RAN ECAM & THE ACFT RETURNED. LG VMO MMO SWITCH SELECTED TO THE LG DOWN POSITION IAW AMM 05-59-32-869-001-A. THE ACFT WAS APPROVED FOR FERRY FLIGHT. UPON INVESTIGATION MX NOTED THE MLG SHOCK ABSORBER WAS FOUND UNDER SERVICED. RE-SERVICED NLG SHOCK ABSORBER IAW MM A320-12-12-32-611-005. PERFORMED NORMAL EXTENSION & RETRACTION, NO FAULTS NOTED ON ECAM. ALL OPERATIONAL CHECKED GOOD IAW AMM A320-32-31-00-720-002.

Source: SDR F3LA2016053100049

2015

OTHER · 2015-09-20 Matched by certificate designator
ATA 5347

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,535 hrs · 15,850 cycles

CORROSION ON SEAT TRACK HARD POINT AREA Y765, FRAME 16. ORIGINAL THICKNESS .080", CURRENT THICKNESS .037" & MATERIAL LOSS 53%. REPLACED SEAT TRACK IAW SRM 51-42-11 PAR 7. MATERIAL LOSS BEYOND LIMITS IAW SRM 53 -11-14 PB 101.

Source: SDR F3LA2015092901149
OTHER · 2015-09-20 Matched by certificate designator
ATA 5347

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,535 hrs · 15,850 cycles

CORROSION ON SEAT TRACK HARD POINT AREA Y1292, FRAME 16 - 18. ORIGINAL THICKNESS .080", CURRENT THICKNESS .040" & MATERIAL LOSS 50%. REPLACED SEAT TRACK IAW SRM 51-42-11 PAR 7. MATERIAL LOSS BEYOND LIMITS IAW SRM 53-11-14 PB 101.

Source: SDR F3LA2015092901148
OTHER · 2015-09-20 Matched by certificate designator
ATA 5347

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,535 hrs · 15,850 cycles

CORROSION ON SEAT TRACK HARD POINT AREA Y254, FRAME 16. ORIGINAL THICKNESS .080", CURRENT THICKNESS .060" & MATERIAL LOSS 20%. REPLACED SEAT TRACK IAW SRM 51-42-11 PAR 7. MATERIAL LOSS BEYOND LIMITS IAW SRM 53-11-14 PB 101.

Source: SDR F3LA2015092901147
OTHER · 2015-09-13 Matched by certificate designator
ATA 5320

Part: SHEAR PLATE — CRACKED (FUSELAGE) · airframe 38,535 hrs · 15,850 cycles

MAIN CABIN FLOOR RT SHEAR PLATE IS CRACKED 4" AFT OF FRAME 69. TWO EACH CRACKS .750" & .200" IN LENGTH. REPLACED CRACKED SHEAR PLATE IAW SRM 51-42-11 PAR 6B & EO AO-53EO-31434. NO ALLOWABLE REPAIR IAW SRM 53-41-14 PB 001.

Source: SDR F3LA2015092901146
OTHER · 2015-09-12 Matched by certificate designator
ATA 5320

Part: SHEAR PLATE — CRACKED (FUSELAGE) · airframe 38,535 hrs · 15,850 cycles

MAIN CABIN FLOOR LT SHEAR PLATE IS CRACKED 4" AFT OF FRAME 69. TWO EACH CRACKS .750" & .200" IN LENGTH. REPLACED CRACKED SHEAR PLATE IAW SRM 51-42-11 PAR 6B & EO AO-53EO-31434. NO ALLOWABLE REPAIR IAW SRM 53-41-14 PB 001. NR 30686.

Source: SDR F3LA2015092801145