N209FR

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.

7 reports on file, 2012-09-15 – 2017-03-29.

OTHER · 2017-03-29 Matched by certificate designator
ATA 5322

Part: SHEAR TIE — CRACKED (FRAME 67) · airframe 21,746 hrs · 8,781 cycles

SHEAR TIE CRACKED AT FRAME 67, STRINGER 23R. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-42-11.

Source: SDR F3LA2017041300100
OTHER · 2017-03-23 Matched by certificate designator
ATA 5320

Part: DOOR SILL — CORRODED (FRAME 66) · corrosion level 2 · airframe 21,746 hrs · 8,781 cycles

L2 DOOR SILL LOWER CUT OUT FRAME 66, STRINGER 23, HAS SURFACE CORROSION ALONG OTBD SCREW ATTACHMENT HOLE. REMOVED AND REPLACED L2 DOOR SILL IAW SRM 53-41-14.

Source: SDR F3LA2017041200096
OTHER · 2017-03-23 Matched by certificate designator
ATA 5320

Part: DOOR SILL — CORRODED (FRAME 66) · corrosion level 2 · airframe 21,746 hrs · 8,781 cycles

R2 DOOR LOWER AFT CUT OUT FRAME 66, STRINGER 23, HAS SURFACE CORROSION AROUND OTBD SCREW ATTACHMENT HOLE. REMOVED AND REPLACED R2 DOOR SILL IAW SRM 51-72-11-911-001.

Source: SDR F3LA2017041200095
OTHER · 2017-03-19 Matched by certificate designator
ATA 5330

Part: SKIN — DENTED (FRAMES 78-79) · airframe 21,746 hrs · 8,781 cycles

FUSELAGE DENTED BETWEEN STRINGERS 16 AND 17L, FRAMES 78 AND 79. DENT FOUND TO BE OUT OF LIMITS IAW SRM 53-11-283-009, FIGURE 1 DIAGRAM 1, REPAIRED IAW SRM 53-51-11-300-002.

Source: SDR F3LA2017041300097
OTHER · 2017-03-19 Matched by certificate designator
ATA 5320

Part: ANGLE — CORRODED (FRAMES 31-33) · corrosion level 2 · airframe 21,746 hrs · 8,781 cycles

FORWARD CARGO, LEFT SIDE TRANSITION ANGLE BETWEEN FRAMES 31-33, CORROSION AROUND FASTNER HOLES. REMOVED AND REPLACED FOWARD CARGO TRANSITION ANGLE IAW SRM 51-72-11.

Source: SDR F3LA2017041300099
OTHER · 2017-03-19 Matched by certificate designator
ATA 5330

Part: SKIN — DENTED (FRAME 23) · airframe 21,746 hrs · 8,781 cycles

EXTERIOR FUSELAGE SKIN DENTED AT FRAME 23 + 15" STRINGER 24L. CUT OUT DAMAGE AREA, FABRICATED AND INSTALLED A DOUBLER REPAIR IAW SRM 53-11-11, AND 53-00-00-11-300-042.

Source: SDR F3LA2017041300098
OTHER · 2012-09-15 Matched by certificate designator
ATA 5411

Part: SPAR — CHAFED (ZONE 400) · airframe 5,152 hrs · 2,039 cycles

C-CHECK: LT ENGINE PYLON, AFT REMOVABLE FAIRING. HYD LINE CHAFED INTO SPAR BETWEEN RIBS 13 AND 14, C1 CHECK. BLENDED OUT CHAFE APPRX DIMENSIONS 1.7" X .25" INSTALLED DOUBLER IAW EA A2-54R-32441. HYD LINE REPOSITIONED TO CREATE MORE CLEARANCE.

Source: SDR F3LA2012091700791