N641

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

GRUMMAN G21 No injuries Part 91operator not named in the NTSB record
Source: NTSB case UNK64X1861

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.

5 reports on file, 2003-11-29 – 2019-02-27.

NO TEST · 2019-02-27 Matched by certificate designator
ATA 3350

Part: CRADLE — DEFECTIVE (CABIN) · airframe 40,652 hrs · 26,924 cycles

NDIS 641 33-40 0021530 27FEB19 RIC CLOSE LT & RT ABOVE WING EMERGENCY LIGHTS ARE INOP. 26924 00 NGR FACT 27FEB19 11:05 RIC R/R'D #400 EMERGENCY BATTERY/CRADLE ASSY IAW AMM 33-30-04-000/400-801-A. NO DEFECTS NOTED OK FOR SERVICE.

Source: SDR HNAA2019030100055
OTHER · 2017-05-18 Matched by certificate designator
ATA 3240

Part: BRAKE SYS — CONTAMINATED · airframe 41,121 hrs · 37,203 cycles

BRAKE OUTBOARD INOPERATIVE CAUTION LIGHT APPEARED TWICE. TROUBLESHOT IAW FIM 32-41-00-810-801-A. FOUND AIR BUBBLES IN SYSTEM 2 OF THE BRAKES. BLED BRAKES OF AIR BUBBLES IAW MM 32-40-22, LEAK AND OPS CHECKED GOOD. OK FOR SERVICE.

Source: SDR HNAA
WARNING INDICATION · 2017-05-18 Matched by certificate designator
ATA 3240

Part: BRAKE SYS — CONTAMINATED · airframe 41,121 hrs · 37,203 cycles

BRAKE INOPERATIVE CAUTION LIGHT APPEARED TWICE. TROUBLESHOT IAW FIM 32-41-00-810-801-A. FOUND AIR BUBBLES IN THE SYSTEM. BLED BRAKES OF AIR BUBBLES IAW MM 32-40-22, LEAK AND OPS CHECKED GOOD. OK FOR SERVICE.

Source: SDR HNAA2017051900173
WARNING INDICATION · 2017-05-17 Matched by certificate designator
ATA 3620

Part: O-RING — FAILED (BLEED SYSTEM) · airframe 41,117 hrs · 37,197 cycles

AFTER PUSHBACK, STARTED NR 1 ENGINE, BLEED 1 LEAK MASTER WARNING AND EICAS MESSAGE ILLUMINATED AND LEAK INSCRIPTION BAR ILLUMINATED. INSPECTED THE NR 1 BLEED SYSTEM, FOUND A BROKEN O-RING ON THE BLEED SYSTEM JOINT UNDER PANEL 271DLW. REMOVED AND REPLACED THE O-RING IAW MM 36-11-10-400-801-A. OPS AND LEAK CHECKED GOOD. NO DEFECTS. OK FOR SERVICE.

Source: SDR HNAA2017051900175
OTHER · 2003-11-29 Matched by certificate designator
ATA 2710

Part: CONTROL CABLE — CHAFED (AILERONS) · airframe 949 hrs · 764 cycles

PERFORMED AILERON WING CABLE INSPECTION PER CESSNA ASL560XL-27-12, FOUND CABLES CHAFED/BROKEN BEYOND MANUFACTURER'S LIMITS. REMOVED AND REPLACED LEFT AND RIGHT WING AILERON CABLES IAW CESSNA 560XL MM CHAPTER 27-10-03.

Source: SDR DXTA200300192