N630SH

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.

4 reports on file, 2014-01-14 – 2014-05-01.

OTHER · 2014-05-01 Matched by certificate designator
ATA 5347

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 46,394 hrs · 20,892 cycles

SEAT TRACK AT BS 440 LBL 45 HAS NICKS & GOUGES. FOUND SEAT TRACK AT LBL 45, STATION 440 - 680, TO BE OUT OF LIMITS, DUE TO DAMAGE EXCEEDING THE LIMITS GIVEN IN SRM 53-00-52 FIG 101 DETAIL I. SEAT TRACK REMOVED & INSTALLED ON STAM WC 118250302DSSR10. THIS NR FOR TRACKING PURPOSES ONLY. MAJOR REPAIR CAT A.

Source: SDR FDEA201405010903
OTHER · 2014-04-21 Matched by certificate designator
ATA 5310

Part: CREASE BEAM — CORRODED (BS 1260) · corrosion level 2 · airframe 46,394 hrs · 20,892 cycles

MAIN CABIN AT BS 1260 RT INBD CREASE BEAM CORRODED. BLENDED CORROSION IAW SRM 53-40-13. FOUND TO BE OUT OF LIMITS IAW SRM 53-40-13 FIG 101 DETAIL II. REPLACED CREASE BEAM IAW SRM 51-40-02 & DWG 146N5590. REPAIR CLASSIFIED AS CATEGORY A MAJOR.

Source: SDR FDEA201404210781
FLT CONT AFFECTED; WARNING INDICATION · 2014-01-15 Matched by certificate designator
ATA 2750

Part: FSEU — MALFUNCTIONED (NR 1) · airframe 46,388 hrs · 20,891 cycles

LEADING EDGE SLAT ASYM ON TAKEOFF, OCCURRED AT WEIGHT OFF WHEELS ON TAKEOFF ROTATION. IAW AML 1565931 REPLACED NR 1 FSEU IAW MM 27-51-01-2. REPLACED RT INBD SLAT LOSS SWITCH IAW MM 27-81- 41-4. OPERATIONS CHECKED BAD, SUSPECT OUT OF ADJUSTMENT.

Source: SDR FDEA201401150106
OTHER · 2014-01-14 Matched by certificate designator
ATA 2822

Part: CIRCUIT BREAKER — TRIPPED (BOOST PUMP) · airframe 46,388 hrs · 20,891 cycles

DURING CLIMB OUT 20 MINS INTO FLIGHT, LT FWD BOOST PUMP CIRCUIT BREAKER TRIPPED.

Source: SDR FDEA2014011400119