N628NP
Registered owner: FLOAT ALASKA HOLDINGS LLC, AK (owner ≠ operator)
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.
9 reports on file, 2023-06-22 – 2025-10-12.
Part: BATTERY PACK — INOPERATIVE (ZONE 200)
FWD GALLEY EMERGENCY LIGHT INOP.
Part: STOP FITTING — GOUGED (ZONE 200)
L4 DOOR FWD FRAME UPPER STOP FITTING IS GOUGED.
Part: HEAT SHIELD — CRACKED (ZONE 700)
LEFT MLG BODY DOOR OUTER SURFACE HEAT SHIELD COVER IS CRACKED AND DELAMINATED.
Part: SLEEVE — DENTED (THRUST REVERSER)
NR 2 ENGINE INBD THRUST REVERSER SLEEVE HAS A DENT 18 INCHES FROM TOP EDGE AND 15 INCHES FROM FWD EDGE.
Part: PANEL — DELAMINATED (ZONE 300) · airframe 80,893 hrs · 27,304 cycles
DURING SCHEDULED "A" CK EVENT THE VERTICAL STABILIZER R/H FWD PANEL WAS FOUND DELAMINATED L=40", W=22" BETWEEN FSS195.390AND FSS 270.784. CORRECTIVE ACTION: PROCURED, LOCATED AND DRILLED NEW VERTICAL STAB R/H SIDE FIXED PANEL321CL PN: 175N20010U4 SN: 0004399709 IAW B757-200 SRM 51-40-08, B757-200SRM 51-40-05, TREATED AND PRIMED HOLES FOR THE FASTENERS AND SURROUNDING EDGES ONPANEL 321CL IAW B757-200 SRM 51-20-01, OK TO INSTALL PANEL 321CL PN: 175N2001U4 SN: 0004399709
Part: SKIN PANEL — CRACKED (ZONE 200) · airframe 82,227 hrs · 27,734 cycles
WHILE PERFORMING INSPECTIONS PER AD 2017-20-05, PARA (G), BOEING SB 757- A CRACK MEASURING 1.2" IN LENGTH WAS FOUND ON FUSELAGE SKIN PANEL P/N 141N3312-7 AT THE S-4R LAP SEAM BETWEEN BS 418 AND 439. DAMAGE WAS REPAIRED IAW BOEING MESSAGES C04-C04-25-0006-01C THROUGH -10B, 8100-9 DTD. 02/20/2025, REF. ID 202502150036-0004.
Part: GENERATOR — FAULTED (RIGHT) · airframe 82,080 hrs · 27,658 cycles
RIGHT GEN CONT OFF ILLUMINATED ON TAKEOFF
Part: TRANSMITTER — FAILED (UNKNOWN) · airframe 81,387 hrs · 27,286 cycles
AFTER FLAPS RETRACTED AIRCRAFT REQUIRED 6 UNITS OF LEFT RUDDER TRIM TO ZERO OUR YAW. WHEN FLAPS DEPLOYED PAST FLAP 5 BACK TO NORMAL. R/R FLAP TRANSMITTER
Part: BULB — BURNED OUT (ZONE 200) · airframe 81,289 hrs · 27,246 cycles
R AFT EMERGENCY DOOR LIGHT INOP - EXTERIOR LIGHT.