Registered owner
Jmac Inc
Location
Columbus, OH
Owner type
Corporation
Serial number
27809
Year built
1995
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
May 11, 1995
Certificate issued
August 20, 2026
Expires
August 31, 2033
Mode S code
A8352F

From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Rolls-Royce RB-211 model are included below.

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Airworthiness directives that may apply · 140

Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.

1973In forceSuperseded2026
ADs by the year they took effect: 211 ADs
19731
19752
19761
19771
19781
19821
19832
19864
19872
19891
19941
19951
19973
19984
20008
20015
20025
200316
20049
200510
200610
20077
200810
20093
20108
201111
201214
201315
20146
20158
20163
201711
20183
20192
20203
20213
20222
20235
20243
20251
20265
See all 211 ADs

Information bulletins that may apply · 1

Advisory, not mandatory.

NTSB investigations

No NTSB investigations matched to N628NPMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Boeing 757-2B7 aircraft

FAA incident reports

No FAA accident or incident reports matched to N628NPMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Boeing 757-2B7 aircraft

Service difficulty reports · 9

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR 7C7A2025101200043Battery Pack · inoperativeFWD GALLEY EMERGENCY LIGHT INOP.Oct 12, 2025 · N628NP · Boeing 7572B7 · Emergency LightingSDR 7C7A2025100300042Stop Fitting · gougedL4 DOOR FWD FRAME UPPER STOP FITTING IS GOUGED.Oct 3, 2025 · N628NP · Boeing 7572B7 · Fuselage Main, StructureSDR 7C7A1900010000041Sleeve · dentedNR 2 ENGINE INBD THRUST REVERSER SLEEVE HAS A DENT 18 INCHES FROM TOP EDGE AND 15 INCHES FROM FWD EDGE.Oct 2, 2025 · N628NP · Boeing 7572B7 · Engine Thrust ReverserSDR 7C7A2025100200040Heat Shield · crackedLEFT MLG BODY DOOR OUTER SURFACE HEAT SHIELD COVER IS CRACKED AND DELAMINATED.Oct 2, 2025 · N628NP · Boeing 7572B7 · Landing Gear DoorsSDR 7C7A2025060900017Panel · delaminatedDURING 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: 0004399Jun 9, 2025 · N628NP · Boeing 7572B7 · Vertical Stabilizer, Plate/SkinSDR 7C7A202502220008Skin Panel · crackedWHILE 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 Feb 21, 2025 · N628NP · Boeing 7572B7 · Fuselage Main, Plate/SkinSDR 7C7A1900010000011Generator · faultedRIGHT GEN CONT OFF ILLUMINATED ON TAKEOFFDec 11, 2024 · N628NP · Boeing 7572B7 · AC Generator-AlternatorSDR 7C7A2023081000047Transmitter · failedAFTER 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 TRANSMITTERAug 10, 2023 · N628NP · Boeing 7572B7 · Trailing Flap Position Indicating SystemSDR 7C7A2023062200039Bulb · burned outR AFT EMERGENCY DOOR LIGHT INOP - EXTERIOR LIGHT.Jun 22, 2023 · N628NP · Boeing 757200 · Emergency Lighting

STCs that may be installed · 3

Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.