- Registered owner
- Bc2 43862 LLC
- Location
- Camden, DE
- Owner type
- LLC
- Serial number
- 43862
- Year built
- 2017
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- April 5, 2017
- Certificate issued
- April 6, 2017
- Expires
- April 30, 2027
- Mode S code
- A540E2
From the FAA registry file of October 22, 2026. The registry lists only the engine series, so ADs for every GE GENX model are included below.
On this page
Airworthiness directives that may apply · 104
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2012 | 1 |
|---|---|
| 2013 | 1 |
| 2014 | 1 |
| 2015 | 3 |
| 2016 | 9 |
| 2017 | 6 |
| 2018 | 15 |
| 2019 | 7 |
| 2020 | 11 |
| 2021 | 9 |
| 2022 | 14 |
| 2023 | 10 |
| 2024 | 8 |
| 2025 | 9 |
| 2026 | 18 |
See all 122 ADs
Information bulletins that may apply · 9
Advisory, not mandatory.
Airframe · Boeing 787-9
SAIB 2025-09INSTRUMENT PANEL, Potential Installation of Lockwire on Switch Guards that May Restrict Access to Passenger Oxygen and Ram Air Turbine (RAT) SwitchesSAIB AIR-22-09R1AUTOPILOT FLIGHT DIRECTOR SYSTEM: ALT HOLD Engaged on Takeoff on Boeing Model 777/787 common fleets.SAIB AIR-20-19Flight Management Computing Software SystemSAIB AIR-20-15Navigation Localizer SystemSAIB NM-20-07Navigation - Glideslope SystemSAIB NM-20-06Electrical Power System: Lug Terminal TracksSAIB NM-18-33Engine Fuel and ControlSAIB NM-17-15Equipment/Furnishings - Inflatable Airbag AssemblySAIB NM-15-03Flight ControlsNTSB investigations
No NTSB investigations matched to N438AMMatched 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 787-9 aircraft
FAA incident reports
No FAA accident or incident reports matched to N438AMMatched 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 787-9 aircraft
Service difficulty reports · 12
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR ASMF20260910201Warning Message · illuminatedSTATUS MESSAGE "ENG EEC C1 R", BY MESSAGE WAS PERFORMED TEST IAW FIM DMC B787-A-G73-20-F1-L8A-421A-A.SDR ASMF2026030300008Latch · missingDURING WALK AROUND INSPECTION L ENG WAS FOUND ITH THRUST REVERSER TENSION LATCH MISSING. LT ENG T/R TENSION LATCH INSTALLED IAW TASK AMM DMC B787-A-G78-31-04-00A-720A-ASDR ASMF202110007Flaperon · damagedDURING TRANSIT CHECK, IT WAS DETECTED A SEVERAL LIGHTNING STRIKES ON RH WING FLAPERON TRAILING EDGE. MAINTENANCE PERSONNEL PERFORMED A LIGHTNING STRIKE CONDITIONAL INSPECTION PHASE 1A, LEVEL EXAMINATION AND PHASE 1B AND II, GENERAL VISUAL INSPECTION AND SYSTEMSDR ASMF202104005Brake · overtempDURING TRANSIT CHECK, IT WAS DETECTED HIGH TEMPERATURE IN MAIN BRAKE ASSEMBLY NUMBER 5 WITHOUT FLAT TIRE WITH DISCHARGE THE FIRE EXTINGUISHER IN THE MAIN BRAKE NUMBER 5. MAINTENANCE PERSONNEL PERFORMED HIGH ENERGY STOP / HEAT DAMAGE CONDITION INSPECTION WAS PESDR ASMF202101014Skin · dentedDURING TRANSIT CHECK, IT WAS DETECTED DAMAGES ON RIGHT WING. MAINTENANCE PERSONNEL PERFORMED REVISION, DETECTING SEVERAL DENTS, GOUGES, NICKS, SCRATCHES, DELAMINATION AND STATIC DISCHARGER NUMBER 4 ON RIGHT WING. THE WO´S 7193314, 7193319, 7193321, 7193322, 7SDR ASMF202011008Skin · damagedDURING OVERNIGHT CHECK AT MEX STATION, IT WAS DETECTED TWO NICKS AT FUSELAGE SKIN SECTION 41 BETWEEN STRINGERS S-39L AND S-38L. MAINTENANCE PERSONNEL PERFORMED A REVISION, DETECTING A NICK OF 0.250" DIAMETER STA 348 AND A NICK OF 0.250" DIAMETER STA 349 A UT-SDR ASMF2020090711Engine · damagedIAW CNR 20200717011 OF REMOTE DIAGNOSTIC GE/CFM SYSTEM AT MEX, THE LEFT ENGINE HAD A TREND CHANGE IN COMPRESSOR EFFICIENCY, DUE TO PISTON RING DISTRESS. MAINTENANCE PERSONNEL PERFORMED THE LT ENG BORESCOPE INSPECTION OF THE HIGH PRESSURE COMPRESSOR, IAW SB 72SDR ASMF2020090708Engine · vibrationCAPTAIN REPORTED THAT DURING CRUISE, THE RIGHT ENGINE VIBRATION EICAS MESSAGE VIBRATION INDICATION HIGH RIGHT ENGINE WITH FAILURE CODE OF FDE 710 342 52. MAINTENANCE PERSONNEL PERFORMED FIM DMC-B787-A-G77-30-F1-50A-421A-A PROCEDURE, DETECTING THE MAINTENANCE SDR ASMF20200603023Deflector · crackedIN ACCORDANCE WITH MAINTENANCE PROGRAM 600 FC CHECK, IT WAS FOUND TWO AXIAL CRACKS WITH 0.268" AND 0.263", SPACED AT 0.305" BETWEEN CRACKS, LOCATED ON CUP 22 DOME DEFLECTOR OF LEFT ENGINE COMBUSTION CHAMBER. PERMITTED FOR 100 FC FOR A ONE TIME RECOMMENDATIONSDR ASMF201904230016Skin · damagedCAPTAIN REPORTED A LIGHTNING STRIKE ON THE LEFT FRONT SIDE OF THE AIRCRAFT. MAINTENANCE PERSONNEL PERFORMED A CONDITIONAL INSPECTION IAW AMM DMC B787-A-05-51-19-00C-280B-A, DETECTING DAMAGES AT RH ICE DETECTOR PROBE, AT LEFT REAR POSITION LIGHT; AT LOWER FUSELSDR ASMF201901090013Control Unit · crackedCAPTAIN REPORTED THAT DURING DESCENT, THE RIGHT WINDSHIELD HEAT PROTECTION UNIT WAS CRASHING; MAINTENANCE PERSONNEL PERFORMED INSPECTION FOUND WINDSHIELD HEAT PROTECTION UNIT CRACKED; AIRCRAFT WAS SENT TO THE HANGAR AND MAINTENANCE PERSONNEL REPLACED THE RH WISDR ASMF2018010100001Starter Gen · damagedDURING A TRANSIT CHECK, AN OIL LEAK WAS DETECTED IN THE VARIABLE FREQUENCY STARTER GENERATORS L1 AND L2. MAINTENANCE PERFORMED REVISION DETECTING THE VARIABLE FREQUENCY STARTER GENERATORS SENSOR SCREWS BROKEN SO THE VARIABLE FREQUENCY STARTER GENERATORS WERE
STCs that may be installed · 56
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.