# Boeing 767-2J6

- Type: Aircraft model (FAA registry)
- Registry code: 1385109
- Manufacturer (registry): BOEING
- Model: 767-2J6
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Turbo-fan
- Seats: 255
- Weight class: 20,000 lb and over
- Certification: Type certificated
- Registered aircraft: 0
- Page: https://openairdocs.org/model/boeing-767-2j6

Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker.

## ADs that may apply (OpenAirDocs)

Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment.

None matched.

## Registered aircraft

None registered with this model now.

## NTSB investigations

None matched to aircraft with this model.

## FAA accident and incident reports

None matched to aircraft with this model.

## Service difficulty reports (9)

As reported by operators and repair stations, by the model named in the report.

- [SDR IXXA11KILN002S](https://openairdocs.org/sdr/IXXA11KILN002S), Jan 5, 2011: DOOR. CRACKED. DURING ROUTINE C CHECK INSPECTION FOUND A CRACK UNDER OUTBOARD HYDRAULIC BAY DOOR AFT LOWER PIN RECEPTACALE AND PIN GOUGES IN CHANNEL UNDER AFT LOWER RECEPTACAL
- [SDR IXXA11KLIN001S](https://openairdocs.org/sdr/IXXA11KLIN001S), Dec 22, 2010: STRUCTURE. DELAMINATED. DURING ROUTINE C CHECK INSPECTION FOUND DELAMINATION ON THE LEFT MAIN LANDING GEAR BODY DOOR AT AFT STOP PAD. REPAIR WAS ACCOMPLISHED IAW B767 SRM 52-00-02, 52-
- [SDR KNNA20090007](https://openairdocs.org/sdr/KNNA20090007), Jun 26, 2009: UNKNOWN. UNKNOWN. JUST AFTER ROTATION, A LOUD BANG WAS HEARD AND THE ACFT HAD A NOTICEABLE SHUDDER. DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. LANDING WAS UNEVENTFUL. SUSPE
- [SDR ABXA200905300027](https://openairdocs.org/sdr/ABXA200905300027), May 30, 2009: STIFFENER. CORRODED. STIFFENER CORRODED ON RIGHT I/B FLAP FORWARD SPAR INBOARD END. REMOVED & REPLACED STIFFENER IAW B767 SRM 51-40-02.
- [SDR ABXA200905300026](https://openairdocs.org/sdr/ABXA200905300026), May 30, 2009: PANEL. CORRODED. FAYING SURFACE FOR PANEL 655 EB CORRODED AT LWR I/B FORWARD EDGE ON INNER SURFACE. REPAIRED LOWER CHORD IAW B767 SRM 51-70-02 FIG 1 PG 3.
- [SDR ABXA200905300025](https://openairdocs.org/sdr/ABXA200905300025), May 30, 2009: CHANNEL. CORRODED. FWD SERVICE DOOR, CORNER SCUFF PLATES HAVE CORRODED STIFFENER CHANNELS. FABBED NEW STIFFENER CHANNELS FROM 7075 T6 .050 AND INSTALLED IAW B767 SRM 51-40-02.
- [SDR ABXA200905300024](https://openairdocs.org/sdr/ABXA200905300024), May 30, 2009: SKIN. CRACKED. CRACK INDICATION IN SKIN FS 1654.5 AT APPROX S3R VERIFIED WITH ET. REPAIRED IAW B767-200 SRM 53-80-01, 1 INCH CRACK.
- [SDR ABXA200905300023](https://openairdocs.org/sdr/ABXA200905300023), May 30, 2009: STRUCTURE. CRACKED. RBL 25 NOSE WHEEL WELL VERTICAL CHORD STA 287 IS CRACKED ABOVE WL 159. REPAIRED VERTICAL CHORD NWW RBL 25 STA 287 ABOVE WL 159 IAW B767 SRM 51-70-12 FIG 1, .5 I
- [SDR ABXA200905300022](https://openairdocs.org/sdr/ABXA200905300022), May 30, 2009: JACKSCREW. DAMAGED. STAB TRIM ACTUATOR BALL NUT/SCREW (JACKSCREW) FAILED INSPECTION. REMOVED AND REPLACED JACK SCREW. P/N 251T4310-1 PITTING.

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