# Boeing 767-2Q8

- Type: Aircraft model (FAA registry)
- Registry code: 1385157
- Manufacturer (registry): BOEING
- Model: 767-2Q8
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Turbo-fan
- Seats: 292
- Weight class: 20,000 lb and over
- Certification: Type certificated
- Registered aircraft: 0
- Page: https://openairdocs.org/model/boeing-767-2q8

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 (11)

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

- [SDR IXXA20140115002](https://openairdocs.org/sdr/IXXA20140115002), Jan 14, 2014: BATTERY PACK. DISCHARGED. EMERGENCY LIGHTS WILL NOT TEST PROPERLY WHEN TESTED FROM NLG SWITCH. FOUND BATTERY PACKS M736 & M737 TO BE LOW. R & R BATTERIES, REPLACED LAMPS R3 & R4 EXTERIOR
- [SDR ABXR2011070100039](https://openairdocs.org/sdr/ABXR2011070100039), Jul 1, 2011: COWLING. WORN. NR 2 ENGINE O/B CORE COWL EXHAUST DUCT THAT MATES TO THE PRECOOLER HAS HOLE WORN THROUGH. WELDED CORE COWL IAW ROHR CMM.
- [SDR ABXR2011070100038](https://openairdocs.org/sdr/ABXR2011070100038), Jul 1, 2011: BEAM. CORRODED. T-ANGLE BEAM UNDER BULK CARGO SILL PLATE CORRODED. REMOVED AND REPLACED T-ANGLE AND WEB IAW B767 SRM.
- [SDR XV6A2011030600005](https://openairdocs.org/sdr/XV6A2011030600005), Mar 6, 2011: APU. FLAMED OUT. DURING FLIGHT AT FL390 APU FLAMED OUT WITH EICAS MSG "APU FAULT". APU IN USE AS SECOND GENERATOR. DESCENDED TO FL350 FOR RESTART. APU STARTED NORMALLY THEN FLAM
- [SDR XV6A2011F00059](https://openairdocs.org/sdr/XV6A2011F00059), Mar 6, 2011: ENGINE. FLAMED OUT. DURING FLIGHT AT FL390 APU FLAMED OUT WITH EICAS MSG "APU FAULT". APU IN USE AS SECOND GENERATOR. DESCENDED TO FL350 FOR RESTART. APU STARTED NORMALLY THEN FLAM
- [SDR ASMF201012005](https://openairdocs.org/sdr/ASMF201012005), Dec 3, 2010: SENSOR. DAMAGED. ACFT PERFORMED AN UNSCHEDULED LANDING, DURING CRUISE THE ENG OIL FILTER RT LIGHT TURNED ON WITH AN OIL TEMP INDICATION OF 60 CENTIGRADE DEGREES AND OIL PRESSURE
- [SDR XV6A2010110400013](https://openairdocs.org/sdr/XV6A2010110400013), Oct 31, 2010: WATER HEATER. ODOR. AFTER DEPARTURE FROM F/A REPORTED BURNING ODOR FROM AFT GALLEY.
- [SDR XV6A2010061400011](https://openairdocs.org/sdr/XV6A2010061400011), Jun 14, 2010: BULB. BURNED OUT. EMERGENCY EXIT LIGHT INOP LEFT SIDE EXTERNAL NR 4.
- [SDR XV6A2010053000008](https://openairdocs.org/sdr/XV6A2010053000008), May 30, 2010: SOLENOID. ODOR. ACRID ODOR NOTICED IN COCKPIT, VERIFIED IN CABIN. EXAMINATION POINTED TO COCKPIT DOOR LOCK.
- [SDR DL75E081480](https://openairdocs.org/sdr/DL75E081480), Nov 1, 2008: WARNING SYSTEM. ACTIVATED. AFTER STARTING RT ENGINE GOT STEADY RT GEN DRIVE LIGHT. IDG GEN OIL SERVICED AND INSPECTED RUN UP REFORMED AND PROBLEM CONTINUE. FWD TO MEL 24-00-01. APU OIL CH
- [SDR DL75E080772](https://openairdocs.org/sdr/DL75E080772), May 23, 2008: LIGHT. INOPERATIVE. THE 36C EMERGENCY LIGHT INOP. RELAMPED EMERGENCY LIGHT, OPS OK.

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