# Boeing 747SP-J6

- Type: Aircraft model (FAA registry)
- Registry code: 1384960
- Manufacturer (registry): BOEING
- Model: 747SP-J6
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 4 · Turbo-fan
- Seats: 490
- Weight class: 20,000 lb and over
- Certification: Type certificated
- Registered aircraft: 0
- Page: https://openairdocs.org/model/boeing-747sp-j6

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 CA150612010](https://openairdocs.org/sdr/CA150612010), Jun 7, 2015: CONTROL MODULE. LEAKING. (CAN) DURING WALK AROUND, MX CREWS FOUND EVIDENCE OF HYD LEAKING COMING FROM TAIL SECTION. AFTER FURTHER INVESTIGATION, THE HYD SYS 3 WAS COMING FROM UPPER RUDD
- [SDR CA120808002](https://openairdocs.org/sdr/CA120808002), Aug 7, 2012: ROD END. SHEARED. (CAN) DURING WALK AROUND, MAINTENANCE CREW FOUND AN EVIDENCE OF HYDRAULIC LEAK COMING FROM RT INBD AILERON POWER CONTROL PACKAGE. FURTHER INVESTIGATION SHOWN TH
- [SDR CA120126002](https://openairdocs.org/sdr/CA120126002), Jan 25, 2012: ACTUATOR. FAILED. (CAN) WHILE CARRYING OUT THROTTLE RIGGING ON NR 3 ENGINE FOUND FUEL CONDITION CONTROL MOTOR ACTUATOR WITH ONE OF THE 3 ATTACH LUGS BROKEN. NO SYMPTOMS DURING AI
- [SDR CA110715004](https://openairdocs.org/sdr/CA110715004), Jul 14, 2011: HOUSING. FRACTURED. DURING TAKEOFF ROTATION, THE NR 4 HYD PRESSURE CAUTION LIGHT CAME ON. FLIGHT ENGINEER REPORTED FLUID QTY WENT TO ZERO AFTER GEAR RETRACTION. TOWER REPORTED SMOK
- [SDR CA110421002](https://openairdocs.org/sdr/CA110421002), Apr 15, 2011: CHANNEL. MISINSTALLED. (CAN) UPON REMOVAL OF LT WING L/E THROTTLE CABLE PULLEY BRACKET AT BS 445.5 FOR ACCESS, FOUND SUPPORT CHANNEL WRONGLY INSTALLED IAW IPC 76-11-44-02. AFT ATTACHM
- [SDR CA110421005](https://openairdocs.org/sdr/CA110421005), Apr 15, 2011: SUPPORT BEAM. CRACKED. (CAN) UPON LT NR 4 L/E FLAP PDU REMOVAL FOR ACCESS, FOUND PDU SUPPORT BEAM CRACKED. PART WAS REMOVED FOR REPAIR IAW SRM 51-40-03. AN INSPECTION WAS CALLED FOR A
- [SDR CA110212001](https://openairdocs.org/sdr/CA110212001), Feb 10, 2011: SLEEVE. LOOSE. WHILE REMOVING NR 2 ENGINE PYLON, FOUND A LT WING L/E FLAPS DRIVE SHAFT COUPLING SLEEVE, AT WSTA 468, WITH ATTACH SCREWS LOOSENING OUT DUE TO MISSING LOCKWIRE. 
- [SDR CA101105001](https://openairdocs.org/sdr/CA101105001), Oct 22, 2010: DUCT. BLOWN. (CAN) AT ROTATION, EXPERIENCED NOTICEABLE VIBRATION FROM THE THROTTLE QUADRANT ACCOMPANIED BY NOISE. UPON RAISING THE GEAR, LEADING EDGE ANNUNCIATOR FLICKERING 
- [SDR CA100521003](https://openairdocs.org/sdr/CA100521003), May 18, 2010: STAND OFF. BROKEN. CARRYING A ROUTINE LEAK TEST ON NR 1 AUX PITOT SYSTEM. FOUND SYSTEM LEAKING. DISCOVERED THE NR 1 AUX PITOT PRESSURE TUBE (3/8IN) AT BS 1301, WORN OPENED. THE TU

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