# Service difficulty reports: Boeing 767-259

A list on [Boeing 767-259](https://openairdocs.org/model/boeing-767-259.md).

Newest first. General aviation reporting is voluntary.

- [SDR ANCF2009042500041](https://openairdocs.org/sdr/ANCF2009042500041.md): Access Door · broken · Apr 25, 2009 · N985AN · Boeing 767259 · Service Doors
  > A STRONG NOISE FELT DURING DESCEND IN THE AFT PART OF THE FUSELAGE. UPON INSPECTION FOUND HYDRAULIC RESERVOIR FILL ACCESS DOOR MISSING IAW AMM 52-49-12/401. REMOVED AND REPLACED HYDRAULIC RESERVOIR FILL ACCESS DOOR. OPS CHECK NORMAL, P/N 149T7611-9.
- [SDR ANCF200800027](https://openairdocs.org/sdr/ANCF200800027.md): Control Rod · defective · Oct 31, 2008 · N986AN · Boeing 767259 · Leading Edge Slat Control System
  > AIR TURN BACK REPORT LEADING EDGE SLAT ASYM EICAS MSG, DISPLAYED AT 400 FT WITH LEADING EDGE LIGHT ON WITH FLAPS TO 5 DEGREE WHILE TURNING LT WITH 180KTS, 25 DEGREE BANK, WITHOUT FLAPS MOVEMENT STICK SHACKER WAS ACTIVATED WITH NO REASON AND STOPPED FEW SECOND
- [SDR 2008FA0000478](https://openairdocs.org/sdr/2008FA0000478.md): Window · leaking · Jun 18, 2008 · N985AN · Boeing 767259 · Flight Compartment Windows
  > REJECTED TAKEOFF, VERY STRONG NOISE AT 2R WINDOW DURING ROLL. IT WAS APPLY SEALANT IN THE FINISH AROUND THE WINDOW EDGE IAW AMM 56-11-00 PAGE 801, DID THE WINDOW TEST IAW AMM 56-11-02, PAGE 601, TEST OK. (K)
- [SDR ANCF200800003](https://openairdocs.org/sdr/ANCF200800003.md): Pump · malfunctioned · Feb 3, 2008 · N986AN · Boeing 767259 · Hydraulic Pump (Electric/Engine), Main
  > C ACMP 04=1 PRESS IS ZERO. EICAS MSG C HYD SYS MAINT IS DISPLAYED. PRESS NORMAL WHEN USING OTHER ACMP. EICAS MSG DOORS DISPLAYED & DOOR AMBER LIGHT ILLUM WITH MLG DOWN MSG & LGT REMAINED ILLUM AFTER LANDING. NLG GREEN DOWN LIGHT FAIL TO ILLUM WITH MLG HAND
- [SDR ANCF200700027](https://openairdocs.org/sdr/ANCF200700027.md): Filter · clogged · Oct 30, 2007 · N985AN · Boeing 767259 · Aircraft Fuel Filter/Strainer
  > RT ENGINE FUEL FILTER DISPLAYED ON EICAS MESSAGE IAW AMM 73-11-02 /401 THE FUEL PUMP FILTER WAS REMOVED AND REPLACED AND TEST WITH RUNNING ENGINE SATISFACTORY (FILTER PN 218321).
- [SDR ANCF200700016](https://openairdocs.org/sdr/ANCF200700016.md): Duct · loose · Jun 27, 2007 · N986AN · Boeing 767259 · Air Distribution System
  > L DUCT LEAK LGT ILLUM, EICAS MSG BLD DUCT LEAK DISPLAYED, LGT EXTINGUISH AFTER ENG BLEED AIR SUPPLY AND ISOLATION VALVES CLOSED. PERFORMED PNEUMATIC DUCT FLEXIBLE BALL JOINTS INSPECTION IN ACCORDANCE WITH AMM 36-11-01 FOUND 1 OF 5 FLEXIBLE JOINT LOOSE. RETIG
- [SDR ANCF200600047](https://openairdocs.org/sdr/ANCF200600047.md): Skin · delaminated · Feb 28, 2007 · N986AN · Boeing 767259 · Trailing Edge Flaps
  > NON ROUTINE WRITEUP. N: 448686-135: RT IB FLAP. AFT FLAP LOWER SKIN WITH DELAMINATION. DELAMINATION WAS FOUND ON THE WEDGE LOWER AND UPPER SKIN BETWEEN STA:IFS 277 TO ISF 293 AREA LONG 15.5 INCHES WIDE 11.5 INCHES. IN RT IB WING FLAP. THE AFT FLAP WAS REPLACE
- [SDR ANCF200600043](https://openairdocs.org/sdr/ANCF200600043.md): Engine · overtemp · Jan 21, 2007 · N986AN · Boeing 767259 · Engine (Turbine/Turboprop)
  > EICAS MESSAGE (LE SLAT ASSYM) DISPLAYED. LEADING EDGE LIGHT ILLUM WITH FLAP LEVER IN 1 POS. BOTH FLAP POINTERS WERE CORRECT. RT ENGINE WAS SHUTDOWN DUE A HIGH EGT EXCEEDED. DIGITAL FLIGHT DATA RECORDER WAS REMOVED FOR READING IN SHOP. THE FLAP/SLAT SYSTEM
- [SDR ANCF200400028](https://openairdocs.org/sdr/ANCF200400028.md): Fairing · damaged · Aug 24, 2004 · N985AN · Boeing 767259 · Trailing Edge Flaps
  > DURING WALK AROUND FOUND DAMAGE TO THE RT EXTERIOR FAIRING FLAP. FAIRING WAS REMOVED IAW CDL 57-51-2 AND TRANS ITEM TO DMI 567.
- [SDR ANCF200400021](https://openairdocs.org/sdr/ANCF200400021.md): Antenna · defective · Jul 22, 2004 · N985AN · Boeing 767259 · Weather Radar System
  > WXR FAIL DISPLAYED ON HSI WITH BOTH SYSTEMS SELECTED. WXR FAIL ANTENNA ON HSI. IT WAS REPLACED WXR ANTENNA IAW AMM34-43-03/401.
- [SDR ANCF200400005](https://openairdocs.org/sdr/ANCF200400005.md): Indicator · malfunctioned · Mar 23, 2004 · N986AN · Boeing 767259 · Fuel Quantity Indicator
  > TOTAL FUEL DIFFERS FROM CAPT AND F/0 FMC(S) CALCULATED FUEL QTY. FUEL QTY ERROR PROG 2/2 ALERT MSG DISPLAYED ON CDU AND EICAS MSG FMC MESSAGE DISPLAYED FUEL FLOW WAS NORMAL TOTAL FUEL 94.100 LBS FMC CALCULATED 101.300 LBS. TRANSFER TO DMI 436 MEL 28-41-1-2 CA
- [SDR ANCF200300030](https://openairdocs.org/sdr/ANCF200300030.md): Pressure Switch · active · Dec 19, 2003 · N985AN · Boeing 767259 · Engine Fuel Pump
  > EICAS MSG R ENG FUEL FILTER DISPLAYED. C/A: WAS REPLACED FUEL FILTER ELEMENT IN RT ENGINE IAW A-M-M 73-11-02. FUEL PUMP FILTER DIFFERENTIAL PRESSURE SWITCH WAS REMOVED AND REPLACED IAW AMM 73-34-01 PAGE 401. P/N ON AND OFF 42D395//42D362, S/N ON 0111, S
- [SDR ANCF200300020](https://openairdocs.org/sdr/ANCF200300020.md): Access Door · out of rig · Jul 23, 2003 · N985AN · Boeing 767259 · Electrical/Electronic Compartment Doors
  > DURING TAKE OFF ACCESS DOOR LIGHT ILLUMINATED AND EICAS MSG E/E ACCESS DOOR DISPLAYED; TAKE OFF WAS REJECTED AND WHEN LEAVING THE RUNWAY THE MESSAGE WAS NO LONGER DISPLAYED. C/A: MAINTENANCE PEOPLE CHECKED THE DOOR IAW SECURITY AND CONDITION AND WAS FOUND IN
- [SDR ANCF200300013](https://openairdocs.org/sdr/ANCF200300013.md): Warning Light · illuminated · Mar 23, 2003 · N985AN · Boeing 767259 · Door Warning System
  > DURING T/O ROLL AT 80 KNOTS ACCESS DOORS LIGHT ILLUM STEADY. EICAS MSG E/E ACCESS DOOR DISPLAYED STEADY. T/O WAS REJECTED (90 KNOTS)CORRECTIVE ACTION: E/E ACCESS DOOR INDICATION WAS TRANSFERED TO DMI NO 406 MEL 52-71-1-8 CAT C AND MAINTENANCE PROCEDURE WAS ACC
- [SDR ANCF200300008](https://openairdocs.org/sdr/ANCF200300008.md): Pump · failed · Feb 24, 2003 · N985AN · Boeing 767259 · Engine Fuel Pump
  > EICAS MSG RT ENGINE FUEL FILTER DISPLAYED. WIRING CHECK IN CONNECTOR D10996, D4232P, D6238P AND SIGNAL IN BOTH EICAS COMPUTERS WAS PERFORMED IAW WDM 73-34-11 PAG 1 WITH NORMAL RESULTS. IT WAS REPLACED RT FUEL PUMP IAW AMM 73-11-01/401 WITH SATISFACTORY RESULT
- [SDR ANCF200300007](https://openairdocs.org/sdr/ANCF200300007.md): Filter · dirty · Feb 15, 2003 · N985AN · Boeing 767259 · Engine Fuel/Oil Cooler
  > EICAS(STATUS)MSG L ENG.FUEL FILTER DISPLAYED.ACTION. WAS REPLACED FUEL FILTER ELEMENT ENG.LH IN ACCORDING AMM 73-11-02/401.IT WAS CLEANED FUEL DISTRIBUTION VALVE STRAINER FILTER IAW AMM 73-11-04 PAG 401. TEST IAW AMM 71-00-00 PAG.501
- [SDR ANCF200300001](https://openairdocs.org/sdr/ANCF200300001.md): Engine · stalled · Jan 12, 2003 · N985AN · Boeing 767259 · Engine (Turbine/Turboprop)
  > LT ENGINE STALLED DURING DESCENT OUT AT 390 TO 380. ALL LT ENGINE PARAMETERS FLUCTUATED DURING STALL. CARRY OUT T/S IAW FIM 71-05-00. PAGE 105, WITHOUT FINDING DAMAGES OR FAULTS. CARRY OUT WATER TRAP IAW MM 73-21-04. PAGE 601 WITHOUT EVIDENCE OF WATER. TESTS
- [SDR ANCF200200023](https://openairdocs.org/sdr/ANCF200200023.md): Warning System · false activation · Nov 5, 2002 · N985AN · Boeing 767259 · Door Warning System
  > E/E ACCESS DOOR EICAS MESSAGE DISPLAYED DURING TAKE OFF AT MAD, TAKE OFF WAS REJECTED AND RETURNED BACK TO APRON. CHECKED FOR MATERIAL OR BLOCKAGES FROM ALL OF THE ELECTRONIC ACCESS DOOR LATCH PINS AND LATCH FITTINGS, PERFORMED FIM 52-71-00/101 FIG 106 BLOCK
- [SDR ANCF200200024](https://openairdocs.org/sdr/ANCF200200024.md): Seal · damaged · Oct 14, 2002 · N986AN · Boeing 767259 · Window/Windshield System
  > DURING CRUISE WITH A DIFFERENTIAL PRESSURE OVER 4.5, THERE IS A LOUDLY NOISE COMING OUT OF 2L WINDOW. MASKING CREW AND ATC COMMUNICATIONS IMPOSSIBLE, CREW DECIDED TO RETURN TO EDR.CORRECTIVE ACTION:WAS FOUND 2L WINDOW SEAL DAMAGED, CAUSING A PRESSURIZATION LEA
- [SDR ANCF200200019](https://openairdocs.org/sdr/ANCF200200019.md): Seal · damaged · Oct 14, 2002 · N986AN · Boeing 767259 · Flight Compartment Windows
  > DURING CRUISE WITH A DIFFERENTIAL PRESSURE OVER 4.5, THERE IS A LOUDLY NOISE COMING OUT OF 2L WINDOW. MASKING CREW AND ATC COMMUNICATIONS IMPOSSIBLE, CREW DECIDED TO RETURN TO EDR. FOUND 2L WINDOW SEAL DAMAGED, CAUSING A PRESSURIZATION LEAK, REMOVED AND REPL
- [SDR ANCF200200009](https://openairdocs.org/sdr/ANCF200200009.md): Wire · chafed · Apr 26, 2002 · N986AN · Boeing 767259 · Electrical Power System Wiring
  > DURING FLIGHT EICAS MESSAGE RT GEN DRIVE DISPLAYED, GENERATOR DRIVE LIGHT ILLUMINATED. GENERATOR DRIVE DISCONNECTED. RECONNECTED RT GENERATOR AND PERFORMED OIL SERVICE, ADDITIONALLY PERFORMED BITE TO BPCU, RT OIL PRESSURE SWITCH WAS SHOWN, CHECKED WIRING A
- [SDR ANCF200100010](https://openairdocs.org/sdr/ANCF200100010.md): Valve · failed · Jun 9, 2001 · N986AN · Boeing 767259 · Fuel Transfer Valve
  > DURING CRUISE 1:30 HOURS AFTER T/O FUEL CROSSFEED VALVE LIGHT REMAINED ILLUMINATED WHEN VALVE SELECTED OPEN. EICAS MESSAGE FUEL CROSSFEED DISPLAYED. AIRCRAFT RETURNED TO MAD. PERFORMED PROCEDURE IAW FIM 28-22-00/101 FIG 108 BLOCKS 1, 2 AND 14. REPLACED FUE
- [SDR ANCF200100002](https://openairdocs.org/sdr/ANCF200100002.md): Indicator · failed · Jan 7, 2001 · N985AN · Boeing 767259 · Airspeed/Mach Indicator
  > DURING TAKE OFF CAPTAIN AIRSPEED INDICATOR GOT STUCK AT 100 KNTS. TAKE OFF WAS ABORTED AT 116 KNTS. DEFERRED AIRSPEED INDICATOR INOPERATIVE PER MEL 34-13-1 ITEM 199 CAT C, ALSO CHECKED EFIS AIRSPEED INDICATOR ON CAPTAIN SIDE, IT WORKS NORMALLY.
- [SDR ANCF200100004](https://openairdocs.org/sdr/ANCF200100004.md): Connector · dirty · Jan 7, 2001 · N986AN · Boeing 767259 · Trailing Flap Position Indicating System
  > AFTER T/O BOTH FLAP POINTERS WERE ON 1° WITH THE FLAP LEVER IN UP POSITION, AIRCRAFT RETURNED TO MEX. CLEANED CONNECTORS AT FSEU PERFORMED BITE TEST AND OPERATIONAL TEST IAW AMM 27-58-05 TEST OK, COULD NOT DUPLICATED FAULT, FLAP/SLAT VISUAL CHECK OK.
- [SDR ANCF200000003](https://openairdocs.org/sdr/ANCF200000003.md): Warning Light · illuminated · Nov 21, 2000 · N985AN · Boeing 767259 · Engine Thrust Reverser
  > DURING TAKE OFF RT REVERSER ISOLATION VALVE MESSAGE. DISPLAYED AND REVERSER ISOLATION LITE ILLUMINATED, AND, T/O WAS ABORTED. ACCORDING FIM78-34-00 RT REVERSER SYSTEM WAS CHECKED AND FOUND SYSTEM FAILURE. WAS TRANSFER TO DMI 189 AS PER MEL 78-31-1 CAT C.
- [SDR 0302277](https://openairdocs.org/sdr/0302277.md): Alternator · leaking · Aug 31, 2000 · N985AN · Boeing 767259 · Engine Oil Quantity
  > DURING FLIGHT RH ENGINE OIL DROPPED TO ZERO (0), OIL PRESS. WAS NORMAL, ONE HOUR DEFORE LANDING AT BOG OIL PRESS. WAS INTERMITTENT BETWEEN 120-104 PSI, LATER ON, THE PRESS. DROPPED TO 104-92 PSI THEM IT WENT TO 78 PSI WHEN ENGINE WAS IN IDLE POWER, FOR PRECAUT
- [SDR 20000609SH020](https://openairdocs.org/sdr/20000609SH020.md): Actuator · malfunctioned · May 17, 2000 · N985AN · Boeing 767259 · Engine Thrust Reverser
  > SAO/BOG - FLT 086 - REJECTED TAKEOFF. DURING TAKEOFF, RIGHT REVERSER INTERLOCK MSG CAME ON. REJECTED TAKEOFF WAS ACCOMPLISHED. RIGHT ENGINE THRUST REVERSER WAS DEACTIVATED IAW AMM 78-31-01, ACCOMPLISHED MEL INDICATIONS, TRANSFERRED TO DMI LOG BOOK ITEM NR 1
- [SDR 99ZZZX2776](https://openairdocs.org/sdr/99ZZZX2776.md): Engine · malfunctioned · Jun 14, 1999 · N985AN · Boeing 767259 · Engine (Turbine/Turboprop)
  > GOB/LON - FLT 016 - AIR TURN-BACK. DURING LIFT-OFF, LEFT ENGINE STARTED TO STALL. EGT WENT TO 802. LEFT ENGINE WAS REDUCED AND STALL CONDITION DISAPPEARED. AIRCRAFT RETURNED AND MADE AN OVERWEIGHT LANDING WITH LEFT ENGINE IN IDLE. SUBMITTER STATED ENGINE
- [SDR 99ZZZX611](https://openairdocs.org/sdr/99ZZZX611.md): Idg · malfunctioned · Jul 13, 1998 · N986AN · Boeing 767259 · Engine (Turbine/Turboprop)
  > BOG/APR - FLT 014 - AIR TURN BACK. EICAS MSG LT GENERATOR DRIVE AND IDG TEMP SENSOR AND DRIVE WARNING LIGHT FLICKERS. IDG WAS DISCONNECTED. LT IDG WAS REPLACED. TEST ACCORDING MM 24-20-00 WITH ENGINE RUN-UP OK.
- [SDR ANCF9600003](https://openairdocs.org/sdr/ANCF9600003.md): Warning Light · illuminated · Nov 14, 1996 · N985AN · Boeing 767259 · Door Warning System
  > MAC/BOG - FLT 011 - EMERGENCY DOOR LIGHT ILLUMINATED STEADY EICAS MSG L EMER DOOR DISPLAYED STEADY. TAKEOFF WAS REJECTED AT 129 KNOTS. PERFORMED PROCEDURE FOR F1M 52-71-00 FIG 105 THE OVERWING EMERG EXIT LT SIDE BITE CHECKED TO PROXIMITY SWITCH AND NO FAULT
- [SDR ANCF173C](https://openairdocs.org/sdr/ANCF173C.md): Warning Light · illuminated · Nov 14, 1996 · N985AN · Boeing 767259 · Door Warning System
  > MAC/BOG - FLT 011 - EMERGENCY DOOR LIGHT ILLUMINATED STEADY EICAS MSG L EMER DOOR DISPLAYED STEADY. TAKEOFF WAS REJECTED AT 129 KNOTS. PERFORMED PROCEDURE FOR F1M 52-71-00 FIG 105 THE OVERWING EMERG EXIT LT SIDE BITE CHECKED TO PROXIMITY SWITCH AND NO FAULT
- [SDR 96ZZZX3123](https://openairdocs.org/sdr/96ZZZX3123.md): Idg · failed · Jan 27, 1996 · N986AN · Boeing 767259 · AC Generator-Alternator
  > CTG/MAD - FLT 010 - EICAS MSG 01=L GEN DRIVE DISPLAYED. GEN DRIVE LIGHT ILLUMINATED, GEN DRIVE DISCONNECTED. CHANGED IDG. CYCLES, 4,257. HOURS, 22,648.
- [SDR 96ZZZX2230](https://openairdocs.org/sdr/96ZZZX2230.md): Blade · failed · Jan 4, 1996 · N985AN · Boeing 767259 · Turbine Engine Compressor Section
  > ON TOP OF DESCENT FINISHING FLIGHT 019 FROM FRA TO BOG, ENGINE NR 2 (RIGHT) FLAMED OUT. RESTART WAS NOT SUCCESSFUL. PRELIMINARY INSPECTION SHOWED SOME ROTOR BLADES OF LOW PRESSURE COMPRESSION WERE DESTROYED.
- [SDR 96ZZZX3122](https://openairdocs.org/sdr/96ZZZX3122.md): Outflow Valve · malfunctioned · Jan 10, 1995 · N985AN · Boeing 767259 · Pressure Regulator/Outflow Valve
  > PAR/BOG - FLT 015 - AUTO INOP LIGHT ILLUMINATED. EICAS MESSAGE, CABIN AUTO INOP AND CABIN ALT AUTO 1 AND DISPLAYED. OPERATION IN MANUAL MODE WAS OK. CABIN ALTITUDE WARNING AND MESSAGE CAME ON. OXYGEN MASKS WERE DROPPED BY PILOTS. PERFORMED BITE PROCEDURE

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE aircraft_model_key = '767259'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-767-259/reports

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