# Service difficulty reports: Boeing 767-3G5

A list on [Boeing 767-3G5](https://openairdocs.org/model/boeing-767-3g5.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 15 · 724 reports

- [SDR HALA2013091000105](https://openairdocs.org/sdr/HALA2013091000105.md): Drive Assy · failed · Sep 10, 2013 · N586HA · Boeing 7673G5 · Weather Radar System
  > BOTH WEATHER RADARS INOPERATIVE. REPLACED WX RADAR ANTENNA DRIVE. OPS CHECK OK BOTH WX RADAR SYSTEMS IAW M/M34-43--05.
- [SDR HALA2013072400093](https://openairdocs.org/sdr/HALA2013072400093.md): Tru · faulted · Jul 24, 2013 · N586HA · Boeing 7673G5 · Airborne Auxiliary Power Unit (APU) System
  > VERIFICATION FLIGHT FOR APU COMPLETED UNSATISFACTORY, FAILED. EICAS APU FAULT. TROUBLESHOT IAW FIM 49-11-00-101, R & R TRU IAW 24-32-04-404-003 APU STARTED NORMAL OK FOR SERVICE.
- [SDR HALA2013062200083](https://openairdocs.org/sdr/HALA2013062200083.md): Coupling · failed · Jun 22, 2013 · N586HA · Boeing 7673G5 · Communications System Wiring
  > BOTH HF RADIOS NOT CHANNELIZING. R & R LT AND RT HF ANTENNA COUPLERS IAW AMM TASK 23-11-01-024-001/23-11-01-424-008, R & R LT HF TRANSCEIVER IAW AMM TASK 23-11-03-424-005, PERFORMED OPS CHECK TEST OF LT AND RT HF TRANSCEIVER, TEST NORMAL, IAW TASK 23-11-00-71
- [SDR HALA201306240135](https://openairdocs.org/sdr/HALA201306240135.md): Coupler · failed · Jun 22, 2013 · N586HA · Boeing 7673G5 · HF Communications System
  > BOTH HF RADIOS NOT CHANNELIZING. R & R LT AND RT HF ANTENNA COUPLERS IAW AMM TASK 23-11-01-024-001/23-11-01-424-008, R & R LT HF TRANSCEIVER IAW AMM TASK 23-11-03-424-005, PERFORMED OPS CHECK TEST OF LT AND RT HF TRANSCEIVER, TEST NORMAL, IAW TASK, 23-11-00-71
- [SDR HALA2013060500075](https://openairdocs.org/sdr/HALA2013060500075.md): Circuit Card · malfunctioned · Jun 5, 2013 · N585HA · Boeing 7673G5 · Fire Detection
  > EICAS MESSAGE, FOUND RT ENG FIRE LOOP 1. REPLACED CIRCUIT CARD M683, RT WING FIRE LOOP 1, FIRE DETECT CONTROL CARD IAW AMM 26-10-01. OPS CHECKED GOOD. OK FOR SERVICE.
- [SDR HALA2013042900049](https://openairdocs.org/sdr/HALA2013042900049.md): Starter · faulted · Apr 29, 2013 · N586HA · Boeing 7673G5 · APU Start/Ignition System
  > APU FAULT DISPLAYED WHEN APU START ATTEMPTED ON FINAL APPROACH. BITE CHECKED ECU BOX. FAULTED APU STARTER. REPLACED APU STARTER IAW AMM 49-41-01. SECURITY AND COND OK. OK FOR SVC.
- [SDR HALA2013040200033](https://openairdocs.org/sdr/HALA2013040200033.md): Interrogator · malfunctioned · Apr 2, 2013 · N585HA · Boeing 7673G5 · Door Warning System
  > LT WING SLIDE ILLUMINATED DURING TAKE OFF ROLL, 100 KNOTS. R & R OVERWING ESCAPE SLIDE INTERROGATOR IAW AMM 25-65-12, OPS CHECKED GOOD.
- [SDR HALA2013040100032](https://openairdocs.org/sdr/HALA2013040100032.md): Interrogator · failed · Apr 1, 2013 · N585HA · Boeing 7673G5 · Door Warning System
  > LEFT WING EXIT SLIDE ILLUMINATED DURING TAKE OFF ROLL. R & R WING ESCAPE SLIDE INTEROGATOR IAW AMM 25-65-12, OPS CHECK GOOD.
- [SDR HALA2013021300020](https://openairdocs.org/sdr/HALA2013021300020.md): Engine · malfunctioned · Feb 13, 2013 · N585HA · Boeing 7673G5 · Engine (Turbine/Turboprop)
  > RT ENGINE EPR, N1, N2, F/F ALL FLUCTUATE. CLIMB EPR 1.5 PERCENT, N1.5 PERCENT, N2.2 PERCENT, F/F 200LBS LESS IN CRUISE.
- [SDR HALA2013021300019](https://openairdocs.org/sdr/HALA2013021300019.md): Slide · detached · Feb 13, 2013 · N585HA · Boeing 7673G5 · Escape Slide
  > DOOR SLIDE FOUND R4 DETACHED FROM DOOR AFTER CATERERS ATTEMPTED ENTRY (BLOCKED SEATS ROWS 36-45). (MAIN ENTRY DOOR SLIDES PASSSENGER CONFIG). INSTALLED R4 SLIDE IAW TASK CARD 25-035-51-AFTER. SECURITY CHECK OK.
- [SDR HALA2013021200018](https://openairdocs.org/sdr/HALA2013021200018.md): Connector · broken · Feb 12, 2013 · N584HA · Boeing 7673G5 · Light System Wiring
  > AT DEPARTURE TIME CREW REPORTS MID GALLEY EMERGENCY LIGHTING FLOOR STRIP LT SIDE CONNECTOR BROKE LOOSE. RESECURED MID GALLEY EMERGENCY LIGHT FLOOR STRIP WIRES. OPS CK OK IAW AMM 33-51-00.
- [SDR HALA2013013100014](https://openairdocs.org/sdr/HALA2013013100014.md): Connector · dirty · Jan 31, 2013 · N586HA · Boeing 7673G5 · APU System Wiring
  > AIR TURNBACK, APU AUTO SHUTDOWN, APU VERIFICATION UNSATISFACTORY. ECU BIT INDICATES "HIGH TEMP" WITH MINI FLAGS 11, 45 & 48. PERFORMED MEGGER TEST FOUND NR 2 THERMOCOUPLE CIRCUIT FAULTY WITH HIGH RESISTANCE. ISOLATED FAULT ON CONNECTOR D4082J, PIN 29 AND 30
- [SDR HALA2013011300011](https://openairdocs.org/sdr/HALA2013011300011.md): Starter · failed · Jan 13, 2013 · N585HA · Boeing 7673G5 · Engine Starter
  > AFTER PUSH BACK, AFTER CONTROL SWITCH TO RUN N2 DECREASED TO 23 PERCENT, ESS, & CAS RAMP CONTROL REPORTED FIRE/SPARKS COMING FROM LT ENGINE. FUEL CONTROL SWITCH MOVED TO CUTOFF, ATTEMPED TO MOTOR ENGINE. LEFT ENGINE START SWITCH TO OFF. WILL NOT MOTOR. R
- [SDR HALA2013011100009](https://openairdocs.org/sdr/HALA2013011100009.md): Battery · inoperative · Jan 11, 2013 · N585HA · Boeing 7673G5 · APU Start/Ignition System
  > APU UNABLE TO START COMPLETELY. R & R APU BATTERY IAW AMM 24-31-04. OPERATION CHECK GOOD. OK FOR SERVICE.
- [SDR HALA2013010200001](https://openairdocs.org/sdr/HALA2013010200001.md): Warning Message · illuminated · Jan 2, 2013 · N585HA · Boeing 7673G5 · Pneumatic Distribution System
  > AFTER RT ENGINE START HPSOV ILLUMINATED ON EICAS AND STATUS PAGE. RESET THE EICAS IAW FIM 31-41, FAULT TREE 812. CHECKED AIR BITE AMM 36-11-00-715-149. RAN ENG. OPS CHECKED GOOD.
- [SDR HALA2012123100237](https://openairdocs.org/sdr/HALA2012123100237.md): Warning Light · false activation · Dec 31, 2012 · N585HA · Boeing 7673G5 · Pneumatic Distribution System
  > RT ENGINE HPSOV ON EICAS AFTER ENGINE START. RESET EICAS IAW FIM 31-41- FAULT 2 TREE 812, CHECKED AIR BITE SYS, NO PR'S NOTED. RAN ENG. OPS CHECKED GOOD IAW AMM 36-11-00-715-419.
- [SDR HALA2012120300230](https://openairdocs.org/sdr/HALA2012120300230.md): Eec · malfunctioned · Dec 3, 2012 · N586HA · Boeing 7673G5 · Fuel Controlling System
  > LEFT ENGINE EEC C1 LT ENG CONTROL. R & R NR 1 ENGINE EEC IAW AMM 73-21-04. RUN/OPS CHECK PENDING AND (STEPS G) 5-8 PENDING. ACCOMPLISHED STEPS 5-8 & RUN. CONDITION SAME. REPLACED NR 1 ENG P2T2 PROBE IAW AMM 73-21-03. ACCOMPLISHED ENG RUN - COND. SAME.
- [SDR HALA2012102900224](https://openairdocs.org/sdr/HALA2012102900224.md): Connector · shorted · Oct 29, 2012 · N586HA · Boeing 7673G5 · Water/Waste System Wiring
  > F/A REPORTED STRONG ELECTRICAL ODOR NEAR 4R DOOR. COLLARED CIRCUIT B H006 AND DISCONNECTED CONNECTOR PLUG FROM WATER AIR COMPRESSOR. (POTABLE WATER SYS).
- [SDR HALA2012101900221](https://openairdocs.org/sdr/HALA2012101900221.md): Processor · faulty · Oct 19, 2012 · N586HA · Boeing 7673G5 · Fuel Quantity Indicator
  > B1 FAULT FOUND ON FQIS PROCESSOR.. BITE IAW FIM 28-41 TASK 852. B1 FAULT-FIM 28-41 TASK 856. IAW FIM REPLACED FQIS PROCESSOR IAW AMM 28-41-08. OPS CHECK GOOD.
- [SDR HALA2012091700211](https://openairdocs.org/sdr/HALA2012091700211.md): Line · leaking · Sep 17, 2012 · N585HA · Boeing 7673G5 · Hydraulic System, Main
  > RIGHT HYD QTY (EICAS), PERFORMED QRH RT WAS.48 RF WHEN HYD QTY EICAS CAME ON. CENTER HYD QUANITY.55 RF AT SHUTDOWN INFLT.93 TO.78 TO.74 RF. NEW HYD FLEX-LINE INSTALLED, HYD FLUID SERVICED AS REQUIRED. R & C HYD SYS, OPS CHECKS NORMAL. CLEANED RT WHEEL
- [SDR HALA2012091700208](https://openairdocs.org/sdr/HALA2012091700208.md): Warning Light · false activation · Sep 17, 2012 · N584HA · Boeing 7673G5 · Fire Detection
  > NR 1 ENGINE AND APU FIRE LOOP SHOWED EICAS MESSAGE NO TEST. PERFORMED ENG AND APU FIRE LOOP TEST IAW FIM 26-15 FIG 803 & 804. OPS CHECKED GOOD, NO FAULTS NOTED.
- [SDR HALA2012090900204](https://openairdocs.org/sdr/HALA2012090900204.md): Warning Light · false activation · Sep 9, 2012 · N586HA · Boeing 7673G5 · Aileron Control System
  > DURING CLIMB OUT AND DESCENT EICAS MESSAGE "AILERON LOCKOUT. "ACCOMPLISHED FIM 27-11 FAULT TREE. NO DEFECTS NOTED. OK FOR SERVICE.
- [SDR HALA2012090700203](https://openairdocs.org/sdr/HALA2012090700203.md): Warning Message · illuminated · Sep 7, 2012 · N586HA · Boeing 7673G5 · Aileron Control System
  > DURING CLIMB AT APPROX 290 KTS RECEIVED AN AILERON LOCKOUT EICAS AND AILERON LOCK LIGHT. AFTER 10 MINS MESSAGE CLEARED. OPS NORMAL. PERFORMED FIM PROCEDURE 27-11 FAULT TREE 804 -NO FAULTS FOUND. ACFT OK FOR CONTINUED SERVICE.
- [SDR HALA2012090400201](https://openairdocs.org/sdr/HALA2012090400201.md): Warning Message · false activation · Sep 4, 2012 · N585HA · Boeing 7673G5 · Engine (Turbine/Turboprop)
  > EICAS MESSAGE, LT ENG CONTROL DISPLAYED ALONG WITH STATUS MESSAGE, LT ENG CONTROL AND LT ENG EEC C1. RAN LT ENG BITE CK LT PIMU. FOUND FAULTS EEC CHANNEL B SVA TR -CHECK FAIL PERFORMED FIM 71-01 TASK 827. SUSPECT ENG SHUTOFF VALVE ON FMU, BITE NR 1 PIMU NO
- [SDR HALA2012090400199](https://openairdocs.org/sdr/HALA2012090400199.md): Fmu · malfunctioned · Sep 4, 2012 · N585HA · Boeing 7673G5 · Fuel Controlling System
  > DURING ENGINE START ENG VALVE ADVISORY LIGHT REMAINED ON DURING START. AFTER ENGINE STARTED OK. AT IDLE LIGHT AND LT ENG VALVE EICAS LIGHT WENT OUT. R & R LEFT ENGINE FMU. OPS & LEAK CHECKED OK IAW AMM 73-21-01. OK FOR SERVICE.
- [SDR HALA2012082000195](https://openairdocs.org/sdr/HALA2012082000195.md): Coupler · faulted · Aug 20, 2012 · N586HA · Boeing 7673G5 · HF Communications System
  > TRANSMISSION AND RECEPTION ON RT-HF INOPERATIVE. (IT WOULD NOT CHANELIZE). FOUND RT TRANCEIVER FAULTING HF COUPLER. R & R NR 2 HF COUPLER IAW MM 23-11-01. GROUND CHECK OK.
- [SDR HALA2012082000194](https://openairdocs.org/sdr/HALA2012082000194.md): Radio · malfunctioned · Aug 20, 2012 · N586HA · Boeing 7673G5 · HF Communications System
  > TRANSMISSION AND RECEPTION ON LT-HF INOPERATIVE (IT WOULD NOT CHANELIZE. RERACKED NR 1 HF TRANSCEIVER IAW MM 23-11-03. GROUND CHECK OK.
- [SDR HALA2012081800192](https://openairdocs.org/sdr/HALA2012081800192.md): Apu · auto shutdown · Aug 18, 2012 · N585HA · Boeing 7673G5 · APU Core Engine
  > APU AUTO SHUTDOWN IN FLIGHT. EICAS MESSAGE, APU FAULT. R & R APU IAW M266-767. LEAK AND OPS CHECKED OK.
- [SDR HALA2012073100188](https://openairdocs.org/sdr/HALA2012073100188.md): Pump · leaking · Jul 31, 2012 · N586HA · Boeing 7673G5 · Hydraulic Pump (Electric/Engine), Main
  > FOUND NR 1 ENG HYD PUMP LEAKING. R & R NR 1 HYD EDP IAW AMM 29-11-05, LEAK & OPS CHECKED OK.
- [SDR HALA2012071900177](https://openairdocs.org/sdr/HALA2012071900177.md): Compensator · faulty · Jul 19, 2012 · N586HA · Boeing 7673G5 · Fuel Quantity Indicator
  > RT FUEL QUANITY INDICATOR AND BOTH TOTALIZERS WENT BLANK. 40 MIN LATER RT QUANTITY GAUGE WENT FROM 31.7 DOWN TO 29.2 OSCILATING THERE FOR ABOUT 10 MINS. PERFORMED FUEL QUANITY INDICATION SYS BITE, FOUND C6 FAULT,(AMM 28-41-00). RT WING MAIN TANK COMPENSATOR
- [SDR HALA2012071800176](https://openairdocs.org/sdr/HALA2012071800176.md): Relief Valve · leaking · Jul 18, 2012 · N584HA · Boeing 7673G5 · Fuel Controlling System
  > RIGHT FUEL TANK QUANTITY DECREASED 1500 LBS DURING CLIMB WHILE BOTH CENTER TANK PUMPS ARE ON AND OPERATING. FOUND PRESSURE RELIEF VALVE LEAKING. REPLACED PRESSURE RELIEF VALVE IAW AMM 28-21-08. OK TO CLOSE RT MAIN TANK ACCESS DOOR 541HB. LEAK CHECK OF PANEL
- [SDR HALA2012071000170](https://openairdocs.org/sdr/HALA2012071000170.md): Bypass Valve · leaking · Jul 10, 2012 · N584HA · Boeing 7673G5 · APU Oil System
  > APU AUTO SHUTDOWN AT GATE. BITE APU IAW FIM HIGH OIL TEMP FAULT IAW FIM 49-11-00, FIG 110. NO OTHER FAULTS FOUND. IAW FIM REPLACED OIL COOLER BYPASS VALVE IAW AMM 49-27-10. LEAK CHECKED FAILED. REPLACED OIL COOLER BYPASS VALVE WITH ANOTHER NEW VALVE LEAK
- [SDR HALA2012070200165](https://openairdocs.org/sdr/HALA2012070200165.md): Coupling · sheared · Jul 2, 2012 · N584HA · Boeing 7673G5 · Engine Starter
  > RT ENGINE STARTER TO GEARBOX COUPLING SHEARED. R & R STARTER DRIVE COUPLING IAW AMM 72-61-09.
- [SDR HALA2012062900163](https://openairdocs.org/sdr/HALA2012062900163.md): Module · malfunctioned · Jun 29, 2012 · N585HA · Boeing 7673G5 · Fire Detection
  > FIRE BELL WARNING AT 95 KTS ON TAKEOFF. ABORT EXERCISED. COULD NOT CANCEL/MUTE BELL CHIME AND NO VISUAL INDICATION NOTED. INSPECTED WIRING AT CONNECTOR D4349P & P51 PANEL DISCONNECTS, NO BENT OR PUSH BACK PINS. R & R M1000 BELL CHIME MODULE IAW AMM 31-51-
- [SDR HALA2012060500159](https://openairdocs.org/sdr/HALA2012060500159.md): Warning Light · false activation · Jun 5, 2012 · N584HA · Boeing 7673G5 · Pneumatic System
  > RT ENG BLEED OFF EICAS AND LIGHT APPEARED TWICE DURING FLIGHT. FIRST DURING CLIMB FOR 30 SECONDS, SECOND DURING CRUISE DESCENT FOR 10-15 SECONDS. RAN NR NR 2 ENGINE IAW AMM 71-00-00. NO FAULTS OR ABNORMALITIES NOTED. OPS CHECKED GOOD. NO FAULTS NOTED ON AI
- [SDR HALA2012053100153](https://openairdocs.org/sdr/HALA2012053100153.md): Fmc · malfunctioned · May 31, 2012 · N586HA · Boeing 7673G5 · Flight Management Computing Hardware System
  > AFTER LANDING LT FMC INOPERATIVE. TROUBLESHOT IAW FIM 34-61-00/101 FIG 111. MESSAGE CLEARED, NO FAULTS AT THIS TIME.
- [SDR HALA2012050900134](https://openairdocs.org/sdr/HALA2012050900134.md): Blade · damaged · May 9, 2012 · N586HA · Boeing 7673G5 · Turbine Engine Compressor Section
  > ON WALKAROUND FOUND RT ENGINE NR 6 FAN BLADE HAS FOD DAMAGE, APPROXIMATELY TWELVE INCHES FROM BLADE ROOT (AREA F). BLENDED DAMAGED AREA WITHIN LIMITS IAW AMM 72-31-02, NO CRACKS NOTED ON EDDY CURRENT. OK FOR SERVICE.
- [SDR HALA2012042900127](https://openairdocs.org/sdr/HALA2012042900127.md): Sensor · open · Apr 29, 2012 · N584HA · Boeing 7673G5 · Windshield/Door Rain/Ice Removal
  > CLIMBING THROUGH 9,000' RECEIVED "RT FWD WINDOW" LIGHT AND INOPERATIVE LIGHT ON, FOLLOWED QRH. LIGHT STAYED ON, RETURNED TO DEPARTURE. ACCOMPLISHED FIM 30-41-00/101, FIG 104, FOUND 1R WINDOW MAIN SENSOR OPEN CIRCUIT. SWAPPED TO SPARE WINDOW SENSOR IAW AMM 3
- [SDR HALA2012042900126](https://openairdocs.org/sdr/HALA2012042900126.md): Control Unit · malfunctioned · Apr 29, 2012 · N584HA · Boeing 7673G5 · Windshield/Door Rain/Ice Removal
  > CLIMBING THROUGH APPROX 25,000' RECEIVED RT FWD WINDOW EICAS MESSAGE AND INOPERATIVE LIGHT ON THE RT FWD WINDOW LIGHT SWITCH. FOLLOWED QRH. LIGHT STAYED ON. RETURNED TO DEPARTURE. ACCOMPLISHED FIM 30-41-00, FIG 104. NO FAULTS NOTED. 1R WINDOW HEATER AND
- [SDR HALA2012021800126](https://openairdocs.org/sdr/HALA2012021800126.md): Control Unit · malfunctioned · Apr 29, 2012 · N584HA · Boeing 7673G5 · Windshield/Door Rain/Ice Removal
  > CLIMBING THROUGH APPROX 25,000', RECEIVED RT FWD WINDOW EICAS MESSAGE AND INOPERATIVE LIGHT ON THE RT FWD WINDOW LIGHT SWITCH. FOLLOWED QRH. LIGHT STAYED ON. ACCOMPLISHED FIM 30-41-00, FIG 104. NO FAULTS NOTED. 1R WINDOW HEATER AND SENSOR RESISTANCE CHECK
- [SDR HALA2012041400125](https://openairdocs.org/sdr/HALA2012041400125.md): Gearbox · binding · Apr 14, 2012 · N585HA · Boeing 7673G5 · Leading Edge Slat Control System
  > NR 3 SLAT E/B GEARBOX BINDING IN RETRACT POSITION. R & R NR 3 SLAT INBD GEARBOX IAW AMM 27-81-20. INSPECTED AND IS SAFE FOR THE INTENDED FLIGHT.
- [SDR HALA2012031800113](https://openairdocs.org/sdr/HALA2012031800113.md): Connector · unsecure · Mar 18, 2012 · N584HA · Boeing 7673G5 · Light System Wiring
  > ON OVERNIGHT CHECK, FOUND EMERGENCY FLOOR LIGHTING BETWEEN L1 & R1 DOOR INOPERATIVE. RECONNECTED AND RESECURED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR. OPS CHECKED IAW AMM 33-51-00.
- [SDR HALA2012030500099](https://openairdocs.org/sdr/HALA2012030500099.md): Warning Light · multiple fail · Mar 5, 2012 · N585HA · Boeing 7673G5 · Central Warning
  > IN CRUISE, NO LAND 3 INDICATED ON THE ASA INDICATOR. RA WARNING INDICATED BRIEFLY ON CAPT ADI. FLT FAULTS INDICATED CRA NO LAND 3. ON FLT LOGS 1 AND 2 PERFORMED BITE OF LT & RT RADIO ALTIMETER "FAILED 51, FOUND QC SWAPED POS WITH LT RA. NO FAULT FOUND RETURN
- [SDR HALA2012022900088](https://openairdocs.org/sdr/HALA2012022900088.md): Warning Light · false activation · Feb 29, 2012 · N586HA · Boeing 7673G5 · Central Warning
  > FLT DECK TEMP DISPLAYED AND FLT COMPT TEMP "INOPERATIVE" LIGHT ILLUMINATED IN "AUTO", MANUAL OPS NORMAL. PERFROMED BITE TEST ON ZONE TEMP & PACK CONTROLLERS, NO FAULT NOTED, FUNCTIONAL CHECKED NORMAL IAW AMM 21-51-14/501. NO ACTIVE EICAS MESSAGE.
- [SDR HALA2012022600081](https://openairdocs.org/sdr/HALA2012022600081.md): Warning Message · false activation · Feb 26, 2012 · N584HA · Boeing 7673G5 · Cabin Cooling System
  > LEFT PACK TEMPERATURE EICAS MESSAGE. LT PACK INOP ON OVERHEAD MULTIPLE TIMES AT 5 SECS EACH TIME, SELECTED STANDBY IAW QRH. BITE CHECKED LT PACK CONTROLLER, NO FAULTS. RAN PACK AND OPS CHECKED GOOD.
- [SDR HALA2012021800064](https://openairdocs.org/sdr/HALA2012021800064.md): Wire · damaged · Feb 18, 2012 · N586HA · Boeing 7673G5 · Electrical Power System Wiring
  > RIGHT IDG TEMPERATURE SENSOR DISPLAYED IDG OUT: 80-180 IDG RISE 8-180 AT TOP OF CLIMB. ACCOMPLISHED FIM 24-20-00, REPAIRED DAMAGED WIRE, JACKED ON D10966 PLUG, IAW SWAPM 20-10-13, REPLACED RT GCU IAW 24-22-02. GROUND OPS CHECKED OK.
- [SDR HALA201202180006](https://openairdocs.org/sdr/HALA201202180006.md): Warning Light · illuminated · Feb 18, 2012 · N585HA · Boeing 7673G5 · APU Oil System
  > APU DISPLAYED "APU FAULT" AND APU AUTO SHUTDOWN DURING VERIFICATION FLIGHT, VERIFICATION FAILED. BITE CHECKED ECU, FOUND "AUTO SHUTDOWN GEN FILTER" ACCOMPLISHED FIM 49-11-00, CHECKED GOOD. AS A PRECAUTION, REPLACED OIL PRESSURE AND SCAVENGE FILTER ALSO GENER
- [SDR HALA2012021800063](https://openairdocs.org/sdr/HALA2012021800063.md): Apu · faulted · Feb 18, 2012 · N585HA · Boeing 7673G5 · Airborne Auxiliary Power Unit (APU) System
  > APU DISPLAYED "APU FAULT" AND APU AUTO SHUTDOWN DURING A VERIFICATION FLIGHT. BITE CHECKED ECU, FOUND "AUTO SHUTDOWN GENERATOR FILTER" ACCOMPLISHED FIM 49-11-00 CHECKED GOOD, AS A PRECAUTION, REPLACED OIL PRESSSURE AND SCABENGE FILTER ALSO GENERATOR FILTER D
- [SDR HALA2012021200056](https://openairdocs.org/sdr/HALA2012021200056.md): Computer · malfunctioned · Feb 12, 2012 · N586HA · Boeing 7673G5 · Flight Management Computing Hardware System
  > DURING FLT, BOTH FMC`S BLANKED OUT. THEN DISPLAYED "RESET TIMEOUT". RESELECTED FMC AND DISPLAYED NORMALLY EXCEPT ON PROGRAM PAGE 2, LT & RT FUEL USED AND TOTAL FUEL USED BLANK, ALL OTHERS NORMAL. PERFORMED FMC OPS TEST, PER AMM TASK 34-61-00. FMC NOW OK FOR
- [SDR HALA2012021200055](https://openairdocs.org/sdr/HALA2012021200055.md): Warning Message · illuminated · Feb 12, 2012 · N586HA · Boeing 7673G5 · Cabin Cooling System
  > RECEIVED AN EICAS MESSAGE OF RT PACK TEMPERATURE. RT SELECTOR PLACED IN STBY-N-OPS NORMAL. PERFORMED BITE TEST IAW FIM 21-51-00, FIG 103. MESSAGE NOT ACTIVE. OK FOR SERVICE.

Next page: https://openairdocs.org/model/boeing-767-3g5/reports.md?page=2

## 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 = '7673G5'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-767-3g5/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.