# Service difficulty reports: N594HA, cancelled May 7, 2019

A list on [N594HA, cancelled May 7, 2019](https://openairdocs.org/deregistered/N594HA-2019-05-07.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 9 · 411 reports

- [SDR HALA2018120500632](https://openairdocs.org/sdr/HALA2018120500632.md): Wire Harness · damaged · Dec 4, 2018 · N594HA · Boeing 767332 · Light System Wiring
  > EMERGENCY LIGHT INOP AT SEAT 26 H/J.// REPAIRED WIRES FOR EMERGENCY LIGHTS AT SEAT 26 H/J PER SWPM 20-10-13. OPS GOOD. OK FOR SVC.
- [SDR HALA2018120500631](https://openairdocs.org/sdr/HALA2018120500631.md): Wire Harness · damaged · Dec 4, 2018 · N594HA · Boeing 767332 · Light System Wiring
  > EMERGENCY LIGHT INOP AT SEAT 37, 38, 39 A/B.// REPAIRED WIRES FOR EMERGENCY LIGHTS AT SEAT 37, 38, 39 A/B PER SWPM 20-10-13. OPS GOOD. OK FOR SVC.
- [SDR HALA2018112700617](https://openairdocs.org/sdr/HALA2018112700617.md): Charger · inoperative · Nov 26, 2018 · N594HA · Boeing 767332 · Emergency Lighting
  > DURING SERVICE CHECK FOUND EMERGENCY PATH LIGHT 25-31AB INOP. REPLACED EMERGENCY LIGHT BATTERY CHARGER AT M9009 PER AMM 33-51-07. OPS CHECK GOOD FOR SEATS 25-31AB. OK FOR SERVICE.
- [SDR HALA2018112760614](https://openairdocs.org/sdr/HALA2018112760614.md): Fmc · malfunctioned · Nov 22, 2018 · N594HA · Boeing 767332 · Flight Management Computing Hardware System
  > ETOPS SIGNIFICANT SYSTEM - FO SIDE VPI SHOWED HIGHER ON PROFILE BY ERROR OF 12,000', PROG PAGE 2 VTK ERROR MISMATCH BETWEEN CA AND FO FMC// RESET #1 & 2 FMC'S. PERFORMED OPS TEST PER AMM 34-61-00-715-001. OK FOR SERVICE.
- [SDR HALA2018112000603](https://openairdocs.org/sdr/HALA2018112000603.md): Control Unit · malfunctioned · Nov 19, 2018 · N594HA · Boeing 767332 · Brake Anti-Skid Section
  > EICAS MESSAGE, ANTI-SKID INOP EICAS MESSAGE ALT ANTI-SKID INOP, DIVERTED TO NEAREST AIRPORT FOR LONGER RUNWAY. MESSAGES OUT AFTER LANDING. REMOVED AND REPLACED ANTI-SKID / AUTO BRAKE CONTROL UNIT PER AMM 32-42-01, OPS CHECK GOOD SYSTEM RE-ACTIVATED. BITE TES
- [SDR HALA2018112000602](https://openairdocs.org/sdr/HALA2018112000602.md): Wire · exposed · Nov 19, 2018 · N594HA · Boeing 7673CB · Light System Wiring
  > EMERGENCY PATH LIGHTING WIRES NEAR 4R DOOR EXPOSED.// RE-RECURRED WIRES AND EMERGENCY LIGHT COVER. OK FOR SERVICE.
- [SDR HALA2018111900591](https://openairdocs.org/sdr/HALA2018111900591.md): Lens · missing · Nov 17, 2018 · N594HA · Boeing 7673CB · Emergency Lighting
  > MISSING EMERGENCY LIGHT COVER BY 4R DOOR ISLE. // REMOVED AND REPLACED EMERGENCY LIGHT COVER BY 4R DOOR. OPS CHK GOOD, OK TO CONTINUE.
- [SDR HALA2018102900549](https://openairdocs.org/sdr/HALA2018102900549.md): Valve · leaking · Oct 28, 2018 · N594HA · Boeing 7673CB · Brake Anti-Skid Section
  > RIGHT HYD SYSTEM LEAK. FULL ON DEPARTURE. 3 HOURS INTO FLT RF(.67) STILL DECREASE NOTE: CENTER HYD QUAN. 1.35, 1.11 ON DEPARTURE.// PERFORMED FIM TASK 29-11 FAULT TREE 830 THROUGH STEP 2 INSPECTION OF CENTER RESERVOIR PRESS SHUT OFF VALVE FOUND CLEAN. NEED TO
- [SDR HALA2018100900483](https://openairdocs.org/sdr/HALA2018100900483.md): Sleeve · torn · Oct 8, 2018 · N594HA · Boeing 767332 · Engine (Turbine/Turboprop)
  > ETOPS SIGNIFICANT SYSTEM - FOUND SEVERAL OGV SLEEVES TORN AT 4 O CLOCK POSITION ON NR 2 ENGINE. REPLACED OGV SLEEVES AT POSITIONS 33, 35, 36, 37, 38, 39, 32 PER TASK CARD E105-C60012-PERM ITEM 1.
- [SDR HALA20181009483](https://openairdocs.org/sdr/HALA20181009483.md): Sleeve · torn · Oct 8, 2018 · N594HA · Boeing 767332 · Engine (Turbine/Turboprop)
  > ETOPS SIGNIFICANT SYSTEM - FOUND SEVERAL OGV SLEEVES TORN AT 4 O CLOCK POSITION ON NR 2 ENGINE. REPLACED OGV SLEEVES AT POSITIONS 33, 35, 36, 37, 38, 39, 32 PER TASK CARD E105-C60012-PERM ITEM 1.
- [SDR HALA2018100100460](https://openairdocs.org/sdr/HALA2018100100460.md): Guide Vane · missing · Sep 30, 2018 · N594HA · Boeing 767332 · Turbine Engine Compressor Section
  > ETOPS SIGNIFICANT SYSTEM - FOUND MISSING OUTLET GUIDE VANE NR 2 ENGINE AT 4 O CLOCK POSITION. ACCOMPLISH INTERIM REPAIR, IAW M105 FILE R0333. OK FOR SERVICE.
- [SDR HALA2018092500432](https://openairdocs.org/sdr/HALA2018092500432.md): Solenoid · faulty · Sep 24, 2018 · N594HA · Boeing 767332 · Fuel Controlling System
  > ETOPS SIGNIFICANT SYSTEM - ON THE TAKEOFF ROLL, WE HAD A LARGE THROTTLE SPLIT ABOUT 2". SOON AFTER LIFT OFF RIGHT ENGINE REACHED 940C FOR TWO SECONDS AS WE REDUCED THRUST. NR 2 ENG EGT WITHIN LIMIT PER AMM 71-00-00. REMOVED AND REPLACED FLIGHT/ GROUND IDLE SOL
- [SDR HALA2018090800418](https://openairdocs.org/sdr/HALA2018090800418.md): Wire · broken · Sep 8, 2018 · N594HA · Boeing 767332 · Flight Control System Wiring
  > RUDDER RATIO EICAS IN FLIGHT. AIR TURNBACK, TROUBLESHOT TO A BROKEN WIRE W1261-304R-22. REMOVED THE WIRE & CAPPED. INSTALLED THE SPARE WIRE. OPS CHECKED THE RUDDER RATIO, AND YAW DAMP SYSTEM, ALL OPS NORMAL, OK FOR SERVICE IAW AMM 27-21-13.
- [SDR HALA2018082300399](https://openairdocs.org/sdr/HALA2018082300399.md): Connector · dirty · Aug 22, 2018 · N594HA · Boeing 767332 · Engine Indicating System Wiring
  > ETOPS SIGNIFICANT SYSTEM - ON CLIMB OUT THROUGH FL 180 Z11OZ RIGHT ENG EGT FLUCTUATED BETWEEN 140 - 830 ALL THE WAY TO CRUISE FL370 THEN STABILIZED. TS PER FIM 77-21FT-803 CLEANED ALL CONNECTORS AND THERMOCOUPLE PROBES, OPS CHECKED GOOD. EGT STABLE.
- [SDR HALA2018081500379](https://openairdocs.org/sdr/HALA2018081500379.md): Smoke Detector · false activation · Aug 14, 2018 · N594HA · Boeing 767332 · Smoke Detection
  > LAVATORY D SMOKE ALARM ACTIVATED. NO SMOKE EVIDENT. OPS CHECKED THE LAVATORY D SMOKE DETECTOR. OPS CHECKED NORMAL. OK FOR SERVICE.
- [SDR HALA2018081400373](https://openairdocs.org/sdr/HALA2018081400373.md): Warning Message · false activation · Aug 13, 2018 · N594HA · Boeing 767332 · Hydraulic System, Main
  > RIGHT HYD SYS LOW, RF INDICATION.73 3 HRS INTO FLT..70 AT TOD.66 AT SHUTDOWN, CENTER SYS AT 1.20 IN FLT, 1.05 AT ENG START. TRANSFERRED CENTER HYD TO RIGHT IAW AMM 29-11-00-862-230. CYCLED LEFT AND RIGHT ANTI-SKID SHUTTLE VALVES. MONITORED CENTER AND RIGH
- [SDR HALA2018080900366](https://openairdocs.org/sdr/HALA2018080900366.md): Warning Light · false activation · Aug 8, 2018 · N594HA · Boeing 767332 · Rudder Control System
  > RUDDER RATIO EICAS MESSAGE AND DISCREET LIGHT ILLUMINATED DURING TAKE OFF ROLL, AND REMAINED ON FOR THE DURATION OF FLIGHT. PERFORMED FIM 27-21-804, 27-09 F/T 803, & 27-00 FT 814 SYSTEM OK, OK TO CONTINUE.
- [SDR HALA0218080800364](https://openairdocs.org/sdr/HALA0218080800364.md): Connector · loose · Aug 6, 2018 · N594HA · Boeing 767332 · Engine Indicating System Wiring
  > RIGHT ENGINE EGT INDICATION ERRATIC IN ALL PHASES OF FLIGHT. TROUBLESHOT IAW FIM 77-21FT803. FOUND A LOOSE WIRE CONNECTION AT THE RIGHT ENGINE OTBD EGT THERMOCOUPLE PROBE AT THE 2:30 POSITION. TIGHTENED THE CONNECTION. FLT CREW PERFORMED A HIGH POWER RUN, E
- [SDR HALA0218080800361](https://openairdocs.org/sdr/HALA0218080800361.md): Warning Light · false activation · Aug 5, 2018 · N594HA · Boeing 767332 · Rudder Control System
  > DURING TAKEOFF AT ROTATION, AMBER EICAS FOR RUDDER RATION ILLUMINATED. COMPLIED WITH QRH AND CONTINUED. COMPLIED WITH FIM 27-21 F/T 804, 27-09 F/T 803, & 27-09 F/T 814 THE SYSTEM OK, OK TO CONTINUE.
- [SDR HALA2018072300333](https://openairdocs.org/sdr/HALA2018072300333.md): Motor · faulty · Jul 22, 2018 · N594HA · Boeing 767332 · APU Start/Ignition System
  > ETOPS SIGNIFICANT SYSTEM - APU FAULT MESSAGE UPON START ATTEMPT ON GROUND. HUNG START AT 30% RPM AND 770 DEGREE C EGT. REMOVED AND REPLACED APU STARTER MOTOR PER AMM 49-41-01. OPS AND LEAK CHECK OK. REMOVED AND REPLACED APU GENERATOR SCAVENGE FILTER AND APU LU
- [SDR HALA2018072300332](https://openairdocs.org/sdr/HALA2018072300332.md): Display · defective · Jul 22, 2018 · N594HA · Boeing 767332 · Central Display
  > ETOPS SIGNIFICANT SYSTEM - AIR DIVERSION, LDW 2930 W/IN LIMITS. LOWER CRT FAILED IN THE CRUISE. EICAS DISPLAY MSG. COMPLIED W QRH. LANDING WEIGHT NOTED. REPLACED LOWER EICAS DISPLAY PER AMM 31-41-01-404-002. OPS CHECK GOOD. OK FOR SERVICE. AIRCRAFT DIVERTED T
- [SDR HALA2018072300334](https://openairdocs.org/sdr/HALA2018072300334.md): Display · defective · Jul 20, 2018 · N594HA · Boeing 767332 · Central Display
  > ETOPS SIGNIFICANT SYSTEM, LOWER EICAS SCREEN INTERMITTENTLY VERY BLURRY. APPEARS TO BECOME BLURRY WHEN LIGHT SENSORS ARE MOST ILLUMINATED BY SUN. REMOVED AND REPLACED LOWER EICAS DISPLAY PER AMM 31-41-01. OPERATIONAL CHECK GOOD. NO FAULTS NOTED. OK FOR SERVICE
- [SDR HALA2018071900324](https://openairdocs.org/sdr/HALA2018071900324.md): Wire · damaged · Jul 19, 2018 · N594HA · Boeing 767332 · Light System Wiring
  > EMERGENCY LIGHTS AT SEATS 1H, 2H, 3B, 23H, 25B, 37B, 38B AND 39B INOPERATIVE. CRIMPED THE SEAT 2H WIRE. REPLACED THE LAMPS AT SEATS 1H, 3B, 23H, 25B, 37B, 38B AND 39B. OPS CHECKED OK.
- [SDR HALA2018071900325](https://openairdocs.org/sdr/HALA2018071900325.md): Ecu · malfunctioned · Jul 16, 2018 · N594HA · Boeing 767332 · APU Start/Ignition System
  > ETOPS SIGNIFICANT SYSTEM - APU WILL NOT START ON LANDING. 2 ATTEMPTS. REMOVED AND REPLACED APU ECU PER AMM 49-61-05. OPS CHECK GOOD. NO FAULTS DETECTED. OK FOR SVC
- [SDR HALA2018062700311](https://openairdocs.org/sdr/HALA2018062700311.md): Warning Light · false activation · Jun 26, 2018 · N594HA · Boeing 767332 · Rudder Control System
  > AFTER TAKE OFF, RUDDER RATIO MESSAGE DISPLAYED ON EICAS, WITH ASSOCIATED DISCRETE LIGHT ILLUMINATED. HYDRAULIC PRESSURE NORMAL. PREFORMED FIM 27-09 FAULT TREE 814, RUDDER RATIO CHANGER MODULE BITE. NO FAULTS NOTED. OK TO CONTINUE.
- [SDR HALA2018062000290](https://openairdocs.org/sdr/HALA2018062000290.md): Mec · malfunctioned · Jun 19, 2018 · N594HA · Boeing 7673CB · Fuel Controlling System
  > IDENTICAL RT ENGINE IDLE POWER PROBLEM AS PREVIOUS FLIGHT 23 BUT WITH EEC OFF THRUST LEVER IDLE N1 42.7, N2 79.1, FF 1.3. REMOVED & REPLACED THE RT ENGINE MEC IAW AMM 73-21-01-404-032-G00 UP TO STOP 2E(14)(C). COMPLETED UP TO STEPS 2F(9). COMPLETED 73-21-01-4
- [SDR HALA2018062000289](https://openairdocs.org/sdr/HALA2018062000289.md): Mec · malfunctioned · Jun 19, 2018 · N594HA · Boeing 767332 · Fuel Control/Reciprocating Engines
  > RIGHT ENGINE DID NOT REDUCE TO IDLE ON INITIAL DESCENT, FL370 - 11,000, CORRECTED ITSELF FOR FINAL DESCENT N1 53.0 & N2 80.9, FF 1.2. REMOVED & REPLACED THE RT ENGINE MEC IAW AMM 73-21-01-404-032-G00, UP TO STOP 2E(14)(C) COMPLETED UP TO STEPS 2F(9). COMP
- [SDR HALA2018060400274](https://openairdocs.org/sdr/HALA2018060400274.md): Engine · malfunctioned · Jun 3, 2018 · N594HA · Boeing 767332 · Engine (Turbine/Turboprop)
  > RIGHT ENGINE PARAMETERS HIGH DURING DECENT AND LANDING, N1 32.0 (L), N2 65.1 (L), N1 48 (R), N2 79.4 (R), > 18000. SUSPECT LEFT ENGINE WENT TO GROUND IDLE ON APPROACH. BITE OF EEC MONITOR SHOWS NO FUALTS. REPLACED RELAYS K433 RT ENG AND K434 L ENG. PERFO
- [SDR HALA2018060400273](https://openairdocs.org/sdr/HALA2018060400273.md): Sensor · malfunctioned · Jun 1, 2018 · N594HA · Boeing 767332 · Engine Indicating System
  > DURING DECENT, AT IDLE POWER. THE RIGHT ENGINE INDICATION WAS 47% N1, THE LEFT ENGINE WAS 33% N1. AUTO THROTTLE OFF, RIGHT ENGINE HAD AT HIGH FLIGHT IDLE. TROUBLESHOT IAW FIM 73-21-00-815-817-G00, REMOVED AND REPLACED THE LEFT ENGINE CIT SENSOR IAW AMM 73-21-
- [SDR HALA2018060400272](https://openairdocs.org/sdr/HALA2018060400272.md): Engine · malfunctioned · May 31, 2018 · N594HA · Boeing 767332 · Engine (Turbine/Turboprop)
  > DURING DESCENT, THE RIGHT ENGINE STAYED AT 41% N1 AND LEFT AT30 % N1, EQUALIZE AT 10000 FEET. TROUBLESHOT IAW FIM 71.01 F/T 804 EEC BITE WITH NO FAULT. PERFORMED PSEU BITE NO FAULT NOTED. PER TASK 71-00-00-735-001-G00 PERFORMED TEST 3, GROUND TEST FOR IDLE P
- [SDR HALA2018052900260](https://openairdocs.org/sdr/HALA2018052900260.md): Connector · loose · May 25, 2018 · N594HA · Boeing 767332 · Engine Control System Wiring
  > OPEN - ETOPS SIGNIFICANT SYSTEM - DURING DESCENT W/ BOTH THROTTLES AT IDLE STOPS R ENGINE POWER WAS SIGNIFICANTLY HIGHER THAN LT ENGINE POWER. AT FL 250 L ENG N1= 31.8; R ENG N1= 46.7. L ENG N2= 65.2%, RT ENG N2= 79.8% (CONT) (CONTINUED) AT FL 250, IDLE DESCEN
- [SDR HALA2018052300241](https://openairdocs.org/sdr/HALA2018052300241.md): Display · malfunctioned · May 22, 2018 · N594HA · Boeing 767332 · Flight Management Computing Hardware System
  > CAPTAIN`S MCDU AND SCREEN WAS UNUSABLE FOR 15 MINUTES, FLICKERING, DISTORTING AND GOING BLANK. FULL MCDU RECOVERY. CHECKED THE CONNECTOR PLUGS, CLEANED FILTER, NO DEFECTS NOTED. OK TO CONTINUE.
- [SDR HALA2017052200239](https://openairdocs.org/sdr/HALA2017052200239.md): Engine · power loss · May 21, 2018 · N594HA · Boeing 767332 · Engine (Turbine/Turboprop)
  > LEFT THRUST LEVER REQUIRED MANUAL ADJUSTMENT TO OBTAIN TAKEOFF THRUST AT FULL FORWARD STOP. EGT, N1, FUEL FLOWS MATCHED. THREE INCH THRUST LEVER SPLIT FROM FM 1 THR HLD INDICATED AT 100 KTS. LEFT ENGINE ACCELERATION ON TAKEOFF SLOW. LEFT ENGINE RESPONSE A
- [SDR HALA208051700237](https://openairdocs.org/sdr/HALA208051700237.md): Module · malfunctioned · May 16, 2018 · N594HA · Boeing 767332 · Rudder Control System
  > RUDDER RATIO EICAS AND DISCRETE LIGHT. PERFORMED FIM 27-21 F/T 804. RESET LEFT AND RIGHT RUDDER CHANGE MODULES. OPERATED SYSTEM, NO MESSAGES. OK FOR SERVICE.
- [SDR HALA2018051600228](https://openairdocs.org/sdr/HALA2018051600228.md): Filter · contaminated · May 12, 2018 · N594HA · Boeing 767332 · Engine Fuel Distribution
  > RIGHT ENGINE FUEL FILTER EICAS MESSAGE ILLUMINATED INTERMITTENTLY THROUGHOUT FLIGHT. REMAINED FOR LAST 2 HOURS OF FLIGHT. REPLACED THE FUEL FILTER, FOUND DEBRIS ON THE FILTER ELEMENT IAW AMM 73-11-08. ACCOMPLISHED A NR 2 ENGINE RUN UP TEST, NR 3, OPS & LEA
- [SDR HALA2018051600226](https://openairdocs.org/sdr/HALA2018051600226.md): Unknown · sparks · May 9, 2018 · N594HA · Boeing 767332 · Passenger/Crew Doors
  > WHEN OPERATING THE L1 DOOR THERE ARE SPARKS COMING FROM THE SLOT WHERE THE YELLOW SAFETY PLACARD UNDERNEATH THE ARMING LEVER. OPERATED THE L1 DOOR ELECTRONICALLY AND MECHANICALLY SEVERAL TIMES. DOOR OPERATES NORMALLY. NO DEFECTS NOTED. NO WIRING OR SURFACES
- [SDR HALA2018051600225](https://openairdocs.org/sdr/HALA2018051600225.md): Antenna · inoperative · May 8, 2018 · N594HA · Boeing 767332 · Global Positioning System
  > WITH ONLY THE R GPS EICAS MESSAGE DISPLAYED, IT APPEARS BOTH LT AND RT GPS ARE INOPERATIVE. IAW THE POS REF PAGE ON THE CDU. REPLACED THE LEFT GPS ANTENNA IAW AMM 34-58-02. OPS CHECKED OK.
- [SDR HALA2017122000308](https://openairdocs.org/sdr/HALA2017122000308.md): Indicator · inoperative · Dec 19, 2017 · N594HA · Boeing 767332 · Weather Radar System
  > ATB - TCAS AND WX SCREEN ON CENTER CONSOLE INOP. REMOVED AND REPLACED WXR/TCAS INDICATOR PER AMM 34-43-06. OPS CHECK GOOD. OK FOR SVC.
- [SDR HALA2017112100282](https://openairdocs.org/sdr/HALA2017112100282.md): Wire · damaged · Nov 21, 2017 · N594HA · Boeing 767300 · Pneumatic System Wiring
  > LEFT ENGINE BLEED VALVE EICAS MESSAGE. RETURNED TO DEPARTURE. FOUND HPSOV TERM 1 CONNECTOR D4210P PIN 10 OPEN AND HPSOV TERM 2 TO D4210P OPEN. REPLACED THE TERMINAL 1 ON WIRE.
- [SDR HALA2017080800217](https://openairdocs.org/sdr/HALA2017080800217.md): Controller · failed · Aug 8, 2017 · N594HA · Boeing 767332 · Cabin Pressure Controller
  > CABIN PRESS AUTO INOP LT ILLUMINATED ON GROUND AFTER ENG START/TAXI. CABIN DIFF CLIMBED TO 4 PSI DIFF. NO CHANGE TO CONDITION W/ SWITCH TO AUTO 2. OUTFLOW VALVE REMAINED CLOSED. CABIN ALT AUTO 2 EICAS MSG DISPLAYED. CPC NR 2 FAULTED ON BITE TEST. MANUAL MODE O
- [SDR HALA2017080200216](https://openairdocs.org/sdr/HALA2017080200216.md): Adc · faulty · Aug 2, 2017 · N594HA · Boeing 767332 · Air Data Computer
  > INTERMITTENT "RUDDER RATIO" EICAS MSG AND ANNUNCIATOR LIGHT, ACCOMPANIED BY LOSS OF CAPTAIN'S MACH AIRSPEED AND ALTITUDE INFORMATION, W/ASSOCIATED OFF FLAGS PRESENT. SWITCHED TO "ALTN" ON CAPTAIN AIR DATA SWITCH, NO MORE LOSS OF AIRSPEED AND ALT INFO, BUT "RUD
- [SDR HALA2017071900194](https://openairdocs.org/sdr/HALA2017071900194.md): Warning System · false activation · Jul 18, 2017 · N594HA · Boeing 767332 · Cabin Pressure Control System
  > AFTER PUSH BACK STATUS PG "CABIN ALT AUTO 1", "CABIN ALT AUTO 2". PERFORMED BITE FOR CABIN PRESS CONTROL 1 & 2 PER FIM 21-31-803, NO FAULTS NOTED, EICAS MESSAGES CLEARED, VISUALLY INSPECTED, LUBED OUTFLOW VALVE LINKAGES, MANUALLY OPERATED VALVE, NO FAULTS NO
- [SDR HALA2017061400156](https://openairdocs.org/sdr/HALA2017061400156.md): Pressure Switch · inoperative · Jun 13, 2017 · N594HA · Boeing 767332 · Hydraulic System, Main
  > RT ENGINE DRIVEN PUMP PRESSURE INDICATION NOT ILLUMINATED WITH ZERO PRESSURE. ASSOCIATED DEMAND PUMP AUTO FUNCTION INOPERATIVE, NO HYD PRESSURE IN AUTO MODE. REMOVED AND REPLACED THE RT EDP PRESSURE SWITCH IAW AMM 29-11-17. OPS CHECKED OK, OK FOR SERVICE.
- [SDR HALA2017061200151](https://openairdocs.org/sdr/HALA2017061200151.md): Unknown · unknown · Jun 10, 2017 · N594HA · Boeing 767300 · Trailing Edge Flap Control System
  > AFT FLAPS EXTENDED TO 5 DEG. FOR TAKEOFF, SPL INDICATED RT INBD AILERON DID NOT DROOP. CYCLING AILERONS BLED SYSTEM, OPS CHECKED AILERONS AND FLAPS IAW AMM 27-11-00 AND 27-51-00. OPS NORMAL, LT & RT INDICATION OF AILERON DROOP NORMAL. OK FOR SERVICE.
- [SDR HALA2017060600138](https://openairdocs.org/sdr/HALA2017060600138.md): Lever · binding · Jun 5, 2017 · N594HA · Boeing 767332 · Power Lever
  > RIGHT TRUST LEVER BINDING, TAKEOFF POWER NEEDED MANUAL ASSIST. AUTOTHROTTLE DISC TWICE IN CRUISE FLIGHT. LEVEL OFF ON DESCENT L TRUST LEVER ADVANCED TO FULL, R THRUST LEVER STUCK, MANUALLY DISCONNECTED A/T AND RESET. TAXING OFF RWY STUCK.// ACCOMPLISHED HAL M1
- [SDR HALA2017051400118](https://openairdocs.org/sdr/HALA2017051400118.md): Gcu · malfunctioned · May 14, 2017 · N594HA · Boeing 767324 · AC Regulator
  > LEFT GENERATOR FAULT RAN QRH ATTEMPTED RESET ONCE WOULD NOT RESET. PERFORMED BPCU BITE PER AMM 24-22-00-745-071. REMOVED AND REPLACED LT GCU PER AMM 24-22-02-004-001. OPERATIONAL CHECK GOOD. OK FOR RETURN TO SERVICE.
- [SDR HALA2017041700102](https://openairdocs.org/sdr/HALA2017041700102.md): Sensor · faulty · Apr 17, 2017 · N594HA · Boeing 767332 · Fuel Control/Turbine Engines
  > ATB, ON TAKE OFF RT ENG DID NOT ACHIEVE TO THRUST. REDUCED THRUST WAS 103.5. RT ENG ONLY ACHIEVE 101.1 (RT THROTTLE FULL FWD AT). PERFORMED FIM 73-21 TREE 811 TAKEOFF/CLIMB N1 LIMITED BY EEC. NO FAULT PRESENT ON EEC MONITOR UNIT. INSPECTED CDP TUBES AND MEC CD
- [SDR HALA2017030700055](https://openairdocs.org/sdr/HALA2017030700055.md): Idg · malfunctioned · Mar 7, 2017 · N594HA · Boeing 767332 · AC Generator-Alternator
  > ATB, L GEN OFF LIGHT UNABLE TO RESET BITE BPCU PER FIM 24-20 TREE 801. R&R LEFT IDG PER AMM 24-11-01 AND OPS CHECKED PER AMM 24-11-02-715-005. R&R GCU PER AMM 24-22-02. OFF: PN: 729825M SN: C1467 OFF: PN: 734284F SN: 5438 ON: PN: 729825H SN: 4369 ON: PN: 73428
- [SDR HALA2017022100043](https://openairdocs.org/sdr/HALA2017022100043.md): Gcu · faulted · Feb 21, 2017 · N594HA · Boeing 767332 · AC Regulator
  > IN TURB LT GEN OFF EICAS AND LT GEN CONT OFF LIGHTS ILLUM. ATTEMPTED QRH RESET, UNSUCCESSFUL. PERF BCPU BITE TEST RT GCU FAULT. R&R RT GCU PER 24-22-02. RAN BOTH ENGINES TO TEST 1+2 IDG PER 24-11-00. BOTH IDG 1+2 OPS OK. NO FAULTS NOTED ON BPCU. OK FOR SERVICE
- [SDR HALA2017021300032](https://openairdocs.org/sdr/HALA2017021300032.md): Charger · no test · Feb 13, 2017 · N594HA · Boeing 767332 · Rudder Control System
  > RUDDER RATIO EICAS CAUTION MESSAGE AT TOUCHDOWN. PERFORMED RUDDER RATIO CHANGER SYSTEM TEST IAW AMM 27-21-00-715-001-001. LVDT & TEST FAIL FAULT BALLS PRESENT ON RIGHT RRCM. IAW FIM 27-09-00 FAULT TREE 814, BLOCKS 1, 51, 51A. REPLACED THE RRCM LVDT IAW

Next page: https://openairdocs.org/deregistered/N594HA-2019-05-07/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 n_number = 'N594HA' AND deregistration_id = 'N594HA-2019-05-07'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N594HA-2019-05-07/reports

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