# N594HA: 1986 Boeing 767-332, registration cancelled 2019-05-07

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: May 7, 2019
- Status when cancelled: Valid registration
- Airframe: [Boeing 767-332](https://openairdocs.org/model/boeing-767-332) (registry code 1385101)
- Engine: [GE CF6-80 series](https://openairdocs.org/engine/ge-cf6-80-series) (registry code 30025)
- Data sheets: [TCDS A1NM](https://openairdocs.org/tcds/A1NM), [TCDS E13NE](https://openairdocs.org/tcds/E13NE) (OpenAirDocs)
- Serial number: 23275
- Year built: 1986
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 11, 1986
- Certificate issued: March 14, 2019
- Last registry action: March 14, 2019
- Mode S code: A7ACF3
- Owner when cancelled: [Aar Supply Chain Inc](https://openairdocs.org/faa-owner/AAR%20SUPPLY%20CHAIN%20INC)
- Location: [Wood Dale, IL](https://openairdocs.org/faa-place/IL/Wood%20Dale)
- Owner type: Corporation
- Owner's area on the map: 41.9744° N, 87.9865° W: Placed by OpenAirDocs at the center of ZIP code 60191, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N594HA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=594HA
- Page: https://openairdocs.org/deregistered/N594HA-2019-05-07

From the FAA registry file of November 4, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Boeing 767-332: https://openairdocs.org/model/boeing-767-332.md

## Service difficulty reports (411, newest 50)

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

- [SDR HALA2018120500632](https://openairdocs.org/sdr/HALA2018120500632), Dec 4, 2018: WIRE HARNESS. DAMAGED. 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), Dec 4, 2018: WIRE HARNESS. DAMAGED. 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), Nov 26, 2018: CHARGER. INOPERATIVE. 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 25-31
- [SDR HALA2018112760614](https://openairdocs.org/sdr/HALA2018112760614), Nov 22, 2018: FMC. MALFUNCTIONED. 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. 
- [SDR HALA2018112000603](https://openairdocs.org/sdr/HALA2018112000603), Nov 19, 2018: CONTROL UNIT. MALFUNCTIONED. 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 
- [SDR HALA2018112000602](https://openairdocs.org/sdr/HALA2018112000602), Nov 19, 2018: WIRE. EXPOSED. 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), Nov 17, 2018: LENS. MISSING. 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), Oct 28, 2018: VALVE. LEAKING. 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 FAU
- [SDR HALA2018100900483](https://openairdocs.org/sdr/HALA2018100900483), Oct 8, 2018: SLEEVE. TORN. 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
- [SDR HALA20181009483](https://openairdocs.org/sdr/HALA20181009483), Oct 8, 2018: SLEEVE. TORN. 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
- [SDR HALA2018100100460](https://openairdocs.org/sdr/HALA2018100100460), Sep 30, 2018: GUIDE VANE. MISSING. 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), Sep 24, 2018: SOLENOID. FAULTY. 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 REDU
- [SDR HALA2018090800418](https://openairdocs.org/sdr/HALA2018090800418), Sep 8, 2018: WIRE. BROKEN. 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 RUD
- [SDR HALA2018082300399](https://openairdocs.org/sdr/HALA2018082300399), Aug 22, 2018: CONNECTOR. DIRTY. 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 
- [SDR HALA2018081500379](https://openairdocs.org/sdr/HALA2018081500379), Aug 14, 2018: SMOKE DETECTOR. FALSE ACTIVATION. 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), Aug 13, 2018: WARNING MESSAGE. FALSE ACTIVATION. 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 I
- [SDR HALA2018080900366](https://openairdocs.org/sdr/HALA2018080900366), Aug 8, 2018: WARNING LIGHT. FALSE ACTIVATION. 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 8
- [SDR HALA0218080800364](https://openairdocs.org/sdr/HALA0218080800364), Aug 6, 2018: CONNECTOR. LOOSE. 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 THERMOCO
- [SDR HALA0218080800361](https://openairdocs.org/sdr/HALA0218080800361), Aug 5, 2018: WARNING LIGHT. FALSE ACTIVATION. 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 
- [SDR HALA2018072300333](https://openairdocs.org/sdr/HALA2018072300333), Jul 22, 2018: MOTOR. FAULTY. 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 PE
- [SDR HALA2018072300332](https://openairdocs.org/sdr/HALA2018072300332), Jul 22, 2018: DISPLAY. DEFECTIVE. 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. REPLACE
- [SDR HALA2018072300334](https://openairdocs.org/sdr/HALA2018072300334), Jul 20, 2018: DISPLAY. DEFECTIVE. ETOPS SIGNIFICANT SYSTEM, LOWER EICAS SCREEN INTERMITTENTLY VERY BLURRY. APPEARS TO BECOME BLURRY WHEN LIGHT SENSORS ARE MOST ILLUMINATED BY SUN. REMOVED AND RE
- [SDR HALA2018071900324](https://openairdocs.org/sdr/HALA2018071900324), Jul 19, 2018: WIRE. DAMAGED. 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 A
- [SDR HALA2018071900325](https://openairdocs.org/sdr/HALA2018071900325), Jul 16, 2018: ECU. MALFUNCTIONED. 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 
- [SDR HALA2018062700311](https://openairdocs.org/sdr/HALA2018062700311), Jun 26, 2018: WARNING LIGHT. FALSE ACTIVATION. AFTER TAKE OFF, RUDDER RATIO MESSAGE DISPLAYED ON EICAS, WITH ASSOCIATED DISCRETE LIGHT ILLUMINATED. HYDRAULIC PRESSURE NORMAL. PREFORMED FIM 27-09 FAULT TREE 8
- [SDR HALA2018062000290](https://openairdocs.org/sdr/HALA2018062000290), Jun 19, 2018: MEC. MALFUNCTIONED. 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 I
- [SDR HALA2018062000289](https://openairdocs.org/sdr/HALA2018062000289), Jun 19, 2018: MEC. MALFUNCTIONED. 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 
- [SDR HALA2018060400274](https://openairdocs.org/sdr/HALA2018060400274), Jun 3, 2018: ENGINE. MALFUNCTIONED. 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 AP
- [SDR HALA2018060400273](https://openairdocs.org/sdr/HALA2018060400273), Jun 1, 2018: SENSOR. MALFUNCTIONED. 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. TROUB
- [SDR HALA2018060400272](https://openairdocs.org/sdr/HALA2018060400272), May 31, 2018: ENGINE. MALFUNCTIONED. 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. PERFORME
- [SDR HALA2018052900260](https://openairdocs.org/sdr/HALA2018052900260), May 25, 2018: CONNECTOR. LOOSE. 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 N
- [SDR HALA2018052300241](https://openairdocs.org/sdr/HALA2018052300241), May 22, 2018: DISPLAY. MALFUNCTIONED. CAPTAIN`S MCDU AND SCREEN WAS UNUSABLE FOR 15 MINUTES, FLICKERING, DISTORTING AND GOING BLANK. FULL MCDU RECOVERY. CHECKED THE CONNECTOR PLUGS, CLEANED FILTER, 
- [SDR HALA2017052200239](https://openairdocs.org/sdr/HALA2017052200239), May 21, 2018: ENGINE. POWER LOSS. 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
- [SDR HALA208051700237](https://openairdocs.org/sdr/HALA208051700237), May 16, 2018: MODULE. MALFUNCTIONED. 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), May 12, 2018: FILTER. CONTAMINATED. RIGHT ENGINE FUEL FILTER EICAS MESSAGE ILLUMINATED INTERMITTENTLY THROUGHOUT FLIGHT. REMAINED FOR LAST 2 HOURS OF FLIGHT. REPLACED THE FUEL FILTER, FOUND DEBRIS
- [SDR HALA2018051600226](https://openairdocs.org/sdr/HALA2018051600226), May 9, 2018: UNKNOWN. SPARKS. 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 ELECTRONICALL
- [SDR HALA2018051600225](https://openairdocs.org/sdr/HALA2018051600225), May 8, 2018: ANTENNA. INOPERATIVE. 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 A
- [SDR HALA2017122000308](https://openairdocs.org/sdr/HALA2017122000308), Dec 19, 2017: INDICATOR. INOPERATIVE. 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), Nov 21, 2017: WIRE. DAMAGED. 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 TERM
- [SDR HALA2017080800217](https://openairdocs.org/sdr/HALA2017080800217), Aug 8, 2017: CONTROLLER. FAILED. 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
- [SDR HALA2017080200216](https://openairdocs.org/sdr/HALA2017080200216), Aug 2, 2017: ADC. FAULTY. INTERMITTENT "RUDDER RATIO" EICAS MSG AND ANNUNCIATOR LIGHT, ACCOMPANIED BY LOSS OF CAPTAIN'S MACH AIRSPEED AND ALTITUDE INFORMATION, W/ASSOCIATED OFF FLAGS PRE
- [SDR HALA2017071900194](https://openairdocs.org/sdr/HALA2017071900194), Jul 18, 2017: WARNING SYSTEM. FALSE ACTIVATION. 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 MESSAGE
- [SDR HALA2017061400156](https://openairdocs.org/sdr/HALA2017061400156), Jun 13, 2017: PRESSURE SWITCH. INOPERATIVE. RT ENGINE DRIVEN PUMP PRESSURE INDICATION NOT ILLUMINATED WITH ZERO PRESSURE. ASSOCIATED DEMAND PUMP AUTO FUNCTION INOPERATIVE, NO HYD PRESSURE IN AUTO MODE. RE
- [SDR HALA2017061200151](https://openairdocs.org/sdr/HALA2017061200151), Jun 10, 2017: UNKNOWN. UNKNOWN. 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 27-1
- [SDR HALA2017060600138](https://openairdocs.org/sdr/HALA2017060600138), Jun 5, 2017: LEVER. BINDING. 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 
- [SDR HALA2017051400118](https://openairdocs.org/sdr/HALA2017051400118), May 14, 2017: GCU. MALFUNCTIONED. 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 24-22-02-00
- [SDR HALA2017041700102](https://openairdocs.org/sdr/HALA2017041700102), Apr 17, 2017: SENSOR. FAULTY. 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 T
- [SDR HALA2017030700055](https://openairdocs.org/sdr/HALA2017030700055), Mar 7, 2017: IDG. MALFUNCTIONED. 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 2
- [SDR HALA2017022100043](https://openairdocs.org/sdr/HALA2017022100043), Feb 21, 2017: GCU. FAULTED. 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 BOT
- [SDR HALA2017021300032](https://openairdocs.org/sdr/HALA2017021300032), Feb 13, 2017: CHARGER. NO TEST. 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 O

All 411: https://openairdocs.org/deregistered/N594HA-2019-05-07/reports.md

## Other aircraft with N594HA

- [Cancelled 2003-09-08](https://openairdocs.org/deregistered/N594HA-2003-09-08): Boeing 767-3CB, S/N 33469, built 2003. Exported to Bermuda. Owner: [Boeing Company](https://openairdocs.org/faa-owner/BOEING%20COMPANY), [Seattle, WA](https://openairdocs.org/faa-place/WA/Seattle)

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