# Service difficulty reports: N596HA, cancelled Mar 11, 2014

A list on [N596HA, cancelled Mar 11, 2014](https://openairdocs.org/deregistered/N596HA-2014-03-11.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 6 · 251 reports

- [SDR HALA201312250181](https://openairdocs.org/sdr/HALA201312250181.md): Connector · failed · Dec 25, 2013 · N596HA · Boeing 767332 · Fuel System Wiring
  > FUEL QTY INDICATION STATUS MESSAGE CENTER TANK FUEL & TOTALIZER ON OVERHEAD ARE BLANK. R & R FQIS PROCESSOR IAW AMM 28-41-08 CONDITION SAME. FQIS BITE FAULT CODE 71. ACCOMPLISHED LT AUX TANK INSULATION RESISTANCE TEST AMM 28-41-00. FOUND LT AUX BUSSING PLUG
- [SDR HALA2013111100167](https://openairdocs.org/sdr/HALA2013111100167.md): Pump · failed · Nov 11, 2013 · N596HA · Boeing 767332 · Hydraulic Pump (Electric/Engine), Main
  > LEFT HYD PRIMARY OVERHEAT EICAS MESSAGE. IAW MOC INSTRUCTION/TSI T/S FIM 29-11, FT821. R & R ENG DRIVEN HYD PUMP IAW AMM 29-11-05. RAN LT ENGINE. LT EDP PRESSURE CHECKED GOOD AT 3000 PSI.
- [SDR HALA2013092600122](https://openairdocs.org/sdr/HALA2013092600122.md): Circuit Card · failed · Sep 26, 2013 · N596HA · Boeing 767332 · Stall Warning System
  > WARN ELEX ADVISORY DISPLAYED IN FLIGHT ALONG WITH AMBER SPLIM ON F/O ADI SPEED TAPE WITH LOSS OF RED SPEED TAPE INDICATOR BAR. REPLACED RT WARNING ELEX STALL WARNING CARD. OPS CHECK OK IAW FIM 27-32-00, FIG 105.
- [SDR HALA2013072400094](https://openairdocs.org/sdr/HALA2013072400094.md): Transformer · inoperative · Jul 24, 2013 · N596HA · Boeing 767332 · Trailing Edge Flap Control System
  > ACFT DIVERTED TO AN ALTERNATE STATION. T/E FLAP DISAGREE EICAS AND CVE LIGHTS ILLUMINATED WHEN FLAPS SELECTED TO 15 DEGREES. AND STATUS T/E FLAP SHUTDOWN. ACCOMPLISHED FIM 27-51, FIG 114C, ACCOMPLISHED FSPM BITE FIM 27-58, FIG 104, ACCOMPLISHED FSEU BI
- [SDR HALA2013071500089](https://openairdocs.org/sdr/HALA2013071500089.md): Connector · dirty · Jul 15, 2013 · N596HA · Boeing 767332 · Engine Indicating System Wiring
  > ON RIGHT ENG START EGT FLUCTUATING DID NOT INCREASE. CLEANED CONNECTOR ON RT ENG. OPS NORMAL, OK FOR SERVICE.
- [SDR HALA2013071200087](https://openairdocs.org/sdr/HALA2013071200087.md): Connector · disconnected · Jul 12, 2013 · N596HA · Boeing 767332 · Engine Indicating System Wiring
  > AFTER START RT ENGINE EGT FAILED (13DEG) (BTB). INSPECTED RT ENG THERMOCOUPLES, FOUND CONNECTOR DISCONNECTED ON THE FWD SIDE OF J-BOX. CONNECTED CONNECTOR, RAN ENGINE, EGT INDICATION NORMAL. ALL WORK PERORMED IAW AMM 77-21-02 AND 71-00-00.
- [SDR HALA2013061400081](https://openairdocs.org/sdr/HALA2013061400081.md): Skin · dented · Jun 14, 2013 · N596HA · Boeing 767332 · Fuselage Main, Plate/Skin
  > DENT FOUND FWD AND LOWER OF AFT CARGO COMPT. APPROX BS 1329, BETWEEN STRINGERS S36-37. NDT INSPECTION-NO CRACKS NOTED. PERFORMED INTERNAL VISUAL INSPECTION IAW SRM 53-00-01, NO DEFECTS NOTED. ACCOMPLISHED E105-596232-IN.
- [SDR HALA2013061400080](https://openairdocs.org/sdr/HALA2013061400080.md): Skin · damaged · Jun 14, 2013 · N596HA · Boeing 767332 · Fuselage Main, Plate/Skin
  > DENT FOUND FWD AND LOWER OF AFT CARGO COMPT APPROX BS 1280.5. BETWEEN STRINGERS S36-38. DENT 9"L X 12"W X.1875 DEPTH. GOUGE NOTED IN DENT.040 DEPT. NDT INSPECTION-CRACK INDICATION AT GOUGE. PERFORMED FLUORESCENT PENETRANT INSP OF AREA. NO CRACKS NOTED.
- [SDR HALA2013042700046](https://openairdocs.org/sdr/HALA2013042700046.md): J-Box · failed · Apr 27, 2013 · N596HA · Boeing 767332 · Engine Indicating System Wiring
  > RT PRIMARY ENGINE EGT INDICATOR READS ZERO USING LDRR ICAS COMPUTER STANDBY ENGINE INSTRUMENT ALSO READS ZERO. TROUBLESHOT IAW FIM 77-21, FAULT TREE 803 INSPECTED EGT THERMOCOUPLE CABLES TERMINALS AND BRACKET FOR DAMAGE INSPECTED CONNECTORS AND PINS AT FIREWA
- [SDR HALA2013041700039](https://openairdocs.org/sdr/HALA2013041700039.md): Engine · making metal · Apr 17, 2013 · N596HA · Boeing 767300 · APU Core Engine
  > APU AUTO SHUTDOWN. LOW OIL PRESSURE FAULT ON ECU. DP POPPED ON OIL FILTER. METAL PARTICLES FOUND ON GEARBOX CHIP DETECTOR. REPLACED APU IAW M266, AUXILIARY POWER UNIT (APU) CHANGE.
- [SDR HALA2012121000233](https://openairdocs.org/sdr/HALA2012121000233.md): Engine · hung start · Dec 10, 2012 · N596HA · Boeing 767332 · Engine (Turbine/Turboprop)
  > LEFT ENGINE HUNG START, N1 18.37. EGT 740. N2 56.47 F/F 1,200. REPLACED LT ENGINE MEC & LEAK CHECKED IAW AMM 73-21-01. REPLACED LT ENGINE T2 SENSOR IAW AMM 73-21-05. REPLACED CIT SENSOR. COMPLIED WITH ALL COMPONENT REPLACEMENT TESTS IAW AMM 71-00-00 TESTS
- [SDR HALA2012101000226](https://openairdocs.org/sdr/HALA2012101000226.md): Skin · damaged · Oct 10, 2012 · N596HA · Boeing 767332 · Fuselage Main, Plate/Skin
  > LIGHTING STRIKE FOUND AT BS 148.2, 6.5" BELOW & -24L. DAMAGED AREA CUT OUT IAW SRM 53-00-01-2R-16, REPAIR 14D6347210, REV. 90. REPAIR PARTS FABRICATED IAW SRM 53-00-01-2R-14 REPAIR 14, D634T210, REV 90. REPAIR PARTS INSTALLED IAW SRM 53-00-01-2R-14. REPAIR
- [SDR HALA2012053000151](https://openairdocs.org/sdr/HALA2012053000151.md): Circuit Card · failed · May 30, 2012 · N596HA · Boeing 767332 · Fire Detection
  > ACFT ARRIVED SAFELY, NR 1 & 2 FIRE BOTTLES FOR RT ENGINE WERE DISCHARGED BY THE FLT CREW DURING APPROACH. WHILE LINING UP FOR APPROACH RECEIVED "FIRE WARNING" ANNUNCIATION, FLT CREW DISCHARGED NR 1 BOTTLE. "WARNING DID NOT EXTINGUISH, THEN NR 2 BOTTLE DISCH
- [SDR HALA2012052900149](https://openairdocs.org/sdr/HALA2012052900149.md): Wire Harness · malfunctioned · May 29, 2012 · N596HA · Boeing 767332 · Engine Indicating System Wiring
  > RIGHT ENGINE LP2 STATUS MESSAGE WAS INTERMITTENT. R & R WIRE HARNESS ON RESPONDERS IAW AMM 26-11-02/401 AND ACCOMPLISHED LEAK CHECK ON ALL DUCTING IAW AMM 36-11-09-782-104-001, NO LEAKS, RAN ENGINE AT IDLE, NO EICAS OR STATUS MESSAGE ON RT ENGINE.
- [SDR HALA2012052700148](https://openairdocs.org/sdr/HALA2012052700148.md): Check Valve · malfunctioned · May 27, 2012 · N596HA · Boeing 767332 · Pneumatic Distribution System
  > RT ENGINE FIRE LP 2 STATUS MESSAGE INTERMITTENT. FOUND & REPLACED INTERMEDIATE CHECK VALVE & DUCT ASSY. OPS & LEAK CHECKED GOOD IAW AMM 36-11-06. LEAK CK GOOD.
- [SDR HALA2012052700147](https://openairdocs.org/sdr/HALA2012052700147.md): Warning Light · no indication · May 27, 2012 · N596HA · Boeing 767332 · Cabin Cooling System
  > LEFT PACK OFF LIGHT & LT PACK OFF EICAS MESSAGE NEVER ILLUMINATED WHEN PACK SELECTOR IN OFF POSITION. PERFORMED BITE CHECK ON LT PACK CONTROLLER NO FAULTS NOTED. TRIED TO DUPLICATE PROBLEM NUMEROUS TIMES. OPS CHECKED OK IAW AMM21-51-00-705-001.
- [SDR HALA2012052100143](https://openairdocs.org/sdr/HALA2012052100143.md): Fire Detector · false activation · May 21, 2012 · N596HA · Boeing 767332 · Fire Detection
  > RIGHT ENGINE FIRE LP2 EICAS ILLUMINATED. PERFORMED FIM 26-11-00/101, FIG 104, ENGINE FIRE DETECTION SYS BITE PROCEDURE RESECURED COUPLINGS AT HIGH STAGE BLEED MANIFOLD LEAK CHECKED NORMAL AT NR 2 POS.
- [SDR HALA2012051900141](https://openairdocs.org/sdr/HALA2012051900141.md): Unknown · warning message · May 19, 2012 · N596HA · Boeing 767332 · Central Warning
  > RIGHT EEC EICAS ILLUMINATED, DID NOT RESET IAW QRA. TROUBLESHOOTING PERFORMED, ECC MONITOR BITE NO FAULTS NOTED. RESET EEC SWITCH RAN ENGINE FOR 10 MIN. NO FAULTS NOTED. 2ND EEC MONITOR BITE SHOWED NO FAULTS. OK FOR CONTINUED SERVICE.
- [SDR HALA2012051900140](https://openairdocs.org/sdr/HALA2012051900140.md): Transceiver · not seated · May 19, 2012 · N596HA · Boeing 767332 · Ground Proximity System
  > A/S 192 KTS FLAP 20 DEGREE WHEN SPEEDBRAKES EXTENDED. RECEIVED RED CONFIG WARNING & GEAR NOT DOWN EICAS. RERACKED NR 1 RADIO ALT TRANSCEIVER, GROUND CHECKED OK. PERFORMED MCDP 30, NO FAULTS NOTED, TEST PASSES. ACFT LMP STATUS REMAINS LAND 3.
- [SDR HALA2012051400139](https://openairdocs.org/sdr/HALA2012051400139.md): Fire Detector · malfunctioned · May 14, 2012 · N596HA · Boeing 767332 · Fire Detection
  > AFTER PARKING, STATUS MESSAGE DISPLAYED RT ENGINE FIRE LOOP. AFTER A FEW MINUTES THE STAUS MESSAGE EXTINGUISHED. INSPECTED RT ENGINE FIRE LOOP WIRE HARNESS IAW WDM 26-11-21. NO DEFECTS NOTED. REPLACED RT ENGINE FIRE DETECTORS TS44, TS45, TS46 IAW AMM 26-11
- [SDR HALA2012051400138](https://openairdocs.org/sdr/HALA2012051400138.md): Warning Message · false activation · May 14, 2012 · N596HA · Boeing 767332 · Fire Detection
  > RECEIVED A STATUS MESSAGE "RT ENGINE FIRE LP 2". PERFORMED FIM 26-11-00/101 FIG 104. CHECKED RT ENG LP2 AND LP1 CONNECTIONS AND CLEANED. SECURITY/ATTACHMENT VERIFIED. OPERATION OF FIRE TEST NORMAL. REF AMM 26-11-00. STATUS MESSAGE EXTINGUISHED.
- [SDR HALA2012051300137](https://openairdocs.org/sdr/HALA2012051300137.md): Circuit Card · malfunctioned · May 13, 2012 · N596HA · Boeing 767332 · Fire Detection
  > RIGHT ENGINE FIRE LOOP, STATUS MESSAGE ILLUMINATED ON DECENT. EXTINGUISHED AFTER LANDING. CHECKED RESISTANCE AT M684, PINS 19 & 20 - 1.5 K OHMS. CHECKED INSULATION RESISTANCE BETWEEN PING 18 & 19, & PINS 18 & 20-54 OHMS. "SHAKE CHECKED" RT ENG FIRE LOOP HARNE
- [SDR HALA2012051000132](https://openairdocs.org/sdr/HALA2012051000132.md): Ecu · faulted · May 10, 2012 · N596HA · Boeing 767332 · APU Bleed Air System
  > PRIOR TO ENGINE START, APU FAULTED AND AUTO SHUTDOWN. BITE CHECKED APU ECU FOUND REVERSE FLOW FAULT. PERFORMED FIM 49-11-00-1 FIG 108. GROUND OPS CHECKED OK.
- [SDR HALA2012031800112](https://openairdocs.org/sdr/HALA2012031800112.md): Compressor · stalled · Mar 18, 2012 · N596HA · Boeing 767332 · Turbine Engine Compressor Section
  > NR 2 ENGINE COMPRESSOR STALL AT TOP OF CLIMB. FLT CREW DECLARED EMERGENCY AND DIVERTED BACK, WHERE AN UNEVENTFUL LANDING WAS MADE. OPEN.
- [SDR HALA2012030700107](https://openairdocs.org/sdr/HALA2012030700107.md): Fire Detector · malfunctioned · Mar 7, 2012 · N596HA · Boeing 767332 · Fire Detection
  > ETOPS SIGNIFICANT SYSTEM - ON COCKPIT PREFLIGHT FOUND NO AURAL WARNING WHEN WHEEL WELL AND ENG/APU/CARGO FIRE SYS TESTED. RE-SET MASTER WARNING CAUTION SWITCH, OPS CHECKED GOOD. W/W & ENG/APU,CARGO FIRE SYS CK GOOD.
- [SDR HALA2012030500105](https://openairdocs.org/sdr/HALA2012030500105.md): Connector · loose · Mar 5, 2012 · N596HA · Boeing 767332 · Navigation System Wiring
  > ETOPS SIGNIFICANT SYS - F/O RADIO ALTIMETER IS INMT ON ADI. CONDITION NORM WITH ALTERNATE EFI SELECTED. PERFORMED BITE OF RT RADIO ALTIMETER. NO FAULTS INDICATED. INSPECTED ANTENNA CONNECTOR FOUND RECEIVE ANTENNA CONNECTOR LOOSE, CLEARED AND RESEATED CONN
- [SDR HALA2012022900093](https://openairdocs.org/sdr/HALA2012022900093.md): Engine · hung start · Feb 29, 2012 · N596HA · Boeing 767332 · Engine (Turbine/Turboprop)
  > LEFT ENGINE HUNG START, FUEL FLOW AND DUCT PRESSURE WERE NORMAL. HUNG AT 56 PERCENT N2 AND EGT 710 DEGREES WHEN START ABORTED. SECOND START NORMAL. GROUND START 1 & 2, NO DEFECTS NOTED ON NR 1 ENGINE.
- [SDR HALA2012022700085](https://openairdocs.org/sdr/HALA2012022700085.md): Connector · dirty · Feb 27, 2012 · N596HA · Boeing 767332 · Pneumatic System Wiring
  > ETOPS SIGNIFICANT SYS - ON INITIAL CLIMB EICAS MESSAGE, RT ENG HIGH STAGE, DISPLAYED RT HI STAGE LIGHT ILLUMINATED, QRH PROCEDURES C/W, LIGHT EXTINGUISHED. CONDUCTED AIR SUPPLY BITE PROCEDURE IAW FIM 36-20-00 FAULTED FAMV. TROUBLESHOT FAN AIR MODULATING VAL
- [SDR HALA2012022400073](https://openairdocs.org/sdr/HALA2012022400073.md): Control System · malfunctioned · Feb 24, 2012 · N596HA · Boeing 767332 · Leading Edge Slat Control System
  > FLAP /SLAT, ELEVATOR EICAS MESSAGE, UNABLE TO LOWER FLAPS. PERFORMED FSEU, FSPM BITE, NO FAULTS NOTED. CYCLED POWER FROM ENGINE TO APU, FLAP/SLAT ELEVATOR EICAS MESSAGE CLEARED. CYCLED FLAPS SEVERAL TIMES, NO FAULTS NOTED. ACFT OK FOR SERVICE.
- [SDR HALA2012011800043](https://openairdocs.org/sdr/HALA2012011800043.md): Irs · split · Jan 18, 2012 · N596HA · Boeing 767332 · Flight Management Computing Hardware System
  > ETOPS SIGNIFICANT SYS- FMC MESSAGE SPLIT IRS OPERATION LT IRS 034/0.5, CENTER IRS. RT IRS 350/0.6. REMOVED POWER FROM ACFT RE-ESTABLISHED POWER AND ALIGNED TRU'S IAW SUB TASK 34-45-00, 745-075-003 AMM, NO SPLIT NOTED, OPS CHECKED OK.
- [SDR HALA2011122100604](https://openairdocs.org/sdr/HALA2011122100604.md): Control Unit · out of rig · Dec 21, 2011 · N596HA · Boeing 767332 · Trailing Edge Flap Control System
  > CALLED FOR FLAPS 20 AT APPROX 8-10' OF FLAP GOT FLAP DISAGREE, T/E LIGHT AND T/E FLAP SHUTDOWN. STATUS MESSAGE. FOLLOWED QRH AND EXTENDED FLAPS TO 20' WITH ALTERNATE METHOD. BITE FSEU IAW FIM 27-51-00, FIG 104. FOUND FAULT M548 MISRIGGED. REPLACED M548 IAW
- [SDR HALA2011120700577](https://openairdocs.org/sdr/HALA2011120700577.md): Relay · failed · Dec 7, 2011 · N596HA · Boeing 767332 · Trailing Edge Flap Control System
  > EICAS MESSAGE T/E FLAP DISAGREE DISPLAYED, T/E LIGHT ILLUMINATED WHEN ANY T/E FLAP POSITION WAS SELECTED. FLAPS FAILED TO MOVE TO SELECTED POSITION. DECLARED AN EMERGENCY AND LANDED SAFELY. PERFORMED FIM27-51-00-1, BLOCK 26, FIG 105, SHEET 3. R & R RELAY
- [SDR HALA2011120400565](https://openairdocs.org/sdr/HALA2011120400565.md): Warning Message · multiple fail · Dec 4, 2011 · N596HA · Boeing 767332 · Central Warning
  > FLAP ASSY MESSAGE ON GROUND. ON GEAR RETRACTION, RECEIVED A GEAR UN-SAFE LIGHT. OPEN.
- [SDR HALA2011112800544](https://openairdocs.org/sdr/HALA2011112800544.md): Control Unit · malfunctioned · Nov 28, 2011 · N596HA · Boeing 767332 · Trailing Edge Flap Control System
  > FLAPS WOULD NOT EXTEND BEYOND 15DEG ACCOMPANIED BY T/E FLAP ASSYMETRY ANNOUNCIATION. USED ALTERNATE FLAPS TO EXTEND TO 30 DEG, NORMAL LANDING. ACFT ARRIVED WITH NO ASSYM MSG. HOWEVER T/E FLAP SHUTDOWN MESSAGE ON EICAS, ACCMO FIM 27-58-00/101 FIG 104 AND AMM
- [SDR HALA2011114000518](https://openairdocs.org/sdr/HALA2011114000518.md): Bulb · missing · Nov 14, 2011 · N596HA · Boeing 767332 · Emergency Lighting
  > ON OVERNIGHT CHECK, FOUND SEAT 1H FWD AISLE EMERGENCY LIGHT MISSING LENS & BULBS AND SEAT 2H BOTH AISLE EMERGENCY LIGHTS INOPERATIVE. REPLACED LENS AND BULBS. OPS CHECKED OK IAW AMM 33-51-00.
- [SDR HALA2011114000517](https://openairdocs.org/sdr/HALA2011114000517.md): Blade · damaged · Nov 14, 2011 · N596HA · Boeing 767332 · Turbine Engine Compressor Section
  > ETOPS SIGNIFICANT SYS - ON OVERNIGHT CHECK, FOUND NR 2 ENGINE, NR 33 BLADE FR. INDEX ON SPINNER HAS FOD DAMAGE. ACCOMPLISHED AMM 72-31-02, NR 2 ENGINE NR 33 BLADE FROM INDEX ON SPINNER.
- [SDR HALA2011111100516](https://openairdocs.org/sdr/HALA2011111100516.md): Blade · damaged · Nov 11, 2011 · N596HA · Boeing 767332 · Turbine Engine Compressor Section
  > ETOPS SIGNIFICANT SYS - FOUND.2500 X.2500 BLADE DAMAGE ON NR 2 ENGINE FAN. IAW AMM 72-31-02-801 WITHIN LIMITS AREA B, 4" BELOW BLADE SHROUD. BLENDED IAW AMM 72-31-02-801. OK FOR SERVICE.
- [SDR HALA2011111000511](https://openairdocs.org/sdr/HALA2011111000511.md): Flap System · malfunctioned · Nov 10, 2011 · N596HA · Boeing 767332 · Trailing Edge Flap Control System
  > ON APPROACH, SELECTED FLAPS 15 DEGREE, GOT EICAS FLAP DISAGREE MSG HANDLE IN DETENT AND FLAP GAUGE SHOWED APPROX 10 DEGREE. FOLLOWED PROCEDURE AND LANDED WITHOUT INCIDENT, ON FINAL ALL ALERTS OFF AND SEL FLAP 25 DEGREE, FLAPS MOVED TO 25 DEGREE NORMALLY. TRO
- [SDR HALA2011102800497](https://openairdocs.org/sdr/HALA2011102800497.md): Fmc · unknown · Oct 28, 2011 · N596HA · Boeing 767332 · Flight Management Computing Hardware System
  > ETOPS SIGNIFICANT SYS - FMC BOTH WHILE IN ATC MODE ON ATC INDEX PAGE PRINTING IS ILLUMINATED ON ATC LOG PAGE. ALL INFO UPLINK WILL NOT PRINT, L6 INDICATES PRINT BUSY. CANNOT DUPLICATE ATC LOGGED IN CONDITION ON GROUND. FMC CHECKED GOOD IAW AMM 34-61-00-735-
- [SDR HALA2011102400486](https://openairdocs.org/sdr/HALA2011102400486.md): Oil System · low · Oct 24, 2011 · N596HA · Boeing 767332 · APU Oil System
  > ETOPS SIGNIFICANT SYS - AT GATE APU AUTO SHUTDOWN. BITE CHECKED ECU FOUND LOW OIL PRESSURE FAULT, SERVICED APU WITH 2.5 QTS, RAN APU NO LEAKS NOTED, OK FOR SVC.
- [SDR HALA2011101400461](https://openairdocs.org/sdr/HALA2011101400461.md): Engine · hung start · Oct 14, 2011 · N596HA · Boeing 7673G5 · Engine (Turbine/Turboprop)
  > ETOPS SIGNIFICANT SYS - LT ENGINE HUNG START AT EGT 739 DEG; N2 53 PERCENT; FUEL FLOW 1500; OAT 14DEG C. ABORTED START, RESTARTED SUCCESSFUL. ACCOMPLISHED LT ENG START & IDLE RUN TEST 3 IAW AMM 71-00-00, ALL LT ENG PARAMETERS WITHIN LIMITS IAW AMM 71-00-00-8
- [SDR HALA2011091500403](https://openairdocs.org/sdr/HALA2011091500403.md): Indicator · malfunctioned · Sep 15, 2011 · N596HA · Boeing 767332 · Attitude Gyro and Indicating System
  > ETOPS SIGNIFICANT SYS - ATTITUDE INDICATION OF STANDBY ALTITUDE INDICATOR IS ABNORMAL IN PITCH & ROLL. GYRO FLAG RETRACTED. REPLACED STANDBY ATTITUDE INDICATOR - CHECKS OK IAW AMM 34-24-01.
- [SDR HALA2011081600368](https://openairdocs.org/sdr/HALA2011081600368.md): Circuit Card · malfunctioned · Aug 16, 2011 · N596HA · Boeing 767332 · Hydraulic System, Main
  > ETOPS SIGNIFICANT SYS - C DEMAND PUMP EICAS "ON" WITH CTR AIR DEMAND PUMP "PRESS" LIGHT "ON" INTERMITTENTLY FROM INITIAL DESCENT TO LANDING. T/S IAW FIM 29-11-00-1, FIG 10. REPLACED SPEED CARD (P50) ALSO SUSPECT SPOILER ISSUE REF L/P 358540 ITM 30. OPS CK C
- [SDR HALA2011072300335](https://openairdocs.org/sdr/HALA2011072300335.md): Totalizer · inaccurate · Jul 23, 2011 · N596HA · Boeing 767332 · Fuel Quantity Indicator
  > ETOPS SIGNIFICANT SYS - CALC & TOTALIZER HAS A 2,300 LB DIFF IAW FIM 28-41-00, FIG 107 TOTAL FUEL & FMC CAL FUEL CHECKED OK.
- [SDR HALA2011070600315](https://openairdocs.org/sdr/HALA2011070600315.md): Processing Unit · faulted · Jul 6, 2011 · N596HA · Boeing 767332 · Fuel Indicating System
  > ETOPS SIGNIFICANT SYS - INTERMITTENT FUEL QTY BITE EICAS MESSAGE. BITE CHECKED FUEL QTY PROCESSOR UNIT. FOUND "D2" FAULT. PERFORMED RESET VERIFY CONFIRMED NO FAULTS MESSAGE. OK FOR SVC.
- [SDR HALA2011070200303](https://openairdocs.org/sdr/HALA2011070200303.md): Overheat Loop · malfunctioned · Jul 2, 2011 · N596HA · Boeing 767332 · Overheat Detection
  > ETOPS SIGNIFICANT SYS - STATUS EICAS WARNING ON DESCENT. "R ENG OH LP 2". REPLACED DAMAGED RT ENGINE OVERHEAT LOOP DETECTOR AND OPS CHECK OK IAW MM 26-11-02.
- [SDR HALA2011062500291](https://openairdocs.org/sdr/HALA2011062500291.md): Circuit Card · malfunctioned · Jun 25, 2011 · N596HA · Boeing 767332 · Overheat Detection
  > ETOPS SIGNIFICANT SYS - EICAS STATUS MSG: RT ENG OH LP2 DISPLAYED. ACCOMPLISHED FIM DAL D633T605 AND WDM 26-11-22. REPLACED RT ENG LP2 OVERHEAT DETECTION CARD (M690). ENG GROUND RUN CHECKED OK.
- [SDR HALA2011061800269](https://openairdocs.org/sdr/HALA2011061800269.md): Computer · unknown · Jun 18, 2011 · N596HA · Boeing 767332 · Flight Management Computing Hardware System
  > TCAS COMPUTER FAILURE NR 1 & NR 2 TRANSPONDER DATA BUSS FAILURE. 1 & 2 PROCESSER FAILURE RA DISPLAY NR2 RADIO ALT NR1. RECYCLED TCAS C/B. GROUND CHECK OK.
- [SDR HALA2011051700207](https://openairdocs.org/sdr/HALA2011051700207.md): Line · loose · May 17, 2011 · N596HA · Boeing 767332 · Pneumatic Distribution System
  > ETOPS SIGNIFICANT SYS - ON DESCENT WITH POWER IDLE LEFT ENGINE BLEED VALVE LIGHT ON. TROUBLESHOT IAW FIM 36-10-00, FIG 111. FOUND & SECURED LOOSE SENSE LINE AT HPSOV. PERFORMED HIGH PWR ENG RUN NO PROBLEMS NOTED. OK FOR SERVICE.
- [SDR HALA2011041900163](https://openairdocs.org/sdr/HALA2011041900163.md): A/C Pack · malfunctioned · Apr 19, 2011 · N596HA · Boeing 767332 · Cabin Cooling System
  > ETOPS SIGNIFICANT SYS - RT PACK INOP LIGHT ILLUM, EICAS MESSAGE RT PACK TEMP DISPLAYED NORMAL AFT STBY SELECTED. T/S IAW FIM 21-51-00/101, FIG 103. DID PACK TEMP CONTROLLER BITE CHECK. NO FAULTS. RAN PACKS FOR APPROX 30 MINS. PACK OPEN AND TEMP NORMAL. R

Next page: https://openairdocs.org/deregistered/N596HA-2014-03-11/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 = 'N596HA' AND deregistration_id = 'N596HA-2014-03-11'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N596HA-2014-03-11/reports

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