# Service difficulty reports: N580HA, cancelled Feb 21, 2019

A list on [N580HA, cancelled Feb 21, 2019](https://openairdocs.org/deregistered/N580HA-2019-02-21.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 · 280 reports

- [SDR HALA201809140421](https://openairdocs.org/sdr/HALA201809140421.md): Indicator · malfunctioned · Sep 13, 2018 · N580HA · Boeing 76733A · Attitude Gyro and Indicating System
  > STANDBY ADI UNCAGES AUTOMATICALLY. REPLACED THE STANDBY ATTITUDE INDICATOR. GROUND OPS CHECKED OK IAW AMM 34-24-01.
- [SDR HALA2018091200419](https://openairdocs.org/sdr/HALA2018091200419.md): Indicator · false indication · Sep 12, 2018 · N580HA · Boeing 76733A · Fuel Quantity Indicator
  > POSSIBLE FUEL QTY INDICATION MALFUNCTION. FUEL CONFIGURATION EICAS MESSAGE DISPLAYED. FUEL DISAGREE PROG 2 ON FMC. AIR TURNBACK. PERFORMED FIM 28-41 FAULT TREE 847, WITH NO FAULT FOUND. INSPECTED AND CLEANED LEFT BUSS CONNECTOR, NO DEFECTS NOTED. REMOVED
- [SDR HALA2018082900406](https://openairdocs.org/sdr/HALA2018082900406.md): Processing Unit · failed · Aug 29, 2018 · N580HA · Boeing 76733A · Fuel Quantity Indicator
  > AT TOP OF CLIMB LEFT FUEL QTY AND TOTALIZER INOP. DIVERTED A/C TO OAK. ON DESCENT BECAME INTERMITTENT. REMOVED AND REPLACED FUEL QUANTITY INDICATING SYSTEM PROCESSOR UNIT PER AMM 28-41-08. PERFORMED OPERATIONAL TEST PER AMM 28-41-00 AND OPS CHECKS GOOD WITH NO
- [SDR HALA2018082600403](https://openairdocs.org/sdr/HALA2018082600403.md): Warning System · false activation · Aug 26, 2018 · N580HA · Boeing 76733A · Rudder Control System
  > AIR TURN BACK, AFTER TAKEOFF RUDDER RATIO EICAS MESSAGE DISPLAYED WITH RUDDER RATIO DISCRETE LIGHT ILLUMINATED. PERFORMED FIM TASK 27-09 FAULT TREE 814. NO FAULTS NOTED. RUDDER OPS NORMAL. OK FOR SVC.
- [SDR HALA2018073100353](https://openairdocs.org/sdr/HALA2018073100353.md): Sign · detached · Jul 30, 2018 · N580HA · Boeing 7673CB · Emergency Lighting
  > EXIT SIGN ABOVE FLIGHT DECK DOOR DETACHED. ATTACHED THE SIGN. OPS TESTED GOOD.
- [SDR HALA2018072600404](https://openairdocs.org/sdr/HALA2018072600404.md): Warning System · false activation · Jul 25, 2018 · N580HA · Boeing 76733A · Rudder Control System
  > ETOPS SIGNIFICANT SYSTEM - RUDDER RATIO ON STEADY AT 1500 FT AND 160 KTS. RESET RUDDER RATIO CIRCUIT BREAKER. PERFORMED RUDDER RATIO CHANGER MODULE BITE PROCEDURE PER FIM 27-09 FT 814 NO FAULTS NOTED OK FOR SERVICE.
- [SDR HALA2018072300335](https://openairdocs.org/sdr/HALA2018072300335.md): Solenoid · failed · Jul 22, 2018 · N580HA · Boeing 76733A · APU Core Engine
  > VERIFICATION FLIGHT FOR APU COMPLETED UNSATISFACTORILY. THREE ATTEMPTS AT FL 400 FAILED 30% RPM MAX FOLLOWED BY APU FAULT EICAS. REMOVED AND REPLACED THE DE-OIL SOLENOID VALVE IAW AMM 49-27-08-404-010. APU OPS & LEAK CHECKED GOOD. NO FAULTS.
- [SDR HALA2018052900259](https://openairdocs.org/sdr/HALA2018052900259.md): Filter · contaminated · May 27, 2018 · N580HA · Boeing 76733A · Engine Fuel Distribution
  > ETOPS SIGNIFICANT SYSTEM - OBSERVED PERIODIC SURGE OF LEFT ENGINE, ROUGHLY 30 CYCLES PER MINUTE, ALL POWER SETTINGS. EPR +/- 0.01, N1 +/- 0.2, FF +/- 100 LBS/HR, OIL PRESSURE +/- 2 PSI. CONTINUOUS. PERFORMED FIM TASK 73-21 FAULT TREE 827 FOUND CONTAMINATION IN
- [SDR HALA208042500186](https://openairdocs.org/sdr/HALA208042500186.md): Unknown · unknown · Apr 23, 2018 · N580HA · Boeing 76733A · Navigation System
  > AFTER DEPARTURE, OBSERVED THAT THE FOB AND MACH SPEED ARE NOT LINKING TO THE ACARS POS RPT PAGE. ALL FQIS AND FMC FUNCTIONS NORMAL. FMC NR 01 & 2 CHECKED OK IAW FIM 34-61-00. ACARS CHECKED OK IAW FIM 23-22-00.
- [SDR HALA2018042400183](https://openairdocs.org/sdr/HALA2018042400183.md): Engine · malfunctioned · Apr 22, 2018 · N580HA · Boeing 76733A · Engine (Turbine/Turboprop)
  > DURING CRUISE FLIGHT, THE NR 2 ENGINE FUEL FLOW 400 LBS AN HOUR HIGHER, NR 2 ENGINE EGT 25 DEGREE'S C HIGHER THAN NR 1. RAN BOTH ENGINES FOR 5 MINUTES ON GROUND IAW AMM 71-00. RIGHT ENGINE WITHIN LIMITS AT THIS TIME, NOTIFIED MOC.
- [SDR HALA2018042300180](https://openairdocs.org/sdr/HALA2018042300180.md): Warning Light · false activation · Apr 21, 2018 · N580HA · Boeing 76733A · Drag Control System
  > AIR TURNBACK DUE TO A SPOILERS CAUTION ILLUMINATED INFLIGHT. PILOT REPORTED MESSAGE CAME ON DURING DESCENT, ONCE SPOILERS WERE ARMED. PERFORMED FIM 27-09 FAULT 803. STEP 62. NO FAULTS. PERFORMED FIM 27-09 FAULT 808 SCM BITE. FOUND NO ACTIVE FAULTS. PERFORMED
- [SDR HALA2018041100166](https://openairdocs.org/sdr/HALA2018041100166.md): Warning System · false activation · Apr 10, 2018 · N580HA · Boeing 76733A · Fuel Control/Turbine Engines
  > ETOPS SIGNIFICANT SYSTEM - "L ENG EEC C1" STATUS MSG ON LANDING. ACCOMPLISHED FIM 73-21-828. FAULT CLEARED. NO OTHER FAULTS NOTED. A/C OK TO CONTINUE.
- [SDR HALA0218040900148](https://openairdocs.org/sdr/HALA0218040900148.md): Warning Message · false activation · Apr 8, 2018 · N580HA · Boeing 76733A · Fuel Controlling System
  > LEFT ENGINE EEC STATUS APPEARED DURING DESCENT, PASSING FL180. NO CURRENT FAULT DISPLAYED. TROUBLESHOT IAW FIM 71-01, FAULT TREE 803. FAULT DID NOT RETURN. OK FOR SERVICE.
- [SDR HALA0218040900147](https://openairdocs.org/sdr/HALA0218040900147.md): Warning Message · false activation · Apr 6, 2018 · N580HA · Boeing 76733A · Fuel Controlling System
  > DURING DESCENT, STATUS MESSAGE FOR THE LT ENGINE EEC NR 1 DISPLAYED. NO STATUS FOUND ON GROUND. AIRCRAFT OK FOR SERVICE.
- [SDR HALA2018032900130](https://openairdocs.org/sdr/HALA2018032900130.md): Oil System · low · Mar 28, 2018 · N580HA · Boeing 76733A · AC Generator-Alternator
  > DURING CLIMB, LEFT GENERATOR DRIVE EICAS MESSAGE, COMPLETED QRH AND GOING TO DISCONNECT DRIVE, THE MESSAGE AND LIGHT EXTINGUISHED. GENERATOR VOLTS AND FREQUENCIES NORMAL. DURING CLIMB IDG TEMP OUT 80/80, RISE 20/10, DURING CRUISE, IDG TEMP OUT 83/90, RISE
- [SDR HALA2018031600108](https://openairdocs.org/sdr/HALA2018031600108.md): Fmc · failed · Mar 15, 2018 · N580HA · Boeing 76733A · Flight Management Computing Hardware System
  > LEFT FMC FAILED IN FLT. PERFORMED FIM 34-61, FAULT TREE 857. NO FAULTS AT THIS TIME. AS A PRECAUTION, REMOVED AND REPLACED THE LEFT FMC IAW AMM 34-61-01. ALL APPLICABLE CROSS LOADS COMPLIED WITH. OK FOR SERVICE. AIRCRAFT DIVERTED TO THE CLOSEST AIRPORT, W
- [SDR HALA2018031200090](https://openairdocs.org/sdr/HALA2018031200090.md): Pump · inoperative · Mar 9, 2018 · N580HA · Boeing 76733A · Fuel Boost Pump
  > RT FWD FUEL PUMP INOPERATIVE. RESET GFI CONTROL RELAY K10704. VERIFIED POWER OK AT RT FWD FUEL BOOST PUMP. REMOVED AND REPLACED THE RT FWD FUEL PUMP IAW AMM 28-22-03. OPS & LEAK CHECKED GOOD. OK FOR SERVICE.
- [SDR HALA2018022600049](https://openairdocs.org/sdr/HALA2018022600049.md): Module · malfunctioned · Feb 23, 2018 · N580HA · Boeing 76733A · Rudder Control System
  > DURING CLIMB OUT, HAD A RUDDER RATIO EICAS MESSAGE WITH ASSOCIATED DISCRETE LIGHT ILLUMINATED. HYDRAULIC SYSTEM PRESSURE ALL NORMAL. DIVERTED, PERFORMED A BITE TEST OF RUDDER RATIO CHANGER MODULE IAW FIM 27-09 814. NO FAULTS NOTED. OK FOR SERVICE.
- [SDR HALA2018012300007](https://openairdocs.org/sdr/HALA2018012300007.md): Warning System · false activation · Jan 20, 2018 · N580HA · Boeing 76733A · Hydraulic Pressure Indicator
  > ETOPS SIGNIFICANT SYSTEM - C HYD PRIM 1 EICAS AND PRESS LIGHT ILLUMINATED. OPERATIONAL CHECK OF CENTER HYD (ELECTRIC) PUMPS PER AMM 29-11-00. OPS CHK OK. PERFORMED PILOT ENGINE RUN OF 1 & 2 ENG. CYCLED ALL (4) ELEC PUMPS OFF THEN ON. COULD NOT RECREATE. OK FOR
- [SDR HALA2017122600316](https://openairdocs.org/sdr/HALA2017122600316.md): Acm · failed · Dec 25, 2017 · N580HA · Boeing 76733A · Cabin Cooling System
  > DURING DESCENT, A STRONG ODOR WAS PRESNT IN THE COCKPIT AND CABIN. DURING TAXI IN, THE LT PACK TEMP EICAS ILLUMINATED. ACCOMPLISHED QRH, LEFT PACK RESET. REMOVED AND REPLACED THE ACM IAW AMM 21-51-03/401. OPS CHECKED OK.
- [SDR HALA2017120700291](https://openairdocs.org/sdr/HALA2017120700291.md): Actuator · malfunctioned · Dec 7, 2017 · N580HA · Boeing 76733A · Aileron Tab Control System
  > ETOPS / AILERON LOCKOUT AT 240 KIAS FROM 10,000 THROUGH ROLL OUT WITH ASSYMETERICAL AILERON DISPLACEMENT. REMOVED AND REPLACE L/H AILERON LOCKOUT ACTUATOR.
- [SDR HALA2017102500262](https://openairdocs.org/sdr/HALA2017102500262.md): Unknown · malfunctioned · Oct 24, 2017 · N580HA · Boeing 76733A · Passenger/Crew Doors
  > DURING CLIMB OUT F/A REPORTED 2R DOOR BECAME HOT TO THE TOUGH AND HAD A SMELL OF ELECTRICAL MOTOR OVERHEATING. INSPECTED 2R DOOR AND PERFORMED OPERATIONAL TEST PER AMM 52-11-00. NO FAULTS FOUND AT THIS TIME. A/C OK FOR SERVICE.
- [SDR HALA2017102000256](https://openairdocs.org/sdr/HALA2017102000256.md): Transmitter · malfunctioned · Oct 19, 2017 · N580HA · Boeing 767300 · Hydraulic Pressure Indicator
  > LEFT HYDRAULIC QTY LIGHT ILLUMINATED. LEFT SYSTEM EICAS ILLUMINATED. HYD QTY INDICATED.5 RF. COMPLIED W/ QRH DEPRESSURIZED SYSTEM. HYD QTY INDICATES.92. COMPLIED WITH QRH HYD SYST PRESSURE, PRESSURIZE AND LT HYD SYSTEM DURING LANDING AND QTY AND PRESSURE HE
- [SDR HALA2017101700253](https://openairdocs.org/sdr/HALA2017101700253.md): Warning Message · false activation · Oct 17, 2017 · N580HA · Boeing 76733A · Rudder Control System
  > RUDDER RATIO EICAS AND OVERHEAD DISCRETE ANNUNCIATOR ILLUMINATED DURING TAKE OFF. NO OTHER INDICATIONS NOTED. PERFORMED A BITE IAW FIM 27-09/814, NO FAULTS NOTED, OK FOR CONTINUED SERVICE.
- [SDR HALA2017101700252](https://openairdocs.org/sdr/HALA2017101700252.md): Warning Message · illuminated · Oct 17, 2017 · N580HA · Boeing 76733A · Aileron Control System
  > AILERON LOCKOUT EICAS AND OVERHEAD DISCRETE ILLUMINATED ON APP. WITH FLAPS 15, AND SLOWING THRU 180KTS. WARNINGS WENT OUT WITH LANDING GEAR DOWN, FLAPS 25. PERFORMED A BITE IAW FIM 27-11/804, TESTED OK, NO FAULTS. OK FOR CONTINUED SERVICE.
- [SDR HALA2017082100231](https://openairdocs.org/sdr/HALA2017082100231.md): Unknown · odor · Aug 19, 2017 · N580HA · Boeing 76733A · Air Distribution System
  > DURING CLIMB, MID CABIN REPORTED SMOKE AND ODOR IN CABIN. FURTHER INVESTIGATION BY A COCKPIT CREW MEMBER, INDICATED A BURNING RUBBER ODOR. BOTH ODOR AND SMOKE DISSIPATED AND DID NOT RETURN. PERFORMED AMM 21-00-21-102-030, NO CONTAMINATION OR DEFECTS NOTED
- [SDR HALA2017081600224](https://openairdocs.org/sdr/HALA2017081600224.md): Ecu · unknown · Aug 15, 2017 · N580HA · Boeing 76733A · APU Controls
  > APU FAILED, ATTEMPTED 1 RESTART, SUSPECT BFS ECU APU BITE FAULTED ECU 20 PLUS MINI FAGS. REMOVED AND REPLACED APU ECU IAW AMM 49-61-05, OPS CHECKED GOOD.
- [SDR HALA2017071700190](https://openairdocs.org/sdr/HALA2017071700190.md): Skin · damaged · Jul 15, 2017 · N580HA · Boeing 76733A · Fuselage Main, Plate/Skin
  > DAMAGE TO AIRCRAFT SKIN OBSERVED AFT OF AFT CARGO DOOR.. DAMAGE IS 1.5 INCH LONG, 1 INCH WIDE. LOCATION ALONG BS 1360, BETWEEN STRINGERS 23 - 24R. REPAIRED IAW EO.
- [SDR HALA2017071200185](https://openairdocs.org/sdr/HALA2017071200185.md): Indicator · reads low · Jul 12, 2017 · N580HA · Boeing 76733A · Cabin Pressure Control System
  > AT LEVEL FLT 16,000 PRESSURE RATE. WAS SHOWING 1,000 DOWN. PERFORMED AMM 21-31-00-705-001. NO FAULTS NOTED. ALL TEST PASSED. OK FOR SERVICE.
- [SDR HALA2017070300171](https://openairdocs.org/sdr/HALA2017070300171.md): Fmc · reads high · Jul 1, 2017 · N580HA · Boeing 76733A · Flight Management Computing Hardware System
  > AT TOP O0F DESCENT, THE FIRST OFFICER`S VERTICAL PATH INDICATOR REACH 10,000 FEET HIGH, CAPTAIN`S SIDE OPERATES NORMAL. BELOW 10,000 FT F/O SIDE OPERATE NORMAL. PERFORMED FIM 34-16 FAULT TREE 851, REMOVED AND REPLACED THE RT FMC IAW AMM 34-61-01-424-005. OK
- [SDR HALA2017062600170](https://openairdocs.org/sdr/HALA2017062600170.md): Acm · seized · Jun 26, 2017 · N580HA · Boeing 76733A · Cabin Cooling System
  > L PACK TEMP, CABIN SMOKE + FUME. LT PACK INOP (AIR CONDITIONING PACKS). FOUND LEFT ACM SEIZED. TROUBLESHOT PER FIM 21-51-804, TEST PASSED. NO FAULTS NOTED. RAN BOTH ENG AND RT PACK, NO DEFECTS NOTED. INSPECTED LEFT PACK COMPARTMENT. NO DEFECTS NOTED. NO INDICA
- [SDR HALA2017042100106](https://openairdocs.org/sdr/HALA2017042100106.md): Idg · malfunctioned · Apr 21, 2017 · N580HA · Boeing 76733A · AC Generator-Alternator
  > "L GEN OFF" EICAS MESSAGE OCCURRED IN FLIGHT. ATTEMPTED RESET, GEN REMAINED OFFLINE. T/S REF FIM 24-20. BITE MSG GEN FOR OPEN PHASE TRIP. FOUND T3 TO N, T1, T2 OPEN ON IDG. REMOVED IDG REF AMM 24-11-01. REPLACED GEN CONTROL UNIT, MCC REQUEST. REF AMM 24-32-02.
- [SDR HALA2017032800080](https://openairdocs.org/sdr/HALA2017032800080.md): Ecu · faulted · Mar 28, 2017 · N580HA · Boeing 76733A · APU Start/Ignition System
  > APU RAN FOR 5 MINUTES, THEN SHUT DOWN WITHOUT A FAULT, RESTARTED, RAN FOR 5 MINUTES THEN SHUT DOWN WITH A FAULT LIGHT. PREFORMED APU BITE CHECK IAW AMM 49-61-05. FOUND ECU FAULT. REMOVED AND REPLACE APU ECU IAW AMM 49-61-05. BITE TEST OK. OPS OK. OK FOR SERV
- [SDR HALA2017032800083](https://openairdocs.org/sdr/HALA2017032800083.md): Ecu · faulted · Mar 28, 2017 · N580HA · Boeing 767300 · APU Start/Ignition System
  > APU RAN FOR 5 MINUTES, THEN SHUT DOWN WITHOUT A FAULT, RESTARTED, RAN FOR 5 MINUTES THEN SHUT DOWN WITH A FAULT LIGHT. PREFORMED APU BITE CHECK IAW AMM 49-61-05. FOUND ECU FAULTED. REMOVED AND REPLACED THE APU ECU IAW AMM 49-61-05. BITE TESTED OK. OPS OK.
- [SDR HALA2017032100074](https://openairdocs.org/sdr/HALA2017032100074.md): Isolation Valve · malfunctioned · Mar 21, 2017 · N580HA · Boeing 76733A · Pneumatic Distribution System
  > AFTER ENGINE START, THE RT BLEED ISOLATION VALVE EICAS DISPLAYED AND RT ISOLATION VALVE LIGHT ON OVERHEAD, REMAINED DISPLAYED WITH RT ISOLATION SWITCH LATCHED IN OR OUT. REMOVED AND REPLACED RIGHT BLEED ISOLATION VALVE IAW AMM 36-11-04-404-013. LEAK AND OPS
- [SDR HALA2017030400047](https://openairdocs.org/sdr/HALA2017030400047.md): Pump · failed · Mar 4, 2017 · N580HA · Boeing 76733A · Fuel Boost Pump
  > RIGHT AFT FUEL PRESSURE LIGHT ILLUMINATED. REMOVED AND REPLACED THE RT BOOST PUMP IAW AMM 28-22-03. OPS CHECKED GOOD. SECURITY CHECKED OK. LEAK CHECKED OK. OK FOR SERVICE.
- [SDR HALA2017020900025](https://openairdocs.org/sdr/HALA2017020900025.md): Skin · punctured · Feb 9, 2017 · N580HA · Boeing 76733A · Elevator, Plate/Skin
  > TWO PUNCTURES FOUND ON THE LT ELEVATOR. REPAIRED IAW SRM 55-20-01-2R-1 AND SRM 51-70-17-0G-0.
- [SDR HALA2017010110014](https://openairdocs.org/sdr/HALA2017010110014.md): Power Supply · inoperative · Jan 11, 2017 · N580HA · Boeing 76733A · Emergency Lighting
  > EMERGENCY LIGHTS INOP, A/C LEFT ROW 20-31. REPLACED POWER SUPPLY W BATTERY AND FEEDER CABLE ASSY. P/N'S BPS7-3, 58822-40 POWER SUPPLIES A/C OK FOR SERVICE
- [SDR HALA2016122100558](https://openairdocs.org/sdr/HALA2016122100558.md): Apu · failed · Dec 21, 2016 · N580HA · Boeing 76733A · APU Core Engine
  > OIL LEAKING FROM APU DRAIN AS WELL AS BLACK SMOKE OUT OF THE TAIL PIPE WHILE OPERATING. TROUBLESHOT IAW FIM 49-11-00, FOUND OIL IN THE TAIL PIPE INSPECTED CHIP DETECTORS & FOUND METAL ON RT DETECTOR. R & R THE APU,OPS CKS GOOD IAW AMM 49-11-01-004-001, & 49
- [SDR HALA2016121500546](https://openairdocs.org/sdr/HALA2016121500546.md): Indication Sys · malfunctioned · Dec 15, 2016 · N580HA · Boeing 76733A · Fuel Quantity Indicator
  > AIR TURNBACK DUE TO FUEL QTY INDICATION ON STATUS PAGE, NO FUEL INDICATION ON LT SIDE AND TOTALIZER ON OVERHEAD PANEL. ATER RERACKING FQIS, LT QTY STARTED WORKING, SUMPED TANK AND NO ABNORMAL AMOUNT OF H20 COLLECTED; CHKED WIRING FROM PROCESSOR TO WING PER WDM
- [SDR HALA2016120600520](https://openairdocs.org/sdr/HALA2016120600520.md): Valve · leaking · Dec 6, 2016 · N580HA · Boeing 76733A · Landing Gear Brake System
  > RT MLG WHEEL WELL, ALTERNATE BRAKE SELECTOR VALVE LEAKING. DEPRESSURIZED HYDRAULIC SYSTEM AND TIGHTENED ALTERNATE BRAKE SELECTOR VALVE REDUCING NUT AND SAFETIED PRESSURIZED AND LEAK CHECK OK IAW AMM 29-11-00 AND AMM 32-41-047.
- [SDR HALA2016092700362](https://openairdocs.org/sdr/HALA2016092700362.md): Warning Message · false activation · Sep 27, 2016 · N580HA · Boeing 76733A · Attitude and Direction Data System
  > LT IRS FAULT EICAS MESSAGE DISPLAYED AT TOUCHDOWN. PERFORMED IRS BITE TEST IAW FIM TASK 34-21 FAULT TREE 818. NO FAULTS NOTED MESSAGE CLEARED.
- [SDR HALA2016092600360](https://openairdocs.org/sdr/HALA2016092600360.md): Warning Message · false activation · Sep 26, 2016 · N580HA · Boeing 76733A · Rudder Control System
  > RUDDER RATIO EICAS DURING CLIMB OUT. ACCOMPLISHED FIM TASK 27-21 FAULT TREE 804. NO FAULTS NOTED AT THIS TIME. OK FOR SERVICE.
- [SDR HALA2016080200341](https://openairdocs.org/sdr/HALA2016080200341.md): Warning System · activated · Sep 2, 2016 · N580HA · Boeing 76733A · Cabin Cooling System
  > ETOPS SIGNIFICANT SYS-2 HRS INTO FLT AT FL40, 0 RT PACK OFF AND RT PACK TEMP EICAS DISPLAYED INOPERATIVE AND PACK OFF LIGHTS DISPLAYED ON PACK SWITCH QRH PERFORMED. RIGHT PACK OFF & RT PACK TEMP RESET PACK AFTER 5 MIN RT PACK REMAINS IN STBY AT RT PACK TEMP E
- [SDR HALA2016082700335](https://openairdocs.org/sdr/HALA2016082700335.md): Acars · malfunctioned · Aug 27, 2016 · N580HA · Boeing 76733A · Data Transmission Auto Call
  > ACARS NO COMMS AFTER REACHING CRUISE, ATC NO COMMS DURING CRUISE UNABLE CPDLC OVERHEAD SBB FAIL LIGHT ILLUMINATED, BUT ABLE TO CALL MOC ON SBB SAT PHONE. MADE HF POSITION REPORTS. RESET ACARS MU AND SBB SYSTEM. OPS TEST GOOD ON GROUND IAW AMM 23-26-00.
- [SDR HALA2016082300333](https://openairdocs.org/sdr/HALA2016082300333.md): A/C Pack · malfunctioned · Aug 23, 2016 · N580HA · Boeing 76733A · Cabin Cooling System
  > RT PACK TEMP EICAS. PERFORMED QRH PACK SWITCH REMAINS IN STANDBY WITH NO FURTHER ACTION. PERFORMED BITE TEST RIGHT PACK TEMP CONTROLLER, NO FAULT FOUND. RESET RIGHT PACK SYSTEM AND OPERATION CHECK OF RIGHT PACK SYSTEM PER AMM21-51-00, NORMAL.
- [SDR HALA2016080900325](https://openairdocs.org/sdr/HALA2016080900325.md): Warning Message · false activation · Aug 9, 2016 · N580HA · Boeing 76733A · Rudder Control System
  > RUDDER RATIO EICAS MESSAGE. TROUBLESHOT IAW FIM 27-21 FIG 104, RUDDER RATIO OPS NORMAL. NO FAULTS ON CSUE. OK FOR SERVICE.
- [SDR HALA2016073100308](https://openairdocs.org/sdr/HALA2016073100308.md): Duct · cracked · Jul 31, 2016 · N580HA · Boeing 76733A · Pneumatic Distribution System
  > ROW 33 LEFT SIDE, PASSENGER REPORTED HOT AIR FROM FLOOR VENT. FOUND CRACKED DUCT FOR APU AIR SUPPLY & BULK CARGO HEAT AT BS 1197. REMOVED AND REPLACED THE DUCT. LEAK CHECKED OK.
- [SDR HALA2016071900287](https://openairdocs.org/sdr/HALA2016071900287.md): Warning Light · false activation · Jul 19, 2016 · N580HA · Boeing 76733A · Air Distribution System
  > DUCT LEAK WARNING ILLUMINATED. NO DUCT LEAKS FOUND. OPENED PACK DOORS AND HORIZONTAL STAB ACCESS AND APPLIED COOLING AIR. DUCT LEAK LIGHT EXTINGUISHED, OK FOR SERVICE.
- [SDR HALA2016071900282](https://openairdocs.org/sdr/HALA2016071900282.md): Shuttle Valve · unknown · Jul 19, 2016 · N580HA · Boeing 76733A · Brake Anti-Skid Section
  > ON ARRIVAL TO THE GATE, HYD QUANTITIES WERE L1.01, C0.90, R1.27. AFTER EQUALIZING ALL QUANTITIES TO L1.01, C1.01, R1.01 FLUID MIGRATED BACK TO L1.01, C0.80, R1.50. REPLACED RT ANTI SKID CONTROL MODULE SHUTTLE VALVE IAW AMM 32-42-07, A/S BITE CHECKED GOOD. H

Next page: https://openairdocs.org/deregistered/N580HA-2019-02-21/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 = 'N580HA' AND deregistration_id = 'N580HA-2019-02-21'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N580HA-2019-02-21/reports

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