# Service difficulty reports: N584HA, cancelled Dec 17, 2013

A list on [N584HA, cancelled Dec 17, 2013](https://openairdocs.org/deregistered/N584HA-2013-12-17.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 5 · 215 reports

- [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 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 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 HALA2012070200166](https://openairdocs.org/sdr/HALA2012070200166.md): Starter · seized · Jul 2, 2012 · N584HA · Boeing 7673CB · Engine Starter
  > NR 2 ENGINE WOULD NOT START, NO N1 OR OIL PRESSURE NOTED. PNEU PRESSURE WAS NORMAL & START VALVE OPENED AND CLOSE NORMAL. FOUND NR 2 ENGINE STARTER SEIZED. R & R NR 2 ENGINE STARTER IAW AMM 80-11-01. NR 2 ENGINE START, OPS GOOD. ALL ENGINE INDICATIONS NORM
- [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 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 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 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 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 HALA2012011900045](https://openairdocs.org/sdr/HALA2012011900045.md): Engine · malfunctioned · Jan 19, 2012 · N584HA · Boeing 7673G5 · Engine (Turbine/Turboprop)
  > ETOPS SIGNIFICANT SYSTEM - LEFT ENGINE STARTED NORMALLY TILL 50 PERCENT, THEN REMAINED AT 50 PERCENT FOR 50 SECOUNDS BEFORE SLOWLY ACCELERATING - TOTAL TIME FROM FUEL ON TILL ENGINE STABLE TOOK 110 SECONDS, PEAK TEMP EGT WAS 397. TROUBLESHOT IAW FIM 73-21-00/
- [SDR HALA2012011700041](https://openairdocs.org/sdr/HALA2012011700041.md): Generator · malfunctioned · Jan 17, 2012 · N584HA · Boeing 7673G5 · AC Generator-Alternator
  > ETOPS SIGNIFICANT SYS - GENERATOR FIELD MANUAL RESET (RT) FIELD OFF LIGHT ON. BITE CHECKED BPCU AND NO FAULTS NOTED. RAN NR 2 ENGINE RESET NR 2 GENERATOR. OPS CHECKED OK IAW 24-20-00, OK FOR SERVICE.
- [SDR HALA2012011600035](https://openairdocs.org/sdr/HALA2012011600035.md): Display · malfunctioned · Jan 16, 2012 · N584HA · Boeing 7673G5 · Independent Position Determining System
  > ETOPS SIGNIFICANT SYS - F/O RADAR SCREEN FLICKERS IN WX MODE. REPLACED F/O EMSI DISPLAY. OPS CHECKED OK IAW MM 34-22-00. PERFORMED MCDP TEST 30 TEST PASSED.
- [SDR HALA2012011500036](https://openairdocs.org/sdr/HALA2012011500036.md): Transceiver · failed · Jan 15, 2012 · N584HA · Boeing 7673G5 · Ground Proximity System
  > ETOPS SIGNIFICANT SYS - AMBER RADAR ALITMETER WARNING BOX ILLUMINATED ON FO ADI " NO LAND 3" APPEARS IN AUTOLAND STATUS. REPLACED RT RADIO ALTIMETER TRANSCEIVER, NOW OPS NORMAL IAW MM 34-33-01. OK FOR SERVICE.
- [SDR HALA2012011300024](https://openairdocs.org/sdr/HALA2012011300024.md): Warning Light · illuminated · Jan 13, 2012 · N584HA · Boeing 7673G5 · DC Generating System
  > ETOPS SIGNIFICANT SYS - ON POST FLIGHT FOUND ENGINE NR 2 GENERATOR FIELD OFF LIGHT ILLUMINATED. ACCOMPLISHED BPCU BITE CHECK IAW AMM 24-22-00-745-071. RERACKED GCU. RESET RT GENERATOR FIELD LIGHT. RT ENGINE GROUND RUN-UP OK. SYS VOLTAGE AND FREQUENCY NORMA
- [SDR HALA2012011100018](https://openairdocs.org/sdr/HALA2012011100018.md): Gcu · failed · Jan 11, 2012 · N584HA · Boeing 7673G5 · AC Generation System
  > ETOPS SIGNIFICANT SYS - FOUND RT GENERATOR FIELD LIGHT ILLUMINATED ON P61. SERVICED IDG RESET FIELD LIGHT IAW AMM 24-22-00. PERFORMED IDLE ENGINE RUN. FAULT DID NOT RETURN. DUE TO HISTORY, REPLACED RT GCU IAW AMM 24-22-02. TESTED OK IAW AMM. OK FOR SERVICE.
- [SDR HALA2012010100002](https://openairdocs.org/sdr/HALA2012010100002.md): Warning Light · illuminated · Jan 1, 2012 · N584HA · Boeing 7673G5 · Attitude and Direction Data System
  > ETOPS SIGNIFICANT SYS - EICAS MESSAGE TRACK FAIL ILLUMINATED AFTER TAKEOFF. PERFORMED TROUBLESHOOTING, PLACED IECAS COMPUTER SELECTED SWITCH TO ALTERNATE POSITION, OPENED AND RESET CIRCUIT BREAKER TO EICAS COMPUTER. ALL CHECKED GOOD.
- [SDR HALA2011122600618](https://openairdocs.org/sdr/HALA2011122600618.md): Warning Light · false activation · Dec 26, 2011 · N584HA · Boeing 7673G5 · AC Generator-Alternator
  > ETOPS SIGNIFICANT SYS - AFTER ENGINE SHUTDOWN, NOTE GENERATOR FIELD TRIP ON RT ENG. ACCOMPLISHED FIM 24-20-00. NO FAULTS NOTED. RESET RT GEN FIELD SWITCH. GROUND RUN CHECK OK IAW AMM 24-11-00. OK FOR SERVICE.
- [SDR HALA2011122500611](https://openairdocs.org/sdr/HALA2011122500611.md): Warning Light · false activation · Dec 25, 2011 · N584HA · Boeing 7673G5 · AC Generator-Alternator
  > ETOPS SIGNIFICANT SYS - AUX PANEL HAS GENERATOR FIELD OFF INDICATOR ON AFTER LANDING. PERFORMED BPCU BITE ON NR 2 BPCE IAW FIM 24-20-00, FIG 101. INSPECTED WIRING, NO DEFECTS NOTED. RESET FIELD OFF LIGHT, OPS NORMAL ON ENG RUN UP.
- [SDR HALA2011122200606](https://openairdocs.org/sdr/HALA2011122200606.md): Sensor · out of position · Dec 22, 2011 · N584HA · Boeing 7673G5 · Door Warning System
  > ON TAXI OUT LT FWD ENTRY DOOR, EICAS AND ENTRY DOORS WARNING LIGHT ILLUMINATED. UPON BEING TUGGED IN LIGHT WENT OUT BY ITSELF. FOUND LT FWD ENTRY DOOR OPEN SENSOR BINDING. REPOSITIONED SENSOR. SECURITY CHECK AND OPS CHECK OK. OK FOR SERVICE.
- [SDR HALA2011120200596](https://openairdocs.org/sdr/HALA2011120200596.md): Support Channel · corroded · Dec 2, 2011 · N584HA · Boeing 7673G5 · Fuselage Internal Mounting Structure
  > INTERNAL SUPPORT CHANNEL CORRODED, BS 1425 AT DRAIN MAST FOR WASTE WATER. FITTED NEW SKIN STIFFENER IAW SRM 53-00-03.
- [SDR HALA2011120200581](https://openairdocs.org/sdr/HALA2011120200581.md): Floor Support · cracked · Dec 2, 2011 · N584HA · Boeing 7673G5 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT CRACKED 1 INCH, BETWEEN BS 742 AND 764 AT RBL 40. REPLACED FLOOR SUPPORT IAW SRM 51-40-02, D634T210, REV 87.
- [SDR HALA2011120100584](https://openairdocs.org/sdr/HALA2011120100584.md): Floorbeam · corroded · Dec 1, 2011 · N584HA · Boeing 7673G5 · Fuselage Main, Floor Beam
  > AFT CARGO HOLD, FLOOR STRUCTURE, UPPER HORIZONTAL FLANGE A FRAME STA 1197+66, HAS CORROSION OUTSIDE SRM LIMITS AND NUMEROUS CORRODED ANCHOR NUTS. INNER CHORD PN 146T1060-2, REPLACED IAW SRM 51-40-02, REV 87, CORRODED ANCHOR NUTS REPLACED IAW SRM 51-40-02, REV
- [SDR HALA2011113000583](https://openairdocs.org/sdr/HALA2011113000583.md): Floorbeam · corroded · Nov 30, 2011 · N584HA · Boeing 7673G5 · Fuselage Main, Floor Beam
  > NET CARGO FLOOR STRUCTURE, UPPER HORIZONTAL FLANGE AT BS 1175, HAS CORROSION AS MARKED. REPLACED IAW SRM 51-40-02, REV 87.
- [SDR ANZY20111120102](https://openairdocs.org/sdr/ANZY20111120102.md): Stringer · corroded · Nov 30, 2011 · N584HA · Boeing 7673G5 · Fuselage Main, Longeron/Stringer
  > ON C CHECK, CORROSION OF STRINGER AT S34R HAD CAUSED MULTIPLE HOLES IN EXTRUSION TO THE POINT THAT NO STRUTURAL MATERIAL WAS LEFT. REPAIR UNDER WAY AT THIS TIME.
- [SDR HALA2011112900597](https://openairdocs.org/sdr/HALA2011112900597.md): Mechanism · corroded · Nov 29, 2011 · N584HA · Boeing 7673G5 · Landing Gear Door Retract Section
  > NLG FWD DOOR OPERATING MECHANISM FOUND CORRODED BS 180.5. REPLACED NLG FWD DOOR OPERATING MECHANISM ON LT SIDE IAW AMM 32-22-04, REV 77.
- [SDR HALA2011112900580](https://openairdocs.org/sdr/HALA2011112900580.md): Stringer Clip · cracked · Nov 29, 2011 · N584HA · Boeing 7673G5 · Fuselage Main, Attach Fittings
  > CRACK IN STRINGER CLIP AT STA. 1678, S3R, 1". REPLACED STRINGER CLIP IAW SRM 51-40-02.
- [SDR HALA2011112800602](https://openairdocs.org/sdr/HALA2011112800602.md): Seat Track · corroded · Nov 28, 2011 · N584HA · Boeing 7673G5 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK FOUND CORRODED AT RBL 88.5 AT STA 605. REPLACED SEAT TRACK IAW SRM 53-00-52, REV 87.
- [SDR HALA2011112800600](https://openairdocs.org/sdr/HALA2011112800600.md): Seat Track · corroded · Nov 28, 2011 · N584HA · Boeing 7673G5 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK FOUND CORRODED AT RBL 88.5 AT STA 594. REPLACED SEAT TRACK IAW SRM 53-00-52, REV 87.
- [SDR HALA2011112800601](https://openairdocs.org/sdr/HALA2011112800601.md): Seat Track · corroded · Nov 28, 2011 · N584HA · Boeing 7673G5 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK FOUND CORRODED AT RBL 88.5 AT STA 594. REPLACED SEAT TRACK IAW SRM 53-00-52, REV 87.
- [SDR HALA2011128000600](https://openairdocs.org/sdr/HALA2011128000600.md): Seat Track · corroded · Nov 28, 2011 · N584HA · Boeing 7673G5 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK FOUND CORRODED AT RBL 88.5 AT STA 575. REPLACED SEAT TRACK IAW SRM 53-00-52, REV 87.
- [SDR HALA2011112800599](https://openairdocs.org/sdr/HALA2011112800599.md): Seat Track · corroded · Nov 28, 2011 · N584HA · Boeing 7673G5 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK FOUND CORRODED AT RBL 88.5, AT STA. 565. REPLACED SEAT TRACK IAW SRM 53-00-52, REV 87.
- [SDR HALA2011112800598](https://openairdocs.org/sdr/HALA2011112800598.md): Seat Track · corroded · Nov 28, 2011 · N584HA · Boeing 7673G5 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK FOUND CORRODED AT RBL 88.5 AT BS 544. REPLACED SEAT TRACK IAW 53-00-52-REV 87.
- [SDR HALA2011112800592](https://openairdocs.org/sdr/HALA2011112800592.md): Wedge · debonded · Nov 28, 2011 · N584HA · Boeing 7673G5 · Leading Edge Devices
  > NR 8 SLAT OTBD END HAS A T/E WEDGE AREA OF DISBOND. REPAIRED IAW SRM 57-43-02-2R-1, REV 87 AND 51-70-10, REV 87.
- [SDR HALA2011112800591](https://openairdocs.org/sdr/HALA2011112800591.md): Skin · damaged · Nov 28, 2011 · N584HA · Boeing 7673G5 · Fuselage Main, Plate/Skin
  > LIGHTING STRIKE NEAR RIVET HEAD AT BS 395, 1 INCH BELOW S33L. DAMAGE REMOVED IAW SRM 53-00-01-2R-8 REV 88. FASTENER REPLACED IAW SRM 51-40-02, REV 88.
- [SDR HALA2011112800582](https://openairdocs.org/sdr/HALA2011112800582.md): Tee Fitting · corroded · Nov 28, 2011 · N584HA · Boeing 7673G5 · Fuselage Miscellaneous Structure
  > CORROSION ON TEE FITTING BETWEEN STA 808 & 933, BETWEEN RBL 10 & LBL 10. REPLACED TEE FITTING IAW SRM 51-40-02.
- [SDR HALA2011113000512](https://openairdocs.org/sdr/HALA2011113000512.md): Engine · malfunctioned · Nov 13, 2011 · N584HA · Boeing 7673G5 · Engine (Turbine/Turboprop)
  > ETOPS SIGNIFICANT SYS - LEFT ENGINE HESITATED AT 50 PERCENT N2 DURING ENGINE START AFTER START VALVE CLOSED AND STARTER CUTOUT WITH SELECTOR BACK IN AUTO. OTHER PARAMETERS NORMAL. GROUND RAN LT ENGINE, FOUND WITHIN LIMITS OF AMM 71-00-00. OK FOR SERVICE.
- [SDR HALA2011110100500](https://openairdocs.org/sdr/HALA2011110100500.md): Unknown · unknown · Nov 1, 2011 · N584HA · Boeing 7673G5 · VHF Communications System
  > ETOPS SIGNIFICANT SYS - HF DATALINK INOPERATIVE BOTH RADIOS, VOICE OK. PERFORMED A BITE TEST ON BOTH HF TRANSCEIVERS, NO FAULTS NOTED. PERFORMED A SYS TEST IAW 23-11-00-735-042, ALL CHECKED ARE GOOD.
- [SDR HALA2011102300484](https://openairdocs.org/sdr/HALA2011102300484.md): Warning System · false activation · Oct 23, 2011 · N584HA · Boeing 7673G5 · Central Warning
  > ETOPS SIGNIFICANT SYS - EICAS STATUS MESSAGE LT ENG EEC C1 DISPLAYED ON LOWER EICAS. TROUBLE SHOT IAW FIM 73-21-00. PIMU CHECKED AND HAD RNG FAIL-CLEARED MESSAGE. RAN ENGINE, NO FAULTS ON PIMU OR EICAS-OK FOR SERVICE.
- [SDR HALA2011102300483](https://openairdocs.org/sdr/HALA2011102300483.md): Fuel Sys · malfunctioned · Oct 23, 2011 · N584HA · Boeing 7673G5 · Fuel Quantity Indicator
  > ETOPS SIGNIFICANT SYS - RT FUEL QTY DECREASED 2800 WITH CENTER TANK PUMPS ON. ELAPSED TIME 42MINS. DECREASED AN ADDITIONAL 600 NR DURING THE NEXT 56 MINS. W/C. TANK PUMPS ON. TOTALIZER INDICATED 2400 MORE THAN CALCULATED INDICATION ON FMS PROG. PAGE 2. PERF
- [SDR HALA2011100900441](https://openairdocs.org/sdr/HALA2011100900441.md): Overheat Sys · malfunctioned · Oct 9, 2011 · N584HA · Boeing 7673G5 · Overheat Detection
  > ETOPS SIGNIFICANT SYS - FOUND LEFT ENGINE OVERHEAT LOOP 2 STATUS MESSAGE ON ETOPS CHECK. ACCOMPLISHED FIM 26-11-00, FIG 104. SWAPPED LT ENGINE O/H CARDS, RERACKED AND REINSTALLED IN ORIGINAL POSITION. FAULT MESSAGE CLEARED AND LT ENGINE O/H DETECTION TEST C
- [SDR HALA2011100600434](https://openairdocs.org/sdr/HALA2011100600434.md): Indicator · inoperative · Oct 6, 2011 · N584HA · Boeing 7673G5 · Altimeter, Barometric/Encoder
  > ETOPS SIGNIFICANT SYS -CAPTS ALTIMETER OFF FLAG FLICKERS CONTINUOUSLY. REPLACED CAPT ALTIMETER INDICATOR IAW AMM 34-13-01-404-004, TEST GOOD.
- [SDR HALA2011091700405](https://openairdocs.org/sdr/HALA2011091700405.md): Oil System · leaking · Sep 17, 2011 · N584HA · Boeing 7673G5 · Turbine Engine Oil System
  > ETOPS SIGNIFICANT SYS - OIL FOUND IN LT ENGINE FAN COWL. OIL LEAKAGE BELOW IDLE SPEED IS WITHIN LIMITS IAW AMM 71-00-00-795-003-N00. OK FOR SERVICE.
- [SDR HALA2011082100377](https://openairdocs.org/sdr/HALA2011082100377.md): Apu · malfunctioned · Aug 21, 2011 · N584HA · Boeing 7673G5 · Airborne Auxiliary Power Unit (APU) System
  > ETOPS SIGNIFICANT SYS - AFTER TURNING OFF THE LT PACK AT THE GATE APU AUTO SHUTDOWN NOTE: JUST BEFORE SHUTDOWN APU BLEED DUCT PRESSURE DROPPED TO APPROX 10 PSI. PERFORMED APU ECU BITE IAW FIM 49-11-00. FAULT MSG SHOWED REVERSE FLOW, RESTARTED APU AND NO DEFE
- [SDR HALA2011081900379](https://openairdocs.org/sdr/HALA2011081900379.md): Duct · damaged · Aug 19, 2011 · N584HA · Boeing 7673G5 · APU Bleed Air System
  > ETOPS SIGNIFICANT SYS - 2 FLEXIBLE DUCT SEGMENTS ON THE APU OVER PRESSURE VENT DUCT HAVE HOLES IN THEM. R & R 2 FLEXIBLE DUCT SEGMENTS ON THE APU OVERPRESSURE VENT DUCT. OPS NORMAL IAW AMM 49-00.
- [SDR HALA2011081600371](https://openairdocs.org/sdr/HALA2011081600371.md): Transmitter · malfunctioned · Aug 16, 2011 · N584HA · Boeing 7673G5 · Altimeter, Barometric/Encoder
  > ETOPS SIGNIFICANT SYS - ASA NO LAND 3 DISPLAYED CENTER RADIO ALTIMETER. RA FLAG DISPLAYED FROM T/O TO CRUISE ALT, THEN RESUMED NORMAL OPS. R & R RADIO ALTIMETER TRANSMITTER IAW 34-33-01-004-001. OPS TEST GOOD. -40 TEST REQUIRED. GROUND TEST OF AUTO LAND SY
- [SDR HALA2011081400365](https://openairdocs.org/sdr/HALA2011081400365.md): B-Nut · loose · Aug 14, 2011 · N584HA · Boeing 7673G5 · Turbine Engine Oil System
  > ETOPS SIGNIFICANT SYS - NR 1 ENG TOOK 6 PINT DURING SERVICING. TIGHTENED OIL INLET TUBE B-NUT IAW 79-21-01, LEAK CHECKED GOOD. (AT OIL COOLER) (ACFT M/M 79-21-011).
- [SDR HALA2011080400348](https://openairdocs.org/sdr/HALA2011080400348.md): Flex Line · leaking · Aug 4, 2011 · N584HA · Boeing 7673G5 · Hydraulic System, Main
  > C-HYD QTY DECREASED TO 0.58 IN FLIGHT, 0.40 ON GROUND. REPLACED NR 4 BRAKE FLEX LINE ABOVE RT MLG IAW AMM 32-42-02. REF IPC 32-41-62-05, ITEM 172. LEAK AND OPS CK GOOD. RESERVICED CTR HYD SYS.

Next page: https://openairdocs.org/deregistered/N584HA-2013-12-17/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 = 'N584HA' AND deregistration_id = 'N584HA-2013-12-17'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N584HA-2013-12-17/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.