# Service difficulty reports: N598HA, cancelled Feb 23, 2015

A list on [N598HA, cancelled Feb 23, 2015](https://openairdocs.org/deregistered/N598HA-2015-02-23.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 · 227 reports

- [SDR HALA2014111700193](https://openairdocs.org/sdr/HALA2014111700193.md): Overheat Loop · malfunctioned · Nov 17, 2014 · N598HA · Boeing 767332 · Overheat Detection
  > ENGINE FIRE OVERHEAT LOOP 2 FAULT. FOUND BAD O/H LOOP. REPLACED LOOP ASSY NR 2 ENGINE NR 2 SYS IAW AMM 26-11-02.
- [SDR HALA2014110600183](https://openairdocs.org/sdr/HALA2014110600183.md): Accessory Unit · malfunctioned · Nov 6, 2014 · N598HA · Boeing 767332 · Interphone/Passenger Announcement (PA) System
  > F/A REPORT THAT THEY HAD EMERGENCY AUDIO CHIMES ON FINAL 3-4 TIMES AND ALSO DUIRNG TAXI IN 2 TIMES, COCKPIT DID NOT INITIATE ANY EMERGENCY CHIMES. RESEATED AUDIO ACCESSORY UNIT AND OPS CHECKED OK IAW FIM 23-42, TREE 804.
- [SDR HALA2014091100136](https://openairdocs.org/sdr/HALA2014091100136.md): Warning Message · false activation · Sep 11, 2014 · N598HA · Boeing 767332 · APU Bleed Air System
  > NO APU DUCT PRESSURE. IAW APU ECU BITE, FAULTING PT2 INLET PRESSURE SENSOR. RESET APU ECB. BITE TEST COMPLETED AND ALL PASSED. OPERATED APU BLEED VALVE SEVEARL TIMES. ALL OPS NORMAL. PRESSURE 32PSI. OPERATED PACKS. ALL INDICATIONS NORMAL. OK FOR FURTHE
- [SDR HALA2014081400117](https://openairdocs.org/sdr/HALA2014081400117.md): Wire Harness · damaged · Aug 14, 2014 · N598HA · Boeing 767332 · Fuel System Wiring
  > LOST ALL FUEL TANK QTY PANEL INDICATIONS. REMOVE AND REPLACE RT TANK WIRING HARNESS IAW AMM 28-41-09.
- [SDR HALA2014081000113](https://openairdocs.org/sdr/HALA2014081000113.md): Compensator · malfunctioned · Aug 10, 2014 · N598HA · Boeing 767332 · Fuel Quantity Indicator
  > FUEL QTY INDICATOR STATUS MESSAGE ILLUMINATED. RT FUEL QTY AND TOTALIZER BLANK -CALC-OK. BITE OF FQ PRECESSOR SHOWED FAULTS A4, B3, C6. CAPACITANCE VALUES IAW 28-41-00-715-001, OK FOR ALL RT MAIN TANK UNITS, INSTALATION RESISTANCE TEST OK FOR COMPENSATOR. R
- [SDR HALA2014080900112](https://openairdocs.org/sdr/HALA2014080900112.md): Processor · malfunctioned · Aug 9, 2014 · N598HA · Boeing 767332 · Fuel Quantity Indicator
  > ALL FUEL TANK QTY INDICATIONS BLANK. EICAS MESSAGE FOR FUEL QTY CHANNEL DISPLAYED. R & R FUEL QTY PROCESSOR IAW AMM 28-41-08. OPS CHECKED OK.
- [SDR HALA2014060300075](https://openairdocs.org/sdr/HALA2014060300075.md): Control Unit · out of alignment · Jun 3, 2014 · N598HA · Boeing 76733A · DME/TACAN System
  > LEFT IRS SYS DISPLAYS 25 KNOTS GROUND SPEED & INCREASING. ALIGNED IRUS AND OPS CHECKED IAW MM34-51-00. ACFT OK FOR SERVICE.
- [SDR HALA2014040500044](https://openairdocs.org/sdr/HALA2014040500044.md): Line · damaged · Apr 5, 2014 · N598HA · Boeing 767332 · Hydraulic System, Main
  > AIR DIVERSION, RT HYD QTY INDICATOR ILLUMINATED. FOLLOWED QRH. NOTED QTY ON RT TO 0.48. HYD TUBE ASSY ON LT ANTI SKID SHUTTLE VALVE DAMAGED. FLEX LINE INSTALLED.
- [SDR HALA2014021100023](https://openairdocs.org/sdr/HALA2014021100023.md): Rvdt · malfunctioned · Feb 11, 2014 · N598HA · Boeing 767332 · Central Warning
  > ENROUTE, STATUS MESSAGE OBSERVED FLAP AND SLAT ELEC MOC ADVISED, REQUESTED ACFT RETURN TO PAE. R & R NR 2 RVDT, AND CORRECTED MISWIRING AT TB215. PERFORMED GOOD CONTINUITY CHECK, AND GOOD INSTALLATION TEST. EICAS MESSAGE NO LONGER APPEARS. REG AMM 27-51-26
- [SDR HALA2014012100009](https://openairdocs.org/sdr/HALA2014012100009.md): Adc · unknown · Jan 21, 2014 · N598HA · Boeing 767332 · Altimeter, Barometric/Encoder
  > F/O ALTIMETER IS NEAR RVSM LIMITS. R & R RT ADC IAW AMM 34-12-01-404-006. PERFORMED FUNCTIONAL TEST IAW AMM SUB TASK 34-12-01-744-016, CHECKED OK. LEAK CHECKED GOOD IAW AMM 34-11-00, CAPTAIN`S AND FIRST OFFICER`S ALTIMETER WITHIN LIMITS IAW FIM TASK 34-13.
- [SDR HALA2014011000002](https://openairdocs.org/sdr/HALA2014011000002.md): Grommet · cut · Jan 10, 2014 · N598HA · Boeing 767332 · Power Lever
  > LEFT ENGINE AFT THROTTLE CABLE CUTTING INTO PHENOLIC GROMMENT FAIRLEAD INBD OF PYLON. R & R AFT THROTTLE CABLE PHONOLIC GROMMET. OK FOR SERVICE.
- [SDR HALA2014010700001](https://openairdocs.org/sdr/HALA2014010700001.md): Altimeter · failed · Jan 7, 2014 · N598HA · Boeing 767332 · Altimeter, Barometric/Encoder
  > F/O ALTIMETER FAILED DURING DESCENT. REPLACED ALTIMETER IAW AMM 34-13-01. OPS CHECKED IAW 34-12-00 GOOD.
- [SDR HALA2013101800158](https://openairdocs.org/sdr/HALA2013101800158.md): Power Supply · inoperative · Oct 18, 2013 · N598HA · Boeing 767332 · Emergency Lighting
  > BOTH FWD OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. REPLACED M1209 EMERGENCY LIGHT PWR SUPPLY IAW AMM 33-51-07.
- [SDR HALA2013101700157](https://openairdocs.org/sdr/HALA2013101700157.md): Shear Tie · corroded · Oct 17, 2013 · N598HA · Boeing 767332 · Fuselage Internal Mounting Structure
  > CORROSION ON SHEAR TIE, BS 1562 BETWEEN STR 39R & 39L. REPLACED SHEAR TIE SRM 51-40-05-0G-0.
- [SDR HALA2013101700156](https://openairdocs.org/sdr/HALA2013101700156.md): Skin · corroded · Oct 17, 2013 · N598HA · Boeing 767332 · Fuselage Main, Plate/Skin
  > CORROSION ON INTERIOR SURFACE OF SKIN BS 1544 STR. 39L. REPAIRED SKIN ON ARA 598184.
- [SDR HALA2013101700155](https://openairdocs.org/sdr/HALA2013101700155.md): Stringer · corroded · Oct 17, 2013 · N598HA · Boeing 767332 · Fuselage Main, Longeron/Stringer
  > CORROSION ON BULK CARGO AFT BULKHEAD BS 1544 STRINGER 39R. REPAIRED STRINGER FROM BS 1550-1530 IAW SRM 53-00-03-2R-2.
- [SDR HALA2013101700154](https://openairdocs.org/sdr/HALA2013101700154.md): Stringer · corroded · Oct 17, 2013 · N598HA · Boeing 767332 · Fuselage Main, Longeron/Stringer
  > CORROSION AFT BULKHEAD BS 1544, STR 39L. REPAIRED STRINGER FROM BS 1555-1530 IAW SRM 53-00-03-2R-2.
- [SDR HALA2013101700153](https://openairdocs.org/sdr/HALA2013101700153.md): Roller Tray · cracked · Oct 17, 2013 · N598HA · Boeing 767332 · Fuselage Miscellaneous Structure
  > ROLLER TRAY AT BS 654+5 HAS TWO CRACKS. REPLACED ROLLER TRAY IAW DWG 451T1005, SRM 51-40-05-0G-0, AMM 51-21-10-307-020 AND 25-53-02-404-004.
- [SDR HALA2013101500152](https://openairdocs.org/sdr/HALA2013101500152.md): Doubler · corroded · Oct 15, 2013 · N598HA · Boeing 767332 · Fuselage Main, Plate/Skin
  > CORROSION FOUND ON INTERIOR SURFACE OF E/E COOLING CUT OUT DOUBLER AT BS 478-479, S39R. REPAIRED DOUBLER IAW ARA 598180.
- [SDR HALA2013101500151](https://openairdocs.org/sdr/HALA2013101500151.md): Stringer Clip · corroded · Oct 15, 2013 · N598HA · Boeing 767332 · Fuselage Main, Attach Fittings
  > CORROSION ON STRINGER CLIP AT 18R BS 1197+110. REPAIRED STRINGER CLIP IAW SRM 53-00-03-2R-1.
- [SDR HALA2013101500150](https://openairdocs.org/sdr/HALA2013101500150.md): Skin · corroded · Oct 15, 2013 · N598HA · Boeing 767332 · Fuselage Main, Plate/Skin
  > CORROSION FOUND ON INTERIOR SKIN AT BS 479-481, STR 39R. REPAIRED SKIN IAW ARA 598180.
- [SDR HALA2013101500149](https://openairdocs.org/sdr/HALA2013101500149.md): Stringer · corroded · Oct 15, 2013 · N598HA · Boeing 767332 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 36L, BS 452. REPAIRED STRINGER FROM BS 437-465 IAW SRM 53-00-03-2R.
- [SDR HALA2013101100148](https://openairdocs.org/sdr/HALA2013101100148.md): Seat Track · corroded · Oct 11, 2013 · N598HA · Boeing 767332 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK BS 360, LBL 54.75, WL 200. REPAIRED SEAT TRACK IAW 53-00-52-2R-2.
- [SDR HALA2013101000147](https://openairdocs.org/sdr/HALA2013101000147.md): Stringer · cracked · Oct 10, 2013 · N598HA · Boeing 767332 · Fuselage Main, Longeron/Stringer
  > STRINGER END IS CRACKED AT OVERWING ILLUMINATION LIGHT BS 654+27, STR 19L. REPAIRED STRINGER IAW SRM 53-30-03-2R-2.
- [SDR HALA2013101000146](https://openairdocs.org/sdr/HALA2013101000146.md): Stringer · cracked · Oct 10, 2013 · N598HA · Boeing 767332 · Fuselage Main, Longeron/Stringer
  > STRINGER END IS CRACKED AT OVERWING ILLUMIATION LIGHT BS 654+39, STR 19L. REPAIRED STRINGER IAW SRM 53-30-03-2R-2.
- [SDR HALA2013101000145](https://openairdocs.org/sdr/HALA2013101000145.md): Stringer · cracked · Oct 10, 2013 · N598HA · Boeing 767332 · Fuselage Main, Longeron/Stringer
  > STRINGER END CRACKED AT OVERWING ILLUMIATION LIGHT BS 654+27, STR 19R. REPAIRED STRINGER IAW SRM 53-30-03-2R-2.
- [SDR HALA2013100900141](https://openairdocs.org/sdr/HALA2013100900141.md): Pan · corroded · Oct 9, 2013 · N598HA · Boeing 767332 · Fuselage Miscellaneous Structure
  > CORROSION ON FWD CARGO BIN, MOTOR PAN 8R, BS 616, RBL 34. R & R PDU PAN IAW SRM 51-40-02-0G-0, 51-40-05-0G-0 AND AMM 25-53-01-404-010.
- [SDR HALA2013100900139](https://openairdocs.org/sdr/HALA2013100900139.md): Floor Support · cracked · Oct 9, 2013 · N598HA · Boeing 767332 · Fuselage Miscellaneous Structure
  > CRACKED FLOOR SUPPORT, BS 654+82, RBL-38. REPLACED FLOOR SUPPORT IAW DWG 143T5400 AND SRM 51-40-02-0G-0.
- [SDR HALA2013102300138](https://openairdocs.org/sdr/HALA2013102300138.md): Floor Support · cracked · Oct 9, 2013 · N598HA · Boeing 767332 · Fuselage Miscellaneous Structure
  > CRACKED CABIN FLOOR SUPPORT BS 654+82 RBL-38. REPLACED SUPPORT IAW DWG 143T5400 AND SRM 51-40-02-0G-0.
- [SDR HALA2013091200111](https://openairdocs.org/sdr/HALA2013091200111.md): Filter · unknown · Sep 12, 2013 · N598HA · Boeing 767332 · Aircraft Fuel Filter/Strainer
  > DURING CLIMBOUT, RT FUEL MESSAGE DISPLAYED. DIVERTED TO AN ALTERNATE STATION. ACCOMPLISHED FUEL FILTER BYPASS TEST. NO PR'S NOTED. R & R FUEL FILTER AS A PRECAUTION, RAN ENGINE. OPS & LEAK CHECKED GOOD IAW AMM 73-34-00.
- [SDR HALA2013081200100](https://openairdocs.org/sdr/HALA2013081200100.md): Idg · failed · Aug 12, 2013 · N598HA · Boeing 767332 · AC Generator-Alternator
  > AIR DIVERSION - RT GEN DRIVE EICAS DISCONNECTED GEN DRIVE. R & R NR 2 IDG IAW AMM 24-11-01. LEAK AND OPS CHECKED GOOD. OK FOR SERVICE.
- [SDR HALA2013071600090](https://openairdocs.org/sdr/HALA2013071600090.md): Pump · failed · Jul 16, 2013 · N598HA · Boeing 767332 · Hydraulic Pump (Electric/Engine), Main
  > LEFT HYD DEMAND PUMP FAILURE. R & R LT HYD ACMP IAW AMM 29-11-01, OPS AND LEAK CHECK GOOD.
- [SDR HALA2013041100037](https://openairdocs.org/sdr/HALA2013041100037.md): Actuator · inoperative · Apr 11, 2013 · N598HA · Boeing 767332 · Aircraft Fuel Distribution System
  > LT FUEL SPAR VALVE LIGHT REMAINED ILLUMINATED AFTER ENG SHUTDOWN. R & R LT ENGINE FUEL SHUTOFF VALVE ACTUATOR IAW AMM 28-22-11. OPS CHECKED NORMAL.
- [SDR HALA2013010300002](https://openairdocs.org/sdr/HALA2013010300002.md): Pump · failed · Jan 3, 2013 · N598HA · Boeing 767332 · Hydraulic Pump (Electric/Engine), Main
  > RT HYD PRIM PUMP EICAS. CHECKED RT HYD PUMP DEPRESS PLUG, WIRING CHECKED OK IAW SYS SCH MANUAL 29-00-03. RT ENG HYD PUMP SPLINE INTACT, HEAD PRESSURE LINE FROM RES PRESS MODULE TO RESERVIOR CHECK OK. R & R NR 2 EDP IAW AMM 29-11-05. LEAK AND OPS CHECK GOOD.
- [SDR HALA2012123100238](https://openairdocs.org/sdr/HALA2012123100238.md): Shaft · sheared · Dec 31, 2012 · N598HA · Boeing 767332 · Hydraulic Pump (Electric/Engine), Main
  > DURING CLIMBOUT RECEIVED " B HYD PRIM PUMP " EICAS MESSAGE ALONG WITH ASSOCIATED "PRESS" LIGHT ON OVERHEAD PANEL. VOLTAGE CHECK AT HYD PUMP DEPRESS VALVE GOOD IAW WDM 29-11-21. REMOVED NR 2 ENG EDP IAW MM 29-11-05. FOUND PUMP DRIVE SHAFT SHEARED. INSTALLED
- [SDR HALA2012072700185](https://openairdocs.org/sdr/HALA2012072700185.md): Terminal · shorted · Jul 27, 2012 · N598HA · Boeing 767332 · Electrical Power System Wiring
  > ETOPS SIGNIFICANT SYSTEM, UPON APU START, ARCING WAS NOTICED AT APU BATTERY GROUNDING STUDS/LUGS. REPLACED GROUND LUG IAW SWPM 20-30-11. R & R APU BATTERY GROUND BRACKET AND STUD ASSY, SECURITY CHECKED GOOD.
- [SDR HALA2012072700184](https://openairdocs.org/sdr/HALA2012072700184.md): Ground Stud · arced · Jul 27, 2012 · N598HA · Boeing 767332 · APU System Wiring
  > ETOPS SIGNIFICANT SYS - UPON APU START, ARCING WAS NOTICED AT APU BATTERY GROUNDING STUDS/LUGS. REPLACED GROUND LUG IAW SWPM 20-30-11. R & R APU BATTERY GROUND BRACKET AND STUD ASSY SECURITY CK GOOD.
- [SDR HALA2012060300156](https://openairdocs.org/sdr/HALA2012060300156.md): Blade · damaged · Jun 3, 2012 · N598HA · Boeing 767332 · Turbine Engine Compressor Section
  > NR 2 ENGINE BOROSCOPE INDICATES ENGINE DAMAGED. FOUND FIRST STAGE HPT BLADES DAMAGED BEYOND AMM LIMITS. CHANGED NR 2 ENGINE. LEAK CHECK & OPS CHECK GOOD. OK FOR SERVICE.
- [SDR HALA2012052200144](https://openairdocs.org/sdr/HALA2012052200144.md): Fuel Filter · warning light · May 22, 2012 · N598HA · Boeing 767332 · Engine Fuel Distribution
  > DURING CLIMB, AFTER 1000 FT AGL. EICAS DISPLAY RT ENGINE FUEL FILTER. R & R RT ENGINE FUEL FILTER IAW AMM73-11-02 ENG RUN. OPS & LEAK CHECKED GOOD, OK FOR SERVICE.
- [SDR HALA2012030300102](https://openairdocs.org/sdr/HALA2012030300102.md): Tee Fitting · cracked · Mar 3, 2012 · N598HA · Boeing 767332 · Ailerons
  > INBD TEE FITTING ON AFT ATTACH BEAM FOR INBD AILERON ACTUATOR ACCESS PANEL CRACKED. REPLACED INBD TEE FITTING ON AFT ATTACH BEAM, SECURITY CHECKED GOOD.
- [SDR HALA2011123000622](https://openairdocs.org/sdr/HALA2011123000622.md): Sensor · dirty · Dec 30, 2011 · N598HA · Boeing 767332 · Cabin Temperature Control System
  > ETOPS SIGNIFICANT SYS - AFT CABIN TEMP INDICATION IS APPROX 20 DEG TOO HIGH, FWD AND MID SHOW APPROX 73 AFT 93, F/A'S REPORT TEMP FEELS NORMAL. FOUND AFT CABIN TEMP SENSOR DIRTY AND NO FLOW ACROSS SENSOR. CLEANED BOTH LINE AND SENSOR CHECKS OK.
- [SDR HALA2011121500590](https://openairdocs.org/sdr/HALA2011121500590.md): Idg · failed · Dec 15, 2011 · N598HA · Boeing 767332 · AC Generator-Alternator
  > ETOPS SIGNIFICANT SYS - LEFT GENERATOR DRIVE LIGHT ILLUMINATED, DISCONNECTED LEFT IDG. REMOVED NR 1 ENGINE IDG REF AMM 24-11-01. INSTALLED IDG IAW MM 24-11-01-404-003-001. OPS AND LEAK CHECKED OK.
- [SDR HALA2011121400589](https://openairdocs.org/sdr/HALA2011121400589.md): Warning Light · false activation · Dec 14, 2011 · N598HA · Boeing 767332 · AC Generator-Alternator
  > ETOPS SIGNIFICANT SYS - GENERATOR DRIVE LIGHT ILLUMINATED. GENERATOR DRIVE DISCONNECTED. SERVICED LT ENGINE IDG, BITE CHECK COMPLETED, ON BPCU & NO FAULTS NOTED. LT ENGINE IDG RECONNECTED. GROUND IDLE RUN COMPLETED, ON LT ENGINE CYCLED GENERATOR SWITCH SEVE
- [SDR HALA2011112300540](https://openairdocs.org/sdr/HALA2011112300540.md): Fan · malfunctioned · Nov 23, 2011 · N598HA · Boeing 767332 · Air Distribution Fan
  > ETOPS SIGNIFICANT SYS - AFT EQUIPMENT EXHAUST FAN 1 LIGHT ON. RESET AFT EQUIPMENT EXHAUST FAN & OPS CHECKED OK.
- [SDR HALA2011102700496](https://openairdocs.org/sdr/HALA2011102700496.md): Transceiver · failed · Oct 27, 2011 · N598HA · Boeing 767332 · Weather Radar System
  > ETOPS SIGNIFICANT SYS - RETURN NOISY ON HSI WXR DISPLAY AND WXR INDICATOR DISPLAY INTERMITTENT. REPLACED WXR TRANSCEIVER IAW MM 34-43-01, GROUND CHECK OK.
- [SDR HALA2011102500493](https://openairdocs.org/sdr/HALA2011102500493.md): Fmc · malfunctioned · Oct 25, 2011 · N598HA · Boeing 767332 · Flight Management Computing Hardware System
  > ETOPS SIGNIFICANT SYS. - FUEL CONFIGURATION EICAS MESSAGE, TOTALIZER AND CALCULATED FUEL GREATER THAN 3000 LBS DIFFERENCE. ITEM DIS NR 008921 ON M55 T/S TOTAL FUEL DIFFERING FROM CALC FUEL. REPLACED RT FMC IAW FIM 34-61-00/101 FIG 106. ALL READINGS NORMAL.
- [SDR HALA2011102300487](https://openairdocs.org/sdr/HALA2011102300487.md): Indication Sys · unknown · Oct 23, 2011 · N598HA · Boeing 767332 · Fuel Indicating System
  > ETOPS SIGNIFICANT SYS - FUEL TOTALIZER QTY GREATER THAN CALCULATE FUEL QTY BY 2400 LBS. CALCULATED FUEL APPEARS TO BE MORE ACCURATE. PERFORMED FIM 28-41-00, FIG 107 BITE FUEL PROSSESSOR NO FAULTS NOTED FMC SHOWING FUEL ON BOARD SAME AS FUEL TOTALIZER.
- [SDR HALA2011102100480](https://openairdocs.org/sdr/HALA2011102100480.md): Unknown · unknown · Oct 21, 2011 · N598HA · Boeing 767332 · Aircraft Fuel System
  > ETOPS SIGNIFICANT SYS - AT TOP OF DESCENT, FUEL TOTALIZER READ 21.7. CALCULATED READ 18.5, A DIFFERENC OF -3.2. PERFORMED FIM 28-41-00, FIG 107, NO FAULTS NOTED ON BITE CHECK OF F/Q PROCESSOR, SHOWED NO FAULTS FMC SHOWING FUEL ON BOARD SAME AS TOTALIZER IAW
- [SDR HALA2011101500462](https://openairdocs.org/sdr/HALA2011101500462.md): Shutoff Valve · malfunctioned · Oct 15, 2011 · N598HA · Boeing 767332 · Cabin Cooling System
  > ETOPS SIGNIFICANT SYS - LT PACK REMAINS OFF WITH SWITCH IN AUTO OR STBY FOR OVER 1 MIN BEFORE COMING ON. TROUBLESHOT IAW FIM 21-51-22. R & R LT PACK FLOW CONTROL & SHUTOFF VALVE. OPS CHECKED GOOD IAW AMM 21-51-01.
- [SDR HALA2011100700440](https://openairdocs.org/sdr/HALA2011100700440.md): Engine · failed · Oct 7, 2011 · N598HA · Boeing 767332 · Engine (Turbine/Turboprop)
  > ETOPS SIGNIFICANT SYS - ON APPROACH, AT APPROX 2,400, FLAPS 20, STEADY THROTTLE POSITION, BOTH PILOTS HEARD A MUTED THUD OR BANG AND SHORTLY NOTICED THE LT ENGINE WAS NOT PRODUCING POWER, 21.7 PERCENT N1 AND 697 EGT. LANDED ON RT ENGINE. R & R LT ENGINE PER M

Next page: https://openairdocs.org/deregistered/N598HA-2015-02-23/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 = 'N598HA' AND deregistration_id = 'N598HA-2015-02-23'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N598HA-2015-02-23/reports

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