# Service difficulty reports: N393HA

A list on [N393HA](https://openairdocs.org/aircraft/N393HA.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 4 · 185 reports

- [SDR ASAA2026053164989](https://openairdocs.org/sdr/ASAA2026053164989.md): Light · detached · May 31, 2026 · N393HA · Airbus A330243 · Emergency Lighting
  > FWD GALLEY EMERGENCY PATH STRIP LIGHTING IS UNATTACHED ALONG FORWARD BANK OF CARTS. GROUNDED - YES. RESECURED FWD GALLEY EMERGENCY PATH STRIP. SECURITY CHECK OK.
- [SDR HALA20251008309](https://openairdocs.org/sdr/HALA20251008309.md): Cooling Duct · cracked · Oct 7, 2025 · N393HA · Airbus A330243 · Turbine Engine Air Inlet Section
  > ETOPS - ON WALK AROUND, FOUND #2 ENG EEC COOLING INLET DUCT CRACKED. REMOVED AND REPLACED #2 ENG EEC COOLING DUCT INLET PER CMM 71-60-00. SEC CHK GOOD. OK FOR SVC
- [SDR HALA20250929293](https://openairdocs.org/sdr/HALA20250929293.md): Line · leaking · Sep 26, 2025 · N393HA · Airbus A330243 · Turbine Engine Oil System
  > ETOPS - ON WALK AROUND FOUND OIL LEAKING FROM FAN COWLS ON #1 ENG. FOUND #1 ENG OIL PRESSURE TRANSDUCER LINE LEAKING (AFT LINE) REMOVED AND REPLACED BOTH OIL PRESSURE TRANSDUCER LINES PER TASK CARD 330-79-HIW-03. LEAK CHK OK. OK FOR SVC.
- [SDR HALA20250918282](https://openairdocs.org/sdr/HALA20250918282.md): Mount · sheared · Sep 17, 2025 · N393HA · Airbus A330243 · Engine Thrust Reverser
  > ETOPS - ENG 1 REV FAULT ON LANDING (CLEARED ON SHUTDOWN). PERFORMED TSM 78-37-00-810-833-A. FOUND ENG 1 PCM SUPPORT MOUNTING BRACKET SHEARED FROM MOUNTS. REMOVED ENG 1 PCM PER AMM 73-21-34. REPAIRED MOUNTING BRACKET PER E105-C20228-INI. INSTALLED #1 ENG PCM PE
- [SDR HALA20250818253](https://openairdocs.org/sdr/HALA20250818253.md): Transfer Sys · faulted · Aug 17, 2025 · N393HA · Airbus A330243 · Aircraft Fuel Distribution System
  > ETOPS - BTB ON TAXI OUT ECAM FUEL AFT XFR FAULT. REMOVED & REPLACED LEFT INNER TANK INLET VALVE ACTUATOR PER AMM 28-26-53/400. OPS CHECK GOOD. OK FOR SVC.
- [SDR HALA20250708209](https://openairdocs.org/sdr/HALA20250708209.md): Exciter · out of limits · Jul 7, 2025 · N393HA · Airbus A330243 · Exciter
  > ETOPS - #2 ENG IDG EXCITER FIELD CHECKS OUT OF LIMITS PER TSM 24-20-00-810-875-A PARA 4 (A) (1). IDG REMOVED UP TO AMM 24-21-51-000-804A STEP 4(A). CONTINUED REMOVAL OF #2 IDG AND REPLACED #2 IDG PER AMM 24-21-51 OPS AND DISCONNECT TEST CHECK GOOD OK FOR SVC.
- [SDR HALA20250627201](https://openairdocs.org/sdr/HALA20250627201.md): Transceiver · faulted · Jun 25, 2025 · N393HA · Airbus A330243 · Weather Radar System
  > ETOPS - ECAM: "NAV PRED W/S DET FAULT" DISPLAYED WHEN WXR/PWS SWITCH IS SELECTED TO 1. REMOVED AND REPLACED #1 RTU PER 34-41-00. BITE TEST PASSED. NO FAULT NOTED. OK FOR SERVICE.
- [SDR HALA20250625198](https://openairdocs.org/sdr/HALA20250625198.md): Clamp · disconnected · Jun 24, 2025 · N393HA · Airbus A330243 · Wing Main, Frame Structure
  > ETOPS - AIR- L- WING LEAK. FOUND CLAMP DISCONECTED FROM TRIM AIR PRESSURE REGULATING VALVE. INSTALLED NEW SEAL PER AMM 21-63-52. INSTALLED CLAMP PER M105 #R0483. OPS CHECK GOOD. LEAK CHECK GOOD. NO DEFECTS NOTED. OK FOR SERVICE.
- [SDR HALA20250611177](https://openairdocs.org/sdr/HALA20250611177.md): Boost Pump · faulted · Jun 10, 2025 · N393HA · Airbus A330243 · Fuel Boost Pump
  > ETOPS - ECAM FUEL LEFT PUMP 1 LO PR. C/B TRIPPED FUEL L PUMP 1 SUPPLY. REMOVED AND REPLACED LH PUMP 1 (121QA1) PER AMM 28-21-51. OPS AND LEAK CHECK GOOD.
- [SDR 2025FA0000303](https://openairdocs.org/sdr/2025FA0000303.md): Seat Track · corroded · Apr 24, 2025 · N393HA · Airbus A330243 · Fuselage, Seat/Cargo Attach Fittings
  > DURING ROUTINE MAINTENANCE INSPECTION, FOUND SEAT TRACK CORRODED AT FR62 - 63 (-Y450).
- [SDR 2025FA0000301](https://openairdocs.org/sdr/2025FA0000301.md): Seat Track · corroded · Apr 24, 2025 · N393HA · Airbus A330243 · Fuselage, Seat/Cargo Attach Fittings
  > DURING ROUTINE MAINTENANCE INSPECTION, FOUND SEAT TRACK CORRODED AT FR61-62 (-Y1959).
- [SDR HALA2025042300309](https://openairdocs.org/sdr/HALA2025042300309.md): Web · corroded · Apr 23, 2025 · N393HA · Airbus A330243 · Fuselage Miscellaneous Structure
  > DURING ROUTINE MAINTENANCE INSPECTION, FOUND LONGITUDINAL WEB CORRODED AT AFT OF D1R AT B/W FR 16 -18 (Y-2462).
- [SDR 2025FA0000307](https://openairdocs.org/sdr/2025FA0000307.md): Seat Track · corroded · Apr 21, 2025 · N393HA · Airbus A330243 · Fuselage, Seat/Cargo Attach Fittings
  > DURING ROUTINE MAINTENANCE INSPECTION, FOUND SEAT TRACK CORRODED AT FR74 - 75 (Y450).
- [SDR 2025FA0000305](https://openairdocs.org/sdr/2025FA0000305.md): Seat Track · corroded · Apr 21, 2025 · N393HA · Airbus A330243 · Fuselage, Seat/Cargo Attach Fittings
  > DURING ROUTINE MAINTENANCE INSPECTION, FOUND SEAT TRACK CORRODED AT FR71 (-Y1959).
- [SDR 2025FA0000304](https://openairdocs.org/sdr/2025FA0000304.md): Seat Track · corroded · Apr 21, 2025 · N393HA · Airbus A330243 · Fuselage, Seat/Cargo Attach Fittings
  > DURING ROUTINE MAINTENANCE INSPECTION, FOUND SEAT TRACK CORRODED AT FR62 - 63 (-Y450).
- [SDR 2025FA0000302](https://openairdocs.org/sdr/2025FA0000302.md): Seat Track · corroded · Apr 21, 2025 · N393HA · Airbus A330243 · Fuselage, Seat/Cargo Attach Fittings
  > DURING ROUTINE MAINTENANCE INSPECTION, FOUND SEAT TRACK CORRODED AT FR61 - 62 (Y1959).
- [SDR 2025FA0000299](https://openairdocs.org/sdr/2025FA0000299.md): Seat Track · corroded · Apr 21, 2025 · N393HA · Airbus A330243 · Fuselage, Seat/Cargo Attach Fittings
  > DURING ROUTINE MAINTENANCE INSPECTION, FOUND SEAT TRACK CORRODED AT FR53.6 (Y1959).
- [SDR 2025FA0000298](https://openairdocs.org/sdr/2025FA0000298.md): Seat Track · corroded · Apr 21, 2025 · N393HA · Airbus A330243 · Fuselage, Seat/Cargo Attach Fittings
  > DURING MAINTENANCE INSPECTION, FOUND SEAT TRACK CORRODED AT FR53.6 (Y1959).
- [SDR HALA20250401095](https://openairdocs.org/sdr/HALA20250401095.md): Bleed Valve · faulted · Mar 31, 2025 · N393HA · Airbus A330243 · Compressor Bleed Valve
  > ETOPS - DURING ENG 2 IDLE RUN. HP VALVE NOT WORKING. REMOVED AND REPLACED #2 HP BLEED VALVE PER AMM 36-11-51. OPS/LEAK CHECK GOOD. OK FOR SVC.
- [SDR HALA20250121026](https://openairdocs.org/sdr/HALA20250121026.md): Thermocouple · broken · Jan 19, 2025 · N393HA · Airbus A330243 · Engine Temperature Indicating System
  > ETOPS - #ENG 1 HP/IP TURBINE VENT OVERHEAT CHANNEL A THERMOCOUPLE BROKEN. REPLACED THERMOCOUPLE AS HP/IP BEARING COMPARTMENT VENT TUBE BORESCOPE AND CLEANING PER TC A2010-0709-PART 01 OPS/LK CHK GOOD OK FOR SVC.
- [SDR HALA20250106006](https://openairdocs.org/sdr/HALA20250106006.md): Fire Loop · false activation · Jan 5, 2025 · N393HA · Airbus A330243 · Fire Detection
  > ETOPS - MOMENTARY ENG 2 FIRE LOOP A FAULT ECAM IN CLIMB. REMOVED AND REPLACED FDU 2 PER AMM 26-12-34-400-803-A AND 26-12-34-000-803-A. OPS CHECK GOOD. OK FOR SVC.
- [SDR HALA20250102002](https://openairdocs.org/sdr/HALA20250102002.md): Clamp · broken · Dec 31, 2024 · N393HA · Airbus A330243 · Cabin Cooling System
  > ETOPS - FOUND BAND CLAMP ON BELLOWS UP STREAM OF RH PACK BROKEN. REPLACED CLAMP AS NEEDED PER AMM 21-52-41-400-801-A. OK FOR SERVICE
- [SDR HALA20241231393](https://openairdocs.org/sdr/HALA20241231393.md): Fire Detector · faulted · Dec 30, 2024 · N393HA · Airbus A330243 · Fire Detection
  > ETOPS - ENG 2 FIRE LOOP A FAULT. REMOVED AND REPLACED ENG 2 FDU PER AMM 26-12-34. OPS CHECK FAILED, CONDITION REMAINS. PERFORMED T/S OF ENG#2 FIRE LOOP A PER TSM 26-12-00-810-937-A. FOUND SHORT CIRCUIT FROM 3015VC TO ZONE 2 DETECTOR. REMOVED AND REPLACED HARNE
- [SDR HALA20241231392](https://openairdocs.org/sdr/HALA20241231392.md): Unknown · odor · Dec 30, 2024 · N393HA · Airbus A330243 · Air Distribution System
  > ATB - HEAVY DIRTY SMELL THROUGHOUT CABIN AND COCKPIT DURING TAKEOFF & CLIMB. HEAVY SMELL DURING LANDING IN AFT CABIN. ODOR LASTED ABOUT 34 MINUTES. FLT CREW DONNED OXYGEN MASK. PERFORMED SMOKE AND/OR OIL SMELL IN THE CABIN TROUBLE SHOOTING PER TSM 71-00-81-810
- [SDR HALA20241209354](https://openairdocs.org/sdr/HALA20241209354.md): Seal · broken · Dec 6, 2024 · N393HA · Airbus A330243 · Turbine Engine Oil System
  > ETOPS - ENG #2 FILLER #21 SEALS BROKEN. REPLACED ANNULUS FILLER PER AMM 72-31-41-400-802-A
- [SDR HALA20241023297](https://openairdocs.org/sdr/HALA20241023297.md): Actuator · faulted · Oct 22, 2024 · N393HA · Airbus A330243 · APU Engine Fuel and Control
  > ETOPS - BTB FUEL APU LP VALVE FAULT. REMOVED AND REPLACED APU LP VALVE ACTUATOR PER AMM 28-29-52. OPS CHECK GOOD. SECURITY CHECK GOOD. BTB AGAIN FOR SAME ISSUE. REMOVED AND REPLACED RELAY 6QF, NO CHANGE FAULT STILL ACTIVE AT SHUT DOWN.ECB RERACKED, FAULT CONTI
- [SDR HALA20241011287](https://openairdocs.org/sdr/HALA20241011287.md): Fan · inoperative · Oct 11, 2024 · N393HA · Airbus A330243 · Air Distribution Fan
  > BULK CARGO VENT FAULT. DIV TO OAK. REMOVED AND REPLACED BULK CARGO EXTRACTION FAN PER AMM 21-28-53. OP CHK GOOD OK FOR SVC.
- [SDR HALA20241007281](https://openairdocs.org/sdr/HALA20241007281.md): A/C Pack · faulted · Oct 5, 2024 · N393HA · Airbus A330243 · Cabin Cooling System
  > ETOPS - PACK 2 REG FAULT. FAULT CODE 215352. REPLACED PACK 2 AIR OUTLET FLAP ACTUATOR AMM 215352. OK FOR SERVICE.
- [SDR HALA20240911255](https://openairdocs.org/sdr/HALA20240911255.md): Control Unit · faulted · Sep 10, 2024 · N393HA · Airbus A330243 · Compressor Bleed Control
  > ETOPS - "BTB" DURING START #2 ENG ECAM "ENG 2 CTL SYST FAULT". REMOVED AND REPLACED #2 ENGINE VSV CONTROL UNIT PER AMM 75-33-51. LEAK AND OPS CHECK GOOD - OK FOR SERVICE.
- [SDR HALA20248026244](https://openairdocs.org/sdr/HALA20248026244.md): Coupler · faulted · Aug 23, 2024 · N393HA · Airbus A330243 · HF Communications System
  > ETOPS - HF #2 DOES NOT TUNE. REMOVED AND REPLACED HF #2 COUPLER PER AMM 23-11-36. OPS TEST GOOD. OK FOR SERVICE.
- [SDR HALA20240729203](https://openairdocs.org/sdr/HALA20240729203.md): Bracket · broken · Jul 28, 2024 · N393HA · Airbus A330243 · Engine (Turbine/Turboprop)
  > ETOPS - UPON PERFORMING SCHEDULED TASK CARDS, DISCOVERED BROKEN DRAIN LINE BRACKET. REMOVED AND REPLACED DRAIN LINE BRACKET IN REF WITH AMM 72-00-41. SECURITY CHECK GOOD. A/C OK FOR SVC.
- [SDR HALA20240729202](https://openairdocs.org/sdr/HALA20240729202.md): Exciter · faulted · Jul 27, 2024 · N393HA · Airbus A330243 · APU Start/Ignition System
  > ETOPS - APU CLASS 2 FAULTS, IGNITION/EXCITER FAULTS ON PREVIOUS FLIGHT LEGS. REF:TSI 003228. TROUBLESHOT PER TSM 49-00-00-810-881-A. MAINT MESSAGE IGN PLUG (59KA31)/IGN EXCITER (59KA10) FAULT CODE 072 RECEIVED. REMOVED AND REPLACED 2EA UPPER.LOWER IGNITER
- [SDR HALA20240711187](https://openairdocs.org/sdr/HALA20240711187.md): Actuator · faulted · Jul 10, 2024 · N393HA · Airbus A330243 · Aircraft Fuel Distribution System
  > ETOPS - AFTER STARTING ENG 1 AT TYHE GATE WITH EXTERNAL AIR FUEL- AFT XFER FAULT RESET FCMC 1 AND 2 PER MOC AND MESSAGE CLEARED THEN RETURNED. REMOVED SMA FIN 501 QU IN SERVICEABLE COND. REMOVED & REPLACED SMA FIN 603QL1 WITH 501QU. REF. AMM 28-25-57-000-802
- [SDR HALA20240701176](https://openairdocs.org/sdr/HALA20240701176.md): Fadec · faulted · Jun 28, 2024 · N393HA · Airbus A330243 · Fuel Controlling System
  > ETOPS - BTB AFTER ENG #1 START FADEC 1 FAULT 2 START ATTEMPT AS PER MX FAULT REACURED. PERFORMED WIRING CHECKS PER AMM SUB TASK 77-11-00-810-210-A CONTINUITY CKS GOOD NO STORT TO GROUND INSULATION CK OF WIRES GOOD 6/28/24 8054 REPLACED OVERSPEED PROTECTION UNI
- [SDR HALA20240624168](https://openairdocs.org/sdr/HALA20240624168.md): Control Unit · faulted · Jun 21, 2024 · N393HA · Airbus A330243 · Compressor Bleed Governor
  > ETOPS - ENG 1 CONTROL SYS FAULT ON ECAM PAGE. REMOVED AND REPLACED VSV CONTROL UNIT PER AMM 75-33-51 ON #1 ENG. VERIFICATION FLIGHT FOR #1 ENGINE EEC COMPLETED SATISFACTORILY.
- [SDR HALA20240620530](https://openairdocs.org/sdr/HALA20240620530.md): Slide · faulted · Jun 20, 2024 · N393HA · Airbus A330243 · Escape Slide
  > WHILE PERFORMING BITE TEST PER TASK CARD 330-335100-1 FOUND CLASS 1 FAULT (13WL AND 14 WL) FOR ESCAPE SLIDE LIGHT DOOR 2L AND 2R. REMOVED AND INSTALLED LH DOOR 2 SLIDE/RAFT ASSEMBLY PER AMM 25-62-42. REMOVED AND REPLACED RH DOOR 2 SLIDE RAFT ASSEMBLY PER AMM 2
- [SDR HALA20240618162](https://openairdocs.org/sdr/HALA20240618162.md): Handset · intermittent · Jun 17, 2024 · N393HA · Airbus A330243 · Interphone/Passenger Announcement (PA) System
  > ETOPS - 1R INTERPHONE INTERMITTENT. REMOVED AND REPLACED 1R HANDSET PER AMM 23-73-44. OK FOR SVC.
- [SDR HALA20240513132](https://openairdocs.org/sdr/HALA20240513132.md): Check Valve · leaking · May 11, 2024 · N393HA · Airbus A330243 · Hydraulic System, Main
  > ETOPS - IN CRUISE @ FL380 ECAM HYD Y RSVR LO LVL HYD Y SYS LO PR ECAM ACTIONS FOLLOWED. YELLOW HYD QUANTITY INDICATING EMPTY. FOUND YELLOW HP MANIFOLD- SUPPLY CHECK VALVE LEAKING. REPLACED O-RING PER AMM 29-13-53-000-813-A. OPS AND LEAK CHECK GOOD. PERFORMED E
- [SDR HALA20240321073](https://openairdocs.org/sdr/HALA20240321073.md): Line · unknown · Mar 20, 2024 · N393HA · Airbus A330243 · Aircraft Fuel Distribution System
  > ETOPS - APU FAULT APU AUTO SHUT DOWN. PERFORMED AMM 28-27-53 OPS CHECK APU. REMOVED AND REPLACED FUEL TRIM PIPE ISOLATION-VALVE ACTUATOR. NO FAULT NOTED OK FOR SVC.
- [SDR HALA20240318068](https://openairdocs.org/sdr/HALA20240318068.md): Hinge Fitting · damaged · Mar 17, 2024 · N393HA · Airbus A330243 · Nacelle/Pylon, Main Frame
  > WHILE OPENING IMBOARD(RIGHT) FAN COWL DOOR ON ENG 1 FOR ENGINE 1A CHECK, FOUND CRACK ON FAN COWL DOOR. SECONDARY STRUCTURE ON PYLON TO NACELLE STRUCTURE CRACKED 3.5" ON RIVET LINE. RH FAN COWL DOOR SECOND HINGE MOUNTING BOLT NUT/WASHER ASSEMBLY HAS WORN THROUG
- [SDR HALA20240308063](https://openairdocs.org/sdr/HALA20240308063.md): Bleed Valve · faulted · Mar 7, 2024 · N393HA · Airbus A330243 · Compressor Bleed Valve
  > ETOPS - AFTER LANDING ENG 1 HP VALVE NOT OPEN ECAM APPEARED UNTIL ENGINE SHUTDOWN. PERFORMED BITE TEST ON BMC 1, FAULTING HP BLEED-V. REMOVED AND REPLACED ENG #1 HP VALVE IN REF W/ AMM 36-11-51 OPS CHECK IDLE RUNON ENG #1 COMPLETE. OK FOR SVC.
- [SDR HALA20240220047](https://openairdocs.org/sdr/HALA20240220047.md): Bleed Valve · failed · Feb 19, 2024 · N393HA · Airbus A330243 · Compressor Bleed Valve
  > ETOPS - AIR ENG 2 BLEED NOT-CLOSD REPEATED WRITE UP. MESSAGE EXTINGUISHED ON ARRIVAL #2 BLEED VALVE POSITION SHOWING CLOSED ON ECAM. DUE TO HISOTORY, REMOVED + REPLACED BMC 2 PER AMM 36-11-34. TEST OKAY. OK FOR SERVICE
- [SDR HALA20240110011](https://openairdocs.org/sdr/HALA20240110011.md): Unknown · unknown · Jan 9, 2024 · N393HA · Airbus A330243 · AC Generator-Alternator
  > ETOPS - ELEC IDG 2 OIL LO PR. ELEC C/B TRIPPED, GEN 2 FAULT. REMOVED AND REPLACED #2 IDG PER AMM 24-21-51. OPS OK, LEAK CHECK GOOD. OK FOR SERVICE
- [SDR HALA20250107008](https://openairdocs.org/sdr/HALA20250107008.md): Wire · damaged · Jan 6, 2024 · N393HA · Airbus A330243 · Fire Protection System Wiring
  > ETOPS - ENG 2 FIRE LOOP A FAULT. WIRING CHECK AT FDU 2A CONNECTOR PIN J TO K 1.5K OHMS. J TO GND 1.5K OHMS. K TO GND 25.3 OHMS. AFTER DISCONNECTED 3015VCA READING CHANGED J TO GND 1.9K OHMS. K TO GND 29.3 OHMS. FOUND WIRE 3K001(B AND R)20 DAMAGED NEAR 3822VC2-
- [SDR HALA20230103002](https://openairdocs.org/sdr/HALA20230103002.md): Unknown · unknown · Jan 2, 2024 · N393HA · Airbus A330243 · Turbine Engine Oil System
  > ETOPS - POSSIBLE OIL LEAK ON #2 ENGINE. QTY DECREASING BY APPROX 1.5 QT/HR. FOUND #2 ENGINE PRESSURE OIL FILTER WITH WRONG PACKING INSTALLED. REMOVED AND INSTALLED NEW FILTER AND PACKING PER AMM 79-22-43. PRECAUTIONARY REMOVED AND REPLACED SCAVENGE OIL FILTER
- [SDR HALA20231227288](https://openairdocs.org/sdr/HALA20231227288.md): Unknown · unknown · Dec 26, 2023 · N393HA · Airbus A330243 · Weather Radar System
  > ETOPS - IN CRUISE FLIGHT, WX/PWS SWITCH IN POSITION 2 SHOWED RED WX CTL MESSAGE ON NAV DISPLAY - INTERMITTENTLY. SWITCHED TO POSITION 1 - OPS NORMAL. REMOVED AND REPLACED WX RADAR CONTROL PANEL (3SQ). PERFORMED WX RADAR BITE TEST PER AMM 34-41-00. NO FAULTS, O
- [SDR HALA20231124256](https://openairdocs.org/sdr/HALA20231124256.md): Unknown · unknown · Nov 23, 2023 · N393HA · Airbus A330243 · Engine Oil System (Airframe Furnished)
  > ETOPS - ECAM ENG1 OIL CHIP DETECTED AFTER LANDING. PERFORMED TSM 79-20-00-810-823-A. FOUND & COLLECTED MINISCUAL DEBRIS BRIDGING GAP. WILL SEND TO ENGINEERING. CHANGED SCAVENGE FILTER & INSPECTED. 79-00-00-200-804. NO DEBRIS FOUND. ENGINE RUN LEAK CHECK G
- [SDR HALA20231020233](https://openairdocs.org/sdr/HALA20231020233.md): Unknown · unknown · Oct 19, 2023 · N393HA · Airbus A330243 · Hydraulic System, Main
  > ETOPS - ECAM: HYD G RSVR LO AIR PR AFTER LANDING. T/S IAW TSM 29-11-00-810-806-A FOUND G RSVR AIR RELIEF VALVE FAULT. REPLACED. FUNCTIONAL TEST OK. LEAKAGE CHECK OK. HYDRAULIC FLUID SERVICED. A/C OK FOR SERVICE.
- [SDR HALA20231003217](https://openairdocs.org/sdr/HALA20231003217.md): Unknown · unknown · Oct 1, 2023 · N393HA · Airbus A330243 · Engine Controls
  > ATB - CREW REPORTING LIGHTNING STRIKE AND ENG2 STALL MSG, BUT REPORTS TO DISPATCH BOTH ENGS ARE OPERATIONAL. PER POWERPLANT ENGINEERING, MUST ACCOMPLISH ENG SURGE AMM TASK WHICH WILL REQUIRE A BORESCOPE. NO REPORTS OF ANY FINDINGS ON THE LIGHTNING STRIKE AND O
- [SDR HALA20230918201](https://openairdocs.org/sdr/HALA20230918201.md): Unknown · unknown · Sep 17, 2023 · N393HA · Airbus A330243 · Engine (Turbine/Turboprop)
  > ETOPS - ENG 2 ADVISORY VIB N1 IN CLIMB FL380 VIB N1 - 5.7 VIB N2 - 0.6 VIB N3 - 0.7 N1 - 87% N3 - 90.1% EGT 700 DEG C IN CRUISE OK. REMEOVED/REPLACED #2 ENG FAN BLADE SET AND APPLIED DRY FILM LUBE PER T/C: E1128-330-77-001 WO#265361. PERFORMED TEST 11 ENG VIBE

Next page: https://openairdocs.org/aircraft/N393HA/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 = 'N393HA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N393HA/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.
