# Service difficulty reports: N213HA

A list on [N213HA](https://openairdocs.org/aircraft/N213HA.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 2 · 53 reports

- [SDR ASAA2026081466337](https://openairdocs.org/sdr/ASAA2026081466337.md): Smoke Detector · no discrepancy · Aug 14, 2026 · N213HA · Airbus A321271NX · Fire Detection
  > INFO TO MX: SMOKE LAVATORY SMOKE ECAM DURING CRUISE, F/A REPORTS PAX VAPING IN MID CABIN LAC ON A/C L SIDE. NO VISABLE DAMAGE. GROUNDED - YES. INFO NOTED BY MX. OPS CHECK OK PER AMM 26-17-00. A/C OK FOR SERVICE.
- [SDR ASAA2026050364573](https://openairdocs.org/sdr/ASAA2026050364573.md): Epsu · failed · May 3, 2026 · N213HA · Airbus A321271N · Emergency Lighting
  > EPSU SYS TEST: EPSU 11WL FAIL. GROUNDED - YES. REMOVED & REPLACED EPSU 11WL. OPS CHECK PASS. REFERENCE AMM 33-51-00.
- [SDR HALA20251002297](https://openairdocs.org/sdr/HALA20251002297.md): Fire Loop · faulted · Oct 1, 2025 · N213HA · Airbus A321271N · Fire Detection
  > ETOPS - FIRE LOOP A CORE ECAM MESSAGE. REPLACED FIRELOOP A CORE PER AMM 26-12-17. OPS CHECK NOT GOOD. REPLACED LOOP A FIRE LOOP HARNESS PER AMM 26-12-61. OPS CHECK NOT GOOD. REMOVED AND REPLACED FIRE LOOP CORE LOOP B PER AMM 26-12-17. OPS CHECK IS GOOD. OKAY T
- [SDR HALA20250929291](https://openairdocs.org/sdr/HALA20250929291.md): Pressure Switch · faulted · Sep 27, 2025 · N213HA · Airbus A321271N · APU Oil System
  > ETOPS - APU AUTO SHUTDOWN. REMOVED & REPLACED. ECB & OIL PRESSURE SW PER AMM 49-61-34 & AMM 49-91-14. OPS + LEAK CK GOOD. OK FOR SVC
- [SDR HALA20250620187](https://openairdocs.org/sdr/HALA20250620187.md): Sdu · leaking · Jun 18, 2025 · N213HA · Airbus A321271N · Turbine Engine Oil System
  > ETOPS - DIRTY SOCK SMELL DECSENDING THROUGH 6,000' - 3,000'. DURATION APPROXIMATELY 10 MIN. PUSHED DFDR EVENT BUTTON. FOUND OIL STREAKS COMING FROM #1 ENG INLET CONE WEEP HOLES AND OIL PUDDLING INSIDE OF #1 ENG INLET CONE. REPLACED THE FAN SHAFT COVER SEAL PE
- [SDR HALA20250617184](https://openairdocs.org/sdr/HALA20250617184.md): Sensor · faulted · Jun 16, 2025 · N213HA · Airbus A321271N · Engine Indicating System
  > ETOPS - ON DECENT AS THRUST WENT TO IDLE "ENG 1 SENSOR FAULT". REMOVED BURNER PRESSURE SENSOR AND BURNER PRESSURE SENSOR TUBE IN REFERENCE TO AMM 73-21-23-000-801-A AND 73-21-23-000-802A K.H. 25197 06/15/2025. INSTALLED BURNER PRESSURE AND LINE PER AMM 73-21-2
- [SDR HALA20250505121](https://openairdocs.org/sdr/HALA20250505121.md): Oil Filter · faulted · May 3, 2025 · N213HA · Airbus A321271N · APU Oil System
  > ETOPS - APU AUTO SHUTDOWN AFTER 2 ATTEMPTS. PERFORMED TSM 49-00-81-810-849-A. REMOVED & REPLACED APU OIL FILTER ELEMENTS PER AMM 49-91--41-200-002-A. OPERATED APU PER AMM 49-00-00-860-009-A. NO DEFECTS NOTED. OK FOR SERVICE.
- [SDR HALA20250421110](https://openairdocs.org/sdr/HALA20250421110.md): Fuel Filter · faulted · Apr 18, 2025 · N213HA · Airbus A321271N · APU Engine Fuel and Control
  > ETOPS-APU AUTO SHUTDOWN TWICE ON STARTUP. FOUND CLOGGED OIL FILTER GEN SCAV + LUBE FILTERS MSG. REMOVED AND REPLACED OIL FILTERS APU. OPS AND LEAK CHK GOOD REF AMM49-91-41. REMOVED AND REPLACED APU FUEL FILTER PER AMM 49-32-41-920-001-A. OPS CHECK GOOD NO LEAK
- [SDR HALA20250124031](https://openairdocs.org/sdr/HALA20250124031.md): Wire Harness · damaged · Jan 22, 2025 · N213HA · Airbus A321271N · Electrical Power System Wiring
  > ETOPS - FOUND 440VT2 TERMINAL BLOCK & WIRE 704001-000W24-22 DAMAGED WHILE TROUBLESHOOTING REPEAT GEN 2 FAULT. REMOVED AND REPLACED 440VT2 TERMINAL BLOCK AND WIRE 704001-000W24-22. PER AMM 24-21-61 AND AMM 24-92-00. OPS CHECK OKAY. OK FOR SVC. OSD: 1/24/2025
- [SDR HALA20250110015](https://openairdocs.org/sdr/HALA20250110015.md): Bleed Valve · damaged · Jan 9, 2025 · N213HA · Airbus A321271N · Compressor Bleed Valve
  > ETOPS - WHILE PERFORMING ASSIGNED BOROSCOPE TASK CARDS, FOUND BLEED PRESSURE REGULATING VALVE DAMAGED. REMOVED AND REPLACED BLEED PRESSURE REGULATING VALVE IAW A321 AMM 36-11-52. LEAK CHECK OK. ENGINE IDLE RUN PERFORMED. A/C OK FOR SERVICE.
- [SDR HALA20240816228](https://openairdocs.org/sdr/HALA20240816228.md): Sensor · faulted · Aug 15, 2024 · N213HA · Airbus A321271N · Cabin Cooling System
  > ETOPS - CLASS 2 TEMP CONTROL MESSAGE FOUND ON STATUS PAGE. REMOVED AND REPLACED PACK 1 INLET SENSOR PER AMM 21-51-13-400-001-A. OPS CHECK GOOD, OK FOR SERVICE
- [SDR HALA20240319070](https://openairdocs.org/sdr/HALA20240319070.md): Shuttle Valve · faulted · Mar 18, 2024 · N213HA · Airbus A321271N · Turbine Engine Oil System
  > ETOPS - ENG1 OIL SYSTEM FAULT ON ECAM AFTER SHUTDOWN AT GATE. PERFROMED TSM 79-33-00810840A- NO DECTS NOTED REPLACED SHUTTLE VLV PER AMM 79-21-15-000-801A- REPLACED MAIN OIL PRESS OIL SENSOR PER AMM 79-33-21-400-801 SWAPPED #1 AND #2 PHMU TO ASSIT TROUBLESHOOT
- [SDR HALA20230908193](https://openairdocs.org/sdr/HALA20230908193.md): Unknown · faulty · Sep 7, 2023 · N213HA · Airbus A321271N · Engine Indicating System
  > ETOPS - ON PDC FOUND ECAM MESSAGE ENG 1 FUEL VALVE FAULT FUEL VALVE NOT OPEN AND ENG 1 FADEC IDENT FAULT. PERFORMED TSM 77-31-00-810-801A FOUND #1 PHMU FAIL MESSAGE. REPLACED #1 PHMU PER AMM TASK 77-31-400-801A, RAN ENG NO FAULTS NOTED, OK TO CONTINUE.
- [SDR HALA20230906191](https://openairdocs.org/sdr/HALA20230906191.md): Unknown · unknown · Sep 5, 2023 · N213HA · Airbus A321271N · Fuel Controlling System
  > ETOPS - ON ENG START UP FOUND ENG 2 FADEC FAULT ON ECAM. N2 SPEED VIB INDICATION HAD AMBER X'S. REPLACED EEC PER AMM 73-21-01-400-801-A & AMM 73-21-01-400-801-A. OPS CHECK IS GOOD. OK TO CONTINUE.
- [SDR HALA2023083100184](https://openairdocs.org/sdr/HALA2023083100184.md): Unknown · unknown · Aug 29, 2023 · N213HA · Airbus A321271N · Engine Fuel and Control
  > ETOPS - ENG2 FADEC SYS FAULT ECAM ILLUMIANTED FOR 5 SECONDS AND CLEARED. PERFORMED TSM 77-11-00-818-811-A TO (3) (D), CHECKED CONTINUITY AT WIRE HARNESS WO4, P63 AND P3. PINS Y-4,1,5. CONTINUITY CHECKED GOOD. SWAPPED PHMU 1+2 CONDITION SAME. RETURNED PHU 1+2 T
- [SDR HALA2023082800179](https://openairdocs.org/sdr/HALA2023082800179.md): Unknown · unknown · Aug 27, 2023 · N213HA · Airbus A321271N · Fuel Controlling System
  > ETOPS - ENG 2 FADEC SYS FAULT ON ENGINE START. ATTEMPTED ENGINE START BY MAINT DIRECTION. NORMAL ENGINE START. FAULT CLEARED WHEN AVAIL APPEARED. REMOVED & REPLACED #2 ENG EEC PER AMM 73-21-01. OPS CHECK GOOD. RAN #2 ENG IDLE. NO FAULTS NOTED OK TO CONTINU
- [SDR HALA2023082500178](https://openairdocs.org/sdr/HALA2023082500178.md): Unknown · faulty · Aug 24, 2023 · N213HA · Airbus A321271N · Engine Indicating System
  > ETOPS - ENG 2 FADEC SYS FAULT CODE 733101. REPLACED #2 PHMU PER AMM 77-31-01 NO FAULTS NOTED ENG RUN GOOD OK FOR SERVIC
- [SDR HALA2023080400167](https://openairdocs.org/sdr/HALA2023080400167.md): Igniter · faulty · Aug 3, 2023 · N213HA · Airbus A321271N · Spark Plug/Igniter
  > ETOPS - DURING BOROSCOPE INSPECTION FOUND #2 IGNITER WORN. REMOVED AND REPLACED IGNITER PER AMM 74-21-01. OPS CHK GOOD. A/C OK FOR SVC.
- [SDR HALA2023071700144](https://openairdocs.org/sdr/HALA2023071700144.md): Unknown · unknown · Jul 15, 2023 · N213HA · Airbus A321271N · Airborne Auxiliary Power Unit (APU) System
  > ETOPS - APU AUTO SHUT DOWN ON ARRIVAL, ATEMPTED 3 STARTS UNSUCCESSFULLY. REMOVED AND REPLACED APU IGNITION EXCITER UNIT PER AMM 49-41-38. OPS CHECK GOOD NO FAULTS DETECTED.
- [SDR HALA2023062000129](https://openairdocs.org/sdr/HALA2023062000129.md): Unknown · unknown · Jun 18, 2023 · N213HA · Airbus A321271N · Air Conditioning System
  > ETOPS - SKIN INLET FAULT. INITIALLY OVRD FOR BOTH INLET/EXHAUST EXTINGUISHED THE ECAM. DESCENDING THROUGH 13,000 FT, ECAM REOCCURED AND FORCED INTO MANUAL MODE TO DEPRESSURIZED TO SL. REMOVED AND REPLACED SKIN OUTLET VALVE PER AMM 21-26-53. REF DMI 207107 F
- [SDR HALA2023061600128](https://openairdocs.org/sdr/HALA2023061600128.md): Unknown · unknown · Jun 16, 2023 · N213HA · Airbus A321271N · Smoke Detection
  > ETOPS - INFO TO MX INFLIGHT ENG2 FIRE LOOP A FAULT ECAM. THE ECAM WENT AWAY AFTER 2 MINUTES. REPLACED ENG2 FIRE LOOP A HARNESS FIN 4165KS PER AMM 26-11-61. OPS CHECK OK. NO FAULTS NOTED. SECURITY CHECK GOOD OK FOR SERVICE.
- [SDR HALA2023061200123](https://openairdocs.org/sdr/HALA2023061200123.md): Unknown · unknown · Jun 11, 2023 · N213HA · Airbus A321271N · Fire Protection System
  > ETOPS - DURING #1 ENGINE CHANGE FOUND DAMAGED FIRE DETECTOR HARNESS. REMOVED AND REPLACED FIRE DETECTOR HARNESS PER AMM 26-12-16. CHECK IS GOOD NO DEFECTS NOTED OK TO CONTUNE SERVICE.
- [SDR HALA2023041200017](https://openairdocs.org/sdr/HALA2023041200017.md): Unknown · unknown · Apr 11, 2023 · N213HA · Airbus A321271N · Fire Protection System
  > MOMENTARY LAV SMOKE ECAM DURING CRUISE. PERFORMED SYS RESET AND INSPECTED IAW AMM 26-17-00. NO FAULTS FOUND, A/C GOOD FOR SERVICE.
- [SDR HALA2022123000015](https://openairdocs.org/sdr/HALA2022123000015.md): Slide · unwanted deploy · Dec 29, 2022 · N213HA · Airbus A321271N · Escape Slide
  > SLIDE AT R1 DOOR ACCIDENTALLY DEPLOYED. R & R THE R1 DOOR DAMPER DIAPHRAM IAW AMM 52-11-14. NO LEAKS NOTED. R & R R1 DOOR ESCAPE SLIDE IAW AMM 25-62-44. INDICATIONS OK. OPS CHECKED OK. OK FOR SERVICE.
- [SDR HALA2022120200305](https://openairdocs.org/sdr/HALA2022120200305.md): Radar · faulted · Dec 1, 2022 · N213HA · Airbus A321271N · Weather Radar System
  > ETOPS - WX RADAR GCS (GROUND CLUSTER SWITCH) IS BROKEN ( WEATHER RADAR SYSTEMS GROUND CLUTTER SUPPRESSION). REMOVED AND REPLACED WEATHER RADAR CTL UNIT AND BITE TEST OK IAW AMM 34-41-12 PB 401.
- [SDR HALA2022101100270](https://openairdocs.org/sdr/HALA2022101100270.md): None · none · Oct 7, 2022 · N213HA · Airbus A321271N · Fire Detection
  > BTB - ENG 1 FIRE LOOP A FAULT, 5TH WRITE FROM 9-29-2022. FOUND WIRE 708003-20R26-12 SHORTED TO GROUND. REMOVED AND REPLACED HARNESS 4165KS PER AMM 71-51-75, OPS CHECK GOOD PER AMM 26-12-00. PLACARDS REMOVED & MIC SHEET CLEARED.
- [SDR HALA2022061500113](https://openairdocs.org/sdr/HALA2022061500113.md): None · none · Jun 14, 2022 · N213HA · Airbus A321271N · Engine (Turbine/Turboprop)
  > DESCENDING THOUGHT 5,000' - 3,000 ' ENGINE AT IDLE EXPERIENCE DIRTY SHOCK SMELL AGAIN // FOUND EVIDANCE OF OIL LEAK ON #1 ENG AT 9 O CHOCK POSITION IN THE FIC REPLACED SEAL FROM LP62 OIL PRESSURE TUBE REF AMM PW 10006-C-72-00-30-00A-702A-B LEAK CHECK GOOD 1843
- [SDR HALA2022011300014](https://openairdocs.org/sdr/HALA2022011300014.md): Switch · inoperative · Jan 12, 2022 · N213HA · Airbus A321271N · Hydraulic Power System
  > ETOPS - RAT FAULT DURING RAT EXTENSION AND STOWAGE TEST // REMOVED AND REPLACED RAT ACTUATOR PRESSURE SWITCH REF AMM 29-22-53-400-013-A. OPS CHECK AND LEAK CHECK GOOD.
- [SDR HALA2021110500153](https://openairdocs.org/sdr/HALA2021110500153.md): Connector · damaged · Nov 3, 2021 · N213HA · Airbus A321271N · Fire Protection System Wiring
  > ETOPS - ENG 1 FIRELOOP A FAULT CAME ON SHORTLY AFTER T/O. FOUND STUD C CONNECTOR OF ENG 1 LOOP A COMMON FWD DETECTOR CABLE BROKEN. REMOVED AND REPLACED (4181KS) PER AMM 26-12-61. ALSO PER MOC AS PRECAUTIONARY REMOVED & REPLACED #1 LOOP A AGB PER AMM 26-12-17
- [SDR HALA2021102800147](https://openairdocs.org/sdr/HALA2021102800147.md): Wire Harness · chafed · Oct 27, 2021 · N213HA · Airbus A321271N · Fire Protection System Wiring
  > ETOPS - ENG 2 FIRE LOOP A FAULT. RESISTANCE CHECK AT PIN J - K AT FDU 2 (2WD2) CONNECTOR A. FOUND 1.49K OHMS. RESISTANCE GOOD WITH TAPPING DETECTORS. NO FAULT NOTED. NO SHORT TO GND. INSULATION TEST OK. DURING T/S FOUND CHAFED WIRE ON 4165KS HARNESS. REPLACED
- [SDR HALA2021061500072](https://openairdocs.org/sdr/HALA2021061500072.md): Gcu · faulted · Jun 15, 2021 · N213HA · Airbus A321271N · AC Generator-Alternator
  > ETOPS - ATB - ELECT GEN 2 FAULT//REMOVED AND REPLACED GCU 2 IAW AMM 24-22-34. BITE TEST OK. PERFORMED ENGINE 2 RUN UP. OPS TEST GEN 2 NORMAL. NO FAULLTS NOTED.
- [SDR HALA2021012500010](https://openairdocs.org/sdr/HALA2021012500010.md): Gcu · defective · Jan 22, 2021 · N213HA · Airbus A321271N · AC Generator-Alternator
  > ETOPS ECAM MX STATUS "AC GEN". REMOVED & REPLACED NR 1 GCU, PER AMM 24-22-34. MX STATUS CLEARED, OK FOR SERVICE.
- [SDR HALA2020091430181](https://openairdocs.org/sdr/HALA2020091430181.md): Blade · damaged · Sep 13, 2020 · N213HA · Airbus A321271N · Turbine Engine Air Inlet Section
  > NR 4 FAN BLADE ON NR 2 ENGINE S/N JB1AEA4305 MISSING POLYURETHANE COAT. REMOVED AND REPLACED NR 4 FAN BLADE, PER AMM 72-11-03-400-801-A. FUNCTIONAL TEST FAN TRIM BALANCE AMM TASK 71-00-00-710-807-A PENDING. PERFORMED FUNCTION TEST (FAN TRIM BALANCE), PER AM
- [SDR HALA2020080400167](https://openairdocs.org/sdr/HALA2020080400167.md): Panel · leaking · Aug 3, 2020 · N213HA · Airbus A321271N · Compressor Bleed Valve
  > ETOPS SIGNIFICANT SYSTEM - DURING CRUISE ECAM AIR ENG 2 BLEED LEAK. THIRD WRITE UP TODAY. FOUND GAP CLEARANCE OF OVER PRESSURE FLAP DOOR ON PANEL 423DT. REWORKED PRECOOLER PANEL 423DT #2 PYLON PER TASK CARD E105-213003-INI. REPLACED PANEL AND CLEARANCE CHE
- [SDR HALA2019111400484](https://openairdocs.org/sdr/HALA2019111400484.md): None · none · Nov 13, 2019 · N213HA · Airbus A321271N · Standard Practices/Structures
  > ATB - BIRD STRIKE ON DEPARTURE. RIGHT SIDE OF AIRCRAFT. // ACCOMPLISHED AMM TASK 05-51-14-200-803-A. FOUND EVIDENCE OF BIRD STRIKE ON INBOARD RH FLAP. WILDLIFE SVC COLLECTED EVIDENCE. CLEANED AREA. NO DEFECTS NOTED. A/C OK FOR SVC.
- [SDR HALA2019090300358](https://openairdocs.org/sdr/HALA2019090300358.md): Smoke Detector · false activation · Sep 1, 2019 · N213HA · Airbus A321271N · Smoke Detection
  > SMOKE AFT LAV ECAM WARNING ILLUMINATED MOMENTARILY NEAR TOP OF DESCENT. SUSPECTED VAPING NOTHING CONFIRMED. FLT ATTENDANT WITNESSED PASSENGER ENTER AFT LAV WITH VAPE PEN. OPS CHECKED DETECTOR - NO DEFECTS FOUND. OK FOR CONTINUED SVC.
- [SDR HALA2019041100185](https://openairdocs.org/sdr/HALA2019041100185.md): Warning Message · false indication · Apr 10, 2019 · N213HA · Airbus A321271N · Engine Cooling System
  > ETOPS SIGNIFICANT SYSTEM - ENG 2 AIR SYSTEM FAULT ON APPROACH. // PERFORMED BITE TEST ON EEC 1 & 2, NO FAULTS NOTED. DID A HISTORY SEARCH ON THIS FAULT AND NONE WERE FOUND PREVIOUS OF THIS ONE. WILL CONTINUE MONITORING AS REQUIRED PER TSM 75-26-00-810-819-A.
- [SDR HALA2019010200003](https://openairdocs.org/sdr/HALA2019010200003.md): Warning System · false activation · Jan 1, 2019 · N213HA · Airbus A321271N · Engine Oil Indicating System
  > ETOPS SIGNIFICANT SYSTEM - AFTER 30S ON IGN/START,#2ENG OIL CHIP DETECTION ON ECAM. CLEARED AFTER 5 SECONDS, NO FURTHER INDICATIONS.//INSPECTED MAGNETIC CHIP DETECTORS PER AMM 75-00-00-281-802-A NO CHIP DETECTED. OK TO CONTINUE.
- [SDR HALA2018123100693](https://openairdocs.org/sdr/HALA2018123100693.md): Warning System · false activation · Jan 1, 2019 · N213HA · Airbus A321271N · Engine Oil Indicating System
  > ETOPS SIGNIFICANT SYSTEM - AFTER 30S ON IGN/START, NR 2 ENG OIL CHIP DETECTION ON ECAM. CLEARED AFTER 5 SECONDS, NO FURTHER INDICATIONS. INSPECTED MAGNETIC CHIP DETECTORS PER AMM 75-00-00-281-802-A NO CHIP DETECTED. OK TO CONTINUE.
- [SDR HALA2018123100692](https://openairdocs.org/sdr/HALA2018123100692.md): Warning System · false activation · Dec 31, 2018 · N213HA · Airbus A321271N · Engine Oil Indicating System
  > SUP - ETOPS SIGNIFICANT SYSTEM - NR 2 ENG OIL CHIP DETECTION ECAM WHEN IGN/START SELECTED. EXTINGUISHED AFTER 30 SECONDS. NO FURTHER INDICATIONS. CHECKED MAGNETIC CHIP DETECTORS PER AMM 79-00-00-281-802-A - NO CHIPS DETECTED - OK TO CONTINUE.
- [SDR HALA2018123100690](https://openairdocs.org/sdr/HALA2018123100690.md): Warning System · false activation · Dec 28, 2018 · N213HA · Airbus A321271N · Engine Oil Indicating System
  > ETOPS SIGNIFICANT SYSTEM - NR 2 ENG OIL CHIP DETECTOR ECAM WHEN IGN/START SELECTED. EXTINGUISHED AFTER 1 MINUTE. NO FURTHER INDICATIONS. PERFORMED AMM TASK 79-00-00-281-802-A. CHECKED CHIP DETECTOR-NO CONTAMINANTS FOUND. RAN NR 2 ENG- NO ECAM MESSAGE ASSOCIAT
- [SDR HALA2018122400677](https://openairdocs.org/sdr/HALA2018122400677.md): Warning Light · false activation · Dec 22, 2018 · N213HA · Airbus A321271N · Turbine Engine Oil System
  > ETOPS SIGNIFICANT SYSTEM - ENG 2 OIL CHIP DETECTED WHILE ATTEMPTING TO START ENGINE #2.// PERFORMED CHIP DETECTOR INSP PER TSM 79-00-00-281-802A. NO FAULTS FOUND. CLOSED COWLS. RAN ENGINE, NO ECAM MESSAGE NOTED.
- [SDR HALA2018111400580](https://openairdocs.org/sdr/HALA2018111400580.md): Warning Message · false activation · Nov 13, 2018 · N213HA · Airbus A321271N · Central Warning
  > ETOPS SIGNIFICANT SYSTEM - UPON PLACING ENGINE MODE SELECTOR TO IGN/START, ENG 2 OIL CHIP DETECTED ECAM DISPLAYED. MAINTENANCE ADVISED TO START ENG 2, ENG HAD A NORMAL START AND CAM DISAPPEARED WHEN ENG 2 MASTER SWITCH WAS PLACED TO ON.// PERFORMED AMM 79-00-0
- [SDR HALA2018111400579](https://openairdocs.org/sdr/HALA2018111400579.md): Warning Light · false activation · Nov 13, 2018 · N213HA · Airbus A321271N · Turbine Engine Oil System
  > ETOPS SIGNIFICANT SYSTEM - UPON PLACING ENGINE MODE SELECTOR TO IGN/START, ENG 2 OIL CHIP DETECTED ECAM DISPLAYED. MAINTENANCE ADVISED TO START ENG 2, ENG HAD A NORMAL START AND CAM DISAPPEARED WHEN ENG 2 MASTER SWITCH WAS PLACED TO ON.// PERFORMED AMM 79-00-0
- [SDR HALA2018110700571](https://openairdocs.org/sdr/HALA2018110700571.md): Warning Message · false activation · Nov 6, 2018 · N213HA · Airbus A321271N · Engine Indicating System
  > ETOPS SIGNIFICANT SYSTEM - DURING PREFLIGHT - ECAM ENG 2 BOWED ROTOR PROTECTION FAULT DISPLAYED. // PERFORMED EEC SYSTEM TEST PER AMM 73-21-00. TEST OK. PERFORMED EEC RESET TO CONFIRM IF ACTUAL FAULT. MESSAGE CLEARED. CONTACT PRATT & WHITNEY REP. PERFORMED ID
- [SDR HALA2018102300537](https://openairdocs.org/sdr/HALA2018102300537.md): Unknown · odor · Oct 22, 2018 · N213HA · Airbus A321271N · Air Distribution System
  > STRONG ODOR CIRCULATED THROUGHOUT ENTIRE AIRCRAFT DURING DESCENT FROM FL200 DOWN TO THE SURFACE, SMELLED LIKE DIRTY SOCKS & CHEMICALS. NOTICED SMELL IN CABIN UPON ENTRY TO AIRCRAFT. ISOLATED EACH BLEED SYSTEM AND OPERATED PACKS ON FULL HOT/ FULL COLD. SMELL D
- [SDR HALA2018102300538](https://openairdocs.org/sdr/HALA2018102300538.md): Bearing · failed · Oct 21, 2018 · N213HA · Airbus A321271N · Engine (Turbine/Turboprop)
  > ETOPS SIGNIFICANT SYSTEM - IN CRUISE, ECAM MASTER WARNING AIR-BLEED LEAK. FOLLOWED ECAM PROCEDURE AND ECAM CLEARED. REMAINING ECAM: AIR ENG 1 AND 2 BLEED FAULT RIGHT COND HOT AIR FAULT, ENG 1 OIL CHP DETECTED. SMOKE SMELL DETECTED AFTER ENGINE NR 1 START// BOR
- [SDR HALA2018101500496](https://openairdocs.org/sdr/HALA2018101500496.md): Warning System · false activation · Oct 13, 2018 · N213HA · Airbus A321271N · Engine Oil Indicating System
  > ETOPS SIGNIFICANT SYSTEM - AFTER LANDING ENG 1 OIL CHIP DETECTED. PERFORMED ENG 1 OIL CHIP DETECTORS INSPECTION PER AMM 79-00-00 281-802-A. NO DEBRIS FOUND INSPECTED AND REPLACED ENG 1 OIL FILTER PER 79-21-06-960-801-A. ENG 1 RUN OK.
- [SDR HALA2018101500495](https://openairdocs.org/sdr/HALA2018101500495.md): Duct · contaminated · Oct 13, 2018 · N213HA · Airbus A321271N · Pneumatic Distribution System
  > BTB SMOKE SMELL DETECTED AFTER ENGINE NR 1 START. FOUND OIL INTERMEDIATE PRESSURE DUCTING ON ENG NR 1.
- [SDR HALA2018101000486](https://openairdocs.org/sdr/HALA2018101000486.md): Igniter · faulted · Oct 9, 2018 · N213HA · Airbus A321271N · Spark Plug/Igniter
  > ETOPS SIGNIFICANT SYSTEM - BTB ENG 2 IGN A FAULT. REMOVED AND REPLACED ENG 2 IGN A PER AMM 74-21-01, IGNITER TEST GOOD ON CH A+B. OK FOR SVC.

Next page: https://openairdocs.org/aircraft/N213HA/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 = 'N213HA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N213HA/reports

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