# Service difficulty reports: N202HA

A list on [N202HA](https://openairdocs.org/aircraft/N202HA.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 · 63 reports

- [SDR 2026F00182](https://openairdocs.org/sdr/2026F00182.md): Engine · vibration · Aug 22, 2026 · N202HA · Airbus A321271N · Engine (Turbine/Turboprop)
  > ATB - AFTER TAKEOFF, ENGINE 1 EXPERIENCED INCREASES IN EGT, WF, ICT, AND LPR; DECREASES IN N2, CET, AND TER; INCREASED N2 VIBRATION LEVELS; AND DECREASED EGTM. INITIAL BORESCOPE INSPECTION FOUND MATERIAL LOSS AND DAMAGE IN THE HPT AND COMBUSTION CHAMBER; TROUB
- [SDR 2026FA0000663](https://openairdocs.org/sdr/2026FA0000663.md): Engine · vibration · Aug 22, 2026 · N202HA · Airbus A321271N · Engine (Turbine/Turboprop)
  > ATB - AFTER TAKEOFF, ENGINE 1 EXPERIENCED INCREASES IN EGT, WF, ICT, AND LPR; DECREASES IN N2, CET, AND TER; INCREASED N2 VIBRATION LEVELS; AND DECREASED EGTM. INITIAL BORESCOPE INSPECTION FOUND MATERIAL LOSS AND DAMAGE IN THE HPT AND COMBUSTION CHAMBER; TROUB
- [SDR HALA20250915278](https://openairdocs.org/sdr/HALA20250915278.md): Gauge · abnormal · Sep 14, 2025 · N202HA · Airbus A321271N · Hydraulic System, Main
  > ETOPS - ACCUMULATOR GAUGE WAS FILLED WITH HYDRAULIC FLUID. REMOVED AND REPLACED GREEN SYSTEM ACCUMULATOR AND PRESSURE GAUGE. OPS CHECK GOOD, OKAY FOR SERVICE PER AMM 29-11-42.
- [SDR HALA20250609166](https://openairdocs.org/sdr/HALA20250609166.md): Fire Loop · faulted · Jun 8, 2025 · N202HA · Airbus A321271N · Fire Detection
  > ETOPS - ENG 2 FIRE LOOP B FAULT -IN CRUISE FL320-. PERFORMED TSM TASK 26-12-00-801-861-A, FAULT CONFIRMED, REMOVED AND REPLACED FIRE LOOP ASSY FWD IAW AMM 26-12-17-000-802, 26-12-17-400-802-A OPS CHECK GOOD, OK FOR SERVICE
- [SDR HALA20250604161](https://openairdocs.org/sdr/HALA20250604161.md): Fire Loop · faulted · Jun 3, 2025 · N202HA · Airbus A321271N · Fire Detection
  > ETOPS - ENG 1 FIRE LOOP B FAULT IN CRUISE. REMOVED & REPLACED FWD FIRE / OVERHEAT DETECTOR PER AMM 26-12-17. ECAM CLEARED OPS TEST OF FDU 1 PER AMM 26-12-00 TEST OK. OK FOR SERVICE.
- [SDR HALA20250303074](https://openairdocs.org/sdr/HALA20250303074.md): Generator · faulted · Feb 28, 2025 · N202HA · Airbus A321271N · AC Generator-Alternator
  > ETOPS - RECEIVED ELEC APU GEN FAULT ECAM AFTER LANDING. ECAM PROCEDURE DID NOT RESTORE APU GENERATOR POWER. REMOVED AND REPLACED APU GENERATOR PER AMM 24-23-51. OPS AND LEAK CHECK GOOD. NO FAULTS NOTED. OK FOR SERVICE.
- [SDR HALA20250218007](https://openairdocs.org/sdr/HALA20250218007.md): Autothrottle Sys · faulted · Feb 16, 2025 · N202HA · Airbus A321271N · Auto Throttle System
  > RTO APPROX 70 KTS. ECAMS: AUTO FLT/ AUTO THROTTLES OFF, RUD TRAVEL LIMIT & RED SPD LIMIT ANNUNCIATOR ON PFD. F.O. AIRSPEED READ ZERO THRU 70 KTS. REMOVE /REPLACED #2 ADM PER AMM 34-11-17-400-001-A. REPLACED FAC 1& 2 PER AMM22-66-34-400-002-A. PERFORMED AF
- [SDR HALA20241209350](https://openairdocs.org/sdr/HALA20241209350.md): Oil System · leaking · Dec 8, 2024 · N202HA · Airbus A330243 · Turbine Engine Oil System
  > ETOPS - FOUND #1 ENG LEAKING OIL FROM INLET CONE. REMOVED AND REPLACED #1 ENG FAN SHAFT COVER PACKING PER AMM 71-15-00/801.
- [SDR HALA20241108317](https://openairdocs.org/sdr/HALA20241108317.md): Ramp · damaged · Nov 7, 2024 · N202HA · Airbus A321271N · Nacelle/Pylon Structure
  > ETOPS - FIRELOOP RAMP ASSY-PYLON DAMAGED #2 ENGINE. REMOVED AND REPLACED RAMP ASSY COMPLETE WITH DETECTORS #2 ENG PER AMM 26-12-16.OPS CHECK GOOD OK FOR SERVICE
- [SDR HALA20240726199](https://openairdocs.org/sdr/HALA20240726199.md): Rod · broken · Jul 25, 2024 · N202HA · Airbus A321271N · Engine Bleed Air System
  > ETOPS - BTB: AIR ENG 1 BLEED FAULT RESET UNSUCCESSFUL. PERFORMED TSM 36-11-00-810-988-A. FOUND FAV ACTUATOR ROD BROKEN. REMOVED AND REPLACED ACTUATOR ROD PER AMM 36-11-54. IDLE RAN AND OPS CHECK GOOD. OK FOR SVC.
- [SDR HALA20240611159](https://openairdocs.org/sdr/HALA20240611159.md): Generator · faulted · Jun 10, 2024 · N202HA · Airbus A321271N · AC Generator-Alternator
  > ETOPS - ELEC APU GEN FAULT AFTER APU STARTED ON GROUND DURING TAXI IN. PERFORMED ECAM. RESET UNSUCCESSFUL. REMOVED & REPLACED APU GEN PER AMM 24-23-51. OPS CHECK GOOD. NO DEFECTS NOTED. A/C OK FOR SVC.
- [SDR HALA20240603154](https://openairdocs.org/sdr/HALA20240603154.md): Hydraulic Line · leaking · Jun 2, 2024 · N202HA · Airbus A321271N · Hydraulic System, Main
  > OTHER - IN CRUISE FL350 HYD Y RSVR LO LVL ECAM. COMPLIED W/ECAM ACTIONS. LANDED NORMAL CLEARED RUNWAY ON HIGH SPEED TAXIWAY AND TUGGED TO THE GATE. FOUND PRESSURE HYD LINE LEAKING. REPAIRED YELLOW PRESSURE HYD LINE WITH PERMASWAGE UNION PER AMM 20-23-11-300-00
- [SDR HALA20240522141](https://openairdocs.org/sdr/HALA20240522141.md): Liner · damaged · May 21, 2024 · N202HA · Airbus A321271N · Engine (Turbine/Turboprop)
  > ETOPS - ON LANDING, POSSIBLE BIRD STRIKE, RIGHT SIDE OF AIRCRAFT WITH POSSIBLE BIRD INGESTION #2 ENG. PERFORMED VISUAL EXAMINATION OF #2 ENG. PER AMM 72-00-00-210-807-A. FOUND OUTER LINER SEGMENT POSITIONS 6 AND 8 DAMAGED. REMOVED AND REPLACED SEGMENTS IAW AMM
- [SDR HALA20240520135](https://openairdocs.org/sdr/HALA20240520135.md): Wire · shorted · May 19, 2024 · N202HA · Airbus A321271N · Fire Protection System Wiring
  > ETOPS - ECAM ENG 1 FIRE LOOP B FAULT APPEARED IN CRUISE. WHILE PERFORMING T/S, FOUDN SHORTING ON WIRES (WH1NVR1, WH2NVR1). REMOVED AND REPLACED ENG #1 CH.B PYLON FIRE-DETECTOR HARNESS PER AMM 26-12-63. PERFORMED WIRE CHECKS. COUNTINUITY GOOD. NO SHORT TO GROUN
- [SDR HALA20240103003](https://openairdocs.org/sdr/HALA20240103003.md): Unknown · unknown · Jan 2, 2024 · N202HA · Airbus A321271N · Aerodynamic Fairings
  > BIRD STRIKE ON CLIMB-OUT IN SMF. PERFORMED BIRD STRIKE INSPECTIN PER AMM 05-51-14. FOUND DAMAGE TO LEFT HAND SIDE OF RADOME. NO OTHER DAMAGE NOTED. FERRY FLIGHT REQUIRED. REMOVED AND REPLACED RADOME PER AMM 53-15-11. SECURITY CHK GOOD. OK FOR SVC.
- [SDR HALA20231019230](https://openairdocs.org/sdr/HALA20231019230.md): Unknown · unknown · Oct 18, 2023 · N202HA · Airbus A321271N · Compressor Bleed Valve
  > ETOPS - BTB AIR ENG HI TEMP AFTER COMPLETING PROCEDURE FOR MEL 36-11-07B ON TAXI OUT. REFERENCE DEFERRAL 207735 FOR REMOVAL AND REPLACEMENT OF #2 HP VALVE ON LP 946395-1. REMOVED AND REPLACED #2 ENG HPV PER AMM 36-11-51. CONDITION SAME. PERFORMED WIRING CHECK
- [SDR HALA20231003214](https://openairdocs.org/sdr/HALA20231003214.md): Unknown · unknown · Oct 2, 2023 · N202HA · Airbus A321271N · Engine (Turbine/Turboprop)
  > ETOPS - DURING PDC, FOUND OIL COMING FROM #1 ENGINE INLET CONE. REMOVED AND REPLACED FAN SHAFT COVER O-RING PER AMM 72-15-00-960-801-A. LEAK CHECK GOOD. OK FOR SERVICE.
- [SDR HALA2023062100131](https://openairdocs.org/sdr/HALA2023062100131.md): Pump · faulty · Jun 20, 2023 · N202HA · Airbus A321271N · Fuel Boost Pump
  > ETOPS - IN CRUISE @ GL 330; ECAM: FUEL R TK PUMP 2 LO PR RAN ECAM SEL R TK PUMP 2 OFF CONT. TO HNL. REMOVED & REPLACED 26QA FUEL PUMP. REF A321 AMM 28-21-51-000-001-A & 28-21-51-400-001-A. CHECKS OK
- [SDR HALA2022120900306](https://openairdocs.org/sdr/HALA2022120900306.md): Blades · damaged · Dec 8, 2022 · N202HA · Airbus A321271N · Turbine Section
  > NR 2 ENGINE N2 VIBRATION AT 6.2 NEED TO ACCOMPLISH TSM 71-00-00-810-873-A PARAGRAPH 4.D. DURING BORESCOPE, FOUND LPT 3RD STAGE BLADES DAMAGED. PER POWERPLANT ENGINEER, MANUFACTURER EVALUATION, REQUIRES ENGINE REMOVAL. REMOVED AND REPLACED RH ENGINE S/N: P7714
- [SDR HALA2022120100304](https://openairdocs.org/sdr/HALA2022120100304.md): Blades · damaged · Nov 30, 2022 · N202HA · Airbus A321271N · Turbine Engine Compressor Section
  > NR 2 ENGINE N2 VIBRATION AT 6.2, DURING BORESCOPE, FOUND LPT 3RD STAGE BLADES DAMAGED. PER POWERPLANT ENGINEER, MANUFACTURER EVALUATION, REQUIRES ENGINE REMOVAL.
- [SDR HALA2022112300299](https://openairdocs.org/sdr/HALA2022112300299.md): Connector · unsecure · Nov 22, 2022 · N202HA · Airbus A321271N · Hydraulic Power System Wiring
  > ETOPS- UPON ENGINE 1 START, RECIEVED ECAM HYD B SYS LO PR. C/W TSM TASK 29-12-00-810-805-A. NO ACTIVE FAULTS. RESECURED PRESSURE SWITCH CONNECTORS. A/C OK FOR SERVICE.
- [SDR HALA2022012700031](https://openairdocs.org/sdr/HALA2022012700031.md): Unknown · odor · Jan 26, 2022 · N202HA · Airbus A321271N · Air Distribution System
  > @ 3000' ON FINAL APP WE GOT FUMES SMELL OF DIRTY SOX IN FLIGHT DECK. ON GND SWITCHED TO APU BLD RIGHT AWAY AND STILL HAD SMELL. SHUT DOWN #2 AND STILL HAD SMELL TO GATE. (NO SMELL IN BACK FOR FA'S) // CHECKED ENG 1, ENG 2 & APU FOR CORRECT OIL QUANTITIES AND F
- [SDR HALA2022011300013](https://openairdocs.org/sdr/HALA2022011300013.md): Seal · dirty · Jan 12, 2022 · N202HA · Airbus A321271N · Doors
  > IN CRUISE FLT, LOUD MID FREQ NOISE AVAILABLE IN FWD GALLEY LASTING -2HOURS. POSSIBLE IL DOOR SEAL LEAK. CHANGED CABIN ALT BY 500' WITH NO EFFECT. RESOLVED ON ITS OWN.// CHECKED & CLEANED DOOR SEALS AT 1L DOOR, PERFORMED PRESSURIZATION TEST IAW AMM 05-53-00-780
- [SDR HALA2021120600180](https://openairdocs.org/sdr/HALA2021120600180.md): Oil Filter · abnormal · Dec 5, 2021 · N202HA · Airbus A321271N · Airborne Auxiliary Power Unit (APU) System
  > ETOPS - APU AUTO SHUT DOWN // REMOVED AND INSTALLED NEW OIL FILTERS APU IAW AMM 49-91-41-200-002-A. INSPECTED METAL CHIP DETECTOR IAW AMM 49-91-42-200-004-A. APU START NORMAL. NO DEBRIS FOR FILTERS OR CHIP DETECTOR FOUND. A/C OK TO CONT.
- [SDR HALA2021051100061](https://openairdocs.org/sdr/HALA2021051100061.md): Igniter · faulted · May 7, 2021 · N202HA · Airbus A321271N · Engine Oil Cooler
  > ETOPS - ENG START 2 FAULT. ENG 2 IGN A FAULT. SUCCESSFUL AUTOSTART AFTER SECOND ATTEMPT. BTB// REMOVED AND REPLACED IGN PER AMM 74-21-01-00-801-A ON #2 ENG. OPS CHECK GOOD. OK TO CONTINUE
- [SDR HALA2020101900192](https://openairdocs.org/sdr/HALA2020101900192.md): Fire Detector · defective · Oct 18, 2020 · N202HA · Airbus A321271N · Fire Detection
  > ETOPS-ENGINE 2 FIRE LOOP A FAULT. REMOVED AND REPLACED FIRE DETECTION UNIT, PER AMM 26-12-34-000-001-A AND AMM 26-12-34-400-001-A. OPERATIONS TEST OK.
- [SDR HALA2020071600147](https://openairdocs.org/sdr/HALA2020071600147.md): Bleed Air Sys · faulted · Jul 15, 2020 · N202HA · Airbus A321271N · Pneumatic Indicating System
  > OPEN - ETOPS SIGNIFICANT SYSTEM - AIR ENG 2 BLEED FAULT. REPAIR IN WORK
- [SDR HALA2020021300036](https://openairdocs.org/sdr/HALA2020021300036.md): Engine · making metal · Feb 10, 2020 · N202HA · Airbus A321271N · Engine (Turbine/Turboprop)
  > ETOPS SIGNIFICANT SYSTEM - #1 ENG FBC MAG CHIP DETECTOR FOUND METAL. // PERFORMED AMM 79-00-00-281-802-A CH4 A SECTION 6.0 FINDINGS SENT TO MANAGEMENT. REF CASE NUMBER: CAS-69938-Q9M7V2 PRATT AND WHITNEY. LAB REF SEMUS816. LAB REF SEMUS817. NO FOLLOW UP ACTION
- [SDR HALA2019062540332](https://openairdocs.org/sdr/HALA2019062540332.md): Fire Detector · faulted · Jun 24, 2019 · N202HA · Airbus A321271N · Fire Detection
  > ETOPS - BTB - ECAM ENG 2 FIRE LOOP B FAULT AFTER ENG START. REMOVED AND REPLACED FIRE LOOP P/N 8891-48.
- [SDR HALA2019042900205](https://openairdocs.org/sdr/HALA2019042900205.md): Warning Light · false indication · Apr 28, 2019 · N202HA · Airbus A321271N · Turbine Engine Oil System
  > ETOPS SIGNIFICANT SYSTEM - ENG 1 OIL CHIP DETECTED ON LANDING. T/S PER TSM 79-35-00-810-808-A. NO CONTAMINATION FOUND ON CHIP DETECTORS. INSPECTED OIL FILTER, NO CONTAMINANTS FOUND. INSPECTED W03 HARNESS AND PHMU CONNECTIONS P10 AND P36 ALL LOOKS NORMAL RAN
- [SDR HALA2019042900203](https://openairdocs.org/sdr/HALA2019042900203.md): Warning Light · false activation · Apr 28, 2019 · N202HA · Airbus A321271N · Turbine Engine Oil System
  > ETOPS SIGNIFICANT SYSTEM - ENG 1 OIL CHIP ECAM ON TAXI IN - THEN EXTINGUISHED. // INSPECTED #1 ENG CHIP DETECTOR (NOTED NO SIGNS OF CONTAMINATION) PER AMM 79-00-00-281-802-A, VISUALLY INSPECTED, #1 ENG MAIN OIL FILTER (NOTED NO CONTAMINATION), RAN #1 ENG FOR 5
- [SDR HALA2019042900204](https://openairdocs.org/sdr/HALA2019042900204.md): Chip Detector · false indication · Apr 27, 2019 · N202HA · Airbus A321271N · Turbine Engine Oil System
  > ETOPS SIGNIFICANT SYSTEM - ECAM: ENG1 OIL CHIP DETECTED. // REMOVED AND REPLACED OIL DEBRIS SENSOR PER AMM 79-35-21-400-801-A. OPS CHECK GOOD. MESSAGE EXTINGUISHED OK FOR SERVICE.
- [SDR HALA2019042900202](https://openairdocs.org/sdr/HALA2019042900202.md): Warning Light · false activation · Apr 26, 2019 · N202HA · Airbus A321271N · Turbine Engine Oil System
  > ETOPS SIGNIFICANT SYSTEM - RECALL PAGE SHOWS ENGINE 1 CHIP DETECTOR FAULT. // PERFORMED INSPECTION OF THE MAGNETIC CHIP DETECTORS AMM 79-00-00-281-802-A (NOTED NO METAL PARTICLES). VISUAL INSPECTION OF #1 ENGINE OIL FILTER AMM 79-00-00-210-809-A, RUN #1 ENGINE
- [SDR HALA201904230198](https://openairdocs.org/sdr/HALA201904230198.md): Engine · making metal · Apr 22, 2019 · N202HA · Airbus A321271N · Engine (Turbine/Turboprop)
  > ETOPS SIGNIFICATION - UPON ENG START WHEN START SWITCH TO IGN/START, ECAM ENG 1 OIL CHP DETECT ILLUMINATED. ABORTED START, ECAM CLEARED, MX CONTROL IN HNL SAID OK TO START. NEXT START NORMAL. // PERFORMED TSM 79-35-00-810-808-A, FOUND 2 "MAGNETIC FINE" PARTICL
- [SDR HALA2019042320197](https://openairdocs.org/sdr/HALA2019042320197.md): Warning Message · false activation · Apr 20, 2019 · N202HA · Airbus A321271N · Turbine Engine Oil System
  > ETOPS SIGNIFICATION - ENG 1 OIL CHIP DETECTED BTB ON ENGINE ONE START. MESSAGE HAPPENED WHEN MODE SELECTOR PUT TO IGN / START. // PERFORMED TSM 79-35-00-810-808 CHIP DETECTORS CLEAN. NO ECAM MSG DISPLAYED. IDLE RUN ENGINE #1 FOR 5 MIN. NO FAULT NOTED. OK FOR S
- [SDR HALA2019042320196](https://openairdocs.org/sdr/HALA2019042320196.md): Warning Light · false activation · Apr 19, 2019 · N202HA · Airbus A321271N · Turbine Engine Oil System
  > ETOPS SIGNIFICATION - ON ENGINE START UP ENG 1 OIL CHIP DETECTED CAME UP ON ECAM AND THEN SELF CLEARED. PERFORMED TSM 79-35-00-810-808-A NO EVIDENCE OF METAL FOUND ON CHIP DETECTORS, ALSO ACCOMPLISHED ENGINE RUN OF #1 ENGINE FOR 5 MINUTES REOPENED COWLS AND
- [SDR HALA2019031900136](https://openairdocs.org/sdr/HALA2019031900136.md): Warning System · false activation · Mar 18, 2019 · N202HA · Airbus A321271N · Engine Oil Indicating System
  > ETOPS SIGNIFICANT SYSTEM - AFTER ENGINE SHUTDOWN. ENG 2 OIL CHIP DETECTED ECAM. PERFORMED INSPECTION OF NR 2 ENGINE MAGNETIC CHIP COLLECTORS PER AMM 79-00-00-281-802-A. NO CHIPS OR FLAKES NOTED. PERFORMED NR 2 ENGINE RUN. NO FAULTS NOTED. OK FOR CONTINUED SER
- [SDR HALA2019031100112](https://openairdocs.org/sdr/HALA2019031100112.md): Warning System · false activation · Mar 10, 2019 · N202HA · Airbus A321271N · Engine Oil Indicating System
  > ETOPS SIGNIFICANT SYSTEM - ENG NR 1 CHIP DETECT ON START FOR ~2-3 MINS BEFORE DISAPPEARING. INSPECTED CHIP DETECTOR AND MAIN OIL FILTER ON NR 1 ENG. NO METAL OR DEBRIS NOTED. PER TSM 79-35-00-810-808-A. RAN NR 1 ENG. NO MSG DISPLAYED. FADEC 1 GROUND REPOR
- [SDR HALA2019031200113](https://openairdocs.org/sdr/HALA2019031200113.md): Filter · odor · Mar 9, 2019 · N202HA · Airbus A321271N · Air Distribution System
  > OIL SMELL DETECTED AFTER TAXI IN FROM HIGH POWER RUN. PERFORMED DECONTAMINATION OF ECS PER AMM 21-00-00-615-002-A WITH APU BLEED UP TO STEP W(STAGE 2 CLEANING). ACCOMPLISHED AMM 21-00-00-615-002-A STEP W, STILL HAD OIL SMELL DETECTED, REMOVED AND REPLACED RECI
- [SDR HALA2019030500086](https://openairdocs.org/sdr/HALA2019030500086.md): Unknown · odor · Mar 4, 2019 · N202HA · Airbus A321271N · Air Distribution System
  > STRONG ODOR IN CABIN ON POWER UP FROM IDLE DECENT @3000' MSL. ODOR LASTED 5 MIN IN BACK CABIN AND 5 SEC IN COCKPIT. PERFORMED TSM 05-50-00-810-831. RAN BOTH NR 1/2 ENGINES. RAN AND ISOLATED EACH PACK WITH EACH ENGINE AND APU. COULD NOT DUPLICATE PROBLEM. NO OD
- [SDR HALA2019030400083](https://openairdocs.org/sdr/HALA2019030400083.md): Fire Loop · faulty · Mar 4, 2019 · N202HA · Airbus A321271N · Fire Detection
  > ETOPS SIGNIFICANT SYSTEM - ENG 1 FIRE LOOP B FAULT ILLUMINATED 3 TIMES, STAYED ON FOR 15 SEC TO 1.5 MIN. REMOVED AND REPLACED NR 1 ENGINE PYLON FIRE LOOP B IAW AMM 26-12-16-04 CONF 21. NO ECAM MESSAGES DISPLAYED, OPS TEST GOOD PER AMM 26-12-00-710-002-A. OK FO
- [SDR HALA2019030400082](https://openairdocs.org/sdr/HALA2019030400082.md): Warning System · false activation · Mar 3, 2019 · N202HA · Airbus A321271N · Fire Detection
  > ETOPS SIGNIFICANT SYSTEM - ECAM MESSAGE: ENG 1 FIRE LOOP B FAULT ILLUMINATED TWICE IN 5 MINUTE,1.5 HRS PRIOR TO TOD THEN OPS NORMAL. PERFORMED OPERATIONAL TEST OF ENGINE FIRE AND OVERHEAT DETECTION SYSTEMS PER AMM 26-12-00-710-002A. ALL TEST PASSED, AIRCRAFT O
- [SDR HALA2019030400081](https://openairdocs.org/sdr/HALA2019030400081.md): Warning System · false activation · Mar 3, 2019 · N202HA · Airbus A321271N · Fire Detection
  > ETOPS SIGNIFICANT SYSTEM - ECAM MESSAGE: ENG1 FIRE LOOP B FAULT ILLUMINATED 4 DIFFERENT TIMES WITHIN 10 MINUTES AND THEN OPS NORMAL. PERFORMED TSM 26-12-00-810-804, PERFORMED GVI OF ENG 1 LOOP B FIRE DETECTORS (4WD1)(4001WD2)(4002WD2)(41WD1)AND (42WD1). NO DEF
- [SDR HALA2019030100076](https://openairdocs.org/sdr/HALA2019030100076.md): Unknown · odor · Feb 28, 2019 · N202HA · Airbus A321271N · Air Distribution System
  > DESCENDING THROUGH 3,000 FT A MILD ODOR THAT SMELLED LIKE DIRTY WET SOCKS WAS OBSERVED IN THE COCKPIT AND 1L JUMPSEAT. THE ODOR WAS GONE BY 1,000 FT. PERFORMED INSPECTION OF ENG 1&2 & PACKS 1&2 PER TSM TASK 05-50-00-810-831A. NO LEAKS OR ODOR PRESENT. OK TO CO
- [SDR HALA2019030100077](https://openairdocs.org/sdr/HALA2019030100077.md): Warning System · false activation · Feb 27, 2019 · N202HA · Airbus A321271N · Fire Detection
  > ETOPS SIGNIFICANT SYSTEM - ENG 1 LOOP B ECAM ILLUMINATED FOR 2-3 MINUTES THEN WENT AWAY. PERFORMED OPERATIONAL TEST IAW AMM 26-12-00, NO FAULT AND DEFECT NOTED, OK TO CONTINUE.
- [SDR HALA2019022800074](https://openairdocs.org/sdr/HALA2019022800074.md): Unknown · odor · Feb 27, 2019 · N202HA · Airbus A321271N · Air Distribution System
  > STRONG ODOR OF BURNING/MELTING PLASTIC/OIL THROUGHOUT COCKPIT LAST 15 MIN OF FLT. NO SMELL IN CABIN REPORTED. STRONGEST SMELL AT 8000FT.STRONG ODOR OF BURNING/MELTING PLASTIC/OIL THROUGHOUT COCKPIT LAST 15 MIN OF FLT. NO SMELL IN CABIN REPORTED. STRONGEST SMEL
- [SDR HALA2019022600070](https://openairdocs.org/sdr/HALA2019022600070.md): Unknown · odor · Feb 25, 2019 · N202HA · Airbus A321271N · Air Distribution System
  > STRONG ODOR OF BURNING/MELTING PLASTIC THOUGHT OUT THE CABIN LAST 10 MIN OF FLIGHT.// COMPLIED WITH TSM 05-50-00-810-831-A. RAN PACK ON ENG 1 ENG 2 AND APU SEPARATELY. CONFIRMED WITH HA MAINTENANCE CONTROL. NO SMELL RE-PRODUCIBLE THRU SUGGESTED PROCEDURES.
- [SDR HALA2019022600069](https://openairdocs.org/sdr/HALA2019022600069.md): Chip Detector · false indication · Feb 25, 2019 · N202HA · Airbus A321271N · Engine Oil Indicating System
  > ETOPS SIGNIFICANT SYSTEM - ENG 2 OIL CHIP DETECTED ECAM. // PERFORMED #2 ENG OIL CHIP DETECTOR INSPECTION PER TSM 79-35-00-810-808A. NO CHIP NOTED, RUN AND LEAKED CHK GOOD, MESSAGE ERASED OK TO CONTINUE.
- [SDR HALA2019022500062](https://openairdocs.org/sdr/HALA2019022500062.md): Compressor · leaking · Feb 22, 2019 · N202HA · Airbus A321271N · Turbine Engine Compressor Section
  > SOCKS SMELL ON DESCENT OUT OF 8000' ODOR STRONGEST OVER WING INTENSIFYING AT LANDING.// CONFIRMED ODOR COMING FROM #2 ENG WITH BOTH PACKS RUNNING REF. TSM 71-00-00-810-847 ACP'D TO STEP 5. NO CONTAMINATION FOUND. NEXT STEP BORESCOPE. ACCOMPLISHED TSM 71-00-00-
- [SDR HALA2019011700029](https://openairdocs.org/sdr/HALA2019011700029.md): Warning System · false activation · Jan 16, 2019 · N202HA · Airbus A321271N · Smoke Detection
  > SUP - MX STATUS MSG SMOKE DISPLAYED (CLASS II MAINTENANCE MESSAGES DISPLAYED ON ECAM STATUS PAGE OF ECAM SYSTEM DISPLAY FAULT(S) INDICATED BY SMOKE (WITH MOD 30354 OR WITH MOD 33100). PERFORMED TSM 26-16-00-810-821-A, NO FAULTS DETECTED. MAINT STATUS "SMOKE" G

Next page: https://openairdocs.org/aircraft/N202HA/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 = 'N202HA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N202HA/reports

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