# Service difficulty reports: N604NK

A list on [N604NK](https://openairdocs.org/aircraft/N604NK.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 · 78 reports

- [SDR GTIA2025122639223](https://openairdocs.org/sdr/GTIA2025122639223.md): A/C Pack · odor · Dec 23, 2025 · N604NK · Airbus A320232 · Cabin Cooling System
  > FUME EVENT ON TAKEOFF PACK 1-REF LP-6019368-2, OIL LEAK ON APU GENERATOR FOUND AND COORECTED AND PERFORMED DECONATMINATION OF THE BLEED AIR DUCTS PER PER TSM 05-50-00-810-831. CONTINUED TSM AND PERFORMED DECONTAMINATION OF THE ENVIRONMENTAL CONTROL SYSTEM IAW
- [SDR GTIA2025122239219](https://openairdocs.org/sdr/GTIA2025122239219.md): A/C Pack · odor · Dec 20, 2025 · N604NK · Airbus A320232 · Cabin Cooling System
  > PILOT REPORTED, JUST BEFORE APPROACH FA CALLED TO REPORT FUMES IN FRONT AND BACK OF CABIN. PERFORMED ODOR IDENTIFICATION IAW TSM 05-50-00-810-831-A. SUSPECT PACK 1 TO BE CAUSE OF ODOR.
- [SDR GTIA2025110339163](https://openairdocs.org/sdr/GTIA2025110339163.md): Unknown · odor · Oct 30, 2025 · N604NK · Airbus A320232 · Air Distribution System
  > DURING DESCENT BELOW 10000FT FAS REPORTED A STRONG DIRTY SOCK SMELL. DESCRIPTION OF ODOR/FUMES: CONTINOUS AND DISCOMFORTABLE, DIRTY SOCKS/ ACRID/ PUNGENT/ IRRITATING/ BURNING EYE SMELL. SOURCE: CABIN AIR SUPPLY VENTS. FWD CABIN AND MID CABIN. NO VISIBLE SMOKE
- [SDR GTI2025F00009](https://openairdocs.org/sdr/GTI2025F00009.md): Unknown · odor · Oct 30, 2025 · N604NK · Airbus A320232 · Air Distribution System
  > DURING DESCENT BELOW 10000FT FAS REPORTED A STRONG DIRTY SOCK SMELL. DESCRIPTION OF ODOR/FUMES: CONTINOUS AND DISCOMFORTABLE, DIRTY SOCKS/ ACRID/ PUNGENT/ IRRITATING/ BURNING EYE SMELL. SOURCE: CABIN AIR SUPPLY VENTS. FWD CABIN AND MID CABIN. NO VISIBLE SMOKE
- [SDR GTIA2025090239061](https://openairdocs.org/sdr/GTIA2025090239061.md): Unknown · odor · Sep 1, 2025 · N604NK · Airbus A320232 · Air Distribution System
  > FA REPORTED BAD ODOR FROM AFT LAV ON TAKE OFF & DURING DECENT -PERFORM INSP OF AFT LAV IAW AMM 25-43-00.NO DEFECTS FOUND AT THIS TIME.A/C OK TO RETURN TO SVC
- [SDR GTIA2025060938946](https://openairdocs.org/sdr/GTIA2025060938946.md): Thermocouple · out of limits · Jun 5, 2025 · N604NK · Airbus A320232 · Engine EGT/TIT Indicating System
  > ENG. ONE EGT OVERLIMIT-FOUND #1 ENG THERMOCOUPLES READING OUT OF LIMITS. REPLACED ALL THERMOUCOUPLES ON #1 ENG PER AMM 77-21-15. OPS CHECK NORMAL. REPLACED #1 ENG LPC BLEED MASTER ACTUATOR PER AMM 75-31-42. OPS & LEAK CHECK NORMAL. THIS CLOSES RIN-17185.
- [SDR GTIA2025060538944](https://openairdocs.org/sdr/GTIA2025060538944.md): Panel · damaged · Jun 5, 2025 · N604NK · Airbus A320232 · Passenger/Crew Doors
  > "L1 DOOR DENT FWD LOWER EDGE OF 2.5INCH L X. 187INCH D ALLOWABLE DAMAGE AS PER SRM 52-10-00 PB 101 DIA 106, FIG 109 REPAIR CATEGORY B. HFEC I NSP DUE IN 3000FC AS PER NTM CH 51-10-08 PB 601. (GENERAL WATCH ITEM). RAF 3336560-02 CREATED AND SDR 3336560-02 CREA
- [SDR GTIA2025060538943](https://openairdocs.org/sdr/GTIA2025060538943.md): Skin Panel · damaged · Jun 5, 2025 · N604NK · Airbus A320232 · Fuselage Main, Plate/Skin
  > CRACK INDICATION ON FRAME 16 LH SIDE OPEN FASTENER HOLE H1 AND H2 IN CROSSBEAM SPLICING AREA. H1 LENGTH.136 INCH, H2 LENGTH.146 INCH. PERFORMED PERMANENT REPAIR ON FRAME 16LH SIDE OPEN FASTENER HOLE H1 ON CROSSBEAM SPLICING AREA AT I OCLOCK I.A.W. DWG R5311
- [SDR GTIA2025060538942](https://openairdocs.org/sdr/GTIA2025060538942.md): Skin Panel · damaged · Jun 5, 2025 · N604NK · Airbus A320232 · Wing, Plate/Skin
  > LEFT WING - TOP SKIN PANEL 2 - RIB 9-10 UPPER & STRG11, TE OH: RIB 8-9 UPPER/LOWER, RIB 11 & RIB 14 LOWER - CORROSION. RIB 8-9 L 2.577 W 2.463 D.113, RIB 11 L 2.546 W 2.074 D.118, RIB 9-10 L 1.592 W.362 D.028, RIB 14 L 5.010 W 2.363 D.143. PERFORMED PE
- [SDR GTIA2025060238937](https://openairdocs.org/sdr/GTIA2025060238937.md): Power Supply · inoperative · Jun 1, 2025 · N604NK · Airbus A320232 · Emergency Lighting
  > DURING BITE TEST OF EMERGENCY POWER SUPPLY UNITS WAS FOUND FAULT EPSU 10WL-REMOVED AND REPLACED EPSU IOWL I.A.W AMM 33-51-38-000-001-A AND AMM 33-51-38-400-001-A
- [SDR GTIA2025060238936](https://openairdocs.org/sdr/GTIA2025060238936.md): Slide · faulty · Jun 1, 2025 · N604NK · Airbus A320232 · Escape Slide
  > REPLACE SLIDE RAFT PASSENGER CREW DOOR 831 FWD GALLEY ARE I.A.W. TSM 25*-62-000-810-811-A DUE TO INTERNAL LIGHT FAULT -REPLACED SLIDE RAFT PASSENGER CREW DOOR 831 AT FWD GALLEY AREA I.A.W. AMM 25-62-44-400-007.
- [SDR GTIA2025042138860](https://openairdocs.org/sdr/GTIA2025042138860.md): Feeder Cable · damaged · Apr 16, 2025 · N604NK · Airbus A320232 · Electrical Power System Wiring
  > "IN FLIGHT AUTO FLIGHT YAW DAMPER 1, RUDDER TRIM 1 FAULT, RUDDER TRV LIM 1 SEE LOG 3437049 & 3437048-REMOVED # 1 ENG PYLON IDG FEEDER CABLE HARNESS & CONNECTOR 400VCI IAW AMM 24-92-00.INSTALLED FEEDER CABLE HARNES & CONNECTOR 400 VCI IAW AMM 24-92-00 OPS CK G
- [SDR GTIA2025041438852](https://openairdocs.org/sdr/GTIA2025041438852.md): Elec Connector · inoperative · Apr 12, 2025 · N604NK · Airbus A320232 · Auto Flight System Wiring
  > IN CRUISE AT FL 340 AUTOPILOT DISCONNECTED AIRCRAFT PITCHED UP AND RIGHT. ECAM ELEC GEN 1 FAULT, AUTO FLT YAW DAMPER 1, RUD TRIM 1 FAULT, RUD TRU CIM 1. FCOM AND EQRH RAN. RESETS SUCCESSFUL. ABOUT 30 MINUTES LATER SAME AXACT ECAMS. ELEC GEN 1 RESET UNSUCCESSFU
- [SDR GTIA2025040738836](https://openairdocs.org/sdr/GTIA2025040738836.md): Unknown · odor · Apr 5, 2025 · N604NK · Airbus A320232 · Air Distribution System
  > FAS REPORT FUME SMELL AT 5,000 ON APPROACH CONFIGURED FLAPS 1. DESCRIPTION OF ODOR/FUMES: PERSISTENT, MOLDY SMELL. APPARENT CABIN SOURCE: UNKNOWN. FWD CABIN, MID CABIN, AFT CABIN, AND FLIGHT DECK. NO VISIBLE SMOKE/HAZE. NO MEDICAL ATTENTION REQUIRED.-PERFORMED
- [SDR GTIA2025040538834](https://openairdocs.org/sdr/GTIA2025040538834.md): Sensor · faulted · Apr 2, 2025 · N604NK · Airbus A320232 · Trailing Flap Position Indicating System
  > ON APPROACH WHEN SELECTING FLAPS 2 GOT ECAM F/CTL FLAPS LOCKED WING TIP BRK ON-FOLLOWED TSM 27-51-00-810-819-A. PERFORMD MANUAL RETRACTION OF THE FLAPS IAW AMM 27-50-00-866-012-A AND READOUT OF THE FLAP POSITION PICKOFF UNIT AMM 27-50-00-860-801-A. R/R SFCC-2
- [SDR GTIA2024101238425](https://openairdocs.org/sdr/GTIA2024101238425.md): Megaphone · no test · Oct 9, 2024 · N604NK · Airbus A320232 · Emergency Equipment
  > AFT FA MEGAPHONE INOP-R&R AFT FA MEGAPHONE IAW NKS DRAWING A320 EMER-EQUIP REV. 4. A/C OK FOR SVC.
- [SDR GTIA2024062438194](https://openairdocs.org/sdr/GTIA2024062438194.md): Switch · faulty · Jun 23, 2024 · N604NK · Airbus A320232 · Hydraulic Indicating System
  > ON TAKEOFF ECAM: HYD Y RSVR LO LVL-AS PER TSM 29-13-00-810-816-A R&R SWITCH LOW LEVEL REF: AMM 29-13-41. OPS CHECK GOOD MESSAGE CLEARED
- [SDR GTIA2024061438175](https://openairdocs.org/sdr/GTIA2024061438175.md): Actuator · overtemp · Jun 12, 2024 · N604NK · Airbus A320232 · Engine Indicating System
  > ENG #2 OVERTEMP ON TOGA TAKE OFF PACKS OFF TEMP 637C 10 SECONDS-REF TSM 77-00-00-810-818-B STEP 4(F)9, FOUND EGT HARNESS AND JUNCTION BOX CHAFFED. R/R EGT HARNESS AND JUNCTION BOX IAW AMM 77-21-43. SEE LOGPAGE 3340675-2 FOR OPS CHECK.
- [SDR GTIA2023121137675](https://openairdocs.org/sdr/GTIA2023121137675.md): Fan · odor · Dec 8, 2023 · N604NK · Airbus A320232 · Air Distribution Fan
  > LEVEL OFF FL 350 FUME SMELL IN THE COCKPIT BLOWER FAULT. -R+R AVIONICS FAN BLOWER VALVE IAW AMM 21-26-51. OPS CK GOOD. PERFORMED PACK BURNOUT IAW TSM 05-50-00-810-831-A NO FUMES NOTED DURING TEST. OK FOR SVC.
- [SDR GTIA2022082636615](https://openairdocs.org/sdr/GTIA2022082636615.md): None · cracked · Aug 24, 2022 · N604NK · Airbus A320232 · Fuselage Main, Plate/Skin
  > CRACK FOUND ON MILLED FRAME AT FR43L STGR 24L TO 18L. RAF-01 2803718-01 OPENED. REF EO 5331-2059.-REPLACED FRAME 43LH (FOOT FRAME) IAW EA 53-0355-22 AND EO 5331-2241 REF AEROMAN NR 2022-391291
- [SDR GTIA2022082636614](https://openairdocs.org/sdr/GTIA2022082636614.md): None · corroded · Aug 24, 2022 · N604NK · Airbus A320232 · Fuselage Main, Structure
  > CORROSION ON BORE OF RH ELEVATOR FITTING #6. RAF 01 2803723-2 GENERATED-REPAIRED RH ELEVATOR HINGE FITTING #6 IAW SRM 55-26-41-300-006, FIRST INSPECTION THRESHOLD IS 6 YEARS AFTER COMPONENT FIRST FLIGHT, SUBSEQUENT INSPECTIONS AT INTERVAL OF 6 YEARS, INSPECTI
- [SDR GTIA2022082636613](https://openairdocs.org/sdr/GTIA2022082636613.md): None · corroded · Aug 24, 2022 · N604NK · Airbus A320232 · Fuselage Main, Structure
  > CORROSION ON BORE OF LH ELEVATOR FITTING # 4. RAF 01-2803725-2 GENERATED-REPAIRED LH ELEVATOR HINGE FITTING #4 IAW SRM 55-26-41-300-005 FIRST INSPECTION THRESHOLD IS 6 YEARS AFTER COMPONENT FIRST FLIGHT SUBSEQUENT INSPECTIONS INTERVAL IS 6 YEARS INSPECTION TY
- [SDR GTIA2022082636612](https://openairdocs.org/sdr/GTIA2022082636612.md): None · corroded · Aug 24, 2022 · N604NK · Airbus A320232 · Fuselage Main, Structure
  > CORROSION ON BORE OF LH ELEVATOR FITTING # 1, 2, 3 & 5. RAF 01-2803724-2 GENERATED-REPAIRED LH ELEVATOR HINGE FITTING #1, 2, 3 AND 5 IAW SRM 55-26-41-300-004. FIRTS INSPECTION THRESHOLD IS 6 YEARS AFTER COMPONENT FIRST FLIGHT, SUBSEQUENT INSPECTIONS INTERVAL
- [SDR GTIA2022082636611](https://openairdocs.org/sdr/GTIA2022082636611.md): None · corroded · Aug 24, 2022 · N604NK · Airbus A320232 · Fuselage Main, Structure
  > CORROSION ON BORE OF RH ELEVATOR FITTING #4. RAF-012803724-1 GENERATED-REPAIRED RH ELEVATOR HINGE FITTING #4 IAW SRM 55-26-41-300-005 FIRST INSPECTION THRESHOLD IS 6 YEARS AFTER COMPONENT FIRST FLIGHT, SUBSEQUENT INSPECTIONS INTERVAL IS 6 YEARS. INSPECTION TY
- [SDR GTIA2022082636610](https://openairdocs.org/sdr/GTIA2022082636610.md): None · corroded · Aug 24, 2022 · N604NK · Airbus A320232 · Fuselage Main, Structure
  > CORROSION ON BORE OF LH ELEVATOR FITTING # 6. RAF 01-2803725-1 GENERATED-REPAIRED LH ELEVATOR HINGE FITTING #6 IAW SRM 55-26-41-300-006 FIRST INSPECTION THRESHOLD IS 6 YEARS AFTER COMPONENT FIRST FLIGHT SUBSEQUENT INSPECTIONS INTERVAL IS 6 YEARS INSPECTION TY
- [SDR GTIA2022082636609](https://openairdocs.org/sdr/GTIA2022082636609.md): None · none · Aug 24, 2022 · N604NK · Airbus A320232 · Elevator Structure
  > LH ELEVATOR INBD & OUTB SERVO CONTROL ACTUATOR BUSHINGS REQUIRE REPLACEMENT-REPAIRED LH ELEVATOR INBD AND OUTBD SERVOCONTROL ACTUATOR FITTING, BUSHINGS REPLACED IAW TI 5513-1602 SRM 55-26-47-300-002 AND CMM 55-21-15-410-801-A01 INSPECTION THRESHOLD IS 6 YEARS
- [SDR GTIA2022082636608](https://openairdocs.org/sdr/GTIA2022082636608.md): None · corroded · Aug 24, 2022 · N604NK · Airbus A320232 · Fuselage Main, Structure
  > CORROSION ON RH ELEVATOR FITTINGS 1, 2, 3 &5. RAF-01 2803723-1 GENERATED-REPAIRED RH ELEVATOR HINGE FITTING #1, 2, 3 AND 5 IAW SRM 55-26-41-300-004 FIRST INSPECTION THRESHOLD IS 6 YEARS AFTER COMPONENT FIRST FLIGHT, SUBSEQUENT INSPECTIONS AT INTERVALS OF 6 YE
- [SDR GTIA2022082636607](https://openairdocs.org/sdr/GTIA2022082636607.md): None · damaged · Aug 24, 2022 · N604NK · Airbus A320232 · Wing Structure
  > RH SPOILER #3 CENTER HINGE FITTING HAS DAMAGED AND MIGRATING BUSHINGS. RAF-01 2803728-1 OPENED-REPAIRED SPOILER #3 CENTER HINGE FITTING IAW EA #57-0376-22 PANT #1 REV. #0 CAT C REPAIR INSPECTION TIME LINE 6 MONTHS ONE TIME
- [SDR GTIA2022082636606](https://openairdocs.org/sdr/GTIA2022082636606.md): None · none · Aug 24, 2022 · N604NK · Airbus A320232 · Elevator Structure
  > RH ELEVATOR INBD & OUTBD SERVO CONTROL ACTUATOR BUSHINGS REQUIRE REPLACEMENT. RAF-01 2803727-1 GENERATED-REPAIRED RH ELEVATOR INBD AND OUTBD SERVOCONTROL ACTUATOR FITTING, BUSHINGS REPLACED IAW TI 5513-1602 SRM 55-26-47-300-002 AND CMM 55-21-15-410-801-A01 IN
- [SDR GTIA2022021436270](https://openairdocs.org/sdr/GTIA2022021436270.md): Megaphone · damaged · Feb 11, 2022 · N604NK · Airbus A320232 · Escape Slide
  > FWD MEGAPHONE VOLUME KNOB MISING -R/R FWD MEGAPHONE AS REQ'D IAW EMQ DRAWING A320
- [SDR GTIA2021050335705](https://openairdocs.org/sdr/GTIA2021050335705.md): Seal · leaking · Apr 30, 2021 · N604NK · Airbus A320232 · Air Distribution System
  > "FUME EVENT ON APROACH / LANDING F/A IN AFT NOTICED IT FIRST THEN THE COCKPIT. ( PACKS A320 WITH MOD 31283/MP P7125 (FWC H2-F1 STND) AND WITH MOD. 30626/MP K6443 (ENHANCED ECS) - FAULT CAUTIONS ASSOCIATED WITH OPERATIVE SIDE NOT DISPLAYED)-R & R LH RECIRCULAT
- [SDR GTIA2021032935657](https://openairdocs.org/sdr/GTIA2021032935657.md): A/C Pack · odor · Mar 25, 2021 · N604NK · Airbus A320232 · Cabin Cooling System
  > DIRTY SOCK SMELL ON CLIMB OUT OF EWR TURNED PACK 1 OFF SMELL SUBSIDED ON ARRIVAL INTO FLL AT 8000 SMELL RETURNED TURNED PACK 2 OFF SMELL SUBSIDED-PERFORMED PACK # 1 + # 2 BURN OUT WITH APU + ENG 1+2 IAW TSM 05-50-00 AFTER BURN OUT NO ODOR NOTED AT THIS TIME
- [SDR GTIA2020123135526](https://openairdocs.org/sdr/GTIA2020123135526.md): Unknown · odor · Dec 30, 2020 · N604NK · Airbus A320232 · Air Distribution System
  > FUME EVENT DESCENDING THROUGH 4000 FEET DIRTY SOCKS SMELL. AFT FA REPORTED STRONGEST SMELL COMING FROM ROWS 14 AND BACK. ACCOMPLISHED TSM 05-50-810-831 FOR CABIN ODOR IDENTIFICATION USED AEROTRACER FOUND NO CONTAMINATION OR ODORS PERFORMED ENGINE 1 AND 2 RUN
- [SDR GTIA2019102874739](https://openairdocs.org/sdr/GTIA2019102874739.md): A/C Pack · odor · Oct 27, 2019 · N604NK · Airbus A320232 · Cabin Cooling System
  > FA REPORTED ATRONG SMELL IN CABIN REAR. ACCOMPLISH COM PROCEDURE W PACK 2 OFF. SMELL DISSIPATED.-PERFORMED TSM 05-50-00-810-831-A. PERFORMED PACK BURN OF #1 AND #2 PACK. FOUND ODOR TO BE TYPE 9. NO ODORS NOTED. NO DEFECTS FOUND.
- [SDR GTIA2019081534553](https://openairdocs.org/sdr/GTIA2019081534553.md): Proximity Sensor · out of limits · Aug 13, 2019 · N604NK · Airbus A320232 · Landing Gear Position and Warning
  > LG NOT UPLOCKED, L/G SYS DISAGREE, LG DOORS NOT CLOSED CAUTIONS AFTER GEAR SELECTED UP. AIR RETURN TO DEPARTURE. R & R THE PROXIMITY SENSOR 25GA IAW AMM 32-31-73, FOUND BOTH SENSORS OUT OF LIMITS. ADJUSTED AS REQUIRED IAW AMM 32-31-73 220-078. LGCIU TEST
- [SDR GTIA2019071903491](https://openairdocs.org/sdr/GTIA2019071903491.md): Warning System · activated · Jul 19, 2019 · N604NK · Airbus A320232 · Engine Vibration Analyzer
  > ENG 1 N2 VIB INDICIATION WENT TO AMBER XX ON TAKEOFF ROLL THEN, ENG VIB SYS FAULT APPEARED ON INITIAL CLIMB CLEARED + REAPPEARED SEVERAL TIMES BEFORE LANDING ( ECAM INDICATIONS (LOWER DISPLAY) N2 VIBRATION)--
- [SDR GTIA2019071703488](https://openairdocs.org/sdr/GTIA2019071703488.md): Unknown · contaminated · Jul 17, 2019 · N604NK · Airbus A320232 · Air Distribution Fan
  > FUME EVENT FA REPORTED FUMES IN BACK ON FINAL APPROACH LANDED PERFORMED COM PROCEDURE. FOUND UNKNOWN LIQUID BETWEEN FWD CARGO DOOR PANELS, REMOVED PANELS TO CLEAN SEALS AN DPANELS INSTALLED PANELS PER 53-22-14 R/R RECIRCULATION FILTERS PER AMM 21-21-41. PERFO
- [SDR GTIA2019060303378](https://openairdocs.org/sdr/GTIA2019060303378.md): Unknown · odor · May 30, 2019 · N604NK · Airbus A320232 · Air Distribution System
  > FWD F/A REPORTS DIRTY SOCK SMELL DURING APPROACH. AFTER TURNING PACK 1 OFF SMELL SEEMED TO DISSIPATE-PERFORMED OPERATION CHECK OF PACK 1 & 2 IAW AMM 21-63-60. NO DEFECTS FOUND. RUNNING BOTH PACKS FULL HOT/FULL COLD 30 MINS
- [SDR GTIA2019050103316](https://openairdocs.org/sdr/GTIA2019050103316.md): Unknown · odor · May 1, 2019 · N604NK · Airbus A320232 · Air Distribution System
  > MUSKY ODOR IN COCKPIT AS WELL AS REPORTED BY, I/A @ AROUND ROW 4, AND 18 ( APU SYSTEM)--
- [SDR GTIA2019050103315](https://openairdocs.org/sdr/GTIA2019050103315.md): Ecs · contaminated · May 1, 2019 · N604NK · Airbus A320232 · Air Distribution System
  > THROUGH 12,000 FT DIRTY SOCK ODOR PERSISTED UNTIL AFTER LANDING. QRM PROCEDURE WAS COMPLIED WITH TO NO AVAIL PACK 1 OFF OR PACK 2 OFF DID NOT MAKE SMELL GO AWAY-PERFORMED DECONTAMINATION OF THE ECS WITH NR 1 AND NR 2 ENG. IAW AMM 21-00-00. OPS CHECK GOOD. NO O
- [SDR GTIA2019041703288](https://openairdocs.org/sdr/GTIA2019041703288.md): Garlock Seal · leaking · Apr 17, 2019 · N604NK · Airbus A320232 · Turbine Engine Oil System
  > ODOR IN AFT GALLEY (DIRTY SOCK SMELL). TURNED PACK 2 OFF PER PROCEDURE. ODOR ELIMINATED. PROCEEDED W/O EVENT ( PACKS A320 WITH MOD 31283/MP P7125 (FWC H2-F1 STND) AND WITH MOD. 30626/MP K6443 (ENHANCED ECS) - FAULT CAUTIONS ASSOCIATED WITH OPERATIVE SIDE NOT
- [SDR GTIA2018092002850](https://openairdocs.org/sdr/GTIA2018092002850.md): Megaphone · broken · Sep 18, 2018 · N604NK · Airbus A320232 · Emergency Equipment
  > DURING RON CHECK, FOUND R2 DOOR FLIGHT ATTENDANT MEGAPHONE BROKEN. R&R OF R2 DOOR FLIGHT ATTENDANT MEGAPHONE IAW EMERGENCY LAYOUT DRAWING.
- [SDR GTIA2018090502831](https://openairdocs.org/sdr/GTIA2018090502831.md): Not Reported · dented · Sep 4, 2018 · N604NK · Airbus A320232 · Fuselage Main, Frame
  > FOUND DENT FR8-9 RT LATERAL STR TO RT SIDE STR. PERFORMED A DOUBLER REPAIR AS PER EO 5311-1854.
- [SDR GTIA2018031502522](https://openairdocs.org/sdr/GTIA2018031502522.md): Unknown · odor · Mar 15, 2018 · N604NK · Airbus A320232 · APU Bleed Air System
  > STRONG ODOR DURING ACTIVATION OF THE APU BLEED. TROUBLESHOT IAW TSM 05-50-00-810-831-A. PERFORMED GVI OF APU COMPARTMENT, NO EVIDENCE OF OIL, COULD NOT DUPLICATE. ACFT OK FOR SERVICE
- [SDR GTIA2018012802369](https://openairdocs.org/sdr/GTIA2018012802369.md): Flashlight · inoperative · Jan 28, 2018 · N604NK · Airbus A320232 · Emergency Equipment
  > L1 FA FLASHLIGHT INOPERATIVE. R & R THE FLASHLIGHT IAW DRAWING NK320-232-EQ REV4. OPS CHECKED GOOD.
- [SDR GTIA2017091702173](https://openairdocs.org/sdr/GTIA2017091702173.md): Seal · leaking · Sep 17, 2017 · N604NK · Airbus A320232 · Turbine Engine Oil System
  > DIRTY SOCK ODOR STARTED AROUND 3000 FT IT WAS VERY FAINT IN THE COCKPIT BUT USED OXYGEN MASKS.THE F/A'S REPORTED A DIRTY SOCK ODOR ON THE GROUND AFTER. ODOR SEEMS WORSE IN CABIN. PERFORMED TSM 05-50-00-810-831A AND R & R NR 1 AND NR 2 ENGINE DEOILER SEALS I
- [SDR GTIA2017052401941](https://openairdocs.org/sdr/GTIA2017052401941.md): Oxygen Mask · unwanted deploy · May 24, 2017 · N604NK · Airbus A320232 · Passenger Oxygen System
  > PAX OXYEGEN MASK 11 E IS DEPLOYED. REPACKED OXYGEN MASKS AT ROW 11 DEF PER AMM 35-21-43.
- [SDR GTIA2017041401873](https://openairdocs.org/sdr/GTIA2017041401873.md): Oxygen Mask · damaged · Apr 14, 2017 · N604NK · Airbus A320232 · Crew Oxygen System
  > CAPTAIN`S OXYGEN MASK HOSE TO MASK APPEARS BROKEN, IT LEAKS OXYGEN WHEN HOSE IS MOVED AROUND AND IS NOT SEATED FULLY TO AGAINST THE MASK. R & R THE OBSERVER OXYGNE MASK IAW AMM 35-12-41. LEAK CHECKED GOOD. OPS CHECKED GOOD.
- [SDR GTIA2017040601866](https://openairdocs.org/sdr/GTIA2017040601866.md): A/C Pack · odor · Apr 6, 2017 · N604NK · Airbus A320232 · Cabin Cooling System
  > RA REPORTED ODOR IN AFT CABIN DURING CLIMB WENT AWAY AFTER 5 MIN. ODOR RETURNED ON DESCENT APPROACH. TURNED OFF PACK 1 ODOR WENT AWAY. PERFORMED PACK 1 BURNOUT IAW AMM 21-00-00-615-002-A.NO NOTED DEFECTS. THIS CLEARS DMI 2177810-1. PLACARD REMOVED.
- [SDR GTIA2017031401829](https://openairdocs.org/sdr/GTIA2017031401829.md): Packing · damaged · Mar 14, 2017 · N604NK · Airbus A320232 · Turbine Engine Oil System
  > FUME EVENT DURING FINAL DESCENT AND APPROACH INTO PBI 28R. FAULT CAUTIONS ASSOCIATED WITH OPERATIVE SIDE NOT DISPLAYED. PERFORMED A CLEANING OF THE ECS TO PACK NR 2 IAW AMM 21-00-00, NO CONTAMINATION FOUND, LEAK CHECK GOOD, OPS CHECK GOOD. PRECAUTIONARY FOUND

Next page: https://openairdocs.org/aircraft/N604NK/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 = 'N604NK' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N604NK/reports

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