# Service difficulty reports: N336NB

A list on [N336NB](https://openairdocs.org/aircraft/N336NB.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 · 224 reports

- [SDR DALA2026092105253](https://openairdocs.org/sdr/DALA2026092105253.md): Unknown · odor · Sep 20, 2026 · N336NB · Airbus A319114 · Air Distribution System
  > ON THE PREVIOUS FLIGHT FROM DTW TO AUS, A BURNING ELECTRICAL ODOR WAS OBSERVED IN FLIGHT DECK ON CLIMB OUT FROM 5000-15000 AND THEN DISSAPATED. UPON ARRIVAL AND AFTER DISCUSSION WITH MCC, IT WAS DETERMINED THE PLANE WAS OKAY FOR SERVICE. DURING ENGINE START IN
- [SDR DALA2026092105243](https://openairdocs.org/sdr/DALA2026092105243.md): Engine · power loss · Sep 18, 2026 · N336NB · Airbus A319114 · Engine (Turbine/Turboprop)
  > RTO - RIGHT ENG DID NOT SPOOL UP AS FAST AS THE LEFT ENGINE. NR 1 ENG REACHED 80% N1 WHILE END #2 WAS MUCH SLOWER. PERFORMED TSM 71-00-00-810-807-A, ENG SLOW TO ACCEL; PERFORMED A319 AMM 73-21-60-740-028-A, CORRECT FAULTS OF ENG SCHED MAINT RPTS; NO FAULTS RE
- [SDR DALA2026091805197](https://openairdocs.org/sdr/DALA2026091805197.md): Engine · vibration · Sep 18, 2026 · N336NB · Airbus A319114 · Engine (Turbine/Turboprop)
  > ATB- RETURNED TO AUS DUE TO ENGINE 1 VIBES ABOVE 4.0. CREW ALSO REPORTED FEELING A PULSE. MTC REPORTED HIGHEST N1 VIBE OBSERVED ON NUMBER ONE ENGINE WAS 4.2 UNITS. C/W FAN LUBE PER WORK CARD 7221-9601-01. C/W VIBE SURVEY PER AMM 71-00, N1 VIBES WITHIN LIMITS
- [SDR DALA2026062403743](https://openairdocs.org/sdr/DALA2026062403743.md): Secu · faulted · Jun 24, 2026 · N336NB · Airbus A319114 · Flight Control System
  > DIV TO BOS DUE TO F/CTL SEC 3 FAULT. REPLACED SEC 3 AND RELAY 41CE3. (LP: 8320072, AIRCRAFT WAS GROUNDED)
- [SDR DALA2025072405554](https://openairdocs.org/sdr/DALA2025072405554.md): Skin · corroded · Jul 23, 2025 · N336NB · Airbus A319114 · Wing, Plate/Skin
  > SHIP 3136 CORROSION INDICATION WAS FOUND IN TOP SKIN PANEL 2, TRAILING EDGE OVERHANG AREA, LH WING. CORRECTIVE ACTION: COMPLIED WITH ER/A 621980-14. (1101703).
- [SDR DALA2025071405281](https://openairdocs.org/sdr/DALA2025071405281.md): Protector · faulted · Jul 12, 2025 · N336NB · Airbus A319114 · Landing Gear Position and Warning
  > SHIP 3136 L/G SYS DISAGREE ECAM MSG AFTER LANDING. COMPLETED INSP AND TARGET CLEARANCE ON NLG PROX SENSOR 25GA IAW A319AMM 32-31-73-200-002-A. R/R 25GA PROX SENSOR REF A319 AMM 32-31.
- [SDR DALA2025032002105](https://openairdocs.org/sdr/DALA2025032002105.md): Hmu · faulted · Mar 17, 2025 · N336NB · Airbus A319114 · Fuel Controlling System
  > SHIP 3136 -DIV- DIVERTED TO PHL DUE TO RIGHT ENGINE COMPRESSOR STALL. ENGINE THROTTLE WAS NOT PULLED BACK AND ENGINE RESUMED NORMAL POWER. COMPLETED REQUIRED BOROSCOPE WITH NO ABNORMALITIES FOUND AND REPLACED HMU. (LP: 6826498)
- [SDR DALA2025022001280](https://openairdocs.org/sdr/DALA2025022001280.md): Slide · out of position · Feb 19, 2025 · N336NB · Airbus A319114 · Escape Slide
  > SHIP 3136 DISC: 1R DOOR SLIDE PIN WON'T ENGAGE WHEN DOOR ARMED. C/A: FWD TO NEF 52-22-02. THIS IS NORMAL OPERATION. PIN CAN NOT BE INSERTED WHEN DOOR IS ARMED. PIN OPS CK OK. OL FOR SVC. 1R DOOR SLIDE PIN WON'T ENGAGE WHEN DOOR ARMED. C/A: FWD TO NEF 52-22-
- [SDR DALA2025020400823](https://openairdocs.org/sdr/DALA2025020400823.md): Window Frame · cracked · Feb 1, 2025 · N336NB · Airbus A319114 · Fuselage Main, Structure
  > SHIP 3136 CRACK INDICATION FOUND AT LH FRONT WINDSHIELD FRAMING (CENTER POST, UPPER RADIUS). CORRECTIVE ACTION: REPAIRED PER ER/A 622029-14. (0791399)
- [SDR DALA2025020400822](https://openairdocs.org/sdr/DALA2025020400822.md): Profile · cracked · Jan 31, 2025 · N336NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > SHIP 3136 CRACK ON LH AND RH LOAD TRANSMITTING PROFIL EMERGENCY EXIT DOOR 834 IN PASSENGER CABIN. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS AS PER ER/A 554715-14AD REV. B. (0789647)
- [SDR DALA2025020400821](https://openairdocs.org/sdr/DALA2025020400821.md): Skin · corroded · Jan 31, 2025 · N336NB · Airbus A319114 · Wing, Plate/Skin
  > SHIP 3136 CORROSION LOWER SKIN LOCATED BTW RIB 15 TO RIB 16 T RAILING EDGE OF LH WING. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS PER ER/A 621980-14. (0789351)
- [SDR DALA2025020400820](https://openairdocs.org/sdr/DALA2025020400820.md): Skin · corroded · Jan 31, 2025 · N336NB · Airbus A319114 · Wing, Plate/Skin
  > SHIP 3136 CORROSION ON LOWER SKIN LOCATED BTW RIB 8 TO RIB 9 TRAILING EDGE OF LH WING. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS AS PER ER/A 621980-14. (0789347)
- [SDR DALA2025020400819](https://openairdocs.org/sdr/DALA2025020400819.md): Skin · corroded · Jan 31, 2025 · N336NB · Airbus A319114 · Wing, Plate/Skin
  > SHIP 3136 CORROSION ON LOWER SKIN LOCATED AT RIB 10 TRAILING EDGE OF LH WING. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS AS PER ER/A 621980-14. (0789338)
- [SDR DALA2025020400818](https://openairdocs.org/sdr/DALA2025020400818.md): Skin · corroded · Jan 31, 2025 · N336NB · Airbus A319114 · Wing, Plate/Skin
  > SHIP 3136 CORROSION EXTERNAL SKIN UPPER SURFACE AT RIB 9 LH WING. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS AS PER ER/A 621980-14. (0789330)
- [SDR DALA2025020400817](https://openairdocs.org/sdr/DALA2025020400817.md): Skin · corroded · Jan 31, 2025 · N336NB · Airbus A319114 · Wing, Plate/Skin
  > SHIP 3136 CORROSION ON LOWER SKIN LOCATED AT RIB 10 TRAILING EDGE OF LH WING. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS AS PER ER/A 621980-14. (0789317)
- [SDR DALA2025020400816](https://openairdocs.org/sdr/DALA2025020400816.md): Skin · corroded · Jan 31, 2025 · N336NB · Airbus A319114 · Wing, Plate/Skin
  > SHIP 3136 CORROSION ON LOWER SKIN BTW RIB 16 TO RIB 17 TRAILING EDGE OF LH WING. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS AS PER ER/A 621980-14. (0789146)
- [SDR DALA2025013000716](https://openairdocs.org/sdr/DALA2025013000716.md): Door · cracked · Jan 30, 2025 · N336NB · Airbus A319114 · Emergency Exits
  > SHIP 3136 WHILE ACCOMPLISHING INSPECTIONS OF DOOR 844 CRACKS INDICATIONS WERE FOUND. CORRECTIVE ACTIONS: COMPLIED WITH ER/A 623607-14AD. (0786815)
- [SDR DALA2025012900682](https://openairdocs.org/sdr/DALA2025012900682.md): Skin · corroded · Jan 29, 2025 · N336NB · Airbus A319114 · Wing, Plate/Skin
  > SHIP 3136 CORROSION INDICATION WAS FOUND IN TOP SKIN PANEL 2, TRAILING EDGE OVERHANG AREA, LH WING. CORRECTIVE ACTION: PERFORMED ZERO STRESS JACKING LOAD CHECK AS PER A319 SRM 51-51-10-911-001 AND AS PER ER/A 621980-14. (0785041)
- [SDR DALA2025012900681](https://openairdocs.org/sdr/DALA2025012900681.md): Skin · corroded · Jan 29, 2025 · N336NB · Airbus A319114 · Wing, Plate/Skin
  > SHIP 3136 CORROSION INDICATION WAS FOUND IN TOP SKIN PANEL 2, TRAILING EDGE OVERHANG AREA, LH WING. CORRECTIVE ACTION: PERFORMED ZERO STRESS JACKING LOAD CHECK AS PER A319 SRM 51-51-10-911-001 AND AS PER ER/A 621980-14. (0785036)
- [SDR DALA2025012900686](https://openairdocs.org/sdr/DALA2025012900686.md): Skin · corroded · Jan 28, 2025 · N336NB · Airbus A319114 · Wing, Plate/Skin
  > SHIP 3136 CORROSION AT TOP SKIN PANEL 2, LOWER SURFACE, RS, TEOH, RIBS 13-18, LEFT HAND WING. CORRECTIVE ACTION: COMPLIED WITH ER/A 621980-14. (0784747)
- [SDR DALA2025012900685](https://openairdocs.org/sdr/DALA2025012900685.md): Skin · corroded · Jan 28, 2025 · N336NB · Airbus A319114 · Wing, Plate/Skin
  > SHIP 3136 CORROSION INDICATION WAS FOUND IN TOP SKIN PANEL 2. CORRECTIVE ACTION: REPAIRED PER ER/A 621980-14. (0784735)
- [SDR DALA2025012900684](https://openairdocs.org/sdr/DALA2025012900684.md): Skin · corroded · Jan 28, 2025 · N336NB · Airbus A319114 · Wing, Plate/Skin
  > SHIP 3136 LH WING TOP SKIN PANEL 2 TE OVERHANG CORROSION. CORRECTIVE ACTION: REPAIRED PER ER/A 621980-14. (0784719)
- [SDR DALA2025012900683](https://openairdocs.org/sdr/DALA2025012900683.md): Skin · corroded · Jan 28, 2025 · N336NB · Airbus A319114 · Wing, Plate/Skin
  > SHIP 3136 CORROSION LH WING TOP SKIN PANEL 2 TE OVERHANG. CORRECTIVE ACTION: REPAIRED PER ERA 621980-14. (0784702)
- [SDR DALA2025012400587](https://openairdocs.org/sdr/DALA2025012400587.md): Pushrod · corroded · Jan 23, 2025 · N336NB · Airbus A319114 · Rudder Control System
  > SHIP 3136 CORROSION ON ROD END PUSH ROD RUDDER CONTROL MECHANISM LOC. THS COMPARTMENT. CORRECTIVE ACTION: REPLACED CONTROL ROD OF THE RUDDER MECHANICAL CONTROL ON THS COMPARTMENT AS PER A320FAM AMM 27-21-00-840-001-A AND AMM27-21-00-820-001-A. (0775794)
- [SDR DALA2025012400586](https://openairdocs.org/sdr/DALA2025012400586.md): Support · cracked · Jan 23, 2025 · N336NB · Airbus A319114 · Aerodynamic Fairings
  > SHIP 3136 FINDING CRACK SUPPORT WEB BELLY FAIRING STRUCTURE AT FR52 LH SIDE LOWER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH ER/A 623195-14. (0775586)
- [SDR DALA2025012400585](https://openairdocs.org/sdr/DALA2025012400585.md): Window Frame · cracked · Jan 23, 2025 · N336NB · Airbus A319114 · Fuselage Main, Structure
  > SHIP 3136 CRACK INDICATION WAS FOUND AT LH FRONT WINDSHIELD FRAMING (CENTER POST, UPPER RADIUS). CORRECTIVE ACTION: COMPLIED WITH ER/A 622114-14AD. (0775567)
- [SDR DALA2025012400584](https://openairdocs.org/sdr/DALA2025012400584.md): Window Frame · cracked · Jan 23, 2025 · N336NB · Airbus A319114 · Fuselage Main, Structure
  > SHIP 3136 CRACK INDICATION FOUND ON WINDSHIELD FRAME LOWER CENTER POST LH SIDE STARTING FROM UPPER FASTENER. CORRECTIVE ACTION: COMPLIED WITH ER/A 622025-14AD. (0775563)
- [SDR DALA2025012300549](https://openairdocs.org/sdr/DALA2025012300549.md): Stiffener · cracked · Jan 22, 2025 · N336NB · Airbus A319114 · Fuselage Main, Structure
  > SHIP 3136 CRACK INDICATION FOUND ON THE HORIZONTAL UPPER STIFFENER OF THE LATERAL WINDOW FRAME AT FR 4, RH. CORRECTIVE ACTION: COMPLIED WITH ER/A 576072-14AD. (0774234)
- [SDR DALA2025012200515](https://openairdocs.org/sdr/DALA2025012200515.md): Stiffener · cracked · Jan 21, 2025 · N336NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > SHIP 3136 FUSELAGE FR4 RH LATERAL WINDOW FRAME UPPER ATTACHMENT STIFFENER CRACK. CORRECTIVE ACTION: REPAIRED PER ER/A 576072-14AD. (0772199)
- [SDR DALA2025012000441](https://openairdocs.org/sdr/DALA2025012000441.md): Skin · corroded · Jan 17, 2025 · N336NB · Airbus A319114 · Wing, Plate/Skin
  > SHIP 3136 CORROSION UPPER SKIN LOWER SURFACE LOCATED BTW RIB20 TO RIB22 TRAILING EDGE AREA ON RH WING. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS AS PER A319 SRM 57-21-11-283-026. (0766169)
- [SDR DALA2025012000440](https://openairdocs.org/sdr/DALA2025012000440.md): Plate · corroded · Jan 17, 2025 · N336NB · Airbus A319114 · Trailing Edge Flaps
  > SHIP 3136 CORROSION WAS FOUND AFFECTING THE OB AL PLATE (FACE AND BORE) AT TRACK #4 LEVEL, SPECIFICALLY AT PENDULUM SUPPORT.CORRECTIVE ACTION: REPAIRED ERA 622710-14. (0765737)
- [SDR DALA2025011400314](https://openairdocs.org/sdr/DALA2025011400314.md): Light · broken · Jan 13, 2025 · N336NB · Airbus A319114 · Emergency Lighting
  > SHIP 3136 BROKEN EMERGENCY LIGHT IN CEILING PANEL ROW 1, 10,16 IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED EMERGENCY LIGHT IN CEILING PANEL ROW 1, 10,16 IN PASSENGER CABIN AS PER A320 FAM AMM 33-51-11-000-400-001-A AND AMM 33-51-11-400-001. (0759327)
- [SDR DALA2025010900179](https://openairdocs.org/sdr/DALA2025010900179.md): Hinge Fitting · cracked · Jan 8, 2025 · N336NB · Airbus A319114 · Fuselage, Door Hinge
  > SHIP 3136 CRACK INDICATION FOUND ON HINGE FITTING, KEEL BEAM, MLG DOOR RH. CORRECTIVE ACTION: COMPLIED WITH ER/A 622081-14AD. (0751986)
- [SDR DALA2025010700135](https://openairdocs.org/sdr/DALA2025010700135.md): Window Frame · cracked · Jan 6, 2025 · N336NB · Airbus A319114 · Fuselage Main, Structure
  > SHIP 3136 FUSELAGE NOSE FUSELAGE WINDSHIELD FRAMING CENTER POST LH CRACK DAMAGE. CORRECTIVE ACTION: REPAIRED PER ER/A 622025-14AD. (0748054)
- [SDR DALA2025010700134](https://openairdocs.org/sdr/DALA2025010700134.md): Window Frame · cracked · Jan 6, 2025 · N336NB · Airbus A319114 · Fuselage Main, Structure
  > SHIP 3136 CRACK INDICATION WAS FOUND AT LH FRONT WINDSHIELD FRAMING (CENTER POST, UPPER RADIUS). CORRECTIVE ACTION: REPAIRED PER ER/A 622025-14AD. (0748034)
- [SDR DALA2025010600078](https://openairdocs.org/sdr/DALA2025010600078.md): Plate · corroded · Jan 6, 2025 · N336NB · Airbus A319114 · Wing Main, Frame Structure
  > SHIP 3136 CORROSION TRAILING EDGE PLATE LOCATED ON WING TIP BRAKE BTW RIB 15 TO RIB 16 ON LH WING. CORRECTIVE ACTION: REPLACED PLATE (TEE PIECE) LOC. WING TIP BRAKE AREA ON LH WING AS PER A319 SRM 51-42-11. (0747361)
- [SDR DALA2025010900180](https://openairdocs.org/sdr/DALA2025010900180.md): Skin · corroded · Dec 31, 2024 · N336NB · Airbus A319114 · Trailing Edge Flaps
  > SHIP 3136 CORROSION LOWER SKIN BTW RIB 17 TO RIB 19 TRAILING EDGE LH WING. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS AS PER A319 SRM 57-21-11-283-026. (0738505)
- [SDR DALA2025010200007](https://openairdocs.org/sdr/DALA2025010200007.md): Floor Panel · corroded · Dec 31, 2024 · N336NB · Airbus A319114 · Fuselage Floor Panel
  > SHIP 3136 CORROSION ON FLOOR PANEL 261DF AND INSERT PLUGS (34EA) IN AFT GALLEY AREA. CORRECTIVE ACTION: COMPLIED WITH ER/A 622197-14. (0738487)
- [SDR DALA2025010900181](https://openairdocs.org/sdr/DALA2025010900181.md): Skin · corroded · Dec 30, 2024 · N336NB · Airbus A319114 · Wing, Plate/Skin
  > SHIP 3136 CORROSION UPPER SKIN LOWER SURFACE LOCATED BTW RIB15 TO RIB16 TRAILING EDGE AREA ON RH WING. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS AS PER A319 SRM 57-21-11-283-026. (0736546)
- [SDR DALA2024123112102](https://openairdocs.org/sdr/DALA2024123112102.md): Skin · dented · Dec 30, 2024 · N336NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > SHIP 3136 DENT EXTERNAL SKIN LOCATED AT FR 10 AND 6 INCHES ABOVE OF RH LOWER STRINGER AT LOWER FUSELAGE. CORRECTIVE ACTION: REPAIRED PER ER/A 622531-14. (0736537)
- [SDR DALA2024123012087](https://openairdocs.org/sdr/DALA2024123012087.md): Skin · dented · Dec 27, 2024 · N336NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > SHIP 3136 DENT AT EXTERNAL FUSELAGE SKIN BETWEEN FRAME 09 TO FRAME 10. CORRECTIVE ACTION: REPAIRED PER ER/A 622531-14. (0731835)
- [SDR DALA2024122712024](https://openairdocs.org/sdr/DALA2024122712024.md): Skin · cracked · Dec 26, 2024 · N336NB · Airbus A319114 · Passenger/Crew Doors
  > SHIP 3136 BENT EXTERNAL SKIN PASSENGER CREW DOOR 842 LOCATED LOWER CORNER AFT PO SITION IN PASSENGER CABIN. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN PASSENGER CREW DOOR 842 LOCATED LOWER CORNER AFT POSITION IN PASSENGER CABIN AS PERA319 S
- [SDR DALA2024122311908](https://openairdocs.org/sdr/DALA2024122311908.md): Frame · cracked · Dec 22, 2024 · N336NB · Airbus A319114 · Fuselage Main, Frame
  > SHIP 3136 CRACK INDICATION WAS FOUND ON FR20RH. CORRECTIVE ACTION: REPAIRED PER ER/A 576073-14AD. (0723798)
- [SDR DALA2024122311904](https://openairdocs.org/sdr/DALA2024122311904.md): Plate · corroded · Dec 22, 2024 · N336NB · Airbus A319114 · Wing Main, Frame Structure
  > SHIP 3136 CORROSION PLATE LOCATED WING TIP BRAKE AREA TRAILING EDGE ON RH WING. CORRECTIVE ACTION: REPLACED PLATE AND FASTENERS LOC. ON WING TIP BRAKE AREA TRAILING EDGE RH WING AS PER A320 FAM AMM 27-51-51-400-001-A. (0724057)
- [SDR DALA2024122311903](https://openairdocs.org/sdr/DALA2024122311903.md): Bonding Plate · corroded · Dec 22, 2024 · N336NB · Airbus A319114 · Wing Main, Frame Structure
  > SHIP 3136 CORROSION BONDING PLATE FLAP TRACK FAIRING 4 (533CB) ON LH WING. CORRECTIVE ACTION: REPAIRED PER ER/A 622286-14. (0722533)
- [SDR DALA2024122311909](https://openairdocs.org/sdr/DALA2024122311909.md): Receptacle · corroded · Dec 21, 2024 · N336NB · Airbus A319114 · Aileron Control System
  > SHIP 3136 CORROSION ELECTRICAL RECEPTACLE FIN (7541VC) AND (7543VC) INTERCONNECTING STRUT I/B FLAP LH WING (2 EA). CORRECTIVE ACTION: REPLACED ELECTRICAL RECEPTACLE FIN (7541VC) AND (7543VC) ON INTERCONNECTING STRUT I/B FLAP LH WING (2 EA) AS PER A320 FAM AWM
- [SDR DALA2024122311894](https://openairdocs.org/sdr/DALA2024122311894.md): Support Angle · broken · Dec 20, 2024 · N336NB · Airbus A319114 · Elevator Structure
  > SHIP 3136 BROKEN SUPPORT ANGLE LOCATED AT ELEVATOR HINGE ARM 1 LH ELEVATOR. CORRECTIVE ACTION: REPLACED SUPPORT ANGLE LOCATED AT ELEVATOR HINGE ARM #1 LH ELEVATOR (1 EA) AS PER A320 FAM AMM 55-16-42-000-001-A AND A320 FAM AMM 55-16-42-400-001-A. (0720164)
- [SDR DALA2024122011863](https://openairdocs.org/sdr/DALA2024122011863.md): Not Reported · corroded · Dec 19, 2024 · N336NB · Airbus A319114 · Standard Practices/Structures
  > SHIP 3136 CORROSION COMPARTMENT GALLEY 110, 111, 112 BELLOW WORK DECK AREA AT FWD GALLEY AREA. CORRECTIVE ACTION: COMPLIED WITH ER/A 622088-14. (0718742)
- [SDR DALA2024121811807](https://openairdocs.org/sdr/DALA2024121811807.md): Angle · cracked · Dec 18, 2024 · N336NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > SHIP 3136 CRACK ON TI-ANGLE LOC FR42 RH SIDE HYDRAULIC COMPARTMENT LOWER FUSELAGE. CORRECTIVE ACTION: REPLACED TI-ANGLE LOC. FR42 RH SIDE HYDRAULIC COMPARTMENT LOWER FUSELAGE PCW AA CARD 5353-01006-03. (0716113)
- [SDR DALA2024121811804](https://openairdocs.org/sdr/DALA2024121811804.md): Light · inoperative · Dec 18, 2024 · N336NB · Airbus A319114 · Emergency Lighting
  > SHIP 3136 BROKEN EMERGENCY LIGHTS IN FWD CLOSET RH. CORRECTIVE ACTION: REPLACED EMERGENCY LIGHTS IN FWD CLOSET RH AS PER ENCORE CMM 25-31-94-01. (0716117)

Next page: https://openairdocs.org/aircraft/N336NB/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 = 'N336NB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N336NB/reports

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