# Service difficulty reports: N364NB

A list on [N364NB](https://openairdocs.org/aircraft/N364NB.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 3 · 144 reports

- [SDR DALA2026082404779](https://openairdocs.org/sdr/DALA2026082404779.md): Brake · smoke · Aug 23, 2026 · N364NB · Airbus A319114 · Landing Gear Brake System
  > SHIP 3164 DISC: ALA CALLED MAINT TO REPORT, RT MLG SMOKING. SAW TEMP 465C, LT GEAR 175C. C/A: JACKED AIRCRAFT, #4 BRAKE ASSY GRABBING. R/R #4 BRAKE ASSY PER A319 AMM 32-40. OPS CHK GOOD. NO LEAKS. OK FOR SERVICE. (LP: 9121434, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026032602012](https://openairdocs.org/sdr/DALA2026032602012.md): Skin · corroded · Mar 24, 2026 · N364NB · Airbus A319114 · Wing, Plate/Skin
  > RIGHT WING, TOP SKIN, PANEL 2, LOWER SURFACE, T/E OVERHANG AREA WITH CORROSION AT RIB 11+520MM. C/A: PERFORMED REPAIR AT RH WING TOP SKIN PANEL 2/0 WER SURFACE T/E OVERHANG AREA AT RIB 11 + 520MM (AREA2) IAW ER/A NO. 632748-14AD REV ORIGINAL DATED 21 MAR 26. T
- [SDR DALA2026032602010](https://openairdocs.org/sdr/DALA2026032602010.md): Skin · corroded · Mar 24, 2026 · N364NB · Airbus A319114 · Wing, Plate/Skin
  > RIGHT WING, TOP SKIN, PANEL 2, LOWER SURFACE, T/E OVERHANG WITH CORROSION AT RIB 10 AREA. C/A: PERFORMED REPAIR AT RH WING TOP SKIN PANEL 2 LOWER SURFACE, T/E OVERHANG AREA AT RIB 10 (AREA1) I.A.W ER/A NO. 632748-14AD REV ORIGINAL DATED 21-MAR-26. THIS IS A MA
- [SDR DALA2026032602009](https://openairdocs.org/sdr/DALA2026032602009.md): Stop Fitting · not reported · Mar 24, 2026 · N364NB · Airbus A319114 · Standard Practices/Structures
  > PASSENGER CABIN AT FR68 AFT FACE AREA, BETWEEN STGR21R AND STGR23R, LEVEL DOOR STOP 1 FOUND REPAIR FITTING INSTALLED. WORK CARD 5311-01244-02B, SB A320-53-1491. CONTACT DELTA LIAISON ENGINEERING FOR ALTERNATE INSPECTION INSTRUCTION THAT MAY BE REQUIRED TO COMP
- [SDR DALA2026032602013](https://openairdocs.org/sdr/DALA2026032602013.md): Torque Link · corroded · Mar 23, 2026 · N364NB · Airbus A319114 · Main Landing Gear
  > LOWER FUSELAGE RH MLG TORQUE LINK UPPER PIN WITH CORROSION. REPLACED RH MLG TORQUE LINK UPPER PIN IAW A319 AMM TASK 32-11-27 -000-001-A AND AMM TASK 32-11-27-400-001-A REV 134.01 DATED 12/ FEB/26. (LP: 1508509)
- [SDR DALA2026032401961](https://openairdocs.org/sdr/DALA2026032401961.md): Skin · corroded · Mar 23, 2026 · N364NB · Airbus A319114 · Wing, Plate/Skin
  > SHIP 3164 DISC: RH WING TOP SKIN PANEL 2 LOWER SURFACE, T/E OVERHANG AREA AT RIB 11+140MM SKIN WITH CORROSION. NOTE: WAS FOUND DURING THE PROCESS OF ORNRC 600-126. C/A: PERFORMED REPAIR AT RH WING TOP SKIN PANEL 2 LOWER SURFACE, T/E OVERHANG AREA AT RIB 11+140
- [SDR DALA2026032401960](https://openairdocs.org/sdr/DALA2026032401960.md): Skin · corroded · Mar 23, 2026 · N364NB · Airbus A319114 · Wing, Plate/Skin
  > R/H WING, TOP SKIN, PANEL 2, LOWER SURFACE, T/E OVERHANG WITH CORROSION AT RIB 15 AREA. C/A: PERFORMED REPAIR AT RH WING TOP SKIN PANEL 2 LOWER SURFACE, T/E OVERHANG AREA AT RIB 15 (AREA 4) I.A.W ER/A NO. 632748-14AD REV ORIGINAL DATED 21-MAR-26. THIS IS A MAJ
- [SDR DALA2026032602018](https://openairdocs.org/sdr/DALA2026032602018.md): Skin · corroded · Mar 21, 2026 · N364NB · Airbus A319114 · Wing, Plate/Skin
  > ER/A 632748-14AD ISSUED FOR REPAIR AND REWORK TO RH WING TRAILIN G EDGE SKIN CORROSION. FOLLOW ON ACTION REQUIRED. C/A: PERFORM SECTION IV EVERY SOONER OF 12200FC OR 24500FH AFTER SECT ION I. ASSOCIATED ER/A 14-632748 ADDED FOR AC 3164. (LP: 1505733)
- [SDR DALA2026032602019](https://openairdocs.org/sdr/DALA2026032602019.md): Skin · corroded · Mar 21, 2026 · N364NB · Airbus A319114 · Wing, Plate/Skin
  > ER/A 632748-14AD ISSUED FOR REPAIR AND REWORK TO RH WING TRAILIN G EDGE SKIN CORROSION. FOLLOW ON ACTION REQUIRED. C/A: PERFORM SECTION III EVERY SOONER OF 15000FC OR 30000FH AFTER SEC TION I. ASSOCIATED ER/A 14-632748 ADDED FOR AC 3164. (LP: 1505729)
- [SDR DALA2026032401959](https://openairdocs.org/sdr/DALA2026032401959.md): Skin · corroded · Mar 21, 2026 · N364NB · Airbus A319114 · Wing, Plate/Skin
  > ER/A 632748-14AD ISSUED FOR REPAIR OF CORROSION TO RH WING TRAIL ING EDGE SKIN. FOLLOW ON ACTION IS REQUIRED. PERFORM SECTION V EVERY SOONER OF 15000FC OR 30000FH AFTER SECTI ON I.
- [SDR DALA2026032401958](https://openairdocs.org/sdr/DALA2026032401958.md): Skin · corroded · Mar 21, 2026 · N364NB · Airbus A319114 · Wing, Plate/Skin
  > DAMAGE TOLERANCE EVALUATION ( DTE) REQUIRED FOR REPAIR OF RH WI NG TRAILING EDGE SKIN CORROSION PER ER/A 632748-14AD. C/A: SECTION I IS LIMITED TO SOONER OF 60000FC / 120000FH. ER/A TO BE REVISED PRIOR TO THIS LIMIT ELSE REMOVE A/C FROM SERVICE.
- [SDR DALA2026032401957](https://openairdocs.org/sdr/DALA2026032401957.md): Skin · damaged · Mar 21, 2026 · N364NB · Airbus A319114 · Wing, Plate/Skin
  > ER/A 632748-14AD ISSUED FOR RH WING TRAILING EDGE SKIN CORROSION REWORK. FOLLOW ON ACTION IS REQUIRED. PERFORM SECTION II EVERY SOONER OF 10000FC OR 20000FH AFTER SECTION I.
- [SDR DALA2026032201921](https://openairdocs.org/sdr/DALA2026032201921.md): Angle · corroded · Mar 20, 2026 · N364NB · Airbus A319114 · Engine Thrust Reverser
  > NR 1 ENGINE INBD AND OTBD THRUST REVERSERS T/E HEAT SHIELD SUPPORT ANGLES WITH CORROSION. FOUND DURING PROCESS OF ORNRC N 131. REPLACED ANGLES RADIAL REAR P/N: 321-162-001-6 (2EA) AT ENGINE 1 INBD AND OTBD TRUST REVERSE IAW SPM (GFM) 70-43-31-390-005, PARAG
- [SDR DALA2026031901895](https://openairdocs.org/sdr/DALA2026031901895.md): Angle · corroded · Mar 18, 2026 · N364NB · Airbus A319114 · Nacelle/Pylon Miscellaneous Structure
  > NR 1 ENGINE AFT PYLON ACCESS PANEL # 476BR AFT I/B CUT-OUT ANGLE WITH CORROSION. REPLACED ANGLE P/N: ATTACHED WITH SOLID RIVETS IAW A319 BSRM 51-72-11-911-001 PARAG B AND 51-42-11-801 2E (2) ( REV 155 DATED 17/NOV/25) AND REF DWG D545 10054 ITEM 32 ISSUE U. (
- [SDR DALA2026031101670](https://openairdocs.org/sdr/DALA2026031101670.md): Seat Track · corroded · Mar 10, 2026 · N364NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > UPPER FUSELAGE,FR 16,Y+1292,LH LONGITUDINAL BEAM WITH CORROSION. REPLACED SEAT TRACK BTW FR12 THRU FR24 AT Y+ 1292 IAW SRM 51-72-11-911-001 REV 155.00 AND DWG D53112812.
- [SDR DALA2026030801579](https://openairdocs.org/sdr/DALA2026030801579.md): Fitting · damaged · Mar 3, 2026 · N364NB · Airbus A319114 · Nacelle/Pylon, Main Frame
  > ENGINE NR 2 PYLON FOUND SPIGOT LOWER FITTING AND SPIGOT BALL JOINT DAMAGE. REPLACED ENGINE # 2 PYLON SPIGOT LOWER FITTING AND SPIGOT BALL JOINT IAW SRM 54-51-12. REPLACED #2 PYLON LOWER SPIGOT FITTIN G IAW A319 SRM TASK 54-51-12-300-001 REV 155 DATED 17 NOV 2
- [SDR DALA2026030801578](https://openairdocs.org/sdr/DALA2026030801578.md): Fitting · damaged · Mar 3, 2026 · N364NB · Airbus A319114 · Nacelle/Pylon, Main Frame
  > ENGINE NR 1 PYLON FOUND SPIGOT LOWER FITTING AND SPIGOT BALL JOINT DAMAGE. REPLACE ENGINE NR 1 PYLON SPIGOT LOWER FITTING AND SPIGOT BALL JOINT IAW SRM 54-51-12. (LP: 1477390)
- [SDR DALA2026030801577](https://openairdocs.org/sdr/DALA2026030801577.md): Seat Track · corroded · Mar 3, 2026 · N364NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > UPPER FUSELAGE, FR 16, Y+765, LH LONGITUDINAL BEAM WITH CORROSION. REPLACED SEAT TRACK AT UPPER FUSELAGE, BETWEEN FR12 AND FR24, Y+765 IAW A319 SRM 53-11-15-01A FIGURE 001, ITEM 015-A REV 155.00 DATED 17/NOV/25 AND REFRENCE AIRBUS DWG #D53112813, ISSUE B, ITEM
- [SDR DALA2026030301457](https://openairdocs.org/sdr/DALA2026030301457.md): Beam · corroded · Feb 27, 2026 · N364NB · Airbus A319114 · Fuselage Main, Structure
  > UPPER FUSELAGE, FR 67+530MM, Y-1162, RH LONGITUDINAL BEAM WITH CORROSION. REPLACED LONGITUDINAL BEAM BETWEEN FR67+530MM AND FR68, Y-162 IAW A319 SRM 53-41-14-03A FIGURE 303, ITEM 145A AND SRM 51-72-11-911-001 PARAG C, REV 155.00 AND AIRBUS DWG D53472780 ITEM
- [SDR DALA2026030301456](https://openairdocs.org/sdr/DALA2026030301456.md): Web · cracked · Feb 27, 2026 · N364NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > UPPER FUSELAGE, FR 68+180MM, LH LATERAL WEB WITH CRACK. REPLACED LATERAL WEB IAW SRM 51-72-11- 911-001 AND SRM 53-41-14-804A PAGE 24, ITEM 20 REV 155.00 AND DWG D534480505 SHEET 38, ITEM 339 AND 266 ( ISSUE EG) AND ITEM 142. (LP: 1470915)
- [SDR DALA2026030301455](https://openairdocs.org/sdr/DALA2026030301455.md): Beam · corroded · Feb 27, 2026 · N364NB · Airbus A319114 · Fuselage Main, Structure
  > UPPER FUSELAGE, FR 69+490MM, Y-160, LONGITUDINAL BEAM WITH CORROSION. REPLACED LONGITUDINAL BEAM P/N D5347219720000 BETWEEEN FR68 ANF FR7, Y-160 IAW IAW A319 SRM 53-41-14-03A FIGURE 303, ITEM 165 AND SRM 51-72-11-911-001 PARG C. (REV 155.00 DATED 17 NOV 25) A
- [SDR DALA2026010400044](https://openairdocs.org/sdr/DALA2026010400044.md): Warning Message · false activation · Jan 3, 2026 · N364NB · Airbus A319114 · Fuel Storage
  > LAX-PDX CREW REPORTED, FWD LT OUTER TANK LOW TEMP AT 40 KNOTS. FLIGHT CREW PLACARD INSTALLED IN LAX PER MEL 28-40-09E. NO PREVIOUS FAULTS. TROUBLESHOT PER TSM 28-42-00-810-843A SYSTEM CHECKS GOOD, REMOVED PLACARD.) AT 40KTS DUE TO A LT OUTER FUEL TEMP LOW ME
- [SDR DALA2025102707846](https://openairdocs.org/sdr/DALA2025102707846.md): Heat Exchanger · cracked · Oct 26, 2025 · N364NB · Airbus A319114 · Cabin Pressure Control System
  > SHIP 3164 - PRES - AND EMERGENCY DECLARED DUE TO CAB PR EXCESS CAB ALT ECAM WARNING AT 34,000 FEET. BEGAN DESCENT AND CABIN STARTED TO RECOVER ABOUT 28,000 FEET. CORRECTIVE ACTION: FOUND THE PRIMARY HEAT EXCHANGER WITH A LARGE CRACK, AND THE ACM INLET GASKET L
- [SDR DALA2025022801554](https://openairdocs.org/sdr/DALA2025022801554.md): Light · inoperative · Feb 28, 2025 · N364NB · Airbus A319114 · Emergency Lighting
  > DURING SERVICE CHECK ROW 25 SEAT D. UNDER SEAT EMERGENCY LIGHT FOUND INOP. REMOVED AND REPLACED SEAT EMERGENCY LIGHT. MCO/PLAC REMOVED. DURING SERVICE CHECK ROW 25 SEAT D. UNDER SEAT EMERGENCY LIGHT FOUND INOP. C/A: FORWARD TO MEL 33-50-03A. NRO M PROCEDURES.
- [SDR DALA2025021701178](https://openairdocs.org/sdr/DALA2025021701178.md): Light · burned out · Feb 15, 2025 · N364NB · Airbus A319114 · Flight Compartment Lighting
  > SHIP 3164 BURNING ELECTRICAL SMELL THROUGH APP PHASE UNTIL GATE. CORRECTIVE ACTION: FOUND FO DOME LIGHTS BURN OUT AND ODOR. RELAMPED DOME LIGHTS PER A319 AMM 33-18. (6423487)
- [SDR DALA2025012100474](https://openairdocs.org/sdr/DALA2025012100474.md): Proximity Switch · disconnected · Jan 20, 2025 · N364NB · Airbus A319114 · Door System Wiring
  > SHIP 3164 LEFT OVERWING EXIT SLIDE NOT ARMED ON DOOR/OXY ECAM PAGE. CORRECTIVE ACTION: CONNECTED PROX SWITCH AND INSTALLED DOOR LINING OPS CKS GOOD REF A319 AMM 52-73. REMOVED SAFETY PIN FROM LT OVERWING EMERGENCY SLIDE. (6383966)
- [SDR DALA2025012000439](https://openairdocs.org/sdr/DALA2025012000439.md): Filter · dirty · Jan 18, 2025 · N364NB · Airbus A319114 · Air Distribution System
  > SHIP 3164 BURNING SMELL APU & BLEED ON UPON ARRIVAL, FOUND PETROLEUM JELLY ON RT PACK COMPONENTS AND RECIRC FILTERS VERY DIRTY. CORRECTIVE ACTION: CLEANED COMPONETS & REPLACED RECIRC FILTERS, USING A320 AMM TASK 21-00-00-615- 802-A, DECONTAMINATED ECS USING BO
- [SDR DALA2024122311919](https://openairdocs.org/sdr/DALA2024122311919.md): Door · no discrepancy · Dec 21, 2024 · N364NB · Airbus A319114 · Passenger/Crew Doors
  > SHIP 3164 ENTRY DOOR HARD TO OPEN OR CLOSE. CORRECTIVE ACTION: OPENED & CLOSED FLIGHT DECK DOOR MULTIPLE TIMES. FOUND NO ISSUES. OK FOR SVC. (0720993)
- [SDR DALA2024120911557](https://openairdocs.org/sdr/DALA2024120911557.md): Panel · damaged · Dec 8, 2024 · N364NB · Airbus A319114 · Horizontal Stabilizer, Plate/Skin
  > SHIP 3164 DURING PAINT VISIT FOUND INBOUND DAMAGE TO L/H UPPER HORIZONTAL STAB PANEL #2. CORRECTIVE ACTION: NEW PANEL INSTALLED PER A319 AMM 55-13-07. (5144355)
- [SDR DALA2024112611233](https://openairdocs.org/sdr/DALA2024112611233.md): Unknown · odor · Nov 25, 2024 · N364NB · Airbus A319114 · Air Distribution System
  > SHIP 3164 DIRTY SOCK SMELL. CORRECTIVE ACTION: T/S PER A319 TSM 05-50-00-810-831-A, PERFORMED WORK CARDS 0550-2002 AND 0550-2003. NO TROUBLE FOUND. OK FOR SERVICE. (5144320)
- [SDR DALA2024112511197](https://openairdocs.org/sdr/DALA2024112511197.md): Oxygen Mask · unwanted deploy · Nov 22, 2024 · N364NB · Airbus A319114 · Passenger Oxygen System
  > SHIP 3164 FORWARD LAV AND ROW 23DEF O2 MASK DROPPED DURING CLIMB OUT. CORRECTIVE ACTION: REPACKED MASKS PER A319 AMM 35-23. OK FOR SERVICE. (5144308)
- [SDR DALA2024112211146](https://openairdocs.org/sdr/DALA2024112211146.md): Spar · debonded · Nov 21, 2024 · N364NB · Airbus A319114 · Horizontal Stabilizer, Spar/Rib
  > SHIP 3164 LOWER SPAR ANGLE OUTER PLY FOUND DISBONDED ON REMOVAL OF SPAR WEB, BETWEEN RIB 10 AND 11. CORRECTIVE ACTION: COMPLIED WITH ERA 620110-14. (0671622)
- [SDR DALA2024112211145](https://openairdocs.org/sdr/DALA2024112211145.md): Spar · dented · Nov 21, 2024 · N364NB · Airbus A319114 · Horizontal Stabilizer, Spar/Rib
  > SHIP 3164 LT HORIZONTAL AFT OF LEADING-EDGE SPAR MID SPAN OF HORIZONTAL HAS LARGE DENT. POSSIBLE PREVIOUS REPAIR. NO MONITOR STICKER OR EVIDENCE OF ONE MISSING. CORRECTIVE ACTION: COMPLIED WITH ERA 620110-14. (0671621)
- [SDR DALA2024112111123](https://openairdocs.org/sdr/DALA2024112111123.md): Skin · dented · Nov 20, 2024 · N364NB · Airbus A319114 · Horizontal Stabilizer, Plate/Skin
  > SHIP 3164 LH HORIZONTAL STABILIZER UPPER SKIN RIB 10-11 STR 2-3 DENT. CORRECTIVE ACTION: REPAIRED WITH ER/A 620110-14. (0669994)
- [SDR DALA2024110710720](https://openairdocs.org/sdr/DALA2024110710720.md): Light · no test · Nov 7, 2024 · N364NB · Airbus A319114 · Emergency Lighting
  > SHIP 3164 DURING SLIDE INSTALL PER AMDS 2561-4002-RF FOUND THAT EMERGENCY LIGHT TEST FAILED AT R1 DOOR. CORRECTIVE ACTION: TROUBLESHOT WITH REF TO A319 TSM 52-21-00-810-808-A. (0648129)
- [SDR DALA2024091609075](https://openairdocs.org/sdr/DALA2024091609075.md): Door Frame · cracked · Sep 14, 2024 · N364NB · Airbus A319114 · Fuselage Main, Structure
  > SHIP 3164 FR16 LHS AND RHS FASTENERS HOLES IN DOUBLE JOGGLE AREA AT LEVEL OF DOOR STOP 1 AND 7, CRACK INDICATIONS WERE FOUND ON FR16RH, FASTENER HOLES #6 AND #7. CORRECTIVE ACTION: REPAIRED PER ER/A 593392-14AD. (0556078)
- [SDR DALA2024091609074](https://openairdocs.org/sdr/DALA2024091609074.md): Door Frame · cracked · Sep 14, 2024 · N364NB · Airbus A319114 · Fuselage Main, Structure
  > SHIP 3164 FRAME 16 RH AT DOOR STOPS NUMBER 7 DOUBLE JOGGLE HOLES 6 & 7 CRACKS. CORRECTIVE ACTION: REPAIRED PER ER/A 593392-14AD. (0556079)
- [SDR DALA2024090408736](https://openairdocs.org/sdr/DALA2024090408736.md): Door Frame · out of tolerance · Sep 3, 2024 · N364NB · Airbus A319114 · Fuselage Main, Structure
  > SHIP 3164 FR 68 RH DOOR STOP FITTING #3 AND #4 HOLES OUT OF TOLERANCE. CORRECTIVE ACTION: REPAIRED PER ER/A 619949-14AD. (0537413)
- [SDR DALA2024082908557](https://openairdocs.org/sdr/DALA2024082908557.md): Door Frame · out of tolerance · Aug 28, 2024 · N364NB · Airbus A319114 · Fuselage Main, Structure
  > SHIP 3164 FRAME 66 R/H DOOR STOP FITTING #4 ALL FOUR HOLES OUT OF TOLERANCE. CORRECTIVE ACTION: REPAIRED PER ER/A 619947-14AD. (0526395)
- [SDR DALA2024082908555](https://openairdocs.org/sdr/DALA2024082908555.md): Fitting · unknown · Aug 28, 2024 · N364NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > SHIP 3164 DEVIATIONS ON FR68 RHS FITTINGS 1, 3, 4. CORRECTIVE ACTION: REPAIRED PER ER/A 619949-14. (0527406)
- [SDR DALA2024082908554](https://openairdocs.org/sdr/DALA2024082908554.md): Fitting · out of tolerance · Aug 28, 2024 · N364NB · Airbus A319114 · Fuselage Main, Attach Fittings
  > SHIP 3164 FR68 RHS FITTING 1, 3, 4 OUT OF TOLERANCE. CORRECTIVE ACTION: REPAIRED PER ERA 619949-14AD. (0527399)
- [SDR DALA2024082808515](https://openairdocs.org/sdr/DALA2024082808515.md): Door Frame · cracked · Aug 27, 2024 · N364NB · Airbus A319114 · Fuselage Main, Structure
  > SHIP 3164 FRAME/FORMERS FRAME 16 RH AT DOOR STOPS NUMBER 7 DOUBLE JOGGLE HOLES 6 & 7 CRACKS. CORRECTIVE ACTION: REPAIRED PER ERA 593392-14AD. (0524996)
- [SDR DALA2024082808514](https://openairdocs.org/sdr/DALA2024082808514.md): Door Frame · cracked · Aug 27, 2024 · N364NB · Airbus A319114 · Fuselage Main, Structure
  > SHIP 3164 FRAME/FORMERS FRAME 16 RH AT DOOR STOPS NUMBER 7 DOUBLE JOGGLE HOLES 6 & 7 CRACKS. CORRECTIVE ACTION: REPAIRED PER ERA 593392-14AD. (0524992)
- [SDR DALA2024082808513](https://openairdocs.org/sdr/DALA2024082808513.md): Frame · cracked · Aug 27, 2024 · N364NB · Airbus A319114 · Fuselage Main, Frame
  > SHIP 3164 CRACK INDICATIONS WERE FOUND ON FR16RH, FASTENER HOLES #6 AND #7. CORRECTIVE ACTION: REAPIRED PER ERA 593392-14AD. (0524989)
- [SDR DALA2024082608464](https://openairdocs.org/sdr/DALA2024082608464.md): Fitting · cracked · Aug 25, 2024 · N364NB · Airbus A319114 · Fuselage Main, Structure
  > FRAME 68 L/H FITTING #1 HOLE 2 AND 4 ARE CRACKED. REPAIRED HOLES PER A319 SRM 53-41-12-300-011.
- [SDR DALA2024082608463](https://openairdocs.org/sdr/DALA2024082608463.md): Fitting · cracked · Aug 25, 2024 · N364NB · Airbus A319114 · Fuselage Main, Structure
  > FRAME 68 L/H FITTING #6 HOLE 2 IS CRACKED. CORRECTIVE ACTION: REPAIRED PER A319 SRM 53-41-12-300-010.
- [SDR DALA2024082608455](https://openairdocs.org/sdr/DALA2024082608455.md): Door Frame · damaged · Aug 22, 2024 · N364NB · Airbus A319114 · Fuselage Main, Structure
  > FR 68 RH DOORSTOP FITTING #3 HOLE #1 AND DOORSTOP FITTING #4 HOLE # 1 AND 3 WERE FOUND OUT OF TOLERANCE. REPAIRED PER ERA 619949-14AD.
- [SDR DALA2024082608454](https://openairdocs.org/sdr/DALA2024082608454.md): Door Frame · damaged · Aug 22, 2024 · N364NB · Airbus A319114 · Fuselage Main, Structure
  > FR 68 RH DOOR STOP FITTING #1, #3 AND #4, HOLES OUT OF TOLERANCE. REPAIRED PER ER/A 619949-14AD.
- [SDR DALA2024082608453](https://openairdocs.org/sdr/DALA2024082608453.md): Fitting · damaged · Aug 22, 2024 · N364NB · Airbus A319114 · Fuselage Structure (General)
  > DEVIATIONS ON FR68 RHS FITTINGS 1, 3, 4. CORRECTIVE ACTION: REPAIRED PER ERA 619949-14AD. (0516249)
- [SDR DALA2024081308082](https://openairdocs.org/sdr/DALA2024081308082.md): Door Frame · cracked · Aug 12, 2024 · N364NB · Airbus A319114 · Fuselage Main, Structure
  > SHIP 3164 FRAME 68 R/H DOOR STOP FITTING #1, HOLE #4 HAS CRACK INDICATION. CORRECTIVE ACTION: REPAIRED PER A319 SRM 53-41-12-300-011. (0498703)

Next page: https://openairdocs.org/aircraft/N364NB/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 = 'N364NB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N364NB/reports

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