# Service difficulty reports: N316NB

A list on [N316NB](https://openairdocs.org/aircraft/N316NB.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 4 · 177 reports

- [SDR DALA2025112508580](https://openairdocs.org/sdr/DALA2025112508580.md): Access Panel · damaged · Nov 24, 2025 · N316NB · Airbus A319114 · Wing, Plate/Skin
  > MULTIPLE ELONGATED FASTENER HOLES ON THE BOTTOM L/H WING SKIN BOLT HOLES FOR ACCESS PANEL 540JB, BETWEEN RIB 14 AND RIB 15. COMPLIED WITH ER/A 494440-14. (1319780).
- [SDR DALA2025112108513](https://openairdocs.org/sdr/DALA2025112108513.md): Blower · failed · Nov 20, 2025 · N316NB · Airbus A319114 · Air Distribution Fan
  > ON DESCENT INTO JAC JOINING APPROACH AT 14K FEET, NOTICED A SMELL OF BURNING FOOD OR SMOKE SCENT. R & R AVIONIC VENT BLOWER 20HQ PER A319 AMM 21-26. TEST OK. (7727282)
- [SDR DALA2025101707586](https://openairdocs.org/sdr/DALA2025101707586.md): Radome · damaged · Oct 16, 2025 · N316NB · Airbus A319114 · Aerodynamic Fairings
  > RADOME DAMAGED DUE TO BIRD STRIKE. REMOVED RADOME PER A319 AMM 53-15. (7744877).
- [SDR DALA2025081806164](https://openairdocs.org/sdr/DALA2025081806164.md): Unknown · malfunctioned · Aug 15, 2025 · N316NB · Airbus A319114 · Landing Gear System
  > AIRCRAFT PULLS LT WHILE TAXING. NO CAUSE KNOWN FROM FLIGHT DECK. PERFORMED GVI OF NOSE GEAR AND TIRES LOOKED GOOD TIRE PSI CORRECT, PERFORMS OPS CHECK NOSE WHEEL STEARING WITH CFDS IAW AMM 32-51 NO FAULTS NOTED.
- [SDR DALA2025071805431](https://openairdocs.org/sdr/DALA2025071805431.md): Lever · binding · Jul 18, 2025 · N316NB · Airbus A319114 · Passenger/Crew Doors
  > SHIP 3116 ENTRY DOOR ARMING LEVER HARD TO OPERATE, MISSING THE NUT TO HOLD IT TO THE SILVER HANDLE. IT IS OPERABLE BUT IT FALLS OFF WHEN IN THE DISARMED POSITION AND SOMEONE BUMPS INTO IT.. INSTALLED NEW NUT IAW A319 AMM 52-11. (1091409).
- [SDR DALA2025031602002](https://openairdocs.org/sdr/DALA2025031602002.md): Door Frame · cracked · Mar 13, 2025 · N316NB · Airbus A319114 · Fuselage Main, Structure
  > SHIP 3116 CRACK INDICATION ON FR 68 AT AFT GALLEY AREA, DOOR STOOP FITTING. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON FR 68 AT AFT GALLEY AREA, DOOR STOP FITTING #1 LOWER INBOARD HOLE 4 RH SIDE AS PER A319 SRM53-41-12-300-011. (0855505)
- [SDR DALA2025031602000](https://openairdocs.org/sdr/DALA2025031602000.md): Access Panel · cracked · Mar 11, 2025 · N316NB · Airbus A319114 · Nacelle/Pylon, Plate/Skin
  > SHIP 3116 CRACK ON ACCESS PANEL 413DL ON LH PYLON. CORRECTIVE ACTION: REPAIRED ACCESS PANEL 413DL PYLON L/H AS PER ER/A #540187-14MA. (0851394)
- [SDR DALA2025031101896](https://openairdocs.org/sdr/DALA2025031101896.md): Damper · no test · Mar 10, 2025 · N316NB · Airbus A319114 · Passenger/Crew Doors
  > SHIP 3116 DISC: DONT PASS OPERATIONAL TEST EMERGENCY DOOR DAMPER ON PASSENGER CREW DOO R 842 (REFER TO AMDS CARD 5210-7089-RA RII). C/A: REMOVED DOOR DAMPER P/N FE240-004 S/N 2183 ON UNSERVICEABLE CONDITION ON PASSENGER CREW DOOR 842 AS PER A320 FAM AMM 52-13-
- [SDR DALA2025031101895](https://openairdocs.org/sdr/DALA2025031101895.md): Stop Fitting · cracked · Mar 10, 2025 · N316NB · Airbus A319114 · Fuselage Main, Structure
  > SHIP 3116 DISC: CRACK INDICATION ON FR 68 AT AFT GALLEY AREA, DOOR STOOP FITTING 4, LO WER INBOARD, HOLE 4, RH SIDE, CRACK POSITION AT 12 OCLOCK, CRACK DEPTH 0.110 INCHES, HOLE DIAMETER 0.250 INCHES, AA 5311-01216, AD RELATED, ACTIONS REQUIRED PRIOR TO FURTHER
- [SDR DALA2025021000991](https://openairdocs.org/sdr/DALA2025021000991.md): Door · intermittent · Feb 6, 2025 · N316NB · Airbus A319114 · Passenger/Crew Doors
  > SHIP 3116 2L DOOR WILL NOT ARM INTERMITTANT. CORRECTIVE ACTION: T/S PER TSM 52-13-00-810-802-A AND IPC 52-73-84-01. DOOR OPS AS REQUIRED. NO 90 DAY HISTORY. (0799118)
- [SDR DALA2025012800652](https://openairdocs.org/sdr/DALA2025012800652.md): Light · damaged · Jan 25, 2025 · N316NB · Airbus A319114 · Emergency Lighting
  > SHIP 3116 EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE / LOCATIONS:29D. AFT RIGHT GALLEY WALL TRIM HANGING OUT AND WIRE EXPOSED. CORRECTIVE ACTION: RE-SECURED LIGHT GALLEY PER A320 AMM 33-51. (0779187)
- [SDR DALA2024122311921](https://openairdocs.org/sdr/DALA2024122311921.md): Access Door · punctured · Dec 19, 2024 · N316NB · Airbus A319114 · Fluid Service Doors
  > SHIP 3116 WATER SERVICE DOOR 171AL HAS A PUNCTURE IN COMPOSITE ACCESS DOOR TO POTABLE WATER FILLING AND DRAINAGE. CORRECTIVE ACTION: INSTALLED NEW DOOR IAW A319 AMM 52-42. OPS CK GOOD. CDL & PLACARD REMOVED. (6754518)
- [SDR DALA2024120511457](https://openairdocs.org/sdr/DALA2024120511457.md): Galley · smoke · Dec 4, 2024 · N316NB · Airbus A319114 · Air Conditioning System
  > SHIP 3116 FA IN THE AFT GALLEY REPORTED THE SMELL OF FUMES AND AN IMMEDIATE HEADACHE. CORRECTIVE ACTION: PERFORMED GVI OF ENGINE 1 & ENG 2 & APU PER WORKCARD 0550-2002. NO FINDINGS. (6621352)
- [SDR DALA2024100509718](https://openairdocs.org/sdr/DALA2024100509718.md): Filter · odor · Oct 4, 2024 · N316NB · Airbus A319114 · Air Distribution System
  > SHIP 3116 STRONG "DIRTY" SOCK SMELL DETECTED IN CABIN AND COCKPIT. CORRECTIVE ACTION: REPLACED BOTH RECIRC FAN FILTER AND VERIFIED NO SMELL PRESENT PER AMDS CARD # 0550-2003 MC. (9997762)
- [SDR DALA2024052705529](https://openairdocs.org/sdr/DALA2024052705529.md): Proximity Sensor · faulted · May 25, 2024 · N316NB · Airbus A319114 · Landing Gear Position and Warning
  > SHIP 3116 L/G SYS DISAGREE AFTER LANDING. CORRECTIVE ACTION: REF TSM 32-31-00-810-842. BITE SHOWS N L/G EXT PROX SNSR (24GA) IAW A319 AMM 32-31. CKS GOOD. (5662506)
- [SDR DALA2023062205070](https://openairdocs.org/sdr/DALA2023062205070.md): Unknown · unknown · Jun 20, 2023 · N316NB · Airbus A319114 · Electrical Power System
  > SHIP 3116 - ATO - DUE TO A NUMBER 2 IDG LOW OIL PRESSURE ECAM MESSAGE. CORRECTIVE ACTION: DEFERRED #2 IDG PER MEL AND CONTINUED. REMOVED AND REPLACED #2 ENG IDG PER A319 AMM 24-21-51. OPS AND LEAKS CK GOOD. (8170650)
- [SDR DALA2023072105918](https://openairdocs.org/sdr/DALA2023072105918.md): Unknown · unknown · Jun 6, 2023 · N316NB · Airbus A319114 · Rudder, Plate/Skin
  > SHIP 3116 CORROSION RUDDER TOP SURFACE HINGE BEARING 6 ON VERTICAL STABILIZER. CORRECTIVE ACTION: REPLACED HINGE BEARING #6 ON VERTICAL STABILIZER AS PER A320 FAM AMM 55-46-11-000-001-A AND AMM55-46-11-400-001-A. (2803695)
- [SDR DALA2023072105917](https://openairdocs.org/sdr/DALA2023072105917.md): Unknown · unknown · Jun 6, 2023 · N316NB · Airbus A319114 · Trailing Edge Flaps
  > SHIP 3116 CORROSION BONDING PLATE FLAP TRACK FAIRING 632CB ON RH WING. CORRECTIVE ACTION: REPAIRED PER ER/A 608480-14. (2803132).
- [SDR DALA2023072105916](https://openairdocs.org/sdr/DALA2023072105916.md): Unknown · unknown · Jun 6, 2023 · N316NB · Airbus A319114 · Trailing Edge Flaps
  > SHIP 3116 CORROSION BONDING PLATE FLAP TRACK FAIRING 2 (531CB) ON LH WING. CORRECTIVE ACTION: REPAIRED PER ER/A 608480-14. (2803113)
- [SDR DALA2023060704638](https://openairdocs.org/sdr/DALA2023060704638.md): Unknown · unknown · Jun 6, 2023 · N316NB · Airbus A319114 · Trailing Edge Flaps
  > AIRCRAFT 3116, CRACK FLAP TRACK FAIRING 633CB BONDING PLATE ON RH WING. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON FLAP TRACK FAIRING 633CB OF RH WING AS PER ER/A 608480-14 REV. ORIGINAL APPROVEDDATE: 30/MAY/23. SECTION I HAS BEEN COMPLIED WITH. (LP 2
- [SDR DALA2023060504480](https://openairdocs.org/sdr/DALA2023060504480.md): Unknown · unknown · Jun 4, 2023 · N316NB · Airbus A319114 · Fuselage Structure (General)
  > SHIP 3116 CRACK WASTE TANK PANEL 172AR AT LOWER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH ER/A 608339-14 REV. ORIGINAL. (2800365)
- [SDR DALA2023060504478](https://openairdocs.org/sdr/DALA2023060504478.md): Unknown · unknown · Jun 3, 2023 · N316NB · Airbus A319114 · Fuselage Structure (General)
  > SHIP 3116 CRACK INDICATION ON FRAME 20 RH SIDE UPPER DOUBLE JOGGLE AREA AT OPEN FASTENER HOLE C. CORRECTIVE ACTION: COMPLIED WITH ER/A 608100-14AD REV. ORIGINAL. (2798836)
- [SDR DALA2023060504477](https://openairdocs.org/sdr/DALA2023060504477.md): Unknown · unknown · Jun 3, 2023 · N316NB · Airbus A319114 · Fuselage Structure (General)
  > SHIP 3116 CORROSION INTERNAL SKIN LOCATED BETWEEN FR54 TO FR55 AND STR41R TO STR 43R IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: COMPLIED WITH ER/A 608609-14 REV.ORIGINAL. (2798424)
- [SDR DALA2023060504466](https://openairdocs.org/sdr/DALA2023060504466.md): Unknown · unknown · Jun 3, 2023 · N316NB · Airbus A319114 · Wing Structure
  > SHIP 3116 CORROSION TRAILING EDGE LOWER SURFACE SKIN AT LEVEL RIB 6 TO RIB 7 ON RH WING. CORRECTIVE ACTION: COMPLIED WITH A319 SRM 57-21-11-52B. (2798697)
- [SDR DALA2023060504482](https://openairdocs.org/sdr/DALA2023060504482.md): Unknown · unknown · Jun 2, 2023 · N316NB · Airbus A319114 · Flight Control System Wiring
  > SHIP 3116 CORROSION IB FLAP CONNECTORS 7541VC AND 7543VC ON LH WING. CORRECTIVE ACTION: COMPLIED WITH AMDS 2751-9202-DE. (2797256)
- [SDR DALA2023060504481](https://openairdocs.org/sdr/DALA2023060504481.md): Unknown · unknown · Jun 2, 2023 · N316NB · Airbus A319114 · Flight Control System Wiring
  > SHIP 3116 CORROSION IB FLAP CONNECTORS 7542VC AND 7540VC ON RH WING. CORRECTIVE ACTION: REPLACED IB FLAP CONNECTORS 7542VC AND 7540VC ON RH WING. (2797252)
- [SDR DALA2023053104343](https://openairdocs.org/sdr/DALA2023053104343.md): Unknown · unknown · May 30, 2023 · N316NB · Airbus A319114 · Fuselage Main, Bulkhead
  > SHIP 3116 GOUGE AFT PRESSURE BULKHEAD WEB FWD FACE FR70 AND LEVEL STR2LH AT AFT GALLEY AREA. CORRECTIVE ACTION: COMPLIED WITH ER/A 608589-14 REV. ORIGINAL. (2791810)
- [SDR DALA2023053004304](https://openairdocs.org/sdr/DALA2023053004304.md): Unknown · unknown · May 29, 2023 · N316NB · Airbus A319114 · Fuselage Main, Frame
  > SHIP 3116 CRACK INDICATION ON FRAME 68 LH SIDE IN AFT FACE FRAME WEB AND HORIZONTAL FLANGE RADIUS AT STGR 8. CORRECTIVE ACTION: REPAIRED PER A319 SRM 53-41-12. OK FOR SERVICE. (2790176)
- [SDR DALA2023052604195](https://openairdocs.org/sdr/DALA2023052604195.md): Unknown · unknown · May 25, 2023 · N316NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > AIRCRAFT 3116, CORROSION THRESHOLD SHEET LOC BTW FR 55A TO FR 59 IN AFT CARGO COMPARTMENT (SSI 534107). CORRECTIVE ACTION: REPLACED THRESHOLD SHEET AND FASTENERS LOC BTW FR 55A TO FR 59 IN AFT CARGO COMPARTMENT AS PERA319 SRM 51-72-11 AND DWG D53477100ISSUE V.
- [SDR DALA2023052504160](https://openairdocs.org/sdr/DALA2023052504160.md): Unknown · unknown · May 24, 2023 · N316NB · Airbus A319114 · Fuselage Structure (General)
  > AIRCRAFT 3116, CORROSION FRAME 29 STRAP BTW STR 40RH TO STR 42RH IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED STRAP LOC. FR29 BTW STR 40RH TO STR 42RH IN FWD CARGO COMPARTMENT, ASPER SRM A319 51-72-11 AND DWG: D53233211. (LP 2782364)
- [SDR DALA2023051903993](https://openairdocs.org/sdr/DALA2023051903993.md): Unknown · unknown · May 18, 2023 · N316NB · Airbus A319114 · Fuselage Main, Longeron/Stringer
  > AIRCRAFT 3116, CORROSION SHEAR TIE LOCATED BETWEEN FR55 AND STR42L TO STR43L IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE LOCATED BETWEEN FR55 AND STR42L TO STR43L IN AFT CARGO COMPARTMENT AS PER A319 SRM 51-72-11 AND DWG D53476318. (LP 2773
- [SDR DALA2023051903992](https://openairdocs.org/sdr/DALA2023051903992.md): Unknown · unknown · May 16, 2023 · N316NB · Airbus A319114 · Fuselage Main, Frame
  > AIRCRAFT 3116, CRACK INDICATION ON FRAME 68 RH SIDE IN AFT FACE FRAME WEB AND HORIZONTAL FLANGE RADIUS AT STGR 8, CRACK LENGTH IS 0.875 INCH APPROX, SSI 534124-01-2, 534124-01-3 AT AFT GALLEY AREA (1 EA). CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR LOCATED A
- [SDR DALA2023051303794](https://openairdocs.org/sdr/DALA2023051303794.md): Unknown · unknown · May 12, 2023 · N316NB · Airbus A319114 · Nacelle/Pylon Structure
  > AIRCRAFT 3116, CORROSION SPIGOT RECEPTACLE FITTING LH PYLON. CORRECTIVE ACTION: REPLACED SPIGOT RECEPTACLE FITTING LH PYLON MEASURE OF FIRST CASE DIAMETER IS 4.341 INCHES TOOL USED: DIGITAL CALIPER P/N500-196-30 S/N A20230758. (LP 2764257)
- [SDR DALA2023051303793](https://openairdocs.org/sdr/DALA2023051303793.md): Stringer · corroded · May 12, 2023 · N316NB · Airbus A319114 · Fuselage Main, Longeron/Stringer
  > AIRCRAFT 3116, CORROSION STRINGER 41R AT LEVEL FR 62 IN AFT CARGO COMPARTMENT (SSI 534107). CORRECTIVE ACTION: REPLACED STRINGER SECTION AND FASTENERS LOC. STRINGER 41R BTW FR61 TO FR64 AS PER A319 SRM 51-72-11 AND DWG D53476324. (LP 2763949)
- [SDR DALA2023051003682](https://openairdocs.org/sdr/DALA2023051003682.md): Fitting · corroded · May 9, 2023 · N316NB · Airbus A319114 · Nacelle/Pylon, Attach Fittings
  > AIRCRAFT 3116, CORROSION SPIGOT FITTING RECEPTACLE ON RH PYLON. CORRECTIVE ACTION: REPLACED SPIGOT FITTING RECEPTACLE ON RH PYLON, MEASURE OF FIRST CASE DIAMETER IS. 4.343 INCHES. (LP 2759529)
- [SDR DALA2023050403490](https://openairdocs.org/sdr/DALA2023050403490.md): Unknown · unknown · May 2, 2023 · N316NB · Airbus A319114 · Fuselage Main, Longeron/Stringer
  > AIRCRAFT 3116, CRACK EXTERNAL SKIN STIFENER LOCATED AT Z169 AND FRAME 1 ON FWD FACE ON FORWARD PRESSURE BULKHEAD. CORRECTIVE ACTION: REPLACED STIFFENER ON EXTERNAL SKIN LOCATED AT Z169 AND FRAME 1 ON FWD FACE ON FORWARD PRESSURE BULKHEAD AS PER A319 SRM 51-42-
- [SDR DALA2023050403489](https://openairdocs.org/sdr/DALA2023050403489.md): Unknown · unknown · May 2, 2023 · N316NB · Airbus A319114 · Fuselage Main, Longeron/Stringer
  > AIRCRAFT 3116, CRACK EXTERNAL SKIN STIFENER LOCATED AT Z169 AND FRAME 1 ON FWD FACE ON FORWARD PRESSURE BULKHEAD. CORRECTIVE ACTION: REPLACED STIFFENER ON EXTERNAL SKIN LOCATED AT Z169 AND FRAME 1 ON FWD FACE ON FORWARD PRESSURE BULKHEAD AS PER A319 SRM51-42 -
- [SDR DALA2022072505100](https://openairdocs.org/sdr/DALA2022072505100.md): Cooling Fan · burned · Jul 25, 2022 · N316NB · Airbus A319114 · Cabin Cooling System
  > SHIP 3116 - AS FO & I BOARDED THE A/C WE BOTH NOTICED A STRONG ELECTRICAL SMOKE SMELL. CORRECTIVE ACTION: R/R AVIONICS COOLING BLOWER FILTER P/N P616780 PER A319 AMM 21 -26. (9265830)
- [SDR DALA2022071504911](https://openairdocs.org/sdr/DALA2022071504911.md): None · none · Jul 14, 2022 · N316NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > SHIP 3116 - POSSIBLE FCS REPAIR FRAME 67 LOCATED BTW STR 41R TO STR 42R IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: CONFIRMED DT EVALUATION FOR POSSIBLE FCS REPAIR FRAME 67 LOCATED BTW STR 41R TO STR 42R IN AFT CARGO COMPARTMENT AND FOUND MEETS THE GENERAL RE
- [SDR DALA2022071504910](https://openairdocs.org/sdr/DALA2022071504910.md): None · none · Jul 14, 2022 · N316NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > SHIP 3116 - POSSIBLE FCS REPAIR EXTERNAL SKIN LOC. FR 59 TO FR 60 BTW STR 18 TO STR 20 R/H ON UPPER FUSELAGE. CORRECTIVE ACTION: CONFIRMED DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOC. FR 59 TO FR 60 BTW STR 18 TO STR 20 R/H ON UPPER MEETS THE GENER
- [SDR DALA2022071504909](https://openairdocs.org/sdr/DALA2022071504909.md): None · none · Jul 14, 2022 · N316NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > SHIP 3116 - POSSIBLE FCS REPAIR EXTERNAL SKIN LOC. FR 59 TO FR 60 BTW STR 41 TO STR 43 L/H AT LOWER FUSELAGE. CORRECTIVE ACTION: CONFIRMED DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOC. FR 59 TO FR 60 BTW STR 41 TO STR 43 L/H AT LOWER FUSELAGE AND FO
- [SDR DALA2022071504908](https://openairdocs.org/sdr/DALA2022071504908.md): None · none · Jul 14, 2022 · N316NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > SHIP 3116 - POSSIBLE FCS REPAIR EXTERNAL SKIN LOC. FR 29 TO FR 30 BTW STR 40 TO STR 42 L/H AT LOWER FUSELAGE. CORRECTIVE ACTION: CONFIRMED DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOC. FR 29 TO FR 30 BTW STR 40 TO STR 42 L/H MEETS THE GENERAL REQUIR
- [SDR DALA2022071504907](https://openairdocs.org/sdr/DALA2022071504907.md): None · none · Jul 14, 2022 · N316NB · Airbus A319114 · Fuselage, Wing Attach Fittings
  > SHIP 3116 - FITTING FRAME 68 LOCATED BTW STR 22R TO STR 23R AFT PAX DOOR SILL. CORRECTIVE ACTION: FABRICATED FITTING FRAME 68 (1EA),LOCATED BTW STR 22R TO STR 23R AFT PAX DOOR SILL AT AFT GALLEY AREA, AS PER ER/A 600551. (2320229)
- [SDR DALA2022071504906](https://openairdocs.org/sdr/DALA2022071504906.md): None · none · Jul 14, 2022 · N316NB · Airbus A319114 · Fuselage Main, Longeron/Stringer
  > SHIP 3116 - CRACK INDICATION FOUND ON FRAME 35 FWD FACE AT LEVEL OF STR 28L. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTION S ON FR 35 AT LEVEL STR28L TO STR 30L LOWER FUSELAGE AS PER ER/A 600183. (2320728)
- [SDR DALA2022071504905](https://openairdocs.org/sdr/DALA2022071504905.md): None · none · Jul 14, 2022 · N316NB · Airbus A319114 · Fuselage Main, Frame
  > SHIP 3116 - CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR FRAME 68. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON FRAME 68 LOCATED BTW STR 22R TO STR 23R AFT PAX DOOR SILL AT AFT GALLEY AREA ASPER ER/A 600551-14 REV. ORIGINAL.(2320249)
- [SDR DALA2022071304874](https://openairdocs.org/sdr/DALA2022071304874.md): None · none · Jul 12, 2022 · N316NB · Airbus A319114 · Horizontal Stabilizer Structure
  > SHIP 3116 - CRACK ACCESS PANEL 332AB ON LH HORIZONTAL STABILIZER. CORRECTIVE ACTION: COMPLIED WITH ER/A 600529-14 REV.ORIGINAL. (2317585)
- [SDR DALA2022071304873](https://openairdocs.org/sdr/DALA2022071304873.md): None · none · Jul 12, 2022 · N316NB · Airbus A319114 · Leading Edge Devices
  > SHIP 3116 - CRACK OB FIXED LEADING EDGE SUPPORT ANGLE AT RIB 12 ON RH WING. CORRECTIVE ACTION: COMPLIED WITH ER/A 530598-14MA REV.A. (2317592)
- [SDR DALA2022071304872](https://openairdocs.org/sdr/DALA2022071304872.md): None · none · Jul 12, 2022 · N316NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > SHIP 3116 - FCS:REPAIR EXTERNAL SKIN LOC FR1 TO FR2 BELOW UPPER STRINGER R/H AT LOWER FUSELAGE. CORRECTIVE ACTION: REPAIR INSTRUCTIONS ON EXTERNAL SKIN LOC FR1 TO FR 2 BELOW UPPER STRINGER R/H AT LOWER FUSELAGE AS PER ER/A 600477-14 REV. ORIGINAL SECTION I.(2
- [SDR DALA2022070804756](https://openairdocs.org/sdr/DALA2022070804756.md): None · none · Jul 7, 2022 · N316NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > SHIP 3116 - CORROSION SEAT TRACK -Y1292 LOC FR12 TO FR 24 IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED SEAT TRACK -Y1292 LOC FR12 TO FR 24 IN PASSENGER CABIN AS PER SRM A319 51-42-11.(2310599)
- [SDR DALA2022070804755](https://openairdocs.org/sdr/DALA2022070804755.md): None · none · Jul 7, 2022 · N316NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > SHIP 3116 - CORROSION SEAT TRACK Y1292 LOC ON FR 12 TO FR24 IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED SEAT TRACK Y1292 LOC ON FR 12 TO FR24 IN PASSENGER CABIN. (2310593)

Next page: https://openairdocs.org/aircraft/N316NB/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 = 'N316NB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N316NB/reports

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