# Service difficulty reports: N378NW

A list on [N378NW](https://openairdocs.org/aircraft/N378NW.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 · 178 reports

- [SDR DALA2026102105781](https://openairdocs.org/sdr/DALA2026102105781.md): Panel · missing · Oct 18, 2026 · N378NW · Airbus A320211 · Aerodynamic Fairings
  > BELLY FAIRING SLIDING PANEL, LT BELLY FAIRING SLIDING PANEL MISSING. FWD TO CDL 57-00-02. "M" PROC C/W. DISPATCH APPROVED. CDL AND PLAC INSTALLED. (LP: 9191132, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026091605157](https://openairdocs.org/sdr/DALA2026091605157.md): Computer · faulty · Sep 15, 2026 · N378NW · Airbus A320211 · Trailing Edge Flap Control System
  > SHIP 3278 - ATB - TO DUE TO A FLAPS SYS 1 FAULT MESSAGE. SKYWISE FAILURE MESSAGES INDICATE COMPLETE FAILURE OF SFCC 1. FLAPS WERE NOT LOCKED. SWAPPED SFCC 1 WITH 2. PROBLEM FOLLOWED. DEFERRED SFCC 2 FLAP CHANNEL PER MEL. (LP: 9092130, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026082004762](https://openairdocs.org/sdr/DALA2026082004762.md): Window Frame · cracked · Aug 19, 2026 · N378NW · Airbus A320211 · Fuselage Main, Structure
  > CRACK INDICATION FOUND ON WINDSHIELD FRAME LH SIDE, LOWER CENTER POST, LOWER INBOARD RADIUS. CRACK LENGTH: 0.500 INCHES APPROX., CRACK DIREC TION: FWD. AD 2020-17-03/WORKCARD 5311-01226-01. REQUESTING REPAIR DIS POSITION. REPAIR MUST BE ACCOMPLISHED PRIOR TO
- [SDR DALA2026082004761](https://openairdocs.org/sdr/DALA2026082004761.md): Fitting · damaged · Aug 19, 2026 · N378NW · Airbus A320211 · Fuselage Main, Structure
  > REPLACE CONTINUITY FITTINGS RT/LT SIDE LOC BTW FR1 TO FR4 ON WINDSHIEL D CENTER POST AREA. COMPLIED WITH ER/A 635443 -14AD REV.ORIGINAL MATCHES WITH ALL STEPS ON PRI 635443-14AD PRI REV 0,1, IT`S HAS BEEN VALIDATED. PERFORMED REPAIR INSTRUCTIONS ON FUSELAGE F
- [SDR DALA2026081804710](https://openairdocs.org/sdr/DALA2026081804710.md): Skin · damaged · Aug 18, 2026 · N378NW · Airbus A320211 · Wing, Plate/Skin
  > ELONGATED HOLES ON CUT OUT LOC BTW RIB14 AND RIB15 FUEL TANK ON RH WING, REPAIRED CUT OUT HOLES PER SRM 57 -21-11-300-002 AND REPLACED GANG CHANNEL AS PER A320 SRM 51-72- 11. (1762554) (AIRCRAFT GROUNDED).
- [SDR DALA2026081904725](https://openairdocs.org/sdr/DALA2026081904725.md): Stringer · corroded · Aug 16, 2026 · N378NW · Airbus A320211 · Fuselage Main, Longeron/Stringer
  > LEVEL 2 CORROSION, CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR STRINGER 43L, BTW FR 56 - FR 57 IN AFT CARGO BAY. CONFIRMED DT EVALUATION FOR POSSIBLE FCS LOCATED STRINGER 43L BTW FR56 TO FR 57 REPAIR NR 26 & DOES NOT MEET THE GENERAL REQUIREMENTS IAW ER/A 5
- [SDR DALA2026081704684](https://openairdocs.org/sdr/DALA2026081704684.md): Fitting · cracked · Aug 16, 2026 · N378NW · Airbus A320211 · Fuselage Main, Structure
  > CRACKS FOUND AT WINDSHIELD CENTRAL NODE CONTINUITY FITTINGS AND WINDSHIELD FRAMES ON LT AND RT SIDES, COMPLIED WITH ER/A 635443-14AD. (1758935) (AIRCRAFT GROUNDED).
- [SDR DALA2026081704682](https://openairdocs.org/sdr/DALA2026081704682.md): Skin · scratched · Aug 16, 2026 · N378NW · Airbus A320211 · Fuselage Main, Plate/Skin
  > SCRATCH EXTERNAL SKIN LOCATED BTW FR 52 TO FR 53 AND STR 29L TO STR 30L AT LOWER FUSELAGE, COMPLIED WITH ER/A 636062-14. (1760064) (AIRCRAFT GROUNDED).
- [SDR DALA2026081704681](https://openairdocs.org/sdr/DALA2026081704681.md): Fairing · damaged · Aug 16, 2026 · N378NW · Airbus A320211 · Trailing Edge Flaps
  > ELONGATED HOLE (1EA) WAS FOUND AFFECTING THE AFT FIXED FAIRING PANEL 533BB AT LEVEL OF FLAP TRACK FAIRING #4 ON LH WING, COMPLIED WITH ER/A 635816-14. (1760182) (AIRCRAFT GROUNDED).
- [SDR DALA2026081704685](https://openairdocs.org/sdr/DALA2026081704685.md): Window Frame · cracked · Aug 15, 2026 · N378NW · Airbus A320211 · Fuselage Main, Structure
  > CRACKS FOUND AT LT WINDSHIELD, CENTER POST, LOWER ATTACHMENT AREA, UPPER CORNER, FRONT WINDSHIELD FRAMING AND LT WINDSHIELD, CENTER POST, LOWER ATTACHMENT AREA, LOWER CORNER, FRONT WINDSHIELD FRAMING, COMPLIED WITH ER/A 635322-14. (1758425) (AIRCRAFT GROUNDED
- [SDR DALA2026081704683](https://openairdocs.org/sdr/DALA2026081704683.md): Skin · scratched · Aug 15, 2026 · N378NW · Airbus A320211 · Fuselage Main, Plate/Skin
  > TWO SCRATCHES (2EA) WERE FOUND COMMON TO THE EXTERNAL SURFACE OF THE FUSELAGE SKIN PANEL, THE REWORKED AREA WAS EVALUATED AGAINST SRM TASK 53-41-11-283-001 RESULTING OUT OF LIMITS, COMPLIED WITH ER/A 636062-14. (1758115) (AIRCRAFT GROUNDED).
- [SDR DALA2026081904724](https://openairdocs.org/sdr/DALA2026081904724.md): Stringer · damaged · Aug 13, 2026 · N378NW · Airbus A320211 · Fuselage Main, Longeron/Stringer
  > CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR STRINGER 5L LOCATED BTW FR 43 - FR 45 IN PASSENGER CABIN. CONFIRMED DT EVALUATION FCS ON EXISTING REPAIR STR 5L LOC. BTW FR 43 - FR 45 IN PAX CABIN UPPER FUSELAGE, ENGINEERING CONTACTED DUE TO NOT COMPLIED WITH RE
- [SDR DALA2026082504822](https://openairdocs.org/sdr/DALA2026082504822.md): Oxygen Mask · leaking · Aug 11, 2026 · N378NW · Airbus A320211 · Crew Oxygen System
  > LEAK ON SECOND OBSERVER CREW OXYGEN MASK AT COCKPIT. REMOVED SECOND OBSERVER CREW OXYGEN MASK P/N: MF10-05-11, S/N: 06700 ON UNSERVICEABLE CONDITION AT COCKPIT AS PER A320 FAM AMM 35-12-41-000-002-A. JOB IN PROGRESS. REPLACED SECOND OBSERVER CREW OXYGEN MASK
- [SDR DALA2026080604533](https://openairdocs.org/sdr/DALA2026080604533.md): Elec Connector · corroded · Aug 3, 2026 · N378NW · Airbus A320211 · Equipment/Furnishings Wiring
  > CORROSION ELECTRICAL CONNECTOR ESCAPE SLIDE OF PASSENGER CREW DOOR 841 (REFERENCE RII AMDS CARD 5210-7089-RF). REMOVED ESCAPE SLIDE OF PASSENGER CREW DOOR 841 IN UNSERVICEABLE CONDITION PN D31516-717 SN A8111RP AS PER AMDS CARD 2561-4002- RF. STEP 1 THRU STEP
- [SDR DALA2026080604532](https://openairdocs.org/sdr/DALA2026080604532.md): Skin · scratched · Aug 3, 2026 · N378NW · Airbus A320211 · Fuselage Main, Plate/Skin
  > SCRATCH EXTERNAL SKIN LOCATED BTW FR 56 TO FR 57 AND STR 25L TO STR 26L AT LOWER FUSELAGE. PERFORMED REPAIR INSTRUCTIONS ON EXTERNAL SKIN LOCATED BTW FR 56 - 57, S25L - 26L AT LOWER FUSELAGE IAW SRM 53-41-11-300-109, RECHK IS REQUIRED DUE TO THIS REPAIR IS CO
- [SDR DALA2026072404314](https://openairdocs.org/sdr/DALA2026072404314.md): Web · corroded · Jul 23, 2026 · N378NW · Airbus A320211 · Fuselage Miscellaneous Structure
  > LEVEL 2 CORROSION, WEB FRAME 16 LOCATED AT LEVEL STR 23L AT FWD GALLEY AREA. REPLACED WEB LOCATED BTW FR12 TO FR16 AT LEVEL STR23L FWD GALLEY AREA IAW SRM 51-72-11, SRM 51-42-11, DWG# D53112570, AND DWG D53114392, TOOK MEASURES OF CORROSION ARE:L=0.734 IN
- [SDR DALA2026080704567](https://openairdocs.org/sdr/DALA2026080704567.md): Strut · corroded · Jul 22, 2026 · N378NW · Airbus A320211 · Fuselage Main, Structure
  > LEVEL 2 CORROSION, CORROSION ON INTERCONNECTING STRUT RH WING (REFERENCE RII AMDS CARD 2751-9202-DE). REMOVED INTERCONNECTING STRUT ON RH WING UNSERVICEABLE CONDITION PN: D5757032200200, SN: 04647 AS PER A320 FAM AMM 27-51-44-000- 001-A STEP 1 THRU 3.D(1) AND
- [SDR DALA2026072304301](https://openairdocs.org/sdr/DALA2026072304301.md): Floor Support · corroded · Jul 21, 2026 · N378NW · Airbus A320211 · Fuselage Miscellaneous Structure
  > LEVEL 2 CORROSION, FLOOR SUPPORT +Y254, FR 67, REPLACED THE FLOOR SUPPORT Y254 AND FASTENERS BTW FR 66 - FR 68. MEASURE OF CORROSION WERE: L: 0.335 INCHES, W: 0.175 INCHES W: 0.040 INCHES. IAW SRM 51-42-11, SRM 51-72-11, DWG D53472173, AND DWG D53472780.
- [SDR DALA2026072304300](https://openairdocs.org/sdr/DALA2026072304300.md): Seat Track · corroded · Jul 20, 2026 · N378NW · Airbus A320211 · Fuselage, Seat/Cargo Attach Fittings
  > LEVEL 2 CORRODED SEAT TRACK, +Y1292 BTW FR 64 - FR 66. REPLACED WITH A NEW SEAT TRACK IAW SRM 51-42-11, SRM 51-72 -11, AND DWG 10N01474. MEASURES OF CORROSION WAS: L=2.5330 INCH W=1.1880 INCH D=0.040 INCH. (LP: 1710636, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026072304299](https://openairdocs.org/sdr/DALA2026072304299.md): Floor Support · corroded · Jul 20, 2026 · N378NW · Airbus A320211 · Fuselage Miscellaneous Structure
  > LEVEL 2 CORROSION, FLOOR SUPPORT BTW FR 66 TO FR 68, Y1292 - Y1162.5 AT AFT GALLEY AREA. REPLACED FLOOR SUPPORT IAW SRM 51-42-11, SRM51- 72-11, DWG 53474250 AND DWG 10N01474. MEASURE OF CORROSION WAW: L=2.0315 INCH W=1.7975 INCH D=0.0270 INCH. (LP: 171031
- [SDR DALA2026072304298](https://openairdocs.org/sdr/DALA2026072304298.md): Floor Support · corroded · Jul 20, 2026 · N378NW · Airbus A320211 · Fuselage Miscellaneous Structure
  > LEVEL 2 CORROSION, CORROSION FLOOR SUPPORT +Y1162.5, BTW FR 68 TO FR 69 IN AFT GALLEY AREA REPLACED FLOOR SUPPORT IAW SRM 51-42-11, SRM 51-72-11, DWG D53472780, DWG D53470100 AND DWG D53474250. MEASURE OF CORROSION WAS L=1.3505 INCH W= 1.0460 INCH D=0.024
- [SDR DALA2026072004243](https://openairdocs.org/sdr/DALA2026072004243.md): Seat Track · corroded · Jul 19, 2026 · N378NW · Airbus A320211 · Fuselage, Seat/Cargo Attach Fittings
  > LEVEL 2 CORROSION, SEAT TRACK Y1292 & FASTENERS LOC. BTW FR64 TO FR66 AT AFT GALLEY AREA IAW SRM 51-42-11, SRM 51-72 -11 AND DWG 10N01474, MEASURES OF CORROSION ARE: L=2.5330 INCH W=1.1880 INCH D=0.040 INCH. RII INSPECTION COMPLETE. REPLACED WITH NEW SEAT
- [SDR DALA2026072004242](https://openairdocs.org/sdr/DALA2026072004242.md): Floor Support · damaged · Jul 19, 2026 · N378NW · Airbus A320211 · Fuselage Miscellaneous Structure
  > SHIP 3278 DISC: LEVEL 2 CORROSION, FLOOR SUPPORT +Y765 LOCATED BTW FR 66 TO FR 68 AT AFT GALLEY AREA. REPLACED FLOOR SUPPORT Y765 AND FASTENERS LOC. BTW FR 66 TO FR 70 AT AFT GALLEY AREA IAW SRM 51-42-11, SRM 51-72-11; DWG D53472816, DWG D53474250, DWG D53
- [SDR DALA2026072004240](https://openairdocs.org/sdr/DALA2026072004240.md): Seat Track · corroded · Jul 18, 2026 · N378NW · Airbus A320211 · Fuselage, Seat/Cargo Attach Fittings
  > LEVEL 2 CORROSION, SEAT TRACK +Y765 LOCATED BTW FR 64 TO FR 66 AT AFT GALLEY AREA. REPLACED SEAT TRACK Y765 LOCATED BTW FR 64 TO FR 66 AT AFT GALLEY AREA IAW SRM 51-42-11 AND SRM 51-72-11 MEASURE OFCORROSION WERE: L=3.873 IN W= 0.395 IN D= 0.045 IN. RII I
- [SDR DALA2026072004239](https://openairdocs.org/sdr/DALA2026072004239.md): Support · corroded · Jul 18, 2026 · N378NW · Airbus A320211 · Fuselage Miscellaneous Structure
  > LEVEL 2 CORROSION, LOWER SILL LOCATED AT FR 68 AT LEVEL STR 23L AT AFT GALLEY AREA (SSI 534147). PERFORMED PERMANENT REPAIR LOCATED ON LOWER SILL AT FR 68 LEVEL STR 23L AT AFT GALLEY AREA IAW SRM53-41-14-300-001. CORROSION MEASURE WERE: L= 1.000 INCH W= 0.80
- [SDR DALA2026072004238](https://openairdocs.org/sdr/DALA2026072004238.md): Plate · cracked · Jul 18, 2026 · N378NW · Airbus A320211 · Fuselage Miscellaneous Structure
  > CRACK PLATE LOCATED BTW FR 68 TO FR 69 AT LEVEL STR 23L AT AFT GALLEY AREA. REPLACED PLATE LOCATED BTW FR 68 TO FR 69 AT LEVEL STR 23L AT AFT GALLEY AREA IAW SRM 51-42-11, SRM 51-72-11, DWG D53480505, AND DWG D53474250. TOOK MEASURE OF CRACK ON PLATE IS:4
- [SDR DALA2026072004237](https://openairdocs.org/sdr/DALA2026072004237.md): Seat Track · corroded · Jul 16, 2026 · N378NW · Airbus A320211 · Fuselage, Seat/Cargo Attach Fittings
  > LEVEL 2 CORROSION, SEAT TRACK -Y765 LOCATED BTW FR 64 TO FR 66 AT AFT GALLEY AREA (SSI 534147). REPLACED SEAT TRACK -Y765 LOCATED BTW FR 64 TO FR 66 AT AFT GALLEY AREA AS PER A320 SRM 51-72-11, A320 SRM 51-42-11, DWG NAT14N00031 RELEASE DATE 21/ DEC / 16 ISS
- [SDR DALA2026072004236](https://openairdocs.org/sdr/DALA2026072004236.md): Seat Track · corroded · Jul 16, 2026 · N378NW · Airbus A320211 · Fuselage, Seat/Cargo Attach Fittings
  > LEVEL 2 CORROSION, CORROSION SEAT TRACK +Y1292 LOCATED AT FR 20 AT FWD GALLEY AREA (SSI 531189). C/A: REPLACED SEAT TRACK Y1292 LOCATED AT FR12 TO FR24 AT FWD GALLEY AREA IAW SRM 51-42-11, SRM 51-72-11 AND DWG D53112812, DWG D53110984, DWG D53110920, MEASURE
- [SDR DALA2026071604180](https://openairdocs.org/sdr/DALA2026071604180.md): Seat Track · corroded · Jul 16, 2026 · N378NW · Airbus A320211 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK +Y765 LOCATED ON HARD POINT, FR 16 AT FWD GALLEY AREA. REPLACED THE SEAT TRACK Y765 LOCATED BTW FR12 TO FR24 AT FWD GALLEY AREA IAW SRM 51-72-11, SRM 51-42-11 DWG D53110920 AND DWG D53112812. MEASURE OF CORROSION SEAT TRACK Y765 WAS
- [SDR DALA2026071504154](https://openairdocs.org/sdr/DALA2026071504154.md): Seat Track · corroded · Jul 15, 2026 · N378NW · Airbus A320211 · Fuselage, Seat/Cargo Attach Fittings
  > LEVEL 2 CORROSION ON SEAT TRACK -Y1292, FR 20 AT FWD GALLEY AREA. REPLACED SEAT TRACK -Y1292 BTW FR 12 TO FR 24 IAW SRM 51-42-11, SRM 51-72-11, DWG D53110920, AND DWG D53110984. MEASURES OF CORROSION WERE L= 2.027 INCHES, W= 0.424 INCHES D= 0.050 INCHES. RI
- [SDR DALA2026071504152](https://openairdocs.org/sdr/DALA2026071504152.md): Web · corroded · Jul 14, 2026 · N378NW · Airbus A320211 · Fuselage Miscellaneous Structure
  > LEVEL 2 CORROSION, WEB FRAME 20 AT LEVEL STR 23L AT FWD GALLEY AREA. REPLACED THE WEB BTW FR 20 - 24, STR 23L AT FWD GALLEY AREA IAW SRM 51-42-11, SRM 51-72-11, DWG: D53114392 ISSUE: B00, DWG D53114332 ISSUE: B00, DWG D53111225 ISSUE: B00, AND DWG D5311
- [SDR DALA2026071504151](https://openairdocs.org/sdr/DALA2026071504151.md): Seat Track · corroded · Jul 14, 2026 · N378NW · Airbus A320211 · Fuselage, Seat/Cargo Attach Fittings
  > LEVEL 2 CORROSION, CORROSION SEAT TRACK -Y1292 LOCATED BTW FR 64 TO FR 66 AT AFT GALLEY AREA. REPLACED SEAT TRACK -Y1292 LOC. BTW FR64 TO FR 66 IN AFT GALLEY AREA IAW SRM 51-72-11, SRM 51-42-11 AND DWG: D38370017 ISSUE: K, DWG: D21270904 ISSUE: T AND DWG:
- [SDR DALA2026071504149](https://openairdocs.org/sdr/DALA2026071504149.md): Fitting · corroded · Jul 13, 2026 · N378NW · Airbus A320211 · Fuselage Miscellaneous Structure
  > LEVEL 2 CORROSION, CENTER FITTING LOCATED BTW FR 16 TO FR 20 AT LEVEL STR 23L CUT OUT FWD GALLEY AREA. REPLACED CENTER FITTING AND FASTENERS LOC. BTW FR 16 TO FR 20 AT LEVEL STR 23L CUT OUT FWD GALLEY AREA IAW SRM 51-42-11, SRM 51-72-11 AND DWG D53112109,
- [SDR DALA2026071304089](https://openairdocs.org/sdr/DALA2026071304089.md): Frame · corroded · Jul 13, 2026 · N378NW · Airbus A320211 · Fuselage Main, Frame
  > LEVEL 2 CORROSION, CORROSION WEB FRAME 20 LOCATED LEVEL STR 23R AT FWD GALLEY AREA. REPLACED WEB AND FASTENERS LOC. ON FRAME 20 AT LEVEL STR 23R IN FWD GALLEY AREA AS PER A320 SRM 51-42-11, A320 SRM 51-72-11,DWG: D53114392 RELEASE DATE: 01-FEB-19 ISSUE:B00 AN
- [SDR DALA2026071304088](https://openairdocs.org/sdr/DALA2026071304088.md): Support · corroded · Jul 12, 2026 · N378NW · Airbus A320211 · Fuselage Miscellaneous Structure
  > LEVEL 2 CORROSION, CORROSION LOWER SILL LOCATED AT FR 68 AT LEVEL STR 23R AT AFT GALLEY AREA (SSI 534147). PERFORMED REPAIR INSTRUCTIONS ON LOWER SILL LOCATED AT FR 68 AT LEVEL STR 23R AT AFT GALLEY AREA AS PER SRM 53-41-14-300- 001 PARAGRAPH 2. A ITEM (1) T
- [SDR DALA2026071304086](https://openairdocs.org/sdr/DALA2026071304086.md): Floor Support · cracked · Jul 11, 2026 · N378NW · Airbus A320211 · Fuselage Miscellaneous Structure
  > CRACK FLOOR STRUCTURE BEAM LOCATED BTW FR 20 TO FR 21 AT LEVEL -Y 189 AT FWD GALLEY AREA. REPLACED FLOOR STRUCTURE BEAM -Y189 LOCATED BTW FR 20 TO FR 24 AT LEVEL FWD GALLEY AREA AS PER A320 SRM 51-42-11, SRM 51-72-11, DWG D53111406 RELEASE DATE:20-DEC-96 ISSU
- [SDR DALA2026071304085](https://openairdocs.org/sdr/DALA2026071304085.md): Seat Track · corroded · Jul 10, 2026 · N378NW · Airbus A320211 · Fuselage, Seat/Cargo Attach Fittings
  > LEVEL 2 CORROSION, CORROSION SEAT TRACK -Y765 LOCATED AT FR 20 AT FWD GALLEY AREA (SSI 531189). REPLACED SEAT TRACK - Y765 LOC. BTW FR12 TO FR24 AT FWD GALLEY AREA AS PER A320 SRM 51-72-11, AS PER A320 SRM 51-42-11 AND DWGD53112812; RELEASE DATE: 08-JAN-97; I
- [SDR DALA2026070904016](https://openairdocs.org/sdr/DALA2026070904016.md): Seat Track · corroded · Jul 8, 2026 · N378NW · Airbus A320211 · Fuselage, Seat/Cargo Attach Fittings
  > SHIP 3278 DISC: LEVEL 2 CORROSION, CORROSION SEAT TRACK LOCATED BTW FR 66 TO FR 68 AND -Y1292 TO-Y1162.5 AT AFT GALLEY AREA (SSI534147). REPLACED SEAT TRACK LOCATED BTW FR 66 TO FR 68 AND -Y1292 TO-Y1162.5 AT AFT GALLEY AREA AS PER A320 SRM 51-42-11, A320 SRM
- [SDR DALA2026070904015](https://openairdocs.org/sdr/DALA2026070904015.md): Seat Track · corroded · Jul 8, 2026 · N378NW · Airbus A320211 · Fuselage, Seat/Cargo Attach Fittings
  > LEVEL 2 CORROSION, CORROSION SEAT TRACK -Y1162.5 LOCATED BTW FR 68 TO FR 69 AT AFT GALLE Y AREA (SSI 534147). REPLACED SEAT TRACK -Y1162.5 LOCATED BTW FR 68 TO FR 69 AT AFT GALLEY AREA AS PER A320 SRM 51-42-11, A320 SRM 51-72-11, DWGD53472780 RELEASE DATE: 26
- [SDR DALA2026070904014](https://openairdocs.org/sdr/DALA2026070904014.md): Dummy Rail · corroded · Jul 8, 2026 · N378NW · Airbus A320211 · Fuselage, Seat/Cargo Attach Fittings
  > LEVEL 2 CORROSION, CORROSION RAIL DUMMY Y503.2 LOCATED AT FR 16 FWD GALLEY AREA (SSI 531189). REPLACED RAIL DUMMY AND FASTENERS LOC Y503.2 BTW FR12 TO FR16 FWD GALLEY AREA, AS PER A320 SRM 51-42-11 AND A320 SRM 51-72-11 ANDDWG D53112825 RELEASE DATE 08-JAN-97
- [SDR DALA2026070904013](https://openairdocs.org/sdr/DALA2026070904013.md): Seat Track · corroded · Jul 8, 2026 · N378NW · Airbus A320211 · Fuselage, Seat/Cargo Attach Fittings
  > LEVEL 2 CORROSION, CORROSION SEAT TRACK LOCATED BTW FR 66 TO FR 68 AND -Y1292 TO-Y1162.5 AT AFT GALLEY AREA (SSI534147). REPLACED SEAT TRACK LOCATED BTW FR 66 TO FR 68 AND -Y1292 TO-Y1162.5 AT AFT GALLEY AREA AS PER A320 SRM 51-42-11, A320 SRM51-72-11 AND DWG
- [SDR DALA2026070904012](https://openairdocs.org/sdr/DALA2026070904012.md): Seat Track · corroded · Jul 8, 2026 · N378NW · Airbus A320211 · Fuselage, Seat/Cargo Attach Fittings
  > LEVEL 2 CORROSION, CORROSION SEAT TRACK -Y1162.5 LOCATED BTW FR 68 TO FR 69 AT AFT GALLE Y AREA (SSI 534147). REPLACED SEAT TRACK -Y1162.5 LOCATED BTW FR 68 TO FR 69 AT AFT GALLEY AREA AS PER A320 SRM 51-42-11, SRM 51-72-11, DWGD53472780 RELEASE DATE: 26/APR/
- [SDR DALA2026070603922](https://openairdocs.org/sdr/DALA2026070603922.md): Floorbeam · corroded · Jul 6, 2026 · N378NW · Airbus A320211 · Fuselage Main, Floor Beam
  > LEVEL 2 CORROSION, CORROSION FLOOR BEAM -Y765 LOCATED AT FR 68 AT AFT GALLEY AREA (SSI 5 34147). REPLACED FLOOR BEAM -Y765 LOCATED BTW FR 66 TO FR70 AT AFT GALLEY AREA AS PER A320 SRM 51-42-11, A320 SRM 51-72-11 AND DWGD53472093 RELEASE DATE 06-DEC-24 ISSUE L
- [SDR DALA2026070503912](https://openairdocs.org/sdr/DALA2026070503912.md): Floor Support · corroded · Jul 4, 2026 · N378NW · Airbus A320211 · Fuselage Miscellaneous Structure
  > LEVEL 2 CORROSION, CORROSION FLOOR BEAM Y254 LOCATED BTW FR 18 TO FR 21 AT FWD GALLEY AR EA (SSI 531189). REPLACED FLOOR BEAM Y254 LOC. FR12 TO FR24 AT FWD GALLEY AREA AS PER A320 SRM 51-42-11, A320 SRM 51-72-11 AND DWG D53110920RELEASE DATE: 28-APR-21 ISSUE:
- [SDR DALA2026070503911](https://openairdocs.org/sdr/DALA2026070503911.md): Shear Plate · cracked · Jul 3, 2026 · N378NW · Airbus A320211 · Fuselage Miscellaneous Structure
  > LEVEL 2 CORROSION, CORROSION SHEAR PLATE LOCATED BTW FR 69 TO FR 70 AT LEVEL STR 23L AT AFT GALLEY AREA. REPLACED SHEAR PLATE, AND FASTENERS LOCATED BTW FR 69 TO FR 70 AT LEVEL STR 23L AT AFT GALLEY AREA AS PER A320 SRM 51-42-11, SRM 51-72-11 AND DWG D5347418
- [SDR DALA2026070503910](https://openairdocs.org/sdr/DALA2026070503910.md): Shear Plate · cracked · Jul 3, 2026 · N378NW · Airbus A320211 · Fuselage Miscellaneous Structure
  > CRACKED SHEAR PLATE LOCATED BTW FR 69 TO FR 70 AT LEVEL STR 23R AT AFT GALLEY AREA. REPLACED SHEAR PLATE, AND FASTENERS LOCATED BTW FR 69 TO FR 70 AT LEVEL STR 23R AT AFT GALLEY AREA AS PER A320 SRM 51-42-11, SRM 51-72-11 AND DWG D53474180 AA AND DWG D92490
- [SDR DALA2026070203881](https://openairdocs.org/sdr/DALA2026070203881.md): Receptacle · corroded · Jul 2, 2026 · N378NW · Airbus A320211 · Nacelle/Pylon, Main Frame
  > LEVEL 2 CORROSION, CORROSION SPIGOT FITTING RECEPTACLE ON LH PYLON. REPLACED SPIGOT FITTING RECEPTACLE ON LH PYLON AS PER A320 SRM 54-51-12-300-001. TOOK MEASURE INITIAL DIAMETER IS: 4.331 INCH. (LP: 1677696, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026070203880](https://openairdocs.org/sdr/DALA2026070203880.md): Receptacle · corroded · Jul 1, 2026 · N378NW · Airbus A320211 · Nacelle/Pylon, Main Frame
  > LEVEL 2 CORROSION, CORROSION SPIGOT FITTING RECEPTACLE ON RH PYLON. REPLACED SPIGOT FITTING RECEPTACLE ON RH PYLON AS PER A319 SRM 54-51-12-300-001. TOOK MEASURE INITIAL DIAMETER IS: 4.331 INCH.SEE INDIVIDUAL SIGN OFF ON ORNRC 68/400. RII INSPECTION COMPLETE.
- [SDR DALA2026011700397](https://openairdocs.org/sdr/DALA2026011700397.md): Light · detached · Jan 13, 2026 · N378NW · Airbus A320211 · Emergency Lighting
  > EMERGENCY SEAT MOUNTED LIGHTING DAMAGED, INOPERATIVE. LOCATION: 20D. LIGHT ASSEMBLY DETACHED, HANGING FROM SEAT. R &R REPLACED 20D LIGHT ASSY HOUSING AND OPS TEST GOOD ALL WORK DONE IAW AMM 33-20. (LP: 1399329)
- [SDR DALA2026011100247](https://openairdocs.org/sdr/DALA2026011100247.md): Flap System · faulted · Jan 10, 2026 · N378NW · Airbus A320211 · Trailing Edge Flap Control System
  > AFTER T/O, TE FLAP DID NOT FULLY RETRACT WING TIP BREAK ON. LANDED WITH SLATS EXTENTED, FLAP <1 MED BRAKES. T/S IN REF A320 TSM 27-51-00-810-840-A RESET WTB FAULT WENT AWAY NO OTHER FAULTS NOTED. OPS CK FLAP SYS IN REF A320 AMM 27-54 OPS CK GOOD NO DEFECTS OR

Next page: https://openairdocs.org/aircraft/N378NW/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 = 'N378NW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N378NW/reports

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