# Service difficulty reports: N341NW

A list on [N341NW](https://openairdocs.org/aircraft/N341NW.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 · 204 reports

- [SDR DALA2026091405116](https://openairdocs.org/sdr/DALA2026091405116.md): Fan · failed · Sep 13, 2026 · N341NW · Airbus A320212 · Air Distribution Fan
  > TEN MINUTES PRIOR TO TOP OF DESCENT BOTH PILOTS SMELLED A BURRING PLASTIC SMELL WHICH CONTINUED THROUGH MOST OF THE DESCENT. WE HEARD A SLIGHT WAILING NOISE JUST PRIOR TO THE SMELL. C/A: STARTED TROUBLESHOOTING PER AMDS WORK CARD 0550-2002. INSPECTED COCKPIT I
- [SDR DALA2026090705013](https://openairdocs.org/sdr/DALA2026090705013.md): Unknown · odor · Sep 4, 2026 · N341NW · Airbus A320212 · Air Distribution System
  > CREW VERBALIZED ELECTRICAL ODOR IN THE CABIN FOLLOWED MUSK. APU ON, NO PAX ON BOARD. T/S ODOR IAW WC 0550-2002. PER GVI OF APU COMPARTMENT W/ BLACKLIGHT INSIDE INTAKE PLENUM. NO OIL VISIBLE W BLACK LIGHT INSIDE INTAKE PLENUM. PER STE 5 OF WC 0550-2002, PERF L
- [SDR DALA2026082504806](https://openairdocs.org/sdr/DALA2026082504806.md): Oxygen Mask · unwanted deploy · Aug 23, 2026 · N341NW · Airbus A320212 · Passenger Oxygen System
  > AFTER TAKEOFF PAX MASK AT 21DEF DEPLOYED. REPACKED THE PASSENGER OXYGEN MASK AT SEAT 21DEF IAW A320 AMM 35 -21-43. (LP: 9197306, IARCRAFT WAS GROUNDED)
- [SDR DALA2026071304090](https://openairdocs.org/sdr/DALA2026071304090.md): Oxygen Mask · unwanted deploy · Jul 6, 2026 · N341NW · Airbus A320212 · Passenger Oxygen System
  > O2 MASKS DROPPED AT 10A-C. RESET O2 MASK COVER PER AMM 35-12. ACFT OK. FOR SERVICE. (LP: 8441468, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026062203692](https://openairdocs.org/sdr/DALA2026062203692.md): Oxygen Panel · open · Jun 17, 2026 · N341NW · Airbus A320212 · Passenger Oxygen System
  > PASSENGER OXYGEN MASK PANEL OPENED IN FLIGHT ABOVE SEATS 2C AND D. FWD TO MEL 35- 21-01A. M PROCEDURE C/W AND PLACARD INSTALLED. SEATS 2 C AND D UNUSABLE. RESECURED O2 CONTAINER DOOR AT 2CD PER AMM 35-21. M PROCEDURES REVERSED. MEL PLACARD REMOVED. OK FOR SE
- [SDR DALA2026060503399](https://openairdocs.org/sdr/DALA2026060503399.md): Window Frame · cracked · Jun 4, 2026 · N341NW · Airbus A320212 · Fuselage Main, Structure
  > CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHM ENT AREA CONTINUITY FITTING RH SIDE, CRACK LENGTH IS 0.200 INCH, AD RE LATED, AA 5311-01226, AD 2020-17-03, WORK CARD 5311-01226-01. REQUESTI NG REPAIR DISPOSITION. REPAIR MUST BE ACCOMPLISH
- [SDR DALA2026060503398](https://openairdocs.org/sdr/DALA2026060503398.md): Window Frame · none · Jun 4, 2026 · N341NW · Airbus A320212 · Fuselage Main, Structure
  > PERFORM ER/A 633637-14AD FOR WINDSHIELD FRAMING CENTER POST LT AND RT SIDE AT COCKPIT AREA. COMPLIED WITH ER/A 633637-14AD REV. ORIGINAL APPROVED DATE 28- MAY-26 MATCHES WITH ALL STEPS ON PRI 633637-14AD REV. 0; REV. 1; ITHAS BEEN VALIDATED. PERFORMED REPAIR I
- [SDR DALA2026060203349](https://openairdocs.org/sdr/DALA2026060203349.md): Window Frame · cracked · Jun 1, 2026 · N341NW · Airbus A320212 · Fuselage Main, Structure
  > CRACK INDICATION FOUND IN FASTENER HOLE LOCATED AT THE LT FR4 LATERAL WINDOW UPPER JUNCTION. CRACK DEPTH = 0.138 INCHES, CRACK DIRECTION 10 O CLOCK. IN COCKPIT. AA NUMBER 5311-01236-01. AD RELATED, WORK CARD 53 11-01236-01. REQUESTING REPAIR DISPOSITION. REPAI
- [SDR DALA2026053103303](https://openairdocs.org/sdr/DALA2026053103303.md): Floorbeam · cracked · May 30, 2026 · N341NW · Airbus A320212 · Fuselage Main, Floor Beam
  > AD RELATED AA 5711-01036-CENTER WING FRONT SPAR VERTICAL STRINGERS, CRACKS FOUND ON FLOORBEAM SIDE VERTICAL RADIUS AT-Y765 ZONE 1 CRACK L= 0.250 INCHES APPROX AT ZONE 2 CRACK L= 0.400 INCH APPROX, REPAIR IS R EQUIRED PRIOR TO FUTHER FLIGHT. COMPLIED WITH ER/A
- [SDR DALA2026053103302](https://openairdocs.org/sdr/DALA2026053103302.md): Structure · damaged · May 30, 2026 · N341NW · Airbus A320212 · Fuselage Miscellaneous Structure
  > DURING DVI WAS FOUND EXISTENT REPAIR BUSHING LOCATED ON SPAR VERTICAL STRINGER AT FR 36 ZONE 1 AND 2 -Y765 ( AD RELATED AA 5711-01036). PERFORMED REPAIR INSTRUCTION ON SPAR VERTICAL STRINGER AT FR 36 ZONE 1 AND ZONE 2 ON -Y765 AS PER ER/A 587692-14AD REV. B S
- [SDR DALA2026053103301](https://openairdocs.org/sdr/DALA2026053103301.md): Structure · damaged · May 30, 2026 · N341NW · Airbus A320212 · Fuselage Miscellaneous Structure
  > DURING DVI WAS FOUND EXISTENT REPAIR BUSHING LOCATED ON SPAR VERTICAL STRINGER AT FR 36 ZONE 1 AND 2 -Y254 (AD RELATED AA 5711-01036). PERFORMED REPAIR INSTRUCTIONS ON SPAR VERTICAL STRINGER AT FR 36 ZONE 1 AND ZONE 2 ON -Y254 AS PER ER/A 587692-14AD REV. B S
- [SDR DALA2026053103299](https://openairdocs.org/sdr/DALA2026053103299.md): Stop Fitting · damaged · May 29, 2026 · N341NW · Airbus A320212 · Fuselage Main, Structure
  > EXISTING REPAIR FR68, INNER CAP & FR FLANGE, STRG 22 RH AT LEVEL DOOR STOP FITTING 1. CONTACT DELTA LIAISON ENGINEERING FOR ALTERNATE INSPECTION INSTRUCTIONS THAT MAY BE REQUIRED TO COMPLETE WORK CARD 5311-0124 4-02B DUE TO PREVIOUS REPAIR IN THE INSPECTION AR
- [SDR DALA2026053103297](https://openairdocs.org/sdr/DALA2026053103297.md): Floorbeam · cracked · May 29, 2026 · N341NW · Airbus A320212 · Fuselage Main, Floor Beam
  > DURING M2 AND WHILE ACCOMPLISHING EM 5711-01036-03B, PREVIOUSLY REPAIRED HOLES FOUND AT -Y254 AND -Y765 ALONG WITH CRACK INDICATION FOUND IN THE RADIUS OF HORIZONTAL FLOOR BEAM AT -Y765. PER SECTION IV OF 587692-14AD REV B, ACCOMPLISH SECTION IV REPETITIVE IN
- [SDR DALA2026053103295](https://openairdocs.org/sdr/DALA2026053103295.md): Window Frame · cracked · May 28, 2026 · N341NW · Airbus A320212 · Fuselage Main, Structure
  > *DTE* DURING M2 AND WHILE INSPECTING PER EM 5311-01236-01 CRACK INDICATIONS FOUND IN LH LATERAL WINDOW FRAME UPPER JUNCTION FASTENER HOLE #1 AND HOLE #3. *DTE* PER SECTION DTE OF 633473-14, THE REPAIR OF SECTION I IS LIMITED TO 20,700 FC FROM SECTION I (18MAY
- [SDR DALA2026052803237](https://openairdocs.org/sdr/DALA2026052803237.md): Window Frame · cracked · May 28, 2026 · N341NW · Airbus A320212 · Fuselage Main, Frame
  > AIRCRAFT 3241, CRACK INDICATION FOUND IN FASTENER HOLE LOCATED AT THE RH FR4 LATERAL WINDOW UPPER JUNCTION. CRACK DEPTH = 0.079 INCHES, CRACK DIRECTION 2 O CLOCK. IN COCKPIT. AA NUMBER 5311-01236-02. AD RELATED, WORK CARD 531 1-01236-02. CORRECTIVE ACTION: PER
- [SDR DALA2026053103294](https://openairdocs.org/sdr/DALA2026053103294.md): Fitting · cracked · May 27, 2026 · N341NW · Airbus A320212 · Fuselage Main, Structure
  > *DTE* DURING M2 WHILE INSPECTING PER EM 5311-01226-01, THE RHS CONTINUITY FITTING WAS FOUND CRACKED. FURTHER INSPECTION REVEALED HOLES D1 ON RH AND LH SIDES WERE ALSO CRACKED IN FRONT WINDSHIELD LWR CTR NODE AREA. C/A: *DTE* PER SECTION DTE OF 633637-14AD THE
- [SDR DALA2026053103293](https://openairdocs.org/sdr/DALA2026053103293.md): Fitting · cracked · May 27, 2026 · N341NW · Airbus A320212 · Fuselage Main, Structure
  > DURING M2 AND WHILE INSPECTING PER EM 5311-01226-01, THE RHS CONTINUITY FITTING WAS FOUND CRACKED. FURTHER INSPECTION REVEALED THAT HOLES D1 ON RH AND LH SIDES WERE ALSO CRACKED IN FRONT WINDSHIELD LWR CTR NODE AREA. PER SECTION II OF 633637-14AD, ACCOMPLISH
- [SDR DALA2026053103292](https://openairdocs.org/sdr/DALA2026053103292.md): Fitting · cracked · May 27, 2026 · N341NW · Airbus A320212 · Fuselage Main, Structure
  > DURING M2 AND WHILE INSPECTING PER EM 5311-01226-01, THE RHS CONTINUITY FITTING WAS FOUND CRACKED. FURTHER INSPECTION REVEALE D THAT HOLES D1 ON RH AND LH SIDES WERE ALSO CRACKED IN FRONT WINDSHIELD LWR CTR NODE AREA. PER SECTION II OF 633308-14AD, ACCOMPLISH
- [SDR DALA2026052703214](https://openairdocs.org/sdr/DALA2026052703214.md): Window Frame · damaged · May 21, 2026 · N341NW · Airbus A320212 · Fuselage Main, Structure
  > SHIP 3241 DISC: DTE ERA 633400-14AD REV. ORIGINAL. REPAIR AT FR4 LATERAL WINDOW FRAME REQUIRES DTE FOLLOW UP PRIOR TO 64,502 TFC. C/A: REVISE AND UPDATE ERA 633400-14AD WITH DTE RESULTS PRIOR TO 64,502 TFC. REFERENCE AIRBUS DOSSIER 81769612. ASSOCIATED AA 5311
- [SDR DALA2026051603023](https://openairdocs.org/sdr/DALA2026051603023.md): Repair · none · May 11, 2026 · N341NW · Airbus A320212 · Standard Practices/Structures
  > INSPECTION ER/A 633568-14 REV ORIGINAL. REPAIR AT REAR FUSELAGE, SKIN AT FR70, BTWN STR31-32RH REQUIRES FOLLOW ON INSPECTIONS PRIOR TO 56,802 TFC AND EVERY 13,000 FC, THEREAFTER. ACCOMPLISH FOLLOW ON INSPECTIONS PER ER/A 633568-14 SECTION II, PRIOR TO 56,802 T
- [SDR DALA2026051102939](https://openairdocs.org/sdr/DALA2026051102939.md): Stringer · corroded · May 11, 2026 · N341NW · Airbus A320212 · Fuselage Main, Longeron/Stringer
  > LEVEL 2 CORRSION, STRINGER 43L BTW FR 56 TO FR 58 IN AFT CARGO COMPARTMENT (SSI 534107). REPLACED STRINGER 43L BTW FR 54 TO FR 60 IN AFT CARGO COMPARTMENT AS PER 320 SRM 51-72-11, A320 SRM 51-42-11 AND DWG D53470345ISSUE: W, RELEASE DATE: 02-NOV-98 AND DWG D5
- [SDR DALA2026051102937](https://openairdocs.org/sdr/DALA2026051102937.md): Skin · dented · May 10, 2026 · N341NW · Airbus A320212 · Fuselage Main, Plate/Skin
  > : RE-EVALUATE DENT FOR BIRD STRIKE EXTERNAL SKIN LOC. BTW FR1 TO FR 2 AT LEVEL OF -Z339 RH SIDE UPPER FUSELAGE (REFERENCE TO LOG PAGE 8221811). PERFORMED PERMANENT REPAIR AS PER A320 SRM 53-11-11-300-041, LOCATED ON EXTERNAL SKIN BTW FR 1 TO FR 3 AT LEVEL OF
- [SDR DALA2026050802917](https://openairdocs.org/sdr/DALA2026050802917.md): Floor Support · cracked · May 7, 2026 · N341NW · Airbus A320212 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL FITTING LOCATED INTERNAL STRUCTURE FROM FR11 TO FR1 2 AND Y765 IN COCKPIT. REPLACED INTERCOSTAL FITTING LOCATED INTERNAL STRUCTURE FROM FR11 TO FR12 AND Y765 IN COCKPIT AS PER A320 SRM 51-42-11, SRM 51-72-11 AND DWG D53112787 ISSUE: DOO REL
- [SDR DALA2026050802916](https://openairdocs.org/sdr/DALA2026050802916.md): Floor Support · cracked · May 7, 2026 · N341NW · Airbus A320212 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL FITTING LOCATED INTERNAL STRUCTURE FROM FR11 TO FR12 AND Y765 IN COCKPIT. REPLACED INTERCOSTAL FITTING LOCATED INTERNAL STRUCTURE FROM FR11 TO FR12 AND Y765 IN COCKPIT AS PER A320 SRM 51-42-11, SRM51 -72-11 AND DWG D53112787 ISSUE: DOO REL
- [SDR DALA2026050802914](https://openairdocs.org/sdr/DALA2026050802914.md): Shear Tie · punctured · May 6, 2026 · N341NW · Airbus A320212 · Fuselage Internal Mounting Structure
  > PUNCTURE SHEAR TIE ON FR 58 AND BTW STR 43R TO STR 44 IN AFT CARGO COMPARTMENT. REPLACED SHEAR TIE ON FR 58 AND BTW STR 43R TO STR 44 IN AFT CARGO COMPARTMENT AS PER A320 SRM 51-72-11, SRM 51-42-11-801, DWG D53470342 ISSUE AE RELEASE DATE 08-JUL-97, DWG D5347
- [SDR DALA2026050502834](https://openairdocs.org/sdr/DALA2026050502834.md): Floor Support · corroded · May 3, 2026 · N341NW · Airbus A320212 · Fuselage Miscellaneous Structure
  > CORRODED FLOOR SUPPORT -Y765 LOCATED BTW FR 66 TO FR 68 AT AFT GALLEY AREA. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, SRM 51-42-11, DWG D53472816 ISSUE: F AND DWG D53472815, ISSUE: G. MEASURE OF CORROSION WAS L=0.793 IN, W=0.636 IN. D= 0.020 IN. (LP: 1
- [SDR DALA2026050302787](https://openairdocs.org/sdr/DALA2026050302787.md): Floor Support · corroded · May 1, 2026 · N341NW · Airbus A320212 · Fuselage Miscellaneous Structure
  > LEVEL 2 CORROSION FLOOR BEAM +Y254 LOCATED BTW FR 16 TO FR 21 FWD GALLEY AREA (SSI 531189). REPLACED FLOOR BEAM Y254 AND FASTENERS LOCATED BTW FR12 TO FR 24 AT FWD GALLEY AREA AS PER A320 SRM 51-72-11, A320 SRM 51-42-11 AND DWG D53212367 RELEASE DATE 18-MAY-2
- [SDR DALA2026050302786](https://openairdocs.org/sdr/DALA2026050302786.md): Web · corroded · May 1, 2026 · N341NW · Airbus A320212 · Fuselage Miscellaneous Structure
  > LEVEL 2 CORROSION WEB LOCATED AT FR 16 LEVEL STR 23R AT FWD GALLEY AREA. REPLACED WEB LOCATED ON FR12 TO FR16 AT LEVEL STR 23R AT FWD GALLEY AREA IAW SRM 51-72-11; A320 SRM 51-42-11, DWG D53114392 ISSUE B00, RELEASE DATE 01-FEB-19, DWG D53112781 ISSUE E00, RE
- [SDR DALA2026050102760](https://openairdocs.org/sdr/DALA2026050102760.md): Floor Support · corroded · Apr 29, 2026 · N341NW · Airbus A320212 · Fuselage Miscellaneous Structure
  > CORROSION LEVEL 2 FLOOR BEAM +Y765 HARD POINT BTW FR 69 TO FR 70 AT AFT GALLE Y AREA (SSI 534147). REPLACED FLOOR BEAM Y765 AND FASTENERS LOCATED BTW FR 66 TO FR 70 AT AFT GALLEY AREA. AS PER A320 SRM 51-72-11, A320 SRM 51-42-11. (LP 1569278 - AIRCRAFT WAS G
- [SDR DALA2026050102759](https://openairdocs.org/sdr/DALA2026050102759.md): Floor Support · corroded · Apr 29, 2026 · N341NW · Airbus A320212 · Fuselage Miscellaneous Structure
  > CORROSION LEVEL 2 FLOOR BEAM -Y1162.5 LOCATED BTW FR 68 TO FR 69 AFT GALLEY AREA (SSI 534147). REPLACED BEAM -Y 1162.5 LOC. BTW FR 68 TO FR 69 AT AFT GALLEY AREA AND FASTENERS AS PER A320 SRM 51-42-11, A320 SRM 51-72-11. (LP 1569179 - AIRCRAFT WAS GROUNDED)
- [SDR DALA2026050102758](https://openairdocs.org/sdr/DALA2026050102758.md): Seat Track · corroded · Apr 29, 2026 · N341NW · Airbus A320212 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION LEVEL 2 SEAT TRACK -Y1292 LOCATED AT FR 20 AT FWD GALLEY AREA (SSI 531189). REPLACED SEAT TRACK -Y1292 AND FASTENERS LOC. FR12 TO FR24 AT FWD GALLEY AREA AS PER A320 SRM 51-42-11, A320 SRM 51-72-11. (LP 1569168 - AIRCRAFT WAS GROUNDED)
- [SDR DALA2026050102757](https://openairdocs.org/sdr/DALA2026050102757.md): Floor Support · corroded · Apr 29, 2026 · N341NW · Airbus A320212 · Fuselage Miscellaneous Structure
  > CORROSION LEVEL 2 FLOOR BEAM +Y1162.5 LOCATED BTW FR 68 TO FR 69 AT AFT GALLE Y AREA (SSI 534147). REPLACED FLOOR BEAM Y1162.5 AND FASTENERS LOCATED BTW FR 68 TO FR 69 AT AFT GALLEY AREA AS PER A320 SRM 51-42-11, A320 SRM 51-72-11. (LP 1569105 - AIRCRAFT WAS
- [SDR DALA2026050102756](https://openairdocs.org/sdr/DALA2026050102756.md): Floor Support · corroded · Apr 29, 2026 · N341NW · Airbus A320212 · Fuselage Miscellaneous Structure
  > CORROSION LEVEL 2 FLOOR BEAM +Y1292 TO Y1162.5 BTW FR 66 TO FR 68 AT AFT GALLEY AREA (SSI 534147). REPLACED FLOOR BEAM Y1292 AND FASTENERS LOC. BTW FR 66 TO FR 68 AT AFT GALLEY AREA AS PER A320 SRM 51-42-11, A320 SRM 51-72-11. (LP 1569095 - AIRCRAFT WAS GROU
- [SDR DALA2026050102777](https://openairdocs.org/sdr/DALA2026050102777.md): Bottle · no test · Apr 28, 2026 · N341NW · Airbus A320212 · Passenger/Crew Doors
  > WILL NOT PASS TEST PASSENGER CREW DOOR 832 DOOR DAMPER OPS CYLINDER AT AFT GALLEY AREA (1 EA). REMOVED DOOR DAMPER P/N FE174-004 S/N 553 ON UNSERVICEABLE CONDITION ON PASSENGER CREW DOOR 832 IAW FAM AMM-52-13- 14-000-001-A STEP 3.B,C AND 4.A JOB IN PROGRESS.
- [SDR DALA2026042902713](https://openairdocs.org/sdr/DALA2026042902713.md): Floor Support · corroded · Apr 26, 2026 · N341NW · Airbus A320212 · Fuselage Miscellaneous Structure
  > LEVEL 2 CORROSION FLOOR BEAM -Y1292 TO -Y1162.5 BTW FR 66 TO FR 68 AT AFT GA LLEY AREA (SSI 534147). C/A: REPLACED FLOOR BEAM -Y1292 LOC. BTW FR 66 TO FR 68 AT AFT GALLEY AREA AND FASTENERS AS PER A320 SRM 51-42-11, A320 SRM 51-72- 11AND DWG: D53472780, RELEAS
- [SDR DALA2026042902712](https://openairdocs.org/sdr/DALA2026042902712.md): Shear Plate · corroded · Apr 26, 2026 · N341NW · Airbus A320212 · Fuselage Miscellaneous Structure
  > LEVEL 2 CORROSION SHEAR PLATE LOCATED BTW FR 69 TO FR 70 LEVEL STR 23R AT AFT GALLEY AREA. REPLACED SHEAR PLATE AND FASTENERS LOCATED BTW FR69 TO FR70 AT LEVEL STR23R AT AFT GALLEY AREA AS PER A320 SRM 51-42-11, A320 SRM 51-72-11 AND DWG: D53474180, RELEASE D
- [SDR DALA2026042902711](https://openairdocs.org/sdr/DALA2026042902711.md): Fitting · corroded · Apr 26, 2026 · N341NW · Airbus A320212 · Nacelle/Pylon, Main Frame
  > LEVEL 2 CORROSION BORE SPIGOT FITTING RECEPTACLE ON RH PYLON. REPLACED SPIGOT FITTING LOC. ON RH PYLON IAW SRM 54-51- 12-300-001-A. MEASURE OF DIAMETER WAS: 4.350 INCH. TOOL USED: DIGITAL CALIPER P/N 500-197-30; S/N: B23316908; DUE DATE: 12-NOV -26. SEE INDIV
- [SDR DALA2026042902710](https://openairdocs.org/sdr/DALA2026042902710.md): Dampener · no test · Apr 25, 2026 · N341NW · Airbus A320212 · Passenger/Crew Doors
  > DONT PASS TEST PASSENGER CREW DOOR 841 DOOR DAMPER OPERATIONAL CYLINDER (REFER TO AMDS CARD 5210-7089-RF-RII) AT FWD GALLEY AREA (1 EA). REMOVED DOOR DAMPER P/N FE174-0011 S/N 1129 ON UNSERVICEABLE CONDITION ON PASSENGER CREW DOOR 841 AS PER A320 FAM AMM 52-1
- [SDR DALA2026042502625](https://openairdocs.org/sdr/DALA2026042502625.md): Support · corroded · Apr 23, 2026 · N341NW · Airbus A320212 · Fuselage Miscellaneous Structure
  > CORROSION LOWER SILL LOCATED AT FR 68 LH SIDE AT AFT GALLEY AREA (SSI 534147). PERFORMED PERMANENT REPAIR ON LOWER SILL LOCATED AT LEVEL FR68 LH SIDE AFT GALLEY AREA AS PER A320 SRM 53-41-14-300-001, TOOK MEASURE OF CORROSION ARE P1: L= 0.212 INCH, W: 0.117 I
- [SDR DALA2026042202557](https://openairdocs.org/sdr/DALA2026042202557.md): Shear Plate · corroded · Apr 21, 2026 · N341NW · Airbus A320212 · Fuselage Miscellaneous Structure
  > CORROSION SHEAR PLATE LOCATED BTW FR 69 TO FR 70 LEVEL STR 23L AT AFT GALLEY AREA. REPLACED SHEAR PLATE, BRACKETS (2 E/A) AND NEW FASTENERS LOC.BTW FR 69 TO FR 70 AT LEVEL STRG 23LH AT AFT GALLEY AREA AS PER A320 SRM 51-42-11, A320 SRM 51-72-11 AND DWG 534741
- [SDR DALA2026042202556](https://openairdocs.org/sdr/DALA2026042202556.md): Shear Plate · corroded · Apr 21, 2026 · N341NW · Airbus A320212 · Fuselage Miscellaneous Structure
  > CORROSION SHEAR PLATE LOCATED BTW FR 69 TO FR 70 LEVEL STR 23L AT AFT GALLEY AREA. C/A: REPLACED SHEAR PLATE, BRACKETS (2 E/A) AND NEW FASTENERS LOC.BTW FR 69 TO FR 70 AT LEVEL STRG 23LH AT AFT GALLEY AREA AS PER A320SRM 51-42-11, A320 SRM 51-72-11 AND DWG 534
- [SDR DALA2026042002472](https://openairdocs.org/sdr/DALA2026042002472.md): Support · corroded · Apr 19, 2026 · N341NW · Airbus A320212 · Fuselage Miscellaneous Structure
  > CORROSION LOWER SILL LOCATED AT FR 68 RH SIDE AT AFT GALLEY AREA. PERFORMED PERMANENT REPAIR ON LOWER SILL LOCATED AT LEVEL FR68 RH SIDE AFT GALLEY AREA IAW SRM 53-41-14-300-001, TOOK MEASURE OF CORROSION IS: L= 0.3895 INCH W= 0.2695 INCH, (LP: 1551682)
- [SDR DALA2026042002471](https://openairdocs.org/sdr/DALA2026042002471.md): Fitting · cracked · Apr 19, 2026 · N341NW · Airbus A320212 · Fuselage Miscellaneous Structure
  > CRACK INTERNAL STRUCTURE FITTING LOCATED BTW FR 11 TO FR 12 AND -Y765 IN COCKPIT. REPLACED FITTING LOCATED BTW FR 11 TO FR 12 AND -Y765 IN COCKPIT IAW SRM 51-42-11, SRM 51-72-11, AND DWG D53110097, (LP: 1551681). AIRCRAFT WAS GROUNDED
- [SDR DALA2026042002467](https://openairdocs.org/sdr/DALA2026042002467.md): Floor Support · damaged · Apr 17, 2026 · N341NW · Airbus A320212 · Fuselage Miscellaneous Structure
  > MISSING MATERIAL FLOOR SUPPORT LOCATED BTW FR 14 TO FR 16 AND Y940 AT FWD GALLEY AREA. REPLACED FLOOR SUPPORT LOCATED BTW FR 14 TO FR 16 AND Y940 AT FWD GALLEY AREA AS PER A320 SRM 51-72-11; A320 SRM 51-42-11 AND DWG D53112823; ISSUE: F00; RELEASE DATE:14-MAR
- [SDR DALA2026041702443](https://openairdocs.org/sdr/DALA2026041702443.md): Web · corroded · Apr 16, 2026 · N341NW · Airbus A320212 · Fuselage Miscellaneous Structure
  > CORROSION WEB LOCATED AT FR 20 AND -Y1732 AT FWD GALLEY AREA. REPLACED WEB LOC. BTW FRAME 20 AND -Y1732 AT FWD GALLEY AREA AS PER A320 SRM 51-42-11, A320 SRM 51-72-11 AND DWG: D53114392, ISSUE: B00, RELEASE DATE:01/ FEB/19. CORROSION MEASURE WERE: L= 1.442 I
- [SDR DALA2026041702442](https://openairdocs.org/sdr/DALA2026041702442.md): Plate · cracked · Apr 16, 2026 · N341NW · Airbus A320212 · Fuselage Miscellaneous Structure
  > CRACK PLATE LOCATED BTW FR 68 TO FR 69 LEVEL STR 23L AT AFT GALLEY AREA. C/A: REPLACED PLATE AND FASTENERS LOCATED BTW FR 68 TO FR 69 LEVEL STR 23L AT AFT GALLEY AREA. AS PER A320 SRM 51-42-11, A320 SRM 51-72-11 AND DWG: D53480009 RELEASE DATE: 02/MAR/99, ISSU
- [SDR DALA2026041302316](https://openairdocs.org/sdr/DALA2026041302316.md): Web · corroded · Apr 11, 2026 · N341NW · Airbus A320212 · Fuselage Miscellaneous Structure
  > CORROSION WEB LOCATED AT FR 20 LEVEL STR 23L AT FWD GALLEY AREA. REPLACED WEB LOCATED AT FR 20 LEVEL STR 23L AT FWD GALLEY AREA AS PER A320 SRM 51-72-11, SRM 51-42-11 AND DWG D53112545 RELEASE DATE 30-JUN-98 ISSUE: F00 AND DWG D53114392 RELEASE DATE: 01- FEB-
- [SDR DALA2026020600856](https://openairdocs.org/sdr/DALA2026020600856.md): Coffeemaker · odor · Feb 4, 2026 · N341NW · Airbus A320212 · Buffet/Galleys
  > BURNT ELECTRIC SMELL IN FWD GALLEY LEFT COFFEE POT WHEN IN USE. FOUND BURNT SMELL COMING FROM COFFEE MAKER LOCATION 107. REMOVED COFFEE MAKER AND INSPECTED WIRES AND HARNESS FOR DAMAGE. NO TROUBLE FOUND. INSTALLED A NEW COFFEE MAKER. OPS CHECKED AND LEAK CHECK
- [SDR DALA2025021901234](https://openairdocs.org/sdr/DALA2025021901234.md): Engine · failed · Feb 19, 2025 · N341NW · Airbus A320212 · Engine (Turbine/Turboprop)
  > SHIP 3241 -IFSD- RIGHT ENGINE FAILURE/SHUTDOWN CREW DECLARING AN EMERGENCY. CORRECTIVE ACTION: METAL DEBRIS IN TAILPIPE, ENGINE CHANGE IN PROGRESS. (LP: 6883614)
- [SDR DALA2025012700637](https://openairdocs.org/sdr/DALA2025012700637.md): Light · detached · Jan 23, 2025 · N341NW · Airbus A320212 · Emergency Lighting
  > SHIP 3241 DISC: EMERGENCY LIGHTING MOUNTED ON SEAT DETACHED 28D. C/A: FWD TO MEL 33-50-03A. NO "M" PROC. PLACARDS INSTALLED. R/R FLOOR PROXIMITY LIGHT AT 28D REF A320 CMM 25-23-51. MEL AND PLACARD REMOVED. OK FOR SVC. (LP: 6764818)

Next page: https://openairdocs.org/aircraft/N341NW/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 = 'N341NW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N341NW/reports

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