# Service difficulty reports: Airbus A320-212

A list on [Airbus A320-212](https://openairdocs.org/model/airbus-a320-212.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 164 · 8,163 reports

- [SDR DALA2026102305836](https://openairdocs.org/sdr/DALA2026102305836.md): Battery · faulted · Oct 23, 2026 · N360NW · Airbus A320212 · Emergency Lighting
  > FOUND FWD LT EPSU BATTERY FAULT DURING SVC CK. R & R EPSU SUPPLY AND BATTERY IAW AMM 33-51. (LP: 9099389, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026102305835](https://openairdocs.org/sdr/DALA2026102305835.md): Shear Tie · corroded · Oct 21, 2026 · N362NW · Airbus A320212 · Fuselage Internal Mounting Structure
  > LEVEL 2 CORROSION, LOWER FWD FUSELAGE, FWD CARGO COMPARTMENT AT FR33 BETWEEN STGR 40L AND STGR 41L, FRAME CLIP WITH CORROSION. NOTE: FOUND DURING PROCESS OF ORNRC 100-251. REPLACED SHEAR TIE AT FWD CARGO COMPARMENT AT FR 33 BETWEEN STGR 40L AND STGR 40L AND S
- [SDR DALA2026102105782](https://openairdocs.org/sdr/DALA2026102105782.md): Unknown · odor · Oct 20, 2026 · N373NW · Airbus A320212 · Air Distribution System
  > DUE TO BURNING PLASTIC ODOR IN COCKPIT AND FWD GALLEY AREA. NO TROUBLE FOUND. (LP: 7749532, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026102105778](https://openairdocs.org/sdr/DALA2026102105778.md): Anchor Fitting · corroded · Oct 20, 2026 · N362NW · Airbus A320212 · Fuselage, Landing Gear Attach Fittings
  > LOWER FUSELAGE, LT MLG ANCHORAGE FITTING WITH CORROSION. REPAIRED LT MLG ANCHORAGE FITTING UPPER AND LOWER BEARING FACES, LUG BORE AND EDGE CHAMFERS I.A.W. SRM 57-26-13-300-008 REV.159 DATED 15 SEP, 26. THIS IS A REPAIR CATEGORY C. REPAIR LIFE LIMIT AT 48000
- [SDR DALA2026102105777](https://openairdocs.org/sdr/DALA2026102105777.md): Coupling · corroded · Oct 19, 2026 · N362NW · Airbus A320212 · Fuselage Miscellaneous Structure
  > AFT PASSENGER CABIN AT Y-1292 BETWEEN FR67 AND FR68 FLOOR SUPPORT, COUPLING AREA, AT INBD UPPER SECTION COUPLING ANGLE WITH CORROSION. FOUND DURING PROCESS OF ORNRC 200-327. REPLACED COUPLING P/N: D5347210220000 LOC BTW FR67 AND FR68 Y- 1292 LONGITUDINAL FLO
- [SDR DALA2026102105776](https://openairdocs.org/sdr/DALA2026102105776.md): Floor Support · corroded · Oct 19, 2026 · N362NW · Airbus A320212 · Fuselage Miscellaneous Structure
  > AFT PASSENGER CABIN BTWN FR 67 - 68, -Y 765, FLOOR SUPPORT CORRODED. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11-911-001, REV 159, DWG D53474250, SHEET 9, ISSUE Q, DWG D38370319, SHEET 3, ISSUE C, DWG D53472800, SHEET 10, ISSUE A, & DWG 53472816, SHEET 2, ISS
- [SDR DALA2026102105775](https://openairdocs.org/sdr/DALA2026102105775.md): Floor Support · corroded · Oct 19, 2026 · N362NW · Airbus A320212 · Fuselage Miscellaneous Structure
  > AFT PASSENGER CABIN BTWN FRS 66 - 69, -Y 1292, FLOOR SUPPORTS CORRODED. REPLACED THE FLOOR SUPPORTS IAW SRM 51-72-11-911-001, PARA 2.A(1), REV 159, DWG 10N01036, SHEET 4, REV B, DWG D53472816, SHEETS 1 & 2, REV A, DWG D53472800, SHEET 9, REV A, DWG D5347418
- [SDR DALA2026102105774](https://openairdocs.org/sdr/DALA2026102105774.md): Shear Plate · corroded · Oct 19, 2026 · N362NW · Airbus A320212 · Fuselage Miscellaneous Structure
  > AFT PASSENGER CABIN, BTWN FRS 69-70, RT FLOOR SHEAR PLATE CORRODED. REPLACED THE SHEAR PLATE IAW SRM 51-72-11-911-001, REV 159 AND DWG D534 74180, SHEET 6, ISSUE U. (LP: 1874370, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026102105780](https://openairdocs.org/sdr/DALA2026102105780.md): Flap System · locked · Oct 18, 2026 · N373NW · Airbus A320212 · Trailing Edge Flap Control System
  > FLT CTL FLAP SYS 2 LOCKED. FLT CTL FLAPS SYS 2 FAULT MESSAGE. FWD TO MEL SFCS 2 FLAP CHANNEL PER MEL 27-51-01A. DISPATCH APPROVED. PLACARD INSTALLED. BACKDATED TO 18OCT26SFCC #2 FLAP CHANNEL DE-ACTIVATED. TROUBLESHOT I.A.W A321 TSM 27-51. REMOVED AND REPLACED
- [SDR DALA2026101905706](https://openairdocs.org/sdr/DALA2026101905706.md): Battery · faulted · Oct 16, 2026 · N372NW · Airbus A320212 · Emergency Lighting
  > EPSU INT LOAD FWD L MESSAGE WHILE WORKING WORKCARD 2562-4001. R & R 10WL EPSU BATTERY PER AMM 33-51. OPS AND BITE CKS GOOD. OK FOR SVC. (LP: 9143598, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026101305621](https://openairdocs.org/sdr/DALA2026101305621.md): Thrust Reverser · faulted · Oct 11, 2026 · N351NW · Airbus A320212 · Engine Thrust Reverser
  > ATB - DUE TO ENG 2 REVERSE UNLOCKED ECAM WARNING AFTER TAKEOFF. NR 2 T/R PLACED ON MEL. RE-ACTIVATED NBR 2 ENGINE THRUST REVERSER, FAILED INBOARD TR LOWER LATCH SWITCH, REPLACED NBR 2 ENGINE INBOARD THRUST REVERSER UPPER DOOR LATCH. (LP 9485726 - AIRCRAFT WA
- [SDR DALA2026101005579](https://openairdocs.org/sdr/DALA2026101005579.md): Floor Support · corroded · Oct 9, 2026 · N362NW · Airbus A320212 · Fuselage Miscellaneous Structure
  > LEVEL 2 CORROSION, AFT PASSENGER CABIN AT FR 68, -Y 464.8, LONGITUDINAL FLOOR SUPPORT WITH CORROSION. REPLACED FLOOR SUPPORT AT AFT PASSENGER FLOOR SUPPORT AT AFT PASSENGER CABIN BTW FR 68 & FR 70, -Y464.8 IAW SRM 51-72-11-911-001, PARAG 2.A (1), SRM 51-42-
- [SDR DALA2026101305620](https://openairdocs.org/sdr/DALA2026101305620.md): Lamp · inoperative · Oct 8, 2026 · N360NW · Airbus A320212 · Passenger Compartment Lighting
  > OVERWING EMERGENCY EXIT HANDLE LIGHTS INOPERATIVE ALL 4 DOORS. RELAMPED, OPS NORMAL. (LP 9099331 - AIRCRAFT WAS GROUNDED)
- [SDR DALA2026100905572](https://openairdocs.org/sdr/DALA2026100905572.md): Frame · cracked · Oct 7, 2026 · N357NW · Airbus A320212 · Fuselage Main, Frame
  > CRACK INDICATION FOUND ON FR 68, STRINGER 22R, INNER CAP AREA, COMPLIED WITH ER/A 637146-14AD REV.ORIGINAL MATCHES WITH ALL STEPS ON PRI 637146-14AD PRI REV 0,1 ITS HAS BEEN VALIDATED. PERFORMED REPAIR INSTRUCTIONS ON FUSELAGE FRAME, FR 68, STR 22R IAW ER/A
- [SDR DALA2026100705553](https://openairdocs.org/sdr/DALA2026100705553.md): Light · detached · Oct 5, 2026 · N361NW · Airbus A320212 · Emergency Lighting
  > FLOOR PROXIMITY EMERGENCY LIGHT ATTACHED TO SEAT 30D WAS DETACHED FROM UNDER THE SEAT. SECURED THE EMERGENCY LIGHTING. CHKD GOOD. IAW AMM 33-52. (LP: 8963817, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026100805560](https://openairdocs.org/sdr/DALA2026100805560.md): Apu · odor · Oct 4, 2026 · N369NW · Airbus A320212 · Airborne Auxiliary Power Unit (APU) System
  > ODOR - APU PLACED ON MEL FOR SMOKE/FUME EVENT AND REQUIRES APU WASH. PERFORMED W/C 4916-2001 AND W/C 4900-2001. CLEANED AND INSPECTED APU REF W/C 4916-2001, CONTAMINATION NOTED AT APU AIR INTAKE AND PLENUM BEFORE CLEANING. RAN APU AFTER CLEANING FOR 20 MINUTE
- [SDR DALA2026100105466](https://openairdocs.org/sdr/DALA2026100105466.md): None · none · Sep 30, 2026 · N373NW · Airbus A320212 · Standard Practices/Structures
  > AFTER ENGINE STARTS FLIGHT ATTENDANTS REPORTED BURNING PLASTIC ODOR AS WELL AS STRONG GAS/FUEL SMELL. BOTH FIRST OFFICER AND I ALSO SMELLED THE SAME ODORS. TURN OFF PACKS AND RETURNED TO GATE. FOUND SOURCE OF CONTAMINATION FROM AIR START CART. SEE LOG PAGE 1
- [SDR DALA2026100105465](https://openairdocs.org/sdr/DALA2026100105465.md): Accumulator · leaking · Sep 29, 2026 · N373NW · Airbus A320212 · Hydraulic Reservoir, Main
  > DE - DUE TO HYD B RSVR LO LVL ECAM WARNING DURING CRUISE. FOUND BLUE SYSTEM ACCUMULATOR LEAKING FLUID FROM THE NITROGEN SERVICE FITTING. DEACTIVATED ACCUMULATOR AND PLACED ON MEL. (LP: 9153416, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026100105467](https://openairdocs.org/sdr/DALA2026100105467.md): Oxygen Mask · unsecure · Sep 27, 2026 · N340NW · Airbus A320212 · Passenger Oxygen System
  > OXYGEN MASK PANEL ON AIRCRAFT LEFT IN THE AFT GALLEY (LOCATED ABOVE THE COFFEE POTS) IS LOOSE. THE PANEL COVERING THE MASKS FELL OPEN DURING TAXI AS WELL AS TAKEOFF. THE PANEL WILL NOT REMAIN SHUT ON ITS OWN. RE-SECURED; INSPECTED & RESET LATCH, PANEL CLOSED
- [SDR DALA2026100105464](https://openairdocs.org/sdr/DALA2026100105464.md): Oxygen Mask · unwanted deploy · Sep 26, 2026 · N349NW · Airbus A320212 · Passenger Oxygen System
  > PAX 02 MASKS DEPLOYED AT 1A AND 1B. RE-PACKED 02 MASKS AT 1A AND 1B REF AMM 35-21. (LP: 9196702, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026092705364](https://openairdocs.org/sdr/DALA2026092705364.md): Computer · malfunctioned · Sep 26, 2026 · N353NW · Airbus A320212 · Flight Control System
  > DURING DECENT FOR APPROACH, WITH SPEED BRAKES DEPLOYED. AIRCRAFT MADE AN UNCOMMANDED RIGHT ROLL WITH NOTICEABLE BANK. T/S IAW TSM 27-10-00-810-842A, PERFORMED OPS TEST OF BOTH ELACS 1 & 2. TESTED OK. PERFORMED ELAC TEST IAW AMM 27-93-00-710-001-A. PERFORMED
- [SDR DALA2026092805368](https://openairdocs.org/sdr/DALA2026092805368.md): Computer · faulty · Sep 25, 2026 · N352NW · Airbus A320212 · Flight Control System
  > ON THE ARRIVAL TO DTW, THE ACFT HAD A NOSE DOWN PITCH. THE ECAM FOR FLT CONTROL ELAC 2 PITCH FAULT COMPLIED WITH ECAM & QRH. IAW AMM 27 93 34, TSM 27-93-00 810 867 710-001, REPLACED ELAC 2. OPS TESTED GOOD. PERFORMED EFCS AND SIDESTICK TESTING, NO FAULTS. A
- [SDR DALA2026092205299](https://openairdocs.org/sdr/DALA2026092205299.md): Radome · damaged · Sep 20, 2026 · N369NW · Airbus A320212 · Aerodynamic Fairings
  > BIRD STRIKE ON RADOME ON APPROACH NO UNUSUAL INDICATION OR SMELL FOLLOWING STRIKE. C/W BIRD STRIKE INSPECTION IAW AMM 05-51-14. NO OTHER DAMAGE NOTED. STRIKE ON RADOME DEFERRED TO MON WITH COMPLETIOIN OF ERA 637070-14 REV ORIGINAL. SEC 1. PERMINENT REPAIR WIT
- [SDR DALA2026092105249](https://openairdocs.org/sdr/DALA2026092105249.md): Door Sill · corroded · Sep 20, 2026 · N353NW · Airbus A320212 · Fuselage Main, Structure
  > PAX CABIN, PASSENGER DOOR CUTOUT, LOWER SILL BEAM I/B FLANGE WITH CORROSION LOC. AT FR67+450MM. REPLACED LOWER SILL BEAM P/N: 5348004320601, LOCATED AT PAX CABIN, PASSENGER DOOR CUTOUT I/A/W A320 SRM 51-72-11-911-001 PARAG 2 REV: 158.00 DATED: 01-JUN-26 AND R
- [SDR DALA2026092105252](https://openairdocs.org/sdr/DALA2026092105252.md): Oxygen Mask · no test · Sep 18, 2026 · N375NC · Airbus A320212 · Crew Oxygen System
  > CAPTAIN`S O2 MASK FAILED PREFLIGHT TEST. FLOW BLINKER DOES NOT SHOW WHEN PRESS TO TEST. REPACKED MASK REF A320 M/M 35-13. (LP: 9490280, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026092105251](https://openairdocs.org/sdr/DALA2026092105251.md): Radome · damaged · Sep 18, 2026 · N375NC · Airbus A320212 · Aerodynamic Fairings
  > BIRD STRIKE ON JACCC SID NEAR L IDAS AT APPROX 6000 FT. NOSE OF A/C. CLEANED LOWER PART OF THE RADOME WHERE BIRD STRUCK. PERFORMED INSPECTION OF THE AIRCRAFT AFTER A BIRD STRIKE PER A320 AMM TASK 05-51-14-200-803-A, FOUND INTERNAL DISBONDING/DELAMINATION AND
- [SDR DALA2026092105247](https://openairdocs.org/sdr/DALA2026092105247.md): Skin · corroded · Sep 18, 2026 · N344NW · Airbus A320212 · Fuselage Main, Plate/Skin
  > ON MG FOUND CORROSION AROUND LAV EXHAUST VENT. TRANSFERRED TO NRF 1 IAW TOPP 50-30-05. 278320. SUMMARY: CORROSION REMOVED, DAMAGE CONTAINED, AND REPAIR INSTALLED IAW ER /A 636893-14, REV ORIGINAL. RII'S COMPLIED WITH. (LP: 9490440, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026092105248](https://openairdocs.org/sdr/DALA2026092105248.md): Skin · corroded · Sep 17, 2026 · N344NW · Airbus A320212 · Fuselage Main, Plate/Skin
  > DTE REQUIRED. ERA 636893-14 ISSUED FOR CORROSION DAMAGE TO THE RHS AFT FUSELAGE SKIN AT FR70 BETWEEN S-31R AND S-32R. C/A: STAGE III DTE REQUIRED. ACCOMPLISH SECTION II INSPECTION WITHIN 20,000FC OR 40,000FH WHICHEVER OCCURS FIRST FOLLOWING SECTION I COMPLETIO
- [SDR DALA2026092105246](https://openairdocs.org/sdr/DALA2026092105246.md): Door Sill · corroded · Sep 17, 2026 · N353NW · Airbus A320212 · Fuselage Main, Structure
  > PAX CABIN, CREW DOOR CUTOUT, LOWER SILL BEAM I/B FLANGE WITH CORROSION LOC. AT FR67+450MM. C/A: PERFORMED REPAIR AT PASSENGER CABIN, CREW DOOR CUTOUT LOWER SILL BEAM I/B FLANGE FROM FR67+290MM TO FR68 I/A/W DELTA ER/A #636581-14 SECTION I REV ORIGINAL DATED 11
- [SDR DALA2026092105245](https://openairdocs.org/sdr/DALA2026092105245.md): Beam · corroded · Sep 17, 2026 · N353NW · Airbus A320212 · Fuselage Main, Structure
  > PAX CABIN, LONGITUDINAL BEAM UPPER FLANGE WITH CORROSION LOC. AT FR67+430MM Y1292. REPLACED LONGITUDINAL BEAM P/N: D5347218820400 AT Y1292 BTW FR68 TO FR69 I/A/W A 320 SRM TASK 51-72-11-911-001 PARAG 2 REV: 158.00 DATED 01-JUN-26. AND REF DWGS: 53474180, D534
- [SDR DALA2026091705192](https://openairdocs.org/sdr/DALA2026091705192.md): Floor Support · corroded · Sep 16, 2026 · N353NW · Airbus A320212 · Fuselage Miscellaneous Structure
  > LEVEL 2 CORROSION, PASSENGER CABIN LONGITUDINAL BEAM -Y1292, FR68 (COUPLING AREA), UPPER I/B AND AT FR66 UPPER AND LOWER I/B COUPLING ANGLES WITH ELONGATED HOLES AND CORROSION. NOTE: FOUND DURING PROCESS WITH ORNRC 200-378. C/A: REPLACED COUPLINGS AT LONGITUDI
- [SDR DALA2026091705191](https://openairdocs.org/sdr/DALA2026091705191.md): Floor Support · corroded · Sep 16, 2026 · N353NW · Airbus A320212 · Fuselage Miscellaneous Structure
  > LEVEL 2 CORROSION, PAX CABIN, LONGITUDINAL BEAM UPPER FLANGE WITH CORROSION LOC.BTW FR66+220MM TO FR68-Y1292. REPLACED LONGITUDINAL FLOOR SUPPORT D5347218920200 LOC.BTW FR66 TO FR69 AT -Y1292 I/A/W A320 SRM TASK 51-72-11-911-001 PARAG 2 REV 158.00 DATED 01-JU
- [SDR DALA2026091705190](https://openairdocs.org/sdr/DALA2026091705190.md): Skin · dented · Sep 16, 2026 · N353NW · Airbus A320212 · Fuselage Main, Plate/Skin
  > NOSE FWD EXTERNAL FUSELAGE, AT FR11 BETWEEN -Z 88 AND -Z 263, L/ H SIDE, SKIN WITH DENTS. C/A: PERFORMED REPAIR AT FWD EXTERNAL FUSELAGE SKIN SECTION AT FR11 BETWEEN -Z 88 AND -Z 263 L/H SIDE AS PER DELTA ER/A NO 636719-14 REV ORIGINAL SECTION I PART A, PART B
- [SDR DALA2026091705189](https://openairdocs.org/sdr/DALA2026091705189.md): Skin · scratched · Sep 16, 2026 · N353NW · Airbus A320212 · Fuselage Main, Plate/Skin
  > NOSE FWD EXTERNAL FUSELAGE, AT FR10 -Z361 L/H SIDE, SKIN WITH SCRATCH. PERFORMED REPAIR AT FWD EXTERNAL FUSELAGE SKIN SECTION AT FR 10 -Z361 LH SIDE AS PER DELTA ER/A NO. 636719-14 REV ORIGINAL SECTION I PART A, PART B STEP 15, 19 AND 20, DATED 11-SEP-26. NOT
- [SDR DALA2026091705188](https://openairdocs.org/sdr/DALA2026091705188.md): Coupling · corroded · Sep 16, 2026 · N353NW · Airbus A320212 · Fuselage Main, Structure
  > LEVEL 2 CORROSION, PAX CABIN LONGITUDINAL BEAM AT FR68 Y1292 COUPLING AREA, I/B UPPER COUPLING ANGLE WITH CORROSION. FOUND DURING PROCESS WITH ORNRC 200-337. REPLACED COUPLING AT FR68 Y1292 LOCATED I/B UPPER IAW SRM 51-72-11-911-001 PARAG 2. REV 158. AND DWG
- [SDR DALA2026091605158](https://openairdocs.org/sdr/DALA2026091605158.md): Controller · faulty · Sep 16, 2026 · N367NW · Airbus A320212 · Cabin Pressure Controller
  > ATB - DUE TO CAB PR EXCESS CAB ALT ECAM WARNING FOLLOWED BY CAB PR SYS 2 FAULT. #2 CPC REPLACED. (LP: 9548118, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026091505146](https://openairdocs.org/sdr/DALA2026091505146.md): Seat Track · corroded · Sep 14, 2026 · N353NW · Airbus A320212 · Fuselage, Seat/Cargo Attach Fittings
  > PAX CABIN, LONGITUDINAL BEAM WITH CORROSION AT SEAT TRACK CROWN AREA LOC. BTW FR65 TO FR 66 -Y765. REPLACED SEAT TRACK BEAM P/N 14N00031-103 AT Y-765 BETWEEN FR64 AND FR66 I/A/W A320 SRM 51-72-911-001 PARAG 2 REV 158.00 DATED 01-JUN-26 AND REFERENCE NAT DRAWI
- [SDR DALA2026091505145](https://openairdocs.org/sdr/DALA2026091505145.md): Beam · corroded · Sep 14, 2026 · N353NW · Airbus A320212 · Fuselage Main, Structure
  > LEVEL 2 CORROSION, PAX CABIN, LONGITUDINAL BEAM UPPER FLANGE WITH CORROSION LOC. AT FR66 Y765. C/A: REPLACED SEAT TRACK BEAM P/N 14N00031-103 AT Y 765 BETWEEN FR64 AND FR66 I/A/W A320 SRM 51-72-911-001 PARAG 2 REV 158.00 DATED 01-JUN-26 AND REFERENCE NAT DRAWI
- [SDR DALA2026091505144](https://openairdocs.org/sdr/DALA2026091505144.md): Beam · corroded · Sep 14, 2026 · N353NW · Airbus A320212 · Fuselage Main, Structure
  > LEVEL 2 CORROSION, PAX CABIN, LONGITUDINAL BEAM UPPER FLANGE WITH CORROSION LOC. AT FR66+70MM Y1292. C/A: REPLACED SEAT TRACK BEAM P/N 14N00031-101 AT Y1292 BETWEEN FR64 AND FR66 I/A/W A320 SRM 51-72-911-001 PARAG 2 REV 158.00 DATED 01-JUN-26 AND REFERENCE NAT
- [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 DALA2026092105250](https://openairdocs.org/sdr/DALA2026092105250.md): Skin · corroded · Sep 12, 2026 · N344NW · Airbus A320212 · Fuselage Main, Plate/Skin
  > CORROSION DAMAGE WAS FOUND AROUND THE LAVATORY VENT LOCATED BETWEEN FR 69 AND FR 70, AT STRG 31RH AND STRG 32RH. REWORKED BY BLENDING THE CORRODED AREA AROUND THE LAV VENT AREA PER A320 SRM 53-41-11-101, SUBSECTION 53-41-11-283-065 FOR FR64- FR70. THE REMOVED
- [SDR DALA2026091505147](https://openairdocs.org/sdr/DALA2026091505147.md): Rudder · excess play · Sep 12, 2026 · N365NW · Airbus A320212 · Rudder Structure
  > REMOVE RUDDER. REMOVED AND REPLACED RUDDER REF AMDS CARD 2721-4001. (LP: 1809694, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026091305113](https://openairdocs.org/sdr/DALA2026091305113.md): Microphone · inoperative · Sep 12, 2026 · N351NW · Airbus A320212 · Crew Oxygen System
  > F/O OS MASK MICROPHONE NOT WORKING. C/A: SWAPPED THIRD OBSERVER SEAT OT MASK WITH F/O AND FWD THIRD OBSERVER SAET TO MEL 25-11-07. R/R THIRD OBESERVER O2 MASK PER A320 AMM 35-12. LEAK AND OPS TESTS OK. RFID INDUCTION C/W. F/O MASK RFID REPLACEMENT C/W TO REFLE
- [SDR DALA2026091305112](https://openairdocs.org/sdr/DALA2026091305112.md): Skin · corroded · Sep 12, 2026 · N353NW · Airbus A320212 · Fuselage Main, Plate/Skin
  > LEVEL 2 CORROSION, LOWER FUSELAGE AFT CARGO COMPARTMENT FROM FR56 TO FR 57 BETWEEN STRG-42L AND STRG-43L AFT ATG4 ANTENNA INTERNAL DOUBLER WITH CORROSION. PERFORMED REPAIR AT LOWER FUSELAGE AFT CARGO COMPARTMENT SKIN PANEL SECTION FROM FR 56 TO FR 57, BETWEEN
- [SDR DALA2026091305111](https://openairdocs.org/sdr/DALA2026091305111.md): Shear Plate · corroded · Sep 12, 2026 · N353NW · Airbus A320212 · Fuselage Miscellaneous Structure
  > LEVEL 2 CORROSION, PAX CABIN, LATERAL SHEAR PLATE WITH CORROSION LOC.BTW FR 69 TO FR 70 STR 23L. REPLACED SHEAR PLATE AT PAX CABIN BETWEEN FR 69 TO FR 70 STG 23L AS PER A320 SRM 51-72-11-911-001 PARAG 2, REV 158.00 DATED 01-JUN-26 AND REFERENCE DRAWING D5347
- [SDR DALA2026091705193](https://openairdocs.org/sdr/DALA2026091705193.md): Skin · damaged · Sep 11, 2026 · N353NW · Airbus A320212 · Fuselage Main, Plate/Skin
  > DAMAGE TOLERANCE EVALUATION ( DTE) REQUIRED FOR FUSELAGE SKIN R EPAIR AT FR11LH, -Z88 & -Z263 PER ER/A 636719-14. C/A: SECTION I IS LIMITED TO SOONER OF 60000FC OR 120000FH. ER/A TO B E REVISED PRIOR TO THIS DATE ELSE REMOVE A/C FROM SERVICE.. (LP: 1807237,
- [SDR DALA2026091405115](https://openairdocs.org/sdr/DALA2026091405115.md): Microphone · inoperative · Sep 11, 2026 · N351NW · Airbus A320212 · Crew Oxygen System
  > F/O OXYGEN MASK MICROPHONE DOESN'T WORK. RESEATED MIC CONNECTOR. CHK NORMAL. IAW AMM 35-13. (LP: 9494820, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026091305108](https://openairdocs.org/sdr/DALA2026091305108.md): Shear Plate · corroded · Sep 11, 2026 · N353NW · Airbus A320212 · Fuselage Miscellaneous Structure
  > LEVEL 2 CORROSION, PAX CABIN, LATERAL SHEAR PLATE WITH CORROSION LOC. BTW FR69 TO FR70 STGR 23R. REPLACED SHEAR PLATE P/N: D5347112420300 LOCATED BTW FR69 TO FR70, STGR 23R IAW SRM 51-72-11-911-001 PARAG 2 REV 158.00 DATED 01-JUN-26 AND REF DWG A320 #D534741
- [SDR DALA2026091305109](https://openairdocs.org/sdr/DALA2026091305109.md): Warning Message · illuminated · Sep 10, 2026 · N351NW · Airbus A320212 · Fuel Indicating System
  > CAUTION ON ECAM - TK LO TEMP LEFT OUTTER LO TEMP. FLIGHT CREW PLACARD VALIDATION IS ACCOMPLISHED REJECTED TAKEOFF DUE TO FUEL L OUTER TK LO TEMP INDICATION. LEFT OUTER TANK INDICATED -51C. AFTER CLEARING RUNWAY, FUEL TEMP INDICATED~ +42C. FLIGHT CREW PLACARD
- [SDR DALA2026091305105](https://openairdocs.org/sdr/DALA2026091305105.md): Skin · damaged · Sep 10, 2026 · N353NW · Airbus A320212 · Fuselage Main, Plate/Skin
  > ER/A 636728-14 IS ISSUED FOR FUSELAGE SKIN REPAIR INSTALLED AT F R56/57, S42/43LH WHICH WAS INSTALLED PER SRM 53-00-11-300-013. F OLLOW ON ACTION IS REQUIRED. SECTION II, AS REQUIRED IAW SRI 53-00-11-205-035, REQUIRED PRIOR TO SOONER OF 33600FC OR 67200FH & E

Next page: https://openairdocs.org/model/airbus-a320-212/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 aircraft_model_key = 'A320212'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/airbus-a320-212/reports

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