Airbus A320-211

Service difficulty reports · 5,271

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duckdb -csv -c "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 = 'A320211'
  ORDER BY difficulty_date DESC"

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SDR DALA13028983218Floor Panel · damagedDURING INSPECTION, FOUND AFT UTILITY FLOOR PANEL 261PF SEVERAL INSERTS MISSING & BROKEN. FLOOR PANEL FABRICATED IAW SRM 53-02-00, FIG 209 AND DWG 3D25-37498.Jun 12, 2013 · N318US · Airbus A320211 · Fuselage Floor PanelSDR DALA13028973218Floorboard · damagedDURING INSPECTION, FOUND MAIN CABIN FLOORBOARD 251MF IS DAMAGED, L=84, W=20. FLOORBOARD FABRICATED IAW SRM 53-02-00, FIG 209 AND DWG 3D25-37498.Jun 12, 2013 · N318US · Airbus A320211 · Fuselage Floor PanelSDR DALA13028963218Floorboard · damagedDURIING INSPECTION, FOUND MAIN CABIN FLOORBOARD 251JF IS DAMAGED, W=18 L=63. FLOORBOARD FABRICATED IAW SRM 53-02-00, FIG 209 AND DWG 3D25-37498.Jun 12, 2013 · N318US · Airbus A320211 · Fuselage Floor PanelSDR DALA13028943218Floor Panel · delaminatedDURING INSPECTION, FOUND MID CABIN FLOOR PANEL 251YF DELAMINATED 1" X 24". FLOOR PANEL FABRICATED IAW SRM 53-02-00, FIG 209 AND DWG 3D25-37498.Jun 12, 2013 · N318US · Airbus A320211 · Fuselage Floor PanelSDR DALA13028933218Floorboard · damagedDURING INSPECTION, FOUND MAIN CABIN FLOORBOARD 251AF IS DAMAGED, L=84 W=20. FABRICATED NEW FLOORBOARD IAW SRM 53-02-00.Jun 12, 2013 · N318US · Airbus A320211 · Fuselage Floor PanelSDR DALA13028873216Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON FITTING LOCATED INTERNAL STRUCTURE OF CUT OUT DOOR LOCKING FITTING AREA AND BETWEEN FR 26 AND FR 27 FWD CARGO. REPLACED FITTING AND FASTENER LOCATED INTERNAL STRUCTURE OF CUT OUT DOOR LOCKING FITTING AREA AND BETWEEN FR 2Jun 12, 2013 · N316US · Airbus A320211 · Fuselage Main, StructureSDR CA130613003Idg · failed(CAN) MULTIPLE ELECTRICAL FAILURES ON CLIMBOUT THRU APPROX FL305. A/P OFF, A/THR OFF AND BLANK SCREENS. NR 1 IDG RE & RE IAW AMM24-21-51, PB401. NR 1 GCU RE AND RETEST SERVICE IAW AMM 24-22-34, PB401. GROUND RUN CARRIED OUT. FAN COWLS CS.Jun 11, 2013 · Airbus A320211 · AC Generator-AlternatorSDR DALA13028563216Skin · dentedDURING INSPECTION, FOUND DENT ON EXTERNAL FUSELAGE SKIN LOCATED FR 24+7" AND BETWEEN STR 41L AND STR 42L. PERFORMED PERMANENT REPAIR ON EXTERNAL FUSELAGE SKIN BETWEEN FR 24 AND FR 25 AND BETWEEN STR 41L AND STR 43L IAW SRM 53-21-11, PARA 5K, FIG 214, MUST BE Jun 11, 2013 · N316US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA13028923218Floor Panel · corrodedDURING INSPECTION, FOUND AFT CARGO COMPARTMENT THRESHOLD FLOOR PANEL 152KF CORRODED ON SEVERAL AREAS L=6" W=3" D=.030". FLOOR PANEL INSTALLED.Jun 11, 2013 · N318US · Airbus A320211 · Fuselage Floor PanelSDR DALA13028913218Floorbeam · crackedDURING INSPECTION, FOUND FWD CABIN FLOORBEAM AT AFT FR24, Y254 UPPER FLANGE CRACKED. NO LIMITS FOUND ON CRACKED FLANGE IAW SRM 53-00-14. REMOVED DAMAGED AREA OF FLOORBEAM IAW SRM 53-00-14. FABRICATED FOUR REPAIR SPLICES AND TWO STRAPS IAW SRM 53-00-14. HEAT Jun 11, 2013 · N318US · Airbus A320211 · Fuselage Main, Floor BeamSDR DALA13028903218Floor Panel · brokenDURING INSPECTION, FOUND AFT UTILITY FLOOR PANEL 261DF SEVERAL INSERTS MISSING & BROKEN. FABRICATED NEW FLOOR PANEL IAW SRM 53-02- 00.Jun 11, 2013 · N318US · Airbus A320211 · Fuselage Floor PanelSDR DALA13028893218Floor Panel · puncturedDURING INSPECTION, FOUND AFT UTILITY FLOOR PANEL 261EF PUNCTURED. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00.Jun 11, 2013 · N318US · Airbus A320211 · Fuselage Floor PanelSDR DALA13028883218Floor Panel · damagedDURING INSPECTION, FOUND AFT UTILITY FLOOR PANEL 262EF SEVERAL INSERT MISSING & BROKEN. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00.Jun 11, 2013 · N318US · Airbus A320211 · Fuselage Floor PanelSDR DALA13028543216Skin · dentedDURING INSPECTION, FOUND DENT ON EXTERNAL SKIN LOCATED AT FR 80+2" AFT UPPER FUSELAGE. PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN BETWEEN FR 80 AND FR 81 AFT UPPER FUSELAGE IAW SRM 53-51-11, PARA 5.B, FIG 203 (SHEET 1).Jun 11, 2013 · N316US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA13029063218Bolt · scoredDURING INSPECTION, FOUND RT WING AILERON NR 1 HINGE PIN (BOLT) SCORED. RECEIVED 1 EA BOLT, PN D5755103720051 TO BE INSTALLED ON AMDS CARD 5760-1010S-RT. WEAR LIMIT .20" FOUND OUT OF LIMITS IAW AMM 27-14-41-200-001-A.Jun 10, 2013 · N318US · Airbus A320211 · AileronsSDR DALA13028533218Web · crackedDURING INSPECTION, FOUND COCKPIT FLOOR STRUCTURE RT SIDE AT FWD FR11 Y-765 LOWER CORNER WEB CRACKED. REMOVED CRACK IAW SRM 51-42-11. LOCATED AND DRILLED NEW WEB IAW SRM 51-44-11. TREATED AND PRIMED IAW SRM 51-21-11. INSTALLED NEW WEB IAW SRM 51-42-11 AND DJun 10, 2013 · N318US · Airbus A320211 · Fuselage Floor PanelSDR DALA13028523218Floor Panel · corrodedDURING INSPECTION, FOUND FWD UTILITY FLOOR PANEL 221FF HAS CORROSION. NEW FLOOR PANEL INSTALLED.Jun 10, 2013 · N318US · Airbus A320211 · Fuselage Floor PanelSDR DALA13028513218Floor Support · corrodedDURING INSPECTION, FOUND FWD CABIN FLOOR SUPPORT RT SIDE FR20, S23R UPPER FLANGE WEB AND ANGLE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. NOT ESTABLISHED LIMITS FOUND IN SRM. REMOVED FLOOR SUPPORT IAW SRM 51-42-11. LOCATED AND DRILLED IAW SRM 51-44-Jun 10, 2013 · N318US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13028503218Floor Support · damagedDURING INSPECTION, FOUND MID CABIN FLOOR SUPPORT BETWEEN FR 32 AND FR 33 AT -Y245 UPPER FLANGE DAMAGED. BLENDED AREA IAW SRM 51-73-00, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14, FIG 204, CUTOUT DAMAGED AREA. FABRICATED REPAIR PARTS ONE ANGLE AND ONE FILLERJun 10, 2013 · N318US · Airbus A320211 · Fuselage Miscellaneous StructureSDR CA130610005Connector · unsecure(CAN) DURING THE FLIGHT THE HEADPHONE JACK AT SEAT 23E BECAME VERY HOT AND PRODUCED A BURNING ODOR. THE IFE ANS ISPS SYSTEMS WERE TURNED OFF AND THE JACK COOLED AND THE ODOR DISSIPATED. FOUND CONNECTOR UNDER 22 DEF ADRIFT, BENT PINS. REPAIRED PINS, RECONNECJun 9, 2013 · Airbus A320211 · Communications System WiringSDR DALA13027993216Floor Support · damagedDURING INSPECTION, FOUND ELONGATED HOLES ON FLOOR SUPPORT STRUCTURE LOCATED AFT PAX CABIN BETWEEN FR 66+5" AND FR 67+17" LEVEL Y1162 REPLACED FLOOR SUPPORT LOCATED AFT PAX CABIN BETWEEN FR 66+5" ANDFR 67+17" Y1162 IAW SRM 51-72-11.Jun 9, 2013 · N316US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13027983216Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT STRUCTURE LOCATED AFT PAX CABIN BETWEEN FR 68 AND FR 69, LEVEL Y1162. REPLACED FLOOR SUPPORT LOCATED AFT PAX CABIN BETWEEN FR 68 AND FR 69 Y1162 IAW SRM 51-72-11 AND DWG D53472000.Jun 9, 2013 · N316US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13027973216Floorbeam · corrodedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM STRUCTURE LOCATED AFT PAX CABIN AT FR 66, LEVEL Y-765. REPLACED FLOORBEAM STRUCTURE LOCATED AFT PAX CABIN AT FR 66, LEVEL Y-765 IAW SRM 51-72-11.Jun 9, 2013 · N316US · Airbus A320211 · Fuselage Main, Floor BeamSDR DALA13027963216Floorbeam · corrodedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM STRUCTURE LOCATED AFT PAX CABIN AT FR 68+5" LEVEL Y-765; REPLACED FLOORBEAM LOCATED AFT PAX CABIN AT FR 68+5" LEVEL -Y765 IAW SRM 51-72-11 AND DWG D53472000.Jun 9, 2013 · N316US · Airbus A320211 · Fuselage Main, Floor BeamSDR DALA13028553218Floor Panel · corrodedDURING INSPECTION, FOUND AFT UTILITY FLOOR PANEL 261FF HAS CORROSION. NEW FLOOR PANEL INSTALLED.Jun 8, 2013 · N318US · Airbus A320211 · Fuselage Floor PanelSDR DALA13027953218Floor Support · corrodedDURING INSPECTION, FOUND AFT CABIN UTILITY AREA FLOOR SUPPORT BETWEEN FR 65-66, Y1292. UPPER SURFACE & HARD POINT HOLES HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00 BLEND SIZE: L=1.6" W=1.3" D=.030" FOUND TO BE OUT OF LIMIT IAW TRM 53-41-15, ORIGINAL MATJun 8, 2013 · N318US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13027943218Floorbeam · corrodedDURING INSPECTION, FOUND AFT CABIN UTILITY AREA FLOOR SUPPORT BETWEEN FR 68-69, Y1292 HARD PT. HOLES & UPPER FLANGE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00 BLEND SIZE: L=1.6", W=1", D=.062. FOUND TO BE OUT OF LIMIT IAW TRM 53-41-15 ORIGINAL MATERIJun 8, 2013 · N318US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13027933218Floor Support · corrodedDURING INSPECTION, FOUND AFT CABIN UTILITY AREA FLOOR SUPPORT BETWEEN FR66-68 Y1292, UPPER FLANGE, NUTPLATES & HOLES HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00 BLEND SIZE: L=1.6" W=1" D=.035" ORG MATERIAL .087" FOUND TO BE OUT OF LIMIT IAW TRM 53-41-15Jun 8, 2013 · N318US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13027923218Floor Support · corrodedDURING INSPECTION, FOUND FORWARD CABIN UTILITY AREA FLOOR SUPPORT, BETWEEN FR12-FR20 Y-254 UPPER FLANGE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00, L=.2"XW=1.1"XD=.020", ORG MAT .079. NO ALLOWABLE DAMAGE IAW SRM 53-11-14. REMOVED FLOOR SUPPORT IAW SRJun 8, 2013 · N318US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13027913216Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CENTER FITTING LOCATED BETWEEN FR 66 AND FR 68 AT LEVEL STR 23 LT L=0.500", W=0.250", D=0.001" APPROX. REPLACED CENTER FITTING LOCATED BETWEEN FR 66 TO FR 68 AT LEVEL STR 23 LT IAW SRM 51-72-11 AND DWG D53480020.Jun 8, 2013 · N316US · Airbus A320211 · Fuselage Main, Attach FittingsSDR DALA13027903216Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CENTER FITTING LOCATED BETWEEN FR 66 AND FR 68 AT LEVEL STR 23 RT L=0.500" W=0.250" D=0.001" APROX SSI 534132. REPLACED CENTER FITTING LOCATED BETWEEN FR 66 AND FR 68 AT LEVEL STR 23 RT IAW SRM 51-72-11 AND DWG D53480020.Jun 8, 2013 · N316US · Airbus A320211 · Fuselage Main, Attach FittingsSDR DALA13027893218Beam · corrodedDURING INSPECTION, FOUND LT AFT PASSENGER/CREW DOOR SILL BEAM AT AFT FR66 INBD. AROUND GIRT BAR HOLES HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00 DIMENSION HOLE DIAMETER 0.473" FOUND TO BE OUT OF LIMITS IAW TRM 53-41-14. REPLACED LT AFT PASSENGER/CREWJun 7, 2013 · N318US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13027883218Tray · crackedDURING INSPECTION, FOUND AFT CABIN UTILITY AREA FLOOR SUPPORT TRAY LT SIDE BETWEEN FR68-69, STRG 23L CRACKED. REPLACED FLOOR SUPPORT TRAY IAW SRM 51-42-11, 51-44-11, 51-75-12 AND DWG 18D53480019, PN: D5348002069601, BATCH 0 002385967, CRACKED DIM 4.5".Jun 6, 2013 · N318US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13027563218Floor Support · corrodedDURING INSPECTION, FOUND AFT CABIN UTILITY AREA FLOOR SUPPORT BETWEEN FR65-FR67, Y-308 UPPER FLANGE HOLES HAS CORROSION. BLENDED AFT CABIN UTILITY AREA FLOOR SUPPORT BETWEEN FR65-67 Y-308 IAW SRM 51-74-00. CHECKED LIMITS L=1.75" W=2.0" D=0.027".MAX ALL ALLOWJun 6, 2013 · N318US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13027553218Floor Support · corrodedDURING INSPECTION, FOUND AFT CABIN UTILITY AREA FLOOR SUPPORT BETWEEN FR 66-68 Y-1292 UPPER FLANGES, NUTPLATES & HOLES HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00 DIMENSION L=1.4" W=.600"D=0.056". FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15; REPLACED FLOJun 6, 2013 · N318US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13027543218Floor Support · corrodedDURING INSPECTION, FOUND AFT CABIN UTILITY AREA FLOOR SUPPORT BETWEEN FR 65-66 Y-1292, UPPER FLANGES & HOLES HAVE CORROSION. REMOVED CORROSION IAW SRM 51-74-00 DIMENSION L=1.3" W=1.2"D=0.031" FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15; REPLACED FLOOR SUPPORTJun 6, 2013 · N318US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13027533218Floor Support · corrodedDURING INSPECTION, FOUND AFT CABIN UTILITY AREA FLOOR SUPPORT BETWEEN FR 68-69, Y-1292 UPPER FLANGES & HARD POINT HOLES HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00 DIMENSION L=2.0" W=1.25" D=0.065". FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15; REPLACED Jun 6, 2013 · N318US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13027393218Floor Support · corrodedDURING INSPECTION, FOUND AFT CABIN UTILITY AREA FLOOR SUPPORT BETWEEN FR65 TO FR67 Y-465 UPPER FLANGE HOLES HAS CORROSION. BLENDED AREA IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-14. LOCATED & DRILLED NEW FLOOR BEAM IAW SRM 51-44-11. REPLACJun 4, 2013 · N318US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13026683218Web · crackedDURING INSPECTION, FOUND COCKPIT FLOOR STRUCTURE LT SIDE AT FWD FR 11, Y765 LOWER CORNER WEB CRACKED. FOUND TO FOUND TO BE OUT OF LIMITS IAW SRM 53-41-14, FIG 205, SHT 1. REPLACED CRACKED WEB, BATCH IAW SRM 51-42-11 & DWG D53113219; CRACK DIM 0.700".May 31, 2013 · N318US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13026673218Sill · corrodedDURING INSPECTION, FOUND AFT LT PASSENGER/CREW DOOR SILL BEAM AT FR 68 AFT CORNER FITTING HAS CORROSION. REPLACED FITTING CORNER IAW SRM 51-42-11. DAMAGE DIMENSIONS L=0.400" W=0.080" D=0.025". NO LIMITS FOUND IN SRM 53-41-14, FIG 101.May 31, 2013 · N318US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13026633218Floor Support · corrodedDURING INSPECTION, FOUND FORWARD CABIN UTILITY AREA FLOOR SUPPORT BETWEEN FR 16 TO FR 24 Y1292 UPPER FLANGE HOLES & SEAT TRACK CROWN AREA HAS CORROSION. CHECKED LIMITS MEASURES AS FOLLOWS, ORIG THICKNESS 0.079, L=4.3" W=1.3", D=0.033 MAX DEPTH ALLOWABLE 0.03May 31, 2013 · N318US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13026623218Floor Support · corrodedDURING INSPECTION, FOUND FORWARD CABIN FLOOR SUPPORT BETWEEN FR20 -FR23 Y-189 UPPER FLANGE HAS CORROSION. REPLACED FLOOR SUPPORT IAW SRM 51-42-11 AND DWG. REMOVED CORROSION IAW SRM 51-74-00 L=.900" W=1.40" D=.023 NO ESTABLISHED LIMITS IAW SRM 53-11-14.May 30, 2013 · N318US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13026613218Floor Support · corrodedDURING INSPECTION, FOUND FWD CABIN UTILITY AREA FLOOR SUPPORT BETWEEN FR12-FR16, Y503.2 UPPER FLANGE HOLES HAS CORROSION AND SCRIBE LINE MARKS. REMOVED CORROSION AND SCRIBE LINE MARKS IAW SRM 51-74-00 AND SRM 51-73-00, CHECKED LIMITS MEASURES AS FOLLOWS BLENMay 29, 2013 · N318US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13026533218Floorbeam · corrodedDURING INSPECTION, FOUND FWD CABIN UTILITY AREA FLOORBEAM BETWEEN FR16 -20, Y254 UPPER FLANGE HAS CORROSION. BLENDED CORROSION IAW SRM 51-74-00 CHECK LIMITS ORIG MAT (0.079"). L=2.5", W=1.47" D=0.43" OUT OF LIMITS IAW SRM 53-11-15, FIG 104. REMOVED BEAM Y254May 29, 2013 · N318US · Airbus A320211 · Fuselage Main, Floor BeamSDR DALA13025573218Skin · dentedDURING CURRENT M-CHECK, LT SIDE OF FWD FUSELAGE JUST AFT OF FR 21 AT STR 24L, SKIN IS DENTED AND IT WAS REPAIRED IAW SRM 53-11-11, FIG 212. DOUBLER REPAIR ACCOMPLISHED IAW SRM 53-11-11, FIG 212.May 28, 2013 · N318US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA13025113221Light · missingEMERGENCY ESCAPE PATH LIGHT MISSING. INSTALLED MISSING EMERGENCY LIGHT IAW AMM 33-51. OPS CHECKED GOOD. OK FOR SERVICE.May 22, 2013 · N321US · Airbus A320211 · Emergency LightingSDR DALA13023993211Door · out of adjustAFT RT EMERGENCY OVERWING EXIT AMBER CAUTION LIGHT CAME ON, ON UPPER ECAM DURING FCF. AFT RT EMERGENCY OVERWING EXIT COVER FLAP ADJUSTED IAW AMM 52-21-11-700-050-B. OPS TEST GOOD.May 16, 2013 · N311US · Airbus A320211 · Emergency ExitsSDR DALA13022533211Epsu · failedDURING NON ROUTINE CHECK, FOUND POWER SUPPLY 13WL FAILED TEST. REMOVED EPSU 13WL IAW AMM 33-51-38-000-001-A. MX INSTALLED SERVICEABLE EPSU AT 13WL AND FUNCTIONAL CHECK WAS NORMAL.May 14, 2013 · N311US · Airbus A320211 · Emergency LightingSDR DALA13029473216Floorbeam · corrodedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM STRUCTURE LOCATED AFT PAX CABIN AT FR 66 LEVEL -Y465. REPLACED FLOORBEAM AND FASTENERS IAW SRM 51-72-11 AND DWG D53472000.May 12, 2013 · N316US · Airbus A320211 · Fuselage Main, Floor BeamSDR CA130513011Actuator · leaking(CAN) CREW REPORTED A LOSS OF THE GREEN HYDRAULIC SYSTEM AND DECLARED AND EMERGENCY ON ARRIVAL. FOUND GREEN SYSTEM YAW DAMPNER WITH EXCESSIVE LEAKAGE. R & R OF GREEN SYSTEM YAW DAMPNER IAW AMM 27-26-51-PB401. ALL CHECKS CARRIED OUT SERVICEABLE. RESET LANDINMay 11, 2013 · Airbus A320211 · Rudder Tab Control System
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