Airbus A320-232

Service difficulty reports · 32,653

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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 = 'A320232'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR YENA2021121700859Shear Tie · corrodedDURING HEAVY MAINTENANCE, CORROSION SHEAR TIE LOCATED AT FR 31 BTW DTR 41R AND 42R IN FED CARGO COMPARTMENT ; (RESOLVED ON W/O: 1130692 TASKCARD: NR-00017 ) REMOVED AND REPLACED SHEAR TIE AT FR 31 BTW STR 41R AND 42R IN FWD CARGO COMPARTMENT IAW SRM 51-42-11Dec 11, 2021 · N504JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2021121700858Shear Tie · corrodedDURING HEAVY MAINTENANCE, CORROSION SHEAR TIE LOCATED AT FR 32 BTW DTR 41R AND 42R IN FWD CARGO COMPARTMENT ; (RESOLVED ON W/O: 1130692 TASKCARD: NR-00018 ) REMOVED AND REPLACED SHEAR TIE IAW SRM 51-42-11. WORK ACCOMPLISHED ON AEROMAN NR 2021-475448Dec 11, 2021 · N504JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2021121700857Shear Tie · corrodedDURING HEAVY MAINTENANCE, CORROSION SHEAR TIE LOCATED AT FR 31 BTW DTR 43R AND 44R IN FWD CARGO COMPARTMENT ; (RESOLVED ON W/O: 1130692 TASKCARD: NR-00019 ) REMOVED AND REPLACED SHEAR TIE IAW SRM 51-42-11. WORK ACCOMPLISHED ON AEROMAN NR 2021-475473Dec 11, 2021 · N504JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2021121700856Stringer · corrodedDURING HEAVY MAINTENANCE, CORROSION STRINGER 41R LOCATED AT FR 33R IN FWD CARGO COMPARTMENT ; (RESOLVED ON W/O: 1130692 TASKCARD: NR-00021 ) REFORMED REPAIR IAW SRM 51-21-13-300-003 FIGURE OO1 SHEET 1. THIS REPAIR IS CATEGORY B AND REQUIRES FURTHER INSPECTIODec 11, 2021 · N504JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2021121700855Shear Tie · corrodedDURING HEAVY MAINTENANCE, CORROSION SHEAR TIE LOCATED AT FR33 BTW STR 40R AND 41R ; REMOVED AND REPLACED SHEAR TIE IAW A320 SRM 51-72-11 REF AEROMAN NR 2021-475444Dec 11, 2021 · N504JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2021121700854Shear Tie · corrodedDURING HEAVY MAINTENANCE, CORROSION SHEAR TIE LOCATED AT FR32 BTW STR40R AND41R IN FWD CARGO COMPARTMENT ; REMOVED AND REPLACED SHEAR TIE IAW A320 SRM 51-72-11. REF AEROMAN NR 2021-475447Dec 11, 2021 · N504JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2021121700853Sill Drain · corrodedDURING HEAVY MAINTENANCE, CORROSION LOWER SILL FR 68 AT STR 23L IN PASSENGER CABIN; REMOVED CORROSION AT LOWER SILL FR 68 AT STR 23L IAW SRM 51-74-00. EVALUATED REWORK AND FOUND TO EXCEED ALLOWABLE LIMITS. PERFORMED REPAIR IAW SRM 53-41-14-300-001. REF AEROMADec 11, 2021 · N504JB · Airbus A320232 · Fuselage, Wing Attach FittingsSDR YENA2021121700852Shear Tie · corrodedDURING HEAVY MAINTENANCE, CORROSION SHEAR TIE LOCATED AT FR31 BTW STR 41R AND 42R ; REMOVED AND REPLACED SHEAR TIE IAW SRM 51-42-11. REF AEROMAN NR 2021-475472Dec 11, 2021 · N504JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2021121700851Shear Tie · corrodedDURING HEAVY MAINTENANCE, CORROSION SHEAR TIE AT FR32 BTW STR 41R AND 42R ; REMOVED AND REPLACED SHEAR TIE IAW SRM 51-42-11 REF AEROMAN NR 2021-475448Dec 11, 2021 · N504JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2021121700850Stringer · corrodedDURING HEAVY MAINTENANCE, CORROSION STRINGER 41R AT FR33R IN FWD CARGO COMPARTMENT ; PERFORMED REPAIR IAW SRM 51-21-13-300-003 FIGURE 001 SHEET 1 REF AEROMAN NR 2021-475446Dec 11, 2021 · N504JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2021121700849Epsu · failed inspDURING HEAVY MAINTENANCE, EPSU 10WL FAILS OPS TEST ; REF AEROMAN NR 2021-365/1-2021-475618 - REPLACED EPSU 10WL BATTERY IAW A320 AMM 33-51-38-00-002-A. OPS CHECK GOOD IAW A320 AMM 33-51-00-710-001-A.Dec 11, 2021 · N504JB · Airbus A320232 · Emergency LightingSDR YENA2021121600846Stringer · corrodedDURING HEAVY MAINTENANCE, CORROSION STRINGER 41R LOCATED AT FR 33R IN FWD CARGO COMPARTMENT; REFORMED REPAIR IAW SRM 51-21-13-300-003 FIGURE OO1 SHEET 1. THIS REPAIR IS CATEGORY B AND REQUIRES FURTHER INSPECTION FROM TIME OF ADL/REPAIR EMBODIMENT 40000FC/80000Dec 11, 2021 · N504JB · Airbus A320232 · Fuselage Main, Longeron/StringerSDR YENA2021121600844Shear Tie · corrodedDURING HEAVY MAINTENANCE, CORROSION SHEAR TIE LOCATED AT FR 31 BTW DTR 43R AND 44R IN FWD CARGO COMPARTMENT; REMOVED AND REPLACED SHEAR TIE IAW SRM 51-42-11. WORK ACCOMPLISHED ON AEROMAN NR 2021-475473(CLASSIFIED A MAJOR REPAIR)Dec 11, 2021 · N504JB · Airbus A320232 · Fuselage Internal Mounting StructureSDR YENA2021121600843Shear Tie · corrodedDURING HEAVY MAINTENANCE, CORROSION SHEAR TIE LOCATED AT FR 32 BTW DTR 41R AND 42R IN FWD CARGO COMPARTMENT; REMOVED AND REPLACED SHEAR TIE IAW SRM 51-42-11. WORK ACCOMPLISHED ON AEROMAN NR 2021-475448 (CLASSIFIED A MAJOR REPAIR)Dec 11, 2021 · N504JB · Airbus A320232 · Fuselage Internal Mounting StructureSDR YENA2021121600842Shear Tie · corrodedDURING HEAVY MAINTENANCE, CORROSION SHEAR TIE LOCATED AT FR 31 BTW DTR 41R AND 42R IN FED CARGO COMPARTMENT; REMOVED AND REPLACED SHEAR TIE AT FR 31 BTW STR 41R AND 42R IN FWD CARGO COMPARTMENT IAW SRM 51-42-11. WORK ACCOMPLISHED ON AEROMAN NR 2021-475472 (CLDec 11, 2021 · N504JB · Airbus A320232 · Fuselage Internal Mounting StructureSDR YENA2021121600841Frame · corrodedDURING HEAVY MAINTENANCE, CORROSION LOWER SILL FR 68 AT STR 23L IN PASSENGER CABIN; REMOVED CORROSION AT LOWER SILL FR 68 AT STR 23L IAW SRM 51-74-00. EVALUATED REWORK AND FOUND TO EXCEED ALLOWABLE LIMITS. PERFORMED REPAIR IAW SRM 53-41-14-300-001. WORK ACCOMDec 11, 2021 · N504JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2021121600840Shear Tie · corrodedDURING HEAVY MAINTENANCE, CORROSION SHEAR TIE LOCATED FR 33 BTW STR 40R AND 41 R IN FORWARD CARGO COMPARTMENT; REMOVED AND REPLACED SHEAR TIE IAW 51-72-11. WORK ACCOMPLISHED ON AEROMAN NR 2021-475444Dec 11, 2021 · N504JB · Airbus A320232 · Fuselage Structure (General)SDR YENA2021121600839Shear Tie · corrodedDURING HEAVY MAINTENANCE, CORROSION SHEAR TIE LOCATED AT FR 32 BTW STR 40R AND 41R IN FWD CORDO COMP ; REMOVED AND REPLACED SHEAR TIE LOCATED FR 32 BTW STR 40R AND 41R IN FWD CARGO COMP IAW A320 SRM 51-72-11 WORK ACCOMPLISHED ON AEROMAN NR 20121-475447 (CONSIDDec 11, 2021 · N504JB · Airbus A320232 · Fuselage Internal Mounting StructureSDR GTIA2021121336171Unknown · odorBURNT ELECTRICAL ODOR REPORTED BY AFT FA-ACCOMPLISHED TSM 05-50-810-831 FOR CABIN ODOR AERO TRACER FOUND PACK #2 FOR SOURCE OF CABIN ODOR. REF LP 2760189-2 FOR ADDITIONAL INFO.Dec 11, 2021 · N649NK · Airbus A320232 · Air Distribution SystemSDR YENA2021121300835Receiver · failedFLT 1239, LAS-CUN(DIVERTED TO TPA). GPS PRIMARY LOST IN FLIGHT ; T/S PER TSM 34-52-00-810-847-A. MMR 1& 2 TEST GOOD. ATC 1 & 3 TEST GOOD. GPS VISIBILITY GOOD. R&R MMR1 AS PRECAUTION IAW AMM 34-36-31. BITE TEST GOOD. NO FAULTS NOTED @ THIS TIMEDec 11, 2021 · N644JB · Airbus A320232 · Flight Management Computing Hardware SystemSDR YENA2021121300834Unknown · odorFLT 613, HPN-FLL. ON DESCENT AT FL 280 SMELLED A MODERATE MUSTY CHEMICAL SMELL IN FLIGHTDECK. ODOR LASTED APPROX 20 MIN AND WAS CONSISTENT UNTIL PACK1 AND XBLEED VLV SHUT PER FUMES/ODOR CHECKLIST ; INSPECTED APU BAY AREA: FOUND OIL RESIDUES IN VARIOUS SECTION.Dec 11, 2021 · N554JB · Airbus A320232 · Air Distribution SystemSDR GTIA2021121336168Fan · failed"VENT EXTRACT FAULT IN CRUISE PRECEEDED BY LOUD FAN AND HOT /BURNING SMELL-R/R EXTRACT FAN IAW AMM 21-26-51 OPS CHECK GOOD."Dec 10, 2021 · N647NK · Airbus A320232 · Air Distribution FanSDR CALA2021121202342Fitting · corrodedMAIN CABIN R2 DOOR SILL HAS (2EA) AREAS OF CORROSION ON UPPER SU RFACE CENTER SHAPE SILL ONLY. GENERATED BY N078592 PER HAECO LCQ NR 9294286/22286 REMOVED AND REPLACED R-2 DOOR SILL SHAPE SILL IAW A320 SRM 51-42 -11/001 PARA 6 DOT REMOVED KC50 BY MECH V061630 Dec 10, 2021 · N484UA · Airbus A320232 · Fuselage Structure (General)SDR CALA2021121202341Fitting · corrodedR2 DOOR SILL FWD CORNER FITTING HAS CORROSION. GENERATED BY N078 592 PER HAECO LCQ NR 9294287. REMOVED AND REPLACED CORNER FITTING AT R2 DOOR SILL IAW A320 SRM 51-42-11/001 PARA 6 B,F DOT REMOVED KC51 BY MECH V061630 INSP BY V919150Dec 10, 2021 · N484UA · Airbus A320232 · Fuselage Structure (General)SDR GTIA2021120936166None · noneL1 DOOR ASSIST BOTTLE LIMITS-SVCD L1 DOOR IAW AMM 52-10-00Dec 9, 2021 · N619NK · Airbus A320232 · Passenger/Crew DoorsSDR AALA202112094063None · noneON INITIAL CLIMB AFTER TAKEOFF FMGC SHOWED ENGINE FAILURE WITH AUTO THRUST ECAM TO MOVE THRUST LEVERS TO MCT CONDITION CORRECTED CLIMBING THROUGH 10000. REPLACED #1 FLIGHT MANAGEMENT AND GUIDANCE COMPUTER (FMGC) PER AMM 22-83-34.Dec 8, 2021 · N601AW · Airbus A320232 · Auto Throttle SystemSDR CALA2021120802303Stop Fitting · crackedCRACK FOUND IN THE RH FR20 #1 DOOR STOP FITTING FASTENER HOLE #3 . CRACK IS IN THE INTERCOSTAL ONLY. REMOVED AND REPLACED R/H FR20 #1 DOOR STOP INTERCOASTAL IAW SRM 51-42-11. R5311 3118 FORM 44-0008 ATTACHED EMP# V935774 WORK AC COMPLISHED AT ST ENGINEERING ADec 8, 2021 · N471UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2021120802300None · failedHYD G ENG 1 PUMP LO PR ON ECAM TS FOUND NUMBER ONE ENGINE HYD PUMP SHAFT BROKEN. INSPECTED CASE WORKS NORMALY. CYCLED HYD AUCTORS. CK OK. CLOSED ENGINE COWLING DRAIN FOUND FILTER CLEAN . REINSTALLED PER AMM 29-11-43 NO ROTABLE PARTS CHANGE WAS INDICATED - TT #Dec 7, 2021 · N486UA · Airbus A320232 · Hydraulic Power Accumulator, MainSDR CALA2021120802291Plate · noneREFERENCE LP 7553624 PALNNING TO CONTACT ENGINEERING AFTER 22APR 22 BUT BEFORE 01MAY22 FOR THE ECRA 5330-06890 PART 3- PERMANENT REPAIR REFERENCE LP 7553624 PLANNING TO CONTACT ENGINEERING AFTER 22APR 22 BUT BEFORE 01MAY22 FOR THE ECRA 5330-06890 PART 3- PERMADec 7, 2021 · N444UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2021120802290Plate · crackedFRAME 36 PRESSURE PANEL HOLES 1, 2, 3, 4, 5, 6, 7 AND 8 BETWEEN Y1523 AND Y1292. PRESSURE PANEL HOLES 13, 14, 15, 16, 17, 19, 21 , 22, 24, 25 AND 28 BETWEEN Y1292 AND Y765 HAVE CRACK INDICATION S ON THE PRESSURE PANEL. L23423 & ECRA 5330-05216 OP002 WITH NO DEDec 7, 2021 · N444UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR YENA2021120800832Strap · unsecureFLT 1865, BOS-RSW. GROUND CREW REPORTED BLACK STRAP HANGING OUT FROM BOTTOM OF L1 DOOR ; REMOVED & REPLACED L/H FWD ESCAPE SLIDE IAW AMM 25-62-44 OPS CHECK GOODDec 6, 2021 · N524JB · Airbus A320232 · Emergency EquipmentSDR GTIA2021120636163None · noneL2 CREW/PASSENGER DOOR ASSIST BOTTLE REQUIRES SERVICING-SERVICED L2 CREW/PASSENGER DOOR ASSIST BOTTLE, REF A320 AMM 52-10-00Dec 6, 2021 · N630NK · Airbus A320232 · Passenger/Crew DoorsSDR CALA2021120602262Panel · damagedEMERGENCY EXIT HATCH FRAME ( EXIT AT SEAT 21A) HAS DAMAGED FILLER PANEL AT FRAME FR41 (LH). DAMAGE IS APROX .5 SQ IN IN HATCH SEAL CONTACT AREA WITH PROBABLE PRESSURIZATION LEAK OF MATING SEAL / FILLER PANEL. FILLER PANEL MUST BE RESTORED PER AMM: 53-31-00-440Dec 6, 2021 · N490UA · Airbus A320232 · Fuselage Structure (General)SDR AALA202112067597Lamp · burned outAIRCRAFT WAS NOT GROUNDED: NUMEROUS BULB BURNT OUT RIGHT OVERWING EMERGENCY EXIT LIGHTS. RIGHT EMERGENCY EXIT LIGHT RELAMPED AND OPERATIONS CHECK GOOD PER AMM 33-51-16.Dec 4, 2021 · N656AW · Airbus A320232 · Emergency LightingSDR CALA2021120602247Plate · corrodedCARGO PIT IB TORSION BOX COVER SHEET HAS CORROSION AROUND TIE DO WN FITTINGS PER NR9294383/22383 GEN BY V052030. RMVD AFT CARGO PIT INBD TORSION BOX COVER SHEET AND INSTALLED NE W TORSION BOX COVER SHEET IAW SRM 53-41-49-283-004. APPLIED TOP COAT IAW SRM 51-75Dec 4, 2021 · N484UA · Airbus A320232 · Fuselage Structure (General)SDR AALA202112068555Cover · out of positionAIRCRAFT WAS NOT GROUNDED: DOOR RIGHT FORWARD EMERGENCY EXIT ELECTRONIC CENTRALIZED AIRCRAFT MONITOR. CLIMBING THROUGH 16000 FEET. TROUBLE SHOOTING PER TSM 52-22-00-810-802A , FOUND SLIDE COVER INSTALLED IN WRONG LOCATION, TARGET WAS 180 DEGREES OUT. INSTALLEDDec 3, 2021 · N601AW · Airbus A320232 · Escape SlideSDR AALA202112061193Yaw Damper · malfunctionedAIRCRAFT HAD A BRIEF UN-COMMANDED RIGHT RUDDER INPUT AT CRUISE/ AIRCRAFT BANKED ABOUT 5 DEGREES RIGHT AND YAWED SIGNIFICANTLY RIGHT THEN RETURNED IMMEDIATELY TO LEVEL FLIGHT. REPLACED YAW DAMPER ACTUATOR 3CC1 PER AMM 27-26-51.Dec 3, 2021 · N668AW · Airbus A320232 · Rudder Control SystemSDR CALA2021120602245Plate · crackedFRAME 36 PRESSURE PANEL HOLES 102,103,106 AND 120 BETWEEN Y765 A ND Y1292 HAVE CRAC INDICATIONS IN THE PRESSURE PANEL. A3NB-53-4- 6324; AD2019-23-01 PER HAECO LCQ N/R 9297008/31008 GENERATED BY V061633. ECRA 5331-02786 & REO-L23431 REV I & ECRA 5330-05216 OP00Dec 3, 2021 · N444UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR YENA2021120700830Smoke Detector · fault messageFLT 2110, SDQ-JFK. SMOKE DET FAULT ON ECAM ; UPON INITIAL INSPECTION COULD NOT RUN SYS TEST ON SDCU, SUSPECT SDCU. REMOVED & REPLACED SDCU PER AMM 26-17-34, NO HELP. SUSPECT SMOKE DET FAIL. REMOVED & REPLACED AFT CARGO SMOKE DETECTOR 5WH PER AMM 26-16-15. OPS Dec 1, 2021 · N630JB · Airbus A320232 · Smoke DetectionSDR YENA2021120700829Smoke Detector · failedFLT 2110, SDQ-JFK. SMOKE DET FAULT ON ECAM ; UPON INITIAL INSPECTION COULD NOT RUN SYS TEST ON SDCU, SUSPECT SDCU. REMOVED & REPLACED SDCU PER AMM 26-17-34, NO HELP. SUSPECT SMOKE DET FAIL. REMOVED & REPLACED AFT CARGO SMOKE DETECTOR 5WH PER AMM 26-16-15. OPS Dec 1, 2021 · N630JB · Airbus A320232 · Smoke DetectionSDR AALA202112039985Limiter · faultedAIRCRAFT WAS GROUNDED: VERY SLIGHT UNCOMMANDED RUDDER MOVEMENT DURING DECENT AT APPROXIMATELY 4500FT, DFDR EVENT PB PRESSED SECDS LATER. MAINTENANCE ACCOMPLISHED A GENERAL VISUAL INSPECTION OF THE RUDDER CONTROL SYS & FOUND RUDDER NEUTRAL POSITION DID NOT ALDec 1, 2021 · N668AW · Airbus A320232 · Rudder Control SystemSDR GTIA2021120236159Pump · leakingMUSTY ODOR SMELLED DURING APPROACH AND LANDING -PREFORMED TSM 05-50-00-810-831-A FOUND SOURCE OF SMELL TO BE PACK ONE. FOUND HYD PUMP ON #1 ENG LOOSE RESECURED HYD PUMP IAW AMM 29-00-00. LEAK CHECK GOODDec 1, 2021 · N601NK · Airbus A320232 · Hydraulic Pump (Electric/Engine), MainSDR AALA202112027659None · stickingAIRCRAFT WAS NOT GROUNDED: ARM LEVER AT THE 2L DOOR IS DIFFICULT TO MOVE. ACCOMPLISHED MONITOR AND CHALLENGE PER GPM 13-19 CLEANED EXCESS TAPE OFF OF DOOR SILL, LUBRICATED GIRT BAR ATTACH POINTS PER AMM 52-10-00.Dec 1, 2021 · N660AW · Airbus A320232 · Passenger/Crew DoorsSDR CALA2021120102228None · noneFLAPS FAULT DISPLAYED ON UPPER ECAM SCREEN. - F-CTL PLEASE WORK TSM 27-51-00-810-821-A THEN CONTACT TOMC 847-700-9980....TOMC SMITH. FURTHER DETAILS AWAITED.Dec 1, 2021 · N473UA · Airbus A320232 · Flight Control SystemSDR CALA2021120102218Structure · corroded(A3NB-53-3-6299) AFT RH FR68 AT STRG23 HAS CORROSION. DOT 52-46 () WORK PER FINAL EA 320-5341-13-A2716 REV - AND UAL ECRA 5341-0128 6 ACCOMPLISHED BY EMP#V933438 AT BFM ST AEROSPACE MOBILE. NR#001 5810.Dec 1, 2021 · N486UA · Airbus A320232 · Fuselage, Wing Attach FittingsSDR YENA2021120100826Thermostat · leakingFLT 1557, FLL-BOG (AIRTURN BACK TO FLL). AIR ENG 2 BLEED ABNORMAL PR INTERMITTENT; FOUND SENSE LINE TO PRV LEAKING REPLACED LINE PER AMM 36-11-52. ALSO REMOVED AND REPLACED PRV SELENOID PER AMM 36-11-55. ACCOMP ENG RUN AND NO FURTHER ABNORMAL PRESSURE NOTEDDec 1, 2021 · N537JT · Airbus A320232 · Pneumatic Indicating SystemSDR CALA2021120102212Intercostal · crackedLEFT FR 16 DOOR STOP FITTING #7, INBD UPPER HOLE HAS A CRACK IND ICATION AT 5 O''CLOCK POSITION AT FRAME TO INTERCOSTAL LAYER. (AD 2019-20-10). GENERATE BY V061671 AT HAECO LCQ PER NR 9294263 (2 2263) REMOVED AND REPLACED L/H FRAME 16 DOOR STOP #7 INTERCOSTAL Nov 30, 2021 · N484UA · Airbus A320232 · Fuselage Main, FrameSDR CALA2021120102211Intercostal · crackedAD 2019-20-10; RIGHT FR 16 DOOR STOP FITTING #7, INBD LOWER HOLE HAS A CRACK INDICATION AT 7 O''CLOCK POSITION AT FRAME TOTO INTE RCOSTAL LAYER GENERATED BY V061671 ON HAECO LCQ NR 9294264 (2226 4) REMOVED AND REPLACED R/H FRAME 16 DOOR STOP FITTING #7 INTERCONov 30, 2021 · N484UA · Airbus A320232 · Fuselage Main, FrameSDR CALA2021120102206Hinge Arm · delaminated(A3NB-55-3-6005) LH ELEVATOR #4 HINGE ARM IS DELAM. (REMOVE AND REPLACE DELAM LH #4 ELEVATOR HINGE ARM) REMOVED AND REPLACED LH #4 ELEVATOR HINGE ARM PN#D5598152200200 BFM ST AEROSPACE MOBILE. NR#0016181 IAW SRM 51-42-21 & SRM 51-72-11-911-001. REMOVED AND REINov 30, 2021 · N486UA · Airbus A320232 · Flight Control SystemSDR CALA2021120102205Lever · chippedA3NB-55-3-6005 RH ELEVATOR HINGE ARM LWR EDGE I/B SIDE CHIPPED D OT 42-070 () REMOVED LINES HYD ACCESS IAW AMM 27-34-51-000-001-A. RECEIVED NE W PART P/N D55981442003002 B/N 0003855407 LOCATED AND DRILLED IA W SRM 51-44-21 INSTALED NEW PART IAW SRM 51-42-21/00Nov 30, 2021 · N486UA · Airbus A320232 · Empennage Structure
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