N437UA

Service difficulty reports · 127

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
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 n_number = 'N437UA' AND registry_match = 'registration'
  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 CALA2026092819853Light · inoperativeROW 12ABC RED EMERGENCY ISLE LIGHT INOPERATIVE. REMOVED AND REPLACED RED SEAT MOUNTED EMERGENCY LIGHT AT ROW 12ABC REF AMM 33-51-18. OPS CHECK GOOD. GOOD FOR SERVICE.Sep 28, 2026 · N437UA · Airbus A320232 · Emergency LightingSDR CALA2026040615102Door · unsecureABORTED TAKEOFF, FWD CARGO DOOR OPEN FOUND FWD CARGO DOOR NOT LATCHED PROPERLY, ON CLOSING OF HANDLE INDICATION OF DOOR OPEN WENT OUT. REJECT OCCURRED AT APPROX 80 KNOTS WITH MAX AUTOBRAKE STOPPING AIRCRAFT. MAX BRAKE TEMP WAS 720 ON BRAKE NR 3. VERIFIED NOMar 31, 2026 · N437UA · Airbus A320232 · Cargo/Baggage DoorsSDR CALA2025081307696Helicoil · damagedAFT CARGO DOOR LATCHOPENED DURING FLT PERFORMED TSM 32-31-00-810-886-A, AFT CARGO DOOR INDICATION PROXIMITY SWITCH TGT POS FAULT. WHILE PERFORMING OPERATIONAL CHECK OF THE AFT CARGO COMPARTMENT DOOR. FOUND HANDLE MECHANISM BEARING LOOSE, MISSING HARDWARE. MAKIAug 10, 2025 · N437UA · Airbus A320232 · Cargo/Baggage DoorsSDR CALA2025062605930Fuel Cap · missingFUELER REPORTS FUEL CAP MISSING. REPLACED FUELING CAP ON CDL.VERIFIED FUEL NOT LEAKING FROM FUELING RECEPTACLE.Jun 25, 2025 · N437UA · Airbus A320232 · Fuel StorageSDR CALA2025061305530None · noneREMOVED FWD LH EXIT HATCH IAW AMM 52-21-11-000-001-A AND INSTALLED LOCKPIN ON LH INFLATION RESERVOIR IAW AMM 25-62-00-481-001-A INSTALLED FWD LH EXIT HATCH IAW AMM 52-21-11-400-001-A AND REMOVED LOCKPIN FROM LH INFLATION RESERVOIR IAW AMM 25-62-00-081-001-A INJun 10, 2025 · N437UA · Airbus A320232 · Standard Practices/StructuresSDR CALA2024061401799Door · missingPDA 1 #2 ENG OIL SERVICE DOOR MISSING ON ARRIVAL TO DENVER HINGE IS MISSING PIC CHECKED BONDING BETWEEN COWL HINGE AND PYLON FOR NEW COWL OIL SERVICE DOOR MEASURES 20.5 IN X 18.5 IN INSTALL PER AMM 20-28-00. WITHIN LIMTS. REF LOGPAGE 8256271 OIL SVC DOOR MISSIJun 11, 2024 · N437UA · Airbus A320232 · Nacelle/Pylon, Main FrameSDR CALA2024041501086Drain Line · damagedHYD Y RSVR LO LVL UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. INSPECTED ENG # 2 PYLON AREA CASE DRAIN LINE PIPE ITEM 250 WAS FOUND WITH A SMALL HOLE DUE TO CHAFING BETWEEN PIPE AND BROKEN PYLON BRACKET THEREFOREApr 11, 2024 · N437UA · Airbus A320232 · Hydraulic Power SystemSDR CALA2023103003237Skin · contaminatedL/H ELEVATOR HAS POSSABLE LIQUID INGRESS AT INDICATION "C" 86 1/ 2 IN FROME I/B END, 15 IN FROME TRAILING EDGE, 1 IN DIAMITER "REPAIR BEFORE NEXT FLIGHT" (SUPPORT TASK) GENERATED AT HAECO LCQ P ER NR 9290285 (28285. REPAIRED LH ELEVATOR 86.5IN FROM IB 15IN FROct 27, 2023 · N437UA · Airbus A320232 · Elevator, Plate/SkinSDR CALA2023103003236Frame · crackedAD 2022-08-08. LH FRAME 16 UPPER DOUBLER JOGGLE, HOLE "A", HAS A CRACK INDICATION IN THE FRAME LAYER AT THE 5:0 CLOCK POS, 50% S H. "REPAIR BEFORE NEXT FLIGHT" (AD RELATED TASK) GENERATED AT HAECO LCQ PER NR 9290200 (28200). REPAIRED HOLE A AT LH FR 16 UPPER Oct 27, 2023 · N437UA · Airbus A320232 · Fuselage Main, FrameSDR CALA2023103003235Skin · contaminatedLH ELEVATOR HAS POSSABLE LIQUID INGRESS AT INDICATION "A" 123IN FROM I/B END, 8 1/2 IN FROME TRAILING EDGE, 3/4 IN DIAMITER "REPAIR BEFORE NEXT FLIGHT" (SUPPORT TASK) GENERATED AT HAECO LCQ PE R NR 9290282 (28282) . REPAIRED LH ELEVATOR UPPER SKIN 123IN FROM Oct 27, 2023 · N437UA · Airbus A320232 · Elevator, Plate/SkinSDR CALA2023103003239Skin · contaminatedL/H ELEVATOR HAS POSSABLE LIQUID INGRESS AT INDICATION "C" 108 I N FROM I/B END, 16 IN FROME TRAILING EDGE, 3/4 IN DIAMITER "REPA IR BEFORE NEXT FLIGHT" (SUPPORT TAKS) GENERATED AT HAECO LCQ PER NR 9290284 (28284). REPAIRED LH ELEVATOR 108IN FROM IB AND 16INOct 27, 2023 · N437UA · Airbus A320232 · Elevator, Plate/SkinSDR CALA2023103003238Skin · contaminatedL/H ELEVATOR HAS POSSABLE LIQUID INGRESS AT INDICATION "B" 109 I N FROM I/B END, 8 IN FROME TRAILING EDGE 1 IN DIAMITER REPAIR BEFORE NEXT FLIGHT. REPAIRED LH ELEVATOR 109IN FROM IB 8IN FROM TE 1.5IN DIA ZONE 1- 3 IAW A320 SRM 55-21-11-300-005 CAT A REPAIR UPOct 27, 2023 · N437UA · Airbus A320232 · Elevator, Plate/SkinSDR CALA2023102703198Stiffener · crackedREVB AD 2020-06-10 FLIGHT DECK FR4 F.O SLIDING WINDOW VERTICAL STIFFENER PRODUCED CRACK DURING HFEC INSPECTION (EA 5310-07673) GENERATED AT HAECO LCQ ON NR 9290067 (28067) BY MECH V061690 REPAIRED DISCREPANT AREA AT FLIGHT DECK FR4 F.O. SLIDING WINDOW VERTICALOct 20, 2023 · N437UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2023102303164Fitting · crackedREV.L AD 2015-02-14 LMLG DOOR FWD HINGE PRODUCED CRACK INDICATIO NS DURING HFEC INSPECTION AROUND LOWER FWD FASTENER HOLE COMMON TO THE HINGE CONNECTING PLATE (EA 5330-04821)Oct 20, 2023 · N437UA · Airbus A320232 · Landing Gear SystemSDR CALA2023071702264Cap · missingFUELER REPORTS FUEL CAP IS MISSING MOORE, ROBERT (V082625)APPLIED CEL WITH TOMC FOR FUEL CAP MISSING DISPATCH DESK: 34 NAME: TP DATE: 14-JUL-23- DEFERRED DIRECTLY BY TOMC UPDATED MAA CODE FIX USING VENDOR MAA SCREEN MAC METER INITIATED FOR WITH VENDOR Jul 14, 2023 · N437UA · Airbus A320232 · Aircraft Fuel SystemSDR CALA2023020100303Battery · noneCABIN EMERGENCY LIGHTS OPERATIONAL CHECK: {A3NB-33-3-6012} - TEST FAULTS EPSU BATTERY AFT L RPLD EPSU 13WL AND OPS CK CK NORMAL REF AMM 33-51-38-000-001-A AND AMM 33-51-00-710-001-AFeb 1, 2023 · N437UA · Airbus A320232 · Lighting SystemSDR CALA2022091402360Fitting · crackedCRACK INDICATION ON FRAME 36 PRESSURE DECK MEMBRANE UPPER SURFACE ON OPEN FASTENER HOLE 1 INCH OUTBOARD FROM BEAM Y1292, CRACK DIRECTION IS 12 OCLOCK IN FWD CARGO COMPARTMENT (1 EA).SEE AEROMAN NON ROUTINE 2022-343339. TION INTERVAL AND METHOD AS DETAILED. HOLSep 12, 2022 · N437UA · Airbus A300* · Fuselage Structure (General)SDR CALA2022091402359None · crackedCRACK INDICATION ON FRAME 36 PRESSURE DECK MEMBRANE UPPER SURFACE ON OPEN FASTENER HOLE 5 INCH OUTBOARD FROM BEAM -Y1292, CRACK DIRECTION IS 12 OCLOCK IN FWD CARGO COMPARTMENT (1 EA) SEE AEROMAN NON ROUTINE 2022-343338 LATEST REVISION OF EC5311-02882 ON OR BESep 12, 2022 · N437UA · Airbus A300* · Fuselage Structure (General)SDR CALA2022091202342Pressure Panel · crackedCRACK INDICATION ON FRAME 36 PRESSURE DECK MEMBRANE UPPER SURFACE ON OPEN FASTENER HOLE 5 INCH OUTBOARD FROM BEAM -Y1292, CRACK DIRECTION IS 12 OCLOCK IN FWD CARGO COMPARTMENT (1 EA) SEE AEROMAN NON ROUTINE 2022-343338 LATEST REVISION OF EC5311-02882 ON OR BESep 12, 2022 · N437UA · Airbus A300* · Fuselage Main, FrameSDR CALA2022091202335Skin · noneLIGHTNING STRIKE EXTERNAL SKIN BTW FRAME 43 TO FRAME 44 AND BTW STRIN GER 1R TO STRINGER 1L ON UPPER FUSELAGE. SEE AEROMAN NON ROUTINE 2022-343081. (SHEET 03). PERFORMED ROTOTEST INSPECTION ON OPEN FASTENERS DIAMETER HOLES ARE : 0.187 INCH . TOOL USED ELECTROSep 10, 2022 · N437UA · Airbus A300* · Fuselage Main, StructureSDR CALA2022091202333None · crackedCRACK INDICATION ON FRAME 68 RH SIDE IN OPEN FASTENER HOLE LOWER INBOARD AT DOOR STOP FITTING 1 POSITION, CRACK DIRECTIONS ARE 12 AND 6 OCLOCK, REPAIR BEFORE NEXT FLIGHT AT AFT GALLEY AREA (2 EA) SEE AEROMAN NON ROUTINE 2022-343066 LEVEL REPAIR AREA AT DOOR SSep 10, 2022 · N437UA · Airbus A300* · Fuselage, Wing Attach FittingsSDR CALA2022091202332None · crackedCRACK INDICATION ON FRAME 66 LH SIDE IN OPEN FASTENER HOLE LOWER IN BOARD AT DOOR STOP 1 POSITION, CRACK DIRECTION IS 2 OCLOCK, REPAIR BEFORE NEXT FLIGHT AT AFT GALLEY AREA (1 EA) SEE AEROMAN NON ROUTINE 2022-343324 INSPECTION THRESHOLD FROM TIME OF ADL/REPASep 10, 2022 · N437UA · Airbus A300* · Fuselage, Wing Attach FittingsSDR CALA2022081902124Channel · corrodedCORROSION LOWER SILL LOCATED FR66 TO FR68 LEVEL STRG23L IN PASSENGER CABIN.SEE AEROMAN NON ROUTINE 2022-343198 REMOVED AND REPLACED LOWER SILL LOCATED FR66 TO FR68 AT LEVEL POINT AREA:L=0.604 IN W=0.485 IN;D=0.079 IN, NOMINAL THICKNESS= SILL PERFORMED VISUAL IAug 17, 2022 · N437UA · Airbus A320232 · Fuselage, Wing Attach FittingsSDR CALA2022081702112Frame · crackedCRACK INDICATION ON FRAME 66 LH SIDE IN OPEN FASTENER HOLE LOWER IN BOARD AT DOOR STOP 1 POSITION, CRACK DIRECTION IS 2 OCLOCK, REPAIR BEFORE NEXT FLIGHT AT AFT GALLEY AREA (1 EA) SEE AEROMAN NON ROUTINE 2022-343324 INSPECTION THRESHOLD FROM TIME OF ADL/REPAAug 17, 2022 · N437UA · Airbus A320232 · Fuselage, Wing Attach FittingsSDR CALA2022081602072Channel · corrodedCORROSION LOWER SILL LOCATED FR66 TO FR68 LEVEL STRG23L IN PASSENGER CABIN.REMOVED AND REPLACED LOWER SILL LOCATED FR66 TO FR68 AT LEVEL POINT AREA.Aug 16, 2022 · N437UA · Airbus A320232 · Fuselage, Wing Attach FittingsSDR CALA2022081002033Angle · crackedCRACK FLOOR STRUCTURE ANGLE LOCATED FR68 LEVEL STRG23L IN PASSENGER CABIN (1 EA) REMOVED AND REPLACED FLOOR STRUCTURE ANGLE AND FASTENERS AND NOT FOUND MORE DAMAGE IAW NTM 51-90-00. PERFORMED LOCATED FR68 AT LEVEL STR 23L IN PASSENGER CABIN IAW A320 SCEPTRE Aug 9, 2022 · N437UA · Airbus A320232 · Fuselage Floor PanelSDR CALA2022080801983Beam · corrodedCORROSION FLOOR BEAM +Y765 LOCATED FR66 IN PASSENGER CABIN REMOVED AND REPLACED FLOOR BEAM +765 LOCATED BTW INSPECTION ON AREA AND NOT FOUND ADDITIONAL W=0.115IN. TOOL USED: CALIPER PN:700-113-10, FR64 TO FR66 AT AFT GALLEY AREA IN PSSENGER CABIN DAMAGE IAW NAug 5, 2022 · N437UA · Airbus A300* · Fuselage Structure (General)SDR CALA2022080801981Angle · crackedCRACK FLOOR STRUCTURE ANGLE LOCATED FR66 LEVEL STRG 23L IN PASSENGER CABIN, SEE AEROMAN NON ROUTINE 2022-343169 REMOVED AND REPLACED FLOOR STRUCTURE ANGLE LOCATED FR.66 LEVEL 24-JUN-23, PERFORMED VISUAL INSPECTION ON AREA AND NOT FOUND STR. 23L IN PASSENGER CAAug 5, 2022 · N437UA · Airbus A300* · Fuselage Structure (General)SDR CALA2022080801980Angle · crackedCRACK FLOOR STRUCTURE ANGLE LOCATED FR66 LEVEL STRG23R IN PASSE ABIN. SEE AEROMAN NON ROUTINE 2022-343195 REMOVED AND REPLACED FLOOR STRUCTURE ANGLE LOCATED FR 66 LEVEL 24-JUN-23. PERFORMED VISUAL INSPECTION ON AREA AND NOT FOUND STR 23R IN PASSEGER CABIN IAAug 5, 2022 · N437UA · Airbus A300* · Fuselage Structure (General)SDR CALA2022080801979None · corrodedCORROSION FLOOR STRUCTURE LOCATED FR68 Y160.5 IN IN PASSENGER CABIN REPLACED FLOOR STRUCTURE LOCATED FR68 Y160.5 NTM 51-90-00. PERFORMED SCEPTRE ENTRY IN PASSENGER CABIN IAW A320 51-72-11 AND ON LOGPAGE NUMBER IS:9153134. MEASURE OF CORROSION DRAWING #D534720Aug 5, 2022 · N437UA · Airbus A300* · Fuselage Structure (General)SDR CALA2022080501967Floorbeam · corrodedCORROSION FLOORBEAM +Y1292 LOCATED FR66 IN PASSENGER CABIN SEE AEROMAN NON ROUTINE 2022-343175 REMOVED AND REPLACED FLOOR BEAM + Y1292 LOCATED BTW FR 64 TO FR D=2.29MM (0.090IN). TOOL SPLICES AND NOT FOUND MORE DAMAGE IAW NTM 51-90-00. PERFORMED 66 AFT GALLEYAug 4, 2022 · N437UA · Airbus A320232 · Fuselage Main, Floor BeamSDR CALA2022080501966Fitting · crackedCRACK INDICATION ON FRAME 58 IN OPEN FASTENER HOLE IN HORIZONTAL FLANGE AT LEVEL OF STGR 37LH, CRACK DIRECTION IS 9 OCLOCK, REPAIR BEFORE FURTHER FLIGHT IN AFT CARGO COMPARTMENT (1 EA) REMOVED AND REPLACED SUPPORT FITTING AND FASTENER LOC. ON FR58 BRACKET LAYAug 4, 2022 · N437UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2022080501965Frame · crackedCRACK INDICATION ON FRAME 43 FOOT COUPLING LH SIDE IN OPEN FASTENER HOLE AT LEVE OF STGR22, CRACK DIRECTION IS 3 OCLOCK IN PASSENGER CABIN (1 EA) REPAIR BEFORE NEXT FLIGHT REMOVED AND REPLACED FRAME 43 FOOT COUNPLING AND FASTENERS LOC FOOT FITTING AT LEVEL STRAug 4, 2022 · N437UA · Airbus A320232 · Fuselage Main, FrameSDR CALA2022080501964Beam · corrodedCORROSION LOWER SILL LOCATED FR66 TO FR68 R/H SIDE AT AFT GALLEY AREA REMOVED AND REPLACED LOWER SILL LOCATED FR66 TO FR68 R/H SIDE CORRODED AREAS ARE:DEEPEST POINT L=3.980 IN W=2.049 IN D=0.055 IS 9151970.SEE AEROMAN NON ROUTINE 2022-343194 AT AFT GALLEY AREAAug 4, 2022 · N437UA · Airbus A320232 · Fuselage, Wing Attach FittingsSDR CALA2022080301948Floor Support · crackedCRACK FLOOR STRUCTURE ANGLE LOCATED FR66 LEVEL STRG 23L IN PASSENGER CABIN, SEE AEROMAN NON ROUTINE 2022-343169 REMOVED AND REPLACED FLOOR STRUCTURE ANGLE LOCATED FR.66 LEVEL 24-JUN-23, PERFORMED VISUAL INSPECTION ON AREA AND NOT FOUND STR. 23L IN PASSENGER CAAug 3, 2022 · N437UA · Airbus A320232 · Fuselage Main, Floor BeamSDR CALA2022080301947Floorbeam · corrodedCORROSION FLOORBEAM +Y1292 LOCATED FR66 IN PASSENGER CABIN SEE AEROMAN NON ROUTINE 2022-343175 REMOVED AND REPLACED FLOORBEAM + Y1292 LOCATED BTW FR 64 TO FR D=2.29MM (0.090IN). TOOL SPLICES AND NOT FOUND MORE DAMAGE IAW NTM 51-90-00. PERFORMED 66 AFT GALLEY Aug 3, 2022 · N437UA · Airbus A320232 · Fuselage Main, Floor BeamSDR CALA2022080301946Floor Support · crackedCRACK FLOOR STRUCTURE ANGLE LOCATED FR66 LEVEL STRG23R IN PASSE ABIN. SEE AEROMAN NON ROUTINE 2022-343195 REMOVED AND REPLACED FLOOR STRUCTURE ANGLE LOCATED FR 66 LEVEL 24-JUN-23. PERFORMED VISUAL INSPECTION ON AREA AND NOT FOUND STR 23R IN PASSEGER CABIN IAAug 3, 2022 · N437UA · Airbus A320232 · Fuselage Main, Floor BeamSDR CALA2022080301945Floor Support · corrodedCORROSION FLOOR STRUCTURE -Y1162.5 AND FR68 IN PASSENGER CABIN REMOVED AND REPLACED FLOOR STRUCTURE -Y1162.5 LOC. FR.68 TO DIGITRAL CALIPER P/N: 500-197-30; S/N: A21147760; CAL DUE DATE: PERFORMED SCEPTRE ENTRY ON LOG PAGE NUMBER 9206195 FR.69 AND -Y1162.5 IAAug 3, 2022 · N437UA · Airbus A320232 · Fuselage Main, Floor BeamSDR CALA2022080101934Coupling · crackedCRACK INDICATION ON FRAME 43 FOOT COUPLING LH SIDE IN OPEN FASTENER HOLE AT LEVE OF STGR22, CRACK DIRECTION IS 3 OCLOCK IN PASSENGER CABIN. REMOVED AND REPLACED FRAME 43 FOOT COUNPLING AND FASTENERS LOC FOOT FITTING AT LEVEL STR21 LH.Aug 1, 2022 · N437UA · Airbus A320232 · Fuselage Main, FrameSDR CALA2022080101933Frame · crackedCRACK INDICATION ON FRAME 58 IN OPEN FASTENER HOLE IN HORIZONTAL FLANGE AT LEVEL OF STGR 37LH, CRACK DIRECTION IS 9 OCLOCK, REMOVED AND REPLACED SUPPORT FITTING AND FASTENER LOC. ON FR58 BRACKET LAYER.Aug 1, 2022 · N437UA · Airbus A320232 · Fuselage Main, FrameSDR CALA2022080101932Floor Support · corrodedCORROSION FLOOR STRUCTURE Y1162.5 AND FR68 IN PASSENGER CABIN REMOVED AND REPLACED FLOOR STRUCTURE Y1162.5 AND FASTENER LOC D=1.150 MM (0.045 INCH).Aug 1, 2022 · N437UA · Airbus A320232 · Fuselage Main, Floor BeamSDR CALA2022072901913Channel · corrodedCORROSION LOWER SILL LOCATED FR66 TO FR68 R/H SIDE AT AFT GALLEY AREA REMOVED AND REPLACED LOWER SILL LOCATED FR66 TO FR68 R/H SIDE CORRODED AREAS ARE:DEEPEST POINT L=3.980 IN W=2.049 IN D=0.055 IS 9151970.SEE AEROMAN NON ROUTINE 2022-343194 AT AFT GALLEY AREAJul 29, 2022 · N437UA · Airbus A320232 · Fuselage, Wing Attach FittingsSDR CALA2022072701890Floorbeam · corrodedCORROSION FLOORBEAM +Y765 LOCATED FR66 IN PASSENGER CABIN REMOVED AND REPLACED FLOORBEAM +765 LOCATED BTW INSPECTION ON AREA AND NOT FOUND ADDITIONAL W=0.115IN. TOOL USED: CALIPER PN:700-113-10, FR64 TO FR66 AT AFT GALLEY AREA IN PSSENGER CABIN DAMAGE IAW NTMJul 27, 2022 · N437UA · Airbus A320232 · Fuselage Main, Floor BeamSDR CALA2022072701904Floorbeam · corrodedCORROSION FLOORBEAM -Y765 LOCATED FR21 AT FWD GALLEY AREA REMOVED AND REPLACED FLOOR BEAM -Y765 LOC BTW FR12 TO FR24 AT FWD GALLEY AREA IAW A320 SRM 51-42-11 AND DWG D53112812, D53110984, D53110876, D53112814 AND PERFORMED VISUAL INSPECTION ON AREA NOT FOUND Jul 25, 2022 · N437UA · Airbus A320232 · Fuselage Main, Floor BeamSDR CALA2022072701901Floorbeam · corrodedCORROSION FLOORBEAM +Y765 LOCATED FR67 TO FR68 IN PASSENGER CABIN REMOVED AND REPLACED FLOOR BEAM +Y765 LOC BTW FR66 TO FR70 IN PASSENGER CABIN I.A.W A320 SRM 51-42-11 AND DWG D53472040 AND PERFORMED VISUAL INSPECTION ON AREA AND NOT FOUND ADDITIONAL DAMAGE IJul 25, 2022 · N437UA · Airbus A320232 · Fuselage Main, Floor BeamSDR CALA2022072001845None · corrodedCORROSION FLOOR BEAM -Y765 LOCATED FR21 AT FWD GALLEY AREA REMOVED AND REPLACED FLOOR BEAM -Y765 LOC BTW FR12 TO FR24 AT FWD GALLEY AREA IAW A320 SRM 51-42-11 AND DWG D53112812, D53110984, D53110876, D53112814 AND PERFORMED VISUAL INSPECTION ON AREA NOT FOUNDJul 20, 2022 · N437UA · Airbus A300* · Fuselage Floor PanelSDR CALA2022072001844None · corrodedCORROSION FLOOR BEAM Y-1292 AND FR21 AT FWD GALLEY AREA (1EA) REMOVED AND REPLACED FLOOR BEAM -Y1292 LOC BTW FR12 TO FR24 AT F WD GALLEY AREA IAW A320 SRM 51-42-11, 51-72-11 AND DWG: D5311281 4, D53110876, D53112812 AND PERFORMED VISUAL INSPECTION ON AREA NOT Jul 20, 2022 · N437UA · Airbus A300* · Fuselage Miscellaneous StructureSDR CALA2022072001843None · corrodedCORROSION FLOOR BEAM +Y765 LOCATED FR67 TO FR68 IN PASSENGER CABIN REMOVED AND REPLACED FLOOR BEAM +Y765 LOC BTW FR66 TO FR70 IN PASSENGER CABIN I.A.W A320 SRM 51-42-11 AND DWG D53472040 AND PERFORMED VISUAL INSPECTION ON AREA AND NOT FOUND ADDITIONAL DAMAGE Jul 20, 2022 · N437UA · Airbus A300* · Passenger Compartment WindowsSDR CALA2018011900248Cover · looseDOOR R AFT EMERGENCY EXIT ECAM 4X WHILE IN FLGHT INSPECTED AND INSTALLED COVER FLAP, INDICATION OPS NORMAL IAW AMM 25-23-47-400-001-AJan 19, 2018 · N437UA · Airbus A320232 · Service DoorsSDR CALA2018011500210Cover · looseR AFT EMER EXIT DISPLAYED ON UPPER ECAM SCREEN. DOOR ECAM ANNUNCIATED AT 11000 ON DEPARTURE PRESSURIZATION NORMAL PAX SAID COVER FELL OFF REINSTALLED COVER AT EMER EXIT DOOR STATUS NORMAL.Jan 15, 2018 · N437UA · Airbus A320232 · Emergency Exits
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