Airbus A319-111
Service difficulty reports · 2,475
Newest first. General aviation reporting is voluntary.
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 aircraft_model_key = 'A319111' 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.
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 = 'A319111' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR WX0A2023032431741Epsu · unknownEMERGENCY LIGHTS AND SIGNS ARE INOP AT L1 DOOR AT L1 AND R1 WHILE ON BATTERY POWER / REMOVED AND REPLACED EMERG BATTERY PER AMM 33-51-338-400-002-A"SDR EE4Y2023032317488Hinge Arm · out of limitsDURING OPERATIONAL CHECK OF EMERGENCY POWER SUPPLY WAS FOUND L2 DOOR ESCAPE SLIDE FAILED. DUE THIS FACT, IT WAS REPLACED THE AFT LH DOOR ESCAPE SLINE PACK ASSY IAW A319 AMM 25-44-000-002-A TASK 25-62-44-400-006-A STEPS 1 THRU 4. SEE COOPESA JOB A1N011 ITEM 2-SDR EE4Y2023032317489Hinge Arm · out of limitsITEM 3-32 17489
DURING THE STRUCTURAL INSPECTION PER ALLEGIANT WORK CARD Nº: 553005-01-1-001_P1-OP-UP/003, IT WAS FOUND THE EMPENAGE, RUDDER HINGE ARM N° 4 P/N D5537131420054 AND FITTING P/N P/N D5537131802800 OUT LIMITS, DUE THIS FACT THE PART MUST BE REPLSDR EE4Y2023032317490Hinge Arm · out of limitsDURING THE STRUCTURAL INSPECTION PER ALLEGIANT WORK CARD Nº: 553005-01-1-001_P1-OP-UP/003, IT WAS FOUND THE EMPENNAGE, RUDDER HINGE ARM N° 1 P/N D5537131620054 AND HINGE ARM N° 7 P/N D5537131720400 OUT LIMITS, DUE THIS FACT THE PARTS MUST BE REPLACED. SEE COOPSDR EE4Y2022032317487Skin Panel · corrodedDURING THE STRUCTURAL INSPECTION PER WORK CARD Nº: 572179-01-1-001, IT WAS FOUND AT LH WING, TOP SKIN LOWER SURFACE AT RIB 15 OVERHANG AREA WITH CORROSION. DUE TO THERE IS NOT SRM AVAILABLE TO PERFORM PERMANENT REPAIR, AIRBUS WAS CONTACTED REQUESTING REPAIR INSDR WX0A2023031731741Epsu · unknownLH,RH,AFT,FWD EPSU BATTERY 11WL,12WL,13WL,10WL FAILED CAP CHECK / REMOVED AND REPLACED EPSU BATTERIES IAW AMM 33-51-38. OPS CHECK GOOD."SDR EE4Y2023031017408Unknown · corrodedDURING INSPECTION TASK 534150-01-2-001 LOWER FUSELAGE AFT CARGO DOOR CUTOUT BETWEEN FR55A AND FR59 AT LOWER SILL BELOW SHEET COVER WEB WITH NUT PLATE RUSTY AT SEVERAL PLACES WAS FOUND. THE SILL D5347715020200 WAS REPLACED IAW A319 SRM 51-72-11-911-001 REV 142 SDR EE4Y2023031017407Frame · unknownDURING TASK INSPECTION 53-260-003 REAR FUSELAGE AFT PAX DOOR STOP FITTING # 1 CRACK WAS FOUND. PERMANENT REPAIR AT AFT ENTRY DOOR FRAME 68LH AT LOWER I/B HOLE DOOR STOP FITTING IAW A319 SRM TASK 53-41-12-300-011 PARAG 2.A TABLE 004 FIGURE 008 (SHEET 1,2,AND 3)SDR EE4Y2023031017402Skin Panel · dentedDURING THE INSPECTION PER TASK ZL-500-02-1-001_P1-OP-UP/0 MPD ALLEGIANT TASK CARD WAS FOUND THE, LH WING SLAT #2 P/N D5746027700200 S/N SA3634 SKIN WITH DENT.
REPAIRED SLAT #2 NOSE SKIN SECTION OVER TRACK RIB #5 IAW A319 SRM TASK 57-40-00-300-224 FIGURE 001.SDR EE4Y2023031017371Frame · corrodedDURING THE STRUCTURE INSPECTION PER ALLEGIANT ENGINEERING ORDER E5316-0002 REV00 WE FOUND FOUND AT UPPER FUSELAGE FR20, RH SIDE, AT LEVEL OF DOOR STOP #1, FRAME WITH CORROSION. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR PER AIRBUS INSTRUCTIONS STATED IN COOSDR EE4Y2023031017369Fitting · crackedDURING THE STRUCTURE INSPECTION PER ALLEGIANT ENGINEERING ORDER E5316-0002 REV00 WE FOUND FOUND AT UPPER FUSELAGE FR20, RH SIDE, AT LEVEL OF DOOR STOP #1, INTERCOSTAL FITTING WITH CRACKS. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR PER AIRBUS INSTRUCTIONS STSDR EE4Y2023031017394Beam · corrodedDURING TH ESTRUCTURE INSPECTION WAS FOUND AT UPPER FUSELAGE FORWARD PAX CABIN AT FR 16, Y503.2 LONGITUDINAL BEAM WITH CORROSION. DUE TO THIS FACT LONGITUDINAL BEAM P/N: D5311282720200 FROM FR 12 TO FR 16 Y503.2 WAS REPLACED IAW A319 SRM 51-72-11-911-001. THE RSDR EE4Y2023031017368Fitting · crackedDURING THE STRUCTURE INSPECTION PER ALLEGIANT ENGINEERING ORDER E5316-0002 REV00 WE FOUND AT UPPER FUSELAGE FR16, LH SIDE, AT LEVEL OF DOOR STOP #7, INTERCOSTAL FITTING WITH CRACKS. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR PER AIRBUS INSTRUCTIONS STATED ISDR EE4Y2023031017393None · corrodedDURING TH ESTRUCTURE INSPECTION WAS AT UPPER FUSELAGE AFT PASSENGER CREW DOOR CUTOUT BETWEEN FR 66 AND FR 68 AT STRG 23R SILL BEAM WITH CORROSION. DUE TO THIS FACT SILL BEAM P/N D5348004320701 WAS REPLACED IAW A319 SRM 51-72-11-911-001 PARAGRAPH 2B. THE REPLACSDR EE4Y2023031017392Beam · corrodedDURING TH ESTRUCTURE INSPECTION WAS AT UPPER FUSELAGE AFT PAX CABIN AT FR 68+80MM Y160.5 LONGITUDINAL BEAM WITH CORROSION. DUE TO THIS FACT LONGITUDINAL BEAM FROM FR 68 TO FR 70 Y160.5 WAS REPLACED IAW A319 SRM 51-72-11-911-001. THE REPLACE WAS HANDLED UNDER CSDR EE4Y2023031017367Door Sill · corrodedDURING THE STRUCTURE INSPECTION WE FOUND AT REAR FUSELAGE PASSENGER/CREW DOORE RH CUTOUT LOWER AREA FROM FR66 TO FR68 SILL AND SOLID RIVETS WITH CORROSION. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR AT RH PASSENGER/CREW DOOR SILL WEB AREA BETWEEN 230MM FWD SDR EE4Y2023031017413Beam · corrodedDURING THE INSPECTION PER ALLEGIANT TASK IT WAS FOUND AT THE PAX CABIN, AFT PASSENGER LH SIDE AT FR68 DORR SILL BEAM WITH CORROSION. THE REPORTED DAMAGED PART WAS REPAIRED I/A/W THE A319 SRM 53-41-14-300-001, FIGURE 001, REPAIR PRINCIPLE 5. SEE COOPESA WORK ORSDR EE4Y2023031017412Beam · corrodedDURING THE INSPECTION PER ALLEGIANT TASK IT WAS FOUND AT THE PAX CABIN, AFT PASSENGER RH SIDE AT FR68 AROUND GIRT BAR A FITTING WITH CORROSION. THE REPORTED DAMAGED PART WAS REPAIRED I/A/W THE A319 SRM 53-41-14-300-001, FIGURE 001, REPAIR PRINCIPLE 5. SEE COOPSDR EE4Y2023031017391Beam · corrodedDURING TH ESTRUCTURE INSPECTION WAS FOUND IN THE UPPER FUSELAGE AFT PAX CABIN AT FR 68 Y765 LONGITUDINAL BEAM WITH CORROSION. DUE TO THIS FACT LONGITUDINAL BEAM P/N D5472192200000 WAS REPLACED IAW A319 SRM 51-72-11-911-001 PARAGRAPH 2 . THE REPAIR WAS HANDLED SDR EE4Y2023031017390Frame · noneDURING TH ESTRUCTURE INSPECTION WAS FOUND IN THECCKPIT WINSHIEL SIDE POST FR 4LH UPPER ATTACHMENT FITTING AND FRAME SECTION WITH DOUBLE HOLE. DUE TO THIS FACT FITTING P/N D5311086620200 AND FRAME P/N D53111068202200 WERE REPLACED. THE REPAIR WAS HANDLED UNDER SDR EE4Y2023031017382None · noneDURING INSPECTION CRACK SEGMENT 1 APROX RIVET 56RH LIP SKIN AND CRACK APROX 5 O´CLOCK POSITION LOKING AFT 16TH RIVET TO THE RIGHT COUNTING FROM BOTTOM CENETER LIP SKIN HAS CINRCUNFERENTIAL CRACK FROM RIVET LENGHT 5/32. THE LIP SKIN WAS REPAIRED IAW ROHR REPAISDR EE4Y2023100317401Skin Panel · dentedDESCRIPTION:
DURING THE STRUCTURAL INSPECTION, IT WAS FOUND AT LH WING SLAT #1 FROM TRACK #2 100MM O/B AND 111MM FROM THE LOWER EDGE, EXTERNAL SKIN WITH DENT
CORRECTIVE ACTION
EVALUATED DENT AND IT WAS FOUND WITHIN LIMITS IAW A319 SRM 57-40-00-283-001 FIGURSDR EE4Y2023031017410Skin Panel · corrodedTHE LH WING MAIN BOX TOP FORWARD PANEL SKIN SURFACE ON STRINGER11 BUTTSTRAP BETWEN RIB3 AND RIB4 WAS FOUND WITH CORROSION. THE REPORTED DAMAGED AREA WAS REPAIRED I/A/W AIRBUS DOSSIER 81133275 REPAIR INSTRUCTIONS. FOR FURTHER DETAILS SEE COOPESA WORK ORDER A1M1SDR EE4Y2023100317400Skin Panel · corrodedDESCRIPTION:
DURING THE STRUCTURAL INSPECTION PER ALLEGIANT WORK CARD 200003-01-1-001_P1-OP-UP/0 PROCESS, COO FOUND AT EMPENNAGE, DORSAL FIN AREA WITH CORROSION BETWEEN THE SKIN AND CONNECTOR 7113VC.
CORRECTIVE ACTION
REPAIRED FUSELAGE SKIN SECTION FROM FSDR EE4Y2023031017379None · corrodedDURING INSPECTION #1 ENGINE LH PYLON AFT MOVABLE FAIRING ACCESS PANEL 477AL, FIXED CUTOUT INTERNAL AFT LOWER CORNER WITH CORROSION WAS FOUND.PERMANENT REPAIR WAS PERFORMED IAW A319 SRM54-55-12-300-006 FIGURE 001 SHEET 1 AND SHEET 2 REV 140 DATED 02-01-2022. THSDR EE4Y2023031017378Floorbeam · corrodedDURING INSPECTION ON REAR FUSELAGE PAX CABIN FROM FR66+140MM TO FR 68 AT -Y 765 FLOOR BEAM WITH CORROSION WAS FOUND. THE AFFECTED FLOOR BEAM WAS REPLACED IAW A319 SRM 51-72-11-911-001 AND 51-72-11-911-002 REV140 DATED 02/01/2022 . THE REPAIR IS CAPTURED IN COOSDR EE4Y2023031017377Profile · noneDURING INSPECTION LOWER FUSELAGE AFT CARGO COMPARTMENT AT FR56, BETWEEN 260 AND Y 680 PROFILES WITH ELONGATED HOLES WAS FOUND. THE AFFECTED PROFILES WERE REPLACED IAW A319 SRM 51-72-11-911-001 PARAG 2 REV 140 DATE 02-01-2022 AND DRAWING D53974965 ISSUE 5. THISSDR EE4Y2023031017415Rack · crackedDURING DETAILED INSPECTION AS PER ALLEGIANT TASK IT WAS FOUND THE 80VU RACK IN CONTACT WITH THE STRUCTURE DUE TO THIS FACT A REPAIR WAS ACCOMPLISHED PER EO E2571-0005. SEE COOPESA WORK ORDER A1N009, 22-6 FOR FURTHER DETAILS.SDR EE4Y2023031017376Stringer · corrodedDURING INSPECTION AT COOPESA MRO COORSION WAS REPORTED AT AFT CARGO COMPARTMENT STGR 42RH BETWEEN FR57-FR59 AND STGR43LH BETWEEN FR56-FR58 COOPESA ASSESSED THE DAMAGE AND COORDINATED A REPAIR WITH AIRBUS VIA TECH REQUEST DOSSIER # 810422127. AIRBUS ISSUED A RESDR EE4Y2023031017399Fitting · corrodedDESCRIPTION:
DURING THE STRUCTURAL INSPECTION PER WORK CARD Nº: 553006-01-2-001 MPD, IT WAS FOUND AT EMPENNAGE RUDDER HINGE ARM#7 WITH CORROSION.
CORRECTIVE ACTION:
REPLACED HINGE ARM BR7 IAW A319-SRM TASK 55-36-42-300-003. SEE COOPESA WORK ORDER A1M116 SDR EE4Y2023031017398Fitting · noneDESCRIPTION:
DURING THE STRUCTURAL INSPECTION PER WORK CARD Nº: 553006-01-2-001 MPD, IT WAS FOUND AT EMPENNAGE RUDDER HINGE #3 BEARING WITH PLAY.
CORRECTIVE ACTION:
REPLACED FORK AND END FITTING AT HINGE ARM BR3 IAW A319-SRM TASK 55-36-42-300-008.
SEESDR EE4Y2023031017414Beam · corrodedDURING THE INSPECTION PER ALLEGIANT TASK IT WAS FOUND CORROSION AT THE AFT PASSENGER DOOR SILL AT FR68 LH SIDE. A PERMANENT REPAIR WAS PERFORMED AS PER A319 SRM 53-41-14-300-001 REPAIR PRINCIPLE 8 FIGURE 001. SEE COOPESA WORK ORDER A1M148, 2-25 FOR DETAILS.SDR EE4Y2023031017397Fitting · noneDESCRIPTION:
DURING THE STRUCTURAL INSPECTION PER WORK CARD Nº: 553006-01-2-001 MPD, IT WAS FOUND AT EMPENNAGE RUDDER HINGE #7 BEARING WITH PLAY.
CORRECTIVE ACTION:
REPLACED FORK AND END FITTING AT HINGE ARM BR7 IAW A319-SRM TASK 55-36-42-300-008.
SEESDR EE4Y2023031017396Fitting · excess playDURING THE STRUCTURAL INSPECTION PER WORK CARD Nº: 553006-01-2-001 MPD, IT WAS FOUND AT EMPENNAGE RUDDER HINGE#5 BEARING WITH PLAY.
REPLACED FORK AND END FITTING AT HINGE ARM BR5 IAW A319-SRM TASK 55-36-42-300-008.
SEE COOPESA WORK ORDER A1M116 3-16SDR EE4Y2023031017395Fitting · excess playDURING THE STRUCTURAL INSPECTION PER WORK CARD Nº: 553006-01-2-001
MPD, IT WAS FOUND AT EMPENNAGE RUDDER HINGE#4 BEARING WITH PLAY.
REPLACED FORK AND END FITTING AT HINGE ARM BR4 IAW A319-SRM TASK 55-36-42-300-008.
SEE COOPESA WORK ORDER A1M116 3-15SDR EE4Y2023031017375Shear Plate · corrodedDURING MAINTENANCE AT COOPESA MRO CORROSION WAS REPORTED ON AFT CARGO COMPARTMENT SHEAR PLATES AT STGR-38RH AND FR52-FR60. COOPESA ASSESSED THE DAMAGE AND COORDINATED A REPAIR WITH AIRBUS VIA TECH REQUEST DOSSIER 81044409. AIRBUS ISSUED A REPAIR APPROVAL BY MESDR EE4Y2023031017374Intercostal · corrodedAFT CARGO COMPARTMENT FROM FR47/51 TO FR65 BETWEEN 38LH AND 38RH NUT PLATES RUSTY AT SEVERAL PLACES WAS FOUND.AIRBUS WAS CONTACTED FOR REPAIR INSTRUCTIONS. AIRBUS PROVIDED REPAIR INSTRUCTIONS AND DAMAGE WAS REPAIRED IAW COOPESA EO COO-EO-2022-15305-R03 AND THESDR WX0A2023022731739Epsu · noneRIGHT OVERWING EMERGENCY LIGHTS AND EXIT SIGN INOP ON BATTERY POWER. / PERFORMED EPSU BITE TEST~FAILS 12WL AT RT EXIT. REMOVED AND REPLACED 12WL EPSU AND TESTS OK (BITE TEST OK AND LIGHTS ILLUMINATE WITH POWER OFF). REF AMM 33-51-38-000-001-A AND 33-51-38-400-SDR EE4Y2023022417244Fitting · crackedDURING THE TASK 53-210-003_P1-OP-UP-NDT/00 WORK CARD INSTRUCTIONS ACCOMPLISHMENT RELATED TO AD 2020-17-03, WAS FOUND THE RH CONTINUITY FITTING WITH CRACK. AIRBUS WAS CONTACTED TO REQUEST THE KITS P/N FOR REPLACEMENT. AIRBUS PROVIDED THE INFORMATION WITH DOSSISDR WX0A2023020331724Epsu · not enteredEPSU TEST SHOWS FAULT FOR 13WL BATTERY / REMOVED AND REPLACED EPSU BATTERY (13WL), OPS CHECK GOOD, IAW AMM REF 33-51-38-000-002-A AND 33-51-38-400-002-A"SDR WX0A2023022231737Unknown · unknownNRC 1000-0060: 35199-5 AFT WET AREA, CORROSION FOUND AROUND NUTPLATE OF L2 FLOOR SILL BEAM NEAR FR 68./AFT WET AREA, L2 FLOOR SILL BEAM NEAR FR 68 REPAIRED AS PER SRM 53-41-14-300-001, REPAIR PRINCIPLE 5, REV. 143 / BAC1503-100096 7075, PO 1763364 HL11VSDR WX0A2023020331722Epsu · not enteredREF. W/O# 00471872-3 CABIN EMERGENCY LIGHTING. FAULTED EPSU BATTERY 13WL DURING TEST. / R&R EPSU BATTERY 13WL IAW AMM 33-51-38 PB401. NO FAULTS NOTED. SYS. OPS CHECK WAS GOOD."SDR WX0A2023012731714Power Supply · no testAFT EPSU POWER SUPPLY UNIT FAILS BATTERY TEST / REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT, BITE CHECK GOOD, OPS CHECK GOOD, WITH REFERENCE TO AMM 33-51-38-000-001-A AND AMM 33-51-38-400-001-A."SDR WX0A2023020331723Not Entered · not enteredNRC 1000-0060: 35199-5 AFT WET AREA, CORROSION FOUND AROUND NUTPLATE OF L2 FLOOR SILL BEAM NEAR FR 68. / AFT WET AREA, L2 FLOOR SILL BEAM NEAR FR 68 REPAIRED AS PER SRM 53-41-14-300-001, REPAIR PRINCIPLE 5, REV. 143 BAC1503-100096 7075, PO 1763364 HL11VFSDR WX0A2023011731705Power Supply · corrodedFOUND EMERGENCY LIGHT BATTERY AFT 13WL INOP DURING WEEKLY CHECK / REMOVED AND REPLACED EMERGENCY LIGHT BATTERY 13 LW IAW AMM 33-51-38-000-001-A. OPS CHECK GOOD AT THIS TIME"SDR WX0A2023011331698Lens · brokenFOUND EXIT SIGN LENS BROKEN AT 90WL3 / REMOVED AND REPLACED EXIT SIGN LENS IN REF TP AMM 33-51-13 PB401"SDR WX0A2023011131695Battery · inoperativeBAT/EPSU(12WL) EMER R MESSEGE DURING BATTERY CAPACITY TEST / REMOVED AND REPLACED EPSU BATTERY 12WL, IAW AMM 33-51-38-000-002-A AND 33-51-38-400-002-A"SDR WX0A2023010931694Megaphone · no testAFT MEGAPHONE FAILED PRE FLIGHT INSPECTION / REMOVED AND REPLACED MEGAPHONES PER LOPA ""A125000L03"" REV ""00"" AND PER AMM 25-65-51"SDR WX0A2023010931693Megaphone · noneFWD MEGAPHONE FAILED PRE FLIGHT INSPECTION / PERFORMED OPS CHECK ON MEGAPHONE ""FLASHING GREEN"" INDICATES GOOD BATTIERIES. OPS CHECK GOOD PER AMM 25-65-710-002"SDR EE4Y2023050116909Window Post · crackedDURING THE SPECIAL DETAILED INSPECTION OF WINDSHIELD SIDE POST AT FR4, UPPER ATTACHMENT, INTERNAL LH SIDE PER ALLEGIANT TASK CARD 531135-01-2-001, A320 FAMILY MPD, IT WAS FOUND A HOLE ELONGATED WITH CRACK INDICATION. CORRECTIVE ACTION: A DAMAGE REPORT WAS SENT
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