N811UA

Service difficulty reports · 103

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 = 'N811UA' 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 CALA2026101320357Light · inoperativeAISLE SEAT 8C EMERGENCY LIGHT INOP. REMOVED AND REPLACED PATHWAY ILLUMINATION LIGHT ON SEAT 8C IN REFERENCE TO AMM 33-51-19. OPS CHECK GOOD. PARTS USED: BR9644-21,QTY :1Oct 11, 2026 · N811UA · Airbus A319131 · Emergency LightingSDR CALA2026071617809Skin · damagedLIGHTNING STRIKE ON FASTNER AT STA 4546. 18.25 INCHES ABOVE STRINGER. PERFORMED MATERIAL LOSS MEASUREMENT INSP PER NTM TASK 51-10-04-270-802-A WITH REMAINING MATERIAL AT THINNEST IN BLENDED AREA AT 0.081 AND THICKNESS BARE METAL AREA AT 0.093. REMOVED LIGHTNJul 15, 2026 · N811UA · Airbus A319131 · Fuselage Main, Plate/SkinSDR CALA2026010212636Diaphragm · damagedLEFT WING DRY BAY STRUCTURE, RIB 6 - 6B, CLOSING PANEL AND DIAPHRAGM WERE REPLACED AT MLB. REPAIR IS EXPECTED TO BECOME A PERMANENT SOLUTION WITH NO SUPPLEMENTAL INSPECTION REQUIREMENTS. ACCOMPLISH PERMANENT REPAIR ACTION IAW PART 3 OF THE LATEST REVISION OF EDec 29, 2025 · N811UA · Airbus A319131 · Wing Main, Frame StructureSDR CALA2025032803293Access Panel · damagedLEFT WING FUEL TANK ACCESS PANEL 540K B HAS ONE ELONGATED HOLE AT APPROX 7:00 POSTION. REWORKED AND REPAIRED LANDING IAW ECRA 5720-02626 ACP INITIAL RE QUIREMENTS PER PART 2 OF ECRA BEFORE ACFT REACHES 85800T OR 4290 0C WHICHEVER COMES 1ST. ACP REPEAT INSP PERMar 26, 2025 · N811UA · Airbus A319131 · Wing, Plate/SkinSDR CALA2024070300110Tire · worn04 MLG TIRE FOUND BEYOND AMM LIMITS. MUST BE REPLACED PRIOR TO T HE NEXT FLIGHT. DUE TO FOD DAMAGE, #4 TIRE HAS CUT THAT REACHES PROTECTOR PLIES AND IS NOT CONTAINED WITHIN A RIB, OUT OF LIM REF AMM 32-41-00-210-002-A ROTABLE PARTS INFO ROTABLE PARTS CHANGE Jul 1, 2024 · N811UA · Airbus A319131 · TireSDR CALA2024041901144Fuel Cap · missingPDA 2 REF L/P 7703099 FOR FUEL CAP MISSING ON ARRIVAL MISSING FUEL CAP HAS BEEN PUT ON MEL USING MEL REF 28A. SDR AND ESFR HAS BEEN FILED.Apr 19, 2024 · N811UA · Airbus A319131 · Fuel StorageSDR CALA2023092902917Motor · seizedYELLOW HYD SYS OVHTWITH SPOILERS 2/4DEPLOYED ON BOTH WINGS POST FLT REPORT. SEE PIC NOTED ELEC Y PUMP DOES NOT COME ON AND ENG DRIVEN PUMP HAS PRESSURE DURING DRY MOTOR. FOUND Y ELEC PUMP NORM (AB 3) POPPED. RESET BREAKER, POPS AS SOON AS ELEC PUMP TURNED ON ISep 26, 2023 · N811UA · Airbus A319131 · Hydraulic Pump (Electric/Engine), MainSDR CALA2023062301982Fitting · gougedCOCKPIT CO-PILOT SLIDING WINDOW FWD GUIDE RAIL HAS 2EA GOUGES. REMOVED AND REPLACED RAIL #D5311401820700 IAW SRM 51-42-11. STA: ST ENG BFM WC:56513 INSPECTED AND APPROVEDJun 22, 2023 · N811UA · Airbus A319131 · Flight Compartment WindowsSDR CALA2023062602033Guide · gougedCOCKPIT CO-PILOT SLIDING WINDOW FWD GUIDE RAIL HAS 2EA GOUGES. REMOVED AND REPLACED RAIL #D5311401820700 IAW SRM 51-42-11. STA: ST ENG BFM WC:56513 INSPECTED AND APPROVED.Jun 21, 2023 · N811UA · Airbus A319131 · Flight Compartment WindowsSDR CALA2023061201824Door Sill · corrodedAFT CARGO COMPARTMENT DOOR SILL UPPER SURFACE FR56-FR58 CORRODED. REQUIRES REPLACEMENT. AFT CARGO DOOR SILL REPLACED IAW SRM 51-42-11. ESFR COMPLIED WITHJun 11, 2023 · N811UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2023053101723Frame · corroded10SEP SFO CF -T :AFT FACE OF FRAME 16R ABOVE DOOR THRESHOLD IS CORRODED.REPAIRED REF ECRA 5311-01825.APPROVED AS CAT C TEMP REPAIR.ACP PART2 INSP BEGINING AT 25,804C AND REPEAT EVERY 1000C .ACP PART 3 PERMANENT REPAIR ON OF BEFORE 34,554C.NOTE TO PLANNI G CONTMay 30, 2023 · N811UA · Airbus A319131 · Fuselage Main, FrameSDR CALA2023052401627Fitting · corrodedMAIN CABIN BELOW FLOOR PNL 262GF FR70 R/H ANGLE FITTINGS SIGNS O F CORROSION DOT 43-143 () REPLACED DAMAGED CORNER FITTING IAW A319 SRM 51-42-11 AMD 51-44- 11, NEW FITTING PN: D5357030120700 BATCH: 0004112648 ATTACHED FO RM 44-0008 EMP#: V934583 WORK ACCOMPLISMay 22, 2023 · N811UA · Airbus A319131 · Fuselage Main, Attach FittingsSDR CALA2023051501517Intercostal · crackedRH EMER.EXIT ESCAPE HATCH RH LOAD LIMITING FROFIL CRACKED AT FAS TENER HOLES. REMOVED RH INTERCOSTAL IAW SRM 51-42-11, RECEIVVE NEW SEGMENT AN AND RESTORED SURFACE PROTECTION IAW SRM 51-75-11/001. EMP: V9363 GLE P/N D5227902620551, BATCH# 0004061454, LOCATED AMay 13, 2023 · N811UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2023051501516Floor Support · corrodedMAIN CABIN BETWEEN FR16-12 L/H CENTER FLOOR BEAM SIGNS OF CORROS ION REPLACED DAMAGED BEAM Y503.2 FOUND OUT OF LIMITS IAW A319 SRM 53 -11-14-283-007, NEW BEAM PN: D5311282600200 BATCH: 0004052059 IN STALLED IAW A319 SRM 51-42-11 AND 51-44-11.- EMP: V934583 WC:May 13, 2023 · N811UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2023051101456Seat Track · corrodedMAIN CABIN BETWEEN FR 16-12 L/H O/B FLOOR BEAM SIGNS OF CORRSION DOT 43-126 () REMOVED CORROSION ON FLOORBEAM Y765 AREA HARD POINT AND FOUND OU 51-42-11 ATTACH FORM 44-0008 EMP#: V936636 WORK ACCOMPLISHED AT T OF LIMITS IAW SRM 53-11-14-283-007 FID 011, L=1.22May 10, 2023 · N811UA · Airbus A319131 · Fuselage, Seat/Cargo Attach FittingsSDR CALA2023051201466Floorbeam · corrodedMAIN CABIN BETWEEN FR 16-12 L/H O/B FLOOR BEAM SIGNS OF CORRSION DOT 43-126 () REMOVED CORROSION ON FLOORBEAM Y765 AREA HARD POINT AND FOUND OU 51-42-11 ATTACH FORM 44-0008 EMP#: V936636 WORK ACCOMPLISHED AT T OF LIMITS IAW SRM 53-11-14-283-007 FID 011, L=1.22May 10, 2023 · N811UA · Airbus A319131 · Fuselage Main, Floor BeamSDR CALA2023050801414Angle · crackedLH EMER. EXIT ESCAPE HATCH LH LOAD LIMITING FROFIL CRACKED AT FA STENER HOLES. REMOVED ANGLE LH EMER. EXIT ESCAPE HATCH, RECIVED NEW ANGLE, INS TALLED NEW ANGLE P/N D522290260451, BTCH 0004060884 IAW SRM 51-4 2-11 EMP: V934337 WC: 56340 STA: ST ENG BFMMay 8, 2023 · N811UA · Airbus A319131 · Emergency ExitsSDR CALA2022082902220None · noneG RSVR LO LVL DISPLAYED ON UPPER ECAM SCREEN. - HYD INSP AC FOUND GREEN SYSTEM HIGH PRESSURE MODULE LEAKING AT CHECK VALVE FITTING ON BOTTOM OF UNIT. SRVICED GREEN SYSTEM FLUID TO FULL. TURNED OFF PTU SWITCH AND TAGGED SAME DO NOT USE. REPLACED O-RING ON HP MAAug 29, 2022 · N811UA · Airbus A300* · Hydraulic System, MainSDR CALA2022050201115Frame · corrodedRH FR68 STR 23R-22R FWD FACE HAS CORROSION ON HAECO LCQ REF 9296 380/22380 SUPPORT TASK. NR GENERATED BY N078625 DEFECT ACCOMPLISHED REF LOG PAGES 8495768 AND 8495677 FOR THE CORROSION FOUND AT FR68 FWD FACE BETWEEN STR22R AND 23R LOCATED AROUND A PREVIOUS REPMay 1, 2022 · N811UA · Airbus A300* · Fuselage Structure (General)SDR CALA2022050201114Skin · bentR2 DOOR EXTERIOR SKIN AT LOWER END IS BENT ON HAECO LCQ REF 9296 034/22034 SPEC A3NB-52-3-6078. NR GENERATED BY V892442 -00-300-003. BENT SECTION MEASURED DEPTH .160 INCHES, LENGTH 3.3 SRI 52-10-00-205-022 INSPECTION THRESHOLD FROM TIME OF ADL/ INSPECTION AT IMay 1, 2022 · N811UA · Airbus A300* · Passenger/Crew DoorsSDR CALA2022042501062Door Sill · corrodedR2 DOOR SILL HAS CORROSION AT FR 68. GENERATED BY N078625 ON HAE CO LCQ NR 9296231/22231 REMOVED AND REPLACED R2 DOOR SILL IAW A319 SRM 53-41-14-80, SRM 53-41-14-285-002, SRM 51-42-11/001. ACMP BY MECH V077956 INSP BY N078625Apr 25, 2022 · N811UA · Airbus A319131 · Fuselage Structure (General)SDR CALA2022042101031Plate · crackedAFT CABIN LH AFT SHEAR WEB IS CRACKED AT FR69 ON HAECO LCQ REF 9 296239/22239 SPEC A3NB-53-3-6222. NR GENERATED BY N078625 REMOVED & REPLACED AFT CABIN SHEAT WEB AT FR69-70 IAW A319 SRM 5 1-72-11-911-001, 51-44-11/001, 51-46-11/001 AT HAECO LCQ ON HANG AR NR 9Apr 19, 2022 · N811UA · Airbus A319131 · Fuselage Structure (General)SDR CALA2022041801008Door Sill · corrodedL2 DOOR SILL HAS CORROSION AT FR68 ON HAECO LCQ REF 9296244/2224 4 SPEC A3NB-53-3-6222. NR GENERATED BY N078625 CUT OUT DAMAGED AREAS, FABRICATED FILLER & RECEIVED REPAIR ANGLE FOR REPAIR PRINCIPLE #5, INSTALLED REPAIR ANGLE & FILLER IAW A3 19 SRM 53-41-14-300Apr 17, 2022 · N811UA · Airbus A319131 · Fuselage Structure (General)SDR CALA2022030100542Rivet · missingPDA 3 PDA 3 FOR MISSING RIVETS AT FWD CARGO THRESHOLD AND ENG 2 PEN NIB FAIRING. REF LP 8076485 FOR 4 MISSING RIVEST AND ENG 2 PEN NIB FAITRING AND LP8076487 FOR 1 RIVET MISSING AT FWD CARGO THRESHOLD AREAMar 1, 2022 · N811UA · Airbus A319131 · Fuselage Structure (General)SDR CALA2021043000588Scanner · inoperativeWX RADAR INOPERATIVE, NO FAULTS FOUND ON PFR. HOWEVER CAPT TOOK A VIDEO SHOWING RADAR ONLY PAINTING FROM 10 TO 12 OCLOCK, CAPT ALSO REPORTED TILT FUNCTION WAS ERRACTIC AND HEARD SLAPPING NOISE FROM NOSE OF THE ACFT. REMOVED AND REPLACED SCANNER ASSY PEDESTALApr 30, 2021 · N811UA · Airbus A319131 · Weather Radar SystemSDR CALA2020040600789Intercostal · crackedR1 DOOR FRAME 16 STOP FITTING NO 1 INBOARD LOWER HOLE IS CRACKED IN THE WEB AND INTERCOSTAL PER HAECO LCQ NR LP 9290112 GENERATE D REPAIRED I/B LOWER HOLE AT R1 DOOR FR16 STOP FITTING #1 IAW A319 SRM 51-44-11 AND REPLACED INTERCOSTAL IAW A319 SRM 51-72-11-911-Apr 4, 2020 · N811UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2020033000740Intercostal · crackedL1 DOOR FRAME 16 STOP FITTING NO 7 INBOARD LOWR HOLE IS CRACKED IN THE INTERCOSTAL LAYER PER HAECO LCQ NR LP 9290111 GENERATED REMOVED AND REPLACED L1 DOOR FR16 DOOR STOP #7 INTERCOSTAL IAW A 319 SRM 51-72-11-911-001Mar 27, 2020 · N811UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2020033000739Intercostal · crackedR1 DOOR FRAME 16 STOP FITTING NO 7 INBOARD UPPER AND LOWER HOLE IS CRACKED IN THE INTERCOSTAL LAYER PER HAECO LCQ NR LP 9290113 GENERATED REMOVED AND REPLACED R1 DOOR FR16 #7 DOOR STOP INTERCOSTAL IAW A 319 SRM 51-72-11-911-001.Mar 27, 2020 · N811UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2016101795812Door Frame · corrodedAFT FUSE R2 DOOR CUTOUT FR68 AT STR 23R FRAME HAS CORROSION. CUTOUT DAMAGE & INSTALLED REPAIR IAW SRM53-41-12 FIG 202.Oct 14, 2016 · N811UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2016051895372Battery · faultyAFTER TAKEOFF THE CAPTAIN LOST MAP, TR1 IN AMBER WITH THE LOSS OF NAV1 & INTERMITTENT LOSS OF NAV SYS ON CAPTAINS SIDE. CREW REPORTS LOSING THE NR 1 BATTERY WITH VOLTAGE AT 23VDC & DECREASING. ON ARRIVAL NR 1 BATTERY VOLTAGE WAS IN AMBER WITH 95 AMP SHOWINGMay 15, 2016 · N811UA · Airbus A319131 · Battery/Charger SystemSDR CALA2015101594592Skin · saturatedLEFT ELEVATOR UPPER SKIN PANEL HAS TRAPPED WATER INDICATIONS IN 5 LOCATIONS. 73" FROM INBD & 8" FROM TE, 3" DIAMETER. 101" FROM INBD, 5" FROM TE, 5" DIAMETER. 204" FROM INBD, 5.5" FROM TE, 3" DIAMETER. 138" FROM INBD, 5" FROM TE, 3.5" DIAMETER. 189" FROM Oct 14, 2015 · N811UA · Airbus A319131 · Elevator, Plate/SkinSDR CALA2015101594590Skin · saturatedRIGHT ELEVATOR UPPER SURFACE HAS A TRAPPED WATER INDICATION 113" FROM INBD, 12" FROM TE, 6" DIAMETER & THE LOWER SURFACE 80" FROM INBD, 5" FROM TE, 2" DIAMETER. CARRIED FROM 12 15 14. CUT OUT TRAPPED WATER & APPLIED REPAIR CONFIG 1 & RESTORED FINISH IAW SRM Oct 14, 2015 · N811UA · Airbus A319131 · Elevator, Plate/SkinSDR CALA2015092594400Power Supply · faultedEMERGENCY LIGHT TEST FAULTS FWD LT EMER POWER SUPPLY UNIT. REPLACED BATTERY PACK & POWER SUPPLY IAW AMM 33-51-38.Sep 25, 2015 · N811UA · Airbus A319131 · Emergency LightingSDR CALA2015070694045Access Panel · damagedLEFT WING FUEL TANK ACCESS PANEL 540KB HAS TWO EACH ELONGATED HOLES, LOOKING UP & FWD ONE 11:00 & 4:00 POSITIONS. REPAIRED ACCESS PANEL LANDING AT 11:00 & 4:00. CLEANED UP HOLES & FABRICATED BUSHING & INSTALLED IAW SRM 57-21-11 FIG 202.Jul 4, 2015 · N811UA · Airbus A319131 · Wing, Plate/SkinSDR CALA2015070694039Door · malfunctionedCABIN PSU'S AT LOCATIONS DOOR 1R, DOOR 2L, SEATS 7ABC, 11DEF, 23DEF, 34DEF, 35ABC & LAVATORY D, ACCT. PSU DOORS DID NOT DROP WHILE ACCOMPLISHING THE OPERATIONAL CHECK OF MANUAL MASK RELEASE IAW AMM 35-23-00-710-00 1-A. WHILE ACCOMPLISHING COA 409421 & EA 352Jul 2, 2015 · N811UA · Airbus A319131 · Passenger Oxygen SystemSDR CALA2015063094036Access Panel · damagedLEFT WING FUEL TANK ACCESS PANEL 540KB HAS 2 EACH ELONGATED HOLES, LOOKING UP & FWD ONE 11:00 & 4:00 POSITIONS, 12 15 2014 DEFERRAL. REPAIRED ACCESS PANEL LANDING AT 11:00 & 4:00. CLEANED UP HOLES & FABRICATED BUSHING & INSTALLED IAW SRM 57-21-11 FIG 202.Jun 29, 2015 · N811UA · Airbus A319131 · Wing, Plate/SkinSDR CALA2015012393011Warning System · activatedON TAKEOFF ROLL GOT HOT BRAKE ECAM. ABORTED TAKEOFF AT 80 KTS. NR 1 INDICATED 490 DEGREES, NR 2 440, 390 & 490 DEGREES. ACFT NEVER MET 800 DEGREES & NO FUSE PLUGS MELTED SO OVERHEAT INSPECTION REQUIRED IAW AMM 05-51-16 NOT REQUIRED. CHECKED IAW TSM 32-42-0Jan 20, 2015 · N811UA · Airbus A319131 · Landing Gear Brake SystemSDR CALA2014122392851Skin · damagedLEFT WING FUEL TANK ACCESS PANEL 540K B HAS 3 EACH ELONGATED HOLES AT 4:00, 7:00 &11:00 POSITIONS. REWORKED & REPAIRED LANDING IAW ECRA 5720-02626. ACCOMPLISH INITIAL REQUIREMENTS IAW PART 2 OF ECRA BEFORE ACFT REACHES 85800T OR 4290 0C WHICHEVER COMES FIRSTDec 15, 2014 · N811UA · Airbus A319131 · Wing, Plate/SkinSDR CALA2014122392850Skin · damagedRIGHT ELEVATOR UPPER SURFACE HAS A TRAPPED WATER INDICATION. 113 INCHES FROM INBD, 12 INCHES FROM TE & 6 INCHES IN DIAMETER & THE LOWER SURFACE 80 INCHES FROM INBD, 5 INCHES FROM TE & 2 INCHES IN DIAMETER. CUT OUT TRAPPED WATER & APPLIED REPAIR CONFIG 1 & REDec 15, 2014 · N811UA · Airbus A319131 · Elevator, Plate/SkinSDR CALA2014122392846Door Frame · corrodedAFT FUSE R2 DOOR CUT OUT FRAME 68 AT STRINGER 23R FRAME HAS CORROSION. CUT OUT DAMAGE & INSTALLED REPAIR IAW SRM 53-41-12 FIG 202. CATEGORY B REPAIR SRI 53-41-12-2-002-00 REQUIRES FIRST INSPECTION AT 64000C AFTER ACFT DELIVERY. CURRENT 22528C, FIRST INSPECTDec 14, 2014 · N811UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2014122392845Shear Plate · corrodedRIGHT AFT SHEAR PLATE HAS CORROSION. REMOVED & INSTALLED NEW SHEAR PLATE & FRAME SUPPORT IAW SRM 51-42-11 PG 7, 23, 24 & 30 - 32 & 46 - 48.Dec 14, 2014 · N811UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2014122392844Door Sill · corrodedR2 DOOR SILL HAS CORROSION FRAME 66 - 68. R & R NEW DOOR SILL IAW SRM 51-42-11 PARA 5, 6, & 8.Dec 14, 2014 · N811UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2014122392843Skin Panel · damagedLEFT ELEVATOR UPPER SKIN PANEL HAS TRAPPED WATER INDICATIONS IN 5 LOCATIONS. 1. 73 INCHES FROM INBD, 8 INCHES FROM TE & 3 INCHES IN DIAMETER. 2. 101 INCHES FROM INBD, 5 INCHES FROM TE & 5 INCHES IN DIAMETER. 3. 204 INCHES FROM INBD, 5.5 INCHES FROM TE & Dec 13, 2014 · N811UA · Airbus A319131 · Elevator, Plate/SkinSDR CALA2014120992799Door Sill · corrodedL2 DOOR SILL HAS CORROSION AT FRAME 68. INSTALLED REPAIR IAW SRM 53-41-14 FIG 201 SHEET 3 PRINCIPLE 4.Dec 8, 2014 · N811UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2013112193148Warning System · activatedENG ANTI ICE MESSAGE ON UPPER ECAM.Nov 20, 2013 · N811UA · Airbus A319131 · Central WarningSDR CALA2013092591437Antenna · defectiveALL AIRBORNE FREQUENCY INOPERATIVE ON COM 1. REPLACED UPPER NR 1 VHF ANTENNA IAW AMM. TESTED GOOD.Sep 19, 2013 · N811UA · Airbus A319131 · VHF Communications SystemSDR CALA2013091091178Light · inoperativeCEILING LIGHT AT SEAT ROW 22RT INOPERATIVE. RELAMPED, OPERATIONS CHECKED GOOD.Sep 7, 2013 · N811UA · Airbus A319131 · Passenger Compartment LightingSDR CALA2013082690761Controller · faultyCABIN PRESSURE CONTROLLER ONE, SYSTEM 1 FAULT. ITEM ROLLED FORWARD. REMOVED & REPLACED CABIN PRESSURE CONTROLLER ONE IAW AMM. TESTED IAW AMM.Aug 25, 2013 · N811UA · Airbus A319131 · Cabin Pressure ControllerSDR CALA2013081490440Extinguisher · unsecureF/A REPORTS AFT GALLEY HALON FIRE EXTINGUISHER PIN UNSECURE. RESEALED AND SECURED EXTINGUISHER.Aug 13, 2013 · N811UA · Airbus A319131 · Fire Bottle, PortableSDR UALA2013070104569Fastener · looseDURING WALK AROUND, FOUND FASTENER LOOSE ON ACFT BELLY TWO FT BEHIND ANTI COLLISION BEACON. REPLACED FASTENER IAW AMM.Jun 28, 2013 · N811UA · Airbus A319131 · Fuselage Miscellaneous Structure
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