# Service difficulty reports: N806UA

A list on [N806UA](https://openairdocs.org/aircraft/N806UA.md).

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

Page 1 of 3 · 121 reports

- [SDR CALA2026020213485](https://openairdocs.org/sdr/CALA2026020213485.md): Drain · missing · Jan 29, 2026 · N806UA · Airbus A319131 · Nacelle/Pylon, Main Frame
  > ON WALK AROUND, FOUND NR 2 ENGINE AFT PYLON CLAMP BLOCK MISSING WITH DAMAGE TO AFT LOWER PYLON LINE & SUPPORT ASSY INSPECTED NR 2 ENGINE AFT PYLON AND FOUND CLAMP BLOCK, SEVERE CHAFING TO LOWER PYLON DRAIN LINE & ELONGNATED DAMAGED TO SUPPORT ASSY. REF IPC 54
- [SDR CALA2025081107548](https://openairdocs.org/sdr/CALA2025081107548.md): Hydraulic Line · leaking · Aug 11, 2025 · N806UA · Airbus A319131 · Hydraulic System, Main
  > HYD SYSTEM G RESERVOIR LOW LEVEL. PILOTS VERBALLY REPORTED THE SYSTEM WENT TO ZERO. THEY FOLLOWED PROTOCOL AND TURNED OFF THE NR 1 ENGINE PUMP & ISOLATED THE SYSTEM. SERVICED GREEN HYD SYS IAW AMM 12-12-29. PRESSURIZED ELECTRIC PUMP & MOVED GREEN RELATED SY
- [SDR CALA2025040903663](https://openairdocs.org/sdr/CALA2025040903663.md): Unknown · fumes · Apr 6, 2025 · N806UA · Airbus A319131 · Air Distribution System
  > FA REPORTS NOXIOUSFUMES IN AFT GALLEYAFTER SELECTING APUBLEED ON CREW REPORTS NO ODOR OR SMOKE OR FUME IS PRESENT. NO SMOKE OR FUME OR ORDER PRESENT AT THIS TIME. WAS NOT ABLE TO DUPLICATE FAULT AT THIS TIME AMM 05-50-00-810-831-A. SMOKE/ODOR REPORT SHEET WAS
- [SDR CALA2025013000244](https://openairdocs.org/sdr/CALA2025013000244.md): Frame · cracked · Jan 25, 2025 · N806UA · Airbus A319131 · Fuselage Main, Frame
  > RH FRAME 68 AT STR 8 HAS CRACK INDICATION ABOVE TOP FASTENER IN FRAME JUST BELOW STR 8 CRACK APPROX.150 INCH LONG. REPAIR PART PER PART 2 OF THE LATEST REVISION OF ECRA 5341-01471 CYCLES. PERFORM REPEAT INSPECTIONS AT INTERVALS NOT TO EXCEED ON OR BEFORE THE
- [SDR CALA2025012700221](https://openairdocs.org/sdr/CALA2025012700221.md): Frame · cracked · Jan 22, 2025 · N806UA · Airbus A319131 · Fuselage Main, Frame
  > "REPAIR BEFORE NEXT FLIGHT" LEFT FRAME 16 DOUBLER JOGGLE HOLE LE TTER "C" HAS CRACK INDICATION IN THE FRAME LAYER AT THE 3:0 CLOC K POSITION 100% S.H.. GENERATED BY V062335 ON HAECO LCQ NR 92983 32 / 26332 IAW SRM 51-73-12/001. REPETITIVE INSPECTIONS REQUIRED
- [SDR CALA2025012700220](https://openairdocs.org/sdr/CALA2025012700220.md): Frame · cracked · Jan 22, 2025 · N806UA · Airbus A319131 · Fuselage Main, Frame
  > "REPAIR BEFORE NEXT FLIGHT" RIGHT FRAME 16 DOUBLER JOGGLE HOLE L ETTER "C" HAS A CRACK INDICATION IN THE FRAME LAYER AT THE 9:0 C LOCK POSITION 100% S.H.. IAW SRM 51-73-12/001. REPETITIVE INSPECTIONS REQUIRED PER SRI AND SUBSEQUENT INSPECTIONS AT 5900 FLIGHT
- [SDR CALA2025012700222](https://openairdocs.org/sdr/CALA2025012700222.md): Frame · cracked · Jan 21, 2025 · N806UA · Airbus A319131 · Fuselage Main, Frame
  > LEFT FRAME 16 DOUBLER JOGGLE HOLE LETTER ''A'' HAS CRACK INDICATIO N IN THE FRAME LAYER AT THE 3 OCLOCK POSITION 100% S.H. SRI 53-11-12-205-008 AT 6800 FLIGHT CYCLES SINCE REPAIR FLIGHT HOURS ARE NOT RELEVANT FOR THESE REPETITIVE INSPECTIONS. EMBODIMENT AND S
- [SDR CALA2025012300187](https://openairdocs.org/sdr/CALA2025012300187.md): Frame · cracked · Jan 21, 2025 · N806UA · Airbus A319131 · Fuselage Main, Frame
  > LEFT FRAME 16 DOUBLER JOGGLE HOLE #7 HAS A CRACK INDICATION IN T HE FRAME LAYER AT THE 3 OCLOCK POSITION 100%
- [SDR CALA2024110401001](https://openairdocs.org/sdr/CALA2024110401001.md): Wire · damaged · Nov 2, 2024 · N806UA · Airbus A319131 · Light System Wiring
  > SEAT 3AB EMERGENCY PATHWAY LIGHT INOP FOUND AND REPAIRED CUT WIRES REF A319 ESPM 20-43-11 EMERGENCY LIGHTS OPS CHK NORMAL REF A319 AMM 33-51-00
- [SDR CALA2024101100814](https://openairdocs.org/sdr/CALA2024101100814.md): Eec · faulted · Oct 10, 2024 · N806UA · Airbus A319131 · Fuel Controlling System
  > FADEC FAULT DISPLAYED ON UPPER ECAM SCREEN. ENGINE FAIL CONFIRM ED ENGINE SHUTDOWN. - ENG 1 REF LP 9512804 FOR WORK PERFORMED. INSTALLED NEW EEC. ALL TESTS GOOD E1 ESN V10546 - PLEASE R&R THE EEC PER AMM TASK 73-22-34/401 CONFIG 13. FOR THE REMOVED EEC, PLEASE
- [SDR CALA2023120803587](https://openairdocs.org/sdr/CALA2023120803587.md): Control Panel · inoperative · Dec 6, 2023 · N806UA · Airbus A319131 · Communications System
  > CREW REPORTED WATER SPILLED ONTO THE F/O''S SIDE RADIO MNGMNT PANEL AN AUDIO CONTROL PANEL CAUSING ALL 3 VHF COMM RADIO FREQUENCY DISPLAYS TO GO BLANK. C/B''S ON 49VU; G7, G9 121VU; L2, L4, L5, L6, L7, OPENED AND TAG FOR MAINTENANCE PERFORMED TSM 23-13-00-810-
- [SDR CALA2023080702432](https://openairdocs.org/sdr/CALA2023080702432.md): Panel · damaged · Aug 4, 2023 · N806UA · Airbus A319131 · Nacelle/Pylon Structure
  > PDA 2 REF LOG PAGE 5354332, AND ECRA 5450-02357, THE AIRCRAFT ARRIVED WITH PANEL 110 MISSING. MISSING PANEL PLACED ON DIP FOR 25 FLT HOURS. MISSING FLEX SEAL PANEL 110 HAS BEEN PLACED ON DIP. REMOVED AND REPLACED CRACKED METAL SEAL PANEL. NO FURTHER DEFECTS N
- [SDR CALA2022080801994](https://openairdocs.org/sdr/CALA2022080801994.md): Fuel Cap · missing · Aug 4, 2022 · N806UA · Airbus A300* · Aircraft Fuel System
  > THIS IS A SUPPLEMENTAL REPORT FOR THE SAME CONTROL NUMBER SUBMITTED ON 8/08/22. FUEL CAP MISSING FROM ACFT. PLACING FUELING CAP ON CDL. REPLACED FUEL CAP.
- [SDR CALA2022060201423](https://openairdocs.org/sdr/CALA2022060201423.md): Keelbeam · elongated · Jun 2, 2022 · N806UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > DURING ACCOMPLISHMENT OF FCD5330-05575 FOR KEEL BEAM RH MLG DOOR ACTUATOR FITTINGS, MULTIPLE FASTENER HOLES WERE FOUND OUT OF ROUND AND ELONGATED HOLES, ON HAECO NR 9294831 BY V061680. S WERE FOUND DAMAGED. ECRA 5330-06947 GENERATED TO REPAIR. ACCO EQUIRED TO
- [SDR CALA2022060201419](https://openairdocs.org/sdr/CALA2022060201419.md): Fitting · elongated · Jun 1, 2022 · N806UA · Airbus A319131 · Fuselage Main, Frame
  > LMLG KEEL BEAM FWD ACTUATOR HINGE FITTING FWD AND AFT REINFORCEM ENT ANGELS HAVE ELONGATED HOLES TOOL MARKS PER HAECO LCQ NON ROU TINE 9294832/36832 GENERATED BY V061680 THIS ITEM CARRIED VIA LP8715411 SEE FOR REPAIR INFORMATION. THIS ITEM OK TO CLEAR
- [SDR CALA2022060201418](https://openairdocs.org/sdr/CALA2022060201418.md): Fitting · elongated · Jun 1, 2022 · N806UA · Airbus A319131 · Fuselage Main, Frame
  > DURING INSPECTION OF KEEL BEAM LMLG DOOR ACTUATOR FITTING MULTIP LE FASTENER HOLES WERE FOUND OUT-OF-ROUND FCD 5330-05575 PER HAE CO LCQ NON ROUTINE 9294809/36809 GENERATED BY V061680 PART 1 OF ECRA5330-06946 AND REO L23767. DIP REQUIRED TO HOLES PER PART 3 OF
- [SDR CALA2022060101412](https://openairdocs.org/sdr/CALA2022060101412.md): Fitting · cracked · May 31, 2022 · N806UA · Airbus A319131 · Landing Gear Door Actuator
  > LEFT MLG DOOR ACTUATOR FITTING LWR OTBD FWD HOLE HAS CRACK INDICATION MARKED DOT 01-L AD 2015-02-14 PER HAECO LCQ NON ROUTINE 92 94677/36677 GENERATED BY V909079 THIS ITEM CARRIED VIA LP8715411 SEE FOR REPAIR INFORMATION. THIS ITEM OK TO CLEAR.
- [SDR CALA2022060101411](https://openairdocs.org/sdr/CALA2022060101411.md): Frame · corroded · May 31, 2022 · N806UA · Airbus A319131 · Fuselage Main, Frame
  > R/H FR68 FWD FACE APPROX. 1 INCH ABOVE DOOR SILL HAS CORROSION A ROUND FASTENER HOLE. PER HAECO LCQ NON ROUTINE 9294729/36729 GEN ERATED BY V077960 THE RH FR68 STR22-24 REPAIR IN THE AREA OF THE ANCHOR NUT PER TTL FC. ACCOMPLISH REPEAT INSP AT INTERVALS NOT TO
- [SDR CALA2022060101407](https://openairdocs.org/sdr/CALA2022060101407.md): Skin · gouged · May 30, 2022 · N806UA · Airbus A319131 · Wing, Control Surfaces
  > LH WING L/E #5 SLAT AND #12 TRACK CAVITY UPPER SKIN GOUGE PER HA ECO LCQ NON ROUTINE 9294591/36591 GENERATED BY V061682 REPAIRED LH WING #5 SLAT AND #12 SLAT TRACK CAVITY UPPER 11-300- 037 FIG 001 SHEET 03 REPAIRED TOPCOAT IAW SRM 51-75-12-911-002
- [SDR CALA2022060101406](https://openairdocs.org/sdr/CALA2022060101406.md): Skin · gouged · May 30, 2022 · N806UA · Airbus A319131 · Wing, Control Surfaces
  > LH WING #1 SLAT AND #2 TRACK CAVITY UPPER SKIN LOWER SIDE IS GOU GE AT BOTH SIDES PER HAECO LCQ NON ROUTINE 9294583/36583 GENERAT ED BY V061682 REPAIRED LH WING #1 SLAT AND #2 SLAT TRACK CAVITY UPPER SKIN IAW SRM 57-41-11-300-037 FIG 001 SHEET 03 REPAIRED TOP
- [SDR CALA2022060101405](https://openairdocs.org/sdr/CALA2022060101405.md): Skin · gouged · May 30, 2022 · N806UA · Airbus A319131 · Wing, Control Surfaces
  > LH WING #1 SLAT AND #1 TRACK CAVITY UPPER SKIN LOWER SIDE IS GOUGE AT BOTH SIDE PER HAECO LCQ NON ROUTINE 9294584/36584 GENERATE D BY V061682 REPAIRED LH WING #1 SLAT AND #1 SLAT TRACK CAVITY UPPER SKIN IAW SRM 57-41-11-300-037 FIG 001 SHEET 03 REPAIRED TOPCOA
- [SDR CALA2022053001383](https://openairdocs.org/sdr/CALA2022053001383.md): Frame · cracked · May 28, 2022 · N806UA · Airbus A319131 · Fuselage Main, Frame
  > RH FR 68 AT STR 22 FLANGE HAS CRACK INDICATION IN RADIUS PER HAE CO LCQ NON ROUTINE 9294407/36407 GENERATED BY V892444 68 STR 22-24 REPAIR PER PART2 ITEM 1&4 OF LATEST REV OF ECRA5341 T TO EXCEED19700FC THEREAFTER. ACCOMPLISH INITIAL INSP OF RH FR REV OF ECRA
- [SDR CALA2022052701365](https://openairdocs.org/sdr/CALA2022052701365.md): Frame · cracked · May 26, 2022 · N806UA · Airbus A319131 · Fuselage Structure (General)
  > FR68 STR 22 LH FRAME HAS CRACK INDICATION IN RADIUS OF STR22 FLA NGE. GEN BY V892444 PER NR9294428/36428 9 FOR REF. ON HAECO LP 9294428 WITH NO DEVIATIONS ON THE FR68 ST EPAIR ON THE LH FR68 STR22LH FRAME INNER WEB PER PART 3 OF THE L R22LH FRAME INNER WEB/STI
- [SDR CALA2022052701364](https://openairdocs.org/sdr/CALA2022052701364.md): Stringer · corroded · May 26, 2022 · N806UA · Airbus A319131 · Fuselage Main, Longeron/Stringer
  > AFT CARGO STRINGER 25RT CORRODED FR64-65 A3NB-53-3-6185 PER HAEC O LCQ NON ROUTINE 9294916/36916 GENERATED BY V892285 FOUND AFT CARGO STRINGER 25RT TO HAVE 50% MATERIAL LOSS FOUND TO BE OUT OF LIMITS IAW A319 SRM 53-00-13-300-002 REMOVED AND REPL ACED STRINGER
- [SDR CALA2022052701363](https://openairdocs.org/sdr/CALA2022052701363.md): Stringer · corroded · May 26, 2022 · N806UA · Airbus A319131 · Fuselage Main, Longeron/Stringer
  > AFT CARGO STRINGER 26RT CORRODED FR64-65 A3NB-53-3-6185 PER HAEC O LCQ NON ROUTINE 9294917/36917 GENERATED BY V892285 FOUND AFT CARGO STRINER 26RT TO HAVE 50% MATERIAL LOSS FOUND TO BE OUT OF LIMITS IAW A319 SRM 53-00-13-300-002 REMOVED AND REPLA CED STRINGER
- [SDR CALA2022052301321](https://openairdocs.org/sdr/CALA2022052301321.md): Frame · cracked · May 23, 2022 · N806UA · Airbus A319131 · Fuselage Structure (General)
  > FR68 STR 22 LH FRAME HAS CRACK INDICATION IN RADIUS OF STR22 FLA NGE. GEN BY V892444 PER NR9294428/36428 9 FOR REF. ON HAECO LP 9294428 WITH NO DEVIATIONS ON THE FR68 ST EPAIR ON THE LH FR68 STR22LH FRAME INNER WEB PER PART 3 OF THE L R22LH FRAME INNER WEB/STI
- [SDR CALA2022052001290](https://openairdocs.org/sdr/CALA2022052001290.md): None · corroded · May 18, 2022 · N806UA · Airbus A319131 · Fuselage Structure (General)
  > AFT CABIN R2 DOOR LOWER CORNERS HAS CORROSION AT FR66 AND FR68 A 3NB-53-3-6299 PER HAECO LCQ N/R 9294539/36539 GEN BY V061771 RMVD AND RPLD AFT CABIN R2 DOOR SILL AT FR66-68 IAW A319 SRM 51- 42-11/001 AND SRM 53-41-14-283-002 REPAIRED FINAL TOPCOAT IAW SR M 51
- [SDR CALA2022050901181](https://openairdocs.org/sdr/CALA2022050901181.md): Door · corroded · May 8, 2022 · N806UA · Airbus A319131 · Passenger/Crew Doors
  > AFT CABIN L2 DOOR LOWER CORNERS HAS CORROSION AT FR66 AND FR68 A 3NB-53-3-6299 PER HAECO LCQ NON ROUTINE 9294538/36538 GENERATED BY V061771 BLENDED CORROSIO AT FR66 & 68 DOOR SILL IAW A319 SRM 51-74-00/00 1 FR66 REPAIRED IAW A319 SRM 53-41-14-300-001 PRINCIPLE
- [SDR CALA2022050401128](https://openairdocs.org/sdr/CALA2022050401128.md): None · corroded · May 3, 2022 · N806UA · Airbus A319131 · Fuselage Structure (General)
  > AFT CARGO FR65 STGR31R CORRODED A3NB-53-3-6185 PER HAECO LCQ NON ROUTINE 9294833/36833 GENERATED BY V061629
- [SDR CALA2022042501054](https://openairdocs.org/sdr/CALA2022042501054.md): None · corroded · Apr 21, 2022 · N806UA · Airbus A319131 · Fuselage Structure (General)
  > AFT CARGO COMPARTMENT, FS59-60 STR33R, STRINGER HAS CORROSION FS 59-60, STR 33R PER HAECO LCQ NON ROUTINE 9294458/36458 GENERATED BY V917055 REMOVED CORROSION ON STRINGER 33R F559-60 AFT CARGO. FOUND TO BE PERFOREMD BY V932428 INSP BY V061704. OUT OF LIMITS IA
- [SDR CALA2022042101040](https://openairdocs.org/sdr/CALA2022042101040.md): Skin · none · Apr 20, 2022 · N806UA · Airbus A319131 · Elevator, Spar/Rib
  > R/H ELEVATOR SHOWS POSSABLE LIQUID INGRESS ON UPPER SURFACE AT 1 4 1/2 IN FROM I/B EDGE, 11 1-2 IN FROM TRAILING EDGE APPROX. 2 I N AROUND PER HAECO LCQ NON ROUTINE 9294439/36439 GENERATED BY V0 61632
- [SDR CALA2022041801005](https://openairdocs.org/sdr/CALA2022041801005.md): Attach Bracket · discovered · Apr 15, 2022 · N806UA · Airbus A319131 · Emergency Exits
  > R/H EMER. EXIT INTERIOR STRUCTURE LOWER FRAME ATTACH BRACKET HAS START DRILL PER HAECO LCQ NON ROUTINE 9294730/36730 GENERATED B Y V077960 REMOVED AND REPLACED RH EMERGENCY EXIT LOWER FRAME IAW SRM 51-42 -11 PERFORMED BY V917067 SUERVISOR V935356 INSP BY V0779
- [SDR CALA2022041801006](https://openairdocs.org/sdr/CALA2022041801006.md): Attach Bracket · misrepaired · Apr 15, 2022 · N806UA · Airbus A319131 · Emergency Exits
  > L/H EMER. EXIT INTERIOR STRUCTURE LOWER FRAME ATTACH BRACKET HAS START DRILL PER HAECO LCQ NON ROUTINE 9294731/36731 GENERATED B Y V077960 REMOVED AND REPLACED LH EMERGENCY DOWN LOWER FRAME IAW SRM 51-42 -11 PERFORMED BY V917067 SUPERVISOR V935356 INSP BY V077
- [SDR CALA2022041400978](https://openairdocs.org/sdr/CALA2022041400978.md): Stringer · corroded · Apr 12, 2022 · N806UA · Airbus A319131 · Fuselage Main, Structure
  > AFT CARGO COMP. STR38R IS CORRODED BETWEEN FR59 AND FR60. GENERA TED BY V061690 ON HAECO LCQ NR 9294386/36386 REMOVED CORROSION AFT CARGO COMP. STR38R BETWEEN FR59 AND FR60 F OUND TO BE OUT OF LIMITS IAW A319 SRM 53-41-13-283-002 REMOVED A ND REPLACED STRINGER
- [SDR CALA2022041400977](https://openairdocs.org/sdr/CALA2022041400977.md): Stringer · corroded · Apr 12, 2022 · N806UA · Airbus A319131 · Fuselage Main, Structure
  > AFT CARGO COMP. STR37R IS CORRODED BETWEEN FR59 AND FR61. GENERA TED BY V061690 ON HAECO LCQ NR 9294385/36385 REMOVED CORROSION AFT CARGO COMP. STR37R BETWEEN FR59 AND FR61 F OUND TO BE OUT OF LIMITS IAW A319 SRM 53-41-13 REMOVED AND REPLA CED STRINGER IAW A31
- [SDR CALA2022033100820](https://openairdocs.org/sdr/CALA2022033100820.md): None · none · Mar 28, 2022 · N806UA · Airbus A319131 · Emergency Exits
  > L/H EMERGENCY EXIT INTERIOR STRUCTURE LOWER FRAME ATTACH BRACKE HAS CORROSION A3NB-05-3-6168 PER HAECO LCQ NON ROUTINE 9294304/3 6304 GENERATED BY V077960 REMOVED AND REPLACED LH EMERGENCY EXIT INTERIOR STRUCTURES LOWER FRAME ATTACH BRACKET IAW SRM 51-42-11 AC
- [SDR CALA2022033100818](https://openairdocs.org/sdr/CALA2022033100818.md): None · cracked · Mar 28, 2022 · N806UA · Airbus A319131 · Emergency Exits
  > RIGHT EMEERGENCY EXIT FWD VERTICAL FRAME CRACKED A3NB-52-4-6032 PER HAECO LCQ NON ROUTINE 9294319/36319 GENERATED BY V892285 REMOVED AND REPLACED RT EMERGENCY DOOR VERTICAL FRAME IAW SRM 51 -42-11 ACMP BY MECH V935356 INSP BY V061629
- [SDR CALA2022033100819](https://openairdocs.org/sdr/CALA2022033100819.md): Angle · none · Mar 28, 2022 · N806UA · Airbus A300* · Emergency Exits
  > R/H EMERGENCY EXIT INTERIOR STRUCTURE LOWER FRAME ATTACH BRACKET S 2EA HAVE CORROSION A3NB-05-3-6168 PER HAECO LCQ NON ROUTINE 92 94303/36303 GENERATED BY V077960 REMOVED AND REPLACED 2EA EXIT INTERIOR DOOR LOWER FRAME BRACKETS IAW SRM 51-42-11 ACMP BY MECH V9
- [SDR CALA2018091901953](https://openairdocs.org/sdr/CALA2018091901953.md): Solenoid · inoperative · Sep 16, 2018 · N806UA · Airbus A319131 · Passenger Oxygen System
  > O2 CONTAINER ABOVE R2 DOOR, DIDN'T OPEN DURING DROP TEST. R&R SOLENOID IN O2 CONTAINER IAW CMM35-21-12 PAGE 3008 & 7002. OP CHECK GOOD ON TC17-3351-1-7907.
- [SDR CALA2018091701946](https://openairdocs.org/sdr/CALA2018091701946.md): Stiffener · cracked · Sep 16, 2018 · N806UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > LT WINDSHIELD SIDE POST AT FR 4 LOWER ATTACHMENT, AFT LOWER WEB HAS CRACK INDICATION. ACCOMPLISHED INTERIM REPAIR PART 1 STEPS 1-7 ON LT VERTICAL STIFFENER SIDE POST OF FR 4 WINDSHIELD IAW ECRA 53-02006.
- [SDR CALA2018091701942](https://openairdocs.org/sdr/CALA2018091701942.md): Solenoid · defective · Sep 16, 2018 · N806UA · Airbus A319131 · Passenger Oxygen System
  > O2 CONTAINER ABOVE R2 DOOR, DIDN'T OPEN DURING DROP TEST. R&R SOLENOID IN O2 CONTAINER IAW CMM35-21-12 PAGE 3008 & 7002. OP CHECK GOOD ON TC17-3351-1-7907.
- [SDR CALA2018091701944](https://openairdocs.org/sdr/CALA2018091701944.md): Oxygen Box · failed · Sep 16, 2018 · N806UA · Airbus A319131 · Passenger Oxygen System
  > O2 CONTAINER ABOVE L2 DOOR FAILED TO OPEN DURING DROP TEST REMOVED O2 CONTAINER ABOVE L2 DOOR IAW AMM 35-21-41-000-001 -A. INSTALLED NEW O2 CONTAINER IAW AMM 35-21-41-400-001-A OPS CHECK GOOD. VARIFIED O2 CONTAINER IS ARMED.
- [SDR CALA2017093003356](https://openairdocs.org/sdr/CALA2017093003356.md): Battery · failed · Sep 30, 2017 · N806UA · Airbus A319131 · Emergency Lighting
  > DURING EMERGENCY LIGHT TEST, AFT AND RIGHT SIDE POWER SUPPLY UNIT BATTERIES, FOUND FAILED. REPLACED BOTH POWER SUPPLY UNIT BATTERIES PER AMM 33-51-38, TEST GOOD.
- [SDR CALA2017090102962](https://openairdocs.org/sdr/CALA2017090102962.md): Unknown · odor · Sep 1, 2017 · N806UA · Airbus A319131 · Air Distribution System
  > MUSTY/FOUL ODOR FROM AIR CONDITIONING SYSTEM. PERFORMED AN OPERATIONAL TEST OF BLEED AND PACK SYS IAW AMM 21-00-0 0. NO ODOR EMINATING FROM AIR SYS. OTBD CREW WILL ATTEMPT TO ISOLATE COMPONENT IF ODOR RETURNS. OK TO CONTINUE.
- [SDR CALA2017082802923](https://openairdocs.org/sdr/CALA2017082802923.md): Ecs · odor · Aug 28, 2017 · N806UA · Airbus A319131 · Air Distribution System
  > FOUL/MUSTY SMELL FROM A/C SYSTEM PERFORMED CLEANING OF ECS WITH PACKS ON HOT FOR 45 MINUTES. NO ODORS DETECTED. CKS OK ON COLD AS WELL. PER AMM 21-00-00-615-001 -A
- [SDR CALA2017063002058](https://openairdocs.org/sdr/CALA2017063002058.md): Power Supply · failed · Jun 30, 2017 · N806UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY LIGHTS TEST FAILED FWD LT EPSU MESSAGE. REPLACED FWD LEFT EMERGENCY POWER SUPPLY UNIT IAW AMM 33-50-00 AND BATTERY. OPS CHECKED GOOD. TEST PASSED.
- [SDR CALA2017040400805](https://openairdocs.org/sdr/CALA2017040400805.md): Unknown · odor · Apr 4, 2017 · N806UA · Airbus A319131 · Air Distribution System
  > STRANGE ODOR IN CABIN. SMELLS LIKE BURNT OIL OR RUBBER. GAVE FA A HEADACHE RAN BOTH PACKS, COULD NOT DUPLICATE SMELL, CHECK ENG AND HYDRAULIC FLUID LEVELS CHECKED GOOD. REPLACED BOTH RECIRCULATION FILTER S PER AMM 21-21-41-400-001-A.
- [SDR CALA2017011600115](https://openairdocs.org/sdr/CALA2017011600115.md): Valve · faulty · Jan 16, 2017 · N806UA · Airbus A319131 · Landing Gear Brake System
  > AFTER PUSHBACK WITH ENG1 RUNNING AND PARKING BRAKE ON. ALL BRAKE PRESS LOST AND ACCUM LOST TROUBLESHOT REF TSM 32-44-00-810-808-A TO STEP 4A (3)(A). NEED TO R&R ALTN BRK DISTR DUAL VALVE REF AMM 32-43-14-000-001-A REMOVED VALVE REF AMM 32-43-14-000-001-A COMPL
- [SDR CALA2017010900033](https://openairdocs.org/sdr/CALA2017010900033.md): Skin · corroded · Jan 8, 2017 · N806UA · Airbus A319131 · Aircraft Fuel Distribution System
  > CENTER WING TANK UPPER SKIN AT FWD OF FR43 RT O/B OF 1292 SEAT TRACKS C1 HAS CORROSION. INTERIM REPAIR ACCOMPLISHED PER ECRA5710-02585 PART 1. ACCOMPLISHED HFEC SURFACE SCAN IAW NTM 51-10-16. ACCOMPLISH INITIAL INSPECTIONS OF THE AFFECTED AREA PER PART 2 OF EC
- [SDR CALA2016120501033](https://openairdocs.org/sdr/CALA2016120501033.md): Epsu · faulty · Dec 5, 2016 · N806UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY LIGHT TEST FAULTED EPSU BATTERY EMER. REMOVED FAULTY EMER BATT AT RT O/W REF MM33-51-38. INSTALLED EPSU BATTERY REF MM 33-51-38-000. OP CHECK NORMAL

Next page: https://openairdocs.org/aircraft/N806UA/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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 = 'N806UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N806UA/reports

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