# Service difficulty reports: N820UA

A list on [N820UA](https://openairdocs.org/aircraft/N820UA.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 · 106 reports

- [SDR CALA2025092909388](https://openairdocs.org/sdr/CALA2025092909388.md): Lamp · no test · Sep 27, 2025 · N820UA · Airbus A319131 · Emergency Lighting
  > DURING CABIN EMERGENCY LIGHT TEST, EPSU EXT LOAD EMER R DISPLAYED ON PTP. REPLACED RIGHT SIDE AFT OVERWING EMERGENCY LIGHT FWD LAMP IAW AMM 33-51-15-400-001-A STEP 4.B(2), TEST PERFORMED IAW AMM 33-51-00-710-001A AND TEST OK.
- [SDR CALA2025053005124](https://openairdocs.org/sdr/CALA2025053005124.md): Fuel Cap · missing · May 28, 2025 · N820UA · Airbus A319131 · Fuel Storage
  > PRESSURE REFUEL CAP MISSING PER LOG PAGE 5001779 FOLLOWED 02-30-95 FOR PDA PROGRAM.5001779
- [SDR CALA2025051904789](https://openairdocs.org/sdr/CALA2025051904789.md): Fuel Cap · missing · May 18, 2025 · N820UA · Airbus A319131 · Fuel Storage
  > PDA 2 FOUND FUEL CAP MISSING ON WALKAROUND. UPDATE FOR SDR INFORMATION REQUESTING CDL FOR MISSING FUEL CAP. NO LEAKS NOTED. VERIFIED COUPLING SEAL INTEGRITY. PART NIS IN EWR DISPATCH DESK: 37 NAME: MF DATE: 18-MAY-25 APPROVED CDL FOR MISSING FUEL CAP. R
- [SDR CALA2024110400980](https://openairdocs.org/sdr/CALA2024110400980.md): Unknown · odor · Oct 30, 2024 · N820UA · Airbus A319131 · Air Distribution System
  > OIL SMELL AFTER BOTH ENGINES SHUT DOWN, REF PREVIOUS WRITE UP L/P 9709104. RAN BOTH ENGINES INDEPENDENTLY AND WITH ASSOCIATED PACKS, NO SMELLS NOTED DURING RUNNING OR SHUTDOWN, REF AMM 71-00-00-710-043-A AND TSM 05-50-00-810-831-A.
- [SDR CALA2024080100338](https://openairdocs.org/sdr/CALA2024080100338.md): Slide · faulty · Jul 30, 2024 · N820UA · Airbus A319131 · Escape Slide
  > REF LOG PAGE 8771606 SLIDE 1R DIDNT DEPLOYED AS INTENTED AFTER ACCIDENTAL ACTIVATION SLIDE REMOVED AND REPLACED AS CORRECTED IN LOG PAGE 8771606 NOW SLIDE IS IN NORMAL CONFIGURATION OK FOR SVC.REMOVED AND REPLACED SLIDE PACK ASSY PER AMM 25-62-44/401 OPS. CKS
- [SDR CALA2024011000074](https://openairdocs.org/sdr/CALA2024011000074.md): Stringer · corroded · Jan 8, 2024 · N820UA · Airbus A319131 · Fuselage Main, Longeron/Stringer
  > AFT CARGO, FR54-56 LH STR 43 5EA SPOTS OF PITTING CORROSION PER NR 9298400/32400. REPLACED SECTION OF STR 43 LT BETWEEN FRAMES 53-56 IAW SRM 53-41 -13-283 AND REO L24677.
- [SDR CALA2024010800067](https://openairdocs.org/sdr/CALA2024010800067.md): Floor Support · cracked · Jan 5, 2024 · N820UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > ACCOMPLISH INITIAL INSPECTION OF RH FR68 STRG 8 RH AFT CORNER FRAME VERTICAL FLANGE REPAIRED AREA PER PART 2A OF THE LATEST REVISION OF ECRA 5341-01425. ITIAL INSPECTION OF RH FR68 STRG 8 RH AFT CORNER FRAME VERTICAL ON OR BEFORE THE AIRCRAFT REACHES 55,609 T
- [SDR CALA2024010800066](https://openairdocs.org/sdr/CALA2024010800066.md): Frame · corroded · Jan 5, 2024 · N820UA · Airbus A319131 · Fuselage Main, Frame
  > ACCOMPLISH INITIAL INSPECTION OF THE RH FR68 INNER CAP JOINT TO GUSSET PLATES FROM STRG 10-16 RH, LATERAL FR68 JOINT TO UPPER FR68 FROM STRG 4-5 RH, AND FR68 WEB AT DOORSTOP FITTING ATTACHMENT HOLES PER PART 2B OF THE LATEST REVISION OF ECRA 5341-01425 FR68 FR
- [SDR CALA2024010800061](https://openairdocs.org/sdr/CALA2024010800061.md): Stringer · corroded · Jan 5, 2024 · N820UA · Airbus A319131 · Fuselage Main, Longeron/Stringer
  > AFT CARGO, FR. 53-60 R/H STR. 42 AND CORRESPONDING SKIN MULTIPLE SPOTS OF PITTING. GEN BY V920443 PER HAECO LCQ NR 9298404/32404 REMOVED AND REPLACED SECTION OF STRINGER 42 RT BETWEEN FR52-53 T FITTING SUPPORT FRAME 57L IAW A319 SRM 51-42-11 P 15-21, ACCOMPL O
- [SDR CALA2023122603723](https://openairdocs.org/sdr/CALA2023122603723.md): Door Sill · corroded · Dec 22, 2023 · N820UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > R2 DOOR FR68 CORNER SHAPE SILL HAS CORROSION. REMOVED AND REPLACED CORRODED R2 DOOR FR68 CORNER SHAPE SILL IAW A319 SRM 51-72-11-911-001,SRM 53-41-79-283-002.
- [SDR CALA2023122203719](https://openairdocs.org/sdr/CALA2023122203719.md): Door Sill · mislocated · Dec 21, 2023 · N820UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > MAIN CABIN BELOW R2 DOOR SILL AT FRAME 67RT LOWER FRAME SEGMENT MISLOCATED PER NR 9299042/33042 GEN BY V052030. REMOVED AND REPLACED MISLOCATED LOWER FRAME SEGMENT 67RT BELOW R 2 DOOR SILL IAW SRM 53-41-12-75A AND SRM 51-72-11-911-00 MECH V9 14232 INSP BY V077
- [SDR CALA2023122203718](https://openairdocs.org/sdr/CALA2023122203718.md): Door Sill · mislocated · Dec 21, 2023 · N820UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > R2 DOOR SILL MISLOCATED. RECEIVE AND LOCATE (DRILL UP) NEW DOOR SILL PER NR9299046/33046. RMVD AND RPLD DRILLED/ TRANSFER HOLES, DEBURRED NEW R2 DOOR SILL IAW SRM 51-72-11-911-001 & SRM 53-41-69.
- [SDR CALA2023120803594](https://openairdocs.org/sdr/CALA2023120803594.md): Stringer · corroded · Dec 6, 2023 · N820UA · Airbus A319131 · Fuselage Main, Longeron/Stringer
  > AFT CARGO FWD OF FR60 RH STR 37 FITTING/CORROSION ON STRINGER AND 6EA RIVETS. AT HAECO LCQ PER NR 9298406 / 32406. REMOVED AND REPLACED STRINGER 37RT IN AFT CARGO FR 59-60 IAW A31 9 SRM 51-72-11 AND REINSTALLED CLEAT AT FR 60RT IAW A319 SRM 651 -72-11.
- [SDR CALA2023120103518](https://openairdocs.org/sdr/CALA2023120103518.md): Stringer · corroded · Nov 30, 2023 · N820UA · Airbus A319131 · Fuselage Main, Longeron/Stringer
  > CABIN, AFT UNDER FLOOR COMPARTMENT, FR. 65. STR. R/H 26, STRINGE R WITH EXFOLIATION CORROSION. PER HAECO LCQ NR 92 98791/32791. REMOVED AND REPLACED STRINGER 26RT PN64-67 IAW A319 SRM 51-72-11 & ECRA5341-01417, APPLIED TOP COAT IAW A319 SRM 51-25-12-911.
- [SDR CALA2023121103619](https://openairdocs.org/sdr/CALA2023121103619.md): Stringer · cracked · Nov 12, 2023 · N820UA · Airbus A319131 · Fuselage Main, Longeron/Stringer
  > ACCOMPLISH INITIAL INSPECTION OF FR35 STGR30 LH HOLE NO. 2 AFT SKIN LAYER, FWD SKIN LAYER, ANGLE FITTING AND RH HOLE NO. 3 ALL LAYERS PER PART 2B OF THE LATEST REVISION OF ECRA 5331-03057 LAYERS PER PART 2B OF THE LATEST REVISION OF ECRA 5331-03057 ON COMES FI
- [SDR CALA2023111503352](https://openairdocs.org/sdr/CALA2023111503352.md): Frame · mechanic error · Nov 8, 2023 · N820UA · Airbus A319131 · Fuselage Main, Frame
  > FALSE FRAME AT FR1 MISDRILLED PER HAECO LCQ NON ROUTINE 9298954/ 32954. REMOVED AND REPLACED FWD FALSE FRAME IAW SRM 51-42-11/001 AND AIRBUS DWG D531-13145 REPAIRED SURFACE PROTECTION IAW A319 SRM 51- 75-12-911-002.
- [SDR CALA2023102703204](https://openairdocs.org/sdr/CALA2023102703204.md): Plate · corroded · Oct 26, 2023 · N820UA · Airbus A319131 · Cargo/Baggage Doors
  > AFT CARGO COMPARTMENT DOOR BOX UPPER SURFACE PLATE HAS CORR FWD FR59 PER HAECO LCQ NR 9298550 (32550) REMOVED AND REPLACED AFT CARGO COMAPRTMENT DOOR BOX UPPER PLATE IAW A319 SRM 51-42-11 PG 6-15.
- [SDR CALA2023102703195](https://openairdocs.org/sdr/CALA2023102703195.md): Fitting · cracked · Oct 19, 2023 · N820UA · Airbus A319131 · Fuselage Main, Structure
  > WINDHSIELD CONTINUITY FITTING HAS CRACK INDICATION ON L&R SIDE A PPROX.50 INSH FROM IB FLANGE. LH MOST IB HOLE IS CRACKED ON OB FWD SURFACE APPROX.200" IN LENGTH AT 6 O''CLOCK POSITION. RH MOS T IB HOLE CRACKS ON OB FWD SURFACE APPROX.100" AT 6 O''CLOCK POS
- [SDR CALA2023101303045](https://openairdocs.org/sdr/CALA2023101303045.md): Stringer · corroded · Oct 11, 2023 · N820UA · Airbus A319131 · Fuselage Main, Longeron/Stringer
  > AFT PIT AT FR65 RIGHT BETWEEN STR30-31 CLEAT HAS CORROSION PER L CQ HAECO NR 9298946 (32946) REMOVED AND REPLACED CLEAT @ FR65 RH STRINGER 30-31 IAW A319 SRM 51-72-11-911-001.
- [SDR CALA2023101303048](https://openairdocs.org/sdr/CALA2023101303048.md): Skin · dented · Oct 6, 2023 · N820UA · Airbus A319131 · Horizontal Stabilizer, Plate/Skin
  > RH HORIZ STAB TIP 342AB HAS LE DENTS PER NR 9298451 / 32451 EVALUATED 2EA DENTS ON RH HORIZONTAL STAB TIP, 342AB. DENT #1 WA IAW SRM 55-41-11-283-001 FIG 5 AND 6 AND 55-14-11-300-006. REPAIRS LOCATED IN ZONE #3 I/B OF RIB 25 AND REQUIRED REPAIR. CUT OUT R FOR
- [SDR CALA2023100902990](https://openairdocs.org/sdr/CALA2023100902990.md): Stringer · corroded · Oct 6, 2023 · N820UA · Airbus A319131 · Fuselage Main, Longeron/Stringer
  > CABIN, AFT UNDER FLOOR COMPARTMENT, FR.65 STR. R/H 31, STRINGER AND STRINGER BRACKET EXFOLIATION CORROSION PER HAECO LCQ NR 9298 790 (32790) REMOVED & REPLACED STRINGER 31 RT FR65 IAW A319 SRM 51-72-11.
- [SDR CALA2023100602957](https://openairdocs.org/sdr/CALA2023100602957.md): Door Sill · cracked · Sep 30, 2023 · N820UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > FR67 UNDER R2 DOOR SILL IS CRACKED AND HAS PREVIOUS CUT OUT. GEN BY V061742 ON HAECO LCQ NR 9298904/32904 REMOVED AND REPLACED FR67 SECTION UNDER R2 DOOR SILL IAW A319 SR M 51-42-11.
- [SDR CALA2023100602946](https://openairdocs.org/sdr/CALA2023100602946.md): Stringer · corroded · Sep 28, 2023 · N820UA · Airbus A319131 · Fuselage Main, Longeron/Stringer
  > AFT CARGO FR 60-62 R/H STR 42 AND CORRESPONDING SKIN MULTIPLE SPOTS OF FITTINGS (A3NB-53-4-6179).. REMOVED AND REPLACED STRINGER 42RH AT FR 59 TO FR 64 IAW A319 SR M 51-72-11 PAR 2.
- [SDR CALA2023092902904](https://openairdocs.org/sdr/CALA2023092902904.md): Door Sill · corroded · Sep 27, 2023 · N820UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > L2 PAX DOOR SILL HAS MULTIPLE SPOTS OF CORROSION. GEN BY V937268 ON HAECO LCQ NR 9298715 REPAIRED L2 PAX DOOR SILL BEAM AT FR68 IAW A319 SRM 53-41-14-300 -001 AND 51-42-11/001.
- [SDR CALA2023100602947](https://openairdocs.org/sdr/CALA2023100602947.md): Frame · cracked · Sep 22, 2023 · N820UA · Airbus A319131 · Fuselage Main, Frame
  > FRAME AT FR1 CRACKED AT BOTH ENDS PER NR 9298836 / 32836 GEN BY V061742 REMOVED AND REPLACED FRAME TO SKIN AT FR1 IAW A319 SRM 51-72-11- 911-001
- [SDR CALA2023092502870](https://openairdocs.org/sdr/CALA2023092502870.md): Door Sill · corroded · Sep 22, 2023 · N820UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > R2 DOOR SHAPE SILL HAS CORROSION PER NR 9298803 / 32609 GEN BY V 061680 RMVD AND RPLDE SHAPE SILL ON R-2 DOOR SILL IAW SRM 51-42-11/001 AND 53-41-69-02-A BY MECH V906030 INSP BY V921658
- [SDR CALA2023092202851](https://openairdocs.org/sdr/CALA2023092202851.md): Panel · corroded · Sep 20, 2023 · N820UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT WET AREA RH AFT SHEAR PLATE AND STRUCTURE UNDERNEATH SHEAR PLATE CORRODED PER NR 9298708 / 32708. RMVD AND RPLD NEW SHEAR PLATE ON AFT WET AREA RH IAW SRM 51-72-1 1-911-001. STRUCTURE UNDER SHEAR WEB REPAIRED ON NR 92988 01
- [SDR CALA2023091802808](https://openairdocs.org/sdr/CALA2023091802808.md): Skin · punctured · Sep 15, 2023 · N820UA · Airbus A319131 · Elevator, Plate/Skin
  > R/H ELEVATOR UPPER SURFACE HAS A PUNCTURE 29.5INCHES FROM I/B AN D 12.5 FROM T/E,.5 DIAMETER. GEN BY V061647 PER HAECO LCQ NR 92 98786/32786 REPAIRED RH ELEVATOR UPPER SURFACE 29.5IN FROM IB 12.5IN FROM TE.5IN DIA ZONE 1 IAW A319 SRM 55-21-11-300-004 CATEGOR
- [SDR CALA2023091802807](https://openairdocs.org/sdr/CALA2023091802807.md): Skin · contaminated · Sep 15, 2023 · N820UA · Airbus A319131 · Elevator, Plate/Skin
  > L/H ELEVATOR HAS LIQUID INGRESS ON UPPER SURFACE 162 1/4 IN FROM INBOARD END, 13 IN FROM TRAILING EDGE, 1 INCH DIAMETER "REPAIR BEFORE NEXT FLIGHT" GEN BY V061632 PER HAECO LCQ NR 9298594/3559 4 REPAIRED LH ELEVATOR UPPER SKIN 162.25IN FROM VB 13IN FROM T/E Z
- [SDR CALA2023100602949](https://openairdocs.org/sdr/CALA2023100602949.md): Door Frame · cracked · Sep 14, 2023 · N820UA · Airbus A319131 · Fuselage Main, Structure
  > R/H OVERWING EMERGENCY EXIT DOOR, AFT FRAME CRACKED PER NR 92982 52. REMOVED AND REPLACED RH OVERWING EMERGENCY EXIT DOOR AFT FRAME I AW A319 SRM 51-72-11-911-801.
- [SDR CALA2023100602948](https://openairdocs.org/sdr/CALA2023100602948.md): Door Frame · cracked · Sep 14, 2023 · N820UA · Airbus A319131 · Fuselage Main, Structure
  > R/H OVERWING EMERGENCY EXIT DOOR FWD, FRAME CRACKED PER NR929825 1 / 32251. REMOVED AND REPLACED RH OVERWING EMERGENCY EXIT DOOR FWD FRAME I AW UAL A319 SRM 51-72-11-911-001.
- [SDR CALA2023073102372](https://openairdocs.org/sdr/CALA2023073102372.md): Switch · unserviceable · Jul 27, 2023 · N820UA · Airbus A319131 · Hydraulic System, Main
  > HYD B RSVR LO LVL ECAM. R&R LEVEL SWITCH IAW AMM 29-12-41-000-003-A. OPS CHECK OK. NO LEAKS NOTED AT THIS TIME PARTS USED: 31-2912-3-0002,QTY:1.
- [SDR CALA2023041901152](https://openairdocs.org/sdr/CALA2023041901152.md): Check Valve · failed · Apr 17, 2023 · N820UA · Airbus A319131 · Hydraulic Pump (Electric/Engine), Main
  > ECAM, HYD Y RSVR LO LVL. FOLLOWED CHECKLIST, SHUT DOWN #2 ENGINE PUMP. DID NOT GET YELLOW SYSTEM LOW PRESSURE MSG PRIOR TO SHUTTING PUMP OFF. FOUND GREEN MAIN HYDROLIC POWER CHECK VALVE ON PTU TO BE LEAKING. REMOVED AND REPLACED CHECK VALVE. REFF AMM 29-11-15
- [SDR CALA2022111603138](https://openairdocs.org/sdr/CALA2022111603138.md): Line · leaking · Nov 15, 2022 · N820UA · Airbus A319131 · Hydraulic System, Main
  > ECAM CAUTION MESSAGE - Y ENG PUMP LO PR MESSAGE INOP - HYD UPON ARRIVAL TO FLT DECK, FOUND YELLOW HYD QTY AT ZERO. R&R #2 ENGINE HYDRAULIC LINE PART #D2901010201200, REF IPC IDENTIFIED HYDRAULIC FLUID BENEATH #2 ENGINE. FOUND HYD PIPE 29-13-06-02L ITEM #260.
- [SDR CALA2022042901106](https://openairdocs.org/sdr/CALA2022042901106.md): None · none · Apr 29, 2022 · N820UA · Airbus A300* · Hydraulic Pressure Sensor
  > ECAM CAUTION MESSAGE - Y RSVR LO LVL MESSAGE INOP - HYD LEAK APPEARS TO BE AT THE PTU MANIFOLD. NEED MORE TIME TO FOUND 2WAY HYD VALVE DRUM SEAL ITEM 100 IPC 29-13-15-02A LEAKING TROUBLESHOOT. AND O-RING 40 FOR CHECK VALVE 10. REPLACED THE O-RINGS AND BONNETS
- [SDR CALA2022042501072](https://openairdocs.org/sdr/CALA2022042501072.md): Landing Gear · none · Apr 25, 2022 · N820UA · Airbus A319131 · Landing Gear Retraction/Extension System
  > LANDING GEAR WOULD NOT RETRACT AFTER T/O. CYCLED GEAR PER ECAM N O HELP TOP OF THE GEAR HANDLE SELECT PACKAGE ONLY OTHER LIGHT THAT WAS BLINKING WAS ADIRU1 WAS FLASHING THE WHOLE TIME CONTACT TOMC 847-700-9980 DE-BRIEFED INBD CREW THEY SAID THEY CYCLED THE GEA
- [SDR CALA2022040400877](https://openairdocs.org/sdr/CALA2022040400877.md): Bolt · sheared · Apr 4, 2022 · N820UA · Airbus A319131 · Flight Control System
  > *EMERGENCY DECLARED* GREEN HYDRAULIC SYSTEMQUANTITY IS VERY LOW. OPENED PANEL 325BL ON LEFT SIDE OF VERT STAB. FOUND 1 OF 3 BOLTS R&R LH SERVOACTUATOR YAW DAMPER IAW AMM 27-26-51. OPS CHECK LEAK INSPECTED ACTUATOR PER GMM 09-10-05.MARCHAND U098190. SHEARD FR
- [SDR CALA2021072601189](https://openairdocs.org/sdr/CALA2021072601189.md): Sink · leaking · Jul 25, 2021 · N820UA · Airbus A319131 · Wash Water System
  > REF LP 6685795 DUE TO WATER SPILL FROM AFT AFT LAV SINK INITIAL CLEAN UP WAS ACCOMPLISHED REF ECRA 2011-01000 REV AB IN DEPTH CLEAN UP NEEDS TO BE ACCOMPLISHED IN AFT AFT LAV AND AFT GALLEY AREA. CARRIED ITEM REF ECRA 2011-01000 REV AB IN DEPTH CLEAN UP TO BE
- [SDR CALA2021031200311](https://openairdocs.org/sdr/CALA2021031200311.md): Window Frame · cracked · Mar 11, 2021 · N820UA · Airbus A319131 · Fuselage Main, Structure
  > CRACK FOUND WHILE ACCOMPLISHING EA 5310-07639 REV A AT L/H HORIZ UPPER STIFFENER INTERNAL SECTION OF LATERAL WINDOW FRAME AT FR4 (UPPER FASTENER HOLE). REMOVED BOLT, CONFIRMED CRACK BY HFEC & FPI REF A319 NTM 51-10-01 & 51-80-00; REINSTALLED BOLT AT LT LATERAL
- [SDR CALA2020091801122](https://openairdocs.org/sdr/CALA2020091801122.md): Door Frame · cracked · Sep 16, 2020 · N820UA · Airbus A319131 · Fuselage Main, Structure
  > CRACK INDICATION OBTAINED AT RT FWD DOOR STOP FITTING NR 1 FR 16 LOWER INBOARD HOLE AT 7:00 POSITION WITH LENGTH OF APPROX 0.020 IN. REF AAR N/R: 99900282 GENERATED BY: V903469 REMOVED & REPLACED INTERCOSTAL AT RT FR 16 JUST FWD OF DOOR STOP FITTING NR 1, AS
- [SDR CALA2020091801121](https://openairdocs.org/sdr/CALA2020091801121.md): Door Frame · cracked · Sep 16, 2020 · N820UA · Airbus A319131 · Fuselage Main, Structure
  > CRACK INDICATIONS OBTAINED AT LT FWD PASSENGER CREW DOOR STOP NR 7 UPPER I/B FR 16 AT 5:00 POSITION WITH LENGTH APPROX 0.020', REF AAR N/R: 99900285 GENERATED BY: V903469. REMOVED AND REPLACED INTERCOSTAL AT LT FR 16 JUST FWD OF DOOR STOP FITTING, AS PER AIRB
- [SDR CALA2019052700850](https://openairdocs.org/sdr/CALA2019052700850.md): Fuel Cap · missing · May 27, 2019 · N820UA · Airbus A319131 · Fuel Storage
  > PDA 2 FUEL CAP MISSING NOTED BEFORE FUELING FLIGHT 2092-26. REF LOG PAGE 3328986 FOR CORRECTIVE ACTION CONDUCTED INVESTIGATION, NO REPORTS OF EXTRA FUEL CAPS FOUND IN IAH. CORRECTIVE ACTION TAKEN ON LOG PAGE 3328986
- [SDR CALA2017121104397](https://openairdocs.org/sdr/CALA2017121104397.md): Support Bracket · damaged · Dec 11, 2017 · N820UA · Airbus A319131 · Emergency Lighting
  > EXIT LIGHT ROW 21DEF INOP REPLACED EMER SIDE WALL LIGHT SUPPORT BRACKET FOR LIGHT(90WL4)AT SEAT ROW 21DEF,OPS NORMAL. INSP INSTALLATION OF EMERGENCY LIGHTING OP CK OK
- [SDR CALA2017111704100](https://openairdocs.org/sdr/CALA2017111704100.md): Unknown · odor · Nov 17, 2017 · N820UA · Airbus A319131 · Air Distribution System
  > F/A REPORTED A STRONG ACRID ELECTRICAL ODOR IN THE AFT GALLEY. DISSIPATED BEFORE FA PULLED CIRCUIT BREAKERS. ACCOMPLISHED A SMOKE OR FUMES IN CABIN INSPECTION. CHECKED IAW AMM 05-51-10. NO DEFECTS NOTED IN AFT CABIN GALLEY. ALL CIRCUIT BREAKERS RESET ALL
- [SDR CALA2017060501671](https://openairdocs.org/sdr/CALA2017060501671.md): Windshield · cracked · Jun 5, 2017 · N820UA · Airbus A319131 · Flight Compartment Windows
  > CAPTAIN'S WINDSHIELD CRACKED. EMERGENCY DECLARED. REMOVED AND REPLACED THE WINDSHIELD IAW AMM 56-11-11, AND AMM 56-11-11-400-001-A01.
- [SDR CALA2017052601558](https://openairdocs.org/sdr/CALA2017052601558.md): Pump · overserviced · May 26, 2017 · N820UA · Airbus A319131 · Hydraulic Pump (Electric/Engine), Main
  > AIR RETURN DUE TO BLUE SYSTEM LOW PRESSURE. ACFT RETURNED TO GATE WITH BLUE SYS PUMP NOT OPERATING, NO FLUID LOSE. NO SYSTEM OVERHEAT, PUMP OK. CYCLED ACFT POWER AND PUMP OPERATION RESTORED. BLUE QTY OVERSERVICED. DRAINED TO PROPER LEVEL, REMOVED AND R
- [SDR CALA2017050101224](https://openairdocs.org/sdr/CALA2017050101224.md): Battery Pack · no test · May 1, 2017 · N820UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY LIGHTS TEST FAILED. EPSU BATTERY EMER R. REPLACED RIGHT EPSU BATTERY PER MM 33-51-38. OPS CK GOOD.
- [SDR CALA2015111994847](https://openairdocs.org/sdr/CALA2015111994847.md): Battery Pack · faulty · Nov 19, 2015 · N820UA · Airbus A319131 · Emergency Lighting
  > IN ACCORDANCE WITH NR 2 SERVICE STEP 2.O, FAILED EMER LIGHTS OPERATIONAL TEST WITH EPSU BATTERY FWD LT MSG. REMOVED & REINSTALLED FWD LT BATTERY PACK. FAULT CLEARED & TESTED OKAY.
- [SDR CALA2015080794183](https://openairdocs.org/sdr/CALA2015080794183.md): Actuator · malfunctioned · Aug 2, 2015 · N820UA · Airbus A319131 · Passenger Oxygen System
  > PASSENGER OXYGEN MASKS DID NOT DROP AT SEATS 27 ABC, 28 ABC, 12 DEF, 26 DEF, 20 ABC & DOOR 2L. REPLACED O2 MASK CONTAINER ACTUATOR ASSEMBLIES AT 27 ABC, 28 ABC, 20 ABC DOOR 2L. SEAT 12 DEF, 26 DEF OPERATIONS CHECKED NORMALLY & DIDN'T NEED REPLACED. OPERATIO
- [SDR CALA2015071794133](https://openairdocs.org/sdr/CALA2015071794133.md): Light · inoperative · Jul 15, 2015 · N820UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY LIGHT TEST FAULTS EPSU EXT LOAD EMER RT. RT OVERWING EXIT LIGHTS WILL NOT ILLUMINATE, COMPLIED WITH MEL.

Next page: https://openairdocs.org/aircraft/N820UA/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 = 'N820UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N820UA/reports

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