# Service difficulty reports: N811UA

A list on [N811UA](https://openairdocs.org/aircraft/N811UA.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 · 103 reports

- [SDR CALA2026101320357](https://openairdocs.org/sdr/CALA2026101320357.md): Light · inoperative · Oct 11, 2026 · N811UA · Airbus A319131 · Emergency Lighting
  > AISLE 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:1
- [SDR CALA2026071617809](https://openairdocs.org/sdr/CALA2026071617809.md): Skin · damaged · Jul 15, 2026 · N811UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > LIGHTNING 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 LIGHTN
- [SDR CALA2026010212636](https://openairdocs.org/sdr/CALA2026010212636.md): Diaphragm · damaged · Dec 29, 2025 · N811UA · Airbus A319131 · Wing Main, Frame Structure
  > LEFT 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 E
- [SDR CALA2025032803293](https://openairdocs.org/sdr/CALA2025032803293.md): Access Panel · damaged · Mar 26, 2025 · N811UA · Airbus A319131 · Wing, Plate/Skin
  > LEFT 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 PER
- [SDR CALA2024070300110](https://openairdocs.org/sdr/CALA2024070300110.md): Tire · worn · Jul 1, 2024 · N811UA · Airbus A319131 · Tire
  > 04 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
- [SDR CALA2024041901144](https://openairdocs.org/sdr/CALA2024041901144.md): Fuel Cap · missing · Apr 19, 2024 · N811UA · Airbus A319131 · Fuel Storage
  > PDA 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.
- [SDR CALA2023092902917](https://openairdocs.org/sdr/CALA2023092902917.md): Motor · seized · Sep 26, 2023 · N811UA · Airbus A319131 · Hydraulic Pump (Electric/Engine), Main
  > YELLOW 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 I
- [SDR CALA2023062301982](https://openairdocs.org/sdr/CALA2023062301982.md): Fitting · gouged · Jun 22, 2023 · N811UA · Airbus A319131 · Flight Compartment Windows
  > COCKPIT 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
- [SDR CALA2023062602033](https://openairdocs.org/sdr/CALA2023062602033.md): Guide · gouged · Jun 21, 2023 · N811UA · Airbus A319131 · Flight Compartment Windows
  > COCKPIT 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.
- [SDR CALA2023061201824](https://openairdocs.org/sdr/CALA2023061201824.md): Door Sill · corroded · Jun 11, 2023 · N811UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT DOOR SILL UPPER SURFACE FR56-FR58 CORRODED. REQUIRES REPLACEMENT. AFT CARGO DOOR SILL REPLACED IAW SRM 51-42-11. ESFR COMPLIED WITH
- [SDR CALA2023053101723](https://openairdocs.org/sdr/CALA2023053101723.md): Frame · corroded · May 30, 2023 · N811UA · Airbus A319131 · Fuselage Main, Frame
  > 10SEP 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 CONT
- [SDR CALA2023052401627](https://openairdocs.org/sdr/CALA2023052401627.md): Fitting · corroded · May 22, 2023 · N811UA · Airbus A319131 · Fuselage Main, Attach Fittings
  > MAIN 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 ACCOMPLIS
- [SDR CALA2023051501517](https://openairdocs.org/sdr/CALA2023051501517.md): Intercostal · cracked · May 13, 2023 · N811UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > RH 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 A
- [SDR CALA2023051501516](https://openairdocs.org/sdr/CALA2023051501516.md): Floor Support · corroded · May 13, 2023 · N811UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > MAIN 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:
- [SDR CALA2023051101456](https://openairdocs.org/sdr/CALA2023051101456.md): Seat Track · corroded · May 10, 2023 · N811UA · Airbus A319131 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN 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=1.22
- [SDR CALA2023051201466](https://openairdocs.org/sdr/CALA2023051201466.md): Floorbeam · corroded · May 10, 2023 · N811UA · Airbus A319131 · Fuselage Main, Floor Beam
  > MAIN 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=1.22
- [SDR CALA2023050801414](https://openairdocs.org/sdr/CALA2023050801414.md): Angle · cracked · May 8, 2023 · N811UA · Airbus A319131 · Emergency Exits
  > LH 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 BFM
- [SDR CALA2022082902220](https://openairdocs.org/sdr/CALA2022082902220.md): None · none · Aug 29, 2022 · N811UA · Airbus A300* · Hydraulic System, Main
  > G 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 MA
- [SDR CALA2022050201115](https://openairdocs.org/sdr/CALA2022050201115.md): Frame · corroded · May 1, 2022 · N811UA · Airbus A300* · Fuselage Structure (General)
  > RH 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 REP
- [SDR CALA2022050201114](https://openairdocs.org/sdr/CALA2022050201114.md): Skin · bent · May 1, 2022 · N811UA · Airbus A300* · Passenger/Crew Doors
  > R2 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 I
- [SDR CALA2022042501062](https://openairdocs.org/sdr/CALA2022042501062.md): Door Sill · corroded · Apr 25, 2022 · N811UA · Airbus A319131 · Fuselage Structure (General)
  > R2 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 N078625
- [SDR CALA2022042101031](https://openairdocs.org/sdr/CALA2022042101031.md): Plate · cracked · Apr 19, 2022 · N811UA · Airbus A319131 · Fuselage Structure (General)
  > AFT 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 9
- [SDR CALA2022041801008](https://openairdocs.org/sdr/CALA2022041801008.md): Door Sill · corroded · Apr 17, 2022 · N811UA · Airbus A319131 · Fuselage Structure (General)
  > L2 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 53-41-14-300
- [SDR CALA2022030100542](https://openairdocs.org/sdr/CALA2022030100542.md): Rivet · missing · Mar 1, 2022 · N811UA · Airbus A319131 · Fuselage Structure (General)
  > PDA 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 AREA
- [SDR CALA2021043000588](https://openairdocs.org/sdr/CALA2021043000588.md): Scanner · inoperative · Apr 30, 2021 · N811UA · Airbus A319131 · Weather Radar System
  > WX 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 PEDESTAL
- [SDR CALA2020040600789](https://openairdocs.org/sdr/CALA2020040600789.md): Intercostal · cracked · Apr 4, 2020 · N811UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > R1 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-
- [SDR CALA2020033000740](https://openairdocs.org/sdr/CALA2020033000740.md): Intercostal · cracked · Mar 27, 2020 · N811UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > L1 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 51-72-11-911-001
- [SDR CALA2020033000739](https://openairdocs.org/sdr/CALA2020033000739.md): Intercostal · cracked · Mar 27, 2020 · N811UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > R1 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.
- [SDR CALA2016101795812](https://openairdocs.org/sdr/CALA2016101795812.md): Door Frame · corroded · Oct 14, 2016 · N811UA · Airbus A319131 · Fuselage Main, Structure
  > AFT FUSE R2 DOOR CUTOUT FR68 AT STR 23R FRAME HAS CORROSION. CUTOUT DAMAGE & INSTALLED REPAIR IAW SRM53-41-12 FIG 202.
- [SDR CALA2016051895372](https://openairdocs.org/sdr/CALA2016051895372.md): Battery · faulty · May 15, 2016 · N811UA · Airbus A319131 · Battery/Charger System
  > AFTER 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 SHOWING
- [SDR CALA2015101594592](https://openairdocs.org/sdr/CALA2015101594592.md): Skin · saturated · Oct 14, 2015 · N811UA · Airbus A319131 · Elevator, Plate/Skin
  > LEFT 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
- [SDR CALA2015101594590](https://openairdocs.org/sdr/CALA2015101594590.md): Skin · saturated · Oct 14, 2015 · N811UA · Airbus A319131 · Elevator, Plate/Skin
  > RIGHT 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
- [SDR CALA2015092594400](https://openairdocs.org/sdr/CALA2015092594400.md): Power Supply · faulted · Sep 25, 2015 · N811UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY LIGHT TEST FAULTS FWD LT EMER POWER SUPPLY UNIT. REPLACED BATTERY PACK & POWER SUPPLY IAW AMM 33-51-38.
- [SDR CALA2015070694045](https://openairdocs.org/sdr/CALA2015070694045.md): Access Panel · damaged · Jul 4, 2015 · N811UA · Airbus A319131 · Wing, Plate/Skin
  > LEFT 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.
- [SDR CALA2015070694039](https://openairdocs.org/sdr/CALA2015070694039.md): Door · malfunctioned · Jul 2, 2015 · N811UA · Airbus A319131 · Passenger Oxygen System
  > CABIN 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 352
- [SDR CALA2015063094036](https://openairdocs.org/sdr/CALA2015063094036.md): Access Panel · damaged · Jun 29, 2015 · N811UA · Airbus A319131 · Wing, Plate/Skin
  > LEFT 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.
- [SDR CALA2015012393011](https://openairdocs.org/sdr/CALA2015012393011.md): Warning System · activated · Jan 20, 2015 · N811UA · Airbus A319131 · Landing Gear Brake System
  > ON 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 32-42-0
- [SDR CALA2014122392851](https://openairdocs.org/sdr/CALA2014122392851.md): Skin · damaged · Dec 15, 2014 · N811UA · Airbus A319131 · Wing, Plate/Skin
  > LEFT 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 FIRST
- [SDR CALA2014122392850](https://openairdocs.org/sdr/CALA2014122392850.md): Skin · damaged · Dec 15, 2014 · N811UA · Airbus A319131 · Elevator, Plate/Skin
  > RIGHT 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 & RE
- [SDR CALA2014122392846](https://openairdocs.org/sdr/CALA2014122392846.md): Door Frame · corroded · Dec 14, 2014 · N811UA · Airbus A319131 · Fuselage Main, Structure
  > AFT 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 INSPECT
- [SDR CALA2014122392845](https://openairdocs.org/sdr/CALA2014122392845.md): Shear Plate · corroded · Dec 14, 2014 · N811UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > RIGHT 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.
- [SDR CALA2014122392844](https://openairdocs.org/sdr/CALA2014122392844.md): Door Sill · corroded · Dec 14, 2014 · N811UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > R2 DOOR SILL HAS CORROSION FRAME 66 - 68. R & R NEW DOOR SILL IAW SRM 51-42-11 PARA 5, 6, & 8.
- [SDR CALA2014122392843](https://openairdocs.org/sdr/CALA2014122392843.md): Skin Panel · damaged · Dec 13, 2014 · N811UA · Airbus A319131 · Elevator, Plate/Skin
  > LEFT 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 &
- [SDR CALA2014120992799](https://openairdocs.org/sdr/CALA2014120992799.md): Door Sill · corroded · Dec 8, 2014 · N811UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > L2 DOOR SILL HAS CORROSION AT FRAME 68. INSTALLED REPAIR IAW SRM 53-41-14 FIG 201 SHEET 3 PRINCIPLE 4.
- [SDR CALA2013112193148](https://openairdocs.org/sdr/CALA2013112193148.md): Warning System · activated · Nov 20, 2013 · N811UA · Airbus A319131 · Central Warning
  > ENG ANTI ICE MESSAGE ON UPPER ECAM.
- [SDR CALA2013092591437](https://openairdocs.org/sdr/CALA2013092591437.md): Antenna · defective · Sep 19, 2013 · N811UA · Airbus A319131 · VHF Communications System
  > ALL AIRBORNE FREQUENCY INOPERATIVE ON COM 1. REPLACED UPPER NR 1 VHF ANTENNA IAW AMM. TESTED GOOD.
- [SDR CALA2013091091178](https://openairdocs.org/sdr/CALA2013091091178.md): Light · inoperative · Sep 7, 2013 · N811UA · Airbus A319131 · Passenger Compartment Lighting
  > CEILING LIGHT AT SEAT ROW 22RT INOPERATIVE. RELAMPED, OPERATIONS CHECKED GOOD.
- [SDR CALA2013082690761](https://openairdocs.org/sdr/CALA2013082690761.md): Controller · faulty · Aug 25, 2013 · N811UA · Airbus A319131 · Cabin Pressure Controller
  > CABIN PRESSURE CONTROLLER ONE, SYSTEM 1 FAULT. ITEM ROLLED FORWARD. REMOVED & REPLACED CABIN PRESSURE CONTROLLER ONE IAW AMM. TESTED IAW AMM.
- [SDR CALA2013081490440](https://openairdocs.org/sdr/CALA2013081490440.md): Extinguisher · unsecure · Aug 13, 2013 · N811UA · Airbus A319131 · Fire Bottle, Portable
  > F/A REPORTS AFT GALLEY HALON FIRE EXTINGUISHER PIN UNSECURE. RESEALED AND SECURED EXTINGUISHER.
- [SDR UALA2013070104569](https://openairdocs.org/sdr/UALA2013070104569.md): Fastener · loose · Jun 28, 2013 · N811UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > DURING WALK AROUND, FOUND FASTENER LOOSE ON ACFT BELLY TWO FT BEHIND ANTI COLLISION BEACON. REPLACED FASTENER IAW AMM.

Next page: https://openairdocs.org/aircraft/N811UA/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 = 'N811UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N811UA/reports

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