# Service difficulty reports: N821UA

A list on [N821UA](https://openairdocs.org/aircraft/N821UA.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 · 132 reports

- [SDR CALA2026082418818](https://openairdocs.org/sdr/CALA2026082418818.md): Battery Pack · faulted · Aug 21, 2026 · N821UA · Airbus A319131 · Emergency Lighting
  > RT EPSU BATTERY FAULT, FOUND ON EMERGENCY LIGHT OPS CHK. REMOVED AND REPLACED RIGHT CABIN EMERGENCY POWER SUPPLY UNIT BATTERY IAW AMM 33-51-38/401. OPS CHKD GOOD.
- [SDR CALA2025092609289](https://openairdocs.org/sdr/CALA2025092609289.md): None Aircraft · odor · Sep 25, 2025 · N821UA · Airbus A319131 · Standard Practices/Structures
  > FLIGHT CREW REPORTS ELECTRICAL SMELL IN THE AREA WHERE BUISNESS MEETS ECONOMY. UPON ARRIVAL MX NOTICED A FAINT ELECTRICAL SMELL NEAR ROW 8. SMELL WAS NOT CONSITANT AND WAS ONLY ABLE TO PICK IT UP ONCE ON MULTIPLE PASSES THROUGH THE AREA OF ROW 8. ADVISED TS
- [SDR CALA2025061905714](https://openairdocs.org/sdr/CALA2025061905714.md): Unknown · odor · Jun 17, 2025 · N821UA · Airbus A319131 · Air Distribution System
  > FA REPORTS PLASTIC BURNING SMELL IN AFT CABIN DURING DESCENT INSPECTED AFT GALLEY AREA. NO SMELLS NOTED. INSPECTED ALL OVENS AND COFFEE MAKERS, NO SMELLS OR ISSUES NOTED. NO HISTORY. REF MM 25-33-00 ADD EMP: U414325
- [SDR CALA2024123001699](https://openairdocs.org/sdr/CALA2024123001699.md): Unknown · odor · Dec 28, 2024 · N821UA · Airbus A319131 · Air Distribution System
  > FA AND PAX REPORTEDSMOKE SMELL NEAR ROWS8-10NO VISIBLE SMOKE SEE N TSM 05-50-00-810-831-A NO SMOKE OR ODOR PRESENT. INSPECTED NO DEFECTS FOUND AT THIS TIME. COULD NOT DUPLICATE ODOR
- [SDR CALA2024121301504](https://openairdocs.org/sdr/CALA2024121301504.md): Battery · inoperative · Dec 11, 2024 · N821UA · Airbus A319131 · Emergency Lighting
  > WHILE PERFORMING OPERATIONAL TEST OF EPSU, RECIEVED FAULT MESSAGES "EPSU BATTERY EMER L, AND EPSU BATTERY AFT L" ON PTP. REPLACED BOTH EPSU BATTERY LEFT (11WL) AND EPSU BATTERY AFT L (13WL) REF AMM 33-51-38-400-002-A. OPS CHECK OK.PARTS USED: 18-3351-3-0001,QT
- [SDR CALA2024121201482](https://openairdocs.org/sdr/CALA2024121201482.md): Battery · no test · Dec 10, 2024 · N821UA · Airbus A319131 · Emergency Lighting
  > OPERATIONAL CHECK OF CABIN EMERGENCY LIGHTS {A3NB-33-3-6012} - FAILED TEST EPSU BATTERY FWD LEFT 33-51-38 REPLACED FWD LEFT EPSU BATTERY REF AMM 33-51-38-400-002-A, OPS CHECK OK.
- [SDR CALA2024091300629](https://openairdocs.org/sdr/CALA2024091300629.md): Warning Message · false activation · Sep 12, 2024 · N821UA · Airbus A319131 · Landing Gear Brake System
  > CREW REPORTS BRAKE SYS 1 FAULT DURING TAKE OFF ROLL CREW PERFORMED RESET FOR BRAKE SYS 1 FAULT PER THE QRH, BRAKE TEMPS DID NOT REACH THE OVERHEAT THRESHOLD, INSPECTION NOT REQUIRED PER AMM 05-51-16-200-001
- [SDR CALA2023073102378](https://openairdocs.org/sdr/CALA2023073102378.md): Window Frame · cracked · Jul 30, 2023 · N821UA · Airbus A319131 · Fuselage Main, Structure
  > WINDSHIELD FRAME LWR RH NODE VERTICAL FLANGE AFT FACE HAS A CRACK. "LH & RH FWD WINDSHIELD FRAME ASSY''S ALONG WITH THE PERMANENT SOLUTION WITH INSP REQUIREMENTS. ACCOMPLISH THE LATEST REV OF EC/RA 5311-03037 ON OR BEFORE THE AC REPEAT INSP''S PER THE LATEST R
- [SDR CALA2023072602328](https://openairdocs.org/sdr/CALA2023072602328.md): Stringer · damaged · Jul 25, 2023 · N821UA · Airbus A319131 · Fuselage Main, Longeron/Stringer
  > FR35 STGR 30 HOLES 1-4 & LH FR35 STGR 30 HOLE 2/3 OVERSIZED. 30 HOLES WERE REPAIRED AT BFM. REPAIR IS A PERMANENT SOLUTION ST 2 OF LATEST REV OF ECRA5321-02113 ON OR BEFORE THE AC REACHES INSP''S AT INTERVALS NOT TO EXCEED 6500FC OR 13000FH (WHICHEVER WITH INS
- [SDR CALA2023071702266](https://openairdocs.org/sdr/CALA2023071702266.md): Skin · unknown · Jul 15, 2023 · N821UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > FOUND 1 EA LIGHTNING STRIKE ON SKIN AT LHS FR8 Z-339 CREATED BY MEHRDAD PARSA 91105046 60000 FC/120000 FH IAW SRI 53-11-11-205-037 REPAIR EMBODIMENT AT ZONE 1. PERFORMED PERMANENT REPAIR CATEGORY B IAW SRM 53-11-11-3000-041. IT IS NECESSARY TO INSPECT THIS REP
- [SDR CALA2023071402253](https://openairdocs.org/sdr/CALA2023071402253.md): Profile · cracked · Jul 13, 2023 · N821UA · Airbus A319131 · Fuselage Structure (General)
  > (A3NB-52-4-6032) LH EMERGENCY ESCAPE HATCH AFT LOAD TRANSMITTING PROFIL IS CRACKED BETWEEN FASTENERS. DOT NO. 17-39. W/C:58438 REMOVED LH EMERGENCY HATCH LOAD TRANSMITTING PROFIL IAW SRM 51-4 2-11 2 EA INSTALLED NRU FWD LOAD TRANSMITTING PROFIL AND SHEET 2 EA
- [SDR CALA2023071402241](https://openairdocs.org/sdr/CALA2023071402241.md): Profile · cracked · Jul 12, 2023 · N821UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > LH EMERGENCY ESCAPE HATCH FWD LOAD TRANSMITTING PROFIL IS CRACKED BETWEEN FASTENERS. DOT NO 17-41. W/C:58440 REMOVED CRACKED ANGLE IAW SRM 51-42-11 INSTALLED NEW ANGLE AT LH EMERGENCY WINDOW IAW SRM 51-42-11 RESTORED SURFACE PROTECT ION IAW SRM 51-75-12. W/C:5
- [SDR CALA2023071402240](https://openairdocs.org/sdr/CALA2023071402240.md): Profile · cracked · Jul 12, 2023 · N821UA · Airbus A319131 · Fuselage Structure (General)
  > RH EMERGENCY ESCAPE HATCH AFT LOAD TRANSMITTING PROFIL IS CRACKED BETWEEN FASTENERS. DOT NO. 17-40. W/C:58439 REMOVED RH EMERGENCY ESCAPE HATCH AFT LOAD TRANSMITTING PROFIL IAW SRM 51-42-11. INSTALLED NEW TRANSMITTING PROFIL 2EA IAW SRM 51-42-11. TREATED AND P
- [SDR CALA2023071402259](https://openairdocs.org/sdr/CALA2023071402259.md): Skin · damaged · Jul 12, 2023 · N821UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > FOUND 1 EA LIGHTNING STRIKE ON SKIN AT LHS FR8 Z-339 CREATED BY MEHRDAD PARSA 91105046 60000 FC/120000 FH IAW SRI 53-11-11-205-037 REPAIR EMBODIMENT AT ZONE 1. PERFORMED PERMANENT REPAIR CATEGORY B IAW SRM 53-11-11-3000-041. IT IS NECESSARY TO INSPECT THIS REP
- [SDR CALA2023071202233](https://openairdocs.org/sdr/CALA2023071202233.md): Profile · cracked · Jul 11, 2023 · N821UA · Airbus A319131 · Emergency Exits
  > LH EMERGENCY ESCAPE HATCH FWD LOAD TRANSMITTING PROFIL IS CRACKED BETWEEN FASTENERS. DOT NO 17-41. W/C:58440 REMOVED CRACKED ANGLE IAW SRM 51-42-11 INSTALLED NEW ANGLE AT LH EMERGENCY WINDOW IAW SRM 51-42-11 RESTORED SURFACE PROTECT ION IAW SRM 51-75-12.
- [SDR CALA2023071202232](https://openairdocs.org/sdr/CALA2023071202232.md): Profile · unknown · Jul 11, 2023 · N821UA · Airbus A319131 · Emergency Exits
  > RH EMERGENCY ESCAPE HATCH AFT LOAD TRANSMITTING PROFIL IS CRACKED BETWEEN FASTENERS. DOT NO. 17-40. W/C:58439 REMOVED RH EMERGENCY ESCAPE HATCH AFT LOAD TRANSMITTING PROFIL IAW SRM 51-42-11. INSTALLED NEW TRANSMITTING PROFIL 2EA IAW SRM 51-42-11. TREATED AND P
- [SDR CALA2023071202231](https://openairdocs.org/sdr/CALA2023071202231.md): Profile · cracked · Jul 11, 2023 · N821UA · Airbus A319131 · Emergency Exits
  > LH EMERGENCY ESCAPE HATCH AFT LOAD TRANSMITTING PROFIL IS CRACKED BETWEEN FASTENERS. DOT NO. 17-39. W/C:58438 REMOVED LH EMERGENCY HATCH LOAD TRANSMITTING PROFIL IAW SRM 51-4 2-11 2 EA INSTALLED NRU FWD LOAD TRANSMITTING PROFIL AND SHEET 2 EA IAW SRM 51-42-11
- [SDR CALA2023070702180](https://openairdocs.org/sdr/CALA2023070702180.md): Fitting · corroded · Jul 5, 2023 · N821UA · Airbus A319131 · Fuselage Main, Structure
  > FLOOR STR UNDER L1 AFT GIRT BAR FITTING HAS CORROSION AROUND FAS TENERS. BLENDED AREA IAW SRM 51-74-00 D=0.065" NOMINAL THICKNESS 0.200" FOUND TO BE OUT OF LIMIT IAW SRM 53-11-14-283-005. REMOVED AND R EPLACED L1 DOOR SILL IAW SRM 51-42-11.
- [SDR CALA2023070302142](https://openairdocs.org/sdr/CALA2023070302142.md): Seat Track · corroded · Jul 1, 2023 · N821UA · Airbus A319131 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK -Y1292 HAS SCRATCHES AND CORROSION FR62 TO FR63 DOT 4 1-15 BLENDD SEAT TRACK-Y765 BETWEEN FR62 TO FR63 DIMENTIONS L=3 W=1'' EMP V943483 STA ST ENG BFM D=0.78'' FOUND TO BE OUT OF LIMITS CUT OUT SEAT TRACK FR 61; FABR ICATED (AEA) DOUBLERS AND (4EA)S
- [SDR CALA2023070302137](https://openairdocs.org/sdr/CALA2023070302137.md): Seat Track · corroded · Jul 1, 2023 · N821UA · Airbus A319131 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN LH SEAT TRACK Y1292 AT FR16-20 HAS CORROSION. DOT 102 -182. REMOVED AND REPLACED SEAT TRACK Y1292 BTW FR12 AND FR24 I.A.W. S RM 51-72-11-911-001 ATTACHED FORM 44-0008 EMP#: V935833 WORK ACC OMPLISHED AT ST ENGINEERING OF MOBILE AT BFM ON NR#: 58670
- [SDR CALA2023070302136](https://openairdocs.org/sdr/CALA2023070302136.md): Angle · corroded · Jul 1, 2023 · N821UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT CARGO BILGE STR 43L ANGLE HAS CORROSION FR47/51. REMOVED AND REPLACED COUPLING P/N D5347100720490 BATCH# 00041310 38 RECEIVED. IAW. SRM 51-42-11/001, SRM 51-72-11-911-001, SRM 51 -49-00. EMP: V940362 WC: 58608 STA: ST ENG BFM INSPECTED AND APPROVED
- [SDR CALA2023070302131](https://openairdocs.org/sdr/CALA2023070302131.md): Skin · deformed · Jun 30, 2023 · N821UA · Airbus A319131 · Leading Edge Devices
  > RT WING AT #1 SLAT #3 TRACK FIXED L/E SKIN CUT-OUT DEFORMED/DENTED. EVALUATED DAMAGE IAW A319 SRM 57-41-11-263-009 AND FOUND OUT OF LIMITS AND REPIARED IAW A319 SRM 57-41-11-300-037. EMP: V934583 WC: 58329 STA: ST ENG BFM
- [SDR CALA2023070302130](https://openairdocs.org/sdr/CALA2023070302130.md): Floorbeam · corroded · Jun 30, 2023 · N821UA · Airbus A319131 · Fuselage Main, Floor Beam
  > AFT CABIN FLOOR BEAM Y-765 HAS CORROSION FR64 TO FR66. REMOVED CORROSION ON AFT CABIN BEAM Y-765 FR64 TO FR66 L=1.3" W= 1.0" D=0.91" FOUND TO BE OUT OF LIMITS IAW SRM 51-41-15 REMOVED AND REPLACED BEAM Y-765 IAW SRM 51-42-11. EMP: V934143 WC: 58844 STA: ST ENG
- [SDR CALA2023070302127](https://openairdocs.org/sdr/CALA2023070302127.md): Floor Support · corroded · Jun 30, 2023 · N821UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR SILL AREA HAS SEVERAL AREAS OF CORROSION. REMOVED AND REPLACED COMPONENTS (SHEET-CONNECTION; PROFILE; SHEE T-THREHOLD) AT AFT CARGO DOOR SILL IAW SRM 51-42-11, REMOVED CORROSION AT AFT CARGO DOOR SILL FOIND WITHOUT ALLOWABLE DAMAGE IAW SRM 53-41
- [SDR CALA2023063002106](https://openairdocs.org/sdr/CALA2023063002106.md): Coupling · corroded · Jun 29, 2023 · N821UA · Airbus A319131 · Fuselage Structure (General)
  > AFT CARGO BILGE STR 43L ANGLE HAS CORROSION FR47/51. REMOVED AND REPLACED COUPLING P/N D5347100720490 BATCH# 00041310 38 RECEIVED. IAW. SRM 51-42-11/001, SRM 51-72-11-911-001, SRM 51 -49-00. EMP: V940362 WC: 58608 STA: ST ENG BFM.
- [SDR CALA2023063002105](https://openairdocs.org/sdr/CALA2023063002105.md): Door Sill · corroded · Jun 29, 2023 · N821UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR SILL AREA HAS SEVERAL AREAS OF CORROSION. REMOVED AND REPLACED COMPONENTS (SHEET-CONNECTION; PROFILE; SHEET-THREHOLD) AT AFT CARGO DOOR SILL IAW SRM 51-42-11, REMOVED CORROSION AT AFT CARGO DOOR SILL FOUND WITHOUT ALLOWABLE DAMAGE IAW SRM 53-41-
- [SDR CALA2023063002104](https://openairdocs.org/sdr/CALA2023063002104.md): Floorbeam · corroded · Jun 29, 2023 · N821UA · Airbus A319131 · Fuselage Main, Floor Beam
  > AFT CABIN FLOOR BEAM Y-765 HAS CORROSION FR64 TO FR66. REMOVED CORROSION ON AFT CABIN BEAM Y-765 FR64 TO FR66 L=1.3" W= 1.0" D=0.91" FOUND TO BE OUT OF LIMITS IAW SRM 51-41-15 REMOVED AND REPLACED BEAM Y-765 IAW SRM 51-42-11. EMP: V934143 WC: 58844 STA: ST ENG
- [SDR CALA2023063002103](https://openairdocs.org/sdr/CALA2023063002103.md): Skin · deformed · Jun 29, 2023 · N821UA · Airbus A319131 · Wing, Plate/Skin
  > RT WING AT #1 SLAT #3 TRACK FIXED L/E SKIN CUT-OUT DEFORMED/DENTED. EVALUATED DAMAGE IAW A319 SRM 57-41-11-263-009 AND FOUND OUT OF LIMITS AND REPIARED IAW A319 SRM 57-41-11-300-037. EMP: V934583 WC: 58329 STA: ST ENG BFM.
- [SDR CALA2023062802078](https://openairdocs.org/sdr/CALA2023062802078.md): Floorbeam · corroded · Jun 26, 2023 · N821UA · Airbus A319131 · Fuselage Main, Floor Beam
  > FLOOR BEAM Y765 UPPER SURFACE HAS SEVERAL SPOTS WITH CORROSION FR66 TO FR68 DOT 41-20
- [SDR CALA2023062802076](https://openairdocs.org/sdr/CALA2023062802076.md): Floor Support · corroded · Jun 26, 2023 · N821UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > A3NB-53-3-6038 MAIN CABIN FLOOR STR RH BET -Y254/Y254 FR 14-16 HAS CORROSION AND SCRATCHES REMOVED CORROSION ON RERAINER -Y81 ALL THICKNESS OF FLANGE. REMO VED AND REPLACED RETAINER -Y81 P/N D5311282900200 BATCH# 0001779 280. IAW SRM 51-74-00, SRM 53-11-14-10-
- [SDR CALA2023062602027](https://openairdocs.org/sdr/CALA2023062602027.md): Skin · dented · Jun 25, 2023 · N821UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > DENT ON LH UPPER FUSELAGE BETWEEN FR''S 45-46, STR''S13-14 D IS GREATER THAN.080", OUT OF LIMITS IAW SRM 53-31-11-283-002 NOTED, TRIMMED OUT DAMAGE & REP''D AREA PER SRM 53-00-11 PROTECTION AS REQ''D, INITIAL INSP THRESHOLD FROM TIME OF 5000FC/10000FH, METHOD
- [SDR CALA2023071702268](https://openairdocs.org/sdr/CALA2023071702268.md): Floor Support · corroded · Jun 23, 2023 · N821UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > FLOOR BEAM Y765 UPPER SURFACE HAS SEVERAL SPOTS WITH CORROSION FR66 TO FR68 DOT 41-20 REMOVED CORROSION IAW SRM 51-74-00 D: 0.045 OUT OF LIMITS IAW SR 51-75-12 SEE ATTACHMENT 44-0008 EMP#: V936322 WORK ACCOMPLISHED M 53-41-14-283-009, RECEIVE NEW PART, P/N D53
- [SDR CALA2023062101972](https://openairdocs.org/sdr/CALA2023062101972.md): Beam · corroded · Jun 19, 2023 · N821UA · Airbus A319131 · Fuselage Main, Structure
  > MAIN CABIN FLOOR BEAM UPPER SURFACE Y765 HAS A OUT OF LIMIT DENT AND CORROSION FR64 TO FR66 DOT 41-23 SEE LOG PAGE 4913899 FOR SIGNOFF.
- [SDR CALA2023061901924](https://openairdocs.org/sdr/CALA2023061901924.md): Seat Track · corroded · Jun 17, 2023 · N821UA · Airbus A319131 · Fuselage, Seat/Cargo Attach Fittings
  > A3NB-53-3-6038 MAIN CABIN FR 20 FLOOR STR -Y1292 HAS CORROSION D OT 102-192 MAIN CABIN SEAT TRACK -Y1292 BETWEEN FR 12 TO FR 24, WAS REPLACE D I.A.W A319 SRM 51-42-11 ATTACHED FORM 44-0008 EMP#: V934585 WO RK ACCOMPLISHED AT ST ENGINEERING OF MOBILE AT BFM ON
- [SDR CALA2023061901902](https://openairdocs.org/sdr/CALA2023061901902.md): Seat Track · corroded · Jun 16, 2023 · N821UA · Airbus A319131 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK Y1292 HAS CORROSION AND SCRATCHES FR62 TO FR65
- [SDR CALA2023061901901](https://openairdocs.org/sdr/CALA2023061901901.md): Floorbeam · corroded · Jun 16, 2023 · N821UA · Airbus A319131 · Fuselage Main, Floor Beam
  > A3NB-53-3-6038 MAIN CABIN FLOOR BEAM 7254-765 HAS CORROSION AT F R16
- [SDR CALA2023061901900](https://openairdocs.org/sdr/CALA2023061901900.md): Floorbeam · corroded · Jun 16, 2023 · N821UA · Airbus A319131 · Fuselage Main, Floor Beam
  > AA3NB-53-6038 MAIN CABIN LF FLOOR BEAM Y254 CORRODED AT FR 16
- [SDR CALA2023062301992](https://openairdocs.org/sdr/CALA2023062301992.md): Floorbeam · corroded · Jun 14, 2023 · N821UA · Airbus A319131 · Fuselage Main, Floor Beam
  > AA3NB-53-6038 MAIN CABIN LF FLOOR BEAM Y254 CORRODED AT FR 16 REMOVED CORROSION ON LH FLOOR BEAM Y254 AT FR16 TO 12 0.0760" AL L THICKNESS FOUND OUT LIMIT. REMOVED AND REPLACED OF FLOOR BEAM IAW SRM 53-11-14-283-007, SRM 51-74-00, SRM 51-42-11. EMP: V9403 62 W
- [SDR CALA2023062301991](https://openairdocs.org/sdr/CALA2023062301991.md): Floorbeam · corroded · Jun 14, 2023 · N821UA · Airbus A319131 · Fuselage Main, Floor Beam
  > A3NB-53-3-6038 MAIN CABIN FLOOR BEAM 7254-765 HAS CORROSION AT F R16 REMOVED CORROSION ON AREA DAMAGE AT TRACK ASSY Y503.2 AND FOUND REPLACED TRACK ASSY IAW SRM 51-75-12 AND REMOVED AND REINSTALLED OUT OF LIMITS IAW SRM 51-74-11. MEASURE: TRACK THICKNESS 0.160
- [SDR CALA2023052601655](https://openairdocs.org/sdr/CALA2023052601655.md): Frame · cracked · May 24, 2023 · N821UA · Airbus A319131 · Fuselage Main, Frame
  > WHILE PERFORMING ROTO INSPECTION OF LH FR 43 CRACK FOUND AT 9 O- CLOCK IN FRAME LAYER. REPAIR BEFORE NEXT FLIGHT REAMED LH FR 43 HOLE TO CRACK FREE AT 0.2810", REAMED HOLE AT 0. WORK ACCOMPLISHED AT ST ENGINEERING OF MOBILE AT BFM ON 3150" FOR INSTALL FREEZE
- [SDR CALA2022110403033](https://openairdocs.org/sdr/CALA2022110403033.md): Warning Message · false activation · Nov 4, 2022 · N821UA · Airbus A319131 · Fuel Controlling System
  > MAINTENANCE STATUS MESSAGE ENG 1 FADEC DISPLAYED ON THE LOWER EC AM SCREEN. NO MESSAGE SHOWN. ENG 1 FADEC CHANNEL A AND B TESTS PASSED.
- [SDR CALA2022071901811](https://openairdocs.org/sdr/CALA2022071901811.md): Actuator · warning message · Jul 19, 2022 · N821UA · Airbus A319131 · Compressor Bleed Valve
  > COMPRESSOR VANE DISPLAYED ON UPPER ECAM SCREEN. ENGINE PARAMETERS NORMAL. LOW SPEED ABORTED TAKEOFF. REMOVED AND REPLACED VARIABLE STATOR VANE (VSV) ACTUATOR. PERFORMED DRY MOTORING OF #1 ENG. LEAK CHECK PASSED. ACP TEST # 11 HIGH POWER ASSURANCE TEST, ACP 2 E
- [SDR CALA2021112202159](https://openairdocs.org/sdr/CALA2021112202159.md): Door · none · Nov 21, 2021 · N821UA · Airbus A319131 · Doors
  > ECAM..DOOR AVIONICSAAFT DOOR OPEN VERIFIED DOOR WAS CLOSED LOCKED WHEN CAME IN. APPLIE MEL VERIFIED DOOR IS LOCKED AND CLOSED APPLIED PLACCARD OK TO DEFER
- [SDR CALA2021050600620](https://openairdocs.org/sdr/CALA2021050600620.md): Stop Fitting · cracked · May 6, 2021 · N821UA · Airbus A319131 · Fuselage Main, Structure
  > R2 DOOR FRAME 68 AT STOP FITTING #1 AFT SIDE OF FRAME STR.22 IN UPPER RADIUS RADIUS. CRACK INDICATION RUNNING INBOARD TO OUTBOAR D. "CONTACT ENGINEERING FOR REPAIR INSTRUCTIONS BEFORE NEXT FLIG HT." PER HAECO LCQ N/R 9290296/20296 GENERATED BY V061633 COMPLETE
- [SDR CALA2021050600615](https://openairdocs.org/sdr/CALA2021050600615.md): Door Frame · cracked · May 5, 2021 · N821UA · Airbus A319131 · Fuselage Main, Structure
  > R2 DOOR FRAME 68 AT STOP FITTING #1 AFT SIDE OF FRAME STR.22 IN UPPER RADIUS RADIUS. CRACK INDICATION RUNNING INBOARD TO OUTBOAR D. "CONTACT ENGINEERING FOR REPAIR INSTRUCTIONS BEFORE NEXT FLIG HT." PER HAECO LCQ N/R 9290296/20296 GENERATED BY V061633 COMPLETE
- [SDR CALA2019042200622](https://openairdocs.org/sdr/CALA2019042200622.md): Bulkhead Web · cracked · Apr 19, 2019 · N821UA · Airbus A319131 · Fuselage Main, Bulkhead
  > L/H SIDE PRESSURE PANEL BTW FR35-36, ROTO PROBE INSP SHOWS CRACK INDICATION IN FASTENER HOLES OUTSIDE THE CUTOUT AREA. CONTACT ENGINEERING FOR REPAIR INST AND REPAIR BEFORE NEXT FLIGHT. REPAIRED HOLES 4,5,7,10 AND 11 IAW ECRA 5331-02353. ACCOMPLISH THE PERMANE
- [SDR CALA2019041900613](https://openairdocs.org/sdr/CALA2019041900613.md): Frame · cracked · Apr 18, 2019 · N821UA · Airbus A319131 · Fuselage Main, Frame
  > CRACK INDICATION IN FRAME LAYER AT FR16 L/H SIDE HOLE "D" REPAIR L/H FR16 CROSSBEAM BEFORE NEXT FLIGHT PER STEP 6 ACCOMPLISHED INTERIM REPAIR ON FRAME LAYER AT FR16 L/H HOLE D PER ECRA 5311-02131 PART 1, ACCOMPLISH INSPECTION REQUIREMENTS PER PART 2 OF ECRA 53
- [SDR CALA2019041200561](https://openairdocs.org/sdr/CALA2019041200561.md): Frame · cracked · Apr 9, 2019 · N821UA · Airbus A319131 · Fuselage Main, Frame
  > RH AFT PAX DOOR CUTOUT FR68 UPPER CORNER AT STR8, RADIUS ON FRAME HAS A CRACK INDICATION REPAIRED FR68 UPPER CORNER AT STR8 RH AFT PAX DOOR CUTOUT IAW A319 SRM 53-41-12-300-012, INSPECTION OF THE REPAIR PART TRANSVERSAL FLANGE FOR LINTEL ATTACHMENT EXTERNAL SU
- [SDR CALA2019040500542](https://openairdocs.org/sdr/CALA2019040500542.md): Window Post · cracked · Apr 5, 2019 · N821UA · Airbus A319131 · Fuselage Main, Structure
  > RH WINDSHIELD SIDE POST AT FR4 LOWER ATTACHMENT, AFT LOWER WEB CRACKED REPAIRED RH WINDSHIELD SIDE POST AT FR4 LOWER ATTACHMENT IAW ECRA 5311-02117 PART 1. ACCOMPLISHED A PERMANENT REPAIR PER PART 3 OF ECRA 5311-02117
- [SDR CALA2018100802083](https://openairdocs.org/sdr/CALA2018100802083.md): Control Panel · inoperative · Oct 8, 2018 · N821UA · Airbus A319131 · Weather Radar System
  > WEATHER RADAR SYSTEM INOP - NAV FOUND RADAR WOULD NOT TILT REPLACED RADAR CONTROL PANEL REF AMM TASK 34-41-12 AND RADAR TILTS AND BITE TEST NORMAL ROTABLE PARTS CHANGE WAS INDICATED - TT 1202201 SN OFF 4456 PANEL, WX RADAR OFF 31-3416-9-9002 4456 ON 31-3416-9-

Next page: https://openairdocs.org/aircraft/N821UA/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 = 'N821UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N821UA/reports

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