# Service difficulty reports: N826UA

A list on [N826UA](https://openairdocs.org/aircraft/N826UA.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 · 130 reports

- [SDR CALA2026062917376](https://openairdocs.org/sdr/CALA2026062917376.md): Battery · inoperative · Jun 26, 2026 · N826UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY LIGHTS TEST FAILS RECEIVED FAULT MESSAGE EPSU UNIT FWD L REMOVED AND REPLACED FWD L EPSU BATTERY OPS CHECK GOOD REF AMM 33-51-38
- [SDR CALA2026042415685](https://openairdocs.org/sdr/CALA2026042415685.md): Servo Valve · faulted · Apr 22, 2026 · N826UA · Airbus A319131 · Landing Gear Brake System
  > AUTO BRAKES FAULT ON ECAM. POST FLIGHT REPORTED FAILED BRAKE NORMAL SERVO VALVE 16GG FAILED REMOVED AND REPLACED NORMAL BRAKE SERVO VALVE PER AMM 32-42-48-400-001-A, PERORMED OPS CHECK PER AMM 32-42-00-720-005-A, OPS CHECK GOOD, AND FONCTIONAL TEST OF TECHOMET
- [SDR CALA2026012713348](https://openairdocs.org/sdr/CALA2026012713348.md): Wire · detached · Jan 26, 2026 · N826UA · Airbus A319131 · Light System Wiring
  > EMERGENCY LIGHT BULB NEAR AISLE UNDER SEAT 31C BURNT OUT. REMOVED AND REPLACED LIGHT MODULE. OPS CHECK FAILED. FOUND WIRING PULLED OUT OF CONNECTOR. TERMINATED EMERGENCY LIGHTING WIRE AND MOLEX CONNECTOR IAW ESPM 20-44. REPLACED SEAT MOUNTED EMERGENCY LIGHTI
- [SDR CALA2026012713331](https://openairdocs.org/sdr/CALA2026012713331.md): Fuel Cap · missing · Jan 23, 2026 · N826UA · Airbus A319131 · Fuel Storage
  > FUEL CAP MISSING. CHECKED COUPLING FOR LEAKS, NO LEAKS AT THE COUPLING. INSTALLED A FUEL CAP IAW MM 28-25-41. SECURED ATTACHMENT LANYARD, NO DEFECTS NOTED.
- [SDR CALA2026012313191](https://openairdocs.org/sdr/CALA2026012313191.md): Fuel Cap · missing · Jan 20, 2026 · N826UA · Airbus A319131 · Fuel Storage
  > CREW REPORTED FUEL CAP MISSING AFTER FUELING. FUEL REPORTS NO CAP ON ARRIVAL TO AIRCRAFT INFO NOTED, SEE LOG PAGE FOR MEL.
- [SDR CALA2025120211698](https://openairdocs.org/sdr/CALA2025120211698.md): Fitting · broken · Nov 28, 2025 · N826UA · Airbus A319131 · Elevator Miscellaneous Structure
  > UPON INSTALLATION OF LT ELEVATOR OTBD ELEVATOR SERVO. FOUND BROKEN TAB ON ELEVATOR SIDE. TECHNICIAN WAS CLEANING FLUID IN AREA WHEN THE TAB BROKE OFF & FELL INTO THE LIFT. UPON CLOSER INSPECTION GLUE WAS FOUND ON TAB. TAB IS PART OF THE FITTING TO HOLD COTTE
- [SDR CALA2025110610964](https://openairdocs.org/sdr/CALA2025110610964.md): Fuel Cap · missing · Nov 3, 2025 · N826UA · Airbus A319131 · Fuel Storage
  > FUELER REPORTS FUEL CAP IS MISSING FROM AIRCRAFT. INSTALLED A NEW FUEL CAP IAW AMM 28-25-41.
- [SDR CALA2025102010305](https://openairdocs.org/sdr/CALA2025102010305.md): Light · malfunctioned · Oct 20, 2025 · N826UA · Airbus A319131 · Passenger Compartment Lighting
  > CABIN ENTRY LIGHT NEAR DOOR 1R FLASHES RED INTERMITTENTLY RESET LIGHTS FOR FWD ENTRY DOOR, PROFORMED OPS CHECK REF AMM 33-21-00-710-001-A, NO FAULTS NOTED, OK TO CONTINUE.
- [SDR CALA2025101410072](https://openairdocs.org/sdr/CALA2025101410072.md): Channel · delaminated · Oct 13, 2025 · N826UA · Airbus A319131 · Wing Miscellaneous Structure
  > L/H AILERON HAS COMPOSITE DAMAGE ON TOP T/E. REPAIRED DAMAGED COMPOSITE IAW A319 SRM 51-77-12-911-002 RMVD AND RPLD AILERON TRAILING EDGE CHANNEL IAW A319 SRM 51-42-11 CMM 57-61-21 SRM 51-72-11 CAT A.
- [SDR CALA2025082708171](https://openairdocs.org/sdr/CALA2025082708171.md): Switch · out of position · Aug 26, 2025 · N826UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS ONUNABLE TO TURN OFF LIGHT SWITCH WAS IN THE WRONG POSITION. EMERGENCY LIGHTS WORKING NORMALLY OK TO CONT.
- [SDR CALA2025080507338](https://openairdocs.org/sdr/CALA2025080507338.md): Toilet · malfunctioned · Aug 3, 2025 · N826UA · Airbus A319131 · Waste Disposal System
  > FWD AFT LAV TOILET OVERFLOWED DURING CLIMB SENDING WATER INTO AF T AFT LAV AND AFT GALLEY. UPON INITIAL INSPECTION FOUND TOILET FULL OF LIQUID. FLUSHED TOILET TO CHECK FLUSH VALVE, NO EVIDANCE OF LEAKING FROM FLUSH VALVE, SUSPECT FILL SIDE OF SYSTEM. FOUND LA
- [SDR CALA2025041703929](https://openairdocs.org/sdr/CALA2025041703929.md): Unknown · odor · Apr 15, 2025 · N826UA · Airbus A319131 · Air Distribution System
  > FLT ATTS REPORTED CABIN AIR SMELLED LIKE ROTTEN EGGS AT BEGINNI NG OFDESCENT AND DOWN PER FLIGHT ATTENDANT DEBRIEF, AT TOP OF DESCENT FWD CABIN ONLY SMELLED STRONGLY OF SULFUR. WENT AWAY AFTER PARKING AT GATE. PER PILOTS NO SMELL NOTED IN FLIGHT DECK AT ANY P
- [SDR CALA2025041103714](https://openairdocs.org/sdr/CALA2025041103714.md): Outflow Valve · faulted · Apr 9, 2025 · N826UA · Airbus A319131 · Pressure Regulator/Outflow Valve
  > VENT BLOWER/EXTRACT FAULT ON TAKEOFF ROLL. REF L/P 4453445. 21-26-53 SKIN AIR OUTLET VAVLE CALL OUT AFTER AEVC TEST REMOVED AND REPLACED SKIN AIR OUTLET VALVE PER AMM 21-26-53. PERFORMED OPS CHECK PER AMM 21-26-00-710-001A. TEST OK.
- [SDR CALA2024121301500](https://openairdocs.org/sdr/CALA2024121301500.md): Fan · faulty · Dec 10, 2024 · N826UA · Airbus A319131 · Air Distribution Fan
  > GRINDING NOISE AND HOT FRICTION SMELL FROM FRONT LOWER FRONT OF AIRCRAFT. LASTED 2 MIN THEN UPON INSPECTION FOUND VENT BLOWER FAN 20HQ VIBRATING WITH STRONG ELEC SMELL IN MAIN AVIONICS BAY. ITEM HAD HISTORY OF CB TRIPPING EARLIER THIS MORNING. SMOKE FORM ATTAC
- [SDR CALA2024110400989](https://openairdocs.org/sdr/CALA2024110400989.md): Unknown · odor · Nov 2, 2024 · N826UA · Airbus A319131 · Air Distribution System
  > F/A RPTS BURNING RUBBER ODOR FRM AFT GALLEY AFTER PARKING AT GAT E ADDING PICTURES OF FORM. ADD PERFOMED INSPECTIONS ON APU AND ACTIVATED APU BLEED AIR. RAN AIR PACKS, CHILLERS, AND OVENS. ALL FUNCTION NORMALLY. NO CIRCUIT BREAKERS ARE POPPED. THERE WAS NO OIL
- [SDR CALA2024101000807](https://openairdocs.org/sdr/CALA2024101000807.md): Plate · broken · Oct 8, 2024 · N826UA · Airbus A319131 · Leading Edge Devices
  > PDA 2 REF LOG PAGE 9490433, A PORTION OF THE LEFT WING #2 SLAT INBOARD CLOSING PLATE WAS MISSING ON ARRIVAL INTO RDM ON FLIGHT 2082. THE MISSING PLATE WAS PLACED ON CDL 27B. SEE LOG PAGE 9490433.
- [SDR CALA2024012500231](https://openairdocs.org/sdr/CALA2024012500231.md): Tape · separated · Jan 23, 2024 · N826UA · Airbus A319131 · Flight Compartment Windows
  > TAPE APPLIED CAPT AFT WINDOW SEPARATED, TAPE APPLIED TO CAPT SIDE WINDOW THAT IS COVERING SEALANT HAS COME LOOSE AND IS FLAPPING. NOISE ASSOCIATED. CABIN PRESS OK. NO PRESSURIZATION ISSUES, NOISE ASSOCIATED WITH TAPE. TORQUED, SEALED AND REMOVED TAPE ON L3 WIN
- [SDR CALA2023122103704](https://openairdocs.org/sdr/CALA2023122103704.md): Skin · dented · Dec 18, 2023 · N826UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > AFT FUSELAGE 4EA DENTS AROUND TAIL JACKING POINT, REQUIRING EVALUATIONS. REPAIR 04EA DENTS AROUND TAIL JACKING POINT DOOR FR73 AND FR74 B STA: ST ENG BFM. REF ELB 7404529 FOR DMG. BETWEEN STGRS 31RH AND 31LH PER EC/RA 5351-01220, FOUND REPAIR IS PERMANENT REPA
- [SDR CALA2023122003697](https://openairdocs.org/sdr/CALA2023122003697.md): Fitting · cracked · Dec 18, 2023 · N826UA · Airbus A319131 · Flight Compartment Windows
  > LEFT & RIGHT WINDSHIELD CONTINUITY FITTINGS FOUND TO BE CRACKED DUR ING HFEC INSPECTION. REMOVED AND REPLACED LT & RT WINDSHIELD CONTINUITY FITTING PER PER EC/RA 5311-03129 PART 1 STEP 2.
- [SDR CALA2023122003694](https://openairdocs.org/sdr/CALA2023122003694.md): Skin · dented · Dec 18, 2023 · N826UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > RIGHT EXTERNAL FUSELAGE SKIN FR25-26 STR 41R-42R HAS 2EA DENTS. REPAIRED RT EXTERNAL FUSELAGE SKIN BETWEEN FR25-26 AND 241R-42R. PER EC/RA # 5321-02124 REV ORIGINAL AND FINAL EA 319-5321-13-A34 55 REV -.
- [SDR CALA2023120503558](https://openairdocs.org/sdr/CALA2023120503558.md): Skin · gouged · Nov 30, 2023 · N826UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > DENT WITH GOUGE FOUND AT FR23 BETWEEN STR42 AND 43RH DURING HMV AT VTAERO ON NR80072. IAW SRM53-11-11-300-041. THIS IS A CAT B REPAIR WITH REINP REQ''D REPAIR EMBODIMENT. WHICHEVER COMES FIRST, SUBSEQUENT INSP TBD. IAW SRI53-11-11-205-037 IN ZONE 1 AT 60000FC
- [SDR CALA2023111703420](https://openairdocs.org/sdr/CALA2023111703420.md): Fitting · corroded · Nov 15, 2023 · N826UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > FWD CABIN, L1 DOOR SILL, MID FITTING IS CORRODED AROUND FASTENER S HOLE. () REMOVE CORROSION AROUND FASTENERS HOLES L=.925", W=.875", D=.062 CHED FORM: 44-0008 WORK ACCOMPLISHED AT ST ENGINEE " REWORK 51% OF THICKNESS, REMOVED L1 DOOR SILL, MID FITTING AND RIN
- [SDR CALA2023111503366](https://openairdocs.org/sdr/CALA2023111503366.md): Fitting · corroded · Nov 9, 2023 · N826UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > MAIN CABIN THRESHOLD AT R1 DOOR CUT OUT, FLOOR PANEL SUPPORT STR HAS CORROSION AT FASTENER HOLES. DOT 102-252 () REPLACED CENTER FITTING P/N: D5311219820106 BTCH: 0002527532 IAW A319 SRM 51-42-11.
- [SDR CALA2023111503364](https://openairdocs.org/sdr/CALA2023111503364.md): Seat Track · corroded · Nov 9, 2023 · N826UA · Airbus A319131 · Fuselage Structure (General)
  > CABIN FOOR SEAT TRACK Y1292 FRAME 24 TO 35 SEVERIAL POINTS OF CORROSION. () REMOVED AND REPLACED SEAT TRACK Y1292 AT MAIN CABIN BETWEEN LH FR24 TO FR35 IAW SRM 51-42-11.
- [SDR CALA2023111503362](https://openairdocs.org/sdr/CALA2023111503362.md): Stringer · corroded · Nov 9, 2023 · N826UA · Airbus A319131 · Fuselage Main, Longeron/Stringer
  > UNDER R1 SCUFF PLATE FR 16 CORNER STR HAS CORROSION. DOT 102-141 () REPLACED FWD CORNER FITTING P/N D5311222320104 BTCH: 0004192306 IAW A319 SRM 51-42-11
- [SDR CALA2023110803312](https://openairdocs.org/sdr/CALA2023110803312.md): Skin · corroded · Nov 2, 2023 · N826UA · Airbus A319131 · Trailing Edge Flaps
  > RIGHT WING O/B FLAP T/E AFT OF #3 TRACK LOWER EDGE HAS EXFOILATI NG CORROSION AT PREVIOUS REPAIR. DOT 102-139 () REPAIRED R/H O/B FLAP T/E AFT OF #3 TRACK, LOWER SKIN, I.A.W. SR M 57-53-00-300-120 AND SRM 51-77-11-911 SEE FORM: 44-0008
- [SDR CALA2023110803314](https://openairdocs.org/sdr/CALA2023110803314.md): Skin · delaminated · Nov 1, 2023 · N826UA · Airbus A319131 · Elevator, Plate/Skin
  > DURING THERMOGRAPHIC INSPECTION AND TAP TEST OF LH ELEVATOR NDT NOTED INDICATION OF WATER INGRESS AROUND THE 12TH FASTENER FROM I/B EDGE. AREA OF CONCERN IS CIRCLED IN RED AND MARKED WITH AN '' X''. () REPAIRED L/H ELEVATOR T/E, I.A.W. SRM 55-21-11-300-005, AN
- [SDR CALA2023110803313](https://openairdocs.org/sdr/CALA2023110803313.md): Skin · delaminated · Nov 1, 2023 · N826UA · Airbus A319131 · Elevator, Plate/Skin
  > DURING THERMOGRAPHIC INSPECTION AND TAP TEST OF RH ELEVATOR NDT NOTED INDICATION OF WATER INGRESS AROUND A TRAILING EDGE FASTENE R AT THE 6TH FROM OUTBOARD. WATER INDICATION CIRCLED IN RED WITH A ''X'' DRAWN THROUGH IT. () REPAIRED R/H ELEVATOR T/E I.A.W. SRM
- [SDR CALA2023110803310](https://openairdocs.org/sdr/CALA2023110803310.md): Floorbeam · corroded · Nov 1, 2023 · N826UA · Airbus A319131 · Fuselage Main, Floor Beam
  > FWD CABIN FLOOR SUPPORT STRUCTURE HAS CORROSION LOC. FR 16, +Y 1 300. () FWD CABIN FLOOR SUPPORT FOUND DAMAGE OUT OF LIMITS, REMOVED, REP LACED FLOOR SUPPORT P/N D5311281300251 BTCH 0003979250 IAW SRM 5 1-42-11.
- [SDR CALA2023102303145](https://openairdocs.org/sdr/CALA2023102303145.md): Floor Support · corroded · Oct 20, 2023 · N826UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > FWD CABIN FLOOR SUPPORT STRUCTURE HAS CORROSION LOC. FR 16, +Y40 0. () REMOVED AND REPLACED 1EA FLOOR BEAM BETWEEN LH FR 12 TO FR 16 IA W SRM 51-42-11 ATTACHED FORM 44-0008 EMP#: V935975 WORK ACCOMPLISHED AT ST ENGINEERING OF MOBILE AT BFM ON NR#: 79858
- [SDR CALA2023102303141](https://openairdocs.org/sdr/CALA2023102303141.md): Seat Track · corroded · Oct 19, 2023 · N826UA · Airbus A319131 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN FOOR SEAT TRACK -Y765 FRAME 24 TO 35 SEVERAL POINTS OF CORROSION. () REMOVED CORROSION ON AREA AND FOUND OUT OF LIMITS I.A.W SRM 53-2 1-15-283-004. REMOVED AND REPLACED SEAT TRACK -Y765 FR 24 TO 35 I.A.W SRM 51-72-11 WORK ACCOMPLISHED AT ST ENGINEERING O
- [SDR CALA2023102003128](https://openairdocs.org/sdr/CALA2023102003128.md): Seat Track · corroded · Oct 18, 2023 · N826UA · Airbus A319131 · Fuselage, Seat/Cargo Attach Fittings
  > FWD CABIN FLOOR SUPPORT STRUCTURE HAS CORROSION LOC. FR16 +Y 600. REMOVED AND REPLACED SEAT TRACK Y765 BETWEEN FR12 TO FR24 IAW SR M 51-42-11. EMP: V935975 WC: 79857 STA: ST ENG BFM
- [SDR CALA2022091602394](https://openairdocs.org/sdr/CALA2022091602394.md): Fuel Cap · missing · Sep 15, 2022 · N826UA · Airbus A300* · Aircraft Fuel System
  > THIS IS A SUPPLEMENTAL REPORT FOR THE SAME CONTROL NUMBER SUBMITTED ON 9/16/22. PDA 3 FUELER REPORTS FUEL CAP LANYARD IS MISSING. REPLACED FUEL CAP LANYARD.
- [SDR CALA2022052501348](https://openairdocs.org/sdr/CALA2022052501348.md): None · missing · May 24, 2022 · N826UA · Airbus A300* · Placards and Markings
  > THIS IS A SUPPLEMENTAL REPORT FOR THE SAME CONTROL NUMBER GENERATED ON 5/25/22. SERVICING CHART RH MAIN LANDING GEAR MISSING GEAR SHOCK STRUT. REMOVED AND REPLACED WITH SERVICEABLE PLACARD.
- [SDR CALA2021110302027](https://openairdocs.org/sdr/CALA2021110302027.md): Skin · none · Nov 2, 2021 · N826UA · Airbus A319131 · Fuselage Structure (General)
  > DENT ALONG STRINGER 22L BETWEEN FRAME 21 AND 23 REQUIRES REPAIR PER 9290286/44286 GEN BY V079529 REPAIRED DENT ALONG STRINGER 22L BTWN FRAME 21 AND 23 IAW A319 S V079529 INSP BY V898117 RM 53-11-11-300-041 FIG.002 SHEET 01 THIS REPAIR IS CONSIDER CAT EGORY B P
- [SDR CALA2021102901991](https://openairdocs.org/sdr/CALA2021102901991.md): Beam · cracked · Oct 27, 2021 · N826UA · Airbus A319131 · Doors
  > R/H EMER EXIT AFT AND FWD FRAME WEB CRACKED PER 9290245/44245 GE N BY V077960 REMOVED AND REPLACED R/H EMERGENCY EXIT FWD AND AFT FRAME WEB TO P COATED AND CIC''D IAW A319 SRM 51-72-11-911-001,51-44-11/001,51 -75-12-911-002 BY MECH V079529 INSP BY V898117
- [SDR CALA2021102901990](https://openairdocs.org/sdr/CALA2021102901990.md): Frame · cracked · Oct 27, 2021 · N826UA · Airbus A319131 · Doors
  > L/H EMER. EXIT AFT AND FWD FRAME WEB CRACKED PER 9290244/44244 G EN BY V077960 REMOVED AND REPLACED LOCATED DRILLED DEBURRED INSTALLED AND TOP COATED LEFT HAND EMERGENCY EXIT FWD AND AFT FRAME WEB IAW SRM 51 -72-11-911-001,51-44-11,51-21-11,51-75-12-911-002 BY
- [SDR CALA2021083001450](https://openairdocs.org/sdr/CALA2021083001450.md): Indicator · false indication · Aug 30, 2021 · N826UA · Airbus A319131 · Hydraulic Indicating System
  > ECAM CAUTION MESSAGE - Y RSVR LO LVL MESSAGE INOP - HYD AFTER TAKEOFF GOTHYD Y RSVR LO LVL ECAM. COULD NOT DUPLICATE ECAM Y RSVR LO LVL WITH YELLOW ELE PUMP. RAN #2 ENG YELLOW HYD PUMP PER TSM 52-36-00-810-805-A OPS CHECK GOOD. R&R LOW LEVEL SWITCH AND QUANT
- [SDR CALA2021072801209](https://openairdocs.org/sdr/CALA2021072801209.md): Panel · missing · Jul 28, 2021 · N826UA · Airbus A319131 · Escape Slide
  > PDA 3 REF LOG PAGE 6736380. LEFT OVERWING SLIDE PANEL HAS PIECE OF THE SKIN MISSING. CLOSED PARENT LOG PAGE. NO NEED FOR DUPLICATE LOG. UPDATING THIS LOG PAGE WITH PICTURES OF DAMAGE TO LEFT OVER WING SLIDE. REPLACED L-H OFFWING ESCAPE SLIDE AND OPS CK''D GO
- [SDR CALA2019101801774](https://openairdocs.org/sdr/CALA2019101801774.md): Pressure Panel · cracked · Oct 16, 2019 · N826UA · Airbus A319131 · Fuselage Main, Structure
  > LH PRESSURE PANEL BETWEEN FRAME 35-36 HOLE 2,4,13,14,15,16,21,23,24,25,26,27 AND 28 ARE CRACKED IN THE PRESSURE PANEL CONTACT EN GINEERING FOR INSTRUCTIONS AND REPAIR BEFORE NEXT FLIGHT AD 2018 -06-04 PER LCQ NON ROUTINE 9292324. LH PRESSURE PANEL AT FR35-36
- [SDR CALA2019101801773](https://openairdocs.org/sdr/CALA2019101801773.md): Fitting · cracked · Oct 16, 2019 · N826UA · Airbus A319131 · Fuselage Main, Attach Fittings
  > RH PRESSURE PANEL BETWEEN FRAME 35-36 HOLE #7 IS CRACKED IN FITT ING ABOVE PRESSURE PANEL CONTACT ENGINEERING FOR REPAIR BEFORE N EXT FLIGHT AD 2018-06-04 PER LCQ NON ROUTINE 9292328. REMOVED AND REPLACED R/H CORNER FITTING FR36 IAW A319 SRM 51-42- 11 PARA 2F
- [SDR CALA2019101801772](https://openairdocs.org/sdr/CALA2019101801772.md): Fitting · cracked · Oct 16, 2019 · N826UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > LH PRESSURE PANEL BETWEEN FRAME 35-36 HOLE #7 IS CRACKED IN THE FITTING ABOVE THE PRESSURE PANEL CONTACT ENGINEERING FOR INSTRUC TIONS AND REPAIR BEFORE NEXT FLIGHT AD 2018-06-04 PER LCQ NON ROUTINE 9292325. REMOVED AND REPLACED L/H CORNER FITTING FR36 IAW A3
- [SDR CALA2019101801762](https://openairdocs.org/sdr/CALA2019101801762.md): Skin · dented · Oct 14, 2019 · N826UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > AFT UPPER L/H TAIL SECTION OF FUSELAGE HAS DENT/CREASE ON SURFAC E BETWEEN FR 72-FR73 STRGRS 6L-8L A3NB-05-3-6062 PER HAECO LCQ N R 9292189 GENERATED BY V901665 DURING C-2 HAECO LCQ TECHNICIAN V892069 AND QC LC-32 REPAIRED DE NT INSTALLING REPAIR DOUBLER L=1.5
- [SDR CALA2019100501700](https://openairdocs.org/sdr/CALA2019100501700.md): Gusset · damaged · Oct 2, 2019 · N826UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > RH FR68 ON 3RD GUSSET FROM THE TOP ON BOTTOM HOLE HAS REJECTABLE DAMAGE INDICATION. REPAIR REQUIRED PRIOR TO NEXT FLIGHT CYCLE S UPPORT TASK AD RELATED (2015-05-02) PER HAECO LCQ NR 9292205 GEN ERATED BY V916887 REPLACED GUSSET ON R2 PASSENGER DOOR AT FR68 STR
- [SDR CALA2019093001668](https://openairdocs.org/sdr/CALA2019093001668.md): Intercostal · cracked · Sep 29, 2019 · N826UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > RH FR16 DOOR STOP 7 LOWER INBOARD HOLE HAS CRACK INDICATION SUSP ECTED TO BE IN INTERCOSTAL REPAIR REQUIRED PRIOR TO NEXT FLIGHT CYCLE A3NB--53-4-6304 AS RELATED TASK (2018-25-02) PER HAECO LCQ NR 9292191 GENERATED REMOVED NAD REPLACED #7 DOOR STOP INTERCOSTAL
- [SDR CALA2019031500411](https://openairdocs.org/sdr/CALA2019031500411.md): Actuator · leaking · Mar 13, 2019 · N826UA · Airbus A319131 · Stabilizer Actuator
  > (SUPPORT TASK) REMOVE AND REPLACE THE THSA. REFER TO N/R: 96 17583. CHANGED DUE TO A LEAK. REMOVED & REPLACED THSA IAW AMM 27-44-51-000-001-A & 27-44- 51-400-001. OPS CHECK GOOD NO DEFECTS NOTED IAW AMM 27-41-0 0-730-001. REFER TO N/R: 9617583. WORK PERFORMED.
- [SDR CALA2018022100729](https://openairdocs.org/sdr/CALA2018022100729.md): Power Supply · no test · Feb 21, 2018 · N826UA · Airbus A319131 · Emergency Lighting
  > RT OVERWING EPSU FAILED TO TEST. FOUND RIGHT POWER SUPPLY AT FAULT. REPLACED THE EPSU IAW AMM 33-51-38-400-001. PERFORMED BITE TEST AND FOUND EMERGENCY LIGHTS OPS CKS GOOD.
- [SDR CALA2018022100728](https://openairdocs.org/sdr/CALA2018022100728.md): Battery · inoperative · Feb 21, 2018 · N826UA · Airbus A319131 · Emergency Lighting
  > WITH EMERGENCY LIGHT SWITCH ARMED, AND POWER OFF AIRCRAFT, EMERGENCY LIGHTS BY DOOR 1L AND 1R DO NOT ILLUMINATE. REPLACED THE BATTERY. OPS GOOD.
- [SDR CALA2017092203298](https://openairdocs.org/sdr/CALA2017092203298.md): Cylinder · low pressure · Sep 22, 2017 · N826UA · Airbus A319131 · Escape Slide
  > RIGHT OVERWING SLIDE RESERVOIR CYLINDER PRESSURE IN THE RED BAND. REMOVED AND REPLACED THE CYLINDER IAW AMM 25-62-46-000-001-A, AND 25-62-46-400-001-A. OP CHECKED GOOD.
- [SDR CALA2017092203267](https://openairdocs.org/sdr/CALA2017092203267.md): Housing · corroded · Sep 19, 2017 · N826UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > FWD CARGO POTABLE WATER VALVE INTERNAL HOUSING, FRAMES 28 - 29 STRINGERS 42 - 44L HAS CORROSION. REMOVED CORROSION AND FOUND TO BE BEYOND LIMITS IAW DWG D53230935. REMOVED AND REPLACED THE HOUSING IAW SRM 51-42-11-001, AND 51-44-11-0 01.

Next page: https://openairdocs.org/aircraft/N826UA/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 = 'N826UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N826UA/reports

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