# Service difficulty reports: N848UA

A list on [N848UA](https://openairdocs.org/aircraft/N848UA.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 · 114 reports

- [SDR CALA2026100820218](https://openairdocs.org/sdr/CALA2026100820218.md): Access Panel · damaged · Oct 7, 2026 · N848UA · Airbus A319131 · Wing, Plate/Skin
  > DURING REMOVAL OF ACCESS PANEL 540KB, ACFT SKIN WAS DAMAGED. EXCEEDED LIMITS OF SRM 57-21-11-300-002, INTERIM REPAIR PERFORMED TO FUEL ACCESS PANEL 540KB IAW PART 1 OF ECRA 5721-01445. ACCOMPLISH PERMINATE REPAIR AT LT WING BOTTOM FUEL ACCESS PANEL 540KB HO
- [SDR CALA2026100520071](https://openairdocs.org/sdr/CALA2026100520071.md): Light · disconnected · Oct 2, 2026 · N848UA · Airbus A319131 · Light System Wiring
  > EMERGENCY LIGHTS AT SEATS 27C AND 28C WILL NOT ILLUMINATE. FOUND LIGHT ASSEMBLIES AT SEATS 27C AND 28C TO BE DISCONNECTED. CONNECTED LIGHTING ASSEMBLIES AND PERFORMED OPS CHECK IAW AMM 33-51-00. OPS CHKD GOOD.
- [SDR CALA2026090119175](https://openairdocs.org/sdr/CALA2026090119175.md): Power Supply · no test · Aug 30, 2026 · N848UA · Airbus A319131 · Emergency Lighting
  > DURING 2SC TEST, EMERGENCY LIGHT TEST ON TEST PANEL (PTP) 110RH, FOUND EPSU BATTERY AFT LT STATUS MESSAGE. PER TSM 33-51-00-810-802-A PERFORMED TEST OF THE EPSU IAW AMM 33-51-00-710-006-A. OPS CHECKED GOOD. PERFOMED EMERGENCY LIGHT TEST IAW AMM 33-51-00-710-0
- [SDR CALA2026090119174](https://openairdocs.org/sdr/CALA2026090119174.md): Light · no test · Aug 30, 2026 · N848UA · Airbus A319131 · Emergency Lighting
  > DURING 2SC TEST, EMERGENCY LIGHT SYS TEST ON TEST PANEL (PTP) 110RH, FOUND EPSU BATTERY FWD LT STATUS MESSAGE IAW TSM 33-51-00-810-802-A, PERFORMED TEST OF THE EPSU IAW AMM 33-51-00-710-006-A. OPS CHKD GOOD. PERFOMED EMERGENCY LIGHT TEST IAW AMM 33-51-00-7
- [SDR CALA2026020213481](https://openairdocs.org/sdr/CALA2026020213481.md): Fuel Cap · missing · Jan 26, 2026 · N848UA · Airbus A319131 · Fuel Storage
  > BEFORE FURTHER FLIGHT AN SDR REPORT MUST BE FILED FOR MISSIN FUEL CAP SDR FILE REFER LP 7725293
- [SDR CALA2025122412424](https://openairdocs.org/sdr/CALA2025122412424.md): Battery · failed · Dec 23, 2025 · N848UA · Airbus A319131 · Emergency Lighting
  > EPSU BATTERY EMERGENCY LIGHT FAILED. EPSU BATTERY WAS REPLACED IAW AMM 33-51-38-000-002-A0, & 33-51-38-400-002-A0.
- [SDR CALA2025081407712](https://openairdocs.org/sdr/CALA2025081407712.md): Light · malfunctioned · Aug 11, 2025 · N848UA · Airbus A319131 · Emergency Lighting
  > FOUND FLOOR EMERGENCY LIGHT ROW 28 INOP ALL ADJACENT LIGHTS OPERATE NORMALLY. PLACE INOP LIGHT ON MEL INSPECTED FLOOR EMERGENCY LIGHT ROW 28 NOT ABLE TO DUPLICATE FAULT ON GROUND AT THIS TIME, FLOOR EMERGENCY LIGHT ILLUMINATE NORMAL. OK TO CONTINUE.
- [SDR CALA2025081307680](https://openairdocs.org/sdr/CALA2025081307680.md): Door · no discrepancy · Aug 11, 2025 · N848UA · Airbus A319131 · Standard Practices/Structures
  > LEFT OVERWING EMERGENCY DOOR HATCH OPENED TO COMPLETE TURBULANCE INSPECTION. INSTALLED LT OVERWING EMERGENCY DOOR IN REF TO AMM 52-21-11. RENDER SAFE EMERGENCY SLIDE CHECKLIST COMPLETED. DOOR SECURE AND SLIDE HAS BEEN REACTIVATED IN REF TO AMM. RII INSPECTION
- [SDR CALA2025063006078](https://openairdocs.org/sdr/CALA2025063006078.md): Water System · leaking · Jun 23, 2025 · N848UA · Airbus A319131 · Wash Water System
  > WATER SOAKING CARPET AFT 3 ROWS. RAMP FOUND WATER LEAKING INSIDE AFT CARGO BIN.
- [SDR CALA2024111802887](https://openairdocs.org/sdr/CALA2024111802887.md): Stringer · damaged · Nov 13, 2024 · N848UA · Airbus A319131 · Fuselage Main, Longeron/Stringer
  > FR68 STR8 REPAIR CORNER FITTING P/N: D53480041210 REQUIRES NEW R EPLACEMENT PART OR APPROVED REPAIR DOUBLER. ACCOMPLISH A PERMANENT REPAIR AT LH FR68 STGR8L AFT STIFFENER LWR RADIUS PER PART 3 OF THE LATEST REVISION OF ECRA 5341-01468 INTERIM REPAIR HAS BEEN
- [SDR CALA2024111802886](https://openairdocs.org/sdr/CALA2024111802886.md): Intercostal · cracked · Nov 13, 2024 · N848UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > LH FR 68 AT STR 8, FOUND CRACK INDICATION ABOVE UPPER MOST FASTE NER IN RADIUS, AFT FACE. ACCOMPLISH A PERMANENT REPAIR AT LH FR68 STGR8L FASTENER HOLES #A AND #B PER PART 3 OF THE LATEST REVISION OF ECRA 5341-01468 INTERIM REPAIR HAS BEEN ACCOMPLISHED PER PA
- [SDR CALA2024111202835](https://openairdocs.org/sdr/CALA2024111202835.md): Fitting · cracked · Nov 5, 2024 · N848UA · Airbus A319131 · Fuselage Main, Structure
  > WINDSHIELD CENTER POST LEFT AND RIGHT CONTINUITY FITTINGS HAVE C RACK INDICATIONS ON HORIZONTAL LEG APPROX.400 INCH OB OF CENTER "CONTACT ENGINEERING FOR REPAIR INSTRUCTIONS BEFORE NEXT FLIGHT " GEN BY V892444 ON HAECO LCQ NR 9296311 / 36311 REMOVED & REPLACE
- [SDR CALA2024110502798](https://openairdocs.org/sdr/CALA2024110502798.md): Skin · contaminated · Nov 4, 2024 · N848UA · Airbus A319131 · Elevator, Plate/Skin
  > LH ELEVATOR, UPPER SURFACE, HAS ONE AREA WITH EVIDENCE OF WATER INGRESS. 38.5 INCHES FROM IB EDGE AND 11 INCHES FROM AFT EDGE. G EN BY V892444 ON HAECO LCQ NR 9296407 / 36407 REPAIRED L/H ELEVATOR, UPPER SURFACE 38.5" FROM I/B EDGE 11" FR OM AFT EDGE IAW A319
- [SDR CALA2024110502797](https://openairdocs.org/sdr/CALA2024110502797.md): Skin · damaged · Nov 4, 2024 · N848UA · Airbus A319131 · Elevator, Plate/Skin
  > LT ELEVATOR HAS PREVIOUS REPAIR ERRODED ON BOTTOM SURFACE ON BOT TOM SURFACE 99.5" OB OF RIB 2 5.25" FWD OF TRAILING EDGE. GEN BY V079881 ON HAECO LCQ NR 9296435 / 36435 REMOVED AND REPLACED PREVIOUS REPAIR ON L/H ELEVATOR BOTTOM SURF ACE 99.5"IN O/B OF RIB 2
- [SDR CALA2024111102827](https://openairdocs.org/sdr/CALA2024111102827.md): Channel · cracked · Nov 1, 2024 · N848UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > L/H O/W HATCH HAS CRACKS AT RIVETS AT L/H AND R/H LOAD TRANSMITT ING PROGILE. REMOVED & REPLACED L/H O/W HATCH L/H & R/H LOAD TRANSMITTING PRO FILE (FRAME SEGMENT) IAW A319 SRM 51-72-11-911-001. PN: D5227902 620551, PO: 1153067.1, PN: D5227902620451, PO: 115
- [SDR CALA2024110402789](https://openairdocs.org/sdr/CALA2024110402789.md): Door Frame · cracked · Nov 1, 2024 · N848UA · Airbus A319131 · Fuselage Main, Structure
  > R/H O/W HATCH HAS CRACKS AT RIVETS AT L/H AND R/H LOAD TRANSMITT ING PROFILE. GEN BY ON HAECO LCQ NR 9296165 / 36165 REMOVED & REPLACED R/H O/W HATCH L/H & R/H LOAD TRANSMITTING PRO FILE (FRAME SEGMENT) IAW A319 SRM 51-72-11-911-001. AFT FRAME SE GMENT PN D52
- [SDR CALA2024110402788](https://openairdocs.org/sdr/CALA2024110402788.md): Door Frame · cracked · Nov 1, 2024 · N848UA · Airbus A319131 · Fuselage Main, Structure
  > R/H O/W HATCH HAS CRACKS AT RIVETS AT L/H AND R/H LOAD TRANSMITT ING PROFILE. GEN BY ON HAECO LCQ NR 9296165 / 36165 REMOVED & REPLACED R/H O/W HATCH L/H & R/H LOAD TRANSMITTING PRO FILE (FRAME SEGMENT) IAW A319 SRM 51-72-11-911-001. AFT FRAME SE GMENT PN D522
- [SDR CALA2024062801927](https://openairdocs.org/sdr/CALA2024062801927.md): Oxygen Mask · unwanted deploy · Jun 26, 2024 · N848UA · Airbus A319131 · Passenger Oxygen System
  > ROW 1AB O2 PANEL CAME DOWN DURING FLIGHT CAUSING AN AIR RETURN. NO MASKS DROPPED. REINSTALL STORAGE CONTAINER PANEL AND SECURED AT ROW 1AB O2 PANEL PER REF 35-21-41.
- [SDR CALA2023102503166](https://openairdocs.org/sdr/CALA2023102503166.md): Packing · damaged · Oct 22, 2023 · N848UA · Airbus A319131 · Hydraulic System, Main
  > HYD Y SYS LOW PRESSLOW SPEED REJECTEDTAKEOFF AT 30KTS REFER TO L/P 6089998 FOR COMPLETED REPAIRS. HYD Y SYS LOW PRESS FOUND HYD LEAK FROM PARKING BRAKE VALVE FIN 2579GM PACKING REF AIPC 32-45-03-03D ITEM NUMBER 230. REPLACED PACKING AT PARKING BRAKE VALVE REF
- [SDR CALA2023031500753](https://openairdocs.org/sdr/CALA2023031500753.md): Skin · dented · Mar 14, 2023 · N848UA · Airbus A319131 · Fuselage Structure (General)
  > DENT ON FUSELAGE SKIN BTW FR1-2 L/H LAP JOINT. AS NOTED ON LTPR 5001217873-0010.
- [SDR CALA2022112303196](https://openairdocs.org/sdr/CALA2022112303196.md): Idg · faulted · Nov 23, 2022 · N848UA · Airbus A319131 · AC Generator-Alternator
  > GEN 1 INDICATIONS INOP ON ELEC SYSTEM ECAM PAGE AT GEAR RETRACTIONLOST GEN 1. FLIGHT CREW ACCOMPLISHED DISCONNECTION OF NR 1 IDG, 24-21-43-210-048C1 IAW AD 2011-19-01 R1. PERFORMED AUTOMATIC GALLEY SHEDDING TEST IAW AMM 24-27-00. VERIFIED APU OIL LEVEL OK,
- [SDR CALA2022102402930](https://openairdocs.org/sdr/CALA2022102402930.md): None · missing · Oct 24, 2022 · N848UA · Airbus A319131 · Engine Exhaust System
  > PDA 3 FOUND ON WALK AROUND: #1 ENGINE COMMON EXHAUST NOZZLE APPOX 1 O''CLOCK IS MISSING METAL. SEE PICS ADDED PICS ADD PIC REMOVED NUMBER 1 ENG COMMON NOZZLE ASSEMBLY REF AMM 71-11-11-00-010A. REMOVED AND REPLACED CNA ASSY REF AMM 78-11-11 ALL CHECKS GOOD AT T
- [SDR CALA2022011600154](https://openairdocs.org/sdr/CALA2022011600154.md): Servo Valve · low quantity · Jan 16, 2022 · N848UA · Airbus A319131 · Hydraulic Power Accumulator, Main
  > *EMERGENCY DECLARED* GREEN HYD LOW LEVEL INFLIGHT, FOLLOWED QRH AND TURNED OFF PUMP AND PTU REPORTED TO TOMC CONTACT TOMC ITEM UNLOCKED FOR SIGN OFF ALSO SYSTEM WAS NEVER RUN TO EMPTY. FOUND GREEN SYSTEM WITH 2.25 GALS, SVC SYSTEM TO FULL. RAN GREEN SYSTEM WIT
- [SDR CALA2022011400143](https://openairdocs.org/sdr/CALA2022011400143.md): Flt Controls · fault message · Jan 13, 2022 · N848UA · Airbus A319131 · Flight Control System Wiring
  > F/CTL MESSAGESFCS MESSAGE ON SHUTDOWN NO FAULTS NOTED OK TO CONTINUE
- [SDR CALA2021120102220](https://openairdocs.org/sdr/CALA2021120102220.md): Fuel Cap · missing · Dec 1, 2021 · N848UA · Airbus A319131 · Aircraft Fuel System
  > PDA 3 REF LOG PAGE 7525733 FUEL CAP LANYARD FOUND MISSING. PER LOG PAGE 7525733 REPLACED FUEL CAP LANYARD ASSY. OPS CK GOOD
- [SDR CALA2021052600738](https://openairdocs.org/sdr/CALA2021052600738.md): Servo · faulted · May 26, 2021 · N848UA · Airbus A319131 · Elevator Control System
  > ELEVATOR SERVO FAULT ON ECAM. - TOMC KROWN PERFORMED TSM 27-93-00-810-861-A. FOUND CONNECTOR AT SERVO 34CE4 DISCONNECTED. INSPECTED CONNECTOR FOR DEFECTS. NONE NOTED. CLEANED INSTALLED AND SECURED CONNECTOR. CHECKED ALL CONNECTIONS FOR SECURITY. CHECKS GOOD. R
- [SDR CALA2021032200364](https://openairdocs.org/sdr/CALA2021032200364.md): Access Panel · damaged · Mar 22, 2021 · N848UA · Airbus A319131 · Wing, Plate/Skin
  > DURING REMOVAL OF PANEL 540KB A/C SKIN WAS DAMAGED ONHAECO LCQ R EF 9290614. 2 REPAIR ACTION EXCEEDED LIMITS OF SRM57-21-11-300-002, DEVIATION REQUIRED ECRA5721-01445 AND DIP TO ACCOMPLISH PERMANENT REPAIR AT LH WING BOTTOM FUEL ACCESS PANEL 540KB HOLES PER PA
- [SDR CALA2021032200352](https://openairdocs.org/sdr/CALA2021032200352.md): Fitting · cracked · Mar 19, 2021 · N848UA · Airbus A319131 · Fuselage Main, Attach Fittings
  > AFT CARGO DOOR SILL SUPPORT UNDER THRESHOLD,TORSION BOX SHEET CO VER BETWEEN FR 56-59 RESPECTIVELY HAS MULTIPLE HOLES NOTED WITH CRACK INDICATIONS. REF ECRA 5341-01238 PART 1 STEP 2 DIP REQUIRE D. ACCOMPLISHED INTERIM REPAIR IAW ECRA 5341-01238 PART 1.1 REQUIR
- [SDR CALA2021031900334](https://openairdocs.org/sdr/CALA2021031900334.md): Threshold · corroded · Mar 17, 2021 · N848UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT CARGO THRESHOLD PLATE HAS CORROSION- A3NB-53-4-6179 PER HAEC O LCQ NR 9290247/422247. REMOVED AND REPLACED AFT CARGO THRESHOLD PLATE IAW A319 SRM 51-7 2-11-911-001.
- [SDR CALA2021022600229](https://openairdocs.org/sdr/CALA2021022600229.md): Fitting · corroded · Feb 25, 2021 · N848UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > FORWARD RT ENTRY DOOR AT FR16 THE FWD CUTOUT FOR GIRT BAR FITTING HAS 4EA BOLT HOLES CORRODED GEN BY V061588 PER NR9290534 OPS 42534. RT ENTRY DOOR AT FR16 DOOR SILL WAS CORRODED OUT OF LIMITS PER SRM 53-11-14-283-005 FIG 001. RMVD AND RPLD IAW SRM 51-72-11
- [SDR CALA2021022300220](https://openairdocs.org/sdr/CALA2021022300220.md): Intercostal · damaged · Feb 23, 2021 · N848UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > FR54-55 INTERCOSTAL HAS INCOMING DAMAGE. 2 FASTENER HOLES WERE FOUND ELONGATED AFTER REMOVAL OF CORNER ASSEMBLY. (SUPPORT TASK). GENERATED BY B918284 AT HAECO LCQ PER NR 9290744 (42744). REMOVED AND REPLACED FR 54-55 INTERCOSTAL IAW A319 SRM 51-72-11- 911-0
- [SDR CALA2021022300219](https://openairdocs.org/sdr/CALA2021022300219.md): Skin · damaged · Feb 23, 2021 · N848UA · Airbus A319131 · Wing, Plate/Skin
  > RIGHT WING RIB 17-18 BOTTOM SKIN LOWER SURFACE AROUND FUEL ACCESS DOOR CUT OUT HAS 1 EA ELONGATED HOLE PER NR9290630 HAECO OPS42630. REPAIRED BOTTOM SKIN LOWER SURFACE AROUND FUEL ACCESS DOOR CUT OUT AT RT WING RIB 17-18 IAW SRM 57-27-11-283-002 REQUIRES INSP
- [SDR CALA2021022300218](https://openairdocs.org/sdr/CALA2021022300218.md): Fitting · corroded · Feb 23, 2021 · N848UA · Airbus A319131 · Fuselage Main, Structure
  > FR57 RT LOWER CARGO DOOR FITTING UNDERNEATH THRESHOLD HAS CORROSION AT FASTENER HOLE. REMOVED AND REPLACED FR57 RT LOWER CARGO DOOR FITTING IAW SRM 51 -72-11.
- [SDR CALA2021022200217](https://openairdocs.org/sdr/CALA2021022200217.md): Skin · damaged · Feb 22, 2021 · N848UA · Airbus A319131 · Wing, Plate/Skin
  > RIGHT WING RIB 17-18 BOTTOM SKIN LOWER SURFACE AROUND FUEL ACCESS DOOR CUT OUT HAS 1 EA ELONGATED HOLE (A3NB 57-3-6147). PER NR 92906 30 GENERATED AT HAECO LCQ. REPAIRED BOTTOM SKIN LOWER SURFACE AROUND FUEL ACCESS DOOR CUT OUT AT RT WING RIB 17-18. FINAL
- [SDR CALA2021022200195](https://openairdocs.org/sdr/CALA2021022200195.md): Fitting · corroded · Feb 19, 2021 · N848UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT CARGO SUPPORT FITTING AT FR 56RH UNDERNEATH TORSION BOX COVER HAS CORROSION.(SUPPORT TASK). AT HAECO LCQ PER NR 9290725( 42725). REMOVED AND REPLACED FITTING AT FR 56 RH IAW A319 SRM 51-72-11- 911-001.
- [SDR CALA2021022200194](https://openairdocs.org/sdr/CALA2021022200194.md): Fitting · mismanufactured · Feb 19, 2021 · N848UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > SUPPORT FITTING UNDERNEATH TORSION BOX COVER AT FR 57RH HAS DOUBLE DRILLED HOLE, (SUPPORT TASK). GENERATED AT HAECO LCQ PER NR 9290704 (42704). REMOVED AND REPLACED FITTING AT FR 57 RT IAW A319 SRM 51-72-11- 911-001.
- [SDR CALA2021022200193](https://openairdocs.org/sdr/CALA2021022200193.md): Fitting · corroded · Feb 19, 2021 · N848UA · Airbus A319131 · Fuselage Main, Attach Fittings
  > FITTING AT FR 58 UNDERNEATH TORSION BOX COVER HAS CORROSION IN FA STENER HOLES AND HOLES ARE OUT OF ROUND, REPLACEMENT REQUIRED PER NR9290727. REMOVED AND REPLACED FITTING AT FR 58 UNDER TORSION BOX IAW SRM 5 1-72-11-911-001 PER NR9290727.
- [SDR CALA2021020800143](https://openairdocs.org/sdr/CALA2021020800143.md): Fitting · corroded · Feb 7, 2021 · N848UA · Airbus A319131 · Fuselage Main, Attach Fittings
  > FWD LH ENTRY DOOR AT FR.16 FWD CUTOUT FOR GIRT BAR FITTING HAS 4 EA BOLT HOLES CORRODED A3NB-53-3-6298 ON HAECO LCQ REF 9290533 N R 42533 GENERATED BY MECH V061588 REMOVED AND REPLACED FWS LH FWD LWR DOOR SILL FITTING FR16-20 IA W A319 SRM 51-72-11-911-001. PE
- [SDR CALA2021012800100](https://openairdocs.org/sdr/CALA2021012800100.md): Door Sill · corroded · Jan 27, 2021 · N848UA · Airbus A319131 · Fuselage, Wing Attach Fittings
  > R2 SILL DOOR CENTER SHAPE SEAL HAS CORROSION FR 66-FR 68 A3NB-53 -3-6187-NR 9290511 (42511) AT HAECO LCQ. REMOVED AND REPLACED SHAPE SILL AT R-2 DOOR CENTER FR 66-FR 68, IAW A319 SRM 51-72-00-801 AND 51-42-11-801. REMOVED DOT.
- [SDR CALA2021012800099](https://openairdocs.org/sdr/CALA2021012800099.md): Gusset · gouged · Jan 27, 2021 · N848UA · Airbus A319131 · Fuselage Main, Floor Beam
  > LT AFT FUSELAGE UNDER FLOOR GUSSET PLATE HAS GOUGES AT FR 70 STR 31L-A3NB-3-6187 - NR 9290514 (42514) AT HAECO LCQ. REMOVED & REPLACED LT AFT FUSELAGE AT FR 70, STR 31L GUSSET PLATE, IAW A 319 SRM 51-42-11. FABRICATED NEW PLATE, IAW AB DWG 18D53471208.
- [SDR CALA2019093001671](https://openairdocs.org/sdr/CALA2019093001671.md): Epsu · failed · Sep 27, 2019 · N848UA · Airbus A319131 · Emergency Lighting
  > EPSU 10WL FAILS OPS TEST AND BATTERY FAILS DATE INSPECTION SPEC NO. A3NB-33-3-6016 GEN BY V901995 PER NR9296046 AT HAECO LCQ REMOVED AND REPLACED EPSU BATTERY IAW AMM 33-51-38-000-002-A AND 33-51-38-400-002-A. OPS CK GOOD IAW AMM 33-51-38-710-052-A PER NR 9296
- [SDR CALA2019092301620](https://openairdocs.org/sdr/CALA2019092301620.md): Hinge Fitting · damaged · Sep 20, 2019 · N848UA · Airbus A319131 · Elevator Structure
  > LT ELEVATOR #5 HINGE FITTING UPPER I/B FLANGE IS DISBONDED SUPPO RT TASK PER NR 9298410. REMOVED AND REPLACED #5 HINGE ARM ON LT HORZ STAB IAW AMM 55-16 -42-420-050-B.
- [SDR CALA2019092301601](https://openairdocs.org/sdr/CALA2019092301601.md): Door Sill · corroded · Sep 16, 2019 · N848UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > R-2 DOOR SILL I/B SIDE FR 68 CORROSIN AROUND 2EA FASTENER HOLES ON REF 9296358. REPAIRED R-2 DOOR SILL I/B SIDE AT FR68 (2EA) FASTENER HOLES IAW SRM 53-41-14-300-001. REPAIR PRINCIPLE #5 (CATEGORY A) WITH NO REINSP.
- [SDR CALA2019092301600](https://openairdocs.org/sdr/CALA2019092301600.md): Door Sill · corroded · Sep 16, 2019 · N848UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT CABIN L2 DOOR SILL FR 68 AROUND FASTENER HOLES CORROSION ON REF9296370. REPAIRED L-2 DOOR SILL I/B SIDE AT FR68 (2EA) FASTENER HOLES IAW SRM 53-11-14-300-001, REPAIR PRINCIPLE #5 (CATEGORY A) WIT H NO REINSP.
- [SDR CALA2019092301599](https://openairdocs.org/sdr/CALA2019092301599.md): Door Sill · corroded · Sep 16, 2019 · N848UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT CABIN L-2 DOOR SILL FR66 HAS CORROSION ON REF 9296 369. REMOVED CORROSION AND PERFORM REPAIR ANGLE ON AFT CABIN L-2 DOOR SILL AT FR66 IAW SRM 53-41-14-300-001 FIG001 SHEET 04, PRINCIPLE 6. THE REPAIR IS A CATEGORY A REPAIR.
- [SDR CALA2018010800105](https://openairdocs.org/sdr/CALA2018010800105.md): Power Supply · inoperative · Jan 8, 2018 · N848UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY LIGHT TEST FAILED. REMOVED AND REPLACED THE EPSU AT THE L1 DOOR IAW AMM 33-51-38-400-001-A, CHECKED OK.
- [SDR CALA2017111704098](https://openairdocs.org/sdr/CALA2017111704098.md): Light · malfunctioned · Nov 17, 2017 · N848UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY LIGHT FAILED DURING AN A-10 CHECK IAW 33-51- 38. SIDS PANEL BATTERY TEST PUSHBUTTON ON PTP FAILED. ALL EMERGENCY LIGHTS IN CABIN CHECKED WITH FLIGHT DECK SWITCH & AFT FLIGHT ATTENDANT PANEL. RESET BREAKERS SYSTEM CHECKED GOOD.
- [SDR CALA2017111104028](https://openairdocs.org/sdr/CALA2017111104028.md): Battery Pack · failed · Nov 11, 2017 · N848UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY LIGHT TEST FAILED. EPSU BATTERY AFT LT. REPLACED EMERGENCY POWER SUPPLY BATTERY IAW AMM 33-51-38. OPS CHECKED GOOD.
- [SDR CALA2017073102456](https://openairdocs.org/sdr/CALA2017073102456.md): Spring · broken · Jul 31, 2017 · N848UA · Airbus A319131 · Emergency Equipment
  > L1 DOOR GIRT BAR FLOOR FITTING ON LEFT SIDE, SPRING BROKEN ON GIRT BAR RETAINING CLIP. REPLACED SPRING IAW AMM 52-11-31-400-003-A, AND ADJUSTMENT CHECK IAW AMM 52-11-00-820-001-A. OPS CHECKED GOOD.
- [SDR CALA2016012595028](https://openairdocs.org/sdr/CALA2016012595028.md): Power Supply · inoperative · Jan 24, 2016 · N848UA · Airbus A319131 · Emergency Lighting
  > FAILED CIDS SYS BITE TEST FOR EMER LIGHTS. REPLACED POWER SUPPLY, LHF WD IAW AMM TASK 33-51-38-400-001-A & BATTERIES AT LT FWD, CTR RT, AFT LT LOCATIONS IAW AMM TASK 33-51-38-400-002-A. SYS TESTED OK IAW AMM SUB TASK 740-050-B.

Next page: https://openairdocs.org/aircraft/N848UA/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 = 'N848UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N848UA/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.