# Service difficulty reports: N838UA

A list on [N838UA](https://openairdocs.org/aircraft/N838UA.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 2 · 93 reports

- [SDR CALA2026061717147](https://openairdocs.org/sdr/CALA2026061717147.md): Fuel Cap · missing · Jun 14, 2026 · N838UA · Airbus A319131 · Fuel Storage
  > FUEL CAP MISSING REQUIRES PDA UNABLE TO LOCATE FUEL CAP AT STATION PLACED ON CDL LP: 9255512 - FUEL CAP MISSING THE CAPTAIN VERIFIED NO LEAKAGE FROM THE COUPLING. INOP STICKER IS INSTALLED ADJACENT TO THE REGISTRATION NUMBER ON THE FORWARD INSTRUMENT PANEL. RE
- [SDR CALA2025102710616](https://openairdocs.org/sdr/CALA2025102710616.md): Isolation Valve · faulted · Oct 24, 2025 · N838UA · Airbus A319131 · Pneumatic Distribution System
  > AIR X BLEED FAULT ON CLIMB OUT PFR SHOWS 36-12 AIR X BLEED FAULT W/ CORRELATED MSG'S 36-11-34 BMC 1 OR SOLENOID, 36-12-00 X FEED VALVE 6HV AND 36-12-00 X FEED VALVE 6HV OR CKT. ACP BMC 1 & 2 BITE CHKS GOOD ON THE GRND ALSO OPERATED X BLEED SWITCH AND ALL ECAM
- [SDR CALA2025101610166](https://openairdocs.org/sdr/CALA2025101610166.md): Unknown · odor · Oct 15, 2025 · N838UA · Airbus A319131 · Air Distribution System
  > MUSTY SMELL IN COCKPIT UPON ARRIVAL AT A/C UPON ARRIVAL TO AIRCRAFT THE ODOR WAS VERY FAINT AND ALMOST GONE. FOLLOWED FIM TASK 05-50-00-810-831-A. AIRPLANE HAS HISTORY OF HYDRAULIC LEAK AND SUSPECT RESIDUAL HYDRAULIC FLUID GOT INTO APU INLET AND HAD MOMENTARY
- [SDR CALA2025082007949](https://openairdocs.org/sdr/CALA2025082007949.md): Indicator · no discrepancy · Aug 16, 2025 · N838UA · Airbus A319131 · Cargo/Baggage Doors
  > AFT CARGO DOOR GREEN LATCH INDICATORS ARE NOT VISIBLE. INSPECTED LATCHES FOR ALL GREEN INDICATIONS, ALL ARE GREEN OK TO CONTINUE. A
- [SDR CALA2025081107527](https://openairdocs.org/sdr/CALA2025081107527.md): Exciter · faulted · Aug 11, 2025 · N838UA · Airbus A319131 · Exciter
  > HUNG START ON NUMBER 1 ENGINE AFTER STARTER CUT OUT. STRONG FUEL ODOR IN FLTDECK AFTER CRANK CLASS 3 FUEL DEPULSE ACTIVATED 1. LEADS TO TSM 80-00-00-810-819-A. ENG START INITIAL TO IDLE SPEED TOOK 2 PLUS MINUTES ON 2 STARTS. ODOR OF FUEL SMELL IN FLIGHT DECK U
- [SDR CALA2025080807484](https://openairdocs.org/sdr/CALA2025080807484.md): Door · leaking · Aug 7, 2025 · N838UA · Airbus A319131 · Emergency Exits
  > LOUD NOISE FROM RIGHT SIDE EMERGENCY EXIT, NOISE ALREADY ON DIP. INSPECTED EXISTING SPEED TAPE, FOUND MULTIPLE AREAS PEELING. REMOVED AND REAPPLIED DAMAGED SPEED TAPE.
- [SDR CALA2025061305534](https://openairdocs.org/sdr/CALA2025061305534.md): Cover · detached · Jun 10, 2025 · N838UA · Airbus A319131 · Door Warning System
  > SLIDE ARMED INDICATOR COVER FOUND ON FLOOR IN FRONT OF 1L. ACCOMPLISHED INTERIM REPAIR PER PART 1, INSPECT EACH FLIGHT, AND ACCOMPLISH PERMANENT REPAIR WITHIN 3 DAYS.
- [SDR CALA2025052304923](https://openairdocs.org/sdr/CALA2025052304923.md): Idg · faulted · May 20, 2025 · N838UA · Airbus A319131 · AC Generator-Alternator
  > ACFT RETURN TO FIELD, CREW STATED ALL FAULTS STARTED TO OCCUR AT WHEELS OFF GROUND. FIRST FAULTS ON PFR INDICATE ELEC AC BUS 2 FAULT, ELEC DC BUS 2 FAULT, ELEC GEN 2 FAULT.ALSO ON PFR TOO MANY FAULTS TO LIST! REF TSM 24-20-00-810-813. CHECKED AIRCRAFT WIRING
- [SDR CALA2025052104894](https://openairdocs.org/sdr/CALA2025052104894.md): Contactor · faulty · May 19, 2025 · N838UA · Airbus A319131 · AC Generator-Alternator
  > GEN 2 FAILURE/TR2 FAILURE CAP REPORTED T/O INHIBIT OCCURRED DURING T/O FOLLOWED BY A TR2 FAULT AND GEN 2 FAULT. BOTH SCREENS ON FO SIDE BLANKED OUT. ABLE TO RECOVER GEN 2 BY CYCLING. TR2 FAULT REMAINS. PFR PIC ATTACHED. UPDATING TIME REF TSM 24-20-00-810-814
- [SDR CALA2025031402819](https://openairdocs.org/sdr/CALA2025031402819.md): Tape · peeling · Mar 14, 2025 · N838UA · Airbus A319131 · Emergency Exits
  > LOUD WHISTLE FM RH OVERWING EXIT EVEN AT 8 PSID FOUND PEELING SPEED TAPE FROM DIP TEMP REPAIR IN LP 4125574. REPLACED SPEED TAPE IAW SRM 57-41-11. OK TO CONTINUE
- [SDR CALA2025031702870](https://openairdocs.org/sdr/CALA2025031702870.md): Tape · loose · Mar 13, 2025 · N838UA · Airbus A319131 · Emergency Exits
  > LOUD WHISTLING NOISE COMING FROM RH OVERWING EXI TS. NOISE STARTED JUST A FTER TAKEOFF FOUND TAPE LOOSE AREA ALREADY ON DIP LOG. 9620908 RE-SECURED WITH MISSING TAPE.
- [SDR CALA2025012902100](https://openairdocs.org/sdr/CALA2025012902100.md): Fuel Cap · missing · Jan 29, 2025 · N838UA · Airbus A319131 · Fuel Storage
  > PDA, FUELER REPORT FUEL CAP MISSING. INSTALLED NEW FUEL CAP IN REFERENCE TO AMM 28-25-41. OK TO CONTINUE. PARTS USED: 31-2825-9-0001,QTY:1 1339735,QTY:1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1339735 SN OFF 1111 IPC REFERENCE # 28-00-00 CAP, COUPLIN
- [SDR CALA2024120501412](https://openairdocs.org/sdr/CALA2024120501412.md): Battery · faulted · Dec 3, 2024 · N838UA · Airbus A319131 · Emergency Lighting
  > EPSU BATTERY EMER R FAULT R/R EPSU BATTERY AT EPSU 12WL WITH A SERVICABLE UNIT FROM A/C 4046 REF AMM 33-51-38. OPS CHECKS OK
- [SDR CALA2024120401402](https://openairdocs.org/sdr/CALA2024120401402.md): Battery · failed · Dec 2, 2024 · N838UA · Airbus A319131 · Emergency Lighting
  > OPERATIONAL CHECK OF CABIN EMERGENCY LIGHTS {A3NB-33-3-6012} - SYS OK LIGHT DOES NOT COME ON AFTER TEST. EPSU BATTERY AFT L 33-51-58. EPSU COMM AFT L. 33-51-38 R/R EPSU BATTERY AT EPSU 13WL WITH A SERVICABLE UNIT FROM A/C 4046 REF AMM 33-51-38. OPS CHECKS OK
- [SDR CALA2024082602266](https://openairdocs.org/sdr/CALA2024082602266.md): Support Frame · cracked · Aug 19, 2024 · N838UA · Airbus A319131 · Fuselage Main, Structure
  > R/H O/W EMERGENCY EXIT HAS CRACKS IN FRAME SUPPORT FWD & AFT, REMOVED & REPLACED R/H O/W EMERGENCY EXIT FWD & AFT FRAME SUPPOR TS IAW A319 SRM 51-72-11-911-001.
- [SDR CALA2024082602265](https://openairdocs.org/sdr/CALA2024082602265.md): Support Frame · cracked · Aug 19, 2024 · N838UA · Airbus A319131 · Fuselage Main, Structure
  > L/H O/W EMERGENCY EXIT HAS CRACKS IN AFT FRAME SUPPORT, REMOVED & REPLACED L/H O/W EMERGENCY AFT FRAME SUPPORT IAW A319 SRM 51-72-11-911-001 FRAME PN# D5227902620451 PO# 1145773.5,
- [SDR CALA2023122003687](https://openairdocs.org/sdr/CALA2023122003687.md): Skin · dented · Dec 18, 2023 · N838UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > AFT FUSELAGE TAIL SECTION FR73 STRINGER 30R-31R HAS INWARD DENT. THIS REPAIR IS CONSIDERED A CAT B REPAIR PER SRI 53-00-11-205-053. FABRICATED AND INSTALLED DOUBLER REPAIR AT FR73 STRINGER 30R-31R REPAIRED DENT TO AFT FUSELAGE TAIL SECTION, FR73 STRINGER CAT
- [SDR CALA2022030100537](https://openairdocs.org/sdr/CALA2022030100537.md): Pump · failed · Mar 1, 2022 · N838UA · Airbus A319131 · Hydraulic Pump (Electric/Engine), Main
  > YELLOW HYD RESV OVHTINFLIGHT. EMERGENCY RETURNED TO KDEN. OPERATED BOTH FWD AND AFT CARGO DOORS SEVERAL TIMES AND THE DOOR ENTERED ROTABLE PART INFO. SELECTOR SWITCHES RETURNED TO THE NEUTRAL POSITION EACH TIME ROTABLE PARTS CHANGE WAS INDICATED - TT # 1958381
- [SDR CALA2022011000098](https://openairdocs.org/sdr/CALA2022011000098.md): Probe · failed · Jan 9, 2022 · N838UA · Airbus A319131 · Central Warning
  > FUEL RT TANK OVERFLOW ECAM CAME ON TWICE AND BOTH TIMES CLEARED IT SELF WAS ON DURING EVENT WAS IAD TO LAX SO ASSUME FULL WING TANKS. FULL TANKS HUNTING MOST LIKELY CAUSE FOR "RT FUEL TANK OVERFLOW" MSG. MULTIPLE FAULTS FOR " RT QTY PROBE 28QT2" MULTIPLE LEGS.
- [SDR CALA2021122002417](https://openairdocs.org/sdr/CALA2021122002417.md): Repair · none · Dec 20, 2021 · N838UA · Airbus A300* · Fuselage Structure (General)
  > REF DTA LP 7628364 AS PER ECRA 5331-02818 PART 1 STEP 3;PLANNING TO CONTACT ENGINEERING AFTER 09 OCTOBER 2022 BUT BEFORE 09 NOVEMBER 2022 FOR ECRA 5331-02818 PART 3 PERMAMANT REPAIR. REFERENCE ECRA 5331-02818 PART 1 STEP 3. BEFORE 09 NOVEMBER 2022 FOR ECRA 533
- [SDR CALA2021122002415](https://openairdocs.org/sdr/CALA2021122002415.md): Repair · none · Dec 20, 2021 · N838UA · Airbus A300* · Fuselage Structure (General)
  > ACCOMPLISH A PERMANENT REPAIR PER PART 3 OF LATEST REVION OF ECRA 5331-02818 ON OR BEFORE 09 DECEMBER 2022. REF DTA LP 7037108 ACCOMPLISH PERMANENT REPAIR PER PART 3 OF LATEST REVISION OF ECRA 5331-02818 ON OR BEFORE 09 DECEMBER 2022. REF DTA LP7037108 ACCOMPL
- [SDR CALA2021121202350](https://openairdocs.org/sdr/CALA2021121202350.md): Intercostal · cracked · Dec 12, 2021 · N838UA · Airbus A319131 · Fuselage Structure (General)
  > (REPAIR BEFORE NEXT FLT) ROTO PROBE OF RH FR16 #7 DOOR STOP FIT TING HOLES FOUND CRACKS IN THE I/B TOP AND I/B BOTTOM HOLES.() REPAIRED HOLES #1-3 FROM FRAME AND INTERCOASTAL DOOR STOP FITTIN G #7 FR16 LH IAW EA 319-5311-13-A2715, ECRA 5311-02680. EMP# V93 33
- [SDR CALA2021121202345](https://openairdocs.org/sdr/CALA2021121202345.md): Bulkhead · cracked · Dec 11, 2021 · N838UA · Airbus A319131 · Fuselage Structure (General)
  > (AD 2019-20-10) LH FR16 DOOR STOP FITTING #7 HAS CRACK INDICATIO NS ON I/B TOP HOLE AND I/B BOTTOM HOLE. REPAIR BEFORE NEXT FLIGH T.() REPAIRED HOLES #1-3 FROM FRAME AND INTERCOASTAL DOOR STOP FITTIN BFM ON NR# 0017169 G #7 FR16 LH IAW A319-5311-13-A2731 AND C
- [SDR CALA2021121002338](https://openairdocs.org/sdr/CALA2021121002338.md): Antenna · corroded · Dec 10, 2021 · N838UA · Airbus A319131 · Fuselage Structure (General)
  > (A3NB-44-3-6004) GCS ANTENNA ADAPTER PLATE HAS EXFOLIATING CORRO SION CENTER AREA AFT ON ANTENNA. DOT 102-116.() GCS ANTENNA ADAPTER PLATE REPAIRED IAW EA 319-4420-13-A2749 REV'' _'' AND UAL EC/RA 5341-01290. NO DEVIATIONS EMP# V934344 WORK ACC OMPLISHED T ST
- [SDR CALA2021121002337](https://openairdocs.org/sdr/CALA2021121002337.md): Fitting · cracked · Dec 10, 2021 · N838UA · Airbus A319131 · Fuselage Structure (General)
  > (REPAIR BEFORE NEXT FLT) ROTO PROBE OF RH FR16 #7 DOOR STOP FIT TING HOLES FOUND CRACKS IN THE I/B TOP AND I/B BOTTOM HOLES.() REPAIRED HOLES #1-3 FROM FRAME AND INTERCOASTAL DOOR STOP FITTIN G #7 FR16 LH IAW EA 319-5311-13-A2715, ECRA 5311-02680. EMP# V93 33
- [SDR CALA2021121002336](https://openairdocs.org/sdr/CALA2021121002336.md): Fitting · cracked · Dec 10, 2021 · N838UA · Airbus A319131 · Standard Practices/Structures
  > (AD 2019-20-10) LH FR16 DOOR STOP FITTING #7 HAS CRACK INDICATIO NS ON I/B TOP HOLE AND I/B BOTTOM HOLE. REPAIR BEFORE NEXT FLIGH T.() REPAIRED HOLES #1-3 FROM FRAME AND INTERCOASTAL DOOR STOP FITTIN BFM ON NR# 0017169 G #7 FR16 LH IAW A319-5311-13-A2731 AND C
- [SDR CALA2021112902186](https://openairdocs.org/sdr/CALA2021112902186.md): Stringer · corroded · Nov 28, 2021 · N838UA · Airbus A319131 · Fuselage, Wing Attach Fittings
  > (A3NB-53-4-6179) AREA AFT OF BULK CARGO STRINGER BELOW OUTFLOW V ALVE IS CORRODED. DOT 102-130 () REMOVED & REPLACED STRINGER 31 R/H FR.64 TO FR67 R/H IAW SRM 51- 42-11. ACCOMPLISHED AT BFM ST AEROSPACE MOBILE. NR#0017016
- [SDR CALA2021112502170](https://openairdocs.org/sdr/CALA2021112502170.md): Stringer · corroded · Nov 25, 2021 · N838UA · Airbus A319131 · Fuselage, Wing Attach Fittings
  > (A3NB-53-4-6179) AREA AFT OF BULK CARGO STRINGER BELOW OUTFLOW V ALVE IS CORRODED. DOT 102-130 () REMOVED & REPLACED STRINGER 31 R/H FR.64 TO FR67 R/H IAW SRM 51- 42-11. ACCOMPLISHED AT BFM ST AEROSPACE MOBILE. NR#0017016
- [SDR CALA2021111502097](https://openairdocs.org/sdr/CALA2021111502097.md): Beam · corroded · Nov 12, 2021 · N838UA · Airbus A319131 · Fuselage Structure (General)
  > (A3NB-53-3-6040), FWD PASSENGER CABIN FLOOR, MAIN STRUCTURE, BTW FR20-FR24 AT Y-1292, SEAT TRACK WITH CORROSION. DOT 88-001.() DAMAGE FOUND WITHOUT OF LIMITS IAW A319 SRM 53-00-15-283-001, RE PLACED PER NEW FLOOR BEAM P/N: D5311278220201 BATCH 0003778671, INST
- [SDR CALA2021111102089](https://openairdocs.org/sdr/CALA2021111102089.md): Beam · corroded · Nov 11, 2021 · N838UA · Airbus A319131 · Fuselage Main, Structure
  > (A3NB-53-6102), FWD PASSENGER CABIN FLOOR, MAIN STRUCTURE, FROM FR25 AT Y-1292, SEAT TRACK WITH CORROSION. DOT 88-006() DAMAGE FOUND OUT OF LIMITS IAW A319 SRM 53-00-15-283-001, REPLAC ED PER NEW P/N: D5323345920000 BATCH: 00038644381, INSTALLED IAW A319 SRM 5
- [SDR CALA2021111002083](https://openairdocs.org/sdr/CALA2021111002083.md): Floorbeam · corroded · Nov 10, 2021 · N838UA · Airbus A319131 · Fuselage Main, Structure
  > (A3NB-53-3-6038), FWD PASSENGER CABIN FLOOR, MAIN STRUCTURE, FRO M FR14 TO FR20, BTW Y-254 AND Y254, STRUCTURE WITH CORROSION (2 PLACES) DOT 88-009() REMOVED AND REPLACED SEAT TRACK P/N: D5311146100200 AT FWD CABIN FLOOR Y-254, FR12-FR24 IAW SRM 51-42-11. SEE
- [SDR CALA2021111002082](https://openairdocs.org/sdr/CALA2021111002082.md): Seat Track · corroded · Nov 10, 2021 · N838UA · Airbus A319131 · Fuselage Structure (General)
  > (A3NB-53-3-6040), FWD PASSENGER CABIN FLOOR, MAIN STRUCTURE, BTW FR20-FR21 AT Y-765, SEAT TRACK WITH CORROSION. DOT 88-002() NEW SEAT TRACK INSTALLED IAW A-319 SRM 51-42-11/001 PARAGRAPH 2. E AND 2.F. EMP# V936039 WORK ACCOMPLISHED AT ST ENGINEERING AERO SPACE
- [SDR CALA2021111002081](https://openairdocs.org/sdr/CALA2021111002081.md): Seat Track · corroded · Nov 10, 2021 · N838UA · Airbus A319131 · Fuselage Main, Structure
  > (A3NB-53-3-6038), FWD PASSENGER CABIN FLOOR, FR20, BTW FUSELAGE INNER SKIN AND SEAT TRACK AT Y-1292, STRUCTURE WITH CORROSION. D OT 88-010 () CORROSION FOUND OUT OF LIMITS IAW A319 SRM 53-11-14-283-007, REC EIVED NEW SUPPORT WEB P/N: D5311278520301 BATCH: 0003
- [SDR CALA2021110802062](https://openairdocs.org/sdr/CALA2021110802062.md): Seat Track · corroded · Nov 7, 2021 · N838UA · Airbus A319131 · Fuselage Main, Structure
  > (A3NB-53-3-6038), FWD PASSENGER CABIN FLOOR, MAIN STRUCTURE, FRO M FR14 TO FR20, BTW Y-254 AND Y254, STRUCTURE WITH CORROSION (2 PLACES) DOT 88-009() REMOVED AND REPLACED SEAT TRACK P/N: D5311146100200 AT FWD CABIN FLOOR Y-254, FR12-FR24 IAW SRM 51-42-11. SEE
- [SDR CALA2021110802061](https://openairdocs.org/sdr/CALA2021110802061.md): Seat Track · corroded · Nov 7, 2021 · N838UA · Airbus A319131 · Fuselage Structure (General)
  > (A3NB-53-3-6040), FWD PASSENGER CABIN FLOOR, MAIN STRUCTURE, BTW FR20-FR21 AT Y-765, SEAT TRACK WITH CORROSION. DOT 88-002() NEW SEAT TRACK INSTALLED IAW A-319 SRM 51-42-11/001 PARAGRAPH 2. E AND 2.F. EMP# V936039 WORK ACCOMPLISHED AT ST ENGINEERING AERO SPACE
- [SDR CALA2021110802060](https://openairdocs.org/sdr/CALA2021110802060.md): Floor Support · corroded · Nov 7, 2021 · N838UA · Airbus A319131 · Fuselage Main, Structure
  > (A3NB-53-3-6038), FWD PASSENGER CABIN FLOOR, FR20, BTW FUSELAGE INNER SKIN AND SEAT TRACK AT Y-1292, STRUCTURE WITH CORROSION. D OT 88-010 () CORROSION FOUND OUT OF LIMITS IAW A319 SRM 53-11-14-283-007, REC EIVED NEW SUPPORT WEB P/N: D5311278520301 BATCH: 0003
- [SDR CALA2021110802044](https://openairdocs.org/sdr/CALA2021110802044.md): Beam · corroded · Nov 5, 2021 · N838UA · Airbus A319131 · Fuselage Main, Structure
  > (A3NB-53-3-6040), FWD PASSENGER CABIN FLOOR, MAIN STRUCTURE, BTW FR20-FR21 AT Y-254, SEAT TRACK WITH CORROSION. DOT 88-033() REMOVED AND REPLACED RAIL DUNMY Y-189 BETWEEN FR20 AND FR24 AT F WD PASSENGER CABIN FLOOR IAW SRM 51-42-11. EMP# V933866 WORK ACC OMPLI
- [SDR CALA2021110802043](https://openairdocs.org/sdr/CALA2021110802043.md): Beam · corroded · Nov 5, 2021 · N838UA · Airbus A319131 · Fuselage Main, Structure
  > (A3NB-53-3-6187), AFT PASSENGER CABIN FLOOR, MAINSTRUCTURE BTW F R66 AND FR68, LONGERON BEAM WITH CORROSION (5 PLACES) DOT 88-015 () LONGERON BEAM REPLACED IAW A319 SRM 51-42-11/001 PARAGRAPH 2.E A ND 2.F. FORM 44-0008 ATTACHED EMP# V933870 WORK ACCOMPLISHED A
- [SDR CALA2021102901988](https://openairdocs.org/sdr/CALA2021102901988.md): Beam · corroded · Oct 27, 2021 · N838UA · Airbus A319131 · Fuselage Main, Structure
  > (A3NB-53-3-6187) CABIN FLOOR STRUCTURE FR 66 Y765 HAS CORROSION AT 2 SPOTS. DOT NO 17-25() REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS ON HARD POINT AREA IAW SRM 51-74-00. REMOVED AND REPLACED PN# D534 720900200 BATCH# 0008380224 IAW SRM 51-4
- [SDR CALA2018062101452](https://openairdocs.org/sdr/CALA2018062101452.md): Door Sill · corroded · Jun 10, 2018 · N838UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > R2 DOOR SILL HAD CORROSION, AFT OF FRAME 66. REMOVED AND REPLACED THE R2 DOOR SILL IAW SRM 51-42-11.
- [SDR CALA2018012600345](https://openairdocs.org/sdr/CALA2018012600345.md): Light · detached · Jan 26, 2018 · N838UA · Airbus A319131 · Emergency Lighting
  > SEAT 30C EMERGENCY LIGHT DETACKED. INSTALLED THE LIGHT. OPS OK
- [SDR CALA2017123104708](https://openairdocs.org/sdr/CALA2017123104708.md): Actuator · faulty · Dec 31, 2017 · N838UA · Airbus A319131 · Leading Edge Slat Actuator
  > F/CTL SLATS FAULT DISPLAYED. EMERGENCY DECLARED. FOUND LT NR 4 SLAT TRANSMISSION TORQUE LIMITER TRIPPED. REPLACED PER AMM27-84-49-000-002-A AND 27-84-49-400-002-A FOR TYPE B ACTUATOR. ALL OTHER TRANSMISSION FOUND OK. SLAT SYS OPS CHECKS OK. CA T CHK ACP ALL CH
- [SDR CALA2017123004688](https://openairdocs.org/sdr/CALA2017123004688.md): Computer · faulty · Dec 30, 2017 · N838UA · Airbus A319131 · Leading Edge Slat Control System
  > FLT CONTROLS, SLATS FAULT DISPLAYED. EMERGENCY DECLARED. REMOVED AND REPLACED THE SFCC NR 1 AND 2 IAW AMM 27-5 1-34. ACCOMPLISHED BITE TEST IAW AMM 27-51-00-740-002-A, BITE TEST IAW AMM 27-81-00-740-002-A, OPS TESTED IAW AMM TASK 27-54-00-710 -002-A AND CAT
- [SDR CALA2017103003872](https://openairdocs.org/sdr/CALA2017103003872.md): Battery · faulted · Oct 30, 2017 · N838UA · Airbus A319131 · Emergency Lighting
  > DURING 2SVC CHK, FOUND FAULT DURING THE CABIN EMERGENCY LIGHTS OPERATIONAL TEST, SYSTEM FAULT ''EPSU BATTERY FWD LEFT". PERFORMED OPERATIONAL CHECK OF ESS ALL CHECKS NORMAL NO FAULTS FOUND REF AMM 33-51-38.
- [SDR CALA2017090303040](https://openairdocs.org/sdr/CALA2017090303040.md): Battery Pack · inoperative · Sep 3, 2017 · N838UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY LIGHT TEST FAILED AT PTP PANEL. REPLACED THE BATTERY AT EPSU 13WL IAW AMM 33-51-38. OK FOR SERVICE
- [SDR CALA2017060501727](https://openairdocs.org/sdr/CALA2017060501727.md): Lens · missing · Jun 5, 2017 · N838UA · Airbus A319131 · Emergency Lighting
  > 1L EXIT DOOR LIGHT LENS MISSING. REPLACED THE LENS.
- [SDR CALA2017052201534](https://openairdocs.org/sdr/CALA2017052201534.md): Slide · cracked · May 22, 2017 · N838UA · Airbus A319131 · Escape Slide
  > LT OVERWING SLIDE HAS 2 EACH CRACKS IN AREA 2 THAT EXTEND PAST LIMITS REF MM 25-62-42-210-002. REPLACED LT OVERWING ESCAPE SLIDE REF AMM25-62-42.
- [SDR CALA2017050101227](https://openairdocs.org/sdr/CALA2017050101227.md): Power Supply · no test · May 1, 2017 · N838UA · Airbus A319131 · Emergency Lighting
  > DURING TEST OF EMERGENCY BATTERIES, THE EPSU BATTERY AFT LT FAILED TO TEST. REPLACED EMERGENCY POWER SUPPLY. OPS CHECKED OK.
- [SDR CALA2017022400445](https://openairdocs.org/sdr/CALA2017022400445.md): Skin · dented · Feb 21, 2017 · N838UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > DENT IN RIGHT FORWARD FUSELAGE JUST BELOW AND FORWARD OF DOOR 1R. REPAIRED DENT IN FUSELAGE PER ECRA 5311-01852. ACP PERM REPAIR IN 335D OR 20 FEB 2018 TOMC-APPROVAL. ACCOMPLISH A PERMANENT REPAIR AT FR12-13 RT FUSELAGE SKIN JUST BELOW THE Z-520 FLOOR LEVEL PE
- [SDR CALA2016061595458](https://openairdocs.org/sdr/CALA2016061595458.md): Keelbeam · damaged · Jun 14, 2016 · N838UA · Airbus A319131 · Fuselage Main, Keel
  > DAMAGED HOLES ON KEELBEAM FOUND DURING ACP OF FCD 5330-05575, REV A. ALL HOLES REPAIRED IAW ECRA 5330-05726.

Next page: https://openairdocs.org/aircraft/N838UA/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 = 'N838UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N838UA/reports

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