# Service difficulty reports: N816UA

A list on [N816UA](https://openairdocs.org/aircraft/N816UA.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 · 115 reports

- [SDR CALA2026081718667](https://openairdocs.org/sdr/CALA2026081718667.md): Frame · cracked · Aug 14, 2026 · N816UA · Airbus A319131 · Fuselage Main, Frame
  > FRAME 68, STR 22L INNER CAP & WEB FLANGE HAS A CRACK INDICATIONS 5CM LONG AND 100% SH IAW AAR LCQ N/R 9296334/20334. REFERENCE LOG PAGES 9953498, 9962986 AND 9963050 FOR DIP AND WORK ACCOMPLISHMENTS.
- [SDR CALA2026081718663](https://openairdocs.org/sdr/CALA2026081718663.md): Gusset · damaged · Aug 14, 2026 · N816UA · Airbus A319131 · Fuselage Main, Structure
  > RIGHT FR 68 AT STGR 14 GUSSET 2EA LOWER HOLES HAVE REJECTABLE INDICATIONS IN GUSSET PLATE LAYER FROM ELONGATION. ALL WORK ACCOMPLISHED UNDER AAR SERVICE ORDER 375538, NONROUTINE 9296340, & ACCOMPLISHED IAW EC/RA 5311-02470 REV A.
- [SDR CALA2026081918729](https://openairdocs.org/sdr/CALA2026081918729.md): Skin · damaged · Aug 13, 2026 · N816UA · Airbus A319131 · Wing, Plate/Skin
  > RIGHT WING FUEL TANK PANEL 640JB LANDING HAS 1 HOLE OUT OF ROUND.PERFORMED REPAIR OF HOLE ON THE LANDING OF PANEL 640JB IAW SRM 57-21-11-300-002. HOLE REAMED TO 0.433 IN., COLD WORKED AND BUSH REPAIR INSTALLED IAW SRM 57-21-11-300-002, 51-44-11/001, 51-48-00/0
- [SDR CALA2026081418623](https://openairdocs.org/sdr/CALA2026081418623.md): Frame · cracked · Aug 13, 2026 · N816UA · Airbus A319131 · Fuselage Main, Frame
  > LEFT FRAME 68, STGR 22L INNER CAP AND WEB FLANGE HAD CRACK INDICATIONS, 5CM LONG AND 100% SH. PERFORMED REPAIR ON INNER CAP IAW EC/RA 5341-01580.
- [SDR CALA2026081418621](https://openairdocs.org/sdr/CALA2026081418621.md): Frame · cracked · Aug 13, 2026 · N816UA · Airbus A319131 · Fuselage Main, Frame
  > FRAME 68, STRINGER 22R INNER CAP AND WEB FLANGE HAD A CRACK INDICATION, 5CM LONG AT 100% SH. PERFORMED REPAIR ON INNER CAP IAW EC/RA 5341-01580.
- [SDR CALA2026081418589](https://openairdocs.org/sdr/CALA2026081418589.md): Fitting · cracked · Aug 12, 2026 · N816UA · Airbus A319131 · Fuselage Main, Structure
  > CRACK INDICATIONS THROUGH LH AND RH CONTINUITY FITTINGS AT WINDSHIELD CENTER POST LOWER ATTATCHMENT AREA PER AAR LCQ N/R 9296408/20408. ALL WORK ACCOMPLISHED UNDER ORDER 375538, NONROUTINE 9296408, THIS CLOSES THIS LOG PAGE.
- [SDR CALA2026072117906](https://openairdocs.org/sdr/CALA2026072117906.md): Skin · contaminated · Jul 19, 2026 · N816UA · Airbus A319131 · Elevator, Plate/Skin
  > LEFT ELEVATOR TOP SKIN PANEL, FOUND LIQUID ENGRESS INDICATION AT 125 INCHES FROM INBD EDGE & 12 INCHES FROM T/E. DEFECT IS 1 INCH DIA. REPAIRED LT ELEVATOR UPPER SKIN IAW SRM 55-21-11-300-004, CATEGORY A,
- [SDR CALA2026083119104](https://openairdocs.org/sdr/CALA2026083119104.md): Skin · chafed · Jul 13, 2026 · N816UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > EXTERNAL SKIN AT FR34, STR 43L AND STR 43R HAD CHAFE DAMAGE 14CM LONG X 2CM WIDE TO INCLUDE SIX DAMAGED FASTENERS. PERFORMED REWORK ON EXTERNAL SKIN AT FR34 BTWN STR 43L & STR 43R IAW EA 5300-02120, SRM 53-21-11-283-018. AS PER SRM 53-21-11-283-018, DAMAGE I
- [SDR CALA2026010912835](https://openairdocs.org/sdr/CALA2026010912835.md): Fuel Cap · missing · Jan 6, 2026 · N816UA · Airbus A319131 · Fuel Storage
  > FUEL CAP FOUND MISSING ITEM CREATED TO ACCOUNT PDA FUEL CAP CURRENTLY ON CDL REPLACED FUEL CAP IAW AMM 28-25-41-400-007-A.
- [SDR CALA2025070306196](https://openairdocs.org/sdr/CALA2025070306196.md): Fuel Cap · missing · Jun 30, 2025 · N816UA · Airbus A319131 · Fuel Storage
  > REFUEL CAP MISSING ON ARRIVAL. REPLACED MISSING REFUEL/DEFUEL CAP IRW AMM 28-25-41-400-005-A.
- [SDR CALA2025043004347](https://openairdocs.org/sdr/CALA2025043004347.md): Fuel Cap · missing · Apr 27, 2025 · N816UA · Airbus A319131 · Fuel Storage
  > PDA 2 FUELERS REPORTED FUEL CAP MISSING. NOTIFIED TOMC CONTROLLER JAY NEWMAN APPROVED CDL FOR FUEL CAP MISSING.REF LOG PAGE 4650533. INSTALLED UNDERWING FUEL CAP REF AMM 28-25-41-400-005
- [SDR CALA2025022602471](https://openairdocs.org/sdr/CALA2025022602471.md): Oven · fire · Feb 22, 2025 · N816UA · Airbus A319131 · Buffet/Galleys
  > OVEN 105 R11 IN FWD GALLEY HAD SMALL FLAME AND POSSIBLE DAMAGE TO INSIDE. REMOVED THE OVEN AT POSITION R11. INSPECTED THE OVEN EXTERNALLY AND ALSO THE COMPARTMENT FOR THE OVEN. VERIFY NO EVIDENCE OF HEAT DAMAGE IS PRESENT. THE FLAME WAS A PIECE OF FOOD INSI
- [SDR CALA2025011001850](https://openairdocs.org/sdr/CALA2025011001850.md): Oxygen Gen · no discrepancy · Jan 8, 2025 · N816UA · Airbus A319131 · Passenger Oxygen System
  > REF LP3459199 ENCOUNTERED SEVERE TURBULENCE ON DECENT AT AROUND 5-6K WITH AGGRESSIVE VERTICAL SHIFT OF THE AIRCRAFT THAT DEPLOYED ALL THE O2 MASKS. SMOOTH LANDING WITH AN EMERGENCY DECLARED. FA'S NOTICED A HOT SMELL IN THE CABIN THAT THE FIRE DEPARTMENT SUSPEC
- [SDR CALA2024121601528](https://openairdocs.org/sdr/CALA2024121601528.md): Battery · no test · Dec 16, 2024 · N816UA · Airbus A319131 · Emergency Lighting
  > CABIN EMERGENCY LIGHTING BATTERY CAPACITY OPERATIONAL CHECK. FOUND FWD BATTERY PACK 10WL, FAILED RED LIGHT. REPLACED EPSU BATTERY PACK, IAW 33-51-38-400-002-A0, OPS TEST GOOD.
- [SDR CALA2024112101234](https://openairdocs.org/sdr/CALA2024112101234.md): Fuel Cap · missing · Nov 21, 2024 · N816UA · Airbus A319131 · Fuel Storage
  > PDA 2 FUEL CAP REPORTED MISSING ON ARRIVAL. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. MAC METER INITIATED FOR WITH VENDOR ID V123456 MAC RELATED WORK ORDER 000000003122843 AND PRTR VERIFIED NO LEAKS FROM COUPL
- [SDR CALA2024082600491](https://openairdocs.org/sdr/CALA2024082600491.md): Packing · leaking · Aug 22, 2024 · N816UA · Airbus A319131 · Hydraulic System, Main
  > HYD Y SYSTEM LO PR ECAM MESSAGE WITH THE ASSOCIATED HYD Y RSVR LO LVL AND ENGINE 2 PUMP LO PR MESSAGES..... UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. CONTACT TOMC 847-700-9980 UPON A WALKAROUND INSPECTION FOU
- [SDR CALA2023100903007](https://openairdocs.org/sdr/CALA2023100903007.md): Skin · cracked · Oct 8, 2023 · N816UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > FOR THE REPAIR ACCOMPLISHED AT LH FR35 STR30 HOLES, PLANNING TO CONTACT ENGINEERING AFTER 29FEB2024 BUT BEFORE 15MAR2024, FOR THE EC 5331-03055 PART 3 PERMANENT REPAIR REQUIREMENTS. REF LP 5966875. THE EC 5331-03055 PART 3 PERMANENT REPAIR REQUIREMENTS. REF LP
- [SDR CALA2023100903006](https://openairdocs.org/sdr/CALA2023100903006.md): Skin · cracked · Oct 8, 2023 · N816UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > ACCOMPLISH PERMANENT REPAIR AT LH FR35 STR30 HOLE 2 AND HOLES A, B, AND C PER PART 3 OF THE LATEST REVISION OF ECRA 5331-03055 ON OR BEFORE 29MAR2024. OR BEFORE 29MAR2024. ACCOMPLISH PERMANENT REPAIR AT LH FR35 STR30 HOLE 2 AND HOLES A, B, AND C PER PART 3 OF
- [SDR CALA2023100302924](https://openairdocs.org/sdr/CALA2023100302924.md): Fitting · cracked · Sep 29, 2023 · N816UA · Airbus A319131 · Fuselage Main, Attach Fittings
  > RMLG DOOR ACTUATOR FITTING KEEL BEAM HOLE R16 AN R20 PRODUCED CRACK INDICATIONS IN THE 3 POSITION DURING LFEC INSPECTION FWD LUG. ACCOMPLISH A PERMANENT REPAIR FOR HOLES R1, R2, R12, R16, R18, PART 3B OF THE LATEST REVISION OF ECRA 5330-05721 ON OR BEFORE R20
- [SDR CALA2023092202848](https://openairdocs.org/sdr/CALA2023092202848.md): Panel · corroded · Sep 20, 2023 · N816UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT CARGO DRAIN MAST EXHAUST VENT INNER RETAINING PLATE HAS CORROSION BETWEEN RH STRG 38 AND 35 BETWEEN FRM 68 AND 69. RMV AND RPL AFT CARGO DRAIN MAST EXHAUST VEN INNER RETAINING PLATE REINFORCEMENT BETWEEN STRG 38R-STGR 35R AND BETWEEN FR68 AND FR69 IAW A319
- [SDR CALA2023091402778](https://openairdocs.org/sdr/CALA2023091402778.md): Door Sill · corroded · Sep 11, 2023 · N816UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > R2 PAX DOOR SILL AFT CORNER FITTING CORRODED GEN ON H AECO LCQ NR 9290566/40566 REMOVED AND REPLACED AFT CORNER FITTING ON FR 68 RT IAW A319 SRM 51-72-11.
- [SDR CALA2023091402777](https://openairdocs.org/sdr/CALA2023091402777.md): Door Sill · corroded · Sep 11, 2023 · N816UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > R2 PAX DOOR SILL HAS MULTIPLE SPOTS OF CORROSION, ON HAECO LCQ NR 9290565/40565 REMOVED AND REPLACED R2 DOOR SILL FR 66-68 IAW A319 SRM 51-72-11 P 1&2- INSTALLED ATTACHING PARTS IAW A319 SRM 51-72-11.
- [SDR CALA2023090502709](https://openairdocs.org/sdr/CALA2023090502709.md): Frame · cracked · Sep 4, 2023 · N816UA · Airbus A319131 · Fuselage Main, Structure
  > UPON REMOVAL OF R2 DOOR SILL FR 67 FRAME SEGMENT (STRAP) WAS FOUND TO HAVE CRACK ON UPPER I/B REDIUS. GEN BY V061616 ON HAECO LC Q NR 9290815/40815 REMOVED AND REPLACED FRAME SEGMENT STRAP AT FRAME 67 IAW A319 SR M 51-72-11 P 1&2 ACMP BY V052030 INSP BY V07988
- [SDR CALA2023090402699](https://openairdocs.org/sdr/CALA2023090402699.md): Gusset · cracked · Sep 3, 2023 · N816UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > R/H FR68 GUSSET #3 HOLE #3 HAS A INDICATION AT THE 12 O CLOCK PO SITION IN FRAME LAYER GEN BY V061632 ON NR 9290457/ 40457 REPAIRED RH FR68 GUSSET #3 HOLE #3 IAW ECRA 5311-02470 AS DIRECTED BY RFTS 60012.
- [SDR CALA2023090402698](https://openairdocs.org/sdr/CALA2023090402698.md): Gusset · cracked · Sep 3, 2023 · N816UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > R/H FR68 GUSSET #3, HOLE #3 AND #4 HAS A CRACK INDICATION AT THE 12 O''CLOCK POSITION IN FRAME LAYER (A3NB-53-4-6355) GENERATED BY MECH V061632 GENERATED AT HAECO LCQ PER NR 9290457 (40457) REPAIRED RH FR68 GUSSET HOLE #3 HOLE #4 IAW ECRA 5311-02470 AS D IRECT
- [SDR CALA2023090402693](https://openairdocs.org/sdr/CALA2023090402693.md): Shear Plate · gouged · Sep 2, 2023 · N816UA · Airbus A319131 · Fuselage Structure (General)
  > AFT WET AREA AFT L/H SHEAR PLATE MULTIPLE HOLES ARE ELONGATED AND GOUGE (A3NB-53-3-6357) PER HAECO LCQ NON ROUTINE 9290574/40574 GENERATED BY V937268. REMOVED AND REPLACED LH SHEAR PLATE IAW A319 SRM 51-42-11 PAGE 6 ACMP BY MECH V944156 INSP BY V061771
- [SDR CALA2023090402692](https://openairdocs.org/sdr/CALA2023090402692.md): Shear Plate · cracked · Sep 2, 2023 · N816UA · Airbus A319131 · Fuselage Structure (General)
  > AFT WET AREA AFT RH SHEAR PLATE CRACKED (A3NB-53-3-6357) PER HAE CO LCQ NON ROUTINE 9290567/40567 GENERATED BY V937268 REMOVED AND REPLACED RH SHEAR PLATE IAW A319 SRM 51-42-11 PAGE 6 AND 7. ACMP BY MECH V944156 INSP BY V061771
- [SDR CALA2023090402690](https://openairdocs.org/sdr/CALA2023090402690.md): Angle · cracked · Sep 2, 2023 · N816UA · Airbus A319131 · Emergency Exits
  > RH OVERWING EMERGENCY HATCH HAS SUSPECTED CRACK AT AFT VERTICAL SUPPORT @ RIVET POINTS (A3NB-05-3-6170) PER HAECO LCQ NON ROUTIN E 9290527/40527 GENERATED BY V899260 REMOVED FOR CRACK 2EA ANGLE SEGMENT FWD FR38 & AFT FR39 FROM R/H EMERGENCY DOOR & INSTALLED 2E
- [SDR CALA2023090402689](https://openairdocs.org/sdr/CALA2023090402689.md): Angle · cracked · Sep 2, 2023 · N816UA · Airbus A319131 · Emergency Exits
  > LH OVERWING EMERGENCY EXIT HAS SUSPECTED CRACKS AT FWD AND AFT VERTICAL SUPPORTS @ RIVET POINTS (A3NB-05-3-6171) PER HAECO LCQ NON ROUTINE 9290526/40526 GENERATED BY V899260 REMOVED CRACKED 2EA ANGLE SEGMENT AND INSTALLED NEW 2EA ANGLES SEGMENT FROM LH EMERGEN
- [SDR CALA2022051101210](https://openairdocs.org/sdr/CALA2022051101210.md): Fuel Cap · missing · May 11, 2022 · N816UA · Airbus A319131 · Aircraft Fuel System
  > PDA 3 FUEL CAP MISSING REPLACED MISSING FUEL CAP PART CHANGE UPDATE ROTABLE PARTS CHANGE WAS INDICATED - TT # 1613986 SN OFF 2830 CAP, COUPLING R OFF 31-2825-9-0001 2830 ON 31-2825-9-0001 0457
- [SDR CALA2022022400491](https://openairdocs.org/sdr/CALA2022022400491.md): Clamp · broken · Feb 24, 2022 · N816UA · Airbus A319131 · Potable Water System
  > REFERENCE 8020643, NEED TO ACCOMPLISH ECRA 2011-01000 DUE TO POTABLE WATER LEAK. NEED DEEP CLEANING FROM STA 19761FR47 TO STA 26695 FR64 DID INITIAL CLEAN UP,NEED FURTHER CLEAN FROM STA19761FR47 TO STA26895FR64 WATER LEAK WAS CONFINED TO BELOW THE FLOOR FROM
- [SDR CALA2021072101151](https://openairdocs.org/sdr/CALA2021072101151.md): Bolt · broken · Jul 20, 2021 · N816UA · Airbus A319131 · Wheel/Ski/Float
  > #1 MLG TIRE TIE BOLT BROKEN.. FOUND SHEAR TIE BOLT BROKEN AND MISSING FROM FAIRLY NEW TIRE UPDATING SDR REPLACED NUMBER 1 MAIN GEAR TIRE REF AMM32-41-11 WHEEL ASSYMBLY SERIAL NUMBER REMOVED 9336P INSTALLED SERIAL NUMBER 7106P. TIRE REMOVED WAS JUST INSTALLED Y
- [SDR CALA2020110601246](https://openairdocs.org/sdr/CALA2020110601246.md): Intercostal · cracked · Nov 4, 2020 · N816UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > R1 DOOR FRAME 16 STOP FITTING NR 7 LOWER INBOARD HOLE IS CRACKED IN THE WEB AT 1 O'CLOCK AND IN THE INTERCOASTAL AT 7 O'CLOCK REPAIR BEFORE NEXT FLIGHT CONTACT ENGINEERING FOR APPROVED REPAIR INSTRUCTIONS ON HAECO LCQ, REF 9298093 GEN BY V061633. REMOVED AND
- [SDR CALA2020072701078](https://openairdocs.org/sdr/CALA2020072701078.md): Battery Pack · failed · Jul 26, 2020 · N816UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY BATTERY 13WL FAILS TEST.
- [SDR CALA2020020300324](https://openairdocs.org/sdr/CALA2020020300324.md): Pump · inoperative · Feb 3, 2020 · N816UA · Airbus A319131 · Hydraulic Pump (Electric/Engine), Main
  > ECAM AFTER TAKEOFFHYD B LO PRESS REMOVED AND REPLACED THE BLUE HYDRAULIC SYSTEM ELECTRIC POMP PER
- [SDR CALA2019042900672](https://openairdocs.org/sdr/CALA2019042900672.md): Seal · damaged · Apr 29, 2019 · N816UA · Airbus A319131 · Engine (Turbine/Turboprop)
  > PDA 2 ENGINE 2 INBOARD FLEX SEAL SEGMENT IS BENT, BROKEN, CRACKED, WITH PIECE MISSING.
- [SDR CALA2018082701852](https://openairdocs.org/sdr/CALA2018082701852.md): Fitting · corroded · Aug 24, 2018 · N816UA · Airbus A319131 · Wing, Landing Gear Attach Fittings
  > LEFT MLG SIDESTAY UPPER CARDAN OTBD BUSHING ROTATING. REMOVED THE BUSHING. THE BORE AND SPOTFACED INBD & OTBD FACES TO REMOVE ALL CORROSION. ACCOMPLISHED ISSURANCE CUTS TO ALL REWORKED AREAS AND RESTORED CHAMFERS. INSTALLED A NEW BUSHING. HONED TO FINAL DI
- [SDR CALA2018082701851](https://openairdocs.org/sdr/CALA2018082701851.md): Bushing · damaged · Aug 24, 2018 · N816UA · Airbus A319131 · Wing, Landing Gear Attach Fittings
  > LEFT MLG SIDE STAY UPPER INBD CARDAN BUSHING WAS DAMAGED IN THE INBD FACE. REMOVED TWO INBD SIDE STAY BUSHINGS AND OVERSIZED INBD LUG BORE TO 3.2515 FINAL SIZE. INSTALLED NEW BUSHINGS & HONED TO FINAL DIMENTIONS. SEALED BUSHING FLANGES. INSTALLED NEW GREA
- [SDR CALA2018011200108](https://openairdocs.org/sdr/CALA2018011200108.md): Valve · leaking · Jan 12, 2018 · N816UA · Airbus A319131 · Hydraulic System, Main
  > RESERVOIR LOW DISPLAYED ON UPPER ECAM SCREEN. EMERGENCY DECLARED. FOUND SAFETY VALVE 49GA LEAKING AT SWITCH ASSY. REPLACED LANDING GEAR SAFETY VALVE IAW AMM 32-31-17-000-001, LEAK CHECKED GOOD. COMPLETED MM 32-31-17, TESTED SAFETY VALVE IAW MM 32 -31-00.
- [SDR CALA2018010100002](https://openairdocs.org/sdr/CALA2018010100002.md): Selector Valve · faulty · Jan 1, 2018 · N816UA · Airbus A319131 · Landing Gear Selector
  > GEAR WOULD NOT EXTEND NORMALLY AFTER CYCLING HANDLE 2 TIMES. HAD TO PERFORM MANUAL EXTENSION. EMERGENCY DECLARED. REMOVED AND REPLACED LDG SELECTOR VALVE REF AMM 32-31-12, EXTENSION & RETRACTION TESTS CHECK NORMAL. REMOVED AND REPLACED LDG SAFETY VALVE REF AM
- [SDR CALA2017033100768](https://openairdocs.org/sdr/CALA2017033100768.md): Controller · failed · Mar 29, 2017 · N816UA · Airbus A319131 · Cabin Pressure Controller
  > CREW REPORTED AT 6000 FT, CABIN PRESSURE LIGHT ON ECAM. AT 8000 FT, CREW RECEIVED A MASTER CABIN PRESSURE LIGHT. UNABL E TO CONTROL THE PRESSURIZATION AS CABIN CLIMBED. NEVER ASSENDED ABOVE 10000 FEET. TROUBLESHOT IAW TSM 21-31-00-810-831-A, AND FOUND A CP
- [SDR CALA2016082395663](https://openairdocs.org/sdr/CALA2016082395663.md): Actuator · malfunctioned · Aug 19, 2016 · N816UA · Airbus A319131 · Stabilizer Control System
  > HORIZONTAL STAB THSA NO BACK YOKE AFT INNER YOKE FLANGE IS CONTACTING THE BASE OF ROD SPHERE WITH DAMAGE TO FLANGE AND ROD SPHERE (AT THE PRIMER COLORED RINGS ON THE ROD SPHERE). THSA REQUIRES REPLACEMENT IAW EA 2744-01056 REV C OP 002 STEP 5.3. REF AMM27-44-
- [SDR CALA2016061395444](https://openairdocs.org/sdr/CALA2016061395444.md): Keelbeam · damaged · Jun 8, 2016 · N816UA · Airbus A319131 · Fuselage Main, Keel
  > DURING EG 1384, KEELBEAM, INSP 8 HOLES WERE FOUND TO BE DISCREPANT. ALL HOLES REPAIRED IAW ECRA 5330-05721.
- [SDR CALA2014092992321](https://openairdocs.org/sdr/CALA2014092992321.md): Actuator · failed · Oct 2, 2014 · N816UA · Airbus A319131 · Engine Bleed Air System
  > NR 1 ENGINE EGT OVERLIMIT DURING TAKEOFF. FAULTED 2.5 BLEED ACTUATOR. EXCEEDANCE RECORDED WAS 640 FOR 8 SECONDS. REPLACED 2.5 BLEED ACTUATOR IAW AMM 75-31-42-400-010-B13
- [SDR CALA2014033190719](https://openairdocs.org/sdr/CALA2014033190719.md): Flight Recorder · faulted · Mar 30, 2014 · N816UA · Airbus A319131 · Data Recorders (Flight/Maintenance)
  > DFDR FAULT DISPLAYED ON UPPER ECAM. SYS FAULT ECAM AT PARKING INTERMITTENT. NO PREVIOUS HISTORY LAST LEG & PLR NO FAULTS. OPERATIONS CHECKED GOOD IAW AMM 31-33-00-710-007.
- [SDR CALA2014021290360](https://openairdocs.org/sdr/CALA2014021290360.md): Oil System · overserviced · Feb 12, 2014 · N816UA · Airbus A319131 · Turbine Engine Oil System
  > ENG 2 OIL QTY GAUGE SHOWING AMBER XX. LATER OIL QTY INDICATOR BECAME NORMAL, SHOWING 26Q TS. REMOVED 2.5 QTS OF OIL IAW AMM 12-13-79, 5 MIN IDLE RUN QTY WITHIN ACCEPTABLE LIMITS & PRESENT IN ECAM AFTER ENG RUN, NO FURTHER SERVICE NEEDED.
- [SDR CALA2013120593485](https://openairdocs.org/sdr/CALA2013120593485.md): Pump · leaking · Dec 3, 2013 · N816UA · Airbus A319131 · Fuel Boost Pump
  > FLUID SEEP ON WALK AROUND. FOUND PUMP 37-QA LEAKING. REMOVED PUMP IAW AMM 28-21-51-000-002-A & INSTALLED PUMP IAW AMM 28-21-51-400-002-1 THRU STEP B 8. INSTALL PROC COMPLETED SEE SEQ 9562004.
- [SDR CALA2013112693277](https://openairdocs.org/sdr/CALA2013112693277.md): Pump · leaking · Nov 25, 2013 · N816UA · Airbus A319131 · Aircraft Fuel Distribution System
  > NR 1 CTR FUEL PUMP LEAKING. REMOVED NR 1 CTR FUEL PUMP REPLACE O-RING SEALS & PUMP, LEAK CHECKED GOOD IAW MM.
- [SDR CALA2013092391379](https://openairdocs.org/sdr/CALA2013092391379.md): Oxygen Mask · unsecure · Sep 19, 2013 · N816UA · Airbus A319131 · Passenger Oxygen System
  > O2 MASKS FELL IN ROW 8 DEF. REPACKED & ACCOMPLISHED TEST MT35-00.
- [SDR CALA2013090591035](https://openairdocs.org/sdr/CALA2013090591035.md): Seat Back · loose · Sep 4, 2013 · N816UA · Airbus A319131 · Passenger Compartment Equipment
  > SEAT BACK LOOSE & ROCKING AT 11E. SWAPPED A NUT FROM SEAT 32F, SEAT 11E WORKS NORMALLY. DEFER 32F IAW MEL, LOCKED UPRIGHT. INSTALLED LOCK NUT ON 32F SEAT STILL LOCKED UPRIGHT.

Next page: https://openairdocs.org/aircraft/N816UA/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 = 'N816UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N816UA/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.