# Service difficulty reports: N448UA

A list on [N448UA](https://openairdocs.org/aircraft/N448UA.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 · 117 reports

- [SDR CALA2026092819939](https://openairdocs.org/sdr/CALA2026092819939.md): Battery · discharged · Sep 27, 2026 · N448UA · Airbus A320232 · Emergency Equipment
  > FOUND FLIGHT DECK FLASHLIGHT NOT SEATED CORRECTLY, BATTERY DRAINED. REMOVED AND REPLACED THE FLASHLIGHT BATTERY AMM 25-65-00. OK FOR SERVICE.
- [SDR CALA2026090119171](https://openairdocs.org/sdr/CALA2026090119171.md): Unknown · odor · Aug 29, 2026 · N448UA · Airbus A320232 · Air Distribution System
  > FA REPORTED ODOR COMING FROM AFT GALLEY AIR VENT. OUTFLOW TEMP OF NR 2 PACK, 40C. GREATER THAN NR 1 PACK. NR 2 PACK OFF. ODOR DISAPAITED. NR 2 PACK FLOW CONTROL VALVE CLOSED & COND ZONE REGUL FAULT NOT ACTIVE. PERFORMED VISUAL INSP OF BOTH HEAT EXCHANGER T
- [SDR CALA2026083119039](https://openairdocs.org/sdr/CALA2026083119039.md): Unknown · odor · Aug 29, 2026 · N448UA · Airbus A320232 · Air Distribution System
  > AFTER 2ND ENG START, BURNING PLASTIC ODOR IN BACK WITH VISIBLE SMOKE IN AFT GALLEY. PILOT STATED THE PLASTIC ODOR RETURNED AFTER ENG 2 WAS STARTED & APU DESELECTED, ENG 1 ON. ACCOMPLISHED ENGINE RUN. ATTEMPTED TO REPLICATE FLT CREW ENGINE START PROCEEDURE A
- [SDR CALA2026022314023](https://openairdocs.org/sdr/CALA2026022314023.md): Plate · worn · Feb 12, 2026 · N448UA · Airbus A320232 · Nacelle/Pylon, Main Frame
  > LEFT PYLON AT LOWER RIB 5 SPAR AND CHAFE STRIP IS WORN. LEFT PYLON LOWER RIB 5 SPAR CHAFED WAS BLENDED PER SRM 54-51-12-283-003, AREA OF CHAFE IS 1 INCH FWD OF FASTENER ROW AND 6 INCHES FROM INBD EDGE. POST BLENDING AREA MEASURES: D=0.010, W-0.500, L=0.250.
- [SDR CALA2025110410857](https://openairdocs.org/sdr/CALA2025110410857.md): Fire Loop · out of position · Nov 3, 2025 · N448UA · Airbus A320232 · Fire Detection
  > NUMBER 2 ENG FIRE WARNING APPEARED TO ROLL 100 KTS. INDICATIONS CEASED CREW DEBRIEF: AFTER FIRE WARNING INDICATION, FO PULLED THROTTLES BACK AND WARNING STOPPED. GOT AN AVERAGE OF 1 TURN ON BOTH CLAMPS FOR THE 5TH STAGE CHECK VALVE, UPPER CLAMP ON THE PRSOV AN
- [SDR CALA2025101410053](https://openairdocs.org/sdr/CALA2025101410053.md): Filter · clogged · Oct 11, 2025 · N448UA · Airbus A320232 · Air Distribution System
  > CABIN AND FLIGHT DECKHAVE STRONG ODOR OF POSSIBLE TOXIC FUMES FOUND THAT THE SMELL WAS FROM THE APU BLEED. REPLACED BOTH RECIRCULATION FILTER CARTRIDGE REF AMM 21-21-41. RAN BOTH ENGINES FOR PACK BURN OFF AND REPLACED BOTH FILTERS AGAIN. SMELL NO LONGER PRESEN
- [SDR CALA2025091008720](https://openairdocs.org/sdr/CALA2025091008720.md): Unknown · odor · Sep 6, 2025 · N448UA · Airbus A320232 · Air Distribution System
  > FLIGHT CREW CLAIMS TO HAVE SMELLED A LIGHT ODOR IN CABIN AREA WHEN TURNING ON APU BLEED FOR AIR COND, IN COCKPIT AREA AND GALLEY AREAS FLIGHT CREW EXPOUNDED THAT ODOR WAS NOT THAT OF BURNING OR OF SMOKE, BUT A DIFFERENT KIND OF ODOR. RAN APU WITH APU BLEED OP
- [SDR CALA2025090808568](https://openairdocs.org/sdr/CALA2025090808568.md): None · none · Sep 6, 2025 · N448UA · Airbus A320232 · Standard Practices/Structures
  > ODD SMELL NOTICED BY MULTIPLE CREW MOSTLY IN COCKPIT, GLUEY-ISH IN NATURE UPON INSPECTION FOUND SMELL COMING FROM JET BRIDGE /PC AIR. COULD NOT FIND ANY ISSUES WITH ACFT. INSPECTED E&E BAYS, NO DEFECTS NOTED AT THIS TIME.
- [SDR CALA2024120501407](https://openairdocs.org/sdr/CALA2024120501407.md): Unknown · odor · Dec 2, 2024 · N448UA · Airbus A320232 · Air Distribution System
  > STRONG FUEL SMELL IN BACK OF PLANE DURING TAXIIN INSPECTED CABIN WITH APU RUNNING AND PACKS ON. NO FUEL SMELL NOTED. INSPECTED FUSELAGE FOR FUEL LEAKS NO EVIDENCE FOUND. FUEL SMELL MOST LIKELY CAME FROM ENGINE SHUTDOWN
- [SDR CALA2024051501476](https://openairdocs.org/sdr/CALA2024051501476.md): Fuel Cap · missing · May 12, 2024 · N448UA · Airbus A320232 · Fuel Storage
  > PDA 1 FUEL CAP REPORTED MISSING BY FUELER IN PHL WILL FOLLOW UP WITH PHL STATION IF LEFT BEHIND.IF FOUND WILL UPDATE LOGPAGE. FUEL CAP MISSING FUELING AND DEFUELING CAP MISSING. REQUESTING DEFERAL. APPROVED BY TOMC OK TO CONTINUE. C/W DDP DISPATCH DESK: 12 NAM
- [SDR CALA2023081802574](https://openairdocs.org/sdr/CALA2023081802574.md): Fuel Cap · missing · Aug 7, 2023 · N448UA · Airbus A320232 · Fuel Storage
  > PDA 2 REFERENCE 5387814 FUEL CAP MISSING PDA 3 LOG CREATED IAW GMM 02-30-95. VARGAS TOMC DOCUMENTED IAW GMM 02-30-95 FUEL CAP MISSING, VARGAS TOM. REPLACED FUEL CAP.ROTABLE PARTS CHANGE WAS INDICATED - TT # 1509941 SN OFF 2794 CAP, COUPLING R OFF 31-2825-9-0
- [SDR CALA2023062802061](https://openairdocs.org/sdr/CALA2023062802061.md): Actuator · warning light · Jun 24, 2023 · N448UA · Airbus A320232 · Compressor Bleed Control
  > ABORTED T/O AT 90 KIASFOR ENG 2 COMPRESSOR VANE ECAM. NO OTHER P ROBLEMS NOTED RAN PFR AND CFDS TEST, VERIFIED FAULT CODE PER FAULT FINDER VSV REPLACED VSV ACTUATOR ON ENGINE TWO PER AMM 75-32-41 UP TO STEP VERIFIED ENG 2 REVERSER AND COWLINGS CLOSED AND LATCH
- [SDR CALA2023040300967](https://openairdocs.org/sdr/CALA2023040300967.md): Beam · unknown · Mar 31, 2023 · N448UA · Airbus A320232 · Fuselage Main, Frame
  > DURING ACCOMPLISHMENT EA 5310-06784 REV A OP 003 (SB 53-1286 REV 01), HOLE DISCREPANCIES WERE NOTED ON LH/RH FR16/FR20 CROSSBEAMS. 5311-02962 PT 1 WITH NO DEVIATIONS. "LHS FR16 WAS REPLACED + LH/RH FR16/FR20 CROSSBEAM REPAIR IS A PERMANENT SOLUTION WITH INSPEC
- [SDR CALA2023040300966](https://openairdocs.org/sdr/CALA2023040300966.md): Crossbeam · unknown · Mar 31, 2023 · N448UA · Airbus A320232 · Fuselage Main, Frame
  > DURING ACCOMPLISHMENT EA 5310-06784 REV A OP 003 (SB 53-1286 REV 01), HOLE DISCREPANCIES WERE NOTED ON LH/RH FR16/FR20 CROSSBEAMS. 5311-02962 PT 1 WITH NO DEVIATIONS. "PLANNING TO CONTACT ENGINEERING AFTER 69,917FC''S, REQUIREMENTS ON THE LHS FR16 + LH/RH FR16
- [SDR CALA2023033100953](https://openairdocs.org/sdr/CALA2023033100953.md): Crossbeam · unknown · Mar 31, 2023 · N448UA · Airbus A320232 · Fuselage Structure (General)
  > DURING ACCOMPLISHMENT EA 5310-06784 REV A OP 003 (SB 53-1286 REV 01), HOLE DISCREPANCIES WERE NOTED ON LH/RH FR16/FR20 CROSSBEAMS. 5311-02962 PT 1 WITH NO DEVIATIONS. "PLANNING TO CONTACT ENGINEERING AFTER 69,917FC''S, REQUIREMENTS ON THE LHS FR16 + LH/RH FR16
- [SDR CALA2023033100936](https://openairdocs.org/sdr/CALA2023033100936.md): Unknown · damaged · Mar 30, 2023 · N448UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING ACCOMPLISHMENT OF EA 5310-07772 REV. ORIG OP 001 (SB 53-1383 R00), HOLES 2 &4 ON THE LH FRAME 35 AND HOLES 1, 2 & 3 ON THE RH FRAME 35 WERE FOUND DAMAGED. DURING REPAIR EMBODIMENT, HOLES #10 ON BOTH THE LH / RH SIDE WERE FOUND TO BE OUTSIDE OF EA 5310-0
- [SDR CALA2023033100930](https://openairdocs.org/sdr/CALA2023033100930.md): Frame · damaged · Mar 29, 2023 · N448UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING ACCOMPLISHMENT OF EA 5310-07772 REV. ORIG OP 001 (SB 53-1383 R00), HOLES 2 &4 ON THE LH FRAME 35 AND HOLES 1, 2 & 3 ON THE RH FRAME 35 WERE FOUND DAMAGED. DURING REPAIR EMBODIMENT, HOLES #10 ON BOTH THE LH / RH SIDE WERE FOUND TO BE OUTSIDE OF EA 5310-0
- [SDR CALA2023031300707](https://openairdocs.org/sdr/CALA2023031300707.md): Unknown · corroded · Mar 10, 2023 · N448UA · Airbus A320232 · Doors
  > FWD CARGO DOOR CUTOUT LOWER AREA BETWEEN FR24 TO FR28 ABOVE STRI NGER 38RH SHOWS SEVERAL CORROSION AS MARKED. REMOVED CORROSION IAW SRM 51-74-00 FROM FWD CARGO DOOR CUTOUT LO STA: ST ENG BFM WER AREA BETWEEN FR24 AND FR28 L=2" W=1.1" D=0.065" FOUND TO BE OUT O
- [SDR CALA2023031000683](https://openairdocs.org/sdr/CALA2023031000683.md): Door · corroded · Mar 10, 2023 · N448UA · Airbus A320232 · Doors
  > FWD CARGO DOOR CUTOUT LOWER AREA BETWEEN FR24 TO FR28 ABOVE STRI NGER 38RH SHOWS SEVERAL CORROSION AS MARKED. REMOVED CORROSION IAW SRM 51-74-00 FROM FWD CARGO DOOR CUTOUT LO STA: ST ENG BFM WER AREA BETWEEN FR24 AND FR28 L=2" W=1.1" D=0.065" FOUND TO BE OUT O
- [SDR CALA2023030600631](https://openairdocs.org/sdr/CALA2023030600631.md): Flange · cracked · Mar 4, 2023 · N448UA · Airbus A320232 · Fuselage Main, Attach Fittings
  > DURING HMV4 VISIT AT BFM ACCOMPL''G EA5341-01231 (B) CRACKS WERE FOUND AT FR68 LH STGR 22 WEB HORIZ FLANGE UPPER & LWR BOTTOM RADIUS. ADDITIONALLY, WHILE ACCOMPL''G EA5340-01724(C) OP2 A CRACK WAS NOTED AT FR68 LH DOOR STOP FITTING #1 WORK ACCOMPLISHED ON VTAE
- [SDR CALA2023022000480](https://openairdocs.org/sdr/CALA2023022000480.md): Stop · cracked · Feb 17, 2023 · N448UA · Airbus A320232 · Passenger/Crew Doors
  > EA 5340-01724 REV C, STEP 3.1-- FR 66 LEFTHAND AFT DOORSTOP #1 LOWER INBOARD FITTING HOLE CRACKED IN 2 PLACES "REPAIR BEFORE NE XT FLIGHT"
- [SDR CALA2023022000479](https://openairdocs.org/sdr/CALA2023022000479.md): Stop · cracked · Feb 17, 2023 · N448UA · Airbus A320232 · Fuselage Main, Attach Fittings
  > DURING ROTO INSP ON LH FR68 DOOR STOP #1. CRACK INDICATION NOTED IN LWR I/B HOLE. REPAIR BEFORE NEXT FLIGHT, REPAIRED LH FR68 DOOR STOP #1 LOWER I/B HOLE PER SRM 53-41-12-30 0-011. EMP: V934143 WC: 45467 STA: ST ENG BFM
- [SDR CALA2023012700211](https://openairdocs.org/sdr/CALA2023012700211.md): Seat Track · corroded · Jan 25, 2023 · N448UA · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN FED PASSENGER FR20 BETWEEN FLOOR PANEL 232DF AND 232EF THE SEAT TRACK FWD AREA HAS CORROSIOON DOT 68-39
- [SDR CALA2023012300182](https://openairdocs.org/sdr/CALA2023012300182.md): Seat Track · corroded · Jan 22, 2023 · N448UA · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN FWD PASSENGER FRAME 20 BETWEEN FLOOR PANEL 232FF AND 232EF THE SEAT TRACK FWD AREA HAD CORROSION. REMOVED AND REPLACED FLOOR BEAM Y-1292 BETWEEN FR12 TO FR24 IAW SRM 51-42-11.
- [SDR CALA2023012300175](https://openairdocs.org/sdr/CALA2023012300175.md): Seat Track · corroded · Jan 20, 2023 · N448UA · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > FWD CABIN BETWEEN FR16 TO FR20 SEAT TRACK Y1292 HAD CORROSION (10EA) PLACES.
- [SDR CALA2023012300174](https://openairdocs.org/sdr/CALA2023012300174.md): Floorbeam · corroded · Jan 20, 2023 · N448UA · Airbus A320232 · Fuselage Main, Floor Beam
  > CABIN FWD FLOOR STUCTURE RH FR20 THE FLOOR BEAM HAS CORROSION (0 1 EA) PLACE.
- [SDR CALA2023012300173](https://openairdocs.org/sdr/CALA2023012300173.md): Stringer · corroded · Jan 20, 2023 · N448UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AFT CARGO COMPARMENT FLOOR STRUCTURE THE STRINGER 43LH HAS SEVER AL CORROSION BETWEEN FR54 TO FR58.
- [SDR CALA2023012300172](https://openairdocs.org/sdr/CALA2023012300172.md): Floorbeam · corroded · Jan 20, 2023 · N448UA · Airbus A320232 · Fuselage Main, Floor Beam
  > CABIN FWD PASSENGER FRAME 20 UNDER FLOOR PANEL 232DF THE FLOORBEAM FWD AREA HAD CORROSION.
- [SDR CALA2023012300176](https://openairdocs.org/sdr/CALA2023012300176.md): Floor Support · corroded · Jan 20, 2023 · N448UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > CABIN FWD FLOOR SUPPORT LT BETWEEN FRAMES 16 - 20 THE FLOOR SUPPORT Y254 WAS CORRODED NINE PLACES.
- [SDR CALA2022082902216](https://openairdocs.org/sdr/CALA2022082902216.md): None · none · Aug 29, 2022 · N448UA · Airbus A300* · Hydraulic Handpump, Main
  > HYD Y RSVR LO LVL INFLIGHT. FLASHED SEVERAL TIMES AT CRUISE. MSG RETURNED AND INITIAL T/S FOUND HYD RES LEVEL WITHIN LIMITS, POST FLIGHT STAYED ON. REPLACED YELLOW RESERVOIR LOW LIMIT SWITCH. OPS CK NORMAL. NO LEAKS.
- [SDR CALA2022052301324](https://openairdocs.org/sdr/CALA2022052301324.md): Fuel Cap · missing · May 23, 2022 · N448UA · Airbus A320232 · Aircraft Fuel System
  > PDA 1 FUEL CAP MISSING ON ARRIVAL. OPBLM CHRISTIANSEN FUEL CAP PLACED ON CDL # 8636283.
- [SDR CALA2022030900623](https://openairdocs.org/sdr/CALA2022030900623.md): None · none · Mar 9, 2022 · N448UA · Airbus A320232 · Air Conditioning System
  > AFTER TAKEOFF POWERUP AT LESS THAN 50KTS PACK1FAULT LIGHT ECAM A NDMASTER CAUTION. RTO. CREW CONFIRMED WITH PACK #1 SWITCH OFF VLV IS CLOSED ON ECAM CREW COMPLIED WITH MEL STICKER APPLIED. REJECTED TAKEOFF BELOW 50 KTS. DEFERRED DIRECTLY BY TOMC APPLY MEL 2152
- [SDR CALA2021102201955](https://openairdocs.org/sdr/CALA2021102201955.md): None · missing · Oct 22, 2021 · N448UA · Airbus A320232 · Lighting System
  > PDA 3 RIGHT LANDING LIGHT BULB AND RETAINING RING MISSING AFTER LANDING AT MSY, LIGHT ASSEMBLY REPLACED REPLACED LANDING LIGHT ASSY
- [SDR CALA2021081601345](https://openairdocs.org/sdr/CALA2021081601345.md): Spoiler · inoperative · Aug 15, 2021 · N448UA · Airbus A320232 · Drag Control System
  > SPOILER SURFACE 1 RIGHT INOP - F-CTL SPLR 1L/1R FAULT. 1R IS EXTENDED. 1L IS RETRACTED.VIBRATION FELT. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. OP[S CHECK SPOILERS PER AMM 27-64-00, DEFER PER MEL 2764A IF RE
- [SDR CALA2020121801397](https://openairdocs.org/sdr/CALA2020121801397.md): Pressure Panel · damaged · Dec 17, 2020 · N448UA · Airbus A320232 · Fuselage Main, Structure
  > EA5330-05216 REV B OP 003 RT SIDE PRESSURE PANEL BETWEEN FR 35-3 6. ACCOMPLISHED EA 5330-05216 REV B OP 003 RT SIDE PRESSURE PANEL BETWEEN FR 35-36. THIS LOG PAGE WAS CREATED TO CORRECT ERROR ON LP 5613857, LOG WAS INCORRECTLY GENERATED AGAINST AIRCRAFT 4249
- [SDR CALA2020121801396](https://openairdocs.org/sdr/CALA2020121801396.md): Pressure Panel · damaged · Dec 16, 2020 · N448UA · Airbus A320232 · Fuselage Main, Structure
  > EA 5330-05216 REV B OP 003 R/H SIDE PRESSURE PANEL BETWEEN FR 35-36. ACCOMPLISHED EA 5330-05216 REV B OP003 RT SIDE PRESSURE PANEL BETWEEN FR 35-36. ADD EMP:V894270 INSP C/W THIS ITEM WAS ENTERED IN ERROR WAS FOR A/C N4248 ADD EMP:V891438. THIS ITEM WAS CR
- [SDR CALA2020020300325](https://openairdocs.org/sdr/CALA2020020300325.md): Unknown · vibration · Feb 3, 2020 · N448UA · Airbus A320232 · Engine (Turbine/Turboprop)
  > HIGH VIBE NO 1 ENGINEHIGHEST READING 1.0CURRENTLY 0.7 AT CRUISEF L 200 UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE DEBRIEF THE FLIGHT CREW FOR MORE INFORMATION. TAIL CLIMBING THROUGH FL220. IT WAS A MEDIUM FREQUENCY VIBRATION. ASKED THEM TO FILL OUT TH
- [SDR CALA2019051300762](https://openairdocs.org/sdr/CALA2019051300762.md): Cowling · peeling · May 11, 2019 · N448UA · Airbus A320232 · Engine Cowling System
  > PIECE OF ENGINE COWLING NR 1 ENGINE IS PEELED BACK INTO AIR STREAM. ON RIGHT OF PYLON ADDED PARTS NEEDED INFO TAPED SECURED PANEL STOPPED DRILL CRACK. INSPECT AFTER EACH FLIGHT FOR TAPE BEING SECURED. MUST BE REPLACED WITHIN 50 HOURS. INTERIM REPAIR ACCOMPLISH
- [SDR CALA2019032900491](https://openairdocs.org/sdr/CALA2019032900491.md): Seal · not reported · Mar 29, 2019 · N448UA · Airbus A320232 · Wing Miscellaneous Structure
  > REAL BAD SHUDDER FROM ACFT AT.79IMN AND 28300FT. RETURNED TO IAH. REFERENCE LOGPAGE 9247300, RT UNDERWING PANEL BULB SEAL REPLACED. ITEM IDENTIFIED ON AIRFRAME INSPECTION REFERENCE TSM 05-50-00-810-801-A.
- [SDR CALA2018031200895](https://openairdocs.org/sdr/CALA2018031200895.md): Floor Support · corroded · Mar 12, 2018 · N448UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > LT AFT DOOR ENTRANCE HAS EVIDENCE OF CORROSION UNDER THE FWD GIRT BAR BLANKING PLATE. REMOVED AND REPLACED DOOR SILL BEAM AT LT AFT DOOR AS PER SRM 51-42-11 AND DRAW D53480043.
- [SDR CALA2018011200173](https://openairdocs.org/sdr/CALA2018011200173.md): Light · malfunctioned · Jan 12, 2018 · N448UA · Airbus A320232 · Emergency Lighting
  > EMERGENCY LIGHT SYSTEM FAILED TO TEST. SHOWS EPSU UNIT FWD LT. RESET SYSTEM. THE EMERGENCY LIGHTS SYSTEM TESTED OK.
- [SDR CALA2016122101148](https://openairdocs.org/sdr/CALA2016122101148.md): Battery Pack · failed · Dec 21, 2016 · N448UA · Airbus A320232 · Emergency Lighting
  > AFT CABIN EEL BATTERY PACK FAILS CAPACITY CHECK. REPLACED BATTERY PACK REF AMM 33-51-38-000-002A AND 33-51-400- 002A. OPS CHECKED OK.
- [SDR CALA2016122101140](https://openairdocs.org/sdr/CALA2016122101140.md): Power Supply · faulted · Dec 21, 2016 · N448UA · Airbus A320232 · Emergency Lighting
  > LT OVERWING EXIT EMERGENCY POWER SUPPLY UNIT IS FAULTING DURING EEL TEST. REPLACED EPSU REF AMM 33-51-38-000-001A AND 33-51-38-400-001A. OPS CHECKED OK.
- [SDR CALA2014103192644](https://openairdocs.org/sdr/CALA2014103192644.md): Door Sill · corroded · Oct 28, 2014 · N448UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > R2 DOOR SILL CORRODED JUST AFT OF FRAME 68. R2 DOOR SILL WAS FOUND CORRODED OUT OF LIMITS BETWEEN FRAME 66 & 68 IAW SRM 53-41- 14 FIG 101. R & R R2 DOOR SILL BEAM IAW SRM 51-42-11.
- [SDR CALA2014102792613](https://openairdocs.org/sdr/CALA2014102792613.md): Skin Panel · contaminated · Oct 25, 2014 · N448UA · Airbus A320232 · Elevator, Plate/Skin
  > MAJOR REPAIR & SDR. RT ELEVATOR UPPER SKIN PANEL HAS TRAPPED WATER INDICATION 101.5 FROM INBD, 4.5 INCHES FROM TE, 3 INCHES DIAMETER. CUT OUT THE DAMAGED SKIN & CORE. REMOVED WATER APPLIED REPAIR & RESTORED FINISH IAW SRM 55-21-11 PARA 5E. REQUIRES RE-INSP
- [SDR CALA2014051391012](https://openairdocs.org/sdr/CALA2014051391012.md): Adiru · out of alignment · May 11, 2014 · N448UA · Airbus A320232 · Integrated Flight System
  > IR 2 & 3 FAULT. REALIGNED ADIRUS RESET FMGC 1 & 2 RETURNED TO NORMAL.
- [SDR CALA2014030390507](https://openairdocs.org/sdr/CALA2014030390507.md): Connector · not seated · Mar 3, 2014 · N448UA · Airbus A320232 · Light System Wiring
  > EMERGENCY LIGHT TEST FAILED ON 2 SERVICE. RE SEATED CONNECTOR ON LT EMERGENCY EXIT POWER SUPPLY, OPERATIONS CHECKED GOOD IAW 33-51-38.
- [SDR CALA2013123094034](https://openairdocs.org/sdr/CALA2013123094034.md): Flex Line · damaged · Dec 28, 2013 · N448UA · Airbus A320232 · Fuel Controlling System
  > NR 2 ENG P5 FLEXIBLE TUBE TO EEC DAMAGED. R & R P5 FLEX LINE IAW MM.
- [SDR CALA2013121293623](https://openairdocs.org/sdr/CALA2013121293623.md): Cowling · punctured · Dec 12, 2013 · N448UA · Airbus A320232 · Engine Cowling System
  > NR 2 ENG INLET COWL HAS A 3-16"X 1" PUNCTURE AT 10 O'CLOCK POSITION ON ACOUSTICAL LINER. ACCOMPLISHED REPAIR 2 IAW MT 71-006 ITEMS A THRU I, FINISHED REPAIR IAW MT71-006 ITEM L. REPAIR NEEDS A GRAPHITE COVER AT NEXT C CHECK IAW SRM 54-10-00 REPAIR 15.
- [SDR CALA2013120293342](https://openairdocs.org/sdr/CALA2013120293342.md): Proximity Sensor · faulty · Nov 29, 2013 · N448UA · Airbus A320232 · Landing Gear Position and Warning
  > NR 1 ADR & NR 3 ADR SHOW FAULTS. FAULTS RELATED NR 2 LGCIU FAILURE. REPLACED NR 2 LGCIU IAW MM32-31-71-400-001. NO MESSAGE FOR ADR'S. LGCIU SHOW SENSOR 23GA FAILURE. REPLACED NR 2 LT MLG EXT PROX SENSOR 23GA IAW AMM 32-31-73 PB401. NR 2 LGCIU BITE CHECKE

Next page: https://openairdocs.org/aircraft/N448UA/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 = 'N448UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N448UA/reports

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