# Service difficulty reports: N445UA

A list on [N445UA](https://openairdocs.org/aircraft/N445UA.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 · 131 reports

- [SDR CALA2025121212068](https://openairdocs.org/sdr/CALA2025121212068.md): Skin · damaged · Dec 11, 2025 · N445UA · Airbus A320232 · Trailing Edge Flaps
  > LEFT WING INBD FLAP HAS DAMAGE ON UPPER SURFACE FROM SCISSOR LIFT. REPAIRED LT WING INBD FLAP UPPER SURFACE ZONE 4 IAW SRM 51-77-12-911-002 AND ECRA 5752-02045 AND REO L25728. REPAIRED LT WING INBD FLAP UPPER SURFACE ZONE 4 IAW SRM 51- 77-12-911-002 AND EC/R
- [SDR CALA2025081807876](https://openairdocs.org/sdr/CALA2025081807876.md): Light · no discrepancy · Aug 16, 2025 · N445UA · Airbus A320232 · Standard Practices/Structures
  > SEAT ROW 21ABC REQUIRE CABIN EMERGENCY LIGHT TEST REF AMM 33-51-11-400-001-A. ACCOMPLISHED CABIN EMERGENCY LIGHT TEST REF AMM 33-51-11-400-001-A NORMAL. 21 ABC SEAT POWER CONNECTED EEL OP CHECK GOOD.
- [SDR CALA2025072106783](https://openairdocs.org/sdr/CALA2025072106783.md): Elec Connector · not seated · Jul 18, 2025 · N445UA · Airbus A320232 · Light System Wiring
  > EMERGENCY EXIT LIGHT IN ROW 24 SEAT C NOT ILLUMINATING CHECKED CONNECTION, CONNECTION SECURE. RELAMPED EMERGENCY LIGHT IN ROW 24 SEAT C PER AMM TASK 33-51-19-000-002-A. NO HELP. RESEATED CONNECTOR OPS CHECKED GOOD.
- [SDR CALA2025072106777](https://openairdocs.org/sdr/CALA2025072106777.md): Elec Connector · damaged · Jul 18, 2025 · N445UA · Airbus A320232 · Light System Wiring
  > EMERGENCY EXIT LIGHT OVERHEAD IN ROW 27 SEAT C NOT ILLUMINATING CHECKED CONNECTION, CONNECTION SECURE. NEEDS MORE TROUBLESHOOTING RELAMPED LIGHT BULBS FOR OVERHEAD EMERGENCY LIGHT IN ROW 27 SEAT C REF IPC 33-51-11-01. NO HELP. REINSTALLED 2 EACH PINS IN THE C
- [SDR CALA2025041003670](https://openairdocs.org/sdr/CALA2025041003670.md): Wire · disconnected · Apr 8, 2025 · N445UA · Airbus A320232 · Light System Wiring
  > NEED TO RECONNECT EMERGENCY LIGHTS AT SEAT ROWS 12 TO 25 LEFT SIDE. RECONNECTED EMERGENCY LIGHT WIRES TO SEATS, CLOSED ELECTRONIC BOXES. REPLACED 1 MISSING COVER. HAVE ANOTHER AMT TO CLOSED ELOTTO C/B, I KEPT ON GETTING ERROR MESSAGE TO CLOSE C/B. REF. TASK
- [SDR CALA2025041003669](https://openairdocs.org/sdr/CALA2025041003669.md): Power Supply · no test · Apr 8, 2025 · N445UA · Airbus A320232 · Emergency Lighting
  > OPERATIONAL CHECK OF CABIN EMERGENCY LIGHTS {A3NB-33-3-6012} - ESPU INT LOAD EMERGENCY LEFT. ESPU IS SEAT ROW 21 DADO PNL. 2 EXIT SIGNS ON DADO PANEL HAS 1 EACH BULB OUT. ORDERED ESPU. NEED TO CHANGE 2 BULBS FIRST. RELAMPED 2EA LIGHT BULB FOR LH OVERWING DOO
- [SDR CALA2025032503186](https://openairdocs.org/sdr/CALA2025032503186.md): Lamp · no test · Mar 24, 2025 · N445UA · Airbus A320232 · Emergency Lighting
  > OPERATIONAL CHECK OF CABIN EMERGENCY LIGHTS {A3NB-33-3-6012} - CIDS EMERG LIGHT TEST FAILS: EPSU INT LOAD FWD LH, ATA 33-51-38 RPLCD LAMPS AT LH LWR EXIT SIGN, CIDS EMERG LTS PASS REF AMM 33-51-38
- [SDR CALA2025010800057](https://openairdocs.org/sdr/CALA2025010800057.md): Panel · dented · Jan 6, 2025 · N445UA · Airbus A320232 · Engine Thrust Reverser
  > #2 ENG O/B T/R SLEEVE AFT OUTER SKIN DENTED PER HAECO LCQ N/R 9292111/20111 GEN BY V061642 REMOVED AND REPLACED #2 ENGINE O/B T/R SLEEVE IAW A320 AMM 78-32 -46-000-010-A/400-010-A BY MECH V077079 INSP BY V892285 ROTABLE PARTS CHANGE WAS INDICATED - TT # 179303
- [SDR CALA2024111101099](https://openairdocs.org/sdr/CALA2024111101099.md): Contactor · faulted · Nov 11, 2024 · N445UA · Airbus A320232 · Electrical Power System
  > ELEC DC ESS BUS SHEDECAM MSSG DSLAYED TSM TASK 24-60-00-810-810-A LOSS OF THE 28VDC SHED ESS BUS 801PP PERFORMED TSM 24-60-00-810-810-A. FOUND CB 1PH ( EMER/SHED/CONTOR/SPLY) OPEN. CLOSED CB AND WAIT 30 MIN, CB STAYS CLOSED. MSG CLEARED.TOMC RECOMMENDS REPLACI
- [SDR CALA2024110400984](https://openairdocs.org/sdr/CALA2024110400984.md): Contactor · failed · Nov 3, 2024 · N445UA · Airbus A320232 · Electrical Power System Wiring
  > FCDC 1 COCKPIT INDICATIONS. FOUND MULTIPLE MSGS ON ARRIVAL. TOP LEVEL MSG "ELEC DC ESS BUS SHED" WARNING REF TSM 24-60-00-810-801-A. FOUND CB 1PH POPPED. REF ASM 24-62-01 CB 1PH IS INLINE AND POWERS 8PH DC SHED ESS CONTACTOR. REPLACED 8PH REF AMM 24-62-55-401
- [SDR CALA2024061401800](https://openairdocs.org/sdr/CALA2024061401800.md): Warning Message · false activation · Jun 11, 2024 · N445UA · Airbus A320232 · Central Warning
  > RA1 CLASS 2 MSG AFTERSHUTDOWN CYCLED BREAKER K11 AND K12 IN REF TO AMM 34-42-00-740-002. MSG CLEARED ACCOMPLISHED TSM 34-43-00-740-001A LOSS OF RA1 DATA TO TCAS. ACCOMPLISHED TCAS BITE AS PER 34-43-00-810-817-A. MESSAGE NO LONGER PRESENT.
- [SDR CALA2024010900071](https://openairdocs.org/sdr/CALA2024010900071.md): Connector · not seated · Jan 6, 2024 · N445UA · Airbus A320232 · Hydraulic Power System Wiring
  > HAD -WHEEL N/W STRGFAULT- ECAM WITHAMBER -STEERING- MESSAGE ON W HEEL PAGE. LAST LEG REPORT ON BSCU 1&2 SHOWED FAULT STEERING ELECTRO HYDRAULIC MODULE (6GC). REF TSM 32-51-00-810-826-A, INSPECTED CONNECTOR ON MODULE FOUND CONNECTOR TO BE NOT ALL THE WAY SEATED
- [SDR CALA2023011600133](https://openairdocs.org/sdr/CALA2023011600133.md): Frame · mechanic error · Jan 16, 2023 · N445UA · Airbus A320232 · Fuselage Main, Structure
  > UPON REMOVAL OF CORNER FITTING AT FRAME 68 L2 DOOR HAS AN OUT OF ROUND HOLE LWR OUTBRD A3NB-53-3-6299 PER N/R 9292 471/36471. INITIAL INSP OF THE REPAIRED DOUBLE-DRILLED HOLE COMMON TO THE OF ECRA 5340-02083 ON OR BEFORE THE ACFT REACHES 60,000 TOTAL LOWER CO
- [SDR CALA2023011600132](https://openairdocs.org/sdr/CALA2023011600132.md): Not Reported · damaged · Jan 16, 2023 · N445UA · Airbus A320232 · Fuselage Main, Structure
  > PREVIOUSLY OVERSIZED FASTENER HOLES FOUND AT FR35 STGR28-31R DURING ACP OF EA 5310-07772 AD RELATED AD2016-14-03 PER NR9292442/3 6442. ACCOMPLISH INITIAL INSPECTION AT RH FR35 ECRA 5331-02989 ON OR BEFORE 99,172 TOTAL AIRCRAFT FLIGHT CYCLES STR30 HOLES #1, #2
- [SDR CALA2023011600131](https://openairdocs.org/sdr/CALA2023011600131.md): Crossbeam · cracked · Jan 16, 2023 · N445UA · Airbus A320232 · Fuselage Main, Structure
  > RIGHT FR 16 CROSSBEAM HOLE H7 HAS A CRACK INDICATION AT 6 O''CLOCK P OSITION, AT INERFACE OF CROSSBEAM AND FRAME. HOLE H10 HAS A REJE CTABLE INDICATION BOTH LAYERS FROM OUT OF ROUND CONDITION. PER NR 9292448/36448 & 9292449/36449, AD 2018-14-09. ECRA 5310-080
- [SDR CALA2023011600121](https://openairdocs.org/sdr/CALA2023011600121.md): Crossbeam · cracked · Jan 14, 2023 · N445UA · Airbus A320232 · Fuselage Main, Structure
  > RIGHT FR 20 CROSSBEAM, HOLE H36 HAS A REJECTABLE INDICATION IN B OTH LAYERS, FROM AND OF ROUND CONDITION. REPAIR RH FR 16 CROSSBE AM BEFORE NEXT FLIGHT PER STEP 9. (AD RELATED TASK 2018-14-09). REVISION OF ECRA 5310-08092 ON OR BEFORE THE AIRCRAFT REACHES 119
- [SDR CALA2023011600125](https://openairdocs.org/sdr/CALA2023011600125.md): Structure · cracked · Jan 14, 2023 · N445UA · Airbus A320232 · Passenger/Crew Doors
  > DOOR FR16 DOUBLE JOGGLE FASTENERS HOLE PRODUCED CRACK INDICATIONS AT THE 12:00 POSITION AND #10 PRODUCED CRACK INDICATIONS AT TH E 10:00 POSITION DURING THE ABHEC INSPECTION. GEN BY V061690 ON HAECO LCQ NR 92920382/36382 BY LCQ EMP V929087 AS PER ECRA 5311-029
- [SDR CALA2023011600117](https://openairdocs.org/sdr/CALA2023011600117.md): Fitting · damaged · Jan 13, 2023 · N445UA · Airbus A320232 · Fuselage Main, Structure
  > UPON REMOVAL OF CORNER FITTING AT FRAME 38 L2 DOOR HAS A OUT A OUT OF ROUND HOLE LOWER O/B A3NB-53-3-6299 PER HAECO LCQ N/R 9292 471/36471 OF THE LATEST REVISION OF ECRA 5340-02083 ON OR BEFORE THE AIRCRAFT REACHES 60000 TOTAL AIRCRAFT CYCLES. ACCOMPLISH INITI
- [SDR CALA2023011600116](https://openairdocs.org/sdr/CALA2023011600116.md): Shear Tie · damaged · Jan 13, 2023 · N445UA · Airbus A320232 · Fuselage Internal Mounting Structure
  > LH FR43 FOOT, 2EA IB FASTENER HOLES IN LOWER FRAME HAVE OUT OF ROUND INDICATIONS AD2020-18-06 PER NR9292505/36505 GEN BY V892444 V929087. AT LH FR43 FOOT ATTACHMENT REPAIRED HOLES, ACCOMPLISH ECRA 5331-02996 ON OR BEFORE 09JUL2023 V929087. AT LH FR43 FOOT ATTA
- [SDR CALA2023011600115](https://openairdocs.org/sdr/CALA2023011600115.md): Fitting · cracked · Jan 13, 2023 · N445UA · Airbus A320232 · Fuselage Main, Structure
  > FLIGHT DECK, AT WINDSHIELD CTR POST, LEFT AND RIGHT CONTINUITY F ITTINGS HAVE CRACK INDICATIONS ON UPPER FLANGE APPROX.55 INCH O UT FROM CENTER POST AD2020-17-03 PER NR9292350/36350 GEN BY V892 444 097. WORK C/W BY LCQ EMP V929087. FOR THE REPAIR TO THE FRONT
- [SDR CALA2023011300110](https://openairdocs.org/sdr/CALA2023011300110.md): Frame · cracked · Jan 11, 2023 · N445UA · Airbus A320232 · Fuselage Main, Frame
  > RH FR 16 CROSSBEAM HOLE H7 HAS A CRACK INDICATION AT 6 O''CLOCK P OSITION, AT INERFACE OF CROSSBEAM AND FRAME. HOLE H10 HAS A REJE CTABLE INDICATION BOTH LAYERS FROM OUT OF ROUND CONDITION. PER N R''S 9292448/36448 & 9292449/36449 AD 2018-14-09, ECRA 5310-0809
- [SDR CALA2022122303463](https://openairdocs.org/sdr/CALA2022122303463.md): Skin · corroded · Dec 21, 2022 · N445UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > INTERNAL FUSELAGE SKIN AFT OF AFT LAV EXHAUST VENT CORRODED. A3N B-53-3-0047. REMOVED AND REPLACED AFT LAV EXHAUST REENFORCEMENT PLATE IAW A32 0 SRM 51-42-11/001.
- [SDR CALA2022120203263](https://openairdocs.org/sdr/CALA2022120203263.md): Stringer Splice · corroded · Dec 1, 2022 · N445UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > FORWARD CARGO COMPARTMENT STRINGER 41L SPLICE HAS CORROSION FWD OF FR31. REMOVED AND REPLACED SPLICE ON FWD CARGO STRINGER 41LT AT FRAME 31 IAW A320 SRM 51-72-11-002.
- [SDR CALA2022112503217](https://openairdocs.org/sdr/CALA2022112503217.md): Intercostal · cracked · Nov 23, 2022 · N445UA · Airbus A320232 · Passenger/Crew Doors
  > SUPPORT TASK LH FWD EMERGENCY EXIT FWD AND AFT INTERNAL STRUCTUR E WEB SUPPORT CRACK PER HAECO LCQ NON-ROUTINE 9292096/36096 GENE RATED BY V061682. REMOVED & REPLACED FWD & AFT INTERNAL STRUCTURE WEBS ON L/H FWD EMERGENCY EXIT DOOR IAW A320 SRM 51-72-11-911-00
- [SDR CALA2022092602522](https://openairdocs.org/sdr/CALA2022092602522.md): None · none · Sep 26, 2022 · N445UA · Airbus A300* · Fuselage Structure (General)
  > ECAM CAUTION MESSAGE - Y RSVR LO LVL MESSAGE INOP - REPLACED DAMAGED UNION O-RING TO DUAL VALVE. SERVICED YELLOW ACCUMULATOR TO PROPER LEVEL. COMPLIED WITH ALL LEAK CHECKS AND SYSTEM CHECKS FOR NORMAL OPERATION OF HYDRAULICS.
- [SDR CALA2022052301313](https://openairdocs.org/sdr/CALA2022052301313.md): Fitting · gouged · May 21, 2022 · N445UA · Airbus A320232 · Empennage Structure
  > DURING REMOVAL OF THE RUDDER, VERTICAL STABILIZER HINGE FITTINGS NO.2 FOUND WITH PLAY AND GOUGE. REPLACEMENT IS REQUIRES AS NOTED ON LTPR NR# 5001156950-0010 REF BQN LHT LOG NUMBER 50001156950-0010. REPLACED RUDDER HINGE FITTING #2 PER SRM 55-36-42-300-008. R
- [SDR CALA2022052301312](https://openairdocs.org/sdr/CALA2022052301312.md): Fitting · gouged · May 21, 2022 · N445UA · Airbus A320232 · Empennage Structure
  > DURING REMOVAL OF THE RUDDER, VERTICAL STABILIZER HINGE FITTINGS NO.7 FOUND WITH PLAY AND GOUGE. REPLACEMENT IS REQUIRED AS NOTED ON LTPR NR# 5001156958-0010. REF BQN LHT LOG 5001156958-0010.REPLACED RUDDER HINGE FITTING #7 PER SRM 55-36-42-300-008. REPLACEMEN
- [SDR CALA2022052301311](https://openairdocs.org/sdr/CALA2022052301311.md): Fitting · gouged · May 21, 2022 · N445UA · Airbus A320232 · Empennage Structure
  > DURING REMOVAL OF THE RUDDER, VERTICAL STABILIZER HINGE FITTINGS NO.3 FOUND WITH PLAY AND GOUGE.REPLACEMENTE IS REQUIRED AS NOTED ON LTPR NR#5001156951-0010. REPLACED #3 HINGE FITTING. REPLACEMENT REQUIRED IAW SRM REF BQN LHT NRC 5001156951-0010. 55-36-42-300-
- [SDR CALA2022052301310](https://openairdocs.org/sdr/CALA2022052301310.md): Fitting · gouged · May 21, 2022 · N445UA · Airbus A320232 · Empennage Structure
  > DURING REMOVAL OF THE RUDDER, VERTICAL STABILIZER HINGE FITTINGS NO.6 FOUND WITH PLAY AND GOUGE. REPLACEMENT IS REQUIRED AS NOTED ON LTPR NR# 5001156957-0010. REPLACED #6 HINGE FITTING. REPLACEMENT REQUIRED IAW SRM REF BQN LHT NRC 5001156957-0010 55-36-42-300-
- [SDR CALA2022052301309](https://openairdocs.org/sdr/CALA2022052301309.md): Fitting · gouged · May 21, 2022 · N445UA · Airbus A320232 · Empennage Structure
  > DURING REMOVAL OF THE RUDDER, VERTICAL STABILIZER HINGE FITTINGS NO.4 FOUND WITH PLAY AND GOUGE. REPLACEMENT IS REQUIRED AS NOTED ON LTPR NR# 5001156954-0010. REPLACED #4 HINGE FITTING. REPLACEMENT REQUIRED IAW SRM REF BQN LHT NRC 5001156954-0010 55-36-42-300-
- [SDR CALA2022052301306](https://openairdocs.org/sdr/CALA2022052301306.md): Fitting · loose · May 20, 2022 · N445UA · Airbus A320232 · Empennage Structure
  > RUDDER HINGE BEARINGS/FITTINGS BR1 AND BR5 HAVE EXCESSIVE PLAY. LTPR NR# 5001156747-0010(BR1), 5001156956-010(BR5). AT 60000FC FROM TIME OF COMPONENT FIRST FLIGHT, SUBSEQUENT SRI 55-36-42-205-004 TABLE 001. INSPECTION INTERVALS AND METHOD OF INSPECTION ARE TBD
- [SDR CALA2022052001284](https://openairdocs.org/sdr/CALA2022052001284.md): Beam · corroded · May 18, 2022 · N445UA · Airbus A320232 · Fuselage, Wing Attach Fittings
  > DURING REMOVAL OF NTF ON AFT WET AREA, CORROSION FOUND ON PREVIOUS REPAIR OF L2 DOOR SILL BEAM, EVALUATION IS RECORDED UNDER LP# 8445827. PERFORMED INSTALLATION OF REPAIR PARTS OH LH DOOR 2 SILL BEAM FR.68 IAW A320-200 SRM 53-41-14-300-001 REV 140, AS NOTED ON
- [SDR CALA2021061800899](https://openairdocs.org/sdr/CALA2021061800899.md): Battery Pack · no test · Jun 18, 2021 · N445UA · Airbus A320232 · Emergency Lighting
  > REF 2SVC. EMERGENCY LIGHT TEST FAILS. FAULTS EPSU BATTERY FWD L 33-51-38. REPLACED FWD LEFT BATTERY PACK,TEST CK GOOD.
- [SDR CALA2021060700804](https://openairdocs.org/sdr/CALA2021060700804.md): Bleed Valve · failed · Jun 7, 2021 · N445UA · Airbus A320232 · Compressor Bleed Valve
  > ENG 1 EPR AND N1 SURGING DURING T/O AND CLB. NO EGT SURGING. ENG SETTLED BY 9000. DID A ELECTRICAL TEST OF THE PNEUMATIC BMC 1 AND 2 TEST IN REF TSM 71-00-00-810-832-A. TEST PASS. OPS CHECK GOOD. NO HISTORY. AS PER LP 6421143, 7A BLEED VALVE FAILS THE FUNCTION
- [SDR CALA2021053100772](https://openairdocs.org/sdr/CALA2021053100772.md): Lanyard · missing · May 31, 2021 · N445UA · Airbus A320232 · Fuel Storage
  > PDA 3 VERBAL FUELER REPORT - FUEL CAP LANYARD RING MISSING. INSTALLED RING FOR FUEL CAP LANYARD.
- [SDR CALA2020071201045](https://openairdocs.org/sdr/CALA2020071201045.md): Battery · faulted · Jul 6, 2020 · N445UA · Airbus A320232 · Emergency Lighting
  > EMERGENCY EXIT LIGHT SYSTEM HAS FAULT OF ESPU BATTERY EMER R. REPLACED EPSU BATTERY PACK IAW AMM 33-51-38-000-002-A & 33-51-38-400-002-A. OPS CHECKED OK. ACCOMPLISHED IDT INSPECTION OF REPLACED BATTERY IAW GMM 09-10-05.
- [SDR CALA2020040300772](https://openairdocs.org/sdr/CALA2020040300772.md): Pressure Panel · cracked · Apr 1, 2020 · N445UA · Airbus A320232 · Fuselage Main, Structure
  > LH SIDE PRESSURE PANEL BETWEEN FR 35-36. NOTED CRACKS IN THE FOL LOWING HOLES: #1/2/4/5/6/7/8/9/10/13/14/17/20/22/26. NOTED REJEC TABLE INDICATIONS ON THE FOLLOWING HOLE # 30/32/34/35/38/39/40/4 3/45/46/48/53/54/58/59/60/63/65 AND I/B BRACKET HOLES: UPPER AND
- [SDR CALA2020040300771](https://openairdocs.org/sdr/CALA2020040300771.md): Power Supply · faulted · Apr 1, 2020 · N445UA · Airbus A320232 · Emergency Lighting
  > "ESPU UNIT FWD L" FAULT IS DISPLAYED ON THE PTP EMERGENCY LIGHTS TEST-A3NB-33-3-6012 PER HAECO LCQ N/R# 9296490 GENERATED REMOVED AND REPLACED L/H FWD ESPU 10WL IAW A320 AMM 33-51-38-000 -001-A & A320 AMM 33-51-38-420-050-A. SYSTEM OPERATION CHECKS GO OD IAW A
- [SDR CALA2020033000747](https://openairdocs.org/sdr/CALA2020033000747.md): Door Frame · cracked · Mar 29, 2020 · N445UA · Airbus A320232 · Fuselage Main, Structure
  > AD 2018-25-02 L1 FRAME 16 DOOR STOP #1 INBOARD LOWER HOLE IS CRACKED IN THE WEB AND INTERCOSTAL LAYERS ON HAECO LCQ REF 9296352 SPEC A3NB-53-4-0017 GENERATED HAECO TECHNICIAN AND QC REPAIRED FR16 LH STOP FIT TING #1 HOLES #3 AND #4 IN WEB IAW ECRA 5311-02428 P
- [SDR CALA2020033000743](https://openairdocs.org/sdr/CALA2020033000743.md): Door Frame · cracked · Mar 29, 2020 · N445UA · Airbus A320232 · Fuselage Main, Structure
  > AD 2018-25-01 FRAME 2O R1 DOOR STOP #1 INBOARD LOWER HOLE IS CRA CKED IN THE WEB AND INTERCOSTAL LAYERS ON HAECO LCQ REF 9296200 SPEC A3NB-53-4-0018 GENERATED HAECO AND REPAIRED FR20 RH STOP FITT ING #1 HOLES #3 AND #4 IAW ECRA 5311-02427 PART 1. DTA LOG PAGE
- [SDR CALA2020033000741](https://openairdocs.org/sdr/CALA2020033000741.md): Intercostal · cracked · Mar 27, 2020 · N445UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > FRAME 16 R1 DOOR STOP #1 INBOARD LOWER HOLE IS CRACKED IN THE IN TERCOSTAL. AD 2018-25-02, A3NB-53-4-0018. PER HAECO LCQ N/R# 929 6198 GENERATED. REMOVED AND REPLACED FR 16 R1 DOOR #1 INTERCOSTAL IAW A320 SRM 5 1-72-11, 51-44-11, 51-42-11. AND 53-11-13-02A.
- [SDR CALA2020032700702](https://openairdocs.org/sdr/CALA2020032700702.md): Intercostal · cracked · Mar 24, 2020 · N445UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > L1 FRAME 16 DOOR STOP #7 INBOARD UPPER AND LOWER HOLE IS CRACKED IN THE INTERCOSTAL LAYER. AD2018-25-02: A32NB-53-4-0017 PER HAE CO LCQ N/R# 9296354 GENERATED. REMOVED AND REPLACED L1 FRAME 16, INTERCOSTAL ATR DOOR STOP #7 A TTACH LOCATION IAW A320 SRM 51-72-1
- [SDR CALA2020032700697](https://openairdocs.org/sdr/CALA2020032700697.md): Intercostal · cracked · Mar 23, 2020 · N445UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > FRAME 16 R1 DOOR STOP #7 INBOARD UPPER AND LOWER HOLES ARE CRACK ED IN THE INTERCOASTAL. A3NB-53-4-0018; AD 2018-25-02 PER HAECO LCQ N/R 9296197 GENERATED. REMOVED FASTENERS, REMOVED #7 INTERCOASTAL AT FR-16 (CRACKED) RE CEIVED NEW INTERCOSTAL AND INSTALLED IA
- [SDR CALA2018112302410](https://openairdocs.org/sdr/CALA2018112302410.md): Warning Message · false activation · Nov 22, 2018 · N445UA · Airbus A320232 · Hydraulic Accumulator, Auxiliary
  > B RSVR LO LVL DISPLAYED ON UPPER ECAM SCREEN. - HYD GREATED CREW, STATED ALL HYD LEVELS NORMAL, NO ABNORMAL FLIGHT INDICATIONS. NO HYD FLUID LEAKING, A/C MOVED FROM GATE.
- [SDR CALA2018022500803](https://openairdocs.org/sdr/CALA2018022500803.md): Battery · failed · Feb 25, 2018 · N445UA · Airbus A320232 · Emergency Lighting
  > THE FWD L EMERGENCY LIGHTING EPSU FAILS THE CAPACITY TEST. REMOVED AND REPLACED FWD L/M EPSU BATTERY IAW AMM 33-51-38-000-002-A AND 33-51-38-400-002-A AND PERFORMED BATTERY CAPACITY TEST IAW AMM 33-51-00-710-003-A AND NO DEFECTS NOTED.
- [SDR CALA2018022500802](https://openairdocs.org/sdr/CALA2018022500802.md): Battery · failed · Feb 25, 2018 · N445UA · Airbus A320232 · Emergency Lighting
  > OPERATIONAL CHECK OF CABIN EMERGENCY LIGHTING BATTERY CAPACITY FAILS WITH MSG "EMR L". REMOVED AND REPLACED LT ESPU BATTERY IAW AMM 33-51-38-000-002-A AND 33-51-38-400-002-A AND PERFORMED BATTERY CAPACITY TEST IAW AMM 33-51-00-710-003-A AND NO DEFECT NOTED.
- [SDR CALA2018022500801](https://openairdocs.org/sdr/CALA2018022500801.md): Battery · failed · Feb 25, 2018 · N445UA · Airbus A320232 · Emergency Lighting
  > OPERATIONAL CHECK OF CABIN EMERGENCY LIGHTING BATTERY CAPACITY FAILS WITH MSG "EMER AFT L". REMOVED AND REPLACED AFT L/M ESPU BATTERY IAW AMM 33-51-38- 000-002-A AND 33-51-38-400-002-A AND PERFORMED BATTERY CAPACITY TEST IAW AMM 33-51-00-710-003-A AND NO DEFE
- [SDR CALA2018022500800](https://openairdocs.org/sdr/CALA2018022500800.md): Reservoir · low pressure · Feb 25, 2018 · N445UA · Airbus A320232 · Escape Slide
  > LT OVERWING SLIDE RESERVOIR BOTTLE PRESSURE AT 0. REMOVED AND REPLACED LT OVERWING SLIDE RESERVOIR BOTTLE ASSY IAW AMM 25-62-46-400-001. PRESSURE INDICATION TBT THROUGH CIDS IS GOOD.
- [SDR CALA2018021800680](https://openairdocs.org/sdr/CALA2018021800680.md): Slide · damaged · Feb 18, 2018 · N445UA · Airbus A320232 · Escape Slide
  > R2 DOOR, GREEN LANYARD ON BOTTOM OF THE SLIDE PANEL PARTIALLY SHEARED AND SLIDE UNRAVELLED. REMOVED AND REPLACED THE DOOR SLIDE IAW AMM 25-62-44-400-8 02. OPS AND FUNCTIONAL CHECKED GOOD.
- [SDR CALA2017100203421](https://openairdocs.org/sdr/CALA2017100203421.md): Power Supply · no test · Oct 2, 2017 · N445UA · Airbus A320232 · Emergency Lighting
  > PERFORMED EMERGENCY LIGHT OPS CHECK IAW 18-0550-1-0002. RECEIVED A FAULT CODE FOR EPSU BATTERY EMERGENCY L,EPSU UNIT AFT L. REMOVED AND REPLACED THE ESPU IAW AMM 33-51-38. OPS CHECKED SAT.

Next page: https://openairdocs.org/aircraft/N445UA/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 = 'N445UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N445UA/reports

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