# Service difficulty reports: N438UA

A list on [N438UA](https://openairdocs.org/aircraft/N438UA.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 · 127 reports

- [SDR CALA2026102220530](https://openairdocs.org/sdr/CALA2026102220530.md): Plate · corroded · Oct 20, 2026 · N438UA · Airbus A320232 · Fuselage Main, Structure
  > AFT CARGO BAY, AFT LAV EXHAUST VENT BETWEEN FR 69 & FR 70, STR 30R - 33R HAD CORROSION ON LOWER, INBD SIDE AT CONTACT POINT OF VENT OUTLET & AIRFRAME. R & R THE PLATE, FR 69-70 S30-33R IAW SRM 53-41-00-210 -030-C1, SRM 53-41-11-283-065, & SRM 51-72-11-911-001
- [SDR CALA2026102220520](https://openairdocs.org/sdr/CALA2026102220520.md): Sign · missing · Oct 20, 2026 · N438UA · Airbus A320232 · Emergency Lighting
  > MAIN CABIN EMERGENCY EXIT IDENTIFIERS AT THE LT & RT OVERWING HATCH (4EA, FWD AND AFT) ARE NOT INSTALLED. INSTALLED MAIN CABIN EMERGENCY EXIT IDENTIFIERS AT THE LT & RT OVERWING HATCHES FWD AND AFT IAW AMM 33-51-13-400-001-A OPS CHECK GOOD IAW AMM 33-51-13-4
- [SDR CALA2026092119596](https://openairdocs.org/sdr/CALA2026092119596.md): Transceiver · faulted · Sep 17, 2026 · N438UA · Airbus A320232 · Weather Radar System
  > ELECTRICAL BURNING ODOR AFTER LANDINGPICTURE UPDATE. BRIEFED FLIGHT CREW. CREW STATED A BURNING ODOR WAS PRESENT IN FLIGHT DECK, AND WAS NOTIEABLE UPON ENTERING THE COCKPIT. CAPT ALSO REPORTED HEARING A CRACKLING/POPPING NOISE NEAR THE LT INSTRUMENT PANEL. V
- [SDR CALA2026081918736](https://openairdocs.org/sdr/CALA2026081918736.md): Battery · faulted · Aug 18, 2026 · N438UA · Airbus A320232 · Emergency Lighting
  > EPSU EMERGENCY LEFT BATTERY MESSAGE DISPLAYED ON EMERGENCY BATTERY TEST REPLACED EPSU BATTERY IAW AMM 33-51-38.
- [SDR CALA2026033014900](https://openairdocs.org/sdr/CALA2026033014900.md): Hydraulic Line · broken · Mar 27, 2026 · N438UA · Airbus A320232 · Hydraulic System, Main
  > IN FLIGHT ECAMG SYS LO PRESSUREG RSVR LO LVLG ENG1 PUMP LO PR LOCKING LOG CAPT STATED THEY FOLOWED PROCEDURES AFTER ECAM WARNING. PUMP RAN APROX 2MIN AFTER ECAM WARNING FOR G HYD LOW PRESS AS THEY FOLLOWED CHECKLIST. HYD FLUID COMING FROM ENG 1 PYLON. ZONE C
- [SDR CALA2026012913428](https://openairdocs.org/sdr/CALA2026012913428.md): Seal · damaged · Jan 26, 2026 · N438UA · Airbus A320232 · Windshield/Door Rain/Ice Removal
  > SOUNDED LIKE ELECTRICAL ARCING & STATIC SIZZLING. SPOKE WITH FLT CREW. FLIGHT CREW CONFIRMED THE INITIAL POPPING SOUND FOLLOWED SIZZLING SOUND THROUGHOUT THE ENTIRE FLIGHT AS RECORDED BY CAPTAIN. UPON INSPECTION OF CAPTAINS SIDE, FIXED WINDOW, ON EXTERIOR, FOU
- [SDR CALA2025102410479](https://openairdocs.org/sdr/CALA2025102410479.md): Battery Pack · failed · Oct 22, 2025 · N438UA · Airbus A320232 · Emergency Lighting
  > CABIN EMERGENCY LIGHTING CARD 18-3351-1-0003 IS FAILING FOR EPSU BATTERY EMERGENCY LIGHT. IAW MM 33-51-38, REMOVED AND REPLACED BATTERY OF 11WL & 13WL EPSU'S OPS CK'D GOOD.
- [SDR CALA2025090208387](https://openairdocs.org/sdr/CALA2025090208387.md): Skin · dented · Aug 22, 2025 · N438UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > UPPER FUSELAGE DENT APROX.5" FWD OF FR 12 & 1" ABOVE STGR 1L. PERFORMED A DOUBLER REPAIR TO EXTERNAL SKIN AT LOCATION OF DAMAGE FR12 STRG 1L IAW SRM 53-11-11-300-054. THIS IS A CATEGORY B REPAIR.
- [SDR CALA2025081107522](https://openairdocs.org/sdr/CALA2025081107522.md): Lavatory · odor · Aug 7, 2025 · N438UA · Airbus A320232 · Lavatories
  > AFT LAV D GIVING VERYROUGH SMELL. NO WASTE VISIBLE. STARTED SMELLING AFTER TAKEOFF, NOTIFY LAV SERVICE TO DUMP AND RESERVICE LAV SYS, NO WATER OR WASTE LEAKS NOTED, NO FOUL ODORS NOTED AT AFT LAV D.
- [SDR CALA2025061205488](https://openairdocs.org/sdr/CALA2025061205488.md): Proximity Sensor · dirty · Jun 8, 2025 · N438UA · Airbus A320232 · Door Warning System
  > DOOR 2L SHOWS ARMED ONECAM. BUT F/A SAYS DOORSHOWING DISARMED. CLEANED ARM/UNARMED PROX SENSOR, NO HELP REMOVED AND REPLACED ARMED/UNARMED PROX SENSOR DOOR 2L REF AMM 52-71-11, AJUSTED AND OPS CHECK GOOD PER AMM 52-71-00 VERIFIED REPLACEMENT OF #2 L DOOR PROX
- [SDR CALA2025041603894](https://openairdocs.org/sdr/CALA2025041603894.md): Slide · no discrepancy · Apr 13, 2025 · N438UA · Airbus A320232 · Escape Slide
  > RIGHT HAND OFF-WING ESCAPE SLIDE, REMOVE {A3NB-25-3-6280} - PERFORMED INSTALLATION OF THE LOCK PIN ASSEMBLY IN THE INFLATION RESERVOIR OF THE RH OFFWING/EMERGENCY-EXIT-DOOR ESCAPE-SLIDE SYSTEMS IAW AMM TASK 25-62-00-481-001-A PERFORMED REMOVAL OF THE LOCK PIN
- [SDR CALA2025021702348](https://openairdocs.org/sdr/CALA2025021702348.md): Lanyard · missing · Feb 14, 2025 · N438UA · Airbus A320232 · Emergency Equipment
  > PURSER REPORTS R WINGEMERGENCY EXITS HAVEONE ESCAPE ROPE WHENIT SHOULD BE TWO. REPLACED MISSING RH OVERWING EMERGENCY EXIT LIFELINE ESCAPE ROPE AS REQUIRED.PARTS USED: 31-2565-3-0002,QTY:1
- [SDR CALA2025013002127](https://openairdocs.org/sdr/CALA2025013002127.md): Battery · no test · Jan 28, 2025 · N438UA · Airbus A320232 · Emergency Lighting
  > OPERATIONAL CHECK OF CABIN EMERGENCY LIGHTS {A3NB-33-3-6012} - FAULT 'EPSU BATTERY EMER R' SHOWING. REPLACED EMERGENCY POWER SUPPLY BATTERY REF. AMM 33-51-00. OPS CHECKS GOOD.
- [SDR CALA2025013002125](https://openairdocs.org/sdr/CALA2025013002125.md): Power Supply · no test · Jan 28, 2025 · N438UA · Airbus A320232 · Emergency Lighting
  > OPERATIONAL CHECK OF CABIN EMERGENCY LIGHTS {A3NB-33-3-6012} - FAULT 'EPSU INT LOAD AFT L' SHOWING. TEST AT LEFT AFT EPSU GETS NO RESPONSE. REPLACED POWER SUPPLY ASSEMBLY REF. AMM 33-51-00. OPS CHECKS GOOD.PARTS USED: 31-3350-9-9001,QTY:1 ROTABLE PARTS CHANG
- [SDR CALA2024041201043](https://openairdocs.org/sdr/CALA2024041201043.md): Lamp · missing · Apr 11, 2024 · N438UA · Airbus A320232 · Exterior Lighting
  > PDA 2 CREW REPORTED LEFT (RETRACTABLE) LANDING LIGHT WAS FOUND MISSING ON LOGPAGE 7620746, REF GMM 02-30-95,
- [SDR CALA2023120103515](https://openairdocs.org/sdr/CALA2023120103515.md): Battery · no test · Nov 29, 2023 · N438UA · Airbus A320232 · Emergency Lighting
  > EPSU BATTERY (13WL) FAILED EMERGENCY LIGHTNING CAPACITY TEST. REPLACEMENT REQUIRED IAW AMM: 33-51-38/401 REV 122. WORK ACCOMP BY LHT EMP 5H0332 & INSP BY LHT EMP 5P0052 AS RECORDED ON LTPR NR#5001274773-0040. PERFORMED EPSU BATTERY REPLACEMENT (13WL) IAW AMM:
- [SDR CALA2023120103513](https://openairdocs.org/sdr/CALA2023120103513.md): Battery · no test · Nov 29, 2023 · N438UA · Airbus A320232 · Emergency Lighting
  > EPSU BATTERY (12WL) FAILED EMERGENCY LIGHTNING CAPACITY TEST. REPLACEMENT REQUIRED IAW AMM: 33-51-38/401 REV 122. WORK ACCOMP BY LHT AS RECORDED ON LTPR NR#5001274773-0030. PERFORMED EPSU BATTERY REPLACEMENT (12WL) IAW AMM: 33-51-38-000- 002 / 33-51-38-400-00
- [SDR CALA2023120103511](https://openairdocs.org/sdr/CALA2023120103511.md): Battery · no test · Nov 29, 2023 · N438UA · Airbus A320232 · Emergency Lighting
  > EPSU BATTERY (11WL) FAILED EMERGENCY LIGHTNING CAPACITY TEST. REPLACEMENT REQUIRED IAW AMM: 33-51-38/401 REV 122. WORK ACCOMP BY LHT EMP 5H0332 & INSP BY LHT EMP 5P0052 AS RECORDED ON LTPR NR#5001274773-0020. PERFORMED EPSU BATTERY REPLACEMENT (11WL) IAW AMM:
- [SDR CALA2023120103509](https://openairdocs.org/sdr/CALA2023120103509.md): Battery · no test · Nov 29, 2023 · N438UA · Airbus A320232 · Emergency Lighting
  > EPSU BATTERY (10WL) FAILED EMERGENCY LIGHTNING CAPACITY TEST. REPLACEMENT REQUIRED IAW AMM: 33-51-38/401 REV 122. WORK ACCOMP BY LHT EMP 5H0332 & INSP BY LHT EMP 5P0052 AS RECORDED ON LTPR NR#5001274773-0010. PERFORMED EPSU BATTERY REPLACEMENT (10WL) IAW AMM:
- [SDR CALA2023061901944](https://openairdocs.org/sdr/CALA2023061901944.md): Manifold · unknown · Jun 16, 2023 · N438UA · Airbus A320232 · Hydraulic System, Main
  > Y SYS LO PR MANIFOLD. FOUND YELLOW SYS PTU MANIFOLD PTU SUPPLY CHECK VALVE NUT/SEAL PARTS ADDED FOUND EXTRUDED O-RING ON MANIFOLD CHECK VALVE. DISCONNECTED PTU REUPLOAD PICTURE LEAKING OR MANIFOLD CRACKED AT THE MATING SURFACE, SEE IMAGE QUICK-DISCONNECT LINE
- [SDR CALA2023052401606](https://openairdocs.org/sdr/CALA2023052401606.md): Battery · no test · May 23, 2023 · N438UA · Airbus A320232 · Emergency Lighting
  > LH EPSU BATTERY FAILD OPS CHECK PER STS N0292 REMOVED AND REPLACED 13WL EPSU BATTERY PER A320 AMM 33-51-38-000 -002-A/33-51-38-400-002-A. PERFORMED OP CHECK PER A320 AMM SUBTA SK 33-51-00-710-050-A. TESK OK. PER STS N0292
- [SDR CALA2023051501502](https://openairdocs.org/sdr/CALA2023051501502.md): Battery · no test · May 13, 2023 · N438UA · Airbus A320232 · Emergency Lighting
  > FWD LEFT EPSU BATTERY FAILED TEST REQUIRES REPLACEMENT UPDATE INFO TO INCLUDE STS NR281 REMOVED AND REPLACED FWD LEFT EPSU BATTERY PER A320 AMM 33-51-38 -000/400-002-A. OPS CHECK GOOD AT THIS TIME
- [SDR CALA2023051201476](https://openairdocs.org/sdr/CALA2023051201476.md): Wire · broken · May 11, 2023 · N438UA · Airbus A320232 · Light System Wiring
  > CEILING CABIN EMERGENCY LIGHT INOP. FIN 205WL REFERENCE STS NR N0248 REPAIRED BROKEN WIRE IAW ESPM 20-48-11 PR EFORMED OPS IAW AMM 33-51-00-710-805 TEST OK STS QC 0047
- [SDR CALA2022081902128](https://openairdocs.org/sdr/CALA2022081902128.md): Fitting · cracked · Aug 17, 2022 · N438UA · Airbus A320232 · Fuselage Main, Frame
  > CRACK INDICATION ON CONTINUITY FITTING RH SIDE. CRACK LENGTH 0.2 00 INCHES APPROX. SEE AEROMAN NON ROUTINE 2022-293704 01 CRACK INDICATION NOT FOUND DIP REPETITIVE INSPECTION REPAIR IS CATEGORY B. REQUIRED AFTER 57,000 TOTAL FLIGHT CICLES BUT BEFORE 58,000 TOT
- [SDR CALA2022081902127](https://openairdocs.org/sdr/CALA2022081902127.md): Fitting · cracked · Aug 17, 2022 · N438UA · Airbus A320232 · Fuselage Main, Frame
  > CRACK INDICATION ON CONTINUITY FITTING LH SIDE. CRACK LENGTH 0.2 00 INCHES APPROX. SEE AEROMAN NON ROUTINE 2022-293703 01 CRACK INDICATION NOT FOUND DIP REPETITIVE INSPECTION REPAIR IS CATEGORY B. REQUIRED AFTER 57,000 TOTAL FLIGHT CICLES BUT BEFORE 58,000 TOT
- [SDR CALA2022081902126](https://openairdocs.org/sdr/CALA2022081902126.md): Frame · cracked · Aug 17, 2022 · N438UA · Airbus A320232 · Fuselage Main, Frame
  > CRACK INDICATION ON WINDSHIELD CENTRAL LOWER NODE FITTING LH SID E CRACK LENGTH 0.080 INCHES APPROX. CICLES FOR EC 5311-02858 PART 2 INSPECTION REQUIREMENTS I.A.W EC/RA #5311-02858 PART 1 STEP 7. THIS REPAIR IS CATEGORY "B". SEE AEROMAN NON ROUTINE 2022-293701
- [SDR CALA2022081902125](https://openairdocs.org/sdr/CALA2022081902125.md): Frame · cracked · Aug 17, 2022 · N438UA · Airbus A320232 · Fuselage Main, Frame
  > CRACK INDICATION ON WINDSHIELD CENTRAL LOWER NODE FITTING RH SID E. CRACK LENGTH 0.100 INCHES APPROX.SEE AEROMAN NON ROUTINE 2022 -293702 CICLES FOR EC 5311-02858 PART 2 INSPECTION REQUIREMENTS I.A.W EC/RA #5311-02858 PART 1 STEP 7. THIS REPAIR IS CATEGORY "B"
- [SDR CALA2022081602077](https://openairdocs.org/sdr/CALA2022081602077.md): Fitting · cracked · Aug 16, 2022 · N438UA · Airbus A320232 · Fuselage Main, Frame
  > CRACK INDICATION ON CONTINUITY FITTING RH SIDE. CRACK LENGTH 0.2 00 INCHES APPROX.THIS PERFORMED PERMANET REPAIR (REPLACED)CONTINUITY FITTING RH SIDE. ROTO TEST INSPECTION OF THE CONTINUITY FITTINGS TO SPLICE FITTINGS 3 FASTENER HOLES.
- [SDR CALA2022081602076](https://openairdocs.org/sdr/CALA2022081602076.md): Fitting · cracked · Aug 16, 2022 · N438UA · Airbus A320232 · Fuselage Main, Frame
  > CRACK INDICATION ON WINDSHIELD CENTRAL LOWER NODE FITTING RH SIDE. CRACK LENGTH 0.100 INCHES APPROX. PERFORMED PERMANENT REPAIR (REPLACED) WINDSHIELD CENTRAL RH SIDE.
- [SDR CALA2022081602075](https://openairdocs.org/sdr/CALA2022081602075.md): Fitting · cracked · Aug 16, 2022 · N438UA · Airbus A320232 · Fuselage Main, Frame
  > CRACK INDICATION ON WINDSHIELD CENTRAL LOWER NODE FITTING LH SIDE CRACK LENGTH 0.080 INCHES APPROX. PERFORMED PERMANENT REPAIR (REPLACED) WINDSHIELD CENTRAL LH SIDE.
- [SDR CALA2022081602074](https://openairdocs.org/sdr/CALA2022081602074.md): Fitting · cracked · Aug 16, 2022 · N438UA · Airbus A320232 · Fuselage Main, Frame
  > CRACK INDICATION ON CONTINUITY FITTING LH SIDE. CRACK LENGTH 0.2 00 INCHES APPROX.PERFORMED PERMANENT REPAIR (REPLACED)CONTINUITY FITTING LH SIDE.
- [SDR CALA2022081202037](https://openairdocs.org/sdr/CALA2022081202037.md): Frame · corroded · Aug 10, 2022 · N438UA · Airbus A320232 · Fuselage, Wing Attach Fittings
  > CORROSION LOWER SILL FR 66 RH SIDE AT AFT GALLEY AREA, SEE AEROMAN NON ROUTINE 2022-293845 PERFORMED PERMANENT REPAIR ON LOWER SILL RH SIDE AT AFT GALLEY L=2.755IN, W=1.984IN, D=0.087IN, EDDY CURRENT DONE ON REWORKED ULTRASONIC THICKSNESS MEASURES ON REWORKED
- [SDR CALA2022071801799](https://openairdocs.org/sdr/CALA2022071801799.md): Floorbeam · corroded · Jul 17, 2022 · N438UA · Airbus A320232 · Fuselage Floor Panel
  > CORROSION FLOORBEAM +Y1162 LOCATED BTW FR 68 AND FR 69 AT AT AFT GALLEY AREA REMOVED AND REPLACED FLOORBEAM +Y1162 LOCATED BTW FR.68 AND ADDITIONAL DAMAGE ON AREA IAW NTM 51-90-00 FR.69 AT AFT GALLEY AREA IAW A320 SRM 51-72-11 AND DWG D53472000 TOOL USED CALIP
- [SDR CALA2022071801798](https://openairdocs.org/sdr/CALA2022071801798.md): Floorbeam · corroded · Jul 17, 2022 · N438UA · Airbus A320232 · Fuselage Floor Panel
  > CORROSION FLOORBEAM +Y160 LOCATED BTW FRAME 68 TO FRAME 70 AT AFT GALLEY AREA REMOVED AND REPLACED FLOORBEAM +Y160 LOCATED BTW FRAME 68 TO INSPECTION AND FOUND ADDTIONAL DAMAGE IAW NTM 51-90-00 FRAME 70 AT AFT GALLEY AREA IAW A320 SRM 51-72-11 AND DWG 53472040
- [SDR CALA2022071801797](https://openairdocs.org/sdr/CALA2022071801797.md): Floorbeam · corroded · Jul 17, 2022 · N438UA · Airbus A320232 · Fuselage Floor Panel
  > CORROSION FLOORBEAM -Y765 LOCATED BTW FR 67 AND FR 70 AT AFT GALLEY AREA REMOVED AND REPLACED FLOOR BEAM -Y765 LOC. BTW FR 67 AND FR S/N 604311, DUE DATE JUL-30-2022. 70 AT AFT GALLEY AREA IAW A320 SRM 51-72-11 AND DWG D53472040 TOOL USED DIGITAL CALIPER: P/N
- [SDR CALA2022071801796](https://openairdocs.org/sdr/CALA2022071801796.md): Floorbeam · corroded · Jul 17, 2022 · N438UA · Airbus A320232 · Fuselage Floor Panel
  > CORROSION FLOORBEAM +Y765 LOCATED BTW FR 67 AND FR 70 AT AFT GALLEY AREA REMOVED AND REPLACED FLOORBEAM +Y765 LOC. BTW FR.67 AND FR.70 ADJACENT AREA AND NO FOUND ADDITIONAL DAMAGE IAW NTM 51-90-00 AT AFT GALLEY AREA IAW A320 SRM 51-72-11 AND DWG D53472040, TOO
- [SDR CALA2022071801795](https://openairdocs.org/sdr/CALA2022071801795.md): Floorbeam · corroded · Jul 17, 2022 · N438UA · Airbus A320232 · Fuselage Floor Panel
  > CORROSION FLOORBEAM +Y512 LOCATED BTW FRAME 64 TO FRAME 70 AT AFT GALLER AREA REMOVED AND REPLACED FLOORBEAM TY512 LOC BTW FR 64 TO FR 70 AREA AND NO FOUND ADDTIONAL DAMAGE IAW NTM 51-90-00 AT AFT GALLEY AREA IAW A320 SRM 51-72-11 AND DWG 53472094000 TOOL USE
- [SDR CALA2022071801794](https://openairdocs.org/sdr/CALA2022071801794.md): Floorbeam · corroded · Jul 17, 2022 · N438UA · Airbus A320232 · Fuselage Main, Floor Beam
  > CORROSION FLOORBEAM -Y765 LOCATED BTW FR 64 AND FR 66 AT AFT GALLEY AREA REMOVED AND REPLACED FLOOR BEAM -Y765 LOC BTW FR64 AND FR66 AT AFT GALLEY AREA IAW A320 SRM 51-42-11 AND DWG D92495124 AND D53472201 AND PERFORMED DETAIL VISUAL INSPECTION ON AREA AND NOT
- [SDR CALA2022071801793](https://openairdocs.org/sdr/CALA2022071801793.md): Floorbeam · elongated · Jul 17, 2022 · N438UA · Airbus A320232 · Fuselage Main, Floor Beam
  > ELONGATED HOLE FLOORBEAM -Y1292 LOCATED BTW FRAME 64 AND FRAME 66 AT AFT GALLEY AREA REMOVED AND REPLACED FLOORBEAM -Y1292 LOCATED BTW FRAM 64 AND FRAME 66 AT AFT GALLEY AREA IAW A320 SRM 51-72-11 AND DWG D53472201 PERFORMED DETAIL VISUAL INSPECTION ON ADJACEN
- [SDR CALA2022071301723](https://openairdocs.org/sdr/CALA2022071301723.md): None · gouged · Jul 13, 2022 · N438UA · Airbus A320232 · Fuselage Structure (General)
  > GOUGE EXTERNAL SKIN LOCATED FRAME25 AND 3 INCHES BTW STR42L TO STR 43L AT LOWER FUSELAGE 60000 FC, 120000 F/H IAW SRI 53-21-11-205-071 TABLE 001 PERFORMED SCEPTRE AND LOGPAGE NUMBER IS N.9030382 INSTALLED DOT IAW GMM 06-35-05 UPDATE LOG PAGE MAJOR REPAIR IS "Y
- [SDR CALA2020062001020](https://openairdocs.org/sdr/CALA2020062001020.md): Power Supply · no test · Jun 19, 2020 · N438UA · Airbus A320232 · Emergency Lighting
  > EMERGENCY EXIT LIGHT TEST FAILED, EPSU AT LT AFT POSITION. TRIED TESTING AT ESPU NO REPONSE. REPLACED ESPU REF AMM 33-51-38-000-001-A & 33-51-38-400-001-A OPS CHECKED OK. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1103732 SN OFF 8072 POWER SUPPLY, C OFF 31
- [SDR CALA2020012300203](https://openairdocs.org/sdr/CALA2020012300203.md): Web · cracked · Jan 18, 2020 · N438UA · Airbus A320232 · Emergency Exits
  > LEFT AFT OVERWING HATCH FWD AND AFT INNER WEB WAS CRACKED AROUND VARIOUS FASTENER BUCKTAILS, REMOVED & REPLACED IAW SRM 51-72-11-911-002.
- [SDR CALA2020012300202](https://openairdocs.org/sdr/CALA2020012300202.md): Door Frame · cracked · Jan 18, 2020 · N438UA · Airbus A320232 · Fuselage Main, Structure
  > LEFT FWD EMERGENCY EXIT HATCH AFT VERTICAL FRAME WAS CRACKED AT FASTENER AREAS, REMOVED & REPLACED IAW SRM 51-72-11-911-002.
- [SDR CALA2020012300201](https://openairdocs.org/sdr/CALA2020012300201.md): Door Frame · cracked · Jan 18, 2020 · N438UA · Airbus A320232 · Fuselage Main, Structure
  > LEFT FWD EMERGENCY EXIT HATCH FWD VERTICAL FRAME WAS CRACKED AT FASTENE R AREAS, REMOVED & REPLACED THE VERTICAL SEGMENT IAW SRM 51-72-11-911-002.
- [SDR CALA2020012300200](https://openairdocs.org/sdr/CALA2020012300200.md): Web · cracked · Jan 18, 2020 · N438UA · Airbus A320232 · Emergency Exits
  > RH FWD OVERWING HATCH FWD AND AFT INNER WEB IS CRACKED AROUND VA RIOUS FASTENER BUCKTAILS. REMOVED & REPLACED IAW SRM 51-72-11-911-002.
- [SDR CALA2020012300199](https://openairdocs.org/sdr/CALA2020012300199.md): Door Frame · cracked · Jan 18, 2020 · N438UA · Airbus A320232 · Fuselage Main, Structure
  > RIGHT AFT EMERGENCY EXIT DOOR FWD WEB & AFT FRAME CRACKED, REMOVED & REPLACED IAW SRM 51-72-11-910-002.
- [SDR CALA2020012000196](https://openairdocs.org/sdr/CALA2020012000196.md): Angle · corroded · Jan 17, 2020 · N438UA · Airbus A320232 · Emergency Exits
  > RT AFT EMERG EXIT DOOR INNER SURFACE LOWER FWD ANGLE HAS CORROSION - {A3NB-05-3-6159} - GENERATED BY TECH ON N/R 9298395 AT RMVD AND RPLCD ANGLE & RIB ON RT AFT EMERGENCY EXIT DOOR IAW SRM 51-72-11-811-002-2A. PERFORMED BY MECH, INSP.
- [SDR CALA2020012000195](https://openairdocs.org/sdr/CALA2020012000195.md): Plate · corroded · Jan 17, 2020 · N438UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT PIT TORSION BOX COVER SHEET HAS CORROSION UNDER TIE DOWN FIT TINGS - A3NB-25-3-6241 - GENERATED. RMVD & RPLCD AFT CARGO PIT TORSION BOX COVER SHEET IAW SRM 51-72-11-911-002 & SRM 51-42-11-801. PERFORMED BY MECH, INSP.
- [SDR CALA2019112542048](https://openairdocs.org/sdr/CALA2019112542048.md): Controller · faulted · Nov 20, 2019 · N438UA · Airbus A320232 · Cabin Pressure Controller
  > SYS 2 FAULT DISPLAYED ON UPPER ECAM SCREEN. CAB PR ECAM OCCURRED AFTER TO ROTATION. T/S REF TSM 21-31-00-810-806A AND FOUND #2 CPC AT FAULT (12HL). R&R REF AMM 21-31-34-400-001-A. ALL OPS CHECKS GOOD. IPC REF 21-31-08-02A ITEM 130 EFF IS CORRECT. NOTE STEP 4.A
- [SDR CALA201906301078](https://openairdocs.org/sdr/CALA201906301078.md): Hydraulic System · low pressure · Jun 26, 2019 · N438UA · Airbus A320232 · Hydraulic System, Main
  > HYD B SYS LOW PR ECAM, TRIPPED CB, PUMP MAY HAVE OVR-HEAT. ON ARRIVAL, B ELECTRIC 50 AMP HYD PUMP CB GRID AB ON 123VU POPPED. AT THE GATE PUSHED CB IN AND OPERATED THE PUMP AND ALL FLIGHT CONTROLS FOR 60 MINUTES. ALL INDICATION OK. PUMP ITSELF WAS NOT OVERHEAT

Next page: https://openairdocs.org/aircraft/N438UA/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 = 'N438UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N438UA/reports

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