# Service difficulty reports: N476UA

A list on [N476UA](https://openairdocs.org/aircraft/N476UA.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 · 113 reports

- [SDR CALA2026072017862](https://openairdocs.org/sdr/CALA2026072017862.md): Lever · missing · Jul 17, 2026 · N476UA · Airbus A320232 · Cargo/Baggage Doors
  > UPON ARRIVAL TO GATE IN ORD, AFT CARGO DOOR SELECTOR HANDLE MISSING. INSTALLED NEW SELECTOR LEVEL IN REF TO AMM 52-36-15.
- [SDR CALA2026071617826](https://openairdocs.org/sdr/CALA2026071617826.md): Hinge · broken · Jul 16, 2026 · N476UA · Airbus A320232 · Fuselage, Door Hinge
  > AFT CARGO DOOR SELECTOR VALVE DOOR MISSING UPON ARRIVAL. CARGO ACCESS PANEL FOUND OPEN ON ARRIVAL. HINGE BROKEN. FOUND DOOR MISSING CDL APPLIED REF 52UN FOR AFT CARGO DOOR SELECTOR VALVE.
- [SDR CALA2026032614840](https://openairdocs.org/sdr/CALA2026032614840.md): Door · out of rig · Mar 25, 2026 · N476UA · Airbus A320232 · Service Doors
  > F/A FOUND THAT DOOR 2L ARM/DISARM HANDLE MOVED OUT 1 INCH DURING FLIGHT.NO ECAM MESSAGE. ITEM LOCKED TO CONFIRM FINDINGS EMERGENCY ESCAPE SLIDE REF AMM 52-10-00-720-005-A. AT 2 LEFT AT APPROX 6 LBF RELEASE MECHANISM HANDLE BEGINS TO MOVE. UNLOCKED FOR UPDATING
- [SDR CALA2026020113456](https://openairdocs.org/sdr/CALA2026020113456.md): A/C Pack · overtemp · Jan 30, 2026 · N476UA · Airbus A320232 · Cabin Cooling System
  > CREW NOTED ODOR IN CABIN BEFORE PACK OVERHEAT. REQUIRES TSM 05-50-00-810-831-A CONFIRMATION CREW STATED ODOR NOT PRESENT AFTER PACK SHUT OFF. REF L/P 7768776 FOR PACK 1 OK TO CONTINUE.
- [SDR CALA2026012613284](https://openairdocs.org/sdr/CALA2026012613284.md): Gauge · out of position · Jan 26, 2026 · N476UA · Airbus A320232 · Emergency Equipment
  > DOOR 2R SLIDE GAUGE IS NOT ABLE TO BE SEEN TO VERIFY STATUS VERIFIED STATUS DOOR 2R SLIDE GAUGE IS IN GREEN AS REQUIRED.
- [SDR CALA2025121612167](https://openairdocs.org/sdr/CALA2025121612167.md): Acm · faulted · Dec 15, 2025 · N476UA · Airbus A320232 · Cabin Cooling System
  > BURNING ELECTRICAL ODOR OBSERVED AFTER T/O APPRO X. 15K FEET. L ASTED ABOU T A MIN. CREW STATES BURNING SMELL ONLY IN THE COCKPIT DURING TO, LASTED APROX 90 SECS AND WENT AWAY. ODOR REPORTING SHEET LEFT IN COCKPIT. TROUBLESHOOTING SYSTEM REVEALED ACM FAILURE O
- [SDR CALA2025121212064](https://openairdocs.org/sdr/CALA2025121212064.md): Fuel Cap · missing · Dec 10, 2025 · N476UA · Airbus A320232 · Fuel Storage
  > FUELER REPORT FUELING CAP MISSING.
- [SDR CALA2025120811826](https://openairdocs.org/sdr/CALA2025120811826.md): Bottle · no discrepancy · Dec 4, 2025 · N476UA · Airbus A320232 · Standard Practices/Structures
  > F/A REPORTED RT DOOR PRESSURE IN RED. PRESSURE NEEDLE IS STILL WITHIN GREEN BAND AT THIS TIME. BUSTLE VIEWPORT IS NOT CENTERED ON GUAGE AND DIFFICULT TO SEE WITHOUT SUFFICIENT LUMINATION. NO MAINT ACTION TAKEN.
- [SDR CALA2025090908664](https://openairdocs.org/sdr/CALA2025090908664.md): Pin · installed · Sep 6, 2025 · N476UA · Airbus A320232 · Standard Practices/Structures
  > INSTALLED L2 DOOR SLIDE ARM HANDLE PIN & DOOR DAMPNER PIN. REMOVED L2 DOOR SLIDE ARM HANDLE SAFETY PIN AND DOOR DAMPNER PIN, SAFETIED DOOR DAMPNER KNOB. REF. AMM 25-62-44-400-006-A. VERIFIED L2 DOOR SLIDE ARM HANDLE SAFETY PIN AND DOOR DAMPNER PIN REMOVAL, SA
- [SDR CALA2025090908663](https://openairdocs.org/sdr/CALA2025090908663.md): Slide · no discrepancy · Sep 5, 2025 · N476UA · Airbus A320232 · Standard Practices/Structures
  > DOOR 2L SLIDE PACK ASSEMBLY REMOVED TO FOM IAW AMM 25-62-44-000-002-A. REINSTALLED L2 DOOR SLIDE PACK ASSEMBLY AFTER DOOR MAINTENANCE REF. AMM 25-62-44-400-006-A. C/W GMM 09-25-05 RII FOR REINSTALLATION OF L2 DOOR MOUNTED ESCAPE SLIDE PACK ASSY REF AMM 25-6
- [SDR CALA2025090908661](https://openairdocs.org/sdr/CALA2025090908661.md): Handle · unknown · Sep 5, 2025 · N476UA · Airbus A320232 · Passenger/Crew Doors
  > DUE TO REPORTS OF DOOR 2L SLIDE ARM HANDLE NOT REMAINING ARMED IN FLIGHT. ADJUSTMENT/TEST OF THE RELEASE MECHANISM OF THE EMERGENCY ESCAPE SLIDE FOUND SOLID CONTACT BETWEEN THE STOP AND THE EMERGENCY CONTROL HANDLE IN THE ARMED POSITION, NO ASJUSTMENT REQUIRE
- [SDR CALA2025090808597](https://openairdocs.org/sdr/CALA2025090808597.md): Proximity Switch · out of adjust · Sep 5, 2025 · N476UA · Airbus A320232 · Door Warning System
  > DOOR 2L WILL NOT ARM SHOWS CABIN PRESS LIGHT ARMED ON GROUND, FAILED IN FLIGHT FOUND PRESSURE LIGHT INTERMITTENT WHILE ARMED. WIGGLING HANDLE CAUSES LIGHT TO FLICKER.ADJUSTED EMERGENCY SLIDE ARM PROXIMITY SWITCH 7WN1 TARGET REF MM 52-71-00-820-002-A. TESTED SW
- [SDR CALA2025081907929](https://openairdocs.org/sdr/CALA2025081907929.md): Skin · dented · Aug 17, 2025 · N476UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > SHARP DENT ON LOWER CENTER OF EMPANNAGE APPROXIMATELY 10 INCHES FWD OF THE APU AIR INLET STRUCTURE. PERFORMED SKIN REPAIR IAW A320 SRM 53-51-11-300-082 REPAIR REQUI RES REINSPECT AT 60,000 FC / 120,000 FH FROM TIME OF ADL/REPAIR EMBODIMENT SUBSEQUENT INSPECT
- [SDR CALA2025062305782](https://openairdocs.org/sdr/CALA2025062305782.md): O-Ring · leaking · Jun 23, 2025 · N476UA · Airbus A320232 · Hydraulic System, Main
  > G HYD RSVR LO LV ECAM - TOMC KROWN UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. ISOLATE LEAK SOURCE. ISOLATE LEAK SOURCE. FOUND UNION O-RING DAMAGED ON THE PTU-MANIFOLD GREEN, (1113GM). REPLACED "O" RING, LEAK
- [SDR CALA2025052905054](https://openairdocs.org/sdr/CALA2025052905054.md): Girt Bar · fod · May 26, 2025 · N476UA · Airbus A320232 · Emergency Equipment
  > UNABLE TO ARM DOOR 2R DOOR 2R UNABLE TO ARM DUE TO GIRT BAR CONTACTING UPPER PART OF GIRT BAR FLOOR FITTINGS WHEN ARMING SLIDE. FOUND DIRT CAUSING BINDING AND NOT ALLOWING GIRT BAR TO GO DOWN FULLY INTO GIRT BAR FLOOR FITTINGS. CLEANED DIRT FROM DOOR 2R GIRT B
- [SDR CALA2024123101728](https://openairdocs.org/sdr/CALA2024123101728.md): Switch · out of position · Dec 29, 2024 · N476UA · Airbus A320232 · Emergency Lighting
  > CABIN EMERGENCY LIGHTS STUCK ON. FOUND AAP EMER LIGHT SWITCH PRESSED. DESELECTED AND EMERGENCY LIGHTS TURNED OFF. OK FOR SERVICE PER AMM 33-51-00.
- [SDR CALA2022091202341](https://openairdocs.org/sdr/CALA2022091202341.md): Slat Track · none · Sep 12, 2022 · N476UA · Airbus A300* · Leading Edge Devices
  > RH WING L/E #2 SLAT, SLAT TRACK #6 I/B METAL EDGE BROKEN. REPAIRED SLAT RIB IAW EC/RA 5741-01458. SLAT LOCATION #6.
- [SDR CALA2022091202336](https://openairdocs.org/sdr/CALA2022091202336.md): None · none · Sep 10, 2022 · N476UA · Airbus A300* · Fuselage, Wing Attach Fittings
  > REF INSP EA 5340-01724 REV C, REJECTABLE HOLE INDICATTIONS FOR ALL HOLES FOR DOOR STOP #1-7 ON RH FR 66 AND FR68. DOOR STOP HOLES PER PART 2 OF THE LATEST REVISION OF ECRA 5341-01327. ACCOMPLISHED INTERIM REPAIR PER PART 1 OF ECRA 5341-01327. / ON OR BEFORE
- [SDR CALA2022091202334](https://openairdocs.org/sdr/CALA2022091202334.md): None · none · Sep 10, 2022 · N476UA · Airbus A300* · Fuselage, Wing Attach Fittings
  > REF INSP EA 5340-01724 REV C, REJECTABLE HOLE INDICATTIONS FOR ALL HOLES FOR DOOR STOP #1-7 ON LH FR 66 AND FR68. STOP HOLES PER PART 2 OF THE LATEST REVISION OF ECRA 5341-01327. ACCOMPLISHED INTERIM REPAIR PER PART 1 OF ECRA 5341-01327. ON OR BEFORE MARCH 5,
- [SDR CALA2022090702305](https://openairdocs.org/sdr/CALA2022090702305.md): None · cracked · Sep 6, 2022 · N476UA · Airbus A300* · Fuselage Main, Plate/Skin
  > A3NB-27-3-6001 LH LATERAL AVIONICS BAY AREA FR 16 WASTE TUBE SUP PORT BRACKET NEAR STR 32L IS CRACKED ON AFT SIDE OF FRAME. REMOVED, FRABRICATED AND REPLACED MOUNT IAW SRM 51-42-11, D53916 787. EMP# V935774 WORK ACCOMPLISHED AT ST ENGINEERING AEROSPACE OF MOBI
- [SDR CALA2022090502269](https://openairdocs.org/sdr/CALA2022090502269.md): Skin · cracked · Sep 3, 2022 · N476UA · Airbus A300* · Fuselage Structure (General)
  > FR35, STR. 30LH HOLE DAMAGE AND HOLE #2 CRACK INDICATIONS DURING NDT INSPECTION. INSPECTION REQUIREMENTS PER PART 2B OF THE LATEST REVISION OF EC FLIGHT CYCLES OR 121735 TOTAL FLIGHT HOURS (WHICHEVER COMES FIRS 9600 FLIGHT CYCLES OR 19200 FLIGHT HOURS (WHICHEV
- [SDR CALA2022090502268](https://openairdocs.org/sdr/CALA2022090502268.md): None · cracked · Sep 3, 2022 · N476UA · Airbus A300* · Fuselage Structure (General)
  > L/H SIDE PRESSURE PANEL BETWEEN FR 35-36 HOLES 13, 16, 22, 23, A ND 24 HAVE CRACK INDICATIONS. OF EC/RA 5331-02956. ON OR BEFORE FEBRUARY 28, 2023 PERFORM AN INSPECTIONOF THE LH FR 36 PRESSURE PANEL HOLES AREA PER PART 2 OF THE LATEST REVISION DIP 53-DIP NO IN
- [SDR CALA2022090502257](https://openairdocs.org/sdr/CALA2022090502257.md): Panel · damaged · Sep 2, 2022 · N476UA · Airbus A300* · Fuselage Structure (General)
  > RH FR 35-36 I/B PRESSURE PANEL HOLE HAS REJECTABLE DAMAGE INDICATION AT 6 O-CLOCK FACING UPWARD. REVISION OF EC/RA 5331-02954. ON OR BEFORE FEBRUARY 28, 2023 PERFORM AN INSPECTION OF THE FR 36 RH PRESSURE PANEL HOLE #9 AREA PER PART 2 OF THE LATEST DIP 53-DIP
- [SDR CALA2022090202252](https://openairdocs.org/sdr/CALA2022090202252.md): Skin · none · Sep 2, 2022 · N476UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > A3NB-51-4-6001 DURING LOCATED FR59-60 STR 37R SRM 53-00-11 FIG 2 04 USED NOT LOCATED IN CURRENT SRM. DOES NOT COMPLY WITH 14 CFR 121.1109 PER AMM 51-00-80-200-801C1 FLOW CHART 3() REMOVED AND REPLACED DOUBLER IAW ECRA 5341-01331. EMP# V935774 W ORK ACCOMPLISHE
- [SDR CALA2022082902196](https://openairdocs.org/sdr/CALA2022082902196.md): Slat Track · broken · Aug 26, 2022 · N476UA · Airbus A300* · Leading Edge Devices
  > RH WING L/E #2 SLAT, SLAT TRACK #6 I/B METAL EDGE BROKEN
- [SDR CALA2022082402168](https://openairdocs.org/sdr/CALA2022082402168.md): Stringer · corroded · Aug 22, 2022 · N476UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > (SUPPORT TASK) AFT CARGO FR56 TO FR58 STRINGER 37R CORRODED.(REP LACE P/N: D5347552623000) REMOVED AND REPLACED STRINGER IAW SRM 51-42-11, DWG D53475580. E MP# V935774 WORK ACCOMPLISHED AT ST ENGINEERING AEROSPACE OF MOB ILE AT BFM ON NR# 34925.
- [SDR CALA2022081602099](https://openairdocs.org/sdr/CALA2022081602099.md): Stringer · corroded · Aug 14, 2022 · N476UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > (A3NB-05-3-6029) AFT CARGO, FRAME 61-62, STR 37R HAS CORROSION.() STRINGER OUT OF LIMITS IAW SRM 53-41-13, REPLACED WITH NEW STRIN GER P/N: D5347048700000, IAW SRM 51-72-11-911-001. INSTALLED IAW SRM 51-42-11. EMP# V936191 WORK ACCOMPLISHED AT ST ENGINEERING
- [SDR CALA2022081602069](https://openairdocs.org/sdr/CALA2022081602069.md): Doubler · unserviceable · Aug 12, 2022 · N476UA · Airbus A320232 · Fuselage Main, Attach Fittings
  > DURING HMV VISIT REMOVED AND REPLACED DOUBLER REPAIR AT FR52-53 STR 24-26L CAT B MAJOR REPAIR IAW SRM 53-41-11-300-019. LOG CREATED FOR SRI DIP PURPOSE. METHOD OF ULTRASOUND/HFEC SEE SRI FIG. 001 FOR SPECIFIC NTM CHAPTERS. INSPECTIONS DUE AFTER REPAIR EMBODIME
- [SDR CALA2022081602063](https://openairdocs.org/sdr/CALA2022081602063.md): Stringer · corroded · Aug 12, 2022 · N476UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > A3NB-53-4-6175 AFT CARGO COMP STR 41R HAS CORROSION BET FR58-64.REMOVED AND REPLACED STRINGER IAW SRM 51-42-11, DWG D53470332. E MO# V935774 WORK ACCOMPLISHED AT ST ENGINEERING AEROSPACE OF MOB ILE AT BFM ON NR# 34948.
- [SDR CALA2022081602067](https://openairdocs.org/sdr/CALA2022081602067.md): Frame · corroded · Aug 12, 2022 · N476UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HMV VISIT AFT CARGO COMPT. PREVIOUS REPAIR HAS CORROSION BETWEEN FR 63-64 & STR. 41L-42L, NEW REPAIR ACCOMPLISHED PER SRM 53-00-11-300-029. LOG CREATED FOR DIP TO BE ACCOMPLISHED PER SRI 53-00-11-205-017. SUBSEQUENT INSPECTIONS AT INTERVALS OF 2200FC/44
- [SDR CALA2022081602066](https://openairdocs.org/sdr/CALA2022081602066.md): Frame · corroded · Aug 12, 2022 · N476UA · Airbus A320232 · Fuselage Main, Frame
  > AFT CARGO, FRAME 60-62, STR40R HAS CORROSION 20 SRM 51-72-11-911 TREATED AND PRIMED IAW A320 SRM 51-21-11/001 ACCOMPLISHED AT ST ENGINEERING AEROSPACE OF MOBILE AT BFM ON NR@ APPLIED TOP COAT IAW A320 SRM 51-23-11/001. EMP# V935833 WORK # 34536. REPAIRED STRIN
- [SDR CALA2022081602065](https://openairdocs.org/sdr/CALA2022081602065.md): Stringer · corroded · Aug 12, 2022 · N476UA · Airbus A320232 · Fuselage Main, Attach Fittings
  > DURING HMV VISIT AFT BULK CGO. STR FOUND CORRODED @ FR 60-62 STR. 40R. STRINGER REPAIR WAS ACCOMPLISHED PER SRM 53-00-13-300-001 FIG. 001. LOG CREATED FOR INSPECTION TRESHOLD DIP. INTERVALS: TBD, METHOD: TBD, IAW SRI 53-00-13-205-001 TABLE 004. INSPECTION TRE
- [SDR CALA2022081202054](https://openairdocs.org/sdr/CALA2022081202054.md): Stringer · corroded · Aug 12, 2022 · N476UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > A3NB-53-4-6175 AFT CARGO COMP STR 41R HAS CORROSION BET FR58-64. () REMOVED AND REPLACED STRINGER IAW SRM 51-42-11, DWG D53470332. E MO# V935774 WORK ACCOMPLISHED AT ST ENGINEERING AEROSPACE OF MOB ILE AT BFM ON NR# 34948.
- [SDR CALA2022081202053](https://openairdocs.org/sdr/CALA2022081202053.md): Stringer · corroded · Aug 12, 2022 · N476UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > (SUPPORT TASK) AFT CARGO FR56 TO FR58 STRINGER 37R CORRODED.(REP LACE P/N: D5347552623000) REMOVED AND REPLACED STRINGER IAW SRM 51-42-11, DWG D53475580. E MP# V935774 WORK ACCOMPLISHED AT ST ENGINEERING AEROSPACE OF MOB ILE AT BFM ON NR# 34925.
- [SDR CALA2022081202040](https://openairdocs.org/sdr/CALA2022081202040.md): Skin · none · Aug 11, 2022 · N476UA · Airbus A320232 · Fuselage Main, Frame
  > DURING HMV VISIT FUSELAGE DOUBLER REPAIR ACCOMPLISHED AT FR23 STR10-11L IAW SRM 53-11-11-300-041 CAT B MAJOR REPAIR WITH RE-INSPECTIONS PER SRI ZONE 1 TABLE 001. "NOT APPLICABLE" SEE NOTE 2. RE-INSPECTION METHOD "NOT CASE OF A/CLIFE EXXTENSION MORE THAN 60000F
- [SDR CALA2022081202039](https://openairdocs.org/sdr/CALA2022081202039.md): Skin · none · Aug 11, 2022 · N476UA · Airbus A320232 · Fuselage Main, Structure
  > DURING HMV VISIT A DOUBLER REPAIR WAS ACCOMPLISHED AT FR6-7 LHS NEAR TAT SENSOR IAW SRM 53-11-11-300-052 CAT B MAJOR REPAIR REQUIRES DIP FOR REPETITIVE INSPECTIONS IAW SRI 53-11-11-205-051 ZONE A. REF. SRI 53-11-11-205-051 TABLE 001 ZONE A. FLOW CHART 3. INSP
- [SDR CALA2022081002021](https://openairdocs.org/sdr/CALA2022081002021.md): Doubler · inadequate · Aug 9, 2022 · N476UA · Airbus A320232 · Fuselage Floor Panel
  > DURING HMV VISIT FOUND DOUBLER LOCATED AT FR28-29 STR 38L-39L THAT DOES NOT COMPLY WITH CURRENT SRM. ACCOMPLISHED REPAIR PER SRM 53-21-11-300-090 AND 51-42-11. LOG CREATED FOR DIP REPETITIVE INSPECTION REQUIREMENTS. INSPECTION IAW SRI 53-21-11-205-071 ZONE A.
- [SDR CALA2022081002012](https://openairdocs.org/sdr/CALA2022081002012.md): Stringer · corroded · Aug 8, 2022 · N476UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > (A3NB-51-4-6001) AFTER REMOVAL OF DOUBLER FR59 ST36R-38R FOUND S TR38R FR58-62 AND COUPLING FR58 HAS SIGNS OF CORRSION. REMOVED AND REPLACED STRINGER 38R FR58 TO FR64 IAW SRM 51-42-11, DWG D53470339. EMP# V935774 WORK ACCOMPLISHED AT ST ENGINEERING AEROSPACE O
- [SDR CALA2022080801991](https://openairdocs.org/sdr/CALA2022080801991.md): Shear Tie · corroded · Aug 7, 2022 · N476UA · Airbus A300* · Fuselage Miscellaneous Structure
  > AFT CARGO COMPFR 61 SHEAR TIE HAS CORROSION BET STR38R-39R REMOVED AND REPLACED SHEAR TIE IAW A320 SRM 51-42-11/001 AND FAB OF MOBILE AT BFM ON NR# 34950. RICATED ON TRAVELER T22/1626896, FABRICATED ANGLE IAW TRAVELER T 22/1626897 AND T22/1626895 AND INSTALLED
- [SDR CALA2022080801990](https://openairdocs.org/sdr/CALA2022080801990.md): None · corroded · Aug 7, 2022 · N476UA · Airbus A300* · Fuselage Main, Structure
  > A3NB-53-4-6175 AFT CARGO COMP STR39R HAS CORROSION FR58-FR59() AFT CARGO COMPARTMENT BETWEEN FR50 TO FR59, STR39R REPAIRED IAW A320 SRM 53-00-13-300-001 AND SRM 51-42-11. EMP# V934585 WORK AC COMPLISHED AT ST ENGINEERING AEROSPACE OF MOBILE AT BFM ON NR# 3 494
- [SDR CALA2022080501959](https://openairdocs.org/sdr/CALA2022080501959.md): Doubler · misrepaired · Aug 3, 2022 · N476UA · Airbus A320232 · Fuselage, Wing Attach Fittings
  > A3NB-51-4-6001 TOILET VENT DOUBLER LOCATED FR69-70 STR 30-33R DOES NOT COMPLY WITH CFR 121.1109 PER AMM 51-00-80-200-801C1 FLOW CHART 1 STEP 3 NO REPAIR DATA FOUND.() REMOVED AND REPLACED TOILET VENT DOUBLER IAW SRM 53-41-11-300-00 4 CAT A MAJOR REPAIR. EMP# V
- [SDR CALA2022080301955](https://openairdocs.org/sdr/CALA2022080301955.md): Stringer · corroded · Aug 2, 2022 · N476UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > A3NB-53-4-6175 AFT CARGO COMP STR 43L BET FR63-64 HAS CORROSION. () REMOVED, FABRICATED AND PLACED STRINGERS IAW SRM 51-42-11, DWG D 53470418, D5347034. EMP# V935774 WORK ACCOMPLISHED AT ST ENGINEE RING AEROSPACE OF MOBILE AT BFM ON NR# 34951.
- [SDR CALA2022080301953](https://openairdocs.org/sdr/CALA2022080301953.md): Stringer · corroded · Aug 2, 2022 · N476UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > A3NB-53-4-6175 AFT CARGO COMP STR 42L BET FR63-FR64 HAS CORROSIO N() AFT CARGO STR 42L BET FR60-FR64 WAS REMOVED AND MANFACTURED NEW STR IAW AIRBUS DRAWING 17D53470418 AND INSTALLED IAW SRM 51-42-1 1, D53473045. EMP# V936191 WORK ACCOMPLISHED AT ST ENGINEERING
- [SDR CALA2022080301952](https://openairdocs.org/sdr/CALA2022080301952.md): Doubler · discovered · Aug 2, 2022 · N476UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > A3NB-51-4-6001 DOUBLER LOCATED FR69-70 STR 18L-19L DOES NOT COMP LY WITH 14 CFR 121.1109 PER AMM 51-00-80-200-801C1 FLOW CHART 1 STEP 3 NO REPAIR DATA FOUND.() REMOVED AND REPLACED DOUBLER OF FR69-70 STGR 18-19L IAW SRM 53-4 1-11-300-036 CAT A MAJOR REPAIR. EM
- [SDR CALA2022072901920](https://openairdocs.org/sdr/CALA2022072901920.md): Doubler · discovered · Jul 28, 2022 · N476UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > A3NB-51-46001 DOUBLER LOCATED FR 78-80 STR 19L-20L SRM 53-51-11 FIG./DIA 104 USED NOT LOCATED IN CURRENT SRM. DOES NOT COMPLY WI TH 14 CFR 121.1109 PER AMM 51-00-200-801C1 FLOW CHART 3() REMOVED AND REPLACED DOUBLER AT FR 78-80 STRG 15-16L IAW SRM 53- 51-11-30
- [SDR CALA2022072901919](https://openairdocs.org/sdr/CALA2022072901919.md): Doubler · discovered · Jul 28, 2022 · N476UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > A3NB-51-46001 DOUBLER LOCATED FR 78-80 STR 19L-20L SRM 53-51-11 FIG./DIA 104 USED NOT LOCATED IN CURRENT SRM. DOES NOT COMPLY WI TH 14 CFR 121.1109 PER AMM 51-00-200-801C1 FLOW CHART 3() REMOVED AND REPLACED DOUBLER AT FR 78-80 STRG 15-16L IAW SRM 53- 51-11-30
- [SDR CALA2022072901918](https://openairdocs.org/sdr/CALA2022072901918.md): Angle · cracked · Jul 28, 2022 · N476UA · Airbus A320232 · Emergency Exits
  > RH FORWARD EMERG EXIT DOOR FORWARD FRAME WEB CRACKED DOT 38-51
- [SDR CALA2022072501869](https://openairdocs.org/sdr/CALA2022072501869.md): None · corroded · Jul 24, 2022 · N476UA · Airbus A320232 · Standard Practices/Structures
  > AFT CARGO, FRAME 56, CARGO FLOOR SUPPORT HAS CORROSION DOT 31-01 6 AT DOOR THRESHOLD PLATE
- [SDR CALA2022072501865](https://openairdocs.org/sdr/CALA2022072501865.md): Seat Track · corroded · Jul 23, 2022 · N476UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > (A3NB-53-3-6038) RH CABIN: FLOOR SEAT TRACK INBOARD FR20 HAS CORROSION. DOT 61-012() EVALUATES SEAT TRACK Y-765 FOUND OUT OF LIMITS IAW SRM 53-11-15- 001, REMOVED AND REPLACED IAW SRM 57-42-11 AND SRM 51-72-11-911- 001. EMP# V933818 WORK ACCOMPLISHED AT ST ENG
- [SDR CALA2022072501863](https://openairdocs.org/sdr/CALA2022072501863.md): Seat Track · corroded · Jul 22, 2022 · N476UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > (A3NB-53-3-6038) RH FWD CABIN: FLOOR SEAT TRACK OUTBOARD FR20 HAS CORROSION. DOT 61-013() EVALUATED SEAT TRACK Y-1292 FOUND OUT OF LIMITS IAW SRM 53-11-15 -283-010, REMOVED AND REPLACED IAW SRM 51-72-11-911-001. EMP# V9 36041 WORK ACCOMPLISHED AT ST ENGINEERIN

Next page: https://openairdocs.org/aircraft/N476UA/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 = 'N476UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N476UA/reports

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