# Service difficulty reports: N482UA

A list on [N482UA](https://openairdocs.org/aircraft/N482UA.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 · 137 reports

- [SDR CALA2026060316799](https://openairdocs.org/sdr/CALA2026060316799.md): Coffeemaker · leaking · May 19, 2026 · N482UA · Airbus A320232 · Buffet/Galleys
  > GALLEY COFFEEMAKER LEAKS. COFFEEMAKER BAG BROKE OPEN SO NOW HS GROUNDS IN IT AND SMELLS FUNNY WHEN HEATING UP FWD GALLEY COFFEEMAKER INOP LEAKS IN USE CLEANED EXCESS GROUNDS AND AREA. PLACE ON NEF 2522AK BREAKER COLLARED AND PLACARD IN PLACE. APPROVED FOR NE
- [SDR CALA2025101510102](https://openairdocs.org/sdr/CALA2025101510102.md): None · no discrepancy · Oct 13, 2025 · N482UA · Airbus A320232 · Standard Practices/Structures
  > ON ROLL OUT, WENT THROUGH FLOW CHECK OF BIRDS ON RT SIDE, PERFORMED DVI PHASE 1 INSPECTION OF AIRCRAFT IAW MM 05-51-14. INSPECTED RADOME AND WX RADAR WITH NO SIGNS OF DELAMINATION, OR DAMAGE. VERFIED WITH FLIGHT CREW WRITE UP WAS PRECAUTIONARY. FLIGHT CREW O
- [SDR CALA2025092909360](https://openairdocs.org/sdr/CALA2025092909360.md): Girt Bar · obstructed · Sep 26, 2025 · N482UA · Airbus A320232 · Entrance Stairs
  > DOOR 2L SLIDE WILL NOT ARM. CHECK GIRT BAR FOR OBSTRUCTION. REMOVED OBSTRUCTION FROM GIRT BAR FITTING. NO DEFECTS NOTED IAW AMM 52-13-00.
- [SDR CALA2025081807898](https://openairdocs.org/sdr/CALA2025081807898.md): Limiter · faulted · Aug 15, 2025 · N482UA · Airbus A320232 · Rudder Control System
  > ACFT HAS REPEAT HIT OF AUTO FLT RUD TRV LIM SYS. BEFORE FURTHER FLIGHT, REPLACE RUDDER TRAVEL-LIMIT UNIT FIN 4CC REF AMM 27-23-51. CARRIED BY ELB R&R THE RUDDER TRAVEL-LIMITATION UNIT REF AMM: 27-23-51. C/W THE RUDDER TRAVEL-LIMITATION UNIT OPS CHECK REF AMM
- [SDR CALA2025080107195](https://openairdocs.org/sdr/CALA2025080107195.md): Bottle · no discrepancy · Jul 30, 2025 · N482UA · Airbus A320232 · Emergency Equipment
  > L2 DOOR NOT SHOWING GREEN, INSPECTED SLIDE PRESSURE GAUGE. INDICATION SHOWS TO BE AT THE HIGHER END OF PRESSURE BUT REMAINS IN THE GREEN BAND. SLIDE IS CLEAR FOR CONTINUED SERVICE
- [SDR CALA2025061905696](https://openairdocs.org/sdr/CALA2025061905696.md): Compressor · stalled · Jun 15, 2025 · N482UA · Airbus A320232 · Turbine Engine Compressor Section
  > CRUISE ENG 2 COMPRESSOR VANE CAUT LED TO ENG2 STALL AND ENG2 FAI L EGT 757 OBTAINED EIS REPORT DMC1 EGT MAX REACHED OF 766.3. DUE TO #2 ENGINE BEING CHANGED, DISCREPANCY TRANSFERRED TO AC 8802 REF LP5246942
- [SDR CALA2025053005115](https://openairdocs.org/sdr/CALA2025053005115.md): Chiller · faulted · May 25, 2025 · N482UA · Airbus A320232 · Buffet/Galleys
  > ELECTRICAL SMELL IN AFT GALLEY. DISCUSSED AFT GALLEY BURNING SMELL WITH FIGHT ATTENDANT IN AFT GALLEY. UPON ARRIVAL OF MX TO AIRCRAFT SMELL WAS NO LONGER PRESENT. ATTEMPTED TO RECREATE SMELL NO SMELL NOTED. FLIGHT ATTENDANT NOTED THAT SMELL APPEARED AFTER CHIL
- [SDR CALA2025050504434](https://openairdocs.org/sdr/CALA2025050504434.md): Proximity Sensor · out of adjust · Apr 30, 2025 · N482UA · Airbus A320232 · Door Warning System
  > [LEVEL 0 CHRONIC]-FWD CARGO DOOR IND-DUE TO HISTORY, PLEASE CHECK THE 28WV AND 30WV PROX SW INDUCTANCE READINGS PER AMM 32-31-73- 820-008-A AND ADJUST PER AMM 52-71-00-820-003-A AND 52-71-00-820 -004-A AS NEEDED TO GET THE TARGET NEAR INDUCTANCE TO 5.8 MH. P
- [SDR CALA2025050104394](https://openairdocs.org/sdr/CALA2025050104394.md): Warning Light · intermittent · Apr 27, 2025 · N482UA · Airbus A320232 · Door Warning System
  > DURING TAXI OUT FWD CARGO DOOR OPEN INDICATION. MULTIPLE TIMES INTERMITENTLY VERIFIED FWD CARGO DOOR IS CLOSED AND LOCKED. APPROVED FOR MEL 5270J APPLIED MEL *DM* SUGGEST REF TSM 52-31-00-810-801-A FOR FURTHER ISOLATING THE FAULT. M/L UPDATED WITH PROX SW IN
- [SDR CALA2025031302788](https://openairdocs.org/sdr/CALA2025031302788.md): Cover · detached · Mar 10, 2025 · N482UA · Airbus A320232 · Emergency Lighting
  > FA REPORTS - AFT LIGHT P ANEL/EMERGENCY LIGHT SWI TCH CLEAR COVE R DETACHED INSTALLED AFT PANEL EMERGENCY LIGHT PB CLEAR COVER OK TO CONTINUE.
- [SDR CALA2025020202165](https://openairdocs.org/sdr/CALA2025020202165.md): None · none · Feb 1, 2025 · N482UA · Airbus A320232 · Standard Practices/Structures
  > AFT FORWD LAV D NEEDS CLEANING. BODELY FLUIDS ON FLOOR. CLEANER REMOVED ALL SIGNS OF BODIY FLUID AND SMELLS. AIRCRAFT OK TO CONTINUE WITH FLIGHT
- [SDR CALA2025012101954](https://openairdocs.org/sdr/CALA2025012101954.md): Battery · no test · Jan 14, 2025 · N482UA · Airbus A320232 · Emergency Lighting
  > LEVEL 1 CHRONIC - EMERGENCY LIGHTS ON WITH SWITCH IN ARM. REF TSM 33-51-00-810-881-A. IF NFF AFTER COMPLETING TSM, REPLACE EMERGENCY EXIT LIGHT SWITCH 4WL. REPORT ALL FINDINGS AND ACTION TAKEN IN SIGN-OFF. THANK YOU. DENLM MERCIER. CARRIED BY ELB REPLACED EMER
- [SDR CALA2024080902186](https://openairdocs.org/sdr/CALA2024080902186.md): Skin · contaminated · Aug 7, 2024 · N482UA · Airbus A320232 · Elevator, Plate/Skin
  > DURING THERMOGRAPHIC INSPECTION OF RH ELEVATOR WATER INGRESS NOT ED AT 4TH TRAILING EDGE FASTENER FROM OUTBOARD. REPAIRED WATER INGRESSION AT 4TH TRAILING EDGE FASTENER FROM OB ON RH ELEVATOR IAW SRM 55-21-11-300-004
- [SDR CALA2024082202250](https://openairdocs.org/sdr/CALA2024082202250.md): Skin · damaged · Aug 3, 2024 · N482UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING AAI UNABLE TO LOCATE EXTERNAL FUSELAGE REPAIR DOUBLER RECORDS AT LEFT OF THE NOSE WHEEL WELL EXTERNAL SKIN APPROX. FRAME 18 BETWEEN STR 34L AND 37L JUST ABOVE LEFT SIDE OF THE AIRCRAFT NOSE NUMBER. ACCOMPLISH INSPECTION REQUIREMENTS PER PART 2 OF LATEST
- [SDR CALA2024080202149](https://openairdocs.org/sdr/CALA2024080202149.md): Floor Support · corroded · Jul 31, 2024 · N482UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT PAX CABIN FLOORBOARD SUPPORT -Y765 HOLE CORRODED BETWEEN FR-67 - FR-70. REMOVED AND REPLACED FLOOR SUPPORT -Y765 BETWEEN FR66-FR70 I.A.W SR M 51-72-11 AND SRM 51-42-11.
- [SDR CALA2024080102147](https://openairdocs.org/sdr/CALA2024080102147.md): Stringer · corroded · Jul 16, 2024 · N482UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > NO DOT AFT CARGO COMP L/H STRING 33 BTW FR59-61 HAS SIGNS OF COR ROSION (CLEAN EVALUATE,REPAIR, IF NECCESARY)
- [SDR CALA2024050901412](https://openairdocs.org/sdr/CALA2024050901412.md): Fuel Cap · missing · May 9, 2024 · N482UA · Airbus A320232 · Fuel Storage
  > FUEL CAP MISSING. REF LOG 7909758 FOR DISPOSITION.
- [SDR CALA2023100602984](https://openairdocs.org/sdr/CALA2023100602984.md): Release Mech · frozen · Oct 5, 2023 · N482UA · Airbus A320232 · Emergency Exits
  > RH OVERWING AFT HATCH ARM/DISARM PIN WILL NOT RELEASE TO DISARMED POSITION PER HAECO LCQ NR 9294257/22257 CLEANED RH OVERWING RELEASER IAW A319/320 AMM 52-21-00-100-001-A ALL MAINTENANCE COMPLETED ON NR 9294051 OPS 22051
- [SDR CALA2023100602982](https://openairdocs.org/sdr/CALA2023100602982.md): Release Mech · frozen · Oct 5, 2023 · N482UA · Airbus A320232 · Emergency Exits
  > LH FWD AND RH AFT OVERWING HATCH ARM/DISARM PINS WILL NOT RELEASE TO DISARMED POSITION SDR REQ PER HAECO LCQ NR 9294051/22051 CLEANED LH FWD & RH AFT OVERWING HATCH RELEASERS IAW A320 AMM 52 52-21-11-410-013 A01-21-00-100-001-A RESTORING PROPER FUNCTION TO RH
- [SDR CALA2023100602980](https://openairdocs.org/sdr/CALA2023100602980.md): Hinge Fitting · chafed · Oct 4, 2023 · N482UA · Airbus A320232 · Fuselage, Door Hinge
  > LH MLG DOOR FWD HINGE FWD FACE HAS CHAFFING UNDER BOLT HEAD PER HAECO LCQ NONROUTINE 9294195/22195 REMOVED CHAFED HINGE FITTING LOCATED DRILLED AND INSTALLED NEW H INGE FITTING IAW AIRBUS DRAWING RI 53370500F
- [SDR CALA2023072402320](https://openairdocs.org/sdr/CALA2023072402320.md): Fuel Cap · missing · Jul 23, 2023 · N482UA · Airbus A320232 · Fuel Storage
  > PDA 2 RAMP REPORTED ON ARRIVAL FUELING CAP MISSING, DEN. REF. LOG PAGE #5249003. REPLACED FUEL CAP WITH NEW. PARTS USED: 31-2825-9-0001,QTY:1 IPC REFERENCE # 28.
- [SDR CALA2022100302648](https://openairdocs.org/sdr/CALA2022100302648.md): Fastener · missing · Oct 3, 2022 · N482UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > PDA 3 MISSING FWD PANEL FASTENER WAS REPLACED AS REQ REPLACED MISSING FASTENER ON PANEL 191AT, NOTE TOMC NOTIFIED
- [SDR CALA2022062201554](https://openairdocs.org/sdr/CALA2022062201554.md): Safety Valve · leaking · Jun 22, 2022 · N482UA · Airbus A320232 · Hydraulic Power Accumulator, Main
  > LOSS OF GREEN HYDS, HYD G RSVR LO LVL, HYD G SYS LO PR AND HYD G ENG 1 PUMP LO PR. LOCKING FOR POSITIVE FIX. UNLOCK TO UPDATE VERIFIED LANDING GEAR SAFETY VALVE CAUSE OF GREEN HYD SYSTEM LOSS OF FLUID. STARTED REMOVAL OF LANDING GEAR SAFETY VALVE UP TO AND INC
- [SDR CALA2022022100470](https://openairdocs.org/sdr/CALA2022022100470.md): Bearing · worn · Feb 21, 2022 · N482UA · Airbus A320232 · Nose/Tail Landing Gear Attach Section
  > HYDRAULIC LEAK FROM NLG LOWER LEG ASSY BELOW STEERING CYLINDERS. MAY BE DYNAMIC SEALS. SEE PHOTOS. REMOVED AFT NOSE WHEEL STEERING CYLINDER REF AMM 32-51-42-000-001-C01. FOUND BEARING DISC WORN AND ORING AND BACKUP RINGS DAMAGED LOCK WASHERS NOT BENT OVER OR
- [SDR CALA2021100601803](https://openairdocs.org/sdr/CALA2021100601803.md): None · none · Oct 6, 2021 · N482UA · Airbus A320232 · Fuselage Structure (General)
  > REFERENCE LP7161768 PLANNING TO CONTACT ENGINEERING AFTER 29-JAN -22, BUT BEFORE 28-FEB-22 FOR ECRA 5341-01271 PART 3 PERMANENT REPAIR ACCOMPLISH A PERMANENT REPAIR PER PART 3 OF LATEST REVISION OF ECRA 5341-01271. PLANNING TO CONTACT ENGINEERING AFTER 29-JAN-
- [SDR CALA2021100601786](https://openairdocs.org/sdr/CALA2021100601786.md): None · none · Oct 4, 2021 · N482UA · Airbus A320232 · Fuselage Structure (General)
  > REFERENCE VT MAE N/R #0013869 ROTO PROBE OF ADDITIONAL FASTENER HOLES PER STEP 3.2 OF EA 5330-05216 REV B OP002 FOUND SIX ADDITI ONAL FASTENER HOLES WITH CRACKS O/B OF Y+1292 24-MAR-2022 REF VT MAE N/R #0013869. REPAIRED LH PRESSURE PANEL IAW ECRA INTERIM REPA
- [SDR CALA2021100601784](https://openairdocs.org/sdr/CALA2021100601784.md): Bulkhead · cracked · Oct 4, 2021 · N482UA · Airbus A320232 · Fuselage Main, Structure
  > (SUPPORT TASK) DURING ROTO PROBE OF FASTENER HOLES AT RH FR35 ST R30, DAMAGE INDICATIONS WERE NOTED IN THE TOP AFT HOLE.() COMPLIED WITH EC/RA 5321-02055 TO REPAIR FR35 STR 30 HOLE #1 RH WITH NO DEVIATIONS. ACCOMPLISHED BY EMP#V933440 AT BFM VT MOBILE AEROSPAC
- [SDR CALA2021100601783](https://openairdocs.org/sdr/CALA2021100601783.md): Bulkhead · damaged · Oct 4, 2021 · N482UA · Airbus A320232 · Fuselage Structure (General)
  > (AD 2016-14-03) DURING ROTO PROBE INSPECTION OF LH FR35 BTW STGR 28 AND STG31. REJECTABLE DAMAGE INDICATIONS WAS NOTED IN 8 HOLES CIRCLED IN RED. REPAIR BEFORE FURTHER FLIGHT.() REPAIRED LH FR35 HOLES BETWEEN STGR28-31 BY COMPLYING WITH EC/RA 5321-02055 WITH N
- [SDR CALA2021100601782](https://openairdocs.org/sdr/CALA2021100601782.md): Bulkhead · damaged · Oct 4, 2021 · N482UA · Airbus A320232 · Fuselage Main, Structure
  > (SUPPORT TASK) DURING ROTO PROBE OF FASTENER HOLES AT LH FR35 ST R30, DAMAGE INDICATIONS WERE NOTED IN THE TOP AFT HOLE.() REPAIR FR35 STGR30 HOLE #1 L/H BY COMPLY WITH EC/RA 5321-02055 W ITH NO DEVIATIONS. ACCOMPLISHED BY EMP#V933440 AT BFM VT AEROSPA CE MOBI
- [SDR CALA2021100601781](https://openairdocs.org/sdr/CALA2021100601781.md): Bulkhead · cracked · Oct 4, 2021 · N482UA · Airbus A320232 · Fuselage Main, Structure
  > DURING ROTO PROBE OF FASTENER HOLES AT LH FR35 STR30, A CRACK IN DICATION WAS NOTED IN THE BOTTOM AFT HOLE.() REPAIRED LH FR35 STR 30 HOLE #2 BY COMPLYING WITH EC/RA 5321-020 55 WITH NO DEVIATIONS. ACCOMPLISHED BY EMP#V933440 AT BFM VT AER OSPACE MOBILE. NR#00
- [SDR CALA2021100601780](https://openairdocs.org/sdr/CALA2021100601780.md): Bulkhead · none · Oct 4, 2021 · N482UA · Airbus A320232 · Fuselage Main, Structure
  > (SUPPORT TASK) DURING ROTO PROBE OF FASTENER HOLES AT RH FR35 ST R30, A DAMAGE INDICATION WAS NOTED AT THE BOTTOM AFT HOLE.() REPAIRED R/H FR35 STR30 HOLE #2 BY C/W EC/RA 5321-02055 WITH NO DEVIATIONS. EMP#V933440 AT BFM VT AEROSPACE MOBILE. NR#0013369
- [SDR CALA2021100401771](https://openairdocs.org/sdr/CALA2021100401771.md): None · cracked · Oct 3, 2021 · N482UA · Airbus A320232 · Fuselage Structure (General)
  > WHILE AT VT MAE BFM REF N/R #0013859 (EA 5341-01231 REV ORIG) DURING HFEC INSPECTION OF THE LH FR68WEB AT DOOR STOP FITTING #1 A CRACK INDICATION WAS NOTED AT STGR 22 WEB HORIZONTAL FLANGE UPPER & BOTTOM RADUIS, CRACK LENGHT APPROX 0.663IN BEFORE 29-MAR-2022.
- [SDR CALA2021100401768](https://openairdocs.org/sdr/CALA2021100401768.md): None · damaged · Oct 2, 2021 · N482UA · Airbus A320232 · Standard Practices/Structures
  > (AD 2019-20-10) DURING ROTO PROBE INSPECTION OF THE RH DOOR STOP FITTING #1 AT FR16. REJECTABLE DAMAGE INDICATION WAS NOTED IN UP PER I/B AND O/B HOLES DUE TO THREAD DAMAGE. () REPAIRED RH #1 DOOR STOP FITTING HOLES/AREA IAW EC/RA 5311-02639 VT MAE FINAL EA 32
- [SDR CALA2021100401767](https://openairdocs.org/sdr/CALA2021100401767.md): Skin · corroded · Oct 2, 2021 · N482UA · Airbus A320232 · Fuselage Main, Structure
  > REMOVED CORROSION IAW SRM 51-74-00 ORIGINAL SKIN THICKNESS.063" L=1.660" W=1.020" D=.060" FOUND OT BE OUT OF LIMITS IAW SRM 53-4 1-11-283 FIG. REPAIRED IAW FINAL EC/RA 5331-02766 REV "-" AND EA 320-5341-13-A2686 REV "-" REMOVED CORROSION IAW SRM 51-74-00 ORIG
- [SDR CALA2021100101737](https://openairdocs.org/sdr/CALA2021100101737.md): Plate · corroded · Sep 30, 2021 · N482UA · Airbus A320232 · Fuselage Main, Structure
  > RIGHT HAND SHEAR PLATE @ FR68-70 HAS CORROSION() REPLACED SHEAR PLATE AND SUPPORT FRAME IAW A320 SRM 51-42-11, SH EAR PLATE P/N# D5347112420300 BATCH# 0003689234, NEW SUPPORT FRA ME P/N# D5347112320300 BATCH# 0002507052 FORM 44-0008 ARTACHED E MP# V934583 WORK
- [SDR CALA2021100101730](https://openairdocs.org/sdr/CALA2021100101730.md): Stringer · corroded · Sep 29, 2021 · N482UA · Airbus A320232 · Standard Practices/Structures
  > A3NB-05-3-6022:BULK CARGO COMPT FR 64-65 STRINGER 44 HAS CORROSI ON DOT 116-66 () SPLICE AND STRINGER IAW SRM 51-42-11 FROM FR 63 TO FR 67, CUT SECTION OUT OF DAN50B08 BATCH #2478344, D5348003020700 AND SPLICE, FACTORY SPLICE AND STRINGER REPAIR SECTION IAW SR
- [SDR CALA2021100101729](https://openairdocs.org/sdr/CALA2021100101729.md): Stringer · corroded · Sep 29, 2021 · N482UA · Airbus A320232 · Standard Practices/Structures
  > A3NB-05-3-6022: BULK CARGO COMPT FR 63-64 STRINGER 42R HAS CORRO SION. DOT 116-65 () 283-002. REPAIRED STRINGER SECTION 42 BETWEEN FR63 TO FR64 IAW INSPECTION THRESHOLD FROM TIME OF ADL/REPAIR EMBODIMENT IS SRM 53-00-13-300-001, FIG 001, SHT 1. DIM CUT OUT LIM
- [SDR CALA2021092801721](https://openairdocs.org/sdr/CALA2021092801721.md): Shear Plate · corroded · Sep 28, 2021 · N482UA · Airbus A320232 · Fuselage Main, Structure
  > RIGHT HAND SHEAR PLATE @ FR68-70 HAS CORROSION() REPLACED SHEAR PLATE AND SUPPORT FRAME IAW A320 SRM 51-42-11, SH EAR PLATE P/N# D5347112420300 BATCH# 0003689234, NEW SUPPORT FRA ME P/N# D5347112320300 BATCH# 0002507052 FORM 44-0008 ARTACHED E MP# V934583 WORK
- [SDR CALA2021092801712](https://openairdocs.org/sdr/CALA2021092801712.md): Stringer · corroded · Sep 28, 2021 · N482UA · Airbus A320232 · Fuselage Main, Structure
  > A3NB-05-3-6022: BULK CARGO COMPT FR 63-64 STRINGER 42R HAS CORRO SION. DOT 116-65 () 283-002. REPAIRED STRINGER SECTION 42 BETWEEN FR63 TO FR64 IAW INSPECTION THRESHOLD FROM TIME OF ADL/REPAIR EMBODIMENT IS SRM 53-00-13-300-001, FIG 001, SHT 1. DIM CUT OUT LIM
- [SDR CALA2021092801711](https://openairdocs.org/sdr/CALA2021092801711.md): Stringer · corroded · Sep 28, 2021 · N482UA · Airbus A320232 · Fuselage Main, Structure
  > A3NB-05-3-6022:BULK CARGO COMPT FR 64-65 STRINGER 44 HAS CORROSI ON DOT 116-66 () SPLICE AND STRINGER IAW SRM 51-42-11 FROM FR 63 TO FR 67, CUT SECTION OUT OF DAN50B08 BATCH #2478344, D5348003020700 AND SPLICE, FACTORY SPLICE AND STRINGER REPAIR SECTION IAW SR
- [SDR CALA2021092801709](https://openairdocs.org/sdr/CALA2021092801709.md): Skin · corroded · Sep 28, 2021 · N482UA · Airbus A320232 · Fuselage Main, Structure
  > (A3NB-05-3-6071) TOP OF FUSELAGE SKIN UNDER VERT STAB SEVERAL HE ADS HAVE CORROSION, FWD AND BETWEEN LH&RH AFT VERT STAB MOUNT BR ACKETS.DOT NO. 17-71() 69,400 TOTAL AIRCRAFT FLIGHT CYCLES PERFORM AN INSPECTION PER PART 2 OF THE LATEST REVISION OF ECRA 5331-02
- [SDR CALA2021092701687](https://openairdocs.org/sdr/CALA2021092701687.md): Stringer · corroded · Sep 26, 2021 · N482UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > BULK CARGO COMPARTMENT FR61-62 STR33R HAS LIGHT SURFACE CORROSIO N.(REMOVE CORROSION AND CHECK LIMITS. BLENDED DAMAGED AREA IAW A320 SRM 51-74-00, CHECKED LIMITS D=.04 7" W=1.5" L=15" OUT OF LIMITS. REPAIRED STRINGER SECTION 33R BET W FR60 TO FR62, STRINGER MA
- [SDR CALA2021092201651](https://openairdocs.org/sdr/CALA2021092201651.md): Frame · corroded · Sep 21, 2021 · N482UA · Airbus A320232 · Fuselage Structure (General)
  > BULK CARGO COMPARTMENT FR 61-62 STR33R HAS LIGHT SURFACE CORROSION (REMOVE CORROSION AND CHECK LIMITS) DAMAGE LOCATED AT STR 33R FR 60 - 62 BLENDED IAW SRM 51-74-00. BLENDED AREA MEASURES L=15" W= 1.5" D=.047", ORIGINAL THICKNESS.063", REMAINING MATERIAL.016
- [SDR CALA2021092001618](https://openairdocs.org/sdr/CALA2021092001618.md): Stringer · corroded · Sep 20, 2021 · N482UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > (A3NB-52-4-6058) CORROSION ON STRINGER 33R BETWEEN FR 56-57. REMOVED AND REPLACED STINGER AT 33R BETWEEN FR 56 AND 58 IAW SRM 51-42-11. ACCOMPLISHED BY EMP#922369 AT BFM VT AEROSPACE MOBILE NR#0013329
- [SDR CALA2021091001547](https://openairdocs.org/sdr/CALA2021091001547.md): Panel · corroded · Sep 9, 2021 · N482UA · Airbus A320232 · Flight Compartment Windows
  > A3NB-53-3-6185 MAIN CABIN FLOOR LH ANGLE SHEAR PLATE BETWEEN FR6 9-FR70 HAS CORROSION. (DOT 38-30) () DISPLACED COAXIAL CABLE (7102CVB) TO BENEATH LH ANLGE SHEAR PLAT E BETWEEN FR 69-FR70 IAW ESPM 20-33-11-02. REMOVED FASTENER OF L H ANGLE SHEAR PLATE IAW SRM
- [SDR CALA2021090301488](https://openairdocs.org/sdr/CALA2021090301488.md): Floor Support · corroded · Sep 1, 2021 · N482UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > A3NB-53-3-6185 MAIN CABIN FLOOR SUPPORT -Y765 HAS CORROSION BETW EEN FR67-FR68. FLOOR SUPPORT Y-765, FR67 68 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14-293-002 L2.0", W1.75" B0.024 REMOVED DAMAGE AREA IAW SR M 51-42-11 LOCATED AND DRILLED NEW PART IAW SRM 51-
- [SDR CALA2021090101481](https://openairdocs.org/sdr/CALA2021090101481.md): Floor Support · corroded · Sep 1, 2021 · N482UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > A3NB-53-3-6185 MAIN CABIN FLOOR SUPPORT -Y765 HAS CORROSION BETW EEN FR67-FR68. FLOOR SUPPORT Y-765, FR67 68 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14-293-002 L2.0", W1.75" B0.024 REMOVED DAMAGE AREA IAW SR M 51-42-11 LOCATED AND DRILLED NEW PART IAW SRM 51-
- [SDR CALA2021090101475](https://openairdocs.org/sdr/CALA2021090101475.md): Door Sill · corroded · Sep 1, 2021 · N482UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > (A3NB-53-3-6185) R2 DOOR SILL HAS CORROSION FR66 THORUGH FR68. ( REMOVE CORROSION AND CHECK LIMITS.) REMOVED CORROSION R-2 DOOR SILL FR66 AND FR68 I/B SIDE OUT OF LI MITS IAW A320 SRM 53-71-14-283. FIG 002, REMOVED ADN REPLACED R- 2 DOOR SILL P/N D534800432090
- [SDR CALA2021090101462](https://openairdocs.org/sdr/CALA2021090101462.md): Floor Support · corroded · Aug 30, 2021 · N482UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > A3NB-53-3-6185 MAIN CABIN FLOOR SUPPORT -Y765 HAS CORROSION AT F R66. FLOOR SUPPORT Y765 FR86 FOUND TO BE OUT OF LIMITS IAW 53-00-14-2 83-002 L=1.75" W=1.0" D 0.022" REMOVED DAMAGE AREA IAW SRM 51-42 -11 LOCATED AND DRILLED NEW BEAM IAW SRM 51-44-11 INSTALLED
- [SDR CALA2021090101461](https://openairdocs.org/sdr/CALA2021090101461.md): Seat Track · corroded · Aug 30, 2021 · N482UA · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > (A3NB-53-3-6040) CORROSION AT MAIN CABIN SEAT TRACK FR 20-FR24 Y -765. REPLACED SEAT TRACK P/N:D5311281400251 BTCH:0003814572 IAW A320 SRM 51-42-11 AND SRM 51-72-11-811-001.

Next page: https://openairdocs.org/aircraft/N482UA/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 = 'N482UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N482UA/reports

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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.