# Service difficulty reports: N487UA

A list on [N487UA](https://openairdocs.org/aircraft/N487UA.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 2 · 100 reports

- [SDR CALA2026092119564](https://openairdocs.org/sdr/CALA2026092119564.md): Power Supply · faulted · Sep 19, 2026 · N487UA · Airbus A320232 · Emergency Lighting
  > DURING EMERGENCY LIGHT TEST FAIL MESSAGE EPSU INT LOAD EMER RT APPEARED. IAW FIM 33-51-00-810-807-A, REMOVED AND REPLACED EPSU AND BATTERY 12WL IAW AMM 33-51-38-000-001-A. NO FIX. SUGGEST FURTHER TROUBLESHOOTING OF WIRING PER FIM. CONFIRMED ALL EXIT MARKERS
- [SDR CALA2026012613250](https://openairdocs.org/sdr/CALA2026012613250.md): Potable Water · odor · Jan 26, 2026 · N487UA · Airbus A320232 · Potable Water System
  > FA SAYS POTABLE WATER HAS STRONG FISH ODOR. PERFORMED A COMPLETE DRAIN & REFILL AS REQUIRED.
- [SDR CALA2025072406868](https://openairdocs.org/sdr/CALA2025072406868.md): Skin · damaged · Jul 23, 2025 · N487UA · Airbus A320232 · Landing Gear Doors
  > BREAKAWAY ON PUSHBACK TUG DRIVER MENTIONED SCRAPE ON PAINT. RE-EVALUATED SCRAPE FOUND AS FOLLOWS, SCRAPE MEASURES 17.5 INCH L BY 3 INCH W, TOTAL AREA, DEPTH OF SCRAPE IN TO METAL IS.040 DEEP. APPROX 4 INCHES OUT BOARD FROM FORWARD NLG DOOR. SCRAPE HAS A DEN
- [SDR CALA2024110400996](https://openairdocs.org/sdr/CALA2024110400996.md): Drain Line · leaking · Nov 1, 2024 · N487UA · Airbus A320232 · Hydraulic Power System
  > LOSS OF GREEN HYD QTY RESULTED IN ECAM HYD G RSVR LO LVL. FOUND CRACK ON NUMBER ONE ENG RETURN LINE FROM THRUST REVERSER SHUTOFF VALVE DUE TO BROKEN CLAMP, SEE PHOTO FOR LOCATION. REMOVED AND REPLACED HYDRAULIC LINE REF IPC 29-11-06-02L ITEM 260 REQUIRES LEAK
- [SDR CALA2024090900602](https://openairdocs.org/sdr/CALA2024090900602.md): Control Servo · faulty · Sep 6, 2024 · N487UA · Airbus A320232 · Drag Control System
  > SPLR FAULT DISPLAYED ON UPPER ECAM SCREEN. - F-CTL ON DEPARTURE FLT CONTROLSPLR FAULT ON UPPER ECAM SPOKE TO FLIGHT CREW. SPOILER FAULT OCCURED ON TAXI OUT, RESET SEC 1 2 AND 3, FAULT CLEARED. ONCE AIRBORNE, AFTER 5-10 SECONDS OF GEAR UP, FAULT RETURNED. PILOT
- [SDR CALA2024061800026](https://openairdocs.org/sdr/CALA2024061800026.md): Battery · no test · Jun 18, 2024 · N487UA · Airbus A320232 · Emergency Equipment
  > FIRST OFFICERS FLASH LIGHT INOP REMOVED AND REPLACED FIRST OFFICER'S FLASHLIGHT BATTERY. OPS CHECK GOOD PER A320 AMM 25-65-98-910-C-1.
- [SDR CALA2023122003666](https://openairdocs.org/sdr/CALA2023122003666.md): Fuel Cap · missing · Dec 19, 2023 · N487UA · Airbus A320232 · Fuel Storage
  > PDA 2 FUEL CAP DEPARTED AIRCRAFT, DEFERED ON LP 6585440. CAP, COUPLING R OFF 31-2825-9-0001 2989 ON 0000 CAP, COUPLING R OFF 31-2825-9-0001 2989 ON 31-2825-9-0001 7108 INSTALLED NEW FUEL CAP IN REFERENCE TO AMM 28-25-41. PARTS USED: 31-2825-9-0001,QTY:1 ROTAB
- [SDR CALA2023120603572](https://openairdocs.org/sdr/CALA2023120603572.md): Fuel Cap · missing · Nov 30, 2023 · N487UA · Airbus A320232 · Fuel Storage
  > FUEL CAP MISSING FUEL CAP PLACED ON CDL. NO PART IN STOCK PLACED UNDER MEL AND PDA ACCOMPLISHED CAP MISSING DURING ARRIVAL AS PER INFO PROVIDED OK TO DEFERED DISPATCH DESK: S18 NAME: DATE: 30-NOV-23- OKAY TO CDL 28A
- [SDR CALA2023061601894](https://openairdocs.org/sdr/CALA2023061601894.md): Control Panel · inoperative · Jun 14, 2023 · N487UA · Airbus A320232 · Communications System
  > COCKPIT AUDIO CONTROL PANEL 2 INOP - COM DID NOT WORK IN THE AIR REMOVED AND REPLACED AMU REF AMM 23-51-34 BITE TEST PASSED PARTS USED: 31-2355-9-0001,QTY:1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1734629 SN OFF 1172 UNIT, AUDIO MAN OFF 31-2355-9-0001 11
- [SDR CALA2023020100309](https://openairdocs.org/sdr/CALA2023020100309.md): None · failed · Feb 1, 2023 · N487UA · Airbus A320232 · Emergency Lighting
  > EMERGENCY LIGHTS POWER UNITS 11WL AND 12WL FAILED TEST. SECURED CONNECTION TO 11WL EPSU AND REMOVED NUMBER FIN 12WL AND STA: ST ENG BFM INSTALLED NEW EPSU IN 12WL POSITION IAW AMM 33-51-38-400-001-A A ND. PERFORMED BITE TEST FOR INSTALLATION AND OPERATIONAL TE
- [SDR CALA2023010600037](https://openairdocs.org/sdr/CALA2023010600037.md): Door Sill · corroded · Jan 6, 2023 · N487UA · Airbus A320232 · Fuselage Main, Structure
  > RH AFT DOOR SILL FR66 TO FR68 CORRODED AT 4 LOCATIONS (P/N D5348 004320701) REMOVED CORROSION ON DOOR SILL IAW SRM 51-74-00. MEASURED AND FO UND OUT OF LIMITS IAW SRM 53-41-14 L=1.400" W=1.130 D=0.060" O.T =0.177" T.T=.117" REPLACED DOOR SILL IAW SRM 51-72-11-
- [SDR CALA2023010600036](https://openairdocs.org/sdr/CALA2023010600036.md): Stop Fitting · cracked · Jan 6, 2023 · N487UA · Airbus A320232 · Fuselage Main, Structure
  > DURING ROTO INSP OF LH FR 20 DOOR STOP FITTING #7. CRACK INDICATION WAS NOTED IN UPPER I/B HOLE, FRAME AND INTERCOSTAL L AYERS. REPAIR BEFORE NEXT FLIGHT. REPAIRED DAMAGED HOLE IAW REPAIR DRAWING R53113118. EMP:V934583 W/C:6001971315 STENGBFM
- [SDR CALA2023010600044](https://openairdocs.org/sdr/CALA2023010600044.md): Door Sill · corroded · Jan 4, 2023 · N487UA · Airbus A320232 · Fuselage Main, Frame
  > RH AFT DOOR SILL FR66 TO FR68 CORRODED AT 4 LOCATIONS (P/N D5348 004320701) REMOVED CORROSION ON DOOR SILL IAW SRM 51-74-00. MEASURED AND FO UND OUT OF LIMITS IAW SRM 53-41-14 L=1.400" W=1.130 D=0.060" O.T =0.177" T.T=.117" REPLACED DOOR SILL IAW SRM 51-72-11-
- [SDR CALA2023010600042](https://openairdocs.org/sdr/CALA2023010600042.md): Intercostal · cracked · Jan 4, 2023 · N487UA · Airbus A320232 · Fuselage Main, Structure
  > DURING ROTO INSP OF LH FR 20 DOOR STOP FITTING #7. CRACK INDICATION WAS NOTED IN UPPER I/B HOLE, FRAME AND INTERCOSTAL L AYERS. REPAIR BEFORE NEXT FLIGHT. REPAIRED DAMAGED HOLE IAW REPAIR DRAWING R53113118. EMP:V934583 W/C:6001971315 STENGBFM
- [SDR CALA2023010400031](https://openairdocs.org/sdr/CALA2023010400031.md): Door Frame · damaged · Jan 3, 2023 · N487UA · Airbus A320232 · Fuselage Main, Structure
  > DURING ROTO INSP OF RH FR16 DOOR STOP AND IN UPPER O/B HOLE, FRAME AND INTERCOSTAL LAYERS. REPAIR BEFORE NEXT FLIGHT. REPAIRED DAMAGED HOLE IAW REPAIR DRWARING R53113118 AND FINAL EC RA #5311-02931 EMP# V934700 STA: ST ENG BFM WC: 40935
- [SDR CALA2023010400029](https://openairdocs.org/sdr/CALA2023010400029.md): Stringer · corroded · Jan 2, 2023 · N487UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AFT CARGO COMPARTMENT, FRAMES 58-60, S42L CORRODED AFT CARGO STRINGER REMOVED, FOUND OUT OF LIMI TS AREA WERE NO REPAIR ALLOWED. INSTALLED A NEW STRINGER IAW SRM 51-42-11.
- [SDR CALA2023010200013](https://openairdocs.org/sdr/CALA2023010200013.md): Stringer · corroded · Jan 2, 2023 · N487UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AFT CARGO COMPARTMENT, FR58-FR60, STRG42L CORRODED AFT CARGO COMPARTMENT FR60-FR53 STRINGER 42L REMOVED OUT OF LIMI TS AREA WERE NO REMAIR ALL IAWED, RECEIVED NEW STRINGER AND INSTALLED.
- [SDR CALA2022122603487](https://openairdocs.org/sdr/CALA2022122603487.md): Floor Support · corroded · Dec 23, 2022 · N487UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT -Y1292 FR68-FR69 CORRODED AT FR68. FLOOR SUPPORT -Y1292 FR68-FR69 REMOVED IAW SRM 51-42-11, FOUND T WC: 41177 STA: ST ENG BFM O BE OUT LIMITS IAW SRM TASK 53-00-14-283-002 L=1,300" W-1,200", D=0,080" T93986, RECEIVED NEW FLOOR SUPPORT P/N D534721
- [SDR CALA2022122603486](https://openairdocs.org/sdr/CALA2022122603486.md): Stringer · corroded · Dec 23, 2022 · N487UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AFT CARGO COMPARTMENT, FR56-FR58, STRG43L CORRODED. REMOVED AND REPLACED STRINGER 43L FR56 TO FR58 IAW SRM 51-42-11.
- [SDR CALA2022122603485](https://openairdocs.org/sdr/CALA2022122603485.md): Floor Support · corroded · Dec 23, 2022 · N487UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT -Y1292 FR64-FR66 HAS CORROSIONAT FR64 AND FR66. FLOOR SUPPORT -Y1292 FR64-FR66 REMOVED IAW SRM 51-42-11, FOUND T ENGBFM WC: 41194 O BE OUT LIMITS IAW SRM TASK 53-00-14-283-002 L-1.500",W=1.0", D =0.075" T93986, RECEIVED NEW FLOOR SUPPORT P/N D534
- [SDR CALA2022122303476](https://openairdocs.org/sdr/CALA2022122303476.md): Floor Support · corroded · Dec 23, 2022 · N487UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT -Y1292 CORRODED AT FRAME 68. FLOOR SUPPORT REMOVED IAW SRM 51-42-11, FOUND TO BE OUT LIMITS IAW SRM 53-00-14-283-002, AND INSTALLED NEW IAW SRM 51-42-11.
- [SDR CALA2022122303475](https://openairdocs.org/sdr/CALA2022122303475.md): Stringer · corroded · Dec 23, 2022 · N487UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AFT CARGO COMPARTMENT, FR56-FR58, STRINGER 43L CORRODED. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-11.
- [SDR CALA2022121903431](https://openairdocs.org/sdr/CALA2022121903431.md): Floor Support · corroded · Dec 18, 2022 · N487UA · Airbus A320232 · Fuselage Main, Structure
  > FLOOR SUPPORT Y1292 FR68-FR69 CORRODED AT FR68. REMOVED AND REPLACED FLOOR SUPPORT Y1292 FR68 TO 69 I.A.W SRM 51 -42-11-001 AND APPLIED TOP COAT I.A.W SRM 51-23-11. EMP: V934614 WC: 41180 STA: ST ENG BFM
- [SDR CALA2022121903430](https://openairdocs.org/sdr/CALA2022121903430.md): Floor Support · corroded · Dec 18, 2022 · N487UA · Airbus A320232 · Fuselage Main, Structure
  > FLOOR SUPPORT Y1292 FR66-FR68 HAS CORROSION AT FR66 AND FR68. REMOVED AND REPLACED FLOOR SUPPORT Y1292 FR66 TO FR68 I.A.W SRM 51-42-11 AND APPLIED TOP COAT I.A.W SRM 51-23-11. EMP: V934614 W C: 41184 STA: ST ENG BFM
- [SDR CALA2022121903420](https://openairdocs.org/sdr/CALA2022121903420.md): Web · corroded · Dec 16, 2022 · N487UA · Airbus A320232 · Fuselage Main, Structure
  > FWD CABIN WEB AT -Y1732 CORRODED AT FR20. FWD CABIN WEB AT -Y1732 REMOVED AND REPLACED IAW SRM 51-42-11/00 1 AND APPLIED TOPCOAT IAW SRM 51-23-11. EMP: V934614 WC: 41297 S TA: ST ENG BFM
- [SDR CALA2022121903419](https://openairdocs.org/sdr/CALA2022121903419.md): Floor Support · corroded · Dec 16, 2022 · N487UA · Airbus A320232 · Fuselage Main, Structure
  > FLOOR SUPPORT Y515 FR68 TO FR70 CORRODED AT 2 LOCATIONS REMOVED/REPLACED SUPPORT Y515 FR68 TO FR70 P/N D5347209400400 BT CH 0003912854 IAW SRM 51-72-11-911-001. EMP: V934337 WC: 41168 S TA: ST ENG BFM
- [SDR CALA2022121903418](https://openairdocs.org/sdr/CALA2022121903418.md): Floor Support · corroded · Dec 16, 2022 · N487UA · Airbus A320232 · Fuselage Main, Structure
  > FLOOR SUPPORT Y515 FR64 TO FR67 CORRODED AT 2 LOCATIONS REMOVED/REPLACED FLOOR SUPPORT Y515 FR64 TO FR67 P/N D5347209400 800 BTCH 0003809500 IAW SRM 51-72-11-911-001. EMP: V934337 WC: 4 1167 STA: ST ENG BFM
- [SDR CALA2022121903417](https://openairdocs.org/sdr/CALA2022121903417.md): Seat Track · corroded · Dec 16, 2022 · N487UA · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN R/H O/B SEAT TRACK HAS CORROSION AT FR 20. CABIN R/H O/B SEAT TRACK REMOVED TO BE OUT OF LIMITS IAW SRM 53- #41109 11-15-283-010, L=2.75" W= 1.41", D=11.5" TR93985, RECEIVED NEW S EAT TRACK P/N D53112782202001, BTCH 0003999562, AND INSTALLED NW SEAT TRAC
- [SDR CALA2022121903416](https://openairdocs.org/sdr/CALA2022121903416.md): Floor Support · corroded · Dec 16, 2022 · N487UA · Airbus A320232 · Fuselage Main, Structure
  > FLOOR SUPPORT Y765 FR66 TO FR70 CORRODED AT 2 LOCATIONS FLOOR SUPPORT Y765 FR66 TO FR70 REMOVED TO BE FOUND OUT OF LIMIT 6 S IAW 53-00-14-283-002 L=1.500" W=2.00", D=1.10" RECEIVED NEW FL OOR SUPPORT P/N D5347219220000, BTCH 0004031110, AND INSTALLED NEW FLOOR
- [SDR CALA2022121903415](https://openairdocs.org/sdr/CALA2022121903415.md): Floor Support · corroded · Dec 16, 2022 · N487UA · Airbus A320232 · Fuselage Main, Structure
  > FLOOR SUPPORT -Y1292 FR66-FR68 CORRODED AT FR66 AND FR68. FLOOR SUPPORT -Y1292 FR66-FR68 REMOVED IAW SRM 51-42-11, FOUND T WC: 41175 STA: ST ENG BFM O BE OUT LIMITS IAW SRM TASK 53-00-14-283-002 L=1.500", W=1.4--", D=-,078" T93986. RECEIVED NEW FLOOR SUPPORT
- [SDR CALA2022121903414](https://openairdocs.org/sdr/CALA2022121903414.md): Floor Support · corroded · Dec 16, 2022 · N487UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT Y765 FR64 TO FR66 CORRODED AT 2 LOCATIONS. EVALUATED FOR DAMAGE AND FOUND OUT OF LIMIT IAW 53-00-14-283-002. REMOVED FLOOR BEAM AND INSTALLED NEW FLOOR BEAM IAW SRM 51-42- 71/001.
- [SDR CALA2022121903413](https://openairdocs.org/sdr/CALA2022121903413.md): Floor Support · corroded · Dec 16, 2022 · N487UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > FWD CABINDUMMY RAIL FR12 TO 16, Y503.2 CORRODED AT FR16 REMOVED OLD RAIL AND FABRICATE NEW RAIL Y503.2 IAW, AIRBUS DRAWI NG D5311287 AND INSTALLED IAW SRM 51-42-11. EMP#: V936191 STATIO N: BFM WC# 41296
- [SDR CALA2022121903412](https://openairdocs.org/sdr/CALA2022121903412.md): Floor Support · corroded · Dec 16, 2022 · N487UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > CABIN LAVATORY "D" ATTACHMENT POINT TO FLOOR SUPPORT ARE CORRODED. EVALUATED FOR DAMAGE AND FOUND OUT LIMIT IAW SRM 53-00-14-283-00 2 REMOVED FLOOR BEAM AND REPLACED NEW FLOOR BEAM I.AW SRM 51-42- 11/001.
- [SDR CALA2022121603400](https://openairdocs.org/sdr/CALA2022121603400.md): Floorbeam · corroded · Dec 15, 2022 · N487UA · Airbus A320232 · Fuselage Main, Floor Beam
  > FLOOR SUPPORT Y765 FR64 TO FR66 CORRODED AT 2 LOCATIONS. EVALUATED FOR DAMAGE AND FOUND OUT OF LIMIT IAW 53-00-14-283-002. REMOVED FLOOR BEAM AND INSTALLED NEW FLOOR BEAM IAW SRM 51-42- 71/001. EMP: V940360 WC: 41165 STA: ST ENG BFM
- [SDR CALA2022121603399](https://openairdocs.org/sdr/CALA2022121603399.md): Floor Support · corroded · Dec 15, 2022 · N487UA · Airbus A320232 · Fuselage Main, Structure
  > FLOOR SUPPORT Y765 FR66 TO FR70 CORRODED AT 2 LOCATIONS FLOOR SUPPORT Y765 FR66 TO FR70 REMOVED TO BE FOUND OUT OF LIMIT 6 S IAW 53-00-14-283-002 L=1.500" W=2.00", D=1.10" RECEIVED NEW FL OOR SUPPORT P/N D5347219220000, BTCH 0004031110, AND INSTALLED NEW FLOOR
- [SDR CALA2022121603398](https://openairdocs.org/sdr/CALA2022121603398.md): Seat Track · corroded · Dec 15, 2022 · N487UA · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN R/H O/B SEAT TRACK HAS CORROSION AT FR 20. CABIN R/H O/B SEAT TRACK REMOVED TO BE OUT OF LIMITS IAW SRM 53- #41109 11-15-283-010, L=2.75" W= 1.41", D=11.5" TR93985, RECEIVED NEW S EAT TRACK P/N D53112782202001, BTCH 0003999562, AND INSTALLED NW SEAT TRAC
- [SDR CALA2022121603397](https://openairdocs.org/sdr/CALA2022121603397.md): Dummy Rail · corroded · Dec 15, 2022 · N487UA · Airbus A320232 · Fuselage Main, Structure
  > FWD CABINDUMMY RAIL FR12 TO 16, Y503.2 CORRODED AT FR16 REMOVED OLD RAIL AND FABRICATE NEW RAIL Y503.2 IAW, AIRBUS DRAWI NG D5311287 AND INSTALLED IAW SRM 51-42-11. EMP#: V936191 STATIO N: BFM WC# 41296
- [SDR CALA2022121603396](https://openairdocs.org/sdr/CALA2022121603396.md): Floor Support · corroded · Dec 15, 2022 · N487UA · Airbus A320232 · Fuselage Main, Floor Beam
  > FLOOR SUPPORT -Y1292 FR66-FR68 CORRODED AT FR66 AND FR68. FLOOR SUPPORT -Y1292 FR66-FR68 REMOVED IAW SRM 51-42-11, FOUND T WC: 41175 STA: ST ENG BFM O BE OUT LIMITS IAW SRM TASK 53-00-14-283-002 L=1.500", W=1.4--", D=-,078" T93986. RECEIVED NEW FLOOR SUPPORT
- [SDR CALA2022121403377](https://openairdocs.org/sdr/CALA2022121403377.md): Access Panel · gouged · Dec 14, 2022 · N487UA · Airbus A320232 · Fuel Storage
  > RT WING FUEL TANK ACCESS PANEL 640RB HAS GOUGE ON ONE OF THE HOL ES. RT WING FUEL TANK ACCESS PANEL 640RB FOUND TO BE OUT OF LIMITS, RECEIVED NEW PART D5725662400000 BTCH 0004033270 IAW SRM 57-27-1 1-283-002 APPLIED TOP COAT SURFACE PROTECTION IAW SRM 51-75-12
- [SDR CALA2022121403388](https://openairdocs.org/sdr/CALA2022121403388.md): Floorbeam · corroded · Dec 12, 2022 · N487UA · Airbus A320232 · Fuselage Main, Floor Beam
  > FLOOR SUPPORT -Y765 FR66-FR70 CORRODED AT 4 LOCATIONS. EVALUATED FOR DAMAGE AND FOOUND OUT LIMIT IAW 53-00-14-283-002 R EMOVED FLOOR BEAM AND REPLACED NEW FLOOR BEAM IAW SRM 51-42-11/0 01. EMP: V940360 WC: 41198 STA: ST ENG BFM
- [SDR CALA2022121403387](https://openairdocs.org/sdr/CALA2022121403387.md): Seat Track · corroded · Dec 12, 2022 · N487UA · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN R/H I/B SEAT TRACK HAS CORROSION FROM FR20-22. REMOVED CORROSION IAW SRM 51-74-00 AND FOUND TO BE OUT OF LIMITS WC: 41112 STA: ST ENG BFM IAW SRM 53-11-15-283-010, MEASURE: D=0.065", L=1.200", W=0.300" REMOVED CABIN RH, INB SEAT TRACK FROM FR12 TO 22 IAW
- [SDR CALA2022120803342](https://openairdocs.org/sdr/CALA2022120803342.md): Floor Support · corroded · Dec 8, 2022 · N487UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT -Y765 FR66-FR70 CORRODED AT 4 LOCATIONS. EVALUATED FOR DAMAGE AND FOOUND OUT LIMIT IAW 53-00-14-283-002 R EMOVED FLOOR BEAM AND REPLACED NEW FLOOR BEAM IAW SRM 51-42-11/0 01.
- [SDR CALA2022120803341](https://openairdocs.org/sdr/CALA2022120803341.md): Floor Support · corroded · Dec 8, 2022 · N487UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > CABIN LAVATORY "D" ATTACHMENT POINT TO FLOOR SUPPORT ARE CORRODE D. EVALUATED FOR DAMAGE AND FOUND OUT LIMIT IAW SRM 53-00-14-283-00 2 REMOVED FLOOR BEAM AND REPLACED NEW FLOOR BEAM I.AW SRM 51-42- 11/001.
- [SDR CALA2022120803340](https://openairdocs.org/sdr/CALA2022120803340.md): Seat Track · corroded · Dec 8, 2022 · N487UA · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN R/H I/B SEAT TRACK HAS CORROSION FROM FR20-22. REMOVED CORROSION IAW SRM 51-74-00 AND FOUND TO BE OUT OF LIMITS WC: 41112 STA: ST ENG BFM IAW SRM 53-11-15-283-010, MEASURE: D=0.065", L=1.200", W=0.300" REMOVED CABIN RH, INB SEAT TRACK FROM FR12 TO 22 IAW
- [SDR CALA2022120803339](https://openairdocs.org/sdr/CALA2022120803339.md): Web · corroded · Dec 8, 2022 · N487UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > FWD CABIN WEB AT -Y1732 CORRODED AT FR20. FWD CABIN WEB AT -Y1732 REMOVED AND REPLACED IAW SRM 51-42-11/00 1 AND APPLIED TOPCOAT IAW SRM 51-23-11. EMP: V934614 WC: 41297 S TA: ST ENG BFM
- [SDR CALA2022120803338](https://openairdocs.org/sdr/CALA2022120803338.md): Floor Support · corroded · Dec 8, 2022 · N487UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT Y515 FR64 TO FR67 CORRODED AT 2 LOCATIONS REMOVED/REPLACED FLOOR SUPPORT Y515 FR64 TO FR67 P/N D5347209400 800 BTCH 0003809500 IAW SRM 51-72-11-911-001. EMP: V934337 WC: 4 1167 STA: ST ENG BFM
- [SDR CALA2022120803337](https://openairdocs.org/sdr/CALA2022120803337.md): Floor Support · corroded · Dec 8, 2022 · N487UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT Y515 FR68 TO FR70 CORRODED AT 2 LOCATIONS REMOVED/REPLACED SUPPORT Y515 FR68 TO FR70 P/N D5347209400400 BT CH 0003912854 IAW SRM 51-72-11-911-001. EMP: V934337 WC: 41168 S TA: ST ENG BFM
- [SDR CALA2022112803235](https://openairdocs.org/sdr/CALA2022112803235.md): Plate · corroded · Nov 25, 2022 · N487UA · Airbus A320232 · Fuselage Main, Structure
  > SHEAR PLATE RH SIDE FR69 TO FR70 -Y1732 HAS CORROSION UNDERNEATH
- [SDR CALA2022112803236](https://openairdocs.org/sdr/CALA2022112803236.md): Shear Plate · corroded · Nov 25, 2022 · N487UA · Airbus A320232 · Fuselage Main, Structure
  > SHEAR PLATE LH SIDE FR69 TO FR70 Y1732 HAS CORROSION UNDERNEATH
- [SDR CALA2020021200406](https://openairdocs.org/sdr/CALA2020021200406.md): Antenna · malfunctioned · Feb 10, 2020 · N487UA · Airbus A320232 · Weather Radar System
  > WEATHER RADAR SYSTEM INOP - NAV WX RADAR DOES NOT DISPLAY TILT OR ANY RETURNS AND THERE IS A THU MP FROM NOSE WITH RDR ON. COMPLIED WITH MEL DISPATCH DESK: 33 DATE: 07-FEB-19- APPROVED FOR MEL 3441A COMPLIED WITH MEL ON WXR BITE TEST GOT NO DISPLAY PATTERNS NO

Next page: https://openairdocs.org/aircraft/N487UA/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 = 'N487UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N487UA/reports

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