# Service difficulty reports: N447UA

A list on [N447UA](https://openairdocs.org/aircraft/N447UA.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 · 110 reports

- [SDR CALA2026041715430](https://openairdocs.org/sdr/CALA2026041715430.md): Apu · oil consumption · Apr 14, 2026 · N447UA · Airbus A320232 · APU Oil System
  > LEVEL TWO CHRONIC, APU LOW OIL MESSAGE. INDICATION SYS HAS BEEN CONFIRMED TO BE OPERATING CORRECTLY. CURRENTLY APU IS CONSUMING ONE QUART EVERY 8 HOURS. REF TSM 49-00-00-810-979-A AND AMM 49-00-00-810-979. CHECK FOR LEAKS FROM APU DRAINS SUCH AS FUEL CONTOL, A
- [SDR CALA2026021313768](https://openairdocs.org/sdr/CALA2026021313768.md): Proximity Sensor · damaged · Feb 11, 2026 · N447UA · Airbus A320232 · Emergency Equipment
  > FOUND BOTH LT FWD & AFT PROX DETECTOR ASSY ACTUATING RODS BENT IAW AMM 25-62-43. REMOVED LT FWD & AFT PROX SWITCHES, REMOVED RELEASE MECHANISM ASSEMBLIES. INSTALLED NEW ASSEMBLIES IAW AMM 52-73-11. LT FWD & AFT EMERGENCY EXIT DOORS REMOVED. COMPLETED LT FW
- [SDR CALA2026021213743](https://openairdocs.org/sdr/CALA2026021213743.md): Release Mech · damaged · Feb 11, 2026 · N447UA · Airbus A320232 · Escape Slide
  > FOUND BOTH LEFT FWD, & AFT EMERGENCY OVERWING EXITS SLIDE RELEASE MECHANISMS DAMAGED IAW AMM 52-21-11. R & R BOTH LT FWD AND AFT EMERGENCY OVERWING EXITS SLIDE RELEASE MECHANISMS IAW AMM 52-21-11.
- [SDR CALA2026021213744](https://openairdocs.org/sdr/CALA2026021213744.md): Flap · out of adjust · Feb 10, 2026 · N447UA · Airbus A320232 · Passenger/Crew Doors
  > DOOR L AFT EMER EXIT ECAM. ADJUSTED LEFT AFT OVERWING EXIT COVER FLAP, ECAM INDICATION NO LONGER REMAINS REF AMM 25-23-47.
- [SDR CALA2026021113695](https://openairdocs.org/sdr/CALA2026021113695.md): Cover Plate · cracked · Feb 10, 2026 · N447UA · Airbus A320232 · Passenger/Crew Doors
  > L1 DOOR UPPER PLATE APPEARS TO HAVE A CRACK ALONG THE AFT EDGE. REMOVED AND REPLACED L1 DOOR UPPER COVER PLATE IAW A320 SRM 51- 72-11-911-001.
- [SDR CALA2026021013656](https://openairdocs.org/sdr/CALA2026021013656.md): Channel · corroded · Feb 7, 2026 · N447UA · Airbus A320232 · Ailerons
  > RT WING, AILERON UPPER SURFACE T/E CORRODED APROX 30 INCHES OTBD OF INNER EDGE. REMOVED AND REPLACED THE RT WING AILERON T/E CHANNEL IAW SRM 51-42-11, & DWG 576-40033, REV R.
- [SDR CALA2026021113689](https://openairdocs.org/sdr/CALA2026021113689.md): Profile · cracked · Jan 21, 2026 · N447UA · Airbus A320232 · Emergency Exits
  > L/H AFT EMERGENCY EXIT HATCH CRACKED AROUND FASTENERS AT RT LOAD TRANSMITTING PROFILE. REMOVED AND REPLACED LT AFT EMERGENCY EXIT HATCH RT LOAD TRANSMITTING PROFILE ANGLE SEGMENT IAW SRM 51-72-11-911-001.
- [SDR CALA2026021113688](https://openairdocs.org/sdr/CALA2026021113688.md): Profile · cracked · Jan 20, 2026 · N447UA · Airbus A320232 · Emergency Exits
  > LEFT AFT EMERGENCY EXIT HATCH HAS CRACKS AROUND FASTENERS AT LT LOAD TRANSMITTIN PROFILE GEN BY V919150 ON AAR LCQ NR 9294316/443. REMOVED AND REPLACED LT AFT EMERGENCY EXIT HATCH LT LOAD TRANSM ITTING PROFILE ANGLE SEGMENT IAW SRM 51-72-11-911-001.
- [SDR CALA2025112811571](https://openairdocs.org/sdr/CALA2025112811571.md): Fuel Cap · missing · Nov 24, 2025 · N447UA · Airbus A320232 · Fuel Storage
  > FUELERS REPORT, FUEL CAP MISSING. MEL COMPLIED WITH.
- [SDR CALA2025081307670](https://openairdocs.org/sdr/CALA2025081307670.md): Slide · no discrepancy · Aug 10, 2025 · N447UA · Airbus A320232 · Escape Slide
  > DOOR 2L SLIDE PRESSURE SLIDE PRESSURE READING HIGH. VERIFIED 3L SLIDE PRESSURE IN THE GREEN, OK FOR SVC.
- [SDR CALA2024122201613](https://openairdocs.org/sdr/CALA2024122201613.md): Unknown · odor · Dec 20, 2024 · N447UA · Airbus A320232 · Air Distribution System
  > DIRTY SOCK SMELL INCABIN AND COCKPIT ATLOW POWER SETTINGS BELOW 1 8000 FT RAN PACKS FOR 20MINUTES, NO ODORS DETECTED AT THIS TIME. REF AMM TASK 49-00-00-860-005-A, REF AMM 21-00-00
- [SDR CALA2024053001629](https://openairdocs.org/sdr/CALA2024053001629.md): Light · malfunctioned · May 27, 2024 · N447UA · Airbus A320232 · Exterior Lighting
  > RWY TURNOFF LT WILL NOT TURN OFF CALLERED W5 AND W6 CB''S PER WD 33-43-01. CB''S DO NO EFFECT ANY COMPLIED WITH MEL. OTHER SYSTEMS. TOMC APPROVES MEL 3340N. CYCLED RUNWAY TURNOFF LIGHTS C/B. NO CHANGE. LIGHTS CONTINUE TO REMAIN ILLUMINATED WHEN SWITCH IS IN OF
- [SDR CALA2024042901254](https://openairdocs.org/sdr/CALA2024042901254.md): Lamp · missing · Apr 28, 2024 · N447UA · Airbus A320232 · Exterior Lighting
  > PDA 2 AIRCRAFT ARRIVED AND TECH DISCOVERED RH RETRACTABLE LANDING LIGHT AND RETAINING RING MISSING. ITEM IS CLASS 2 PDA AND LAMP WEIGHT IS 2.0LBS. SDR REPORT # 1035963 SUBMITTED. TOMC MX CNTL HILL. FOND RH LANDING LIGHT MISSING. THE WIRE EXPOSED. TOMC NOTIFIED
- [SDR CALA2023072402311](https://openairdocs.org/sdr/CALA2023072402311.md): Landing Light · missing · Jul 21, 2023 · N447UA · Airbus A320232 · Exterior Lighting
  > RIGHT LANDING LIGHT MISSING. PLACING RH WING TAXI LIGHT ON CDL 33G. PLACING RH WING TAXI LIGHT ON CDL 33G. PULLED AND INSTALLED SAFTIES ON LT/R/CTL AND LT/R/SPLY CIRCUIT BREAKERS, SECURED WIRES AND SPEED TAPED OPENING. REF LP 5231100 FOR SPEED TAPE REINSPECTIO
- [SDR CALA2023031000682](https://openairdocs.org/sdr/CALA2023031000682.md): Flange · cracked · Mar 10, 2023 · N447UA · Airbus A320232 · Fuselage Main, Frame
  > ORIGINAL LOP PAGE CLOSED IN ERROR: R/H FR68 STGR22 INNER CAP WEB FLANGE HAS A CRACK INDICATION "CONTACT ENGINEERING FOR REPAIR INSTRUCTIONS BEFORE NEXT FLIGHT" AD RELATED (AD 2022-15-05) PER HAECO LCQ NR 9292565/40565 GENERATED BY V061632. REFERENCE ORIGINAL
- [SDR CALA2023031000681](https://openairdocs.org/sdr/CALA2023031000681.md): Frame · none · Mar 10, 2023 · N447UA · Airbus A320232 · Fuselage Main, Frame
  > AREA REQUIRES INITIAL INSPECTION ON FRAME REPAIR AT R/H FR68, STR22RH PER PART 2B OF THE LATEST REVISION OF ECRA5341-01371 ON OR BEFORE AIRCRAFT REACHES 79200 TOTAL FLIGHT CYCLES. OR BEFORE AIRCRAFT REACHES 79200 TOTAL FLIGHT CYCLES. INSPECTION THRESHOLD. METH
- [SDR CALA2023031000689](https://openairdocs.org/sdr/CALA2023031000689.md): Fitting · cracked · Mar 9, 2023 · N447UA · Airbus A320232 · Fuselage Structure (General)
  > ORIGINAL LOP PAGE CLOSED IN ERROR: R/H FR68 STGR22 INNER CAP WEB FLANGE HAS A CRACK INDICATION "CONTACT ENGINEERING FOR REPAIR INSTRUCTIONS BEFORE NEXT FLIGHT" AD RELATED (AD 2022-15-05) PER HAECO LCQ NR 9292565/40565 GENERATED BY V061632. REFERENCE ORIGINAL
- [SDR CALA2023030600630](https://openairdocs.org/sdr/CALA2023030600630.md): Frame · corroded · Mar 4, 2023 · N447UA · Airbus A320232 · Doors
  > RH FWD EMERGENCY EXIT DOOR LOWER FRAME CORROSION PER HAECO LCQ N R 9292717/40717 GENERATED BY V798788 REMOVED AND REPLACED DOOR FRAME AND EDGE CURVE ON R/H FWD EMERGE NCY EXIT DOOR IAW A320 SRM 51-72-11-911-001 & SRM 51-42-11-001 B Y MECH V061737 INSP V079881
- [SDR CALA2023030300617](https://openairdocs.org/sdr/CALA2023030300617.md): Frame · corroded · Mar 2, 2023 · N447UA · Airbus A320232 · Standard Practices/Structures
  > RH AFT EMERGENCY EXIT DOOR LOWER FRAME CORROSION PER HAECO LCQ N ON ROUTINE 9292719/40719 GENERATED BY V798788 REMOVED AND REPLACED DOOR FRAME AND CURVE EDGE ON R/H EMERGENCY EXIT DOOR I/A/W A320 SRM 51-72-11-911-001 PER MECH V075620
- [SDR CALA2023030300614](https://openairdocs.org/sdr/CALA2023030300614.md): Fitting · cracked · Mar 1, 2023 · N447UA · Airbus A320232 · Fuselage Main, Frame
  > L/H FR68 STGR22 FRAME WEB FLANGE HAS A CRACK INDICATION AD RELATED (AD 2022-15-05) PER HAECO LCQ NON ROUTINE 9292564/40564 GENER ATED BY V061632 REVISION OF ECRA 5341-01372 ON OR BEFORE THE AIRCRAFT REACHES NOT TO EXCEED INTERVALS OF 3900 FLIGHT CYCLES THEREAF
- [SDR CALA2023022400535](https://openairdocs.org/sdr/CALA2023022400535.md): None · none · Feb 23, 2023 · N447UA · Airbus A320232 · Fuselage Structure (General)
  > FWD CARGO PIT L/H BETWEEN FR29-32 STRINGER 42L HAS CORROSION ARO UND FASTENERS AND SPLICE A3NB-53-3-6105 PER HAECO LCQ NON ROUTIN E 9292709/40709 GENERATED BY V919150 REMOVED AND REPLACED SPLICE IN FWD CARGO FR 29-32-STR 42LEFT IAW A320 SRM 51-72-11-911-001 PE
- [SDR CALA2023022400534](https://openairdocs.org/sdr/CALA2023022400534.md): Stringer · corroded · Feb 23, 2023 · N447UA · Airbus A320232 · Fuselage Structure (General)
  > AFT R2 PAX DOOR SILL FASTENER HOLES CORRODED I/B OF FRAME 68 AND 66 A3NB-53-3-6299 PER HAECO LCQ NON ROUTINE 9292592/40592 GENER ATED BY V937268 REMOVED AND REPLACED R3 DOOR SILL IAW A320 SRM 51-42-11-001 AND AIRBUS DWG D53480019007 PERFORMED BY V061616
- [SDR CALA2023022400533](https://openairdocs.org/sdr/CALA2023022400533.md): None · corroded · Feb 23, 2023 · N447UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > FWD CARO PIT R/H FR29 BETWEEN STRINGERS 41R-42R HAS CORROSION O N CLEAT (A3NB-53-3-6105) GENERATED AT HAECO LCQ BY V919150 PER N R 9292693 (40693) REMOVED AND REPLACED CLEAR CLEAT IN FWD CARGO PIT FR29 RT AT STR 41R-42R IAW A320 SRM 51-72-11-911-001 PERFORMED
- [SDR CALA2023022200511](https://openairdocs.org/sdr/CALA2023022200511.md): None · corroded · Feb 21, 2023 · N447UA · Airbus A320232 · Standard Practices/Structures
  > FWD CARGO PIT R/H BETWEEN FR28-32 STRINGER 41R HAS CORROSION AT SPLICE AND AROUND FASTENERS A3NB-53-3-6105 PER HAECO LCQ NON ROU TINE 9292699/40699 GENERATED PER V919150 REMOVED AND REPLACED DISPART PULIKE AT R/H FR28-32-51-41R IAW A3 20 SRM 51-72-11-911-001 P
- [SDR CALA2023022200510](https://openairdocs.org/sdr/CALA2023022200510.md): None · corroded · Feb 21, 2023 · N447UA · Airbus A320232 · Standard Practices/Structures
  > FWD CARGO PIT L/H BETWEEN FR28-32 STRINGER 41L HAS CORROSION ARO UND FASTENERS AND SPLICE A3NB-53-3-6105 PER HAECO LCQ NON ROUTIN E 92992711/40711 GENERATED BY V919150 REMOVED AND REPLACED DISCREPANT FWD CARGO PROFILE AT L/H FR28-32 STR41 IAW A320 SRM 57-72-91
- [SDR CALA2023022200509](https://openairdocs.org/sdr/CALA2023022200509.md): None · corroded · Feb 21, 2023 · N447UA · Airbus A320232 · Standard Practices/Structures
  > FWD CARGO PIT L/H BETWEEN FR28-32 STRINGER 43L HAS CORROSION ARO UND FASTENERS AND SPLICE A3NB-53-3-610 PER HAECO LCQ NON ROUTINE 9292708/40708 GENERATED BY V919150 REMOVED AND REPLACED DISCREPANT FWD CARGO PROFILE AT L/H FR28-32 STR43L IAW A320 SRM 51-72-11-9
- [SDR CALA2023022000493](https://openairdocs.org/sdr/CALA2023022000493.md): None · corroded · Feb 19, 2023 · N447UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > FWD CARGO PIT R/H FR28 BETWEEN STRINGERS 41R-42R HAS CORROSION O N CLEAT A3NB-53-3-6105 PER HAECO LCQ NON ROUTINE 9292691/40691 G ENERATED BY V919150
- [SDR CALA2023022000492](https://openairdocs.org/sdr/CALA2023022000492.md): None · corroded · Feb 19, 2023 · N447UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > FWD CARGO PIT R/H FR30 BETWEEN STRINGERS 40R-41R HAS CORROSION O N CLEAT A3NB-53-3-6105 PER HAECO LCQ NON ROUTINE 9292695/40695 G ENERATED BY V919150
- [SDR CALA2023022000491](https://openairdocs.org/sdr/CALA2023022000491.md): None · corroded · Feb 19, 2023 · N447UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > FWD CARGO PIT R/H FR32 BETWEEN STRINGERS 40R-41R HAS CORROSION O N CLEAT PER HAECO LCQ NON ROUTINE 9292696/40696 GENERATED BY V91 9150
- [SDR CALA2023022000490](https://openairdocs.org/sdr/CALA2023022000490.md): None · corroded · Feb 19, 2023 · N447UA · Airbus A320232 · Fuselage Structure (General)
  > FWD CARGO FR33 BETWEEN STGR 40R & 41R, 1EA CLEAT (FRONT & BACK) SHOWS CORROSION PER HAECO LCQ NON ROUTINE 9292532/40532 GENERATE D BY V940824 REMOVED AND REPLACED CLEAT AT FWD CARGO COMPARTMENT FR33 BETWEEN STRG40R AND STRG41R IAW A320 SRM 51-72-11-911-001 AND
- [SDR CALA2023022000489](https://openairdocs.org/sdr/CALA2023022000489.md): None · corroded · Feb 19, 2023 · N447UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > FWD CARGO PIT R/H FR29 BETWEEN STRINGERS 42R-43R HAS CORROSION O N CLEAT A3NB-53-3-6105 PER HAECO LCQ NON ROUTINE 9292694/40694 G ENERATED BY V919150 REMOVED AND REPLACED CLEAT AT FWD CARGO PIT R/H FR29 BETWEEN STR G42R AND STRG43R IAW A320 SRM 51-72-11-911-00
- [SDR CALA2023022000488](https://openairdocs.org/sdr/CALA2023022000488.md): Cleat · corroded · Feb 19, 2023 · N447UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > FWD CARGO PIT R/H FR28 BETWEEN STRINGERS 42R-43R HAS CORROSION O N CLEAT A3NB-53-3-6105 PER HAECO LCQ NON ROUTINE 9292690/40690 G ENERATED BY V919150 REMOVED AND REPLACED CLEAT AT FWD CARGO PIT R/H FR28 BETWEEN STR 42R AND STRG 43R IAW A320 SRM 51-72-11-911-00
- [SDR CALA2023022000486](https://openairdocs.org/sdr/CALA2023022000486.md): Angle · cracked · Feb 19, 2023 · N447UA · Airbus A320232 · Wing Structure
  > RH HYD. COMP. BAY AFT I/B VERTICAL ANGLE SUPPORT CRACK LOWER ATT ACH FASTENER. A3NB-57-4-6554. PER HAECO LCQ NON ROUTINE 9292150/ 40150 GENERATED BY V061628
- [SDR CALA2023022000477](https://openairdocs.org/sdr/CALA2023022000477.md): None · corroded · Feb 17, 2023 · N447UA · Airbus A320232 · Fuselage Structure (General)
  > R.H. FWD. ENTRY DOOR R-1 CUTOUT FR.16-20 STGR 22-23 HAS CORROSIO N AT MULTIPLE LOCATIONS (A3NB-53-3-6298) GENERATED AT HAECO LCQ BY V921658 PER NR 9292736(40736) REPAIRED RH AND FWD ENTRY DOOR CUT OUT FR16-20, STRG 22-23 IAW A AND METLANDS TBD PERFORMED BY V06
- [SDR CALA2023022000476](https://openairdocs.org/sdr/CALA2023022000476.md): Fitting · corroded · Feb 17, 2023 · N447UA · Airbus A320232 · Flight Compartment Equipment
  > AFT WET AREA CORROSION WEB FITTING RH BETWEEN FR 69-70 A3NB-53-3 -6279 GENERATED AT HAECO LCQ BY V926223 PER NR 9292676(40676) REMOVED AND REPLACE DISCREPANT AFT WET AREA RH SHEAR WEB IAW A32 0 DWG 53471124 AND SRM 51-42-71-001 PER MECH V061616 INSP V06162 9
- [SDR CALA2023022000475](https://openairdocs.org/sdr/CALA2023022000475.md): None · corroded · Feb 17, 2023 · N447UA · Airbus A320232 · Standard Practices/Structures
  > FWD CARGO PIT FR28 BETWEEN STRINGERS 43L-44 CORROSION ON CLEAT D OT MO64 A3NB-53-3-6105 GENERATED AT HAECO LCQ BY V919150 PER NR 9292684(40684) REMOVED AND REPLACED FWD CARGO PIT CLEAT AT FR28 STR43L-44 IAW A 320 SRM 51-42-11-001 PER MECH V061616 INSP V061629
- [SDR CALA2023022000474](https://openairdocs.org/sdr/CALA2023022000474.md): Torsion Box · corroded · Feb 17, 2023 · N447UA · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > FWD CARGO PIT TORSION BOX HAS SPOTS OF CORROSION ON UPPER SURFAC E DOT M062 A3NB-53-3-6330 GENERATED AT HAECO LCQ BY V929150 PER NR 9292559(40559) REMOVED AND REPLACED TORSION BOX PLATE FRONT FR24 TO FR28 IAW SR M 51-42-11-001 BY MECH V932196 INSP BY V927281
- [SDR CALA2023022000473](https://openairdocs.org/sdr/CALA2023022000473.md): None · corroded · Feb 17, 2023 · N447UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > FWD CARGO PIT R/H FR29 BETWEEN STRINGERS 40R-41R HAS CORROSION O N CLEAT DOT M069 A3NB-53-3-6105 GENERATED AT HAECO LCQ BY V91915 0 PER NR 9292692(40692) REMOVED AND REPLACED DISCREPANT FWD CARGO CLEAT AT R/H FR29 STR 40R-41R IAW A320 SRM 51-72-11-911-002 BY M
- [SDR CALA2023022000472](https://openairdocs.org/sdr/CALA2023022000472.md): Shear Plate · corroded · Feb 17, 2023 · N447UA · Airbus A320232 · Standard Practices/Structures
  > AFT WET AREA SHEAR PLATE AT FR70 OUTER SKIN TIE HAS CORROSION A3 NB-53-3-6279 GENERATED AT HAECO LCQ BY V926223 PER NR 9292673 (4 0673) REMOVED AND REPLACED DISCREPANT L/H AFT SHEAR WEB FR69-70 IAW A3 20 DWG 5387124 AND SRM 51-4271-001 PER MECH V061616 INSP V0
- [SDR CALA2023022000478](https://openairdocs.org/sdr/CALA2023022000478.md): Door Sill · corroded · Feb 17, 2023 · N447UA · Airbus A320232 · Fuselage Structure (General)
  > AFT L2 PAX DOOR SILL CORRODED I/B OF FR68 PER HAECO LCQ N/R 9292 593/40593 GEN BY V937268 REMOVED AND REPLACED DISCREPANT L2 PAX DOOR SILD IAW A320 SRM 51 -42-11-001 PERFORMED BY V061616
- [SDR CALA2023020600338](https://openairdocs.org/sdr/CALA2023020600338.md): Web · cracked · Feb 5, 2023 · N447UA · Airbus A320232 · Doors
  > RH FWD EMERGENCY EXIT DOOR FWD AND AFT WEB SUPPORT CRACKED PER H AECO N/R 9292715/40715 GEN BY V798788 RMVD AND RPLD 2EA WEB SUPPORTS ON R/H EMERGENCY EXIT DOOR IAW A3 20 SRM 51-72-11-911-001 BY MECH V061616 INSP BY V921658
- [SDR CALA2023020100279](https://openairdocs.org/sdr/CALA2023020100279.md): Rib · none · Jan 30, 2023 · N447UA · Airbus A320232 · Doors
  > RH AFT EMERGENCY EXIT DOOR FWD AND AFT WEB SUPPORT SIGNS OF CRACKED SUPPORT TASK GENERATED AT HAECO LCQ PER V798788 PER NR 92927 16 (40716) REMOVED AND REPLACED 2EA WEB SUPPORTS ON RH AFT EMER. EXIT DOORS IWA A320 SRM 51-72-11-911-001. PERFORMED BY V061737.
- [SDR CALA2022101802849](https://openairdocs.org/sdr/CALA2022101802849.md): Radar · faulty · Oct 18, 2022 · N447UA · Airbus A320232 · Doppler System
  > WEATHER RADAR SYSTEM INOP - NAV CTL PNL(3SQ)/WXR 1(1SQ1), 34-41-12.SEE TASK 34-41-00-810-812-A FOR TROUBLESHOOTING. CONTACT TOMC TO UNLOCK. UNLOCKED FOR UPDATE. SPOKE WITH RHE INBD CREW, THEY SAID AFTER HITTING A BUMP OVER OCEAN THEY GOT RED "WR CTL" MSG ON TH
- [SDR CALA2022042501066](https://openairdocs.org/sdr/CALA2022042501066.md): Fuel Cap · missing · Apr 25, 2022 · N447UA · Airbus A320232 · Aircraft Fuel System
  > PDA 1 FUEL CAP MISSING ON ARRIVAL PVR. OPBLM CHRISTIANSEN NO DAMAGE ON AIRCRAFT, ENTERED INTO CDL 28A REF LP 8432322. OPBLM CHRISTIANSEN
- [SDR CALA2020032000616](https://openairdocs.org/sdr/CALA2020032000616.md): Pressure Panel · cracked · Mar 9, 2020 · N447UA · Airbus A320232 · Fuselage Main, Structure
  > WHILE PERFORMING EA 5330-05216 REV A FOUND SEVERAL HOLES CRACKED AT FR 36 RHS ON THE PRESSURE PANEL. HOLES THAT WERE CRACKED #6,7,9,12,39&57 SEE ECRA 5331-02636 FOR HOLE NUMBERING ACCOMPLISHED PART 1 OF ECRA 5331-02636 INTERIM REPAIR PLACED ON DIP PER PART 1C
- [SDR CALA2018041801185](https://openairdocs.org/sdr/CALA2018041801185.md): Stringer · damaged · Apr 16, 2018 · N447UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > FWD CARGO STRINGER 42R, FRAME 32 HOLE REQUIRES OVERSIZE FASTENER. REPAIRED THE STRINGER IAW SRM 53-00-11-300-022, FIG 21026.
- [SDR CALA2017121104398](https://openairdocs.org/sdr/CALA2017121104398.md): Battery · failed · Dec 11, 2017 · N447UA · Airbus A320232 · Emergency Lighting
  > RIGHT SIDE EMERGENCY BATTERY FAILED EMERGENCY SYSTEM OP CHECK. REPLACED RH BATTERY,EMERGENCY LIGHT SYSTEM PASSED CIDS SYSTEM CHECK.
- [SDR CALA2017072402346](https://openairdocs.org/sdr/CALA2017072402346.md): Engine · vibration · Jul 24, 2017 · N447UA · Airbus A320232 · Engine (Turbine/Turboprop)
  > NR 1 ENGINE HIGH N1 VIBRATION UP TO 8.0. VARIED WITH THRUST AND PRODUCED NOTICEABLE ODOR. ACCOMPLISHED AN INSPECTION OF THE ENGINE, TOOK THE AIRPLANE OUT FOR A VIBRATION SURVEY. ALL CHECKED GOOD. CHANGED THE EVMU FOR PRECATIONARY IAW AMM 77-32-34
- [SDR CALA2017052601599](https://openairdocs.org/sdr/CALA2017052601599.md): Battery · no test · May 26, 2017 · N447UA · Airbus A320232 · Emergency Lighting
  > DURING AN EMERGENCY LIGHT CHECK, THE EPSU BATTERY AFT LT FAULTED. REPLACED THE EPSU BATTERY IAW MM 33-51-38. OPS CHECKED GOOD.
- [SDR CALA2017051501442](https://openairdocs.org/sdr/CALA2017051501442.md): Slide · low pressure · May 15, 2017 · N447UA · Airbus A320232 · Escape Slide
  > RT AFT ESCAPE SLIDE GAUGE IS IN THE RED. REPLACED R2 DOOR SLIDE PER AMM 25-62-44.

Next page: https://openairdocs.org/aircraft/N447UA/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 = 'N447UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N447UA/reports

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