# Service difficulty reports: N943FR

A list on [N943FR](https://openairdocs.org/aircraft/N943FR.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR F3LA2021041500032](https://openairdocs.org/sdr/F3LA2021041500032.md): Megaphone · inoperative · Apr 15, 2021 · N943FR · Airbus A319112 · Emergency Equipment
  > DISCREPANCY, LP1239913 ITEM 2: AFT BULL HORN INOP. CORRECTIVE ACTION: REMOVED AND REPLACED AFT MEGAPHONE, OPS TEST GOOD. REF AMM 25-65--51-710-002-A. NOTE 1) THIS WAS FOUND DURING PRE BOARDING FOR FLIGHT 383. NOTE 2) TIME SINCE INSPECTION, IS THE LAST TIME TH
- [SDR F3LA2021041500031](https://openairdocs.org/sdr/F3LA2021041500031.md): Megaphone · inoperative · Apr 15, 2021 · N943FR · Airbus A319112 · Emergency Equipment
  > DISCREPANCY, LP1239913 ITEM 1: FWD BULL HORN INOP. CORRECTIVE ACTION: REMOVED AND REPLACED FWD MEGA PHONE BATTERIES, OPS TEST GOOD. REF AMM 25-65-51-970-001-A. NOTE 1 THIS WAS FOUND DURING PRE BOARDING FOR FLIGHT 383. NOTE 2 TIME SINCE INSPECTION, IS THE LAS
- [SDR F3LA2021012800005](https://openairdocs.org/sdr/F3LA2021012800005.md): Battery · failed · Jan 28, 2021 · N943FR · Airbus A319112 · Emergency Lighting
  > EPSU BATTERY FAILED REMOVED AND REPLACED EPSU EMERGENCY POWER SUPPLY UNIT. OPERATIONS CHECK OK, IAW AMM 33-51-38-400-001-A.
- [SDR F3LA2020021850011](https://openairdocs.org/sdr/F3LA2020021850011.md): Tip Cap · damaged · Feb 15, 2020 · N943FR · Airbus A319112 · Wing, Plate/Skin
  > 03/05/2020 SUPPLEMENT: REMOVED DAMAGED R/H WING TIP AND INSTALLED SERVICEABLE R/H WINGTIP IAW AMM 57-31-21-PB401. REMOVED PN D5735052101951A, SN 13572. REMOVED AND REPLACED R/H WINGTIP FENCH IAW AMM 57-31-22-PB401, PN D5735120000300A. SIGNIFICANT DAMAGE TO RH
- [SDR F3LA2020012390003](https://openairdocs.org/sdr/F3LA2020012390003.md): Fitting · cracked · Jan 9, 2020 · N943FR · Airbus A319112 · Fuselage Main, Structure
  > LOWER AFT FASTENER HOLE ON L/H FRAME 16 UPPER DOUBLE JOGGLE SHOWS CRACK INDICATIONS. REPAIRED L1 DOOR FRAME 16 UPPER DOUBLER JOGGLE HOLE 'D' IAW REPAIR DRAWING R53113041 (ISSUE E). REPAIR INSPECTION THRESHOLD 6800 FC WITH INTERVALS OF 4129 FC PER RDAS.
- [SDR F3LA201909200116](https://openairdocs.org/sdr/F3LA201909200116.md): Pipe · cracked · Sep 17, 2019 · N943FR · Airbus A319112 · Extinguishing System
  > DISCREPENCY: PIPE P/N D2621012400400, CRACKED FIRE BOTTLE DISCHARGE LINE, NUMBER 1 ENGINE PYLON. REFERENCE IPC 26-21-06-01D ITEM 310. CORRECTIVE ACTION: REMOVED AND REPLACED PIPE NUMBER 1 ENGINE FIRE BOTTLE TUBE. PERFORMED LEAK CHECK AMM 26-21-49-400-002-A.
- [SDR F3LA2018102900471](https://openairdocs.org/sdr/F3LA2018102900471.md): Generator · leaking · Oct 24, 2018 · N943FR · Airbus A319112 · AC Generator-Alternator
  > DISCREPANCY: REFERENCE LOG PAGE LP1090541 ITEM 1, IMMEDIATELY UPON TURNING ON APU BLEEN AND PACKS 1 AND 2, WE NOTICED AN OILY MUSTY SMELL ON FLIGHT DECK. ONE MINUTE LATER FLIGHT ATTENDANTS IN BACK CALLED TO INFORM US OF ODOR IN BACK OF AIRCRAFT, TRIED TO ISOLA
- [SDR F3LA2018062500359](https://openairdocs.org/sdr/F3LA2018062500359.md): Power Supply · failed · Jun 24, 2018 · N943FR · Airbus A319112 · Emergency Lighting
  > EPSU 10WL FAILED EPSU TEST. REMOVED AND REPLACED EPSU ASSEMBLY 10WL IAW AMM 33-51-38 PAGE BLOCK 401. OPERATIONAL CHECK GOOD.
- [SDR F3LA2018013100285](https://openairdocs.org/sdr/F3LA2018013100285.md): Floorbeam · corroded · Jan 25, 2018 · N943FR · Airbus A319112 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM -Y765 AT FRAME 66. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14-283-002. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-11, 51-72-11-911-001, AND 51-44-11.
- [SDR F3LA2018013100284](https://openairdocs.org/sdr/F3LA2018013100284.md): Floorbeam · corroded · Jan 23, 2018 · N943FR · Airbus A319112 · Fuselage Main, Floor Beam
  > 2 AREAS OF CORROSION ON FLOORBEAM -Y765 BETWEEN FR66 AND FR68. REMOVED AND REPLACED FLOORBEAM AT -Y765 BETWEEN FR66 AND FR68 IAW SRM 51-42-11, 53-00-14-283-002, 51-72-911-001 AND 51-44-11.
- [SDR F3LA2018013100282](https://openairdocs.org/sdr/F3LA2018013100282.md): Floorbeam · corroded · Jan 23, 2018 · N943FR · Airbus A319112 · Fuselage Main, Floor Beam
  > FLOORBEAM Y512 HAS CORROSION AT FR66. REFERENCE NR 1832N291, REMOVED AND REPLACED FLOORBEAM Y512 FR67-64 IAW SRM 51-72-11-911-001, 53-00-14-283-002 AND 51-44-11.
- [SDR F3LA2018012900283](https://openairdocs.org/sdr/F3LA2018012900283.md): Floorbeam · corroded · Jan 23, 2018 · N943FR · Airbus A319112 · Fuselage Main, Floor Beam
  > FLOORBEAM Y1292 HAS CORROSION AT FRAME 68. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14-283-002. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-72-11-911-001, 51-42-11, AND 51-44-11.
- [SDR F3LA2018012900281](https://openairdocs.org/sdr/F3LA2018012900281.md): Floor Support · corroded · Jan 23, 2018 · N943FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > THREE AREAS OF CORROSION ON THE FLOOR SUPPORT Y765 BETWEEN FRAMES 66 AND 68. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11, 51-72-11-911-001, 53-00-14-283-002, AND 51-44-11.
- [SDR F3LA2018012900280](https://openairdocs.org/sdr/F3LA2018012900280.md): Floorbeam · corroded · Jan 23, 2018 · N943FR · Airbus A319112 · Fuselage Main, Floor Beam
  > CORROSION ON THE FLOORBEAM Y1162, FRAME 68. THE FLOORBEAM WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14-283-002. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-72-11, 51-44-11, AND 51-72-11-911-001.
- [SDR F3LA2018012600279](https://openairdocs.org/sdr/F3LA2018012600279.md): Floorbeam · corroded · Jan 23, 2018 · N943FR · Airbus A319112 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM -Y1162 BY FRAME 68. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-72-11, SRM 53-00-14, AND SRM 51-44-11.
- [SDR F3LA2018012600278](https://openairdocs.org/sdr/F3LA2018012600278.md): Floorbeam · corroded · Jan 23, 2018 · N943FR · Airbus A319112 · Fuselage Main, Floor Beam
  > TWO AREAS OF CORROSION ON THE FLOORBEAM -Y1292 BY FRAME 66. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-72-11, SRM 53-00-14, AND SRM 51-44-11.
- [SDR F3LA2016020200002](https://openairdocs.org/sdr/F3LA2016020200002.md): Slide · failed · Jan 27, 2016 · N943FR · Airbus A319112 · Escape Slide
  > EMERGENCY POWER SUPPLY UNIT TEST FAILED FOR L1 DOOR SLIDE. R & R L1 DOOR SLIDE IAW AMM 25-62-44-000-012A & AMM 25-62-44-400-007A. OPERATIONAL CHECKED GOOD.
- [SDR F3LA2016011100001](https://openairdocs.org/sdr/F3LA2016011100001.md): Seal · damaged · Jan 6, 2016 · N943FR · Airbus A319112 · Turbine Engine Oil System
  > LOSS OF OIL QTY ON NR 2 ENG. QTY LESS THAN 2 PSI AT CRUISE. OIL PSI 0 ON APPROACH & LAND. OIL TEMP & PRESS WITH NR 2 ENG AT IDLE 28 PSI & 80 DEGREE C. TROUBLE SHOT, LEAK FOUND HYD PUMP PAD SEAL LEAKING. R & R SEAL ON THE HYD PUMP SHAFT IAW AMM 72-63-00-30
- [SDR F3LA2015122201156](https://openairdocs.org/sdr/F3LA2015122201156.md): Epsu · failed · Dec 19, 2015 · N943FR · Airbus A319112 · Emergency Lighting
  > EMERGENCY POWER SUPPLY UNIT SYS TEST FAILED, CODE 10WL FWD LT. R & R EPSU 10WL. OPERATIONS TESTED GOOD IAW AMM 33-51-38 PB 401. REFERENCE LP 967286.
- [SDR F3LA2015033001126](https://openairdocs.org/sdr/F3LA2015033001126.md): Battery · discharged · Mar 27, 2015 · N943FR · Airbus A319112 · Emergency Lighting
  > EMERGENCY PATH LIGHTING BATTERY OF EPSU 10WL FAILED TEST DURING HEAVY SERVICE CHECK. R & R BATTERY OF EPSU 10WL. OPERATIONS CHECKED GOOD IAW AMM 33-51-38-000-002 & 33-51-38-400-002 LP 925756.
- [SDR F3LA2018102900472](https://openairdocs.org/sdr/F3LA2018102900472.md): Apu · leaking · Oct 24, 2014 · N943FR · Airbus A319112 · APU Core Engine
  > DISCREPANCY: REFERENCE LOG PAGE LP1090541 ITEM 1, IMMEDIATELY UPON TURNING ON APU BLEEN AND PACKS 1 AND 2, WE NOTICED AN OILY MUSTY SMELL ON FLIGHT DECK. ONE MINUTE LATER FLIGHT ATTENDANTS IN BACK CALLED TO INFORM US OF ODOR IN BACK OF AIRCRAFT, TRIED TO ISOLA
- [SDR F3LA2014090201061](https://openairdocs.org/sdr/F3LA2014090201061.md): Floorbeam · corroded · Sep 1, 2014 · N943FR · Airbus A319112 · Fuselage Main, Floor Beam
  > AIRCRAFT DUE C 6 INSPECTION. DISCREPANCY, MAIN CABIN FLOORBEAM FRAME 68 Y1292 CORRODED TO 50% OF MATERIAL THICKNESS. R & R MAIN CABIN FLOORBEAM FRAME 68 Y1292 IAW SRM 51-42-11 PAR 5, 6 & 7 & SRM 51-49-00 TABLE 9. ACFT DUE OUT OF C CHECK SEPTEMBER 2, 2014.
- [SDR F3LA2014040101031](https://openairdocs.org/sdr/F3LA2014040101031.md): Windshield · cracked · Mar 28, 2014 · N943FR · Airbus A319112 · Flight Compartment Windows
  > WINDSHIELD CRACKED AT FL390, SEEMS TO BE OUTER PANE ONLY, NO FLUCTUATIONS IN PRESSURIZATION NOTED. R & R FIRST OFFICER`S WINDSHIELD IAW AMM 56-11-11-000-001 & AMM 56-11-11-400-001, OPERATIONS CHECKED GOOD. REPLACED WINDOW HEAT CONTROLLER SEE LOG PAGE 827954
- [SDR F3LA2012042300748](https://openairdocs.org/sdr/F3LA2012042300748.md): Computer · malfunctioned · Apr 20, 2012 · N943FR · Airbus A319112 · Central Warning
  > ECAM ON DESCENT: CIDS 1 AND 2 FAULT WITH UNCOMMANDED EMERGENCY LIGHTS FLICKERING CABIN LIGHTS LOSS OF CABIN COMMUNICATIONS. THIS WAS INTERMITTENT FOR ONLY A FEW MINUTES THEN WENT BACK TO NORMAL. TROUBLESHOT REPLACED CIDS DIRECTOR IAW AMM 23-73·34PB 401. OPS C
- [SDR F3LA2011122100695](https://openairdocs.org/sdr/F3LA2011122100695.md): Unknown · odor · Dec 19, 2011 · N943FR · Airbus A319112 · Air Distribution System
  > AT 4000 FT AGL, F/A REPORTED A BURNING ODOR COMING FROM THE AFT LT LAV. TROUBLESHOT IAW TSM 24-00-00-810-823. NO DEFECTS NOTED. INSPECTED THE FOLLOWING AREAS, LAVATORY HOT WATER HEATERS, COFFEEMAKERS IN AFT GALLEY INCLUDING WIRING, LIVE TV COMPONENTS WHILE
- [SDR F3LA2011052300651](https://openairdocs.org/sdr/F3LA2011052300651.md): Shear Plate · corroded · May 17, 2011 · N943FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > C-CHECK: NON ROUTINE NR 33802; LT SHEAR PLATE AT FRAME 69-70 HAS CORROSION ON THE UPPER SURFACE. REMOVED AND REPLACED AHEAR PLATE IAW EO A0-53EO-31434 AND SRM 51-42-11.
- [SDR F3LA2011052300650](https://openairdocs.org/sdr/F3LA2011052300650.md): Shear Plate · corroded · May 17, 2011 · N943FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > C-CHECK: NON ROUTINE NR 33801; RT SHEAR PLATE AT FRAME 69 - 70 HAS UPPER SURFACE CORROSION. REMOVED AND REPLACED SHEAR PLATE IAW EO A0-53EO-31-434 AND SRM 51-42-11.
- [SDR F3LA2011052300649](https://openairdocs.org/sdr/F3LA2011052300649.md): Sill · corroded · May 17, 2011 · N943FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > C-CHECK: MAIN CABIN FRAME 66 -Y1500, AFT PASSENGER DOOR SILL BEAM HAS SURFACE CORROSION. REPARED DOOR SILL BEAM IAW SRM 53-41-14, FIG 201.
- [SDR F3LA2011052300648](https://openairdocs.org/sdr/F3LA2011052300648.md): Floorbeam · corroded · May 17, 2011 · N943FR · Airbus A319112 · Fuselage Main, Floor Beam
  > C-CHECK: CABIN FLOORBEAM AT FRAME 68, Y1292 HAS CORROSION. REMOVED AND REPLACED FLOORBEAM IAW SRM 53-00-14, FIG 102 ALSO SRM 51-42-11, PARA 5.
- [SDR F3LA2011052300647](https://openairdocs.org/sdr/F3LA2011052300647.md): Floor Support · corroded · May 17, 2011 · N943FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > C-CHECK: NON ROUTINE NR 33820; CABIN FLOOR SUPPORT FRAME 67-69, -Y1292 HAS CORROSION. REMOVED AND REPLACED FLOORBEAM IAW SRM 53-00-14, FIG 102 ALSO SRM 51-42-11 PARA 5 A, D AND 6 B 1-8.
- [SDR F3LA2009111300227](https://openairdocs.org/sdr/F3LA2009111300227.md): Sill · corroded · Nov 7, 2009 · N943FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > REFERENCE NON ROUTINE C074186. DURING DEN C3 C-CHECK, INSPECTION NOTED CORROSION ON THE L2 DOOR SILL AT FRAME 66 IN FWD SPLICE AREA. MX PERFORMED MAJOR REPAIR IAW SRM 53-41-14, SRM 51-44-00, SRM 51-21-00 AND SRM 51-75-00.
- [SDR F3LA2009111600230](https://openairdocs.org/sdr/F3LA2009111600230.md): Floorbeam · corroded · Nov 6, 2009 · N943FR · Airbus A319112 · Fuselage Main, Floor Beam
  > DURING DEN C3 C-CHECK, INSP NOTED CORROSION ON THE FLOORBEAM Y1162.5 AT FRAME 68. MX REMOVED AND REPLACED THE FLOORBEAM IAW SRM 53-00-14, SRM 51-42-11, SRM 51-11-13, AND EA A9-53R-31489.
- [SDR F3LA2009111600229](https://openairdocs.org/sdr/F3LA2009111600229.md): Floor Support · corroded · Nov 6, 2009 · N943FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > DURING DEN C3 C-CHECK, INSP NOTED CORROSION ON THE FLOOR SUPPORT Y1292 BETWEEN FRAME 64 AND FRAME 66. MX REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 53-00-14, SRM 51-42-11, SRM 51-11-13, SRM 51-44-11 AND AMM 20-28-00 PB 501.
- [SDR F3LA2009111600228](https://openairdocs.org/sdr/F3LA2009111600228.md): Floor Support · corroded · Nov 6, 2009 · N943FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > REFERENCE NON ROUTINE C073981. DURING DEN C3 C-CHECK, INSP, NOTED CORROSION IN THE AFT CABIN AREA ON THE FLOOR SUPPORT Y1292 BETWEEN FRAME 66 AND FRAME 68. MX REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 53-00-14, SRM 51-42-11 AND SRM 51-44-11.
- [SDR F3LA2009111200226](https://openairdocs.org/sdr/F3LA2009111200226.md): Floorbeam · corroded · Nov 6, 2009 · N943FR · Airbus A319112 · Fuselage Main, Floor Beam
  > REFERENCE NON ROUTINE C073982. DURING DEN C3 C-CHECK, INSP NOTED CORROSION ON FLOORBEAM LOCATED AT -Y1292 BETWEEN FRAME 67 AND FRAME 68. MX REPAIRED THE FLOORBEAM IAW SRM 51-73-11, SRM 51-44-11 AND EA A9-53R-31491.
- [SDR F3LA2008123000732](https://openairdocs.org/sdr/F3LA2008123000732.md): Safety Valve · leaking · Dec 28, 2008 · N943FR · Airbus A319112 · Hydraulic System, Main
  > PILOT RETURNED TO BLOCK DUE TO LOSS OF GREEN SYSTEM HYDRAULIC PRESSURE. MAINTENANCE REMOVED AND REPLACED LANDING GEAR SAFETY VALVE AND PERFORMED OPERATIONAL CHECK IAW A319 AMM 32-31-17 PB401 AND 32-31-00-710-005.
- [SDR F3LA200800504](https://openairdocs.org/sdr/F3LA200800504.md): Hook · out of adjust · Jul 20, 2008 · N943FR · Airbus A319112 · Service Doors
  > DURING C-CHECK INSP, NOTED THE R2 DOOR INSIDE HANDLE CAN BE OPERATED WHILE DOOR IS NOT CLOSED. MAINT ADJUSTED THE R2 DOOR HOOK IAW AMM 52-11-21-400-001. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)
- [SDR F3LA200800503](https://openairdocs.org/sdr/F3LA200800503.md): Torsion Bar · out of adjust · Jul 20, 2008 · N943FR · Airbus A319112 · Service Doors
  > DURING C-CHECK, INSP NOTED THE R2 DOOR WOULD NOT ARM WITH DOOR CLOSED AND LOCKED. THIS OCCURRED DURING OPERATION OF THE DOOR WHILE PERFORMING TASK CARD C528002-2. MAINT ADJUSTED TORSION BAR AND PERFORMED OPS CHECK IAW AMM 52-11-21-400-001 AND TASK CARD C5280
- [SDR F3LA200800502](https://openairdocs.org/sdr/F3LA200800502.md): Floor Panel · delaminated · Jul 17, 2008 · N943FR · Airbus A319112 · Fuselage Floor Panel
  > DURING C2 C-CHECK, INSPECTION NOTED THE TOP LAYER DELAMINATED ON FLOOR PANEL 251NF. MAINTENANCE REMOVED DELAMINATED LAYER AND APPLIED MYLAR PATCH IN ACCORDANCE WITH A319 SRM 53-02-00.
- [SDR F3LA200800497](https://openairdocs.org/sdr/F3LA200800497.md): Floor Panel · punctured · Jul 15, 2008 · N943FR · Airbus A319112 · Fuselage Floor Panel
  > DURING C2 C CHECK, INSPECTION NOTED THE AFT PIT TRANSITION PANEL 161UG WAS PUNCTURED. MAINTENANCE RECORDED THAT THIS NON ROUTINE HAS THE PANEL NUMBER INCORRECTLY INDICATED. THE DAMAGED PANEL IS 151UG. MAINTENANCE REPAIRED DAMAGE TO PANEL 151UG IAW THE REQUI
- [SDR F3LA200800496](https://openairdocs.org/sdr/F3LA200800496.md): Floor Panel · punctured · Jul 15, 2008 · N943FR · Airbus A319112 · Fuselage Floor Panel
  > DURING C2 C CHECK, INSPECTION NOTED THE AFT PIT TRANSITION PANEL 151FE WAS PUNCTURED. MAINTENANCE REPAIRED DAMAGE IAW THE REQUIREMENTS OF A319 SRM 53-02-00, PARAGRAPH 8C FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)
- [SDR F3LA200800495](https://openairdocs.org/sdr/F3LA200800495.md): Floor Panel · punctured · Jul 15, 2008 · N943FR · Airbus A319112 · Fuselage Floor Panel
  > DURING C2 C CHECK, INSPECTION NOTED THE AFT PIT TRANSITION PANEL 151DE WAS PUNCTURED. MAINTENANCE REPAIRED DAMAGE IAW THE REQUIREMENTS OF A319 SRM 53-02-00, PARAGRAPH 8C FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)
- [SDR F3LA200800494](https://openairdocs.org/sdr/F3LA200800494.md): Floor Panel · punctured · Jul 15, 2008 · N943FR · Airbus A319112 · Fuselage Floor Panel
  > DURING C2 C-CHECK, INSPECTION NOTED THE AFT PIT TRANSITION PANEL 151BE WAS PUNCTURED. MAINTENANCE REPAIRED THE DAMAGE IAW THE REQUIREMENTS OF A319 SRM 53-02-00, PARAGRAPH 8C FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (S
- [SDR F3LA200800493](https://openairdocs.org/sdr/F3LA200800493.md): Floor Panel · punctured · Jul 15, 2008 · N943FR · Airbus A319112 · Fuselage Floor Panel
  > DURING C2 C CHECK, INSPECTION NOTED THE AFT PIT TRANSITION PANEL 151AE WAS PUNCTURED. MAINTENANCE REPAIRED THE DAMAGE IAW THE REQUIREMENTS OF A319 SRM 53-02-00, PARAGRAPH 8C FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (S
- [SDR F3LA200800492](https://openairdocs.org/sdr/F3LA200800492.md): Floor Panel · punctured · Jul 15, 2008 · N943FR · Airbus A319112 · Fuselage Floor Panel
  > DURING C2 C CHECK, INSPECTION NOTED THE AFT PIT TRANSITION PANEL 151UG WAS PUNCTURED. MAINTENANCE RECORDED THAT THIS IS EITHER A DUPLICATE WRITE-UP (161UG- NON ROUTINE C047467) OR SHOULD HAVE BEEN WRITTEN AS 152UG, WHICH HAD DAMAGE ALSO. THE DAMAGE REPAIR FO

## 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 = 'N943FR' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N943FR/reports

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