# Service difficulty reports: N939FR, cancelled Aug 22, 2022

A list on [N939FR, cancelled Aug 22, 2022](https://openairdocs.org/deregistered/N939FR-2022-08-22.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 · 67 reports

- [SDR F3LA2018112800479](https://openairdocs.org/sdr/F3LA2018112800479.md): Hydraulic Line · leaking · Nov 23, 2018 · N939FR · Airbus A319112 · Hydraulic System, Main
  > HYD G RSVR LO LVL. AIRCRAFT WAS GROUNDED DUE TO THIS DISCREPANCY. REMOVED AND REPLACED NR 1 ENG PRESSURE/SUCTION/RETURN LINE, REF AMM 29-11-49 PB401. NO LEAKS AT THIS TIME. OK TO CONTINUE. OPS CHECK GOOD. DUE TO LANDING GRAVITY EXTENSION MX PERFORMED LANDING G
- [SDR F3LA2018090400420](https://openairdocs.org/sdr/F3LA2018090400420.md): Door Frame · cracked · Aug 22, 2018 · N939FR · Airbus A319112 · Emergency Exits
  > FOUND CRACKS ON LT NR 1 EMERGENCY EXIT. LOCATED ON FWD AND AFT SEGMENTS AND ON THE FWD AND AFT SEGMENTS ON RT NR 1 EMERGENCY EXIT. ACCOMPLISHED OVERWING EMERGENCY EXIT LT AND RT DOOR FRAME OUTER FLANGE REPAIR PER EA A9-52R-34351 ON THE FWD AND AFT FRAME SEGMEN
- [SDR F3LA2018083000418](https://openairdocs.org/sdr/F3LA2018083000418.md): Hydraulic Line · crimped · Aug 19, 2018 · N939FR · Airbus A319112 · Hydraulic System, Main
  > HYDRAULIC LINE IN THE RT AFT UPPER MLG WW WAS DAMAGED. REMOVED AND REPLACED THE HYD LINE IAW AMM 32-43-00-710-001-A, 32-43-00-870-002-A, 12-12-29-611-002-A, AND 20-23-11-300-001.
- [SDR F3LA2018083000417](https://openairdocs.org/sdr/F3LA2018083000417.md): Hydraulic Line · ruptured · Aug 19, 2018 · N939FR · Airbus A319112 · Hydraulic System, Main
  > HYDRAULIC LINE AT THE LT AFT UPPER MLG WW WAS RUPTURED. REMOVED RUPTURED ALTERNATE BRAKING HYDRAULIC LINE & REPLACED WITH NEW IAW AMM 20-23-11-911-001-A. PERFORMED BLEEDING OF ALTERNATE BRAKING SYSTEM IAW AMM 32-43-00-870-002-A, SUCCESSFUL OPS CHECK OF THE
- [SDR F3LA2018083000419](https://openairdocs.org/sdr/F3LA2018083000419.md): Floorbeam · corroded · Aug 17, 2018 · N939FR · Airbus A319112 · Fuselage Main, Floor Beam
  > DISCREPANCY: CORROSION AROUND HARD POINT, BEAM -Y765 FR66. CORRECTIVE ACTION: REFERENCE PEMCO N/R 2082N289 REMOVED AND REPLACED NEW FLOOR BEAM -Y765 IAW A319 SRM 51-72-11-911-001, 53-41-14-283-004 AND 51-21-11./END/
- [SDR F3LA2018082700409](https://openairdocs.org/sdr/F3LA2018082700409.md): Floor Support · corroded · Aug 17, 2018 · N939FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON THE RT FLOOR SUPPORT, -Y1292, FRAMES 66 - 68. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11, 51-44-11, AND 53-41-14-283-004.
- [SDR F3LA2018082700408](https://openairdocs.org/sdr/F3LA2018082700408.md): Floor Support · corroded · Aug 16, 2018 · N939FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > LEFT FLOOR SUPPORT, Y1162 WAS CORRODED BETWEEN FRAMES 66 - 69. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11-911-001, AND 53-00-14-282-002.
- [SDR F3LA2018082400402](https://openairdocs.org/sdr/F3LA2018082400402.md): Floorbeam · corroded · Aug 16, 2018 · N939FR · Airbus A319112 · Fuselage Main, Floor Beam
  > DISCREPANCY: REFERENCE NR 2082N250, LH FLOORBEAM Y765 HAS CORROSION AT FR66. CORRECTIVE ACTION: REMOVED AND REPLACED AFT WET AREA FLOORBEAM AT FR66 LOC Y765 IAW A319 SRM 51-72-11-911-001, 53-00-14-282-002 AND 51-44-11./END/
- [SDR F3LA2018082400401](https://openairdocs.org/sdr/F3LA2018082400401.md): Floorbeam · corroded · Aug 16, 2018 · N939FR · Airbus A319112 · Fuselage Main, Floor Beam
  > DISCREPANCY: REFERENCE NR 2082N247, RH AFT FLOORBEAM -Y1162 HAS CORROSION AROUND FASTENER HOLE FR68. CORRECTIVE ACTION: REMOVED AND REPLACED FLOORBEAM -Y1162 IAW A319 SRM 51-42-11, 51-44-11 AND 53-00-14-283-002 FR68./END/
- [SDR F3LA2018082300400](https://openairdocs.org/sdr/F3LA2018082300400.md): Floor Support · corroded · Aug 16, 2018 · N939FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > LH FLOOR SUPPORT Y512 HAS CORROSION AROUND FASTENER HOLE FR66. REMOVED AND REPLACED FLOOR SUPPORT Y512 FR66 TO 70 IAW SRM 51-72-11-911-002, 53-00-14-283-002 AND 51-72-911-001./END/
- [SDR F3LA2016100400063](https://openairdocs.org/sdr/F3LA2016100400063.md): Door Frame · cracked · Sep 22, 2016 · N939FR · Airbus A319112 · Fuselage Main, Structure
  > RIGHT EMERGENCY OVERWING EXIT FWD AND AFT I/B FRAME HAS INDICATIONS OF CRACKS. REMOVED AND REPLACED IAW SRM 51-42-11.
- [SDR F3LA2016100400062](https://openairdocs.org/sdr/F3LA2016100400062.md): Door Frame · cracked · Sep 20, 2016 · N939FR · Airbus A319112 · Fuselage Main, Structure
  > LEFT EMERGENCY OVERWING EXIT AFT INBD DOOR FRAME HAS INDICATIONS OF CRACKS. REMOVED AND REPLACED EMERGENCY EXIT AFT DOOR FRAME IAW SRM 51-42-11.
- [SDR F3LA2016100400064](https://openairdocs.org/sdr/F3LA2016100400064.md): Floor Support · corroded · Sep 19, 2016 · N939FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > AFT CABIN FRAME 66+10 THROUGH 68+6 Y1292 FLOOR SUPPORT TOP FLANGE CORRODED AT MULTIPLE LOCATIONS. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11.
- [SDR F3LA2016091900059](https://openairdocs.org/sdr/F3LA2016091900059.md): Floorbeam · corroded · Sep 10, 2016 · N939FR · Airbus A319111 · Fuselage Main, Floor Beam
  > AFT CABIN, FRAME 66, Y508 FLOORBEAM CORRODED AT MULTIPLE LOCATIONS. REMOVE CORROSION MAXIMUM DEPTH OF REWORK IS.016, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14, FIG 001. REMOVED OLD BEAM AT Y508, FR 66 IAW SRM 52-42-11. LOCATED & DRILLED NEW FLOORBEAM, INS
- [SDR F3LA2016091900058](https://openairdocs.org/sdr/F3LA2016091900058.md): Floorbeam · corroded · Sep 10, 2016 · N939FR · Airbus A319111 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM Y1292, FASTENER HOLE BETWEEN FRAME 20 AND FRAME 18. R & R FLOORBEAM AT Y1292, FRAME 12-24 IAW SRM 51-72-11-911 AND SRM 51-21-11.
- [SDR F3LA2016091900057](https://openairdocs.org/sdr/F3LA2016091900057.md): Floorbeam · corroded · Sep 10, 2016 · N939FR · Airbus A319112 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM Y1292 BETWEEN FRAME 17 AND FRAME 20. R & R FLOORBEAM AT Y1292, FRAME 17 AND FRAME 20 IAW SRM 51-72-11, 51-42-11, 51-44-11.
- [SDR F3LA2016091900056](https://openairdocs.org/sdr/F3LA2016091900056.md): Floorbeam · corroded · Sep 10, 2016 · N939FR · Airbus A319111 · Fuselage Main, Floor Beam
  > AFT CABIN FRAME 67-FRAME 68, Y765, FLOORBEAM TOP FLANGE CORRODED AT MULTIPLE LOCATIONS. R & R AFT CABIN FLOORBEAM Y765 AT FRAME 67-FRAME 68 IAW SRM 51-72-11.
- [SDR F3LA2014091101069](https://openairdocs.org/sdr/F3LA2014091101069.md): Structure · corroded · Sep 11, 2014 · N939FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > C6 CHECK. PAX CABIN FROM FRAME 69 - 70 RT - Y1292 HAS SURFACE CORROSION AT FIVE EACH MULTIPLE FASTENERS HOLES AT SKIN PLATE. R & R SKIN PLATE IAW EO A0-53EO-31434, SRM 51-42-11 PAR 6B 3 A-D PAR 13D 1-4.
- [SDR F3LA2014081801053](https://openairdocs.org/sdr/F3LA2014081801053.md): Battery · discharged · Aug 18, 2014 · N939FR · Airbus A319112 · Emergency Lighting
  > EPSU EMER LIGHTS BATTERY 12WL FAILED CAPACITY TEST ON TASK CARD A332204-02. R & R THE EPSU BATTERY ASSEMBLY IAW AMM 33-51-38-000-002A & 33-51-38-400-002A.
- [SDR F3LA2014020701005](https://openairdocs.org/sdr/F3LA2014020701005.md): Slide · low pressure · Feb 7, 2014 · N939FR · Airbus A319112 · Escape Slide
  > DOOR R2 SLIDE PRESS LOW. R & R R2 DOOR ESCAPE SLIDE IAW AMM 25-62-44 PB 401.
- [SDR F3LA2013062100868](https://openairdocs.org/sdr/F3LA2013062100868.md): Bleed Air Sys · odor · Jun 17, 2013 · N939FR · Airbus A319111 · Engine Bleed Air System
  > ODOR IN CABIN AT LOW ALTITUDES, BOTH TAKEOFF AND APPROACH (AROUND 10,000' AGL) STRONG ODOR AROUND ROW 20-22. RAN APU, ENGINE NR 1 AND ENGINE NR 2 AND COULD NOT DETECT AN ODOR. R & R RECIRCULATION FILTERS REF AMM 21-21-45, PB401. ACFT NEEDS OPS CHECK FLIGHT T
- [SDR F3LA2012121900822](https://openairdocs.org/sdr/F3LA2012121900822.md): Power Supply · inoperative · Dec 17, 2012 · N939FR · Airbus A319111 · Emergency Lighting
  > C-CHECK, EMERGENCY LIGHT SYS TEST FAILED FOR FWD EPSU 10WL. R & R EPSU IAW AMM 33-51-38-020-051-A. SYSTEM OPS GOOD IAW 33-51-38-740-050-B.
- [SDR F3LA2012082300778](https://openairdocs.org/sdr/F3LA2012082300778.md): A/C Pack · smoke · Aug 21, 2012 · N939FR · Airbus A319111 · Cabin Cooling System
  > ECAM MESSAGE NR 2 PACK OVERHEAT, ON DEPARTURE CLIMBING THROUGH 11,000 F/A CALLED WITH INFO ON SMOKE IN CABIN (AFT), ODOR WAS NOTABLE BUT DISSIPATING. EMERGENCY DECLARED AIR TURN BACK ON LANDING ROLL OUT, ECAM MESSAGE APPEARED, ACTIONS COMPLETED.
- [SDR F3LA2011051900646](https://openairdocs.org/sdr/F3LA2011051900646.md): Floorbeam · corroded · May 19, 2011 · N939FR · Airbus A319111 · Fuselage Main, Floor Beam
  > C-CHECK: NON ROUTINE NR 1287; CORROSION ON UPPER SURFACE OF RT AFT ENTRY AREA, FLOORBEAM AT FR 68, RBL 48, FOUND TO BE OUT OF LIMITS. R & R FLOORBEAM AT FR 68, RBL 48 IAW SRM 51-24-00, PARA 6.
- [SDR F3LA2011501900645](https://openairdocs.org/sdr/F3LA2011501900645.md): Floor Panel · delaminated · May 13, 2011 · N939FR · Airbus A319111 · Fuselage Floor Panel
  > C-CHECK: CABIN FLOOR PANEL 241JF HAS DELAMINATION IN SEVERAL AREAS AND FOUND TO BE OUT OF REPAIRABLE LIMITS. R & R FLOOR PANEL 241JF IAW SRM 53-02-00, PB 101.
- [SDR F3LA201151900644](https://openairdocs.org/sdr/F3LA201151900644.md): Floor Support · corroded · May 13, 2011 · N939FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > C-CHECK: CORROSION ON UPPER SURFACE OF RT AFT ENTRY AREA, FLOORBEAM AT FR 68, RBL 30. R & R FLOORBEAM AT FR 66-70, RBL 30 IAW SRM 51-74-00.
- [SDR F3LA201151900643](https://openairdocs.org/sdr/F3LA201151900643.md): Shear Plate · cracked · May 13, 2011 · N939FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > C-CHECK: NON ROUTINE NR1262; LT AFT LATERAL SHEAR PLATE IS CRACKED, FR69, STR 24. REPLACED LT AFT LATERAL SHEAR PLATE WITH NEW CONFIGURATION IAW EO A0-53EO-31434 AND IAW SRM 51-42-11-1- A, B, C.
- [SDR F3LA201151900642](https://openairdocs.org/sdr/F3LA201151900642.md): Floorboard · damaged · May 13, 2011 · N939FR · Airbus A319111 · Fuselage Floor Panel
  > C- CHECK: NON ROUTINE NR1329: COCKPIT FLOORBOARD, 211GF SURFACE IS DAMAGED. FOUND DAMAGE TO FLOORBOARD 211GF BEYOND REPAIRABLE LIMITS. REPLACED FLOORBOARD IAW SRM 53-12-00, DIAGRAM 101.
- [SDR F3LA2010071800471](https://openairdocs.org/sdr/F3LA2010071800471.md): Computer · faulted · Jul 15, 2010 · N939FR · Airbus A319111 · Flight Control System
  > REF: PILOT REPORT LOG PAGE 549851 ITEM 1. CLIMBING THROUGH FLIGHT LEVEL 380 ELAC NR 2 FAULTED, ACFT WENT INTO ALTERNATE LAW. AIR TURN BACK TO SMF. REPLACED NR 2 ELAC REF AMM 27-93-34 PAGE BLOCK 401, OPS CHECK GOOD. PERFORMED LAND CATAGORY III CAPABILITIES TES
- [SDR F3LA2009122800272](https://openairdocs.org/sdr/F3LA2009122800272.md): Fitting · out of adjust · Dec 25, 2009 · N939FR · Airbus A319111 · Emergency Equipment
  > DURING LANDING THE FLIGHT CREW NOTED THE L2 DOOR SLIDING ARMING LEVER DISARMS IN FLIGHT AND APPEARS RELATED TO CABIN PRESSURE DIFFERENTIAL ABOVE 10000 FEET. MX ADJUSTED ESCAPE SLIDE RELEASE MECHANISM AFT GIRT BAR FITTING ADJUSTED TO CORRECT CLEARANCES AND PER
- [SDR F3LA2009122800271](https://openairdocs.org/sdr/F3LA2009122800271.md): Fitting · out of adjust · Dec 25, 2009 · N939FR · Airbus A319111 · Emergency Equipment
  > DURING CRUISE ALTITUDE, THE FLIGHT CREW NOTED THE L2 DOOR ARM LIGHT WAS ON AND INTERMITTENT. MX ADJUSTED THE GIRT BAR FITTING FOR THE L2 DOOR AND PERFORMED A TEST OF THE EMERGENCY ESCAPE SLIDE RELEASE MECHANISM IAW AMM 52-13-22-820-056 AND AMM 52-73-00-710-050
- [SDR F3LA2009122200259](https://openairdocs.org/sdr/F3LA2009122200259.md): Wire · broken · Dec 18, 2009 · N939FR · Airbus A319111 · Light System Wiring
  > DURING C3 C-CHECK INSP NOTED SEAT ROW 10B AND 10C EMERGENCY EXIT LIGHT WIRE WAS BROKEN AT CONNECTOR OTBD SEAT LEG GOING TO FLOOR. MX REMOVED AND REPLACED EMERGENCY EXIT WIRE HARNESS IAW AMM 25-21-41-000-001 STEP 4A(2)(B), AMM 25-21-41-400-001 STEP 4D(1)(C) AN
- [SDR F3LA2009122300266](https://openairdocs.org/sdr/F3LA2009122300266.md): Sill · corroded · Dec 17, 2009 · N939FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C3 C-CHECK INSP, NOTED THE L2 DOOR SILL CORRODED AT FWD SPLICE IN AND AROUND THE FLOORBOARD ATTACH HOLE. MX REPAIRED DOOR SILL IAW SRM 53-41-14 AND EA A9-53R-31579.
- [SDR F3LA2009122300265](https://openairdocs.org/sdr/F3LA2009122300265.md): Floor Panel · corroded · Dec 16, 2009 · N939FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C3 C-CHECK INSP, NOTED MAIN CABIN FLOOR PANEL 261FF HAS CORROSION. MX REMOVED AND REPLACED FLOOR PANEL 261FF IAW AMM 53-42-12-400-002.
- [SDR F3LA2009122200261](https://openairdocs.org/sdr/F3LA2009122200261.md): Floorbeam · corroded · Dec 16, 2009 · N939FR · Airbus A319111 · Fuselage Main, Floor Beam
  > DURING C3 C-CHECK INSP NOTED A HOLE IN FLOORBEAM Y1292 JUST AFT OF LAVATORY D FROM FRAME 64 TO FRAME 66 AND WAS ALSO CORRODED. MX REMOVED AND REPLACED FLOORBEAM Y1292 IAW SRM 51-42-11 AND SRM 51-44-11.
- [SDR F3LA2009122200260](https://openairdocs.org/sdr/F3LA2009122200260.md): Shear Plate · corroded · Dec 16, 2009 · N939FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C3 C-CHECK INSP NOTED THE RT SHEAR PLATE FROM FRAME 69 TO FRAME 70 WAS CORRODED. MX REMOVED AND REPLACED SHEAR PLATE IAW SRM 51-42-11, SRM 51-44-11 AND SRM 51-21-00.
- [SDR F3LA2009122400270](https://openairdocs.org/sdr/F3LA2009122400270.md): Plate · corroded · Dec 15, 2009 · N939FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C3 C-CHECK INSP NOTED THE ARMED PLATE FOR THE R2 DOOR WAS CORRODED. MX REMOVED AND REPLACED ARM PLATE IAW AMM 53-42-12-420-051.
- [SDR F3LA2009122300269](https://openairdocs.org/sdr/F3LA2009122300269.md): Strip · corroded · Dec 15, 2009 · N939FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C3 C-CHECK INSPECTION, NOTED THE THRESHOLD STRIP FOR PANEL 262EF IS CORRODED. MX REMOVED AND REPLACED STRIP IAW AMM 53-42-12-400-002.
- [SDR F3LA2009122300268](https://openairdocs.org/sdr/F3LA2009122300268.md): Plate · corroded · Dec 15, 2009 · N939FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C3 C-CHECK INSPECTION, NOTED ARMED PLATE FOR L2 DOOR IS CORRODED. MX REMOVED AND REPLACED ARMED PLATE ON L2 DOOR THRESHOLD IAW AMM 20-21-11, PB 201.
- [SDR F3LA2009122300267](https://openairdocs.org/sdr/F3LA2009122300267.md): Threshold · corroded · Dec 15, 2009 · N939FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C3 C-CHECK INSP, NOTED THRESHOLD STRIP FOR L2 DOOR THRESHOLD IS CORRODED. MX REMOVED AND REPLACED THRESHOLD STRIP IAW AMM 53-42-12-400-001.
- [SDR F3LA2009122200263](https://openairdocs.org/sdr/F3LA2009122200263.md): Floor Support · corroded · Dec 15, 2009 · N939FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C3 C-CHECK INSP NOTED UPON REMOVAL OF THE AFT GALLEY FLOOR CORROSION WAS FOUND AT Y1292 FRAME 66 TO FRAME 69. MX REMOVED AND REPLACED FLOOR SUPPORT Y1292 AT FRAME 66 TO FRAME 69 RT SIDE IAW SRM 51-42-11, SRM 51-21-00 AND EA A9-53T-30392.
- [SDR F3LA2009122200262](https://openairdocs.org/sdr/F3LA2009122200262.md): Floor Support · corroded · Dec 15, 2009 · N939FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C3 C-CHECK INSP NOTED UPON REMOVAL OF THE AFT GALLEY FLOOR CORROSION WAS FOUND AT FLOOR SUPPORT Y1292 FROM FRAME 66 TO FRAME 69. MX REPLACED FLOOR SUPPORT Y1292 AT FRAME 66 TO FRAME 69 LT SIDE IAW SRM 51-42-11 AND SRM 51-44-11.
- [SDR F3LA2009021900028](https://openairdocs.org/sdr/F3LA2009021900028.md): Hmu · failed · Feb 18, 2009 · N939FR · Airbus A319111 · Fuel Control/Turbine Engines
  > PILOT REPORTED THAT THE NR 2 ENGINE FAILED ON DESCENT FROM FL 350, THE ENGINE RECOVERED AND FURTHER DESCENT, APPROACH AND LANDING WERE UNEVENTFUL ON TWO ENGINES. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE HYDRO MECHANICAL UNIT AND PERFORMED SATISFACTORY
- [SDR F3LA2008111000711](https://openairdocs.org/sdr/F3LA2008111000711.md): Bushing · out of position · Nov 9, 2008 · N939FR · Airbus A319111 · Passenger/Crew Doors
  > REFERENCE LOG PAGE 420725. PILOT REPORTED THE FORWARD ENTRY DOOR L1 GUST LOCK WILL NOT ENGAGE. MAINTENANCE REINSTALLED BUSHING IN THE FORWARD ENTRY DOOR GUST LOCK MECHANISM IN ACCORDANCE WITH A319 AMM 52-11-11-730-050.
- [SDR F3LA200800405](https://openairdocs.org/sdr/F3LA200800405.md): Floorboard · damaged · Jun 28, 2008 · N939FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C-CHECK INSP NOTED AFT CARGO PIT FWD FLOORBOARD PANEL 151PE HAS A HOLE AT THE AFT LT EDGE. MAINT REMOVED DAMAGED AREA AND FILLED DAMAGED AREA IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)
- [SDR F3LA200800406](https://openairdocs.org/sdr/F3LA200800406.md): Panel · damaged · Jun 28, 2008 · N939FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C-CHECK INSP, NOTED AFT CARGO PIT AFT LT HAND TRANSITION PANEL 161BF HAS A HOLE AT AFT TOP END. MAINT REPAIRED AND INSTALLED SERVICEABLE PANEL 161BF IAW SRM 53-42-44-400-001. COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)
- [SDR F3LA200800407](https://openairdocs.org/sdr/F3LA200800407.md): Panel · damaged · Jun 28, 2008 · N939FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C-CHECK INSP NOTED AFT CARGO PIT FWD LT HAND LOWER TRANSITION PANEL 151AE HAS A HOLE AT FWD LOWER END. MAINT REPAIRED AND INSTALLED SERVICEABLE PANEL 151AE IAW SRM 53-42-14-400-001. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.
- [SDR F3LA200800402](https://openairdocs.org/sdr/F3LA200800402.md): Panel · damaged · Jun 24, 2008 · N939FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C-CHECK INSP, NOTED AFT CARGO PIT AFT RT UPPER TRANSITION PANEL 162CF HAS SEVERAL HOLES AT AFT END. MAINT REPAIRED TRANSITION PANEL 162CF IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)
- [SDR F3LA200800401](https://openairdocs.org/sdr/F3LA200800401.md): Panel · damaged · Jun 24, 2008 · N939FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C-CHECK INSP NOTED AFT CARGO PIT AFT LT UPPER TRANSITION PANEL 161CF HAS HOLES IN SEVERAL PLACED. MAINT REPAIRED TRANSITION PANEL 161CF IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)
- [SDR F3LA200800400](https://openairdocs.org/sdr/F3LA200800400.md): Panel · damaged · Jun 24, 2008 · N939FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C-CHECK INSP, NOTED AFT CARGO PIT FWD LT UPPER TRANSITION PANEL 151FE HAS A HOLE AT FWD TOP CORNER. MAINT REPAIRED TRANSITION PANEL 151FE IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Next page: https://openairdocs.org/deregistered/N939FR-2022-08-22/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 = 'N939FR' AND deregistration_id = 'N939FR-2022-08-22'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N939FR-2022-08-22/reports

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