# Service difficulty reports: N929FR, cancelled Nov 16, 2015

A list on [N929FR, cancelled Nov 16, 2015](https://openairdocs.org/deregistered/N929FR-2015-11-16.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 · 58 reports

- [SDR F3LA2014111001084](https://openairdocs.org/sdr/F3LA2014111001084.md): Slide · defective · Nov 7, 2014 · N929FR · Airbus A319111 · Escape Slide
  > AIRCRAFT DUE C 7 CHECK. DURING SCHEDULED OPERATIONAL CHECK OF R 2 DOOR SLIDE, LIGHTS DID NOT ILLUMINATE WHEN SLIDE DEPLOYED. R & R R2 DOOR SLIDE WITH SERVICEABLE UNIT IAW TASK CARD TC25831-03. ACFT DUE OUT OF C CHECK 11/11/2014.
- [SDR F3LA2014090801063](https://openairdocs.org/sdr/F3LA2014090801063.md): Bottle · discharged · Sep 7, 2014 · N929FR · Airbus A319111 · Portable Oxygen System
  > LOUD NOISE & RUSH OF AIR IN AFT GALLEY AREA RT SIDE OVERHEAD. BLOCK RETURN. FOUND PORTABLE OXYGEN BOTTLE IN AFT CABIN POSITION TO HAVE SUDDENLY DEPRESSURIZED TO ZERO PSI. REPLACED AFT PORTABLE OXYGEN BOTTLE IAW AMM 35-32-42 PAGE BLOCK 401. FLIGHT ATTENDANT
- [SDR F3LA2013050700849](https://openairdocs.org/sdr/F3LA2013050700849.md): Lever · stuck · Apr 23, 2013 · N929FR · Airbus A319111 · Escape Slide
  > RIGHT EMERGENCY EXIT SLIDE RELEASE LEVER ON DOOR WILL NOT RETURN TO NORMAL POSITION. INSTALLED RELEASE CABLE TEST TOOL AND PERFORMED TEST NUMEROUS TIMES. CABLE RELEASE LEVER NOW RETURNS TO NORMAL POSITION IAW AMM 25-62-43-400-003-A, PG 10 & 11 STEPS(B) THUR
- [SDR F3LA2012121300818](https://openairdocs.org/sdr/F3LA2012121300818.md): Battery Pack · inoperative · Dec 13, 2012 · N929FR · Airbus A319111 · Emergency Lighting
  > EMERGENCY LIGHT EPSU BATTERY 10WL FAILED TEST, HEAVY SERVICE. R & R BATTERY FOR 10WL EPSU. OPS CHECK OK, REF AMM 33-51 -38-000-002A AND 33-51-38-400-002A.
- [SDR F3LA2010050600419](https://openairdocs.org/sdr/F3LA2010050600419.md): Epsu · failed · May 4, 2010 · N929FR · Airbus A319111 · Emergency Lighting
  > REFERENCE C-CHECK NON ROUTINE N0768. MULTIPLE EMERGENCY LIGHTS FOR SEAT ROWS INOPERATIVE. R & R EMERGENCY LIGHT HARNESS AT SEAT ROW 18 ABC IAW ESPM 20-33-11. R & R DEFECTIVE EPSU AT POSITION 11WL AND POSITION 13WL IAW AMM 33-51-38 PAGE BLOCK 401.
- [SDR F3LA2010043100406](https://openairdocs.org/sdr/F3LA2010043100406.md): Floor Panel · dented · Apr 24, 2010 · N929FR · Airbus A319111 · Fuselage Floor Panel
  > REF HEAVY MX NON ROUTINE N0689. AFT CARGO PIT PANEL 151UG HAS NUMEROUS DENTS. OFF ACFT PART. FABRICATED PANEL 151UG IAW IRM 9701 REV G.
- [SDR F3LA2010043100405](https://openairdocs.org/sdr/F3LA2010043100405.md): Transition Panel · dented · Apr 24, 2010 · N929FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > HEAVY MX NON-ROUTINE N0688. AFT CARGO PIT TRANSITION PANEL 152UG HAS NUMEROUS DENTS THROUGHOUT ENTIRE PANEL. OFF ACFT PART. FABRICATED PANEL IAW IRM 9701 REV G.
- [SDR F3LA2010043100404](https://openairdocs.org/sdr/F3LA2010043100404.md): Transition Panel · punctured · Apr 24, 2010 · N929FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > REF C-CHECK NON ROUTINE N0686. AFT CARGO COMPARTMENT TRANSITION PANEL 161BF HAS (2) PUNCTURES. OFF ACFT PART. FABRICATED REPLACEMENT TRANSITION PANEL 161BF IAW IRM 9701 REV G.
- [SDR F3LA2010043100403](https://openairdocs.org/sdr/F3LA2010043100403.md): Floor Panel · delaminated · Apr 24, 2010 · N929FR · Airbus A319111 · Fuselage Floor Panel
  > REF HEAVY MX NON-ROUTINE N0687. AFT CARGO PIT PANEL 152TG HAS SEVERAL AREAS OF EDGE DELAMINATION AND SEVERAL SMALL DENTS. OFF ACFT PART. FABRICATED PANEL 152TG IAW IRM 9701 REV G.
- [SDR F3LA2010043100402](https://openairdocs.org/sdr/F3LA2010043100402.md): Transition Panel · dented · Apr 24, 2010 · N929FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > REF C-CHECK NON ROUTINE N0682. AFT CARGO COMPARTMENT TRANSITION PANEL 151BE HAS (2) PUNCTURES AND NUMEROUS DENTS THROUGHOUT ENTIRE PANEL. OFF ACFT PART. FABRICATED REPLACEMENT PANEL 151BE IAW MCG IRM 9701 REV G.
- [SDR F3LA2010043100401](https://openairdocs.org/sdr/F3LA2010043100401.md): Transition Panel · delaminated · Apr 24, 2010 · N929FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > REF HEAVY MX NON-ROUTINE N0678. AFT CARGO TRANSITION PANEL 151FE HAS DELAMINATION AROUND EDGE. OFF ACFT PART. FABRICATED PANEL IAW IRM 9701 REV G.
- [SDR F3LA2010043100400](https://openairdocs.org/sdr/F3LA2010043100400.md): Transition Panel · dented · Apr 24, 2010 · N929FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > REFERENCE C-CHECK NON ROUTINE N0685 AFT CARGO COMPARTMENT TRANSITION PANEL 161CF HAS NUMEROUS DENTS AND BULGES THROUGHOUT PANEL. R & R PANEL 161CF IAW MCG IRM 9701 REV G.
- [SDR F3LA2010043100399](https://openairdocs.org/sdr/F3LA2010043100399.md): Floor Panel · delaminated · Apr 24, 2010 · N929FR · Airbus A319111 · Fuselage Floor Panel
  > REFERENCE HEAVY MX NON-ROUTINE N00680. AFT CARGO PIT PANEL 162BF HAS AREAS OF DELAMINATION AROUND EDGE OF PANEL. FABRICATED PANEL IAW IRM 9701 REV G.
- [SDR F3LA2010043100398](https://openairdocs.org/sdr/F3LA2010043100398.md): Floor Panel · dented · Apr 24, 2010 · N929FR · Airbus A319111 · Fuselage Floor Panel
  > REF HEAVY MX NON-ROUTINE N0679. AFT CARGO PANEL 151DE HAS NUMEROUS DENTS THROUGHOUT PANEL. R & R PANEL.
- [SDR F3LA2010050200409](https://openairdocs.org/sdr/F3LA2010050200409.md): Floor Panel · delaminated · Apr 20, 2010 · N929FR · Airbus A319111 · Fuselage Floor Panel
  > REF C-CHECK NON ROUTINE N0587. CABIN FLOOR PANEL 222CF IS DELAMINATED. OFF ACFT PART. FABRICATED REPLACEMENT CABIN FLOOR PANEL 222CF IAW IRM 9701 REV G.
- [SDR F3LA2010050600418](https://openairdocs.org/sdr/F3LA2010050600418.md): Floorbeam · corroded · Apr 19, 2010 · N929FR · Airbus A319111 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM JUST INBD OF Y765 AT FRAME 68. R & R FLOORBEAM IAW A319 SRM 51-42-11, PAGE 1, STEP A, 51-44-11, PAGE 1 AND 51-21-11 PAGE 1 TABLE 1.
- [SDR F3LA2010050500417](https://openairdocs.org/sdr/F3LA2010050500417.md): Floorbeam · corroded · Apr 19, 2010 · N929FR · Airbus A319111 · Fuselage Main, Floor Beam
  > REFERENCE C-CHECK NON ROUTINE N0479. CORROSION ON NUT PLATE HOLES AT SPLICE ON FLOORBEAM AT Y-1292 FRAME 69. UPPER AND LOWER SIDES OF BEAM. R & R FLOORBEAM IAW SRM 51-72-11.
- [SDR F3LA2010050500416](https://openairdocs.org/sdr/F3LA2010050500416.md): Floorbeam · corroded · Apr 19, 2010 · N929FR · Airbus A319111 · Fuselage Main, Floor Beam
  > REFERENCE C-CHECK NON ROUTINE N0481. CORROSION ON PREVIOUS REPAIR AT FLOORBEAM, Y1292, FRAME 66. R & R FLOORBEAM IAW SRM 51-72-11, SHEETS 1 THROUGH 6.
- [SDR F3LA2010050500415](https://openairdocs.org/sdr/F3LA2010050500415.md): Sill · corroded · Apr 19, 2010 · N929FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > REFERENCE C-CHECK NON ROUTINE N0480. CORROSION ON L-2 DOOR SILL PLATE AT SPLICE FRAME 66. REPAIRED L-2 DOOR SILL PLATE IAW SRM 53-41-11 FIGURE 201 REPAIR PRINCIPLE 6.
- [SDR F3LA2010050400412](https://openairdocs.org/sdr/F3LA2010050400412.md): Sill · corroded · Apr 19, 2010 · N929FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > C-CHECK NON ROUTINE N0482. CORROSION ON R-2 DOORSILL PLATE AT FRAME 66 SPLICE. R & R DOOR SILL AND 3 EACH SCUFF PLATES IAW SRM 51-72-11 AND AMM 53-45-15-400-001.
- [SDR F3LA2010050200411](https://openairdocs.org/sdr/F3LA2010050200411.md): Support Frame · corroded · Apr 19, 2010 · N929FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > REFERENCE C-CHECK NON ROUTINE N0551. RIGHT HAND CABIN FLOOR SHEAR PLATE EXTRUSION IS CORRODED. REPLACED EXTRUSION REF A319 SRM 41-42-11, SRM 51-21-11 AND 51-72-11.
- [SDR F3LA2010050200410](https://openairdocs.org/sdr/F3LA2010050200410.md): Floorbeam · corroded · Apr 19, 2010 · N929FR · Airbus A319111 · Fuselage Main, Floor Beam
  > REFERENCE HEAVY MX NON-ROUTINE N0534. CORROSION DISCOVERED ON NUTPLATE HOLES ON FLOORBEAM Y1292. R & R FLOORBEAM.
- [SDR F3LA2010043100397](https://openairdocs.org/sdr/F3LA2010043100397.md): Floorbeam · corroded · Apr 19, 2010 · N929FR · Airbus A319111 · Fuselage Main, Floor Beam
  > REF C-CHECK NON ROUTINE N0478. CORROSION IN (2) AREAS OF FLOORBEAM -Y765 AT FRAME 68. R & R FLOORBEAM IAW A319 SRM 51-42-11 PAGE 11.
- [SDR F3LA2010050500414](https://openairdocs.org/sdr/F3LA2010050500414.md): Shear Plate · corroded · Apr 18, 2010 · N929FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > REFERENCE C-CHECK NON ROUTINE N0318. SHEAR PLATE AT FRAME 69 TO FRAME 70 BETWEEN STRINGER 23 RT AND 24 RT HAS CORROSION IN 15 AREAS. R & R SHEAR PLATE IAW SRM 51-42-11 PARAGRAPH 6 AND 7 AND EO A0-53EO-31434.
- [SDR F3LA2010050400413](https://openairdocs.org/sdr/F3LA2010050400413.md): Shear Plate · corroded · Apr 18, 2010 · N929FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > REF C-CHECK NON ROUTINE N0317. SHEAR PLATE AT FRAME 69 TO 70 BETWEEN STRINGER 23 LT AND STRINGER 24 LT HAS 6 SQUARE INCHES OF CORROSION. R & R SHEAR PLATE IAW SRM 51-42-11 PARAGRAPH 6 AND 7 AND EO NR A0-53EO-31434.
- [SDR F3LA2010050200408](https://openairdocs.org/sdr/F3LA2010050200408.md): Transition Panel · delaminated · Apr 18, 2010 · N929FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > REF AERO FRAME HEAVY MX NON-ROUTINE N0336. TRANSITION PANEL 131BF HAS AREAS OF PUNCTURES DENTS AND EDGE DELAMINATION. OFF ACFT PART. FABRICATED PANEL IAW IRM 9701 REV G.
- [SDR F3LA2010050200407](https://openairdocs.org/sdr/F3LA2010050200407.md): Transition Panel · dented · Apr 18, 2010 · N929FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > REF C-CHECK NON ROUTINE N0299. FWD CARGO COMPARTMENT TRANSITION PANEL 131DG HAS NUMEROUS DENTS ACCROSS ENTIRE LENGTH OF PANEL. OFF ACFT PART. FABRICATED TRANSITION PANEL 131DG IAW MCG IRM 9701 REV G.
- [SDR F3LA2010043100395](https://openairdocs.org/sdr/F3LA2010043100395.md): Transition Panel · dented · Apr 18, 2010 · N929FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > REFERENCE HEAVY MX NON ROUTINE N0319. FWD CARGO PIT TRANSITION PANEL HAS NUMEROUS DENTS THROUGHOUT ENTIRE LENGTH OF PANEL. FABRICATED REPLACEMENT PANEL IAW IRM9701 REV G. R & R PANEL.
- [SDR F3LA2010043000394](https://openairdocs.org/sdr/F3LA2010043000394.md): Bracket · cracked · Apr 18, 2010 · N929FR · Airbus A319111 · Wing, Attach Fittings
  > REF C4/SI CHECK NON-ROUTINE N0215. LT WING L/E TAI DUCT CUT OUT UPPER SURFACE OTBD PANEL ATTACH ANGLE HAS A 1.5 INCH CRACK. R & R BRACKET.
- [SDR F3LA2010043100396](https://openairdocs.org/sdr/F3LA2010043100396.md): Floor Panel · dented · Apr 17, 2010 · N929FR · Airbus A319111 · Fuselage Floor Panel
  > REFERENCE HEAVY MX NON-ROUTINE N0684. AFT CARGO PIT FLOOR PANEL 162CF HAS NUMEROUS DENTS. R & R PANEL.
- [SDR F3LA2009062200089](https://openairdocs.org/sdr/F3LA2009062200089.md): Servo Control · inoperative · Jun 19, 2009 · N929FR · Airbus A319111 · Drag Control System
  > FLIGHT CREW MADE AN UNSCHEDULED LANDING IN RSW DUE TO "SPOILER FAULT 4". THE AIRCRAFT RETURNED TO DEN ON A SPECIAL FLIGHT PERMIT. MAINTENANCE REMOVED AND REPLACED THE NR 4 RIGHT SPOILER SERVO AND PERFORMED RIG, OPERATIONAL AND LEAK CHECK PER AMM 27-64-51 PB
- [SDR F3LA2009031100041](https://openairdocs.org/sdr/F3LA2009031100041.md): Computer · smoke · Mar 9, 2009 · N929FR · Airbus A319111 · Flight Management Computing Hardware System
  > DURING THE BOARDING PROCESS, BOTH PILOTS DETECTED ELECTRONIC OVERHEAT ODOR. MAINTENANCE PERFORMED TROUBLESHOOTING USING REFERENCE TSM 24-00-00-810-823, ELECTRICAL BURNING SMELL OR FUMES FOUND IN THE CABIN, COCKPIT, CARGO, OR AVIONICS COMPARTMENT AND IDENTIFIE
- [SDR F3LA200800604](https://openairdocs.org/sdr/F3LA200800604.md): Floor Panel · corroded · Sep 8, 2008 · N929FR · Airbus A319111 · Fuselage Floor Panel
  > REF: NON ROUTINE C050752. DURING C3 C-CHECK, INSPECTION FOUND (1) MOUNT BUSHING CORRODED ON FLOOR PANEL 261DE. MAINTENANCE REMOVED AND REPLACED MOUNT BUSHING ON C-CHECK CARD NR C5341032. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (K
- [SDR F3LA200800601](https://openairdocs.org/sdr/F3LA200800601.md): Floorbeam · corroded · Sep 6, 2008 · N929FR · Airbus A319111 · Fuselage Main, Floor Beam
  > DURING C3 C-CHECK, INSPECTION NOTED SEVERAL NUT PLATE HOLES ON FRAME Y-1292 BETWEEN FRAME 66 AND FRAME 68 HAS CORROSION. MAINTENANCE REMOVED AND REPLACED FLOORBEAM IN ACCORDANCE WITH A319 SRM 51-42-11.
- [SDR F3LA200800600](https://openairdocs.org/sdr/F3LA200800600.md): Floorbeam · corroded · Sep 6, 2008 · N929FR · Airbus A319111 · Fuselage Main, Floor Beam
  > REF NON ROUTINE C050600. DURING C3 C-CHECK, INSPECTION NOTED FWD NUT PLATE HOLE ON FRAME Y-1292 AT FRAME 66, HAD CORROSION. MAINT REMOVED CORROSION FROM HOLE, FABRICATED REPAIR BUSHING AND INSTALLED IAW WITH THE REQUIREMENTS OF ENGINEERING AUTHORIZATION NR A9
- [SDR F3L2008F00005](https://openairdocs.org/sdr/F3L2008F00005.md): Floor Support · corroded · Sep 6, 2008 · N929FR · Airbus A319111 · Fuselage Main, Floor Beam
  > REF: NON ROUTINE C050602. DURING C3 C-CHECK, INSPECTION NOTED SEVERAL NUT PLATE HOLES ON FRAME Y-1292 BETWEEN FRAME 66 AND FRAME 68, HAD CORROSION. MAINTENANCE REMOVED AND REPLACED FLOORBEAM IAW WITH THE REQUIREMENTS OF A319 SRM 51-42-11. UPON COMPLETION OF TH
- [SDR F3LA200800599](https://openairdocs.org/sdr/F3LA200800599.md): Floorbeam · corroded · Sep 4, 2008 · N929FR · Airbus A319111 · Fuselage Main, Floor Beam
  > REF NON ROUTINE C050605. DURING C3 C-CHECK, INSPECTION NOTED SEVERAL NUT PLATE HOLES ON FRAME Y-1292 BETWEEN FRAME 66 AND FRAME 68, HAD CORROSION. MAINT REMOVED CORROSION FROM HOLES, FABRICATED REPAIR PROFILE AND FILLER, AND INSTALLED IAW THE REQUIREMENTS OF
- [SDR FELA200800597](https://openairdocs.org/sdr/FELA200800597.md): Floor Panel · corroded · Sep 4, 2008 · N929FR · Airbus A319111 · Fuselage Floor Panel
  > REFERENCE NON ROUTINE C050515. DURING C3 C-CHECK INSPECTION NOTED FLOOR PANEL 261FF HAS CORROSION ON LOWER SURFACE. MX R&R FLOOR PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 AMM 53-42-12 PB 401. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND
- [SDR F3LA200800596](https://openairdocs.org/sdr/F3LA200800596.md): Floor Panel · punctured · Sep 4, 2008 · N929FR · Airbus A319111 · Fuselage Floor Panel
  > REFERENCE NON ROUTINE C050458. DURING C3 C-CHECK INSPECTION NOTED TRANSITION PANEL 131CF WAS PUNCTURED. MX REPAIRED CARGO COMPARTMENT TRANSITION PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR, IT WAS
- [SDR F3LA200800595](https://openairdocs.org/sdr/F3LA200800595.md): Floor Panel · punctured · Sep 4, 2008 · N929FR · Airbus A319111 · Fuselage Floor Panel
  > REFERENCE NON ROUTINE C050457. DURING C3 C-CHECK INSPECTION NOTED TRANSITION PANEL 131EG WAS PUNCTURED. MX REPAIRED CARGO COMPARTMENT TRANSITION PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR, IT WAS
- [SDR F3LA200800594](https://openairdocs.org/sdr/F3LA200800594.md): Floor Panel · punctured · Sep 4, 2008 · N929FR · Airbus A319111 · Fuselage Floor Panel
  > REFERENCE NON ROUTINE C050375. DURING C3 C-CHECK, INSPECTION NOTED TRANSITION PANEL 161CF WAS PUNCTURED. MX REPAIRED CARGO COMPARTMENT TRANSITION PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR, IT WA
- [SDR F3LA200800593](https://openairdocs.org/sdr/F3LA200800593.md): Floor Panel · punctured · Sep 4, 2008 · N929FR · Airbus A319111 · Fuselage Floor Panel
  > REFERENCE NON ROUTINE C050374. DURING C3 C-CHECK, INSPECTION NOTED TRANSITION PANEL 161BF WAS PUNCTURED. MX REPAIRED CARGO COMPARTMENT TRANSITION PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR, IT WA
- [SDR F3LA200800592](https://openairdocs.org/sdr/F3LA200800592.md): Floor Panel · punctured · Sep 4, 2008 · N929FR · Airbus A319111 · Fuselage Floor Panel
  > REFERENCE NON ROUTINE C050372. DURING C3 C-CHECK, INSPECTION NOTED TRANSITION PANEL I51FF WAS PUNCTURED. MX REPAIRED CARGO COMPARTMENT TRANSITION PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR, IT WA
- [SDR F3LA200800591](https://openairdocs.org/sdr/F3LA200800591.md): Floor Panel · punctured · Sep 4, 2008 · N929FR · Airbus A319111 · Fuselage Floor Panel
  > REFERENCE NON ROUTINE C050370. DURING C3 C-CHECK, INSPECTION NOTED TRANSITION PANEL I51UG WAS PUNCTURED. MX REPAIRED CARGO COMPARTMENT TRANSITION PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR, IT WA
- [SDR F3LA200800590](https://openairdocs.org/sdr/F3LA200800590.md): Floor Panel · punctured · Sep 4, 2008 · N929FR · Airbus A319111 · Fuselage Floor Panel
  > REFERENCE NON ROUTINE C050368. DURING C3 C-CHECK, INSPECTION NOTED TRANSITION PANEL I51TG WAS PUNCTURED. MX REPAIRED CARGO COMPARTMENT TRANSITION PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR, IT WA
- [SDR F3LA200800589](https://openairdocs.org/sdr/F3LA200800589.md): Floor Panel · punctured · Sep 4, 2008 · N929FR · Airbus A319111 · Fuselage Floor Panel
  > REFERENCE NON ROUTINE C050366. DURING C3 C-CHECK, INSPECTION NOTED TRANSITION PANEL I52UG WAS PUNCTURED. MX REPAIRED CARGO COMPARTMENT TRANSITION PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR, IT WA
- [SDR F3LA200800598](https://openairdocs.org/sdr/F3LA200800598.md): Floor Panel · corroded · Sep 4, 2008 · N929FR · Airbus A319111 · Fuselage Floor Panel
  > REFERENCE NON ROUTINE C050516. DURING C3 C-CHECK, INSPECTION NOTED FLOOR PANEL 262FF HAS CORROSION ON LOWER SURFACE. MX R&R FLOOR PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 AMM 53-42-12 PB 401. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUN
- [SDR F3LA200800602](https://openairdocs.org/sdr/F3LA200800602.md): Hinge · damaged · Sep 3, 2008 · N929FR · Airbus A319111 · Spoilers
  > REF NON ROUTINE C050746. DURING C3 C-CHECK, INSP FOUND DAMAGE ON THE RT NR (4) SPOILER ANTI-ROTATION WEB. MAINT MACHINED AREA, FABRICATED REINFORCING PLATE AND PROTECTED AREA IAW EA NR A9-57R-30609. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACC
- [SDR F3LA200800603](https://openairdocs.org/sdr/F3LA200800603.md): Hinge · damaged · Sep 3, 2008 · N929FR · Airbus A319111 · Spoilers
  > REF: NOT ROUTINE C050745. DURING C3 C-CHECK, INSPECTION FOUND DAMAGE ON THE RT NR (2) SPOILER ANTI-ROTATION WEB. MAINT MACHINED AREA, FABRICATED REINFORCING PLATE AND PROTECTED AREA IAW ENGINEERING AUTHORIZATION NR A9-57R-30610. UPON COMPLETION OF THE REPAIR,
- [SDR F3LA200800409](https://openairdocs.org/sdr/F3LA200800409.md): Unknown · odor · Jul 1, 2008 · N929FR · Airbus A319111 · Air Distribution System
  > DURING FLIGHT, FLIGHT CREW NOTED AN ODOR OF GAS IN AFT GALLEY. MAINT INSPECTED AC FOR UNSATISFACTORY CABIN AIR QUALITY IAW TSM 21-00-00-810-802. NO ODOR OR SOURCE OF ODOR WAS NOTED. FIRE DEPARTMENT AND HAZMAT CREW INSPECTED THE CABIN AND CARGO COMPARTMENT,

Next page: https://openairdocs.org/deregistered/N929FR-2015-11-16/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 = 'N929FR' AND deregistration_id = 'N929FR-2015-11-16'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N929FR-2015-11-16/reports

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