# Service difficulty reports: N933FR, cancelled May 23, 2016 A list on [N933FR, cancelled May 23, 2016](https://openairdocs.org/deregistered/N933FR-2016-05-23.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR F3LA2015090401144](https://openairdocs.org/sdr/F3LA2015090401144.md): Bottle · leaking · Aug 23, 2015 · N933FR · Airbus A319111 · Passenger/Crew Doors > R2 DOOR ASSIST BOTTLE EMPTY. SERVICED R2 DOOR ASSIST BOTTLE IAW AMM 52-10-00-614-001-A. REFERENCE NR 25069. - [SDR F3LA2015021701106](https://openairdocs.org/sdr/F3LA2015021701106.md): Warning System · false activation · Feb 14, 2015 · N933FR · Airbus A319111 · Smoke Detection > REFERENCE LOG PAGE 910707 ITEM NR 1. SMOKE LAVATORY SMOKE ECAM ON DESCENT. PERFORMED SDCU BITE TEST AS REQUIRED IAW AMM 26-15-00-410-003. PERFORMED LAVATORY SMOKE DETECTOR TEST AS REQUIRED IAW AMM 26-16-00-710-001. NO DEFECTS NOTED. FIRE DEPARTMENT PERFOR - [SDR F3LA2014051401034](https://openairdocs.org/sdr/F3LA2014051401034.md): Battery Pack · discharged · May 14, 2014 · N933FR · Airbus A319111 · Emergency Lighting > OPERATIONAL TEST OF EMERGENCY LIGHTS FAILED DURING HEAVY SERVICE CHECK. R & R EPSU BATTERY PACK L1WL IAW AMM 33-51-00-920-050-A. - [SDR F3LA2014051401033](https://openairdocs.org/sdr/F3LA2014051401033.md): Battery Pack · discharged · May 14, 2014 · N933FR · Airbus A319111 · Emergency Lighting > OPERATIONAL TEST OF EMERGENCY LIGHTS FAILED DURING HEAVY SERVICE CHECK. R & R EPSU BATTERY PACK 10WL IAW AMM 33-51-00-920-050-A. - [SDR F3LA2014010700953](https://openairdocs.org/sdr/F3LA2014010700953.md): Battery · discharged · Jan 4, 2014 · N933FR · Airbus A319111 · Emergency Lighting > EMERGENCY LIGHTS FAILED EMERGENCY LIGHT TEST. EPSU BATTERY EMERGENCY RT FAULT & 12WL, EMERGENCY EXIT RT BATTERY NEEDS REPLACED. R & R EPSU BATTERY EMERGENCY EXIT RT IAW AMM 33-51-38 PB 401, OPERATIONS CHECKED GOOD. - [SDR F3LA2013070800884](https://openairdocs.org/sdr/F3LA2013070800884.md): Battery Pack · discharged · Jul 8, 2013 · N933FR · Airbus A319111 · Emergency Lighting > EPSU BATTERY 13WL FAILED TEST ON HEAVY SERVICE CHECK. R & R BATTERY ASSEMBLY. OPS CHECK GOOD. REF AMM 33-51-39-000-005A AND AMM 33-51-39-400-005A. - [SDR F3LA2012092500797](https://openairdocs.org/sdr/F3LA2012092500797.md): Servo · faulted · Sep 21, 2012 · N933FR · Airbus A319111 · Steering Unit > IN CRUISE, RECEIVED WHEEL NOSE LANDING WHEEL STEERING FAULT. REPLACED NOSE WHEEL STEERING SERVO CONTROL REF AMM 32-5 1-5 1-ODO-OO1 -A, 32-5 1-51 ·400-00 I-A, TEST OK. NO LEAKS NOTED. - [SDR F3LA2010080800484](https://openairdocs.org/sdr/F3LA2010080800484.md): Control Cable · out of limits · Aug 8, 2010 · N933FR · Airbus A319111 · Rudder Control System > REF AEROFRAME NON-ROUTINE N0491 RUDDER CABLE TENSION ON TESSION REGULATOR IS OUT OF LIMITS. R & R RUDDER TENSION REGULATOR IAW AMM 27-21-48, PAGE 401. OPS CHECK RUDDER IAW AMM 27-24-00-710-001. OPS CHECKS GOOD. - [SDR F3LA2010080800483](https://openairdocs.org/sdr/F3LA2010080800483.md): Sill · corroded · Aug 8, 2010 · N933FR · Airbus A319111 · Fuselage Miscellaneous Structure > MAIN CABIN FLOOR STRUCTURE LONGERON AT OTBD POSITION FRAME 66 HAS A 1 SQ IN ARE OF CORROSION REF NON-ROUTINE N0451. CUT OUT CORROSION AT NUTPLATE HOLE IAW SRM 53-42-14 PRINCIPLE 6 FABRICATED REPAIR ANGLES IAW SRM 53-42-14 PRINCIPLE 6 TREATED PRIMED AND TOP COO - [SDR F3LA2010080800482](https://openairdocs.org/sdr/F3LA2010080800482.md): Floor Panel · damaged · Aug 8, 2010 · N933FR · Airbus A319111 · Fuselage Floor Panel > REF NON=ROUTINE N0691, FWD CARGO FLOOR PANEL 131AF BROKEN COTR APPROX 2.0 IN X 2.5 IN. ACFT IS IN C-CHECK. REPAIR DAMAGE AREA ON PANEL 131AF USING RESIN AND GLASS CLOTH PATCH METHOD IAW SRM 53-02-00, PARA 8B. - [SDR F3LA2010080800480](https://openairdocs.org/sdr/F3LA2010080800480.md): Plate · corroded · Aug 8, 2010 · N933FR · Airbus A319111 · Fuselage Miscellaneous Structure > REF NON-ROUTINECARD N0392, AFT CABIN RT SHEAR PLATE BETWEEN FRAMES 69 AND 70, HAS CORROSION THAT IS OUT OF LIMITS. R & R SHEAR PLATE AT AFT CABIN RT SIDE BETWEEN FRAMES 69 AND 70 IAW SRM 51-42-11 AND EO AO-53E0-31434. - [SDR F3LA2010080300478](https://openairdocs.org/sdr/F3LA2010080300478.md): Floor Panel · damaged · Jul 27, 2010 · N933FR · Airbus A319111 · Fuselage Floor Panel > REF HEAVY MX NON ROUTINE N0604. MAIN CABIN FLOOR PANEL 261 PF HAS COMPOSITE DAMAGE. REPAIRED 9 EACH AREAS OF SKIN DAMAGE ON FLOOR PANEL 261PF USING RESIN AND GLASS CLOTH IAW SRM 53-02-00, PARAGRAPH 8. - [SDR F3LA2010080300479](https://openairdocs.org/sdr/F3LA2010080300479.md): Floor Support · corroded · Jul 26, 2010 · N933FR · Airbus A319111 · Fuselage Miscellaneous Structure > REF HEAVY MX NON ROUTINE N0561. RT CABIN FLOOR AT FRAME 69 TO FRAME 70 SUPPORT EXTRUSION BELOW SHEAR PLATE IS CORRODED. R & R SUPPORT IAW SRM 51-72-11. - [SDR F3LA2009040800073](https://openairdocs.org/sdr/F3LA2009040800073.md): Light · no test · Apr 7, 2009 · N933FR · Airbus A319111 · Emergency Lighting > DURING HEAVY CHECK, INSPECTION NOTED THE L2 DOOR EMERGENCY LIGHT FAILED TO TEST. MAINTENANCE REMOVED AND INSTALLED A NEW SLIDE, REFERENCE AMM 25-62-44 PB 401. - [SDR F3LA2009022400032](https://openairdocs.org/sdr/F3LA2009022400032.md): Strut · damaged · Feb 24, 2009 · N933FR · Airbus A319111 · Nose/Tail Landing Gear Strut/Axle > REFERENCE NON-ROUTINE C057865. DURING C3 C-CHECK, INSP NOTED THE LT NLG AFT GROMMET WORN.005 DEEP,.690 VERTICAL,.520 WIDE, 21 INCHES UP FROM THE BOTTOM OF THE BARREL. MX PERFORMED MAJOR REPAIR, BLENDED DAMAGE, PERFORMED FLAP-PEEN, NDT AND PAINTED IAW EA A9- - [SDR F3LA2009022400033](https://openairdocs.org/sdr/F3LA2009022400033.md): Attach Fitting · cracked · Feb 23, 2009 · N933FR · Airbus A319111 · Fuselage, Landing Gear Attach Fittings > REFERENCE NON-ROUTINE C057626. DURING C3 C-CHECK, MAINTENANCE COMPLIED WITH A MAJOR REPAIR OF THE LT NLG ACTUATOR ATTACH FITTING THAT WAS FOUND CRACKED WHILE PERFORMING EO A0-53EO-2073. REPAIR PERFORMED IAW EA A9-53R-12014 REVISION A, STEPS 1-16. - [SDR F3LA2009022300031](https://openairdocs.org/sdr/F3LA2009022300031.md): Floor Panel · corroded · Feb 19, 2009 · N933FR · Airbus A319111 · Fuselage Floor Panel > REFERENCE NON ROUTINE C058373. DURING C3 C-CHECK, INSPECTION CORROSION ON FLOOR PANEL 262FF. MAINTENANCE REMOVED AND REPLACED FLOOR PANEL WITH NEW, REFERENCE WORK CARD C534103-01 AND AMM 53-42-12-400-002. - [SDR F3LA2009022300030](https://openairdocs.org/sdr/F3LA2009022300030.md): Floor Panel · corroded · Feb 19, 2009 · N933FR · Airbus A319111 · Fuselage Floor Panel > REFERENCE NON-ROUTINE C058372. DURING C3 C-CHECK, INSPECTION NOTED CORROSION ON FLOOR PANEL 261FF. MAINTENANCE REMOVED AND REPLACED FLOOR PANEL WITH NEW, REFERENCE WORK CARD C534103-01 AND AMM 53-42-12-400-002. - [SDR F3LA2009022400034](https://openairdocs.org/sdr/F3LA2009022400034.md): Barrel · damaged · Feb 17, 2009 · N933FR · Airbus A319111 · Nose/Tail Landing Gear Strut/Axle > REFERENCE NON-ROUTINE C057860. DURING C3 C-CHECK, INSP NOTED THE RT NLG AFT GROMMET WORN ON CORNER WEB.002 DEEP,.550 VERTICAL,.500 WIDE, 21.375 INCHES UP FROM THE BOTTOM OF THE BARREL AT INTERSECTION OF LOWER WEB TO BARREL. MX PERFORMED MAJOR REPAIR, BLENDE - [SDR F3LA2009022300029](https://openairdocs.org/sdr/F3LA2009022300029.md): Floorbeam · corroded · Feb 17, 2009 · N933FR · Airbus A319111 · Fuselage Main, Floor Beam > REFERENCE NON ROUTINE C057992. DURING C3 C-CHECK, INSPECTION NOTED CORROSION ON VARIOUS NUT CLIP FASTENER HOLES ON FLOORBEAM Y1292 BETWEEN FRAME 66 AND FRAME 68. MAINTENANCE REMOVED AND REPLACED FLOORBEAM WITH NEW PER SRM 51-42-11. - [SDR F3LA200700361](https://openairdocs.org/sdr/F3LA200700361.md): Roller · broken · Dec 4, 2007 · N933FR · Airbus A319111 · Passenger/Crew Doors > MAINTENANCE REPORTED BROKEN ROLLER BEARING ON L2 SERVICE DOOR OUTER HANDLE/LATCH. REMOVED AND REPLACED CRANK ON THE OUTER CONTROL HANDLE IAW AMM 52-13-21-400-001. OPS CHECK NORMAL. - [SDR F3LA200700173](https://openairdocs.org/sdr/F3LA200700173.md): Floor Panel · damaged · Jul 7, 2007 · N933FR · Airbus A319111 · Fuselage Floor Panel > DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR PANEL 151VE DAMAGED. REPAIRED FLOOR PANEL 151VE IAW SRM 53-02-00. - [SDR F3LA200700172](https://openairdocs.org/sdr/F3LA200700172.md): Panel · damaged · Jul 7, 2007 · N933FR · Airbus A319111 · Fuselage Miscellaneous Structure > DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT TRANSITION PANELS 151BE, 151UG, 161BF, AND 161CF DAMAGED. REPAIRED TRANSITION PANELS IAW SRM 53-02-00, FIG 204. - [SDR F3LA200700171](https://openairdocs.org/sdr/F3LA200700171.md): Panel · damaged · Jul 7, 2007 · N933FR · Airbus A319111 · Fuselage Miscellaneous Structure > DURING C-2 CHECK, INSPECTION REPORTED FWD CARGO COMPARTMENT TRANSITION PANEL 131CF DAMAGED. REPAIRED ONE SKIN PENETRATION IAW SRM 53-02-00, PAGE 204, 205, PARA 2-E, FIG. 201, AND AMM 25-00-00-370-001. ## 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 = 'N933FR' AND deregistration_id = 'N933FR-2016-05-23' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N933FR-2016-05-23/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.