# Service difficulty reports: N924FR, cancelled Apr 28, 2016

A list on [N924FR, cancelled Apr 28, 2016](https://openairdocs.org/deregistered/N924FR-2016-04-28.md).

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

- [SDR F3LA2015080701143](https://openairdocs.org/sdr/F3LA2015080701143.md): Light · inoperative · Aug 6, 2015 · N924FR · Airbus A319111 · Emergency Lighting
  > LIGHT INOPERATIVE AT LT EMER ESCAPE HATCH HANDLE. R & R EMER LIGHT 70WL1. OPERATIONS CHECKED GOOD IAW AMM 33-51-11-400-001-A. REF LOG PAGE 895364 ITEM 2.
- [SDR F3LA2014022401024](https://openairdocs.org/sdr/F3LA2014022401024.md): Shear Plate · cracked · Feb 13, 2014 · N924FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > AIRCRAFT OUT OF SERVICE DUE TO C7 S2 CHECK. AFT MAIN CABIN LT SHEAR PLATE HAS CRACK AT FR 69 - FR 70 STRINGER Y 1292. R & R SHEAR PLATE, AIRBUS A319 SRM 53-41-11 PAGE 6 EO A0-53EO-31434.
- [SDR F3LA2014022401023](https://openairdocs.org/sdr/F3LA2014022401023.md): Floorbeam · corroded · Feb 3, 2014 · N924FR · Airbus A319111 · Fuselage Main, Floor Beam
  > AIRCRAFT OUT OF SERVICE DUE TO C7 S2 CHECK. MAIN CABIN FLOOR BEAM RT AT Y 1292, FR 65 - FR 66 HAS CORROSION, BEAM CORROSION IS OUT OF LIMITS. R & R BEAM, AIRBUS A319 SRM 51-42-11 PAR 6.
- [SDR F3LA2014022401022](https://openairdocs.org/sdr/F3LA2014022401022.md): Floorbeam · corroded · Jan 31, 2014 · N924FR · Airbus A319111 · Fuselage Main, Floor Beam
  > AIRCRAFT OUT OF SERVICE DUE TO C7 S2 CHECK. FWD CABIN FLOOR BEAM AT FR 20 RT, Y 1292 HAS LIGHT CORROSION. REMOVED CORROSION ON FLOOR BEAM AT FR 20 RT, Y 1292 IN FWD MAIN CABIN. ORIGINAL THICKNESS.079 INCHES, REMAINING THICKNESS.068 INCHES FOUND TO BE WITH
- [SDR F3LA2014022401021](https://openairdocs.org/sdr/F3LA2014022401021.md): Floorbeam · corroded · Jan 31, 2014 · N924FR · Airbus A319111 · Fuselage Main, Floor Beam
  > AIRCRAFT OUT OF SERVICE DUE TO C7 S2 CHECK. FWD CABIN FLOOR BEAM AT FR 20 LT, Y 1292 HAS LIGHT CORROSION. REMOVED CORROSION ON FLOOR BEAM AT FR 20 LT, Y 1292 IN FWD MAIN CABIN. ORIGINAL THICKNESS.079 INCHES, REMAINING THICKNESS.071 INCHES, FOUND TO BE WIT
- [SDR F3LA2014022401020](https://openairdocs.org/sdr/F3LA2014022401020.md): Cover Plate · corroded · Jan 31, 2014 · N924FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > AIRCRAFT OUT OF SERVICE DUE TO C7 S2 CHECK. AFT CARGO COMPARTMENT DOOR SILL SUB FLOOR COVER PLATE CORRODED IN SPOTS FROM FR 58 TO FR 59. REMOVED SURFACE CORROSION FROM DOOR SILL COVER PLATE, ORIGINAL MATERIAL THICKNESS.080 INCHES, MEASURED MATERIAL LOSS IS
- [SDR F3LA2010041100380](https://openairdocs.org/sdr/F3LA2010041100380.md): Structure · damaged · Apr 7, 2010 · N924FR · Airbus A319111 · Flight Compartment Windows
  > REF LOG PAGE 503298, ITEM 1. ON DESCENT, HAD A LOUD POP FROM THE CAPTAIN'S SLIDING WINDOW, WINDOW THAN BEGAN TO OVERHEAT. SOON THERE AFTER GOT LIGHT FUMES IN THE COCKPIT. PERFORMED INSP OF THE CAPTAIN'S SLIDING WINDOW REF AMM 56-12-11-200-001, NO DEFECTS NOTED
- [SDR F3LA2009111800232](https://openairdocs.org/sdr/F3LA2009111800232.md): Inlet · damaged · Nov 14, 2009 · N924FR · Airbus A319111 · Engine Air Intake System
  > THE FLIGHT CREW MADE AN AIR RETURN DUE TO MULTIPLE BIRD STRIKES DURING CLIMB OUT CAUSING THE NR 2 ENG COMPRESSOR TO STALL. MX REMOVED AND REPLACED THE NR 2 ENG ASSY AND INLET COWL ASSY, REFERENCE MP71042-01 AND MP71042-02. MX PERFORMED AN OPS CHECK, LEAK CHEC
- [SDR F3LA2009111800231](https://openairdocs.org/sdr/F3LA2009111800231.md): Engine · bird ingestion · Nov 14, 2009 · N924FR · Airbus A319111 · Engine (Turbine/Turboprop)
  > FLIGHT CREW MADE AN AIR RETURN DUE TO MULTIPLE BIRD STRIKES DURING CLIMB OUT CAUSING THE NR 2 ENGINE COMPRESSOR TO STALL. MX REMOVED AND REPLACED THE NR 2 ENG ASSY AND INLET COWL ASSY, REFERENCE MP71042-01 AND MP71042-02. MX PERFORMED AN OPS CHECK, LEAK CHEC
- [SDR F3LA2009072800118](https://openairdocs.org/sdr/F3LA2009072800118.md): Power Supply · failed · Jul 26, 2009 · N924FR · Airbus A319111 · Emergency Lighting
  > DURING C4 C-CHECK, INSP NOTED THE AFT EMERGENCY POWER SUPPLY UNIT FAILED. MX REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT AND PERFORMED OPS TEST IAW AMM 33-51-38-000-001 AND 33-51-38-400-001.
- [SDR F3LA2009072700113](https://openairdocs.org/sdr/F3LA2009072700113.md): Profile · corroded · Jul 24, 2009 · N924FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C4 C-CHECK, INSP NOTED THE AFT CARGO COMPARTMENT STRUCTURAL PROFILE AT FRAME 56 HAS CORROSION AT THE NUT PLATES. MX PERFORMED MAJOR REPAIR BY REMOVING CORRODED PROFILE, FABRICATING REPLACEMENT PROFILE AND INSTALLING REPLACEMENT PROFILE IAW SRM 51-42-11
- [SDR F3LA2009072700116](https://openairdocs.org/sdr/F3LA2009072700116.md): Support Bracket · corroded · Jul 23, 2009 · N924FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C4 C-CHECK, INSP NOTED THAT THE LT SUPPORT BRACKET AT FRAME 59 HAS CORROSION IN THE FASTENER HOLES. MX REMOVED AND REPLACED THE SUPPORT BRACKET IAW SRM 51-42-11.
- [SDR F3LA2009072700115](https://openairdocs.org/sdr/F3LA2009072700115.md): Floor Support · corroded · Jul 23, 2009 · N924FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C4 C-CHECK, INSP NOTED THAT THE CENTER LONGITUDINAL SUPPORT FROM FR 58 TO FR 59 HAS CORROSION AT THE NUT PLATE HOLE. MX REMOVED AND REPLACED THE SUPPORT IAW SRM 51-42-11.
- [SDR F3LA2009072700114](https://openairdocs.org/sdr/F3LA2009072700114.md): Bracket · corroded · Jul 23, 2009 · N924FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING DEN C4 C-CHECK, INSP NOTED AT FR 59, THE AFT CENTER SUPPORT BRACKET HAS CORROSION IN FASTENER HOLES. MX PERFORMED MAJOR REPAIR BY REMOVING CORRODED SUPPORT BRACKET, FABRICATING SUPPORT BRACKET AND INSTALLING IAW SRM 51-42-11, 51-44-11, 51-75-12 AND DWG
- [SDR F3LA2009072700112](https://openairdocs.org/sdr/F3LA2009072700112.md): Support Fitting · corroded · Jul 23, 2009 · N924FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C4 C-CHECK, INSP NOTED THAT THE CENTER SUPPORT FITTING UNDER FRAME 58 HAS CORROSION AT NUT PLATE HOLES. MX REMOVED AND REPLACED THE CENTER SUPPORT FITTING IAW SRM 51-42-11.
- [SDR F3LA2009072700117](https://openairdocs.org/sdr/F3LA2009072700117.md): Profile · corroded · Jul 22, 2009 · N924FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C4 C-CHECK, INSP NOTED THAT THE STRUCTURAL PROFILE AT FR 59 HAS SURFACE CORROSION AT NUT PLATE HOLES. MX REMOVED AND REPLACED THE PROFILE AT FR 59 IAW SRM 51-42-11.
- [SDR F3LA2009072700111](https://openairdocs.org/sdr/F3LA2009072700111.md): Support Fitting · corroded · Jul 22, 2009 · N924FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C4 C-CHECK, INSP NOTED THAT THE AFT CARGO CENTER SUPPORT FITTING ON FRAME 56 HAS CORROSION AT NUT PLATE HOLE. MX REMOVED AND REPLACED FITTING IAW SRM 51-42-00 AND 51-42-11.
- [SDR F3LA2009072700110](https://openairdocs.org/sdr/F3LA2009072700110.md): Cowling · damaged · Jul 20, 2009 · N924FR · Airbus A319111 · Nacelle/Pylon, Main Frame
  > DURING C4 C-CHECK, INSP NOTED THAT THE NR 2 ENGINE OTBD FAN COWL HAS DAMAGE ON THE INSIDE OF COWL, 2 FEET FROM THE TOP AND 1 FOOT FROM THE T/E. MX PERFORMED MAJOR REPAIR TO FAN COWL IAW SRM 54-02-00 AND 54-20-00.
- [SDR F3LA2009072700109](https://openairdocs.org/sdr/F3LA2009072700109.md): Battery Pack · no test · Jul 18, 2009 · N924FR · Airbus A319111 · Emergency Lighting
  > DURING C4 C-CHECK, INSP NOTED THAT THE AFT LT EMERGENCY POWER SUPPLY UNIT BATTERY FAILS CAPACITY CHECK. MX REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT AND PERFORMED OPS CHECK IAW AMM 33-51-38 PB 401.
- [SDR F3LA2009012600005](https://openairdocs.org/sdr/F3LA2009012600005.md): Gasket · damaged · Jan 25, 2009 · N924FR · Airbus A319111 · Engine Fuel Indicating System
  > PILOT REPORTED NR 1 ENGINE FAILURE INFLIGHT, RELIGHT UNSUCCESSFUL. MAINTENANCE INSPECTED NR 1 ENGINE AND FOUND THE GASKET AT THE FUEL FLOW TRANSMITTER DAMAGED. MAINTENANCE REMOVED AND REPLACED THE GASKET, PERFORMED LEAK CHECK AND POWER ASSURANCE CHECK IAW A3
- [SDR F3LA2008100600668](https://openairdocs.org/sdr/F3LA2008100600668.md): Servo Control · unresponsive · Oct 4, 2008 · N924FR · Airbus A319111 · Steering Unit
  > ON TAXI OUT, SPEED LESS THAN 10KTS, AIRCRAFT SWERVED TO THE LEFT (UNCOMMANDED) AND DID NOT RESPOND TO STEERING IMPUTS. STOPPED AIRCRAFT USING BRAKES, RECEIVED ELECTRONIC CENTRALIZED AIRCRAFT MONITORING MESSAGE: WHEEL N/W STEERING FAULT. MAINTENANCE REMOVED
- [SDR F3LA200800616](https://openairdocs.org/sdr/F3LA200800616.md): Pin · failed · Sep 18, 2008 · N924FR · Airbus A319111 · Nose/Tail Landing Gear
  > FLIGHT NR 3183. NR 1 ELECTRONIC CENTRALIZED ACFT MONITOR INDICATED LANDING GEAR CONTROL INTERFACE UNIT FAULT. ACFT VIBRATION WAS FELT AFTER LANDING AND ACFT STOPPED ON RUNWAY. MX FOUND NOSE GEAR TIRES TURNED 90 DEGREES AND SEVERAL BROKEN NLG PARTS ON THE RU
- [SDR F3LA200800041](https://openairdocs.org/sdr/F3LA200800041.md): Tube · leaking · Jan 31, 2008 · N924FR · Airbus A319111 · Hydraulic System, Main
  > DURING DESCENT & APPROACH, CREW REPORTED AN ECAM INDICATION OF LOW HYD PRESSURE & LOW HYD FLUID LEVEL FOR GREEN HYDC SYS. AN EMERGENCY DECLARED & CREW MANUALLY EXTENDED MLG. ACFT MADE AN UNEVENTFUL LANDING. MX FOUND A HYD TUBE ASSY LEAKING ON NR 1 ENGINE.
- [SDR F3LA200800035](https://openairdocs.org/sdr/F3LA200800035.md): Floor Panel · damaged · Jan 10, 2008 · N924FR · Airbus A319111 · Fuselage Floor Panel
  > DURING C CHECK INSPECTION, CABIN FLOOR PANEL 241F, LOCATED IN THE COCKPIT, HAD THE SECOND SCREW HOLE, ON THE RIGHT FORWARD SIDE, PULLED THROUGH. MAINTENANCE REPAIRED THE DAMAGE IN ACCORDANCE WITH THE REQUIREMENTS OF EA A8-53R-12384. FOLLOWING COMPLETION OF T
- [SDR F3LA200800021](https://openairdocs.org/sdr/F3LA200800021.md): Cylinder Damper · inoperative · Jan 7, 2008 · N924FR · Airbus A319111 · Emergency Exits
  > DURING C CHECK INSPECTION, THE R1 EMERGENCY DOOR DAMPENER CYLINDER FAILED ITS TEST DUE TO LOW PRESSURE. MAINTENANCE CHARGED THE CYLINDER IN ACCORDANCE WITH THE REQUIREMENTS OF A319 AMM 52-10-00-614-001. UPON COMPLETION OF THE CHARGING, THE CYLINDER PRESSURE
- [SDR F3LA200800020](https://openairdocs.org/sdr/F3LA200800020.md): Cylinder Damper · inoperative · Jan 7, 2008 · N924FR · Airbus A319111 · Emergency Exits
  > DURING C CHECK INSPECTION, THE R2 EMERGENCY DOOR DAMPENER CYLINDER FAILED ITS TEST DUE TO LOW PRESSURE. MAINTENANCE CHARGED THE CYLINDER IN ACCORDANCE WITH THE REQUIREMENTS OF A319 AMM 52-10-00-614-001. UPON COMPLETION OF THE CHARGING, THE CYLINDER PRESSURE
- [SDR F3LA200800019](https://openairdocs.org/sdr/F3LA200800019.md): Battery · inoperative · Jan 7, 2008 · N924FR · Airbus A319111 · Emergency Equipment
  > DURING C CHECK INSPECTION, THE FORWARD FLIGHT ATTENDANT EMERGENCY FLASHLIGHT BATTERY WAS FOUND DEAD. MAINTENANCE REMOVED AND REPLACED THE FLASHLIGHT BATTERY IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 25-65-00. UPON COMPLETION OF THE BATTERY REPLACEMENT, THE
- [SDR F3LA200800034](https://openairdocs.org/sdr/F3LA200800034.md): Shear Plate · corroded · Jan 6, 2008 · N924FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C CHECK INSPECTION, CORROSION WAS FOUND ON THE SHEAR PLATE ON THE RIGHT SIDE, OUTBOARD FLOOR SUPPORT BETWEEN FRAMES 68 AND 70 AT STRINGER 23. MAINTENANCE REMOVED AND REPLACED THE SHEAR PLATE IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-42-11. FO
- [SDR F3LA200800007](https://openairdocs.org/sdr/F3LA200800007.md): Inertia Reel · corroded · Jan 6, 2008 · N924FR · Airbus A319111 · Passenger/Crew Doors
  > DURING C-CHECK INSPECTION, THE R1 DOOR SAFETY TAPE INERTIAL REEL WAS FOUND TO HAVE CORROSION ON IT. MAINTENANCE REMOVED AND REPLACED THE R1 DOOR SAFETY TAPE INERTIA REEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-40-00. FOLLOWING COMPLETION OF THE IN
- [SDR F3LA200800008](https://openairdocs.org/sdr/F3LA200800008.md): Floorbeam · corroded · Jan 6, 2008 · N924FR · Airbus A319111 · Fuselage Main, Floor Beam
  > DURING C-CHECK INSPECTION, CORROSION WAS FOUND ON THE FLOORBEAM, AROUND THE NUT CLIP LOCATIONS (6 EACH) AT THE ATTACH POINTS OF THE FLOOR PANEL, JUST INSIDE THE L2 DOOOR. THE FLOORBEAM WAS FOUND CORRODED (OUT OF LIMITS) IN ACCORDANCE WITH THE REQUIREMENTS OF
- [SDR F3LA200600147](https://openairdocs.org/sdr/F3LA200600147.md): Control Stick · unknown · Oct 23, 2006 · N924FR · Airbus A319111 · Control Column Section
  > FLIGHT CREW REPORTED THAT UPON APPROACH, AT APPROXIMATELY 10 FT ABOVE THE RUNWAY, AIRCRAFT ABRUPTLY NOSED OVER DURING FLARE WITH FULL AFT STICK HELD (HAND-FLOWN APPROACH). NO ECAM WARNINGS OR OTHER INDICATIONS. THE FLIGHT DATA RECORDER HAS BEEN DOWNLOADED AN
- [SDR F3LA200600085](https://openairdocs.org/sdr/F3LA200600085.md): Mask · no test · Jul 28, 2006 · N924FR · Airbus A319111 · Passenger Oxygen System
  > DURING C-2 CHECK, INSPECTION REPORTED MASK BOX OVER L1 DOOR (40WR) DID NOT DROP. REPACKED O2 MASKS OVER L1 DOOR AND OPS CHECKED IAW AMM 35-23-00-720-454. CHECKED GOOD.
- [SDR F3LA200600083](https://openairdocs.org/sdr/F3LA200600083.md): Epsu · no test · Jul 28, 2006 · N924FR · Airbus A319111 · Emergency Lighting
  > DURING C-2 CHECK, INSPECTION REPORTED FWD LT EPSU (EMERGENCY POWER SUPPLY UNIT) FAILED TEST. REPLACED LT FWD EPSU AND PERFORMED OPERATIONAL CHECK. TESTED GOOD.
- [SDR F3LA200600082](https://openairdocs.org/sdr/F3LA200600082.md): Wire · maint error · Jul 27, 2006 · N924FR · Airbus A319111 · Communications System Wiring
  > DURING C-2 CHECK, PRE-RECORDED ANNOUNCEMENT DID NOT COME ON DURING OXYGEN MASK DROP TEST. FOUND PRE-RECORDED ANNOUNCEMENT OUTPUT WIRES CAPPED & STOWED, LIVE TV WIRES IN THEIR PLACE. WIRE 2332-5811 CAPPED & STOWED AT CONNECTOR 166VCA, SHIELDED PAIR WIRE 2332-
- [SDR F3LA200600081](https://openairdocs.org/sdr/F3LA200600081.md): Psu · failed · Jul 27, 2006 · N924FR · Airbus A319111 · Passenger Oxygen System
  > DURING C-2 CHECK, INSPECTION REPORTED THE PASSENGER OXYGEN MASK DOOR AT ROW 7 ABC DID NOT OPEN DURING TEST. REPLACED PASSENGER OXYGEN CONTAINER ASSY PER AMM 35-21-41, PB 401, AND 35-21-41-481-050.
- [SDR F3LA200600080](https://openairdocs.org/sdr/F3LA200600080.md): Rivet · sheared · Jul 27, 2006 · N924FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C-2 CHECK, INSPECTION REPORTED A RIVET HEAD SHEARED OFF AT LT SIDE FWD A/C BAY, FWD LOWER CORNER WEB AT ZONE 191, I/B SIDE OF WEB, LOCATED O/B OF EMERGENCY RAM AIR CONNECTOR. REPLACED SHEARED RIVET PER A319 SRM 51-42-11.
- [SDR F3LA200500047](https://openairdocs.org/sdr/F3LA200500047.md): Controller · malfunctioned · Dec 12, 2005 · N924FR · Airbus A319111 · Pneumatic Distribution System
  > BLOCK TURNBACK. FLIGHT CREW REPORTED LOW PRESSURE BOTH ENGINES DURING START WITH FUMES INTO CABIN. REPLACED BMC NR1. LOW BLEED PRESSURE OPS CHECKED GOOD IAW AMM 36-11-34, PAGE 401. FOUND DE-ICE FLUID IN APU AIR INTAKE WHICH WAS CAUSING FUMES. CLEANED APU

## 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 = 'N924FR' AND deregistration_id = 'N924FR-2016-04-28'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N924FR-2016-04-28/reports

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