# Service difficulty reports: N936FR, cancelled Nov 6, 2012

A list on [N936FR, cancelled Nov 6, 2012](https://openairdocs.org/deregistered/N936FR-2012-11-06.md).

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

- [SDR F3LA2011101800685](https://openairdocs.org/sdr/F3LA2011101800685.md): Solenoid Valve · failed · Oct 14, 2011 · N936FR · Airbus A319111 · Cabin Cooling System
  > A/C PACK 2 FAILED IN FLIGHT. PACK 1 ON MEL SO PACK 2 FAIL CAUSED A CABIN DEPRESSURIZATION AND 02 MASK TO DEPLOY. R & R PRESSURE REGULATOR VALVE SOLENOID 10HA2 IAW AMM 36-11-55, PB 401. OP'S AND LEAK CHECKED GOOD.
- [SDR F3LA2011032100616](https://openairdocs.org/sdr/F3LA2011032100616.md): Servo · slow · Mar 16, 2011 · N936FR · Airbus A319111 · Elevator Control System
  > ON ROTATION ACFT ROLLS RT REGARDLESS OF WIND. PERFORMED FLT CONTROL MOVEMENT CHECKS FOUNFD LT ELEVATOR SERVO SLOW TO REACT. REF LP 596444, ITEM 1, R & R SERVO CONTROL ELEVATOR LT GREEN HYD REF AMM 27-34-51-400-001 AND 27-34-51-0000.001, OPS CHECK NORMAL.
- [SDR F3LA2011022100607](https://openairdocs.org/sdr/F3LA2011022100607.md): Computer · malfunctioned · Feb 17, 2011 · N936FR · Airbus A319111 · Flight Management Computing Hardware System
  > AT LIFT OFF, AN UNCOMMANDED ACFT ROLLED RT. AT TOUCHDOWN, AT SPEEDBRAKE DEPLOYMENT, ACFT AGAIN ROLLED RT AND REQUIRED SIGNIFICANT LT AILERON INPUT TO KEEP LT MLG ON THE GROUND. REPLACED NR 1 SEC IAW AMM 27-94-34, PB 401. OPS CHECKED GOOD AND OPS CHECK FIGHT
- [SDR F3LA2011011800585](https://openairdocs.org/sdr/F3LA2011011800585.md): Sill · corroded · Jan 7, 2011 · N936FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > L2 DOOR SILL BEAM HAS 3 SQ INCH OF CORROSION AND IS OUT OF LIMITS. R & R L2 DOOR SILL BEAM IAW SRM 51-72-11, PG 1-2.
- [SDR F3LA2011011800584](https://openairdocs.org/sdr/F3LA2011011800584.md): Sill · corroded · Jan 7, 2011 · N936FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > R2 DOOR SILL BEAM HAS 1 SQ INCH OF CORROSION AND IS OUT OF LIMITS. R & R R2 DOOR SILL BEAM IAW SRM 51-72-11 PG 1-2.
- [SDR F3LA2011011800583](https://openairdocs.org/sdr/F3LA2011011800583.md): Shear Plate · corroded · Jan 7, 2011 · N936FR · Airbus A319111 · Fuselage Main, Structure
  > LT SHEAR PLATE BETWEEN FRAMES 69 TO 70 HAS 3 SQ INCHES OF CORROSION AND IS OLD CONFIGURATION. R & R SHEAR PLATE WITH NEW CONFIGURATION IAW EO AO-53EO-31434.
- [SDR F3LA2011011800582](https://openairdocs.org/sdr/F3LA2011011800582.md): Shear Plate · corroded · Jan 7, 2011 · N936FR · Airbus A319111 · Fuselage Main, Structure
  > RT SHEAR PLATE BETWEEN FRAMES 69 TO 70 HAS 8 SQ INCHES OF CORROSION AND IS OLD CONFIGURATION. R & R SHEAR PLATE WITH NEW CONFIGURATION IAW EO AO53EO31434.
- [SDR F3LA2011011800581](https://openairdocs.org/sdr/F3LA2011011800581.md): Shock Absorber · scratched · Jan 7, 2011 · N936FR · Airbus A319111 · Main Landing Gear Strut/Axle/Truck
  > LT MLG SHOCK ABSORBER SCRATCHED IN CHROME AREA. 60 TO 80 SCRATCHES 18 INCHES LONG X.003 INCHES DEEP ON FWD SIDE OF STRUT. R & R LT MLG SHOCK ABSORBER IAW AMM 32-11-13-020-058B AND 32-11-13-420-054B.
- [SDR F3LA2011010600580](https://openairdocs.org/sdr/F3LA2011010600580.md): Floor Panel · punctured · Jan 6, 2011 · N936FR · Airbus A319111 · Fuselage Floor Panel
  > C-CHECK: NON ROUTINE N0665; AFT CARGO COMPARTMENT FLOOR PANEL 151AE HAS 3 EACH PUNCTURES. REPAIRED 3 EACH PUNCTURES WITH WET LAYUP IAW SRM 53-02-00, PARA 8B.
- [SDR F3LA2011010600579](https://openairdocs.org/sdr/F3LA2011010600579.md): Floor Panel · punctured · Jan 6, 2011 · N936FR · Airbus A319111 · Fuselage Floor Panel
  > C-CHECK: NON ROUTINE N0660; AFT CARGO COMPARTMENT FLOOR PANEL 151DE HAS 2 EA PUNCTURES. REPAIRED 2 EACH PUNCTURES IAW SRM 53-02-00, PARA 8B.
- [SDR F3LA2011010600578](https://openairdocs.org/sdr/F3LA2011010600578.md): Floor Panel · punctured · Jan 6, 2011 · N936FR · Airbus A319111 · Fuselage Floor Panel
  > C-CHECK: NON ROUTINE N0659; AFT CARGO COMPARTMENT FLOOR PANEL 152TG HAS 1 INCH PUNCTURE. REPAIRED PUNCTURE WITH WET LAYUP REPAIR IAW SRM 53-02-00, PARA 8B.
- [SDR F3LA2011010600577](https://openairdocs.org/sdr/F3LA2011010600577.md): Floorboard · punctured · Jan 6, 2011 · N936FR · Airbus A319111 · Fuselage Floor Panel
  > C-CHECK: NON ROUTINE NR N0657; AFT CARGO COMPARTMENT FLOOR PANEL 162CF PUNCTURED. REPAIR PUNCTURE WITH WET LAYUP REPAIR IAW SRM 53-02-00, PARA 8B.
- [SDR F3LA2011010600576](https://openairdocs.org/sdr/F3LA2011010600576.md): Floor Panel · delaminated · Jan 6, 2011 · N936FR · Airbus A319111 · Fuselage Floor Panel
  > C-CHECK: NON ROUTINE N0644; CABIN FLOOR PANEL 242BF DELAMINATED. REPAIRED 56 SQUARE INCHES OF DEBONDED TOP GLASS LAYER OF PANEL 242BF USING MYLAR FOIL IAW SRM 53-02-00, PARA 8J.
- [SDR F3LA2011010600575](https://openairdocs.org/sdr/F3LA2011010600575.md): Skin · gouged · Jan 6, 2011 · N936FR · Airbus A319111 · Engine Thrust Reverser
  > C-CHECK: NON ROUTINE N0633; NR 2 ENGINE OTBD THRUST REVERSER LOWER BLOCKER INTERNAL SIDE THE PERFORATED SKIN HAS A GOUGE MEASURING.7500 INCH LONG,.2500 INCH WIDE AND.115 INCH DEEP. REPAIRED IAW CMM 78-32-36, REPAIR NR8.
- [SDR F3LA2011010600574](https://openairdocs.org/sdr/F3LA2011010600574.md): Cowl Door · dented · Jan 6, 2011 · N936FR · Airbus A319111 · Engine Thrust Reverser
  > C-CHECK: NON ROUTINE NR N0636; NR 2 ENGINE OTBD THRUST REVERSERS INNER PERFORATED COWL BELOW THE UPPER BLOCKER DOOR THERE IS A DENT MEASURING.1250 INCH CIRCUMFERENCE AND.030 INCHES DEEP. REPAIRED 1 INCH DENT IAW CMM 78-32-36, REPAIR NR8.
- [SDR F3LA2011010600573](https://openairdocs.org/sdr/F3LA2011010600573.md): Floor Panel · damaged · Jan 6, 2011 · N936FR · Airbus A319111 · Fuselage Floor Panel
  > C-CHECK: NON ROUTINE NR N0282; AFT CARGO FLOOR PANEL 152WG DAMAGED, SKIN SEPARATED FROM HONEYCOMB. FABRICATED REPLACEMENT PANEL IAW IRM 9701, REV G.
- [SDR F3LA2011010600572](https://openairdocs.org/sdr/F3LA2011010600572.md): Floorboard · damaged · Jan 6, 2011 · N936FR · Airbus A319111 · Fuselage Floor Panel
  > C-CHECK: NON ROUTINE N0278; MAIN CABIN FLOORBOARD 252NF HAS COMPOSITE DAMAGE DAMAGE 40 SQUARE INCHES. REPAIRED 40 SQUARE OF COMPOSITE DAMAGE, IAW A319 SRM 53-02-00 PARAGRAPH 8J.
- [SDR F3LA2009071700106](https://openairdocs.org/sdr/F3LA2009071700106.md): Floor Panel · cracked · Jul 14, 2009 · N936FR · Airbus A319111 · Fuselage Floor Panel
  > REF: NON ROUTINE C064113. DURING C3 C-CHECK, INSP NOTED THE L2 DOOR FWD SIDE FLOOR PANEL IS CRACKED. MX REMOVED AND REPLACED THE FWD L2 DOOR BLANKING PLATE IAW AMM 52-13-31-000-007 AND 52-13-31-400-007.
- [SDR F3LA2009071700105](https://openairdocs.org/sdr/F3LA2009071700105.md): Floorbeam · corroded · Jul 12, 2009 · N936FR · Airbus A319111 · Fuselage Main, Floor Beam
  > DURING C3 C-CHECK, INSP NOTED CORROSION IN AND AROUND NUT CLIP HOLES ON FLOORBEAM Y1292 RT, BETWEEN FR 66 AND FR 68. CORROSION WAS FOUND BEYOND SRM LIMITS. MX REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-44-11, 51-72-11 AND EO A0-53T-11472.
- [SDR F3LA2009071700104](https://openairdocs.org/sdr/F3LA2009071700104.md): Floorbeam · corroded · Jul 12, 2009 · N936FR · Airbus A319111 · Fuselage Main, Floor Beam
  > DURING C3 C-CHECK, INSP NOTED CORROSION IN AND AROUND NUT CLIP HOLES ON FLOORBEAM Y1292 LT, BETWEEN FRAME 66 AND FRAME 68. CORROSION WAS FOUND BEYOND SRM LIMITS. MX REMOVED AND REPLACED THE FLOORBEAM IAW A319 SRM 51-42-11 AND DWG D53475815.
- [SDR F3LA2009071500103](https://openairdocs.org/sdr/F3LA2009071500103.md): Shear Plate · corroded · Jul 12, 2009 · N936FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C3 C-CHECK, INSP NOTED THAT RT LATERAL SHEAR PLATE BETWEEN FR 68 AND FR 70 AT STR 23 RT SHOWS EVIDENCE OF CORROSION AROUND NUT CLIPS. MX REMOVED AND REPLACED THE SHEAR WEB AND SUPPORT ASSY IAW SRM 51-42-11 PARA 6 AND 7.
- [SDR F3LA2009071500100](https://openairdocs.org/sdr/F3LA2009071500100.md): Support · corroded · Jul 12, 2009 · N936FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C3 C-CHECK, INSP NOTED THAT THE RT LATERAL SHEAR PLATE BETWEEN FR 68 AND FR 70 AT STR 23 RT, SHOWS EVIDENCE OF CORROSION AROUND NUT CLIPS. MX REMOVED AND REPLACED THE SHEAR WEB AND SUPPORT ASSY IAW SRM 51-42-11 PARA 6 AND 7.
- [SDR F3LA2009071500102](https://openairdocs.org/sdr/F3LA2009071500102.md): Shear Plate · corroded · Jul 12, 2009 · N936FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C3 C-CHECK, INSP NOTED LT LATERAL SHEAR PLATE BETWEEN FR 68 AND FR 70 AT STR 23 LT SHOWS EVIDENCE OF CORROSION AROUND NUT CLIPS. MX REMOVED AND REPLACED THE SHEAR WEB AND SUPPORT ASSY IAW SRM 51-42-11 PARA 6 AND 7.
- [SDR F3LA2009071500101](https://openairdocs.org/sdr/F3LA2009071500101.md): Support · corroded · Jul 12, 2009 · N936FR · Airbus A319111 · Fuselage Miscellaneous Structure
  > DURING C3 C-CHECK, INSP NOTED THE LT LATERAL SHEAR PLATE BETWEEN FR 68 AND FR 70 AT STR 23 LT SHOWS EVIDENCE OF CORROSION AROUND NUT CLIPS. MX REMOVED AND REPLACED THE SHEAR WEB AND SUPPORT ASSY IAW A319 SRM 51-42-11 PARAGRAPH 6 AND 7.
- [SDR F3LA2009072000107](https://openairdocs.org/sdr/F3LA2009072000107.md): Strut · chafed · Jul 11, 2009 · N936FR · Airbus A319111 · Nose/Tail Landing Gear Strut/Axle
  > DURING C3 C-CHECK, INSP NOTED THE ELECTRICAL CABLE FOR THE TOWING BYPASS SWITCH WAS RUBBING ON THE NLG STRUT. MX REMOVED DAMAGE, PERFORMED FLUORESCENT PENETRANT INSP AND ROTORY FLAP PEENED BLENDED AREAS IAW SRM 51-73-00 AND EA A9-32R-31199. (MAJOR REPAIR)
- [SDR F3LA200700046](https://openairdocs.org/sdr/F3LA200700046.md): Light · inoperative · Mar 19, 2007 · N936FR · Airbus A319111 · Emergency Lighting
  > MAINTENANCE REPORTED RT AFT EMERGENCY OVERWING OUTSIDE LIGHT (62WL) INOP. REPLACED LIGHT ASSY (62WL) IAW 33-51-15-400-001.
- [SDR F3LA200600086](https://openairdocs.org/sdr/F3LA200600086.md): Light · failed · Jul 29, 2006 · N936FR · Airbus A319111 · Emergency Lighting
  > EPSU TEST FAILED IAW HEAVY CHECK WORK CARD. REPLACED RT OVERWING EXIT HATCH HANDLE LIGHT IAW MM 23-73-47, PB 401 AND 33-51-11-420-052A, PERFORMED ANOTHER EPSU TEST AND CHECKED GOOD.

## 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 = 'N936FR' AND deregistration_id = 'N936FR-2012-11-06'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N936FR-2012-11-06/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.