# Service difficulty reports: N901FR, cancelled Feb 12, 2009

A list on [N901FR, cancelled Feb 12, 2009](https://openairdocs.org/deregistered/N901FR-2009-02-12.md).

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

- [SDR F3LA200800410](https://openairdocs.org/sdr/F3LA200800410.md): Stud · broken · Jul 2, 2008 · N901FR · Airbus A319112 · Escape Slide
  > DURING A DAILY CHECK MAINT NOTED THE L1 DOOR EVACUATION SLIDE AT ATTACH BOLT BROKEN AFT SIDE OF L1 DOOR EVACUATION SLIDE. MAINT REMOVED AND REPLACED ATTACH STUD ASSY ON AFT SIDE OF L1 DOOR SLIDE IAW THE REQUIREMENTS OF AMM 25-62-44-400-007. UPON COMPLETION OF
- [SDR F3LA200700367](https://openairdocs.org/sdr/F3LA200700367.md): Hook · damaged · Dec 10, 2007 · N901FR · Airbus A319112 · Escape Slide
  > DURING C-5 CHECK, INSPECTION REPORTED UPON INSTALLATION OF R2 DOOR SLIDE, OPEN/CLOSE HANDLE COULD BE OPERATED BEFORE DOOR WAS IN HOLE. REMOVED AND REPLACED HOOK ON DOOR LOCKING MECHANISM AND PERFORMED OPS CHECK AND RIG CHECK IAW AMM 52-13-21-400-001.
- [SDR F3LA200700366](https://openairdocs.org/sdr/F3LA200700366.md): Hinge Fitting · corroded · Dec 9, 2007 · N901FR · Airbus A319112 · Nacelle/Pylon, Attach Fittings
  > DURING C-5 CHECK, INSPECTION REPORTED NR 2 PYLON T/R COWL FITTINGS AT RIB 1 AND RIB 2 CORRODED. REMOVED AND REPLACED NR 2 PYLON OTBD T/R COWL FITTINGS AT RIBS 1 AND 2 IAW AMM 54-57-17-000-003 AND 54-57-17-420-053.
- [SDR F3LA200700368](https://openairdocs.org/sdr/F3LA200700368.md): Floor Panel · broken · Dec 7, 2007 · N901FR · Airbus A319112 · Fuselage Floor Panel
  > DURING C-5 CHECK, INSPECTION REPORTED FLOOR PANEL 151PE IN AFT CARGO COMPARTMENT BROKEN INTERNALLY. REMOVED PANEL 151PE IAW SRM 51-42-11. DETERMINED PANEL TO BE BROKEN IN HALF (FULL LENGTH OF PANEL) AND OUT OF LIMITS IAW SRM 53-02-00, FIG 206, SHEET 2. REPL
- [SDR F3LA200700365](https://openairdocs.org/sdr/F3LA200700365.md): Shear Plate · corroded · Dec 7, 2007 · N901FR · Airbus A319112 · Fuselage Internal Mounting Structure
  > DURING C-5 CHECK, INSPECTION REPORTED CORROSION ON FWD CARGO COMPARTMENT FLOORBEAM AT FR 28, AND ON THE AFT DOOR SILL. CORROSION WAS CLASSIFIED AS EXFOLIATION. REMOVED AND REPLACED PROFILE PLATE IAW SRM 51-42-11-PAR 2A1.
- [SDR F3LA20700364](https://openairdocs.org/sdr/F3LA20700364.md): Pin · corroded · Dec 5, 2007 · N901FR · Airbus A319112 · Nose/Tail Landing Gear
  > DURING C-5 CHECK, INSPECTION REPORTED PITTING ON SHOULDER OF NLG TORQUE LINK CENTER PIN. REMOVED AND REPLACED NLG TORQUE LINK CENTER PIN IAW 32-21-27-420-050. PERFORMED FUNCTIONAL CHECK OF THE NORMAL EXTENSION AND RETRACTION OF THE NOSE LAND GEAR IAW AMM 32-
- [SDR F3LA200700363](https://openairdocs.org/sdr/F3LA200700363.md): Lock Tab · failed · Dec 5, 2007 · N901FR · Airbus A319112 · Engine Mount Section
  > DURING C-5 CHECK, INSPECTION REPORTED NR 2 ENG AFT MOUNT INBD LWR LOCKING TAB THAT SECURES BOLT FROM ROTATING BLOWN OUT OF ITS SECURING POSITION TO PREVENT BOLT FROM ROTATING. REMOVED AND REPLACED BEARING AT RIB 10 IAW MM 54-51-17-000-003 AND MM 54-51-17-400-
- [SDR F3LA200700370](https://openairdocs.org/sdr/F3LA200700370.md): Battery Pack · no test · Dec 4, 2007 · N901FR · Airbus A319112 · Emergency Lighting
  > DURING C-5 CHECK, INSPECTION REPORTED LT OVERWING EMERGENCY BATTERY EPSU FAILED CAPACITY TEST. REMOVED AND REPLACED EPSU BATTERY AND PERFORMED OPS CHECK IAW AMM 33-51-38-000-002. CHECKED GOOD.
- [SDR F3LA200700372](https://openairdocs.org/sdr/F3LA200700372.md): Battery Pack · no test · Dec 4, 2007 · N901FR · Airbus A319112 · Emergency Lighting
  > DURING C-5 CHECK, INSPECTION REPORTED RT OVERWING EMERGENCY BATTERY EPSU FAILED CAPACITY TEST. REMOVED AND REPLACED EPSU BATTERY AND PERFORMED OPERATIONAL CHECK IAW AMM 33-51-38-PB401. CHECKED GOOD.
- [SDR F3LA200700371](https://openairdocs.org/sdr/F3LA200700371.md): Battery Pack · no test · Dec 4, 2007 · N901FR · Airbus A319112 · Emergency Lighting
  > DURING C-5 CHECK, INSPECTION REPORTED AFT EMERGENCY BATTERY EPSU FAILED CAPACITY TEST. REMOVED AND REPLACED EPSU BATTERY AND PERFORMED OPS CHECK IAW AMM 33-51-38-400-002. CHECKED GOOD.
- [SDR F3LA200700369](https://openairdocs.org/sdr/F3LA200700369.md): Battery Pack · no test · Dec 4, 2007 · N901FR · Airbus A319112 · Emergency Lighting
  > DURING C-5 CHECK, INSPECTION REPORTED FWD EMERGENCY BATTERY EPSU FAILED CAPACITY TEST. REMOVED AND REPLACED FWD EPSU BATTERY AND PERFORMED OPS CHECK IAW 33-51-38-000-002. CHECKED GOOD.
- [SDR F3LA200700362](https://openairdocs.org/sdr/F3LA200700362.md): Sill · corroded · Dec 4, 2007 · N901FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > DURING C-5 CHECK, INSPECTION REPORTED LIGHT SURFACE CORROSION ON FWD CARGO DOOR SILL WEB. REMOVED NUTPLATE AND REWORKED FOUR SMALL AREAS OF CORROSION IAW SRM 51-42-11 AND 51-74-00. EA NR A9-53R-12316 REQUIRED ACCOMPLISHMENT OF HFEC INSPECTION OF BLENDED AREA
- [SDR F3LA200600055](https://openairdocs.org/sdr/F3LA200600055.md): Battery · failed · Jun 10, 2006 · N901FR · Airbus A319112 · Emergency Lighting
  > DURING C-4 CHECK, INSPECTION REPORTED RT OVERWING EXIT EPSU BATTERY FAILED CAPACITY CHECK. REPLACED EPSU BATTERY AT RT OVERWING EXIT. OPS CHECKED GOOD PER AMM 33-51-38-400-002 AND 33-51-38-000-002.
- [SDR F3LA200600052](https://openairdocs.org/sdr/F3LA200600052.md): Battery · faulted · Jun 9, 2006 · N901FR · Airbus A319112 · Emergency Lighting
  > DURING C-4 CHECK, INSPECTION REPORTED FWD EPSU BATTERY FAULT. REPLACED EPSU BATTERY AT 10WL ABOVE L1 DOOR. OPS CHECKED GOOD PER AMM 33-51-38-000-002 AND 33-51-38-400-002.
- [SDR F3LA200600054](https://openairdocs.org/sdr/F3LA200600054.md): Battery · faulted · Jun 9, 2006 · N901FR · Airbus A319112 · Emergency Lighting
  > DURING C-4 CHECK, INSPECTION REPORTED EPSU BATTERY EMER LEFT FAULT. REPLACED EPSU BATTERY AT LT OVERWING EMERGENCY EXIT. OPS CHECKED GOOD PER AMM 33-51-38-000-002 AND 31-51-38-400-002.
- [SDR F3LA200600053](https://openairdocs.org/sdr/F3LA200600053.md): Battery · faulted · Jun 9, 2006 · N901FR · Airbus A319112 · Emergency Lighting
  > DURING C-4 CHECK, INSPECTION REPORTED AFT EPSU BATTERY FAULT. REPLACED EPSU BATTERY AT 13WL. OPS CHECKED GOOD PER AMM 33-51-38-000-002 AND 33-51-38-400-002.
- [SDR F3LA200600044](https://openairdocs.org/sdr/F3LA200600044.md): Bearing · corroded · May 31, 2006 · N901FR · Airbus A319112 · Main Landing Gear
  > DURING C-4 CHECK, INSPECTION REPORTED LT MLG LWR BEARING ASSY CORRODED, PITTED AND DEFORMED. REMOVED CORROSION ON LT MLG SHOCK ABSORBER GLAND SEAL PER EA A9-32R-11439. PERFORMED FLUORESCENT PENETRANT INSPECTION PER AIRBUS NTM 51-80-00 PART 8, AND EA A9-32R-1
- [SDR F3LA200600041](https://openairdocs.org/sdr/F3LA200600041.md): Floor Panel · corroded · May 30, 2006 · N901FR · Airbus A319112 · Fuselage Floor Panel
  > DURING C-4 CHECK, INSPECTION REPORTED CABIN FLOOR PANEL 222FF AT R1 ENTRYWAY CORRODED IN 3 AREAS. REPLACED FLOOR PANEL PER WORK CARD NR CP753-12.
- [SDR F3LA200600039](https://openairdocs.org/sdr/F3LA200600039.md): Joint · corroded · May 17, 2006 · N901FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > DURING C-4 CHECK, INSPECTION REPORTED JOINT SHEET BETWEEN FR68 AND FR69, LT. SIDE JUST AFT OF L2 SILL, CORRODED. FABRICATED AND INSTALLED NEW JOINT SHEET PER SRM 53-41-14, SRM 51-42-11, AND AIRBUS DRAWING D534-80019.
- [SDR F3LA200600038](https://openairdocs.org/sdr/F3LA200600038.md): Attach Bracket · corroded · May 17, 2006 · N901FR · Airbus A319112 · Fuselage Floor Panel
  > DURING C-4 CHECK, INSPECTION REPORTED MILD SURFACE CORROSION ON CABIN FLOORBOARD PANEL NR 262EF ATTACHMENT BRACKET. FABRICATED AND INSTALLED NEW CONNECTING BRACKET PER SRM 51-42-11 AND AIRBUS DRAWING D536-70099.
- [SDR F3LA200600035](https://openairdocs.org/sdr/F3LA200600035.md): Fairing · cracked · May 17, 2006 · N901FR · Airbus A319112 · Nacelle/Pylon, Plate/Skin
  > DURING C-4 CHECK, INSPECTION REPORTED NR 1 ENGINE PYLON AFT LOWER FAIRING CRACKED. REPAIRED LOWER ENGINE PYLON FAIRING BY WELD PER EA A0-54T-11332. PERFORMED FLUORESCENT PENETRATE CHECK PER NDT MANUAL PART 6-51-80-00, PAGES 801-809.
- [SDR F3LA200600028](https://openairdocs.org/sdr/F3LA200600028.md): Support Angle · corroded · May 17, 2006 · N901FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > DURING C-4 CHECK, INSPECTION REPORTED SUPPORT ANGLE AT FR 69-70, RT SIDE OF AIRCRAFT UNDER WEB SUPPORT PLATE, CORRODED. REPLACED ANGLE SUPPORT AND WEB ASSY PER SRM 51-42-11 AND AIRBUS DWG D534-74180.
- [SDR F3LA200600051](https://openairdocs.org/sdr/F3LA200600051.md): Bushing · cracked · May 15, 2006 · N901FR · Airbus A319112 · Fuselage, Seat/Cargo Attach Fittings
  > DURING C-4 CHECK, INSPECTION REPORTED I/B RT SEAT TRACK EXPANSION JOINT THROUGH BOLT BUSHING CRACKED AT FR35 TO FR36. REPLACED BOLT AND BUSHINGS PER SRM 51-42-11.
- [SDR F3LA200600050](https://openairdocs.org/sdr/F3LA200600050.md): Bushing · broken · May 15, 2006 · N901FR · Airbus A319112 · Fuselage, Seat/Cargo Attach Fittings
  > DURING C-4 CHECK, INSPECTION REPORTED I/B LT SEAT TRACK EXPANSION JOINT THROUGH BOLT HAD BROKEN BUSHING AT FR35 TO FR36. REPLACED BOLT AND BUSHINGS PER SRM 51-42-11.
- [SDR F3LA200600046](https://openairdocs.org/sdr/F3LA200600046.md): Floor Panel · corroded · May 15, 2006 · N901FR · Airbus A319112 · Fuselage Floor Panel
  > DURING C-4 CHECK, INSPECTION REPORTED FLOOR PANEL 221FF CORRODED ALONG INBD EDGE OF L1 DOOR THRESHOLD. REPLACED PANEL 221FF PER WORK CARD CP753-12 AND AMM 53-12-12-400-001.
- [SDR F3LA200600037](https://openairdocs.org/sdr/F3LA200600037.md): Web · corroded · May 13, 2006 · N901FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON WEB BETWEEN FR69 AND FR70, R/H NEXT TO FUSELAGE. INSTALLED NEW ANGLE AND WEB ASSY. PER SRM 51-42-11 AND DRAWING DE534-74180.
- [SDR F3LA200600036](https://openairdocs.org/sdr/F3LA200600036.md): Floor Panel · corroded · May 13, 2006 · N901FR · Airbus A319112 · Fuselage Floor Panel
  > DURING C-4 CHECK, INSPECTION REPORTED L2 DOOR THRESHOLD PANEL 261EF CORRODED. INSTALLED NEW FLOOR PANEL PER DRAWING D5367-1805.
- [SDR F3LA200600034](https://openairdocs.org/sdr/F3LA200600034.md): Floorboard · corroded · May 13, 2006 · N901FR · Airbus A319112 · Fuselage Main, Floor Beam
  > DURING C-4 CHECK, INSPECTION REPORTED FLOORBEAM CORRODED AT FRAME 15, 6TH FLOORBEAM FROM RT CENTER OF FUSELAGE ON THE AFT END OF BEAM. BLENDED CORROSION AND PERFORMED HFEC PER SRM 51-75-12 AND EA A9-53R-11424.
- [SDR F3LA200600033](https://openairdocs.org/sdr/F3LA200600033.md): Support Angle · corroded · May 13, 2006 · N901FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON SUPPORT ANGLE AT FR69 TO FR70, LT. SIDE UNDER SUPPORT WEB PLATE. REPLACED WEB AND SUPPORT ANGLE PER SRM 51-44-11, SRM 51-42-11, AND AIRBUS DRAWING D534-74180.
- [SDR F3LA200600032](https://openairdocs.org/sdr/F3LA200600032.md): Web · corroded · May 13, 2006 · N901FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOOR WEB NEXT TO FUSELAGE BETWEEN FRAMES 69 AND 70. REPLACED SUPPORT ANGLE AND WEB PER SRM 51-42-11, ARM 51-44-11, AND AIRBUS DRAWING D534-74180.
- [SDR F3LA200600031](https://openairdocs.org/sdr/F3LA200600031.md): Dummy Rail · corroded · May 13, 2006 · N901FR · Airbus A319112 · Fuselage, Seat/Cargo Attach Fittings
  > DURING C-4 CHECK, INSPECTION REPORTED FLOORBEAM CORRODED AT FR15, 5TH FLOORBEAM FROM LT. CENTER OF FUSELAGE ON AFT END. DUMMY RAIL AT STATION Y503.2 FOUND TO BE OUT OF LIMITS PER SRM 53-11-14, FIG. 103. REPLACED DUMMY RAIL AT STATION Y503.2 PER SRM 51-42-11
- [SDR F3LA200600030](https://openairdocs.org/sdr/F3LA200600030.md): Support Angle · corroded · May 13, 2006 · N901FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON LT SIDE OF SUPPORT ANGLE THAT ATTACHES WEB SUPPORT PLATE BETWEEN FR69 AND FR70 AT FLOOR LEVEL. INSTALLED NEW WEB AND SUPPORT PER SRM 51-42-11, SRM 53-41-14, AND AIRBUS DRAWING D534-74180.
- [SDR F3LA200600029](https://openairdocs.org/sdr/F3LA200600029.md): Floor Support · corroded · May 13, 2006 · N901FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOOR SUPPORT NUT PLATE HOLES BETWEEN FRAMES 66 AND 68, AND 44 IN RIGHT OF CENTERLINE. REPLACED FLOORBEAM FR66 TO FR68 PER SRM 51-42-11 AND 51-21-00.
- [SDR F3LA200600042](https://openairdocs.org/sdr/F3LA200600042.md): Floor Panel · corroded · May 12, 2006 · N901FR · Airbus A319112 · Fuselage Floor Panel
  > DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON THRESHOLD PANEL AT R2 DOOR. REMOVED CORROSION ON TOP AND BOTTOM SKIN PER SRM 51-22-00. ALLOWABLE SKIN REMOVED FOR CORROSION CLEAN-UP EXCEEDS LIMITS AND THRESHOLD IS BER. REPLACED PANEL.
- [SDR F3LA200600045](https://openairdocs.org/sdr/F3LA200600045.md): Panel · cracked · May 11, 2006 · N901FR · Airbus A319112 · Nacelle/Pylon, Plate/Skin
  > DURING C-4 CHECK, INSPECTION REPORTED LT PYLON PANEL 473AL CRACKED ON RADIUS OF INNER DOUBLER. STOP DRILLED CRACK AND WELDED PER EA A9-54R-11430. PERFORMED HFEC, NO DISCREPANCIES NOTED.
- [SDR F3LA200600049](https://openairdocs.org/sdr/F3LA200600049.md): Bracket · worn · May 9, 2006 · N901FR · Airbus A319112 · Engine Cowling System
  > DURING C-4 CHECK, INSPECTION REPORTED NR 1 ENGINE IB FWD COWL BRACE BRACKET WORN INTO THE ENGINE CASE. INSTALLED NEW BRACKETS AND HARDWARE ON NR 1 ENGINE CASE FOR THE FAN COWL HOLD OPEN ROD PER EA A9-72R-11428 AND CREATED RW 0000808.
- [SDR F3LA200600043](https://openairdocs.org/sdr/F3LA200600043.md): Hook · worn · May 8, 2006 · N901FR · Airbus A319112 · Passenger/Crew Doors
  > DURING C-4 CHECK, INSPECTION REPORTED L2 DOOR GEARBOX ASSY HOOK WORN. REPLACED GEARBOX HOOK PER AMM 52-13-21-400-001, STEP 3C(17)(C) THRU (E).
- [SDR F3LA200500043](https://openairdocs.org/sdr/F3LA200500043.md): Tire · failed · Oct 3, 2005 · N901FR · Airbus A319112 · Tire
  > ON LANDING, BOTH NOSE TIRES BLEW. STOPPED ACFT ON RUNWAY. PERFORMED INSPECTION AFTER TIRE BURST. NO DAMAGE NOTED. REPLACED LT NOSE WHEEL & TIRE ASSEMBLY, P/N 3-1531-1, S/N 4964, TSI 690.80 &CSI 285 SINCE REPAIR, RT NOSE WHEEL & TIRE ASSEMBLY, P/N 3-1531-1,
- [SDR F3LA200500024](https://openairdocs.org/sdr/F3LA200500024.md): Blower · smoke · Jun 1, 2005 · N901FR · Airbus A319112 · Air Distribution Fan
  > AIR TURNBACK, FLIGHT CREW REPORTED AVIONICS SMOKE INDICATION ON DEPARTURE. AIRCRAFT RETURNED TO CUN AND LANDED WITHOUT INCIDENT. PERFORMED OPERATIONAL CHECK OF EXTRACTION AND BLOWER FAN BY MCDU PER MM 21-26-00-710-001. NO FAULTS DETECTED.
- [SDR F3LA200100065](https://openairdocs.org/sdr/F3LA200100065.md): B-Nut · loose · May 16, 2001 · N901FR · Airbus A319111 · Hydraulic System, Main
  > DURING TRAINING FLIGHT, FLIGHT CREW REPORTED LOSS OF GREEN HYDRAULIC SYSTEM. AN EMERGENCY WAS DECLARED AND AIRCRAFT LANDED IN PHX WITHOUT INCIDENT. AIRCRAFT WAS TOWED OFF THE RUNWAY DUE TO THE LOSS OF THE NOSE WHEEL STEERING. THE B-NUT ON THE HYDRAULIC PRES

## 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 = 'N901FR' AND deregistration_id = 'N901FR-2009-02-12'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N901FR-2009-02-12/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.