# N918FR: 2003 Airbus A319-111, registration cancelled 2017-02-01

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 1, 2017
- Status when cancelled: Valid registration
- Airframe: [Airbus A319-111](https://openairdocs.org/model/airbus-a319-111) (registry code 3940000)
- Engine: [CFM International CFM56 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802)
- Data sheets: [TCDS A28NM](https://openairdocs.org/tcds/A28NM) (OpenAirDocs)
- Serial number: 1943
- Year built: 2003
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 22, 2003
- Certificate issued: January 9, 2017
- Last registry action: January 10, 2017
- Mode S code: ACB4F0
- Owner when cancelled: [Ga Telesis LLC](https://openairdocs.org/faa-owner/GA%20TELESIS%20LLC)
- Location: [Fort Lauderdale, FL](https://openairdocs.org/faa-place/FL/Fort%20Lauderdale)
- Owner type: Corporation
- Owner's area on the map: 26.1860° N, 80.1727° W: Placed by OpenAirDocs at the center of ZIP code 33309, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N918FR
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=918FR
- Page: https://openairdocs.org/deregistered/N918FR-2017-02-01

From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Airbus A319-111: https://openairdocs.org/model/airbus-a319-111.md

## Service difficulty reports (104, newest 50)

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

- [SDR F3LA2015021201105](https://openairdocs.org/sdr/F3LA2015021201105), Feb 12, 2015: HYDRAULIC LINE. CHAFED. OIL LEAKING FROM NR 2 ENG PYLON AFT OF BREATHER TUBE. R & R PRESS HYD LINE IN NR 2 PYLON. LOG PAGE 913804.
- [SDR F3LA2014070101047](https://openairdocs.org/sdr/F3LA2014070101047), Jun 20, 2014: SKIN. DEBONDED. LT ELEVATOR THERMO GRAPHIC INSPECTION REVEALED INDICATIONS ON UPPER PANEL IRREGULAR IN SHAPE & BLACK IN COLOR. REPAIRED LT ELEVATOR UPPER SURFACE OF LIQUID INGR
- [SDR F3LA2014070101046](https://openairdocs.org/sdr/F3LA2014070101046), Jun 20, 2014: SKIN. DEBONDED. RT ELEVATOR THERMO GRAPHIC INSPECTION REVEALED INDICATIONS ON UPPER PANEL IRREGULAR IN SHAPE & BLACK IN COLOR. REPAIRED RT ELEVATOR UPPER SURFACE OF LIQUID INGR
- [SDR F3LA2013112200935](https://openairdocs.org/sdr/F3LA2013112200935), Nov 22, 2013: LIGHT. INOPERATIVE. EMERGENCY EXIT LIGHT ON SEAT 25C INOPERATIVE. REPLACED LIGHT ASSEMBLY, OPERATIONS CHECKED GOOD.
- [SDR F3LA2013091600905](https://openairdocs.org/sdr/F3LA2013091600905), Sep 15, 2013: BATTERY PACK. FAULTY. EPSU BATTERY FAULT, 12WL. R & R EPSU BATTERY IAW AMM 33-51-38-000-002 AND AMM 33-51-38-400-002, TESTED OK.
- [SDR F3LA2011121500694](https://openairdocs.org/sdr/F3LA2011121500694), Dec 14, 2011: COFFEEMAKER. SHORTED. ELECTRICAL ODOR, ACRID ODOR REPORTED IN AFT GALLEY AREA ABOVE COFFEE POT - WARM TO THE TOUCH. TOTAL CYCLES 114925. FOUND AFT INBD NR 2 COFFEEMAKER INOPERABLE, C
- [SDR F3LA2011091900679](https://openairdocs.org/sdr/F3LA2011091900679), Sep 16, 2011: FLOOR SUPPORT. CORRODED. C-CHECK: NON ROUTINE 38895; MAIN CABIN FR68 LT AFT DOOR SEAL BEAM HAS CORROSION. REPAIRED LT AFT DOOR SEAL BY REMOVING DAMAGE AND INSTALLING A REPAIR ANGLE IAW 
- [SDR F3LA2011091900678](https://openairdocs.org/sdr/F3LA2011091900678), Sep 16, 2011: FLOOR SUPPORT. CORRODED. C-CHECK: NON ROUTINE 38894; MAIN CABIN FLOORBEAM FROM FR66 TO FR68 HAS CORROSION. REPLACED CABIN FLOORBEAM FR66 TO FR68 IAW SRM 51-42-11.
- [SDR F3LA2011091600677](https://openairdocs.org/sdr/F3LA2011091600677), Sep 16, 2011: FLOORBEAM. CORRODED. C-CHECK: MAIN CABIN FLOORBEAM FR66 Y254 IS CORRODED. REPLACED FLOORBEAM IAW SRM 51-42-11.
- [SDR F3LA2011091600676](https://openairdocs.org/sdr/F3LA2011091600676), Sep 16, 2011: FLOORBEAM. CORRODED. DURING C CHECK, MAIN CABIN FLOORBEAM FR68 -Y1292 FOUND CORRODED. REPLACED FLOORBEAM IAW SRM 51-42-11.
- [SDR F3LA2011091600674](https://openairdocs.org/sdr/F3LA2011091600674), Sep 16, 2011: FLOORBEAM. CORRODED. C-CHECK: MAIN CABIN FLOORBEAM FR68- Y1292 HAS CORROSION. REPLACED MAIN CABIN FLOORBEAM FR68-Y1292 IAW SRM 51-42-11, PARA 5A AND SRM 51 -44-11 TABLE 2.
- [SDR F3LA2011091600673](https://openairdocs.org/sdr/F3LA2011091600673), Sep 16, 2011: FLOORBEAM. CORRODED. C-CHECK, MAIN CABIN FLOORBEAM FR68- V765 HAS CORROSION. REPLACED MAIN CABIN FLOORBEAM FR68-V765 IAW SRM 51 -42-11 AND SRM 51 -44-11.
- [SDR F3LA2011050300639](https://openairdocs.org/sdr/F3LA2011050300639), Apr 29, 2011: ELECTRICAL BOX. FAULTY. PILOT REPORT, ON TAKEOFF AMBER NOSE WHEEL STEERING DISCONNECT ILLUMINATED. NO ASSOCIATED ECAM. PILOT DECLARED EMERGENCY BEFORE LANDING. NO FUTHER ABNORMALITIES.
- [SDR F3LA2010122900571](https://openairdocs.org/sdr/F3LA2010122900571), Dec 28, 2010: SMOKE DETECTOR. FAULTY. PILOT REPORT: LP 594710; AFT CARGO / LAV SMOKE DETECT FAULT. R & R THE AFT CARGO SMOKE DETECT UNIT (3WH) AND AFT LAV (E) DETECT UNIT. IAW AMM 26-46-15, PB 401. 
- [SDR F3LA2010011500300](https://openairdocs.org/sdr/F3LA2010011500300), Jan 14, 2010: CHANNEL. CORRODED. DURING C5 C-CHECK INSP NOTED AFT PIT FRAME 59 FWD U CHANNEL CORRODED AT FASTENER HOLES. MX REMOVED AND REPLACED CHANNEL IAW SRM 51-42-11, SRM 51-44-11 AND SRM 5
- [SDR F3LA2010011200288](https://openairdocs.org/sdr/F3LA2010011200288), Jan 12, 2010: PROFILE. CORRODED. DURING C5 C-CHECK INSP NOTED AFT PIT PROFILE CORRODED. MX REMOVED AND REPLACED AFT PIT PROFILE AT FRAME 61 IAW SRM 51-42-11 PARAGRAPH 5 AND 6.
- [SDR F3LA2010011400297](https://openairdocs.org/sdr/F3LA2010011400297), Jan 11, 2010: PROFILE. CORRODED. DURING C5 C-CHECK INSP NOTED UPON REMOVAL OF PROFILE AT FRAME 58 IN AFT PIT FOUND CORROSION AT 2 FASTENER HOLES. MX REMOVED AND REPLACED SUPPORT FITTING REFEREN
- [SDR F3LA2010011200291](https://openairdocs.org/sdr/F3LA2010011200291), Jan 11, 2010: PROFILE. CORRODED. DURING C5 C-CHECK INSP NOTED AFT PIT CENTER FLOOR SUPPORT FRAME 59 TO FRAME 60 CORRODED AT FASTENER HOLE. MX REMOVED AND REPLACED AFT PIT CTR FLOOR SUPPORT FROM
- [SDR F3LA2010011200290](https://openairdocs.org/sdr/F3LA2010011200290), Jan 11, 2010: PROFILE. CORRODED. DURING C5 C-CHECK INSP NOTED AFT PIT RT FLOOR SUPPORT PROFILE FROM FRAME 52 TO FRAME 55 CORRODED. MX REMOVED AND REPLACED AFT PIT RT FLOOR SUPPORT PROFILE FROM 
- [SDR F3LA2010011200289](https://openairdocs.org/sdr/F3LA2010011200289), Jan 11, 2010: PROFILE. CORRODED. DURING C5 C-CHECK INSP NOTED AFT PIT LT FLOOR SUPPORT PROFILE FRAME 56 TO FRAME 58 CORRODED. MX REMOVED AND REPLACED AFT PIT LT FLOOR SUPPORT PROFILE FROM FRAME
- [SDR F3LA2010011200292](https://openairdocs.org/sdr/F3LA2010011200292), Jan 9, 2010: PROFILE. CORRODED. DURING C5 C-CHECK INSP NOTED AFT PIT LT FLOOR SUPPORT PROFILE FRAME 52 TO FRAME 56 CORRODED. MX REMOVED AND REPLACED AFT PIT LT FLOOR SUPPORT PROFILE FRAME 52 T
- [SDR F3LA2010011200296](https://openairdocs.org/sdr/F3LA2010011200296), Jan 7, 2010: FRAME. CORRODED. DURING C5 C-CHECK INSP NOTED AFT PIT FRAME 56 ANGLE ON FWD SIDE OF FRAME IS CORRODED AT 2 FASTENER HOLES. MX REMOVED AND REPLACED ANGLE AT FRAME 56 IAW SRM 51-4
- [SDR F3LA2010011500303](https://openairdocs.org/sdr/F3LA2010011500303), Jan 6, 2010: PROFILE. CORRODED. DURING C5 C-CHECK INSP NOTED AFT PIT FRAME 59 PROFILE HAS CORROSION. MX REMOVED AND REPLACED PROFILE IAW SRM 51-42-11.
- [SDR F3LA2010011500302](https://openairdocs.org/sdr/F3LA2010011500302), Jan 6, 2010: PROFILE. CORRODED. DURING C5 C-CHECK INSP NOTED AFT PIT CTR FLOOR SUPPORT BETWEEN FRAME 58 AND FRAME 59 CORRODED AT FASTENER HOLE. MX REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51
- [SDR F3LA2010011500301](https://openairdocs.org/sdr/F3LA2010011500301), Jan 6, 2010: FRAME. CORRODED. DURING C5 C-CHECK INSP NOTED AFT PIT FRAME 59 HAS EVIDENCE OF CORROSION IN FASTENER HOLES. MX REMOVED AND REPLACED FITTING IAW EA A9-53R-31612 AND EA A9-53R-316
- [SDR F3LA2010011400298](https://openairdocs.org/sdr/F3LA2010011400298), Jan 6, 2010: PROFILE. CORRODED. DURING C5 C-CHECK INSP NOTED AFT PIT FRAME 58 PROFILE CORRODED AT SEVERAL FASTENER HOLES. MX REMOVED AND REPLACED PROFILE IAW SRM 51-42-11.
- [SDR F3LA2010011200295](https://openairdocs.org/sdr/F3LA2010011200295), Jan 6, 2010: PROFILE. CORRODED. DURING C5 C-CHECK INSP NOTED AFT PIT FRAME 56 PROFILE CORRODED AT FASTENER HOLES. MX REMOVED AND REPLACED PROFILE AT FRAME 56 IAW SRM 51-42-11 AND SRM 51-44-11.
- [SDR F3LA2010011200294](https://openairdocs.org/sdr/F3LA2010011200294), Jan 6, 2010: PROFILE. CORRODED. DURING C5 C-CHECK INSP NOTED AFT PIT CTR FLOOR SUPPORT BETWEEN FRAME 56 AND FRAME 57 CORRODED AT FASTENER HOLE. MX REMOVED AND REPLACED FLOOR SUPPORT BETWEEN FR
- [SDR F3LA2010011200293](https://openairdocs.org/sdr/F3LA2010011200293), Jan 6, 2010: PROFILE. CORRODED. DURING C5 C-CHECK INSP NOTED AFT PIT CTR FLOOR SUPPORT BETWEEN FRAME 57 AND FRAME 58 CORRODED AT FASTENER HOLE. MX REMOVED AND REPLACED FLOOR SUPPORT BETWEEN FR
- [SDR F3LA200800505](https://openairdocs.org/sdr/F3LA200800505), Jul 20, 2008: SIGN. BROKEN. DURING C-CHECK, INSP NOTED R1 DOOR FWD LOWER EXIT LIGHT IS BROKEN. MAINT REMOVED AND REPLACED R1 DOOR FWD LOWER EXIT LIGHT IAW AMM 33-51-13-400-001. UPON COMPLE
- [SDR F3LA200800500](https://openairdocs.org/sdr/F3LA200800500), Jul 19, 2008: SHEAR PLATE. CORRODED. DURING C-CHECK, INSP NOTED THE RT LATERAL SHEAR PLATE AT Y-1162, FROM FRAME 69 TO FRAME 70, HAD CORROSION AND FOUR SHEARED FASTENERS AT THE FWD EDGE. MAINT REMO
- [SDR F3LA200800501](https://openairdocs.org/sdr/F3LA200800501), Jul 19, 2008: SILL. DAMAGED. DURING C-CHECK, INSP NOTED THE R2 DOOR SILL PLATE REQUIRED REPLACEMENT DUE TO MISDRILLED HOLE. MAINT REMOVED AND REPLACED R2 DOOR SILL PLATE IAW A319 SRM 51-42-
- [SDR F3LA200800499](https://openairdocs.org/sdr/F3LA200800499), Jul 18, 2008: FLOOR PANEL. BROKEN. DURING C4 S1 C CHECK, INSPECTION NOTED THE AFT CARGO FLOORBOARD, 151CE, HAD TWO BROKEN CORNERS. MAINTENANCE REMOVED AND REPLACED FLOOR PANEL 151CE. INSTALLATION
- [SDR F3LA200800486](https://openairdocs.org/sdr/F3LA200800486), Jul 16, 2008: PROFILE. CORRODED. DURING C-CHECK INSP NOTED THE AFT CARGO COMPARTMENT RT SIDE PROFILE HAD CORROSION AT FRAME 59 ON RT SIDE IAW A319 SRM 51-72-11 AND 51-44-11. UPON COMPLETION OF 
- [SDR F3LA200800489](https://openairdocs.org/sdr/F3LA200800489), Jul 16, 2008: FITTING. CORRODED. DURING C-CHECK INSP NOTED THE R1 DOOR GIRT BAR FITTING IB MOUNT HOLES ON SILL PLATE HAD CORROSION. MAINT BLENDED CORROSION IAW SRM 51-74-00. MAINT REPAIRED AREA
- [SDR F3LA200800490](https://openairdocs.org/sdr/F3LA200800490), Jul 16, 2008: SKIN. DENTED. DURING C-CHECK INSP NOTED THAT THE DAMAGE ON NR 1 ENGINE INLET COWL REQUIRES PERMANENT REPAIR OF DENT AT THE 2 O`CLOCK POSITION. MAINT REPAIRED DAMAGED AREA IAW
- [SDR F3LA200800482](https://openairdocs.org/sdr/F3LA200800482), Jul 15, 2008: BATTERY BOX. WORN. DURING C-CHECK INSP, NOTED AFT BATTERY TRAY OB FWD AND AFT MOUNTS HAVE WEAR. MAINT REMOVED AND REPLACED AFT BATTERY TRAY, OB FWD AND AFT MOUNTS IAW SRM 51-72-11
- [SDR F3LA200800485](https://openairdocs.org/sdr/F3LA200800485), Jul 15, 2008: PROFILE. CORRODED. DURING C-CHECK INSP NOTED THE AFT CARGO COMPARTMENT SMALL PROFILE RT SIDE JUST INSIDE DOOR FWD OF FRAME C56 HAS CORROSION. MAINT REMOVED SMALL PROFILE, FABRICAT
- [SDR F3LA200800484](https://openairdocs.org/sdr/F3LA200800484), Jul 15, 2008: PROFILE. CORRODED. DURING C-CHECK INSP NOTED THE AFT CARGO COMPARTMENT PROFILE AT FRAME C59 HAD CORROSION AT BOTH ENDS OF THE PROFILE. MAINT REMOVED AND REPLACED THE PROFILE IAW S
- [SDR F3LA200800483](https://openairdocs.org/sdr/F3LA200800483), Jul 15, 2008: PROFILE. GOUGED. DURING C-CHECK INSP NOTED THE AFT CARGO COMPARTMENT PROFILE AT FRAME C63 IS GOUGED AND HAS A RIVET PULLING THROUGH. MAINT REMOVED AND REPLACED PROFILE AT FRAME 
- [SDR F3LA200800488](https://openairdocs.org/sdr/F3LA200800488), Jul 15, 2008: DOOR FRAME. CORRODED. DURING C-CHECK INSP NOTED CORROSION ON TOP LEG OF FRAME C55A AT FWD EDGE OF C2 DOOR. MAINT REPAIRED DAMAGE ON TOP LEG OF FRAME C55A IAW EA NR A9-53R-30442. UPON
- [SDR F3LA200800491](https://openairdocs.org/sdr/F3LA200800491), Jul 15, 2008: FITTING. CRACKED. DURING C-CHECK INSP NOTED THE NR 1 ENGINE PYLON PANEL NR 413CL MOUNTS STRUCTURE WAS CRACKED AT AFT UPPER SCREW HOLE. MAINT REPAIRED NR 1 ENGINE PYLON PANEL NR 4
- [SDR F3LA200800468`](https://openairdocs.org/sdr/F3LA200800468%60), Jul 14, 2008: PROFILE. CORRODED. DURING C-4/S-1 C-CHECK, INSPECTION NOTED AFT CARGO COMPARTMENT PROFILE AT FRAME C58 HAS CORROSION. MAINTENANCE REMOVED AND REPLACED PROFILE IN ACCORDANCE WITH A
- [SDR F3LA200800467](https://openairdocs.org/sdr/F3LA200800467), Jul 14, 2008: FLOORBEAM. CORRODED. DURING C-4/S-1 C-CHECK, INSPECTION NOTED AFT CARGO COMPARTMENT CENTER FLOORBEAM BETWEEN FRAME C58 AND C59 HAS CORROSION. MAINTENANCE REMOVED AND REPLACED CORROD
- [SDR F3LA200800466](https://openairdocs.org/sdr/F3LA200800466), Jul 14, 2008: PROFILE. CORRODED. DURING C-4/ S-1 C-CHECK, INSPECTION NOTED THE AFT CARGO COMPARTMENT, LEFT SIDE PROFILE AFT OF FRAME C62, HAS CORROSION. MAINTENANCE REMOVED AND REPLACED PROFILE
- [SDR F3LA200800465](https://openairdocs.org/sdr/F3LA200800465), Jul 14, 2008: FRAME. CORRODED. DURING C-CHECK INSP NOTED AFT CARGO COMPARTMENT INSIDE OF C2 DOOR SHORT ANGLE PIECE AT FRAME C59 HAS CORROSION. MAINT REMOVED SHORT ANGLE PIECE APPLIED PROTECTI
- [SDR F3LA200800470](https://openairdocs.org/sdr/F3LA200800470), Jul 14, 2008: PROFILE. CORRODED. DURING C-CHECK INSP NOTED CORROSION SEVERAL PLACES ON AFT MOST PROFILE AT FWD CARGO COMPARTMENT AFT OF FRAME C30. MAINT REMOVED AND REPLACED PROFILE IAW SRM 51-
- [SDR F3LA200800469](https://openairdocs.org/sdr/F3LA200800469), Jul 14, 2008: FLOORBEAM. CORRODED. DURING C-CHECK INSP NOTED AFT CARGO COMPARTMENT CENTER FLOORBEAM HAS CORROSION BETWEEN FRAME C57 AND FRAME C58. MAINT REMOVED AND REPLACED CORRODED FLOORBEAM AT
- [SDR F3LA200800481](https://openairdocs.org/sdr/F3LA200800481), Jul 11, 2008: FLOOR PANEL. DAMAGED. DURING C-CHECK INSP, NOTED FLOOR PANEL 261PF HAD COMPOSITE DAMAGE. MAINT REMOVED AND REPLACED FLOOR PANEL 261PF WITH NEW PANEL, REFERENCED ON EAC NON ROUTINE IT
- [SDR F3LA200800487](https://openairdocs.org/sdr/F3LA200800487), Jul 11, 2008: SKIN. CHAFED. DURING C-CHECK INSP NOTED THE RT AILERON APPEARS TO BE CHAFING AT IB LOWER EDGE. MAINT CLEANED AREA OF DAMAGE AND REPAIRED IAW SRM 51-75-12. UPON COMPLETION OF 

All 104: https://openairdocs.org/deregistered/N918FR-2017-02-01/reports.md

---
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.