# Service difficulty reports: N916FR, cancelled Apr 13, 2009 A list on [N916FR, cancelled Apr 13, 2009](https://openairdocs.org/deregistered/N916FR-2009-04-13.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR F3LA200800196](https://openairdocs.org/sdr/F3LA200800196.md): Lamp · burned out · Apr 21, 2008 · N916FR · Airbus A319112 · Emergency Lighting > DURING C4 S1 C CHECK INSPECTION NOTED LIGHT OUT IN AFT LEFT OVERWING EXIT. MAINTENANCE REMOVED AND REPLACED LAMP IN AFT LEFT EMERGENCY OVERWING LIGHT 63WL IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 33-51-15-000-001 AND AMM 33-51-15-400-001. UPON COMPLETION O - [SDR F3LA200800195](https://openairdocs.org/sdr/F3LA200800195.md): Bracket · corroded · Apr 20, 2008 · N916FR · Airbus A319112 · Fuselage Main, Attach Fittings > DURING C4 S1 C CHECK INSPECTION NOTED L2 DOOR SLIDE UPPER AFT MOUNT BRACKET HAD CORROSION. MAINTENANCE REMOVED AND REPLACED L2 DOOR SLIDE UPPER AFT MOUNT BRACKET IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-42-11. UPON COMPLETION OF THE REPAIR IT WAS INSPEC - [SDR F3LA200800194](https://openairdocs.org/sdr/F3LA200800194.md): Bracket · corroded · Apr 20, 2008 · N916FR · Airbus A319112 · Service Doors > DURING C4 S1 C CHECK INSPECTION NOTED R2 DOOR SLIDE UPPER AFT MOUNT BRACKET HAD CORROSION. MAINTENANCE REMOVED AND REPLACED R2 DOOR SLIDE UPPER AFT MOUNT BRACKET IN ACCORDANCE WITH SRM 51-42-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPT - [SDR F3LA200800183](https://openairdocs.org/sdr/F3LA200800183.md): Seat · corroded · Apr 19, 2008 · N916FR · Airbus A319112 · Passenger Compartment Equipment > DURING C4 S1 C CHECK INSPECTION NOTED CORROSION AT MOUNTING HOLES AFT LEFT FLIGHT ATTENDANT SEAT. MAINTENANCE REMOVED AND REPLACED AFT LEFT FLIGHT ATTENDANT SEAT IN ACCORDANCE WITH THE REQUIRMENTS OF AMM 25-22-41-400-011. UPON COMPLETION OF THE REPAIR IT WAS - [SDR F3LA200800191](https://openairdocs.org/sdr/F3LA200800191.md): Floorboard · punctured · Apr 16, 2008 · N916FR · Airbus A319112 · Fuselage Floor Panel > DURING C4 S1 C CHECK INSPECTION NOTED FORWARD GALLEY FLOORBOARD 222EF HAS TWO PUNCTURES IN TOP RIGHT EDGE OF FLOORBOARD. MAINTENANCE REPAIRED PUNCTURES IN GALLEY FLOORBOARD 222EF IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 53-12-00 PAGE 205 AND PAGE 206. MAIN - [SDR F3LA200800189](https://openairdocs.org/sdr/F3LA200800189.md): Floor Panel · damaged · Apr 15, 2008 · N916FR · Airbus A319112 · Fuselage Floor Panel > DURING C4 S1 C CHECK INSPECTION NOTED FLOOR PANEL 232MF HAS HOLE IN FACE 1/4 INCH DIAMETER, 3 INCHES FROM INBOARD EDGE AND 3 FEET FROM FORWARD EDGE. MAINTENANCE REPAIRED DAMAGE IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 53-02-00 PAGE 205 FIGURE 201. UPON COM - [SDR F3LA200800188](https://openairdocs.org/sdr/F3LA200800188.md): Fitting · corroded · Apr 13, 2008 · N916FR · Airbus A319112 · Fuselage Main, Attach Fittings > DURING C4 S1 C CHECK INSPECTION NOTED GIRT BAR FITTING WAS REMOVED ON R1 DOOR DUE TO CORROSION UNDER SPACERS. MAINTENANCE FABRICATED NEW NUT CLIP PLATES IN ACCORDANCE WITH THE REQUIREMENTS OF AIRBUS DRAWING D53112534. MAINTENANCE INSTALLED NEW DRAIN PANS AND - [SDR F3LA200800202](https://openairdocs.org/sdr/F3LA200800202.md): Support Fitting · corroded · Apr 12, 2008 · N916FR · Airbus A319112 · Fuselage Miscellaneous Structure > DURING C4 S1 C CHECK INSPECTION, NOTED CENTER FLOORBEAM SUPPORT FITTING BETWEEN C59 AND C60 CORRODED. MAINTENANCE REMOVED CORROSION ON SUPPORT FITTING AND REINSTALLED SUPPORT FITTING AND CENTER FLOORBEAM IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-42-11 AND - [SDR F3LA200800163](https://openairdocs.org/sdr/F3LA200800163.md): Floor Panel · delaminated · Apr 11, 2008 · N916FR · Airbus A319112 · Fuselage Floor Panel > DURING C4 S1 C CHECK INSPECTION REPORTED FLOOR PANEL 261CG HAD DELAMINATION FROM ONE SCREW HOLE. MAINTENANCE REPAIRED FLOOR PANEL 261CG IN ACCORDANCE WITH SRM 53-08-00 STEP 8J, SRM 51-77-11 PARAGRAPH A11 AND SRM 51-44-21 PARAGRAPH 3A. UPON COMPLETION OF THE - [SDR F3LA200800162](https://openairdocs.org/sdr/F3LA200800162.md): Floorbeam · corroded · Apr 11, 2008 · N916FR · Airbus A319112 · Fuselage Main, Floor Beam > DURING C4 S1 C CHECK INSPECTION REPORTED CORROSION WAS FOUND ON NUT CLIP HOLE FLOORBEAM Y1292 AT FRAME 67 AND WAS FOUND UNSERVICEABLE. MAINTENANCE REMOVED AND REPLACED FLOORBEAM Y1292 AT FRAME 67 IN ACCORDANCE WITH SRM 51-42-11 PARAGRAPHS 5 AND 7 AND AIRBUS D - [SDR F3LA200800161](https://openairdocs.org/sdr/F3LA200800161.md): Floor Support · corroded · Apr 11, 2008 · N916FR · Airbus A319112 · Fuselage Miscellaneous Structure > DURING C4 S1 C CHECK, INSPECTION REPORTED CORROSION AT NUT PLATES FWD CARGO PIT RIGHT SIDE FLOOR SUPPORT PLATE FRAME 28 TO FRAME 31. MAINTENANCE REMOVED AND REPLACED SUPPORT PLATE IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-42-11. UPON COMPLETION OF T - [SDR F3LA200800160](https://openairdocs.org/sdr/F3LA200800160.md): Floor Support · corroded · Apr 11, 2008 · N916FR · Airbus A319112 · Fuselage Miscellaneous Structure > DURING C4 S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON THE AFT BULKHEAD FLOOR SUPPORT PLATE, IN THE FORWARD CARGO PIT, AT FRAME 31, BETWEEN STRINGERS 38 LEFT AND 38 RIGHT. MAINTENANCE REMOVED AND REPLACED THE PLATE IN ACCORDANCE WITH THE REQUIREMENT - [SDR F3LA200800159](https://openairdocs.org/sdr/F3LA200800159.md): Floor Support · corroded · Apr 11, 2008 · N916FR · Airbus A319112 · Fuselage Miscellaneous Structure > DURING C4 S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND AROUND THE NUT PLATE HOLES OF THE FLOOR SUPPORT PLATE ON THE LEFT SIDE OF THE FORWARD CARGO COMPARTMENT BETWEEN FRAMES 28 TO 30. MAINTENANCE REMOVED AND REPLACED THE FLOOR PLATE IN ACCORDANCE WITH - [SDR F3LA200800158](https://openairdocs.org/sdr/F3LA200800158.md): Dummy Rail · corroded · Apr 11, 2008 · N916FR · Airbus A319112 · Fuselage Miscellaneous Structure > DURING C4 S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON DUMMY RAIL Y503.2 AT FRAME 16. MAINTENANCE REMOVED AND REPLACED THE DUMMY RAIL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-42-11. UPON COMPLETION OF THE INSTALLATION, THE NEW DUMMY RAIL - [SDR F3LA200800157](https://openairdocs.org/sdr/F3LA200800157.md): Floor Support · corroded · Apr 11, 2008 · N916FR · Airbus A319112 · Fuselage Miscellaneous Structure > DURING C4 S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON FLOOR SUPPORT-Y1292, BETWEEN FRAMES 16 AND 20. MAINTENANCE REMOVED AND REPLACED THE CORRODED FLOORBEAM IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-42-11 AND A319 SRM 51-72-11. UPON COMPL - [SDR F3LA200800190](https://openairdocs.org/sdr/F3LA200800190.md): Floorbeam · corroded · Apr 10, 2008 · N916FR · Airbus A319112 · Fuselage Main, Floor Beam > DURING C4 S1 C CHECK INSPECTION NOTED CORROSION AT NUT PLATES AFT PIT LEFT FLOORBEAM UNDER COVER PROFILE AT FRAME 56 LOCATED FROM STRINGER 38 LEFT TO 38 RIGHT. MAINTENANCE FABRICATED REPLACEMENT PART IN ACCORDANCE WITH THE REQUIREMENTS OF AIRBUS DRAWING D5347 - [SDR F3LA200800185](https://openairdocs.org/sdr/F3LA200800185.md): Floorbeam · corroded · Apr 10, 2008 · N916FR · Airbus A319112 · Fuselage Main, Floor Beam > DURING C4 S1 C CHECK INSPECTION NOTED CORROSION AT NUT PLATES AFT PIT LEFT HAND FLOORBEAM UNDER COVER PROFILE AT FRAME 58 LOCATED FROM STRINGER 38 LEFT TO 38 RIGHT. MAINTENANCE FABRICATED AND REPLACED FLOORBEAM SUPPORT FITTING IN ACCORDANCE WITH THE REQUIREME - [SDR F3LA200800184](https://openairdocs.org/sdr/F3LA200800184.md): Mount · corroded · Apr 10, 2008 · N916FR · Airbus A319112 · Fuselage Main, Attach Fittings > DURING C4 S1 C CHECK INSPECTION NOTED RIGHT WIND SCREEN LOWER ATTACH MOUNTS WERE CORRODED. MAINTENANCE REMOVED AND REPLACED RIGHT WINDSCREEN LOWER ATTACH MOUNTS IN ACCORDANCE WITH THE REQUIRMENTS OF WORK CARD CP725-18. UPON COMPLETION OF THE REPAIR IT WAS IN - [SDR F3LA200800173](https://openairdocs.org/sdr/F3LA200800173.md): Fitting · corroded · Apr 10, 2008 · N916FR · Airbus A319112 · Fuselage Main, Attach Fittings > DURING C4 S1 C CHECK INSPECTION NOTED R2 FORWARD GIRT BAR FITTING PLATE CORODDED IN SEVERAL PLACES. MAINTENANCE REMOVED AND REPLACED FITTING PLATE. OKAY TO INSTALL AND INSTALL WILL BE ACCOMPLISHED ON WORK CARD CP753-36. - [SDR F3LA200800171](https://openairdocs.org/sdr/F3LA200800171.md): Fitting · corroded · Apr 10, 2008 · N916FR · Airbus A319112 · Fuselage Main, Attach Fittings > DURING C4 S1 C CHECK INSPECTION NOTED R1 FORWARD GIRT BAR FITTING PLATE WAS CORRODED IN SEVERAL PLACES. MAINTENANCE REMOVED AND REPLACED FITTING PLATE. OKAY TO INSTALL AND INSTALL WILL BE ACCOMPLISHED ON WORK CARD CP7553-12. - [SDR F3LA200800198](https://openairdocs.org/sdr/F3LA200800198.md): Support · corroded · Apr 9, 2008 · N916FR · Airbus A319112 · Fuselage Miscellaneous Structure > DURING C4 S1 C CHECK INSPECTION NOTED FRAME 59 COVER PROFILE NUT PLATE HOLES WERE CORRODED FROM STRINGER 38 RIGHT TO 38 LEFT. MAINTENANCE BLENDED OUT CORROSION AND INSTALLED NEW SUPPORT AT FRAME 59 STRINGER 41 LEFT IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 5 - [SDR F3LA200800152](https://openairdocs.org/sdr/F3LA200800152.md): Plate · cracked · Apr 7, 2008 · N916FR · Airbus A319112 · Fuselage Miscellaneous Structure > DURING C4 S1 C CHECK, INSPECTION REPORTED A CRACK WAS FOUND IN THE MOULLION PLATE LOCATED AFT OF THE L2 DOOR FRAME AT THE JOINT SHEET ATTACH POINT. MAINTENANCE REMOVED AND REPLACED THE MOULLION PLATE IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-42-11, P - [SDR F3LA200800203](https://openairdocs.org/sdr/F3LA200800203.md): Floor Panel · delaminated · Apr 6, 2008 · N916FR · Airbus A319112 · Fuselage Floor Panel > DURING C4 S1 C CHECK INSPECTION NOTED FLOOR PANEL 222EF DELAMINATED AT EDGE. MAINTENANCE REPAIRED FLOOR PANEL 222EF IN ACCORDANCE WITH THE REQUIREMENTS OF EA A9-53R-30217 AND SRM 53-02-00. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. - [SDR F3LA200800201](https://openairdocs.org/sdr/F3LA200800201.md): Floorbeam · corroded · Apr 6, 2008 · N916FR · Airbus A319112 · Fuselage Main, Floor Beam > DURING C4 S1 C CHECK INSPECTION NOTED AFT CARGO PIT CENTER FLOORBEAM BETWEEN C58 AND C59 NUT PLATES HAVE SIGNS OF CORROSION. MAINTENANCE REMOVED OLD FLOORBEAM AND REPAIR ANGLES, FABRICATED NEW FLOORBEAM AND REPAIR ANGLES IN ACCORDANCE WITH THE REQUIREMENTS OF - [SDR F3LA200800187](https://openairdocs.org/sdr/F3LA200800187.md): Floor Panel · corroded · Apr 6, 2008 · N916FR · Airbus A319112 · Fuselage Floor Panel > DURING C4 S1 C CHECK INSPECTION NOTED FLOOR PANEL 221PF LAV A HAS CORROSION ON BOLT HOLES. MAINTENANCE RECEIVED NEW FLOOR PANEL 221PK, OKAY TO INSTALL AND INSTALL WILL BE ACCOMPLISHED ON ROUTINE CARD CP753-12. - [SDR F3LA200800186](https://openairdocs.org/sdr/F3LA200800186.md): Strip · corroded · Apr 6, 2008 · N916FR · Airbus A319112 · Fuselage Miscellaneous Structure > DURING C4 S1 C CHECK INSPECTION NOTED BOTH LEFT 1 AND RIGHT 1 GAP STRIPS CORRODED ON LOWER SURFACE. MAINTENANCE REMOVED AND REPLACED LEFT 1 AND RIGHT 1 GAP STRIPS IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 53-12-12 PAGE BREAK 401. UPON COMPLETION OF THE REPA - [SDR F3LA200800172](https://openairdocs.org/sdr/F3LA200800172.md): Floor Support · corroded · Apr 6, 2008 · N916FR · Airbus A319112 · Fuselage Miscellaneous Structure > DURING C4 S1 C CHECK INSPECTION NOTED CORROSION AROUND NUT PLATES AFT CARGO PIT FLOOR PROFILE BETWEEN C55 AND C56. MAINTENANCE CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-35-00 AND SRM 51-42-11 P - [SDR F3LA200800178](https://openairdocs.org/sdr/F3LA200800178.md): Profile · corroded · Apr 6, 2008 · N916FR · Airbus A319112 · Fuselage Miscellaneous Structure > DURING C4 S1 C CHECK INSPECTION NOTED CORROSION AROUND NUT PLATES AFT CARGO PIT LEFT FLOOR PROFILE AT C 58. MAINTENANCE REMOVED AND REPLACED PROFILE IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-42-11 PARAGRAPH 5 AND 6 AND AIRBUS DRAWING D53476318. UPON COMP - [SDR F3LA200800177](https://openairdocs.org/sdr/F3LA200800177.md): Floorbeam · corroded · Apr 6, 2008 · N916FR · Airbus A319112 · Fuselage Main, Floor Beam > DURING C4 S1 C CHECK INSPECTION REPORTED NUT PLATE CORRODED OUTBOARD OF CENTER FLOORBEAM AFT CARGO PIT C 56 1. MAINTENANCE REMOVED AND REPLACED NEW C 56 PROFILE PLATE IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-42-11 PARAGRAPH 6 AND AIRBUS DRAWING 17D539749 - [SDR F3LA200800174](https://openairdocs.org/sdr/F3LA200800174.md): Floorbeam · corroded · Apr 6, 2008 · N916FR · Airbus A319112 · Fuselage Main, Floor Beam > DURING C4 S1 C CHECK INSPECTION REPORTED FLOORBEAM Y1292 SHOWS SIGNS OF CORROSION AT FRAME 16. MAINTENANCE REPLACED ONE SECTION OF THE BEAM IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-42-11 AND BLENDED OTHER AREA LOCATED AT 62.875" AFT OF FWD END OF BEAM I - [SDR F3LA200800136](https://openairdocs.org/sdr/F3LA200800136.md): Dummy Rail · corroded · Apr 6, 2008 · N916FR · Airbus A319112 · Fuselage, Seat/Cargo Attach Fittings > DURING C4 S1 C-CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON DUMMY RAIL Y503.2 AT FRAME 16. MAINTENANCE REMOVED AND REPLACED DUMMY RAIL IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-42-11. UPON COMPLETION OF THE INSTALLATION THE NEW RAIL WAS INSPECTED AN - [SDR F3LA200800199](https://openairdocs.org/sdr/F3LA200800199.md): Floor Panel · delaminated · Apr 5, 2008 · N916FR · Airbus A319112 · Fuselage Floor Panel > DURING C4 S1 C CHECK INSPECTION NOTED FLOOR PANEL 261HG HAS DELAMINATION AROUND EDGES. MAINTENANCE REPAIRED FLOOR PANEL 261HG IN ACCORDANCE WITH THE REQUIREMENTS OF EA A9-53R-30226. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. - [SDR F3LA200800156](https://openairdocs.org/sdr/F3LA200800156.md): Floor Panel · corroded · Apr 5, 2008 · N916FR · Airbus A319112 · Fuselage Floor Panel > DURING C4 S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON THE UNDERSIDE OF FLOOR PANEL 222FF. MAINTENANCE REMOVED THE CORRODED PANEL. THE NEW PANEL WAS INSTALLED IN ACCORDANCE WITH THE REQUIREMENTS OF TASK CARD CP 753-12. UPON COMPLETION OF THE INSTA - [SDR F3LA200800155](https://openairdocs.org/sdr/F3LA200800155.md): Floor Panel · corroded · Apr 5, 2008 · N916FR · Airbus A319112 · Fuselage Floor Panel > DURING C4 S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON THE UNDERSIDE OF FLOOR PANEL 221FF. MAINTENANCE REMOVED CORRODED PANEL. THE NEW PANEL WAS INSTALLED IN ACCORDANCE WITH THE REQUIREMENTS OF TASK CARD CP 753-12. FOLLOWING INSTALLATION OF THE NE - [SDR F3LA200800204](https://openairdocs.org/sdr/F3LA200800204.md): Sill · corroded · Apr 4, 2008 · N916FR · Airbus A319112 · Fuselage Miscellaneous Structure > DURING C4 S1 C CHECK INSPECTION NOTED R2 DOOR SILL HAS CORROSION AROUND NUT CLIP HOLE AT FRAME 66. MAINTENANCE FABRICATED REPAIR ANGLE IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 53-41-14, FABRICATED LEFT AND RIGHT REPAIR ANGLES IN ACCORDANCE WITH THE REQUIREM - [SDR F3LA200800154](https://openairdocs.org/sdr/F3LA200800154.md): Floor Panel · corroded · Apr 4, 2008 · N916FR · Airbus A319112 · Fuselage Floor Panel > DURING C4 S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON THREE INSERTS ON FLOOR PANEL 261PF. MAINTENANCE REMOVED THE CORRODED PANEL. THE NEW PANEL WAS INSTALLED IN ACCORDANCE WITH THE REQUIREMENTS OF TASK CARD CP 753-36. FOLLOWING THE INSTALLATION O - [SDR F3LA200800153](https://openairdocs.org/sdr/F3LA200800153.md): Floorbeam · corroded · Apr 4, 2008 · N916FR · Airbus A319112 · Fuselage Main, Floor Beam > DURING C4 S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON THE FORWARD LAVATORY FLOOR ANGLE BRACKET, ON ITS UNDERSIDE. MAINTENANCE REMOVED AND REPLACED THE ANGLE BRACKET IN ACCORDANCE WITH THE REQUIREMENTS OF A0-25EO-20299. UPON COMPETION OF THE REPLAC - [SDR F3LA200800151](https://openairdocs.org/sdr/F3LA200800151.md): Floor Support · corroded · Apr 4, 2008 · N916FR · Airbus A319112 · Fuselage Miscellaneous Structure > DURING C4 S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND AROUND THE NUT CLIP HOLES ON FLOOR BEAM Y1292 BETWEEN FRAMES 68 AND 69. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-42-11, PARAGRAPH 6. UPON C - [SDR F3LA200800140](https://openairdocs.org/sdr/F3LA200800140.md): Shear Plate · corroded · Apr 4, 2008 · N916FR · Airbus A319112 · Fuselage Miscellaneous Structure > DURING C4 S1 CHECK INSPECTION REPORTED CORROSION WAS FOUND ON SHEAR PLATE AT FLOORBEAM Y1732 AFT OF FRAME 69. MAINTENANCE REMOVED AND REPLACED SHEAR PLATE IN ACCORDANCE WITH SRM 51-42-1 PARAGRAPH 6, 7 AND EA A9-53R-30196. UPON COMPLETION OF THE INSTALLATION - [SDR F3LA200800139](https://openairdocs.org/sdr/F3LA200800139.md): Shear Plate · corroded · Apr 4, 2008 · N916FR · Airbus A319112 · Fuselage Miscellaneous Structure > DURING C4 S1 C-CHECK INSPECTION REPORTED CORROSION WAS FOUND ON SHEAR PLATE AT FLOORBEAM Y1732 AFT OF FRAME 69. MAINTENANCE REMOVED AND REPLACE SHEAR PLATE IN ACCORDANCE WITH SRM 51-42-11 PARAGRAPH 6, 7, 13 AND EA A9-53R-30196. UPON COMPLETION OF THE INSTALL - [SDR F3LA200800138](https://openairdocs.org/sdr/F3LA200800138.md): Support · corroded · Apr 4, 2008 · N916FR · Airbus A319112 · Fuselage Miscellaneous Structure > DURING C4 S1 C-CHECK, INSPECTION REPORTED CORROSION WAS FOUND AT FRAME SUPPORT OF FLOORBEAM Y1732 AFT OF FRAME 69. MAINTENANCE REMOVED AND REPLACED FRAME SUPPORT IN ACCORDANCE WITH SRM 51-42-11 PARAGRAPH 6, 7 AND 14 AND EA A9-53R-30196. UPON COMPLETION OF THE - [SDR F3LA200800137](https://openairdocs.org/sdr/F3LA200800137.md): Support · corroded · Apr 4, 2008 · N916FR · Airbus A319112 · Fuselage Miscellaneous Structure > DURING C4 S1 C-CHECK, INSPECTION REPORTED CORROSION WAS FOUND AT FRAME SUPPORT OF FLOORBEAM Y1732 AFT OF FRAME 69. MAINTENANCE REMOVED AND REPLACED FRAME SUPPORT IN ACCORDANCE WITH SRM 51-42-11 AND SRM 51-72-11 AND SRM 51-44-11. UPON COMPLETION OF THE INSTAL - [SDR F3LA200800200](https://openairdocs.org/sdr/F3LA200800200.md): Support Bracket · corroded · Apr 3, 2008 · N916FR · Airbus A319112 · Landing Gear Doors > DURING C4 S1 C CHECK INSPECTION NOTED THE NOSE LANDING GEAR DECORATIVE DOOR LOWER ATTACH POINTS ON STRUT WERE CORRODED AND WORN. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR SUPPORT BRACKET IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 32-22-15-400-001 - [SDR F3LA200700277](https://openairdocs.org/sdr/F3LA200700277.md): Battery · discharged · Oct 8, 2007 · N916FR · Airbus A319112 · Battery/Charger System > FLIGHT CREW REPORTED EMERGENCY LIGHTS "ON" CAUSING LOW VOLTAGE ON AIRCRAFT BATTERY. REMOVED AND REPLACED NR 1 MAIN BATTERY IAW AMM 24-38-37 PB401. OPS CHECKED GOOD. - [SDR F3LA200600158](https://openairdocs.org/sdr/F3LA200600158.md): Cable · broken · Nov 6, 2006 · N916FR · Airbus A319112 · Escape Slide > DURING C-3 CHECK, INSPECTION REPORTED RT EMERGENCY EXIT SLIDE INFLATION CABLE BROKEN. REPLACED RESERVOIR IAW AMM 25-62-46. - [SDR F3LA200600107](https://openairdocs.org/sdr/F3LA200600107.md): Line · leaking · Sep 8, 2006 · N916FR · Airbus A319112 · Hydraulic System, Main > DURING CRUISE, FLIGHT CREW REPORTED ECAM READING: HYD GREEN RSVR LO LVL G ENG 1 NR 1 PUMP LO PRESS. FOUND NR 1 ENG HYD LOW PRESSURE SWITCH LINE LEAKING. REPLACED LINE AND LEAK CHECKED NORMAL IAW AMM 29-11-49-000-009 AND 29-11-49-400-005. - [SDR F3LA200600040](https://openairdocs.org/sdr/F3LA200600040.md): Filter · dirty · Jun 7, 2006 · N916FR · Airbus A319112 · Air Distribution System > ON SHORT FINAL, A PLASTIC-TYPE BURNING ODOR, WHICH DISSIPATED ON LANDING, NO SMOKE. PERFORMED VISUAL INSP OF CABIN LIVE TV SYSTEM. FOUND SYSTEM OPERATIONAL. PERFORMED TSM TASK 24-00-00-810-823 & TSM TASK 26-15-00-810-804 FOR FUMES & ODORS. NO FAULTS, DAMAG - [SDR F3LA200500014](https://openairdocs.org/sdr/F3LA200500014.md): Fan · inoperative · Mar 22, 2005 · N916FR · Airbus A319112 · Air Distribution Fan > FLIGHT CREW REPORTED VENT EXTRACT FAULT. NOTICED AIRCRAFT VIBRATION, FRONT RIGHTSIDE, AND SMELL OF ELECTRICAL SMOKE FRONT TO BACK OF AIRCRAFT. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE VERIFIED VENT EXTRACT FAN FAILURE AS CAUSE OF ODOR ## 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 = 'N916FR' AND deregistration_id = 'N916FR-2009-04-13' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N916FR-2009-04-13/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.