# Service difficulty reports: N932FR, cancelled Dec 13, 2016 A list on [N932FR, cancelled Dec 13, 2016](https://openairdocs.org/deregistered/N932FR-2016-12-13.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR F3LA2015030501116](https://openairdocs.org/sdr/F3LA2015030501116.md): Light · damaged · Mar 5, 2015 · N932FR · Airbus A319111 · Emergency Lighting > DURING A SCHEDULED HEAVY SERVICE CHECK, THE EMER PATH SEAT MOUNTED LIGHT AT SEAT ROW 22 WAS FOUND DAMAGED. R & R LIGHT ASSEMBLY IAW AMM 33-51-18 PB 401. - [SDR F3LA2014012000955](https://openairdocs.org/sdr/F3LA2014012000955.md): Battery · faulty · Jan 18, 2014 · N932FR · Airbus A319111 · Emergency Lighting > HEAVY CHECK FOUND EPSU BATTERY FAULT 13WL. R & R EPSU BATTERY 13WL IAW AMM 33-51-38-000-002 & AMM 33-51-38-400-002, OPERATIONS CHECKED GOOD. - [SDR F3LA2014012000954](https://openairdocs.org/sdr/F3LA2014012000954.md): Battery Pack · faulty · Jan 18, 2014 · N932FR · Airbus A319111 · Emergency Lighting > HEAVY CHECK FOUND EPSU BATTERY FAULT 12WL. R & R EPSU BATTERY 12WL IAW AMM 33-51-38-000-002 & AMM 33-51-38-400-002, OPERATIONS CHECKED GOOD. - [SDR F3LA2013123000952](https://openairdocs.org/sdr/F3LA2013123000952.md): Battery · discharged · Dec 28, 2013 · N932FR · Airbus A319111 · Emergency Lighting > DURING OVERNIGHT INSPECTION THE LT OVERWING EMERGENCY POWER SUPPLY UNIT BATTERY WAS FOUND DEAD. R & R LT OVERWING EPSU BATTERY IAW AMM 33-51-38 PB 401, OPERATIONS CHECKED GOOD. - [SDR F3LA2013061000867](https://openairdocs.org/sdr/F3LA2013061000867.md): Floorbeam · corroded · Jun 5, 2013 · N932FR · Airbus A319111 · Fuselage Main, Floor Beam > AIRCRAFT OUT OF SERVICE FOR C6 CHECK. CORROSION ON FLOORBEAM AT L2 DOOR, FR67, Y1292. FOUND TO BE OVER 50 PERCENT MATERIAL LOSS, OUT OF LIMITS. REMOVED BEAM, LOCATED AND DRILLED NEW BEAM, REF SRM 51-44-11. INSTALLED NEW BEAM REF SRM 51-42-11, PAR 5. - [SDR F3LA2013061000866](https://openairdocs.org/sdr/F3LA2013061000866.md): Floorbeam · corroded · May 29, 2013 · N932FR · Airbus A319111 · Fuselage Main, Floor Beam > ACFT OUT OF SERVICE DUE TO C6 CHECK. AFT GALLEY FLOORBEAM AT R2 DOOR ENTRY -Y1292, FRAME 68 HAS LIGHT CORROSION UPPER SURFACE. BLENDED IAW SRM 53-00-14, PB101, PARA 4.B AND SRM 51-75-12, PARA 3.C.(6)(7). FOUND TO BE WITHIN LIMITS. - [SDR F3LA2013061000865](https://openairdocs.org/sdr/F3LA2013061000865.md): Floorbeam · corroded · May 29, 2013 · N932FR · Airbus A319111 · Fuselage Main, Floor Beam > AIRCRAFT OUT OF SERVICE DUE TO C6 CHECK. DISCREPANCY: AFT GALLEY FLOORBEAM AT L2 DOOR ENTRY Y1292, FRAME 68 HAS CORROSION. CORRECTIVE ACTION: BLENDED PER SRM 53-00-14, PB101, PARAGRAPH 4.B. AND SRM 51-75-12, PARAGRAPH 3.C.(6)(7). FOUND TO BE WITHIN LIMITS. - [SDR F3LA2013040200845](https://openairdocs.org/sdr/F3LA2013040200845.md): Battery Pack · discharged · Mar 31, 2013 · N932FR · Airbus A319111 · Emergency Lighting > EMERGENCY LIGHT TEST FAILS FORWARD EPSU BATTERY. REPLACED FORWARD EPSU BATTERY REF AMM 33-51-38-400-002-A. OP'S CHECK NORMAL. - [SDR F3LA2011022100604](https://openairdocs.org/sdr/F3LA2011022100604.md): Girt Bar · out of adjust · Feb 16, 2011 · N932FR · Airbus A319111 · Emergency Equipment > PRIOR PUSH BACK, RT FWD DOOR WOULD NOT ARM BTB. ADJUSTED R-1 DOOR SLIDE GIRTBAR ATTACH, OPS CHECK GOOD, SLIDE ARMS AS REQUIRED. REF AMM 25-62.00, PB 501. OK TO CONTINUE FLIGHT. - [SDR F3LA2010071400470](https://openairdocs.org/sdr/F3LA2010071400470.md): Wire · loose · Jul 10, 2010 · N932FR · Airbus A319111 · Light System Wiring > LEFT AFT EMERGENCY SIGN LIGHT INOPERATIVE. FOUND WIRE 3351-1306 NOT LOCKED INTO TERMINAL BLOCK 7222VT. RE-LOCKED POWER WIRE INTO TERMINAL BLOCK REFERENCE A319 AMM 33-51-03. OPERATIONAL CHECK NORMAL REFERENCE A319 AMM 33-51-00-710-007. - [SDR F3LA2010071100464](https://openairdocs.org/sdr/F3LA2010071100464.md): Floor Panel · punctured · Jul 6, 2010 · N932FR · Airbus A319111 · Fuselage Floor Panel > REFERENCE HEAVY MAINTENANCE NON ROUTINE N0894. FLOOR PANEL 231KF HAS TWO EACH PUNCTURES. REPAIRED FLOOR PANEL 231KF IAW A319 SRM 53-02-00 SOLUTION A. - [SDR F3LA2010071100465](https://openairdocs.org/sdr/F3LA2010071100465.md): Sill · corroded · Jul 1, 2010 · N932FR · Airbus A319111 · Fuselage Miscellaneous Structure > REFERENCE HEAVY MAINTENANCE NON ROUTINE N0848. L-2 DOOR SILL CORRODED AT GIRT BAR FITTING MOUNT HOLES. REMOVED AND REPLACED L-2 DOOR SILL IAW A319 SRM 51-42-11 AND 51-72-11 PARAGRAPHS 5A AND 6A. - [SDR F3LA2010071400469](https://openairdocs.org/sdr/F3LA2010071400469.md): Sill · corroded · Jun 29, 2010 · N932FR · Airbus A319111 · Fuselage Miscellaneous Structure > R-1 DOOR SILL IS CORRODED. REMOVED AND REPLACED DOOR SILL IAW A319 SRM 51-44-11 AND SRM 51-72-11 PAGE 1 STEP 6. - [SDR F3LA2010070600458](https://openairdocs.org/sdr/F3LA2010070600458.md): Floor Panel · delaminated · Jun 29, 2010 · N932FR · Airbus A319111 · Fuselage Floor Panel > REFERENCE HEAVY MAINTENANCE NON-ROUTINE N0772. CABIN FLOOR PANEL 231KF HAS DELAMINATION ON TOP LAYER. FABRICATED REPLACEMENT PANEL IAW MCG IRM 9701 REVISION G. - [SDR F3LA2010070600459](https://openairdocs.org/sdr/F3LA2010070600459.md): Floor Panel · delaminated · Jun 28, 2010 · N932FR · Airbus A319111 · Fuselage Floor Panel > REFERENCE HEAVY MAINTENANCE NON-ROUTINE N0649. AFT CARGO FLOOR PANEL 161EF DELAMINATED. FABRICATED REPLACEMENT PANEL IAW MCG IRM 9701 REVISION G. - [SDR F3LA2010071400468](https://openairdocs.org/sdr/F3LA2010071400468.md): Sill · corroded · Jun 27, 2010 · N932FR · Airbus A319111 · Fuselage Miscellaneous Structure > FORWARD CARGO DOOR SILL IS CORRODED. REMOVED AND REPLACED FORWARD CARGO DOOR SILL REFERENCE EA A0-53R-31817 REVISION A PAGES 1 THRU 5. - [SDR F3LA2010071400467](https://openairdocs.org/sdr/F3LA2010071400467.md): Shear Plate · corroded · Jun 27, 2010 · N932FR · Airbus A319111 · Fuselage Miscellaneous Structure > REFERENCE HEAVY MAINTENANCE NON ROUTINE N0531. RIGHT SHEAR PLATE IN CABIN FLOOR STRUCTURE BETWEEN FRAME 69 AND FRAME 70 HAS CORROSION. REMOVED AND REPLACED SHEAR PLATE IAW A319 SRM 51-42-11 AND EO A0-53EO-31434. - [SDR F3LA2010071100463](https://openairdocs.org/sdr/F3LA2010071100463.md): Support · corroded · Jun 27, 2010 · N932FR · Airbus A319111 · Fuselage Miscellaneous Structure > REFERENCE HEAVY MAINTENANCE NON ROUTINE N0613. FRAME SUPPORT FROM FRAME 69L TO FRAME 70L AT STRINGER 23L CORRODED. REMOVED AND REPLACED FRAME SUPPORT IAW A319 SRM 51-42-11 PARAGRAPH 6. - [SDR F3LA2010070900462](https://openairdocs.org/sdr/F3LA2010070900462.md): Floorbeam · corroded · Jun 27, 2010 · N932FR · Airbus A319111 · Fuselage Main, Floor Beam > REFERENCE HEAVY MAINTENANCE NON-ROUTINE N0567. CORROSION ON UPPER SIDE OF FLOORBEAM Y1292 AT FRAME 68. REMOVED AND REPLACED FLOORBEAM Y1292 FROM FRAME 68 TO FRAME 70 IAW A319 SRM 51-42-11 AND 51-72-11. - [SDR F3LA2010070400457](https://openairdocs.org/sdr/F3LA2010070400457.md): Support Frame · corroded · Jun 27, 2010 · N932FR · Airbus A319111 · Fuselage Miscellaneous Structure > REFERENCE HEAVY MAINTENANCE NON-ROUTINE N0612. SUPPORT FRAME CORRODED BETWEEN FRAME 69 AND FRAME 70 RIGHT. REMOVED AND REPLACED SUPPORT FRAME IAW SRM 51-44-11. - [SDR F3LA2010070400456](https://openairdocs.org/sdr/F3LA2010070400456.md): Floor Panel · dented · Jun 27, 2010 · N932FR · Airbus A319111 · Fuselage Floor Panel > REFERENCE HEAVY MAINTENANCE NON-ROUTINE N0502. AFT CARGO PIT FLOOR PANEL 152UG DENTED. FABRICATED REPLACEMENT PANEL IAW MCG IRM 9701 REVISION G. - [SDR F3LA2010070400455](https://openairdocs.org/sdr/F3LA2010070400455.md): Floor Panel · dented · Jun 27, 2010 · N932FR · Airbus A319111 · Fuselage Floor Panel > REFERENCE HEAVY MAINTENANCE NON-ROUTINE NO523. AFT CARGO FLOOR PANEL 152TG DENTED WITH COMPRESSION DAMAGE. FABRICATED REPLACEMENT PANEL IAW MCG IRM 9701 REVISION G. - [SDR F3LA2010070400454](https://openairdocs.org/sdr/F3LA2010070400454.md): Floor Panel · damaged · Jun 27, 2010 · N932FR · Airbus A319111 · Fuselage Floor Panel > REFERENCE HEAVY MAINTENANCE NON-ROUTINE N0505. AFT CARGO PIT FLOOR PANEL 151UG IS DENTED CRACKED AND HAS COMPRESSION DAMAGE. FABRICATED REPLACEMENT FLOOR PANEL IAW MCG IRM 9701 REVISION G. - [SDR F3LA2010070400453](https://openairdocs.org/sdr/F3LA2010070400453.md): Floor Panel · damaged · Jun 27, 2010 · N932FR · Airbus A319111 · Fuselage Floor Panel > REFERENCE HEAVY MAINTENANCE NON-ROUTINE N0524. AFT CARGO FLOOR PANEL 151AE DENTED WITH COMPRESSION DAMAGE. FABRICATED REPLACEMENT PANEL IAW MCG IRM 9701 REVISION G. - [SDR F3LA2010070400452](https://openairdocs.org/sdr/F3LA2010070400452.md): Floor Panel · dented · Jun 27, 2010 · N932FR · Airbus A319111 · Fuselage Floor Panel > REFERENCE HEAVY MAINTENANCE NON-ROUTINE N0504. AFT CARGO FLOOR PANEL 152XG DENTED. FABRICATED REPLACEMENT PANEL IAW MCG IRM 9701 REVISION G. - [SDR F3LA2010070400447](https://openairdocs.org/sdr/F3LA2010070400447.md): Floor Panel · damaged · Jun 27, 2010 · N932FR · Airbus A319111 · Fuselage Floor Panel > REFERENCE HEAVY MAINTENANCE NON-ROUTINE N0526. AFT CARGO FLOOR PANEL 151BE HAS 30 SQUARE INCHES OF DENTS WITH CRACKS AND COMPRESSION DAMAGE. FABRICATED REPLACEMENT PANEL IAW MCG IRM 9701 REVISION G. - [SDR F3LA2010070300446](https://openairdocs.org/sdr/F3LA2010070300446.md): Floor Panel · dented · Jun 27, 2010 · N932FR · Airbus A319111 · Fuselage Floor Panel > REFERENCE HEAVY MAINTENANCE NON-ROUTINE N0473. BULK CARGO FLOOR PANEL 161CF HAS APPROXIMATELY 20 SQUARE INCHES OF DENTS WITH COMPRESSION DAMAGE. FABRICATED REPLACEMENT PANEL 161CF IAW MCG IRM 9701 REVISION G. - [SDR F3LA2010070900461](https://openairdocs.org/sdr/F3LA2010070900461.md): Floor Panel · damaged · Jun 26, 2010 · N932FR · Airbus A319111 · Fuselage Floor Panel > REFERENCE HEAVY MAINTENANCE NON-ROUTINE N0648. AFT CARGO FLOOR PANEL 162EF MISSING SKIN AT CORNER. FABRICATED REPLACEMENT PANEL IAW MCG IRM 9701 REVISION G. - [SDR F3LA2010070400451](https://openairdocs.org/sdr/F3LA2010070400451.md): Skin · damaged · Jun 18, 2010 · N932FR · Airbus A319111 · Fuselage Main, Plate/Skin > REFERENCE HEAVY MAINTENANCE NON-ROUTINE N0003. TEMPORARY REPAIR INSTALLED AT FRAME 12 LEFT AT STRINGER 19 LEFT. INSTALLED PERMANENT REPAIR IAW AIRBUS SRM 53-11-11 PARAGRAPH 5E FIGURE 208 AND EA A9-53R-30716. - [SDR F3LA2010070400450](https://openairdocs.org/sdr/F3LA2010070400450.md): Skin · damaged · Jun 18, 2010 · N932FR · Airbus A319111 · Fuselage Main, Plate/Skin > REFERENCE HEAVY MAINTENANCE NON-ROUTINE N0005. TEMPORARY REPAIR INSTALLED AT FRAME 16 LEFT AT STRINGER 16 LEFT. INSTALLED PERMANENT REPAIR IAW AIRBUS SRM 53-11-11 PARAGRAPH 5B FIGURE 208 AND EA A9-53R-30716. - [SDR F3LA2010070400448](https://openairdocs.org/sdr/F3LA2010070400448.md): Skin · damaged · Jun 18, 2010 · N932FR · Airbus A319111 · Fuselage Main, Plate/Skin > REFERENCE HEAVY MAINTENANCE NON-ROUTINE N0006. TEMPORARY FASTENER INSTALLED AT FRAME 13 LEFT AT STRINGER 18 LEFT. INSTALLED PERMANENT REPAIR IAW AIRBUS SRM 53-11-11 PARAGRAPH 5.E. FIGURE 208 AND EA A9-53R-30716. - [SDR F3LA2008110300707](https://openairdocs.org/sdr/F3LA2008110300707.md): Sill · corroded · Nov 1, 2008 · N932FR · Airbus A319111 · Fuselage Miscellaneous Structure > DURING C3 C-CHECK, INSPECTION NOTED L2 DOOR SILL, AFT OF GIRT BAR FITTING, AFT OUTBOARD NUT PLATE HOLE HAS SIGNS OF CORROSION. MAINTENANCE REMOVED NUT PLATE IN ACCORDANCE WITH A319 SRM 51-42-11, ENLARGED HOLE TO CLEAN CORROSION, PRIMED AND PAINTED IN ACCORDAN - [SDR F3LA2008110300706](https://openairdocs.org/sdr/F3LA2008110300706.md): Floor Panel · corroded · Nov 1, 2008 · N932FR · Airbus A319111 · Fuselage Floor Panel > DURING C3 C-CHECK, INSPECTION NOTED FLOOR PANEL 262FF HAS CORROSION ON THE LOWER SURFACE. MAINTENANCE REPLACED FLOOR PANEL WITH NEW IN ACCORDANCE WITH A319 AMM 53-42-12-400-002. - [SDR F3LA2008110300705](https://openairdocs.org/sdr/F3LA2008110300705.md): Floor Panel · corroded · Nov 1, 2008 · N932FR · Airbus A319111 · Fuselage Floor Panel > DURING C3 C-CHECK, INSPECTION NOTED FLOOR PANEL 261FF HAS CORROSION ON THE LOWER SURFACE. MAINTENANCE REPLACED FLOOR PANEL WITH NEW IN ACCORDANCE WITH A319 AMM 53-42-12-400-002. - [SDR F3LA2008110300701](https://openairdocs.org/sdr/F3LA2008110300701.md): Floorbeam · corroded · Oct 31, 2008 · N932FR · Airbus A319111 · Fuselage Main, Floor Beam > DURING C3 C-CHECK, INSPECTION NOTED LONGERON Y1292 BETWEEN FRAME 66 AND FRAME 68 HAS CORROSION IN NUMEROUS NUT CLIP HOLES. MAINTENANCE REWORKED 4 HOLES TO REMOVE ALL CORROSION IN ACCORDANCE WITH A319 SRM 53-00-14 FIGURE 102. ROTO-PROBED HOLES WITH NO DEFECTS - [SDR F3LA2008110300702](https://openairdocs.org/sdr/F3LA2008110300702.md): Longeron · corroded · Oct 31, 2008 · N932FR · Airbus A319111 · Fuselage Main, Longeron/Stringer > DURING C3 C-CHECK, INSPECTION NOTED LONGERON Y1292 FORWARD OF FRAME 68 HAS CORROSION ON FORWARD INBOARD NUT CLIP HOLE. MAINTENANCE REMOVED CORROSION IN ACCORDANCE WITH A319 SRM 53-00-14, FIGURE 102. ROTO-PROBED HOLES WITH NO DEFECTS NOTED IN ACCORDANCE WITH - [SDR F3LA2008110300704](https://openairdocs.org/sdr/F3LA2008110300704.md): Floorbeam · corroded · Oct 30, 2008 · N932FR · Airbus A319111 · Fuselage Main, Floor Beam > DURING C3 C-CHECK, INSPECTION NOTED LONGERON -Y1292 BETWEEN FRAME 66 AND FRAME 68 HAS CORROSION ON NUMEROUS NUT CLIP HOLES. MAINTENANCE REMOVED DAMAGED BEAM IN ACCORDANCE WITH A319 SRM 51-42-11 PARAGRAPHS 6 AND 7. MAINTENANCE INSTALLED NEW FLOORBEAM IN ACCOR - [SDR F3LA2008110300703](https://openairdocs.org/sdr/F3LA2008110300703.md): Sill · corroded · Oct 30, 2008 · N932FR · Airbus A319111 · Fuselage Miscellaneous Structure > DURING C3 C-CHECK, INSPECTION NOTED R2 DOOR SILL, AFT OF GIRT BAR FITTING, AFT OUTBOARD NUT PLATE HOLE HAS SIGNS OF CORROSION. MAINTENANCE REMOVED NUT PLATE IN ACCORDANCE WITH A319 SRM 51-42-11, ENLARGED HOLE TO CLEAN CORROSION, PRIMED AND PAINTED IN ACCORDAN - [SDR F3LA2008103000700](https://openairdocs.org/sdr/F3LA2008103000700.md): Wire Harness · damaged · Oct 29, 2008 · N932FR · Airbus A319111 · Light System Wiring > DURING C3 C-CHECK, INSPECTION NOTED THE PATH LIGHT PLUG IN FOR ROW 8, SEATS ABC, WAS PULLED OFF. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT WIRING AND PLUG IN ACCORDANCE WITH ASM 33-51-00 SCH 04 P 105, FIGURE 2 AND AMM 33-51-00-710-009. MAINTENANCE - [SDR F3LA200700250](https://openairdocs.org/sdr/F3LA200700250.md): Connector · loose · Sep 24, 2007 · N932FR · Airbus A319111 · Light System Wiring > DURING HEAVY SERVICE CHECK, MAINTENANCE REPORTED EMERGENCY FLOOR PATH LIGHTS INOPERATIVE AT ROWS 15 AND 16. RE-SECURED LOOSE CONNECTOR AT SIDE PANEL. PERFORMED OPERATIONAL CHECK IAW AMM 33-51-00-710-001 AND CHECKED GOOD. - [SDR F3LA200700201](https://openairdocs.org/sdr/F3LA200700201.md): Lamp · inoperative · Aug 17, 2007 · N932FR · Airbus A319111 · Emergency Lighting > DURING HEAVY CHECK, INSPECTION REPORTED EMERGENCY FLOOR PATH WHITE LIGHT AT ROW 5 INOPERATIVE. RELAMPED BOTH LAMPS AT ROW 5 EMERGENCY FLOOR PATH WHITE LIGHT. OPS CHECKED GOOD IAW AMM 33-51-19-400-002. - [SDR F3LA200600123](https://openairdocs.org/sdr/F3LA200600123.md): Control Servo · faulted · Sep 19, 2006 · N932FR · Airbus A319111 · Steering Unit > FLIGHT CREW REPORTED FOLLOWING ECAM: (WHEEL N/W STRL FAULT), AT CRUISE THROUGH LANDING. PRIOR TO LANDING AT SFO, A FLY-BY WAS PERFORMED TO ENSURE THE NOSE WHEEL WAS ALIGNED CORRECTLY. AN EMERGENCY WAS DECLARED UPON LANDING IN SFO AND AIRCRAFT LANDED WITHOUT - [SDR F3LA200600017](https://openairdocs.org/sdr/F3LA200600017.md): Warning Light · illuminated · Apr 17, 2006 · N932FR · Airbus A319111 · Trailing Flap Position Indicating System > DURING APPROACH INTO DEN, FLIGHT CREW RECEIVED A TCAS RA, GENERATED FROM PARALLEL TRAFFIC IN THE AREA AND WAS INSTRUCTED TO INITIATE A GO-AROUND AND CLIMB TO 8000 FT. CLEAN UP AND ACCELERATION WAS NORMAL UNTIL A WING TIP BRAKE ECAM WAS TRIGGERED, WITH FLAPS S - [SDR F3LA200500016](https://openairdocs.org/sdr/F3LA200500016.md): Computer · malfunctioned · Mar 28, 2005 · N932FR · Airbus A319111 · Flight Management Computing Hardware System > AUTOPILOT APPEARED TO ENTER A HARDOVER CONDITION, DISCONNECTED A/P AS ACFT ATTEMPTED TO ROLL RIGHT PAST 30" ADB. PERFORMED AFS TEST, TESTED OK. PERFORMED LAND CAT 3 TEST, TESTED OK. ACCOMPLISHED MEL 02-60-01A. PERFORMED DOWNLOAD OF FLT DATA RECORDER, NO TU ## 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 = 'N932FR' AND deregistration_id = 'N932FR-2016-12-13' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N932FR-2016-12-13/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.