# Service difficulty reports: N910FR

A list on [N910FR](https://openairdocs.org/aircraft/N910FR.md).

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

Page 1 of 2 · 87 reports

- [SDR F3LA201911270144](https://openairdocs.org/sdr/F3LA201911270144.md): Apu · leaking · Nov 23, 2019 · N910FR · Airbus A319112 · Airborne Auxiliary Power Unit (APU) System
  > LP1142467 ITEM 1 & 2 DISCREPENCY --- AT APPROX 10 MI FINAL, STRONG ODOR WAS SMELLED IN FLIGHT DECK. UPON LANDING PACK 1 WAS TURNED OFF WITH LITTLE CHANGE NOTED PACK 2 WAS TURNED OFF AND SMELL EVENTUALLY DISIPATED MOSTLY FLIGHT ATTENDANTS SAID THEY MIGHT HAVE S
- [SDR F3LA2019111320139](https://openairdocs.org/sdr/F3LA2019111320139.md): Unknown · odor · Nov 8, 2019 · N910FR · Airbus A319112 · Air Distribution System
  > LP1232676 ITEM 1 -- FUME EVENT: ON BASE TO FINAL EXTREAMLY STRONG ODOR ONLY ON FLIGHT DECK. /// CORRECTIVE ACTION -- PERFORMED TROUBLESHOOTING OF OIL/SMOKE SMELL IN THE CABIN NO LEAKS OR DEFECTS NOTED AT THIS TIME COULD NOT DUPLICATE DISCREPENCY ON GROUND AC
- [SDR F3LA201909060105](https://openairdocs.org/sdr/F3LA201909060105.md): Attach Angle · corroded · Aug 29, 2019 · N910FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > DISCREPANCY: REFERENCE N/R# 2S13N454 P/R OUTBOARD ATTACHMENT ANGLE CORRODED AT FR67 BEAM-Y765 TOTAL CYCLES 127558. CORRECTIVE ACTION: EVALUATED AND REPLACED OUTBOARD ATTACHMENT ANGLE AT FR 67 BEAM-Y765 IAW SRM 51-73-11 AND SRM 51-72-11-911-001.
- [SDR F3LA201909030094](https://openairdocs.org/sdr/F3LA201909030094.md): Door Sill · corroded · Aug 16, 2019 · N910FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > DISCREPANCY: REFERENCE N/R# 2513N274 DOOR SILL CORRODED AT FWD AND AFT GIRT BAR FITTING ATTACH POINTS CORRECTIVE ACTION: REPAIRED R1 DOOR GIRT BAR FITTING ATTACH POINT IAW SRM 53-11 -14-283-005. SRI REINSPECT REQUIRED AT 60,000 FC FROM AIRCRAFT FIRST FLIGHT RE
- [SDR F3LA201909200117](https://openairdocs.org/sdr/F3LA201909200117.md): Floor Support · corroded · Aug 15, 2019 · N910FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > DISCREPANCY: REFERENCE N/R# 2513NL 93 AFT CABIN, LONGITUDINAL FLOOR PANEL SUPPORT, -Y317, FR65+ 18'~ TOP FLANGE UPR SURFACE, CENTER FASTENER HOLE CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED FLOORBEAM Y317 FR65 IAW SRM 51-72-11-911-002, 53-00-14-283-002.
- [SDR F3LA201909100111](https://openairdocs.org/sdr/F3LA201909100111.md): Floor Support · corroded · Aug 15, 2019 · N910FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > DISCREPANCY: REFERENCE N/R# 2513N377 FWD CABIN LONGITUDINAL FLOORBEAM Y1292 TOP FLANGE CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED FWD CABIN LONGITUDINAL FLOORBEAM Y1292 IAW SRM 51 -72-11-911-001.
- [SDR F3LA201909100110](https://openairdocs.org/sdr/F3LA201909100110.md): Floor Support · corroded · Aug 15, 2019 · N910FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > DISCREPANCY: REFERENCE N/R# 2513NL 90 AFT CABIN, LONGITUDINAL FLOORBEAM-YL 292, FR67, TWO FASTENER HOLES, OTBD UPPER FLANGE, CORRODED. CORRECTIVE ACTION: REMOVED & REPLACED FLOORBEAM-1292 FR67 IAW SRM 51-72-11.
- [SDR F3LA201909100109](https://openairdocs.org/sdr/F3LA201909100109.md): Floor Support · corroded · Aug 15, 2019 · N910FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > DISCREPANCY: REFERENCE N/R# 2513N188 AFT CABIN, LONGITUDINAL FLOORBEAM -Y1292, FR66+ 13" -67+ 12''. TOP FLANGE UPR SURFACE AT SCRIBE LINES CORRODED. CORRECTIVE ACTION: REMOVED & REPLACED FLOORBEAM -1292 FR66 IAW SRM 51-72-11.
- [SDR F3LA201909100108](https://openairdocs.org/sdr/F3LA201909100108.md): Floorbeam · corroded · Aug 15, 2019 · N910FR · Airbus A319112 · Fuselage Main, Floor Beam
  > DISCREPANCY: REFERENCE N/R# 2513N185 FLOORBEAM UNDER PANEL 221 EF HAS CORROSION BETWEEN STA. CL 6 TO STA CL 8. CORRECTIVE ACTION: EVALUATED REMOVED AND REPLACED FLOORBEAM Y+254 IAW SRM 53-11 -14-283-004; SRM 51-42-11 AND SRM 51-72-11-911 -001.
- [SDR F3LA201909060104](https://openairdocs.org/sdr/F3LA201909060104.md): Floor Support · corroded · Aug 15, 2019 · N910FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > DISCREPANCY: REFERENCE N/R# 2513N208 AFT CABIN, LONGITUDINAL FLOORBEAM, -Y765, FR68, CORROSION ACROSS TOP FLANGE UPR SURFACE. CORRECTIVE ACTION: REMOVED AND REPLACED FLOORBEAM -Y765 FR68 IAW SRM 51-72-11-911-002, 53-00-14-283-002, 51-44-11.
- [SDR F3LA201909060103](https://openairdocs.org/sdr/F3LA201909060103.md): Floor Support · corroded · Aug 15, 2019 · N910FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > DISCREPANCY: REFERENCE N/R# 2513N195 AFT CABIN, LONGITUDINAL FLOORBEAM, Y765, 3" FWD OF FR66, TOP FLANGE UPR SURFACE, CENTER FASTENER HOLE CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED FLOORBEAM Y765 FWD OF FR66 IAW SRM 51-72-11 -911-001 AND 51-72-11 -9 11
- [SDR F3LA201909030100](https://openairdocs.org/sdr/F3LA201909030100.md): Door Sill · corroded · Aug 15, 2019 · N910FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > DISCREPANCY: REFERENCE N/R# 2513N273 L1 DOOR SILL CORRODED AT FWD AND AFT GIRT BAR FITTING ATTACH POINTS. CORRECTIVE ACTION: REPAIRED L1 DOOR GIRT BAR FITTING ATTACH POINTS IAW SRM 53-11-14-283-005 SRI REINSPECT REQUIRED AT 60,000 FC FROM FIRST AIRCRAFT FLIGHT
- [SDR F3LA201909030099](https://openairdocs.org/sdr/F3LA201909030099.md): Door Sill · corroded · Aug 15, 2019 · N910FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > DISCREPANCY: REFERENCE N/R# 2513N201 AFT CABIN, LONGITUDINAL FLOORBEAM Y1732, AFT OF AFT GIRT BAR LATCH MOUNT PLATE CORRODED. CORRECTIVE ACTION: EVALUATED AND REPAIRED L-2 DOOR SILL IAW SRM 53-41-14-283-002 AND SRM 53-41-14-300-001. (SEE DETAILS BACK)
- [SDR F3LA201909030098](https://openairdocs.org/sdr/F3LA201909030098.md): Floor Support · corroded · Aug 15, 2019 · N910FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > DISCREPANCY: REFERENCE N/R# 2513N198 AFT CABIN, LONGITUDINAL FLOORBEAM, YL 292, FR67+ 1 O" -FR69 TOP FLANGE UPR SURFACE SCRIBE LINES AND SURFACE AROUND FASTENERS CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED FLOORBEAM AT FR67-69 YL 292 IAW SRM 51-72-11-91
- [SDR F3LA201909030097](https://openairdocs.org/sdr/F3LA201909030097.md): Floorbeam · corroded · Aug 15, 2019 · N910FR · Airbus A319112 · Fuselage Main, Floor Beam
  > DISCREPANCY: REFERENCE N/R# 2513N197 AFT CABIN, LONGITUDINAL FLOORBEAM, YL 292, FR66+ 11" -FR67+9'~ TOP FLANGE UPR SURFACE CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED FLOORBEAM AT FR66-67Y1292 IAW SRM 51-72-11-911-001.
- [SDR F3LA201909030096](https://openairdocs.org/sdr/F3LA201909030096.md): Floor Support · corroded · Aug 15, 2019 · N910FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > DISCREPANCY: REFERENCE N/R# 2513N192 AFT CABIN, LONGITUDINAL FLOORBEAM -Y765, 2" FWD OF FR66, TOP FLANGE UPR SURFACE, CENTER FASTENER HOLE CORRODED CORRECTIVE ACTION: REMOVED AND REPLACED FLOORBEAM -Y765 FR66 IAW SRM 51-72-11 -911 -002, 53-00-14-283-002.
- [SDR F3LA201909030095](https://openairdocs.org/sdr/F3LA201909030095.md): Floorbeam · corroded · Aug 15, 2019 · N910FR · Airbus A319112 · Fuselage Main, Floor Beam
  > DISCREPANCY: REFERENCE N/R# 2513N184 FLOORBEAM UNDER PANEL 221 PF HAS CORROSION Y503.2 AT STA CL 6 TOTAL CYCLES J21558. CORRECTIVE ACTION: EVALUATED AND REPLACED FLOORBEAM Y+503.2 IAW SRM 53-11-14-283-004 SRM 51 -72-11-911 -001 AND SRM 51-44-00.
- [SDR F3LA201909030093](https://openairdocs.org/sdr/F3LA201909030093.md): Floorbeam · corroded · Aug 15, 2019 · N910FR · Airbus A319112 · Fuselage Main, Floor Beam
  > DISCREPANCY: REFERENCE N/R# 2513N194 AFT CABIN, LONGITUDINAL FLOOR PANEL SUPPORT, Y498, FWD OF FR66, TOP FLANGE UPR SURFACE, TWO FASTENER HOLES CORRODED. (FLOORBEAM) REMOVED AND INSTALLED NEW AFT CABIN LONGITUDINAL FLOOR PANEL SUPPORT, Y498, FWD OF FR66 IAW S
- [SDR F3LA201909030092](https://openairdocs.org/sdr/F3LA201909030092.md): Floor Support · corroded · Aug 15, 2019 · N910FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > DISCREPANCY: REFERENCE N/R# 2513N186 AFT CABIN, LONGITUDINAL FLOORBEAM -Y1292, FR64+2.5"-1 O•: TOP FLANGE UPR SURFACE CORRODED. CORRECTIVE ACTION: REMOVED & REPLACED FLOORBEAM -1292 AT FR64 JAW SRM 51-72-11.
- [SDR F3LA201908290090](https://openairdocs.org/sdr/F3LA201908290090.md): Floorbeam · corroded · Aug 15, 2019 · N910FR · Airbus A319112 · Fuselage Main, Floor Beam
  > AFT CABIN, FLOORBEAM Y254, FR69+ 18.5, TOP FLANGE UPR SURFACE, CENTER FASTENER HOLE CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14-283-002. REMOVED & REPLACED FLOORBEAM IAW SRM 51-72-11.
- [SDR F3LA201908290089](https://openairdocs.org/sdr/F3LA201908290089.md): Floorbeam · corroded · Aug 15, 2019 · N910FR · Airbus A319112 · Fuselage Main, Floor Beam
  > AFT CABIN, FLOORBEAM Y1292, FR66 TOP FLANGE UPR SURFACE SCRIBE LINES AND ONE FASTENER HOLE CORRODED. REMOVED CORROSION ON FLOOR BEAM Y1292 FR66. FOUND TO BE OUT OF LIMITS I.AW A319 SRM 53-00-14-283-002.
- [SDR F3LA2019040400030](https://openairdocs.org/sdr/F3LA2019040400030.md): Audio Panel · burned · Apr 2, 2019 · N910FR · Airbus A319112 · Audio Integrating System
  > DISCREPANCY: REFERENCE LP1185665-1. PERFORMED AIR TURN BACK IN KLAS ON TAKE OFF, FIRST OFFICER REPORTED LOUD ELECTRONIC NOISE IN HEADSET, AFTER ROTATION THE #2 ACP LIGHTS ALL ILLUMINATED AND CREW SMELLED A STRONG ELECTRONIC BURNING SMELL. CREW COMPLIED WIT
- [SDR F3LA2018091800438](https://openairdocs.org/sdr/F3LA2018091800438.md): Pump · failed · Sep 16, 2018 · N910FR · Airbus A319112 · Hydraulic Pump (Electric/Engine), Main
  > ATB, Y HYD ENG 2 PUMP LOW PRESSURE. NO OVERHEAT, Y OR G. REMOVED AND REPLACED NR 2 HYDRAULIC PUMP IAW AMM 29-13-51 PB401. T/W F9T0345C DUE DATE 07/19. T/W F9TAB2956C DUE DATE 06/19. OPS CHECK/LEAK CHECK IS SATISFACTORY.
- [SDR F3LA2017113000261](https://openairdocs.org/sdr/F3LA2017113000261.md): Slide · defective · Nov 28, 2017 · N910FR · Airbus A319112 · Escape Slide
  > L1 DOOR SLIDE NOT ARMING. REMOVED AND REPLACED THE LEFT FORWARD DOOR SLIDE IAW AMM 25-62-44PB401. OPERATIONAL CHECKED GOOD.
- [SDR F3LA2017091900225](https://openairdocs.org/sdr/F3LA2017091900225.md): Power Supply · no test · Sep 18, 2017 · N910FR · Airbus A319111 · Emergency Lighting
  > FORWARD POWER SUPPLY FAILED TO TEST AT 10WL. REMOVED AND REPLACED THE POWER SUPPLY IAW AMM 33-51-38, PB401. OPS CHECKED GOOD.
- [SDR F3LA2017020200070](https://openairdocs.org/sdr/F3LA2017020200070.md): Floorbeam · corroded · Jan 20, 2017 · N910FR · Airbus A319112 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM Y254 BETWEEN FR66 AND FR67. REPLACED FLOORBEAM Y254 BETWEEN FR66 AND FR67 IAW SRM 51-72-11-911-001.
- [SDR F3LA2017012500068](https://openairdocs.org/sdr/F3LA2017012500068.md): Floor Support · corroded · Jan 19, 2017 · N910FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > CORROSION ON THE FLOOR SUPPORT Y765 BETWEEN FRAMES 67 AND 68. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW 53-00-14. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11-911-001.
- [SDR F3LA2017020200069](https://openairdocs.org/sdr/F3LA2017020200069.md): Floorbeam · corroded · Jan 17, 2017 · N910FR · Airbus A319112 · Fuselage Main, Floor Beam
  > CORROSION AT FLOORBEAM - Y765 BETWEEN FR67 AND FR68. REMOVED AND REPLACED - Y765 FLOORBEAM AT FR66 TO FR70 IAW SRM 51-72-11-911-001.
- [SDR F3LA2017020200071](https://openairdocs.org/sdr/F3LA2017020200071.md): Floorbeam · corroded · Jan 13, 2017 · N910FR · Airbus A319112 · Fuselage Main, Floor Beam
  > CORROSION AT FLOORBEAM - 1292 JUST FORWARD OF FR68. REPLACED 1292 FR68 FLOORBEAM IAW SRM 51-72-11 AND 51-42-11.
- [SDR F3LA2014082101056](https://openairdocs.org/sdr/F3LA2014082101056.md): Battery Pack · failed · Aug 20, 2014 · N910FR · Airbus A319112 · Emergency Lighting
  > EPSU BATTERY 12WL FAILED CAPACITY TEST AT A8 CHECK INTERVAL. R & R THE BATTERY PACK IAW AMM 33-51-39-000-005-A & 33-51-39-400-005A.
- [SDR F3LA2014082101055](https://openairdocs.org/sdr/F3LA2014082101055.md): Light · inoperative · Aug 20, 2014 · N910FR · Airbus A319112 · Emergency Lighting
  > SEAT EMER EGRESS LIGHT AT ROW 8 FAILED TO ILLUMINATE DURING TEST AT A8 CHECK INTERVAL. R & R THE LAMP ASSEMBLY IAW AMM 33-51-18-000-002A & 33-51-18-400-002A.
- [SDR F3LA2013101500923](https://openairdocs.org/sdr/F3LA2013101500923.md): Floorbeam · corroded · Sep 30, 2013 · N910FR · Airbus A319112 · Fuselage Main, Floor Beam
  > AIRCRAFT OUT OF SERVICE, FOUR C8/S2 CHECK. FLOORBEAM Y1292 HAS CORROSION FWD OF FR 20. REMOVED CORROSION, FLOORBEAM CHECKED OUT OF LIMITS. R & R FLOORBEAM, REF SRM 51-42-11, PARA 7.
- [SDR F3LA2013101500922](https://openairdocs.org/sdr/F3LA2013101500922.md): Floor Support · corroded · Sep 27, 2013 · N910FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > ACFT OUT OF SERVICE FOR C8/S2 CHECK. FWD CABIN FLOOR SUPPORT -Y1292 AT FRAMES 19 - 20, CORRODED OUT OF LIMITS. R & R FLOOR SUPPORT IAW SRM 51-42-11. PARA 5 AND PARA 7.
- [SDR F3LA2013101500921](https://openairdocs.org/sdr/F3LA2013101500921.md): Floorbeam · corroded · Sep 26, 2013 · N910FR · Airbus A319112 · Fuselage Main, Floor Beam
  > ACFT OUT OF SERVICE FOR C8/S2 CHECK. AFT CABIN FLOORBEAM -Y1292 AT FRAME 68, CORRODED OUT OF LIMITS. R & R FLOORBEAM IAW SRM 51-42-11, PARA 7B AND PARA 5.
- [SDR F3LA2013101500920](https://openairdocs.org/sdr/F3LA2013101500920.md): Skin · delaminated · Sep 25, 2013 · N910FR · Airbus A319112 · Elevator, Plate/Skin
  > ACFT OUT OF SERVICE DUE TO C8/52 CHECK. LT ELEVATOR THERMOGHRAPHIC INSPECTION REVEALED INDICATION THAT IS IRREGULAR IN SHAPE AND BLACK IN COLOR, ON UPPER SKIN. SEE NOT REPORT FOR DETAILS. REPAIRED LT ELEVATOR AT 1EA AREA OF LIQUID INGRESS IAW SRM 55-20-00, P
- [SDR F3LA2013101500919](https://openairdocs.org/sdr/F3LA2013101500919.md): Skin · delaminated · Sep 25, 2013 · N910FR · Airbus A319112 · Elevator, Plate/Skin
  > ACFT OUT OF SERVICE FOR C8/S2 CHECK. RT ELEVATOR THERMOGHRAPHIC INSPECTION REVEALED 2EA INDICATIONS IRREGULAR IN SHAPE AND BLACK IN COLOR, ON UPPER SKIN. SEE NDT REPORT FOR DETAILS. CORRECTIVE ACTION: REPAIRED RT ELEVATOR AT 2EA AREA OF LIQUID IAW SRM 55-20-
- [SDR F3LA2013101500918](https://openairdocs.org/sdr/F3LA2013101500918.md): Elt · no test · Sep 23, 2013 · N910FR · Airbus A319112 · Emergency Locator Beacon
  > ACFT OUT OF SERVICE, FOR C8/S2 CHECK. EMERGENCY LOCATOR TRANSMITTER WILL NOT TURN ON. R & R EMERGENCY LOCATOR TRANSMITTER REF AMM 25-65-35, PAGE BLOCK 401, CONFIGURATION 00. OPS CHECK NORMAL, REF AMM 25-65-00-740-051-G.
- [SDR F3LA2013101500917](https://openairdocs.org/sdr/F3LA2013101500917.md): Shear Plate · corroded · Sep 19, 2013 · N910FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > AIRCRAFT OUT OF SERVICE FOR C8/S2 CHECK. AFT CABIN RT LATERAL SHEAR PLATE HAS CORROSION. R & R IAW SRM 51-42-11, PARA 6, 7 AND 13.
- [SDR F3LA2013101500916](https://openairdocs.org/sdr/F3LA2013101500916.md): Shear Plate · cracked · Sep 19, 2013 · N910FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > ACFT OUT OF SERVICE, FOR C8/S2 CHECK. AFT CABIN LT LATERAL SHEAR PLATE CRACKED. R & R IAW SRM 51-42-11, PARA 6, 7 AND 13.
- [SDR F3LA2013101500915](https://openairdocs.org/sdr/F3LA2013101500915.md): Floorbeam · corroded · Sep 18, 2013 · N910FR · Airbus A319112 · Fuselage Main, Floor Beam
  > AIRCRAFT OUT OF SERVICE FOR C8/S2 CHECK. MAIN CABIN FLOORBEAM, Y254 HAS CORROSION AT FRAME 16. REPAIRED FLOORBEAM IAW SRM 53-11-15 PB201.
- [SDR F3LA2013101500914](https://openairdocs.org/sdr/F3LA2013101500914.md): Sill · corroded · Sep 18, 2013 · N910FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > ACFT OUT OF SERVICE FOR C8/S2 CHECK. MAIN CABIN AFT SECTION R2 DOOR SILL HAS CORROSION IN TWO AREAS AT FRAME 68. REPAIRED IAW SRM 53-41-14, FIG 201, SHEET 1 AND FIGURE 201, SHEET 3.
- [SDR F3LA2013101500913](https://openairdocs.org/sdr/F3LA2013101500913.md): Lock · dirty · Sep 14, 2013 · N910FR · Airbus A319112 · Passenger/Crew Doors
  > DURING C8/S2 CHECK. AFT ENTRY DOOR FAILS OPS TEST OF THE INTERLOCK MECHANISM. DISASSEMBLED, CLEANED AND REASSEMBLED, EMERGENCY CONTROL HANDLE IAW AMM 52-13-22-000-002-A, PARA 4.A.(4), AMM 52-13-22-400-001-A, PARA 4.F (18) THROUGH (21) AND AMM 52-10-00-710-002
- [SDR F3LA2013101500912](https://openairdocs.org/sdr/F3LA2013101500912.md): Control Panel · damaged · Sep 14, 2013 · N910FR · Airbus A319112 · Emergency Locator Beacon
  > EMERGENCY LOCATOR TRANSMITTER TEST SWITCH IS INOPERATIVE. R & R EMERGENCY LOCATOR TRANSMITTER REMOTE CONTROL PANEL IAW AMM 25-65-18-020-050-A STEP A AND INSTALLED IAW AMM 25-65-18-420-050-C, STEP A. OPS CHECKED GOOD IAW AMM 25-65-00-740-051-G.
- [SDR F3LA2013042600848](https://openairdocs.org/sdr/F3LA2013042600848.md): Casting · corroded · Apr 22, 2013 · N910FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > FORWARD CARGO DOOR OPENING LOWER AFT CORNER FRAME CRACKED AND CORRODED AT FASTENER HOLE. REMOVED DAMAGED CORNER CASTING. MATCH DRILLED AND INSTALLED NEW CORNER CASTING FORWARD CARGO DOOR CUT OUT AFT LOWER CORNER IAW SRM 51-42-11 AND SRM 51-44-11.
- [SDR F3LA2012011700700](https://openairdocs.org/sdr/F3LA2012011700700.md): Sill · corroded · Jan 16, 2012 · N910FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > C-CHECK: FWD CARGO BETWEEN FRAME 27 AND FRAME 28 DOOR SILL HAS CORROSION. R & R DOOR SILL IAW SRM 51 -42-11, SRM 51 -44-11.
- [SDR F3LA2010072700523](https://openairdocs.org/sdr/F3LA2010072700523.md): Support · corroded · Oct 8, 2010 · N910FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > C-CHECK: NON ROUTINE N0420; UPON REMOVAL OF SHEAR PLATE AT FRAME 68R TO 69R FOUND SUPPORT CORRODED. AIRCRAFT IS IN C-CHECK AND CORROSION IS OUT OF LIMITS. REMOVED AND REPLACED SUPPORT IAW A319 SRM 51-72-11 PAGE 1 & PAGE 2.
- [SDR F3LA2010072700522](https://openairdocs.org/sdr/F3LA2010072700522.md): Floor Panel · delaminated · Oct 8, 2010 · N910FR · Airbus A319112 · Fuselage Floor Panel
  > C-CHECK: NON ROUTINE N0434; AT CARGO PIT PANEL 151HE UPPER SURFACE IS DELEMINATED. FABRICATED FLOOR PANEL IAW MC GILL IRM 9701 REVISION G, PARA 3.2 TABLE 1.
- [SDR F3LA2010072700521](https://openairdocs.org/sdr/F3LA2010072700521.md): Shear Plate · corroded · Oct 8, 2010 · N910FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > C-CHECK: NON ROUTINE N0330 LT SHEAR PLATE AT FRAME 69 TO UPPER CABIN HAS CORROSION. REMOVED AND REPLACED LT SHEAR PLATE IAW FRONTIER E) A0-53EO-31434 REVISION ORIGINAL.
- [SDR F3LA2010072700520](https://openairdocs.org/sdr/F3LA2010072700520.md): Shear Plate · corroded · Oct 8, 2010 · N910FR · Airbus A319112 · Fuselage Miscellaneous Structure
  > C-CHECK: NON ROUTINE N0331; AFT MAIN CABIN RT SHEAR PLATE AT FRAME 69R TO 70R HAS CORROSION. AIRCRAFT IS IN C-CHECK, SHEAR PLATE ALSO OLD CONFIGURATION. REMOVED AND REPLACED SHEAR PLATE IAW FRONTIER EO A)-53EO-31434 REV ORIGINAL AND A319 SRM 51-42-11.
- [SDR F3LA2010072700519](https://openairdocs.org/sdr/F3LA2010072700519.md): Floorbeam · corroded · Oct 8, 2010 · N910FR · Airbus A319112 · Fuselage Main, Floor Beam
  > C-CHECK: NON ROUTINE N0289; AFT CABIN RIGHT FLOORBEAM - Y1292 FORWARD OF FRAME 68R HAS AN AREA OF CORROSION. AIRCRAFT IS IN C-CHECK AFTER CORROSION REMOVED FOUND TO BE OUT OF LIMITS IAW A319 SRM 53-00-14 FIG 102. REMOVED AND REPLACED FLOORBEAM -Y1292 BETWEEN

Next page: https://openairdocs.org/aircraft/N910FR/reports.md?page=2

## 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 = 'N910FR' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N910FR/reports

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