# Service difficulty reports: N271LV

A list on [N271LV](https://openairdocs.org/aircraft/N271LV.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 6 · 251 reports

- [SDR SWAA2022020766120](https://openairdocs.org/sdr/SWAA2022020766120.md): Bracket · cracked · Feb 1, 2022 · N271LV · Boeing 737* · Trailing Edge Flaps
  > RIGHT WING WEB BRACKET BELOW TRAILING EDGE FIXED PANEL OUTBD CLIP CRACKED AT DEFLECTION RIB.; / [01] REMOVED AND REPLACED BRACKET REF SRM 51-40-02.
- [SDR SWAA2022020766119](https://openairdocs.org/sdr/SWAA2022020766119.md): Bracket · cracked · Feb 1, 2022 · N271LV · Boeing 737* · Trailing Edge Flaps
  > RIGHT WING SEAL RETAINER BRACKET ON WEB BRACKET BELOW TRAILING EDGE FIXED PANEL CRACKED.; / [01] REMOVED AND REPLACED BRACKET REF SRM 51-40-02
- [SDR SWAA2021031554380](https://openairdocs.org/sdr/SWAA2021031554380.md): Sign · missing · Mar 11, 2021 · N271LV · Boeing 737705 · Emergency Lighting
  > R1 DOOR LOWER EXIT SIGN MISSING DIRECTIONAL ARROW. / INSTALLED R1 DOOR LOWER EXIT SIGN IAW AMM 33-51-01
- [SDR SWAA2021020445415](https://openairdocs.org/sdr/SWAA2021020445415.md): Lamp · inoperative · Jan 31, 2021 · N271LV · Boeing 737705 · Emergency Lighting
  > ISLE EMERGENCY LIGHT AT 16DEF IS INOP. / REPLACED EMERGENCY EXIT LIGHT LAMP AT SEAT ROW 16DEF IAW AMM 33-51-03-960-801 LIGHT CHECKS GOOD 'A'TAG D90421
- [SDR SWAA2020082610389](https://openairdocs.org/sdr/SWAA2020082610389.md): Light · faulty · Aug 22, 2020 · N271LV · Boeing 737705 · Emergency Lighting
  > FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT TURNS ON WHEN CABIN LIGHTS TURNED ON THE BRIGHT SETTING / FOUND LIGHT IN QUESTION TO BE ENTRY DOOR THRESHOLD ILLUMINATION LIGHT. ILLUMINATION LIGHT OPS CHECK GOOD PER S.I.P. EMERGENCY EXIT. LIGHTS OPS CHECK GOOD PER M.M.
- [SDR SWAA2020041743124](https://openairdocs.org/sdr/SWAA2020041743124.md): Smoke Detector · faulty · Apr 16, 2020 · N271LV · Boeing 737705 · Smoke Detection
  > SUPPLEMENTAL INFORMATION: FORWARD LAV SMOKE ALARM ACTIVATED FOR DURATION OF APPROACH & TAXI TO GATE. NO PASSENGERS WERE IN LAVATORY / CLOSING DMA #0405036 R&R FWD LAV SMOKE DETECTOR IAW AMM 26-14-01 CLEARING # 36546
- [SDR SWAA2021080519504](https://openairdocs.org/sdr/SWAA2021080519504.md): Strip · damaged · Mar 3, 2020 · N271LV · Boeing 737705 · Fuselage Miscellaneous Structure
  > ACB FLOOR PANELS 140DF AND 140CF I/B CAP STRIPS ARE DAMAGED / RECEIVED 2EA NEW CAP STRIPS FOR ACB FLOOR PANELS 140DF AND 140CF. ACB FLOOR PANELS 140DF AND 140CF I/B CAP STRIPS WILL BE INSTALLED ON CUSTOMER CARD JPANEL-141-CLOSE
- [SDR SWAA2020031142350](https://openairdocs.org/sdr/SWAA2020031142350.md): Battery Pack · discharged · Mar 3, 2020 · N271LV · Boeing 737705 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK M1673 ARE INOP. CHARGED M1673 BATTERY PER AMM 33-51-06-610-802. PERFORMED SATISFACTORY EMERGENCY LIGHTS OPERATIONAL TEST PER AMM 33-51-00-710-801.
- [SDR SWAA2020032319489](https://openairdocs.org/sdr/SWAA2020032319489.md): Floor Panel · out of alignment · Feb 26, 2020 · N271LV · Boeing 737705 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 241AAF; 3 FASTENER HOLES ALONG FWD EDGE DO NOT LINE UP WITH EXISTING STRUCTURE / PASSENGER CABIN FLOOR PANEL 241AAF; 3 FASTENER HOLES ALONG FWD EDGE THAT DO NOT LINE UP WITH EXISTING STRUCTURE WERE RELOCATED IAW SRM 53-00-50-2R-6 56
- [SDR SWAA2020030442120](https://openairdocs.org/sdr/SWAA2020030442120.md): Floor Panel · defective · Feb 26, 2020 · N271LV · Boeing 737705 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 241AAF, 3 FASTENER HOLES ALONG FWD EDGE DO NOT LINE UP WITH EXISTING STRUCTURE PASSENGER CABIN FLOOR PANEL 241AAF, 3 FASTENER HOLES ALONG FWD EDGE THAT DO NOT LINE UP WITH EXISTING STRUCTURE WERE RELOCATED IAW SRM 53-00-50-2
- [SDR SWAA2021071319484](https://openairdocs.org/sdr/SWAA2021071319484.md): Skin · delaminated · Feb 24, 2020 · N271LV · Boeing 737705 · Trailing Edge Flaps
  > DELAMINATION ON L/W I/B AFT FLAP LOWER SURFACE / DELAMINATION OF FIBERGLASS OVERLAY PLIES IN 3EA. AREAS ON L/W I/B AFT FLAP LOWER SURFACE WERE REMOVED AND REAPPLIED PER SRM 51-70-04-2R-0.
- [SDR SWAA2020032319451](https://openairdocs.org/sdr/SWAA2020032319451.md): Skin · bent · Feb 21, 2020 · N271LV · Boeing 737705 · Passenger/Crew Doors
  > FWD ENTRY DOOR EXTERNAL SKIN IS BENT AT LOWER HINGE CUTOUT EDGE. L=5.65'; W=.8'; DEPTH.091 / EVALUATED DAMAGE ON FED EXTERNAL SKIN LOWER HINGE CUTOUT. L=5.6'; W=0.8' D=0.0091'. DAMAGE FOUND TO BE BEYOND THE LIMITS IAW SRM 52-10-01-1A-1. FIG 104. ACCOMPLISHED
- [SDR SWAA2020032319432](https://openairdocs.org/sdr/SWAA2020032319432.md): Skin · damaged · Feb 20, 2020 · N271LV · Boeing 737705 · Fuselage Main, Plate/Skin
  > (SKYLINE DTIP) FUSELAGE SKIN REPAIR AT BS 1025; S-15L TO S-17AL REQUIRES ADDITIONAL REWORK. (REF ESR: 20-01837) / FUSELAGE SKIN REPAIR AT BS 1025; S-15L TO S-17AL WAS REPAIRED IAW ATS ER 20-01871 REV IR DATED 28FEB2020 AND EA 1-753-36639 REV IR
- [SDR SWAA2020032331170](https://openairdocs.org/sdr/SWAA2020032331170.md): Skin · dented · Feb 20, 2020 · N271LV · Boeing 737705 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN HAS A DENT BS 1006+3.7; 2.9' BELOW STR 14L; DENT MEASURES: L=2.3'; W=1.9'; Y=.004' W/Y=475 / REPAIR ACCOMPLISHED ON ER NO 20-01888 REV IR & EA NO 1-753-36715 REV IR
- [SDR SWAA2020032331171](https://openairdocs.org/sdr/SWAA2020032331171.md): Skin · dented · Feb 20, 2020 · N271LV · Boeing 737705 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN HAS A DENT BS 992+4; 1' BELOW STR 14L; DENT MEASURES: L=.8'; W=.6'; Y=.003' W/Y=200 / DAMAGE REPAIRED/INSPECTED & EVALUATED PER EA 1-753-36715 REV IR (ATS ER 20-01888 REV IR) INSTALLED DENT DOT PER MPM 52.03.01.02 PARAGRAPH 2.C.(1)(B) NO FURTHER
- [SDR SWAA2020032331172](https://openairdocs.org/sdr/SWAA2020032331172.md): Skin · dented · Feb 20, 2020 · N271LV · Boeing 737705 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN HAS A DENT BS 992+6;.7' BELOW STR 14L; DENT MEASURES: L=.5'; W=.4'; Y=.004' W/Y=100 / DAMAGE REPAIRED/INSPECTED & EVALUATED PER EA 1-753-36715 REV IR (ATS ER 20-01888 REV IR) INSTALLED DENT DOT PER MPM 52.03.01.02 PARAGRAPH 2.C.(1).(B) NO FURTHE
- [SDR SWAA2020031642498](https://openairdocs.org/sdr/SWAA2020031642498.md): Skin · dented · Feb 20, 2020 · N271LV · Boeing 737705 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN HAS A DENT BS 992+6,.7" BELOW STR 14L, DENT MEASURES: L=.5", W=.4", Y=.004" W/Y=100 DAMAGE REPAIRED/INSPECTED & EVALUATED PER EA 1-753-36715 REV IR (ATS ER 20-01888 REV IR) INSTALLED DENT DOT PER MPM 52.03.01.02 PARAGRAPH 2.C.(1).(B) NO
- [SDR SWAA2020031642497](https://openairdocs.org/sdr/SWAA2020031642497.md): Skin · dented · Feb 20, 2020 · N271LV · Boeing 737705 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN HAS A DENT BS 992+4, 1" BELOW STR 14L, DENT MEASURES: L=.8", W=.6", Y=.003" W/Y=200 DAMAGE REPAIRED/INSPECTED & EVALUATED PER EA 1-753-36715 REV IR (ATS ER 20-01888 REV IR) INSTALLED DENT DOT PER MPM 52.03.01.02 PARAGRAPH 2.C.(1)(B) NO FU
- [SDR SWAA2020031642496](https://openairdocs.org/sdr/SWAA2020031642496.md): Skin · dented · Feb 20, 2020 · N271LV · Boeing 737705 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN HAS A DENT BS 1006+3.7, 2.9" BELOW STR 14L, DENT MEASURES: L=2.3", W=1.9", Y=.004" W/Y=475 REPAIR ACCOMPLISHED ON ER NO 20-01888 REV IR & EA NO 1-753-36715 REV IR FACT AS A RESULT OF POST REPAIR INSPECTION
- [SDR SWAA2020031202394](https://openairdocs.org/sdr/SWAA2020031202394.md): Skin · not reported · Feb 20, 2020 · N271LV · Boeing 737705 · Fuselage Main, Plate/Skin
  > (SKYLINE DTIP) FUSELAGE SKIN REPAIR AT BS 1025, S-15L TO S-17AL REQUIRES ADDITIONAL REWORK. (REF ESR: 20-01837) FUSELAGE SKIN REPAIR AT BS 1025, S-15L TO S-17AL WAS REPAIRED IAW ATS ER 20-01871 REV IR DATED 28FEB2020 AND EA 1-753-36639 REV IR
- [SDR SWAA2021082019396](https://openairdocs.org/sdr/SWAA2021082019396.md): Skin · corroded · Feb 19, 2020 · N271LV · Boeing 737705 · Fuselage Main, Plate/Skin
  > CORROSION ON FUSELAGE SKIN AROUND DRAIN VALVE BS 480+18; 6.5' BELOW STR 28L / BLENDED CORROSION ON FUSELAGE SKIN AROUND DRAIN VALVE BS 480+18 6.5' BELOW STR 28 L/H INSPECTED & EVALUATED PER EA 1-753-36709 REV IR & ATS ER 20-01892 REV IR THIS EA THE DAMAGE IS A
- [SDR SWAA2021082019397](https://openairdocs.org/sdr/SWAA2021082019397.md): Skin · corroded · Feb 19, 2020 · N271LV · Boeing 737705 · Fuselage Main, Plate/Skin
  > CORROSION ON FUSELAGE SKIN AROUND DRAIN VALVE BS 500A+3; 6.5' BELOW STR 28L / BLENDED CORROSION ON FUSELAGE SKIN AROUND DRAIN VALVE BS 500A+3 6.5' BELOW STR 28 L/H INSPECTED & EVALUATED PER EA 1-753-36709 REV IR & ATS ER 20-01892. REV IR AS PER THIS EA THE DAM
- [SDR SWAA2021081719422](https://openairdocs.org/sdr/SWAA2021081719422.md): Bracket · cracked · Feb 19, 2020 · N271LV · Boeing 737705 · Fuselage Miscellaneous Structure
  > BRACKET P/N 272A9112-31 @B.S. 663 RBL40 CRACKED / REMOVED; LOCATED; DRILLED AND INSTALLED BRACKET P.N. 272A9112-31 PER SRM 51-40-02 PAR.D(6); SRM 51-40-05 FIG.4; SRM 51-40-02 PAR D(1-5) AND DWG.111A7000 AND DWG.272A9112. APPLIED CHEM.CONVERSION COATING AND PRI
- [SDR SWAA2021081319379](https://openairdocs.org/sdr/SWAA2021081319379.md): Angle · corroded · Feb 19, 2020 · N271LV · Boeing 737705 · Fuselage Miscellaneous Structure
  > ***CORROSION*** APU TRANSITION DUCT ATTACH FLANGE STA 1124 R/H SIDE / REMOVED AND INSTALLED A NEW APU TRANSITION DUCT ATTACH STIFFENER ANGLE PER SRM 51-40-01-0G-0 AND DWG # 148A8650
- [SDR SWAA2021072219395](https://openairdocs.org/sdr/SWAA2021072219395.md): Floor Support · bent · Feb 19, 2020 · N271LV · Boeing 737705 · Fuselage Miscellaneous Structure
  > BENT FLOOR SUPPORT AT AFT CARGO BAY BS787+8 RBL17 WL 157. / REPLACED FLOOR SUPPORT AT ACB. BS 787+8' RBL 77 WL 157 AS PER SRM 51-40-02-0G-0 AND DRAWING# 146A7500 I.D 0004.; FLOOR SUPPORT WAS EVALUATED AND NO FOUND ALLOWABLE DAMAGE AS PER SRM 53-00-53-1A-2
- [SDR SWAA2021071519384](https://openairdocs.org/sdr/SWAA2021071519384.md): Support Angle · corroded · Feb 19, 2020 · N271LV · Boeing 737705 · Fuselage Miscellaneous Structure
  > ***CORROSION*** AROUND THE FASTENER ON AFT FLOOR TO BULKHEAD PANEL SUPPORT ANGLE BS947 LBL7 WL178. / REPLACE BULKHEAD PANEL SUPPORT ANGLE AT BS 947 LBL 7 WL 178 AS PER. DWG. 149A8118 AND SRM 51-40-02-0G-0. 59868U FEB-28-20.
- [SDR SWAA2021071519420](https://openairdocs.org/sdr/SWAA2021071519420.md): Support Angle · cracked · Feb 19, 2020 · N271LV · Boeing 737705 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL SUPPORT ANGLE AT FWD CARGO BAY BS500B FWD SIDE LBL25 WL156. / REMOVED AND REPLACED ON INTERCOSTAL SUPPORT ANGLE AT FWD CARGO BAY BS 500B FWD SIDE LBL 25 IAW SRM 51-40-02 AND DWG 143A7505 REV B P/N 143A7502U159. 80641U 27FEB20
- [SDR SWAA2020032331169](https://openairdocs.org/sdr/SWAA2020032331169.md): Skin · gouged · Feb 19, 2020 · N271LV · Boeing 737705 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN HAS A GOUGE BS 400+2.4; STR 27R / FUSELAGE SKIN GOUGE BS 400+2.4; STR 27R REPAIRED IAW ATS ER 20-01914; REV IR; DATED 10-MAR-2020 AND PER EA NO: 1-753-36694 REV IR 55981U 11MAR20
- [SDR SWAA2020032319418](https://openairdocs.org/sdr/SWAA2020032319418.md): Seat Track · chafed · Feb 19, 2020 · N271LV · Boeing 737705 · Fuselage, Seat/Cargo Attach Fittings
  > CHAFING ON FLOOR RAIL AT FWD CARGO BAY BS500A LBL8 WL157. / REMOVED DAMAGE FROM FCB FLOOR RAIL BS500A LBL8 WL157 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 SEAT CHANNEL EXTRUSION BAC1510-1355 7050-T76511 LOT# 1330259-2 TO MACHIN SHOP AND RECIEVED CHANNEL
- [SDR SWAA2020032319405](https://openairdocs.org/sdr/SWAA2020032319405.md): Support · corroded · Feb 19, 2020 · N271LV · Boeing 737705 · Fuselage Miscellaneous Structure
  > ***CORROSION*** ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS500 - 500C LBL23 WL157. / SIDEPLATE CHANNEL SUPPORT FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-2; MULTIPLES AREAS 1 X 1 MORE THAN 50% MATERIAL LOSS. FABRICATED SIDEWALL SUPPORT IAW SRM 53-30-53-01-2
- [SDR SWAA2020032319392](https://openairdocs.org/sdr/SWAA2020032319392.md): Seat Track · corroded · Feb 19, 2020 · N271LV · Boeing 737705 · Fuselage, Seat/Cargo Attach Fittings
  > ***CORROSION*** ON FLOOR RAIL AT AFT CARGO BAY BS767+5 LBL3 WL157. / ACCOMPLISHED REPAIR AT FLOOR RAIL AFT CARGO BAY BS767+5' LBL3 WL157 AS PER SRM 53-00-53-2R-2 ALT.#5. TABLE 205. FIG.203; DUE TO UPON REMOVAL CORROSION EVALUATED AREA AND FOUND TO BE OUT OF LI
- [SDR SWAA2020031642495](https://openairdocs.org/sdr/SWAA2020031642495.md): Skin · gouged · Feb 19, 2020 · N271LV · Boeing 737705 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN HAS A GOUGE BS 400+2.4, STR 27R FUSELAGE SKIN GOUGE BS 400+2.4, STR 27R REPAIRED IAW ATS ER 20-01914, REV IR, DATED 10-MAR-2020 AND PER EA NO: 1-753-36694 REV IR 55981U 11MAR20
- [SDR SWAA2020031142359](https://openairdocs.org/sdr/SWAA2020031142359.md): Handle · cracked · Feb 19, 2020 · N271LV · Boeing 737705 · Emergency Exits
  > R/H OVER WING EXIT DOOR RELEASE HANDLE ASSEMBLY IS CRACKED REMOVED AND REPLACED R/H OVERWING EXIT DOOR RELEASE HANDLE ASSEMBLY IAW AMM 52-22-51-400-801 3.C.(2) (E-F) AND AMM 52-22-51-000-801 2.B.(1)(D-G) 59576U 07MAR20
- [SDR SWAA2020030542187](https://openairdocs.org/sdr/SWAA2020030542187.md): Support · corroded · Feb 19, 2020 · N271LV · Boeing 737705 · Fuselage Miscellaneous Structure
  > ***CORROSION*** ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS500 - 500C LBL23 WL157. SIDEPLATE CHANNEL SUPPORT FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-2, MULTIPLES AREAS 1 X 1 MORE THAN 50% MATERIAL LOSS. FABRICATED SIDEWALL SUPPORT IAW SRM 53-30-53
- [SDR SWAA2020030442119](https://openairdocs.org/sdr/SWAA2020030442119.md): Support Angle · cracked · Feb 19, 2020 · N271LV · Boeing 737705 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL SUPPORT ANGLE AT FWD CARGO BAY BS500B AFT SIDE LBL25 WL156. REMOVED AND REPLACED ON INTERCOSTAL ANGLE AT FWD CARGO BAY BS 500B AFT SIDE LBL 25 IAW SRM 51-40-02 AND DWG 143A7505 REV A 80641U 27FEB20 P/N 143A7502U5 PO# 755718.
- [SDR SWAA2020030442118](https://openairdocs.org/sdr/SWAA2020030442118.md): Support Angle · cracked · Feb 19, 2020 · N271LV · Boeing 737705 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL SUPPORT ANGLE AT FWD CARGO BAY BS500C FWD SIDE LBL25 WL156. REMOVED AND REPLACED FCB INTERCOSTAL SUPPORT ANGLE BS 500C FWD SIDE LBL 25 IAW SRM 51-40-02 AND DWG 143A7505 89004U 25FEB20
- [SDR SWAA2020030442117](https://openairdocs.org/sdr/SWAA2020030442117.md): Shield · corroded · Feb 19, 2020 · N271LV · Boeing 737705 · Fuselage Miscellaneous Structure
  > ***CORROSION*** ON AFT SHIELD AT FWD CARGO BAY BS494 - 500A RBL23 WL157. REMOVED AND REPLACED ON AFT SHIELD AT FCB FROM BS 494 TO BS 500A RBL 23 WL157, P/N 143A8126-12 IAW SRM 51-40-02 AND DWG 143A0080.
- [SDR SWAA2020030442116](https://openairdocs.org/sdr/SWAA2020030442116.md): Support · corroded · Feb 19, 2020 · N271LV · Boeing 737705 · Fuselage Miscellaneous Structure
  > ***CORROSION*** ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS807 - BS727 LBL21 WL157. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS 727 TO BS 847 LBL 21 WL 157 P/N 146A7502-27 IAW SRM 51-40-02-0G-0 AND DRAWING # 146A7500 AND 14
- [SDR SWAA2020030442074](https://openairdocs.org/sdr/SWAA2020030442074.md): Support · corroded · Feb 19, 2020 · N271LV · Boeing 737705 · Fuselage Miscellaneous Structure
  > FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 420 TO BS. 480, LBL 23. / R&R SUPPORT IAW SRM.
- [SDR SWAA2020030442073](https://openairdocs.org/sdr/SWAA2020030442073.md): Cargo Track · corroded · Feb 19, 2020 · N271LV · Boeing 737705 · Fuselage, Seat/Cargo Attach Fittings
  > AFT CARGO BAY FLOOR RAIL CORRODED AT BS. 767+5, LBL 3. / REPAIRED FLOOR RAIL PER SRM.
- [SDR SWAA2020030442072](https://openairdocs.org/sdr/SWAA2020030442072.md): Support · corroded · Feb 19, 2020 · N271LV · Boeing 737705 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY ON FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 767 TO BS. 727, RBL 21. / R&R SUPPORT PER SRM & DWG.
- [SDR SWAA2020030442071](https://openairdocs.org/sdr/SWAA2020030442071.md): Cargo Track · corroded · Feb 19, 2020 · N271LV · Boeing 737705 · Fuselage, Seat/Cargo Attach Fittings
  > AFT CARGO BAY ON TRACK AROUND THE FASTENER CORRODED AT BS. 927+8, RBL 13. / R&R FLOOR TRACK IAW SRM AND DWG.
- [SDR SWAA2020022841934](https://openairdocs.org/sdr/SWAA2020022841934.md): Web · corroded · Feb 19, 2020 · N271LV · Boeing 737705 · Fuselage Miscellaneous Structure
  > FORWARD CARGO BAY MULTIPLE SPOTS ON SUBTHRESHOLD WEB CORRODED BETWEEN BS. 440 TO BS. 494, RBL 29. / R&R SUBTHRESHOLD WEB IAW SRM & DWG.
- [SDR SWAA2020022841932](https://openairdocs.org/sdr/SWAA2020022841932.md): Shield · corroded · Feb 19, 2020 · N271LV · Boeing 737705 · Fuselage Miscellaneous Structure
  > FORWARD CARGO BAY ON FORWARD SHIELD CORRODED AT BS. 420+2.5, RBL 24. / R&R SHIELD IAW SRM AND DWG.
- [SDR SWAA2020022841931](https://openairdocs.org/sdr/SWAA2020022841931.md): Shield · corroded · Feb 19, 2020 · N271LV · Boeing 737705 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY FORWARD SHIELD CORRODED BETWEEN BS. 767 TO BS. 787, RBL 22. / R&R SHIELD PER SRM AND DWG.
- [SDR SWAA2020022841930](https://openairdocs.org/sdr/SWAA2020022841930.md): Support · corroded · Feb 19, 2020 · N271LV · Boeing 737705 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 887 TO BS. 947, RBL 21. / R&R SUPPORT IAW SRM & DWG.
- [SDR SWAA2020022841929](https://openairdocs.org/sdr/SWAA2020022841929.md): Shield · corroded · Feb 19, 2020 · N271LV · Boeing 737705 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY AFT SHIELD CORRODED BETWEEN BS. 847 TO BS. 867, RBL 21. / R&R SHIELD IAW SRM & DWG.
- [SDR SWAA2020022641833](https://openairdocs.org/sdr/SWAA2020022641833.md): Frame Splice · corroded · Feb 19, 2020 · N271LV · Boeing 737705 · Fuselage Main, Frame
  > AFT CARGO BAY FRAME CORRODED AT BS. 787, RBL 25. / R&R FRAME SPLICE IAW SRM & DWG.
- [SDR SWAA2021080519308](https://openairdocs.org/sdr/SWAA2021080519308.md): Floor Panel · damaged · Feb 18, 2020 · N271LV · Boeing 737705 · Fuselage Floor Panel
  > AFT CABIN FLOOR PANEL 241ABF HAS DAMAGED UPPER SURFACE PLIES / AFT CABIN FLOOR PANEL 241ABF WITH DAMAGED UPPER SURFACE PLIES WAS REPLACED WITH A SERVICEABLE FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE PER SRM 51-10-02-0G-0 PARA 9.A.(1)
- [SDR SWAA2021080519309](https://openairdocs.org/sdr/SWAA2021080519309.md): Floor Panel · damaged · Feb 18, 2020 · N271LV · Boeing 737705 · Fuselage Floor Panel
  > AFT CABIN FLOOR PANEL 241AAF HAS DAMAGED UPPER SURFACE PLIES / DUE TO EXTENT OF DAMAGE TO FLOOR PANEL 241AAF; REPLACED WITH NEW PANEL IAW SRM 51-10-02-0G-0 PARA 9 & AIPC 53-21-00-2G ITEM 150. 57885U 02-19-2020

Next page: https://openairdocs.org/aircraft/N271LV/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 = 'N271LV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N271LV/reports

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