N271LV

Service difficulty reports · 251

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

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR SWAA2022020766120Bracket · crackedRIGHT WING WEB BRACKET BELOW TRAILING EDGE FIXED PANEL OUTBD CLIP CRACKED AT DEFLECTION RIB. ; / [01] REMOVED AND REPLACED BRACKET REF SRM 51-40-02.Feb 1, 2022 · N271LV · Boeing 737* · Trailing Edge FlapsSDR SWAA2022020766119Bracket · crackedRIGHT WING SEAL RETAINER BRACKET ON WEB BRACKET BELOW TRAILING EDGE FIXED PANEL CRACKED. ; / [01] REMOVED AND REPLACED BRACKET REF SRM 51-40-02Feb 1, 2022 · N271LV · Boeing 737* · Trailing Edge FlapsSDR SWAA2021031554380Sign · missingR1 DOOR LOWER EXIT SIGN MISSING DIRECTIONAL ARROW. / INSTALLED R1 DOOR LOWER EXIT SIGN IAW AMM 33-51-01Mar 11, 2021 · N271LV · Boeing 737705 · Emergency LightingSDR SWAA2021020445415Lamp · inoperativeISLE 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 D90421Jan 31, 2021 · N271LV · Boeing 737705 · Emergency LightingSDR SWAA2020082610389Light · faultyFORWARD 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.Aug 22, 2020 · N271LV · Boeing 737705 · Emergency LightingSDR SWAA2020041743124Smoke Detector · faultySUPPLEMENTAL 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 # 36546Apr 16, 2020 · N271LV · Boeing 737705 · Smoke DetectionSDR SWAA2021080519504Strip · damagedACB 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-CLOSEMar 3, 2020 · N271LV · Boeing 737705 · Fuselage Miscellaneous StructureSDR SWAA2020031142350Battery Pack · dischargedEMERGENCY 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.Mar 3, 2020 · N271LV · Boeing 737705 · Emergency LightingSDR SWAA2020032319489Floor Panel · out of alignmentPASSENGER 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 56Feb 26, 2020 · N271LV · Boeing 737705 · Fuselage Floor PanelSDR SWAA2020030442120Floor Panel · defectivePASSENGER 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 53-00-50-2Feb 26, 2020 · N271LV · Boeing 737705 · Fuselage Floor PanelSDR SWAA2021071319484Skin · delaminatedDELAMINATION 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.Feb 24, 2020 · N271LV · Boeing 737705 · Trailing Edge FlapsSDR SWAA2020032319451Skin · bentFWD 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 Feb 21, 2020 · N271LV · Boeing 737705 · Passenger/Crew DoorsSDR SWAA2020032319432Skin · damaged(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 IRFeb 20, 2020 · N271LV · Boeing 737705 · Fuselage Main, Plate/SkinSDR SWAA2020032331170Skin · dentedFUSELAGE 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 IRFeb 20, 2020 · N271LV · Boeing 737705 · Fuselage Main, Plate/SkinSDR SWAA2020032331171Skin · dentedFUSELAGE 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 Feb 20, 2020 · N271LV · Boeing 737705 · Fuselage Main, Plate/SkinSDR SWAA2020032331172Skin · dentedFUSELAGE 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 FURTHEFeb 20, 2020 · N271LV · Boeing 737705 · Fuselage Main, Plate/SkinSDR SWAA2020031642498Skin · dentedFUSELAGE 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 Feb 20, 2020 · N271LV · Boeing 737705 · Fuselage Main, Plate/SkinSDR SWAA2020031642497Skin · dentedFUSELAGE 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 FUFeb 20, 2020 · N271LV · Boeing 737705 · Fuselage Main, Plate/SkinSDR SWAA2020031642496Skin · dentedFUSELAGE 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 INSPECTIONFeb 20, 2020 · N271LV · Boeing 737705 · Fuselage Main, Plate/SkinSDR SWAA2020031202394Skin · not reported(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 IRFeb 20, 2020 · N271LV · Boeing 737705 · Fuselage Main, Plate/SkinSDR SWAA2021082019396Skin · corrodedCORROSION 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 AFeb 19, 2020 · N271LV · Boeing 737705 · Fuselage Main, Plate/SkinSDR SWAA2021082019397Skin · corrodedCORROSION 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 DAMFeb 19, 2020 · N271LV · Boeing 737705 · Fuselage Main, Plate/SkinSDR SWAA2021081719422Bracket · crackedBRACKET 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 PRIFeb 19, 2020 · N271LV · Boeing 737705 · Fuselage Miscellaneous StructureSDR SWAA2021081319379Angle · corroded***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 # 148A8650Feb 19, 2020 · N271LV · Boeing 737705 · Fuselage Miscellaneous StructureSDR SWAA2021072219395Floor Support · bentBENT 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-2Feb 19, 2020 · N271LV · Boeing 737705 · Fuselage Miscellaneous StructureSDR SWAA2021071519384Support Angle · corroded***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.Feb 19, 2020 · N271LV · Boeing 737705 · Fuselage Miscellaneous StructureSDR SWAA2021071519420Support Angle · crackedCRACKED 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 27FEB20Feb 19, 2020 · N271LV · Boeing 737705 · Fuselage Miscellaneous StructureSDR SWAA2020032331169Skin · gougedFUSELAGE 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 11MAR20Feb 19, 2020 · N271LV · Boeing 737705 · Fuselage Main, Plate/SkinSDR SWAA2020032319418Seat Track · chafedCHAFING 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 Feb 19, 2020 · N271LV · Boeing 737705 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2020032319405Support · corroded***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 Feb 19, 2020 · N271LV · Boeing 737705 · Fuselage Miscellaneous StructureSDR SWAA2020032319392Seat Track · corroded***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 LIFeb 19, 2020 · N271LV · Boeing 737705 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2020031642495Skin · gougedFUSELAGE 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 11MAR20Feb 19, 2020 · N271LV · Boeing 737705 · Fuselage Main, Plate/SkinSDR SWAA2020031142359Handle · crackedR/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 07MAR20Feb 19, 2020 · N271LV · Boeing 737705 · Emergency ExitsSDR SWAA2020030542187Support · corroded***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 53-30-53Feb 19, 2020 · N271LV · Boeing 737705 · Fuselage Miscellaneous StructureSDR SWAA2020030442119Support Angle · crackedCRACKED 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.Feb 19, 2020 · N271LV · Boeing 737705 · Fuselage Miscellaneous StructureSDR SWAA2020030442118Support Angle · crackedCRACKED 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 25FEB20Feb 19, 2020 · N271LV · Boeing 737705 · Fuselage Miscellaneous StructureSDR SWAA2020030442117Shield · corroded***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.Feb 19, 2020 · N271LV · Boeing 737705 · Fuselage Miscellaneous StructureSDR SWAA2020030442116Support · corroded***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 14Feb 19, 2020 · N271LV · Boeing 737705 · Fuselage Miscellaneous StructureSDR SWAA2020030442074Support · corrodedFORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 420 TO BS. 480, LBL 23. / R&R SUPPORT IAW SRM.Feb 19, 2020 · N271LV · Boeing 737705 · Fuselage Miscellaneous StructureSDR SWAA2020030442073Cargo Track · corrodedAFT CARGO BAY FLOOR RAIL CORRODED AT BS. 767+5, LBL 3. / REPAIRED FLOOR RAIL PER SRM.Feb 19, 2020 · N271LV · Boeing 737705 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2020030442072Support · corrodedAFT CARGO BAY ON FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 767 TO BS. 727, RBL 21. / R&R SUPPORT PER SRM & DWG.Feb 19, 2020 · N271LV · Boeing 737705 · Fuselage Miscellaneous StructureSDR SWAA2020030442071Cargo Track · corrodedAFT CARGO BAY ON TRACK AROUND THE FASTENER CORRODED AT BS. 927+8, RBL 13. / R&R FLOOR TRACK IAW SRM AND DWG.Feb 19, 2020 · N271LV · Boeing 737705 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2020022841934Web · corrodedFORWARD CARGO BAY MULTIPLE SPOTS ON SUBTHRESHOLD WEB CORRODED BETWEEN BS. 440 TO BS. 494, RBL 29. / R&R SUBTHRESHOLD WEB IAW SRM & DWG.Feb 19, 2020 · N271LV · Boeing 737705 · Fuselage Miscellaneous StructureSDR SWAA2020022841932Shield · corrodedFORWARD CARGO BAY ON FORWARD SHIELD CORRODED AT BS. 420+2.5, RBL 24. / R&R SHIELD IAW SRM AND DWG.Feb 19, 2020 · N271LV · Boeing 737705 · Fuselage Miscellaneous StructureSDR SWAA2020022841931Shield · corrodedAFT CARGO BAY FORWARD SHIELD CORRODED BETWEEN BS. 767 TO BS. 787, RBL 22. / R&R SHIELD PER SRM AND DWG.Feb 19, 2020 · N271LV · Boeing 737705 · Fuselage Miscellaneous StructureSDR SWAA2020022841930Support · corrodedAFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 887 TO BS. 947, RBL 21. / R&R SUPPORT IAW SRM & DWG.Feb 19, 2020 · N271LV · Boeing 737705 · Fuselage Miscellaneous StructureSDR SWAA2020022841929Shield · corrodedAFT CARGO BAY AFT SHIELD CORRODED BETWEEN BS. 847 TO BS. 867, RBL 21. / R&R SHIELD IAW SRM & DWG.Feb 19, 2020 · N271LV · Boeing 737705 · Fuselage Miscellaneous StructureSDR SWAA2020022641833Frame Splice · corrodedAFT CARGO BAY FRAME CORRODED AT BS. 787, RBL 25. / R&R FRAME SPLICE IAW SRM & DWG.Feb 19, 2020 · N271LV · Boeing 737705 · Fuselage Main, FrameSDR SWAA2021080519308Floor Panel · damagedAFT 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)Feb 18, 2020 · N271LV · Boeing 737705 · Fuselage Floor PanelSDR SWAA2021080519309Floor Panel · damagedAFT 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 02-19-2020Feb 18, 2020 · N271LV · Boeing 737705 · Fuselage Floor Panel
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