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 SWAA2021080519306Floor Panel · damagedAFT CABIN FLOOR PANEL 241YF HAS DAMAGED UPPER SURFACE PLIES / REMOVED FLOOR PANEL 241YF IAW AMM TASK 53-21-00-000-801 PARA 2E(1)-(3). 57885U 02-19-2020 10537C 02/19/20 DUE TO EXTENT OF DAMAGE TO PANEL 241YF; REPLACED WITH NEW PANEL IAW SRM 51-10-02-0G-0 PARA 9Feb 18, 2020 · N271LV · Boeing 737705 · Fuselage Floor PanelSDR SWAA2021080519305Floor Panel · damagedAFT CABIN FLOOR PANEL 241XF HAS DAMAGED UPPER SURFACE PLIES / AFT CABIN FLOOR PANEL 241XF 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 SWAA2021062919341Scuff Plate · crackedAFT CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED / ACCOMPLISHED REPAIR AT ACB AFT CORNER SCUFFPLATE IAW ENGINNERING AUTHORIZATION EA.#1-A53-2076 REV.11. THE AFT CORNER INSTALLATION IT'S GOING TO BE ACCOMPLISHED WITH CUSTOMER CARD# 753-140-00-024.Feb 18, 2020 · N271LV · Boeing 737705 · Fuselage Miscellaneous StructureSDR SWAA2021051381769Skate Angle · chafedSKATE ANGLE IS CHAFED AT 1007-1016; W.L. 306; L.B.L. 14. / REMOVED AND REPLACED SKATE ANGLE P/N 147A3200U11; BS 1007 TO BS 1016; LBL 14; WL 306 IAW SRM 51-40-02 AND DWG 147A0030 REV A. 89004U; 29FEB20.Feb 18, 2020 · N271LV · Boeing 737705 · Fuselage Main, StructureSDR SWAA2021051381768Skate Angle · chafedSKATE ANGLE IS CHAFED AT 1007-1016; W.L. 306; R.B.L. 14. / REMOVED AND REPLACED SKATE ANGLE P/N 147A3200U12 BS 1007 TO BS 1016; RBL14; WL 306 IAW SRM 51-40-02 AND DWG 147A0030 REV A. 89004U; 29FEB20.Feb 18, 2020 · N271LV · Boeing 737705 · Vertical StabilizerSDR SWAA2020032319343Skate Angle · chafedSKATE ANGLE IS CHAFED AT 1108-1110; W.L. 306; R.B.L. 14. / REMOVED AND CUT CLOSURE ANGLE 5' FWD AND AFT OF DAMAGE CUT AT BS 1108-1110; WL306; RBL14 IAW 53-80-71-2R-6. ACCOMPLISHED REPAIR IAW SRM 53-80-71-2R-6. APPLIED CHEMICAL CONVERSION COATING AND PRIMED IAWFeb 18, 2020 · N271LV · Boeing 737705 · Fuselage Miscellaneous StructureSDR SWAA2020032319342Skate Angle · chafedSKATE ANGLE IS CHAFED AT 1108-1110; W.L. 306; L.B.L. 14. / REPAIRED SKATE ANGLE AT BS 1108-1110; WL 306 LBL 14 IAW SRM 53-80-71-2R-6Feb 18, 2020 · N271LV · Boeing 737705 · Fuselage Miscellaneous StructureSDR SWAA2020032319310Floor Panel · damagedAFT CABIN FLOOR PANEL 241AEF HAS DAMAGED AFT EDGE / DAMAGE TO THE AFT EDGE ON CABIN FLOOR PANEL 241AEF HAS BEEN REPAIRED IAW SRM 53-00-50-2R-4. 59198U 2.21.20.Feb 18, 2020 · N271LV · Boeing 737705 · Fuselage Floor PanelSDR SWAA2020032319307Floor Panel · damagedAFT CABIN FLOOR PANEL 241ZF HAS DAMAGED UPPER SURFACE PLIES / REMOVED FLOOR PANEL 241ZF IAW AMM TASK 53-21-00-000-801. 57885U 02-19-2020 10537C 02/19/20 REPAIRED DAMAGED UPPER SURFACE PLIES; PANEL 241ZF IAW SRM 53-00-50-2R-1 10537C 02/23/20: OK TO INSTALL FLOOFeb 18, 2020 · N271LV · Boeing 737705 · Fuselage Floor PanelSDR SWAA2020031242393Skate Angle · chafedSKATE ANGLE IS CHAFED AT 1108-1110, W.L. 306, R.B.L. 14. REMOVED AND CUT CLOSURE ANGLE 5" FWD AND AFT OF DAMAGE CUT AT BS 1108-1110, WL306, RBL14 IAW 53-80-71-2R-6. ACCOMPLISHED REPAIR IAW SRM 53-80-71-2R-6. APPLIED CHEMICAL CONVERSION COATING AND PRIMFeb 18, 2020 · N271LV · Boeing 737705 · Fuselage Miscellaneous StructureSDR SWAA2020030942258Skate Angle · chafedSKATE ANGLE IS CHAFED AT 1108-1110, W.L. 306, L.B.L. 14. REPAIRED SKATE ANGLE AT BS 1108-1110, WL 306 LBL 14 IAW SRM 53-80-71-2R-6Feb 18, 2020 · N271LV · Boeing 737705 · Fuselage Miscellaneous StructureSDR SWAA2020030442101Floor Panel · damagedAFT CABIN FLOOR PANEL 241ZF HAD DAMAGED UPPER SURFACE PLIES REMOVED FLOOR PANEL 241ZF IAW AMM TASK 53-21-00-000-801. 57885U 02-19-2020 10537C 02/19/20 REPAIRED DAMAGED UPPER SURFACE PLIES, PANEL 241ZF IAW SRM 53-00-50-2R-1 10537C 02/23/20: OK TO INSTALFeb 18, 2020 · N271LV · Boeing 737705 · Fuselage Floor PanelSDR SWAA2020032319301Pressure Deck · crackedTHE INTERNAL HORIZONTAL PRESSURE DECK WEB IS CRACKED AT BS 675 LBL35. / ACCOMPLISHED REPAIR AT INTERNAL HORIZONTAL PRESSURE DECK WEB BS 675 LBL 35 AS PER SRM 53-40-51-2R-2 FIG.201 REPAIR #2; PRESSURE DECK WEB WAS EVALUATED AND NO FOUND ALLOWABLE DAMAGE AT SRM Feb 17, 2020 · N271LV · Boeing 737705 · Fuselage Main, BulkheadSDR SWAA2020030542174Pressure Deck · crackedTHE INTERNAL HORIZONTAL PRESSURE DECK WEB IS CRACKED AT BS 675 LBL35. ACCOMPLISHED REPAIR AT INTERNAL HORIZONTAL PRESSURE DECK WEB BS 675 LBL 35 AS PER SRM 53-40-51-2R-2 FIG.201 REPAIR #2, PRESSURE DECK WEB WAS EVALUATED AND NO FOUND ALLOWABLE DAMAGE AFeb 17, 2020 · N271LV · Boeing 737705 · Fuselage Main, BulkheadSDR SWAA2020030442082Bulkhead · crackedRIGHT HAND LOWER COMPOSITE BULK HEAD WAS CRACKED AT BS. 663, RBL 53. / R&R VAPOR BARRIER PER SRM, AMM, & DWG.Feb 17, 2020 · N271LV · Boeing 737705 · Fuselage Main, BulkheadSDR SWAA2020022654666Floorbeam · crackedCRACKED FLOOR SUPPORT CRACKED AT BS. 540, BETWEEN BL 0 TO RBL 24.5. / R&R FLOOR SUPPORT IAW SRM AND DWG.Feb 17, 2020 · N271LV · Boeing 737705 · Fuselage Main, Floor BeamSDR SWAA2020022654665Floorbeam · crackedFLOOR SUPPORT CRACKED AT BS. 540, BETWEEN BL 0 TO LBL 24.5. / R&R FLOOR SUPPORT IAW SRM AND DWG.Feb 17, 2020 · N271LV · Boeing 737705 · Fuselage Main, Floor BeamSDR SWAA2020032319261Skin · damagedRH ELEVATOR TE UPPER SKIN; PREVIOUS REPAIR DAMAGED; 72' FROM IB END / AFTER REMOVING PREVIOUS REPAIR 72' FROM I/B END ON R/H ELEVATOR T/E UPPER AND LOWER SKIN; ACCOMPLISHED REPAIR ON 4EA AREAS PER SRM 51-70-04-2R-9 AND SRM 51-70-04-2R-6.Feb 16, 2020 · N271LV · Boeing 737705 · Elevator, Plate/SkinSDR SWAA2020030442115Skin · damagedRH ELEVATOR TE UPPER SKIN, PREVIOUS REPAIR DAMAGED, 72" FROM IB END AFTER REMOVING PREVIOUS REPAIR 72" FROM I/B END ON R/H ELEVATOR T/E UPPER AND LOWER SKIN, ACCOMPLISHED REPAIR ON 4EA AREAS PER SRM 51-70-04-2R-9 AND SRM 51-70-04-2R-6.Feb 16, 2020 · N271LV · Boeing 737705 · Elevator, Plate/SkinSDR SWAA2021082719218Retainer · crackedRIGHT WING FIXED T/E PANEL VERTICAL BULB SEAL RETAINER IS CRACKED 9' I/B OF DEFLECTION RIB. MARKED / REMOVED AND REPLACED RIGHT WING FIXED T/E PANEL VERTICAL BULB SEAL RETAINER P/N 115A2953-2 AT 9' I/B OF DEFLECTION RIB. IAW SRM 51-40-02 AND AIPC 57-50-00-25 8Feb 14, 2020 · N271LV · Boeing 737705 · Wing Main, Frame StructureSDR SWAA2021082719221Retainer · crackedLEFT WING T/E UPPER SEAL RETAINER IS CRACKED 3' BELOW FIXED T/E PANEL 10' I/B OF DEFLECTION RIB ORSS269. / REMOVED AND REPLACED LEFT WING T/E UPPER SEAL RETAINER AT 3' BELOW FIXED T/E PANEL 10' I/B OF DEFLECTION RIB ORSS 269 P/N 115A2982-9. IAW. SRM 51-40-02. Feb 14, 2020 · N271LV · Boeing 737705 · Wing Main, Frame StructureSDR SWAA2020022641832Support Angle · crackedRIGHT WING TRAILING EDGE HAD CRACKED SUPPORT ANGLE 1" INBOARD OF DEFLECTION RIB ORSS 281. / REMOVED AND REPLACED SUPPORT ANGLE IAW SRM.Feb 14, 2020 · N271LV · Boeing 737705 · Wing Miscellaneous StructureSDR SWAA2020022641831Support Angle · crackedLEFT WING TRAILING EDGE HAD CRACKED SUPPORT ANGLE 1" INBOARD OF DEFLECTION RIB ORSS. 281. REMOVED AND RESTORED SUPPORT ANGLE IAW SRM.Feb 14, 2020 · N271LV · Boeing 737705 · Wing Miscellaneous StructureSDR SWAA2020032319150Structure · dentedFLIGHT DECK FLOOR IS DENTED AT B.S. 255; W.L. 207.54; R.B.L. 4 - L.B.L. 14. / REPAIRED FLIGHT DECK FLOOR AT B.S.255; W.L.207.54; R.B.L.4 - L.B.L 14. IAW EA 1-A53-33179 REV IR. AND BOEING DWG 141A0631 55981U 10MAR20Feb 11, 2020 · N271LV · Boeing 737705 · Fuselage Miscellaneous StructureSDR SWAA2020031242402Floor Panel · dentedFLIGHT DECK FLOOR IS DENTED AT B.S. 255, W.L. 207.54, R.B.L. 4 - L.B.L. 14. REPAIRED FLIGHT DECK FLOOR AT B.S.255, W.L.207.54, R.B.L.4 - L.B.L 14. IAW EA 1-A53-33179 REV IR. AND BOEING DWG 141A0631 55981U 10MAR20Feb 11, 2020 · N271LV · Boeing 737705 · Fuselage Floor PanelSDR SWAA2019091937003Light · inoperativeEMERGENCY LIGHT OUT AT 22DEF. RELAMPED & OPS CK'S GOOD IAW AMM 33-51-03.Sep 14, 2019 · N271LV · Boeing 737705 · Emergency LightingSDR SWAA2019091136768Sign · looseEMERGENCY EXIT OVERHEAD SIGN MID CABIN LOOSE. SECURED LIGHT ASSEMBLY IAW MM.Sep 9, 2019 · N271LV · Boeing 737705 · Emergency LightingSDR SWAA2022022423184Flap · delaminatedLEFT OUTBOARD AFT FLAP LOWER SURFACE HAS DAMAGE. DAMAGE IS OUT OF LIMITS DUE TO DELAMINATION TOO CLOSE TO OTHER DAMAGE AND TOO CLOSE TO SPAR WEB / REMOVED AND REPLACED L/H O/B AFT FLAP PER AMM 27-51-22 POS L/H OTBD PN OFF 113A3700-7 SN OFF 00057 PN ON 113A3700Mar 4, 2019 · N271LV · Boeing 737705 · Trailing Edge FlapsSDR SWAA2018112927198Light · inoperativeL2 DOOR EXTERNAL EMERGENCY LIGHT INOP. RELAMPED LIGHT IAW AMM.Nov 27, 2018 · N271LV · Boeing 737705 · Emergency LightingSDR SWAA2018110826614Lanyard · looseR1 DOOR EMERGENCY EVAC SLIDE LANYARD WIRE LOOSE. SECURED LANYARD PER SIP.Nov 8, 2018 · N271LV · Boeing 737705 · Emergency EquipmentSDR SWAA2018071723589Battery · dischargedEMERGENCY EXIT LIGHT BATTERY PACK M1674 INOP. R&R BATTERY PER MM.Jul 9, 2018 · N271LV · Boeing 737705 · Emergency LightingSDR SWAA2018071723509Battery · dischargedEMERGENCY EXIT LIGHT BATTERY PACK M1675 INOP. R&R BATTERY PER MM.Jul 9, 2018 · N271LV · Boeing 737705 · Emergency LightingSDR SWAA2018072323508Connector · damagedG4 GALLEY EMERGENCY EXIT LIGHT CONNECTORS DAMAGED. REPAIRED CONNECTOR PER AMM.Jul 4, 2018 · N271LV · Boeing 737705 · Light System WiringSDR SWAA2018071123396Intercostal · crackedFORWARD CARGO BAY INTERCOSTAL CRACKED BETWEEN BS 500 TO BS 500A, LBL 24. R&R INTERCOSTAL IAW DWG AND SRM.Jul 2, 2018 · N271LV · Boeing 737705 · Fuselage Miscellaneous StructureSDR SWAA2022021523390Panel · crackedAPU INLET UPPER PANEL IS CRACKED P/N (315A2040-24) / APU INLET UPPER AFT PANEL WAS REMOVED ON CC# 753-430-00-01B. RECIEVED NEW APU INLET AFT UPPER PANEL P/N 353A2040-24. LOCATED; DRILLED; COUNTERSANK AND ASSEMBLED PER SRM 51-40-05-0G-0; SRM 51-40-08-0G-0; SRM Jun 26, 2018 · N271LV · Boeing 737705 · Fuselage Miscellaneous StructureSDR SWAA2018071123395Support · corrodedSUPPORT CORRODED AT BS 267, BL 0. R&R SUPPORT IAW DWG AND SRM.Jun 25, 2018 · N271LV · Boeing 737705 · Fuselage Miscellaneous StructureSDR SWAA2022021523386Fitting · corroded***CORROSION*** AFT CARGO COMPARTMENT EQUIPMENT BAY DRAIN MAST SUPPORT FITTING HAS CORROSION; BS992; WL182; LBL22. / REMOVED AND REPLACED DRAIN MAST SUPPORT FITTING DUE TO CORROSION PER SRM 51-40-02-0G-00 & DWG # 147A7443Jun 19, 2018 · N271LV · Boeing 737705 · Fuselage Miscellaneous StructureSDR SWAA2018070223227Intercostal · corrodedAFT CARGO BAY INTERCOSTAL WEB CORRODED AT BS 847, STR 25R. R&R WEB PER SRM AND DWG.Jun 19, 2018 · N271LV · Boeing 737705 · Fuselage Miscellaneous StructureSDR SWAA2018071723507Intercostal · corrodedFUSELAGE INTERCOSTAL CORRODED AT STA 306, STR 23L. R&R INTERCOSTAL PER SRM.Jun 16, 2018 · N271LV · Boeing 737705 · Fuselage Miscellaneous StructureSDR SWAA2018070223226Intercostal · crackedINTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, RBL 31. R&R INTERCOSTAL IAW SRM AND DWG.Jun 15, 2018 · N271LV · Boeing 737705 · Fuselage Miscellaneous StructureSDR SWAA2018070223225Intercostal · crackedINTERCOSTAL CRACKED BETWEEN BS 328 TO BS 344, LBL 45. R&R INTERCOSTAL IAW SRM AND DWG.Jun 15, 2018 · N271LV · Boeing 737705 · Fuselage Miscellaneous StructureSDR SWAA2018070223224Intercostal · crackedINTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, LBL 45. R&R INTERCOSTAL PER SRM & DWG.Jun 15, 2018 · N271LV · Boeing 737705 · Fuselage Miscellaneous StructureSDR SWAA2022021723360Fairing · elongatedFAIRING PANEL 193AR; INBOARD INNER SKIN HAS CHAFF DAMAGE AND COMMON TO DAMAGE AREA ARE FASTENERS HOLES THAT ARE ELONGATED. / FAIRING PANEL 193AR; INBOARD INNER SKIN WITH CHAFF DAMAGE AND COMMON TO DAMAGE AREA WERE FASTNER HOLES THAT WERE ELONGATED WAS REPAIREDJun 14, 2018 · N271LV · Boeing 737705 · Aerodynamic FairingsSDR SWAA2022021723357Seal · crackedLT HORIZ STAB UPPER FWD SLIDE SEAL IS CRACKED. / REMOVED AND REPLACED LT HORIZ STAB UPPER FWD SLIDE SEAL LAW AMM 53-31-31-802 84036U 29JUN18Jun 14, 2018 · N271LV · Boeing 737705 · Horizontal Stabilizer, Plate/SkinSDR SWAA2022021723359Seal · crackedRT HORIZ STAB UPPER FWD SLIDE SEAL IS CRACKED. / REMOVED RT HORIZ STAB UPPER FWD SLIDE SEAL IAW SOPM 20-50-01 LOCATE AND DRILL IAW SRM 50-40-05 84036U 29JUN18. INSTALLED RT HORIZ STAB UPPER FWD SLIDE SEAL IAW AMM 53-31-31-400-801 STEP 3.D. & E. 56790U 09JUL18 Jun 14, 2018 · N271LV · Boeing 737705 · Horizontal Stabilizer, Plate/SkinSDR SWAA2018071223458Crease Beam · corrodedCREASE BEAM WEB CORRODED AT BS 727D+11, RBL 60. R&R CREASE BEAM IAW DWG AND SRM.Jun 14, 2018 · N271LV · Boeing 737705 · Fuselage Main, StructureSDR SWAA2022021723350Scuff Plate · crackedFSD THRESHOLD CRACKED AT AFT CORNER / REPAIRED FSD THRESHOLD IAW EA 1-A53-2076 REV 11Jun 13, 2018 · N271LV · Boeing 737705 · Fuselage Main, Plate/SkinSDR SWAA2022021623330Floor Panel · corroded***CORROSION*** FCB FLOOR PANEL 120AF EDGE HAS SURFACE CORROSION. / FABRICATED OF REPLACEMENT PANEL FWD PIT 120AF I.A.W SRM 51-30-01-0G-0 PPGA & PPG 7; TREATED (CHEM.CONV.COAT) & PRIMED I.A.W SRM 51-00-58-201 PG 2;(C) AMM 27-72-370-801 PG 2 'D;' SWB TASK 2 TABJun 13, 2018 · N271LV · Boeing 737705 · Fuselage Floor PanelSDR SWAA2022021623331Floor Panel · corroded***CORROSION*** FCB FLOOR PANEL 120BF EDGE HAS SURFACE CORROSION. / REPLACED FCB FLOOR PANEL 120 BF WITH NEW PANEL FABRICATED FROM 2024 T3 # 0.71 LOT # 1347031-3 PER DWG 453A1610 AND APPLIED CHEMICAL CONVERSION COATING AND PRIMER PER SOPM 20-43-03 AND AMM 51-2Jun 13, 2018 · N271LV · Boeing 737705 · Fuselage Main, Plate/SkinSDR SWAA2022021623332Floor Panel · corroded***CORROSION*** FCB FLOOR PANEL 120CF EDGE HAS SURFACE CORROSION. / REMOVED CORROSION; CORROSION LENGTH IS GREATER THAN 3' OUT OF LIMITS. FABRICATED A NEW ALUMINUM FLOOR PANEL 2024-T3; .071 LOT # 1347031-3 PER SRM 53-30-53-0I-1; SRM 51-10-02-0G-0; AND SOPM 20-Jun 13, 2018 · N271LV · Boeing 737705 · Fuselage Floor Panel
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