N7731A
Service difficulty reports · 252
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 = 'N7731A' 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.
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 = 'N7731A' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR SWAA2024040459579Floor Panel · pulledAFT FLOOR PANEL 242UF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 242UF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED CORRECTIVE SDR SWAA2024040459585Floor Panel · pulledFWD FLOOR PANEL 221AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO THE EXTENT OF DAMAGE; REPLACED FWD FLOOR PANEL 221AF IAW SRM 51-10-02-0G-0 PARA 9; AIPC 53-21-51-75 ITEM 65 AND MODIFIED PER DWG D1040M002.;[02] VERIFIED CORRECTIVE ACTION 1.SDR SWAA2024040459586Floor Panel · pulledFWD FLOOR PANEL 221BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 221BF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED CORRECTIVE SDR SWAA2024040459594Floor Panel · pulledFWD FLOOR PANEL 221CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 221CF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED CORRECTIVE SDR SWAA2024040459587Floor Panel · pulledFWD FLOOR PANEL 221DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 221DF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED CORRECTIVE SDR SWAA2024040459591Floor Panel · pulledCABIN FLOOR PANEL 241UF HAS PULLED STRANDS.<[01] FABRICATED 241UF FLOORBOARD PANEL IAW SRM 53-00-50-2R-0 ALONG WITH DWG:146A5810 SHEET: 54;[02] VERIFIED FABRICATION OF FLOOR PANEL 241UF PER SRM 53-00-50-2R-0 ALONG WITH DWG:146A5810 SHEET: 54SDR SWAA2024040459592Floor Panel · pulledCABIN FLOOR PANEL 241WF HAS PULLED STRANDS.<[01] CABIN FLOOR PANEL 241WF WITH PULLED STRANDS WAS REPLACED BY FABRICATION IAW SRM 53-00-50-2R-0 AND DRAWING 146A5810 SHEET 28.;[02] VERIFIED CORRECTIVE ACTION #1SDR SWAA2024040459593Floor Panel · pulledCABIN FLOOR PANEL 231JF HAS PULLED STRANDS.<[01] FLOOR PANEL 231JF WITH PULLED STRANDS WAS REPLACED BY FABRICATING A NEW PANEL IAW SRM 53-00-50-2R-0 AND DWG 143A5810 ID:0138;[02] VERIFIED FLOOR PANEL 231JF WAS REPLACED BY FABRICATING A NEW PANEL IAW SRM 53-00-SDR SWAA2024040459598Floor Panel · pulledCABIN FLOOR PANEL 231MF HAS PULLED STRANDS.<[01] DUE TO THE EXTENT OF DAMAGE; REPLACED CABIN FLOOR PANEL 231MF IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-00-09A ITEM 277.;[02] VERIFIED CORRECTIVE ACTION 1.SDR SWAA2024040559033Panel · crackedRT WING T/E PANEL 661BB AFT ROW OF FASTENER HOLES HAVE CRACKS AROUND HOLE<[01] RIGHT WING TRAILING-EDGE PANEL 661BB AFT ROW OF FASTENER HOLES WITH CRACKS AROUND HOLES WERE REPAIRED IAW SRM 51-70-04-2R-9.;[02] VERIFIED CORRECTIVE ACTION #1SDR SWAA2024040462290Vapor Barrier · crackedR/H B/S 663 VAPOR BARRIER IS CRACKED AT RBL 34 WL 157<[01] R/H B/S 663 VAPOR BARRIER IS CRACKED AT RBL 34 WL 157 WAS REPAIRED IAW SRM 51-70-04-2R-10.;[02] VERIFIED REPAIR OF THE R/H B/S 663 VAPOR BARRIER IAW SRM 51-70-04-2R-10.SDR SWAA2024040459306Vapor Barrier · crackedL/H B/S 663 VAPOR BARRIER IS CRACKED AT LBL 33 WL 166<[01] L/H VAPOR BARRIER CRACKS AT BS 663 LBL 33 WL 166 WERE REPAIRED IAW SRM 51-70-04-2R-10;[02] VERIFIED L/H VAPOR BARRIER CRACKS AT BS 663 LBL 33 WL 166 WERE REPAIRED IAW SRM 51-70-04-2R-10;[03] WORKSCOPE SDR SWAA2024040459310Web · corrodedCORROSION; FCB SUBTHRESHOLD BS480+1; RBL28; WL156<[01] VERIFIED STEP 1 COMPLETE.;[02] VERIFIED STEP 5 COMPLETE; STEP 6 IN PARTIAL.;[03] REMOVED AND REPLACED FCB SUBTHRESHOLD WEB WL156 I.A.W SRM 51-10-02-0G-0 AND SRM 51-40-02-0G-0 AND DWG 143A8330.SDR SWAA2024040559031Web · crackedRIGHT WING; TRANSVERSE WEB IS CRACKED; UPPER LEG; O/B END ABOVE #2 PYLON AFT TIP<[01] REMOVED AND REPLACED RIGHT WING; TRANSVERSE WEB AT UPPER LEG; O/B END ABOVE #2 PYLON AFT TIP IAW SRM 51-40-02; AIPC 57-50-00-36A AND DWG 115A2512;[02] VERIFIED CORRECTIVE ACTSDR SWAA2023081588694Strip · loosePHOTOLUMINESCENT STRIPS FROM OVERWING EXIT ROWS HAVE BECOME LOOSE AND DETACHED<[01] REATTACHED PHOTOLUMINESCENT STRIPS AT EMERGENCY EXIT ROWS PER SIPSDR SWAA2022072733107Valve · leaking#2 ENG REACHED 922 ON CLIMB PILOTS REDUCED THRUST TO 900EGT WITHOUT AUTOTHROTTLES TO CRZ #2 FF WAS CONSISTENTLY HIGHER LEADING TO FUEL IMBALANCE #2 EGT WAS CONSISTENTLY HIGHER THAN #1 ENG BY 60*C. / [01] PERFORM EEC BITE TEST PER AMM 73-21-00; NO FAULTS FOUND.SDR SWAA2022070123615Battery Pack · failedEMERGENCY LIGHT BATTERY PACK AT LOCATION M1675 FAILED CAPACITY TEST / [01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT LOCATION M1675 PER AMM 33-51-06SDR SWAA2022070123616Battery Pack · failedEMERGENCY LIGHT BATTERY PACK AT RT FWD CABIN; M1674 FAILED CAP CHECK. / [01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT RT FWD CABIN; M1674 PER AMM 33-51-06SDR SWAA2022070123604Support Bracket · crackedRH AC BAY FWD BLEED DUCT SUPPORT BRACKET IS CRACKED AT THE KEEL BEAM AREA / [01] R&R RH AC BAY FWD BLEED DUCT SUPPORT BRACKET PER AMM 36-13-01;[02] R&R RH AC BAY FWD BLEED DUCT SUPPORT BRACKET PER AMM 36-13-01SDR SWAA2022070123605Support Bracket · crackedLH AC BAY FWD BLEED DUCT SUPPORT BRACKET IS CRACKED AT THE KEEL BEAM AREA / [01] R&R LH AC BAY FWD BLEED DUCT SUPPORT BRACKET PER AMM 36-13-01SDR SWAA2022070123611Vapor Barrier · crackedRH AC BAY AFT WALL 5' FROM THE BOTTOM AND 7' FROM THE O/B EDGE VAPOR BARRIER HAS A 5' CRACK THAT CONTINUES UNDER A REPAIR / [01] PERFORMED INTERIM PATCH REPAIR AT RH AC BAY AFT WALL 5' FROM THE BOTTOM AND 7' FROM THE O/B EDGE VAPOR BARRIER PER SRM 57-10-10.SDR SWAA2022051205555Smoke Detector · no testAFT LAV SMOKE DETECTOR WILL NOT TEST / [01] REMOVED AND REPLACED AFT LAV SMOKE DETECTOR. TEST RESULTS PASS AT THIS TIME. REF AMM. 26-14-01. -END-SDR SWAA2022042797397Battery Pack · defectiveEMERGENCY LIGHTS INOP AT POSITIONS: 6 ABC; 8 DEF; 9 ABC; 12 ABC; 12 DEF AND R2 DOOR; UPPER EMERGENCY EXIT LIGHT. / [01] DURING TROUBLESHOOTING FOUND BATTERY PACK POS. M2335 DEFECTIVE AS PER REF. B737 AMM 33-51-00-710-801.;[02] REMOVED AND REPLACED EMERGENCY BASDR SWAA2022050292378Plate · crackedAFT CARGO IN DOOR CUTOUT; SHIELDS SUPPORT FWD AND AFT IS CRACKED / [01] RECEIVED NEW AFT CARGO DOOR CUT OUT SUPPORT PLATES FWD AND AFT POSITION P/N 453A2611-1 PO#1765963 AND P/N 453A2611-2; PO# 1741204. PLATES WILL BE INSTALLED ON TASK CARD TTG8Q003AYLR;[02] VSDR SWAA2022042992018Door · crackedC/R L/H FIXED MAIN LANDING GEAR DOOR CRACKED / [01] REMOVED L/H MLG CENTER DOOR REF B737 AMM 32-13-11-000-802;[02] VERIFIED STEP 1.;[03] REMOVED L/H MLG INNER DOOR REF. B737 AMM 32-13-11-000-802;[04] OK TO INSTALL NEW L/H MLG INNER DOOR;[05] OK TO INSTALL L/H SDR SWAA2022050293640Panel · crackedFOUND PANEL 194E WITH 11 EACH FASTENER HOLES WITH STRESS CRACKS AND/OR ELONGATED HOLES (MARKED) / [01] MEASUREMENTS;[02] CLEANED AND PREPARED PANEL FOR REPAIR; PERFORMED DRY OUT; FOUND NO WATER AS PER B737 SRM 51-70-05-2R-8;[03] VERIFIED STEPS 1 AND 2;[04] OK SDR SWAA2022042791212Scuff Plate · crackedFWD CARGO DOOR AFT SCUFF PLATE CORNER WITH A CRACK. / [01] ACCOMPLISHED WELD REPAIR AT FWD CARGO DOOR AFT SCUFF PLATE AS PER SRM 53-3015-1A-2. SCUFF PLATE WILL BE INSTALL ON (TTG8Q003E4Z5).SDR SWAA2022050290660Stiffener · corrodedFOUND FWD WET AREA FLOOR STTIFENER WITH CORROSSION STA 328 LBL 5 / [01] REMOVED AND REPLACED FLOOR STIFFENER AT FWD WET AREA STA 328 LBL 5 AS PER 51-40-02-0G-0;[02] VERIFIED STEP 1SDR SWAA2022050290516Doubler · crackedCRACK FOUND AT LEFT HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 193.90 ; 10' FROM REAR SPAR ;I/B ROW .CRACK LENGTH : 0.406' CRACK FOUND AT LEFT HORIONTAL STABILIER LOWER SKIN AT STAB STA 193.90 10' FROM REAR SPAR I/B ROW .CRACK LENGTH : 0.406' / [01] REMOVED SDR SWAA2021092017606Slide · looseFORWARD SERVICE DOOR SLIDE HAD STARTED TO UNPACK FROM CONTAINER ; / [01] RE-SECURED SLIDE IN COMPARTMENT PER TASK CARD MT 725-61-06SDR SWAA2021090914905Lamp · inoperativeEMERGENCY LIGHT AT 20 ABC INOP ; / [01] RELAMPED EMERGENCY AREA LIGHT AT 20ABC IAW AMM 33-51-03.SDR SWAA2021060278152Lens · brokenEMERGENCY EXIT LIGHT COVER PLATE LENS DOOR L1 BROKEN ; / REINSTALLED LENS IAW SIPSDR SWAA2021071410301Floor Support · crackedFORWARD CARGO AFT AT STA 540 UPPER RIGHT SIDE PANEL BREAK SUPPORT CRACK. / REMOVED AND REPLACED FORWARD CARGO AFT AT STA 540 UPPER RIGHT SIDE PANEL BREAK SUPPORT IAW AMM 53-21-00 AND SRM 51-40-02SDR SWAA2020082510303Girt Bar · out of positionR-1 DOOR SLIDE GIRT TO LONG / SECURED GRID TO CORRECT POSITION PER MT 725-61-06SDR SWAA2020072202456Slide · low pressureL2 DOOR SLIDE NOT IN GREEN BAND. R & R THE L1 DOOR SLIDE IAW MT 725-61-06,SDR SWAA2020051176149Battery Pack · dischargedEMERGENCY EVACUATION LIGHTS INOP OVER AFT ENTRY DOOR / M1672 BATTERY PACK REPLACED ON CARD G730383. OPS CHECKS GOOD PER MM 33-51-06SDR SWAA2020051176148Battery Pack · dischargedEMERGENCY EVACUATION LIGHT OUT ON AFT GALLEY CEILING / M1672 BATTERY PACK REPLACED ON CARD G730383. OPS CHECKS GOOD PER MM 33-51-06.SDR SWAA2020051176147Battery Pack · dischargedEMERGENCY LIGHTS INOP ON CABIN O/H BIN BULLNOSE AT 16DEF AND 19DEF / REMOVED AND REPLACED M1672 BATTERY PACK . OPS CHECKS GOOD PER MM 33-51-06SDR SWAA2020051176121Floor Panel · damagedCABIN FLOOR PANEL 231UF IS DAMAGED / REMOVED AND REPLACED CABIN FLOOR PANEL 231UF PER AMM 53-21-00.SDR SWAA2020051176073Floor Panel · damagedCABIN FLOOR PANEL 241AF HAS PULLED FIBERS ON UPPER SURFACE. / REMOVED AND REPLACED CABIN FLOOR PANEL 241AF PER AMM 53-21-00.SDR SWAA2020051176097Rib · crackedACCOMPLISHED HOLE PROBE INSP. OF LOWER FLANGE IN REPAIR AREA OF L/H HORIZONTAL STABILIZER INSPAR RIB ASSEMBLY #4 (STAB STA. 120.30) HAS A CRACK INDICATION 10TH FASTENER HOLE FROM REAR SPAR PER NDT PART 6 51-00-00 PROC. 16 / REPAIRED PER SRM 55-10-09-2R-5SDR SWAA2020051176082Rib · crackedL/H HORIZONTAL STABILIZER INSPAR RIB ASSEMBLY #4 (STAB STA. 120.30) STIFFENER #1 (MOST FWD) CRACKED AT LOWER FLANGE ANGLEOF STIFFENER (FOUND CRACKED AFTER RIB REMOVAL) / INSTALLED REPAIR PER SRM 55-10-09-2R-4 .SDR SWAA2020051176066Skate Angle · chafedL/H VERTICAL STAB. SKATE ANGLE HAS EVIDENCE OF CHAFFING .(MARKED) / REMOVED AND REPLACED LH FWD SKATE ANGLE PER SRM 51-40-02.SDR SWAA2020051176067Skate Angle · chafedR/H VERTICAL STAB. SKATE ANGLE HAS EVIDENCE OF CHAFFING .(MARKED) / REMOVED AND REPLACED RH FWD VERTICAL STABILIZER SKATE ANGLE PER SRM 51-40-02.SDR SWAA2021050676033Seal · crackedPANEL 343AT METAL SLIDER SEAL CRACKED / REMOVED AND REPLACED BLADE ASSY AT PANEL 343AT PER SRM 51-40-02.SDR SWAA2020051176051Seat Track · damagedCAPTAINS SEAT TRACKS ARE ELONGATED. / REMOVED AND REPLACED CAPTAINS SEAT TRACKS IAW AMM 25-11-11.SDR SWAA2020051176052Seat Track · damagedFIRST OFFICERS SEAT TRACKS ARE ELONGATED. / REMOVED AND REPLACED (4 EACH) F/O'S SEAT TRACKS PER AMM 25-11-11SDR SWAA2020051176042Rib · crackedL/H HORIZONTAL STABILIZER INSPAR RIB ASSEMBLY #4 (STAB STA. 120.30) STIFFENER #4 (MOST AFT) CRACKED AT LOWER FLANGE ANGLE OF STIFFENER / REPAIRED HORIZONTAL STABILIZER RIB CRACK IAW SRM 55-10-09-2R-5.SDR SWAA2020051176049Plate · crackedRH WING T/E WAFFLE PLATE CRACKED JUT INBD OF #6 FLAP TRACK / REMOVED AND REPLACED WAFFLE PLATE PER SRM 51-40-02SDR SWAA2020051176002Angle · corrodedMULTIPLE AREAS OF SURFACE CORROSION ON COCKPIT FLOOR ANGLE STA. 270 LBL20-RBL10 / E104286-SNYDER; GEOFFREY - 04/26/2020 23:09 COMPLETE: REPAIRED COCKPIT FLOOR ANGLE AT STA 270 LBL20 TO RBL10 PER EA 1-A53-13812; MFG PART NUMBER 141A5213
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