N8303R
Service difficulty reports · 174
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 = 'N8303R' 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 = 'N8303R' 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 SWAA2024010423407Support Angle · crackedCRACK ANGLE SUPPORT LOCATED STA 727B AND LBL51 CEILING AREA AFT CARGO COMPARTMENT 2023-719787<[01] PERFORMED PERMANENT REPAIR ON ANGLE SUPPORT LOCATED STA 727B AND LBL51 CEILING AREA AFT CARGO COMPARTMENT IAW B737-800 SRM 51-70-11-2R-0 REPAIR GENERAL. SEE INDISDR SWAA2024010423337Tie Clip · crackedCRACK ON TIE CLIP LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA 2023-719783<[01] REPLACED TIE CLIP LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA IAW SRM B737-800 51-10-02; SRM B737-800 51-40-02; AND DRAWING # 141A1110 REV.-. SEE INDIVIDUAL SIGN OFFS SDR SWAA2024010423338Panel · crackedCRACK ACCESS PANEL 661BB TRAILING EDGE AT RT WING 2023-719785<[01] TOOL USED: CALIPER P/N: 500-197-30 S/N: A18135081 DUE DATE: 21-JUL-24.;[02] TOOL USED: HOT BONDER P/N:HCS9200B; S/N:18165044; DUE DATE: 26-MAR-24.;[03] TOOL USED: SCALE PN: PSX621; SN: 83402254SDR SWAA2024010323408Scuff Plate · crackedCRACK ON AFT CORNER SCUFF PLATE AT AFT CARGO DOOR CUT OUT 2023-719789<[01] TOOL USED DIGITAL CALIPER: P/N: 500-196-30; S/N; A22348594; DUE DATE: 13-JUL-24.;[02] TOOL USED: RADIOMETER/PHOTOMETER P/N:XRP-3000; S/N:1753759; DUE DATE:12-APR-24.;[03] REPAIRED AFT CSDR SWAA2024010323336Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED BTW BS 291.5 TO BS 294.5 AT LEVEL STAR 17R AT FWD GALLEY AREA 2023-719781<[01] REPLACED SUPPORT ANGLE LOCATED BTW BS 291.5 TO BS 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA I.A.W B737-800 SRM 51-10-02 AND DWG: 141A8310; SHEET: 33; SDR SWAA2024010423121Web · crackedCRACK WEB LOCATED BETWEEN BS312 TO BS328 LBL46 AND WL208 AT PASSENGER CABIN 2023-719770<[01] REPLACED WEB LOCATED BETWEEN BS312 TO BS328 LBL46 AND WL208 AT PASSENGER CABIN IAW B737-800 SRM 51-10-02 AND DWG: 141A5400 SHET: 26; REV: - SEE INDIVIDUAL SIGN-OFF BELSDR SWAA2024010423120Intercostal · crackedCRACK ON INTERCOSTAL LOCATED BS 540 BTW RBL 1 TO RBL 24.75 WL 208.1 AT PASSENGER CABIN 2023-719584<[01] REPLACED INTERCOSTAL LOCATED BS540 BTW RBL1 TO RBL24.75 WL208.1 AT PASSENGER CABIN I.A.W. B737-800 SRM 51-40-02 AND DWG 143A0060 SHEET 64 REV. -<BR><BR>SEE SDR SWAA2024010422706Support Angle · crackedCRACK SUPPORT ANGLE LOCATED BETWEEN BS695 RBL24.75 AND WL200 AT PASSENGER CABIN 2023-719581<[01] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 25-JAN-24; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811019; DUE DATE: SDR SWAA2024010322573Lens · brokenBROKEN SIDEWALL PANEL EMERGENCY LENS ON POSITION 232ZKW AT PASSENGER CABIN (1 EA) 2023-719432<[01] REPLACED SIDEWALL PANEL EMERGENCY LENS ON POSITION 232ZKW AT PASSENGER CABIN (1 EA) I.A.W B737-800 AMM 33-51-01-960-802 STEP 3C ITEM 5(D) AND ITEM (10).;[02] TASSDR SWAA2024010321926Light · damagedSCRATCH ON STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING RH AT PASSENGER CABIN (9 EA) 2023-719361<[01] REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING RH AT PASSENGER CABIN (9 EA) I.A.W B737-800-AMM-33-51-15-400-802;[02] JOB COMPLETED.SDR SWAA2024010321927Light · brokenBROKEN STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING LH AT PASSENGER CABIN (9 EA) 2023-719360<[01] REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING LH AT PASSENGER CABIN 9(EA) I.A.W. B737-800-AMM-33-51-15-400-802;[02] JOB COMPLETED.SDR SWAA2023072883369Eec · failedDURING CRUISE ATFL230 THE NR 2 ENGINE ROLLED BACK TO IDLE. TURNED OFF AUTO PILOT & AUTOTHROTTLE. NR 2 ENGINE PARAMETERS WERE LOW BUT NORMAL FOR IDLE. NR 2 THROTTLE HAD NO RESPONSE AT ALL RAN QRH & LANDED FLAPS 15. EMERGANCY DECLARED. TAXI TO GATE WAS NORMAL. SDR SWAA2023062671639Megaphone · intermittentMEGAPHONE PUSH BUTTON INTERMMITENT<[01] REMOVED AND REPLACED MEGAPHONE AT FWD GALLEY AS PER AMM 25-64-00SDR SWAA2023012594242Megaphone · inoperativeFA REPORTS MEGAPHONE INOP<[01] R&R MEGAPHONE BATTERIES IAW AMM 25-64-00SDR SWAA2022112975741Indicator · failedCABIN FAILED TO PRESSURIZE AT 10;000FT. NO AUTO FAIL LIGHT OR ALTN LIGHTS ILLUMINATED. DUCT PRESSURE NORMAL @ 40 / [01] REMOVED AND REPLACED CABIN ALTITUDE AND DIFFERENTIAL PRESSURE INDICATOR. IAW AMM 21-33-02SDR SWAA2022060614909Pump · faultyDURING TAKEOFF ROLL; AFTER SELECTING TO/GA; THRUST LEVERS ADVANCED TO 91.8% WHEN 98.7% WAS REQUIRED. NEXT MANUALLY ADVANCED BOTH THRUST LEVERS. #1 ONLY MADE TO 92%. #2 AT 98.7%. #1 THRUST LEVER (CONT) ADVANCED FULL FORWARD. HIGHEST #1 OBSERVED STAYED AT 92%. RSDR SWAA2022010352933Balance Weight · corrodedON THE RIGHT WING AT THE TIP; THE INSTALLED WEIGHTS HAVE EVIDENCE OF CORROSION. ; / [01] C/W EA; [02] C/W EA 21-157-03731; [03] C/W EA 21-157-03731SDR SWAA2021122052934Light · inoperativeFWD ENTRY EMERGENCY LIGHTS INOP / [01] REMOVED AND REPLACED FWD LEFT EMER. LIGHTS BATTERY PACK. TESTS GOOD PER AMM 33-51-06; [02] 1. RAFAEL ZUNIGA (TECHNICIAN); 14-DEC-2021 18:47 UTC<BR>REMOVED AND REPLACED FWD LEFT EMER. LIGHTS BATTERY PACK. TESTS GOOD PER AMSDR SWAA2021122053314Scuff Plate · crackedAFT CARGO DOOR AFT CORNER SCUFF PLATE CRACKED -MARKED. ; AFT CARGO DOOR AFT CORNER SCFF PLATE CRACKED -MARKED. / [01] REMOVED AND REPLACED AFT CARGO AFT CORNER SCUFF PLATE IAW AMM 53-11-02. REFERENCE CARD TTG8Q009GRS FOR WORK PERFORMED. LEAK CHECK TO BE ACCOMPSDR SWAA2021122248561Angle · crackedCABIN CENTER SECTION FLOOR PANEL BRAKE ASSY. SUPPORT ANGLE IS CRACKED AT F.S. 540 BETWEEN #2 SEAT TRACK AND CENTER BEAM BL.0 ; / [01] REMOVED AND REPLACED SUPPORT ANGLE AT STA 540 BETWEEN #2 SEAT TRACK AND BL ZERO PER SRM 51-40-02.SDR SWAA2021123048283Panel · delaminatedFUSELAGE PANEL 193CR HAS FIBER GLASS EROSION ON BOTH SIDES AND DELAMINATION ON INTERIOR SIDE. ; / [01] REPAIRED EROSION DAMAGE PER SRM 53-40-70-2R-1.; [02] REPAIRED EROSION AND DELAMINATION DAMAGE PER SRM 53-40-70-2R-.; [03] MISSING REFERENCESDR SWAA2022010347897Plate · crackedRT WING T/E WIGGLE PLATE CRACKED INBD OF #6 FLAP TRACK. REMOVED AND REPLACE WITH NEW WIGGLE PLATE ASSAY. PER SRM 51-40-02SDR SWAA2022010347590Bracket · brokenLEFT WING INBD OF #2 FLAP TRACK AFT T/E LWR SHELF PNL STRUCTURE SUPPORT BRACKET IS BROKEN AT LWR REAR SPAR ; / [01] REMOVED AND REPLACED FITTING ASSY. PER SRM 51-40-02.; [02] INSPECTION COMPLETE ON CORRECTIVE ACTION #1 FOR FITTING ASSEMBLY REPLACEMENT.SDR SWAA2021101931262Light · inoperativeOVERHEAD EMERGENCY LIGHTS AT 13-14F OVERWING INOP / R+R BATTERY PACK FOR 13-14F OVERWING EMERG. LIGHT PER AMM 33-51-06SDR SWAA2021070689400Battery Pack · inoperativeDUE TO REPEAT FAULTS WITH FWD CABIN EMERGENCY LIGHTING; INSPECT WIRING TO BATTERY PACKS M1675; M1676; M2816; AND M2335 AND REPAIR ANY DEFECTS FOUND. IF NO DEFECTS FOUND; REPLACE BATTERY PACK M2335 AS A PRECAUTION / REMOVED AND REPLACED BATTERY PACK M2335. NO DSDR SWAA2021070689401Circuit Breaker · trippedON THE GROUND; WITH BOTH GROUND PWR OR APU POWER; THE FRONT PROVISIONING DOOR EMER. EXIT LIGHT STAYS ILLUMINATED; AND THE FRONT ENTRY EMER EXIT LT AND COCKPIT DOME LIGHT ILLUMINATE INTERMITTENTLY (IN SYNC WITH EACH OTHER). / FOUND C/B EMER. CHARGER 'FWD' POPPESDR SWAA2021060176780Power Supply · inoperativeRH OVER WING EXIT DOOR; FWD; OUTSIDE EMERGENCY EXIT LIGHT INOP. / REMOVED AND REPLACE POWER SUPPLY M1676 AND BATTERY PER AMM 33-51-06SDR SWAA2021060178768Battery · inoperativeRH OVER WING EXIT DOOR; FWD; OUTSIDE EMERGENCY EXIT LIGHT INOP. / REMOVED AND REPLACE POWER SUPPLY M1676 AND BATTERY PER AMM 33-51-06SDR SWAA2021060176779Battery Pack · inoperativeRH OVERWING EXIT DOOR; OUTSIDE; FWD EMERGENCY LIGHT INOP. / CHARGED OVERWING EXIT DOOR BATTERY PACK OPS CK NORMAL PER 33-51-06SDR SWAA2021050367875Charger · inoperativeEMERGENCY LIGHT CHARGER ASSEMBLY INOP. SI #7240002 ROW 21DEF M1671 / REPLACED EMERGENCY LIGHT CHARGER ASSEMBLY @21DEF IAW AMM 33-51-06. OPS CHECK OK.SDR SWAA2021042064847Bulkhead Web · crackedLH WHEEL WELL VAPOR BARRIER HAS 6' CRACK AT LBL 45.64 REMAINING AFTER PERMANENT REPAIR.ACCOMPLISHED INTERIM REPAIR IAW SRM 5710102R2.REPETITIVE ACTION REQUIRED:DO A DETAILED VISUAL INSPECTION EVERY 3000 FLIGHT CYCLES IAW SRM 5710102R2 PAR.2.C. IF ADDITIONAL DASDR SWAA2021030452703Light · inoperativeR/H AFT LOWER EMERGENCY EXIT LIGHT INOP / RE-LAMPED R/H AFT LOWER EMERGENCY EXIT LIGHT PER AMM 33-51-04. OPS CHECKS GOOD.SDR SWAA2020081107312Battery Pack · inoperativeLEFT OVERWING EMERGENCY LIGHT WAS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AT BS 500 IAW AMM 31-51-06, AMD REPLACED THE LAMP IAW AMM 33-51-04. OPS CHECKED GOOD.SDR SWAA2020060990474Battery Pack · dischargedEMERGENCY EXIT LIGHTS FO SIDE STAY ON WITH SWITCH IN ARMED MODE. FOUND M1695 RT EMERGENCY CHARGER + BATTER PACK INOP. REPLACED CHARGER + BATTERY PACK PER AMM 33-51-06.SDR SWAA2020042743633Charger · inoperativeDURING EMERGENCY LIGHT CHECK FOUND ISLE LIGHT ON RIGHT FWD CABIN OUT BATTERY AT STATION 500C AND CHARGER INOP / R/R BATTERY CHARGER & PACK IAW AMM REF # 33-51-06SDR SWAA2020042743634Battery · dischargedFOUND EMERGECENCY LIGHTS OUT ON LEFT SIDE ISLE / REPLACED BATTERY AT STATION ROW 21 ABC IAW AMM REF # 33-51-06SDR SWAA2020042243334Rivet · missingFWD SERVICE DOOR AFT GIRT BAR HANGAR IS BENT. VERY HARD TO STOW THE BAR IS SAFETY POSITION / FOUND AFT BRACKET ON FWD SERVICE DOOR MISSING 1 RIVET. REMOVED SLIDE ASSY AND INSTALLED SLIDE ASSY ON DOOR IAW MT 725-61-06. REMOVED AND REPLACED RIVET ON AFT SLIDE BRSDR SWAA2020032734763Vapor Barrier · crackedSUPPLEMENTAL INFORMATION: L.H W/W VAPOR BARRIER HAS A CRACK 6' IN LENGTH. C/W REPAIR PER SRM 57-10-10-1A-2 REPETITIVE ACTION REQUIRED DO A VISUAL INSPECTION OF THE REPAIR AREA AT 1200 FLIGHT CYCLE INTERVALS OR MORE FREQUENTLY. MAKE SURE THAT CRACK HAS NOT GROWSDR SWAA2020033134763Vapor Barrier · crackedL.H W/W VAPOR BARRIER HAS A CRACK 6' IN LENGTH. C/W REPAIR PER SRM 57-10-10-1A-2 REPETITIVE ACTION REQUIRED DO A VISUAL INSPECTION OF THE REPAIR AREA AT 1200 FLIGHT CYCLE INTERVALS OR MORE FREQUENTLY. MAKE SURE THAT CRACK HAS NOT GROWN PAST THE INTERIM SEAL /SDR SWAA2022040632667Intercostal · crackedFORWARD CABIN FLOOR INTERCOSTAL STA 312-328 RBL32 UPPER FLANGE IS CRACKED AT BOTH FLOOR BOARD HOLES / REMOVED CRACKED INTERCOSTAL AT CABIN STA 312 TO 328 REB 32 IAW 737-800 SRM 51-50-02-0G-0. VERIFIED NEW INTERCOSTAL AS P/N: 141A5410-12 IAW BOEING DWG 141A5400SDR SWAA2022041132665Cap · corrodedAFT CABIN FLOOR BEAM UPPER SURFACE STA 986 LBL43 WL208 HAS CORROSION AROUND DOME NUT FASTENERS / ACCOMPLISHED FLOOR BEAM T-CAP REPAIR AT STA 986 LBL 43 WL 208 I.A.W SRM 53-70-51-2R-6 REV 68SDR SWAA2022040632663Intercostal · crackedFORWARD CABIN FLOOR MACHINED INTERCOSTAL STA 344-360 RBL11 UPPER FLANGE IS CRACKED AT BOTH FLOOR BOARD HOLES / REMOVED AND REPLACED FORWARD CABIN FLOOR MACHINED INTERCOSTAL STA 344-360 RBL II IAW BOEING DWG 141A5400 REV:- AND B737 SRM 51-40-02-0G-0SDR SWAA2022040632662Intercostal · crackedFORWARD CABIN FLOOR MACHINED INTERCOSTAL STA 344-360 BL0 UPPER FLANGE IS CRACKED AT AFT FLOOR BOARD HOLE / REMOVED AND REPLACED FORWARD CABIN FLOOR MACHINED INTERCOSTAL STA 344-360 BLO IAW BOEING DWG 141-A5400 REV:- AND B737 SRM 51-40-02-0G-0SDR SWAA2022040632661Intercostal · crackedFORWARD CABIN FLOOR MACHINED INTERCOSTAL STA 344-360 LBL11 UPPER FLANGE IS CRACKED AT AFT FLOOR BOARD HOLE / REMOVED AND REPLACED FORWARD CABIN FLOOR MACHINED INTERCOSTAL STA 344-360 LBL II IAW BOEING DWG 141A5400 REV:B AND B737 SRM 51-40-02-0G-0SDR SWAA2022040632660Intercostal · crackedFORWARD CABIN FLOOR INTERCOSTAL STA 312-328 LBL45 UPPER FLANGE IS CRACKED AT FLOOR BOARD HOLE / REMOVED AND REPLACED FWD CABIN FLOOR INTERCOSTAL AT STA 312 - 328 LBL 45 IAW BOEING DWG 141A5400 REV - BOEING 737-800 SRM 51-40-02-0G-0 P/N 141A10012 ATAG A61068SDR SWAA2022040632657Intercostal · crackedFORWARD CABIN FLOOR INTERCOSTAL STA 277-294 BL0 UPPER FLANGE IS CRACKED AT BOTH FLOOR BOARD HOLES / REMOVED AND REPLACED FORWARD CABIN FLOOR INTERCOSTAL STA 227 TO 294 BLO IAW B-737 SRM 51-40-02 AND DWG 141A5400 REV- ATAG WN6748 P/N141A5410-3SDR SWAA2022041132647Support · corrodedAFT CABIN FLOOR SUPPORT STA 947+2 TO 986+3 LBL50 WL208 HAS CORROSION EMITTING FROM UNDER LAV MOUNT / REMOVED AND REPLACED AFT CABIN FLOOR SUPPORT STA 947 +2 TO STA 967 LBL50 IAW DWG 147A5650 REV C AND B-737 SRM 51-40-02 ORIG 'T' .150; REMAINING .120; LOSS OF .SDR SWAA2022041132644Floorbeam · corrodedAFT CABIN FLOOR BEAM STA 947 LBL13-RBL11 WL208 UPPER FLANGE HAS CORROSION IN AND AROUND FASTENER HOLES / REMOVED CORROSION. BLEND AREA AT RBLID. ORIGINAL 'T' .180 REMAINING .146 LOSS OF .034 OUT OF LIMITS IAW B737 SRM 53-70-51-1A-1. FIG 104. REPAIRED AREA IAW SDR SWAA2022041132643Beam · corrodedAFT CABIN R-2 CREASE BEAM INNER CHORD STA 947+12 TO 986+3 RBL51 WL208 HAS CORROSION / REMOVED CORROSION FROM R2 DOOR CREASE BEAM ORIGINAL 'T' .090. REMAINING .072. LOSS OF .018 OUT OF LIMITS IAW B737 SRM 51-70-15-1A-1. REMOVED AND REPLACED CREASE BEAM IAW B737SDR SWAA2022040532641Web · corrodedAFT CARGO COMPARTMENT BETWEEN STA 787+7' AND 847 UNDER CENTER LOWER DOOR TRESHOLD PLATE ;TRESHOLD WEB IS CORRODED IN SEVERAL AREAS BETWEEN RBL 20 AND RBL 28 WL 155.3 AS MARKED / REMOVED CORROSION AFT CARGO COMPARTMENT THRESHOLD WEB STA 787+7 TO 847 IAW SRM 51-
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