N8309C
Service difficulty reports · 193
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 = 'N8309C' 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 = 'N8309C' 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 SWAA2023120815238Scuff Plate · crackedFWD CARGO BAY FWD CORNER SCUFF PLATE IS CRACKED<[01] VERIFIED MEASUREMENTS TABLE;[02] FWD CARGO BAY FWD CORNER SCUFF PLATE REPAIRED PER SRM 53-30-15-2R-1.<BR><BR>TASK CARD COMPLETED;[03] VERIFIED COMPLETION OF CORRECTIVE ACTIONS 2 AND MEASUREMENT TABLE.SDR SWAA2023120814747Bulkhead · crackedCRACKED LOWER L/H COMPOSITE BULKHEAD AT BS663 LBL34 WL158.<[01] CRACK AT THE LOWER LEFT-HAND COMPOSITE BULKHEAD BODY STATION 663; LBL 34; WL 158; WAS REPAIRED IAW SM 51-70-04-2R-10.;[02] ITEM 1 SHOULD READ: CRACK AT THE LOWER LEFT-HAND COMPOSITE BULKHEAD BODY SDR SWAA2023121113981Inlet · corrodedCORROSION ON L/H ENGINE UPPER BARREL SKIN AT 11:45 POSITION; 2' FROM L/E. (MARKED)<[01] COMPLETED LAST STEP; ALL STEPS ARE COMPLETE. REPAIRED #1 ENGINE INLET COWL UPPER BARREL SKIN AT 12:00 PER SRM 54-10-01-1A-1;[02] VERIFIED COMPLETE STEP 6; MEASUREMENTS TABLSDR SWAA2023120814426Battery Pack · inoperativeFWD L/H EMERGENCY OVERWING LT INOP<[01] EMERGENCY LIGHT BATTERIES WERE REPLACED ON CCN TTG8Q00P6HJ7 PERFORMED GOOD OPS CHECK OF <BR> OF THE FWD L/H EMERGENCY OVERWING LIGHT IAW AMM 33-51-00-710-801;[02] VERIFIED EMERGENCY LIGHT BATTERIES WERE REPLACED ON CCN TSDR SWAA2023120814427Battery Pack · inoperativeSTRONGBACK EMERGENCY EXIT LIGHT AT SEAT ROW 13 CBA IS INOP<[01] EMERGENCY LIGHT BATTERIES WERE REPLACED ON CCN TTG8Q00P6HJ7 PERFORMED GOOD OPS CHECK OF <BR> OF THE STRONGBACK EMERGENCY EXIT LIGHT AT SEAT ROW 12 CBA IAW AMM 33-51-00-710-801;[02] UPDATED MEASURESDR SWAA2023120814428Battery Pack · inoperativeSTRONGBACK EMERGENCY EXIT LIGHT AT SEAT ROW 8 CBA IS INOP; STRONGBACK EMERGENCY EXIT LIGHT AT SEAT ROW 8 CBA IS INOP.<[01] EMERGENCY EXIT LIGHT BATTERIES WERE REPLACED ON CCN TTG8Q00P6HJ7 PERFORMED GOOD OPS CHECK OF THE STRONGBACK EMERGENCY EXIT LIGHT AT SEAT SDR SWAA2023050141387Flap · delaminatedLH WING OB AFT FLAP IB LOWER SURFACE DELAMINATED.<[01] REMOVED L/H OUTBOARD AFT FLAP;[02] INSTALLED REPLACEMENT LH OTB AFT FLAP REF MM 27-51-22SDR SWAA2023050141392Wire · looseCABIN RH AOE LOWER EMERGENCY EXIT LIGHT WIRES ARE NOT SECURE BEHIND PANEL.<[01] REMOVED ?RETURN AIR GRILLE? BELOW R/H AOE EMERGENCY EXIT; PULLED WIRES THROUGH AND SECURED; THEN REINSTALLED ?RETURN AIR GRILLE? PER AMM 21-23-03SDR SWAA2023042841376Girt Bar · out of adjustFWD ENTRY DOOR SLIDE GIRT REQUIRES ADJUSTMENT<[01] READJUSTED VELCRO ATTACHMENT ON GIRT BAR SWEEPER SLEEVE PER AMM 25-66-01 SEE MT 725-61-06 TTG8Q00CF7P4SDR SWAA2023021603723Door · crackedFOUND A CRACK ON LOWER PORTION OF ELECTRICAL GROUND POWER RECEPTACLE DOOR SURROUND<[01] UPDATE MEASUREMENTS;[02] PERFORMED HFEC INSPECTION OF DAMAGED AREA PER B737 NDT MANUAL 51-00-00 PROCEDURE 23. NO DEFECTS NOTED;[03] PERFORMED REPAIR TO LOWER PORTION OF ELESDR SWAA2022082946710Charger · inoperativeBOTH LH OVERWING INTERIOR EXIT SIGNS INOP / [01] REPLACED EMER BATTERY CHARGER AND BATTERY PER AMM 33-51-06. OPS GOOD.SDR SWAA2022082947486Battery · inoperativeBOTH LH OVERWING INTERIOR EXIT SIGNS INOP / [01] REPLACED EMER BATTERY CHARGER AND BATTERY PER AMM 33-51-06. OPS GOOD.SDR SWAA2022051908406Bracket · brokenAFT SERVICE DOOR GIRT BAR BRACKET BROKEN / [01] GIRT BAR BRACKET ISN'T BROKEN; IT NEEDED ADJUSTMENT TO HOLD GIRT BAR TO MAKE SURE THAT THE BRACKETS OPERATE CORRECTLY PER MM 25-66-02 STEP 3.E.SDR SWAA2022022275313Slide · lowR2 DOOR SLIDE PRESSURE LOW / [01] REMOVED AND REPLACED AFT SERVICE DOOR SLIDE PER AMM 25-66-01 AND <BR> MT725-61-06-AS REF MT FOR PART NUMBER AND SERIAL NUMBER ONSDR SWAA2022011260087Light · faultyROW 14ABC EMER EXIT WINDOW SIDEWALL LT FLASHING ; / [01] OK TO CONTINUE PER MEL 33-2-04 SP1B. APPLIED TAPE OVER LT.; [02] REMOVED AND REPLACED EMER EXIT OVERWING LIGHT ASSY PER AMM 33-21-00-960-805. OPS CK GOOD. THIS CLEARS MDDR#43096. PLACARDS REMOVED.SDR SWAA2021120747143Battery Pack · inoperativeEMERGENCY EXIT LIGHT BATTERY PACK M1695 WILL NOT CHARGE ; / [01] REMOVED AND REPLACED EMERGENCY BATTERY PACK M1695 IAW AMM 33-51-06-960-805 TEST/OPS CHECK GOOD; [02] VERIFIED STEP 1; [03] AUDITEDSDR SWAA2021120745917Skin · corrodedCORROSION ON EXTERIOR FUSELAGE SKIN AT STA 1016; 2 INCHES ABOVE TO 1 INCH BELOW STR 4L. DOT 203-004 ; / [01] REMOVED CORROSION AND CHECK WITH 10X MAGNIFYING GLASS IAW SRM 51-10-02-0G-0 ITEM 15;.; [17] REMOVED DAMAGE FROM FUSELAGE SKIN STA 1016 S-4L; FABRICATEDSDR SWAA2021120744732Fairing · crackedA-061 DOT 014 LOWER FILLET FAIRING 191D CRACKED AT FASTENER HOLE ; / [01] EVALUATED AND FOUND FASTENER HOLE ON EDGEBAND AS MARKED DAMAGED ON UPPER SIDE. FOUND TO BE REPAIRABLE IAW SRM 53-30-70-2R-1 TABLE 202 AND SRM 51-70-04-2R-9.<BR><BR>CLEANED AND PREPPED IASDR SWAA2021110540352Battery · inoperativeBOTH RT OUTSIDE AND INSIDE OVERWING AND CENTER CEILING LIGHTS INOP ; / [01] REMOVED AND REPLACED BATTERY PACKS AT M1676; M1671; AND BATTERY PACK AND CHARGER AT 1695 PER AMM 33-51-06. OPS CHECK GOOD.SDR SWAA2021110540872Charger · inoperativeBOTH RT OUTSIDE AND INSIDE OVERWING AND CENTER CEILING LIGHTS INOP ; / [01] REMOVED AND REPLACED BATTERY PACKS AT M1676; M1671; AND BATTERY PACK AND CHARGER AT 1695 PER AMM 33-51-06. OPS CHECK GOOD.SDR SWAA2021061882962Battery Pack · inoperativePASSENGER CABIN EMERGENCY LIGHTS AT OVERHEAD BINS 15BC 19 ABC 23ABC AND SIDEWALL LIGHT AFT OF OVERWING EMERGENCY EXIT DOOR ARE INOP / REPLACED EMERGENCY LIGHT BATTERY PACK PER AMM 33-51-06 OPS CHECK GOODSDR SWAA2021012042823Battery Pack · inoperative3 EMERGENCY EXIT SIGNS IN FWD LT ENTRYWAY AND L1 EMERGENCY SLIDE LIGHT INOPERABLE. R & R FWD LT EMERGENCY BATTERY PACK M01675, IAW AMM 33-51-06. OPERATIONS CHECK GOOD.SDR SWAA2019120239255Battery · failedPASSENGER CABIN, FORWARD EMERGENCY FLASHLIGHTS FAILED INSPECTION CHECK ( LIGHTS DID NOT BLINK). / R&R FLASHLIGHT BATTERIES IAW AMM.SDR SWAA2019120239290Battery Pack · dischargedR1 DOOR EMERGENCY LIGHTS INOP. / R&R BATTERY PACK M2816 IAW AMM.SDR SWAA2019120239289Battery Pack · dischargedAFT RH EMERGENCY LIGHT BATTERY AT M1672 INOP. / R&R BATTERY PACK IAW AMM.SDR SWAA2019120239288Battery Pack · dischargedAFT L/H EMERGENCY LIGHT BATTERY AT M1673 INOP. / R&R BATTERY PACK IAW AMM.SDR SWAA2022032534365Cap · crackedAFT CARGO STA 727 CENTER FLOOR PLATE STIFFENER IS CRACKED. / RECEIVED AND VERIFIED NEW AFT CARGO FLOOR STA 727 CAP STRIP ASS AS P/N 453A2611-25 IAW AIPC 25-52-10-19 ITEM 55A TAG# WN1541SDR SWAA2022032534364Rib · cracked: LEFT HORIZONTAL STAB L/E CRACK ON FIFTH RIB IN FROM INB END. MARKED WITH BLACK MARKER / REMOVED FIFTH TAB FROM INB END OF LEFT HORIZONTAL STAB 4E CRACKED AND INSTALLED NEW RIB ASSY P/N 186A130S-1 (RUB CRACKED NOT FOUND ALLOWABLE LIMITS ON THE SRM) IAW B737-8SDR SWAA2019120239253Rib · crackedL/H HORIZONTAL STABILIZER LEADING EDGE CRACKED ON FIFTH RIB IN FROM INBOARD END. / R&R RIB ASSEMBLY IAW SRM & DWG.SDR SWAA2022032434356Scuff Plate · crackedAFT CARGO AFT CORNER SCUFF PLATE CRACKED / REMOVED CRACKED SCUFF PLATE; RE-WORKED SCUFF PLATE AS PER AAR BACKSHOP W/O 40218-1600-0001. RE-INSTALLED SCUFF PLATE AS PER B737 AMM 53-11-02-420-801SDR SWAA2022032434353Skin · delaminatedL/H WING # 4 SPOILER UPPER SURFACE DENT WAS FOUND TO BE DELAMINATED / EVALUATED REMOVED DAMAGE; CLEANED; PREPPED AND REPAIRED DENT DAMAGE/ DELAM ON L/H WING #4 SPOILER UPPER SURFACE IAW B737-800 SRM 57-53-01-2R-4; PAR 3 (A AND B); SRM 51-70-10-2R-2; PAR (4D ANSDR SWAA2019112739186Skin · delaminatedL/H WING # 4 SPOILER UPPER SURFACE DENT WAS FOUND TO BE DELAMINATED. / REPAIRED #4 SPOILER IAW SRM.SDR SWAA2022032434342Floor Panel · debondedPASSENGER CABIN PANEL 221BF FWD I/B CORNER IS CRUSHED AND LOWER SURFACE PLIES DISBONDED AND TORN. / WORK ACCOMPLISHED ON NRC# ( 40216-1000 / 0038 )DEFECT# ( Y135836 )SDR SWAA2022032434331Floor Panel · brokenPASSENGER COMPARTMENT PANEL 221GF FWD O/B CORNER IS BROKEN. / REPAIRED FLOORBOARD 221GF O/B CORNER IAW SRM 53-00-50-2R-1; PG'S 1;2; STEPS 3(A-N0. A06130; A00515SDR SWAA2022032434323Web · cracked#1 ENGINE INBOARD FAN COWL VERTICAL WEB AFT OF OIL SERVICE DOOR IS CRACKED AT UPPER END / REMOVED WEB SHEILD AT #1 ENG I/B FAN COWL VERTICAL WEB AFT OF OIL SERVICE DOOR I.A.W SRM 51-40-02-0G-0. DRILLED NEW WEB SHIELD I.A.W SRM 51-40-05-0G-0 AND CMM 71-13-30. ISDR SWAA2022032334301Attach Angle · crackedFWD CARGO COMPARTMENT STA 500I RBL 23 STRINGER CLIP IS CRACKED AS MARKED. / REMOVED STRINGER CLIP CRACKED AND INSTALLED NEW STRINGER CLIP P/N 143A1010-21 ON FWD CARGO COMPARTMENT STA 500I RBL 23' IAW B737-800 SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; DWG # 143A101SDR SWAA2022032334296Attach Angle · crackedFWD CARGO COMPARTMENT STA 500I LBL 23 STRINGER CLIP IS CRACKED AS MARKED. / REMOVED CRACKED STRINGER STA 500I LBL 23 AND INSTALLED NEW STRINGER CLIP PART NO: 143A1010-47 ATG: A68459 IAW DWG: 143A123469A AND SRM 51-40-02-06-0. APPLIED CIC AS REQUIRED IAW AMM 51SDR SWAA2019112739185Stringer Clip · crackedFORWARD CARGO COMPARTMENT STRINGER CLIP CRACKED AT BS. 500I, LBL 23. / R&R STRINGER CLIP IAW SRM AND DWG.SDR SWAA2019112539085Stringer Clip · crackedFORWARD CARGO COMPARTMENT STRINGER CLIP CRACKED AT BS. 500I, RBL 23. / R&R STRINGER CLIP IAW SRM & DWG.SDR SWAA2022032334283Angle · corrodedAFT CARGO COMPARTMENT L/H 'Z' ANGLE FROM STA 727F TO 807; LBL 25; W/L 157 HAS MULTIPLE AREAS OF CORROSION / REMOVED CORROSION FROM L/H ZEE ANGLE STA 727F TO STA 807 IAW SRM 51-10-02-0G-0 PAR 15. EVALUATED MATERIAL LOSS ORIGINAL=.040' REMAINING=.034' LOSS=.007'SDR SWAA2022032334282Web · corroded: AFT CARGO COMPARTMENT R/H CUSP WEB BELOW THE 'Z' ANGLE FROM STA 747 TO 767; RBL 25; W/L 157 HAS MULTIPLE AREAS OF CORROSION / REMOVED AFT CARGO COMPARTMENT R/H CUSP WEB BELOW THE 'Z' ANGLE FROM STA 737 TO 767; RBL 25. W/L 157 IAW B737 SRM 51-40-02-0G-0. REMOSDR SWAA2022032334276Beam · corrodedPASSENGER CABIN STA 960-993 RBL 53 WL 208; CREASE BEAM INNER CHORD IS CORRODED. / REMOVED DAMAGE ON CREASE BEAM PASS. CABIN STA 960 - 993 RBL 53 WL 208. IAW B-737 SRM 51-10-02-0G-0. VERIFIED MAT LOSS. ORG. 'T' .080; REMAINING MAT. .065; MAT. LOSS .015'. FOUND SDR SWAA2022032334269Cap · corrodedFWD PIT; RH #2 CAP STRIP HAS CORROSION ON LOWER SURFACE. 21' FROM FWD END / REMOVED AND REPLACED; FWD PIT RH#2 CAP SSTRIP PN 453A1611-31 TO SI# 4251070 ATAG WN4395. IAW B-737 SRM 51-40-02-0G-0 AND IPC 25-52-10-03 ITEM 380. PART REPLACED DUE TO NO PUBLISHED SRMSDR SWAA2022032334267Floor Panel · corrodedAFT CARGO COMPARTMENT PANEL 140AF HAS CORROSION AT THE EDGES AS MARKED. / THE ACCUMULATED CORROSION DAMAGE LENGTH IS MORE THAN 20' INCHES THEREFORE PANEL 140AF IS OUT OF LIMITS IAW SRM 53-00-53-1A-1 FIG 102. FABRICATED NEW PANEL 140AF IAW SRM 51-40-5-0G-0 AND SDR SWAA2022032334266Floor Panel · corrodedAFT CARGO COMPARTMENT PANEL 140CF HAS CORROSION AT THE EDGE AS MARKED. / LENGTH OF CORROSION (12') ON AFT CARGO COMPARTMENT PANEL 140CF EXCEEDS ALLOWABLE LIMITS AS PER B737 SRM 53-00-53-1A-1 FIG 102 SHT 1. REPLACEMENT PNL IS 453A2610-18 (WO3657) (SI) 7253212. SDR SWAA2022032334265Floor Panel · corrodedAFT CARGO COMPARTMENT PANEL 140DF HAS CORROSION AT THE EDGE AS MARKED. / EVALUATED CORROSION DAMAGE DAMAGE EXCEEDS 20' IN LENGTH FOUND TO BE OUT OF LIMITS RECEIVED AND VERIFIED NEW PANEL 140DF AS P/N 453A2610-20 IAW SRM 53-00-53-1A-1 FIG 102; AIPC 25-52-10-19 SDR SWAA2022032334264Scuff Plate · crackedFWD CARGO. FWD CORNER SCUFF PLATE IS CRACKED AT WELD AND UPPER AFT EDGE. (2EA PLACES) / REPAIRED FWD CORNER SCUFF PLATE OF FWD CARGO PIT I.A.W W/O # 40218-1400-0001 & REMOVED & INSTALLED I.A.W AMM 53-11-02-420-801.SDR SWAA2022032334263Floor Panel · corrodedFWD CARGO FLOOR PANEL 120AF HAS CORROSION AROUND PERIMETER OF PANEL. / FWD CARGO FLOOR PANEL FOUND TO BE OUT OF LIMITS AND REPLACED FLOOR PANEL 2024 T3 0.071' AND TESTED AND PRIMED PANEL IAW B737-800 SRM 51-40-05-0G-0; SRM 51-20-01-0G-0; AWG 3 453A1610 REV: 'FSDR SWAA2022032334262Floor Panel · corrodedFWD CARGO FLOOR PANEL 120DF; UPPER SURFACE OF PANEL HAS CORROSION AROUND PERIMETER OF PANEL / REPLACED PANEL # 120 DF FWD CARGO FLOOR PANEL DF I/A/W 737 IPC 25-52-10-17 CORROSION REMOVAL AROUND PERIMEMTER OF PANEL WAS MORE THAN 20' IN LENGTH OUT OF LIMITS PER SDR SWAA2022032334259Web · corrodedFWD CARGO DOOR CUTOUT; LOWER DOOR SILL WEB HAS CORROSION ON UPPER SURFACE. STA 400 TO 480+4; RBL 21 TO RBL 26 / BLENDED CORROSION ON UPPER SURFACE OF FWD CARGO LOWER DOOR SILL WEB STA 480+4" RBL 21-26, ORIGINAL THICKNESS .045, REMAINING .027, LOSS OF .018 FOUN
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