N8514F
Service difficulty reports · 115
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 = 'N8514F' 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 = 'N8514F' 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 SWAA2025010677586Floor Panel · pulledPASSENGER CABIN FLOOR ACCESS PANEL 231AF HAS PULLED FIBERS.<[01] REPLACED PANEL PER AMM 53-21-00. REFERENCE TASK CARD TTG8Q00X75K4 FOR INDIVIDUAL SIGN OFFS.;[02] 02 - INSPECTED PER [AMM 53-21-00-400-801-NG (PASSENGER CABIN FLOOR PANEL INSTALLATION - PERMANENT)SDR SWAA2025010677564Floor Panel · pulledPASSENGER CABIN FLOOR ACCESS PANEL 222DF HAS PULLED FIBERS.<[01] REPLACED PANEL PER AMM 53-21-00. REFERENCE TASK CARD TTG8Q00X75KA FOR INDIVIDUAL SIGN OFFS.;[02] 02 - INSPECTED PER [AMM 53-21-00-400-801-NG (PASSENGER CABIN FLOOR PANEL INSTALLATION - PERMANENT)SDR SWAA2025010677587Floor Panel · pulledPASSENGER CABIN FLOOR ACCESS PANEL 222CF HAS PULLED FIBERS.<[01] REPLACED PANEL PER AMM 53-21-00. REFERENCE TASK CARD TTG8Q00X75KC FOR INDIVIDUAL SIGN OFFS.;[02] 02 - INSPECTED PER [AMM 53-21-00-400-801-NG (PASSENGER CABIN FLOOR PANEL INSTALLATION - PERMANENT)SDR SWAA2025010677565Floor Panel · pulledPASSENGER CABIN FLOOR ACCESS PANEL 221GF HAS PULLED FIBERS.<[01] REPLACED PANEL PER AMM 53-21-00. REFERENCE TASK CARD TTG8Q00X75KE FOR INDIVIDUAL SIGN OFFS.;[02] 02 - INSPECTED PER [AMM 53-21-00-400-801-NG (PASSENGER CABIN FLOOR PANEL INSTALLATION - PERMANENT)SDR SWAA2025010677588Floor Panel · pulledPASSENGER CABIN FLOOR ACCESS PANEL 221FF HAS PULLED FIBERS.<[01] REPLACED PANEL PER AMM 53-21-00. REFERENCE TASK CARD TTG8Q00X75KG FOR INDIVIDUAL SIGN OFFS.;[02] 02 - INSPECTED PER [AMM 53-21-00-400-801-NG (PASSENGER CABIN FLOOR PANEL INSTALLATION - PERMANENT)SDR SWAA2025010677589Floor Panel · pulledPASSENGER CABIN FLOOR ACCESS PANEL 221EF HAS PULLED FIBERS.<[01] REPLACED PANEL PER AMM 53-21-00. REFERENCE TASK CARD TTG8Q00X75KJ FOR INDIVIDUAL SIGN OFFS.;[02] 02 - INSPECTED PER [AMM 53-21-00-400-801-NG (PASSENGER CABIN FLOOR PANEL INSTALLATION - PERMANENT)SDR SWAA2025010677590Floor Panel · pulledPASSENGER CABIN FLOOR ACCESS PANEL 221DF HAS PULLED FIBERS.<[01] 02 - INSPECTED PER [AMM 53-21-00-400-801-NG (PASSENGER CABIN FLOOR PANEL INSTALLATION - PERMANENT)];[02] REMOVED AND REPLACED PANEL 221DF I.A.W. AMM 53-21-00;[03] C/W INSPECTIONSDR SWAA2025010677566Floor Panel · pulledPASSENGER CABIN FLOOR ACCESS PANEL 221CF HAS PULLED FIBERS.<[01] REPLACED PANEL PER AMM 53-21-00. REFERENCE TASK CARD TTG8Q00X75KN FOR INDIVIDUAL SIGN OFFS.;[02] 02 - INSPECTED PER [AMM 53-21-00-400-801-NG (PASSENGER CABIN FLOOR PANEL INSTALLATION - PERMANENT)SDR SWAA2025010877389Web · corrodedAFT CARGO DOOR THRESHOLD WEB STA 794-847; RBL 27 HAS CORROSION.<[01] REMOVED SURFACE CORROSION ON DOOR SILL WEBBING AT STA 794-847. REMOVED OVER .015. PART FOUND TO BE OUT OF LIMITS. REF SRM 53-60-15-1A-1.;[02] REMOVED DOOR SILL WEBBING. SRM 51-40-02;[03] LOCASDR SWAA2025010877416Angle · crackedFORWARD CARGO FLOOR STRUCTURE STRINGER CLIP AT STA 500I AND RBL 21.00 HAS CRACK AT RIVET.<[01] DISPLACED BAFFLE AND RH LOWER BULKHEAD CHORD AT STA. 500I. PER SRM 51-40-02.;[02] REMOVED OLD STRINGER CLIP; LOCATED AND DRILLED NEW CLIP PER SRM 51-40-02.;[03] INSPSDR SWAA2025010877417Angle · crackedFORWARD CARGO FLOOR STRUCTURE STRINGER CLIP AT STA 500I AND LBL 21.00 HAS CRACK AT RIVET.<[01] REMOVED AND REPLACED STRINGER CLIP PER SRM 51-40-02.;[02] REMOVED AND REPLACED STRINGER CLIP PER SRM 51-40-02.;[03] STEPS 1 THRU 4 ARE NOT SIGNED AND NO SRM REFERENCSDR SWAA2025010777231Tie Down · corrodedFWD LAV. I/B TIE-DOWN FITTING AT STA 280 LBL 13 HAVE CORROSION INTERNALLY IN FASTNER HOLE. REMOVED AND REPLACED FWD LAV INBOARD FITTING AT STA 280 LBL 13 PER SRM 51-40-02SDR SWAA2025010777232Tie Down · corrodedFWD LAV. I/B TIE-DOWN FITTING AT STA 303 LBL 13 HAVE CORROSION INTERNALLY IN FASTNER HOLE. REMOVED AND REPLACED FWD LAV INBOARD TIE DOWN FITTING AT STA 303 LBL 13 PER SRM 51-40-02.SDR SWAA2025010777402Nut Plate · corrodedAFT CARGO FLOOR SUPPORT STRAP STA 887; RBL 20 NUT PLATE HAS CORROSION.<[01] REMOVED AND REPLACED CORRODED NUT PLATE ON AFT CARGO FLOOR SUPPORT STRAP PER SRM 51-40-02.;[02] C/W INSP. REMOVED AND REPLACED CORRODED NUT PLATE ON AFT CARGO FLOOR SUPPORT STRAP PER SSDR SWAA2025010877224Angle · corrodedAFT GALLEY SERVICE DOOR Z ANGLE HAS EVIDENCE OF CORROSION AROUND FASTENERS HOLES.<[01] REMOVAL AND REPLACEMENT OF AFT GALLEY SERVICE DOOR Z ANGLE TO BE ACCOMPLISHED ON TTG8Q00XLYB4.;[02] BLENDED CORROSION AFT GALLEY SERVICE DOOR Z ANGLE; ORIGINAL MATERIAL THICSDR SWAA2025010877218Angle · corrodedAFT GALLEY SERVICE DOOR; Z ANGLE HAS EVIDENCE OF CORROSION. ( STA. 947 TO STA. 967)<[01] BLENDED CORROSION PER SRM 51-10-02. DAMAGE REMOVAL FOUND TO BE OUT OF LIMITS PER SRM 53-70-15-1A-1.;[02] REMOVED AFT GALLEY SERVICE DOOR Z ANGLE PER SRM 53-70-15;[03] LOCASDR SWAA2025010877222Angle · corrodedAFT GALLEY SERVICE DOOR; Z ANGLE HAS EVIDENCE OF CORROSION AT STA. 986 +6.<[01] REMOVAL AND REPLACEMENT OF AFT GALLEY SERVICE DOOR Z ANGLE TO BE ACCOMPLISHED ON TTG8Q00XLYB4.;[02] BLENDED CORROSION AFT GALLEY SERVICE DOOR Z ANGLE; ORIGINAL MATERIAL THICKNESS ISDR SWAA2025010777225Floorbeam · corrodedAFT L/H LAV; FLOOR BEAM UNDER AFT OUTBOARD MOUNT; HAS EVIDENCE OF CORROSION AT STA. 947.<[01] EVALUATED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1.;[02] COMPLIED WITH INSP.<BR>1. DAVID BELL (TECHNICIAN); 16-DEC-2024 18:47 UTC<BR>EVALUATED COSDR SWAA2025010777220Floorbeam · cockedAFT R/H LAV; FLOOR BEAM UNDER AFT OUTBOARD MOUNT; HAS EVIDENCE OF CORROSION AT STA. 947.<[01] EVALUATED CORROSION DAMAGE AND FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1.;[02] COMPLIED WITH INSP.<BR>1. DAVID BELL (TECHNICIAN); 16-DEC-2024 21:14 UTC<BR>EVALUSDR SWAA2025010777226Floorbeam · corrodedAFT R/H LAV; FLOOR BEAM UNDER AFT INBOARD MOUNT; HAS EVIDENCE OF CORROSION AT STA. 947.<[01] EVALUATED CORROSION DAMAGE AND FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1.[14] OK TO INSTALL REPAIR PARTS ON STA 947 FLOOR BEAM;[15] INSTALLED RH AND LH STA 947 FSDR SWAA2025010876376Threshold · crackedFORWARD SERVICE DOOR THRESHOLD HAS CRACK AT TOP; FORWARD EDGE. FORWARD SERVICE DOOR THRESHOLD HAS CRACK AT TOP FORWARD EDGE.<[01] REPLACED FORWARD SERVICE DOOR THRESHOLD WITH NEW THRESHOLD. UP-SIZED PILOT HOLES AND COUNTERSUNK I/A/W SRM 51-40-05 AND SRM 51-40-SDR SWAA2024112561797Battery Pack · inoperativeSEVERAL EMERGENCY LIGHTS ARE INOP IN THE CABIN ON BOTH RH AND LH SIDE<[01] M1670<BR>M1676;[02] REMOVED AND REPLACE EMERGENCY LIGHT BATTERY AND CHARGER AT LOCATIONS M1670 AND M1676 PER AMM 33-51-06SDR SWAA2024111960803Flashlight · inoperativeFWD INBD JUMPSEAT FLASHLIGHT INOP.<[01] REMOVED AND REPLACED FWD INBD JUMP SEAT FLASHLIGHT BATTERY REF B737 AMM 25-64-00 OP/C GOODSDR SWAA2024050782507Flashlight · inoperativeFWD ENTRY FLASHLIGHT INOP<[01] REMOVED AND REPLACED FWD ENTRY FLASHLIGHT AND BATTERY IAW AMM 25-64-00. THIS CLEARS MEL 25-12-01.SDR SWAA2023122936098Spar · crackedLH HORIZONTAL STAB FRONT SPAR LOWER CHORD DEFLECTED AT STA 234.23 LENGTH 11 WIDTH 0.67 DEPTH 0.062<[01] PERFORMED HFEC NO DAMAGE NOTED PER NDT PART 6 51-00-00 PROCEDURE 23.;[02] REPAIRED PER 23-155-03701 (COMPONENT - SWA - REPAIR - LHS HORIZONTAL STAB FRONT SPSDR SWAA2023081789657Seal · crackedLT HORIZONTAL UPPER FRONT SLIDING SEAL IS CRACKED.<[01] R+R SLIDING SEAL REF AMM 53-31-31SDR SWAA2023032016717Flap System · lockedFLAPS WOULD NOT EXTEND BEYOND5 DURING APPROACH<[01] RE-SET-?ELECTRIC FLAPS? TO NORMAL & SET TRIM TAB WITHIN GREEN BAND & CYCLED FLAPS FULL UP/DOWN SEVERAL TIMES PER AMM 27-81-00 OPS NORMAL. OK FOR CONTINUED SERVICE;[02] RE-SET-?ELECTRIC FLAPS? TO NORMAL & SET SDR SWAA2022122983706Battery Pack · inoperativeEMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK M2816 INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK M2816. PERFORMED A GOOD OPS TEST IAW AMM 33-51-06-960-805.SDR SWAA2022122983707Battery Pack · inoperativeEMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK M1675 INOPERATIVE. REPLACED THE BATTERY PACK M1675. PERFORMED A GOOD TEST IAW AMM 33-51-06-960-805.SDR SWAA2022123079165Fairing · delaminatedNR 7 FWD FLAP TRACK FAIRING HAS WIND EROSION DAMAGE AT CENTER MOUNT FASTENER HOLES. FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 57-53-70-1A-1, PARA 4 D 1. SRM 57-53-70-2R-3, PARA 4 B 2 AND 5 E 3. REMOVED SURFACE FINISHES AND DELAMINATED PLIES TO A REGSDR SWAA2022123078966Web · crackedRIGHT WING; TRANSVERSE WEB ABOVE NR 2 PYLON AFT TIP IS CRACKED ON UPPER LEG AT O/B ATTACH RIVET LOCATION. REMOVED THE TRANSVERSE WEB IAW SRM 51-40-02-0G-0. INSTALLED A NEW TRANSVERSE WEB IAW SRM 51-40-05-0G-0, SRM 51-40-02-0G-0, & AIPC 57-50-00-36A.SDR SWAA2022123078663Support Plate · corrodedFWD CARGO BAY, RT FLOOR TO SIDEWALL PLATE HAS MULTIPLE AREAS OF CORROSION AROUND NUT PLATE HOLES, BS 500D+7 - 500F+11, RBL 24.5, WL 156. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. REMOVED AND REPLACED THE DAMAGED SUPPORT PLATE AND REPAIRED SRM 53-00-SDR SWAA2022123078665Plate · corrodedFWD CARGO BAY, LEFT FLOOR TO SIDEWALL PLATE HAS MULTIPLE AREAS OF CORROSION AROUND NUT PLATE HOLES BS 500C+12 - 500F+3, LBL 24.5, WL156. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. CUT AND REMOVED DAMAGED SECTION IAW SRM 53-0053-2R-5 STEP 4. B, AND EASDR SWAA2022122278659Panel · crackedCRACKED BREAK PANEL STA 540, LBL 1, WL 208. REPLACED CRACKED BREAK PANEL BS 540, BL 0 - LBL 25, WL 208 IAW SRM 51-40-02-0G-0; SRM 51-40-05-0G-0.SDR SWAA2022123078435Support · corrodedCORROSION ON THE AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT PLATE AT MULTIPLE AREAS AROUND FASTENER HOLES, BS 887 - 907, RBL 21, WL 168. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. FABRICATED A REPAIR IAW SRM 53-00-53-2R-5, EA M-22-153=01550, AND SRM SDR SWAA2022123078432Shield · corrodedCORROSION ON THE AFT CARGO BAY RT SHIELD FWD OF CARGO DOOR AT MULTIPLE AREAS AROUND FASTENER HOLES, BS 767 - 794, RBL 22, WL 156. FOUND TO BE OUT OF LIMITS. REMOVED THE SHIELD IAW SRM 51-40-02-0G-0. LOCATED, DRILLED, AND DEBURRED A NEW SHIELD IAW SRM 51-4SDR SWAA2022123078433Attach Angle · corrodedCORROSION ON THE AFT CARGO ATTACH ANGLE UNDER SHIELD AT MULTIPLE AREAS UNDER NUT PLATES BS 767 - 787, RBL 21, WL 156. FOUND TO BE OUT OF LIMITS. REMOVED THE ATTACH ANGLE IAW SRM 51-40-02-0G-0. LOCATED, DRILLED, DEBURRED, AND INSTALLED NUT PLATES TO THE SDR SWAA2022123078434Support · corrodedCORROSION ON THE AFT CARGO RT FLOOR TO SIDEWALL SUPPORT PLATE AT MULTIPLE AREAS AROUND FASTENER HOLES BS 727E - 767, RBL 22, WL 156. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. REMOVED THE FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-02-0G-0. LOCATED AND SDR SWAA2022123078436Support · corrodedCORROSION ON AFT CARGO BAY LT FLOOR TO SIDE WALL SUPPORT PLATE AROUND MULTIPLE FASTENER HOLES BS 727D - 847, LBL 22, WL 156. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. REMOVED THE DAMAGED FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-02-0G-0. LOCATED AND SDR SWAA2022123078437Strap · corrodedCORROSION AFT CARGO BAY FLOOR SPLICE STRAP BS 767+6, RBL 3, WL 156, AROUND FASTENER HOLES. CORROSION FOUND TO BE OUT OF LIMITS. A NEW AFT CARGO BAY FLOOR SPLICE STRAP WILL BE INSTALLED ON CARD TTG8Q00FEJCV.SDR SWAA2022123077921Skin · delaminatedLEFT WING OTBD AFT FLAP LOWER SKIN WAS DELAMINATED AT AFT I/B CORNER. FOUND TO BE OUT OF LIMITS IAW SRM 57-53-01-1A-2, PARA 4 A 9. FIG 102. REMOVED AND REPLACED THE FLAP IAW AMM 27-51-22-000-801, STEPS 2D, AND AMM 27-51-22-400-801, STEPS 3.SDR SWAA2022123077922Skin · delaminatedLEFT WING INBD MAIN FLAP T/E WEDGE LOWER SKIN HAS AREA OF DELAMINATION. FOUND DAMAGE TO BE OUT OF LIMITS IAW SRM 57-53-01-1A-1, PARA 4 A 7, AND FIG 102. REMOVED AREA OF DELAMINATED SKIN IAW SRM 51-70-10-2R-0, PARA, 6 & 7. REMOVED AND REPLACED THE WEDGE SDR SWAA2022123077452Attach Angle · crackedLEFT BS 663 UPPER ATTACH ANGLE IS CRACKED ON VAPOR BARRIER LBL 8 WL 167.68. INSTALLED A REPAIR IAW SRM 57-10-10-2R-5.SDR SWAA2022123077453Attach Angle · crackedRIGHT BS 663 UPPER ATTACH ANGLE IS CRACKED ON VAPOR BARRIER RBL 8, WL 167.68. REMOVED DAMAGED SECTION OF ATTACH ANGLE IAW SRM 57-10-10-2R-5. INSTALLED A REPAIR IAW SRM 57-10-10-2R-5.SDR SWAA2022060815283Girt Bar · stuckSERVICE DOOR GIRT BAR STUCK / [01] STRAIGHTENED GIRT BAR HOOK PER SIP.SDR SWAA2021062886336Lamp · inoperativeEXTERIOR EMERGENCY LIGHT INOPERATIVE AT L2 DOOR. RELAMPED PER AMM 33-51-04. OPS. OK.SDR SWAA2021032356944Stringer · crackedFIXED LEADING EDGE STRINGER #1 L/H AT WS 206-WS 227 IS CRACKED. /SDR SWAA2021032356943Rib · crackedFIXED LEADING EDGE RIB AT WS227 IS CRACKED /SDR SWAA2021032356947Closeout Panel · chafedINBD LEADING EDGE SKIN ASSY CLOSEOUT PANEL IS CHAFFED /SDR SWAA2021071317463Skin · delaminatedLEFT WING O/B AFT FLAP IS DELAMED AT 1/B AFT CORNER; 11' X 10.5' / REMOVED & REPLACED LEFT WING O/B AFT FLAP FAW AMM 27-51-22.POS L/H O/B P/N OFF 113A3700-23 S/N OFF 002961 P/N ON 113A3700-19 S/N ON 001398AMT 135306
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