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.

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)Dec 15, 2024 · N8514F · Boeing 7378H4 · Fuselage Floor PanelSDR 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)Dec 15, 2024 · N8514F · Boeing 7378H4 · Fuselage Floor PanelSDR 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)Dec 15, 2024 · N8514F · Boeing 7378H4 · Fuselage Floor PanelSDR 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)Dec 15, 2024 · N8514F · Boeing 7378H4 · Fuselage Floor PanelSDR 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)Dec 15, 2024 · N8514F · Boeing 7378H4 · Fuselage Floor PanelSDR 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)Dec 15, 2024 · N8514F · Boeing 7378H4 · Fuselage Floor PanelSDR 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 INSPECTIONDec 15, 2024 · N8514F · Boeing 7378H4 · Fuselage Floor PanelSDR 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)Dec 15, 2024 · N8514F · Boeing 7378H4 · Fuselage Floor PanelSDR 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] LOCADec 14, 2024 · N8514F · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR 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] INSPDec 14, 2024 · N8514F · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR 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 REFERENCDec 14, 2024 · N8514F · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR 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 51-40-02Dec 14, 2024 · N8514F · Boeing 7378H4 · Fuselage, Equipment Attach FittingsSDR 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.Dec 14, 2024 · N8514F · Boeing 7378H4 · Fuselage, Seat/Cargo Attach FittingsSDR 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 SDec 14, 2024 · N8514F · Boeing 7378H4 · Fuselage Main, Attach FittingsSDR 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 THICDec 13, 2024 · N8514F · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR 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] LOCADec 13, 2024 · N8514F · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR 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 IDec 13, 2024 · N8514F · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR 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 CODec 13, 2024 · N8514F · Boeing 7378H4 · Fuselage Main, Floor BeamSDR 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>EVALUDec 13, 2024 · N8514F · Boeing 7378H4 · Fuselage Main, Floor BeamSDR 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 FDec 13, 2024 · N8514F · Boeing 7378H4 · Fuselage Main, Floor BeamSDR 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-Dec 11, 2024 · N8514F · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR 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 33-51-06Nov 20, 2024 · N8514F · Boeing 7378H4 · Emergency LightingSDR SWAA2024111960803Flashlight · inoperativeFWD INBD JUMPSEAT FLASHLIGHT INOP.<[01] REMOVED AND REPLACED FWD INBD JUMP SEAT FLASHLIGHT BATTERY REF B737 AMM 25-64-00 OP/C GOODNov 16, 2024 · N8514F · Boeing 7378H4 · Emergency EquipmentSDR 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.May 5, 2024 · N8514F · Boeing 7378H4 · Emergency EquipmentSDR 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 SPDec 20, 2023 · N8514F · Boeing 7378H4 · Horizontal Stabilizer, Spar/RibSDR SWAA2023081789657Seal · crackedLT HORIZONTAL UPPER FRONT SLIDING SEAL IS CRACKED.<[01] R+R SLIDING SEAL REF AMM 53-31-31Aug 15, 2023 · N8514F · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous StructureSDR 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 Mar 14, 2023 · N8514F · Boeing 7378H4 · Trailing Edge Flap Control SystemSDR 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.Dec 20, 2022 · N8514F · Boeing 7378H4 · Emergency LightingSDR 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.Dec 20, 2022 · N8514F · Boeing 7378H4 · Emergency LightingSDR 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 REGDec 7, 2022 · N8514F · Boeing 7378H4 · Trailing Edge FlapsSDR 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.Dec 6, 2022 · N8514F · Boeing 7378H4 · Wing Miscellaneous StructureSDR 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-Dec 5, 2022 · N8514F · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR 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 EADec 5, 2022 · N8514F · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR 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.Dec 5, 2022 · N8514F · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR 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 Dec 4, 2022 · N8514F · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR 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 51-4Dec 4, 2022 · N8514F · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR 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 Dec 4, 2022 · N8514F · Boeing 7378H4 · Fuselage Main, Attach FittingsSDR 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 Dec 4, 2022 · N8514F · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR 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 Dec 4, 2022 · N8514F · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR 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.Dec 4, 2022 · N8514F · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR 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.Dec 3, 2022 · N8514F · Boeing 7378H4 · Trailing Edge FlapsSDR 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 Dec 3, 2022 · N8514F · Boeing 7378H4 · Trailing Edge FlapsSDR 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.Dec 1, 2022 · N8514F · Boeing 7378H4 · Fuselage Main, BulkheadSDR 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.Dec 1, 2022 · N8514F · Boeing 7378H4 · Fuselage Main, BulkheadSDR SWAA2022060815283Girt Bar · stuckSERVICE DOOR GIRT BAR STUCK / [01] STRAIGHTENED GIRT BAR HOOK PER SIP.Jun 4, 2022 · N8514F · Boeing 7378H4 · Escape SlideSDR SWAA2021062886336Lamp · inoperativeEXTERIOR EMERGENCY LIGHT INOPERATIVE AT L2 DOOR. RELAMPED PER AMM 33-51-04. OPS. OK.Jun 22, 2021 · N8514F · Boeing 7378H4 · Emergency LightingSDR SWAA2021032356944Stringer · crackedFIXED LEADING EDGE STRINGER #1 L/H AT WS 206-WS 227 IS CRACKED. /Mar 19, 2021 · N8514F · Boeing 7378H4 · Wing, Longeron/StringerSDR SWAA2021032356943Rib · crackedFIXED LEADING EDGE RIB AT WS227 IS CRACKED /Mar 19, 2021 · N8514F · Boeing 7378H4 · Wing, Rib/BulkheadSDR SWAA2021032356947Closeout Panel · chafedINBD LEADING EDGE SKIN ASSY CLOSEOUT PANEL IS CHAFFED /Mar 19, 2021 · N8514F · Boeing 7378H4 · Wing, Plate/SkinSDR 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 135306Sep 22, 2020 · N8514F · Boeing 7378H4 · Trailing Edge Flaps
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