Service difficulty reports

1,771,154 reports of malfunctions and defects, newest first. Air carriers must report; general aviation reporting is voluntary.

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'
  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 REXA2026082601728Stringer · corrodedCORROSION ON STGR=21R BTW FS=364 TO FS=379 AT FWD E/E COMPARTMENT. CORROSION ON STGR=21R BTW FS=364 TO FS=379 AT FWD E/E COMPARTMENT WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-00-00-101-001-A01 AND WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND CRJ90Jun 18, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2026082601727Bracket · corrodedCORROSION ON BLOCK CLAMP SUPPORT BTW FS=295 TO 310, STGR=25R AT E/E COMPARTMENT. CORROSION ON BLOCK CLAMP SUPPORT BTW FS=295 TO 310, STGR=25R AT E/E COMPARTMENT WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 51-10-06-001-001-A01 AND WAS REPLACED PER CRJ900 SRM 51-Jun 18, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026082601726Stringer · corrodedCORROSION ON STGR=26R FS=295 TO FS=310, STGRV25R FS=319 TO FS=333, AT FWD E/E COMPARTMENT. STGR=26R FS=295 TO FS=310, STGR=25R FS=319 TO FS=333, AT FWD E/E COMPARTMENT WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 51-10-06-001-001-A01 AND WERE REPLACE PER CRJ90Jun 18, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2026082601725Stringer · corrodedCORROSION ON STGR=26R FS=295 TO FS=310, STGRV25R FS=319 TO FS=333, AT FWD E/E COMPARTMENT. STGR=26R FS=295 TO FS=310, STGR=25R FS=319 TO FS=333, AT FWD E/E COMPARTMENT WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 51-10-06-001-001-A01 AND WERE REPLACE PER CRJ90Jun 18, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2026082601693Floor Support · corrodedCORROSION ON LONGITUDINAL BEAMS (3E/A) FROM FS1000 TO FS1069 ON LBL27, LBL09 AND RBL09 AT AFT BAGGAGE COMPARTMENT CORROSION ON LONGITUDINAL BEAMS (3E/A) FROM FS1000 TO FS1069 ON LBL27, LBL09 AND RBL09 AT AFT BAGGAGE COMPARTMENT WERE EVALUATED OUT OF LIMITS PERJun 18, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026082601692Floor Support · corrodedCORROSION ON LONGITUDINAL BEAMS (3E/A) FROM FS1000 TO FS1069 ON LBL27, LBL09 AND RBL09 AT AFT BAGGAGE COMPARTMENT CORROSION ON LONGITUDINAL BEAMS (3E/A) FROM FS1000 TO FS1069 ON LBL27, LBL09 AND RBL09 AT AFT BAGGAGE COMPARTMENT WERE EVALUATED OUT OF LIMITS PERJun 18, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026082601691Floor Support · corrodedCORROSION ON LONGITUDINAL BEAMS (3E/A) FROM FS1000 TO FS1069 ON LBL27, LBL09 AND RBL09 AT AFT BAGGAGE COMPARTMENT CORROSION ON LONGITUDINAL BEAMS (3E/A) FROM FS1000 TO FS1069 ON LBL27, LBL09 AND RBL09 AT AFT BAGGAGE COMPARTMENT WERE EVALUATED OUT OF LIMITS PERJun 18, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026082601690Stringer · corrodedCORROSION ON STGR=20R, FS=295 TO FS=319, FS=349 TO FS=370 AND FS=445 AT FWD E/E CORROSION ON STGR=20R, FS=295 TO FS=319, FS=349 TO FS=370 AND FS=445 AT FWD E/E WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 51-10-06-001-001-A01, THEREFORE STRINGER 20R BTW FS280 TJun 18, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2026082601689Stringer · corrodedCORROSION ON STGR=20R, FS=295 TO FS=319, FS=349 TO FS=370 AND FS=445 AT FWD E/E CORROSION ON STGR=20R, FS=295 TO FS=319, FS=349 TO FS=370 AND FS=445 AT FWD E/E WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 51-10-06-001-001-A01, THEREFORE STRINGER 20R BTW FS280 TJun 18, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2026082601688Stringer · corrodedCORROSION ON STRINGER 19R BWT FS597 TO FS613 AT FWD BAGGAGE COMPARTMENT. CORROSION ON STRINGER 19R BWT FS597 TO FS613 AT FWD BAGGAGE COMPARTMENT WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 51-10-06-001-001-A01 AND WAS REPAIRED PER CRJ900 SRM 53-00-03-201-001-AJun 18, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2026082601683Fitting · corrodedCORROSION FLOOR FITTING IN AFT ACCESS 205 OUT SIDE (1EA) ON GALLEY 2. SUMMARY OF NRC 00244: FLOOR FITTING IN AFT ACCESS 205 OUT SIDE (1EA) ON GALLEY 2 WAS REPLACED PER SAFRAN CMM 25-32-84 REV 9 DATE JUN 06/24Jun 18, 2026 · N926XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026082601674Seat Track · corroded"CORROSION & WEAR ON FLOOR SEAT TRACK BTW FS927.00 TO BS 977 AND LBL 27 FLOOR SEAT TRACK BTW FS927.00 TO FS977.00 AND LBL 27' WAS REPLACED PER CRJ-900 AMM 53-00-49."Jun 18, 2026 · N926XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2026082601673Seat Track · corrodedCORROSION & WEAR ON FLOOR SEAT TRACKS (3 EAS), BTW FS847.00 TO FS977.00AND RBL 9''. FLOOR SEAT TRACKS (3 EAS), BTW FS847.00 TO FS977.00 AND RBL 9'' WERE REPLACED PER CRJ-900 AMM 53-00-49Jun 18, 2026 · N926XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2026082601672Seat Track · corrodedCORROSION & WEAR ON FLOOR SEAT TRACKS (3 EAS), BTW FS847.00 TO FS977.00AND LBL 9'' FLOOR SEAT TRACKS (3 EAS), BTW FS847.00 TO FS977.00AND LBL 9'' WERE REPLACED PER CRJ-900 AMM 53-00-49.Jun 18, 2026 · N926XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026081327919Inlet · corroded*** SUPPLEMENTAL SDR *** HORZ STAB COMPT. APU INLET SURROUND STRUCTURE ANGLE IS CORRODED BETWN STA. 1787.45 TO 1825 STGR S-6R (059-07) ATA: 53-80 SKILL: STR APU INLET SURROUNDIN STRUCTURE FROM STA 1787.45-1825 WILL BE REPAIR ON LINE # 711 T3F18E0090LLM. NO FUTJun 18, 2026 · N429UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR REXA2026073001334Web · corrodedCORROSION ON WEB FLOOR PROTECTOR (4EAS) AT SERVICE DOOR SURROUND STRUCTURE CORROSION ON WEB FLOOR PROTECTOR (4EAS) AT SERVICE DOOR SURROUND STRUCTURE WAS REMOVED AND EVALUATED OUT OF LIMITS PER CRJ900 SRM 51-21-06-001-001-A01 AND CRJ-900 SRM 53-00-00-101-001-Jun 18, 2026 · N925XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026073001333Bracket · corrodedCORROSION ON WEB FLOOR PROTECTOR (4EAS) AT SERVICE DOOR SURROUND STRUCTURE CORROSION ON WEB FLOOR PROTECTOR (4EAS) AT SERVICE DOOR SURROUND STRUCTURE WAS REMOVED AND EVALUATED OUT OF LIMITS PER CRJ900 SRM 51-21-06-001-001-A01 AND CRJ-900 SRM 53-00-00-101-001-Jun 18, 2026 · N925XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026073001332Protector · corrodedCORROSION ON WEB FLOOR PROTECTOR (4EAS) AT SERVICE DOOR SURROUND STRUCTURE CORROSION ON WEB FLOOR PROTECTOR (4EAS) AT SERVICE DOOR SURROUND STRUCTURE WAS REMOVED AND EVALUATED OUT OF LIMITS PER CRJ900 SRM 51-21-06-001-001-A01 AND CRJ-900 SRM 53-00-00-101-001-Jun 18, 2026 · N925XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026073001331Bracket · corrodedCORROSION ON WEB FLOOR PROTECTOR (4EAS) AT SERVICE DOOR SURROUND STRUCTURE CORROSION ON WEB FLOOR PROTECTOR (4EAS) AT SERVICE DOOR SURROUND STRUCTURE WAS REMOVED AND EVALUATED OUT OF LIMITS PER CRJ900 SRM 51-21-06-001-001-A01 AND CRJ-900 SRM 53-00-00-101-001-Jun 18, 2026 · N925XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR SWAA2026072811416Strap · corrodedCORROSION ON LOWER ATTACH STRAP LOCATED AT OSS 422 LEADING EDGE AT RH WING. PERFORMED REPAIR CATEGORY A ON LOWER ATTACH STRAP LOCATED AT OSS 422 LEADING EDGE AT RH WING IAW EA 26-157-01723.Jun 18, 2026 · N8649A · Boeing 7378H4 · Wing Miscellaneous StructureSDR SWAA2026072850933Panel · crackedRIGHT WING TRAILING EDGE PANEL 661BB HAS CRACKS AROUND FASTENER HOLES. REPAIRED R/H WING TAILING EDGE PANEL 661BB IAW B737-700 SRM 57-51-01-2R-1 REPAIR 1 AND 51-70-05-2R-6 REPAIR 6 AND 51-70-05-2R-0Jun 18, 2026 · N494WN · Boeing 7377H4 · Wing, Plate/SkinSDR SWAA2026072865570Panel · crackedRIGHT WING T/E PANEL 661AB HAD CRACKS AROUND FASTENER HOLES. REPAIRED IAW SRM 57-51-01-2R-1-A01282, REPAIR 1.Jun 18, 2026 · N494WN · Boeing 7377H4 · Wing Main, Frame StructureSDR SWAA2026072851106Panel · crackedRIGHT WING TRAILING EDGE PANEL 661CB HAS CRACKS AROUND FASTENER HOLES. REPAIRED RT WING T/E PANEL 661CB IAW SRM 57-51-01-2R-1 & 51-70-05-2R-0. INSPECTED PER [SRM 57-51-01-2R-1-A01282 (REPAIR 1 - WING FIXED TRAILING EDGE SKIN PANELS MADE OF COMPOSITE MATERIAJun 18, 2026 · N494WN · Boeing 7377H4 · Wing Miscellaneous StructureSDR VNAA202607280016Fitting · corrodedCORROSION FLOOR FITTING IN CONTAINER UNDER WASTE CONTAINER ON FWD LAV (1EA). FLOOR FITTING IN CONTAINER UNDER WASTE CONTAINER ON FWD LAV (1EA) WAS REMOVED PER CMM 25-40-40 ,FABRICATED AND INSTALLED PER EA NO:2542-2026-0770 REV.-- DATE 2026-07-03Jun 18, 2026 · N552NN · Cndair CL6002D24 · Fuselage, Equipment Attach FittingsSDR SWAA2026072435525Support Angle · crackedCRACKED SUPPORT ANGLE LOCATED FWD FACE BS 695 BL 0 WL 208.1 RT SIDE AT PASSENGER CABIN. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02 AND DWG 273A9111 SHEET 10 REV -.Jun 18, 2026 · N8650F · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026072458657Web · crackedCRACKED WEB, BTW BS 927 - 947.5, STR 24R - 25R. REPLACED THE WEB IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 147A7500, SHEET 37, REV-.Jun 18, 2026 · N8650F · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026072474376Web · crackedCRACKED WEB, BTWN BS 312 - 328, LBL 47.5, WL 208.1. REPLACED THE WEB IAW SRM 51-40-02, AND DWG 141A5400, SHEET 26, REV-.Jun 18, 2026 · N8650F · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026072493596Floor Support · corrodedCORRODED FLOOR SUPPORT BTWN BS 312 - 328, LBL 12, WL 208.1. REPLACED THE INTERCOSTAL AND FASTENERS IAW SRM 51-40-02, AND DWG 141A5400, SHEET 27, REV -.Jun 18, 2026 · N8650F · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR HNAA2026072400626Floor Support · crackedONE LT OMEGA BEAM GUSSET AT FR 28 HAS A CRACK. REMOVED AND REPLACED LH OMEGA BEAM GUSSET AT FR 28 PER EMB 145 SRM 51-40-08-PR.Jun 18, 2026 · N931AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026072400625Access Panel · crackedAPU COWLING ACCESS PANEL CRACKED ON THE INTERIOR SIDE NEAR THE HINGE. REMOVED AND REPLACED APU COWLING ACCESS PANEL PER EMB 145 SRM 51-20-03 STEP 3Jun 18, 2026 · N931AE · Emb EMB145LR · APU Cowling/ContainmentSDR HNAA2026072400624Support Bracket · crackedFWD CARGO DOOR MECHANISM SUPPORT BRACKET CRACKED ON BOTTOM LEG. REMOVED AND REPLACED WITH NEW FWD CARGO DOOR MECHANISM SUPPORT BRACKET IAW EMB 145 SRM 51-40-02-PR.Jun 18, 2026 · N931AE · Emb EMB145LR · Cargo/Baggage DoorsSDR HNAA2026072400623Floor Support · crackedONE LT OMEGA BEAM AT FR 23 HAS A CRACKED. COMPLIED WITH PERMANENT REINFORCING REPAIR OF THE LT OMEGA BEAM AT FRAME 23 SPLICE IAW ETD2026-145-010691 REV. AND PIEDMONT EO1-53-26-0291.Jun 18, 2026 · N931AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026072400622Panel · crackedPANEL 191ZB RT LEADING EDGE NR 1 STRAP ASSY ( HORSE COLLAR) IS CRACKED AT THE UPPER RADIUS BY FIRST FASTENER HOLE. COMPLIED WITH REPAIR TO THE RT WING-TO -FUSELAGE FAIRING PANEL 191ZB JOIN STRAP PER EMB 145 ETD2026-145-012463 REV.: / AND PIEDMONT EO1-05-26-03Jun 18, 2026 · N931AE · Emb EMB145LR · Aerodynamic FairingsSDR HNAA2026072400611Gusset · corrodedONE LT FLOOR GUSSET AT FR 59 HAS CORROSION. REMOVED AND REPLACED LT FLOOR GUSSET FROM FR 59 TO FR 61 PER SRM 51-40-02, STEP 2 C, AND 3 BJun 18, 2026 · N931AE · Emb EMB145LR · Fuselage Main, StructureSDR HNAA2026072400610Floor Support · corrodedRIGHT OTBD FLOOR SILL FROM FR 25 TO FR 28 HAS CORROSION. REMOVED AND REPLACED RT OTBD FLOOR SILL FROM FR 23 - FR 29 PER EMB 145 SRM 51-40-02-PRJun 18, 2026 · N931AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026072400609Floor Support · corrodedLEFT OTBD FLOOR SILL FROM FR 24 TO FR 29 HAS CORROSION. REMOVED AND REPLACED THE LT OTBD FLOOR SILL FROM FR24 - FR29 PER EMB 145 SRM 51-40-02-PR.Jun 18, 2026 · N931AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026072400608Floor Support · corrodedLEFT OTB FLOOR SILL FROM FR 20 TO FR 22 HAS CORROSION. REMOVED AND REPLACED WITH NEW LT OTBD FLOOR SILL FROM FR 20 TO FR 22 IAW EMB 145 SRM 51-40-02 STEP 2 B, C AND 4BJun 18, 2026 · N931AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026072400607Floorbeam · corrodedLH FLOOR CROSSBEAM AT FR 18 HAS CORROSION. REMOVED AND REPLACED WITH NEW LH FLOOR CROSSBEAM AT FR 18 IAW EMB 145 SRM 51-40-02-PR.Jun 18, 2026 · N931AE · Emb EMB145LR · Fuselage Main, Floor BeamSDR HNAA2026072400606Door Frame · corrodedSERVICE DOOR CUTOUT LOWER SURROUND STRUCTURE AT FR 21 HAS CORROSION. REMOVED AND REPLACED WITH NEW SERVICE DOOR CUTOUT LOWER SURROUND STRUCTURE AT FR 21 IAW EMB 145 SRM 51-40-02-PRJun 18, 2026 · N931AE · Emb EMB145LR · Fuselage Main, StructureSDR HNAA2026072400605Gusset · corrodedRIGHT FLOOR GUSSET AT FR 22 HAS CORROSION. REMOVED RH FLOOR GUSSET AT FR 22.AND INSTALLED NEW GUSSET AT FR 22 PER EMB 145 SRM 51-40-02-PRJun 18, 2026 · N931AE · Emb EMB145LR · Fuselage Main, StructureSDR HNAA2026072400603Floor Support · corroded00148 1EA RH OB FLOOR SILL AT FR 20 HAS CORROSION. REMOVED AND REPLACED WITH NEW RH OB FLOOR SILL AT FR 20 IAW EMB 145 SRM 51-40-02-PR.Jun 18, 2026 · N931AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026072400602Paint · flakingPANEL 191HL HAS CORROSION UNDER PAINT AND PAINT IS FLAKING OFF. REMOVED CORROSION FOUND ON PANEL 191HL, LOWEST REMAINING THICKNESS FOUND TO BE AT .06995 PARTS FOUND TO BE WITHIN LIMITS PER EMB 145 SRM 51-10-05.Jun 18, 2026 · N931AE · Emb EMB145LR · Fuselage Main, StructureSDR SWAA2026072202988Plate · deterioratedDETERIORATED SEAL - PLATE ACCESS PANEL 343AB AT RT HORIZONTAL STAB (2 EA). REPLACED SEAL - PLATE ACCESS PANEL 343AB AT RT HORIZONTAL STAB (2 EA) IAW SRM 51-40-02 AND DWG 186A3101-48, SHEET 3, REV A.Jun 18, 2026 · N8650F · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2026072159781Attach Angle · crackedDURING HOLE PROBE INSPECTION OF STA 663 VAPOR BARRIER FOUND A CRACK AT A FASTENER HOLE LOCATION LBL 31.5" (JUST INBD OF EXPANSION JOINT/SEAL IN VAPOR BARRIER) REPAIRED VAPOR BARRIER ATTACH ANGLE PER EA M26-157-01480 .Jun 18, 2026 · N8542Z · Boeing 7378H4 · Fuselage Main, Attach FittingsSDR SWAA2026072125817Attach Angle · crackedDURING HOLE PROBE INSPECTION OF BS 663 VAPOR BARRIER FOUND A CRACK AT A FASTENER HOLE LOCATION RBL 31.5, (JUST INBD OF EXPANSION JOINT/SEAL IN VAPOR BARRIER) REPAIRED VAPOR BARRIER ATTACH ANGLE IAW EA M-26-157-01481.Jun 18, 2026 · N8542Z · Boeing 7378H4 · Fuselage Main, Attach FittingsSDR IPXA2026071737767Bracket · brokenIAW TASK CARD T3F18E004V6MO LINE 267 STEP 10, LEFT STRUT STA 149.5 BRACKET WAS INSPECTED AND FOUND BROKEN, FLL-050, INSTALLED FRAME ANGLE AT #1 PYLON UPPER SIDE IAW B757-200PF SRM 51-40-02-0G-0Jun 18, 2026 · N418UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR SWAA2026071744349Rib · crackedCRACKED RIB, LE STA 105.26 ACCESS PANEL 331B AT LT HORIZONTAL STAB. REPLACED RIB AND FASTENERS LOCATED LE STA 105.26 ACCESS PANEL 331B AT LT HORIZONTAL STAB IAW SRM 51-40-02, DWG 186A1304, SHEET 1, REV A AND DWG 186A1001, SHEET 19, REV-.Jun 18, 2026 · N930WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/RibSDR SWAA2026071723575Intercostal · corrodedCORROSION ON WEB INTERCOSTAL UPPER SILL LOCATED BS 827 PLUS 2.5 INCH AT LEVEL S-18R AND WL 200 AFT CARGO BAY. REPLACED WEB INTERCOSTAL UPPER SILL LOCATED BS 827 PLUS 2.5 INCH AT LEVEL S-18R AND WL 200 AFT CARGO BAY IAW SRM 51-10-02, ITEM 9, AND DWG 146A8310, SJun 18, 2026 · N930WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026071773371Angle · corrodedCORROSION ON ANGLE UPPER SILL LOCATED BS 827 PLUS 2.5 INCH AT LEVEL S-18R AND WL 200 AFT CARGO BAY. REPLACED ANGLE UPPER SILL AND FASTENERS LOCATED BS 827 PLUS 2.5 INCH AT LEVEL S-18R AND WL 200 AFT CARGO COMPARTMENT IAW SRM 51-40-02 AND DWG 146A8310 SHEET 16 Jun 18, 2026 · N930WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026071747971Seal Bracket · crackedCRACKED SEAL PLATE, ACCESS PANEL 333AB ON LT HORIZONTAL STAB (2 EA). REPLACED PLATE ACCESS PANEL 333AB AT LT HORIZONTAL STAB IAW SRM 51-10-02, ITEM 9, SRM 51-40-02.Jun 18, 2026 · N930WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure