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 19MA20260707001A/C Pack · overheatedCABIN PACK OVERHEAT CAS MESSAGE ACCOMPANIED WITH AN ASSOCIATED SLOW DEPRESSURIZATION OF THE CABIN; EMERGENCY DECENT PROCEDURE WAS PERFORMED WITH CABIN ALTITUDE OVER 14,000 FEET. MESSAGE DISAPPEARED ABOUT 5 MINUTES AFTER AND AIRFLOW REESTABLISHED; CABIN ALTITUDJul 6, 2026 · N975JS · Cessna 750 · Cabin Pressure Control SystemSDR AALA202607072190Relay · faultedAIRCRAFT WAS GROUNDED: LEFT CENTER TANK LOW PRESSURE LIGHT ILLUMINATED AND STAYED ON. PERFORMED T/S IAW FIM 28-22-00-810-822. FOUND THREE LIGHTS FLASHING SIMULTANEOUSLY ON UFI. MAINTENANCE REPLACED RELAY R54 IAW WDM 28-23-11. OPS CHECK OF LH CENTER PUMP NORMALJul 6, 2026 · N906AN · Boeing 737823 · Fuel Indicating SystemSDR AALA202607076110Door Latch · jammedAIRCRAFT WAS NOT GROUNDED: MDCR DOOR JAMMED LOCK IS BROKEN OR OBSTRUCTED NOT ALLOWING IT TO OPEN. ADJUSTED MDCR DOOR LATCH IAW AMM 25-29-01.Jul 6, 2026 · N778AN · Boeing 777223 · Fixed Inner DoorsSDR AALA202607073455Mount Bracket · inoperativeAIRCRAFT WAS NOT GROUNDED: AFT LEFT FA FLASHLIGHT TEST BUTTON INOP. MAINTENANCE REPLACED AFT LEFT FA FLASHLIGHT BRACKET IAW AMM 25-64-00.Jul 6, 2026 · N314UT · Boeing 7378 · Emergency EquipmentSDR AALA202607077476Girt Bar · misinstalledAIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT SAYS FABRIC STICKING OUT OF MAIN CABIN ENTRY DOOR IN THE WAY OF THE GIRT BAR. MAINTENANCE FOUND GIRT MATERIAL NOT HAVING A Z FOLD. REMOVED SLIDE ASSY AND RII ACCOMPLISHED FOR L1 SLIDE PROPERLY FOLDED GIRT. RE-INSTALLJul 6, 2026 · N928NN · Boeing 737823 · Emergency EquipmentSDR YENA2026070700516Unknown · odorFLT # 1468, PBI-HPN. LEVEL 2 FUME EVENT. STRONG PERSISTENT MAGIC MARKER SMELL DESCENDING THROUGH12,000; CLOUDS AND PRECIPITATION IN THE AREA. SMELLED BY BOTH PILOTS, BUT NO F/A. SUSPECT PACK 1. SHUT OFF PACK 1 AND CLOSED X BLEED. SMELL GOT WEAKER AFTER SEVERALJul 6, 2026 · N623JB · Airbus A320232 · Air Distribution SystemSDR SIMA20260706001Light · inoperativeFWD CORNER EMERGENCY PHOTOLUMINESCENT STRIP WORN OUT DOES NOT ILLUMINATE. MEL 33-32 AUTH 070248-C. .RAR PHOTOLUMINESCENT STRIPS AT RH PAX CABIN THRESHOLD ZONE 226 IAW AMM 33-50-21. NO DEFECTS NOTED. MEL RESTORED.Jul 6, 2026 · N285NN · Emb ERJ170200LR · Emergency LightingSDR SIMA20260706002Engine · faultedENG1 BACKFIRED DURING THRUST REVERSER DEPLOYMENT ON REJECT TWICE. FA AND PASSENGER SMELLED SOMETHING BURNING.RECEIVED 967 ITT ON T/O ROLL REJECTED. THEN ENG EXCEEDANCE DISPLAYED. RAN QRH MESSAGE PERSISTED. ENGINE 1 BACKFIRED TWICE DURING THE REJECTED TAKEOFF. Jul 6, 2026 · N205NN · Emb ERJ170200LR · Engine (Turbine/Turboprop)SDR SIMA20260706003Door · no discrepancyGATE AGENT REPORTS L1 DOOR DIFFICULT TO OPEN FROM OUTSIDE. MAIN HANDLE REQUIRED EXCESSIVE FORCE TO OPERATE. PERFORRMED OPC OF FWD PASSENGER DOOR IAW EMB 170 GHC OPC GOOD NO FAULTS FOUND.Jul 6, 2026 · N781EJ · Emb ERJ170100SU · Passenger/Crew DoorsSDR HNAA2026070700579Control Unit · faultedDURING CLIMB FLAP FAIL AT 0DEG 3MINS AFTER BEING STOWED, ON CLIMB SELECTED FLAP 9 TO 0 AND FLAPS STOWED AT 3,000FT. APPROX 3MINS LATER AT 8,000FT FLAP FAILED. FLAP RT TRANSMISSION FAILED CMC MSGS, 1 OCCURANCE. CMC RT TRANSMISSION FAIL. T/S IAW FIM 27-51-00-8Jul 6, 2026 · N649PP · Emb EMB145LR · Trailing Edge Flap ActuatorSDR 2026FA0000567Oxygen Mask · faultedTHE CREW REPORTS THE OXYGEN MASC CONTINUOUSLY FLOW OF OXYGEN AT 100 % FLOW, ATTEMPTEN TO STOP FLOW WITHOUT SUCCESS MASC WAS DISCONNECTED O2 FLOW STOPPED.MAINTENANCE REPLACED THE MASK WITH OVERHUALED UNITJul 6, 2026 · N325GH · Cessna 525A · Crew Oxygen SystemSDR ASAA2026070667162Skin · crackedLEFT HORIZONTAL STAB LOWER SKIN IS CRACKED AT THE INBD SIDE OF RIB, STAB STA 166.30 NEAR DRAIN HOLE. GROUNDED - YES. REPAIRED LT HORIZONTAL STABILIZER LOWER SKIN IAW SRM 55-10-01-2R-11.Jul 6, 2026 · N533AS · Boeing 737890 · Horizontal Stabilizer, Plate/SkinSDR 2026F00140Stringer · corrodedFOUND EVIDENCE OF CORROSION ON THE APU STINGER ASSY, LOWER AREA, AFT OF PANEL 330BBC. MECHANICALLY REMOVED SEVERAL AREAS OF CORROSION LOCATED ON APU STINGER, LOWER SKIN EDGE JUST FWD OF ACCESS PANEL 330BBC. FOUND CORROSION BLENDS TO BE BEYOND LIMITS IAW CESSNAJul 6, 2026 · N622QS · Cessna 680A · Fuselage Main, Longeron/StringerSDR DALA2026070603926Sign · brokenEXIT SIGN AT 3L DOOR BROKEN. REPAIRED EXIT SIGN, OPS CHECKED OK. (LP 8735843 - AIRCRAFT WAS GROUNDED)Jul 6, 2026 · N423DX · Airbus A330941 · Emergency LightingSDR DALA2026070603925Cover · detachedDURING TAKEOFF THE EXIT COVER SIGN FELL OFF. TRIED PUTTING BACK ON, BUT WOULDNT STAY BC TWO OF THE TABS APPEAR TO BE BROKEN OFF. COVER RE-SECURED NO TROUBLE FOUND. (LP 1684058 - AIRCRAFT WAS GROUNDED)Jul 6, 2026 · N418DX · Airbus A330941 · Emergency LightingSDR JJBA20260706003Charger · inoperativeENTRANCE OVERHEAD EMERGENCY LIGHT INOPERATIVE. TEMP INSTALLED SERVICEABLE LAMP AND SERVICEABLE BATTER POWER SUPPLY (POSITION 1). NO FIX. SUSPECT BAD HOUSING OR WIRING ISSUE. AIRCRAFT RETURNED TO ORIGINAL CONFIGURATION. REMOVED AND REPLACED #1 BATTERY CHARGER. Jul 6, 2026 · N11191 · Emb EMB145XR · Emergency LightingSDR YENA2026070600511Warning Message · illuminatedFLT # 1524, LAX-JFK. (ETOPS) "AIR BLEED CLASS 2 MSG ON STATUS (CLASS II MAINTENANCE MESSAGES DISPLAYED ON ECAM STATUS PAGE OF ECAM SYSTEM DISPLAY FAULT(S) INDICATED BY AIR BLEED )" (SUPPLEMENTAL INFORMATION TO FOLLOW).Jul 6, 2026 · N2188J · Airbus A321271NX · Pneumatic Distribution SystemSDR DALA2026070603922Floorbeam · corrodedLEVEL 2 CORROSION, CORROSION FLOOR BEAM -Y765 LOCATED AT FR 68 AT AFT GALLEY AREA (SSI 5 34147). REPLACED FLOOR BEAM -Y765 LOCATED BTW FR 66 TO FR70 AT AFT GALLEY AREA AS PER A320 SRM 51-42-11, A320 SRM 51-72-11 AND DWGD53472093 RELEASE DATE 06-DEC-24 ISSUE LJul 6, 2026 · N378NW · Airbus A320211 · Fuselage Main, Floor BeamSDR SWIA2026070577147Rib · crackedLEFT WING SLAT 1 FIX LE RIB CRACKED AT WING BS 5841. PERFORMED REPAIR AREA ON SLAT 1 FIX RIB OF LT WING AT WS 5841 IAW SRM 51-42-10, 51-42-13, 51-42-06, REO 670-57-41-715, REV -,Jul 5, 2026 · N794SK · Cndair CL6002C11 · Wing, Rib/BulkheadSDR VNAA202609010019Diaphragm · tornTORN SEAL DIAPHRAGMS OF DECOMPRESSION PANEL ASSY (7EAS) AT FLOOR STRUCTURE SILL ALONG PASSENGER CABIN. SEAL DIAPHRAGMS OF DECOMPRESSION PANEL ASSY (7EAS) AT FLOOR STRUCTURE SILL ALONG PASSENGER CABIN WERE REPLACED IAW SRM 51-42-06-001-001-A01.Jul 5, 2026 · N642NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202609010018Hinge Fitting · corrodedCORROSION ON HINGE FITTINGS (2 EAS) OF ACCESS DOOR AT FAIRING 196DR. HINGE FITTINGS (2 EAS) OF ACCESS DOOR AT FAIRING 196DR WERE REPLACED PER CRJ900 SRM 51-41-02-001-001-A01 AND AMM 20-21-00-910-801-A01Jul 5, 2026 · N642NN · Cndair CL6002D24 · Aerodynamic FairingsSDR VNAA202609010017Angle · corrodedCORROSION ON ANGLE, MLG ELECTRICAL/HYDRAULIC PROTECTIVE COVER IN THE LEFT MLG BAY. ANGLE, MLG ELECTRICAL/HYDRAULIC PROTECTIVE COVER IN THE LEFT MLG BAY WAS EVALUATED OUT LIMITS IAW SRM 53-00-00-101-001-A01 AND REPLACED IAW SRM 51-42-21-001-001-A01.Jul 5, 2026 · N642NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202609010016Intercostal · corrodedCORROSION ON INTERCOSTAL, TIRE BURST COVER IN THE LEFT MLG BAY. INTERCOSTAL, TIRE BURST COVER IN LT MLG BAY WAS REPLACED IAW SRM 51-21-06-001-001-A01, SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, & SRM 51-42-13-001-001-A01.Jul 5, 2026 · N642NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202609010015Seat Track · corrodedCORROSION ON SIDE SEAT TRACK , STGR 15 LT & RT BTW FS 379 - 669.4. CORROSION ON SIDE SEAT TRACK STR 15 LT & RT BTW BS 379 - 669.4 WAS REMOVED IAW SRM 51-21-06-001-001-A01, AND EVALUATED OUT LIMITS IAW SRM 53-21-49-101-001-A01, SRM 53-31-49-101-001-A02, AND SRJul 5, 2026 · N642NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202609010014Seat Track · corrodedCORROSION ON LT SEAT TRACK LBL 9 BTWN BS 374 - 477 (1 EA) IN THE PASSENGER CABIN. LT SEAT TRACK, LBL 9 BTWN BS 374 - 477 (1 EA) EVALUATED OUT OF LIMITS IAW SRM 53-21-49-101-001-A01, & REPLACED IAW AMM 53-00-49.Jul 5, 2026 · N642NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202609010013Seat Track · corrodedCORROSION ON SEAT TRACK LBL 9, BS 669.40 - 977 IN PAX CABIN. CORROSION ON SEAT TRACK LBL 9, BS 669.40 - 977 WAS REMOVED SRM 51-21-06-001-001-A01, EVALUATED OUT OF LIMITS IAW SRM 53-41-49-101-001-A02, SRM 53-51-49-101-001-A02, & REPLACED IAW AMM 53-00-49.Jul 5, 2026 · N642NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202609010012Seat Track · corrodedCORROSION ON SEAT TRACKS RBL 9 BTW BS 669.40 - 977 IN CABIN PAX. CORROSION ON SEAT TRACKS RBL 9 BTW BS 669.40 - 977 AT CABIN PAX WAS REMOVED IAW SRM 51-21-06-001-001-A01, EVALUATED OUT OF LIMITS IAW SRM 53-41-49-101-001-A02, SRM 53-51-49-101-001-A02, & REPLAJul 5, 2026 · N642NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202609010011Seat Track · corrodedCORROSION ON RH SIDE SEAT TRACK AT STR 15RH, BTW BS 669.40 - 977. CORROSION ON RT SIDE SEAT TRACK AT STGR 15RH, BTW BS 669.40 - 977. WAS REMOVED PER SRM 51-21-06-001-001-A01, EVALUATED OUT OF LIMITS IAW SRM 53-41-49-101-001-A02, SRM 53-51-49-101-001-A02 & REJul 5, 2026 · N642NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026082710827Doubler · ground damageUPON REMOVAL, TAILSTAND CONTACTED STANCHION DOUBLER. ACCOMPLISHED ALL REQUIRED AMT STEPS AND VERIFIED ALL OTHER STEPS HAVE BEEN ACCOMPLISHED PER EO-97949-REQ1. THIS REPAIR IS NOW PERMANENT PER EO-97949-REQ3. MAJOR REPAIR.Jul 5, 2026 · N576UP · Boeing 74744AF · Fuselage Main, StructureSDR IPXA2026082316909Bracket · crackedMAIN E&E BAY CENTER WALKWAY CONNECTING BRACKET CRACKED. INSTALLED NUTPLATE ON REPLACEMENT BRACKET AND INSTALLED BRACKET AT THE MAIN E&E BAY CENTER WALKWAY IAW SRM 51-40-02-0G-0.Jul 5, 2026 · N429UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR VNAA202608210029Canister · crackedCRACK ON CANISTER WELDED NO. 3 ON STA WS 148.00 OF INTERNAL RH MAIN FUEL TANK. CANISTER, WELDED NO.3 IN STA. WS148 AT RH MAIN FUEL TANK. WAS REPAIR PER REO 670-57-42-577 REV. --.Jul 5, 2026 · N544EA · Cndair CL6002C10 · Wing Main, Frame StructureSDR VNAA202608210028Canister · crackedCRACK ON CANISTER WELDED NO. 3 ON STA WS 148.00 OF INTERNAL LH MAIN FUEL TANK. CANISTER, WELDED NR 3 IN STA. WS148 AT RH MAIN FUEL TANK. WAS REPAIR PER REO 670-57-42-577 REV. --.Jul 5, 2026 · N544EA · Cndair CL6002C10 · Wing Main, Frame StructureSDR VNAA202608210027Hinge Fitting · excess playFREEPLAY ON BEARING OF RUDDER HINGE FITTING #3 AT REAR SPAR OF VERTICAL STABILIZER. BEARING OF RUDDER HINGE FITTING #3 AT REAR SPAR OF VERTICAL STABILIZER WAS REPLACED PER RIL #2103. REV. B. AND RIL #1213. 03)Jul 5, 2026 · N544EA · Cndair CL6002C10 · Rudder StructureSDR VNAA202608210026Seat Track · corrodedCORROSION ON SEAT RAIL RBL9 (02 SEGMENTS), (SEG 1) BTW FS 677.00 TO FS 863.00, (SEG 2) BTW FS 863.00 TO FS 977.00 AT PASSENGER CABIN. CORROSION ON SEAT RAIL RBL9 (02 SEGMENTS), (SEG 1) BTW FS 677.00 TO FS 863.00, (SEG 2) BTW FS 863.00 TO FS 977.00 AT PASSENGJul 5, 2026 · N544EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202608210025Seat Track · corrodedCORROSION ON SEAT RAIL LBL9 (02 SEGMENTS), (SEG 1) BTW FS 677.00 TO FS 863.00, (SEG 2) BTW FS 863.00 TO FS 989.00 AT PASSENGER CABIN. CORROSION ON SEAT RAIL LBL9 (02 SEGMENTS), (SEG 1) BTW FS 677.00 TO FS 863.00, (SEG 2) BTW FS 863.00 TO FS 989.00 AT PASSENGEJul 5, 2026 · N544EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202608210016Seat Track · corrodedCORROSION ON SEAT RAILS LBL9 BTW FS 477.40 - FS 677.00 (3EA) AT PASSENGER CABIN. CORROSION ON SEAT RAILS LBL9 BTW FS 477.40 - FS 677.00 (3EA) AT PASSENGER CABIN WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01, EVALUATED OUT LIMITS PER CRJ 900 53-31-49-101-00Jul 5, 2026 · N544EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202608210015Seat Track · corrodedCORROSION ON SEAT RAILS RBL9 BTW FS 477.40.00 TO FS 693.00 (SEVERAL LOCATIONS). CORROSION ON SEAT RAILS RBL9 BTW FS 477.40.00 TO FS 693.00 WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01, EVALUATED OUT LIMITS PER CRJ 900 53-31-49-101-001-A02 AND REPLACED PEJul 5, 2026 · N544EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202608210014Seat Track · corrodedCORROSION ON SEAT RAILS RBL9 BTW FS 349.00 - FS 477.40 AT PASSENGER CABIN. SEAT RAILS RBL9 BTW FS 349.00 - FS 477.40 AT PASSENGER CABIN WERE REPLACED PER CRJ-900 AMM 53-00-49Jul 5, 2026 · N544EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026080216819Shear Tie · crackedLEFT WING T/E, NEXT TO NR 5 SPOILER I/B HINGE, WEB WITH CRACK. INSTALLED NEW SKIN SUPPORT IAW SRM 51-40-21.Jul 5, 2026 · N144UP · Airbus A300F4622R · Wing Main, Frame StructureSDR IPXA2026081716817Web · crackedLEFT WING T/E, NEXT TO NR 4 SPOILER OTBD HINGE, WEB CRACKED. WEB, LT WING T/E NEXT TO NR 4 SPOILER OTBD HINGE INSTALLED IAW SRM 51-40-21-001.Jul 5, 2026 · N144UP · Airbus A300F4622R · Wing Miscellaneous StructureSDR SWAA2026081706101Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 661AB, RT WING. REPAIRED THE ACCESS PANEL 661AB IAW SRM 51-70-04-2R-10, REPAIR 10.Jul 5, 2026 · N8651A · Boeing 7378H4 · Wing, Plate/SkinSDR SWAA2026081733965Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 661CB ON RT WING. REPAIRED THE ACCESS PANEL 661CB IAW SRM 51-70-04-2R-10, REPAIR 10.Jul 5, 2026 · N8651A · Boeing 7378H4 · Wing, Plate/SkinSDR SWAA2026081735839Access Panel · damagedELONGATED HOLES ON RT WING ACCESS PANEL 661BBN. REPAIRED THE ACCESS PANEL 661BB IAW SRM 51-70-04-2R-10, REPAIR 10.Jul 5, 2026 · N8651A · Boeing 7378H4 · Wing, Plate/SkinSDR IPXA2026081116351Bracket · crackedLEFT WING, BRACKET WITH CRACK AT FIXED LEADING EDGE (INTERNAL STRUCTURE) INSIDE THE FLAP KRUEGER COMPARTMENT. INSTALLED NEW ANGLE ON WING INBOARD SECTION, LOWER SURFACES IAW SRM 51-40-21.Jul 5, 2026 · N144UP · Airbus A300F4622R · Wing, Attach FittingsSDR SWAA2026081204757Angle · crackedCRACKED ANGLE, BS 400, STR 26L IN THE FWD CARGO BAY. REPLACED THE ANGLE IAW SRM 51-40-02, AND DWG 143A7505, SHEET 81, REV-.Jul 5, 2026 · N7732A · Boeing 7377BD · Fuselage Miscellaneous StructureSDR SWAA2026081285768Stiffener · crackedCRACKED STIFFENER ON FWD SIDE OF THE BULKHEAD BS 540, LBL 25 IN THE FWD CARGO BAY. REPLACED THE STIFFENER AND FASTENERS IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 111A2001, SHT 79, REV -.Jul 5, 2026 · N7732A · Boeing 7377BD · Fuselage Miscellaneous StructureSDR SWAA2026081293681Gusset · crackedCRACKED GUSSET ANGLE, BS 500D, STR 19R IN THE FWD CARGO BAY. REPLACED THE GUSSET AND FASTENERS IAW SRM 51-40-02, 51-10-02, ITEM 9, & DWG 143A7902, SHT 174, REV-.Jul 5, 2026 · N7732A · Boeing 7377BD · Fuselage Miscellaneous StructureSDR SWAA2026081210055Gusset · crackedCRACK GUSSET ANGLE LOCATED BS 500D AT LEVEL STR 19L AT FWD CARGO BAY. REPLACED THE GUSSET AND FASTENERS IAW SRM 51-40-02, 51-10-02, ITEM 9, AND DWG 143A7902, SHT 174, REV -.Jul 5, 2026 · N7732A · Boeing 7377BD · Fuselage Miscellaneous StructureSDR SWIA2026070576835Skin · damagedRIGHT WING LOWER SKIN, DAMAGED AROUND FASTENER HOLE, 8 INCHES INBD OF RIB 23. VERIFIED MATERIAL FOR FABRICATION OF FREEZE PLUG FOR RT WING LOWER SKIN IAW SRM 51-10-07. FABRICATED FREEZE PLUG FOR RT WING LOWER SKIN DAMAGED AROUND FASTENER HOLE 8 INCHES INBD OFJul 5, 2026 · N152SY · Emb ERJ170200LR · Wing, Plate/SkinSDR SWAA2026081124889Scuff Plate · crackedCRACKED FWD SERVICE DOOR SCUFF PLATE, FWD GALLEY. REPAIRED FWD SERVICE DOOR SCUFF PLATE IAW SRM 53-10-15-2R-2, REPAIR 2, AND BAC 5975.Jul 5, 2026 · N7880D · Boeing 7377K5 · Fuselage Miscellaneous Structure