N7887A

Service difficulty reports · 231

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 = 'N7887A' 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 SWAA2024122668004Tank Unit · leakingSUPPLEMENTAL INFORMATION: POSSIBLE FUEL LEAK ON RIGHT SIDE OF FUEL MANIFOLD. #2 ENGINE BURNS 20-50LBS/HR MORE THAN #1 ENGINE; FUEL USED SHOWS #2 ENGINE BURNING SLIGHTLY MORE THAN #1 ENGINE. HOWEVER IN 1:20 OF FLIGHT THE RIGHT MAIN TANK IS DOWN OVER 400 LBS FRODec 21, 2024 · N7887A · Boeing 737752 · Fuel Indicating SystemSDR SWAA2024122668005Tank Unit · leakingSUPPLEMENTAL INFORMATION: POSSIBLE FUEL LEAK ON RIGHT SIDE OF FUEL MANIFOLD. #2 ENGINE BURNS 20-50LBS/HR MORE THAN #1 ENGINE; FUEL USED SHOWS #2 ENGINE BURNING SLIGHTLY MORE THAN #1 ENGINE. HOWEVER IN 1:20 OF FLIGHT THE RIGHT MAIN TANK IS DOWN OVER 400 LBS FRODec 21, 2024 · N7887A · Boeing 737752 · Fuel Indicating SystemSDR SWAA2024122668006Tank Unit · leakingSUPPLEMENTAL INFORMATION: POSSIBLE FUEL LEAK ON RIGHT SIDE OF FUEL MANIFOLD. #2 ENGINE BURNS 20-50LBS/HR MORE THAN #1 ENGINE; FUEL USED SHOWS #2 ENGINE BURNING SLIGHTLY MORE THAN #1 ENGINE. HOWEVER IN 1:20 OF FLIGHT THE RIGHT MAIN TANK IS DOWN OVER 400 LBS FRODec 21, 2024 · N7887A · Boeing 737752 · Fuel Indicating SystemSDR SWAA2024122680095Fuel Unit · leakingPOSSIBLE FUEL LEAK ON RIGHT SIDE OF FUEL MANIFOLD. #2 ENGINE BURNS 20-50LBS/HR MORE THAN #1 ENGINE. FUEL USED SHOWS #2 ENGINE BURNING SLIGHTLY MORE THAN #1 ENGINE. IN 1:20 OF FLIGHT THE RIGHT MAIN TANK IS DOWN OVER 400 LBS FROM THE LEFT MAIN TANK 12/24- HANGDec 21, 2024 · N7887A · Boeing 737752 · Aircraft Fuel Distribution SystemSDR SWAA2024080823214Isolator · crackedAFT PASSENGER DOOR ESCAPE SLIDE FWD UPPER ISOLATOR CRACKED<[01] R&R AFT PASSENGER DOOR ESCAPE SLIDE FWD UPPER ISOLATOR IAW SRM 51-40-02.;[02] INSPECTION C/R&R AFT PASSENGER DOOR ESCAPE SLIDE FWD UPPER ISOLATOR IAW SRM 51-40-02.Aug 7, 2024 · N7887A · Boeing 737752 · Escape SlideSDR SWAA2024070909691Cover · brokenFWD ENTRY DOOR LOWER EXIT LIGHT COVER BROKEN<[01] REPLACED FWD ENTRY DOOR LOWER EXIT LIGHT COVER PER AMM 33-51-01Jul 6, 2024 · N7887A · Boeing 737752 · Emergency LightingSDR SWAA2024042579201Slide · dislodgedLEFT AFT ENTRY DOOR SLIDE FALLING OUT OF CONTAINER. AFT ENTRY DOOR SLIDE WAS SECURED IN THE CONTAINER AND NOT FALLING OUT. TUCKED EXCESS GIRT MATERIAL IN THE SLIDE COMPARTMENT PER MT 725-61-06.Apr 24, 2024 · N7887A · Boeing 737752 · Escape SlideSDR SWAA2024041875943Slide · failedAFT ENTRY DOOR ESCAPE SLIDE FELL OUT OF PACK BUT DID NOT DEPLOY<[01] RE-INSTALLED AFT ENTRY DOOR ESCAPE SLIDE PER MT 725-61-06. A/C OK FOR SERVICE.Apr 16, 2024 · N7887A · Boeing 737752 · Escape SlideSDR SWAA2024022153691Slide · detachedFORWARD ENTRY DOOR ESCAPE SLIDE FELL OUT OF CONTAINER; PREVENTING FORWARD ENTRY DOOR OPERATION<[01] REMOVED AND REINSTALLED SLIDE PER 725-61-06Feb 19, 2024 · N7887A · Boeing 737752 · Escape SlideSDR SWAA2024013146061Handle · crackedAFT ENTRY DOOR ASSIST HANDLE CRACKED AT BOTTOM.<[01] REMOVED AND REPLACED AFT ENTRY DOOR ASSIST HANDLE IAW B737 AMM 52-13-31.Jan 29, 2024 · N7887A · Boeing 737752 · Passenger/Crew DoorsSDR SWAA2023112021302Fastener · looseL1 DOOR ESCAPE SLIDE COMPT GIRT BAR HANGERS LOOSE.<[01] R/R L1 DOOR ESCAPE SLIDE COMPT GIRT BAR HANGERS FASTENERS PER SRM 51-40-02Nov 14, 2023 · N7887A · Boeing 737752 · Emergency EquipmentSDR SWAA2023112021304Fitting · looseL1 DOOR INTERIOR HANDLE FITTING LOOSE.<[01] RE-SECURED L1 DOOR INTERIOR HANDLE FITTING PER AMM 20-50-11Nov 14, 2023 · N7887A · Boeing 737752 · Passenger/Crew DoorsSDR SWAA2023112021306Handle · looseCABIN - R2 DOOR INTERIOR HANDLE FITTING LOOSE.<[01] ADJUSTED AND SAFETIED R2 LOOSE DOOR INTERIOR HANDLE IAW AMM 20-50-11.Nov 14, 2023 · N7887A · Boeing 737752 · Galley DoorsSDR SWAA2023083094822Lens · missingFO SIDE EMERGENCY EXIT ROW FWD LIGHT LENS COVER MISSING<[01] INSTALLED MISSING LENS ON F/O'S OVERWING EMERGENCY PER 33-51-03Aug 28, 2023 · N7887A · Boeing 737752 · Emergency LightingSDR SWAA2023081782231Panel · crackedRT WING L/E PANEL 621PB IS CRACKED AT CORNER (MARKED) PANEL IS ACTUALLY 621HB.<[01] PANEL 621HB WAS REPAIRED IAW SRM 51-70-05-2R-10 AND SRM 51-70-14-2R-3.;[02] VERIFIED CORRECTIVE ACTION 1Jul 25, 2023 · N7887A · Boeing 737752 · Wing Main, Frame StructureSDR SWAA2023081782232Panel · crackedRT WING L/E PANEL 621PB HAS CRACK AT CORNER (MARKED)<[01] PANEL 621PB WAS REPAIRED IAW SRM 51-70-05-2R-6 AND SRM 51-70-14-2R-3.;[02] VERIFIED CORRECTIVE ACTION 1Jul 25, 2023 · N7887A · Boeing 737752 · Wing Main, Frame StructureSDR SWAA2023081781201Intercostal · crackedCRACKED INTERCOSTAL AT AFT CABIN BS927+14 BL0 WL208. MARKED.<[01] CLEANED 'MARKED' AREA IAW AMM 20-10-34-110-802; REQUESTING NDI TO VERIFY ENDS ON CRACK;[02] HFEC INSPECTED SUSPECTED CRACK AREA IAW 737 NDTM PART 6; 51-00-00 PROCEDURE 23.<BR>.3' CRACK NOTED WITJul 21, 2023 · N7887A · Boeing 737752 · Fuselage Miscellaneous StructureSDR SWAA2023081780893Scuff Plate · crackedAFT CARGO BAY FWD CORNER SCUFF PLATE IS CRACKED<[01] WELDED CRACK ON AFT CARGO BAY FWD CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT NUMBER 1131216 PER SRM 53-60-15-2R-1 PARAGRAPH 4.B.(2) AND (4). REPAIR AREA STILL REQUIRES A DYE PENETRANT INSPECTION.<BR>EQUIJul 21, 2023 · N7887A · Boeing 737752 · Fuselage Miscellaneous StructureSDR SWAA2023081780892Scuff Plate · crackedAFT CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED<[01] WELDED CRACK ON AFT CARGO BAY AFT CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT NUMBER 1131216 PER SRM 53-60-15-2R-1 PARAGRAPH 4.B.(2) AND (4). REPAIR AREA STILL REQUIRES A DYE PENETRANT INSPECTION.<BR>EQUIJul 21, 2023 · N7887A · Boeing 737752 · Fuselage Miscellaneous StructureSDR SWAA2023081780909Web · corrodedCORROSION ON SUBTHRESHOLD WEB AT ACB BS807 - BS827 RBL26 WL159.<[01] VERIFIED SRM 53-60-15-0I-1 FOR IDENTIFICATION AND SRM 53-60-15-1A-1 FOR ALLOWABLE DAMAGE.;[02] STEPS 1 AND 2 FOUND TO BE OUT OF LIMITS.;[03] VERIFIED CORRECTIVE ACTION 1 COMPLETE AND UPDATED Jul 21, 2023 · N7887A · Boeing 737752 · Fuselage Miscellaneous StructureSDR SWAA2023081780910Shield · corrodedCORROSION ON FWD SHIELD AT ACB BS767 - BS787 RBL21 WL157.<[01] VERIFIED APPLICABILITY FOR ALLOWABLE DAMAGE LIMITS ON FWD SHIELD AT ACB BS 767 TO BS 787 RBL21 WL 157 IAW SRM 51-10-02;[02] NO ALLOWABLE DAMAGE LIMITS IN SRM REPAIR BY REPACEMENT IAW SRM 51-10-02-0Jul 21, 2023 · N7887A · Boeing 737752 · Fuselage Miscellaneous StructureSDR SWAA2023081780901Support · corrodedCORROSION ON FLOOR TO SIDEWALL SUPPORT AT ACB BS727E - BS767 RBL21 WL157.<[01] VERIFIED SRM 53-60-53-0I-2 FOR IDENTIFICATION AND SRM 53-00-53-1A-2 FOR ALLOWABLE DAMAGE.;[02] STEPS 1 AND 2 FOUND TO BE OUT OF LIMITS.;[03] VERIFIED CORRECTIVE ACTION 1 AND UPDATEDJul 21, 2023 · N7887A · Boeing 737752 · Fuselage Miscellaneous StructureSDR SWAA2023081780510Floor Panel · pulledAFT FLOOR PANEL 242RF UPPER SKIN HAS PULLED STRANDS.<[01] FABRICATED NEW FLOOR PANEL 242RF; INSTALLED INSERTS WITH BMS 5-107 LOT#AK2KP8383K-1; CURED WITH THERMOMETER ID:ATS2208 CAL DUE 10/2023 PER SRM 51-40-02-0G-0 AS SHOWN IN SWA ACO 8722-25 STEP 42 AND AIPC Jul 20, 2023 · N7887A · Boeing 737752 · Fuselage Floor PanelSDR SWAA2023081780517Floor Panel · pulledFWD FLOOR PANEL 221BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 221BF WITH UPPER SKIN THAT HAS AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETJul 20, 2023 · N7887A · Boeing 737752 · Fuselage Floor PanelSDR SWAA2023081780522Floor Panel · pulledFWD FLOOR PANEL 221DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] COMPLETED STEPS 1; 2; 3 AND 5.;[02] FWD FLOOR PANEL 221DF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED PER SRM 53-00-50-2R-1. ATTACHED CURE SHEETS TO THIS FAULT RECORD.;[03] INSPECTED AJul 20, 2023 · N7887A · Boeing 737752 · Fuselage Floor PanelSDR SWAA2023081780888Gusset · crackedFWD CARGO BAY - CRACK ON GOOSED BS 500D S-19L (MARKED)<[01] REMOVED AND REPLACED AT FORWARD CARGO BAY LOCATED BS.500D STR19L IAW SRM 51-40-02 DWG#143A7902 REV: E.;[02] VERIFIED TASK CARD COMPLETE.Jul 20, 2023 · N7887A · Boeing 737752 · Fuselage Miscellaneous StructureSDR SWAA2023081780889Stringer · corrodedAFT OF FORWARD CARGO COMPARTMENT - CORROSION ON STRINGER 23R BS 540 (MARKED)<[01] EVALUATED CORROSION DAMAGE ON STRINGER 23R BS 540; L= 2' W= 1' ORIGINAL THICKNESS 0.036' MAT LOSS MORE THAN 80%; FOUND TO BE OUT OF LIMIT IAW SRM 53-00-03-1A-1;;[02] PERFORMED CUJul 20, 2023 · N7887A · Boeing 737752 · Fuselage Main, Longeron/StringerSDR SWAA2023081780724Panel · crackedCRACK ON BREAK PANEL AT FASTENER BS 540; LBL 1; WL 207<[01] REMOVED BREAK PANEL ON BS 540; LBL 1; WL 207 FOUND PART HAS NOT SRM LIMITS AND SO PART IS REPAIRABLE BY REPLACENENT IAW SRM 51-10-02 STEP 9;[02] LOCATED AND DRILLED NEW BREAK PANEL ON BS 540; LBL 1; WJul 20, 2023 · N7887A · Boeing 737752 · Wing Main, Frame StructureSDR SWAA2023081780322Attach Angle · crackedB.S. 663 VAPOR BARRIER UPPER ATTACH ANGLE IS CRACKED AT R.B.L. 8 W.L. 160.<[01] UPDATE STEP 2.;[02] INSTALLED NEW UPPER ATTACH ANGLE BS 663 VAPOR BARRIER PER SRM 51-40-02 AND DWG 111A1322;[03] UPDATE STEP 3;[04] UPDATED STEP 4;[05] COMPLETED STEP 4.;[06] ALL WJul 19, 2023 · N7887A · Boeing 737752 · Fuselage Main, Attach FittingsSDR SWAA2023081780323Attach Angle · crackedB.S. 663 LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE IS CRACKED AT R.B.L. 45; W.L. 165.<[01] REMOVED AND REPLACED UPPER ATTACH ANGLE BS 663 RBL 6 TO RBL 65 ON N/R # TTG8Q00MAZFH JOB COMPLETED;[02] UPDATE ITEM 1;[03] VERIFIED CORRECTIVE ACTION STEPS 1 AND 2. VEJul 19, 2023 · N7887A · Boeing 737752 · Fuselage Main, Attach FittingsSDR SWAA2023081780320Attach Angle · crackedB.S. 663 LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE IS CRACKED AT L.B.L. 45; W.L. 165.<[01] VERIFIED COMPLETION STEP 6 ITEM 1;[02] REMOVED AND REPLACED B.S. 663 LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE AT L.B.L. 45; W.L. 165 IAW SRM 51-40-02-0G-0; SRM 51-4Jul 19, 2023 · N7887A · Boeing 737752 · Fuselage Main, Attach FittingsSDR SWAA2023081780500Floor Panel · pulledAFT CABIN FLOOR PANEL 241AEF HAS A PULLED THROUGH INSERT<[01] AFT CABIN FLOOR PANEL 241AEF WITH A PULLED THROUGH INSERT WAS REPAIRED PER SRM 53-00-50-2R-1. ATTACHED CURE SHEETS TO THIS FAULT RECORD.;[02] FINAL INSPECTION. JOB COMPLETE.Jul 19, 2023 · N7887A · Boeing 737752 · Fuselage Floor PanelSDR SWAA2023081780052Doubler · crackedLH HORIZONTAL STABILIZER LOWER SKIN - .8' CRACK 18' FROM FWD EDGE ON RIB 193.90<[01] VERIFIED APPLICABILITY OF SRM 55-10-01-2R-11 REPAIR 11.;[02] REMOVED THE DAMAGE AREA OF THE SKIN IAW SRM 55-10-01-2R-11 4. (2) FIG 204/REPAIR 11 DETAIL B AND SRM 51-10-02.<BR>Jul 18, 2023 · N7887A · Boeing 737752 · Horizontal Stabilizer, Plate/SkinSDR SWAA2023081779431Battery Pack · inoperativeREMOVE AND REPLACE EMERGENCY EXIT LIGHT BATTERIES PRIOR TO DELIVERY<[01] PARTIAL WORK FOR STEPS 1 THRU 8.;[02] CERTIFIED ACTION 1.;[03] REMOVED AND REPLACED ALL EMERGENCY EXIT LIGHT BATTERY PACKS AND PERFORMED GOOD INSTALLATION TEST IAW AMM 33-51-06-960-805.;[Jul 17, 2023 · N7887A · Boeing 737752 · Emergency LightingSDR SWAA2023081779639Panel · pulledR/W L/E PANEL 621SB HAS PULLED FASTENER HOLES (MARKED)<[01] EDITED STEP 9.;[02] RIGHT-WING LEADING-EDGE PANEL 621SB WITH PULLED FASTENER HOLES WAS REPAIRED IAW SRM 51-70-04-2R-9.;[03] VERIFIED CORRECTIVE ACTION #2Jul 17, 2023 · N7887A · Boeing 737752 · Wing Main, Frame StructureSDR SWAA2023070675470Flashlight · inoperativeAFT GALLEY FLASHLIGHT INOP. R&R FLASHLIGHT ASSEMBLY IN AFT GALLEY. REF AMM 25-64-00.Jul 6, 2023 · N7887A · Boeing 737752 · Emergency EquipmentSDR SWAA2023051146530Light · inoperativeAFT ENTRY EMERGENCY LT (EXT) INOP<[01] R&RD AFT ENTRY BATT PACK POWER SUPPLY / CHARGER M1673 PER AMM 33-51-06 OPS CHECK GOODMay 8, 2023 · N7887A · Boeing 737752 · Emergency LightingSDR SWAA2022081641472Slide · out of positionSLIDE GIRT BAR WOULD NOT STOW PROPERLY / [01] REPOSITIONED SLIDE IN BOX PER MM 25-66-00Aug 12, 2022 · N7887A · Boeing 737752 · Escape SlideSDR SWAA2022081241030Strip · looseFWD SERVICE DOOR VELCRO STRIPS ON THE GIRT ARE NOT ATTACHED TO VELCRO STRIPS ON THE BACKING PAN SHELF. / [01] REATTACHED VELCRO STRIPS ON THE GIRT TO THE VELCRO STRIPS ON THE BACKING PAN SHELF PER MT 725-61-06. REF TTG8Q004QAASAug 12, 2022 · N7887A · Boeing 737752 · Escape SlideSDR SWAA2022081241032Strip · looseAFT SERVICE DOOR VELCRO STRIPS ON THE GIRT ARE NOT ATTACHED TO VELCRO STRIPS ON THE BACKING PAN SHELF. / [01] REATTACHED VELCRO STRIPS ON THE GIRT TO THE VELCRO STRIPS ON THE BACKING PAN PER MT 725-61-06. REF TTG8Q008K3ZDAug 12, 2022 · N7887A · Boeing 737752 · Escape SlideSDR SWAA2021111138762Slide · out of positionFWD SERVICE DOOR EMERGENCY ESCAPE SLIDE NOT PROPERLY STOWED ; / [01] COMPLIED WITH SWA TASK CARD 725-61-06-FS (REM/INSTL - SLIDE REMOVAL AND INSTALLATION FWD SERVICE DOOR) [TTG8Q0090VQM.; [02] CW; [03] INSTALLED PER AMM 25-66-01.; [04] COMPLIED WITH SWA TASK COct 29, 2021 · N7887A · Boeing 737* · Escape SlideSDR SWAA2021111133929Seat Track · out of toleranceCAPTAINS FWD SEAT TRACKS ARE OUT OF LIMITS. ; / [01] REMOVED AND REPLACED CAPTAINS FWD (2EACH) SEAT TRACKS IAW AMM 25-11-11.; [02] REMOVED AND REPLACED CAPTAINS AFT (2EACH) SEAT TRACKS IAW AMM 25-11-11.Oct 27, 2021 · N7887A · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2021111532187Panel · crackedR/H WING T/E PANEL 661AB HAS MULTIPLE CRACKS AROUND FASTENER HOLES. ; / [01] REMOVED DAMAGE PER SRM 51-70-05-2R-9; [02] C/W STEP 1.; [03] APPLIED RESIN AND CHOPPED FIBERS TO DAMAGED FASTENER HOLES PER SRM 51-70-05-2R-9.; [04] INSPECTED WORK PERFORMED ON C/A #3Oct 21, 2021 · N7887A · Boeing 737* · Wing Miscellaneous StructureSDR SWAA2021111532188Panel · crackedR/H WING T/E PANEL 661BB HAS MULTIPLE CRACKS AROUND FASTENER HOLES. ; / [01] REMOVED DAMAGE PER SRM 51-70-05-2R-9; [02] C/W STEP 1.; [03] APPLIED RESIN AND CHOPPED FIBERS TO DAMAGED FASTENER HOLES PER SRM 51-70-05-2R-9.; [04] INSPECTED WORK PERFORMED ON C/A #3Oct 21, 2021 · N7887A · Boeing 737* · Wing Miscellaneous StructureSDR SWAA2021111532189Panel · crackedR/H WING T/E PANEL 661CB HAS MULTIPLE CRACKS AROUND FASTENER HOLES. ; / [01] C/W DAMAGE REMOVAL PER SRM 51-70-05-2R-9; [02] C/W INSPECTION C/W DAMAGE REMOVAL PER SRM 51-70-05-2R-9; [03] APPLIED RESIN AND CHOPPED FIBERS TO DAMAGED FASTENER HOLES PER SRM 51-70-0Oct 21, 2021 · N7887A · Boeing 737* · Wing Miscellaneous StructureSDR SWAA2021111531167None · corrodedLH TRANSITION ANGLE HAS CORROSION AROUND FASTENER HOLE UPPER SURFACE AT STA 727E+14 ; / [01] COMPLIED WITH TOOL REQUIREMENT.; [02] REMOVED SURFACE CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-60-51-1A-1. REMOVE AND REPLACE ANGLE ON TASK CARD 5360-E-16462-NG Oct 16, 2021 · N7887A · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2021111531165Floor Panel · missingPANEL 242BF FLOOR PANEL CABIN HAS FIBERS MISSING. ; / [01] SEE CLOSE-PANEL 242BF (PANEL 242BF FLOOR PANEL) [TTG8Q006QLTS]FOR OK TO CLOSE; CLOSE AND BUY BACK INSPECTION.; [02] REPLACED FLOOR PANEL. SEE CLOSE-PANEL 242BF (PANEL 242BF FLOOR PANEL) [TTG8Q006QLTS]FOct 16, 2021 · N7887A · Boeing 737* · Fuselage Floor PanelSDR SWAA2021111531180None · corrodedLH TRANSITION ANGLE HAS CORROSION AROUND FASTENER HOLE UPPER SURFACE AT STA 727E+10 ; / [01] COMPLIED WITH TOOL REQUIREMENT.; [02] REMOVED SURFACE CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-60-51-1A-1. REMOVE AND REPLACE ANGLE ON TASK CARD 5360-E-16462-NG Oct 16, 2021 · N7887A · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2021111531181None · corrodedLH TRANSITION ANGLE HAS CORROSION AROUND FASTENER HOLE UPPER SURFACE AT STA 727E+18 ; / [01] COMPLIED WITH TOOL REQUIREMENT.; [02] REMOVED SURFACE CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-60-51-1A-1. REMOVE AND REPLACE ANGLE ON TASK CARD 5360-E-16462-NG Oct 16, 2021 · N7887A · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2021111531179None · corrodedLH TRANSITION ANGLE HAS CORROSION AROUND FASTENER HOLE UPPER SURFACE AT STA 727E+6 ; / [01] COMPLIED WITH TOOL REQUIREMENT.; [02] REMOVED SURFACE CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-60-51-1A-1. REMOVE AND REPLACE ANGLE ON TASK CARD 5360-E-16462-NG (Oct 16, 2021 · N7887A · Boeing 737* · Fuselage Miscellaneous Structure
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