JASC 5310

Service difficulty reports · 38,548

Reports filed under 5310 · Fuselage Main, Structure, 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 jasc_code = '5310'
  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 AALA201911059004Pressure Plate · crackedAIRCRAFT IN BASE VISIT: CRACK INDICATION ON HOLE A LOCATED AT Y+1292 LH SIDE PRESSURE PLATE ATFR 35/36 IN FWD CARGO COMPARTMENT (1 EA) (CRACK DIRECTION:06 O'CLOCK APPROX. D1-D2=0.106 INCH, 2.69 MM APPROX). REPAIR COMPLETED LOCATED IN Y+1292 LH SIDE PRESSURE POct 27, 2019 · N768US · Airbus A319112SDR DALA2019102806224Pressure Panel · crackedA CRACK THAT EXCEEDS THE AUTHORIZED REPAIR AREA WAS FOUND AT THE PRESSURE PLATE AREA BETWEEN FR35LH AND FR36LH. LIAISON ENGINEERING CORRECTIVE ACTION IS REQUIRED PRIOR TO FURTHER FLIGHT. HOLE #B17. AA 5311-01171 SB A320-53-1263 AD- 2018-06-04. REPAIRED PER PRIOct 27, 2019 · N317NB · Airbus A319114SDR DALA2019102806223Pressure Panel · crackedA/C 3117 CLOSED LOG 1334310 FLT/CHK 3117. A CRACK THAT DOES NOT EXCEED THE AUTHORIZED REPAIR AREA WAS FOUND AT THE PRESSURE PLATE AREA BETWEEN FR35LH AND FR36LH. MODIFY IN ACCORDANCE WITH WORK CARD 5311-01171-04A PRIOR TO FURTHER FLIGHT. HOLE # 8.AA 5311-01171Oct 27, 2019 · N317NB · Airbus A319114SDR DALA2019102806222Pressure Panel · crackedFOUND HOLE A CRACKED DURING INSPECTION 5311-01171-02A OF PRESSURE PANEL HOLES FR35/36, CRACK RUNS FWD AND AFT OF HOLE A. REPAIR IAW AMDS 5311-01171-04A. REF. AA 5311-01171,SB A320-53- 1264 AND AD-2018-06-04. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 040-0001:5Oct 27, 2019 · N317NB · Airbus A319114SDR DALA2019102806220Pressure Plate · crackedA CRACK THAT EXCEEDS THE AUTHORIZED REPAIR AREA WAS FOUND AT THE PRESSURE PLATE AREA BETWEEN FR35LH AND FR36LH. LIAISON ENGINEERING CORRECTIVE ACTION IS REQUIRED PRIOR TO FURTHER FLIGHT. HOLE # 20. AA 5311-01171 SB A320-53-1263 AD- 2018-06-04. REPAIRED PER PRIOct 27, 2019 · N317NB · Airbus A319114SDR SWAA2022032387023Channel · corrodedAFT CARGO RIGHT SIDE 'Z' CHANNEL IS CORRODED AT BS 727A TO 767. / REMOVED CORROSION AT AFT CARGO RIGHT SIDE ZEE CHANNEL AT BS 727A TO BS 767 PER REF B737-700 SRM 51-10-02-0G-0. FOUND OUT OF LIMITS. REMOVED AND REPLACED ZEE CHANNEL AT AFT CARGO RIGHT SIDE BS 72Oct 25, 2019 · N765SW · Boeing 7377H4SDR SWAA2022032387021Support · corrodedAFT CARGO FLOOR SUPPORT AT BS 887 IS CORRODED AT 11 INCHES LEFT OF CENTER LINE TO 20' RIGHT OF CENTER LINE. / ACCOMPLISHED INSPECTION AT AFT CARGO FLOOR SUPPORT AT STA 887.FOUND DEEP CORROSION AT FASTENER HOLE.FOUND OUT OF LIMITS.REMOVED AND REPLACED FLOOR SUPOct 25, 2019 · N765SW · Boeing 7377H4SDR SWAA2022032333081Beam · corrodedAFT CABIN R/H INNER CREASE BEAM STA 967-986; RBL52; WL208 UPPER AND LOWER SURFACE HAS CORROSION / REMOVED CORROSION FROM AFT CABIN RH INNER CREASE BEAM STA 967 - 986 RBL 52 WL 208 IAW SRM 53-70-15-1A-1. ORIGINAL THICKNESS .080 REM .056 LOSS OF .024. FOUND TO BOct 25, 2019 · N8605E · Boeing 7378H4SDR SWAA2022032333084Beam · corrodedAFT CABIN R/H INNER CREASE BEAM STA 947; RBL54; WL208 HAS CORROSION UPPER SURFACE / REMOVED AND REPLACED R/H INNER CREASE BEAM STA 887+6 TO 992+8 RBL 65.7' TO RBL 44.3' TO AFT END PN: 147A8540-8 A TAG: WN5698 ON SA-M 112 #4127069Oct 25, 2019 · N8605E · Boeing 7378H4SDR SWAA2022032333085Intercostal · corrodedAFT CABIN OTBD GALLEY FITTNG AT STA 947; RBL49; WL208 HAS CORROSION AT BASE / REMOVED AFT CABIN OUTBD GALLEY FITTING STA 947; RBL49 WL208 IAW SRM 51-40-02-0G-0. REMOVED CORROSION AT INTERCOSTAL BETWEEN STA 967 AND STA 947 RBL49 IAW SRM 51-10-02-0G-0. ORIGINAL Oct 25, 2019 · N8605E · Boeing 7378H4SDR SWIA2019121846978Door Frame · corrodedPAX DOOR FWD FRAME CORRODED. (C-CHECK) RO 12/14/2019 REMOVED AND REPLACED PAX DOOR FWD FORMER WITH NEW PART IAW CRJ 200 SRM. FORM 337, SDR, AND MAJOR REPAIR TASK COMPLETE AND ATTACHED. NO WEIGHT CAHNGE, PART FOR PART REPLACEMENT.Oct 25, 2019 · N437SW · Cndair CL6002B19SDR SWIA2019121846977Door Frame · corrodedPAX DOOR AFT FRAME CORRODED. (C-CHECK) RO 12/14/2019 REMOVED AND REPLACED PAX DOOR CORRODED AFT FORMER WITH NEW PART IAW CRJ 200 SRM.Oct 25, 2019 · N437SW · Cndair CL6002B19SDR SWAA2019110538617Crease Beam · corrodedAFT CABIN R/H INNER CREASE BEAM CORRODED UPPER SURFACE BETWEEN BS. 887+6 TO BS. 992+8, BETWEEN RBL 65.7 TO RBL 44.3. / R&R R/H INNER CREASE BEAM IAW SRM.Oct 25, 2019 · N8305E · Boeing 7378H4SDR SWAA2019110538616Crease Beam · corrodedAFT CABIN INNER CREASE BEAM UPPER AND LOWER SURFACE CORRODED BETWEEN BS. 967 TO BS. 986, RBL 52. / R&R CREASE BEAM IAW SRM AND DWG.Oct 25, 2019 · N8305E · Boeing 7378H4SDR AALA201911059005Stop Fitting · crackedAIRCRAFT IN BASE VISIT: CRACK INDICATION ON FRAME 68 RH DOOR STOP 7 LOWER INB HOLE. CRACK DIRECTION 7 O'CLOCK. IN PASSENGER CABIN (1 EA). PERFORMED PERMANENT REPAIR ON FR 68RH DOOR STOP 7 LOWER INB HOLE IN PASSENGER CABIN IAW A319 SRM 53-41-12-300-010.Oct 25, 2019 · N768US · Airbus A319112SDR YENA2019102950622Fitting · corrodedDURING HEAVY MAINTENANCE, R1 DOOR FITTING CORRODED; REF LTPR NR 5000924154-0010. R1 DOOR FLOOR FITTING REPLACED IAW SRM 51-72-11 REV. 129Oct 25, 2019 · N907JB · Airbus A321231SDR DALA2019102906229Door Frame · crackedSHIP 9213 RIGHT WHEEL WELL FWD DOOR JAMB CRACKED. REMOVED AND REPLACED RT FWD WHEEL WELL FRAME PER BOEING DWG 5930584 (6612127)Oct 25, 2019 · N913DN · Doug MD9030SDR DALA2019102706187Torsion Box · crackedDURING C CHECK, DURING ACCOMPLISHMENT OF WC 5332-2003, CRACK INDICATIONS WERE FOUND ON DOOR 3R TORSION BOX STRINGER S-14R AT FR 53.8, S-15L AT FR 53.5 AND S-15R AT 53.5 DURING SURFACE HFEC INSPECTIONS PER NTM 53-32-07-250-801. REPLACED STRINGER S-15L F53370179Oct 25, 2019 · N806NW · Airbus A330323SDR SWAA2022032333067Angle · corrodedAFT CARGO COMPARTMENT STA 727-827 LBL 20 WL 158; Z ANGLE IS CORRODED. / REMOVED CORROSION AT AFT CARGO Z-ANGLE STA 727 TO 827 LH IAW SRM 53-00-53-2R-5. VERIFIED MATERIAL LOSSORIGINAL .040'; BETWEEN STA 727 - STA 727H L/H LOWEST .036' .004' MATERIAL LOSS AND BEOct 24, 2019 · N8305E · Boeing 7378H4SDR SWAA2022032333068Angle · corrodedAFT CARGO COMPARTMENT STA 727A +13 TO 767 RBL 20 WL 158; Z ANGLE IS CORRODED. / REMOVED CORROSION IAW SRM 53-00-53-1A-2. VERIFIED WITH 10X MAGNIFICATION. CORROSION REMOVAL AT RH Z-ANGLE FROM STA 727A+13 TO 727. ORIGINAL THICKNESS .040' BETWEEN STA 727A+13 TO 7Oct 24, 2019 · N8305E · Boeing 7378H4SDR FDEA201910242741Crossbeam · noneEXISTING REPAIR ON MDCC CROSSBEAM AT FR30 BETWEEN -Y450 AND -Y953 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MDCC CROSSBEAM AT FR30 BETWEEN -Y450 AND -Y953 WAS EVALUATED. NO REPAIR RECORD WAS FOUND AND THE REPAIR DID NOT SUPPORTED BY CURREOct 24, 2019 · N665FE · Airbus A300F4605RSDR REXA2019112641647Doubler · crackedINITIAL INSPECTION: CRACK ON DOUBLER OF COLLER TRAY OF ADG RESTOW PUMP AT FWD EQUIPMENT COMPARTMENT. (FUS). SUMMARY: DOUBLER OF COLLER TRAY OF ADG RESTOW PUMP AT FWD EQUIPMENT COMPARTMENT WAS REPLACED PER CRJ900 SRM 53-11-43-201-001-A01Oct 24, 2019 · N926XJ · Cndair CL6002D24SDR FDEA201910242739Crossbeam · noneEXISTING REPAIR ON MDCC CROSSBEAM AT FR29 BETWEEN -Y450 AND -Y953 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MDCC CROSSBEAM AT FR29 BETWEEN -Y450 AND -Y953 WAS EVALUATED. NO REPAIR RECORD WAS FOUND AND THE REPAIR DID NOT SUPPORTED BY CURREOct 24, 2019 · N665FE · Airbus A300F4605RSDR CALA2019102501818Fitting · crackedL-1 WINDOW POST CRACKED AT UPPER LEFT CORNER L-1 WINDOW POST HAS BEEN REPAIRED IAW ECRA 5311-02271 ACCOMP AN INITIAL INSP PER PART 2 SECTION A ON OR BEFORE THE AIRCRAFT REACHING 50000 TOTAL FLT CYC''S. ACCOMP REPETITIVE INSP''S PER PART 2. SECTION A AT INTERVAOct 24, 2019 · N73283 · Boeing 737824SDR CALA2019102501820Door Frame · crackedR/H FR20 NO.7 DOOR STOP FITTING - HOLE 1 FND CRACK REF NON-ROUTI NE NO:9486634, SPEC NO.A3NB-53-4-0018. RH FR20 NO.7 DOOR STOP FTG INTERCOSTAL REPLACED AND FASTENER HOLES REPAIRED AS PER ECRA 5311-02276 REV -.Oct 24, 2019 · N4871 · Airbus A319132SDR SWAA2022032358980Angle · corrodedAFT CARGO COMPARTMENT 'Z' ANGLE FLOOR PANEL TO SIDEWALL PANEL HAS AREAS OF CORROSION STA 847-867 RBL 20 W/L 157 / AFT CARGO Z-ANGLE SHIELD STA 847 TO STA 867 R/H SIDE HAS CORROSION. BLENDED AND REMOVED CORROSION I/A/W SRM 51-10-02-0G-0. MAT THICKNESS IS .050; Oct 23, 2019 · N908WN · Boeing 7377H4SDR SWAA2022032358979Web · corrodedAFT CARGO COMPARTMENT DOOR THRESHOLD WEB HAS MULTIPLE AREAS OF CORROSION FROM STA 747-827 RBL 25 W/L 157 / AFT CARGO COMPARTMENT DOOR THRESHOLD WEB REPLACED FROM STA 747 - 827 RBL 25 W/L157 IAW SRM 51-40-02-0G-0 AND BOEING DWG 146A8120 ID: 39 REV: -; AND BOEINOct 23, 2019 · N908WN · Boeing 7377H4SDR SWAA2022032358977Angle · corrodedAFT CARGO COMPARTMENT R/H 'Z' ANGLE CONNECTING THE FLOOR PANEL TO THE SIDEWALL PANEL HAS AREAS CORRODED FROM STA 767-787 RBL 23 W/L 157 / REMOVED AND REPLACED AFT CARGO COMPARTMENT R/H 'Z' ANGLE (SHEILD) CONNECTING THE FLOOR PANEL TO THE SIDEWALL PANEL FROM STOct 23, 2019 · N908WN · Boeing 7377H4SDR FDEA2019102432731Crossbeam · crackedMAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM CRACKED, AT FR64, BETWEEN -Y1456 AND -Y1959 REPAIRED THE MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE CROSSBEAM CRACK AT FR64 BETWEEN -Y1456 AND -Y1959 PER A300-600F 53-10-15-201 FIGURE 211. MAJOR REPAOct 23, 2019 · N665FE · Airbus A300F4605RSDR REXA2019111231575Crossbeam · crackedFS 280 CROSSBEAM RBL 9 OB ATTACH ANGEL CRACKED UPON FURTHER INVESTIGATION, FOUND BULKHEAD WEB TO BE PREVIOUSLY REPAIRED PER REO 601R-53-11-926. FABRICATED ANGLE IAW BOMBARDIER REO 601R-53-11-926 REV B FLAGNOTE 20, FROM PREFORMED ANGLE PN S6144-13 PO W56689 & Oct 23, 2019 · N8908D · Cndair CL6002B19SDR F3LA201911060136Fitting · crackedDISCREPANCY: REFERENCE PEMCO N/R: 2650N341 RH FR16 UPPER DOUBLE JOGGLE AREA AFT LOWER HOLE (BL SHOWS CRACK INDICATION IN THE INBD LAYER AT 9 OCLOCK POS. VIEWED FROM THE EXTERIOR CORRECTIVE ACTION: REPAIRED R/H FR16 DOUBLE JOGGLE UPPER CORNER HOLE "B" IAW AIROct 23, 2019 · N949FR · Airbus A319112SDR GR4D20191029001Door Frame · corrodedFOUND CORROSION ON PANEL MATING SURFACE UNDER PANEL 312BL (APU ACCESS DOOR REBATE/PANEL LAND). REQUIRED ENGINEERING DISPOSITION TO CONTINUE IN SERVICEOct 23, 2019 · N529QS · Gulstm GVSPG550SDR C77A2019102300004Beam · corrodedDURING THE CURRENT B6 BASIC CHECK AT EAMS, CORROSION DAMAGE WAS DISCOVERED ON THE FORWARD PASSENGER (L1) DOOR LOWER THRESHOLD BEAM (P/N 170-03719-005) AT FASTENER HOLES AROUND THE FORWARD GIRT BAR FITTING DURING ACCOMPLISHMENT OF EO E175-5300-221.1 FOR A MODIFOct 23, 2019 · N615CZ · Emb ERJ170200LRSDR JGVR20191023001Door Frame · chafedREPAIRED FIVE CHAFFED AREAS AROUND E-EXIT WEB AND FRAME IN STRINGER 3 SURROUNDING AREAS OF THE INTERIOR FUSELAGE AT FS 409.26 AND FS 426.26 BY INSTALLING REPAIR DOUBLERS AND SHIMS PER ENGINEERING REPAIR ORDER.Oct 23, 2019 · N311QS · Cessna 680CESDR SWIA2019102346593Vertical Beam · crackedFS 409.00 + 128 RBL 27.00 VERTICAL BEAM IS CRACKED LOWER INBOARD CORNER AS MARKED. (C-CHECK) RO: 10/22/19. REPLACED WITH NEW FS409.00+128 RBL27.00 VERTICAL BEAM IAW. LEAK CHECK AND OPS TEST GOOD.Oct 23, 2019 · N923SW · Cndair CL6002B19SDR SWIA2019102346585Post · crackedFS 409+128 VERT. POST LBL27 IB HALVE LWR CORNER CRACKED @ FASTENER. (C-CHECK) RO: 10/21/19. REPAIRED F.S. 409+128 VERTICAL POST LBL 27, I/B I.A.W. REO. WORK ACCOMPLISHED BY AAR.Oct 23, 2019 · N874AS · Cndair CL6002B19SDR SWIA2019102346583Post · crackedFS 409+128 VERT. POST RBL27 IB HALVE LWR CORNER CRACKED @ FASTENER. (C-CHECK) RO: 10/21/19. REPAIRED F.S. 409+128 VERTICAL POST, RBL 27, IB I.A.W. REO. WORK ACCOMPLISHED BY AAR.Oct 23, 2019 · N874AS · Cndair CL6002B19SDR SWAA2022032386998None · corrodedLH CREASE BEAM INNER CORD UPPER SURFACE HAS LIGHT CORROSION SPOTS BETWEEN STA 616 AND 727 / BLENDED OUT CORROSION AT L/H CREASE BEAM INNER CORD UPPER SURFACE STA 663; 75+9' TO STA 727 ORIG MAT .071' MAT LOST .003' MAT REMAINING .068' FOUND TO BE IN LIMIT IAW BOct 22, 2019 · N765SW · Boeing 7377H4SDR SWAA2022032347173Web · corrodedAFTER REMOVAL OF FORWARD CARGO DOOR SCUFF PLATE; FOR DENTS. FURTHER CORROSION FOUND ON FRAME DIRECTLY UNDER SCUFF PLATE; CENTER OF THRESHOLD. / REMOVED FWD CORNER SCUFF PLATE FOM IAW 737-800 SRM 51-40-02-0G-0. REMOVED FWD CRGO CENTER THRESHOLD IAW 737-800 SRM Oct 22, 2019 · N8618N · Boeing 7378H4SDR SWAA2022032347157Angle · corrodedAFT CARGO COMPARTMENT L/H SIDE Z-ANGLE STA 727 H TO STA 847 LBL 21 HAS CORROSION / BLENDED CORROSION AFT CARGO L/H Z-ANGLE STA 727-847 LBL 21 VERIFIED MATERIAL LOSS ORG 'T' .040 REMAINING 'T' .029 LOSS OF .011 FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED AFOct 22, 2019 · N8618N · Boeing 7378H4SDR SWAA2022032347154Angle · corrodedAFT CARGO COMPARTMENT R/H SIDE Z-ANGLE STA 727+4 TO 727F RBL 21 HAS CORROSION / BLENDED CORROSION ON AFT CARGO R/H SIDE; Z-ANGLE STA 727+4 - 727F RBL 21. VERIFIED MATERIAL LOSS TO BE ORIG 'T' .040 REMAINING 'T' .031 LOSS OF .009 FOUND TO BE OUT OF LIMITS. REMOOct 22, 2019 · N8618N · Boeing 7378H4SDR SWAA2022032347147Angle · corrodedFWD CARGO COMPARTMENT FLOOR STRUCTURE STA 500I; LBL 24 TO RBL 24; WL 156 BULKHEAD SUPPORT L-ANGLE HAS CORROSION. / REMOVED CORROSION IAW B737 SRM 51-10-02-0G-0. VERFIED MATERIAL LOSS AND LIMITS ORIG. 'T' .071'; REMAINING 'T' .065; .006' LOSS FOUND TO BE OUT OFOct 22, 2019 · N8618N · Boeing 7378H4SDR SWAA2019102838299Crease Beam · corrodedPASSENGER CABIN AFT WET AREA R2 CREASE BEAM INNER CHORD CORRODED BETWEEN BS. 947 TO BS. 986+6, RBL 50, ON UPPER SURFACE. / R&R INNER CHORD IAW SRM AND DWG.Oct 22, 2019 · N908WN · Boeing 7377H4SDR DALA2019102436133Door Frame · cracked(LOG 1326913) DURING INSPECTION FOUND CRACK ON R1 DOOR CUT-OUT FWD LOWER CORNER AT PAX CABIN. CRACK ON R1 DOOR CUT-OUT FWD LOWER CORNER AT PAX CABIN WAS REPAIRED PER B737-800 SRM 53-10-15 REPAIR 7.Oct 22, 2019 · N3765 · Boeing 737832SDR SWAA2022032342912Angle · corroded***CORROSION*** AFT CARGO COMPT-- FROM BS727 TO BS807 LBL22 WL157 L/H Z-ANGLE HAS CORROSION AROUND SEVERAL FASTENER HOLES / INSTALLED SPLICE REPAIR AT B.S. 727E+10 AND BS 737 LBL 22 WL 157 IAW SRM 53-00-53-2R-5; REMOVED AND REPLACED ZEE ANGLE AFT CARGO COMPT BOct 21, 2019 · N8600F · Boeing 7378H4SDR SWAA2022032342913Angle · corroded***CORROSION*** AFT CARGO COMPT-- FROM BS727D TO BS767 RBL22 WL157 R/H Z-ANGLE HAS CORROSION AROUND SEVERAL FASTENER HOLES / REMOVED AND REPLACED 2-ANGLE ON BSM. 727A TO 767 RBL 22; WL 157 IAW-SRM-51-40-02-0G-0; SRM-53-00-53-2R-5; REPAIR 5. SPLICE LOCATED AT BOct 21, 2019 · N8600F · Boeing 7378H4SDR SWAA2022032342915Web · corroded***CORROSION*** AFT CARGO COMPT-- FROM BS787+6 TO BS847 RBL25 WL157 CARGO DOOR WEB HAS CORROSION AROUND SEVERAL FASTENER HOLES. / REMOVED AND REPLACED AFT CARGO DOOR WEB BS787+6+847 RBL25 WL157 WITH PN 146A8123-25 IAW SRM 51-40-02-0G-0 AND DWG #146A8340Oct 21, 2019 · N8600F · Boeing 7378H4SDR SWAA2022032342911Support · corroded***CORROSION*** FWD ENTRY DOOR THRESHOLD SUPPORT HAS CORROSION STA. 346 LBL 63 WL 208 / REMOVED CORROSION FROM FWD ENTRY DOOR THRESHOLD SUPPORT STA. 346 LBL 63 WL 208 AREA 1.0L X 1.0W X 0.010D IAW SRM 51-10-02-0G-0 FOUND TO BE OUT OF LIMITS IAW 53-10-15-1A-1 ROct 21, 2019 · N8600F · Boeing 7378H4SDR C77A2020011210025Beam · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH A PERMANENT REPAIR OF CORROSION DAMAGE DISCOVERED DURING BASIC CHECK AT EAMS ON THE AFT CABIN LH FLOOR BEAM (P/N 170-65669-003) AT FR87 IN THE AFT CABIN FLOOR STRUCTURE. THE BEAM WILL BE REPAIRED BYOct 21, 2019 · N202NN · Emb ERJ170200LRSDR SWAA2022032342901Angle · corroded***CORROSION*** R2 SERVICE DOOR THRESHOLD SUPPORT ANGLE HAS CORROSION STA. 923-987 RBL 53 WL 209 / TRANSFERRED TO CARD #N232088 FOR ALL WORK AND DOCUMENTATION. 20320C 10/22/19Oct 20, 2019 · N8600F · Boeing 7378H4
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