Boeing 737-890

Service difficulty reports · 23,038

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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 aircraft_model_key = '737890'
  ORDER BY difficulty_date DESC"

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SDR ASAA2024053150499Rib · crackedRIGHT HORZ. STAB INTERNAL APPROX. SS 120 BETWEEN FRONT SPAR AND REAR RIB CRACKED. GROUNDED - YES. REPAIRED THE RIGHT HORIZ. STAB RIB AT APPROX SS 120 USING MAT BAC1505-100962 T-SECTION, BAC1490-2793 ANGLE, 0.12 7075-T6 SHIMS PER B737-800 SRM 55-10-09-2R-4.May 31, 2024 · N506AS · Boeing 737890 · Horizontal Stabilizer, Spar/RibSDR ASAA2024053150497Rib · crackedL/H HORIZONTAL STAB AROUND SS 102, AFT VERT. RIB HAS CRACK. GROUNDED - YES. REMOVED DAMAGED AREA. FABRICATED REAPIR PARTS P/N: BAC1490-2793 EXTRUSION 7075T6 PO:1085311.1. P/N: BAC1505-100352 7075-T73511 TEE EXTRUSION PO:843204.1, P/N:7075-T6 .012 ALUMINUM SHEEMay 31, 2024 · N594AS · Boeing 737890 · Horizontal Stabilizer, Spar/RibSDR ASAA2024052950500Floor Support · corrodedMAIN CABIN FLOOR SUPPORT INTERCOSTAL AT STA 947 CORRODED. GROUNDED - YES. BLENDED CORROSION INTERCOSTAL HAS 100% MATERIAL LOSS FOUND OUT OF LIMITS ALLOWABLE DAMAGE IAW B737-800 STM 53-70-51-1A-1 AT STA 242.5 LBL 24.5, DRILLED FIT NEW INTERCOSTAL IAW B737-800 SMay 29, 2024 · N506AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2024052950418Angle · crackedFWD PIT, L/H BAFFLE CLIP AT STA 500H FWD SIDE IS CRACKED. GROUNDED - YES. REMOVED & REPLACED FWD PIT L/H BAFFLE CLIP AT STA 500H PN:143A7502-155 IAW B737-800 SRM 51-40-02 & SRM 51-40-05.May 29, 2024 · N506AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2024052950230Baffle · crackedFWD PIT, L/H BAFFLE CLIP AT STA 500G AFT SIDE IS CRACKED. GROUNDED - YES. REMOVED & REPLACED FWD PIT, L/H BAFFLE CLIP AT AT STA 500G WITH PN: 143A 7502-159 PO: 1092414.1 IAW B737-800 SRM 51-40-02 & SRM 51-40-05.May 29, 2024 · N506AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2024052950090Transition Panel · corrodedFWD PIT R/H TRANSITION PANEL STA 500E+10 TO 500I HAS CORROSION. GROUNDED - YES. REMOVED THE CORROSION FROM THE FWD PIT R/H TRANSITION PANEL AT STA 500E+10 TO 500I IAW B737-800 SRM 53-00-53-1A-2.2.D. ORIG THICKNESS IS .040" IAW B737-800 SRM 53-30-53-01-2 TABLE May 29, 2024 · N506AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2024052950089Transition Panel · corrodedFWD CARGO LT TRANSITION PANEL STA 500G+2 TO 500I HAS CORROSION. GROUNDED - YES. REMOVED CORROSION FROM THE FWD PIT L/H TRANSITION PANEL AT STA 500G+2 TO 500I IAW B737-800 SRM 53-00-53-1A-2.2.D ORIG THICKNESS IS .040 IAW B737-800 SRM 53-30-53-01-2 TABLE 2. REMOMay 29, 2024 · N506AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2024052850723Bracket · wornE/E COMPT. AFT DOOR PIN RECEPTICLE BRACKET IS WORN. GROUNDED - YES. REMOVED AND REPLACED RECEPTICLE BRACKET IAW B737-800 SRM 51-40-02 AND BOEING DWG # 141A3501 REV: - ADJUSTMENT CHECK GOOD.May 28, 2024 · N506AS · Boeing 737890 · Electrical/Electronic Compartment DoorsSDR ASAA2024052850504Floorbeam · corrodedAFT WET AREA STA 947 T-CAP HAS CORROSION AT MOUNT FITTING. GROUNDED - YES. REMOVED CORROSION, ORIGINAL THICK 0.1800 IAW B737-800 SRM 53-70-51-1A-1 AND FLOOR BEAM BAC 1518-1212 REMAINING THICK 0.154 AT RBL 53, 0.026" REMOVE MAT, REMAINING THICK 0.158 AT LBL 4, May 28, 2024 · N506AS · Boeing 737890 · Fuselage Main, Floor BeamSDR ASAA2024052850428Floorbeam · corrodedAFT WET STA 986 HAS CORRODED FASTENER HOLES FLOOR BEAM. GROUNDED - YES. REMOVED CORROSION. ORIGINAL THICKNESS 0.150 IAW B737-800 SRM 53-70-51-0I-1 AND BAC 1518-1211. REMAINING THICKNESS AT RBL 34- 0.100, REMOVED 0.050. REMAINING THICK AT LBL43 0.095, REMOVED 0May 28, 2024 · N506AS · Boeing 737890 · Fuselage Main, Floor BeamSDR ASAA2024052850426Floor Support · corrodedFWD WET AREA STA 328 - 344 LBL11 FLOOR STIFFNER HAS CORROSION. GROUNDED - YES. REMOVED CORROSION FROM FWD WET AREA, STA 328-344, LBL 11 FLOOR STIFFENER (PANEL BREAK) REF B737-800 SRM 53-10-51-0I-2. TABLE 3. ITEM 8 PER. B737-800 SRM 53-10-51-1A-A. PAR 4.F,(2) OMay 28, 2024 · N506AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2024052850425Floor Support · corrodedFWD WET AREA STA 312 - 328 LBL 11 FLOOR STIFFNER HAS CORROSION. GROUNDED - YES. REMOVED CORROSION FROM FWD WET AREA, STA 312-328, LBL 11 FLOOR STIFFENER (PANEL BREAK) REF B737-800 SRM 53-10-51-OI-2, TABLE 3 ITEM (8)PER B737-800 SRM 53-10-51-1A-1, PAR. 4.F (2) May 28, 2024 · N506AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2024052850113Skin · crackedLH HORIZ LWR SKIN IS CRACKED AT STA 97 JUST FWD OF REAR SPAR. GROUNDED - YES. REMOVED CRACKED SKIN DAMAGE BY CUTOUT & INSTALLED FILLER & REPAIR DOUBLER IAW B737-800 SRM 55-10-01-2R-11 CAT B REPAIR.May 28, 2024 · N534AS · Boeing 737890 · Fuselage Main, Plate/SkinSDR ASAA2024052749890Lens · detachedEMERGENCY EXIT SIGN COVER FELL OFF A/C RIGHT NEAR OVERWING EXIT SEAT ROW 16DEF. GROUNDED - YES. INSTALLED NEW COVER ON EMERGENCY LIGHT ASSY AT ROW 16DEF REFER AMM 33-51-01 OPS CHECK GOOD.May 27, 2024 · N516AS · Boeing 737890 · Emergency LightingSDR ASAA2024052550417Skin · dentedR2 DOOR OUTER HANDLE PAN HAS LIGHT CORROSION. GROUNDED - YES. REMOVED WORN HANDLE PAN & INSTALLED NEW HANDLE PAN, REFERENCE BAC DWG#147A6502 REV B, UPON FURTHER INSPECTION FOUND DENT & FOUND HANDLE PAN TO BE OUT OF LIMITS , REFERENCE B737-800 SRM 52-10-02-1A-4May 25, 2024 · N506AS · Boeing 737890 · Service DoorsSDR ASAA2024052550416Skin · dentedR1 DOOR OUTER HANDLE PAN HAS LIGHT CORROSION. GROUNDED - YES. REMOVED DAMAGED PAN ASSY & INSTALLED NEW 141A6554Y1 PAN ASSY IAW B737-800 SRM 51-40-2 & BAC DWG 141A6516 REV.A UPON FURTHER INSPECTION FOUND DENT AND HANDLE PAN TO BE OUT OF LIMITS IAW B737-800 SRM May 25, 2024 · N506AS · Boeing 737890 · Service DoorsSDR ASAA2024052550232Pan · dentedL2 DOOR OUTER HANDLE PAN HAS LIGHT CORROSION. GROUNDED - YES. REMOVED WORN HANDLE PAN & INSTALLED NEW HANDLE PAN REFERANCE BACDWG #147A6116 REV-, UPON FURTHER INSPECTION FOUND DENT & FOUND TO BE OUT OF LIMITS, REFERENCE B737-80 SRM 52-10-02-1A-3.May 25, 2024 · N506AS · Boeing 737890 · Passenger/Crew DoorsSDR ASAA2024052549858Landing Gear · malfunctionedDURING GEAR RETRACTION ON TAKEOFF, NOSE GEAR EXTENDED AFTER MOVING GEAR HANDLE TO THE OFF POSITION. GEAR HANDLE FELT AS THOUGH IT MOMENTARILY SLIPPED OFF THE OFF DETENT. GEAR INDICATED NOSE GEAR DOWN AND GREEN, MAINS RETRACTED (NO LIGHTS). GEAR WAS CYCLED DOWNMay 25, 2024 · N565AS · Boeing 737890 · Landing Gear Retraction/Extension SystemSDR ASAA2024052450721Floor Support · corrodedAFT PIT FLOOR SUPPORT HAS CORROSION BETWEEN STA 794-807 RBL 13.84. GROUNDED - YES. REMOVED THE CORROSION FROM THE AFT PIT FLOOR SUPPORT AT STA 794-807, RBL 13.84 IAW B737-800 SRM 53-00-53-1A-2.2.0 ORIG THICKNESS IS .070" IAW B737-800 SRM 53-60-53-01-2 TABLE 2.May 24, 2024 · N506AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2024052450424Shield · corrodedAFT PIT, DOOR SURROUND FWD SHIELD IS CORRODED. GROUNDED - YES. REMOVED DAMAGE FROM AFT PIT DOOR SURROUND FWD SHIELD IAW B737-800 SRM 53-60-15-1A-1, ORIGIN'L MATERIAL WAS .050 IAW B737-800 SRM 53-60-15-01-1 100% MATERIAL LOSS. FOUND TO BE OUT OF LIMITS IAW B737May 24, 2024 · N506AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2024052450423Floor Support · corrodedAFT PIT FLOOR SUPPORT HAS CORROSION BETWEEN STA 727 AND 727B RBL 13.84. GROUNDED - YES. REMOVED CORROSION FROM AFT PIT FLOOR SUPPORT BETWEEN STA 727 TO 727B RBL 13.84 IAW B737-800 SRM 53-00-53-1A-2 ORIG. THICKNESS IS .070" IAW B737-800 SRM 53-60-53-01-2 TABLE May 24, 2024 · N506AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2024052450422Transition Panel · corrodedAFT PIT R/H TRANSITION PANEL HAS CORROSION BETWEEN STA 727 AND 727F+11. GROUNDED - YES. REMOVED CORROSION FROM AFT PIT R/H TRANSITION PANEL AT STA 727 TO 727F+11 IAW B737-800 SRM 53-00-53-1A-2. ORIG THICKNESS IS .040" IAW B737-800 SRM 53-60-53-10-2 TABLE 2. REMay 24, 2024 · N506AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2024052450421Transition Panel · corrodedAFT PIT L/H TRANSITION PANEL CORROSION BETWEEN STA 727 AND 727F+11 GROUNDED - YES. REMOVED CORROSION FROM AFT PIT L/H TRANSITION PANEL AT STA 727 TO 727 F+11 IAW B737-800 SRM 53-00-53-1A-2-0, 100% MATERIAL LOSS, FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-0May 24, 2024 · N506AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2024052450420Web · corrodedAFT PIT DOOR THRESHOLD WEB IS CORRODED. GROUNDED - YES. REMOVED DAMAGE FROM AFT PIT THRESHOLD WEB IAW ASA B737-800 SRM 53-60-15-1A-1 ORIGINAL MATL THKS .050 PER ASA B737-800 SRM 53-60-15-OI-1 TABLE ITEM 2 REMOVED .009 MATL .041 REMAINING MATL FOUND TO BE OUT OMay 24, 2024 · N506AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2024052450231Strap · corrodedAFT PIT, DOOR SURROUND LOWER MAIN SILL STRAP IS CORRODED BETWEEN STA 767 AND 787. GROUNDED - YES. REMOVED DAMAGE FROM LOWER MAIN SILL STRAP IAW B737-800 SRM 53-60-15-1A-1. ORIG. THICKNESS .080 PER B737-800 SRM 53-60-15-0I-1.REMOVED .037. REMAINING THICKNESS ISMay 24, 2024 · N506AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2024052450225Attach Angle · corrodedAFT PIT, DOOR SURROUND FWD SHIELD ATTACH ANGLE IS CORRODED. GROUNDED - YES. REMOVED DAMAGE FROM AFT PIT FWD SHIELD ATTACH ANGLE IAW B737-800 SRM 53-60-15-1A-1. ORIGN'L MATERIAL WAS .050 IAW B737-800 SRM 53-60-15-01-1. REMOVED .020, REMAINING IS .030. FOUND TO May 24, 2024 · N506AS · Boeing 737890 · Fuselage Main, StructureSDR ASAA2024052350419Floor Support · crackedMAIN CABIN UNDER FLOOR STA 540 PANEL SUPPORT CRACKED AT RBL 0 - RBL 10. GROUNDED - YES. REMOVED PANEL SUPPORT IAW B737-800 SRM 51-40-02. NEW PLATE PART . DRILLED TO FIT IAW B737-800 SRM 51-40-05. INSTALLED PANEL SUPPORT IAW B737-800 SRM 51-40-02 REF AIPC. 53-May 23, 2024 · N506AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2024052350415Floor Panel · delaminatedMAIN CABIN AFT WET AREA FLOOR BOARD DELAME P/N 147A5810-136. GROUNDED - YES. COMPLETED PERMANENT REPAIR OF MAIN CABIN AFT WET AREA FLOOR BOARD DELAMINATION PN 147A5810-136 IAW B737-800-SRM-53-00-50-2R-1 AND 53-00-50-2R-4.May 23, 2024 · N506AS · Boeing 737890 · Fuselage Floor PanelSDR ASAA2024052350410Floor Panel · delaminatedMAIN CABIN AFT WET AREA FLOOR BOARD DELAME P/N 147A5810-28. GROUNDED - YES. COMPLETED PERMANENT REPAIR OF MAIN CABIN AFT WET AREA FLOOR BOARD DELAMINATION P/N 147A5810-28 IAW B737-800-SRM-53-00-50-2R-1 AND 53-00-50-2R-4.May 23, 2024 · N506AS · Boeing 737890 · Fuselage Floor PanelSDR ASAA2024052350409Floor Panel · delaminatedMAIN CABIN AFT WET AREA FLOORBOARD DELAME P/N 147A5810-27. GROUNDED - YES. COMPLETED PERMANENT REPAIR OF MAIN CABIN AFT WET AREA FLOOR BOARD DELAMINATION PN 147A5810-27 IAW B737-800-SRM-53-00-50-2R-1 AND 53-00-50-2R-4.May 23, 2024 · N506AS · Boeing 737890 · Fuselage Floor PanelSDR ASAA2024052350395Floor Panel · delaminatedMAIN CABIN AFT WET AREA FLOOR BOARD DELAME P/N 147A5810-23. GROUNDED - YES. COMPLETED PERMANENT REPAIR OF MAIN CABIN AFT WET AREA FLOOR BOARD DELAMINATION P/N 147A5810-23 IAW B737-800-SRM-53-00-50-2R-1 AND 53-00-50-2R-4.May 23, 2024 · N506AS · Boeing 737890 · Fuselage Floor PanelSDR ASAA2024052350394Floor Panel · delaminatedMAIN CABIN AFT WET AREA FLOOR BOARD DELAME P/N 147A5810-137. GROUNDED - YES. COMPLETED PERMANENT REPAIR OF MAIN CABIN AFT WET AREA FLOORBOARD DELAMINATION PN 147A5810-137 IAW B737-800-SRM-53-00-50-2R-1 AND 53-00-50-2R-4.May 23, 2024 · N506AS · Boeing 737890 · Fuselage Floor PanelSDR ASAA2024052350086Floorboard · delaminatedMAIN CABIN AFT WET AREA FLOOR BOARD DELAME P/N 147A5810-90. GROUNDED - YES. REPAIRED MAIN CABIN AFT WET AREA FLOOR BOARD NOTED DAMAGE BY PREFORMING PERMANENT WET LAY UP REPAIR IAW B737 SRM 53-00-50-2R-0, 53-00-50-2R-1.May 23, 2024 · N506AS · Boeing 737890 · Fuselage Floor PanelSDR ASAA2024052349859Cover · detachedOVERWING EXIT SIGN FELL DOWN. GROUNDED - YES. RE-INSTALLED LENS COVER OF THE OVERWING EXIT SIGN OP CHECKED LIGHT GOOD.May 23, 2024 · N586AS · Boeing 737890 · Emergency LightingSDR ASAA2024052249772Light · brokenL1 DOOR EMERGENCY BOARDING LIGHT, LOCATED LOW AND ON THE FORWARD SIDEWALL, LENSE COVER IS BROKEN. GROUNDED - YES. RELAMPED AND REPLACED LENS COVER. OPS NORMAL.May 22, 2024 · N548AS · Boeing 737890 · Passenger Compartment LightingSDR ASAA2024052150498Rib · crackedLEFT HORZ. STAB INTERNAL LOCATED ABOUT SS 139, BETWEEN FRONT AND REAR SPAR ATTACH RIB CRACKED. GROUNDED - YES. REMOVED 2(EA) FWD SPAR WEBS, REMOVED DAMAGED AREA. FABRICATED REPAIR PARTY P/N: BAC1490-2793 EXTRUSION 7075 T6 PO:1085311.1 P/N:BAC 1505-1008162 7075May 21, 2024 · N594AS · Boeing 737890 · Horizontal Stabilizer, Spar/RibSDR ASAA2024052150496Rib · crackedLEFT HORZ. STAB INTERNAL LOCATED ABOUT SS 102, BETWEEN FRONT AND REAR SPAR ATTACH RIB HAS FWD CRACKS. (STREAMER AND DOT ATTACH). GROUNDED - YES. REMOVED DAMAGED AREA. FABRIATED REPAIR PARTS P/N: BAC1490-2793 EXTRUSION 7075T6 PO:1085311.1, P/N: BAC1505-100352 7May 21, 2024 · N594AS · Boeing 737890 · Horizontal Stabilizer, Spar/RibSDR ASAA2024052150393Floor Panel · delaminatedFLOOR PANEL DELAME FWD WET AREA P/N 141A5810-763. GROUNDED - YES. COMPLETED PERMANENT REPAIR OF FLOOR PANEL DELAMINATION ON FWD WET AREA PANEL PN 141A5810-763 IAW B737-800-SRM-53-00-50-2R-1 AND 53-00-50-2R-4.May 21, 2024 · N506AS · Boeing 737890 · Fuselage Floor PanelSDR ASAA2024052150183Floor Panel · damagedFLOOR PANEL 141A5810-728 HAS 8 BAD INSERTS AND EDGE DAMAGE. GROUNDED - YES. REPAIRED FLOOR PANEL 141A5810-728 AND REMOVED AND REPLACED ALL INSERTS IAW B737-800 SRM 53-00-50-2R-4.May 21, 2024 · N594AS · Boeing 737890 · Fuselage Floor PanelSDR ASAA2024052150182Floor Panel · damagedFLOOR PANEL 147A5810-28 HAS COMPOSITE DAMAGE AND BAD INSERTS. GROUNDED - YES. REPAIRED FLOOR PANEL 147A5810-28 AND REPLACED INSERTS IAW B737-800 SRM 53-00-50-2R-4.May 21, 2024 · N594AS · Boeing 737890 · Fuselage Floor PanelSDR ASAA2024052150181Floor Panel · damagedFLOOR PANEL 147A5810-23 HAS COMPOSITE DAMAGE AND BAD INSERTS. GROUNDED - YES. REPAIRED FLOOR PANEL 147A5810-23 AND REPLACED INSERTS IAW B737-800 SRM 53-00-50-2R-4.May 21, 2024 · N594AS · Boeing 737890 · Fuselage Floor PanelSDR ASAA2024052150180Floor Panel · damagedFLOOR PANEL 146A5810-512 HAS COMPOSITE DAMAGE. GROUNDED - YES. REPAIRED FLOOR PANEL 146A5810-512 AND REPLACED INSERTS IAW B737-800 SRM 53-00-50-2R-4.May 21, 2024 · N594AS · Boeing 737890 · Fuselage Floor PanelSDR ASAA2024052150179Floor Panel · damagedFLOOR PANEL 144A5810-126 HAS COMPOSITE DAMAGE AND BAD INSERTS. GROUNDED - YES. REPAIRED FLOOR PANEL 144A5810-126 AND REPLACED 3EA INSERTS IAW B737-800 SRM 53-00-50-2R-7.May 21, 2024 · N594AS · Boeing 737890 · Fuselage Floor PanelSDR ASAA2024052150085Floor Panel · delaminatedMAIN CABIN FLOOR PANEL DELAME P/N 141A5810-236. GROUNDED - YES. REPAIRED FLOOR PANEL P/N 141A5810-236 NOTED DAMAGE BY PREFORMING PERMANENT WET LAY UP REPAIR IAW B737 SRM 53-00-50-2R-1, 53-00-50-2R-0.May 21, 2024 · N506AS · Boeing 737890 · Fuselage Floor PanelSDR ASAA2024052150080Floor Panel · delaminatedFLOOR PANEL DELAME FWD WET AREA P/N 141A5810-728. GROUNDED - YES. REPAIRED FLOOR PANEL P/N 141A5810-728 NOTED DAMAGE BY PREFORMING PERMANENT WET LAY UP REPAIR IAW B737 SRM 53-00-50-2R-1, 53-00-50-2R-0.May 21, 2024 · N506AS · Boeing 737890 · Fuselage Floor PanelSDR ASAA2024052149776Lamp · inoperativeR1 EMERGENCY SLIDE LIGHT INOP. GROUNDED - YES. REMOVED AND REPLACED LAMP AT R1 EMERGENCY SLIDE REF AMM 33-51-04. OPS CHECK GOOD.May 21, 2024 · N585AS · Boeing 737890 · Emergency LightingSDR ASAA2024052050375Web · gougedAREA BETWEEN STA 500A-500B LBL64 HAS A GOUGE ON LOWER SIDE AROUND FASTENER HOLE. GROUNDED - YES. ACCOMPLISHED REPAIR PER EA#800-53EA-27094, ORIGINAL THICKNESS .063, MAT LOSS .050, REMAINING THICKNESS .013 AREA OUT OF LIMITS PER B737-800 SRM 53-30-13. THIS IS AMay 20, 2024 · N594AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2024052050185Floorbeam · corrodedSTA 986 BETWEEN LBL 9 AND RBL 27.5 UPPER T-CAP HAS SCRIBE MARKS. GROUNDED - YES. UPON EVALUATION OF SCRIBE LINES ON STA 986 UPPER T-CAP. FOUND UNDERLYING CORROSON ON PREVIOUS REPAIR. REMOVED CORROSION FROM UPPER T-CAP PREVIOUS REPAIR STA 986. ORIGINAL MAT THICMay 20, 2024 · N594AS · Boeing 737890 · Fuselage Main, Floor BeamSDR ASAA2024052050184Floor Support · corroded950(RH HAND SIDE) INTERCOSTAL / FLOOR SUPPORT HAS CORROSION AT HOLE. GROUNDED - YES. BLENDED CORROSION ORINGINAL THICKNESS, FROM PART, .080, MAT LOSS .018, NEW THICKNESS .062 THERE ARE NO SRM ALLOWABLE LIMITS , REMOVED DAMAGE SUPPORT AND INSTALLED P# 147A5676-May 20, 2024 · N594AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2024051949732Light · brokenL1 DOOR EMERGENCY EXIT LIGHT COVER FELL OFF. GROUNDED - YES. FOUND L1 DOOR LOWER EMER EXIT SIGN ASSEMBLY TAB BROKEN. REMOVED & REPLACED L1 EMER EXIT FLOOR LIGHT ASSY& COVER REF AMM 33-51-01-960-802, OPS CHK GOOD.May 19, 2024 · N577AS · Boeing 737890 · Emergency Lighting
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