Boeing 737-7CT

Service difficulty reports · 2,414

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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 = '7377CT'
  ORDER BY difficulty_date DESC"

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SDR SWAA2025031095371Bulkhead · crackedB.S. 663 LOWER COMPOSITE BULKHEAD IS CRACKED AT L.B.L. 19; W.L. 152. <[01] APPLIED INTERIM REPAIR AT THE LOWER VAPOR BARRIER LBL 19 BS663 WL 152 IAW SRM 57-10-10-2R-2; [02] VERIFIED ALL STEPS CORRECTION ACTION ITEM 1 MEASUREMENT FIELD COMPLETE; CARD COMPLETE.Feb 12, 2025 · N566WN · Boeing 7377CT · Fuselage Main, KeelSDR SWAA2025030695365Angle · crackedB.S. 663 LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE IS CRACKED AT R.B.L. 45; W.L. 167.<[01] UPDATED STEPS 1-3;[02] REMOVED AND REPLACED BS 663 R/H LOWER COMPOSITE BULKHEAD UPPER ANGLE IAW SRM 51-40-02 AND DWG 111A1000 REV:;[03] VERIFIED COMPLETION CORRECTIVE Feb 12, 2025 · N566WN · Boeing 7377CT · Fuselage Main, BulkheadSDR SWAA2025021294982Battery Pack · inoperativeALL EMERGENCY LIGHTS RELATED TO BATTERY PACK M2335 INOP<[01] REMOVED; REPLACED WITH SERVICEABLE UNIT; AND PERFORMED GOOD INSTALLATION TEST OF M2335 BATTERY PACK AS DOCUMENTED ON ATTACHED STEPS.;[02] VERIFIED CORRECTIVE ACTION 1Feb 11, 2025 · N7825A · Boeing 7377CT · Emergency LightingSDR SWAA2025021094370Slide · out of positionR2 DOOR ESCAPE SLIDE DRAGS ON THE FLOOR<[01]. PROPERLY INSTALLED R2 DOOR ESCAPE SLIDE IAW AMM 25-66-01-400-801;[02] VERIFIED CORRETIVE ACTION ENTRY 1.Feb 9, 2025 · N567WN · Boeing 7377CT · Escape SlideSDR SWAA2025021093811Battery Pack · no testEMERGENCY LIGHTS RELATED TO BATTERY PACK M2355 FAIL TEST<[01] REPLACED EMERGENCY BATTERY PACK M2335; PERFORMED GOOD EMEREGENCY LIGHT TEST PER AMM 33-51-06-960-805;[02] VERIFIED CORRECTIVE ACTION. CARD COMPLETE.Feb 6, 2025 · N567WN · Boeing 7377CT · Emergency LightingSDR SWAA2025021093812Light · inoperativeFWD ESCAPE EMEREGENCY LIGHT OUTSIDE FWD MAIN ENTRY DOOR INOP (L731)<[01] INSTALLED NEW LIGHT AT FWD ESCAPE EMEREGENCY OUTSIDE FWD MAIN ENTRY DOOR; PERFORMED GOOD TEST PER AMM 33-51-04-960-801.;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.Feb 6, 2025 · N567WN · Boeing 7377CT · Emergency LightingSDR SWAA2025020693656Light · inoperativeR1 DOOR OUTER EMERGENCY LIGHT INOP<[01] REPLACED R1 DOOR EMERGENCY EXIT LIGHT IAW AMM 33-51-04.Feb 6, 2025 · N7828A · Boeing 7377CT · Emergency LightingSDR SWAA2025021091146Scuff Plate · missingAFT AND FWD SCUFF PLATES (CORNERS) MISSING AT FWD CARGO BAY<[01] 01 - REMOVED AND REPLACED PER [AMM 53-11-02-420-801-NG (CARGO DOOR SCUFF PLATE - INSTALLATION - PERMANENT)];[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.Jan 29, 2025 · N567WN · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2025021389623Threshold Web · corroded.MULTIPLE SPOT WITH CORROSION ON FCB DOOR CUTOUT SURROUND THRESHOLD BS440+6 TO BS460+13 RBL30;WL156<[01] FCB DOOR CUTOUT SURROUND THRESHOLD REPAIR BY REPLACEMENT PER 51-10-02-0G-0. RECIVED NEW WEB P/N 654A0003-58 LOT. 1588648-1<BR>LOCATED AND DRLLED NEW WEB IAJan 25, 2025 · N7825A · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2025021389624Threshold · corrodedMULTIPLE SPOT WITH CORROSION ON ACB DOOR CUTOUT SURROUND THRESHOLD BS794.3 TO BS827+3 RBL30 WL156.<[01] UPDATED STEP 3;[02] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)];[03] VERIFJan 25, 2025 · N7825A · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2025021388732Seat Track · corrodedCORROSION ON SEAT TRACK RBL 45.5 BS616+10; BS616+13; BS616+14; BS639+15; BS663+15; BS663+18; WL 208 (MARKED)<[01] CERTIFY ACTION #2;[02] UPDATED MEASUREMENT TABLE;[03] PARTIAL UPDATE STEP #4;[04] REMOVED AND REMPLACED SEAT TRACK FROM RBL 45 BS 540 TO BS 727B WJan 23, 2025 · N7825A · Boeing 7377CT · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2025021388731Seat Track · corrodedCORROSION ON SEAT TRACK RBL 45.5 BS540+1.5; BS540+8; BS540+11.5; BS540+19; BS559+7; BS559+15; BS578+13; BS597+4; BS597+8.5; BS597+12; BS597+13 (MARKED)<[01] SEAT TRACK AT BS 540-727B RBL45.5 IS OUT OF LIMITS AT BS 663+15. TO BE REPLACED ON TTG8Q00YA3DT.;[02] VJan 23, 2025 · N7825A · Boeing 7377CT · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2025021388733Seat Track · corrodedCORROSION ON SEAT TRACK RBL 45.5 BS706+4; BS706+5.5; BS706+7; BS706+17.5; BS727+13; BS727+17.5; BS727A+6.5; BS727A+8.5 WL 208 (MARKED<[01] SEAT TRACK AT BS 540-727B; RBL 45 IS OUT OF LIMITS AT BS 663+15. TO BE REPLACED ON TTG8Q00YA3DT;[02] VERIFIED CORRECTIVE Jan 23, 2025 · N7825A · Boeing 7377CT · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2025021288726Floor Panel · pulledFLOOR PANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATED NEW FLOOR PANEL 241AF IAW SRM 53-00-50-2R-0 AND BOEING DWG 144A5810 ID: 0127.;[02] VERIFIED JOB COMPLETEJan 23, 2025 · N7825A · Boeing 7377CT · Fuselage Floor PanelSDR SWAA2025021088724Floor Panel · pulledFLOOR PANEL 231XF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231XF HAS BEEN REPLACED IAW SRM 53-00-50-2R-0 PARA 1. A. NOTE:;[02] VERIFIED CORRECTIVE ACTION ITEM 1.Jan 23, 2025 · N7825A · Boeing 7377CT · Fuselage Floor PanelSDR SWAA2025021088727Floor Panel · pulledFLOOR PANEL 241DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] 04 - REPAIRED PULLED STRANDS ON UPPER SURFACE PER [SRM 53-00-50-2R-0-A00938 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)];[02] VERIFIED JOB COMPLETEJan 23, 2025 · N7825A · Boeing 7377CT · Fuselage Floor PanelSDR SWAA2025021388720Scuff Plate · crackedAFT CARGO COMPARTMENT FWD CORNER SCUFFPLATE IS CRACKED.<[01] VERIFIED APPLICABILITY OF SRM 53-60-15-2R-1;[02] REPAIRED AFT CARGO COMPARTMENT FWD CORNER SCUFFPLATE PER SRM 53-60-15-2R-1. APPLIED CHEMICAL CONVERSION COATING PER SOPM 20-43-03; APPLIED PROTECTIVE Jan 22, 2025 · N7825A · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2025021088431Floorbeam · crackedCRACKED PANEL BREAK BS 540 BL 0 - RBL 25 WL 207 (MARKED)<[01] REMOVED AND REPLACED PANEL BREAK AT BS540 BL0-RBL25 WL207 PER SRM 51-40-02 AND DWG:143A0060 REV:A;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.Jan 22, 2025 · N567WN · Boeing 7377CT · Fuselage Main, Floor BeamSDR SWAA2025021088432Floorbeam · canningCRACKED PANEL BREAK BS 540 BL 0 - LBL 25 WL 207 (MARKED)<[01] REMOVED AND REPLACED PANEL BREAK AT BS540 BL0-LBL25 WL207 PER SRM 51-40-02 AND DWG:143A0060 REV:A;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.Jan 22, 2025 · N567WN · Boeing 7377CT · Fuselage Main, Floor BeamSDR SWAA2025021088206Seat Track · corrodedCORROSION ON SEAT TRACK LBL 24.75 BS500A+8; BS500A+11; BS500A+14.5; BS500A+17; BS500D+9.5; BS 520+5.5 TO BS520+11 WL 208 (MARKED)<[01] BS 480 TO BS 520 LBL25 SEAT TRACK WILL REPLACE DUE TO MECHANICAL DAMAGE ACCORDING TO CUST# TTG8Q00Y9C8F.<BR>UPON FURTHER INVEJan 21, 2025 · N567WN · Boeing 7377CT · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2025021088212Seat Track · corrodedCORROSION ON SEAT TRACK LBL 45.5 BS480+16.5; BS500A+5; BS500A+8; BS500B+16; BS500B+18.5; BS00D+9.5 WL 208 (MARKED)<[01] SEAT TRACK WILL REPLACE DUE TO MECHANICAL DAMAGE ACCORDING TO CUSTOMER # TTG8Q00Y9C43.;[02] VERIFIED ITEM 1Jan 21, 2025 · N567WN · Boeing 7377CT · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2025021087806Skin · crackedCRACK ON RH LOWER HORIZONTAL STABILIZER SKIN AT STAB STA 193.90; 18.5' FROM FWD EDGE; .35' IN LENGTH (MARKED) <[01]. REPAIRED R/H HORIZONTAL STAB LOWER SKIN AT STAB STA 193.90 IAW SRM 55-10-01-2R-11 REPAIR 11.; [02] VERIFIED ACTION ITEMS AND TASK CARD COMPLETEJan 20, 2025 · N567WN · Boeing 7377CT · Horizontal Stabilizer, Plate/SkinSDR SWAA2025021387665Panel · debondedRIGHT WING L/E PANEL 621DB HAS DISBONDS AT I/B FWD CORNER AND FWD PANEL CUTOUT CORNERS<[01] RIGHT WING L/E PANEL 621DB WAS REPAIRED IAW SRM 51-70-05-2R-6;[02] JOB COMPLETE.Jan 19, 2025 · N7825A · Boeing 7377CT · Wing, Plate/SkinSDR SWAA2025021087557Web · crackedRIGHT WING T/E UPPER SURFACE PANEL AT ORSS 276; TRANSVERSE WEB IS CRACKED AT O/B UPPER FASTENER<[01] REMOVED R/W T/E UPPER SURFCE PANEL TRANSVERSE WEB AT ORSS 276 IAW SRM 51-40-02-OG-0 PARA. 4.;[02] VERIFIED ITEM 1Jan 19, 2025 · N567WN · Boeing 7377CT · Wing Miscellaneous StructureSDR SWAA2025021087563Rib · crackedL-CLIP COMMON TO L/W I/B SIDE OF DEFLECTION CONTROL RIB AND UPPER SURFACE PANEL ORSS 271 IS CRACKED <[01]. REMOVED AND REPLACED L- CLIP COMMON TO L/W I/B SIDE OF DEFLECTION CONTROL RIB AND UPPER SURFACE PANEL AT ORSS 271 IAW SRM 51-40-02-0G-0 PARA. 4.;[02] VERJan 19, 2025 · N567WN · Boeing 7377CT · Wing, Rib/BulkheadSDR SWAA2025021187233Panel · debondedRIGHT WING L/E PANEL 621HB HAS DISBOND AT I/B FWD CORNER<[01] 04 - REPAIRED PER [SRM 51-70-05-2R-6-A00737 (REPAIR 6 - REPAIR OF DAMAGE TO THE EDGEBAND OF A HONEYCOMB PANEL - AIRFRAME - PERMANENT)];[02] VERIFEID CORRECTIVE ACTION 1Jan 18, 2025 · N567WN · Boeing 7377CT · Leading Edge DevicesSDR SWAA2025021087434Rib · crackedLEFT HORIZONTAL STAB REMOVABLE L/E 331B RIB #3 IS CRACKED<[01] 1. KENNETH RUDIO (TECHNICIAN); 24-JAN-2025 22:07 UTC<BR>REMOVED AND REPLACED L/H HORIZONTAL STAB. L/E #3 RIB IAW SRM 51-40-02-0G-0 PARA. 4.;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMJan 18, 2025 · N567WN · Boeing 7377CT · Horizontal Stabilizer, Spar/RibSDR SWAA2025021087435Rib · crackedLEFT HORIZONTAL STAB REMOVABLE L/E 331B RIB #5 IS CRACKED<[01] REMOVED AND REPLACED L/H HORIZONTAL STAB. L/E #5 RIB IAW SRM 51-40-02-0G-0 PARA. 4.;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.Jan 18, 2025 · N567WN · Boeing 7377CT · Horizontal Stabilizer, Spar/RibSDR SWAA2025021087226Floor Panel · pulledFLOOR PANEL 231XF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231XF UPPER SKIN WITH 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 COMPLETE.Jan 18, 2025 · N567WN · Boeing 7377CT · Fuselage Floor PanelSDR SWAA2025021087227Floor Panel · pulledFLOOR PANEL 231YF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231YF UPPER SKIN WITH 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] ADDED PART INSTALL INFO.Jan 18, 2025 · N567WN · Boeing 7377CT · Fuselage Floor PanelSDR SWAA2025021087224Floor Panel · pulledFLOOR PANEL 231ZF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231ZF; WITH UPPER SKIN AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0.;[02] JOB COMPLETE.Jan 18, 2025 · N567WN · Boeing 7377CT · Fuselage Floor PanelSDR SWAA2025021087228Floor Panel · pulledFLOOR PANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241AF UPPER SKIN; WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0.;[02] JOB COMPLETE.Jan 18, 2025 · N567WN · Boeing 7377CT · Fuselage Floor PanelSDR SWAA2025021087230Floor Panel · pulledFLOOR PANEL 242AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 242AF; UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0.;[02] JOB COMPLETE.Jan 18, 2025 · N567WN · Boeing 7377CT · Fuselage Floor PanelSDR SWAA2025021087229Floor Panel · pulledPANEL 241DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PANEL 241DF WITH UPPER SKIN HAS AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE IAW SRM 53-00-50-2R-0; DWG 144A5810 ID:0128.;[02] JOB COMPLETE.Jan 18, 2025 · N567WN · Boeing 7377CT · Fuselage Floor PanelSDR SWAA2025021086864Threshold · corrodedFWD CARGO SUBTHRESHOLD HAS CORROSION IN MULTIPLE AREAS<[01] UPON FURTHER INVESTIGATION; FOUND TO BE OUT OF LIMIT AS PER SRM 53-30-15-1A-1. REPAIR BY REPLACEMENT.;[02] UPDATED STEP 4;[03] UPDATED STEP 5;[04] REPLACED FWD CARGO BAY SUB THRESHOLD IAW SRM 51-40-02Jan 17, 2025 · N567WN · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2025021086866Pressure Deck · crackedCRACK IN LH HORIZONTAL PRESSURE DECK BS 672 WL 202 LBL35. CRACK IS .650 INCHES IN LENGTH. MARKED IN RED INK.<[01] REPAIRED LH HORIZONTAL PRESSURE DECK WEB AT BS 663 TO BS 675 LBL 30 TO LBL 60 PER SRM 53-40-51-2R-2 REPAIR 2 FIG. 202.;[02] TASK CARD COMPLETED.;[Jan 17, 2025 · N567WN · Boeing 7377CT · Fuselage Main, StructureSDR SWAA2025021086867Pressure Deck · crackedCRACK IN RH HORIZONTAL PRESSURE DECK BS 664.5 WL 202 RBL 43. CRACK IS .250 INCHES LONG AND MARKED IN RED INK.<[01] REMOVED THE DAMAGE PART OF THE WEB AT BS 663.75 - 6BS75; RBL38 - 60; WL 202; PER SRM 53-40-51-2R-2 PAR. 4. C. FIG. 202.<BR><BR>INSTALLED REPAIR RJan 17, 2025 · N567WN · Boeing 7377CT · Fuselage Main, StructureSDR SWAA2025021086862Web · corrodedAFT CARGO SUBTHRESHOLD WEB HAVE CORROSION MULTIPLE AREAS.<[01] REMOVE AND REMPLACE AFT CARGO SUBTHRESHOLD WEB SRM 51-40-02 DWG 146A8340 ID:0024 REV: A;[02] REMOVED AND REMPLACED AFT CARGO SUBTHRESHOLD WEB BETWEEN BS 794 TO BS 847 PER SRM 51-40-02 DWG 146A8340 Jan 17, 2025 · N567WN · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2025021086863Strap · corrodedAFT CARGO BAY TENSION STRAP HAS CORROSION APPROX BS802; RBL25.<[01] CORROSION ON TENSION STRAP AT ACB BS 806 ; RBL 25 IN L=2' X W=1' X D=0.030' FROM ORIGINAL THICKNESS 0.100' THEREFORE FOUND TO BE OUT OF LIMITS; TENSION STRAP WILL BE REPAIRED BY REPLACEMENT OFJan 17, 2025 · N567WN · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2025021086500Scuff Plate · crackedAFT CARGO FWD SCUFF PLATE IS CRACKED <[01]. WELDED THE CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT NUMBER 1131216 PER SRM 53-60-15-2R-1 PARA 4.B.(4). REFERRED TO BAC 5975. EQUIPMENT USED; WELDING MACHINE I.D. 10583; CAL DATE 01/2025; APPLIED CHEMICAL CONVEJan 16, 2025 · N567WN · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2025021086861Vapor Barrier · crackedCRACKED VAPOR BARRIER IN THE MAIN WHEEL WELL BS663 LBL15 WL147. MARKED <[01]. CRACKED VAPOR BARRIER BS663 LBL15 WL147 WAS REPAIRED IAW SRM 51-70-04-2R-10;[02] VERIFIED CORRECTIVE ACTION.Jan 16, 2025 · N567WN · Boeing 7377CT · Wing Miscellaneous StructureSDR SWAA2025021086319Doubler · damagedCUSTOMER REQUEST: DOUBLER AT BS 407 BETWEEN S-1 AND S-2L REQUIRES REMOVAL AND REPAIR DOUBLER AT BS 407 STR 1 - STR 2L/H <[01]. `THE DAMAGE WAS REPAIRED PER EA 25-153-00120. CONTINUED AIRWORTHINESS REQUIREMENTS ARE TRACKING ON EA 25-153-00120-DTI.' ENSURE THE Jan 15, 2025 · N567WN · Boeing 7377CT · Fuselage Miscellaneous StructureSDR SWAA2025010683384Wedge · delaminatedINBOARD MAIN FLAP TRAILING EDGE WEDGE ASSEMBLY DELAMINATED.<[01] REMOVED DAMAGED OTBBOARD T/E WEDGE FROM RT MAIN FLAP; LOCATED AND DRILLED NEW WEDGE PER SRM 51-40-06;[02] REMOVED AND REPLACED WEDGE PER M/M 27-51-00Jan 6, 2025 · N7821L · Boeing 7377CT · Trailing Edge FlapsSDR SWAA2024122379712Flap · delaminatedRT WING I/B MAIN FLAP WEDGE LOWER SKIN DELAMINATED STARTING FROM 2.4 IN. FROM O/B EDGE. MEASURES APPROX. 7.6 IN. LENGTH; 4.2 IN. WIDTH.<[01] PERFORMED TEMPORARY REPAIR ON RH MAIN INBOARD FLAP TRAILING EDGE REF SRM 57-53-01-1A-1 SECTION 4. A (7) ZONE 3 LOWER SKDec 20, 2024 · N7821L · Boeing 7377CT · Trailing Edge FlapsSDR SWAA2024122079706Battery Pack · failedM1670 FAILED CAPACITY CHECK<[01] R/R M1670 BATTERY PACK PER AMM 33-51-06Dec 20, 2024 · N7821L · Boeing 7377CT · Emergency LightingSDR SWAA2024122079698Battery Pack · failedM1673 AND M1672 FAILED CAPACITY CHECK<[01] R/R M1673 AND M1672 BATTERY PACKS PER AMM 33-51-06Dec 20, 2024 · N7821L · Boeing 7377CT · Emergency LightingSDR SWAA2024120273056Bustle · out of adjustFWD SERVICE DOOR SLIDE BUSTLE TRIM HAS SHARP EDGE ON LOWER RIGHT CORNER.<[01] ADJ DOOR BUSTLE CORRECTED SHARP EDGE PER AMM 52-41-31. AC OK FOR SERVICE.Dec 1, 2024 · N7881A · Boeing 7377CT · Escape SlideSDR SWAA2024120271900Seal · crackedLEFT HORIZONTAL UPPER FORWARD SLIDER SEAL AND TRACK IS CRACKED; BUCKLED.<[01] OK TO CONTINUE PER CDL 55-10-1. AUTHORIZATION # 225145.;[02] REMOVED AND REPLACED FWD. MID; INNER TRACK STRIP P/N 181A8030U57 PER SRM 51-40-02.;[03] C/W STEPS 1-3.;[04] REPLACED LH HNov 26, 2024 · N569WN · Boeing 7377CT · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2024120273333Track · buckledLEFT HORIZONTAL UPPER FORWARD SLIDER SEAL AND TRACK IS CRACKED; BUCKLED.<[01] OK TO CONTINUE PER CDL 55-10-1. AUTHORIZATION # 225145.;[02] REMOVED AND REPLACED FWD. MID; INNER TRACK STRIP P/N 181A8030U57 PER SRM 51-40-02.;[03] C/W STEPS 1-3.;[04] REPLACED LH HNov 26, 2024 · N569WN · Boeing 7377CT · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2024112771594Seal · crackedRIGHT HORIZONTAL LOWER FORWARD SLIDER SEAL IS CRACKED; BUCKLED.<[01] REPLACED RH HORIZONTAL STAB LOWER FWD SLIDER SEAL PER AMM 53-31-31.;[02] VERIFIED REPLACED RH HORIZONTAL STAB LOWER FWD SLIDER SEAL PER AMM 53-31-31;[03] RII IS C/W. VERIFIED REPLACED RH HORINov 26, 2024 · N569WN · Boeing 7377CT · Horizontal Stabilizer Miscellaneous Structure
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