# Service difficulty reports: N8553W A list on [N8553W](https://openairdocs.org/aircraft/N8553W.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 2 · 71 reports - [SDR SWAA2026101961042](https://openairdocs.org/sdr/SWAA2026101961042.md): Seal · cracked · Sep 22, 2026 · N8553W · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous Structure > RIGHT HORIZONTAL STAB, UPPER FWD SLIDING SEAL WAS CRACKED. REMOVED THE FWD SLIDING SEAL IAW AMM 53-31-31. - [SDR SWAA2026101934298](https://openairdocs.org/sdr/SWAA2026101934298.md): Seal · cracked · Sep 22, 2026 · N8553W · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous Structure > LEFT HORIZONTAL STAB UPPER FWD SLIDING SEAL WAS CRACKED. REMOVED & REPLACED THE LT HORIZONTAL STAB UPPER FWD SLIDING SEAL IAW AMM 53-31-31. - [SDR SWAA2026082191932](https://openairdocs.org/sdr/SWAA2026082191932.md): Battery · inoperative · Aug 17, 2026 · N8553W · Boeing 7378H4 · Emergency Equipment > ONE AFT LEFT FA FLASHLIGHT, AND ONE AFT RT FA FLASHLIGHT INOPERATIVE. R & R THE BATTERIES IN THE FLASHLIGHTS IAW AMM 25-64-00. OPS CHKD GOOD - [SDR SWAA2026081147166](https://openairdocs.org/sdr/SWAA2026081147166.md): Battery Pack · inoperative · Aug 7, 2026 · N8553W · Boeing 7378H4 · Emergency Lighting > AFT RT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY (M1671) BATTERY PACK IAW AMM 33-51-06. - [SDR SWAA2026081146823](https://openairdocs.org/sdr/SWAA2026081146823.md): Battery Pack · inoperative · Aug 7, 2026 · N8553W · Boeing 7378H4 · Emergency Lighting > ROW 15DE AFT INTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED THE POWER SUPPLY (M1671) BATTERY PACK IAW AMM 33-51-06. - [SDR SWAA2026072002869](https://openairdocs.org/sdr/SWAA2026072002869.md): Girt Bar · loose · Jul 16, 2026 · N8553W · Boeing 7378H4 · Emergency Equipment > AFT ENTRY DOOR GIRT BAR LOOSE. REPOSITIONED AFT ENTRY GIRT BAR IAW MM 25-66-01. - [SDR SWAA2026071020144](https://openairdocs.org/sdr/SWAA2026071020144.md): Retainer · unsecure · Jul 9, 2026 · N8553W · Boeing 7378H4 · Escape Slide > FORWARD ENTRY DOOR GIRT BAR CLIP LOOSE. SECURED FWD ENTRY DOOR GIRT BAR RETAINING CLIP PER AMM 25-66-01 - [SDR SWAA2026060107562](https://openairdocs.org/sdr/SWAA2026060107562.md): Flashlight · inoperative · May 28, 2026 · N8553W · Boeing 7378H4 · Emergency Equipment > FWD FLASHLIGHT DIDNT TEST. PERFORMED GOOD TEST ON FWD FA FLASHLIGHT PER AMM 25-64-00 - [SDR SWAA2026032683410](https://openairdocs.org/sdr/SWAA2026032683410.md): Slide · low pressure · Mar 25, 2026 · N8553W · Boeing 7378H4 · Escape Slide > FWD ENTRY DOOR SLIDE NOT IN GREEN BAND<[01] REMOVED AND REPLACED FWD ENTRY SLIDE IAW MT 725-61-06 - [SDR SWAA2026021168865](https://openairdocs.org/sdr/SWAA2026021168865.md): Battery Pack · inoperative · Feb 8, 2026 · N8553W · Boeing 7378H4 · Emergency Lighting > OVERWING DOOR, EMERGENCY LIGHTS INOPERATIVE. REMOVED & INSTALLED A NEW BATTERY PACK AND PERFORMED OPS CHECK IAW AMM 33-51-06-960-805. OPS CHECKED GOOD. - [SDR SWAA2025050666301](https://openairdocs.org/sdr/SWAA2025050666301.md): Doubler · cracked · Apr 30, 2025 · N8553W · Boeing 7378H4 · Fuselage Main, Plate/Skin > ELECTRICAL GROUND POWER RECEPTACLE SURROUND DOUBLER IS CRACKED COMMON TO LOWER LATCH AREA; (ZONE 2).<[01] UPDATED TABLE;[02] REMOVED DAMAGE AND REPAIRED ELECTRICAL GROUND POWER RECEPTACLE SURROUND DOUBLER IAW SRM 53-10-15-2R-4; SRM 51-40-05-0G-0; SRM 51-40-02- - [SDR SWAA2025050664740](https://openairdocs.org/sdr/SWAA2025050664740.md): Flashlight · no test · Apr 28, 2025 · N8553W · Boeing 7378H4 · Emergency Equipment > AFT GALLEY LH SIDE FLASHLIGHT WILL NOT TEST<[01] REPLACED AFT GALLEY LH SIDE FLASHLIGHT IAW CMM 25-60-13;[02] TASK COMPLETE - [SDR SWAA2025042862861](https://openairdocs.org/sdr/SWAA2025042862861.md): Battery Pack · inoperative · Apr 24, 2025 · N8553W · Boeing 7378H4 · Emergency Lighting > FWD GALLEY EMERGENCY LIGHTS INOP<[01] FOUND FWD L/H BATTERY PACK INOP. REMOVED AND REPLACED FWD L/H BATTERY PACK REF AMM 33-51-06; OPS CHECKED GOOD. - [SDR SWAA2024110656071](https://openairdocs.org/sdr/SWAA2024110656071.md): Screw · stripped · Nov 2, 2024 · N8553W · Boeing 7378H4 · Emergency Equipment > SET SCREWS IN AFT MEGPHONE ARE STRIPPED<[01] R/R AFT MEGAPHONE PER AMM 25-64-00. - [SDR SWAA2024072918196](https://openairdocs.org/sdr/SWAA2024072918196.md): Battery Pack · inoperative · Jul 28, 2024 · N8553W · Boeing 7378H4 · Emergency Lighting > FOUND AFT ENTRY DOOR EXIT EMERGENCY LIGHT INOP.<[01] REMOVED AND REPLACED AFT RH SERVICE DOOR POWER SUPPLY BATTERY PACK. OPS CHECK GOOD. IN REF TO AMM 33-51-06. - [SDR SWAA2023112824284](https://openairdocs.org/sdr/SWAA2023112824284.md): Light · out of adjust · Nov 24, 2023 · N8553W · Boeing 7378H4 · Emergency Lighting > FWD CABIN PHOTOLUMINESCENT STRIPS ARE PARTIALLY COVERED BY CARPET<[01] REPOSITIONED FWD CABIN PHOTOLUMINESCENT STRIPS PER AMM 33-51-15 - [SDR SWAA2023112820796](https://openairdocs.org/sdr/SWAA2023112820796.md): Battery Pack · inoperative · Nov 12, 2023 · N8553W · Boeing 7378H4 · Emergency Lighting > FWD GALLEY R/H EMERGENCY LIGHTS INOP<[01] REMOVED AND REPLACED BATTERY PACK AT STA 310 PER MM 33-51-06.FWD GALLEY EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06;[02] C/W INSPECTION. - [SDR SWAA2023112820797](https://openairdocs.org/sdr/SWAA2023112820797.md): Battery Pack · inoperative · Nov 12, 2023 · N8553W · Boeing 7378H4 · Emergency Lighting > AFT GALLEY L/H EMERGENCY LIGHTS INOP<[01] REMOVED AND REPLACED STA 952L BATTERY PACK PER MM 33-51-06.AFT GALLEY EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06;[02] C/W INSPECTION. - [SDR SWAA2023112820798](https://openairdocs.org/sdr/SWAA2023112820798.md): Battery Pack · inoperative · Nov 12, 2023 · N8553W · Boeing 7378H4 · Emergency Lighting > AFT L/H CABIN EMERGENCY LIGHTS INOP<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT STA 727C L PER MM 33-51-06.AFT CABIN EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06;[02] C/W INSPECTION. - [SDR SWAA2023112813953](https://openairdocs.org/sdr/SWAA2023112813953.md): Floor Support · cracked · Oct 24, 2023 · N8553W · Boeing 7378H4 · Fuselage Miscellaneous Structure > CABIN FLOOR INTERCOSTAL CRACKED LBL-15 BETWEEN STATION 380-400<[01] REMOVED DAMAGED INTERCOSTAL ANGLE PER SRM 51-40-02. DRILLED REPLACEMENT ANGLE PER SRM 51-40-05. INSTALLED REPLACEMENT ANGLE PER SRM 51-40-02.;[02] INSPECTED AS REQUIRED. CORRECTIVE ACTION #1 - [SDR SWAA2023113013642](https://openairdocs.org/sdr/SWAA2023113013642.md): Angle · corroded · Oct 23, 2023 · N8553W · Boeing 7378H4 · Fuselage Miscellaneous Structure > FWD CARGO STA 500D/500F; LBL 25 TRANSITION ANGEL HAS CORROSION.<[01] BLENDED AREAS; REMOVED.010' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. THIS SECTION OF ANGLE TO BE REPLACED ON TTG8Q00P66RQ FROM STA. 480+10 TO 500E+10.;[02] C/W INSPECTION. - [SDR SWAA2023113013641](https://openairdocs.org/sdr/SWAA2023113013641.md): Angle · corroded · Oct 23, 2023 · N8553W · Boeing 7378H4 · Fuselage Miscellaneous Structure > FWD CARGO STA 500C/500B; LBL 25 TRANSITION ANGEL HAS CORROSION.<[01] BLENDED AREAS; REMOVED.010' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. THIS SECTION OF ANGLE TO BE REPLACED ON NR# TTG8Q00P66RQ FROM STA. 480+10 TO 500E+10.;[02] C/W INSPECT - [SDR SWAA2023113013640](https://openairdocs.org/sdr/SWAA2023113013640.md): Angle · corroded · Oct 23, 2023 · N8553W · Boeing 7378H4 · Fuselage Miscellaneous Structure > FWD CARGO STA 500A/500B; LBL 25 TRANSITION ANGEL HAS CORROSION.<[01] THIS SECTION OF ANGLE TO BE REPLACED ON NR # TTG8Q00P66RQ FROM STA. 480+10 TO 500E+10.;[02] BLENDED AREAS; REMOVED.010 MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.;[03] C/W IN - [SDR SWAA2023113013638](https://openairdocs.org/sdr/SWAA2023113013638.md): Angle · corroded · Oct 23, 2023 · N8553W · Boeing 7378H4 · Fuselage Miscellaneous Structure > FWD CARGO STA 500/500A; LBL 25 TRANSITION ANGEL HAS CORROSION.<[01] BLENDED AREAS; REMOVED.010' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. REMOVED SECTION OF TRANSITION ANGLE FROM STA. 480 +10 TO 500E + 10.;[02] FABRICATED REPAIR PARTS PER SR - [SDR SWAA2023113013631](https://openairdocs.org/sdr/SWAA2023113013631.md): Angle · corroded · Oct 23, 2023 · N8553W · Boeing 7378H4 · Fuselage Miscellaneous Structure > FWD CARGO STA 500E/500F; LBL 25 TRANSITION ANGEL HAS CORROSION.<[01] BLENDED AREAS; REMOVED.010' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. THIS SECTION OF ANGLE TO BE REPLACED ON TTG8Q00P66RQ FROM STA. 480+10 TO 500E+10.;[02] C/W INSPECTION. - [SDR SWAA2023113013630](https://openairdocs.org/sdr/SWAA2023113013630.md): Angle · corroded · Oct 23, 2023 · N8553W · Boeing 7378H4 · Fuselage Miscellaneous Structure > FWD CARGO STA 500C/500D; LBL 25 TRANSITION ANGEL HAS CORROSION.<[01] BLENDED AREAS; REMOVED.010' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. THIS SECTION OF ANGLE TO BE REPLACED ON TTG8Q00P66RQ FROM STA. 480+10 TO 500E+10.;[02] C/W INSPECTION. - [SDR SWAA2023113013628](https://openairdocs.org/sdr/SWAA2023113013628.md): Angle · corroded · Oct 23, 2023 · N8553W · Boeing 7378H4 · Fuselage Miscellaneous Structure > FWD CARGO STA 500H/500G; RBL 25 TRANSITION ANGEL HAS CORROSION.<[01] BLENDED AREAS; REMOVED.009' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-002-53-1A-2.;[02] THIS SECTION OF ANGLE TO BE REPLACED ON NR# TTG8Q00P65VC.;[03] THIS SECTION OF ANGLE TO BE REPLA - [SDR SWAA2023113013623](https://openairdocs.org/sdr/SWAA2023113013623.md): Angle · corroded · Oct 23, 2023 · N8553W · Boeing 7378H4 · Fuselage Miscellaneous Structure > FWD CARGO STA 500D/500E; RBL 25 TRANSITION ANGEL HAS CORROSION.<[01] BLENDED AREAS; REMOVED.004' MATERIAL; FOUND TO BE WITHIN LIMITS PER SRM 53-00-53-1A-2.;[02] THIS SECTION OF ANGLE TO BE REPLACED ON NR# TTG8Q00P65VC FROM STA. 500D + 10 TO 500I.;[03] INSPEC - [SDR SWAA2023113013620](https://openairdocs.org/sdr/SWAA2023113013620.md): Angle · corroded · Oct 23, 2023 · N8553W · Boeing 7378H4 · Fuselage Miscellaneous Structure > FWD CARGO STA 500H/500I; RBL 25 TRANSITION ANGEL HAS CORROSION.<[01] BLENDED AREAS; REMOVED.006' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. THIS SECTION OF ANGLE TO BE REPLACED ON NR# TTG8Q00P65VC.;[02] THIS SECTION OF ANGLE TO BE REPLACED ON - [SDR SWAA2023113013622](https://openairdocs.org/sdr/SWAA2023113013622.md): Angle · corroded · Oct 23, 2023 · N8553W · Boeing 7378H4 · Fuselage Miscellaneous Structure > FWD CARGO STA 500F/500E; RBL 25 TRANSITION ANGEL HAS CORROSION.<[01] BLENDED AREAS; REMOVED.012' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] THIS SECTION OF ANGLE TO BE REPLACED ON NR# TTG8Q00P65VC.;[03] THIS SECTION OF ANGLE TO BE REPLAC - [SDR SWAA2023113013627](https://openairdocs.org/sdr/SWAA2023113013627.md): Web · corroded · Oct 23, 2023 · N8553W · Boeing 7378H4 · Fuselage Miscellaneous Structure > AFT CARGO R/H TRANSITION WEB AT STA. 847-867 HAS LIGHT SURFACE CORROSION.<[01] BLENDED CORROSION ON R/H TRANSITION ANGLE FROM STA. 847 TO STA. 867 AT RBL 21? PER SRM 51-10-02. REMOVED.012? OF MATERIAL. REMAINING THICKNESS IS.038?. DAMAGE REMOVAL IS OUT OF LI - [SDR SWAA2023113013617](https://openairdocs.org/sdr/SWAA2023113013617.md): Web · corroded · Oct 23, 2023 · N8553W · Boeing 7378H4 · Fuselage Miscellaneous Structure > AFT CARGO R/H TRANSITION WEB AT STA. 767-795 HAS LIGHT SURFACE CORROSION.<[01] REMOVED SURFACE CORROSION IN AFT CARGO R/H TRANSITION WEB AT STA. 767-795 PER SRM 51-10-02.;[02] REMOVED.013? OF MATERIAL AT THE DEEPEST POINT. REMAINING THICKNESS IS.037?. DAMAGE - [SDR SWAA2023112913618](https://openairdocs.org/sdr/SWAA2023112913618.md): Strap · corroded · Oct 23, 2023 · N8553W · Boeing 7378H4 · Fuselage Miscellaneous Structure > AFT CARGO R/H SIDE; STRAP ON LOWER SIDE OF INTERCOSTAL RBL 21; STA 787-795. HAS CORROSION AROUND NUTPLATES.<[01] REMOVED CORROSION ON STRAP; FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 REMOVED AND REPLACED STRAP; AFT CARGO R/H SIDE; STRAP ON LOWER SIDE OF - [SDR SWAA2023112813944](https://openairdocs.org/sdr/SWAA2023112813944.md): Floor Support · cracked · Oct 23, 2023 · N8553W · Boeing 7378H4 · Fuselage Miscellaneous Structure > FLOOR SUPPORT BRACKET IS CRACKED AT BS 540; LBL 18.<[01] SEE N/R CARD TTG8Q00P64AG FOR REPLACEMENT OF CABIN FLOOR SUPPORT AT STA 540 BL 0 TO LBL 23.;[02] VERIFIED CA0-1. LONNIE HERMANN (TECHNICIAN); 25-OCT-2023 05:25 UTC
SEE N/R CARD TTG8Q00P64AG FOR REPLAC - [SDR SWAA2023112813945](https://openairdocs.org/sdr/SWAA2023112813945.md): Floor Support · cracked · Oct 23, 2023 · N8553W · Boeing 7378H4 · Fuselage Miscellaneous Structure > FLOOR SUPPORT BRACKET IS CRACKED AT BS 540; RBL 18.<[01] REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-40-02.;[02] C/W INSPECTION - [SDR SWAA2023112813949](https://openairdocs.org/sdr/SWAA2023112813949.md): Attach Angle · cracked · Oct 23, 2023 · N8553W · Boeing 7378H4 · Fuselage Main, Attach Fittings > AFT CARGO ATTACH L ANGLE ON VERT. STANCHION CRACKED AT APPROX BS 865 APPROX LBL13.<[01] INSTALLED NEW AFT CARGO 'L' ANGLE BRACKET PART #149A8109-U114 IAW SRM 51-40-02;[02] CW INSP - [SDR SWAA2023112813647](https://openairdocs.org/sdr/SWAA2023112813647.md): Angle · corroded · Oct 23, 2023 · N8553W · Boeing 7378H4 · Fuselage Miscellaneous Structure > SURFACE CORROSION ON L/H TRANSITION ANGLE LBL 21 STA. 787-807 (MARKED)<[01] REMOVED CORROSION ON LH TRANSITION ANGLE STA 787-807. REMAINING THICKNESS IS 0.030. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2;[02] C/W INSP. REMOVED CORROSION ON LH TRANSITION AN - [SDR SWAA2023112813648](https://openairdocs.org/sdr/SWAA2023112813648.md): Angle · corroded · Oct 23, 2023 · N8553W · Boeing 7378H4 · Fuselage Miscellaneous Structure > SURFACE CORROSION ON L/H TRANSITION ANGLE LBL 21 STA. 727H - 727I (MARKED).<[01] REMOVED CORROSION ON LH TRANSITION ANGLE STA 727H-727I. REMAINING THICKNESS IS 0.033. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2;[02] C/W INSP. REMOVED CORROSION ON LH TRANSI - [SDR SWAA2023112813649](https://openairdocs.org/sdr/SWAA2023112813649.md): Angle · corroded · Oct 23, 2023 · N8553W · Boeing 7378H4 · Fuselage Miscellaneous Structure > SURFACE CORROSION ON L/H TRANSITION ANGLE LBL 21 STA. 727I - 727J (MARKED)<[01] REMOVED CORROSION ON LH TRANSITION ANGLE STA 727I-727J. REMAINING THICKNESS IS 0.030. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2;[02] C/W INSP. REMOVED CORROSION ON LH TRANSIT - [SDR SWAA2023112813650](https://openairdocs.org/sdr/SWAA2023112813650.md): Angle · corroded · Oct 23, 2023 · N8553W · Boeing 7378H4 · Fuselage Miscellaneous Structure > SURFACE CORROSION ON L/H TRANSITION ANGLE LBL 21 STA. 727J - 747 (MARKED)<[01] REMOVED CORROSION ON LH TRANSITION ANGLE STA 727J-747. REMAINING THICKNESS IS 0.035. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2;[02] C/W INSP. REMOVED CORROSION ON LH TRANSITIO - [SDR SWAA2023112813651](https://openairdocs.org/sdr/SWAA2023112813651.md): Angle · corroded · Oct 23, 2023 · N8553W · Boeing 7378H4 · Fuselage Miscellaneous Structure > SURFACE CORROSION ON L/H TRANSITION ANGLE LBL 21 STA. 747 - 767 (MARKED)<[01] REMOVED CORROSION ON LH TRANSITION ANGLE STA 747-767. REMAINING THICKNESS IS 0.035. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2;[02] C/W INSP. REMOVED CORROSION ON LH TRANSITION - [SDR SWAA2023112813652](https://openairdocs.org/sdr/SWAA2023112813652.md): Angle · corroded · Oct 23, 2023 · N8553W · Boeing 7378H4 · Fuselage Miscellaneous Structure > SURFACE CORROSION ON L/H TRANSITION ANGLE LBL 21 STA. 767 - 787 (MARKED)<[01] REMOVED CORROSION ON LH TRANSITION ANGLE STA 767-787 REMAINING THICKNESS IS 0.029. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2;[02] C/W INSP; REMOVED CORROSION ON LH TRANSITION A - [SDR SWAA2023112813656](https://openairdocs.org/sdr/SWAA2023112813656.md): Angle · corroded · Oct 23, 2023 · N8553W · Boeing 7378H4 · Fuselage Miscellaneous Structure > SURFACE CORROSION ON R/H TRANSITION ANGLE STA. 727H - 727I RBL 21<[01] REMOVED CORROSION ON RH TRANSITION ANGLE STA 727H - 727I. REMAINING THICKNESS IS 0.030. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2;[02] C/W INSP. REMOVED CORROSION ON RH TRANSITION ANG - [SDR SWAA2023112813658](https://openairdocs.org/sdr/SWAA2023112813658.md): Angle · corroded · Oct 23, 2023 · N8553W · Boeing 7378H4 · Fuselage Miscellaneous Structure > SURFACE CORROSION ON R/H TRANSITION ANGLE STA. 727I - 727J RBL 21 (MARKED)<[01] REMOVED CORROSION ON RH TRANSITION ANGLE STA 727I - 727J. REMAINING THICKNESS IS 0.034. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2;[02] C/W INSP. CORROSION ON RH TRANSITION AN - [SDR SWAA2023112813657](https://openairdocs.org/sdr/SWAA2023112813657.md): Angle · corroded · Oct 23, 2023 · N8553W · Boeing 7378H4 · Fuselage Miscellaneous Structure > SURFACE CORROSION ON R/H TRANSITION ANGLE STA. 727J - 747 RBL 21 (MARKED)<[01] REMOVED CORROSION ON RH TRANSITION ANGLE STA 727J- 747. REMAINING THICKNESS IS 0.035. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2;[02] C/W INSP. CORROSION ON RH TRANSITION ANGLE - [SDR SWAA2023112813659](https://openairdocs.org/sdr/SWAA2023112813659.md): Angle · corroded · Oct 23, 2023 · N8553W · Boeing 7378H4 · Fuselage Miscellaneous Structure > SURFACE CORROSION ON R/H TRANSITION ANGLE STA. 747 - 767 RBL 21 (MARKED)<[01] REMOVED SURFACE CORROSION IN AFT CARGO R/H TRANSITION ANGLE AT STA. 747-767 RBL 21 PER SRM 51-10-02.;[02] REMOVED CORROSION ON RH TRANSITION ANGLE STA 747 - 767. REMAINING THICKNESS - [SDR SWAA2023112813660](https://openairdocs.org/sdr/SWAA2023112813660.md): Angle · corroded · Oct 23, 2023 · N8553W · Boeing 7378H4 · Fuselage Miscellaneous Structure > SURFACE CORROSION ON R/H TRANSITION ANGLE STA. 727D - 727E RBL 21 (MARKED)<[01] REMOVED CORROSION ON RH TRANSITION ANGLE STA 727D- 727E. REMAINING THICKNESS IS 0.035. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2;[02] C/W INSP.REMOVED CORROSION ON RH TRANSI - [SDR SWAA2023113013610](https://openairdocs.org/sdr/SWAA2023113013610.md): Floor Support · corroded · Oct 22, 2023 · N8553W · Boeing 7378H4 · Fuselage Miscellaneous Structure > CORROSION ON FLOOR SUPPORT AT SEVERAL FASTENER HOLES BS947+3 LBL15 -LBL48<[01] REMOVED FLOOR SUPPORT BS 947 +3 LBL 16 TO LBL 24 IAW SRM 51-40-02.;[02] REMOVED INTERCOSTAL BS947 TO BS967 LBL 24 IAW SRM 51-40-02.;[03] REMOVED FLOOR SUPPORT ANGLE BS947 +3 LBL24 T - [SDR SWAA2023113013592](https://openairdocs.org/sdr/SWAA2023113013592.md): Floor Support · corroded · Oct 22, 2023 · N8553W · Boeing 7378H4 · Fuselage Miscellaneous Structure > CORROSION ON FLOOR SUPPORT AT MULTIPLE FASTENER HOLES BS947+3 RBL39 -RBL46<[01] REMOVED CORROSION ON FLOOR SUPPORT AT BS947+3 RBL39- RBL46 IN BORE HOLES AND SURROUNDING AREAS; DAMAGE FOUND TO BE OUT OF LIMITS (REMOVED 0.009? OF 0.070?) IAW SRM 53-70-51-1A-1.;[ - [SDR SWAA2023113013591](https://openairdocs.org/sdr/SWAA2023113013591.md): Floorbeam · corroded · Oct 22, 2023 · N8553W · Boeing 7378H4 · Fuselage Main, Floor Beam > CORROSION ON FLOOR BEAM AT FASTENER HOLE 986.5 LBL 43<[01] BLENDED CORROSION ON UPPER FLANGE OF FLOOR BEAM 986.5 AT LBL 43? PER SRM 51-10-02. REMOVED.016? OF MATERIAL. REMAINING THICKNESS IS.134?. DAMAGE REMOVAL IS OUT OF LIMITS PER SRM 53-70-51-1A-1.;[02] V Next page: https://openairdocs.org/aircraft/N8553W/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 = 'N8553W' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N8553W/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.