N8544Z

Service difficulty reports · 79

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 = 'N8544Z' 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 SWAA2026091524496Cover · missingAFT EMERGENCY EXIT LIGHT COVER MISSING. OK TO CONT PER MX NOTE FOR 5 DAYS PER MPM REF 9.3 LIGHT COVER MISSING SWITCH WORKS R & R AFT ATTENDANTS PANEL WITH LCD SCREEN. OPS/BITE CKS NO FAULTS NOTED REF AMM 25-25-11.Sep 11, 2026 · N8544Z · Boeing 7378H4 · Emergency LightingSDR SWAA2026071595022Battery Pack · inoperativeEMERGENCY LIGHTS ASSOCIATED WITH BATTERY PACK M1671 INOPERATIVE. REPLACED BATTERY PACK M1671 AND PERFORMED A GOOD FUNCTIONAL TEST OF NEW BATTERY PACK IAW AMM 33-51-06-960-805.Jul 6, 2026 · N8544Z · Boeing 7378H4 · Emergency LightingSDR SWAA2026071586714Panel · crackedCRACKED HOLD OPEN STRUT ON REFUELING PANEL 621GB. REMOVED AND REPLACED HOLD OPEN STRUT ON REFUELING PANEL 621GB IAW AMM 52-49-21-400-801 STEP 3.E.(6).Jun 28, 2026 · N8544Z · Boeing 7378H4 · Fluid Service DoorsSDR SWAA2026071584054Attach Angle · crackedLEFT BS 663, UPPER ATTACH ANGLE IS CRACKED ON VAPOR BARRIER LBL 8 AND LBL 34 WL 167.68. REMOVED, REPLACED, AND INSTALLED A NEW BS 663 LT UPPER ATTACH ANGLE LBL 4 TO LBL 65 IAW SRM 51-40-02-0G-0, DWG 111A1000, REV B, DWG 111A1001 REV B, AND DWG 111A7000 REV Jun 25, 2026 · N8544Z · Boeing 7378H4 · Fuselage Main, Attach FittingsSDR SWAA2026071546017Attach Angle · crackedRT BS 663 UPPER ATTACH ANGLE IS CRACKED ON VAPOR BARRIER RBL 8 AND RBL 34 WL 167.68. REMOVED, REPLACED, AND INSTALLED A NEW BS 663 RT UPPER ATTACH ANGLE RBL 4 TO RBL 65 IAW SRM 51-40-02-0G-0, DWG 111A1000, REV B, DWG 111A1001, REV B, AND DWG 111A7000, REV -.Jun 25, 2026 · N8544Z · Boeing 7378H4 · Fuselage Main, Attach FittingsSDR SWAA2026051903421Battery · inoperativeEMERGENCY EXIT LIGHTS ASSOCIATED WITH (M1694) DO NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY (M1694) AND TESTED GOOD PER AMM 33-51-06-960-805.May 15, 2026 · N8544Z · Boeing 7378H4 · Emergency LightingSDR SWAA2026051896880Skin · delaminatedRH O/B AFT FLAP HAS DELAMINATION AT I/B END ALONG T/E<[01] RECIEVED NEW R/W O/B AFT FLAP. INSTALLATION OF AFT FLAP TO BE ACCOMPLISHED ON FAULT TTG8Q01BR0YJ;[02] VERIFIED CORRECTIVE ACTION STEP 1.May 8, 2026 · N8544Z · Boeing 7378H4 · Trailing Edge FlapsSDR SWAA2026051896878Skin · delaminatedDURING OK TO INSTALL WAS FOUND; RH O/B AFT FLAP IS DELAMINATED AT I/B T/E UPPER SURFACE. GENERAL FAULT RESOLVED ON OTHER FAULT (FAULT WAS RESOLVED ON ANOTHER FAULT). DUPLICATE WRITE UP. AFT FLAP TO BE REPLACED ON FAULT TTG8Q01C3DBE.May 8, 2026 · N8544Z · Boeing 7378H4 · Trailing Edge FlapsSDR SWAA2026020265838Battery Pack · inoperativeTHREE FWD LT EMERGENCY OVERHEAD BIN LIGHTS NOT WORKING. R & R CHARGER ASSEMBLY AND BATTERY PACK IAW AMM 33-51-06. OPS CHECKED GOOD.Jan 30, 2026 · N8544Z · Boeing 7378H4 · Emergency LightingSDR SWAA2025072892749Handle · looseL1 DOOR LINER ASSIST HANDLES LOOSE (BOTH UPPR AND LWR). SECURED UPPER AND LOWER ASSIST HANDLES ON L-1 DOOR IAW AMM 52-11-31-400-802 STEP 3G2.Jul 18, 2025 · N8544Z · Boeing 7378H4 · Passenger/Crew DoorsSDR SWAA2025072892748Handle · looseL2 DOOR LINER ASSIST HANDLE LOOSE. SECURED ASSIST HANDLE ON L-2 DOOR IAW B737-800 AMM 52-13-31-400-802 STEP 3G2. VERIFIED SECURED ASSIST HANDLE ON L-2 DOOR IAW AMM 52-13-31-400-802 STEP 3G2.Jul 18, 2025 · N8544Z · Boeing 7378H4 · Passenger/Crew DoorsSDR SWAA2025033119417Panel · delaminatedLH WING OUTD FIXED TRAILING EDGE LOWER PANEL DENT WITH DELAMINATION 571DB (P/N 115A4710-201)<[01] REMOVED DAMAGE AND APPLIED 250DEG. REPAIR PER SRM 57-51-01-2R-1 AND SRM 51-70-05.;[02] REMOVED DAMAGE AND APPLIED 250DEG. PERMANENT REPAIR PER SRM 57-51-01-2R-1 AMar 29, 2025 · N8544Z · Boeing 7378H4 · Wing Main, Frame StructureSDR SWAA2025022698998Lamp · inoperativeL2 DOOR EXTERIOR EMERGENCY LIGHT INOP<[01] REMOVED AND REPLACED L2 DOOR EXTERIOR EMERGENCY LAMP IAW AMM 33-51-04.Feb 24, 2025 · N8544Z · Boeing 7378H4 · Emergency LightingSDR SWAA2024101446695Battery · inoperativeFLIGHT ATTENDANT REPORT FLASHLIGHT UNDER FORWARD JUMPSEAT IS NOT CHARGED<[01] R&R RIGHT FWD FLIGHT ATTENDANT FLASHLIGHT BATTERY REF AMM 25-64-00Oct 8, 2024 · N8544Z · Boeing 7378H4 · Emergency EquipmentSDR SWAA2024072315031Flashlight · inoperativeFLASHLIGHT IN AFT GALLEY INOP<[01] PREFORM OPS CHECK OF AFT GALLEY FLASHLIGHT IAW MM 25-64-00; OPS CHECK GOODJul 21, 2024 · N8544Z · Boeing 7378H4 · Emergency EquipmentSDR SWAA2024041875963Flashlight · no testRIGHT AFT O/B EMERGENCY FLASHLIGHT WILL NOT TEST<[01] 01 - REMOVED AND REPLACED PER [AMM 25-64-00-900-806-NG (FLASHLIGHT BATTERY REPLACEMENT - PERMANENT)]Apr 17, 2024 · N8544Z · Boeing 7378H4 · Emergency EquipmentSDR SWAA2024040369410Sign · detachedMAIN CABIN CEILING EXIT SIGN FELL OFF IN FLIGHT<[01] RE-ATTACHED CABIN CEILING EXIT SIGN COVER PER SIP.Apr 1, 2024 · N8544Z · Boeing 7378H4 · Emergency LightingSDR SWAA2023082391849Battery Pack · inoperativeAFT OVER-WING LOWER EMERGENCY EXIT LIGHTS WILL NOT ILLUMINATE DURING TEST.<[01] T/S AND FOUND RH O/W L01188 EXIT IND LIGHT WIRING CONNECTED TO ITSELF; REMOVED AND REPLACED BATTERY PACK AND CHARGER ASSY REF WDM 33-51-21 AND MM 33-51-06Aug 21, 2023 · N8544Z · Boeing 7378H4 · Emergency LightingSDR SWAA2023080281714Battery Pack · inoperativeAFT GALLEY EMERGENCY LIGHTS INOP<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS AT STA 952L AND 952R PER MM33-51-06;[02] VERIFIED C/A #1.;[03] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS AT STA 952L AND 952R PER MM 33-51-06.AFT GALLEY EMERGENCYJul 23, 2023 · N8544Z · Boeing 7378H4 · Emergency LightingSDR SWAA2023080180830Battery Pack · inoperativeFWD GALLEY EMERGENCY LIGHTS INOP<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS AT STA 310 AND STA 500C+7R PER MM 33-51-06;[02] INSPECTED AS REQUIRED. CORRECTIVE ACTION #1;[03] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT STA 317 PER MM 33-51-Jul 21, 2023 · N8544Z · Boeing 7378H4 · Emergency LightingSDR SWAA2023080179984Angle · corrodedREF - FWD CARGO COMPT LH TRANSITION ANGLE HAS CORROSION STA 430 [TTG8Q00LZZM2] THIS FAULT MISSING DAMAGE PICTURE UPLOADED .<[01] PHOTO UPLOADED;[02] UPDATED PAPERWORK;[03] C/W INSPECTION.;[04] UPDATED PAPERWORKJul 18, 2023 · N8544Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023080179986Angle · corrodedREF - FWD CARGO COMPT LH TRANSITION ANGLE HAS CORROSION STA 500+5 [TTG8Q00LZZMN] FAULT MISSING UPLOADED DAMAGE PHOTO .<[01] PHOTO UPLOADED;[02] UPDATED PAPERWORK;[03] C/W INSPECTION.Jul 18, 2023 · N8544Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023080179987Angle · corrodedREF - FWD CARGO COMPT LH TRANSITION ANGLE HAS CORROSION STA 460-480 [TTG8Q00LZZMS] FAULT MISSING DAMAGE PHOTO UPLOADED .<[01] PHOTO UPLOADED;[02] UPDATED PAPERWORK;[03] C/W INSPECTION.Jul 18, 2023 · N8544Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023080179989Angle · corrodedREF - FWD CARGO COMPT LH TRANSITION ANGLE HAS CORROSION STA 500D-500E [TTG8Q00LZZNL] FAULT MISSING DAMAGE PHOTO UPLOADED .<[01] PHOTO UPLOADED;[02] UPDATED PAPERWORK;[03] C/W INSPECTION.Jul 18, 2023 · N8544Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023080179990Angle · corrodedREF - FWD CARGO COMPT LH TRANSITION ANGLE HAS CORROSION STA 500C-500D [TTG8Q00LZZNK] FAULT MISSING DAMAGE PHOTO UPLOADED .<[01] PHOTO UPLOADED;[02] UPDATED PAPERWORK;[03] C/W INSPECTION.Jul 18, 2023 · N8544Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023080179991Angle · corrodedREF - FWD CARGO COMPT LH TRANSITION ANGLE HAS CORROSION STA 430 [TTG8Q00M70XP] FAULT MISSING DAMAGE PHOTO UPLOADED .<[01] PHOTO UPLOADED;[02] UPDATED PAPERWORK;[03] C/W INSPECTION.Jul 18, 2023 · N8544Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023080179988Angle · corrodedREF - FWD CARGO COMPT LH TRANSITION ANGLE HAS CORROSION STA 450 [TTG8Q00LZZM3] FAULT MISSING DAMAGE PHOTO UPLOADED .<[01] PHOTO UPLOADED;[02] UPDATED PAPERWORK;[03] C/W INSPECTION.Jul 18, 2023 · N8544Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023080179992Angle · corrodedREJECTION : REF - FWD CARGO COMPT LH TRANSITION ANGLE HAS CORROSION STA 500A+15 [TTG8Q00LZZNA CARD CLOSED AND MARKED LEVEL 2 CORROSION . A DAMAGE PHOTO MUST BE UPLOAD TO CARD .<[01] PHOTO UPLOADED;[02] UPDATED PAPERWORK;[03] C/W INSPECTION.Jul 18, 2023 · N8544Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023080178192Angle · corrodedFWD CARGO COMPT LH TRANSITION ANGLE HAS CORROSION STA 430<[01] ORIGINAL TASK CARD TTG8Q00LZZM2 SIGNED OFF IN ERROR. REFERENCE ALL TASK COMPLETED IN ASSOCIATION WITH THAT TASK TO THIS CARD REFERENCE TTG8Q00LZZM3; TTG8Q00LZZMN; TTG8Q00LZZMS; TTG8Q00LZZNA; TTG8Q0Jul 13, 2023 · N8544Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023080177918Intercostal · crackedCABIN FLOOR INTERCOSTAL HAS 2EA CRACKS AT FASTENER HOLES AT BS387 AND BS394 LBL14<[01] PROCURED REPLACEMENT PART #143A5410-174 FROM ADVANTAGE AVIATION; CUSTOMER PO #P7395685; WORK ORDER #MS55414.;[02] REMOVED CRACKED CHORD PER SRM 51-40-02. FORMED REPLACEMENT Jul 12, 2023 · N8544Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023080476663Support Channel · corrodedU CHANNEL SUPPORT HAS SURFACE CORR STA 747-767. RBL 22<[01] REMOVED CORROSION FROM INTERCOSTAL (U CHANNEL SUPPORT) STA 747- 767. ORIGINAL THICKNESS IS 0.032?; MATERIAL LOSS IS 0.004?; MAX ALLOWED IS 0.003?; REMAINING THICKNESS IS 0.028?. FOUND TO BE OUT OF LIMJul 10, 2023 · N8544Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023080276664Support Angle · corrodedTRANSITION ANGLE SUPPORT HAS SURFACE CORR. STA 767-787. RBL22<[01] REMOVED CORROSION AFT CARGO TRANSITION SUPPORT ANGLE RBL 22 STA 767F TO STA. 787 ORIGINAL THICKNESS IS 0.050?; MATERIAL LOSS IS 0.006?; MAX ALLOWED IS 0.005?; REMAINING THICKNESS IS 0.046?. FOUJul 10, 2023 · N8544Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023080476660Angle · corrodedREJECT: AFT CARGO R/H TRANSITION ANGLE; CORROSION IS STILL PRESENT ON UNDERSIDE OF NUTPLATES STA. 847 TO STA 867 RBL 22.<[01] REMOVED AFT CARGO SHIELD PLATED PER SRM 51-40-05.<BR><BR>LOCATED; DRILLED; AND COUNTERSUNK NEW AFT CARGO DOOR SHIELD PLATE IAW SRM 51-Jul 9, 2023 · N8544Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023080276661Floor Panel · delaminated`FWD GALLEY FLOORBOARD PANEL 222BF DELAMINATED FWD GALLEY FLOORBOARD PANEL 222BF DELAMINATED.<[01] REMOVED AND REPLACED FWD GALLEY PANEL 222BF WITH SERVICABLE PANEL . WILL BE INSTALLED ON CLOSE CARD [TTG8Q00L8AZF];[02] REMOVED AND REPLACED FWD GALLEY PANEL 222Jul 9, 2023 · N8544Z · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2023080176658Splice · corrodedAFT CARGO FLOOR PANEL SPLICE AT STA 767+6 HAS CORROSION<[01] RECEIVED NEW FLOOR PANEL SPLICE. SPLICE WILL BE INSTALLED WITH TASK CARD TTG8Q00L8CXN;[02] VERIFIED NEW SPLICE PROCUREMENT AND TO BE INSTALLED ON CARD <BR> TTG8Q00L8CXNJul 8, 2023 · N8544Z · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2023080474793Support Angle · corrodedAFT CARGO BELT FRAME HAS CORROSION IN AND AROUND N/P HOLE BS727I RBL23.<[01] REMOVED CORROSION FROM AFT CARGO BELT FRAME (PANEL SUPPORT ANGLE) IN AD AND AROUND N/P HOLE BS 727I RBL 23 PER AMM 51-00-53/201. MECHANICALLY MEASURED ANGLE TO BE 0.063? ORIGINAL THICJul 3, 2023 · N8544Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023080474797Angle · corrodedAFT CARGO LT. TRANSITION ANGLE HAS CORROSION IN AND AROUND N/P HOLES BS727F-727G.<[01] REMOVED CORROSION AFT CARGO TRANSITION ANGLE LBL 22 STA 727F- 727G. ORIGINAL THICKNESS IS 0.040?; MATERIAL LOSS IS 0.007?; MAX ALLOWED IS 0.004?; REMAINING THICKNESS IS 0.03Jul 3, 2023 · N8544Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023080474798Angle · corrodedAFT CARGO LT. TRANSITION ANGLE HAS CORROSION IN AND AROUND N/P HOLES BS727G-727H.<[01] REMOVED CORROSION AFT CARGO TRANSITION ANGLE LBL 22 STA 727G- 727H. ORIGINAL THICKNESS IS 0.040?; MATERIAL LOSS IS 0.005?; MAX ALLOWED IS 0.004?; REMAINING THICKNESS IS 0.03Jul 3, 2023 · N8544Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023080474799Angle · corrodedAFT CARGO LT. TRANSITION ANGLE HAS CORROSION IN AND AROUND N/P HOLES BS727H-727I.<[01] REMOVED CORROSION AFT CARGO TRANSITION ANGLE LBL 22 STA 727H-727I. ORIGINAL THICKNESS IS 0.040?; MATERIAL LOSS IS 0.008?; MAX ALLOWED IS 0.004?; REMAINING THICKNESS IS 0.032Jul 3, 2023 · N8544Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023080474800Angle · corrodedAFT CARGO LT. TRANSITION ANGLE HAS CORROSION IN AND AROUND N/P HOLES BS727I-727J.<[01] REMOVED CORROSION AFT CARGO TRANSITION ANGLE LBL 22 STA 727I-727J. ORIGINAL THICKNESS IS 0.040?; MATERIAL LOSS IS 0.007?; MAX ALLOWED IS 0.004?; REMAINING THICKNESS IS 0.033Jul 3, 2023 · N8544Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023080474802Angle · corrodedAFT CARGO TRANSITION ANGLE LBL 22' STA.727J TO STA.747. HAS AREAS OF CORROSION AROUND FASTENER HOLES.<[01] REMOVED CORROSION AFT CARGO TRANSITION ANGLE LBL 22 STA 727J-747. ORIGINAL THICKNESS IS 0.040?; MATERIAL LOSS IS 0.007?; MAX ALLOWED IS 0.004?; REMAININGJul 3, 2023 · N8544Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023080474801Angle · corrodedAFT CARGO LT. TRANSITION ANGLE HAS CORROSION AROUND FASTENER BS727F.<[01] REMOVED CORROSION AFT CARGO TRANSITION ANGLE LBL 22 STA 727F. ORIGINAL THICKNESS IS 0.040?; MATERIAL LOSS IS 0.005?; MAX ALLOWED IS 0.004?; REMAINING THICKNESS IS 0.035?. FOUND TO BE OUTJul 3, 2023 · N8544Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023080474806Angle · corrodedAFT CARGO TRANSITION ANGLE LBL 22' STA.747 TO STA.767. HAS AREAS OF CORROSION AROUND FASTENER HOLES.<[01] REMOVED CORROSION AFT CARGO TRANSITION ANGLE LBL 22 STA 747-767. ORIGINAL THICKNESS IS 0.040?; MATERIAL LOSS IS 0.007?; MAX ALLOWED IS 0.004?; REMAINING TJul 3, 2023 · N8544Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023080474808Angle · corrodedAFT CARGO TRANSITION ANGLE LBL 22' STA.767 TO STA.787. HAS AREAS OF CORROSION AROUND FASTENER HOLES.<[01] REMOVED CORROSION AFT CARGO TRANSITION ANGLE LBL 22 STA 767-787. ORIGINAL THICKNESS IS 0.040?; MATERIAL LOSS IS 0.008?; MAX ALLOWED IS 0.004?; REMAINING TJul 3, 2023 · N8544Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023080474809Angle · corrodedAFT CARGO TRANSITION ANGLE RBL 22' STA.767 TO STA.787. HAS AREAS OF CORROSION AROUND FASTENER HOLES.<[01] REMOVED CORROSION AFT CARGO TRANSITION ANGLE RBL 22 STA 767F TO STA. 787 ORIGINAL THICKNESS IS 0.050?; MATERIAL LOSS IS 0.006?; MAX ALLOWED IS 0.005?; REMJul 3, 2023 · N8544Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023080474784Angle · corrodedAFT CARGO TRANSITION ANGLE LBL 23' STA.787. HAS AREAS OF CORROSION AROUND FASTENER HOLE.<[01] REMOVED CORROSION AFT CARGO TRANSITION ANGLE LBL 23 STA 787. ORIGINAL THICKNESS IS 0.040?; MATERIAL LOSS IS 0.008?; MAX ALLOWED IS 0.004?; REMAINING THICKNESS IS 0.03Jul 3, 2023 · N8544Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023080474810Angle · corrodedAFT CARGO TRANSITION ANGLE LBL 23' STA.807 HAS AREAS OF CORROSION AROUND FASTENER HOLE.<[01] REMOVED CORROSION AFT CARGO TRANSITION ANGLE LBL 23 STA 807. ORIGINAL THICKNESS IS 0.040?; MATERIAL LOSS IS 0.007?; MAX ALLOWED IS 0.004?; REMAINING THICKNESS IS 0.033Jul 3, 2023 · N8544Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023080474785Angle · corrodedAFT CARGO TRANSITION ANGLE RBL 22' STA.847 TO STA.867. HAS AREAS OF CORROSION AROUND FASTENER HOLES.<[01] REMOVED CORROSION AFT CARGO TRANSITION ANGLE RBL 22 STA 847F TO STA. 867 ORIGINAL THICKNESS IS 0.050?; MATERIAL LOSS IS 0.003?; MAX ALLOWED IS 0.005?; REMJul 3, 2023 · N8544Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023080274814Angle · crackedAFT CARGO LAV TANK WALL SUPPORT VERTICAL ANGLE CRACKED STA. 867 LBL16' WL 166'<[01] REMOVED CRACKED ANGLE PER SRM 51-40-02;[02] REMOVED AND REPLACED AFT CARGO LAV TANK WALL SUPPORT VERTICAL ANGLE STA. 867 LBL16' WL 166' PER SRM 51-40-02;[03] INSPECTION C/W REMJul 3, 2023 · N8544Z · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2023080274792Floor Splice · corrodedAFT CARGO FLOOR SPLICE HAS PRIMER MISSING AND CORROSION IN AND AROUND N/P HOLES BS727D+6.<[01] RECEIVED NEW FLOOR SPLICE. SPLICE WILL BE INSTALLED ON ROUTINE TASK CARD TTG8Q00L8CXJ;[02] VERIFIED NEW SPLICE PROCUREMENT AND TO BE INSTALLED ON CARD TTG8Q00L8CXJ. Jul 3, 2023 · N8544Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
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