# Service difficulty reports: N8544Z

A list on [N8544Z](https://openairdocs.org/aircraft/N8544Z.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 · 79 reports

- [SDR SWAA2026091524496](https://openairdocs.org/sdr/SWAA2026091524496.md): Cover · missing · Sep 11, 2026 · N8544Z · Boeing 7378H4 · Emergency Lighting
  > AFT 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.
- [SDR SWAA2026071595022](https://openairdocs.org/sdr/SWAA2026071595022.md): Battery Pack · inoperative · Jul 6, 2026 · N8544Z · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY 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.
- [SDR SWAA2026071586714](https://openairdocs.org/sdr/SWAA2026071586714.md): Panel · cracked · Jun 28, 2026 · N8544Z · Boeing 7378H4 · Fluid Service Doors
  > CRACKED 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).
- [SDR SWAA2026071584054](https://openairdocs.org/sdr/SWAA2026071584054.md): Attach Angle · cracked · Jun 25, 2026 · N8544Z · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > LEFT 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
- [SDR SWAA2026071546017](https://openairdocs.org/sdr/SWAA2026071546017.md): Attach Angle · cracked · Jun 25, 2026 · N8544Z · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > RT 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 -.
- [SDR SWAA2026051903421](https://openairdocs.org/sdr/SWAA2026051903421.md): Battery · inoperative · May 15, 2026 · N8544Z · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY 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.
- [SDR SWAA2026051896880](https://openairdocs.org/sdr/SWAA2026051896880.md): Skin · delaminated · May 8, 2026 · N8544Z · Boeing 7378H4 · Trailing Edge Flaps
  > RH 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.
- [SDR SWAA2026051896878](https://openairdocs.org/sdr/SWAA2026051896878.md): Skin · delaminated · May 8, 2026 · N8544Z · Boeing 7378H4 · Trailing Edge Flaps
  > DURING 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.
- [SDR SWAA2026020265838](https://openairdocs.org/sdr/SWAA2026020265838.md): Battery Pack · inoperative · Jan 30, 2026 · N8544Z · Boeing 7378H4 · Emergency Lighting
  > THREE FWD LT EMERGENCY OVERHEAD BIN LIGHTS NOT WORKING. R & R CHARGER ASSEMBLY AND BATTERY PACK IAW AMM 33-51-06. OPS CHECKED GOOD.
- [SDR SWAA2025072892749](https://openairdocs.org/sdr/SWAA2025072892749.md): Handle · loose · Jul 18, 2025 · N8544Z · Boeing 7378H4 · Passenger/Crew Doors
  > L1 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.
- [SDR SWAA2025072892748](https://openairdocs.org/sdr/SWAA2025072892748.md): Handle · loose · Jul 18, 2025 · N8544Z · Boeing 7378H4 · Passenger/Crew Doors
  > L2 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.
- [SDR SWAA2025033119417](https://openairdocs.org/sdr/SWAA2025033119417.md): Panel · delaminated · Mar 29, 2025 · N8544Z · Boeing 7378H4 · Wing Main, Frame Structure
  > LH 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 A
- [SDR SWAA2025022698998](https://openairdocs.org/sdr/SWAA2025022698998.md): Lamp · inoperative · Feb 24, 2025 · N8544Z · Boeing 7378H4 · Emergency Lighting
  > L2 DOOR EXTERIOR EMERGENCY LIGHT INOP<[01] REMOVED AND REPLACED L2 DOOR EXTERIOR EMERGENCY LAMP IAW AMM 33-51-04.
- [SDR SWAA2024101446695](https://openairdocs.org/sdr/SWAA2024101446695.md): Battery · inoperative · Oct 8, 2024 · N8544Z · Boeing 7378H4 · Emergency Equipment
  > FLIGHT ATTENDANT REPORT FLASHLIGHT UNDER FORWARD JUMPSEAT IS NOT CHARGED<[01] R&R RIGHT FWD FLIGHT ATTENDANT FLASHLIGHT BATTERY REF AMM 25-64-00
- [SDR SWAA2024072315031](https://openairdocs.org/sdr/SWAA2024072315031.md): Flashlight · inoperative · Jul 21, 2024 · N8544Z · Boeing 7378H4 · Emergency Equipment
  > FLASHLIGHT IN AFT GALLEY INOP<[01] PREFORM OPS CHECK OF AFT GALLEY FLASHLIGHT IAW MM 25-64-00; OPS CHECK GOOD
- [SDR SWAA2024041875963](https://openairdocs.org/sdr/SWAA2024041875963.md): Flashlight · no test · Apr 17, 2024 · N8544Z · Boeing 7378H4 · Emergency Equipment
  > RIGHT 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)]
- [SDR SWAA2024040369410](https://openairdocs.org/sdr/SWAA2024040369410.md): Sign · detached · Apr 1, 2024 · N8544Z · Boeing 7378H4 · Emergency Lighting
  > MAIN CABIN CEILING EXIT SIGN FELL OFF IN FLIGHT<[01] RE-ATTACHED CABIN CEILING EXIT SIGN COVER PER SIP.
- [SDR SWAA2023082391849](https://openairdocs.org/sdr/SWAA2023082391849.md): Battery Pack · inoperative · Aug 21, 2023 · N8544Z · Boeing 7378H4 · Emergency Lighting
  > AFT 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 33-51-06
- [SDR SWAA2023080281714](https://openairdocs.org/sdr/SWAA2023080281714.md): Battery Pack · inoperative · Jul 23, 2023 · N8544Z · Boeing 7378H4 · Emergency Lighting
  > AFT 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 EMERGENCY
- [SDR SWAA2023080180830](https://openairdocs.org/sdr/SWAA2023080180830.md): Battery Pack · inoperative · Jul 21, 2023 · N8544Z · Boeing 7378H4 · Emergency Lighting
  > FWD 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-
- [SDR SWAA2023080179984](https://openairdocs.org/sdr/SWAA2023080179984.md): Angle · corroded · Jul 18, 2023 · N8544Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > REF - 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 PAPERWORK
- [SDR SWAA2023080179986](https://openairdocs.org/sdr/SWAA2023080179986.md): Angle · corroded · Jul 18, 2023 · N8544Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > REF - 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.
- [SDR SWAA2023080179987](https://openairdocs.org/sdr/SWAA2023080179987.md): Angle · corroded · Jul 18, 2023 · N8544Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > REF - 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.
- [SDR SWAA2023080179989](https://openairdocs.org/sdr/SWAA2023080179989.md): Angle · corroded · Jul 18, 2023 · N8544Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > REF - 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.
- [SDR SWAA2023080179990](https://openairdocs.org/sdr/SWAA2023080179990.md): Angle · corroded · Jul 18, 2023 · N8544Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > REF - 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.
- [SDR SWAA2023080179991](https://openairdocs.org/sdr/SWAA2023080179991.md): Angle · corroded · Jul 18, 2023 · N8544Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > REF - 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.
- [SDR SWAA2023080179988](https://openairdocs.org/sdr/SWAA2023080179988.md): Angle · corroded · Jul 18, 2023 · N8544Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > REF - 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.
- [SDR SWAA2023080179992](https://openairdocs.org/sdr/SWAA2023080179992.md): Angle · corroded · Jul 18, 2023 · N8544Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > REJECTION: 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.
- [SDR SWAA2023080178192](https://openairdocs.org/sdr/SWAA2023080178192.md): Angle · corroded · Jul 13, 2023 · N8544Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD 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; TTG8Q0
- [SDR SWAA2023080177918](https://openairdocs.org/sdr/SWAA2023080177918.md): Intercostal · cracked · Jul 12, 2023 · N8544Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CABIN 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
- [SDR SWAA2023080476663](https://openairdocs.org/sdr/SWAA2023080476663.md): Support Channel · corroded · Jul 10, 2023 · N8544Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > U 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 LIM
- [SDR SWAA2023080276664](https://openairdocs.org/sdr/SWAA2023080276664.md): Support Angle · corroded · Jul 10, 2023 · N8544Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > TRANSITION 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?. FOU
- [SDR SWAA2023080476660](https://openairdocs.org/sdr/SWAA2023080476660.md): Angle · corroded · Jul 9, 2023 · N8544Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > REJECT: 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-
- [SDR SWAA2023080276661](https://openairdocs.org/sdr/SWAA2023080276661.md): Floor Panel · delaminated · Jul 9, 2023 · N8544Z · Boeing 7378H4 · Fuselage Floor Panel
  > `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 222
- [SDR SWAA2023080176658](https://openairdocs.org/sdr/SWAA2023080176658.md): Splice · corroded · Jul 8, 2023 · N8544Z · Boeing 7378H4 · Fuselage Floor Panel
  > AFT 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> TTG8Q00L8CXN
- [SDR SWAA2023080474793](https://openairdocs.org/sdr/SWAA2023080474793.md): Support Angle · corroded · Jul 3, 2023 · N8544Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT 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 THIC
- [SDR SWAA2023080474797](https://openairdocs.org/sdr/SWAA2023080474797.md): Angle · corroded · Jul 3, 2023 · N8544Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT 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 0.03
- [SDR SWAA2023080474798](https://openairdocs.org/sdr/SWAA2023080474798.md): Angle · corroded · Jul 3, 2023 · N8544Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT 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 0.03
- [SDR SWAA2023080474799](https://openairdocs.org/sdr/SWAA2023080474799.md): Angle · corroded · Jul 3, 2023 · N8544Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT 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 0.032
- [SDR SWAA2023080474800](https://openairdocs.org/sdr/SWAA2023080474800.md): Angle · corroded · Jul 3, 2023 · N8544Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT 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 0.033
- [SDR SWAA2023080474802](https://openairdocs.org/sdr/SWAA2023080474802.md): Angle · corroded · Jul 3, 2023 · N8544Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT 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?; REMAINING
- [SDR SWAA2023080474801](https://openairdocs.org/sdr/SWAA2023080474801.md): Angle · corroded · Jul 3, 2023 · N8544Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT 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 OUT
- [SDR SWAA2023080474806](https://openairdocs.org/sdr/SWAA2023080474806.md): Angle · corroded · Jul 3, 2023 · N8544Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT 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 T
- [SDR SWAA2023080474808](https://openairdocs.org/sdr/SWAA2023080474808.md): Angle · corroded · Jul 3, 2023 · N8544Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT 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 T
- [SDR SWAA2023080474809](https://openairdocs.org/sdr/SWAA2023080474809.md): Angle · corroded · Jul 3, 2023 · N8544Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT 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?; REM
- [SDR SWAA2023080474784](https://openairdocs.org/sdr/SWAA2023080474784.md): Angle · corroded · Jul 3, 2023 · N8544Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT 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 0.03
- [SDR SWAA2023080474810](https://openairdocs.org/sdr/SWAA2023080474810.md): Angle · corroded · Jul 3, 2023 · N8544Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT 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 0.033
- [SDR SWAA2023080474785](https://openairdocs.org/sdr/SWAA2023080474785.md): Angle · corroded · Jul 3, 2023 · N8544Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT 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?; REM
- [SDR SWAA2023080274814](https://openairdocs.org/sdr/SWAA2023080274814.md): Angle · cracked · Jul 3, 2023 · N8544Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT 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 REM
- [SDR SWAA2023080274792](https://openairdocs.org/sdr/SWAA2023080274792.md): Floor Splice · corroded · Jul 3, 2023 · N8544Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT 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.

Next page: https://openairdocs.org/aircraft/N8544Z/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 = 'N8544Z' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8544Z/reports

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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.