# Service difficulty reports: N8573Z

A list on [N8573Z](https://openairdocs.org/aircraft/N8573Z.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 · 87 reports

- [SDR SWAA2026081050812](https://openairdocs.org/sdr/SWAA2026081050812.md): Battery Pack · inoperative · Aug 4, 2026 · N8573Z · Boeing 7378H4 · Emergency Lighting
  > LEFT OVERWING EMERGENCY LIGHTS INOPERATIVE. R & R LT OVERWING BATTERY PACK IAW AMM 33-51-06. OPS CHKD GOOD.
- [SDR SWAA2026062213511](https://openairdocs.org/sdr/SWAA2026062213511.md): Girt Bar · loose · Jun 18, 2026 · N8573Z · Boeing 7378H4 · Emergency Equipment
  > FWD ENTRY DOOR GIRT BAR IS LOOSE. ADJUSTED FWD ENTRY DOOR GIRT BAR IAW AMM 25-66-01.
- [SDR SWAA2026042390812](https://openairdocs.org/sdr/SWAA2026042390812.md): Battery Pack · inoperative · Apr 19, 2026 · N8573Z · Boeing 7378H4 · Emergency Lighting
  > MULTIPLE AFT EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS AFT CABIN LEFT AND RIGHT REF AMM 33-51-06. OPS CHECK GOOD.
- [SDR SWAA2026042392141](https://openairdocs.org/sdr/SWAA2026042392141.md): Battery Pack · inoperative · Apr 19, 2026 · N8573Z · Boeing 7378H4 · Emergency Lighting
  > MULTIPLE AFT EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS AFT CABIN LEFT AND RIGHT REF AMM 33-51-06. OPS CHECK GOOD.
- [SDR SWAA2026022774623](https://openairdocs.org/sdr/SWAA2026022774623.md): Attach Bracket · loose · Feb 26, 2026 · N8573Z · Boeing 7378H4 · Service Doors
  > CREW REPORTS SERVICE DOOR (FW). SAFETY STRAP ATTACH BRACKET LOOSE; ATTACH POINT MISSING A FASTENER. SECURED FWD SERVICE DOOR SAFETY STRAP BRACKET IN PLACE A REQUIRED. OK TO CONT PER MEL 25-10-01 SP#1B. REPLACED HUCK BOLT ON FWD SERVICE DOOR SAFETY STRAP ATT
- [SDR SWAA2025120240514](https://openairdocs.org/sdr/SWAA2025120240514.md): Cradle · inoperative · Nov 28, 2025 · N8573Z · Boeing 7378H4 · Emergency Equipment
  > FWD FLIGHT ATTENDANT EMERGENCY FLASHLIGHT INOPERATIVE. R & R FWD FA FLASHLIGHT BRACKET ASSY IAW AMM 25-64-00. OPS CHECKS GOOD.
- [SDR SWAA2025091514505](https://openairdocs.org/sdr/SWAA2025091514505.md): Battery · no test · Sep 13, 2025 · N8573Z · Boeing 7378H4 · Emergency Equipment
  > FORWARD GALLEY FLASHLIGHT NOT TESTING. R & R FWD GALLEY FLASHLIGHT BATTERY INBD IAW AMM 25-64-00. CHECKS OK.
- [SDR SWAA2025081399878](https://openairdocs.org/sdr/SWAA2025081399878.md): Bulb · inoperative · Aug 9, 2025 · N8573Z · Boeing 7378H4 · Emergency Lighting
  > AFT CABIN CENTER OVERHEAD EMERGENCY LIGHT SIGN 1 EA BULB INOP. RELAMPED AFT CABIN CENTER OVERHEAD EMERGENCY LIGHT SIGN AND OPS CHECK GOOD IAW SWA B737-800 AMM 33-51-01-960-801.
- [SDR SWAA2025081399317](https://openairdocs.org/sdr/SWAA2025081399317.md): Girt Bar · unsecure · Aug 7, 2025 · N8573Z · Boeing 7378H4 · Emergency Equipment
  > CR RR L1 DOOR FWD GIRT BAR FITTING NEEDS SECURED. SECURED L1 DOOR FWD GIRT BAR FITTING IAW B737-800 AMM 25-66-02-201 AND 20-50-11-910-801.
- [SDR SWAA2025081399323](https://openairdocs.org/sdr/SWAA2025081399323.md): Handle · unsecure · Aug 7, 2025 · N8573Z · Boeing 7378H4 · Passenger/Crew Doors
  > L2 DOOR AND AIRFRAME SIDE ASSIST HANDLES NEED SECURED. SECURED L2 DOOR AND AIRFRAME ASSIST HANDLES IAW AMM 52-13-31.
- [SDR SWAA2025081399318](https://openairdocs.org/sdr/SWAA2025081399318.md): Handle · unsecure · Aug 7, 2025 · N8573Z · Boeing 7378H4 · Service Doors
  > CR RR R1 DOOR ASSIST HANDLE NEEDS SECURED. SECURED R1 DOOR ASSIST HANDLE IAW B737-800 AMM 52-41-31.
- [SDR SWAA2025081299322](https://openairdocs.org/sdr/SWAA2025081299322.md): Battery Pack · inoperative · Aug 7, 2025 · N8573Z · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS ON OVERHEAD BINS AT ROW 17DEF; 21DEF; AND RT LOWER EXTERIOR LIGHT ARE INOPERATIVE. REMOVED & REPLACED, OP CHECKED BATTERY PACK IAW AMM 33-51-06-960-805. BATTERY PACK AND LIGHTS OP CHECKED GOOD.
- [SDR SWAA2025081299320](https://openairdocs.org/sdr/SWAA2025081299320.md): Bulb · inoperative · Aug 7, 2025 · N8573Z · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY LIGHTS ABOVE L1 DOOR 2 EA. BULBS INOPERATIVE. RELAMPED EMERGENCY LIGHTS OVER L1 DOOR AND OPS CHECK GOOD IAW AMM 33-51-01-960-801.
- [SDR SWAA2025081299324](https://openairdocs.org/sdr/SWAA2025081299324.md): Bulb · inoperative · Aug 7, 2025 · N8573Z · Boeing 7378H4 · Emergency Lighting
  > CR RR EMERGENCY LIGHTS ABOVE R1 DOOR 2 EA. BULBS INOPERATIVE. RELAMPED EMERGENCY LIGHTS OVER R1 DOOR AND OPS CHECK GOOD IAW AMM 33-51-01-960-801.
- [SDR SWAA2025081299321](https://openairdocs.org/sdr/SWAA2025081299321.md): Bulb · inoperative · Aug 7, 2025 · N8573Z · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY LIGHTS ABOVE R2 DOOR 1 EA. BULB INOPERATIVE RELAMPED EMERGENCY LIGHTS OVER R2 DOOR AND OPS CHECK GOOD IAW AMM 33-51-01-960-801.
- [SDR SWAA2025081398058](https://openairdocs.org/sdr/SWAA2025081398058.md): Handle · loose · Aug 3, 2025 · N8573Z · Boeing 7378H4 · Passenger/Crew Doors
  > L1 DOOR ASSIST HANDLE ON DOOR LOOSE. SECURED LI DOOR LINER ASSIST HANDLE IAW AMM 52-11-31-400-802 SUBTASK 52-11-31-020-011.
- [SDR SWAA2025081398057](https://openairdocs.org/sdr/SWAA2025081398057.md): Handle · loose · Aug 3, 2025 · N8573Z · Boeing 7378H4 · Service Doors
  > R2 DOOR BOTH ASSIST HANDLES LOOSE. SECURED R2 ASSIST HANDLES IAW B737-800 AMM 52-41-31.
- [SDR SWAA2025072493612](https://openairdocs.org/sdr/SWAA2025072493612.md): Light · faulty · Jul 22, 2025 · N8573Z · Boeing 7378H4 · Emergency Lighting
  > AFT RH EMER EXIT SIDE WALL LIGHT WILL NOT TURN OFF WHEN SELECTED FROM ATTENDANT. LOADED SOFTWARE; OPS CHECK NORMAL AFT RH EMER EXIT SIDE WALL LIGHT. PER AMM 33-21-00.
- [SDR SWAA2024090433184](https://openairdocs.org/sdr/SWAA2024090433184.md): Girt Bar · out of adjust · Aug 31, 2024 · N8573Z · Boeing 7378H4 · Emergency Equipment
  > FORWARD SERVICE DOOR GIRT BAR DIFFICULT TO STOW<[01] ADJUSTED FWD SERV DOOR GIRT BARAS PER MM 25-66-01
- [SDR SWAA2024052489001](https://openairdocs.org/sdr/SWAA2024052489001.md): Battery · no test · May 22, 2024 · N8573Z · Boeing 7378H4 · Emergency Equipment
  > 1 FWD FA FLASHLIGHT WILL NOT TEST. & R FWD FA FLASHLIGHT BATTERY REF SIP.
- [SDR SWAA2024052383769](https://openairdocs.org/sdr/SWAA2024052383769.md): Bulb · inoperative · May 9, 2024 · N8573Z · Boeing 7378H4 · Emergency Lighting
  > LAVATORY 'A'; FORWARD L-1 DOOR ENTRY EMERGENCY PATH LIGHT HAS MIDDLE SECTION OF BULBS INOP. LAVATORY 'A' FORWARD L-1 DOOR ENTRY EMERGENCY PATH LIGHT HAS MIDDLE SECTION OF BULBS INOP.<[01] RELAMPED FOWARD ENTRY DOOR EXIT MARKER; OPS CHECKS GOOD PER MM 33-51-01;
- [SDR SWAA2024052383768](https://openairdocs.org/sdr/SWAA2024052383768.md): Battery Pack · inoperative · May 8, 2024 · N8573Z · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY DOOR MARKER LIGHTS AT BOTH FOWARD OVERWING EXITS INOP<[01] REMOVED AND REPLACED FUSE IN BATTERY PACK BASE M1694; OPS CHECKS GOOD PER MM 33-51-06;[02] INSPECTED WORK PERFORMED. REMOVED AND REPLACED FUSE IN BATTERY PACK BASE M1694; OPS CHECKS GOOD PER
- [SDR SWAA2024052383767](https://openairdocs.org/sdr/SWAA2024052383767.md): Battery Pack · inoperative · May 8, 2024 · N8573Z · Boeing 7378H4 · Emergency Lighting
  > FOWARD ENTRY AND SERVICE DOOR EMERGENCY LIGHTS INOP.<[01] REMOVED AND REPLACED FOWARD ENTRY AND FOWARD SERVICE DOOR EMERGENCY LIGHT BATTERY PACKS PER MM 33-51-06. OPS CHECKS GOOD PER MM 33-51-00;[02] INSPECTED WORK PERFORMED. REMOVED AND REPLACED FORWARD ENTRY
- [SDR SWAA2024052382809](https://openairdocs.org/sdr/SWAA2024052382809.md): Baffle · cracked · May 6, 2024 · N8573Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FORWARD CARGO BAFFLE AT 25RBL STA 500G-500H CRACKED AT 500H.<[01] REMOVED AND REPLACED BAFFLE I.A.W SRM 51-40-02.;[02] INSPECTED WORK PERFORMED;[03] C/W. PLEASE SEE INDIVIDUAL SIGNOFFS.
- [SDR SWAA2024052382810](https://openairdocs.org/sdr/SWAA2024052382810.md): Angle · cracked · May 6, 2024 · N8573Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO BAFFLE CLIP AT 25RBL STA 500H IS CRACKED ON FWD SIDE OF FRAME 500H<[01] REMOVED AND REPLACED BAFFLE CLIP I.A.W SRM 51-40-02.;[02] INSPECTED WORK PERFORMED
- [SDR SWAA2024052382811](https://openairdocs.org/sdr/SWAA2024052382811.md): Angle · cracked · May 6, 2024 · N8573Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO BAFFLE CLIP AT 25RBL STA 500H IS CRACKED ON AFT SIDE OF FRAME 500H<[01] REMOVED AND REPLACED BAFFLE CLIP I.A.W SRM 51-40-02.;[02] INSPECTED WORK PERFORMED
- [SDR SWAA2024052382533](https://openairdocs.org/sdr/SWAA2024052382533.md): Stringer Clip · cracked · May 4, 2024 · N8573Z · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > FWD CARGO COMPARTMENT HAS A STRINGER CLIP THAT IS CRACKED AT BOTH FRAME RIVETS; STA 500I STR 26L.<[01] REMOVED LH BAFFLE ASSY. FROM STA. 500H TO 500I TO F.O.M IAW SRM 51-40-02.;[02] REMOVED DAMAGED STRINGER CLIP AT STA. 500I STR. 26L IAW SRM 51-40-02.;[03] LOC
- [SDR SWAA2024052382534](https://openairdocs.org/sdr/SWAA2024052382534.md): Stringer Clip · cracked · May 4, 2024 · N8573Z · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > FWD CARGO COMPARTMENT HAS A STRINGER CLIP THAT IS CRACKED AT THE FRAME RIVETS; STA 500I STR 26R.<[01] REMOVED STRINGER CLIP PER SRM 51-40-02.;[02] INSTALLED NEW STRINGER CLIP PER SRM 51-40-02;[03] RII INSPECTED C/A 2.;[04] C/W INSP. INSTALLED NEW STRINGER CLIP
- [SDR SWAA2024052378127](https://openairdocs.org/sdr/SWAA2024052378127.md): Floorbeam · corroded · Apr 23, 2024 · N8573Z · Boeing 7378H4 · Fuselage Main, Floor Beam
  > FOUND ADDITIONAL CORROSION AT A DEEPER DEPTH ON FLOOR BEAM 947.5 LBL 24 UPPER CHORD AT LAV MOUNT LOCATION.<[01] REMOVED ADDITIONAL CORROSION PER SRM 51-10-02. REMAINING THICKNESS IS.125';[02] C/W C.A. STEP 1. VERIFIED REMOVAL OF CORROSION AND REMAINING THICKN
- [SDR SWAA2024052377288](https://openairdocs.org/sdr/SWAA2024052377288.md): Angle · corroded · Apr 20, 2024 · N8573Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO L/H TRANSITION ANGLE UPPER SURFACE HAS CORROSION AT N/P AND FASTNER HOLES STA 500H - 500I LBL 23-25 WL 156. MRKD<[01] REMOVED CORROSION PER SRM 51-10-02. BLENDED AREA OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] C/W INSP. REMOVED CORROSION PER SRM 51-10
- [SDR SWAA2024052377290](https://openairdocs.org/sdr/SWAA2024052377290.md): Angle · corroded · Apr 20, 2024 · N8573Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO L/H TRANSITION ANGLE UPPER SURFACE HAS CORROSION AT N/P AND FASTNER HOLES STA 500F - 500G LBL 23-25 WL 156. MRKD<[01] REMOVED CORROSION PER SRM 51-10-02. BLENDED AREA OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] C/W INSP. REMOVED CORROSION PER SRM 51-10
- [SDR SWAA2024052377294](https://openairdocs.org/sdr/SWAA2024052377294.md): Angle · corroded · Apr 20, 2024 · N8573Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO L/H TRANSITION ANGLE UPPER SURFACE HAS CORROSION AT N/P AND FASTNER HOLES STA 500C - 500D LBL 23-25 WL 156. MRKD<[01] REMOVED CORROSION PER SRM 51-10-02. BLENDED AREA OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] C/W INSP. REMOVED CORROSION PER SRM 51-10
- [SDR SWAA2024052377297](https://openairdocs.org/sdr/SWAA2024052377297.md): Angle · corroded · Apr 20, 2024 · N8573Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO L/H TRANSITION ANGLE UPPER SURFACE HAS CORROSION AT N/P AND FASTNER HOLES STA 500 - 500A LBL 23-25 WL 156. MRKD<[01] REMOVED CORROSION PER SRM 51-10-02. BLENDED AREA OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] C/W INSP. REMOVED CORROSION PER SRM 51-10-
- [SDR SWAA2024052377292](https://openairdocs.org/sdr/SWAA2024052377292.md): Angle · corroded · Apr 20, 2024 · N8573Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO L/H TRANSITION ANGLE UPPER SURFACE HAS CORROSION AT N/P AND FASTNER HOLES STA 500E - 500F LBL 23-25 WL 156. MRKD<[01] REMOVED CORROSION PER SRM 51-10-02. BLENDED AREA OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] C/W INSP. REMOVED CORROSION PER SRM 51-10
- [SDR SWAA2024052377293](https://openairdocs.org/sdr/SWAA2024052377293.md): Angle · corroded · Apr 20, 2024 · N8573Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO L/H TRANSITION ANGLE UPPER SURFACE HAS CORROSION AT N/P AND FASTNER HOLES STA 500D - 500E LBL 23-25 WL 156. MRKD<[01] REMOVED CORROSION PER SRM 51-10-02. BLENDED AREA OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] C/W INSP. REMOVED CORROSION PER SRM 51-10
- [SDR SWAA2024052377289](https://openairdocs.org/sdr/SWAA2024052377289.md): Angle · corroded · Apr 20, 2024 · N8573Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO L/H TRANSITION ANGLE UPPER SURFACE HAS CORROSION AT N/P AND FASTNER HOLES STA 500G - 500H LBL 23-25 WL 156. MRKD<[01] REMOVED CORROSION PER SRM 51-10-02. BLENDED AREA OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] C/W INSP. REMOVED CORROSION PER SRM 51-10
- [SDR SWAA2024052377295](https://openairdocs.org/sdr/SWAA2024052377295.md): Angle · corroded · Apr 20, 2024 · N8573Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO L/H TRANSITION ANGLE UPPER SURFACE HAS CORROSION AT N/P AND FASTNER HOLES STA 500B - 500C LBL 23-25 WL 156. MRKD<[01] REMOVED CORROSION PER SRM 51-10-02. BLENDED AREA OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] C/W INSP. REMOVED CORROSION PER SRM 51-10
- [SDR SWAA2024052377296](https://openairdocs.org/sdr/SWAA2024052377296.md): Angle · corroded · Apr 20, 2024 · N8573Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO L/H TRANSITION ANGLE UPPER SURFACE HAS CORROSION AT N/P AND FASTNER HOLES STA 500A - 500B LBL 23-25 WL 156. MRKD<[01] REMOVED CORROSION PER SRM 51-10-02. BLENDED AREA OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] C/W INSP. REMOVED CORROSION PER SRM 51-10
- [SDR SWAA2024052377264](https://openairdocs.org/sdr/SWAA2024052377264.md): Angle · corroded · Apr 20, 2024 · N8573Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT STA 727 D-5 RBL 21 TRANSITION ANGLE HAS CORROSION MARKED<[01] REMOVED CORROSION; MAT DEPTH REMOVED IS 0.009; MAT THICKNESS REMAINING IS 0.031; FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2;[02] REMOVED TRANSITION ANGLE FROM STA 727 TO S
- [SDR SWAA2024052377265](https://openairdocs.org/sdr/SWAA2024052377265.md): Angle · corroded · Apr 20, 2024 · N8573Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT STA 727 F RBL21 TRANSITION ANGLE HAS CORROSION MARKED<[01] REMOVED CORROSION; MAT DEPTH REMOVED IS 0.011; MAT THICKNESS REMAINING IS 0.029; OUT OF LIMITS IAW SRM 53-00-53-1A-2.;[02] REMOVED TRANSITION ANGLE FROM STA 727 TO STA 767 FOR REP
- [SDR SWAA2024052377274](https://openairdocs.org/sdr/SWAA2024052377274.md): Angle · corroded · Apr 20, 2024 · N8573Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT STA 727 F+6 LBL 21 TRANSITION ANGLE HAS CORROSION MARKED<[01] REMOVED CORROSION; MAT DEPTH REMOVED IS 0.009; MAT THICKNESS REMAINING IS 0.031; OUT OF LIMITS IAW SRM 53-00-53-1A-2;[02] REMOVED TRANSITION ANGLE FROM STA 767 TO STA 847 FOR R
- [SDR SWAA2024052377276](https://openairdocs.org/sdr/SWAA2024052377276.md): Angle · corroded · Apr 20, 2024 · N8573Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT STA 727 G THRU STA727 H LBL 21 TRANSITION ANGLE HAS NUMEROUS CORROSION AREAS MARKED<[01] REMOVED CORROSION; MAT DEPTH REMOVED IS 0.011; MAT THICKNESS REMAINING IS 0.029; OUT OF LIMITS IAW SRM 53-00-53-1A-2;[02] TRANSITION PANEL REMOVED AN
- [SDR SWAA2024052377277](https://openairdocs.org/sdr/SWAA2024052377277.md): Angle · corroded · Apr 20, 2024 · N8573Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON UPPER SURFACE OF TRANSITION ANGLE IN AFT CARGO BIN AT STATION 827 LBL 22. MARKED<[01] REMOVED CORROSION; MAT DEPTH REMOVED IS 0.007; MAT THICKNESS REMAINING IS 0.033; OUT OF LIMITS IAW SRM 53-00-53-1A-2.;[02] TRANSITION PANEL REMOVED AND REPLACED
- [SDR SWAA2024052377267](https://openairdocs.org/sdr/SWAA2024052377267.md): Angle · corroded · Apr 20, 2024 · N8573Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT STA 727G THRU STA727 H RBL 21 TRANSITION ANGLE HAS NUMEROUS CORROSION AREAS MARKED<[01] REMOVED CORROSIONS; MAT DEPTH REMOVED IS 0.008; MAT THICKNESS REMAINING IS 0.032; OUT OF LIMITS IAW SRM 53-00-53-1A-2.;[02] REMOVED TRANSITION ANGLE F
- [SDR SWAA2024052377278](https://openairdocs.org/sdr/SWAA2024052377278.md): Angle · corroded · Apr 20, 2024 · N8573Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT STA 727H THRU STA727 I LBL 21 TRANSITION ANGLE HAS NUMEROUS CORROSION AREAS MARKED<[01] REMOVED CORROSION; MAT DEPTH REMOVED IS 0.012; MAT THICKNESS REMAINING IS 0.028; OUT OF LIMITS IAW SRM 53-00-53-1A-2;[02] TRANSITION PANEL REMOVED AND
- [SDR SWAA2024052377280](https://openairdocs.org/sdr/SWAA2024052377280.md): Web · corroded · Apr 20, 2024 · N8573Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO THRESHOLD WEB UPPER SURFACE HAS NUMEROUS AREAS OF CORROSION AT N/P AND FASTNER HOLES. STA 440 - 492 RBL 29-30 WL 156. MRKD<[01] BLENDED CORROSION PER SRM 51-10-02. BLENDED AREA OUT OF LIMITS PER SRM 53-30-15-1A-1;[02] C/W INSP. BLENDED CORROSION PER
- [SDR SWAA2024052377279](https://openairdocs.org/sdr/SWAA2024052377279.md): Angle · corroded · Apr 20, 2024 · N8573Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT STA 727H THRU STA727 I RBL 21 TRANSITION ANGLE HAS NUMEROUS CORROSION AREAS MARKED<[01] REMOVED CORROSION; MAT DEPTH REMOVED IS 0.012; MAT REMAINING IS 0.028. OUT OF LIMITS IAW SRM 53-00-53-1A-2.;[02] REMOVED TRANSITION ANGLE FROM STA 727
- [SDR SWAA2024052377268](https://openairdocs.org/sdr/SWAA2024052377268.md): Angle · corroded · Apr 20, 2024 · N8573Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT STA 727 I THRU STA 727 J LBL 21 TRANSITION ANGLE HAS NUMEROUS CORROSION AREAS MARKED<[01] REMOVED CORROSION; MAT DEPTH REMOVED IS 0.009; MAT THICKNESS REMAINING IS 0.031; OUT OF LIMITS IAW SRM 53-00-53-1A-2.;[02] TRANSITION PANEL REMOVED
- [SDR SWAA2024052377282](https://openairdocs.org/sdr/SWAA2024052377282.md): Angle · corroded · Apr 20, 2024 · N8573Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT STA 727 I THRU STA 727 J RBL 21 TRANSITION ANGLE HAS NUMEROUS CORROSION AREAS MARKED<[01] REMOVED CORROSION; MAT DEPTH REMOVED IS 0.010; MAT THICKNESS REMAINING IS 0.030; OUT OF LIMITS IAW SRM 53-00-53-1A-2;[02] REMOVED TRANSITION ANGLE F
- [SDR SWAA2024052377283](https://openairdocs.org/sdr/SWAA2024052377283.md): Angle · corroded · Apr 20, 2024 · N8573Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT STA 727 J THRU STA 747 LBL 21 TRANSITION ANGLE HAS NUMEROUS CORROSION AREAS MARKED<[01] REMOVED CORROSION; MAT DEPTH REMOVED IS 0.007; MAT THICKNESS REMAINING IS 0.033; OUT OF LIMITS IAW SRM 53-00-53-1A-2;[02] TRANSITION PANEL REMOVED AND

Next page: https://openairdocs.org/aircraft/N8573Z/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 = 'N8573Z' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8573Z/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.