# Service difficulty reports: N8574Z

A list on [N8574Z](https://openairdocs.org/aircraft/N8574Z.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 · 63 reports

- [SDR SWAA2026092832413](https://openairdocs.org/sdr/SWAA2026092832413.md): Sill Drain · odor · Sep 24, 2026 · N8574Z · Boeing 7378H4 · Fuselage Main, Structure
  > TSI - REPORTS OF AFT GALLEY SMELL. DURING INSPECTION OF AFT DOOR SILL DRAIN FOUND BOTH CAPT SIDE DOOR SILL DRAIN FITTINGS FILLED WITH DEBRIS CLEANED DOOR SILL SILL DRAIN FITTINGS IRT 38-11-00. NO FOUL SMELL NOTED
- [SDR SWAA2026092833840](https://openairdocs.org/sdr/SWAA2026092833840.md): Seat · odor · Sep 23, 2026 · N8574Z · Boeing 7378H4 · Passenger Compartment Equipment
  > BAD ODOR COMING FROM THE LAST 4 ROWS OF AIRCRAFT. SANITIZED LAST 4 ROWS OF AIRCRAFT SEATS IAW SIP
- [SDR SWAA2026091116924](https://openairdocs.org/sdr/SWAA2026091116924.md): Lamp · inoperative · Sep 7, 2026 · N8574Z · Boeing 7378H4 · Emergency Lighting
  > EXTERIOR EMERGENCY LIGHT BY LT AFT ENTRY DOOR INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-51-04
- [SDR SWAA2026061009570](https://openairdocs.org/sdr/SWAA2026061009570.md): Elec Connector · loose · Jun 6, 2026 · N8574Z · Boeing 7378H4 · Light System Wiring
  > EMERGENCY LIGHT FO SIDE AFT FLICKERS. OK TO CONTINUE PER MEL 33-2-04. SP1 B AUTH 322846; SECURED LOOSE CONNECTOR ON THE LIGHT ASSY IAW AMM 33-21-00. OPS CHKD GOOD. NO DEFECTS NOTED AT THIS TIME.
- [SDR SWAA2026060806756](https://openairdocs.org/sdr/SWAA2026060806756.md): Skin · delaminated · May 26, 2026 · N8574Z · Boeing 7378H4 · Trailing Edge Flaps
  > RIGHT OTBD AFT FLAP HAS AREA OF DELAMINATION, INBOARD AFT EDGE. REMOVED AND REPLACED RT OTBD AFT FLAP ON TASK CARD TTG8Q01BR0XB. REMOVED AND REPLACED RT OTBD AFT FLAP ON TASK CARD TTG8Q01BR0XB.
- [SDR SWAA2026030575737](https://openairdocs.org/sdr/SWAA2026030575737.md): Handle · broken · Mar 2, 2026 · N8574Z · Boeing 7378H4 · Passenger/Crew Doors
  > FORWARD MAIN ENTRY DOOR WHITE ASSIST HANDLE BROKEN. ATTACHED THE FWD MAIN ENTRY DOOR ASSIST HANDLE IAW MM 52-11-31
- [SDR SWAA2025122955381](https://openairdocs.org/sdr/SWAA2025122955381.md): Battery Pack · inoperative · Dec 24, 2025 · N8574Z · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY LIGHTS BATTERY PACK AT POSITION M1672 WILL NOT ILLUMINATES EMERGENCY LIGHTS. REPLACED BATTERY PACK AT POSITION M1672 PER AMM 33-51-06
- [SDR SWAA2025121251761](https://openairdocs.org/sdr/SWAA2025121251761.md): Battery Pack · inoperative · Dec 11, 2025 · N8574Z · Boeing 7378H4 · Emergency Lighting
  > L1 EMERGENCY LIGHTS INOPERATIVE. R & R THE L1 EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-06. OPS CHECK GOOD.
- [SDR SWAA2025102729004](https://openairdocs.org/sdr/SWAA2025102729004.md): Pump · leaking · Oct 25, 2025 · N8574Z · Boeing 737824 · Hydraulic Pump (Electric/Engine), Main
  > 45 MIN INTO FLIGHT, ENG 2 HYD PUMP LOW PRESSURE LIGHTILLUMINATED. ELEC 1 LOW PRESSURE LIGHT ALSO ILLUMINATED. RAN PROCEDURE IAW QRH & EXTENDED FLAPS VIA ALT FLAP SYS TO FLAPS 15 LANDING. REMOVED & REPLACED ENG. NR 2 EDP REF. AMM 29-11-11. OPS TEST GOOD, NO
- [SDR SWAA2025102728412](https://openairdocs.org/sdr/SWAA2025102728412.md): Pump · leaking · Oct 25, 2025 · N8574Z · Boeing 737824 · Hydraulic Pump (Electric/Engine), Main
  > 45 MIN INTO FLIGHT. ENG 2 HYD PUMP LOW PRESSURE LIGHTILLUMINATED. ELEC 1 LOW PRESSURE LIGHT ALSO ILLUMINATED. RAN PROCEDURE IAW QRH & EXTENDED FLAPS VIA ALT FLAP SYS TO FLAPS 15 LANDING. REMOVED & REPLACED ENG NR 2 EDP IAW AMM 29-11-11. OPS TESTED GOOD, NO L
- [SDR SWAA2025021996987](https://openairdocs.org/sdr/SWAA2025021996987.md): Battery Pack · no test · Feb 18, 2025 · N8574Z · Boeing 7378H4 · Emergency Lighting
  > AFT L/H EMERGENCY LIGHTING BATTERY PACK FAILED THE CAPACITY CHECK.<[01] REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.
- [SDR SWAA2024102953341](https://openairdocs.org/sdr/SWAA2024102953341.md): Cover · detached · Oct 25, 2024 · N8574Z · Boeing 7378H4 · Emergency Lighting
  > EXIT ROW EXIT SIGN KNOCKED OFF<[01] SECURED SIGN COVER AS PER AMM 33-51-01 AT ROW 11.
- [SDR SWAA2024102953469](https://openairdocs.org/sdr/SWAA2024102953469.md): Cover · missing · Oct 25, 2024 · N8574Z · Boeing 7378H4 · Emergency Lighting
  > EXIT ROW EXIT SIGN KNOCKED OFF<[01] SECURED SIGN COVER AS PER AMM 33-51-01 AT ROW 11.
- [SDR SWAA2024082830176](https://openairdocs.org/sdr/SWAA2024082830176.md): Coffeemaker · odor · Aug 25, 2024 · N8574Z · Boeing 7378H4 · Buffet/Galleys
  > BURNING SMELL FROM FRONT LEFT COFFEE MAKER<[01] R/R COFFEE MAKER PER AMM 25-30-01.<BR>OPS CHECK GOOD.
- [SDR SWAA2024062796967](https://openairdocs.org/sdr/SWAA2024062796967.md): Stringer Clip · cracked · May 31, 2024 · N8574Z · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > FWD CARGO COMPARTMENT HAS A STRINGER CLIP THAT IS CRACKED AT BOTH FRAME RIVETS; STA 500I STR 25R. HFEC VERIFIED.<[01] REMOVED AND REPLACED IAW SRM 51-40-02 AND SRM 51-40-05.;[02] C/W INSPECTION
- [SDR SWAA2024062791654](https://openairdocs.org/sdr/SWAA2024062791654.md): Angle · cracked · May 30, 2024 · N8574Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > IN THE RH AC BAY; L ANGLE AT STA 663; RBL 31.5 RIVET HAS A CRACK EXTENDING VERTICAL TOWARDS THE CENTER FUEL TANK. VERIFIED WITH HFEC.<[01] THIS L ANGLE WILL BE REMOVED AND REPLACED ON TTG8Q00TH4J4.;[02] VERIFIED
- [SDR SWAA2024062791658](https://openairdocs.org/sdr/SWAA2024062791658.md): Angle · cracked · May 30, 2024 · N8574Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > IN THE RH AC BAY; L ANGLE AT STA 663; RBL 35 RIVET HAS A CRACK EXTENDING VERTICAL TOWARDS THE CENTER FUEL TANK. VERIFIED WITH HFEC.<[01] THIS L ANGLE WILL BE REMOVED AND REPLACED ON TTG8Q00TH4J4.;[02] VERIFIED
- [SDR SWAA2024062890207](https://openairdocs.org/sdr/SWAA2024062890207.md): Angle · corroded · May 27, 2024 · N8574Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPT LH TRANSITION ANGLE CORRODED STA 500A-500B. REMOVED DAMAGE IAW SRM 51-10-02. MEASURED DAMAGE DEPTH TO BE.009. DAMAGE FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-53-1A-2. CUTOUT & REMOVED DAMAGE SECTION OF TRANSITION ANGLE FROM STA 480
- [SDR SWAA2024062890214](https://openairdocs.org/sdr/SWAA2024062890214.md): Angle · corroded · May 27, 2024 · N8574Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPT RH TRANSITION ANGLE CORRODED STA 500F-500G. REMOVED CORROSION AT FWD CARGO R/H TRANSITION ANGLE FROM STA 500A TO STA 500I PER SRM 51-10-02. MEASURED BLEND AREAS OUT OF LIMITS PER SRM 53-00-53-1A-2 FIG.103; DETAIL E. FWD CARGO R/H TRANSITION
- [SDR SWAA2024062890215](https://openairdocs.org/sdr/SWAA2024062890215.md): Angle · corroded · May 27, 2024 · N8574Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPT RH TRANSITION ANGLE CORRODED STA 500E-500F. REMOVED CORROSION AT FWD CARGO R/H TRANSITION ANGLE FROM STA 500A TO STA 500I PER SRM 51-10-02. MEASURED BLEND AREAS OUT OF LIMITS PER SRM 53-00-53-1A-2 FIG.103; DETAIL E. FWD CARGO R/H TRANSITION
- [SDR SWAA2024062890216](https://openairdocs.org/sdr/SWAA2024062890216.md): Angle · corroded · May 27, 2024 · N8574Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPT RH TRANSITION ANGLE CORRODED STA 500D-500E. REMOVED CORROSION AT FWD CARGO R/H TRANSITION ANGLE FROM STA 500A TO STA 500I PER SRM 51-10-02. MEASURED BLEND AREAS OUT OF LIMITS PER SRM 53-00-53-1A-2 FIG.103; DETAIL E. REPLACED IAW SRM 51-10-02
- [SDR SWAA2024062890217](https://openairdocs.org/sdr/SWAA2024062890217.md): Angle · corroded · May 27, 2024 · N8574Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPT RH TRANSITION ANGLE CORRODED STA 500C-500D. REMOVED CORROSION AT FWD CARGO R/H TRANSITION ANGLE FROM STA 500A TO STA 500I PER SRM 51-10-02. MEASURED BLEND AREAS OUT OF LIMITS PER SRM 53-00-53-1A-2 FIG.103; DETAIL E. FWD CARGO R/H TRANSITION
- [SDR SWAA2024062890218](https://openairdocs.org/sdr/SWAA2024062890218.md): Angle · corroded · May 27, 2024 · N8574Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPT RH TRANSITION ANGLE CORRODED STA 500B-500C. REMOVED CORROSION AT FWD CARGO R/H TRANSITION ANGLE FROM STA 500A TO STA 500I PER SRM 51-10-02. MEASURED BLEND AREAS OUT OF LIMITS PER SRM 53-00-53-1A-2 FIG.103; DETAIL E. FWD CARGO R/H TRANSITION
- [SDR SWAA2024062890219](https://openairdocs.org/sdr/SWAA2024062890219.md): Angle · corroded · May 27, 2024 · N8574Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPT RH TRANSITION ANGLE CORRODED STA 500A-500B<[01] REMOVED CORROSION AT FWD CARGO R/H TRANSITION ANGLE FROM STA 500A TO STA 500I PER SRM 51-10-02. MEASURED BLEND AREAS OUT OF LIMITS PER SRM 53-00-53-1A-2 FIG.103; DETAIL E. STEP 1 FWD CARGO R/H T
- [SDR SWAA2024062890223](https://openairdocs.org/sdr/SWAA2024062890223.md): Angle · corroded · May 27, 2024 · N8574Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPT RH SHORT TRANSITION ANGLE AFT OF DOOR CORRODED STA 492-500A<[01] REMOVED CORROSION AT FWD CARGO R/H SHIELD SIDEPLATE ASSY STA 492 TO STA 500A PER SRM 51-10-02. MEASURED REMAINING MATERIAL THICKNESS OUT OF LIMITS PER SRM 53-30-15-1A-1 FIG.103; D
- [SDR SWAA2024062790213](https://openairdocs.org/sdr/SWAA2024062790213.md): Angle · corroded · May 27, 2024 · N8574Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPT RH TRANSITION ANGLE CORRODED STA 500H-500I<[01] REMOVED CORROSION AT FWD CARGO R/H TRANSITION ANGLE FROM STA 500A TO STA 500I PER SRM 51-10-02. MEASURED BLEND AREAS OUT OF LIMITS PER SRM 53-00-53-1A-2 FIG.103; DETAIL E.;[02] RESOLVED ON FAULT T
- [SDR SWAA2024062790212](https://openairdocs.org/sdr/SWAA2024062790212.md): Angle · corroded · May 27, 2024 · N8574Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPT LH TRANSITION ANGLE CORRODED STA 500B-500C<[01] REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAGE DEPTH TO BE.008?. DAMAGE FOUND TO BE OUT OF ALLOWABLE LIMITS AS GIVEN IN SRM 53-00-53-1A-2.;[02] CUTOUT AND REMOVED DAMAGE SECTION OF TRANSITION
- [SDR SWAA2024062790206](https://openairdocs.org/sdr/SWAA2024062790206.md): Angle · corroded · May 27, 2024 · N8574Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPT LH TRANSITION ANGLE CORRODED STA 500C-500D<[01] REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAGE DEPTH TO BE.004?. DAMAGE FOUND TO BE OUT OF ALLOWABLE LIMITS AS GIVEN IN SRM 53-00-53-1A-2.;[02] CUTOUT AND REMOVED DAMAGE SECTION OF TRANSITION
- [SDR SWAA2024062790211](https://openairdocs.org/sdr/SWAA2024062790211.md): Angle · corroded · May 27, 2024 · N8574Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPT LH TRANSITION ANGLE CORRODED STA 500D-500E<[01] REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAGE DEPTH TO BE.0010?. DAMAGE FOUND TO BE OUT OF ALLOWABLE LIMITS AS GIVEN IN SRM 53-00-53-1A-2.;[02] CUTOUT AND REMOVED DAMAGE SECTION OF TRANSITIO
- [SDR SWAA2024062790210](https://openairdocs.org/sdr/SWAA2024062790210.md): Angle · corroded · May 27, 2024 · N8574Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPT LH TRANSITION ANGLE CORRODED STA 500E-500F<[01] REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAGE DEPTH TO BE.005?. DAMAGE FOUND TO BE OUT OF ALLOWABLE LIMITS AS GIVEN IN SRM 53-00-53-1A-2.;[02] CUTOUT AND REMOVED DAMAGE SECTION OF TRANSITION
- [SDR SWAA2024062790209](https://openairdocs.org/sdr/SWAA2024062790209.md): Angle · corroded · May 27, 2024 · N8574Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPT LH TRANSITION ANGLE CORRODED STA 500H-500I. REMOVED DAMAGE IAW SRM 51-10-02. MEASURED DAMAGE DEPTH TO BE.008. DAMAGE FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-53-1A-2. CUTOUT AND REMOVED DAMAGE SECTION OF TRANSITION ANGLE FROM BS 480
- [SDR SWAA2024062790208](https://openairdocs.org/sdr/SWAA2024062790208.md): Angle · corroded · May 27, 2024 · N8574Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPT 500I BULKHEAD ANGLE AT FLOOR CORRODED. REMOVED CORROSION AT FWD CARGO COMPT. AFT BULKHEAD LOWER RAIL ANGLE BS 500I, RBL 22 TO LBL 22 IAW SRM 51-10-02. MEASURED REMAINING MATERIAL THICKNESS, OUT OF LIMITS IAW SRM 53-30-08-1A-1 FIG. 103, DETAIL
- [SDR SWAA2024070189988](https://openairdocs.org/sdr/SWAA2024070189988.md): Floorbeam · cracked · May 26, 2024 · N8574Z · Boeing 7378H4 · Fuselage Main, Floor Beam
  > CABIN FLOOR SUPPORT STIFFENER CRACKED AT STA 540 BL ZERO TO LBL24<[01] REMOVED AND REPLACED STIFFENER AT STA 540 BL 0 TO LBL 24 PER SRM 51-40-02.;[02] VERIFIED C/A #1.
- [SDR SWAA2024070189987](https://openairdocs.org/sdr/SWAA2024070189987.md): Floorbeam · cracked · May 26, 2024 · N8574Z · Boeing 7378H4 · Fuselage Main, Floor Beam
  > CABIN FLOOR SUPPORT STIFFENER CRACKED AT STA 540 BL ZERO TO RBL24<[01] REMOVED AND REPLACED FLOOR SUPPORT STIFFENER PER SRM 51-40-02.
- [SDR SWAA2024070190181](https://openairdocs.org/sdr/SWAA2024070190181.md): Plate · corroded · May 26, 2024 · N8574Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO L/H SIDE PLATE HAS CORROSION AT SEVERAL N/P HOLES STA 727H-727I LBL 21-22 WL 156. MRKD<[01] FOUND CORROSION ON L/H SIDE PLATE AT STA. 727H-727I TO BE OUT OF LIMITS PER SRM 3-00-53-1A-2.;[02] REMOVED DAMAGED SECTION OF L/H SIDE PLATE FROM STA.727G+12-
- [SDR SWAA2024070190192](https://openairdocs.org/sdr/SWAA2024070190192.md): Angle · corroded · May 26, 2024 · N8574Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT RH TRANSITION ANGLE BETWEEN STA.727J-747; RBL 21-RBL 22 HAS SURFACE CORROSION.(MARKED<REMOVED CORROSION PER SRM 53-00-53-1A-2 (0.037' REMAINING THICKNESS). TRANSITION ANGLE (SIDEPLATE) IS OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] CUT AND
- [SDR SWAA2024070190193](https://openairdocs.org/sdr/SWAA2024070190193.md): Angle · corroded · May 26, 2024 · N8574Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT RH TRANSITION ANGLE BETWEEN STA.747-767; RBL 21-RBL 22 HAS SURFACE CORROSION.(MARKED<[01] REMOVED CORROSION PER SRM 53-00-53-1A-2 (0.037' REMAINING THICKNESS). TRANSITION ANGLE (SIDEPLATE) IS OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] REMO
- [SDR SWAA2024062890198](https://openairdocs.org/sdr/SWAA2024062890198.md): Angle · corroded · May 26, 2024 · N8574Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT RH TRANSITION ANGLE BETWEEN STA.767-787; RBL 21-RBL 22 HAS SURFACE CORROSION. MRKD<[01] REMOVED CORROSION PER SRM 53-60-15-1A-1 (0.045' REMAINING THICKNESS). SHIELD (TRANSITION ANGLE) IS OUT OF LIMITS PER SRM 53-60-15-1A-1.;[02] SHIELD AS
- [SDR SWAA2024062889980](https://openairdocs.org/sdr/SWAA2024062889980.md): Floor Support · corroded · May 26, 2024 · N8574Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CABIN WET AREA FLOOR STRUCTURE INTERCOSTAL AT STA 947+4'; AFT OF RIGHT HAND LAV MOUNTS HAS CORROSION AROUND FASTENER HOLE. (MARKED)<[01] BLENDED OUT CORROSION AT AFT CABIN FLOOR STRUCTURE SUPPORT ANGLE STA 947+4?; RBL 28 PER SRM 51-10-02. MEASURED REMAININ
- [SDR SWAA2024062890180](https://openairdocs.org/sdr/SWAA2024062890180.md): Plate · corroded · May 26, 2024 · N8574Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO L/H SIDE PLATE HAS CORROSION AT SEVERAL N/P HOLES STA 727G-727H LBL 21-22 WL 156. REMOVED CORROSION FROM STA.727G-727G+12 PER SRM 51-10-02. REMOVED.002? OF MATERIAL THICKNESS; REMAINING THICKNESS IS.038?.FOUND WITHIN ALLOWABLE LIMITS PER SRM 53-0
- [SDR SWAA2024062890182](https://openairdocs.org/sdr/SWAA2024062890182.md): Plate · corroded · May 26, 2024 · N8574Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO L/H SIDE PLATE HAS CORROSION AT SEVERAL N/P HOLES STA 727I-727J LBL 21-22 WL 156. FOUND CORROSION ON L/H SIDE PLATE AT STA. 727I-727J TO BE OUT OF LIMITS PER SRM 3-00-53-1A-2.;[02] L/H SIDE PLATE WAS FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 A
- [SDR SWAA2024062890183](https://openairdocs.org/sdr/SWAA2024062890183.md): Plate · corroded · May 26, 2024 · N8574Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO L/H SIDE PLATE HAS CORROSION AT SEVERAL N/P HOLES STA 727J-747 LBL 21-22 WL 156. MRKD<[01] FOUND CORROSION ON L/H SIDE PLATE AT STA. 727J-747 TO BE OUT OF LIMITS PER SRM 3-00-53-1A-2.;[02] L/H SIDE PLATE WAS FOUND TO BE OUT OF LIMITS PER SRM 53-00-53
- [SDR SWAA2024062890185](https://openairdocs.org/sdr/SWAA2024062890185.md): Plate · corroded · May 26, 2024 · N8574Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO L/H SIDE PLATE HAS CORROSION AT SEVERAL N/P HOLES STA 747-767 LBL 21-22 WL 156. FOUND CORROSION ON L/H SIDE PLATE AT STA. 747-767 TO BE OUT OF LIMITS PER SRM 3-00-53-1A-2. L/H SIDE PLATE WAS FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 AND A SE
- [SDR SWAA2024062890199](https://openairdocs.org/sdr/SWAA2024062890199.md): Plate · corroded · May 26, 2024 · N8574Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO L/H SIDE PLATE HAS CORROSION AT SEVERAL N/P HOLES STA 767-787 LBL 21-22 WL 156. FOUND CORROSION ON L/H SIDE PLATE AT STA. 767-787 TO BE OUT OF LIMITS PER SRM 3-00-53-1A-2.;[02] L/H SIDE PLATE WAS FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 AND A
- [SDR SWAA2024062890204](https://openairdocs.org/sdr/SWAA2024062890204.md): Shield · corroded · May 26, 2024 · N8574Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT FLOOR STRUCTURES SHIELD BETWEEN BS 767 & 767+25, RBL 21-22 HAS SURFACE CORROSION. REMOVED CORROSION PER SRM 53-60-15-1A-1 (0.045' REMAINING THICKNESS). SHIELD IS OUT OF LIMITS PER SRM 53-60-15-1A-1. REMOVED SHIELD ASSY IAW SRM 51-40-02.
- [SDR SWAA2024062790197](https://openairdocs.org/sdr/SWAA2024062790197.md): Support Bracket · cracked · May 26, 2024 · N8574Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT WASTE TANK ACCESS PANEL STANCHION SUPPORT BRACKET AT STA 867 LBL 15 CRACKED. REMOVED AND REPLACED AFT CARGO BLKHD STANCHION SUPPORT BRACKET AT STA. 867 LBL 15 IAW SRM 51-40-02.
- [SDR SWAA2024070189317](https://openairdocs.org/sdr/SWAA2024070189317.md): Seal · cracked · May 24, 2024 · N8574Z · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous Structure
  > L/H HORZ. STABILIZER FWD ATTACH FITTING UPPER SLIDER SEAL IS CRACKED AT FWD AND AFT SIDES. REMOVED L/H HORIZONTAL STAB. UPPER SLIDER SEAL IAW AMM 53-31-31. INSTALLED L/H HORIZONTAL STAB. UPPER SLIDER SEAL IAW AMM 53-31-31.
- [SDR SWAA2024070189318](https://openairdocs.org/sdr/SWAA2024070189318.md): Seal · cracked · May 24, 2024 · N8574Z · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous Structure
  > R/H HORZ. STABILIZER FWD ATTACH FITTING UPPER SLIDER SEAL IS CRACKED AT AFT END. REMOVED R/H HORIZONTAL STAB. UPPER SLIDER SEAL IAW AMM 53-31-31. INSTALLED R/H HORIZONTAL STAB. UPPER SLIDER SEAL IAW AMM 53-31-31.;[03] INSPECTED WORK PERFORMED
- [SDR SWAA2024070189306](https://openairdocs.org/sdr/SWAA2024070189306.md): Bonding Jumper · corroded · May 23, 2024 · N8574Z · Boeing 7378H4 · Fuselage Main, Bulkhead Fuselage wiring
  > A/C ACCESS PANEL 192CL 2ND FROM FWD END BONDING WIRED TERMINAL END CORRODED.<[01] PERFORMED RESISTANCE CHECK PER AMM 52-48-42 AND SWPM 20-20-00;[02] VERIFIED
- [SDR SWAA2024070189083](https://openairdocs.org/sdr/SWAA2024070189083.md): Support Angle · cracked · May 23, 2024 · N8574Z · Boeing 7378H4 · Wing Miscellaneous Structure
  > UPPER FIXED TRAILING EDGE PANEL I/B OF #5 SPOILER LOWER ANGLE BRACKET CRACKED. REMOVED DEFLECTION RIB CLIP FROM AIRCRAFT I.A.W SRM 51-40-02.. LOCATED AND DRILLED NEW DEFLECTION RIB CLIP I.A.W SRM 51-40-05. INSTALLED DEFLECTION RIB CLIP I.A.W SRM 51-40-02

Next page: https://openairdocs.org/aircraft/N8574Z/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 = 'N8574Z' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8574Z/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.