# Service difficulty reports: N8568Z

A list on [N8568Z](https://openairdocs.org/aircraft/N8568Z.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 · 62 reports

- [SDR SWAA2026101239768](https://openairdocs.org/sdr/SWAA2026101239768.md): Skin · delaminated · Oct 7, 2026 · N8568Z · Boeing 7378H4 · Trailing Edge Flaps
  > RIGHT OTBD T/E FLAP LOWER SKIN DELAMINATED, APPROX 26 1/4 INBD FROM INBD EDGE & 7 1/4 FROM T/E. R & R IAW AMM 27-51-22-401.
- [SDR SWAA2026050896237](https://openairdocs.org/sdr/SWAA2026050896237.md): Battery Pack · inoperative · May 7, 2026 · N8568Z · Boeing 7378H4 · Emergency Lighting
  > CAPTAIN SIDE FWD OVERWING EMERGENCY LIGHT OUT. REMOVED AND REPLACED BATTERY PACK AT STA 500C+7 CAPTAIN SIDE BEHIND AIR GRILLE ON ROW 7ABC. PER AMM 33-51-06.
- [SDR SWAA2026040184339](https://openairdocs.org/sdr/SWAA2026040184339.md): Engine · bird ingestion · Mar 28, 2026 · N8568Z · Boeing 7378H4 · Engine (Turbine/Turboprop)
  > DURING CLIMB, BIRD STRIKE NR 1 ENGINE. VIBRATION INCREASED, HAD ABNORMAL ODORS, ENGINE STILL MAINTAINED THRUST. C/W BIRD STRIKE CONDITIONAL INSPECTION IAW AMM 05-51-18. C/W BIRD STRIKE VISUAL INSPECTION OF NR 1 ENG IAW MT 772-00-00, C/W BIRD STRIKE BORES
- [SDR SWAA2026030575689](https://openairdocs.org/sdr/SWAA2026030575689.md): Sign · out of adjust · Mar 2, 2026 · N8568Z · Boeing 7378H4 · Emergency Lighting
  > CEILING EMERGENCY EXIT SIGN IS CROOKED AT THE OVER WING EXIT. ADJUSTED CEILING EMERGENCY EXIT SIGN IAW AMM 33-51-01.
- [SDR SWAA2025082908633](https://openairdocs.org/sdr/SWAA2025082908633.md): Lamp · inoperative · Aug 26, 2025 · N8568Z · Boeing 737824 · Emergency Lighting
  > AFT CENTER OVERHEAD EMERGENCY EXIT SIGN HAS MULTIPLE BULBS BURNT OUT. RELAMPED AFT CENTER OVERHEAD EMERGENCY EXIT SIGN AND OPS CHECK GOOD IAW SWA B737-800 AMM 33-51-01-960-801.
- [SDR SWAA2025082907737](https://openairdocs.org/sdr/SWAA2025082907737.md): Handle · loose · Aug 21, 2025 · N8568Z · Boeing 7378H4 · Service Doors
  > ASSIST HANDLE IS LOOSE ON G7 GALLEY. SECURED ASSIST HANDLE ON G-7 IAW AMM 25-31-71 & SRM 51-40-02.
- [SDR SWAA2025082907163](https://openairdocs.org/sdr/SWAA2025082907163.md): Handle · loose · Aug 21, 2025 · N8568Z · Boeing 7378H4 · Passenger/Crew Doors
  > UPPER AND LOWER ASSIST HANDLES ARE LOOSE ON L1 DOOR LINER. SECURED UPPER AND LOWER DOOR ASSIST HANDLES IAW AMM 52-11-31 & SRM 51-40-02.
- [SDR SWAA2025082907164](https://openairdocs.org/sdr/SWAA2025082907164.md): Handle · loose · Aug 21, 2025 · N8568Z · Boeing 7378H4 · Passenger/Crew Doors
  > ASSIST HANDLE IS LOOSE ON L2 FWD DOOR SURROUND. SECURED ASSIST HANDLE ON L-2 DOOR FWD SURROUND LINING IAW AMM 25-21-25 & SRM 51-40-02.
- [SDR SWAA2025082907165](https://openairdocs.org/sdr/SWAA2025082907165.md): Handle · loose · Aug 21, 2025 · N8568Z · Boeing 7378H4 · Service Doors
  > ASSIST HANDLES ARE LOOSE ON R2 DOOR LINER AND R2 FOWARD SURROUND. SECURED R-2 DOOR AND FWD SURROUND ASSIST HANDLES IAW AMM 52-41-31; 25-21-25 & SRM 51-40-02.
- [SDR SWAA2025061079213](https://openairdocs.org/sdr/SWAA2025061079213.md): Slide · loose · Jun 7, 2025 · N8568Z · Boeing 7378H4 · Escape Slide
  > FORWARD ENTRY DOOR EMERGENCY SLIDE LOOSE AND SAGS; NEEDS REPACKING<[01] PERF ENTRY DOOR ESCAPE SLIDE PACK CHECK REF AMM 25-66-01; SLIDE OK FOR SERVICE
- [SDR SWAA2025010682899](https://openairdocs.org/sdr/SWAA2025010682899.md): Battery Pack · inoperative · Jan 4, 2025 · N8568Z · Boeing 7378H4 · Emergency Lighting
  > FWD AND AFR RIGHT EXIT DOOR AND SCAPE SLIDE EMERGENCY LIGHTS INOP<[01] R/R FWD AND AFT RIGHT EXIT AND SCAPE SLIDE EMERGENCY LIGHT POEW PACKS IAW AMM 3351-06
- [SDR SWAA2024062705789](https://openairdocs.org/sdr/SWAA2024062705789.md): Flashlight · inoperative · Jun 25, 2024 · N8568Z · Boeing 7378H4 · Emergency Equipment
  > LH AFT F/A STATION EMERGENCY FLASHLIGHT INOP.<[01] REMOVED AND REPLACED LEFT AFT FLIGHT ATTENDANT EMERGENCY FLASHLIGHT. OPS CHECK PERFORMED; OPS CEHCK GOOD NO DEFECTS NOTED AT THIS TIME REF AMM 25-64-00
- [SDR SWAA2024062404585](https://openairdocs.org/sdr/SWAA2024062404585.md): Cradle · inoperative · Jun 22, 2024 · N8568Z · Boeing 7378H4 · Emergency Equipment
  > AFT FLIGHT ATTENDANT EMERGENCY FLASHLIGHT WILL NOT TEST<[01] SECURED FLASHLIGHT IN MOUNTING BRACKET PER AMM 25-64-00; OPS CHECK GOOD.
- [SDR SWAA2024041774906](https://openairdocs.org/sdr/SWAA2024041774906.md): Battery · failed · Apr 14, 2024 · N8568Z · Boeing 7378H4 · Emergency Equipment
  > FWD EMERGENCY FLASHLIGHTS WILL NOT TEST<[01] 01 - REMOVED AND REPLACED PER [AMM 25-64-00-900-806-NG (FLASHLIGHT BATTERY REPLACEMENT - PERMANENT)]
- [SDR SWAA2024041770110](https://openairdocs.org/sdr/SWAA2024041770110.md): Battery Pack · inoperative · Apr 3, 2024 · N8568Z · Boeing 7378H4 · Emergency Lighting
  > FOWARD AND AFT ENTRY EMERGENCY LIGHTS INOP<[01] REMOVED AND REPLACED FOWARD AND AFT ENTRY EMERGENCY BATTERY PACKS PER MM 33-51-06; OPS CHECKS GOOD PER MM 33-51-00;[02] INSPECTED WORK PERFORMED
- [SDR SWAA2024041770109](https://openairdocs.org/sdr/SWAA2024041770109.md): Power Supply · inoperative · Apr 3, 2024 · N8568Z · Boeing 7378H4 · Emergency Lighting
  > LEFT AND RIGHT EMERGENCY OVER WING EXIT LOCATORS STA. 576;INOP<[01] 01 - REMOVED AND REPLACED PER [AMM 33-51-06-960-806-NG (POWER SUPPLY - POWER SUPPLY REPLACEMENT - PERMANENT)] <BR>POWER SUPPLY (M01694) OPS CHECKED GOOD PER AMM 33-51-06.;[02] INSPECTED WORK P
- [SDR SWAA2024041768967](https://openairdocs.org/sdr/SWAA2024041768967.md): Scuff Plate · cracked · Mar 30, 2024 · N8568Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO FWD SCUFF PLATE CORNER CRACKED<[01] REPAIRED PER PO# P8083505 AND INSTALLED SCUFF PLATE PER AMM 53-11-02-420-801.;[02] REMOVED AND REPLACED SCUFF PLATE PER AMM 53-11-02-420-801.;[03] INSPECTED WORK PERFORMED. REMOVED AND REPLACED SCUFF PLATE PER AMM
- [SDR SWAA2024041768968](https://openairdocs.org/sdr/SWAA2024041768968.md): Scuff Plate · cracked · Mar 30, 2024 · N8568Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO AFT SCUFF PLATE CORNER CRACKED<[01] REPAIRED PER PO# P8083506 AND INSTALLED SCUFF PLATE PER AMM 53-11-02-420-801.;[02] REMOVED AND REPLACED SCUFF PLATE PER AMM 53-11-02-420-801.;[03] INSPECTED WORK PERFORMED. REMOVED AND REPLACED SCUFF PLATE PER AMM
- [SDR SWAA2024041768293](https://openairdocs.org/sdr/SWAA2024041768293.md): Seal · cracked · Mar 27, 2024 · N8568Z · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous Structure
  > LEFT HORIZONTAL STAB UPPER FWD SLIDER SEAL CRACKED ON THE FWD AND AFT EDGES.<[01] REMOVED CRACKED UPPER FWD SLIDER SEAL AT L/H HORIZONTAL STAB IAW AMM 53-31-31.;[02] DRILLED NEW SLIDER SEAL PER SRM 51-10-02 AND INSTALLED NEW SLIDER SEAL PER AMM 53-31-31.
- [SDR SWAA2024041768294](https://openairdocs.org/sdr/SWAA2024041768294.md): Seal · cracked · Mar 27, 2024 · N8568Z · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous Structure
  > RIGHT HORIZONTAL STAB UPPER FWD SLIDER SEAL CRACKED ON THE FWD AND AFT EDGES.<[01] REMOVED SLIDER PINS PER SOPM20-50-01;[02] REMOVED; DRILLED; AND ASSEMBLED NEW SLIDER PLATE PER SRM 51-10-02 AND 51-40-02. OK TO REINSTALL.;[03] INSTALLED NEW SLIDER PLATE PER AM
- [SDR SWAA2024041766043](https://openairdocs.org/sdr/SWAA2024041766043.md): Battery Pack · failed · Mar 21, 2024 · N8568Z · Boeing 7378H4 · Emergency Lighting
  > LEFT WING EMERGENCY EXIT ILLUMINATED SIGN ELECTRICAL; PLUGGED INTO THE OVER-WING EXIT DOOR SURROUND HEATER WIRING.<[01] BATTERY CHARGER FOR LEFT FOWARD OVER WING EMERGENCY EXIT LIGHT WAS REPLACED ON CARD TTG8Q00SHP5V LINE 2972.;[02] VERIFIED CORRECTIVE ACTION
- [SDR SWAA2024041766042](https://openairdocs.org/sdr/SWAA2024041766042.md): Skin · delaminated · Mar 20, 2024 · N8568Z · Boeing 7378H4 · Trailing Edge Flaps
  > LEFT HAND WING OUTBOARD TRAILING EDGE FLAP HAS AN AREA OF DELAMINATION AT IB END LOWER SURFACE (MKD).<[01] REMOVED DAMAGE SKIN PER SRM 57-53-01-2R-14;[02] INSPECTED WORK PERFORMED ON C/A #1;[03] REPAIRED DAMAGED AREA PER SRM 57-53-01-2R-14.;[04] RII- INSPECTED
- [SDR SWAA2024041765150](https://openairdocs.org/sdr/SWAA2024041765150.md): Shim · out of position · Mar 18, 2024 · N8568Z · Boeing 7378H4 · Fuselage, Powerplant Attach Fittings
  > SHIM IS NOT CONFIGURED PROPERLY PER E.A. 24-153-00664-WIP2 LINE #2804 TTG8Q00S5KFB<[01] REMOVED LAV MOUNT TO F.O.M IAW SRM 51-40-02.;[02] REMOVED OLD SHIM IAW SRM 51-40-02;[03] FABRICATED NEW SHIM; ALODINE AND PRIMED IAW EA 24-153-00664.;[04] C/W INSPECTION OF
- [SDR SWAA2024041764164](https://openairdocs.org/sdr/SWAA2024041764164.md): Crease Beam · cracked · Mar 16, 2024 · N8568Z · Boeing 7378H4 · Fuselage Main, Structure
  > R/H CREASE BEAM INNER CHORD CRACK AT STA 377 R/H AT STA 377 CREASE BEAM INNER CHORD CRACKED.<[01] HEAT TREAT ANGLE 7075-0 TO 7075 T6 VENDER SERVICES REQUESTED SEE SA-M 1057 P.O. NUMBER P804525;[02] HEAT TREAT ANGLE 7075-0 TO 7075 T6 VENDER SERVICES REQUESTED S
- [SDR SWAA2024041768553](https://openairdocs.org/sdr/SWAA2024041768553.md): Seal · debonded · Mar 13, 2024 · N8568Z · Boeing 7378H4 · Nacelle/Pylon, Main Frame
  > PANEL 433BT PANEL ASSEMBLY - UPPER SPAR WEB - #1 ENGINE HAS DISBONDED RUBBER SEAL.<[01] REPLACED PANEL; PANEL TO BE INSTALLED ON CLOSE TASK CARD TTG8Q00R9FRX (#960)
- [SDR SWAA2024041762439](https://openairdocs.org/sdr/SWAA2024041762439.md): Floorbeam · corroded · Mar 13, 2024 · N8568Z · Boeing 7378H4 · Fuselage Main, Floor Beam
  > AFT WET AREA FLOOR BEAM STA. 947.5 AT L-24 HAS EVIDENCE OF CORROSION<[01] REMOVED LAV. MOUNT TO F.O.M IAW SRM 51-40-02.;[02] REMOVED LAV. MOUNT TO F.O.M IAW SRM 51-40-02. AFTER REMOVAL OF LAV MOUNT CORROSION CONFIRMED FOUND ON FLOOR BEAM UPPER CAP.;[03] REMOVE
- [SDR SWAA2024041762959](https://openairdocs.org/sdr/SWAA2024041762959.md): Web · corroded · Mar 13, 2024 · N8568Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR CUTOUT LOWER THRESHOLD WEB HAS CORROSION.<[01] REMOVED CORROSION PER SRM 53-60-15-1A-1 (0.042' REMAINING THICKNESS). THRESHOLD WEB IS OUT OF LIMITS PER SRM 53-60-15-1A-1.;[02] REMOVED AFT CARGO THRESHOLD WEB IAW SRM 51-40-02.;[03] DRILLED UP AND
- [SDR SWAA2024041762266](https://openairdocs.org/sdr/SWAA2024041762266.md): Web · corroded · Mar 12, 2024 · N8568Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO STA. 485 RBL 31; CORROSION ON ENTRY DOOR THRESHOLD WEB PANEL.<[01] REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAGE DEPTH TO BE.015?. DAMAGE FOUND TO BE OUT OF LIMITS I.A.W SRM 53-30-15-1A-1.;[02] REMOVED LOWER THRESHOLD WEB PANEL I.A.W. SRM 51-40
- [SDR SWAA2024041762273](https://openairdocs.org/sdr/SWAA2024041762273.md): Angle · corroded · Mar 12, 2024 · N8568Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT LEFT TRANSITION ANGLE (SIDE PLATE) HAS CORROSION AT NUTPLATE SCREW HOLES AT STA 727J INCHES TO STA 787. AREA MARKED.<[01] REMOVED CORROSION PER SRM 53-00-53-1A-2 (0.038' REMAINING THICKNESS). SIDEPLATE (TRANSITION ANGLE) IS OUT OF LIMITS
- [SDR SWAA2024041761926](https://openairdocs.org/sdr/SWAA2024041761926.md): Floor Support · corroded · Mar 12, 2024 · N8568Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CABIN WET AREA FLOOR INTERCOSTAL LBL-24 UPPER ATTACH ANGLE HAS CORROSION AT STA. 947 ATTACH POINT.<[01] REMOVED UPPER ATTACH ANGLE TO F.O.M AT LBL 24 IAW SRM 51-40-02.;[02] REMOVED CORROSION ON ATTACH ANGLE; MAT. REMOVED IS.004; MAT THICKNESS REMAINING IS
- [SDR SWAA2024041761927](https://openairdocs.org/sdr/SWAA2024041761927.md): Floorbeam · corroded · Mar 12, 2024 · N8568Z · Boeing 7378H4 · Fuselage Main, Floor Beam
  > AFT WET AREA FLOOR BEAM STA. 947 HAS EVIDENCE OF CORROSION AT LAVD OB MOUNT.<[01] REMOVED LAV MOUNT TO F.O.M IAW SRM 51-40-02.;[02] REMOVED LAV MOUNT TO F.O.M IAW SRM 51-40-02. AFTER REMOVAL OF LAV MOUNT CORROSION IS CONFIRMED FOUND ON FLOOR BEAM UPPER CAP AT
- [SDR SWAA2024041761939](https://openairdocs.org/sdr/SWAA2024041761939.md): Floorbeam · broken · Mar 12, 2024 · N8568Z · Boeing 7378H4 · Fuselage Main, Floor Beam
  > BREAKAWAY INTERCOSTAL AT STA 540 BETWEEN BL0 AND LBL 24.75 IS BROKEN<[01] REMOVED INTERCOSTAL FROM STA 540 BL0 TO LBL 24.75 PER SRM 51-40-02;[02] INSTALLED NEW INTERCOSTAL AT STA 540 BL 0 TO LBL 24.75 IAW SRM 51-40-02.;[03] CORRECTIVE ACTION #2 C/W.
- [SDR SWAA2024041762264](https://openairdocs.org/sdr/SWAA2024041762264.md): Channel · corroded · Mar 12, 2024 · N8568Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO STA.500I LBL 24 TO RBL 24; BULKHEAD NUTPLATE CHANNEL HAS AREAS OF CORROSION.<[01] REMOVED CHANNEL PER SRM 51-40-02;[02] APPROVED CA #1.;[03] REMOVED AND REPLACED PER SRM 51-40-02;[04] VERIFIED REPLACEMENT OF CHANNEL PER SRM 51-40-02
- [SDR SWAA2024041762271](https://openairdocs.org/sdr/SWAA2024041762271.md): Angle · corroded · Mar 12, 2024 · N8568Z · Boeing 7378H4 · Cargo Compartments
  > AFT CARGO COMPARTMENT LEFT TRANSITION ANGLE (SIDE PLATE) HAS CORROSION AT NUTPLATE SCREW HOLES AT STA 727F+9 INCHES TO STA 727F+13 INCHES. AREA MARKED.<[01] REMOVED CORROSION PER SRM 53-00-53-1A-2 (0.038' REMAINING THICKNESS). SIDEPLATE (TRANSITION ANGLE) IS O
- [SDR SWAA2024041762248](https://openairdocs.org/sdr/SWAA2024041762248.md): Angle · corroded · Mar 12, 2024 · N8568Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT LEFT TRANSITION ANGLE (SIDE PLATE) HAS CORROSION AT NUTPLATE SCREW HOLE AT STA 727G+9 INCHES. AREA MARKED.<[01] REMOVED CORROSION PER SRM 53-00-53-1A-2 (0.039' REMAINING THICKNESS). SIDEPLATE (TRANSITION ANGLE) IS OUT OF LIMITS PER SRM 53
- [SDR SWAA2024041762272](https://openairdocs.org/sdr/SWAA2024041762272.md): Angle · corroded · Mar 12, 2024 · N8568Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT LEFT TRANSITION ANGLE (SIDE PLATE) HAS CORROSION AT NUTPLATE SCREW HOLES AT STA 727I+7 INCHES TO STA 727I+18 INCHES. AREA MARKED.<[01] REMOVED CORROSION PER SRM 53-00-53-1A-2 (0.037' REMAINING THICKNESS). SIDEPLATE (TRANSITION ANGLE) IS O
- [SDR SWAA2024041762274](https://openairdocs.org/sdr/SWAA2024041762274.md): Angle · cracked · Mar 12, 2024 · N8568Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT FLOOR LEFT TRANSITION ANGLE (SIDE PLATE) HAS 1/4 INCH CRACK WITH CORROSION AT BEND RADIUS LOCATED AT STA 727G+5. AREA MARKED.<[01] REMOVED AFT CARGO LH SIDE PLATE ASSY. FROM STA. 727 TO 847 IAW SRM 51-40-02.;[02] OK TO INSTALL REPAIR PART
- [SDR SWAA2024041762280](https://openairdocs.org/sdr/SWAA2024041762280.md): Floor Support · corroded · Mar 12, 2024 · N8568Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO FLOOR STRUCTURE INTERCOSTAL FWD OF CARGO DOOR CUTOUT HAS CORROSION AT NUTPLATE SCREW HOLES. STA.767 TO STA.787 RBL22.<[01] REMOVED CORROSION PER SRM 53-60-15-1A-1 (0.047' REMAINING THICKNESS). SHIELD (INTERCOSTAL) IS OUT OF LIMITS PER SRM 53-60-15-1A
- [SDR SWAA2024041762277](https://openairdocs.org/sdr/SWAA2024041762277.md): Angle · corroded · Mar 12, 2024 · N8568Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT RIGHT TRANSITION ANGLE HAD CORROSION AT NUTPLATE HOLES FROM BS 727I TO 767. REMOVED CORROSION PER SRM 53-00-53-1A-2, 0.038' REMAINING THICKNESS. TRANS PANEL IS OUT OF LIMITS IAW SRM 53-00-53-1A-2. CUT OUT DAMAGED TRANSITION ANGLE IAW SR
- [SDR SWAA2024041764532](https://openairdocs.org/sdr/SWAA2024041764532.md): Floor Panel · pulled · Mar 11, 2024 · N8568Z · Boeing 7378H4 · Fuselage Floor Panel
  > PANEL 221BF HAS PULLED FIBERS.<[01] PANEL REMOVED AND NEW PANEL INSTALLED ON TTG8Q00R9G1R LINE 1118 OF THIS CHECK. TORQUE WRENCH QDR50 S/N 96702.;[02] PANEL REMOVED AND NEW PANEL INSTALLED ON TTG8Q00R9G1R LINE 1118 OF THIS CHECK. TORQUE WRENCH QDR50 S/N 96702.
- [SDR SWAA2024041761754](https://openairdocs.org/sdr/SWAA2024041761754.md): Scuff Plate · cracked · Mar 11, 2024 · N8568Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT AFT CORNER SCUFF PLATE CRACKED.<[01] INSTALLED NEW AFT THRESHOLD CORNER PLATE PER AMM 53-11-02.;[02] REMOVED AND REPLACED AFT THRESHOLD CORNER PLATE PER AMM 53-11-02.
- [SDR SWAA2024041761612](https://openairdocs.org/sdr/SWAA2024041761612.md): Floor Panel · pulled · Mar 11, 2024 · N8568Z · Boeing 7378H4 · Fuselage Floor Panel
  > PANEL 222CF PANEL ASSEMBLY - PASSENGER CABIN FLOOR HAS PULLED FIBERS<[01] REMOVED AND REPLACED PANEL 222CF PER AMM 53-21-00. REF TASK CARD TTG8Q008EVNF FOR TOOLING AND PART INFO;[02] INSPECTION C/W REMOVED AND REPLACED PANEL 222CF PER AMM 53-21-00. REF TASK CA
- [SDR SWAA2024041761908](https://openairdocs.org/sdr/SWAA2024041761908.md): Floor Support · corroded · Mar 11, 2024 · N8568Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CABIN WET AREA FLOOR INTERCOSTAL L-24 STA 947 HAS EVIDENCE OF CORROSION.<[01] REMOVED LAV D IB MOUNT TO F.O.M IAW SRM 51-40-02.;[02] REMOVED CORROSION ON FLOOR BEAM STA. 947 AT LBL 24. DEPTH REMOVED IS.041; MAT REMAINING IS.139; FOUND TO BE OUT OF LIMITS
- [SDR SWAA2024041761604](https://openairdocs.org/sdr/SWAA2024041761604.md): Floor Panel · pulled · Mar 10, 2024 · N8568Z · Boeing 7378H4 · Fuselage Floor Panel
  > PANEL 232BF PANEL ASSEMBLY - RH PASSENGER CABIN FLOOR HAS PULLED FIBERS<[01] 01 - REMOVED AND REPLACED PER [AMM 53-21-00-400-801-NG (PASSENGER CABIN FLOOR PANEL INSTALLATION - PERMANENT)];[02] C/W INSPECTION
- [SDR SWAA2024041761610](https://openairdocs.org/sdr/SWAA2024041761610.md): Floor Panel · pulled · Mar 10, 2024 · N8568Z · Boeing 7378H4 · Fuselage Floor Panel
  > PANEL 232AF PANEL ASSEMBLY - RH PASSENGER CABIN FLOOR HAS PULLED FIBERS.<[01] 01 - REMOVED AND REPLACED PER [AMM 53-21-00-400-801-NG (PASSENGER CABIN FLOOR PANEL INSTALLATION - PERMANENT)];[02] C/W INSPECTION
- [SDR SWAA2024041761611](https://openairdocs.org/sdr/SWAA2024041761611.md): Floor Panel · pulled · Mar 10, 2024 · N8568Z · Boeing 7378H4 · Fuselage Floor Panel
  > PANEL 222DF PANEL ASSEMBLY - PASSENGER CABIN FLOOR HAS PULLED FIBERS<[01] 01 - REMOVED AND REPLACED PER [AMM 53-21-00-400-801-NG (PASSENGER CABIN FLOOR PANEL INSTALLATION - PERMANENT)];[02] C/W INSPECTION
- [SDR SWAA2024041761208](https://openairdocs.org/sdr/SWAA2024041761208.md): Angle · cracked · Mar 9, 2024 · N8568Z · Boeing 7378H4 · Wing Miscellaneous Structure
  > LEFT WING TRAILING EDGE SHELF PANEL AT DEFLECTION RIB HAS CRACKED ANGLE BRACKET. (MARKED)<[01] LOCATED AND DRILLED REPLACEMENT NEW DEFLECTION RIB CLIP (MPN 115A6260-1) I.A.W SRM 51-40-05;[02] INSPECTED WORK PERFORMED ON C/A #1;[03] INSTALLED BRACKET PER SRM 51
- [SDR SWAA2024041766895](https://openairdocs.org/sdr/SWAA2024041766895.md): Fastener · loose · Mar 8, 2024 · N8568Z · Boeing 7378H4 · Nacelle/Pylon, Plate/Skin
  > #1 INLET COWL OUTER LIP SKIN HAS SEVERAL LOOSE FASTENERS AT THE 6 O'CLOCK POSITION (MKD)<[01] REMOVED DISCREPANT FASTENERS I.A.W SRM 51-40-02.;[02] C/W NDT PER PART 6 51-00-00 PROCEDURE 23 AND PART 6 53-30-00 PROCEDURE 3. NO DEFECTS NOTED.;[03] INSTALLED FIRST
- [SDR SWAA2024012945075](https://openairdocs.org/sdr/SWAA2024012945075.md): Slide · dislodged · Jan 26, 2024 · N8568Z · Boeing 7378H4 · Escape Slide
  > L1 DOOR SLIDE FELL OUT<[01] RE-INSTALLED L1 DOOR SLIDE IAW MT 725-61-06.
- [SDR SWAA2023110919477](https://openairdocs.org/sdr/SWAA2023110919477.md): Girt Bar · loose · Nov 8, 2023 · N8568Z · Boeing 7378H4 · Emergency Equipment
  > MAIN CABIN DOOR AFT GIRT BAR CLIP LOOSE. / [01] REPLACED MISSING RIVET ON L1 DOOR GIRT BAR CLIP PER SIP.

Next page: https://openairdocs.org/aircraft/N8568Z/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 = 'N8568Z' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8568Z/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.