# Service difficulty reports: N8502Z

A list on [N8502Z](https://openairdocs.org/aircraft/N8502Z.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 · 70 reports

- [SDR SWAA2026092833996](https://openairdocs.org/sdr/SWAA2026092833996.md): Fairing · pulled · Sep 22, 2026 · N8502Z · Boeing 7378H4 · Trailing Edge Flaps
  > NR 3 FLAP TRACK AFT FAIRING HAS 7 CONSECUTIVE FASTENERS MISSING OR PULLED THROUGH ALONG OB UPPER EDGE NEAR TAIL CONE REMOVED AND REPLACED THE #3 FLAP TRACK AFT FAIRING IAW AMM 27-51-18-400-802. REMOVED AND REPLACED THE #3 FLAP TRACK AFT FAIRING IAW AMM 27-51-1
- [SDR SWAA2026092804817](https://openairdocs.org/sdr/SWAA2026092804817.md): Light · inoperative · Sep 21, 2026 · N8502Z · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY DOME LIGHT L273 IS INOP REMOVED REPLACED AND PERFOMED GOOD OPS CHECK OF THE DOME LIGHT L273 IAW AMM 33-51-01-960-801.
- [SDR SWAA2026092871372](https://openairdocs.org/sdr/SWAA2026092871372.md): Lamp · inoperative · Sep 21, 2026 · N8502Z · Boeing 7378H4 · Emergency Lighting
  > EXIT SIGN AT AFT ENTRY DOOR HAS SEVERAL INOPERATIVE LAMPS. REPLACED THE LAMPS AND PERFORMED A GOOD OPS CHECK IAW AMM 33-51-01-960-801.
- [SDR SWAA2026092801323](https://openairdocs.org/sdr/SWAA2026092801323.md): Seat · out of adjust · Sep 20, 2026 · N8502Z · Boeing 7378H4 · Passenger Compartment Equipment
  > SEAT ROW 14A RECLINE REQUIRES ADJUSTMENT. ADJUSTED SEAT 14 A IAW CMM 25-23-65.
- [SDR SWAA2026092890689](https://openairdocs.org/sdr/SWAA2026092890689.md): Strap · loose · Sep 17, 2026 · N8502Z · Boeing 7378H4 · Emergency Equipment
  > AFT LT GALLEY DOOR SAFETY YELLOW STRAP ASSEMBLY FOUND BROKEN. ATTACHED THE STRAP AND TIGHTENED AFT ENTRY DOOR ASSIST HANDLE IAW AMM 25-21-25-420-801 AND AIPC 25-66-10-02.
- [SDR SWAA2025092914113](https://openairdocs.org/sdr/SWAA2025092914113.md): Skin · delaminated · Sep 12, 2025 · N8502Z · Boeing 7378H4 · Trailing Edge Flaps
  > LEFT OTBD AFT FLAP UPPER SURFACE HAS AREA OF DELAMONATION AT INBD END JUST FWD OF T/E. REMOVED; REPLACED AND ADJUSTMENT CHECKED LT O/B AFT FLAP IAW AMM 27-51-22. VERIFIED TORQUES AND SAFETIES; ADJUSTMENT CHECK GOOD. VERIFIED COMPLETION CORRECTIVE ACTION 1
- [SDR SWAA2025092513374](https://openairdocs.org/sdr/SWAA2025092513374.md): Slide · out of adjust · Sep 10, 2025 · N8502Z · Boeing 7378H4 · Escape Slide
  > FED SLIDE SAGGING AND NEEDS TO BE RIG CHECKED. ADJUSTMENT ON FED WAS VERIFIED IAW AMM 52-11-00-820-801 STEP 2.I THROUGH 2.T AND PERFORMED STEP 2.N AND 2.U. PERFORMED FED SYSTEM AND WARNING TEST IAW AMM 52-11-00-700-804 AND AMM 52-71-11-820-801. SATISFACTORY
- [SDR SWAA2025092918597](https://openairdocs.org/sdr/SWAA2025092918597.md): Rib · loose · Sep 9, 2025 · N8502Z · Boeing 7378H4 · Wing, Rib/Bulkhead
  > RIGHT WING DEFLECTION CONTROL RIB LOOSE. REPAIRED RT WING DEFLECTION CONTROL RIB IAW SRM 57-51-02-2R-4 REPAIR 4, SRM 57-51-02-2R-1, REPAIR 1, AND SRM 57-51-02-2R-3, REPAIR 3.
- [SDR SWAA2025092918598](https://openairdocs.org/sdr/SWAA2025092918598.md): Rib · loose · Sep 9, 2025 · N8502Z · Boeing 7378H4 · Wing, Rib/Bulkhead
  > LEFT WING DEFLECTION CONTROL RIB LOOSE. REPAIRED LT WING DEFLECTION CONTROL RIB IAW SRM 57-51-02-2R-4 REPAIR 4, SRM 57-51-02-2R-1 REPAIR 1, AND SRM 57-51-02-2R-3 REPAIR3.
- [SDR SWAA2025092913574](https://openairdocs.org/sdr/SWAA2025092913574.md): Skin · pulled · Sep 8, 2025 · N8502Z · Boeing 7378H4 · Nacelle/Pylon, Plate/Skin
  > PULLED THROUGH FASTENERS AT 10 O CLOCK POSITION RIGHT INLET COWL OUTER LIPSKIN (MARKED)<[01] NEW / SERVICEABLE INLET COWL P/N: 314M2100503. S/N: 4308001 WILL BE REPLACED IN FAULT TTG8Q0156HRJ;[02] VERIFIED CORRECTIVE ACTION 1
- [SDR SWAA2025010683413](https://openairdocs.org/sdr/SWAA2025010683413.md): Cover · missing · Jan 6, 2025 · N8502Z · Boeing 7378H4 · Emergency Lighting
  > AFT GALLEY EXIT SIGN COVER (LEFT SIDE) MISSING<[01] R&R AFT GALLEY EXIT SIGN COVER IAW SIP
- [SDR SWAA2024101045773](https://openairdocs.org/sdr/SWAA2024101045773.md): Lamp · inoperative · Oct 7, 2024 · N8502Z · Boeing 7378H4 · Emergency Lighting
  > AFT LH SERVICE DOOR EMERGENCY EXIT LIGHT INOP.<[01] R&R AFT LH SERVICE DOOR EMERGENCY EXIT LIGHT LAMP PR AMM 33-51-04. OPS CHECK GOOD
- [SDR SWAA2024092439186](https://openairdocs.org/sdr/SWAA2024092439186.md): Battery Pack · no test · Sep 18, 2024 · N8502Z · Boeing 7378H4 · Emergency Lighting
  > L/H OVERWING EMERGENCY LIGHT BATTERY PACK WEAK - FAILS AT 1 MINUTE<[01] REPLACED L/H OVERWING EMERGENCY LIGHT BATTERY PACK M01694 PER AMM 33-51-06. OPS CHECK GOOD;[02] REPLACED L/H OVERWING EMERGENCY LIGHT BATTERY PACK M01694 PER AMM 33-51-06. OPS CHECK GOOD.
- [SDR SWAA2024092439187](https://openairdocs.org/sdr/SWAA2024092439187.md): Battery Pack · inoperative · Sep 18, 2024 · N8502Z · Boeing 7378H4 · Emergency Lighting
  > L/H AFT GALLEY EMERGENCY LIGHT BATTERY PACK INOP<[01] REMOVED AND REPLACED BATTERY PACK AT STA 952L PER MM 33-51-06.EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06;[02] INSPECTED AS REQUIRED. CORRECTIVE ACTION #1
- [SDR SWAA2024092439185](https://openairdocs.org/sdr/SWAA2024092439185.md): Battery Pack · inoperative · Sep 18, 2024 · N8502Z · Boeing 7378H4 · Emergency Lighting
  > R/H AFT GALLEY EMERGENCY LIGHT BATTERY PACK IS INOP<[01] REMOVED AND REPLACED BATTERY PACK AT STA 952R PER MM 33-51-06.EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06;[02] INSPECTED AS REQUIRED. CORRECTIVE ACTION #1
- [SDR SWAA2024092435029](https://openairdocs.org/sdr/SWAA2024092435029.md): Web · corroded · Sep 6, 2024 · N8502Z · Boeing 7378H4 · Fuselage Main, Structure
  > FWD CARGO LOWER SILL THRESHOLD WEB HAS SEVERE CORROSION.<[01] CORROSION IS OUT OF LIMITS PER SRM SRM 53-00-53-1A-2.;[02] REMOVED FASTENERS;REMOVED THREDHOLD WEB FOR REPLACEMENT PER SRM 51-40-02.;[03] CORROSION IS OUT OF LIMITS PER SRM SRM 53-30-15-1A-1.;[04] L
- [SDR SWAA2024092433621](https://openairdocs.org/sdr/SWAA2024092433621.md): Angle · corroded · Sep 3, 2024 · N8502Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO LH TRANSITION ANGLE HAS CORROSION AROUND FASTENER HOLES AT STA. 500C TO 500D<[01] BLENDED AREAS; REMOVED.020 IN. MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] VERIFIED CA #1. BLENDED AREAS; REMOVED.020 IN. MATERIAL; FOUND TO BE OU
- [SDR SWAA2024092532967](https://openairdocs.org/sdr/SWAA2024092532967.md): Panel · cracked · Sep 1, 2024 · N8502Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO FWD BULKHEAD PANEL 142NW HAS NUMEROUS CRACKS. MRKD<[01] REPLACED AFT CARGO FWD BULKHEAD PANEL 142NW. REF AMM 25-52-18. PANEL TO BE INSTALL ON CARD#TTG8Q00USZJE;[02] C/W INSPECTION
- [SDR SWAA2024092432984](https://openairdocs.org/sdr/SWAA2024092432984.md): Panel · cracked · Sep 1, 2024 · N8502Z · Boeing 7378H4 · Emergency Exits
  > R/H OVERWING FWD EXIT DOOR PANEL# 843CZ CRACKED.<[01] REMOVED AND REPLACED R/H OVERWING EXIT PANEL #843CZ PER SRM 51-40-02.;[02] C/W INSPECTION
- [SDR SWAA2024092432559](https://openairdocs.org/sdr/SWAA2024092432559.md): Angle · corroded · Aug 30, 2024 · N8502Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > R/H TRANSITION ANGLE IN FWD CARGO BIN HAS EVIDENCE OF CORROSION STA. 500C TO 500D (MARKED)<[01] REMOVED CORROSION PER SRM 51-10-02. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2..;[02] BLENDED AREAS; REMOVED.015' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM
- [SDR SWAA2024092432566](https://openairdocs.org/sdr/SWAA2024092432566.md): Angle · corroded · Aug 30, 2024 · N8502Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > L/H TRANSITION ANGLE IN FWD CARGO BIN HAS EVIDENCE OF CORROSION STA. 500D TO 500E (MARKED)<[01] BLENDED AREAS; REMOVED.006 IN. MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. THIS SECTION TO BE REPLACED ON NR# TTG8Q00VMHL5.;[02] BLENDED AREAS; REMO
- [SDR SWAA2024092432257](https://openairdocs.org/sdr/SWAA2024092432257.md): Floorbeam · corroded · Aug 30, 2024 · N8502Z · Boeing 7378H4 · Fuselage Main, Floor Beam
  > PASSENGER CABIN AFT WET AREA: CORROSION ON UPPER SURFACE OF FLOOR BEAM STA 947. LOCATED AT LBL 24 THROUGH LBL 26.<[01] PRIOR TO BLENDING; DEEPEST POINT OF CORROSION MEASURES.053'. REMAINING THICKNESS IS.127'. CORROSION DAMAGE IS OUT OF LIMITS PER SRM 53-70-5
- [SDR SWAA2024092432258](https://openairdocs.org/sdr/SWAA2024092432258.md): Floorbeam · corroded · Aug 30, 2024 · N8502Z · Boeing 7378H4 · Fuselage Main, Floor Beam
  > PASSENGER CABIN AFT WET AREA: CORROSION ON UPPER SURFACE OF FLOOR BEAM STA 947. LOCATED AT LBL 51.<[01] BLENDED CORROSION PER SRM 51-10-02. REMOVED.041' OF MATERIAL. REMAINING THICKNESS IS.139'. DAMAGE REMOVAL IS OUT OF LIMITS PER SRM 53-70-51-1A-1.;[02] 1.
- [SDR SWAA2024092432259](https://openairdocs.org/sdr/SWAA2024092432259.md): Floorbeam · corroded · Aug 30, 2024 · N8502Z · Boeing 7378H4 · Fuselage Main, Floor Beam
  > PASSENGER CABIN AFT WET AREA: CORROSION ON UPPER SURFACE OF FLOOR BEAM STA 947. LOCATED AT RBL 51.<[01] BLENDED CORROSION PER SRM 51-10-02. REMOVED.050' OF MATERIAL. REMAINING THICKNESS IS.130'. DAMAGE REMOVAL IS OUT OF LIMITS PER SRM 53-70-51-1A-1.;[02] 1.
- [SDR SWAA2024092432557](https://openairdocs.org/sdr/SWAA2024092432557.md): Shield · corroded · Aug 30, 2024 · N8502Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > R/H TRANSITION ANGLE IN FWD CARGO BIN HAS EVIDENCE OF CORROSION STA. 500 TO 500A (MARKED)<[01] REMOVED CORROSION PER SRM 51-10-02. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A.<BR>REMOVED DAMAGE TRANSITION ANGLE FROM STA 493 TO STA 500 FOR REPLACEMENT PER SRM
- [SDR SWAA2024092432560](https://openairdocs.org/sdr/SWAA2024092432560.md): Angle · corroded · Aug 30, 2024 · N8502Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > R/H TRANSITION ANGLE IN FWD CARGO BIN HAS EVIDENCE OF CORROSION STA. 500D TO 500E (MARKED)<[01] BLENDED AREAS; REMOVED.020' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. THIS SECTION TO BE REPLACED ON NR# TTG8Q00VKFTC];[02] BLENDED AREAS; REMOVED
- [SDR SWAA2024092432561](https://openairdocs.org/sdr/SWAA2024092432561.md): Angle · corroded · Aug 30, 2024 · N8502Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > R/H TRANSITION ANGLE IN FWD CARGO BIN HAS EVIDENCE OF CORROSION STA. 500E TO 500F (MARKED)<[01] BLENDED AREAS; REMOVED.025' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. THIS SECTION TO BE REPLACED ON NR# TTG8Q00VKFTC];[02] BLENDED AREAS; REMOVED
- [SDR SWAA2024092531998](https://openairdocs.org/sdr/SWAA2024092531998.md): Handle · loose · Aug 29, 2024 · N8502Z · Boeing 7378H4 · Galley Doors
  > FWD GALLEY DOOR INNER HANDLE IS LOOSE AT THE CAM PLATE<[01] TIGHTENED CAM PLATE ATTACHMENT NUT PER AMM 52-41-11; NO DEFECTS NOTED.;[02] C/W INSPECTION
- [SDR SWAA2024092532001](https://openairdocs.org/sdr/SWAA2024092532001.md): Handle · loose · Aug 29, 2024 · N8502Z · Boeing 7378H4 · Galley Doors
  > AFT GALLEY DOOR INNER HANDLE IS LOOSE AT THE CAM PLATE<[01] TIGHTENED AFT GALLEY DOOR INNER HANDLE CAM PLATE IAW AMM 52-41-11.;[02] 02 - INSPECTED PER [AMM 52-41-11-401-NG (GALLEY SERVICE DOOR HINGE ARM - REMOVAL/INSTALLATION - PERMANENT)]
- [SDR SWAA2024061099651](https://openairdocs.org/sdr/SWAA2024061099651.md): Girt Bar · stuck · Jun 7, 2024 · N8502Z · Boeing 7378H4 · Emergency Equipment
  > FWD SERVICE DOOR GIRT BAR STUCK / WON'T SECURE.<[01] REPOSITIONED GIRT BAR AS REQUIRED PER AMM 25-66-01. A/C OK FOR SERVICE.
- [SDR SWAA2024052187307](https://openairdocs.org/sdr/SWAA2024052187307.md): Flashlight · inoperative · May 18, 2024 · N8502Z · Boeing 7378H4 · Emergency Equipment
  > FWD GALLEY F/A FLASHLIGHT NOT TESTING<[01] 01 - REMOVED AND REPLACED PER [AMM 25-64-00-900-806-NG (FLASHLIGHT BATTERY REPLACEMENT - PERMANENT)]
- [SDR SWAA2024041774859](https://openairdocs.org/sdr/SWAA2024041774859.md): Battery Pack · inoperative · Apr 15, 2024 · N8502Z · Boeing 7378H4 · Emergency Lighting
  > AFT OVERWING EMERGENCY EXIT LIGHT INOP LOCATION: LH AND RH<[01] 01 - REMOVED AND REPLACED PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)]
- [SDR SWAA2023122033118](https://openairdocs.org/sdr/SWAA2023122033118.md): Lamp · inoperative · Dec 18, 2023 · N8502Z · Boeing 7378H4 · Emergency Lighting
  > R/H LOWER EMERGENCY LIGHT INOP<[01] REPLACED LAMP FOR EMERGENCY EXIT R/H LOWER AREA LIGHT PER AMM 33-51-03. OPS CHK GOOD
- [SDR SWAA2023091901544](https://openairdocs.org/sdr/SWAA2023091901544.md): Battery Pack · inoperative · Sep 17, 2023 · N8502Z · Boeing 7378H4 · Emergency Lighting
  > FWD CABIN ISLE EMERGENCY LIGHTS INOP<[01] R&R POSITION M2335 & M1676 EMERGENCY LIGHT BATTERY PACKS PER AMM 33-51-06 OPS CHECK OK
- [SDR SWAA2023071176568](https://openairdocs.org/sdr/SWAA2023071176568.md): Light · inoperative · Jul 9, 2023 · N8502Z · Boeing 7378H4 · Emergency Lighting
  > FWD EMERGENCY AISLE LIGHT(L1505) INOP. OK TO CONTINUE PER MEL 33-15-02 SP#1. MDDR# 143380. R & R EMERGENCY AISLE LED LIGHT PER AMM 33-51-03 AND DID NOT FIX PROBLEM. ORIGINAL LIGHT INSTALLED BACK. REMOVED AND REPLACED FWD POWER SUPPLY IAW AMM 33-51-06. OPS C
- [SDR SWAA2023061458196](https://openairdocs.org/sdr/SWAA2023061458196.md): Flashlight · inoperative · Jun 11, 2023 · N8502Z · Boeing 7378H4 · Emergency Equipment
  > AFT L/H OUTBOARD EMERGENCY FLASHLIGHT INOP<[01] REPLACED FLASHLIGHT ASSY PER CMM 25-60-13. OPS CHECK GOOD.
- [SDR SWAA2022100552033](https://openairdocs.org/sdr/SWAA2022100552033.md): Battery Pack · inoperative · Oct 3, 2022 · N8502Z · Boeing 7378H4 · Emergency Lighting
  > FWD ENTRY DOOR EXTERIOR AND INTERIOR EMERGENCY LIGHTS INOP. BATTERY PACK INOP. / [01] REPLACED EMERGENCY LIGHT BATTERY PACK FOR FORWARD ENTRY INTERIOR AND EXTERIOR EMERGENCY LIGHTS IAW AMM 33-51-06. OPS CHECK GOOD.
- [SDR SWAA2022100552032](https://openairdocs.org/sdr/SWAA2022100552032.md): Charger · inoperative · Oct 3, 2022 · N8502Z · Boeing 7378H4 · Emergency Lighting
  > FWD SERVICE DOOR INTERIOR AND EXTERIOR EMERGENCY LIGHTS INOP. EMERGENCY LIGHT BATTERY PACK INOP FOR THIS LOCATION. / [01] REPLACED EMERGENCY BATTERY CHARGER ASSEMBLY FOR FORWARD SERVICE DOOR EMERGENCY LIGHTS IAW AMM 33-51-06. NO FIX. REQUIRES BATTERY REPLACEME
- [SDR SWAA2022100552583](https://openairdocs.org/sdr/SWAA2022100552583.md): Battery Pack · inoperative · Oct 3, 2022 · N8502Z · Boeing 7378H4 · Emergency Lighting
  > FWD SERVICE DOOR INTERIOR AND EXTERIOR EMERGENCY LIGHTS INOP. EMERGENCY LIGHT BATTERY PACK INOP FOR THIS LOCATION. / [01] REPLACED EMERGENCY BATTERY CHARGER ASSEMBLY FOR FORWARD SERVICE DOOR EMERGENCY LIGHTS IAW AMM 33-51-06. NO FIX. REQUIRES BATTERY REPLACEME
- [SDR SWAA2022092078361](https://openairdocs.org/sdr/SWAA2022092078361.md): None · inoperative · Sep 17, 2022 · N8502Z · Boeing 737 · Emergency Lighting
  > ALL EMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK M1673 INOP / [01] REMOVED AND REPLACED M1673 EMERGENCY BATTERY PACK AND PERFORMED GOOD INSTALLATION TEST IAW AMM 33-51-06-960-805.;[02] VERIFIED CORRECTIVE ACTION #1.
- [SDR SWAA2022092078360](https://openairdocs.org/sdr/SWAA2022092078360.md): None · inoperative · Sep 16, 2022 · N8502Z · Boeing 737 · Emergency Lighting
  > ALL EMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK M1672 INOP. / [01] REMOVED AND REPLACED; AND PERFORMED TEST OF; BATTERY PACK M1672 IAW AMM 33-51-06-960-805.;[02] VERIFIED CORRECTIVE ACTION #1.
- [SDR SWAA2022091550733](https://openairdocs.org/sdr/SWAA2022091550733.md): None · cracked · Sep 6, 2022 · N8502Z · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > CRACKED BREAK PANEL STA 540; BL0 TO RBL25; WL 207. / [01] REMOVED DAMAGED BREAK PANEL STA 540; BL 0-RBL 25;WL 207 PER SRM 51-40-02-0G-0.;[02] LOCATED AND DRILLED AND DEBURRED NEW BREAK PANEL STA 540; BL0 TO RBL25; WL 207; PER SRM 51-40-02-0G-0; SRM 51-40-05-0G
- [SDR SWAA2022091550732](https://openairdocs.org/sdr/SWAA2022091550732.md): Floor Panel · cracked · Sep 6, 2022 · N8502Z · Boeing 7378H4 · Fuselage Floor Panel
  > CRACKED BREAK PANEL STA 540; BL0 TO LBL25; WL 207. / [01] REMOVED DAMAGED BREAK PANEL STA 540; BL0 TO LBL25; WL 207; PER SRM 51-40-02-0G-0.;[02] LOCATED AND DRILLED AND DEBURRED NEW BREAK PANEL STA 540; BL0 TO LBL25; WL 207; PER SRM 51-40-02-0G-0; SRM 51-40-05
- [SDR SWAA2022091549948](https://openairdocs.org/sdr/SWAA2022091549948.md): Attach Angle · cracked · Sep 3, 2022 · N8502Z · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > CRACKED ATTACH ANGLE AT MID PASSENGER CABIN BS663+28 RBL1 WL205. / [01] REMOVED CRACK DAMAGED BRACKET FROM BS663+28 RBL 1 WL 205 IAW SRM 51-40-02-0G-0 MEASURED CRACK LENGTH TO BE 0.9450 USING MICROMETER PER2242 S/N UNKNOWN CAL DUE 01/2023 NO SRM DAMAGE LIMITS
- [SDR SWAA2022091549160](https://openairdocs.org/sdr/SWAA2022091549160.md): Shield · corroded · Sep 1, 2022 · N8502Z · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > AFT CARGO BAY SHIELD ATTACH ANGLE HAS AREAS OF CORROSION AROUND MULTIPLE NUT PLATE HOLES BS767 TO BS787 RBL21 WL156 / [01] EVALUATED CORROSION ON ATTACH ANGLE BELOW SHIELD BS 767 TO 787 RBL 21 WL 156; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND R
- [SDR SWAA2022091549159](https://openairdocs.org/sdr/SWAA2022091549159.md): Shield · corroded · Sep 1, 2022 · N8502Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY SHIELD HAS MULTIPLE AREAS OF CORROSION BS767 TO BS794 RBL21 WL156 / [01] EVALUATED CORROSION ON SHIELD BS 767 TO 794 RBL 21 WL 156; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0;[02] VERIFIED
- [SDR SWAA2022091549158](https://openairdocs.org/sdr/SWAA2022091549158.md): Splice Strap · corroded · Sep 1, 2022 · N8502Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY CARGO FLOOR SPLICE STRAP HAS CORROSION BS767+6 RBL21 WL156 / [01] EVALUATED CORROSION ON SPLICE STRAP BS 767+6 RBL 21 WL 156; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0;[02] VERIFIED CORRE
- [SDR SWAA2022091549157](https://openairdocs.org/sdr/SWAA2022091549157.md): Plate · corroded · Sep 1, 2022 · N8502Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS OF CORROSION BS727H TO BS807+7 LBL21 WL156 / [01] EVALUATED CORROSION AT ALL LOCATIONS OF FLOOR TO SIDEWALL SUPPORT; FOUND DEEPEST LOCATION TO BE AT BS 747+10 LBL 21 WL 156; FOUND 0
- [SDR SWAA2022091549156](https://openairdocs.org/sdr/SWAA2022091549156.md): Plate · corroded · Sep 1, 2022 · N8502Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS CORROSION BS727F TO BS767 RBL21 WL156 / [01] EVALUATED CORROSION AT ALL LOCATIONS OF FLOOR TO SIDEWALL SUPPORT; FOUND DEEPEST LOCATION TO BE AT BS 727G+10 RBL 21 WL 156; FOUND 0.015 REM
- [SDR SWAA2022091549155](https://openairdocs.org/sdr/SWAA2022091549155.md): Support · corroded · Sep 1, 2022 · N8502Z · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION FWD CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS OF CORROSION BS500 TO BS500E+11 LBL24 WL156 / [01] EVALUATED CORROSION AT ALL LOCATIONS OF FLOOR TO SIDEWALL SUPPORT; FOUND DEEPEST LOCATION TO BE AT BS 500C+10 LBL 24 WL 156; FOUND

Next page: https://openairdocs.org/aircraft/N8502Z/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 = 'N8502Z' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8502Z/reports

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