# Service difficulty reports: N8509U

A list on [N8509U](https://openairdocs.org/aircraft/N8509U.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 3 · 102 reports

- [SDR SWAA2026091569081](https://openairdocs.org/sdr/SWAA2026091569081.md): Floor Panel · cracked · Sep 5, 2026 · N8509U · Boeing 7378H4 · Fuselage Floor Panel
  > FLOOR PANEL 221GF CRACKED RECEIVED NEW FLOOR PANEL P/N 141A5810-181 FLOOR PANEL WILL BE INSTALLED ON TASK CARD 730672 INTERIOR 2290 TTG8Q01DPYXR RECEIVED NEW FLOOR PANEL P/N 141A5810-181 LOT: 15115098 FLOOR PANEL WILL BE INSTALLED ON TASK CARD 730672 INTERIOR
- [SDR SWAA2026072344101](https://openairdocs.org/sdr/SWAA2026072344101.md): Valve · leaking · Jul 22, 2026 · N8509U · Boeing 7378H4 · Engine Cooling System
  > NR 1 ENGINE STEADY FUEL LEAK AFTER ENGINE START. REMOVED AND REPLACED HTPACC PER AMM 75-21-01.
- [SDR SWAA2026062916540](https://openairdocs.org/sdr/SWAA2026062916540.md): Slide · loose · Jun 26, 2026 · N8509U · Boeing 7378H4 · Escape Slide
  > FWD L1 ENTRY DOOR EMERGENCY EXIT SLIDE NOT SECURE. RESECURED L1 FWD ENTRY DOOR SLIDE IAW AMM 25-66-01.
- [SDR SWAA2026012965241](https://openairdocs.org/sdr/SWAA2026012965241.md): Girt Bar · out of adjust · Jan 28, 2026 · N8509U · Boeing 7378H4 · Emergency Equipment
  > FORWARD ENTRY DOOR GIRT BAR REQUIRES ADJUSTMENT. BAR COMES OUT OF ITS HOLDER. REMOVED & INSTALLED THE GIRT BAR IAW AMM 25-66-02. FOUND RETENTION TO BE SATISFACTORY.
- [SDR SWAA2025120442290](https://openairdocs.org/sdr/SWAA2025120442290.md): Boot · cracked · Dec 3, 2025 · N8509U · Boeing 7378H4 · Aerodynamic Fairings
  > NOSE RADOME BOOT CRACKED. REPLACED NOSE RADOME BOOT IAW AMM 53-52-00.
- [SDR SWAA2025111333402](https://openairdocs.org/sdr/SWAA2025111333402.md): Support · corroded · Nov 9, 2025 · N8509U · Boeing 7378H4 · Wing Main, Frame Structure
  > LEFT WING LEADING EDGE; NR 3 SLAT TAI DUCT, OTBD SUPPORT STRUCTURE IS CORRODED. WING STATION OFSS 418. REPLACED TAI SUPPORT ASSY PER SRM 51-10-02.;[02] C/W INSPECTION AS REQUIRED
- [SDR SWAA2025111330742](https://openairdocs.org/sdr/SWAA2025111330742.md): Battery Pack · inoperative · Nov 1, 2025 · N8509U · Boeing 7378H4 · Emergency Lighting
  > OVERWING FORWARD L/H AND R/H EMERGENCY ESCAPE HATCH LIGHTS INOPERATIVE. REMOVED AND REPLACED THE EMERGANCY LIGHT BATTERY PACK ON THE LT SIDE. OPS CHECKED GOOD IAW AMM 33-51-06.
- [SDR SWAA2025111328441](https://openairdocs.org/sdr/SWAA2025111328441.md): Nut Plate · debonded · Oct 25, 2025 · N8509U · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > AFT CARGO LEFT FLOOR TRANSITION ANGLE FROM BS 727I TO 787, DISBONDED NUTPLATES (QTY.10).<[01] INSTALLED BONDED NUTPLATES (QTY.10) ON AFT CARGO L/H FLOOR TRANSITION ANGLE FROM STA 727I TO STA 787 PER SRM 51-41-10.
- [SDR SWAA2025111328439](https://openairdocs.org/sdr/SWAA2025111328439.md): Angle · debonded · Oct 25, 2025 · N8509U · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO RT FLOOR TRANSITION ANGLE FROM STA 727J TO STA 767 DISBONDED NUTPLATES (QTY.6). INSTALLED BONDED NUTPLATES (QTY.6) ON AFT CARGO R/H FLOOR TRANSITION ANGLE FROM STA 727J TO STA 767 PER SRM 51-41-10.
- [SDR SWAA2025111328440](https://openairdocs.org/sdr/SWAA2025111328440.md): Support Angle · cracked · Oct 25, 2025 · N8509U · Boeing 7378H4 · Nacelle/Pylon Miscellaneous Structure
  > #1 ENGINE I/B FAN COWL OIL ACCESS DOOR 414AR INNER SUPPORT ANGLE CRACKED. REMOVED AND REPLACED INNER SUPPORT ANGLE PER SRM 51-40-02.
- [SDR SWAA2025111327538](https://openairdocs.org/sdr/SWAA2025111327538.md): Attach Angle · cracked · Oct 23, 2025 · N8509U · Boeing 7378H4 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK NR 1 ATTACH ANGLE CRACKED ON INBD SIDE OF SEAT TRACK IN RADIUS AT BS 727B UNDER FLOORBOARD 241EF. REMOVED DAMAGED SPLICE STRAP AT BS 727B; LBL 45.5 PER SRM 51-40-02. LOCATED AND DRILLED NEW PART IAW SRM 51-40-05 AND INSTALLED NEW PART IAW SRM 51-
- [SDR SWAA2025111327424](https://openairdocs.org/sdr/SWAA2025111327424.md): Attach Angle · cracked · Oct 23, 2025 · N8509U · Boeing 737824 · Fuselage Main, Attach Fittings
  > RIGHT VAPOR BARRIER ATTACH ANGLE BS 663 CRACKED AT FASTENER RBL 31. REMOVED DAMAGED SECTION OF RH STA 663 VAPOR BARRIER ATTACH ANGLE FROM RBL 31 TO RBL 65 PER SRM 57-10-10-2R-5;[02] RII. VERIFIED. REMOVED DAMAGED SECTION OF RH STA 663 VAPOR BARRIER ATTACH ANG
- [SDR SWAA2025111327044](https://openairdocs.org/sdr/SWAA2025111327044.md): Attach Bracket · cracked · Oct 22, 2025 · N8509U · Boeing 7378H4 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK NR 4 ATTACH BRACKET CRACKED AT BS 727B UNDER FLOORBOARD 242DF. REMOVED DAMAGED SPLICE STRAP AT BS 727B; RBL 45.5 IAW SRM 51-40-02. LOCATED AND DRILLED NEW PART IAW SRM 51-40-05.
- [SDR SWAA2025082909598](https://openairdocs.org/sdr/SWAA2025082909598.md): Flashlight · inoperative · Aug 28, 2025 · N8509U · Boeing 7378H4 · Emergency Equipment
  > FLASHLIGHT FWD FLIGHT ATTENDANT JUMP SEAT INOP. CHECKED BOTH FWD FLIGHT ATTENDANT SEAT FLASHLIGHTS; BOTH OPS CHECK GOOD. REINSTALLED IAW SIP.
- [SDR SWAA2025070787977](https://openairdocs.org/sdr/SWAA2025070787977.md): Flashlight · not seated · Jul 3, 2025 · N8509U · Boeing 7378H4 · Emergency Equipment
  > 2 AFT STATION EMERGENCY FLASHLIGHTS INOP. RESTEATED FLASHLIGHTS OPS CHECK GOOD ER AMM 25-64-00 MEL CLEARED.
- [SDR SWAA2025070387523](https://openairdocs.org/sdr/SWAA2025070387523.md): Charger · overheated · Jul 2, 2025 · N8509U · Boeing 7378H4 · Emergency Lighting
  > FWD GALLEY EMERGENCY LIGHT BATTERY PACK CHARGER (M02816) OVERHEATING/SMOKING<[01] REMOVED AND REPLACED M02816 POWER SUPPLY CHARGER AND BATTERY PACK. DEEP CYCLE CHARGE AND EMERGENCY LIGHT OPS CHECK GOOD. REF: AMM 33-51-06
- [SDR SWAA2025022097337](https://openairdocs.org/sdr/SWAA2025022097337.md): Bracket · contaminated · Feb 18, 2025 · N8509U · Boeing 7378H4 · Landing Gear Brake System
  > AFTER LANDING ATC REPORTED POSSIBLE SMOKE FROM LEFT MAIN LANDING GEAR. ARFF CAME TO THE A/C AND AFTER 10 MINUTES CLEARED US TO PARK AT THE GATE.MECHANIC ON SITE SUSPECTS DE-ICING FLUID IN THE BRAKES CAUSED THE SMOKE<[01] INSPECTED #1 BRAKE PER AMM 32-41-41. SU
- [SDR SWAA2025012087711](https://openairdocs.org/sdr/SWAA2025012087711.md): Lamp · inoperative · Jan 19, 2025 · N8509U · Boeing 7378H4 · Emergency Lighting
  > LIGHTBULB IN AFT SEATBELT SIGN NOT WORKING.<[01] RELAMPED IAW AMM 33-51-14.
- [SDR SWAA2024112560399](https://openairdocs.org/sdr/SWAA2024112560399.md): Battery Pack · inoperative · Nov 16, 2024 · N8509U · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY LIGHTS CONTROLLED BY BATTERY PACK M2816 ARE INOP.<[01] 01 - REMOVED AND REPLACED PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)];[02] 01 - REMOVED AND REPLACED BATTERY PACK; OP CK GOOD PER [AMM 33-51-06-960-805-NG
- [SDR SWAA2024112560396](https://openairdocs.org/sdr/SWAA2024112560396.md): Battery Pack · inoperative · Nov 16, 2024 · N8509U · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY LIGHTS CONTROLLED BY BATTERY PACK M2335 ARE INOP.<[01] 01 - REMOVED AND REPLACED BATTERY PACK; OP CK GOOD PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)];[02] INSPECTION COMPLETE ON CORRECTIVE ACTION #1 FOR REPLACE
- [SDR SWAA2024112560397](https://openairdocs.org/sdr/SWAA2024112560397.md): Battery Pack · inoperative · Nov 16, 2024 · N8509U · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY LIGHTS CONTROLLED BY BATTERY PACK M1695 ARE INOP.<[01] 01 - REMOVED AND REPLACED BATTERY PACK; OP CK GOOD PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)];[02] INSPECTION COMPLETE ON CORRECTIVE ACTION #1 FOR REPLACE
- [SDR SWAA2024112560400](https://openairdocs.org/sdr/SWAA2024112560400.md): Battery Pack · inoperative · Nov 16, 2024 · N8509U · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY LIGHTS CONTROLLED BY BATTERY PACK M1670 ARE INOP.<[01] 01 - REMOVED AND REPLACED BATTERY PACK; OP CK GOOD PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)];[02] INSPECTION COMPLETE ON CORRECTIVE ACTION #1 FOR REPLACE
- [SDR SWAA2024112560398](https://openairdocs.org/sdr/SWAA2024112560398.md): Battery Pack · inoperative · Nov 16, 2024 · N8509U · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY LIGHTS CONTROLLED BY BATTERY PACK M1671 ARE INOP.<[01] 01 - REMOVED AND REPLACED BATTERY PACK; OP CK GOOD PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)];[02] INSPECTION COMPLETE ON CORRECTIVE ACTION #1 FOR REPLACE
- [SDR SWAA2024112560402](https://openairdocs.org/sdr/SWAA2024112560402.md): Battery Pack · inoperative · Nov 16, 2024 · N8509U · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY LIGHTS CONTROLLED BY BATTERY PACK M1672 ARE INOP.<[01] REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK M1672 IAW AMM 33-51-06. OPS CHECK GOOD.;[02] INSPECTION C/W
- [SDR SWAA2024112556598](https://openairdocs.org/sdr/SWAA2024112556598.md): Floor Panel · corroded · Nov 4, 2024 · N8509U · Boeing 7378H4 · Fuselage Floor Panel
  > FLOOR PANEL HOLE AT STA 947 LBL 4.5 & LBK 12 ON THE AFT FLANGE OF THE T REQUIRE RELOCATION DUE TO BEING IN THE RADIUS<[01] REPAIRED PANEL FASTENER HOLE AND INSTALLED INSERTS PER SRM 53-00?50-2R-1.;[02] REPAIRED PANEL FASTENER HOLE PER EA 24-153-03056-WIP2.;[03
- [SDR SWAA2024112155827](https://openairdocs.org/sdr/SWAA2024112155827.md): Angle · elongated · Nov 1, 2024 · N8509U · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > IN THE AFT CARGO BAY RIGHT HAND SIDE AFT OF THE DOOR; THE SHIELD ASSEMBLY FWD INBD SUPPORT/MOUNT ANGLE HAS AN ELONGATED HOLE WITH AN INDICATION OF A CRACK.<[01] REMOVED AFT CARGO BAY RIGHT HAND SIDE AFT OF THE DOOR; THE SHIELD ASSEMBLY SUPPORT ANGLE( P/N 146A8
- [SDR SWAA2024112553572](https://openairdocs.org/sdr/SWAA2024112553572.md): Intercostal · cracked · Oct 25, 2024 · N8509U · Boeing 7378H4 · Fuselage Main, Structure
  > PASSENGER CABIN; FLOOR PANEL INTERCOSTAL (BREAK ASSY.) CRACKED AT STA.540 BL-0 TO LBL24<[01] REMOVED AND REPLACED L/H INTERCOSTAL PER SRM 51-40-02;[02] INSPECTION COMPLETE ON CORRECTIVE ACTION #1 FOR INTERCOSTAL REPLACEMENT.
- [SDR SWAA2024112153571](https://openairdocs.org/sdr/SWAA2024112153571.md): Intercostal · cracked · Oct 25, 2024 · N8509U · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > PASSENGER CABIN; FLOOR PANEL INTERCOSTAL (BREAK ASSY.)CRACKED AT STA.540 BL-0 TO RBL24<[01] REMOVED AND REPLACED R/H INTERCOSTAL PER SRM 51-40-02;[02] INSPECTION COMPLETE ON CORRECTIVE ACTION #1 FOR INTERCOSTAL REPLACEMENT.
- [SDR SWAA2024112551779](https://openairdocs.org/sdr/SWAA2024112551779.md): Intercostal · corroded · Oct 22, 2024 · N8509U · Boeing 7378H4 · Fuselage Main, Structure
  > CORROSION ON FLOOR INTERCOSTAL AT B/S 947 LBL51<[01] FOUND INTERCOSTAL TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1. INTERCOSTAL TO BE REMOVED AND REPLACED ON [TTG8Q00WJ9TR].;[02] FOUND INTERCOSTAL TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1. INTERCOSTAL TO BE REMO
- [SDR SWAA2024112550978](https://openairdocs.org/sdr/SWAA2024112550978.md): Angle · corroded · Oct 20, 2024 · N8509U · Boeing 7378H4 · Fuselage Main, Structure
  > FORWARD PASSENGER COMPARTMENT FLOOR STRUCTURE WET AREA UNDER FWD ENTRY DOOR THRESHOLD HAS MULTIPLE LARGE AREAS OF CORROSION ON CREASE BEAM. (MARKED)<[01] REMOVED CORROSION IAW SRM 51-10-02. CORROSION REMOVAL OUT OF ALLOWABLE LIMITS PER SRM 53-10-15-IA-1.;[02]
- [SDR SWAA2024112550976](https://openairdocs.org/sdr/SWAA2024112550976.md): Angle · elongated · Oct 20, 2024 · N8509U · Boeing 7378H4 · Cargo Compartments
  > IN THE AFT CARGO BAY RIGHT HAND SIDED AFT OF THE DOOR; THE SHIELD ASSEMBLY FWD INBD SUPPORT/MOUNT ANGLE HAS AN ELONGATED HOLE. STATION 847+6 RBL15.<[01] LOCATED AND DRILLED SERVICEABLE ANGLE ASSEMBLY ( SHIELD ASSY. SUPPORT) FOR THE AFT CARGO BAY DOOR SHIP AT
- [SDR SWAA2024112550872](https://openairdocs.org/sdr/SWAA2024112550872.md): Intercostal · corroded · Oct 19, 2024 · N8509U · Boeing 7378H4 · Fuselage Main, Plate/Skin
  > PASSENGER AREA STA 947; LBL 24 UNDER AFT LAV MOUNT HAS EVIDENT OF CORROSION.<[01] FOUND INTERCOSTAL TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1. INTERCOSTAL TO BE REMOVED AND REPLACED ON [TTG8Q00WJ9TR].
- [SDR SWAA2024112550868](https://openairdocs.org/sdr/SWAA2024112550868.md): Angle · corroded · Oct 19, 2024 · N8509U · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > SURFACE CORROSION FOUND ON CREASE BEAM ANGLE IN FWD PASSENGER CABIN FLOOR STRUCTURE WET AREA ON LEFT SIDE NEAR L1 ENTRY THRESHOLD; AT STA 294.5 +8'. (MARKED)<[01] REMOVED AND REPLACED CREASE BEAM ANGLE IN FWD PASSENGER CABIN FLOOR STRUCTURE WET AREA ON LEFT SI
- [SDR SWAA2024112550873](https://openairdocs.org/sdr/SWAA2024112550873.md): Intercostal · corroded · Oct 19, 2024 · N8509U · Boeing 7378H4 · Fuselage Main, Structure
  > 'PASSENGER AREA STA947 LBL 24 INTERCOSTAL TOP SURFACE HAS CORROSION.<[01] FOUND INTERCOSTAL TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1. INTERCOSTAL TO BE REMOVED AND REPLACED ON [TTG8Q00WJ9TR].
- [SDR SWAA2024112550875](https://openairdocs.org/sdr/SWAA2024112550875.md): Angle · corroded · Oct 19, 2024 · N8509U · Boeing 7378H4 · Fuselage Main, Structure
  > PASSSENGER AREA STA 984; LBL47 CREASE BEAM HAS CORROSION ON VERTICAL SURFACE.<[01] CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-70-15-1A-1. <BR><BR>Z ANGLE REMOVED PER SRM 51-40-02; FOR REPLACEMENT.;[02] VERIFIED OUT OF LIMITS CORROSION ON Z ANGLE PER SRM
- [SDR SWAA2024112550871](https://openairdocs.org/sdr/SWAA2024112550871.md): Floorbeam · corroded · Oct 19, 2024 · N8509U · Boeing 7378H4 · Fuselage Main, Floor Beam
  > .PASSENGER AREA STA 947;LBL16 FLOOR BEAM TOP CAP HAS CORROSION..<[01] CORROSION FOUND OUT OF LIMITS PER SRM 53-70-15-1A-1. REMOVED DAMAGED SECTION OF FLOOR BEAM TOP CAP PER SRM 53-70-51-2R-5;[02] FLAP PEENED THE CUT EDGES PER SRM 53-70-51-2R-5 LOCATED; DRILLED
- [SDR SWAA2024112150874](https://openairdocs.org/sdr/SWAA2024112150874.md): Intercostal · corroded · Oct 19, 2024 · N8509U · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > PASSENGER AREA STA 949; LBL50 FLOOR SUPPORT UNDER LAV MOUNT HAS CORROSION.<[01] FOUND INTERCOSTAL TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1. INTERCOSTAL TO BE REMOVED AND REPLACED ON [TTG8Q00WJ9TR].
- [SDR SWAA2024112550158](https://openairdocs.org/sdr/SWAA2024112550158.md): Angle · corroded · Oct 18, 2024 · N8509U · Boeing 7378H4 · Cargo Compartments
  > FWD CARGO R/H TRANSITION ANGLE HAS CORROSION BS 492-500A<[01] REMOVED FWD CARGO R/H TRANSITION ANGLE (AFT DOOR CUTOUT SHIELD) BS 492-500A PER SRM 51-40-02.;[02] LOCATED AND DRILLED NEW R/H TRANSITION ANGLE (AFT DOOR CUTOUT SHIELD) BS 492-500A PER SRM 51-40-0 5
- [SDR SWAA2024112550161](https://openairdocs.org/sdr/SWAA2024112550161.md): Angle · corroded · Oct 18, 2024 · N8509U · Boeing 7378H4 · Cargo Compartments
  > AFT CARGO L/H TRANSITION ANGLE HAS CORROSION AT N/P HOLES STA.727H +2;+6;+9++13+16+20. MRKD<[01] REMOVED L/H TRANSITION ANGLE PER SRM 51-40-02;[02] UPDATED MEASUREMENT PART NUMBER;[03] OK TO INSTALL L/H TRANSITION ANGLE;[04] R/R L/H TRANSITION ANGLE FROM STA 7
- [SDR SWAA2024112550178](https://openairdocs.org/sdr/SWAA2024112550178.md): Angle · corroded · Oct 18, 2024 · N8509U · Boeing 7378H4 · Cargo Compartments
  > AFT CARGO R/H TRANSITION ANGLE HAS CORROSION AT N/P HOLES UNDERSIDE STA.849-850. MRKD<[01] BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IN REFERENCE TO SRM 53-00-53;[02] REMOVED AFT CARGO RH TRANSITION ANGLE AT STA. 847 TO STA. 867 IN REFERENCE TO SRM 51-40
- [SDR SWAA2024112150177](https://openairdocs.org/sdr/SWAA2024112150177.md): Angle · corroded · Oct 18, 2024 · N8509U · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO R/H TRANSITION ANGLE HAS CORROSION AT N/P HOLES ON UNDERSIDE STA.767-794. MRKD<[01] BLENDED CORROSION AND FOUND TO BE OUT OF LIMIT IN REFERENCE TO SRM 53-00-53.;[02] REMOVED AFT CARGO R/H TRANSITION ANGLE STA.767-794 PER SRM 51-40-02.;[03] DRILLED NE
- [SDR SWAA2024112150157](https://openairdocs.org/sdr/SWAA2024112150157.md): Angle · corroded · Oct 18, 2024 · N8509U · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO L/H TRANSITION ANGLE HAS CORROSION AT N/P HOLE STA.727F+16. MRKD<[01] UPDATED CORRODED ELEMENT PART NUMBER;[02] COMPLETED ON TTG8Q00WHFNR;[03] COMPLETE TRANSITION ANGLE WAS CHANGED ALL WORK ACCOMPLISHED WAS COMPLETED ON CARD TTG8Q00WHFNR;[04] COMPLET
- [SDR SWAA2024112150170](https://openairdocs.org/sdr/SWAA2024112150170.md): Angle · corroded · Oct 18, 2024 · N8509U · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO L/H TRANSITION ANGLE HAS CORROSION AT NUMERUS NUT PLATE HOLES BS 500A - 500H (SEE ATTACHED PICS)<[01] BLENDED THE CORROSION AND FOUND TO BE OUT OF LIMIT PER SRM 53-00-53-1A-2.;[02] REMOVED FWD CARGO L/H TRANSITION ANGLE BETWEEN STA 500-500I PER SRM 5
- [SDR SWAA2024112150160](https://openairdocs.org/sdr/SWAA2024112150160.md): Floor Panel · corroded · Oct 18, 2024 · N8509U · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO; AFT BULKHEAD TO FLOOR CORD HAS CORROSION BS 500I LBL 16<[01] BLENDED THE CORROSION AND FOUND TO BE OUT OF LIMIT PER SRM 53-30-08-1A-1.;[02] REMOVED FWD CARGO; AFT BULKHEAD TO FLOOR CORD PER SRM 51-40-02.;[03] DRILLED NEW FWD CARGO; AFT BULKHEAD TO F
- [SDR SWAA2024112150171](https://openairdocs.org/sdr/SWAA2024112150171.md): Angle · corroded · Oct 18, 2024 · N8509U · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO L/H TRANSITION ANGLE HAS CORROSION AT N/P HOLES STA.727I +3+8+10.5+14.5+18.5. MRKD<[01] UPDATED CORRODED ELEMENT PART NUMBER;[02] COMPLETED ON TTG8Q00WHFNR;[03] COMPLETE TRANSITION ANGLE WAS CHANGED ALL WORK ACCOMPLISHED WAS COMPLETED ON CARD TTG8Q00
- [SDR SWAA2024112150172](https://openairdocs.org/sdr/SWAA2024112150172.md): Angle · corroded · Oct 18, 2024 · N8509U · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO L/H TRANSITION ANGLE HAS CORROSION AT N/P HOLES STA.727J +6+10=14.5. MRKD<[01] UPDATED CORRODED ELEMENT PART NUMBER;[02] COMPLETED ON TTG8Q00WHFNR;[03] COMPLETE TRANSITION ANGLE WAS CHANGED ALL WORK ACCOMPLISHED WAS COMPLETED ON CARD TTG8Q00WHFNR
- [SDR SWAA2024112150162](https://openairdocs.org/sdr/SWAA2024112150162.md): Angle · corroded · Oct 18, 2024 · N8509U · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO L/H TRANSITION ANGLE HAS CORROSION AT N/P HOLES STA.747-767. MRKD<[01] UPDATED CORRODED ELEMENT PART NUMBER;[02] COMPLETED ON TTG8Q00WHFNR;[03] COMPLETE TRANSITION ANGLE WAS CHANGED ALL WORK ACCOMPLISHED WAS COMPLETED ON CARD TTG8Q00WHFNR
- [SDR SWAA2024112150173](https://openairdocs.org/sdr/SWAA2024112150173.md): Angle · corroded · Oct 18, 2024 · N8509U · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO L/H TRANSITION ANGLE HAS CORROSION AT N/P HOLES STA.767-787. MRKD<[01] UPDATED CORRODED ELEMENT PART NUMBER;[02] COMPLETED ON TTG8Q00WHFNR;[03] COMPLETE TRANSITION ANGLE WAS CHANGED ALL WORK ACCOMPLISHED WAS COMPLETED ON CARD TTG8Q00WHFNR;[04] COMPLE
- [SDR SWAA2024112150174](https://openairdocs.org/sdr/SWAA2024112150174.md): Angle · corroded · Oct 18, 2024 · N8509U · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO L/H TRANSITION ANGLE HAS CORROSION AT N/P HOLES STA.787-807. MRKD<[01] UPDATED CORRODED ELEMENT PART NUMBER;[02] COMPLETED ON CARD TTG8Q00WHFNR;[03] COMPLETE TRANSITION ANGLE WAS CHANGED ALL WORK ACCOMPLISHED WAS COMPLETED ON CARD TTG8Q00WHFNR;[04] C
- [SDR SWAA2024112150163](https://openairdocs.org/sdr/SWAA2024112150163.md): Angle · corroded · Oct 18, 2024 · N8509U · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO R/H TRANSITION ANGLE HAS CORROSION AT N/P HOLE STA.727E+20.MRKD<[01] REMOVED R/H TRANSITION ANGLE STA 727-767. IAW SRM 51-40-02.;[02] LOCATED AND DRILLED NEW TRANSITION ANGLE STA 727-767 IAW SRM 51-40-02.;[03] VERIFIED WORK PERFORMED ON CORRECTIVE AC

Next page: https://openairdocs.org/aircraft/N8509U/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 = 'N8509U' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8509U/reports

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