# Service difficulty reports: N8699A

A list on [N8699A](https://openairdocs.org/aircraft/N8699A.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 · 93 reports

- [SDR SWAA2026101218971](https://openairdocs.org/sdr/SWAA2026101218971.md): Filter · odor · Oct 11, 2026 · N8699A · Boeing 7378H4 · Air Distribution System
  > SEVERAL PAX SMELLED A SCORCHED ODOR AROUND ROW 27 ON THE RT SIDE OF THE ACFT. RAN PACKS WITH ENG BLEEDS RAN PACKS WITH APU BLEED NO SCORCHED ODOR NOTED. SLIGHT HYD FLUID ODOR NOTED. FOUND A HYD SYSTEM OVER SERVICED. SERVICED A HYD SYSTEM REF AMM 12-12-00. RE
- [SDR SWAA2026101238616](https://openairdocs.org/sdr/SWAA2026101238616.md): Hydraulic System · overserviced · Oct 11, 2026 · N8699A · Boeing 7378H4 · Hydraulic System, Main
  > SEVERAL PAX SMELLED A SCORCHED ODOR AROUND ROW 27 ON THE RIGHT SIDE OF THE AIRCRAFT. RAN PACKS WITH ENG BLEEDS RAN PACKS WITH APU BLEED NO ODOR NOTED. SLIGHT HYD FLUID ODOR NOTED. FOUND A HYD SYSTEM OVERSERVICED. SERVICED A HYD SYS IAW AMM 12-12-00. REPLACED B
- [SDR SWAA2026031679121](https://openairdocs.org/sdr/SWAA2026031679121.md): Access Panel · delaminated · Mar 12, 2026 · N8699A · Boeing 7378H4 · Aerodynamic Fairings
  > WING-TO-BODY FAIRING PANEL 192BL LEADING EDGE DELAMINATION. APPLIED REPAIR PLIES PER SRM 51-70-05. REQIURES PAINT FINISH. PANEL 192BL REMOVED IAW SRM 51-40-02. APPLIED PERMANENT REPAIR PER SRM 53-40-70-2R-1 AND SRM 51-70-05.
- [SDR SWAA2026022473176](https://openairdocs.org/sdr/SWAA2026022473176.md): Panel · delaminated · Feb 22, 2026 · N8699A · Boeing 7378H4 · Aerodynamic Fairings
  > PANEL 192 BL IS DELAMINATED ON FWD LEADING EDGE SKIN. COMPLIED WITH EA 26-153-00501.
- [SDR SWAA2025101421498](https://openairdocs.org/sdr/SWAA2025101421498.md): Filler · missing · Oct 5, 2025 · N8699A · Boeing 7378H4 · Fuselage Main, Structure
  > EGPR DOOR CUT OUT REPAIR FILLER IS MISSING. REPLACED MISSING FILLER ON EXISTING EGPR DOOR CUT OUT REPAIR IAW B737-800 SRM 53-10-15-2R-4.
- [SDR SWAA2025082204445](https://openairdocs.org/sdr/SWAA2025082204445.md): Battery Pack · inoperative · Aug 14, 2025 · N8699A · Boeing 7378H4 · Emergency Lighting
  > L/H OVERWING EMERGENCY LIGHT BATTERY PACK INOP AT. STA 565L<[01] REMOVED AND REPLACED BATTERY PACK PER MM 33-51-06;[02] L/H OVERWING EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06
- [SDR SWAA2025082298619](https://openairdocs.org/sdr/SWAA2025082298619.md): Angle · cracked · Aug 6, 2025 · N8699A · Boeing 7378H4 · Wing Miscellaneous Structure
  > LH WING ANGLE CRACKED INBOARD OF MIDSPAN DEFLECTION CONTROL RIB<[01] REMOVED L/H WING ANGLE INBOARD OF MID SPAN DEFLECTION CONTROL RIB FOR REPLACEMENT.;[02] LOCATED AND DRILLED FASTENER HOLES IN NEW ANGLE PER SRM 51-40-05.;[03] INSPECTED WORK PERFORMED IN CORR
- [SDR SWAA2025082298259](https://openairdocs.org/sdr/SWAA2025082298259.md): Lens · cracked · Aug 4, 2025 · N8699A · Boeing 7378H4 · Emergency Lighting
  > BULL NOSE TRIM ABOVE 28-29 ABC OVERHEAD BIN EMERGENCY LIGHT LENS COVER CRACKED.<[01] R/R LENS PER AMM 33-51-03;[02] 02 - INSPECTED PER [AMM 33-51-03-960-803-NG (EMERGENCY AISLE LIGHT (EAL) - LENS REPLACEMENT - PERMANENT)]
- [SDR SWAA2025082698537](https://openairdocs.org/sdr/SWAA2025082698537.md): Skin · damaged · Aug 3, 2025 · N8699A · Boeing 7378H4 · Wing, Plate/Skin
  > FASTENER HOLE COMMON TO THE FUEL TANK AT STA.663 LBL 60 SHOWS INDICATION OF A DEFECT USING HFEC. (M). HFEC HOLE PROBE INSPECTION OF FASTENER HOLE COMMON TO THE REPAIR AREA PER BOEING NDT MANUAL PART 6;51-00-00 PROCEDURE 16 INDICATES DEFECT. FASTENER HOLE R
- [SDR SWAA2025082296425](https://openairdocs.org/sdr/SWAA2025082296425.md): Panel · cracked · Jul 30, 2025 · N8699A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > PANEL 193AR HAS CRACK ON UPPER FWD EDGE.<[01] REMOVED PANEL 193AR TO F.O.M. PER AMM 53-51-21;[02] DISREGARD CORRECTIVE ACTION STATEMENT #1. SEE FAULT ID TTG8Q014A0P9 FOR REMOVAL AND REINSTALLATION OF PANEL 193AR.;[03] REMOVED DAMAGE PER SRM 51-70-05.;[04] VERI
- [SDR SWAA2025082195573](https://openairdocs.org/sdr/SWAA2025082195573.md): Floor Panel · delaminated · Jul 26, 2025 · N8699A · Boeing 7378H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 241DF DELAMINATED WITH NUMEROUS DENTS. INSTALLED A NEW FLOOR PANEL 241DF IAW AMM 53-21-00.
- [SDR SWAA2025082294441](https://openairdocs.org/sdr/SWAA2025082294441.md): Attach Angle · cracked · Jul 23, 2025 · N8699A · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > BS 663 VAPOR BARRIER ATTACH ANGLE CRACKED ON OUTBD SIDE OF FLEX JOINT @ LBL 34' HFEC VERIFIED.<[01] DAMAGE AT LBL 34 IS VERIFIED USING HFEC PER NDT PART 6; 51-00-00 PROCEDURE 23.;[02] REPLACED ATTACH ANGLE PER SRM 51-40-02 & DRW 111A1000;[03] VERIFIED C/A 2 CO
- [SDR SWAA2025082294129](https://openairdocs.org/sdr/SWAA2025082294129.md): Fitting · cracked · Jul 23, 2025 · N8699A · Boeing 7378H4 · Wing Main, Frame Structure
  > R/H WING INBD TRAILING EDGE; UPPER SHELF PANEL INTERCOSTAL INBD OF DEFLECTION FITTING IS CRACKED<[01] REMOVED INTERCOSTAL WEB INBD OF R/H WING DEFLECTION CONTROL RIB PER SRM 51-40-02.;[02] INSPECTION C/W.;[03] LOCATED; DRILLED AND DEBURRED REPLACEMENT INTERCOS
- [SDR SWAA2025082194119](https://openairdocs.org/sdr/SWAA2025082194119.md): Floor Panel · delaminated · Jul 23, 2025 · N8699A · Boeing 7378H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 242CF DELAMINATED WITH NUMEROUS DENTS. INSTALLED FLOOR PANEL 242CF PER AMM 53-21-00.
- [SDR SWAA2025082693633](https://openairdocs.org/sdr/SWAA2025082693633.md): Plate · cracked · Jul 22, 2025 · N8699A · Boeing 7378H4 · Wing Miscellaneous Structure
  > LEFT WING REAR SPAR, WAFFLE PLATE INBD OF NR 3 FLAP TRACK WAS CRACKED AT FASTNERS. REMOVED AND REPLACED LT WING REAR SPAR WAFFLE PLATE IAW SRM 51-40-02.
- [SDR SWAA2025082293965](https://openairdocs.org/sdr/SWAA2025082293965.md): Attach Angle · cracked · Jul 22, 2025 · N8699A · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > BS 663 VAPOR BARRIER ATTACH ANGLE CRACKED ON INBOARD SIDE OF FLEX JOINT @ RBL 9 AND SUSPECTED CRACK AT RBL 34<[01] ACCOMPLISHED HFEC SURFACE INSPECTION OF RBL 34' VERIFIED AREA IS CRACKED. PER NDT PART 6 51-00-00 PROC. 23;[02] REMOVED RIVETS @ R/H 663 ATTACH A
- [SDR SWAA2025082293628](https://openairdocs.org/sdr/SWAA2025082293628.md): Attach Angle · cracked · Jul 21, 2025 · N8699A · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > BS 663 VAPOR BARRIER ATTACH ANGLE CRACKED ON INBOARD SIDE OF FLEX JOINT @ LBL 9.<[01] REMOVED RIVETS AT L/H STA 663 ATTACH ANGLE COMMON TO VAPOR BARRIER FROM LBL 5 TO LBL 30 PER SRM 51-40-02.;[02] REMOVED CRACKED L ANGLE L/H A/C BAY AFT WALL STA 663 PER SRM 51
- [SDR SWAA2025082292708](https://openairdocs.org/sdr/SWAA2025082292708.md): Skin · delaminated · Jul 18, 2025 · N8699A · Boeing 7378H4 · Trailing Edge Flaps
  > RIGHT OUTBOARD TRAILING EDGE FLAP HAS DELAM ON INBD TRAILING CORNER AND SHARP BEVEL ON TRAILING EDGE AT FLAP CENTER.<[01] REMOVED R/H O/B AFT FLAP PER MM 27-51-22.;[02] OK TO INSTALL R/H OUTBOARD TRAILING EDGE FLAP (RII);[03] REPLACED R/H O/B AFT FLAP PER MM 2
- [SDR SWAA2025060276713](https://openairdocs.org/sdr/SWAA2025060276713.md): Flashlight · broken · May 30, 2025 · N8699A · Boeing 7378H4 · Emergency Equipment
  > FWD F/A FLASHLIGHT WILL NOT TEST AND SEAL IS BROKEN. <[01] REMOVED & REPLACED FWD FA FLASHLIGHT ASSY IAW AMM 25-64-00; OPS CHECK GOOD.
- [SDR SWAA2025032406289](https://openairdocs.org/sdr/SWAA2025032406289.md): Panel · cracked · Mar 18, 2025 · N8699A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT PANEL 141FW HAS CRACKS AT LOWER EDGE <[01]. REMOVED AND FABRICATED PANEL PER AMM 25-52-01. PANEL WILL REQUIRE INSTALLATION.; [02] INSTALLED PANEL PER 25-52-06.; [03] INSTALLED PANEL PER 25-52-06.
- [SDR SWAA2025021896389](https://openairdocs.org/sdr/SWAA2025021896389.md): Battery Pack · no test · Feb 15, 2025 · N8699A · Boeing 7378H4 · Emergency Equipment
  > AFT FLASHLIGHT UNDER FLIGHT ATTENDANT'S JUMPSEAT DOES NOT TEST MOST TIMES; WHEN DOES LIGHT IS RED.<[01] R/R'D AFT R/H O/B EMERG FLASHLIGHT BATTERY PACK & RESEALED AS PER AMM 25-64-00; OPS CK GOOD
- [SDR SWAA2024121979440](https://openairdocs.org/sdr/SWAA2024121979440.md): Slide · out of adjust · Dec 19, 2024 · N8699A · Boeing 7378H4 · Escape Slide
  > REF PREV LOG PAGE 2380351 'FORWARD ENTRY SLIDE FELL OUT OF CONTAINER'<[01] REMOVED FORWARD ENTRY DOOR SLIDE; FOUND SLIDE LATCH ASSY BROKEN. REF AMM 25-66-01 (MT 725-61-06) REF PREVIOUS LOG PAGE 2380351 FOR FINAL CORRECTIVE ACTION.
- [SDR SWAA2024121979439](https://openairdocs.org/sdr/SWAA2024121979439.md): Slide · out of adjust · Dec 18, 2024 · N8699A · Boeing 7378H4 · Escape Slide
  > FWD ENTRY DOOR SLIDE FELL OUT OF CONTAINER<[01] COMPLIED WITH W/O 89269033<BR>01 - REMOVED AND REPLACED PER [AMM 25-66-01-401-NG (DOOR-MOUNTED ESCAPE SYSTEM - REMOVAL/INSTALLATION - PERMANENT)]
- [SDR SWAA2024082026422](https://openairdocs.org/sdr/SWAA2024082026422.md): Bulb · inoperative · Aug 16, 2024 · N8699A · Boeing 7378H4 · Emergency Lighting
  > F.S.D. EMERGENCY EXIT FWD LIGHT HAS SEVERAL INOP BULBS<[01] RELAMPED THE F.S.D. EMERGENCY EXIT FWD LIGHT AND PERFORMED SATISFACTORY OPERATIONAL TEST PER AMM 33-51-01-960-801.;[02] VERIFIED CORRECTIVE ACTION #1
- [SDR SWAA2024081525679](https://openairdocs.org/sdr/SWAA2024081525679.md): Battery Pack · inoperative · Aug 14, 2024 · N8699A · Boeing 7378H4 · Emergency Lighting
  > INOP EMERGENCY LIGHTS ASSOCIATED WITH BATTERY PACK M1676.<[01] REMOVED; REPLACED; AND PERFORMED A GOOD TEST AT BATTERY PACK M1676 IAW AMM 33-51-06-960-805.;[02] VERIFIED ACTION ITEM 1;[03] UPDATED PARTS INFO;[04] VERIFIED CORRECTIVE ACTION 1.
- [SDR SWAA2024081525680](https://openairdocs.org/sdr/SWAA2024081525680.md): Battery Pack · inoperative · Aug 14, 2024 · N8699A · Boeing 7378H4 · Emergency Lighting
  > INOP EMERGENCY LIGHTS ASSOCIATED WITH BATTERY PACK M2335.<[01] REMOVED; REPLACED; AND PERFORMED A GOOD TEST AT BATTERY PACK M2335 IAW AMM 33-51-06-960-805.;[02] VERIFIED ACTION ITEM 1;[03] UPDATED PARTS INFO;[04] VERIFIED CORRECTIVE ACTION 1.
- [SDR SWAA2024081525681](https://openairdocs.org/sdr/SWAA2024081525681.md): Battery Pack · inoperative · Aug 14, 2024 · N8699A · Boeing 7378H4 · Emergency Lighting
  > INOP EMERGENCY LIGHTS ASSOCIATED WITH BATTERY PACK M1672.<[01] REMOVED; REPLACED; AND PERFORMED A GOOD TEST AT BATTERY PACK M1672 IAW AMM 33-51-06-960-805.;[02] UPDATED PARTS INFO;[03] UPDATED PARTS INFO;[04] VERIFIED CORRECTIVE ACTION 1.
- [SDR SWAA2024081921932](https://openairdocs.org/sdr/SWAA2024081921932.md): Panel · cracked · Jul 26, 2024 · N8699A · Boeing 7378H4 · Service Doors
  > ASD PANEL 844DZ IS CRACKED<[01] REMOVED GIRT BAR SEAL FROM PANEL 844DZ AND INSTALLED ON NEW PANEL 844DZ IAW SOPM 20-50-01 TORQUE REQUIREMENTS ACCOMPLISHED USING TORQUE WRENCH PER638 S/N 03047691 CAL DUE 12/2024 PANEL 844DZ WILL BE CLOSED ON SWA CARD TTG8Q00TWZ
- [SDR SWAA2024081617891](https://openairdocs.org/sdr/SWAA2024081617891.md): Support · cracked · Jul 26, 2024 · N8699A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AED SURROUND STRUCTURE SUPPORT CLIP AT STGR 7L STA 1006 CRACKED. (MARKED)<[01] UPDATED 3 MEASUREMENTS;[02] REMOVED AND REPLACED AED SURROUND STRUCTURE SUPPORT CLIP AT STR 7L STA 1006 PER SRM 51-40-02-OG-0 AND DWG 147A0010 SHEET 0782;[03] VERIFIED CORRECTIVE AC
- [SDR SWAA2024081517889](https://openairdocs.org/sdr/SWAA2024081517889.md): Isolator · damaged · Jul 26, 2024 · N8699A · Boeing 7378H4 · Galley Doors
  > AFT SERVICE DOOR HAS 1 EA DAMAGED ISOLATOR AT BOTTOM AFT CORNER (MARKED).<[01] REMOVED AND REPLACED BOTH FWD AND AFT ASD BOTTOM CORNER ISOLATORS PER SRM 51-40-02-0G-0 STEPS 2.D.(1) AND 4.;[02] VERIFIED CORRECTIVE ACTION COMPLETE.
- [SDR SWAA2024081517191](https://openairdocs.org/sdr/SWAA2024081517191.md): Angle · corroded · Jul 26, 2024 · N8699A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO BAY INTERCOSTAL ANGLE UNDER SHIELD BS 767+2 RBL 22 WL 156<[01] EVALUATED CORROSION ON INTERCOSTAL ANGLE BS 767+2 RBL 22 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] VER
- [SDR SWAA2024081517192](https://openairdocs.org/sdr/SWAA2024081517192.md): Web · corroded · Jul 26, 2024 · N8699A · Boeing 7378H4 · Fuselage Main, Structure
  > CORROSION ON AFT CARGO BAY SUB THRESHOLD WEB BS 787+12 TO BS 827+4 RBL 28 WL 155<[01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 807+2 REMOVED 0.015' IN AN AREA OF 1'X1' ORIGINAL THICKNESS 0.045' FOUND TO BE OUT OF LIMITS PER SRM
- [SDR SWAA2024081417190](https://openairdocs.org/sdr/SWAA2024081417190.md): Shield · corroded · Jul 26, 2024 · N8699A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO BAY SHIELD BS 767+11 TO BS 767+16 RBL 22 WL 156<[01] EVALUATED CORROSION ON SHIELD BS 767+11 TO BS 767+16 RBL 22 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 C
- [SDR SWAA2024081317897](https://openairdocs.org/sdr/SWAA2024081317897.md): Floorbeam · corroded · Jul 26, 2024 · N8699A · Boeing 7378H4 · Fuselage Main, Floor Beam
  > CORROSION ON PASSENGER CABIN FLOOR BEAM AT BS 947 LBL 50; LBL 25; RBL 25 CORROSION ON PASSENGER CABIN FLOOR BEAM AT BS 947 LBL 50 LBL 25 RBL 25 WL208<[01] REMOVED DAMAGED ON FLOOR BEAM 947 LBL 25 UPPER SURFACE IN AN AREA OF 2' X 1'; REMAINING THICKNESS IS 0.13
- [SDR SWAA2024081616408](https://openairdocs.org/sdr/SWAA2024081616408.md): Floor Support · corroded · Jul 25, 2024 · N8699A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORT STRUCTURE AROUND FITTING BS 947.5; LBL 50<[01] REMOVED DAMAGED ON FLOOR SUPPORT (INTERCOSTAL) AT BS 947.5 LBL 50 WL 208 IN AN AREA OF 1.1' X 1.1'; REMOVED 0.048'; ORIGINAL MATERIAL THICKNESS 0.200'; REMAINING MATERIAL THICKNESS 0.152
- [SDR SWAA2024081616406](https://openairdocs.org/sdr/SWAA2024081616406.md): Floorbeam · corroded · Jul 25, 2024 · N8699A · Boeing 7378H4 · Fuselage Main, Floor Beam
  > SIGN OF CORROSION ON FLOORBEAM STRUCTURE AROUND FITTING BS 947.5; RBL 50<[01] CORROSION WAS FOUND TO BE ON FLOORBEAM BS 947.5 RBL 50 UPPER SURFACE. ALL DIMENSIONS WILL BE ACCOMPLISHED IN CUSTOMERS CARD# TTG8Q00UUSXR.;[02] VERIFIED CORRECTIVE ACTION STEP 1. TAS
- [SDR SWAA2024081616409](https://openairdocs.org/sdr/SWAA2024081616409.md): Floorbeam · corroded · Jul 25, 2024 · N8699A · Boeing 7378H4 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM STRUCTURE AROUND FITTING BS 947.5; RBL 25<[01] CORROSION WAS FOUND TO BE ON FLOORBEAM BS 947.5 RBL 25 UPPER SURFACE. ALL DIMENSIONS WILL BE ACCOMPLISHED IN CUSTOMERS CARD# TTG8Q00UUSXR.;[02] VERIFIED CORRECTIVE ACTION STEP 1. TASK CARD C
- [SDR SWAA2024081617177](https://openairdocs.org/sdr/SWAA2024081617177.md): Support · cracked · Jul 25, 2024 · N8699A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > BREAKER PANEL CRACKED AT BS 540 LBL1 WL 208.<[01] REMOVED AND REPLACED CRACKED BREAKER PANEL BS 540; LBL 1; WL 208 IAW SRM 51-40-02-0G-0;[02] REMOVED AND REPLACED CRACKED BREAKER PANEL BS 540; RBL 1-24; WL 208 IAW SRM 51-40-02-0G-0;[03] CORRECTION; STEP 2;3 IS
- [SDR SWAA2024081617178](https://openairdocs.org/sdr/SWAA2024081617178.md): Floor Support · cracked · Jul 25, 2024 · N8699A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACKED FLOOR SUPPORT AT BS 396 LBL12 WL208<[01] REMOVED AND REPLACED FLOOR SUPPORT AT BS 396 LBL 12 WL208 IAW SRM 51-40-02; BOEING DWG 143A5400 ID: 0184 REV: -; AND BOEING DWG 143A5400 ID: 0140 REV: -.;[02] VERIFIED CORRECTIVE ACTION #1
- [SDR SWAA2024081617179](https://openairdocs.org/sdr/SWAA2024081617179.md): Floor Support · cracked · Jul 25, 2024 · N8699A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACKED FLOOR SUPPORT AT BS 390 LBL52 WL208<[01] REMOVED AND REPLACED FLOOR SUPPORT AT BS 390 LBL 52 WL208 IAW SRM 51-40-02; BOEING DWG 143A5400 ID:0183 REV: - AND BOEING DWG 143A5400 ID:182 REV: -.;[02] VERIFIED CORRECTIVE ACTION #1
- [SDR SWAA2024081617180](https://openairdocs.org/sdr/SWAA2024081617180.md): Floor Support · corroded · Jul 25, 2024 · N8699A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORT AT BS 317 RBL11 WL208<[01] REMOVED AND REPLACED FLOOR SUPPORT AT BS 312-328 RBL 11 WL 208 IAW SRM 51-40-02-0G-0 AND BOEING DWG 141A5400 ID:0001 REV: -.;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.
- [SDR SWAA2024081617181](https://openairdocs.org/sdr/SWAA2024081617181.md): Plate · corroded · Jul 25, 2024 · N8699A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FED MOPSILL AROUND AFT GRIT BAR FITTING PLATE AT BS 345 LBL59 WL208<[01] EVALUATED CORROSION ON FED MOPSILL AROUND AFT GRIT BAR FITTING PLATE AT BS 345 LBL59 WL208 & DETERMINED TO BE OUT OF LIMITS. REMOVED & REPLACED FED MOPSILL IAW SRM 51-40-02;
- [SDR SWAA2024081617189](https://openairdocs.org/sdr/SWAA2024081617189.md): Floorbeam · corroded · Jul 25, 2024 · N8699A · Boeing 7378H4 · Fuselage Main, Floor Beam
  > CORROSION ON FLOOR BEAM AT FWD WET AREA BS328 RBL54; RBL55 WL208. MARKED<[01] REPAIRED DAMAGED ON FLOOR BEAM AT FWD WET AREA BS 328 RBL 54 RBL 55 WL 208 IAW SRM 53-10-51-2R-7.;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.
- [SDR SWAA2024081517182](https://openairdocs.org/sdr/SWAA2024081517182.md): Angle · corroded · Jul 25, 2024 · N8699A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FED MOPSILL SCUFF PLATE ATTACH ANGLE BS 318; 338; 339 LBL60 WL208<[01] EVALUATED CORROSION ON FED MOPSILL SCUFF PLATE ATTACH ANGLE BS 318; 338; 339 LBL60 WL208 & DETERMINED TO BE OUT OF LIMITS. REMOVED & REPLACED FED MOPSILL SCUFF PLATE ATTACH ANG
- [SDR SWAA2024081517183](https://openairdocs.org/sdr/SWAA2024081517183.md): Angle · corroded · Jul 25, 2024 · N8699A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FSD MOPSILL SCUFF PLATE ATTACH ANGLE AT BS 322 AND 331 RBL 59 WL208<[01] COMPLETED MEASURMENT TABLE;[02] DAMAGE OUT OF LIMITS PER SRM 53-10-15-1A-2; REMOVED AND REPLACED SUPPORT ANGLE AT BS 296-331; RBL 59; WL 208; PER SRM 51-40-02-0G-0; REF BOEIN
- [SDR SWAA2024081417184](https://openairdocs.org/sdr/SWAA2024081417184.md): Floor Panel · delaminated · Jul 25, 2024 · N8699A · Boeing 7378H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 241GF HAS UPPER SURFACE DELAMINATION.<[01] DUE TO THE EXTENT OF ALL OF THE DAMAGE; DECIDED TO FABRICATE A NEW FLOOR PANEL; USING BMS4-17TYVI LOT 1557541-1 AND BMS5-107CL1TY1 LOT 1540837-1 ADHESIVE; CURED THE ADHESIVE; UNDER A HEAT L
- [SDR SWAA2024081417187](https://openairdocs.org/sdr/SWAA2024081417187.md): Floor Panel · delaminated · Jul 25, 2024 · N8699A · Boeing 7378H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 231GF HAS UPPER SURFACE DELAMINATION<[01] REMOVED AND REPLACED FLOOR PANEL 231GF PER AMM 53-21-00-400-801;[02] CORRECTED MEASUREMENT TABLE;[03] VERIFIED CORRECTIVE ACTION 1
- [SDR SWAA2024081316400](https://openairdocs.org/sdr/SWAA2024081316400.md): Floor Panel · pulled · Jul 25, 2024 · N8699A · Boeing 7378H4 · Fuselage Floor Panel
  > AFT FLOOR PANEL 241D UPPER SKIN HAS AN AREA OF PULLED STRANDS. (MARKED)<[01] AFT FLOOR PANEL 241D UPPER SKIN WAS REPAIRED IAW SRM 53-00-50-2R-1;[02] JOB COMPLETE.
- [SDR SWAA2024081316391](https://openairdocs.org/sdr/SWAA2024081316391.md): Floor Panel · pulled · Jul 25, 2024 · N8699A · Boeing 7378H4 · Fuselage Floor Panel
  > FWD FLOOR PANEL 221BF HAS AN AREA OF PULLED STRANDS. (MARKED)<[01] 221BF FLOOR PANEL UPPER SURFACE DAMAGE HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1 AND BOEING DWG: 141A5810 ID: 0729.<BR><BR>ATTACHED CURE SHEETS TO THIS FAULT.;[02] VERIFIED CORRECTIVE ACTION ITEM
- [SDR SWAA2024081316393](https://openairdocs.org/sdr/SWAA2024081316393.md): Floor Panel · pulled · Jul 25, 2024 · N8699A · Boeing 7378H4 · Fuselage Floor Panel
  > FWD FLOOR PANEL 221DF UPPER SKIN HAS AN AREA OF PULLED STRANDS. (MARKED)<[01] 221DF FLOOR PANEL UPPER SURFACE DAMAGE HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1 AND BOEING DWG: 141A5810 ID: 0303.<BR><BR>ATTACHED CURE SHEETS TO THIS FAULT.;[02] JOB COMPLETE.

Next page: https://openairdocs.org/aircraft/N8699A/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 = 'N8699A' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8699A/reports

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