# Service difficulty reports: N8697C

A list on [N8697C](https://openairdocs.org/aircraft/N8697C.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 · 80 reports

- [SDR SWAA2026101500242](https://openairdocs.org/sdr/SWAA2026101500242.md): Doubler · cracked · Oct 2, 2026 · N8697C · Boeing 7378H4 · Fuselage Main, Plate/Skin
  > EGPR SURROUND DOUBLER CRACKED AT LOWER FLANGE. ACCOMPLISHED REPAIR ON EGPR SURROUND DOUBLER LOWER FLANGE IAW SRM 53-10-15-2R-4.
- [SDR SWAA2026091838814](https://openairdocs.org/sdr/SWAA2026091838814.md): Slide · exposed · Sep 14, 2026 · N8697C · Boeing 7378H4 · Escape Slide
  > FWD ENTRY ESCAPE SLIDE HANGING OUT. TUCKED IN ESCAPE SLIDE EXCESS MATERIAL IAW AMM 25-66-00. DID NOT REMOVE OR OPEN SLIDE.
- [SDR SWAA2026090378156](https://openairdocs.org/sdr/SWAA2026090378156.md): Engine · no discrepancy · Aug 30, 2026 · N8697C · Boeing 7378H4 · Engine (Turbine/Turboprop)
  > NR 2 ENGINE AUTO SHUTDOWN WITH FLASHING WHTE BOX, NR 2 ENGINE FOUND AC TO BE POSTIONED WITH TAIL DIRECTLY INTO THE WIND DURING ENG START. NO DEFECTS NOTED IAW 71-00-00.
- [SDR SWAA2026061710896](https://openairdocs.org/sdr/SWAA2026061710896.md): Lens · missing · Jun 10, 2026 · N8697C · Boeing 7378H4 · Emergency Lighting
  > AFT COVE CEILING PANEL EMERGENCY LIGHT LENS MISSING. INSTALLED LENS IAW B737-NG AMM 33-51-03-960-803-NG; NO OPS CHECK REQUIRED. INSTALLED LENS IAW AMM 33-51-03-960-803-NG; NO OPS CHECK REQUIRED.
- [SDR SWAA2026061611064](https://openairdocs.org/sdr/SWAA2026061611064.md): Bracket · missing · Jun 10, 2026 · N8697C · Boeing 7378H4 · Emergency Equipment
  > L1 DOOR FWD GIRT BAR FITTING MISSING. INSTALLED L1 DOOR FWD FLOOR-MOUNTED ESCAPE SLIDE BRACKET IAW AMM 25-66-02-400-801. VERIFIED INSTALLED SERVICEABLE L1 DOOR FWD FLOOR-MOUNTED ESCAPE SLIDE BRACKET IAW AMM 25-66-02-400-801.
- [SDR SWAA2026012864552](https://openairdocs.org/sdr/SWAA2026012864552.md): Battery · no test · Jan 26, 2026 · N8697C · Boeing 7378H4 · Emergency Equipment
  > FORWARD GALLEY FLASHLIGHT WILL NOT TEST. R & R THE FWD GALLEY FLASHLIGHT BATTERY IAW AMM 25-64-00. OPS CHECKED GOOD.
- [SDR SWAA2026010657926](https://openairdocs.org/sdr/SWAA2026010657926.md): Cover · broken · Jan 3, 2026 · N8697C · Boeing 7378H4 · Emergency Lighting
  > LIGHT COVER BROKEN AT ROW 10 CABIN AISLE EMERGENCY LIGHT HOUSING MOUNTED IN THE OVERHEAD BIN BULLNOSE. OK TO CONTINUE IAW MEL 33-15-02 SP1. REMOVED AND REPLACED ROW 10 DEF EMERGENCY LIGHT LENS COVER REFERENCING AMM 33-51-03. OPS CHECK GOOD.
- [SDR SWAA2025091914809](https://openairdocs.org/sdr/SWAA2025091914809.md): Lens · broken · Sep 16, 2025 · N8697C · Boeing 7378H4 · Emergency Lighting
  > AFT SERVICE DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED AFT SERVICE DOOR EMERGENCY EXIT SIGN LENS PER AMM 33-51-01.
- [SDR SWAA2025091911824](https://openairdocs.org/sdr/SWAA2025091911824.md): Battery Pack · inoperative · Sep 5, 2025 · N8697C · Boeing 7378H4 · Emergency Lighting
  > LT AND RT OVERWING EMERGENCY LIGHTS INOP. REMOVED AND REPLACED PER AMM 33-51-06-960-805-NG.
- [SDR SWAA2025091907310](https://openairdocs.org/sdr/SWAA2025091907310.md): Bezel · broken · Aug 22, 2025 · N8697C · Boeing 7378H4 · Emergency Exits
  > ESCAPE HATCH; LEFT SIDE PANEL 833 CLOSING STRAP BEZEL ATTACHED TO DOOR LINER IS BROKEN. SECURED CLOSING STRAP BEZEL TO THE LEFT OVERWING EXIT DOOR 833 PANEL PER SOPM 20-50-12.
- [SDR SWAA2025091907318](https://openairdocs.org/sdr/SWAA2025091907318.md): Strap · unsecure · Aug 22, 2025 · N8697C · Boeing 7378H4 · Emergency Equipment
  > ESCAPE HATCH; LEFT SIDE PANEL 833 ESCAPE STRAP RED VELCRO COVER NOT ATTACHED TO DOOR SURROUND FRAME STRUCTURE. SECURED ESCAPE STRAP RED VELCRO COVER TO DOOR SURROUND FRAME STRUCTURE PER SOPM 20-50-12.
- [SDR SWAA2025091907317](https://openairdocs.org/sdr/SWAA2025091907317.md): Strap · out of adjust · Aug 22, 2025 · N8697C · Boeing 7378H4 · Emergency Equipment
  > ESCAPE HATCH; RIGHT SIDE PANEL 843 ESCAPE STRAP RED VELCRO COVER NOT ATTACHED TO DOOR SURROUND FRAME STRUCTURE.<[01] SECURED ESCAPE STRAP RED VELCRO COVER TO DOOR SURROUND FRAME STRUCTURE PER SOPM 20-50-12.;[02] VERIFIED SECURED ESCAPE STRAP RED VELCRO COVER T
- [SDR SWAA2025092207019](https://openairdocs.org/sdr/SWAA2025092207019.md): Attach Angle · cracked · Aug 21, 2025 · N8697C · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > CRACK FOUND AT BS 663, RBL 34, ON VAPOR BARRIER ATTACH ANGLE. REMOVED VERTICAL ATTACHED FASTENERS ON RT 663 CHORD IAW SRM 51-40-02. REMOVED FUEL TANK FASTENERS AT BS 663 ON VAPOR BARRIER ATTACH ANGLE RBL 6 TO RBL 43 IAW SRM 51-40-02. REMOVED AND REPLACED
- [SDR SWAA2025092206615](https://openairdocs.org/sdr/SWAA2025092206615.md): Angle · cracked · Aug 21, 2025 · N8697C · Boeing 7378H4 · Nacelle/Pylon Miscellaneous Structure
  > NUMBER 1 ENGINE INBD FAN COWL ANGLE AT AFT SIDE OF OIL SERVICE DOOR OPENING CRACKED AT UPPER CORNER. REMOVED AND REPLACED THE NR 1 ENGINE INBD FAN COWL WEB AT OIL SERVICE DOOR IAW AMM 51-40-02.
- [SDR SWAA2025092206607](https://openairdocs.org/sdr/SWAA2025092206607.md): Skin · delaminated · Aug 20, 2025 · N8697C · Boeing 7378H4 · Trailing Edge Flaps
  > LEFT WING OTBD AFT FLAP HAS LARGE AREA OF DELAMINATION ON UPPER SURFACE ON INBD CORNER. REMOVED LT WING OTBD AFT FLAP IAW AMM 27-51-22. INSTALLED LT WING OTBD AFT FLAP IAW AMM 27-51-22.
- [SDR SWAA2025092206605](https://openairdocs.org/sdr/SWAA2025092206605.md): Plate · cracked · Aug 20, 2025 · N8697C · Boeing 7378H4 · Wing Main, Frame Structure
  > HFEC SHOWS EVIDENCE OF CRACK IN WIGGLE PLATE ON FWD INBD CORNER OF PANEL 551EB ATTACH POINT.<[01] HFEC WIGGLE PLATE PER NDT MANUAL 51-00-00 PROCEDURE 23;[02] REMOVED DAMAGED WIGGLE PLATE PER SRM 51-40-02.;[03] REMOVED AND REPLACED WIGGLE PLATE PER SRM 51-40-02
- [SDR SWAA2024122380474](https://openairdocs.org/sdr/SWAA2024122380474.md): Lens · missing · Dec 22, 2024 · N8697C · Boeing 7378H4 · Emergency Lighting
  > BOTH AFT GALLEY EXIT SIGN LENSES MISSING<[01] REINSTALLED GALLEY EXIT SIGN LENSES IAW AMM 33-51-01
- [SDR SWAA2024082228088](https://openairdocs.org/sdr/SWAA2024082228088.md): Slide · dislodged · Aug 19, 2024 · N8697C · Boeing 7378H4 · Escape Slide
  > L1 DOOR SLIDE IS COMING OUT OF ITS CASE<[01] REPOSITION L1 DOOR ESCAPE SLIDE IAW MT 725-61-06
- [SDR SWAA2024072616381](https://openairdocs.org/sdr/SWAA2024072616381.md): Battery Pack · inoperative · Jul 24, 2024 · N8697C · Boeing 7378H4 · Emergency Lighting
  > AFT LEFT EMERGENCY LIGHTS BATTERY PACK INOP. R&R BATTERY PACK PER AMM 33-51-06. EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06. EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06.
- [SDR SWAA2024072614281](https://openairdocs.org/sdr/SWAA2024072614281.md): Battery Pack · inoperative · Jul 19, 2024 · N8697C · Boeing 7378H4 · Emergency Lighting
  > FWD CABIN EMERGENCY LIGHT BATTERY PACK AT STA 500C L/H IS INOP. REMOVED AND REPLACED FWD CABIN EMERGENCY LIGHT POWER PACK AT STA 500C L/H PER AMM 33-51-06. EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06. EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06.
- [SDR SWAA2024072614282](https://openairdocs.org/sdr/SWAA2024072614282.md): Battery Pack · inoperative · Jul 19, 2024 · N8697C · Boeing 7378H4 · Emergency Lighting
  > FWD CABIN EMERGENCY LIGHT BATTERY PACK AT STA 500C R/H IS INOP. REMOVED AND. REPLACED FWD CABIN EMERGENCY LIGHT BATTERY PACK AT STA 500 R/H PER AMM 33-51-06. EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06. EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51
- [SDR SWAA2024072614283](https://openairdocs.org/sdr/SWAA2024072614283.md): Battery Pack · inoperative · Jul 19, 2024 · N8697C · Boeing 7378H4 · Emergency Lighting
  > AFT CABIN EMERGENCY LIGHT BATTERY PACK AT STA 727C L/H IS INOP. REMOVED AND REPLACED AFT CABIN EMERGENCY LIGHT BATTERY PACK AT STA 727C L/H PER AMM 33-51-06. EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06. EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-0
- [SDR SWAA2024072614284](https://openairdocs.org/sdr/SWAA2024072614284.md): Battery Pack · inoperative · Jul 19, 2024 · N8697C · Boeing 7378H4 · Emergency Lighting
  > AFT CABIN EMERGENCY LIGHT BATTERY PACK AT STA 727C RT IS INOP. REMOVED AND REPLACED AFT CABIN EMERGENCY LIGHT BATTERY PACK AT STA 727C R/H PER AMM 3-51-06. EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06. EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06
- [SDR SWAA2024072613573](https://openairdocs.org/sdr/SWAA2024072613573.md): Floor Support · cracked · Jul 17, 2024 · N8697C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > PASSENGER CABIN FLOOR PANEL SUPPORT CRACKED ATTACH FASTENER STA. 540; RBL 2.<[01] REMOVED AND REPLACED PER SRM 51-40-02.;[02] INSPECTED AS REQUIRED. CORRECTIVE ACTION #1
- [SDR SWAA2024072613574](https://openairdocs.org/sdr/SWAA2024072613574.md): Floor Support · cracked · Jul 17, 2024 · N8697C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > PASSENGER CABIN FLOOR PANEL SUPPORT CRACKED ATTACH FASTENER STA. 540; LBL 2.<[01] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-B00069 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)];[02] INSPECTED AS REQUIRED. CORRECTIVE ACTION #1
- [SDR SWAA2024072909913](https://openairdocs.org/sdr/SWAA2024072909913.md): Floor Support · corroded · Jul 7, 2024 · N8697C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FLOOR STRUCTURE INTERCOSTAL LOCATED BETWEEN STAS 947-967; RBL 25 HAS CORROSION ON FWD/RH EDGE<[01] REMOVED CORROSION ON FLOOR SUPPORT INTERCOSTAL LOCATED BETWEEN STA?S 947-967; RBL 25. ORIGINAL THICKNESS OF 0.084; MATERIAL REMOVED.024; REMAINING THICKNESS IS
- [SDR SWAA2024072608010](https://openairdocs.org/sdr/SWAA2024072608010.md): Angle · corroded · Jul 2, 2024 · N8697C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD ENTRY DOOR: THRESHOLD SUPPORT ANGLE LBL 58 FROM STA 312-348; HAS CORROSION AT SEVERAL NUTPLATES AND RADIUS AREA. (M)<[01] REMOVED CORROSION PER SRM 51-10-02.;[02] INSPECTED DAMAGE REMOVAL;[03] TREATED AND PRIMED PER SRM 51-20-02.;[04] TREATED AND PRIMED PE
- [SDR SWAA2024072608012](https://openairdocs.org/sdr/SWAA2024072608012.md): Angle · corroded · Jul 2, 2024 · N8697C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD ENTRY DOOR: THRESHOLD SUPPORT ANGLE LBL 61 FROM STA 312-348; HAS CORROSION AT SEVERAL NUTPLATES. (M) (M)<[01] REMOVED CORROSION PER SRM 51-10-02.;[02] INSPECTED DAMAGE REMOVAL;[03] TREATED AND PRIMED PER SRM 51-20-02.;[04] TREATED AND PRIMED PER SRM 51-20-
- [SDR SWAA2024072907627](https://openairdocs.org/sdr/SWAA2024072907627.md): Floor Support · corroded · Jul 1, 2024 · N8697C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT MACHINED INTERCOSTAL LOCATED BETWEEN STAS 927-947; LBL 51 HAS CORROSION AT STA 946.<[01] REMOVED FLOOR SUPPORT MACHINED INTERCOSTAL LOCATED BETWEEN STA?S 927-947; LBL 51 PER SRM 51-40-02;[02] REMOVED LIGHT SURFACE CORROSION ON FLOOR SUPPORT MACHI
- [SDR SWAA2024072907628](https://openairdocs.org/sdr/SWAA2024072907628.md): Attach Angle · corroded · Jul 1, 2024 · N8697C · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > UPPER WEB ATTACH ANGLE LOCATED BETWEEN STAS 927-947; RBL 25 HAS CORROSION AT STA 946.<[01] REMOVED CORROSION UPPER WEB ATTACH ANGLE LOCATED BETWEEN STA?S 927-947; RBL 25. ORIGINAL THICKNESS OF 0.070; MATERIAL REMOVED.019; REMAINING THICKNESS IS 0.051. ANGLE
- [SDR SWAA2024072907623](https://openairdocs.org/sdr/SWAA2024072907623.md): Intercostal · corroded · Jul 1, 2024 · N8697C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT INTERCOSTAL LOCATED BETWEEN STAS 947-967; RBL 51 HAS CORROSION ON TOP/FWD SURFACE.<[01] REMOVED FLOOR SUPPORT INTERCOSTAL LOCATED BETWEEN STA?S 947-967; RBL 51 PER SRM 51-40-02;[02] REMOVED CORROSION ON FLOOR SUPPORT INTERCOSTAL LOCATED BETWEEN S
- [SDR SWAA2024072907789](https://openairdocs.org/sdr/SWAA2024072907789.md): Plate · corroded · Jul 1, 2024 · N8697C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO COMPARTMENT LH SIDE PLATE BETWEEN STA 727I-727J (MARKED)<[01] REMOVED CORROSION FROM AFT CARGO LEFT SIDE PLATE FROM STA 727I-727J ORIGINAL MATERIAL THICKNESS IS 0.040?; MAX MATERIAL LOSS IS 0.005; MAX ALLOWED IS 0.004 ?; FOUND TO BE OUT
- [SDR SWAA2024072907777](https://openairdocs.org/sdr/SWAA2024072907777.md): Plate · corroded · Jul 1, 2024 · N8697C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO COMPARTMENT LH SIDE PLATE BETWEEN STA 727J-747 (MARKED)<[01] REMOVED CORROSION FROM AFT CARGO LEFT SIDE PLATE FROM STA 727J-747 ORIGINAL MATERIAL THICKNESS IS 0.040?; MAX MATERIAL LOSS IS 0.005; MAX ALLOWED IS 0.004 ?; FOUND TO BE OUT OF
- [SDR SWAA2024072907779](https://openairdocs.org/sdr/SWAA2024072907779.md): Plate · corroded · Jul 1, 2024 · N8697C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO COMPARTMENT LH SIDE PLATE BETWEEN STA 747-767 (MARKED)<[01] REMOVED CORROSION FROM AFT CARGO LEFT SIDE PLATE FROM STA 747-767 ORIGINAL MATERIAL THICKNESS IS 0.040?; MAX MATERIAL LOSS IS 0.005; MAX ALLOWED IS 0.004 ?; FOUND TO BE OUT OF L
- [SDR SWAA2024072907622](https://openairdocs.org/sdr/SWAA2024072907622.md): Floor Support · corroded · Jul 1, 2024 · N8697C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FLOOR STRUCTURE INTERCOSTAL LOCATED BETWEEN STAS 947-967; LBL 25 HAS CORROSION ON FWD/LH EDGE<[01] REMOVED FLOOR SUPPORT INTERCOSTAL LOCATED BETWEEN STA?S 947-967; LBL 51 PER SRM 51-40-02;[02] REMOVED CORROSION ON FLOOR SUPPORT INTERCOSTAL LOCATED BETWEEN STA?
- [SDR SWAA2024072907793](https://openairdocs.org/sdr/SWAA2024072907793.md): Skin · delaminated · Jul 1, 2024 · N8697C · Boeing 7378H4 · Trailing Edge Flaps
  > LH OUTBD AFT FLAP LOWER INBD CORNER HAS DELAMINATION ON UPPER AND LOWER SURFACES.<[01] OK TO INSTALL L/H OUTBD AFT FLAP.;[02] OK TO INSTALL AFT OUTBD FLAP;[03] INSTALLED NEW SERVICEABLE L/H O/B AFT FLAP PER AMM 27-51-22.;[04] INSTALLED NEW SERVICEABLE L/H O/B
- [SDR SWAA2024072907516](https://openairdocs.org/sdr/SWAA2024072907516.md): Plate · corroded · Jun 30, 2024 · N8697C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FWD CARGO COMPARTMENT LH SIDE PLATE BETWEEN STA. 500E-500F.(MARKED)<[01] BLENDED AREAS; REMOVED.010 ' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. THIS SECTION REPLACED ON NR# TTG8Q00UA2SG.;[02] BLENDED AREAS; REMOVED.010 ' MATERIA
- [SDR SWAA2024072907520](https://openairdocs.org/sdr/SWAA2024072907520.md): Plate · corroded · Jun 30, 2024 · N8697C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FWD CARGO COMPARTMENT RH SIDE PLATE BETWEEN STA. 500A-500B.(MARKED)<[01] BLENDED AREAS REMOVED.005' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2;[02] LOCATED AND DRILLED NEW TRANSITION ANGLE P/N #143A7501U188 PER SRM 51-40-05;OK TO
- [SDR SWAA2024072907511](https://openairdocs.org/sdr/SWAA2024072907511.md): Plate · corroded · Jun 30, 2024 · N8697C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FWD CARGO COMPARTMENT RH SIDE PLATE BETWEEN STA. 500C-500D.(MARKED)<[01] BLENDED AREAS REMOVED.005' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2;[02] BLENDED AREAS REMOVED.005' MATERIAL; FOUND TO BE OUT OF LIMITS LIMITS PER SRM 53-0
- [SDR SWAA2024072607513](https://openairdocs.org/sdr/SWAA2024072607513.md): Plate · corroded · Jun 30, 2024 · N8697C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FWD CARGO COMPARTMENT RH SIDE PLATE BETWEEN STA. 500F-500G.(MARKED)<[01] BLENDED AREAS REMOVED.005' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. THIS SECTION TO BE REPLACED ON NR# TTG8Q00UA2QH.;[02] VERIFIED: ROBERT DENSFORD (TECHN
- [SDR SWAA2024072607514](https://openairdocs.org/sdr/SWAA2024072607514.md): Plate · corroded · Jun 30, 2024 · N8697C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FWD CARGO COMPARTMENT RH SIDE PLATE BETWEEN STA. 500H-500I.(MARKED)<[01] BLENDED AREAS REMOVED.005' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. THIS SECTION TO BE REPLACED ON NR# TTG8Q00UA2QH.;[02] VERIFIED: ROBERT DENSFORD (TECHN
- [SDR SWAA2024072607525](https://openairdocs.org/sdr/SWAA2024072607525.md): Plate · corroded · Jun 30, 2024 · N8697C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FWD CARGO COMPARTMENT LH SIDE PLATE BETWEEN STA. 500D-500E.(MARKED)<[01] BLENDED AREAS REMOVED.009' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] VERIFIED OUT OF LIMITS;[03] FABRICATED REPAIR PARTS PER SRM 53-00-53-2R-5 AND EA M
- [SDR SWAA2024072907360](https://openairdocs.org/sdr/SWAA2024072907360.md): Floorbeam · corroded · Jun 29, 2024 · N8697C · Boeing 7378H4 · Fuselage Main, Floor Beam
  > PASSENGER CABIN FLOOR BEAM BS947 RBL50 UNDER AND AROUND LAV TIE DOWN FITTING HAS POSSIBLE CORROSION.<[01] REMOVED LAV TIE DOWN FITTING FROM STA 947 RBL 50 PER SRM 51-40-02;[02] REMOVED CORROSION. ORIGINAL THICKNESS OF 0.180IN; REMOVED 0.075IN MATERIAL; REMAINI
- [SDR SWAA2024072907356](https://openairdocs.org/sdr/SWAA2024072907356.md): Floorbeam · corroded · Jun 29, 2024 · N8697C · Boeing 7378H4 · Fuselage Main, Floor Beam
  > PASSENGER CABIN FLOOR BEAM BS947 RBL25 UNDER AND AROUND LAV TIE DOWN FITTING HAS POSSIBLE CORROSION.<[01] REMOVED LAV TIE DOWN FITTING FROM STA 947 RBL 25 PER SRM 51-40-02;[02] REMOVED CORROSION. ORIGINAL THICKNESS OF 0.180IN; REMOVED 0.052IN MATERIAL; REMAINI
- [SDR SWAA2024072907361](https://openairdocs.org/sdr/SWAA2024072907361.md): Intercostal · corroded · Jun 29, 2024 · N8697C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > PASSENGER CABIN BS952 LBL25 SCREW HOLE HAS POSSIBLE CORROSION.<[01] REMOVED LIGHT SURFACE CORROSION ON PASSENGER CABIN BS952 LBL25 SCREW HOLE. ORIGINAL THICKNESS OF 0.083; MATERIAL REMOVED.003; REMAINING THICKNESS IS 0.080. INTERCOSTAL FOUND TO BE WITHIN LIMI
- [SDR SWAA2024072607354](https://openairdocs.org/sdr/SWAA2024072607354.md): Angle · corroded · Jun 29, 2024 · N8697C · Boeing 7378H4 · Fuselage Main, Floor Beam
  > PASSENGER CABIN FLOOR BEAM AT APPROX. BS987 LBL 43 HAS CORROSION AROUND HOLE. REMOVED DAMAGE. FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1. CUT AND REMOVED DAMAGED PART OF FLOORBEAM IAW SRM 53-70-51-2R-6 REPAIR 6 ALTERNATIVE 4. NDT PART 6;51-00-00 PROCE
- [SDR SWAA2024072617793](https://openairdocs.org/sdr/SWAA2024072617793.md): Floorbeam · corroded · Jun 29, 2024 · N8697C · Boeing 7378H4 · Fuselage Main, Floor Beam
  > PASSENGER CABIN FLOOR BEAM AT APPROX. BS987 LBL 43 HAS CORROSION AROUND HOLE.<[01] REMOVED DAMAGE. FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1.;[02] CUT AND REMOVED DAMAGED PART OF FLOOR BEAM IAW SRM 53-70-51-2R-6 REPAIR 6 ALTERNATIVE 4.;[03] C/W INSPECTIO
- [SDR SWAA2024072607355](https://openairdocs.org/sdr/SWAA2024072607355.md): Floorbeam · corroded · Jun 29, 2024 · N8697C · Boeing 7378H4 · Fuselage Main, Floor Beam
  > PASSENGER CABIN FLOOR BEAM BS947 LBL51 UNDER LAV TIE DOWN FITTING HAS POSSIBLE CORROSION.<[01] REMOVED LAV TIE DOWN FITTING FROM STA 947 LBL 51 PER SRM 51-40-02;[02] REMOVED CORROSION. ORIGINAL THICKNESS OF 0.180IN; REMOVED 0.100IN MATERIAL; REMAINING THICKNES
- [SDR SWAA2024072607357](https://openairdocs.org/sdr/SWAA2024072607357.md): Floorbeam · corroded · Jun 29, 2024 · N8697C · Boeing 7378H4 · Fuselage Main, Floor Beam
  > PASSENGER CABIN FLOOR BEAM BS947 RBL28 HAS SURFACE CORROSION ON TOP SIDE.<[01] REMOVED CORROSION. ORIGINAL THICKNESS OF 0.180IN; REMOVED 0.052IN MATERIAL; REMAINING 0.128IN; FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1..;[02] ENTIRE LENGTH OF FLOOR BEAM UP
- [SDR SWAA2024072906727](https://openairdocs.org/sdr/SWAA2024072906727.md): Bracket · corroded · Jun 28, 2024 · N8697C · Boeing 7378H4 · Wing Miscellaneous Structure
  > RH WING LEADING EDGE FUEL GAUGE BRACKET HAS CORROSION MARKED<[01] REMOVED AND REPLACED WING REFUEL PANEL PER SOPM 20-50-01 AND MM 28-41-61.REFUELING PANELS OPS CHECKED GOOD PER MM 28-41-61;MM 28-21-81 AND MM 28-21-00;[02] C/W INSPECTION

Next page: https://openairdocs.org/aircraft/N8697C/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 = 'N8697C' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8697C/reports

---
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.