# Service difficulty reports: N8606C

A list on [N8606C](https://openairdocs.org/aircraft/N8606C.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 5 · 204 reports

- [SDR SWAA2026083189225](https://openairdocs.org/sdr/SWAA2026083189225.md): Light · unsecure · Aug 27, 2026 · N8606C · Boeing 7378H4 · Emergency Lighting
  > FLOOR LIGHTING STRIP AT 16D RAISED FROM FLOOR. SECURED FLOOR LIGHTING STRIP WITH DOUBLE SIDED TAPE PER S.I.P AND CONDITION CHK GOOD
- [SDR SWAA2026022473519](https://openairdocs.org/sdr/SWAA2026022473519.md): Lens · wrong part · Feb 23, 2026 · N8606C · Boeing 7378H4 · Emergency Lighting
  > AFT LAV EMERGENCY EXIT LIGHT LENS NEEDS TO BE BLANK. REPLACED LENS IAW CMM 25-48-25. NO OPERATIONAL CHECK REQUIRED. REPLACED LENS IAW CMM 25-48-25. NO OPS CHECKED REQUIRED.
- [SDR SWAA2026022472339](https://openairdocs.org/sdr/SWAA2026022472339.md): Girt Bar · unsecure · Feb 19, 2026 · N8606C · Boeing 7378H4 · Emergency Equipment
  > L2 DOOR AFT GIRT BAR FITTING NEEDS SECURED. SECURED L2 DOOR AFT GIRT BAR FITTING IAW AMM 25-66-02-400-801-NG. (
- [SDR SWAA2026022472342](https://openairdocs.org/sdr/SWAA2026022472342.md): Handle · unsecure · Feb 19, 2026 · N8606C · Boeing 7378H4 · Passenger/Crew Doors
  > L1 DOOR ASSIST HANDLE NEEDS TO BE SECURED. SECURED THE DOOR ASSIST HANDLE AMM 25-21-31-420-802.
- [SDR SWAA2026022472341](https://openairdocs.org/sdr/SWAA2026022472341.md): Handle · unsecure · Feb 19, 2026 · N8606C · Boeing 7378H4 · Passenger/Crew Doors
  > L2 DOOR ASSIST HANDLE NEEDS TO BE SECURED. SECURED THE ASSIST HANDLE IAW AMM 25-21-31-420-802.
- [SDR SWAA2026022472340](https://openairdocs.org/sdr/SWAA2026022472340.md): Handle · unsecure · Feb 19, 2026 · N8606C · Boeing 7378H4 · Galley Doors
  > R2 DOOR ASSIST HANDLE NEEDS TO BE SECURED. SECURED THE DOOR ASSIST HANDLE IAW AMM 25-21-31-420-802.
- [SDR SWAA2026022472343](https://openairdocs.org/sdr/SWAA2026022472343.md): Handle · unsecure · Feb 19, 2026 · N8606C · Boeing 7378H4 · Galley Doors
  > R1 DOOR ASSIST HANDLE NEEDS TO BE SECURED. SECURED THE DOOR ASSIST HANDLE IAW AMM 25-21-31-420-802.
- [SDR SWAA2026011360923](https://openairdocs.org/sdr/SWAA2026011360923.md): Fan Cowl · cracked · Jan 13, 2026 · N8606C · Boeing 7378H4 · Nacelle/Pylon, Main Frame
  > AN APPROX 7 INCH CRACK FOUND ON THE NR 2 ENGINE COWLING OTBD, AT THE 4 O`CLOCK POSITION. R & R OTBD NR 2 ENG FAN COWL IAW 71-11-02.
- [SDR SWAA2025100621588](https://openairdocs.org/sdr/SWAA2025100621588.md): Sign · unsecure · Oct 4, 2025 · N8606C · Boeing 7378H4 · Emergency Lighting
  > ISLE EXIT SIGN WONT STAY UP. R & R CENTER ISLE EXIT SIGN IAW AMM 33-51-02.
- [SDR SWAA2025081400110](https://openairdocs.org/sdr/SWAA2025081400110.md): Skin · delaminated · Aug 10, 2025 · N8606C · Boeing 7378H4 · Trailing Edge Flaps
  > LEFT TRAILING EDGE OTBD AFT FLAP HAS DELAMINATION AND DAMAGE ON I/B AFT EDGE. THE DELAMINATION AREA OF THE LOWER SKIN IS APPROX. 11.5' BY 14'. INCLUDING 5 FASTENER HOLES COMPLETELY PULLED THROUGH. THE MISSING MATERIAL TO THE LOWER SKIN IS ROUGHLY 5.5' X 2.0'.
- [SDR SWAA2025012887176](https://openairdocs.org/sdr/SWAA2025012887176.md): Light · broken · Jan 18, 2025 · N8606C · Boeing 7378H4 · Emergency Lighting
  > FOUND ASSY - EXIT EMERGENCY LIGHTS L1208 AND L1189 BROKEN<[01] REMOVED AND REPLACED EXIT EMERGENCY LIGHTS L1208 AND L1189 AND PERFORMED GOOD TEST IAW AMM 33-51-01-960-802.;[02] VERIFIED CORRECTIVE ACTION #1
- [SDR SWAA2025012890460](https://openairdocs.org/sdr/SWAA2025012890460.md): Light · broken · Jan 18, 2025 · N8606C · Boeing 7378H4 · Emergency Lighting
  > FOUND ASSY - EXIT EMERGENCY LIGHTS L1208 AND L1189 BROKEN<[01] REMOVED AND REPLACED EXIT EMERGENCY LIGHTS L1208 AND L1189 AND PERFORMED GOOD TEST IAW AMM 33-51-01-960-802.;[02] VERIFIED CORRECTIVE ACTION #1
- [SDR SWAA2025012887175](https://openairdocs.org/sdr/SWAA2025012887175.md): Tray · out of adjust · Jan 17, 2025 · N8606C · Boeing 7378H4 · Passenger Compartment Equipment
  > SEATS ROW 14 ABC; ROW 14 DEF DON'T HAVE THE PRESENCE OF ONE-WAY TRAY TABLE LATCHES ON THE BACK OF THE EMERGENCY EXIT SEATS. <[01] ALL STEPS COMPLETED REMOVED AND REPLACED SEAT ROW 14 E&F WITH ONE-WAY TRAY TABLE LACHES PAR CMM 25-21-45 REMOVED AND REPLACED SEA
- [SDR SWAA2025012886392](https://openairdocs.org/sdr/SWAA2025012886392.md): Battery Pack · inoperative · Jan 16, 2025 · N8606C · Boeing 7378H4 · Emergency Lighting
  > ALL EMERGENCY LIGHT ASSOCIATED WITH BATTERY PACK WITH M1672 STAT 952 WL 291 AND RBL 14 ARE INOP<[01] REMOVED AND REPLACED BATTERY PACK M1672 AND PERFORMED GOOD EMERGENCY LIGHTS TEST IAW AMM 33-51-06-960-805.;[02] VERIFIED CORRECTIVE ACTION #1
- [SDR SWAA2025012886393](https://openairdocs.org/sdr/SWAA2025012886393.md): Battery Pack · inoperative · Jan 16, 2025 · N8606C · Boeing 7378H4 · Emergency Lighting
  > ALL EMERGENCY LIGHTS ASSOCIATED WITH M1673 BATTERY PACK AT STA 952 WL 290 LBL 14 ARE INOP<[01] REMOVED AND REPLACED BATTERY PACK M1673 AND PERFORMED GOOD EMERGENCY LIGHTS TEST IAW AMM 33-51-06-960-805.;[02] VERIFIED CORRECTIVE ACTION #1
- [SDR SWAA2025012883294](https://openairdocs.org/sdr/SWAA2025012883294.md): Lens · cracked · Jan 5, 2025 · N8606C · Boeing 7378H4 · Emergency Lighting
  > FWD LAV EMERGENCY LIGHT IS DAMAGED<[01] UPON FURTHER INVESTIGATION; FOUND LENS CRACKED ON FWD LAV EMERGENCY LIGHT ASSEMBLY; REMOVED LENS PER AMM 33-51-01-960-802 STEP 3.C.(5).(D) AND INSTALLED SERVICEABLE LENS PER AMM 33-51-01-960-802 STEP 3.C.(10); NO OPERATI
- [SDR SWAA2025012882026](https://openairdocs.org/sdr/SWAA2025012882026.md): Skin Panel · delaminated · Dec 31, 2024 · N8606C · Boeing 7378H4 · Vertical Stabilizer
  > AREA OF DELAMINATION APPROX. 1.9' X 1.8'ON DORSAL FIN L/H SIDE SKIN 23.9' FROM LOWER EDGE; 37.3' FROM AFT EDGE.<[01] AREA OF DELAMINATION APPROX. 1.9' X 1.8' ON DORSAL FIN AT L/H SIDE SKIN 23.9' FROM LOWER EDGE; 37.3' FROM AFT EDGE WAS REPAIRED IAW SRM 51-70-0
- [SDR SWAA2025012980128](https://openairdocs.org/sdr/SWAA2025012980128.md): Intercostal · cracked · Dec 22, 2024 · N8606C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL ANGLE BETWEEN BS 380-400; LBL13; WL208. <[01] ALL STEPS COMPLETED VERIFIED THAT SRM 51-10-02 IS APPLICABLE TO THIS AIRCRAFT. PART FOUND TO BE OUT OF LIMITS DUE TO NO REPAIR REFERENCE PART WILL BE REPLACED. COMPLETED MEASURMENT TABLE. REMOVE
- [SDR SWAA2025012879551](https://openairdocs.org/sdr/SWAA2025012879551.md): Floor Panel · delaminated · Dec 19, 2024 · N8606C · Boeing 7378H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 231LF HAS DELAMINATION<[01] REPLACED PASSENGER CABIN FLOOR PANEL 231LF WITH SERVICEABLE PART IAW SRM 51-10-02-0G-0 PARA 9.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.
- [SDR SWAA2025012879550](https://openairdocs.org/sdr/SWAA2025012879550.md): Floor Panel · delaminated · Dec 19, 2024 · N8606C · Boeing 7378H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 232HF HAS DELAMINATION<[01] DUE TO THE EXTENT OF DAMAGE; REPLACED PASSENGER CABIN FLOOR PANEL 232HF IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-51-58B ITEM 345.;[02] VERIFIED CORRECTIVE ACTION 1
- [SDR SWAA2025012879155](https://openairdocs.org/sdr/SWAA2025012879155.md): Fairing · delaminated · Dec 19, 2024 · N8606C · Boeing 7378H4 · Trailing Edge Flaps
  > #1 CANOE FAIRING PANEL544BB DELAMINATED AREA ON OUTERM SKIN I/B SIDE 12.5' FROM FWD. END AND 4.4' FROM UPPER END.<[01] RECIEVED NEW FAIRING; INSTALLATION OF FAIRING TO BE ACCOMPLISHED ON FAULT TTG8Q00X5HUN
- [SDR SWAA2025013083096](https://openairdocs.org/sdr/SWAA2025013083096.md): Bracket · deformed · Dec 17, 2024 · N8606C · Boeing 7378H4 · Nacelle/Pylon, Attach Fittings
  > #1 ENGINE HAS A DEFORMED AFT FIRE SEAL BRACKET ON THE UNDERSIDE OF THE PYLON (ONE PIECE) <[01]. UPDATED STEP 1 AND 2; [02] UPDATED STEP 1;2 AND 3.; [03] UPDATED STEP 1.; [04] UPDATED STEP 1 AND 3; [05] UPDATED STEP 1 AND 3.; [06] REPLACED AFT FIRE SEAL IAW SRM
- [SDR SWAA2025012978172](https://openairdocs.org/sdr/SWAA2025012978172.md): Floorbeam · corroded · Dec 17, 2024 · N8606C · Boeing 7378H4 · Fuselage Main, Floor Beam
  > CORROSION ON STA 986 BEAM UPPER SURFACE AT RBL 43; RBL 38; AND LBL 43; WL 208.1<[01] REPAIRED CORROSION ON STA 986 BEAM UPPER SURFACE AT RBL 43; RBL 38; AND LBL 43; WL 208.1 IAW SRM 53-70-51-2R-6 REP. 6. ALT. 3 AND SRM 53-70-51-1A-1 ALLOWABLE DAMAGE 1.
- [SDR SWAA2025012878728](https://openairdocs.org/sdr/SWAA2025012878728.md): Intercostal · cracked · Dec 17, 2024 · N8606C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > INTERCOSTAL CRACKED IN PASSENGER CABIN FLOOR STRUCTURE AT BS500I+6 WL208 LBL2.<[01] CARD COMPLETED;[02] REMOVED & REPLACED INTERCOSTAL PASSENGER CABIN FLOOR STRUCTURE AT BS 500I+6' LBL 2 WL 208 AS PER SRM 51-40-02 & DWG 143A5400 REV A.<BR>CARD COMPLETED;[03] V
- [SDR SWAA2025012878732](https://openairdocs.org/sdr/SWAA2025012878732.md): Intercostal · cracked · Dec 17, 2024 · N8606C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > THERE IS CRACKED INTERCOSTAL IN PASSENGER CABIN FLOOR STRUCTURE AT BS380+10 WL208 LBL53.<[01] PARTIAL STEP 1;[02] REMOVED AND REPLACED INTERCOSTAL AT BS380 TO BS400 WL208 LBL53 PER SRM 51-40-02-0G-0 AND BOEING DWG 143A5400 REV -.;[03] VERIFIED CORRECTIVE ACTIO
- [SDR SWAA2025012878731](https://openairdocs.org/sdr/SWAA2025012878731.md): Intercostal · cracked · Dec 17, 2024 · N8606C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > THERE IS CRACKED INTERCOSTAL IN PASSENGER CABIN FLOOR STRUCTURE AT BS380+14 WL208 LBL3.<[01] PARTIAL STEP 1;[02] CORRECTED FASTENER HOLE SIZE REFERENCE IN STEP 1;[03] REMOVED AND REPLACED INTERCOSTAL AT BS380 TO BS400 WL208 LBL3 IAW SRM 51-40-02-0G-0 AND BOEIN
- [SDR SWAA2025012878730](https://openairdocs.org/sdr/SWAA2025012878730.md): Intercostal · cracked · Dec 17, 2024 · N8606C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > THERE IS CRACKED INTERCOSTAL IN PASSENGER CABIN FLOOR STRUCTURE AT BS360+4 WL208 LBL19. THERE IS CRACKED INTERCOSTAL IN PASSENGER CABIN FLOOR STRUCTURE AT BS360-6 WL208 LBL11.<[01] REMOVED AND REPLACED INTERCOSTAL AT BS 344 TO BS 360 LBL 11 WL 208 PER SRM 51-4
- [SDR SWAA2025012878535](https://openairdocs.org/sdr/SWAA2025012878535.md): Floor Panel · delaminated · Dec 17, 2024 · N8606C · Boeing 7378H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 231KF HAS DELAMINATION ON UPPER SURFACE (MARKED)<[01] PASSENGER CABIN FLOOR PANEL 231KF WAS REPLACED DUE TO EXCESSIVE UPPER SURFACE DELAMINATION IAW SRM 51-10-02-0G-0 PARAGRAPH 9 AND AIPC 53-21-51-58B ITEM #370.;[02] VERIFIED JOB CO
- [SDR SWAA2025012878171](https://openairdocs.org/sdr/SWAA2025012878171.md): Strap · corroded · Dec 17, 2024 · N8606C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT PAX CABIN FLOOR STRAP AT STA 1016+4; RBL 2; WL 208.2.<[01] ALL STEPS COMPLETED VERIFIED THAT SRM 51-10-02-0G-0 IS APPLICABLE TO THIS AIRCRAFT AND SUPPORT ANGLE IS OUT OF LIMITS DUE TO NO REPAIR REFERENCE TO SUPPORT CORROSION REMOVAL. PART WILL
- [SDR SWAA2025012878169](https://openairdocs.org/sdr/SWAA2025012878169.md): Support Angle · corroded · Dec 17, 2024 · N8606C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON GALLEY SUPPORT ANGLE AT STA 986+7; LBL 43 AND LBL 37; WL 208.2.<[01] ALL STEPS COMPLETED VERIFIED THAT SRM 51-10-02-0G-0 IS APPLICABLE TO THIS AIRCRAFT AND SUPPORT ANGLE IS OUT OF LIMITS DUE TO NO REPAIR REFERENCE TO SUPPORT CORROSION REMOVAL. PAR
- [SDR SWAA2025012878165](https://openairdocs.org/sdr/SWAA2025012878165.md): Support Angle · corroded · Dec 17, 2024 · N8606C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON GALLEY SUPPORT ANGLE UPPER FLANGE AT STA 986+6; LBL 32; WL 208.5.<[01] ALL STEPS COMPLETED VERIFIED THAT SRM 51-10-02-0G-0 IS APPLICABLE TO THIS AIRCRAFT AND SUPPORT ANGLE IS OUT OF LIMITS DUE TO NO REPAIR REFERENCE TO SUPPORT CORROSION REMOVAL. P
- [SDR SWAA2025012778532](https://openairdocs.org/sdr/SWAA2025012778532.md): Floor Panel · delaminated · Dec 17, 2024 · N8606C · Boeing 7378H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 231NF HAS UPPER SURFACE DAMAGE (MARKED)<[01] PASSENGER CABIN FLOOR PANEL 231NF WAS REPLACED DUE TO EXCESSIVE UPPER SURFACE DELAMINATION IAW SRM 51-10-02-0G-0 PARAGRAPH 9 AND AIPC 53-21-51-58B ITEM #495.;[02] VERIFIED JOB COMPLETE
- [SDR SWAA2025012778530](https://openairdocs.org/sdr/SWAA2025012778530.md): Floor Panel · delaminated · Dec 17, 2024 · N8606C · Boeing 7378H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 231TF HAS UPPER SURFACE DAMAGE (MARKED)<[01] PASSENGER CABIN FLOOR PANEL 231TF WAS REPLACED DUE TO EXCESSIVE UPPER SURFACE DELAMINATION IAW SRM 51-10-02-0G-0 PARAGRAPH 9 AND AIPC 53-21-51-58B ITEM #655.;[02] VERIFIED JOB COMPLETE
- [SDR SWAA2025012778537](https://openairdocs.org/sdr/SWAA2025012778537.md): Floor Panel · delaminated · Dec 17, 2024 · N8606C · Boeing 7378H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 232JF HAS UPPER SURFACE DAMAGE (MARKED)<[01] PASSENGER CABIN FLOOR PANEL 232JF WAS REPLACED DUE TO EXCESSIVE UPPER SURFACE DELAMINATION IAW SRM 51-10-02-0G-0 PARAGRAPH 9 AND AIPC 53-21-51-58B ITEM #295.;[02] VERIFIED JOB COMPLETE
- [SDR SWAA2025011578134](https://openairdocs.org/sdr/SWAA2025011578134.md): Floor Panel · delaminated · Dec 16, 2024 · N8606C · Boeing 7378H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 222DF HAS UPPER SURFACE DAMAGE (MARKED)<[01] PANEL 222DF WAS REPLACED DUE TO EXTENSIVE UPPER SURFACE DELAMINATION IAW SRM 51-10-02-0G-0 PARAGRAPH 9 AND AIPC 53-21-51-22B ITEM 270.;[02] VERIFIED CORRECTIVE ACTION STEP 1. TASK CARD CO
- [SDR SWAA2025012877501](https://openairdocs.org/sdr/SWAA2025012877501.md): Angle · cracked · Dec 15, 2024 · N8606C · Boeing 7378H4 · Wing Miscellaneous Structure
  > CRACK ON ANGLE LH WING TRAILING EDGE ORSS-281 APROX. MARKED WITH RED TAPE. [01] REMOVED; REPLACED; AND INSTALLED A NEW ANGLE AT LH WING; TRAILING EDGE; ORSS-281 IAW SRM 51-40-02 AND IPC 57-45-51-03.; [02] VERIFIED CORRECTIVE ACTION 1.
- [SDR SWAA2025013177369](https://openairdocs.org/sdr/SWAA2025013177369.md): Intercostal · cracked · Dec 14, 2024 · N8606C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > INTERCOSTAL CRACKED IN PAX CABIN FLOOR STRUCTURE AT BS312+6 RBL35 WL208<[01]. REMOVED AND REPLACED INTERCOSTAL BS312-BS328 RBL35 WL208 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 141A5400 REV -; [02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.
- [SDR SWAA2025013177370](https://openairdocs.org/sdr/SWAA2025013177370.md): Intercostal · cracked · Dec 14, 2024 · N8606C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > INTERCOSTAL CRACKED IN PAX CABIN FLOOR STRUCTURE AT BS277+14 BL0 WL208.<[01] REMOVED; REPLACED; AND INSTALLED A NEW INTERCOSTAL PAX CABIN FLOOR STRUCTURE AT BS277+14; BL0; WL208 IAW SRM 51-40-02; AND BOEING DWG 141A5400.
- [SDR SWAA2025013177494](https://openairdocs.org/sdr/SWAA2025013177494.md): Intercostal · corroded · Dec 14, 2024 · N8606C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON CABIN FLOOR STRUCTURE SUPPORT FRAME AT BS328+8 LBL25 WL208.<[01] REMOVED AND REPLACED FLOOR SUPPORT INTERCOSTAL I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 141A5730 REV:A;[02] VERIFIED RII CORRECTIVE ACTION ITEM 1; CARD COMPLETE.
- [SDR SWAA2025012977497](https://openairdocs.org/sdr/SWAA2025012977497.md): Attach Angle · corroded · Dec 14, 2024 · N8606C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FSD CUTOUT SURROUND STRUCTURE MOPSILL FROM BS294.5+8 TO BS328 WL208 RBL60.<[01] EVALUATED DAMAGE ON FSD MOPSILL ATTACH ANGLE BS298-BS331 RBL60 AND FOUND TO BE OUT LIMITS REMOVED; LOCATED; DRILLED; INSTALLED ALL I.A.W SRM 53-10-15-1A-2 ALLOWABLE DA
- [SDR SWAA2025012977499](https://openairdocs.org/sdr/SWAA2025012977499.md): Frame · cracked · Dec 14, 2024 · N8606C · Boeing 7378H4 · Fuselage Main, Frame
  > CRACK ON UPPER CHORD FRAME ASSEMBLY ON FED CUTOUT SURROUND AT BS312; BETWEEN S-5L AND S-6L WL283.<[01] ACOMPLISHED REPAIR I.A.W M-22-153-01244 (737-NG - SWA - BS 312 FRAME UPPER CHORD CRACK DAMAGE AT LBL 33 BETWEEN S-5L AND S-6L) RECORD ON CCN TTG8Q00XN7SS;[02
- [SDR SWAA2025020379148](https://openairdocs.org/sdr/SWAA2025020379148.md): Structure · debonded · Dec 13, 2024 · N8606C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > UNBONDED CAP STRIP FWD SIDE LOWER CORNER ON PANEL 844AW ASD DOOR LINER (MARKED)<[01] REMOVED AND REPLACED CAP STRIP ON FWD SIDE LOWER CORNER OF PANEL 844AW ASD DOOR LINER IAW BOEING DWG# 411A2114-41B SHEETS 1 AND 3; DWG# 411A2114 SHEET 20 FRAME 1; AND DWG# 411
- [SDR SWAA2025012977156](https://openairdocs.org/sdr/SWAA2025012977156.md): Baffle · corroded · Dec 13, 2024 · N8606C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON BAFFLE BS500C TO BS500D WL156 RBL25<[01] REMOVED AND REPLACED NEW BAFFLE BS500C TO BS500D WL156 RBL25 IAW SRM 51-40-02-0G-0. AND DWG 143A7505 REV:A.;[02] VERIFIED CORRECTIVE ACTION ITEM 1; CARD COMPLETE.
- [SDR SWAA2025012977157](https://openairdocs.org/sdr/SWAA2025012977157.md): Baffle · corroded · Dec 13, 2024 · N8606C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON BAFFLE CLIPS BS500H AND BS500F FWD SIDE OF FRAME WL156 LBL25<[01] REMOVED BAFFLE CLIPS BS500H AND BS500F FWD SIDE OF FRAME WL156 LBL25 IAW SRM 51-40-02-0G-0 AND LOCATED; DRILLED AND REPLACED NEW BAFFLE CLIPS BS500H AND BS500F FWD SIDE OF FRAME WL1
- [SDR SWAA2025011577161](https://openairdocs.org/sdr/SWAA2025011577161.md): Baffle · corroded · Dec 13, 2024 · N8606C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION FWD CARGO 3EA BAFFLES FROM BS500D TO BS 500H WL156 RBL25<[01] REMOVED AND REPLACED FWD CARGO 3EA BAFFLES FROM BS500D TO BS 500H WL156 RBL25 IAW SRM 51-40-02-0G-0 AND DWG 143A7505 REV:A.;[02] VERIFIED CORRECTIVE ACTION ITEM 1; CARD COMPLETE.
- [SDR SWAA2025011577160](https://openairdocs.org/sdr/SWAA2025011577160.md): Baffle · corroded · Dec 13, 2024 · N8606C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION FWD CARGO BAY 2EA BAFFLE CLIPS BS500G AND BS500H FWD SIDE OF FRAME WL156 RBL25<[01] REMOVED AND REPLACED FWD CARGO BAY 2EA BAFFLE CLIPS BS500G AND BS500H FWD SIDE OF FRAME WL156 RBL25 IAW SRM 51-40-02-0G-0 AND DWG 143A7505 REV: B.;[02] VERIFIED CORRE
- [SDR SWAA2025011577162](https://openairdocs.org/sdr/SWAA2025011577162.md): Baffle · corroded · Dec 13, 2024 · N8606C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION FWD CARGO BAY ON BAFFLE CLIP BS500H AFT SIDE OF FRAME WL156 RBL25<[01] REMOVED AND REPLACED FWD CARGO BAY ON BAFFLE CLIP BS500H AFT SIDE OF FRAME WL156 RBL25 IAW SRM 51-40-02-0G-0 AND DWG 143A7505 REV:-.;[02] VERIFIED CORRECTIVE ACTION ITEM 1; CARD C
- [SDR SWAA2025012976316](https://openairdocs.org/sdr/SWAA2025012976316.md): Threshold · cracked · Dec 12, 2024 · N8606C · Boeing 7378H4 · Cargo Compartments
  > AFT CARGO BAY AFT CORNER THRESHOLD IS CRACKED<[01]. REPAIRED AFT CARGO BAY AFT CORNER THRESHOLD PER SRM 5360-15-2R-1; [02] VERIFIED.
- [SDR SWAA2025012976577](https://openairdocs.org/sdr/SWAA2025012976577.md): Web · corroded · Dec 12, 2024 · N8606C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY SUB THRESHOLD WEB MULTIPLE AREAS AROUND NUT PLATE HOLES BS794 TO BS847 RBL 26 WL156<[01]. REMOVED DAMAGED AFT CARGO BAY SUB THRESHOLD WEB IAW SRM 51-40-02-0G-0 AND LOCATED; DRILLED; INSTALLED NEW AFT CARGO BAY SUB THRESHOLD WEB BS794 TO
- [SDR SWAA2025011576580](https://openairdocs.org/sdr/SWAA2025011576580.md): Support Plate · corroded · Dec 12, 2024 · N8606C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 RBL22 WL156<[01] CORROSION ON AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE; FOUND TO BE OUT OF LIMITS. REMOVED; REPLACED AND INSTALLED NE

Next page: https://openairdocs.org/aircraft/N8606C/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 = 'N8606C' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8606C/reports

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