# Service difficulty reports: N8309C

A list on [N8309C](https://openairdocs.org/aircraft/N8309C.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 4 · 193 reports

- [SDR SWAA2026100606701](https://openairdocs.org/sdr/SWAA2026100606701.md): Support Angle · cracked · Sep 17, 2026 · N8309C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACKED SUPPORT ANGLE, BS 867, STR 3R REPLACED SUPPORT ANGLE IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, PARAGRAPH 9, & DWG 146A7901, SHEET 66, REV A.
- [SDR SWAA2026100663323](https://openairdocs.org/sdr/SWAA2026100663323.md): Plate · cracked · Sep 17, 2026 · N8309C · Boeing 7378H4 · Wing Main, Frame Structure
  > CRACK ON CORRUGATED PLATE, TRAILING EDGE ORSS 327 RT WING. REPLACED CORRUGATED PLATE AND FASTENERS LOCATED TRAILING EDGE ORSS327 AT RT WING IAW SRM 51-40-02-0G-0, DWG 115A3700, SHEET 60, REV-, AND SRM 51-10-0G-0, PARAGRAPH 9.
- [SDR SWAA2026100666204](https://openairdocs.org/sdr/SWAA2026100666204.md): Plate · cracked · Sep 17, 2026 · N8309C · Boeing 7378H4 · Wing Main, Frame Structure
  > CRACK ON CORRUGATED PLATE LOCATED TRAILING EDGE ORSS297 AT RT WING. REPLACED CORRUGATED PLATE AND FASTENERS LOCATED TRAILING EDGE ORSS297 AT RT WING I.A.W B737-800 SRM 51-40-02-0G-0 DWG 115A3700 SHEET: 60 REV: - AND B737-800 SRM 51-10-02-0G-0 PARAGRAPH 9.
- [SDR SWAA2026100622622](https://openairdocs.org/sdr/SWAA2026100622622.md): Plate · cracked · Sep 17, 2026 · N8309C · Boeing 7378H4 · Wing Main, Frame Structure
  > CRACK ON CORRUGATED PLATE LOCATED TRAILING EDGE ORSS307 AT RT WING. REPLACED CORRUGATED PLATE AND FASTENERS LOCATED TRAILING EDGE ORSS307 AT RT WING IAW SRM 51-40-02-0G-0, DWG 115A3700, SHEET 60, REV -, & SRM 51-10-02-0G-0, PARAGRAPH 9. I
- [SDR SWAA2026100601040](https://openairdocs.org/sdr/SWAA2026100601040.md): Beam · cracked · Sep 17, 2026 · N8309C · Boeing 7378H4 · Wing Main, Frame Structure
  > CRACK ON BEAM LOCATED TRAILING EDGE ORSS279 AT LT WING. REPLACED BEAM LOCATED TRAILING EDGE ORSS279 AT LT WING IAW SRM 51-10-02, ITEM 9, SRM 51-40-02 AND DWG 115A3700 SHEET 60 REV -.
- [SDR SWAA2026100649708](https://openairdocs.org/sdr/SWAA2026100649708.md): Plate · cracked · Sep 17, 2026 · N8309C · Boeing 7378H4 · Wing Main, Frame Structure
  > CRACKED PHENOLIC OF CORRUGATED PLATE LOCATED TRAILING EDGE ORSS 245 AT LT WING. REPLACED CORRUGATED PLATE AND FASTENERS LOCATED TRAILING EDGE ORSS245 AT LT WING IAW DWG 115A2001 SHEET 67, REV -, SRM 51-40-02-0G-0, AND SRM 51-10-02-0G-0, PARAGRAPH 9.
- [SDR SWAA2026100649568](https://openairdocs.org/sdr/SWAA2026100649568.md): Plate · cracked · Sep 17, 2026 · N8309C · Boeing 7378H4 · Wing Main, Frame Structure
  > CRACK ON CORRUGATED PLATE LOCATED TRAILING EDGE IRSS217 AT RT WING. REPLACED CORRUGATED PLATE LOCATED TRAILING EDGE IRSS 217 AT RT WING IAW SRM 51-10-02-0G-0 ITEM 9, AND SRM 51-40-02-0G-0 DWG 115A2001, SHEET 67 REV -.
- [SDR SWAA2026100782166](https://openairdocs.org/sdr/SWAA2026100782166.md): Access Panel · cracked · Sep 16, 2026 · N8309C · Boeing 7378H4 · Wing, Plate/Skin
  > CRACKED ACCESS PANEL 544BB, INTERNAL SKIN, LT WING. REPAIRED THE ACCESS PANEL SKIN IAW EA 26-157-02598, AND EA 26-157-02598-WIP1.
- [SDR SWAA2026100616799](https://openairdocs.org/sdr/SWAA2026100616799.md): Light · deteriorated · Sep 15, 2026 · N8309C · Boeing 7378H4 · Emergency Lighting
  > DETERIORATED PHOTO LUMINESCENT STRIPS. REPLACED PHOTO LUMINESCENT STRIPS IAW AMM 33-51-15- 960-801, AND DWG 33510503, SHEET 14, AND 5, REV B.
- [SDR SWAA2026100561009](https://openairdocs.org/sdr/SWAA2026100561009.md): Plate · cracked · Sep 13, 2026 · N8309C · Boeing 7378H4 · Trailing Edge Flaps
  > CRACKED PLATE ON THE OTBD AFT FLAP TRACK SUPPORT. THE REPLACEMENT OF PLATE ON O/B AFT FLAP TRACK SUPPORT AREA 3 AT LT AFT FLAP IS NOT NECCESARY DUE TO WAS OBTAINED A SERVICIABLE O/B AFT FLAP ON FAULT TTG8Q01E9Y2E.
- [SDR SWAA2026100550157](https://openairdocs.org/sdr/SWAA2026100550157.md): Blade · cracked · Sep 12, 2026 · N8309C · Boeing 7378H4 · Horizontal Stabilizer, Plate/Skin
  > CRACKED ACCESS PANEL 333AB BLADE ASSY AT LT HORIZONTAL STAB. REPLACED THE BLADE ASSY ON ACCESS PANEL 333AB IAW SRM 51-40-02, & SRM 51-10-02, ITEM 9.
- [SDR SWAA2026100603787](https://openairdocs.org/sdr/SWAA2026100603787.md): Skin · debonded · Sep 11, 2026 · N8309C · Boeing 7378H4 · Trailing Edge Flaps
  > DEBONDED O/B AFT FLAP AT LT WING. REPLACED OTBD AFT FLAP REMOVED AND INSTALLED ON TTG8Q01E9Y9V.
- [SDR SWAA2026100525891](https://openairdocs.org/sdr/SWAA2026100525891.md): Scuff Plate · cracked · Sep 11, 2026 · N8309C · Boeing 7378H4 · Service Doors
  > CRACKED SERVICE DOOR SCUFF PLATE. REPAIRED THE SERVICE DOOR SCUFF PLATE IAW SRM 53-10-15-2R-2, REPAIR 2, & BAC 5975.
- [SDR SWAA2026082043249](https://openairdocs.org/sdr/SWAA2026082043249.md): Bulb · inoperative · Aug 16, 2026 · N8309C · Boeing 7378H4 · Emergency Lighting
  > OVERHEAD EMERGENCY EXIT ROW 14 LIGHT HAS TWO BULBS INOPERATIVE. REMOVED AND REPLACED PER [AMM 33-51-01-960-801.
- [SDR SWAA2026062414679](https://openairdocs.org/sdr/SWAA2026062414679.md): Light · inoperative · Jun 22, 2026 · N8309C · Boeing 7378H4 · Emergency Lighting
  > LEFT WING LIGHT INOPERATIVE. REMOVED AND REPLACED THE LAMPS IAW AMM 33-51-04-960-801.
- [SDR SWAA2026062212356](https://openairdocs.org/sdr/SWAA2026062212356.md): Battery Pack · inoperative · Jun 15, 2026 · N8309C · Boeing 7378H4 · Emergency Lighting
  > RIGHT AFT GALLEY EMERGENCY LIGHTS INOPERATIVE. R & R EMERGENCY LIGHT BATTERY PACK IN THE RH AFT GALLEY IAW AMM 33-51-06. OPS CHECKED GOOD.
- [SDR SWAA2026030976352](https://openairdocs.org/sdr/SWAA2026030976352.md): Battery Pack · no test · Mar 4, 2026 · N8309C · Boeing 7378H4 · Emergency Lighting
  > THE AFT LEFT EMERGENCY LIGHT BATTERY PACK FAILED A CAPACITY CHECK. REMOVED & REPLACED THE BATTERY PACK IAW MM 33-51-06.
- [SDR SWAA2026030976362](https://openairdocs.org/sdr/SWAA2026030976362.md): Slider · cracked · Mar 4, 2026 · N8309C · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous Structure
  > LEFT HORIZONTAL STAB, FWD UPPER SLIDER CRACKED. REMOVED AND REPLACED IAW AMM 53-31-31-401, CONFIG 2.
- [SDR SWAA2025122253276](https://openairdocs.org/sdr/SWAA2025122253276.md): Lens · detached · Dec 16, 2025 · N8309C · Boeing 7378H4 · Emergency Lighting
  > LENS ON EMERGENCY OVERHEAD LIGHT ROW 26 FELL OFF. SECURED THE LENS, OPS CHKD GOOD IAW AMM 33-51-00.
- [SDR SWAA2024102149798](https://openairdocs.org/sdr/SWAA2024102149798.md): Bumper · missing · Oct 17, 2024 · N8309C · Boeing 7378H4 · Escape Slide
  > R2 DOOR SLIDE COVER FWD GUARD BUMPER MISSING. PHOTO ADDED TO ATTACHMENT.<[01] INSTALLED MISSING DOOR SLIDE BUMPER COVER END PER AMM 25-66-00.
- [SDR SWAA2024090433202](https://openairdocs.org/sdr/SWAA2024090433202.md): Lens · broken · Aug 31, 2024 · N8309C · Boeing 7378H4 · Emergency Lighting
  > CAPTAIN SIDE PANEL EMERGENCY EXIT LIGHT BROKEN OFF<[01] RR LENS PER MM 33-51-01
- [SDR SWAA2024082730301](https://openairdocs.org/sdr/SWAA2024082730301.md): Wire · chafed · Aug 25, 2024 · N8309C · Boeing 7378H4 · Flight Control System Wiring
  > STAB TRIM FAIL DURING DEPARTURE. REMAINED INOP IN CUT OUT. STAB TRIMMED MANUALLY STAB TRIM FAILED DURING DEPARTURE. REMAINED INOP IN CUTOUT. STAB TRIM MANUALLY.<[01] FOUND CHAFFED WIRE W628-0611-20. PERFORMED WIRE REPAIR PER SWMP 20-30-12. VERIFIED SYSTEM AND
- [SDR SWAA2024052889800](https://openairdocs.org/sdr/SWAA2024052889800.md): Slide · loose · May 24, 2024 · N8309C · Boeing 7378H4 · Escape Slide
  > FWD ENTRY DOOR SLIDE LOOSE IN CONTAINER<[01] R&R FWD ENTRY SLIDE IAW MT 725-61-06
- [SDR SWAA2024020950593](https://openairdocs.org/sdr/SWAA2024020950593.md): Slide · out of limits · Feb 9, 2024 · N8309C · Boeing 7378H4 · Escape Slide
  > FWD SERVICE DOOR ESCAPE SLIDE PRESSURE GAUGE NEEDLE IS IN THE RED BAND.<[01] REF MXI# TTG8Q00RFNZX FOR R/R REF MT 725-61-06 OF FWD SVC DOOR ESCAPE SLIDE DUE TO NEEDLE BEING IN RED BAND.
- [SDR SWAA2023120826708](https://openairdocs.org/sdr/SWAA2023120826708.md): Bulb · inoperative · Dec 3, 2023 · N8309C · Boeing 7378H4 · Emergency Lighting
  > LT AFT EMERGENCY EXIT DOOR; AFT LIGHT HAS 1 BULB OUT<[01] REPLACED LT AFT EMERGENCY EXIT DOOR AFT LIGHT PER AMM 33-51-01-960-801. TEST OK.;[02] VERIFIED CORRECTIVE ACTION #1<BR>VERIFIED MEASUREMENTS
- [SDR SWAA2023120826706](https://openairdocs.org/sdr/SWAA2023120826706.md): Bulb · inoperative · Dec 3, 2023 · N8309C · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY LIGHT HAS 3 BULBS OUT AT AFT ENTRY DOOR; (INTERIOR AFT LOWER)<[01] REPLACED EMERGENCY LIGHT 3 BULBS AT AFT ENTRY DOOR PER AMM 33-51-01-960-801. TEST OK.;[02] VERIFIED CORRECTIVE ACTION #1<BR>VERIFIED MEASUREMENTS
- [SDR SWAA2023120826709](https://openairdocs.org/sdr/SWAA2023120826709.md): Bulb · inoperative · Dec 3, 2023 · N8309C · Boeing 7378H4 · Emergency Lighting
  > LT AFT EMERGENCY EXIT DOOR; FWD LIGHT HAS 1 BULB OUT<[01] REPLACED LT AFT EMERGENCY EXIT DOOR FWD LIGHT PER AMM 33-51-01-960-801.;[02] VERIFIED CORRECTIVE ACTION #1<BR>VERIFIED MEASUREMENTS
- [SDR SWAA2023121124769](https://openairdocs.org/sdr/SWAA2023121124769.md): Light · inoperative · Nov 26, 2023 · N8309C · Boeing 7378H4 · Emergency Lighting
  > L/H OVERWING ESCAPE GROUND ILLUMINATION LIGHT DOES NOT COME ON<[01] UPDATED MEASUREMENTS;[02] REMOVED AND REPLACED CONNECTOR D1108 PER SWPM 22-61-28; OPERATIONAL TEST GOOD PER AMM 33-51-04-960-801.;[03] VERIFIED CORRECTIVE ACTION COMPLETE.<BR>VERIFIED MEASUREM
- [SDR SWAA2023120824770](https://openairdocs.org/sdr/SWAA2023120824770.md): Bulb · inoperative · Nov 26, 2023 · N8309C · Boeing 7378H4 · Emergency Lighting
  > R/H FWD EMERGENCY EXIT DOOR EXIT SIGN LIGHT (L1207) HAS SOME BULBS INOP<[01] RELAMPED AND PERFORMED GOOD OPERATIONAL TEST OF R/H FWD EMERGENCY EXIT DOOR EXIT SIGN LIGHT (L1207) PER AMM 33-51-01-960-801.;[02] VERIFIED CORRECTIVE ACTION STEP 1. VERIFIED MEASUREM
- [SDR SWAA2023120824771](https://openairdocs.org/sdr/SWAA2023120824771.md): Bulb · inoperative · Nov 26, 2023 · N8309C · Boeing 7378H4 · Emergency Lighting
  > L1 DOOR EMERGENCY EXIT INDICATOR LIGHT (L1187) HAS SOME BULBS INOP<[01] RELAMPED AND PERFORMED GOOD OPERATIONAL TEST OF L1 DOOR EMERGENCY EXIT INDICATOR LIGHT (L1187) PER AMM 33-51-01-960-801.;[02] VERIFIED CORRECTIVE ACTION STEP 1. VERIFIED MEASUREMENTS TABLE
- [SDR SWAA2023121123393](https://openairdocs.org/sdr/SWAA2023121123393.md): Splice · corroded · Nov 20, 2023 · N8309C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY FLOOR PNL SPLICE P/N 143A9401-8 IS CORRODED BS 727I+4' LBL 20-RBL 20 W/L 156<[01] REMOVED AND REPLACED AFT CARGO BAY FLOOR PNL SPLICE P/N 143A9401-8 IAW SRM 51-40-02. BS 727I+4' LBL 20-RBL 20 W/L 156;[02] NO ALLOWABLE DAMAGE LIMITS IN SRM REPAIR
- [SDR SWAA2023121121897](https://openairdocs.org/sdr/SWAA2023121121897.md): Support · corroded · Nov 15, 2023 · N8309C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FAULT TTG8Q00PCB4A REQUIRES RII BUYBACK; FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT IS CORRODED AT BS 500I - 500A; RBL 22; WL 155<[01] ACCOMPLISHED RII BUYBACK OF FLOOR TO SIDEWALL REPAIR DOCUMENTED ON TTG8Q00PCB4A.;[02] MEASUREMENTS FOR THIS JOB ARE DOCUMENTED O
- [SDR SWAA2023121119588](https://openairdocs.org/sdr/SWAA2023121119588.md): Baffle · cracked · Nov 8, 2023 · N8309C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO BAY BAFFLE CLIP CRACKED AT BS 500H LBL 23 W/L 155 AFT SIDE OF FRAME<[01] REMOVED AND RE-INSTALLED FWD CARGO BAY BAFFLE CLIP AT BS 500H LBL 23 W/L 155 AFT SIDE OF FRAME IAW SRM 51-10-02 AND DWG 143A7505;[02] REMOVED AND REPLACED FWD CARGO BAY BAFFLE C
- [SDR SWAA2023121119585](https://openairdocs.org/sdr/SWAA2023121119585.md): Baffle · cracked · Nov 8, 2023 · N8309C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO BAY BAFFLE CLIP CRACKED AT BS 500G LBL 23 W/L 155 FWD SIDE OF FRAME<[01] REMOVED AND RE-INSTALLED FWD CARGO BAY BAFFLE CLIP AT BS 500G LBL 23 W/L 155 FWD SIDE OF FRAME IAW SRM 51-10-02 AND DWG 143A7505;[02] REMOVED AND REPLACED FWD CARGO BAY BAFFLE C
- [SDR SWAA2023121119586](https://openairdocs.org/sdr/SWAA2023121119586.md): Baffle · cracked · Nov 8, 2023 · N8309C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO BAY BAFFLE CLIP CRACKED AT BS 500G LBL 23 W/L 155 AFT SIDE OF FRAME<[01] UPDATED STEP 1-3;[02] REMOVED AND REPLACED BAFFLE CLIP AT BS 500G LBL 23 W/L 155 AFT SIDE OF FRAME IAW SRM 51-40-02 AND DWG: 143A7505 REV: - DUE TO NO FOUND ALLOWABLE DAMAGE LIM
- [SDR SWAA2023121119587](https://openairdocs.org/sdr/SWAA2023121119587.md): Baffle · cracked · Nov 8, 2023 · N8309C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO BAY BAFFLE CLIP CRACKED AT BS 500H LBL 23 W/L 155 FWD SIDE OF FRAME<[01] UPDATED STEP 1-3;[02] UPON FUTHER INVESTIGATION FWD CARGO BAY BAFFLE CLIP CRACKED <BR> LOCATED AT BS 500H LBL 23 W/L 155 AFT SIDE OF FRAME;[03] REMOVED AND REPLACED AT BS 500H L
- [SDR SWAA2023113018662](https://openairdocs.org/sdr/SWAA2023113018662.md): Handle · out of adjust · Nov 6, 2023 · N8309C · Boeing 7378H4 · Doors
  > AFT L/H DOOR ASSIST HANDLE IS CRACKED AND MISSING HARDWARE<[01] INSTALLED NEW AFT L/H DOOR ASSIST HANDLE AND HARDWERE IAW SRM 51-40-02;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.
- [SDR SWAA2023121118025](https://openairdocs.org/sdr/SWAA2023121118025.md): Floor Panel · pulled · Nov 5, 2023 · N8309C · Boeing 7378H4 · Fuselage Floor Panel
  > LH PASSENGER FLOOR PANEL 231EF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] LEFT HAND PASSENGER FLOOR PANEL 231EF UPPER SKIN WITH MULTIPLE AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION 1.;[03] VERIFIED COR
- [SDR SWAA2023121118024](https://openairdocs.org/sdr/SWAA2023121118024.md): Floor Panel · pulled · Nov 5, 2023 · N8309C · Boeing 7378H4 · Fuselage Floor Panel
  > LH PASSENGER CABIN FLOOR PANEL 231FF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] LEFT HAND PASSENGER CABIN FLOOR PANEL 231FF UPPER SKIN WITH MULTIPLE AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION #1<BR>VE
- [SDR SWAA2023121118026](https://openairdocs.org/sdr/SWAA2023121118026.md): Floor Panel · pulled · Nov 5, 2023 · N8309C · Boeing 7378H4 · Fuselage Floor Panel
  > LH PASSENGER CABIN FLOOR PANEL 231GF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] L/H PASSENGER CABIN FLOOR PANEL 231GF WITH UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE I
- [SDR SWAA2023121118027](https://openairdocs.org/sdr/SWAA2023121118027.md): Floor Panel · pulled · Nov 5, 2023 · N8309C · Boeing 7378H4 · Fuselage Floor Panel
  > LH PASSENGER CABIN FLOOR PANEL 231DF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] L/H PASSENGER CABIN FLOOR PANEL 231DF WITH UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL USING BMS 4-23 TY 2 LOT#15416
- [SDR SWAA2023121118028](https://openairdocs.org/sdr/SWAA2023121118028.md): Floor Panel · pulled · Nov 5, 2023 · N8309C · Boeing 7378H4 · Fuselage Floor Panel
  > LH PASSENGER CABIN FLOOR PANEL 231KF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE ON LH PASSENGER CABIN FLOOR PANEL 231KF FABRICATED NEW PANEL FROM BMS4-17 TYPE 6 LOT#1534398-1; INSTALLED INSERTS USING BMS5-107 LOT#AK3BA2380A/A
- [SDR SWAA2023121118029](https://openairdocs.org/sdr/SWAA2023121118029.md): Floor Panel · pulled · Nov 5, 2023 · N8309C · Boeing 7378H4 · Fuselage Floor Panel
  > RH PASSENGER CABIN FLOOR PANEL 232DF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] RH PASSENGER CABIN FLOOR PANEL 232DF UPPER SKIN WITH MULTIPLE AREAS OF PULLED STRANDS WAS REPAIRED PER SRM 53-00-50-2R-1.;[02] FINAL INSPECTION. JOB COMPLETE.
- [SDR SWAA2023121118032](https://openairdocs.org/sdr/SWAA2023121118032.md): Floor Panel · pulled · Nov 5, 2023 · N8309C · Boeing 7378H4 · Fuselage Floor Panel
  > RH PASSENGER CABIN FLOOR PANEL 232CF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] RH PASSENGER CABIN FLOOR PANEL 232CF UPPER SKIN WITH MULTIPLE AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO
- [SDR SWAA2023121118030](https://openairdocs.org/sdr/SWAA2023121118030.md): Floor Panel · pulled · Nov 5, 2023 · N8309C · Boeing 7378H4 · Fuselage Floor Panel
  > RH PASSENGER CABIN FLOOR PANEL 232FF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] RH PASSENGER CABIN FLOOR PANEL 232FF UPPER SKIN WITH MULTIPLE AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL PER SRM 53-00-50-2R-0 DUE TO AMOUN
- [SDR SWAA2023121118033](https://openairdocs.org/sdr/SWAA2023121118033.md): Floor Panel · pulled · Nov 5, 2023 · N8309C · Boeing 7378H4 · Fuselage Floor Panel
  > RH PASSENGER CABIN FLOOR PANEL 232EF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE ON RH PASSENGER CABIN FLOOR PANEL 232EF FABRICATED NEW PANEL FROM BMS4-17 TYPE 6 LOT#1534398-1; INSTALLED INSERTS USING BMS5-107 LOT#AK3BA2380A/A
- [SDR SWAA2023121118031](https://openairdocs.org/sdr/SWAA2023121118031.md): Floor Panel · pulled · Nov 5, 2023 · N8309C · Boeing 7378H4 · Fuselage Floor Panel
  > RH PASSENGER CABIN FLOOR PANEL 232HF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] RH PASSENGER CABIN FLOOR PANEL 232HF UPPER SKIN WITH MULTIPLE AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATE FLOOR PANEL PER SRM 53-00-50-2R-0 DUE TO AMOUNT
- [SDR SWAA2023121118021](https://openairdocs.org/sdr/SWAA2023121118021.md): Rib · cracked · Nov 4, 2023 · N8309C · Boeing 7378H4 · Horizontal Stabilizer, Spar/Rib
  > RIGHT HORIZONTAL STAB REMOVABLE L/E 341B RIB #2 IS CRACKED<[01] REMOVED AND REPLACED R HORIZONTAL STAB REMOVABLE L/E 341B; RIB # 2 P/N 186A1302-2; PO # 946197/1; IAW SRM 51-40-02-0G-0 AND DWG. 186A1001.<BR>UPDATED MEASUREMENT TABLE.;[02] UPDATED PART REQUIREME
- [SDR SWAA2023121117291](https://openairdocs.org/sdr/SWAA2023121117291.md): Floor Panel · frayed · Nov 3, 2023 · N8309C · Boeing 7378H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR - FRAYED FIBERS ON OUTER FACESHEET 241FF FLOOR PANEL (MARKED)<[01] FLOOR PANEL 241FF WITH FRAYED FIBERS ON OUTER FACESHEET AS MARKED WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.
- [SDR SWAA2023121117294](https://openairdocs.org/sdr/SWAA2023121117294.md): Floor Panel · frayed · Nov 3, 2023 · N8309C · Boeing 7378H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR - FRAYED FIBERS ON OUTER FACESHEET 221GF FLOOR PANEL (MARKED)<[01] CABIN FLOOR PANEL 221GF WITH FRAYED FIBERS ON OUTER FACESHEET WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02

Next page: https://openairdocs.org/aircraft/N8309C/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 = 'N8309C' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8309C/reports

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