# Service difficulty reports: N8317M

A list on [N8317M](https://openairdocs.org/aircraft/N8317M.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 · 186 reports

- [SDR SWAA2026071319864](https://openairdocs.org/sdr/SWAA2026071319864.md): Spring · out of position · Jul 9, 2026 · N8317M · Boeing 7378H4 · Passenger/Crew Doors
  > FWD ENTRY DOOR HANDLE IN VERTICAL POSITION ON THE OUTSIDE WITH FWD ENTRY DOOR HANDLE ON THE INTERIOR; IN THE CLOSED & LOCKED POSITION. R & R FWD ENTRY DOOR HANDLE SHAFT SPRING IN REF. TO AMM 52-11-11. OPS CHECKED GOOD.
- [SDR SWAA2026070718718](https://openairdocs.org/sdr/SWAA2026070718718.md): Battery Pack · inoperative · Jul 5, 2026 · N8317M · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY LIGHTS AT R/H FORWARD SERVICE DOOR; INTERIOR AND EXTERIOR INOP. REPLACED FWD SERVICE POWER SUPPLY -BATTERY PACK PER AMM 33-51-06. OPS CHKD NORMAL.
- [SDR SWAA2026061109945](https://openairdocs.org/sdr/SWAA2026061109945.md): Girt Bar · out of adjust · Jun 7, 2026 · N8317M · Boeing 7378H4 · Emergency Equipment
  > GIRT BAR FWD SERVICE DOOR NEEDS ADJUSTMENT. ADJUSTED GIRT BAR AND OPS CHKD GOOD IAW AMM 25-66-01.
- [SDR SWAA2025081499997](https://openairdocs.org/sdr/SWAA2025081499997.md): Bulb · inoperative · Aug 10, 2025 · N8317M · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY EXIT PROXIMITY LIGHT ASSEMBLIES AT LEFT AFT OVERWING; AFT ENTRY; AND AFT SERVICE DOORS HAVE INOPERATIVE BULBS. EMERGENCY EXIT PROXIMITY LIGHT ASSEMBLIES AT LEFT AFT OVERWING AFT ENTRY AND AFT SERVICE DOORS HAVE INOPERATIVE BULBS. RELAMPED AND TEST
- [SDR SWAA2024112670911](https://openairdocs.org/sdr/SWAA2024112670911.md): Cover · loose · Nov 22, 2024 · N8317M · Boeing 7378H4 · Emergency Lighting
  > LOWER RH AFT OVWING EMER EXIT EMER LT COVER FELL OFF<[01] RESECURED LOWER AFT EMER EXIT LT COVER PER MM 33-51-01
- [SDR SWAA2024041067578](https://openairdocs.org/sdr/SWAA2024041067578.md): Floor Panel · cracked · Mar 26, 2024 · N8317M · Boeing 7378H4 · Fuselage Floor Panel
  > CRACK ON FLOOR PANEL 120CF FWD CARGO COMPARTMENT 2024-165933<[01] REPLACED FLOOR PANEL 120CF FWD CARGO COMPARTMENT IAW B737-800 AMM 25-52-01-201-801 AND DWG 453A1610 SHEET 65 REV-<BR>MATERIAL USED ALUMINUM SHEET: P/N: 2024-T3 0.071? PO 2022 208767. SEE INDIVI
- [SDR SWAA2024041063461](https://openairdocs.org/sdr/SWAA2024041063461.md): Floor Support · elongated · Mar 14, 2024 · N8317M · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > ELONGATED HOLE ON WEB-INTERCOSTAL LOC. BTW BS 500A TO BS 500B LBL 22 WL 156 AT FWD CARGO COMPARTMENT 2024-165922<[01] REPLACED WEB-INTERCOSTAL AND FASTENERS LOC. BTW BS 500A TO BS 500B LBL 22 WL 156 AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02 AND DWG 14
- [SDR SWAA2024041063462](https://openairdocs.org/sdr/SWAA2024041063462.md): Floor Support · elongated · Mar 14, 2024 · N8317M · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > ELONGATED HOLE ON WEB-INTERCOSTAL LOC. BTW BS 500E TO BS 500F LBL 22 WL 156 AT FWD CARGO COMPARTMENT 2024-165921<[01] REPLACED WEB-INTERCOSTAL AND FASTENERS LOC. BTW BS 500E TO BS 500F LBL 22 WL 156 AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02 AND DWG 14
- [SDR SWAA2024041062810](https://openairdocs.org/sdr/SWAA2024041062810.md): Intercostal · cracked · Mar 13, 2024 · N8317M · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ON WEB INTERCOSTAL LOC. BETWEEN BS500 TO BS500A AT STR 26L FWD CARGO COMPARTMENT 2024-165919<[01] REPLACED WEB INTERCOSTAL LOC. BETWEEN BS500 TO BS500A AT STR 26L FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02-0G-0 AND DWG 143A7505 SHEET 108 REV ?<BR>SE
- [SDR SWAA2024041162308](https://openairdocs.org/sdr/SWAA2024041162308.md): Access Panel · elongated · Mar 12, 2024 · N8317M · Boeing 7378H4 · Wing, Plate/Skin
  > ELONGATED HOLE PLATE ACCESS PANEL 644BB FLAP SUPPORT FAIRING 8 AT RT WING 2024-165916<[01] REPLACED PLATE ACCESS PANEL 644BB FLAP SUPPORT FAIRING 8 AT RT WING I.A.W. B737-800 SRM 51-40-02-0G-0;[02] CERTIFIED WORK PERFORMED
- [SDR SWAA2024041160876](https://openairdocs.org/sdr/SWAA2024041160876.md): Plate · cracked · Mar 8, 2024 · N8317M · Boeing 7378H4 · Wing Miscellaneous Structure
  > CRACK ON CORRUGATED PLATE TRAILING EDGE LOCATED IRSS216 AT LT WING 2024-165872<[01] REPLACED CORRUGATED PLATE LOCATED ON TRAILING EDGE IRSS 216 AT LT WING IAW B737-800 SRM 51-10-02 PARAGRAPH 9 AND SRM51-40-02.<BR>SEE INDIVIDUAL SIGNS-OFF BELOW.;[02] JOB COMPLE
- [SDR SWAA2024041160869](https://openairdocs.org/sdr/SWAA2024041160869.md): Angle · cracked · Mar 8, 2024 · N8317M · Boeing 7378H4 · Wing Miscellaneous Structure
  > CRACK ANGLE TRAILING EDGE ATTACHED ON DEFLECTION CONTROL RIB ORSS273 RT WING 2024-165870<[01] REPLACED ANGLE TRAILING EDGE ATTACHED ON DEFLECTION CONTROL RIB ORSS273 RT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 115A6200 REV: B SHEET 11. MEASURE OF CRACK IS
- [SDR SWAA2024041060864](https://openairdocs.org/sdr/SWAA2024041060864.md): Support · cracked · Mar 8, 2024 · N8317M · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ON SUPPORT ZEE LOCATED BS 480 PLUS 18 INCHES AT LEVEL STR 26L AT FWD CARGO COMPARTMENT 2024-165864<[01] FAULT RESOLVED ON OTHER FAULT TTG8Q00S0PD7;[02] FAULT RESOLVED ON OTHER FAULT TTG8Q00S0PD7
- [SDR SWAA2024041060871](https://openairdocs.org/sdr/SWAA2024041060871.md): Angle · cracked · Mar 8, 2024 · N8317M · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ON ANGLE LOCATED BS 500I AFT FACE AT LEVEL STR 28R AT FWD CARGO COMPARTMENT 2024-165863<[01] REPLACED ANGLE LOCATED BS 500I AFT FACE AT LEVEL STR 28R AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02;SRM 51-10-02;ITEM 9;DWG 143A7902 SHEET 160 REV B.SEE
- [SDR SWAA2024041060874](https://openairdocs.org/sdr/SWAA2024041060874.md): Support · cracked · Mar 8, 2024 · N8317M · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK SUPPORT ZEE LOCATED BS 500C PLUS 9 AT LEVEL STR 26L INCHES AT FWD CARGO COMPARTMENT 2024-165869<[01] FAULT RESOLVED ON OTHER FAULT TTG8Q00S0PD7;[02] FAULT RESOLVED ON OTHER FAULT TTG8Q00S0PD7
- [SDR SWAA2024041060868](https://openairdocs.org/sdr/SWAA2024041060868.md): Support · corroded · Mar 8, 2024 · N8317M · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON SUPPORT ZEE LOCATED BTW BS 500D TO BS 500I LBL 22 WL 156 AT FWD CARGO COMPARTMENT 2024-165868<[01] TOOL USED P/N: 45MG; S/N: 221860711; CAL DUE: 21-NOV-24.;[02] THE DAMAGE WAS REPAIRED PER SRM 53-00-53-2R-5 (REPAIR 5) AND EA M-22-153-01550. SEE IN
- [SDR SWAA2024041060857](https://openairdocs.org/sdr/SWAA2024041060857.md): Door · out of adjust · Mar 8, 2024 · N8317M · Boeing 7378H4 · Service Doors
  > OUT OF ADJUSTMENT AFT ENTRY DOOR AT AFT GALLEY AREA 2024-165823<[01] PERFORMED ADJUSTMENT AFT ENTRY DOOR AT AFT GALLEY AREA IAW B737-800 AMM 52-13-00-820-801;[02] CORRECTED STEP 1<BR>PERFORMED ADJUSTMENT AFT ENTRY DOOR AT AFT GALLEY AREA IAW B737-800 AMM 52-13
- [SDR SWAA2024041060030](https://openairdocs.org/sdr/SWAA2024041060030.md): Floor Panel · cracked · Mar 6, 2024 · N8317M · Boeing 7378H4 · Fuselage Floor Panel
  > CRACK ON PANEL 211B AT COCKPIT 2024-165780<[01] MEASURED THE DAMAGE ON PANEL 211B AT COCKPIT AND FOUND WITHIN LIMITS TO REPAIR; DAMAGE SIZE OF REPAIR AREA IS: L=9 IN W=8 IN (72 IN2) AND REPAIRED IAW B737-800 AMM 25-00-00-340-801 PAR E METHOD 1 TOOL USED CALIPE
- [SDR SWAA2024041059856](https://openairdocs.org/sdr/SWAA2024041059856.md): Angle · cracked · Mar 6, 2024 · N8317M · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ON ANGLE LOCATED BS 867 BTW STAR 2R TO STR 3R AT PASSENGER CABIN 2024-165750 CRACK ON ANGLE LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN<[01] REPLACED ANGLE AND FASTENERS LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN IAW B737-800 SRM 5
- [SDR SWAA2024041060031](https://openairdocs.org/sdr/SWAA2024041060031.md): Angle · cracked · Mar 6, 2024 · N8317M · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE LOCATED BTW STA 380 TO STA 400 LBL 13.5 AT FWD GALLEY AREA 2024-165782<[01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE: 23-JAN-25.TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811019 DUE DATE: 23-JAN-25.;[02] REP
- [SDR SWAA2024041059857](https://openairdocs.org/sdr/SWAA2024041059857.md): Frame · cracked · Mar 6, 2024 · N8317M · Boeing 7378H4 · Fuselage Main, Frame
  > CRACK FRAME STA 312 AND BTW STR 5L TO STR 6L AT PASSENGER CABIN 2024-165776<[01] PERFORMED REPAIR ON FRAME LOCATED STA 312 AND BTW STR 5L TO STR 6L AT PASSENGER CABIN IAW EA M-22-153-01244<BR>SEE INDIVIDUAL SIGN-OFF BELOW;[02] PERFORMED REPAIR ON FRAME LOCATED
- [SDR SWAA2024041059371](https://openairdocs.org/sdr/SWAA2024041059371.md): Angle · cracked · Mar 5, 2024 · N8317M · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE BTW STA 291.5 TO STA 294.5 AND RBL 53 AT FWD GALLEY AREA 2024-165668<[01] REPLACED ANGLE AND FASTENERS LOCATED BTW STA 291.5 TO STA 294.5 AND RBL 53 AT FWD GALLEY AREA IAW B737-800 SRM 51-40-02 AND DWG 141A8310 SHEET 33 REV-.<BR>SEE INDIVIDUAL SIGN
- [SDR SWAA2024041059362](https://openairdocs.org/sdr/SWAA2024041059362.md): Web · cracked · Mar 5, 2024 · N8317M · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ON WEB LOCATED BTW BS 927 TO BS 947.5 AT LEVEL STR 25R AT AFT CARGO COMPARTMENT. REPLACED WEB LOCATED BTW BS 927 TO BS 947.5 AT LEVEL STR 25R AT AFT CARGO COMPARTMENT IAW SRM 51-10-02 ITEM 9 AND DWG:147A7500; SHEET:36; REV-.
- [SDR SWAA2024041059369](https://openairdocs.org/sdr/SWAA2024041059369.md): Strap · broken · Mar 5, 2024 · N8317M · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > BROKEN FLOOR STRUCTURE STRAP LOCATED BTW STA 312 TO STA 344 AND BL 0 AT FWD GALLEY AREA 2024-165666<[01] REPLACED FLOOR STRUCTURE STRAP LOCATED BTW STA 312 TO STA 344 AND BL 0 AT FWD GALLEY AREA IAW #DWG: 141A5400 SHEET: 1 REV:- AND SRM 51-40-02.<BR>SEE INDIVI
- [SDR SWAA2024041059363](https://openairdocs.org/sdr/SWAA2024041059363.md): Angle · cracked · Mar 5, 2024 · N8317M · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE - CLIP LOCATED AFT BS500H STR26R FWD CARGO COMPARTMENT 2024-165582<[01] REPLACED ANGLE - CLIP LOCATED AFT BS500H STR26R FWD CARGO COMPARTMENT AND FASTENER IAW B737-700 #DWG:143A7502 SHEET: 109 REV:- AND SRM 51-40-02.<BR>SEE INDIVIDUAL SIGNS OF BELO
- [SDR SWAA2024041059364](https://openairdocs.org/sdr/SWAA2024041059364.md): Fitting · cracked · Mar 5, 2024 · N8317M · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ON FITTING LOCATED BS 947.5 AT LEVEL STR 26L AT AFT CARGO COMPARTMENT 2024-165658<[01] REPLACED FITTING AND FASTENERS LOCATED BS 947.5 AT LEVEL STR 26L AT AFT CARGO COMPARTMENT IAW B737-800 SRM 51-40-02;SRM 51-10-02;ITEM 9;DWG 149A8103 SHEET 8 REV-.SEE I
- [SDR SWAA2024041059366](https://openairdocs.org/sdr/SWAA2024041059366.md): Support · corroded · Mar 5, 2024 · N8317M · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION SUPPORT ZEE LOCATED BTW BS 767 TO BS 727G RBL 22 WL 156 AFT CARGO COMPARTMENT. REPLACED SUPPORT ZEE LOCATED BTW BS 727G TO 767 RBL 22 WL 156 AFT CARGO COMPARTMENT IAW B737-800 SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02; DWG 146A7500; SHEET 213, REV- AN
- [SDR SWAA2024041059368](https://openairdocs.org/sdr/SWAA2024041059368.md): Floor Support · cracked · Mar 5, 2024 · N8317M · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK WEB - INTERCOSTAL LOCATED BTW STA 344 TO STA 360 AND BL 0 AT FWD GALLEY AREA 2024-165663<[01] REPLACED WEB - INTERCOSTAL LOCATED BTW STA 344 TO STA 360 AND BL 0 AT FWD GALLEY AREA IAW B737-800 SRM 51-40-02 AND DWG 141A5400; SHEET 32; REV -. SEE INDIVIDUA
- [SDR SWAA2024041059365](https://openairdocs.org/sdr/SWAA2024041059365.md): Floor Support · cracked · Mar 5, 2024 · N8317M · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK WEB - INTERCOSTAL LOCATED BTW STA 277 TO STA 294.5 AND BL 0 FWD GALLEY AND LAV 2024-165659<[01] REPLACED WEB - INTERCOSTAL AND FASTENERS LOCATED BTW STA 277 TO STA 294.5 AND BL 0 FWD GALLEY AND LAV I.A.W. B737-800 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND
- [SDR SWAA2024041059059](https://openairdocs.org/sdr/SWAA2024041059059.md): Floor Support · corroded · Mar 4, 2024 · N8317M · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION FLOOR STRUCTURE INTERCOSTAL LOCATED BTW STA 947.5 TO STA 967 AND LBL 50 WL 208.1 AT AFT GALLEY AREA 2024-165644<[01] REPLACED INTERCOSTAL LOCATED FLOOR STRUCTURE BTW STA 947.5 TO STA 967 AND LBL 50 WL 208.1 AT AFT GALLEY AREA IAW B737-800 SRM 51-10-0
- [SDR SWAA2024041167370](https://openairdocs.org/sdr/SWAA2024041167370.md): Support Bracket · elongated · Mar 3, 2024 · N8317M · Boeing 7378H4 · Wing Miscellaneous Structure
  > ELONGATED HOLE ON SUPPORT BRACKET OF PNEUMATIC DUCT INBOARD LEADING EDGE IFSS162 LT WING 2024-165617<[01] REPLACED SUPPORT BRACKET OF PNEUMATIC DUCT INBOARD LEADING EDGE IFSS162 LT WING IAW B737-800 SRM 51-40-02-0G-0;[02] CORRECTED STEP 1: REPLACED SUPPORT BRA
- [SDR SWAA2024041058628](https://openairdocs.org/sdr/SWAA2024041058628.md): Floor Panel · cracked · Mar 3, 2024 · N8317M · Boeing 7378H4 · Fuselage Floor Panel
  > CRACK FLOOR PANEL 140CF AT AFT CARGO COMPARTMENT 2024-165620<[01] FABRICATED FLOOR PANEL 140CF AT AFT CARGO COMPARTMENT IAW B737-800 AMM 25-52-01-201-801;AND DWG 453A2610; SHEET 11; REV C; MATERIAL USED ALUMINUM SHEET 2024-T3;0.071 INCH<BR>SEE INDIVIDUAL SIGN-
- [SDR SWAA2024041058465](https://openairdocs.org/sdr/SWAA2024041058465.md): Handle · deteriorated · Mar 3, 2024 · N8317M · Boeing 7378H4 · Passenger/Crew Doors
  > DETERIORATED ON FWD ENTRY DOOR NUT ASSIST HANDLE UPPER AND LOWER (4EA) 2024-165605<[01] REPLACED FWD ENTRY DOOR NUT ASSIST HANDLE UPPER AND LOWER (4EA) IAW SOPM 20-50-01;[02] REPLACED FWD ENTRY DOOR NUT ASSIST HANDLE UPPER AND LOWER (4EA) IAW SOPM 20-50-01
- [SDR SWAA2024041058466](https://openairdocs.org/sdr/SWAA2024041058466.md): Handle · deteriorated · Mar 3, 2024 · N8317M · Boeing 7378H4 · Passenger/Crew Doors
  > DETERIORATED ON AFT ENTRY DOOR NUT ASSIST HANDLE 2EA 2024-165606<[01] REMOVED AND REPLACED AFT ENTRY DOOR ASSIST HANDLE NUT (2EA) IAW B737-800 AMM 52-13-31-400-802 ITEM 3G(2);[02] REMOVED AND REPLACED AFT ENTRY DOOR ASSIST HANDLE NUT (2EA) IAW B737-800 AMM 52-
- [SDR SWAA2024041058030](https://openairdocs.org/sdr/SWAA2024041058030.md): Angle · cracked · Mar 1, 2024 · N8317M · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE - CLIP LOCATED AFT BS500G AND STR26L FWD CARGO COMPARTMENT 2024-165570<[01] REPLACED CLIP LOCATED AFT BS500G AND STR26L FWD CARGO COMPARTMENT IAW B737-800 SRM 51-10-02 ITEM 9 SRM 51-40-02 AND DRAWING 143A7505 SHEET 109 REV -<BR>SEE INDIVIDUAL SIGN
- [SDR SWAA2024041058032](https://openairdocs.org/sdr/SWAA2024041058032.md): Angle · cracked · Mar 1, 2024 · N8317M · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE - CLIP LOCATED FWD BS500G AND STR26L FWD CARGO COMPARTMENT 2024-165568<[01] REPLACED ANGLE-CLIP AN FASTENERS LOCATED FWD BS500G AND STR26L FWD CARGO COMPARTMENT I.A.W. B737-800 SRM 51-10-02 ITEM 9; B737-800 SRM 51-40-02 AND DRAWING 143A7505; SHEET
- [SDR SWAA2024041058034](https://openairdocs.org/sdr/SWAA2024041058034.md): Angle · cracked · Mar 1, 2024 · N8317M · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE - CLIP LOCATED AFT BS500H AND STR26L FWD CARGO COMPARTMENT 2024-165573<[01] REPLACED CLIP LOCATED AFT BS500H AND STR26L FWD CARGO COMPARTMENT IAW B737-800 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DRAWING 143A7505 SHEET 109 REV -;[02] CORRECTED STEP 1<
- [SDR SWAA2024041058127](https://openairdocs.org/sdr/SWAA2024041058127.md): Angle · cracked · Mar 1, 2024 · N8317M · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE - CLIP LOCATED FWD BS500G STR26R FWD CARGO COMPARTMENT 2024-165579<[01] REPLACED CLIP LOCATED FWD BS500G STR26R FWD CARGO COMPARTMENT IAW B737-800 SRM 51-10-02 SRM 51-40-02 AND DRAWING 143A7505 SHEET 109 REV -<BR>SEE INDIVIDUAL SIGN OFF BELOW;[02]
- [SDR SWAA2024041058129](https://openairdocs.org/sdr/SWAA2024041058129.md): Angle · cracked · Mar 1, 2024 · N8317M · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE - CLIP LOCATED FWD BS500H STR26R FWD CARGO COMPARTMENT 2024-165581<[01] REPLACED CLIP LOCATED FWD BS500H STR26R FWD CARGO COMPARTMENT IAW B737-800 SRM 51-10-02 Ï¿½TEM 9; SRM 51-40-02 AND DRAWING 143A7505 SHEET 109 REV-<BR>SEE INDIVIDUAL SIGN OFF BE
- [SDR SWAA2024041058128](https://openairdocs.org/sdr/SWAA2024041058128.md): Angle · cracked · Mar 1, 2024 · N8317M · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE - CLIP LOCATED AFT BS500A STR26R FWD CARGO COMPARTMENT 2024-165578<[01] REPLACED ANGLE - CLIP LOCATED AFT BS500A STR26R FWD CARGO COMPARTMENT AND FASTENER IAW B737-700 #DWG:143A7502 SHEET: 108 REV:- AND SRM 51-40-02.<BR>SEE INDIVIDUAL SIGNS OF BELL
- [SDR SWAA2024041058126](https://openairdocs.org/sdr/SWAA2024041058126.md): Angle · cracked · Mar 1, 2024 · N8317M · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE (GUSSET) LOCATED BS500I STR19R AT FWD CARGO COMPARTMENT 2024-165583<[01] REPLACED FASTENERS AND ANGLE (GUSSET) LOCATED BS500I STR19R AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-10-02 ITEM 9 SRM 51-40-02 AND DWG 143A7902; SHEET 256; REV B.<BR>SEE I
- [SDR SWAA2024041058029](https://openairdocs.org/sdr/SWAA2024041058029.md): Angle · cracked · Mar 1, 2024 · N8317M · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE FLOOR STRUCTURE LOCATED AT BS695 AND RBL 24.75 AT PASSENGER CABIN 2024-165530<[01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE: 23-JAN-25. TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811019 DUE DATE: 23-JAN-25.;
- [SDR SWAA2024041058033](https://openairdocs.org/sdr/SWAA2024041058033.md): Angle · cracked · Mar 1, 2024 · N8317M · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE - CLIP LOCATED FWD BS500H AND STR26L FWD CARGO COMPARTMENT 2024-165572<[01] EVALUATED CLIP LOCATED FWD BS500H AND STR26L FWD CARGO COMPARTMENT AND NOT FOUND ALLOWABLE DAMAGE IN B737-800 SRM 53-00-53-1A-2 CLIP MUST BE REPLACED. MEASURE OF CRACK IS:
- [SDR SWAA2024041057419](https://openairdocs.org/sdr/SWAA2024041057419.md): Scuff Plate · cracked · Feb 29, 2024 · N8317M · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACK LOCATED ON AFT CORNER SCUFF PLATE OF AFT CARGO COMPARTMENT 2024-165485<[01] TOOL USED DIGITAL CALIPER P/N:500-196-30;S/N:A23325654;DUE DATE:03-JAN-25;[02] TOOL USED ON STEP 4; RADIOMETER PHOTOMETER P/N: XRP-3000; S/N:1753759; CAL DUE DATE: 12-APR-24;[03]
- [SDR SWAA2024041057417](https://openairdocs.org/sdr/SWAA2024041057417.md): Lens · broken · Feb 28, 2024 · N8317M · Boeing 7378H4 · Emergency Lighting
  > BROKEN COVER LENS CEILING PANEL EMERGENCY LIGHT ON POSITION FWD CENTER AND AFT AT PASSENGER CABIN (3 EA) 2024-165449<[01] REPLACED COVER LENS CEILING PANEL EMERGENCY LIGHT ON POSITION FWD CENTER AND AFT AT PASSENGER CABIN (3 EA) IAW B737-800 AMM 35-51-03-960-8
- [SDR SWAA2024041057198](https://openairdocs.org/sdr/SWAA2024041057198.md): Floorbeam · cracked · Feb 28, 2024 · N8317M · Boeing 7378H4 · Fuselage Main, Floor Beam
  > CRACK FLOOR STRUCTURE STIFFENER LOACTAED AT BS540 AND BETWEEN RBL24.75 TO RBL 45.5 AT PASSENGER CABIN 2024-165425<[01] REPLACED FLOOR STRUCTURE STIFFENER LOCATED BS 540 AND BETWEEN RBL24.75 TO RBL 45.5 AT PASSENGER CABIN IAW B737-800 SRM 51-40-02 AND DWG 143A0
- [SDR SWAA2024041056611](https://openairdocs.org/sdr/SWAA2024041056611.md): Light · deteriorated · Feb 27, 2024 · N8317M · Boeing 7378H4 · Emergency Lighting
  > DETERIORATE PHOTOLUMINESCENT STRIP LT SIDE AT PASSENGER CABIN (7EA) 2024-165391<[01] REPLACED PHOTOLUMINESCENT STRIP LT SIDE AT PASSENGER CABIN (7EA) IAW B737-800 AMM 33-51-15-000-802 STEP 1.A(1) (B);[02] CORRECTED STEP 1 <BR>REPLACED PHOTOLUMINESCENT STRIP LT
- [SDR SWAA2024041056612](https://openairdocs.org/sdr/SWAA2024041056612.md): Light · deteriorated · Feb 27, 2024 · N8317M · Boeing 7378H4 · Emergency Lighting
  > DETERIORATE PHOTOLUMINESCENT STRIP RT SIDE AT PASSENGER CABIN (10EA) 2024-165393<[01] REPLACED PHOTOLUMINESCENT STRIP RT SIDE AT PASSENGER CABIN (10EA) IAW B737-800 AMM 33-51-15-400-802 STEP 1.A(1) (B);[02] REPLACED PHOTOLUMINESCENT STRIP RT SIDE AT PASSENGER
- [SDR SWAA2024022355269](https://openairdocs.org/sdr/SWAA2024022355269.md): Lens · missing · Feb 23, 2024 · N8317M · Boeing 7378H4 · Emergency Lighting
  > AISLE EMERGENCY EXIT LIGHT LENS MISSING @ ROW 23ABC.<[01] INSTALLED AISLE EMERGENCY EXIT LIGHT LENS @ 23ABC PER AMM 33-51-00.
- [SDR SWAA2023100406886](https://openairdocs.org/sdr/SWAA2023100406886.md): Motor · out of trim · Oct 2, 2023 · N8317M · Boeing 7378H4 · Stabilizer Control System
  > ON DESCENT STAB OUT OF TRIM LIGHT ILLUMINATED FOLLWED QRH PROCEDURES<[01] REMOVED AND REPLACED STABILIZER TRIM MOTOR PER AMM 27-41-71 OPS CHECK GOOD. EV # E027000

Next page: https://openairdocs.org/aircraft/N8317M/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 = 'N8317M' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8317M/reports

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