# Service difficulty reports: N8324A A list on [N8324A](https://openairdocs.org/aircraft/N8324A.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 · 157 reports - [SDR SWAA2026073080887](https://openairdocs.org/sdr/SWAA2026073080887.md): Pitot Tube · fod · Jul 28, 2026 · N8324A · Boeing 7378H4 · Pitot/Static System > ON ROTATION MAST/CAUTION WITH ENG LIGHT, EEC WENT TO ALTERNATE, CAPTAIN AIRSPEED UNRELIABLE, DECLARED EMER, TRUCKS ROLLED, NOT OVERWEIGHT. AT GATE, MX SAID CAPT PITOT TUBE WAS PLUGGED WITH WASPS R & R CAPTAINS PITOT PROBE IAW AMM 34-11-01 AND LEAK TEST IAW AM - [SDR SWAA2026070719209](https://openairdocs.org/sdr/SWAA2026070719209.md): Trim System · malfunctioned · Jul 7, 2026 · N8324A · Boeing 7378H4 · Stabilizer Control System > STABILIZER TRIM FAILED DURING CRUISE. STAB OUT OF TRIM LIGHT CAME ON AT START OF DESCENT, MAIN AND AUTOPILOT TRIM ELECTRIC INOPERATIVE. PERFORMED FIM 27-41 TASK 804 STM LOGIC CARD RESET. STAB, OPS CHKD NORMAL. PERFORMED TEST 32 SPD/STB TRIM TEST ON A&B WITH - [SDR SWAA2026042090850](https://openairdocs.org/sdr/SWAA2026042090850.md): Slide · out of limits · Apr 18, 2026 · N8324A · Boeing 7378H4 · Escape Slide > FWD SERVICE DOOR ESCAPE SLIDE PRESSURE OUT OF LIMITS. REPLACED FWD SERVICE DOOR ESCAPE SLIDE IAW MT 725-61-06. - [SDR SWAA2025121050129](https://openairdocs.org/sdr/SWAA2025121050129.md): Frame · debonded · Dec 6, 2025 · N8324A · Boeing 7378H4 · Rudder Miscellaneous Structure > LEFT CONDUCTIVE FRAME AT RUDDER WAS DISBONDED REF TLD 25-155-03112 TTG8Q018TDJK. REMOVED 6.125 IN. SECTION OF DISBONDED LOWER CONDUCTIVE FRAME AT RUDDER TE IAW SRM 55-40-01-1A-3. REMOVED SIX RIVETS AT RUDDER TE TO FOM IAW SRM 51-40-02. PERFORMED PERMANENT - [SDR SWAA2025063085948](https://openairdocs.org/sdr/SWAA2025063085948.md): Handle · loose · Jun 26, 2025 · N8324A · Boeing 7378H4 · Passenger/Crew Doors > CUSTOMER WALK ITEM: L1 DOOR AFT AIRFRAME ASSIST HANDLE NEEDS SECURED. SECURED L1 DOOR AFT ASSIST HANDLE IAW B737-800 AMM 25-21-31-420-802. - [SDR SWAA2025063083436](https://openairdocs.org/sdr/SWAA2025063083436.md): Skin · delaminated · Jun 19, 2025 · N8324A · Boeing 7378H4 · Trailing Edge Flaps > LT. OUTBD AFT FLAP UPPER SURFACE DELAMINATED ON INBD. END<[01] 01 - REMOVED AND REPLACED PER [AMM 27-51-22-400-801-NG (OUTBOARD AFT FLAP INSTALLATION - PERMANENT)];[02] VERIFIED REMOVED AND REPLACED PER [AMM 27-51-22-400-801-NG (OUTBOARD AFT FLAP INSTALLATION - [SDR SWAA2025021093781](https://openairdocs.org/sdr/SWAA2025021093781.md): Circuit Breaker · tripped · Feb 6, 2025 · N8324A · Boeing 7378H4 · Light System Wiring > CABIN EMER LIGHTS C.B. TRIPPED CONTACTED CRAIG IN M.O.C. RESET BREAKER SYSTEM RESTORED TO NORMAL. CABIN EMER LIGHTS C.B. TRIPPED CONTACTED CRAIG IN M.O.C RESET BREAKER SYSTEM RESTORED TO NORMAL.<[01] NOTED BY MX. - [SDR SWAA2024111960612](https://openairdocs.org/sdr/SWAA2024111960612.md): Light · inoperative · Nov 16, 2024 · N8324A · Boeing 7378H4 · Emergency Lighting > L1 & L2 EXTERIOR SLIDE EMERGENCY LIGHTS INOP<[01] RELAMPED L1 & L2 EXTERIOR SLIDE EMERGENCY LIGHTS IAW AMM 33-51-04. OPS CHECK GOOD @ THIS TIME. - [SDR SWAA2024092035681](https://openairdocs.org/sdr/SWAA2024092035681.md): Intercostal · cracked · Sep 9, 2024 · N8324A · Boeing 7378H4 · Fuselage Miscellaneous Structure > REPLACE INTERCOSTAL WEB LOCATED BTW BS500F AND BS500G AND LBL21 W156 AT FWD CARGO COMPARTMENT DUE TO EXISTING REPAIR ON SUPPORT ZEE NOT MEETS SPACING FASTENER HOLES REQUIREMENTS GIVEN ON EA M-22-153-0 2024-512618 REPLACE INTERCOSTAL WEB LOCATED BTW BS500F AND - [SDR SWAA2024092432459](https://openairdocs.org/sdr/SWAA2024092432459.md): Winglet · corroded · Aug 30, 2024 · N8324A · Boeing 7378H4 · Wing Main, Frame Structure > CORROSION WINGLET TIP AT LT WING 2024-512594<[01] REPAIRED WINGLET TIP AT LT WING I.A.W B737-800 SRM 57-30-01 REPAIR 6. SEE INDIVIDUAL SIGNS OFF BELOW;[02] REPAIRED WINGLET TIP AT LT WING I.A.W B737-800 SRM 57-30-01 REPAIR 6. SEE INDIVIDUAL SIGNS OFF BELOW - [SDR SWAA2024091931960](https://openairdocs.org/sdr/SWAA2024091931960.md): Stringer · corroded · Aug 29, 2024 · N8324A · Boeing 7378H4 · Fuselage Main, Longeron/Stringer > CORROSION ON STR 27R LOCATED BTW BS 360 TO 380 RBL 15.75 WL 159 AT ELECTRONIC COMPARTMENT 2024-512589<[01] TOOL USED ON STEP 3 UT EQUIPMENT P/N: 45MG; S/N: 130064101; CAL DUE DATE: 13-DEC-24;[02] TOOL USED ON STEP 9: EDDY CURRENT EQUIPMENT P/N: NORTEC 600D S:N - [SDR SWAA2024092429634](https://openairdocs.org/sdr/SWAA2024092429634.md): Angle · corroded · Aug 23, 2024 · N8324A · Boeing 7378H4 · Spoilers > CORROSION RETAINER SEAL ANGLE TRAILING EDGE AT LEVEL SPOILER 1 LT WING 2024-512557<[01] REPLACED RETAINER SEAL ANGLE TRAILING EDGE AT LEVEL SPOILER 1 LT WING I.A.W B737-800 SRM 51-40-02-0G-0 AND DWG# 115A3551; SHEET 3; REV.-.;[02] CERTIFIED CORRECTIVE ACTION S - [SDR SWAA2024092029635](https://openairdocs.org/sdr/SWAA2024092029635.md): Angle · corroded · Aug 23, 2024 · N8324A · Boeing 7378H4 · Wing Miscellaneous Structure > CORROSION INBOARD TRAILING EDGE BONDING JUMPER SUPPORT ANGLE OF AFT BOOST PUMP TANK 2 AT RT WING (2 EA) 2024-512553<[01] REPLACED INBOARD TRAILING EDGE BONDING JUMPER SUPPORT ANGLE OF AFT BOOST PUMP TANK 2 AT RT WING (2 EA) IAW B737-800 AMM 28-22-41-400-801. S - [SDR SWAA2024091929767](https://openairdocs.org/sdr/SWAA2024091929767.md): Balance Weight · out of balance · Aug 23, 2024 · N8324A · Boeing 7378H4 · Elevator Structure > DURING WEIGHT AND BALANCE PROCEDURE OF ELEVATOR RT PN:183A0103-26 SN:006115 FOUND BALANCE WEIGHTS PN:183A0210-15 (1 EA) ON BAY 4 PN:183A0210-14 (1 EA) ON BAY 3 PN:183A0210-14 (1 EA) ON BAY 2 2024-512560<[01] ACCOMPLISHED ELEVATOR BALANCING IAW EA M-22-155-0376 - [SDR SWAA2024092429452](https://openairdocs.org/sdr/SWAA2024092429452.md): Support Angle · cracked · Aug 22, 2024 · N8324A · Boeing 7378H4 · Wing Miscellaneous Structure > CRACK SUPPORT ANGLE FIXED TRAILING EDGE ORSS 297 LT WING 2024-512538<[01] REPLACED SUPPORT ANGLE LOCATED FIXED TRAILING EDGE ORSS 297 LT WING IAW B737-800 SRM 51-40-02 AND DWG 115A3700 REV:-. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED SUPPORT ANGLE LOCATED F - [SDR SWAA2024092428584](https://openairdocs.org/sdr/SWAA2024092428584.md): Nut Plate · corroded · Aug 21, 2024 · N8324A · Boeing 7378H4 · Wing Miscellaneous Structure > CORROSION O/B FIXED LEADING EDGE RAIL NUTPLATE OFSS 449 AT LT WING 2024-512523<[01] REPLACED O/B FIXED LEADING EDGE RAIL NUTPLATE OFSS 449 AT LT WING IAW B737-800 SRM 51-40-02 AND DWG: 112A4402; SHEET: 40; REV: A.;[02] REPLACED O/B FIXED LEADING EDGE RAIL NUTP - [SDR SWAA2024091928583](https://openairdocs.org/sdr/SWAA2024091928583.md): Plate · cracked · Aug 21, 2024 · N8324A · Boeing 7378H4 · Wing Main, Frame Structure > CRACK CORRUGATED PLATE INBOARD TRAILING EDGE IRSS 218 RT WING 2024-512522<[01] TOOK MEASURE OF CRACK IS: 0.275? ON CORRUGATED PLATE INBOARD TRAILING EDGE IRSS 218 RT WING; TOOL USED:CALIPER P/N: 500-197-30; S/N: A18135108; DUE DATE: 12 -JUL-25. EVALUATED DAM - [SDR SWAA2024092428147](https://openairdocs.org/sdr/SWAA2024092428147.md): Support Angle · cracked · Aug 20, 2024 · N8324A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACK ANGLE - SUPPORT BS 500I AND STRINGER 28L FWD CARGO COMPARTMENT 2024-512502<[01] REPLACED ANGLE LOCATED BS 500I AND STRINGER 28L FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 143A7902; SHEET 160; REV: B; SEE INDIVIDUAL SIGN - [SDR SWAA2024092428148](https://openairdocs.org/sdr/SWAA2024092428148.md): Support Angle · cracked · Aug 20, 2024 · N8324A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACK ANGLE - SUPPORT BS 500I AND STRINGER 28R FWD CARGO COMPARTMENT 2024-512503<[01] REPLACED SUPPORT ANGLE LOCATED BS 500I AND STRINGER 28R FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 143A7902; SHEET 160; REV: B.;[02] CORRECT - [SDR SWAA2024092428149](https://openairdocs.org/sdr/SWAA2024092428149.md): Retainer · corroded · Aug 20, 2024 · N8324A · Boeing 7378H4 · Trailing Edge Flaps > CORROSION RETAINER SEAL ANGLE OUTBOARD TRAILING EDGE AT LEVEL SPOILER 10 AT RT WING 2024-512511<[01] REPLACED RETAINER SEAL ANGLE OUTBOARD TRAILING EDGE AT LEVEL SPOILER 10 AT RT WING IAW B737-800 SRM 51-40-02 AND DWG: 115A3551; SHEET: 5; REV: -;[02] CERTIFIED - [SDR SWAA2024092428369](https://openairdocs.org/sdr/SWAA2024092428369.md): Retainer · corroded · Aug 20, 2024 · N8324A · Boeing 7378H4 · Trailing Edge Flaps > CORROSION RETAINER SEAL ANGLE OUTBOARD TRAILING EDGE AT LEVEL SPOILER 3 LT WING 2024-512513<[01] REPLACED RETAINER SEAL ANGLE OUTBOARD TRAILING EDGE AT LEVEL SPOILER 3 LT WING I.A.W B737-800 SRM 51-40-02-0G-0 AND DWG# 115A3551; SHEET 5; REV.-.;[02] CERTIFIED C - [SDR SWAA2024091928146](https://openairdocs.org/sdr/SWAA2024091928146.md): Stringer · cracked · Aug 20, 2024 · N8324A · Boeing 7378H4 · Fuselage Main, Longeron/Stringer > CRACK STRINGER 26L BS 540 AT FWD CARGO COMPARTMENT 2024-512501<[01] TOOL USED ON STEP 3: P/N: 45MG; S/N: 221860711; DUE DATE: 21-NOV-24.;[02] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 23-JAN-25; TEMPERATURE CONTROLLER P - [SDR SWAA2024092427711](https://openairdocs.org/sdr/SWAA2024092427711.md): Support Bracket · cracked · Aug 19, 2024 · N8324A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACK ON SUPPORT BRACKET LOCATED BS867 BTW STR2R AND STR3R AT PASSENGER CABIN 2024-512481<[01] REPLACED SUPPORT BRACKET LOCATED BS867 BTW STR2R AND STR3R AT PASSENGER CABIN I.A.W B737-800 SRM 51-40-02 AND DWG 146A7901 SHEET 66 REV ?A? MEASURE OF CRACK IS: L=0. - [SDR SWAA2024092427973](https://openairdocs.org/sdr/SWAA2024092427973.md): Support Bracket · cracked · Aug 19, 2024 · N8324A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACK PNEUMATIC DUCT SUPPORT BRACKET BS 540 AND LBL 6 AIR CONDITIONING BAY 2024-512487<[01] REPLACED PNEUMATIC DUCT SUPPORT BRACKET BS 540 AND LBL 6 AIR CONDITIONING BAY IAW B737-800 SRM 51-40-02-0G-0. ITEM 9.;[02] REPLACED PNEUMATIC DUCT SUPPORT BRACKET BS 54 - [SDR SWAA2024092427971](https://openairdocs.org/sdr/SWAA2024092427971.md): Web · cracked · Aug 19, 2024 · N8324A · Boeing 7378H4 · Wing Miscellaneous Structure > CRACK WEB TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA LT WING 2024-512484<[01] REPLACED WEB TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA LT WING IAW B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 115A2512 SHEET 16 REV-.

MEASURE OF CRAC - [SDR SWAA2024092427972](https://openairdocs.org/sdr/SWAA2024092427972.md): Angle · cracked · Aug 19, 2024 · N8324A · Boeing 7378H4 · Wing Miscellaneous Structure > CRACK ANGLE TRAILING EDGE ORSS 277 DEFLECTION CONTROL RIB AREA LT WING 2024-512485<[01] REPLACED ANGLE TRAILING EDGE ORSS 277 DEFLECTION CONTROL RIB AREA LT WING IAW B737-800 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DWG 115A2512 SHEET 16 REV-.

MEASURE C - [SDR SWAA2024092427456](https://openairdocs.org/sdr/SWAA2024092427456.md): Angle · cracked · Aug 18, 2024 · N8324A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACK ANGLE LOCATED STA294.5 AND RBL53 WL208.1 AT PASSENGER CABIN 2024-512460<[01] REPLACED ANGLE LOCATED STA294.5 AND RBL53 WL208.1 AT PASSENGER CABIN IAW B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG: 141A8310; SHEET: 33; REV: -; SEE INDIVIDUAL SIGN OF - [SDR SWAA2024092427353](https://openairdocs.org/sdr/SWAA2024092427353.md): Stringer Clip · cracked · Aug 18, 2024 · N8324A · Boeing 7378H4 · Fuselage Main, Attach Fittings > CRACK TIE CLIP LOCATED STA277 AND STR10R AT PASSENGER CABIN 2024-512458<[01] REPLACED TIE CLIP LOCATED STA277 AND STR10R AT PASSENGER CABIN I.A.W. B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG: 141A1110 SHEET: 39; REV: -; AND DWG: 141A8380; SHEET: 21; REV - [SDR SWAA2024092426984](https://openairdocs.org/sdr/SWAA2024092426984.md): Angle · cracked · Aug 17, 2024 · N8324A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACK ANGLE - CLIP LOCATED BS500H AND LBL21 AFT POSITION FWD CARGO COMPARTMENT 2024-512405<[01] REPLACED ANGLE-CLIP LOCATED ON BS500H AND LBL21 AFT POSITION AT FWD CARGO COMPARTMENT I.A.W. B737-800 SRM 51-40-02 AND DWG 143A7505 SHEET:21 REV.: B

SEE INDI - [SDR SWAA2024092426985](https://openairdocs.org/sdr/SWAA2024092426985.md): Angle · cracked · Aug 17, 2024 · N8324A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACK ANGLE - CLIP LOCATED BS500H AND LBL21 FWD POSITION FWD CARGO COMPARTMENT 2024-512406<[01] REPLACED ANGLE-CLIP LOCATED ON BS500H AND LBL21 FWD POSITION AT FWD CARGO COMPARTMENT I.A.W. B737-800 SRM 51-40-02 AND DWG 143A7505 SHEET:21 REV.: B

SEE IND - [SDR SWAA2024092426986](https://openairdocs.org/sdr/SWAA2024092426986.md): Angle · cracked · Aug 17, 2024 · N8324A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACK ANGLE - CLIP LOCATED BS500G AND LBL21 AFT POSITION FWD CARGO COMPARTMENT 2024-512408<[01] REPLACED ANGLE - CLIP LOCATED BS500G AND LBL21 AFT POSITION FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02; SRM: 51-10-02 ITEM 9 AND DWG: 143A7505; SHEET: 108; REV - [SDR SWAA2024092426977](https://openairdocs.org/sdr/SWAA2024092426977.md): Gusset · cracked · Aug 17, 2024 · N8324A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACK ON GUSSET LOCATED BS500I AND STR19R AT FWD CARGO COMPARTMENT 2024-512413<[01] REPLACED GUSSET LOCATED BS500I AND STR19R AT FWD CARGO COMPARTMENT AND FASTENERS IAW B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 143A7902 SHEET 256 AND REV-B. SEE INDIVI - [SDR SWAA2024092426992](https://openairdocs.org/sdr/SWAA2024092426992.md): Support · cracked · Aug 17, 2024 · N8324A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACK SUPPORT ZEE LOCATED BETWEEN STA500E TO STA500F AND LBL21 WL156 AT FWD CARGO COMPARTMENT 2024-512420<[01] PERFORMED PERMANENT REPAIR ON SUPPORT ZEE LOCATED BETWEEN STA 500D TO STA500I AND LBL21 WL156 AT FWD CARGO COMPARTMENT I.A.W 737-800 SRM 53-00-53-2R- - [SDR SWAA2024092427236](https://openairdocs.org/sdr/SWAA2024092427236.md): Angle · cracked · Aug 17, 2024 · N8324A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACK ANGLE - CLIP LOCATED STA500E AND RBL21 FWD CARGO COMPARTMENT 2024-512424<[01] REPLACED ANGLE - CLIP LOCATED STA500E AND RBL21 FWD CARGO COMPARTMENT AND FASTENERS IAW B737-800 SRM 51-40-02 AND DWG: 143A7505; SHEET: 108; REV: -. SEE INDIVIDUAL SIGN OFF BEL - [SDR SWAA2024092426988](https://openairdocs.org/sdr/SWAA2024092426988.md): Stringer Clip · cracked · Aug 17, 2024 · N8324A · Boeing 7378H4 · Fuselage Main, Attach Fittings > CRACK TIE CLIP LOCATED STA500I AND STR26R FWD CARGO COMPARTMENT 2024-512418<[01] REPLACED TIE CLIP LOCATED ON BS500I STR26R AT FWD CARGO COMPARTMENT I.A.W. B737-800 SRM 51-40-02 AND DWG 143A1234 SHEET 13 REV. A

SEE INDIVIDUAL SIGN-OFF BELOW;[02] REPLACE - [SDR SWAA2024092427245](https://openairdocs.org/sdr/SWAA2024092427245.md): Angle · cracked · Aug 17, 2024 · N8324A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACK ANGLE - CLIP LOCATED STA500G AND LBL21 FWD POSITION FWD CARGO COMPARTMENT 2024-512454<[01] REPLACED ANGLE - CLIP LOCATED STA500G AND LBL21 FWD POSITION FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02; SRM: 51-10-02 ITEM 9 AND DWG: 143A7505; SHEET: 108; R - [SDR SWAA2024092427242](https://openairdocs.org/sdr/SWAA2024092427242.md): Bracket · cracked · Aug 17, 2024 · N8324A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACK BRACKET BS 947.5 AND LBL 10 AFT CARGO COMPARTMENT 2024-512438<[01] REPLACED BRACKET BS 947.5 AND LBL 10 AFT CARGO COMPARTMENT IAW B737-800 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DWG 149A8103 SHEET 8 REV-.

MEASURE CRACK IS: L: 1.213?. TOOL USED: - [SDR SWAA2024092326981](https://openairdocs.org/sdr/SWAA2024092326981.md): Angle · cracked · Aug 17, 2024 · N8324A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACK ANGLE - CLIP LOCATED STA500H AND RBL21 FWD POSITION FWD CARGO COMPARTMENT 2024-512407<[01] TOOK MEASURE OF CRACK IS: 0.750? ON ANGLE - CLIP LOCATED STA500H AND RBL21 FWD POSITION FWD CARGO COMPARTMENT TOOL USED:CALIPER P/N: 500-197-30; S/N: B23316997; - [SDR SWAA2024092327243](https://openairdocs.org/sdr/SWAA2024092327243.md): Bracket · cracked · Aug 17, 2024 · N8324A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACK BRACKET BULKHEAD BS 727 AND RBL3 AFT CARGO COMPARTMENT 2024-512437<[01] REPLACED BRACKET LOCATED ON BS727 RBL3 AT AFT COMPARTMENT IAW B737-800 SRM 51-40-02 AND DRW 144A2600 SHEET 1084 REV. - DUE TO NOT FOUND ALLOWABLE DAMAGE LIMITS ON SRM B7377-800
< - [SDR SWAA2024092326979](https://openairdocs.org/sdr/SWAA2024092326979.md): Angle · cracked · Aug 17, 2024 · N8324A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACK ANGLE - CLIP LOCATED STA500F AND RBL21 AFT POSITION FWD CARGO COMPARTMENT 2024-512411<[01] REPLACED ANGLE - CLIP LOCATED STA500F AND RBL21 AFT POSITION FWD CARGO COMPARTMENT AND FASTENERS IAW B737-800 SRM 51-40-02 AND SRM 51-10-02; ITEM 9.DWG: 143A7505; - [SDR SWAA2024092326980](https://openairdocs.org/sdr/SWAA2024092326980.md): Angle · cracked · Aug 17, 2024 · N8324A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACK ANGLE - CLIP LOCATED STA500G AND RBL21 AFT POSITION FWD CARGO COMPARTMENT 2024-512409<[01] TOOK MEASURE OF CRACK IS: 0.267' ON ANGLE - CLIP LOCATED STA500G AND RBL21 AFT POSITION FWD CARGO COMPARTMENT TOOL USED: ELECTRONIC CALIPER P/N: 500-752-20; S/N: - [SDR SWAA2024092326982](https://openairdocs.org/sdr/SWAA2024092326982.md): Angle · cracked · Aug 17, 2024 · N8324A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACK ANGLE - CLIP LOCATED STA500H AND RBL21 AFT POSITION FWD CARGO COMPARTMENT 2024-512404<[01] TOOK MEASURE OF CRACK IS: 0.360' ON ANGLE - CLIP LOCATED STA500H AND RBL21 AFT POSITION FWD CARGO COMPARTMENT TOOL USED: DIGITAL CALIPER P/N: 500-197-30; S/N: B2 - [SDR SWAA2024092326983](https://openairdocs.org/sdr/SWAA2024092326983.md): Angle · cracked · Aug 17, 2024 · N8324A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACK ANGLE - CLIP LOCATED STA500G AND RBL21 FWD POSITION FWD CARGO COMPARTMENT 2024-512410<[01] TOOK MEASURE OF CRACK IS: 0.298' ON ANGLE - CLIP LOCATED STA500G AND RBL21 FWD POSITION FWD CARGO COMPARTMENT TOOL USED: ELECTRONIC CALIPER P/N: 500-752-20; S/N: - [SDR SWAA2024092027240](https://openairdocs.org/sdr/SWAA2024092027240.md): Support Angle · cracked · Aug 17, 2024 · N8324A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACK ANGLE - SUPPORT BS 727B AND LBL 52 CEILING AREA AFT CARGO COMPARTMENT 2024-512427<[01] PERFORMED PERMANENT REPAIR ON ANGLE - SUPPORT BTW BS 727A TO BS 727C AND LBL 52 CEILING AREA AFT CARGO COMPARTMENT IAW B737-800 SRM 51-70-11-2R-0

SEE INDIVIDUA - [SDR SWAA2024092026991](https://openairdocs.org/sdr/SWAA2024092026991.md): Support · corroded · Aug 17, 2024 · N8324A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CORROSION SUPPORT ZEE LOCATED BETWEEN STA500B TO STA500G AND RBL21 WL156 AT FWD CARGO COMPARTMENT 2024-512419<[01] PERFORMED PERMANENT REPAIR ON SUPPORT ZEE LOCATED BETWEEN STA500A TO STA500I AND RBL21 WL156 AT FWD CARGO COMPARTMENT I.A.W B737-800 SRM SRM 53-0 - [SDR SWAA2024092426645](https://openairdocs.org/sdr/SWAA2024092426645.md): Floorbeam · cracked · Aug 16, 2024 · N8324A · Boeing 7378H4 · Fuselage Main, Floor Beam > CRACK ANGLE FLOOR STRUCTURE LOCATED STA540 AND RBL2 AT PASSENGER CABIN 2024-512373<[01] REPLACED ANGLE FLOOR STRUCTURE LOCATED STA540
AND RBL2 AT PASSENGER CABIN AND FASTENERS I.A.W B737-
800 SRM 51-40-02 AND DWG: 143A0060 SHEET: 64 REV: - SEE INDIVIDUAL - [SDR SWAA2024092326978](https://openairdocs.org/sdr/SWAA2024092326978.md): Angle · cracked · Aug 16, 2024 · N8324A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACK ANGLE - CLIP LOCATED STA500F AND RBL21 FWD POSITION FWD CARGO COMPARTMENT 2024-512412<[01] REPLACED ANGLE - CLIP LOCATED STA500F AND RBL21 FWD POSITION FWD CARGO COMPARTMENT I.A.W B737-800 SRM 51-10-02 ITEM (9) SRM 51-40-02 AND DWG 143A7505 SHEET 20 REV - [SDR SWAA2024091926644](https://openairdocs.org/sdr/SWAA2024091926644.md): Angle · cracked · Aug 16, 2024 · N8324A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CRACK ANGLE FLOOR STRUCTURE LOCATED BETWEEN STA380 TO STA400 AND LBL13 AT PASSENGER CABIN 2024-512372<[01] REPLACED ANGLE LOCATED ON FLOOR STRUCTURE BETWEEN STA 380 TO STA 400 AND LBL 13 AT PASSENGER CABIN IAW B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG - [SDR SWAA2024092325992](https://openairdocs.org/sdr/SWAA2024092325992.md): Floor Support · corroded · Aug 14, 2024 · N8324A · Boeing 7378H4 · Fuselage Miscellaneous Structure > CORROSION INTERCOSTAL FLOOR STRUCTURE LOCATED STA947.5 AND RBL50 WL208.1 AT AFT GALLEY AREA 2024-512297<[01] REPLACED INTERCOSTAL FLOOR STRUCTURE LOCATED STA947.5 AND STA967 AND RBL50 WL208.1 AT AFT GALLEY AREA AND FASTENERS I.A.W B737-800 SRM 51-40-02 AND DWG - [SDR SWAA2024091925990](https://openairdocs.org/sdr/SWAA2024091925990.md): Floorbeam · corroded · Aug 14, 2024 · N8324A · Boeing 7378H4 · Fuselage Main, Floor Beam > CORROSION FLOOR BEAM STRUCTURE LOCATED STA986.5 AND RBL43 WL208.1 AT AFT GALLEY AREA 2024-512299<[01] TOOL USED: EDDY CURRENT EQUIPMENT; PN: NORTEC 600D; SN: 60009161631; DUE DATE: 11-MAR-25;[02] STEP 10 TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: Next page: https://openairdocs.org/aircraft/N8324A/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 = 'N8324A' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N8324A/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.