# Service difficulty reports: N8693A A list on [N8693A](https://openairdocs.org/aircraft/N8693A.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 · 88 reports - [SDR SWAA2026102624322](https://openairdocs.org/sdr/SWAA2026102624322.md): Actuator · cracked · Oct 23, 2026 · N8693A · Boeing 7378H4 · Drag Control Actuator > LOSS OFF A HYDRAULIC PRESSURE IN ENGINE AND ELECTRIC PUMP, A HYDRAULIC QTY WENT TO ZERO IN FLIGHT. FOUND NR 12 GROUND SPOILER ACTUATOR HOUSING CRACKED. R & R THE NR 12 GROUND SPOILER ACTUATOR IAW AMM 27-62-94 UP TO STEP E.(6)(D). PERFORMED LEAK CHK & GROUN - [SDR SWAA2026081972945](https://openairdocs.org/sdr/SWAA2026081972945.md): Handle · loose · Aug 15, 2026 · N8693A · Boeing 7378H4 · Passenger/Crew Doors > LOOSE DOOR HANDLE ON AFT ENTRY DOOR. TIGHTENED ASD FWD DOOR ASSIST HANDLE IAW AMM 52-13-31-400-802 SECTION 3.G. - [SDR SWAA2026081996875](https://openairdocs.org/sdr/SWAA2026081996875.md): Handle · loose · Aug 15, 2026 · N8693A · Boeing 7378H4 · Passenger/Crew Doors > LOOSEN TWO DOOR HANDLES AT FWD ENTRY DOOR ON THE DOOR AND ON AFT DOOR LINER TIGHTENED DOOR HANDLES AT FWD ENTRY DOOR ON THE DOOR AND ON AFT DOOR LINER IAW AMM 52-11-31-401-NG. TIGHTENED DOOR HANDLES AT FWD ENTRY DOOR ON THE DOOR AND ON AFT DOOR LINER IAW 52-11 - [SDR SWAA2026081828741](https://openairdocs.org/sdr/SWAA2026081828741.md): Fuse · inoperative · Aug 13, 2026 · N8693A · Boeing 7378H4 · Emergency Lighting > FWD OVERWING LH/RH EXIT LOCATOR SIGNS INOP REPLACED FUSE FOR FWD OVERWING LH/RH EXIT LOCATOR SIGNS IAW AMM 33-51-06-960-804. REPLACED FUSE AND PERFORMED GOOD OPERATIONAL TEST - [SDR SWAA2026081839947](https://openairdocs.org/sdr/SWAA2026081839947.md): Lamp · inoperative · Aug 13, 2026 · N8693A · Boeing 7378H4 · Emergency Lighting > EXTERIOR EMERGENCY LIGHTS RIGHT AFT OWE AND RIGHT FUSELAGE JUST AFT OF FLAPS ARE INOP RELAMPED EXTERIOR EMERGENCY LIGHTS RIGHT AFT OWE AND RIGHT FUSELAGE JUST AFT OF FLAPS AND CHECKED GOOD PER AMM 33-51-04-960-801 VERIFIED - [SDR SWAA2026081868995](https://openairdocs.org/sdr/SWAA2026081868995.md): Switch · disconnected · Aug 12, 2026 · N8693A · Boeing 7378H4 · Light System Wiring > EMERGENCY EXIT LIGHT INTEGRATED SWITCH ASSY DOES NOT OPERATE UPON FURTHER INVESTIGATION FOUND PIN 31 RECESSED ON D14372 INSERTED CONTACT INTO PIN 31 FULLY PER SWPM 20-61-00 AND PERFORMED A GOOD TEST OF THE EMERGENCY EXIT LIGHT VIA THE AFT ATTENDANT PANEL IAW A - [SDR SWAA2026081987670](https://openairdocs.org/sdr/SWAA2026081987670.md): Megaphone · damaged · Aug 5, 2026 · N8693A · Boeing 7378H4 · Emergency Equipment > PORTABLE SAFETY MEGAPHONE DAMAGED WHILE REMOVING FROM G2 GALLEY. REMOVED AND REPLACED PORTABLE SAFETY MEGAPHONE IN G2 GALLEY IAW AMM INTRO SIP AND SWA DWG 25600008. - [SDR SWAA2026081919226](https://openairdocs.org/sdr/SWAA2026081919226.md): Switch · inoperative · Aug 4, 2026 · N8693A · Boeing 7378H4 · Emergency Lighting > FUNCTIONAL CHECK, ALL EMERGENCY LIGHTS, OUTGOING, PERFORMED A GOOD OPS TEST OF ALL EMERGENCY LIGHTS IAW AMM 33-51-00-710-801. FOUND EMERGENCY EXIT LIGHT INTEGRATED SWITCH ASSY DOES NOT OPERATE AND WILL BE ADDRESSED ON CCN: TTG8Q01DNVD2, LT AFT OVERWING EXI - [SDR SWAA2026072442868](https://openairdocs.org/sdr/SWAA2026072442868.md): Flashlight · inoperative · Jul 20, 2026 · N8693A · Boeing 7378H4 · Emergency Equipment > ONE FWD FA FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED FWD F/A OTBD FLASHLIGHT AMM 25-64-00-200-802-NG-01. - [SDR SWAA2026052105198](https://openairdocs.org/sdr/SWAA2026052105198.md): Flashlight · no discrepancy · May 20, 2026 · N8693A · Boeing 7378H4 · Emergency Equipment > FA FLASHLIGHT AFT FO SIDE HOUSING LIGHT IS NOT ILLUMINATING. OPS CHECK NORMAL IAW SIP. NO FURTHER ACTION REQUIRED. - [SDR SWAA2026042090459](https://openairdocs.org/sdr/SWAA2026042090459.md): Flashlight · inoperative · Apr 17, 2026 · N8693A · Boeing 7378H4 · Emergency Equipment > AFT FA FLASHLIGHT BATTERY DEAD. R & R AFTER FA FLASLIGHT & BATTERY IAW AMM 25-64-00. - [SDR SWAA2026042091113](https://openairdocs.org/sdr/SWAA2026042091113.md): Battery · inoperative · Apr 17, 2026 · N8693A · Boeing 7378H4 · Emergency Equipment > AFT FA FLASHLIGHT BATTERY DEAD. R & R AFTER FA FLASLIGHT & BATTERY REF AMM 25-64-00. - [SDR SWAA2026010959376](https://openairdocs.org/sdr/SWAA2026010959376.md): Retainer · loose · Jan 8, 2026 · N8693A · Boeing 7378H4 · Emergency Equipment > FWD ENTRY DOOR AFT GIRT BAR RETAINER CLIP LOOSE. REMOVED AND REPLACED RIVET AT FE DOOR AFT GIRT BAR RETAINER CLIP IAW SRM 51-40-02. - [SDR SWAA2025121953349](https://openairdocs.org/sdr/SWAA2025121953349.md): Lens · missing · Dec 17, 2025 · N8693A · Boeing 7378H4 · Emergency Lighting > EXIT SIGN COVER AT FWD SERVICE DOOR MISSING. INSTALLED THE LENS IAW AMM 33-51-01. - [SDR SWAA2025090309810](https://openairdocs.org/sdr/SWAA2025090309810.md): Flashlight · inoperative · Aug 30, 2025 · N8693A · Boeing 7378H4 · Emergency Equipment > FWD AND AFT FLIGHT ATTENDANT STATION EMERGENCY FLASHLIGHTS INOP. R&R FWD AND AFT FLIGHT ATTENDANT STATION EMERGENCY FLASHLIGHT BATTERIES PER CMM 25-60-02. - [SDR SWAA2025081504794](https://openairdocs.org/sdr/SWAA2025081504794.md): Flashlight · no test · Aug 14, 2025 · N8693A · Boeing 7378H4 · Emergency Equipment > OUTBOARD FLASHLIGHT WONT TEST. R & R THE BATTERY TO FWD OTBD FLASHLIGHT IAW SIP, OPS CHECKED GOOD. - [SDR SWAA2025081199183](https://openairdocs.org/sdr/SWAA2025081199183.md): Sill Drain · odor · Aug 7, 2025 · N8693A · Boeing 7378H4 · Fuselage Main, Structure > TERRIBLE SMELL COMING FROM AFT GALLEY FLOOR DRAINS<[01] CLEANED AND FLUSHED AFT ENTRY AND AFT SERVICE DOOR SILL DRAINS REF AMM 38-31-00 - [SDR SWAA2025072494944](https://openairdocs.org/sdr/SWAA2025072494944.md): Battery · inoperative · Jul 24, 2025 · N8693A · Boeing 7378H4 · Emergency Equipment > F/A FWD EMERGENCY FLASHLIGHT, LEFT SIDE WILL NOT TEST. R & R THE BATTERY IAW AMM 25-64-00. - [SDR SWAA2025071788824](https://openairdocs.org/sdr/SWAA2025071788824.md): Battery Pack · inoperative · Jul 7, 2025 · N8693A · Boeing 7378H4 · Emergency Lighting > EMERGENCY LIGHT RT BATTERY PACK AT BS 565 IS INOPERATIVE. R & R EMERGENCY LIGHT BATTERY PACK AT BS 565 IAW MM 33-51-06. CABIN EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06. - [SDR SWAA2025071784707](https://openairdocs.org/sdr/SWAA2025071784707.md): Attach Angle · cracked · Jun 24, 2025 · N8693A · Boeing 7378H4 · Wing, Attach Fittings > LEFT WING TRAILING EDGE; ATTACH ANGLE FROM DEFLECTION CONTROL RIB TO INTERCOSTAL WEB IS CRACKED. REMOVED CRACKED ANGLE PER SRM 51-40-02.;[02] ANGLE HAS BEEN REMOVED. LOCATED; DRILLED AND DEBURRED REPLACEMENT ANGLE PER SRM 51-40-05. INSTALLED REPLACEMENT ANG - [SDR SWAA2025071784706](https://openairdocs.org/sdr/SWAA2025071784706.md): Intercostal · cracked · Jun 24, 2025 · N8693A · Boeing 7378H4 · Wing Miscellaneous Structure > L/H WING TRAILING EDGE; INTERCOSTAL WEB INBD OF DEFLECTION CONTROL RIB IS CRACKED. REMOVED AND REPLACED INTERCOSTAL WEB PER SRM 51-40-02. - [SDR SWAA2025071784705](https://openairdocs.org/sdr/SWAA2025071784705.md): Angle · cracked · Jun 24, 2025 · N8693A · Boeing 7378H4 · Wing Miscellaneous Structure > L/H WING TRAILING EDGE; ANGLE INBD OF INTERCOSTAL WEB AT DEFLECTION CONTROL RIB IS CRACKED. REMOVED CRACKED ANGLE INBD OF INTERCOSTAL WEB PER SRM 51-40-02. CRACKED ANGLE INBD OF INTERCOSTAL WEB HAS BEEN REMOVED. LOCATED; DRILLED AND DEBURRED REPLACEMENT AN - [SDR SWAA2025071684592](https://openairdocs.org/sdr/SWAA2025071684592.md): Attach Angle · cracked · Jun 23, 2025 · N8693A · Boeing 7378H4 · Fuselage Main, Attach Fittings > R/H BS 663 VAPOR BARRIER UPPER ATTACH ANGLE CRACKED AT RBL 34. FABRICATED & MATCH DRILLED REPAIR PARTS PER SRM 57-10-10-2R-5. INITIAL AREA AND FASTENER HOLES REQUIRE NDT & GVI.;[03] PERFORMED NDT PER BOEING 51-00-00 PART 6. PROCEDURE 16 WITH NO DEFECT NOTED - [SDR SWAA2025071684698](https://openairdocs.org/sdr/SWAA2025071684698.md): Attach Angle · cracked · Jun 23, 2025 · N8693A · Boeing 7378H4 · Fuselage Main, Attach Fittings > CRACK FOUND AT L/H BS 663 VAPOR BARRIER UPPER ATTACH ANGLE LBL 9. CUT OUT AND REMOVED BS 663 ATTACH ANGLE FROM APPROX LBL 18-LBL 5. ALL WORK DONE IAW SRM 57-10-10-2R-5. - [SDR SWAA2025071783852](https://openairdocs.org/sdr/SWAA2025071783852.md): Panel · pulled · Jun 20, 2025 · N8693A · Boeing 7378H4 · Wing, Plate/Skin > LH WING TRAILING EDGE PANEL 561BB HAS DAMAGED SCREW HOLES UPPER SURFACE. LOCATED AFT EDGE ROW FROM SCREWS PULLING THROUGH COMPOSITE PANEL. ACCOMPLISHED REPAIR TO AREA REF SRM 51-70-04-2R-9 PER CORRECTIVE ACTIONS 1 AND 2. RESTORED FINISH TO AREA REF AMM 51- - [SDR SWAA2025071783857](https://openairdocs.org/sdr/SWAA2025071783857.md): Panel · damaged · Jun 20, 2025 · N8693A · Boeing 7378H4 · Wing, Plate/Skin > LH WING TRAILING EDGE PANEL 561AB HAS DAMAGED SCREW HOLES UPPER SURFACE. LOCATED AFT EDGE ROW FROM SCREWS PULLING THROUGH COMPOSITE PANEL. REMOVED DAMAGE AND ACCOMPLISHED REPAIR REF SRM 51-70-04-2R-9 SEE C/A 1-4. RESTORED FINISH TO REPAIR AREA REF AMM 51-21-99 - [SDR SWAA2025071783858](https://openairdocs.org/sdr/SWAA2025071783858.md): Panel · pulled · Jun 20, 2025 · N8693A · Boeing 7378H4 · Wing, Plate/Skin > LH WING TRAILING EDGE PANEL 561CB HAS DAMAGED SCREW HOLES UPPER SURFACE. LOCATED AFT EDGE ROW FROM SCREWS PULLING THROUGH COMPOSITE PANEL. REMOVED DAMAGE AND ACCOMPLISHED REPAIR REF SRM 51-70-04-2R-9 SEE C/A 1-4. RESTORED FINISH TO REPAIR AREA REF AMM 51-21-99 - [SDR SWAA2024083031016](https://openairdocs.org/sdr/SWAA2024083031016.md): Girt Bar · out of adjust · Aug 27, 2024 · N8693A · Boeing 7378H4 · Emergency Equipment > FAS REPORT FWD ENTRY EMERG SLIDE GIRT BAR DIFFICULT TO ARM /INSERT INTO FLOOR RECEPTACLE<[01] ADJUSTED FWD ENTRY DOOR EMERGENCY SLIDE IAW AMM 25-66-01; OPS CHECK GOODS - [SDR SWAA2024081926825](https://openairdocs.org/sdr/SWAA2024081926825.md): Flashlight · inoperative · Aug 16, 2024 · N8693A · Boeing 7378H4 · Emergency Equipment > FWD GALLEY FLIGHT ATT FLASHLIGHT INOP FWD GALLEY FLIGHT ATT FLASHLIGHT INOP< - [SDR SWAA2024052989297](https://openairdocs.org/sdr/SWAA2024052989297.md): Battery Pack · inoperative · May 24, 2024 · N8693A · Boeing 7378H4 · Emergency Lighting > CABIN EMERGENCY LIGHT BATTERY PACK M2335 INOP<[01] REPLACED CABIN EMERGENCY LIGHT BATTERY PACK M2335 PER AMM 33-51-06. OPS CHECK GOOD;[02] VERIFIED. REPLACED CABIN EMERGENCY LIGHT BATTERY PACK M2335 PER AMM 33-51-06. OPS CHECK GOOD - [SDR SWAA2024052989293](https://openairdocs.org/sdr/SWAA2024052989293.md): Battery Pack · inoperative · May 23, 2024 · N8693A · Boeing 7378H4 · Emergency Lighting > CABIN EMERGENCY LIGHT BATTERY PACK M1694 INOP<[01] REPLACED CABIN EMERGENCY LIGHT BATTERY PACK AND POWER SUPPLY M1694 PER AMM 33-51-06. OPS CHECK GOOD;[02] VERIFIED. REPLACED CABIN EMERGENCY LIGHT BATTERY PACK AND POWER SUPPLY M1694 PER AMM 33-51-06. OPS CHECK - [SDR SWAA2024052989294](https://openairdocs.org/sdr/SWAA2024052989294.md): Battery Pack · inoperative · May 23, 2024 · N8693A · Boeing 7378H4 · Emergency Lighting > CABIN EMERGENCY LIGHT BATTERY PACK M1675 INOP<[01] REPLACED CABIN EMERGENCY LIGHT BATTERY PACK M1675 PER AMM 33-51-06. OPS CHECK GOOD;[02] VERIFIED. REPLACED CABIN EMERGENCY LIGHT BATTERY PACK M1675 PER AMM 33-51-06. OPS CHECK GOOD - [SDR SWAA2024052989295](https://openairdocs.org/sdr/SWAA2024052989295.md): Battery Pack · inoperative · May 23, 2024 · N8693A · Boeing 7378H4 · Emergency Lighting > CABIN EMERGENCY LIGHT BATTERY PACK M1676 INOP<[01] REPLACED CABIN EMERGENCY LIGHT BATTERY PACK M1676 PER AMM 33-51-06. OPS CHECK GOOD;[02] VERIFIED. REPLACED CABIN EMERGENCY LIGHT BATTERY PACK M1676 PER AMM 33-51-06. OPS CHECK GOOD - [SDR SWAA2024053188344](https://openairdocs.org/sdr/SWAA2024053188344.md): Web · cracked · May 21, 2024 · N8693A · Boeing 7378H4 · Wing Miscellaneous Structure > R/H WING VERTICAL WEB LOCATED JUST INBOARD OF DEFLECTION RIB AT WS 278.5 IS CRACKED AT OUTBOARD HOLE.<[01] REMOVED CRACKED VERTICAL WEB PER SRM 51-40-02. DRILLED REPLACEMENT WEB PER SRM 51-40-05.;[02] 02 - INSPECTED PER [SRM 51-40-02-0G-0-B00069 (GENERAL - FAS - [SDR SWAA2024053087383](https://openairdocs.org/sdr/SWAA2024053087383.md): Fitting · cracked · May 18, 2024 · N8693A · Boeing 7378H4 · Fuselage Miscellaneous Structure > FWD CARGO AFT CORNER THRESHOLD FITTING IS CRACKED<[01] 01 - REMOVED AND REPLACED PER [AMM 53-11-02-401-NG (CARGO DOOR SCUFF PLATE - REMOVAL/INSTALLATION - PERMANENT)];[02] 02 - INSPECTED PER [AMM 53-11-02-401-NG (CARGO DOOR SCUFF PLATE - REMOVAL/INSTALLATION - - [SDR SWAA2024053085707](https://openairdocs.org/sdr/SWAA2024053085707.md): Skin · delaminated · May 14, 2024 · N8693A · Boeing 7378H4 · Trailing Edge Flaps > L/H O/B AFT FLAP HAS DELAMINATION AT I/B LOWER CORNER LOWER SURFACE.<[01] REMOVED L/H O/B AFT FLAP ASSY. REF AMM 27-51-22;[02] INSTALLED L/H O/B AFT FLAP. REF AMM 27-51-22. PENDING ADJUSMENT CK.;[03] 02 - INSPECTED PER [AMM 27-51-22-401-NG (OUTBOARD AFT FLAP - - [SDR SWAA2024060384930](https://openairdocs.org/sdr/SWAA2024060384930.md): Fuel Panel · corroded · May 11, 2024 · N8693A · Boeing 7378H4 · Wing Main, Frame Structure > FUELING STATION PANEL AT 621GB HAS SURFACE CORROSION.<[01] REMOVED AND REPLACED FUELING PANEL PER SOPM 20-50-01 AND MM 28-41-61;[02] VERIFIED. REMOVED AND REPLACED FUELING PANEL PER SOPM 20-50-01 AND MM 28-41-61;[03] WING REFUELING PANEL INDICATORS AND LIGHTS - [SDR SWAA2024053183039](https://openairdocs.org/sdr/SWAA2024053183039.md): Floorbeam · corroded · May 6, 2024 · N8693A · Boeing 7378H4 · Fuselage Main, Floor Beam > AFT R/H LAV; O/B AFT FLOOR MOUNT AT STA 947 HAS AREA OF SURFACE CORROSION IN FLOOR BEAM. REMOVED CORROSION PER SRM 51-10-02. DAMAGE REMOVAL FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1. CUT AND REMOVED UPPER CHORD FLANGE OF STA. 947 FLOORBEAM FROM RBL - [SDR SWAA2024053083040](https://openairdocs.org/sdr/SWAA2024053083040.md): Mount · corroded · May 6, 2024 · N8693A · Boeing 7378H4 · Fuselage, Equipment Attach Fittings > AFT R/H LAV; O/B AFT MOUNT AT STA 947 HAS AREAS OF SURFACE CORROSION ON INTERCOSTAL. (MARKED)<[01] PRIOR TO BLENDING; DEPTH OF CORROSION IS.092'. REMAINING THICKNESS IS.108'. DAMAGE IS OUT OF LIMITS PER SRM 53-70-51-1A-1.;[02] LOCATED AND DRILLED NEW INTERCO - [SDR SWAA2024053083245](https://openairdocs.org/sdr/SWAA2024053083245.md): Floor Support · corroded · May 6, 2024 · N8693A · Boeing 7378H4 · Fuselage Miscellaneous Structure > INTERCOSTAL LOCATED BETWEEN STAS 947-967; RBL 24 HAS SURFACE CORROSION.<[01] REMOVED CORROSION PER SRM 51-10-02. DAMAGE REMOVAL FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1.;[02] LOCATED AND DRILLED NEW INTERCOSTAL FROM STA. 947 TO STA. 967 AT RBL 24 PER SR - [SDR SWAA2024053182762](https://openairdocs.org/sdr/SWAA2024053182762.md): Floorbeam · corroded · May 5, 2024 · N8693A · Boeing 7378H4 · Fuselage Main, Floor Beam > AFT GALLEY FLOOR STRUCTURE WET AREA AT STA 986.5 APPROXIMATELY 18' I/B OF AFT SERVICE DOOR OPENING HAS SMALL AREA OF SURFACE CORROSION ON FLOOR BEAM FASTENER HOLE. BLENDED LIGHT CORROSION PER SRM 51-10-02. REMAINING THICKNESS.140. DAMAGE REMOVAL IS OUT OF - [SDR SWAA2024053182761](https://openairdocs.org/sdr/SWAA2024053182761.md): Mount · corroded · May 5, 2024 · N8693A · Boeing 7378H4 · Fuselage, Equipment Attach Fittings > AFT L/H LAV; O/B AFT FLOOR MOUNT AT STA 947 HAS AREAS OF SURFACE CORROSION. REMOVED CORROSION IAW SRM 51-10-02. DAMAGE REMOVAL.041' OUT OF LIMITS PER SRM 53-70-51-1A-1 REMAINING THICKNESS ON 947.5 FLOORBEAM. REMOVED AFT L/H LAV; O/B AFT FLOOR MOUNT AT STA - [SDR SWAA2024053082769](https://openairdocs.org/sdr/SWAA2024053082769.md): Stringer Clip · cracked · May 5, 2024 · N8693A · Boeing 7378H4 · Fuselage Main, Attach Fittings > FWD CARGO COMPARTMENT HAS A STRINGER CLIP THAT IS CRACKED AT FRAME RIVETS; STA 500I STR 25L.<[01] REMOVED DAMAGED STRINGER CLIP REF SRM 51-40-02.;[02] REMOVED L/H SIDE BAFFLE TO FOM REF SRM 51-40-02.;[03] LOCATED AND DRILLED NEW CLIP PER SRM 51-40-02.;[04] OK - [SDR SWAA2024053082770](https://openairdocs.org/sdr/SWAA2024053082770.md): Stringer Clip · cracked · May 5, 2024 · N8693A · Boeing 7378H4 · Fuselage Main, Attach Fittings > FWD CARGO COMPARTMENT HAS A STRINGER CLIP THAT IS CRACKED AT FRAME RIVETS; STA 500I STR 25R.<[01] REMOVED RH SIDE PLATE BAFFLE AND BULKHEAD LOWER CHORD TO FOM PER SRM 51-40-02.;[02] REMOVED DAMAGED STRINGER CLIP; LOCATED AND DRILLED NEW CLIP PER SRM 51-40-02. - [SDR SWAA2024053082760](https://openairdocs.org/sdr/SWAA2024053082760.md): Mount · corroded · May 5, 2024 · N8693A · Boeing 7378H4 · Fuselage, Equipment Attach Fittings > AFT GALLEY L/H FWD FLOOR MOUNT HAS POSSIBLE LIGHT CORROSION PRESENT AROUND LOWER O/B EDGE. REMOVED DAMAGE PER SRM 51-10-02. DAMAGE FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1. MEASURES 0.010 DEEP. REMOVED L/H AFT SHEAR WEB PER SRM 51-40-02. LOCATED AN - [SDR SWAA2024053082765](https://openairdocs.org/sdr/SWAA2024053082765.md): Mount · corroded · May 5, 2024 · N8693A · Boeing 7378H4 · Fuselage, Equipment Attach Fittings > AFT R/H LAV; I/B AFT FLOOR MOUNT AT STA 947 HAS AREAS OF SURFACE CORROSION. (MARKED)<[01] REMOVED AFT R/H LAV; I/B AFT FLOOR MOUNT AT STA 947 IAW SRM 51-40-02;[02] REMOVED CORROSION ON FLOOR BEAM AT STA 947; RBL 24 PER SRM 51-10-02. DAMAGE REMOVAL FOUND TO BE - [SDR SWAA2024053082766](https://openairdocs.org/sdr/SWAA2024053082766.md): Floor Support · corroded · May 5, 2024 · N8693A · Boeing 7378H4 · Fuselage Miscellaneous Structure > AFT GALLEY FLOOR STRUCTURE SUPPORT ANGLE AT STA 986.5 +8' APPROXIMATELY 12' I/B OF AFT SERVICE DOOR OPENING HAS SMALL AREA OF SURFACE CORROSION ON FASTENER HOLE. REMOVED CORROSION PER SRM 53-70-51-1A-1. FOUND TO BE OUT OF LIMITS. BLENDED CORROSION ON AFT G - [SDR SWAA2024053182344](https://openairdocs.org/sdr/SWAA2024053182344.md): Angle · corroded · May 4, 2024 · N8693A · Boeing 7378H4 · Fuselage Miscellaneous Structure > FWD CARGO STA 500D TO 500E AT TRANSITION ANGLE ON LEFT SIDE HAS CORROSION AROUND NUT PLATE HOLES.<[01] BLENDED AREAS; REMOVED.010' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. THIS SECTION TO BE REPLACED ON NR# TTG8Q00T572F FROM STA. 480 + 10 TO - [SDR SWAA2024053182349](https://openairdocs.org/sdr/SWAA2024053182349.md): Angle · corroded · May 4, 2024 · N8693A · Boeing 7378H4 · Fuselage Miscellaneous Structure > FWD CARGO STA 500E TO 500F AT TRANSITION ANGLE ON LEFT SIDE HAS CORROSION AROUND NUT PLATE HOLES. BLENDED AREAS; REMOVED.023' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. THIS SECTION TO BE REPLACED ON NR TTG8Q00T572F FROM BS 480 + 10 TO 500E + - [SDR SWAA2024053189291](https://openairdocs.org/sdr/SWAA2024053189291.md): Rib · worn · May 4, 2024 · N8693A · Boeing 7378H4 · Wing, Rib/Bulkhead > RIGHT WING TRAILING EDGE DEFLECTION CONTROL RIB IS WORN AT 2 FASTENER HOLES. TRIMMED OFF DAMAGED UPPER TAB FROM DEFLECTION CONTROL RIB IAW SRM 51-10-02 AND SRM 57-51-02-2R-3 REPAIR 3 STEP E. REPAIRED RIGHT WING TRAILING EDGE DEFLECTION RIB PER SRM 57-51-02-2R Next page: https://openairdocs.org/aircraft/N8693A/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 = 'N8693A' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N8693A/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.