N8690A

Service difficulty reports · 91

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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 = 'N8690A' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR SWAA2026072106335Light · inoperativeCAPT. SIDE OWING EMER EXIT DOOR LIGHT INOP AFT DOOR_ OK TO CONT PER MEL 33-2-04 SP1B AUTH 329716. REPLACED LED LIGHT ASY IAW AMM 33-51-01. OPS CHKD GOOD. PLACARDS REMOVED MEL 33-2-04 CLOSED.Jul 17, 2026 · N8690A · Boeing 7378H4 · Emergency LightingSDR SWAA2026050494082Girt Bar · out of adjustAFT ENTRY DOOR SLIDE GIRT REQUIRES ADJUSTMENT (HOOK AND LOOP NOT SECURED) REMOVED, SECURED GIRT BAR HOOK AND LOOP, AND REINSTALLED IAW AMM 25-66-01. MT 725-61-06 C/W.Apr 30, 2026 · N8690A · Boeing 7378H4 · Emergency EquipmentSDR SWAA2026040987582Flashlight · failedRIGHT AFTER INBD FLASHLIGHTS DOES NOT TEST<[01] OK TO. CONT PER MEL 25-12-01 SP 1B C/W AUTHORIZATION 314060;[02] PERFORMED FUNCTIONAL TEST OF RIGHT AFT INBD FLASHLIGHT IAW AMM 25-64-00 OPS CHECK GOODApr 8, 2026 · N8690A · Boeing 7378H4 · Emergency EquipmentSDR SWAA2026031177487Flashlight · no testFWD GALLEY EMERGENCY FLASHLIGHT DOES NOT TEST. REPOSTIONED FLASHLIGHT PER S. I PMar 7, 2026 · N8690A · Boeing 7378H4 · Emergency EquipmentSDR SWAA2026011260097Engine · bird ingestionPOSSIBLE BIRDSTRIKE ON TAKEOFF SMELL OF SMOKE IN CABIN AND COCKPIT ALL ENGINE INDICATIONS NORMAL. COMPLIED WITH ODOR AND SMOKE CHECK IN CABIN AND COCKPIT PER HMM 05-51-56Jan 10, 2026 · N8690A · Boeing 7378H4 · Air Distribution SystemSDR SWAA2025103029626Battery Pack · no testTHE LT EMERGENCY LIGHTING BATTERY PACK AT ROW 20 FAILED THE CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.Oct 29, 2025 · N8690A · Boeing 7378H4 · Emergency LightingSDR SWAA2025071089669Coffeemaker · odorFO SIDE AFT COFFEE MAKER FA REPORTS BURNING SMELL WHEN ON SMELL GOES AWAY WHEN TURNED OFF<[01] R&R F/O SIDE AFT COFFEE MAKER PER AMM 25-30-01Jul 8, 2025 · N8690A · Boeing 7378H4 · Buffet/GalleysSDR SWAA2025060276501Compensator · faultyAT CRUISE NOTICED #1 FUEL TANK DECREASING RAPIDLY (1200 LB IMBALANCE). DIVERTED TO PSP. NOTICED 2 UNITS LEFT AILERON TRIM. NO OVERWEIGHT LANDING. ON POST FLIGHT INSPECTION (WITH FIRE DEPARTMENT); NO VISIBLE INDICATION OF A FUEL. FINAL IMBALANCE AT THE GAGE WASMay 30, 2025 · N8690A · Boeing 7378H4 · Fuel Quantity IndicatorSDR SWAA2025052774706Flashlight Assy · malfunctionedFWD GALLEY FLASHLIGHT INOP. INSPECTED PER AMM 25-64-00-200-802-NG-01, FLASHLIGHT CHECK WITH FLASHING OR PUSH TO TEST, LED INDICATOR. FOUND NORMAL.May 24, 2025 · N8690A · Boeing 7378H4 · Emergency EquipmentSDR SWAA2025052774059Cover · damagedAFT R/H DOOR ESCAPE SLIDE COVER IS DENTED AT FWD UPPER CORNER<[01] REMOVED DAMAGED ESCAPE SLIDE COVER AND INSTALLED SERVICEABLE COVER PER AMM 25-66-01 AND MT 725-61-06;[02] VERIFIED CORRCTIVE ACTION 1May 22, 2025 · N8690A · Boeing 7378H4 · Escape SlideSDR SWAA2025052772146Battery Pack · inoperativeALL ASSOCIATED LIGHTS FOR EMERGENCY BATTERY PACK M1670 IS INOP<[01] AFTER DEEP CYCLE CHARGE FOUND ALL ASSOCIATED LIGHTS FOR EMERGENCY BATTERY PACK M1670 TESTED GOOD IAW AMM 33-51-06-600-802; AMM 33-51-06-610-802 AND WDM 33-51-13 PG.15 SH.2;[02] CORRECTIVE ACTIMay 18, 2025 · N8690A · Boeing 7378H4 · Emergency LightingSDR SWAA2025052771085Seal · crackedLT. HORIZONTAL STAB L/E UPPER FWD SLIDE SEAL CRACKED.<[01] REMOVED AND REPLACED R/H HORIZONTAL STAB SLIDE SEAL IAW AMM 53-31-31/401;[02] TASK C/WMay 14, 2025 · N8690A · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2025052771084Seal · crackedRT. HORIZONTAL STAB L/E FWD UPPER SLIDE SEAL CRACKED.<[01] REMOVED AND REPLACED R/H HORIZONTAL STAB SLIDE SEAL IAW AMM 53-31-31/401;[02] TASK C/WMay 14, 2025 · N8690A · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2025052770750Floor Panel · pulledFLOOR PANEL 241AF HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241AF WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL PER SRM 53-00-50-2R-0 DUE TO AMOUNT OF ALL DAMAGE.May 13, 2025 · N8690A · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2025052770755Floor Panel · pulledFLOOR PANEL 232SF HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 232SF WITH AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.May 13, 2025 · N8690A · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2025052770134Floorbeam · cracked540 BREAK PANEL IS CRACKED AT RBL 1; WL 208.<[01] REMOVED AND REPLACED BS-540 BREAK PANEL RBL-1 TO RBL-25; WL-208 IAW SRM 51-40-02-0G-0 AND DWG#143A5240May 13, 2025 · N8690A · Boeing 7378H4 · Fuselage Main, Floor BeamSDR SWAA2025052770135Floorbeam · cracked540 BREAK PANEL IS CRACKED AT LBL 1; WL 208.<[01] REMOVED AND REPLACED BS-540 BREAK PANEL LBL-1 TOLBL-25; WL-208 IAW SRM 51-40-02-0G-0 AND DWG#143A5240May 13, 2025 · N8690A · Boeing 7378H4 · Fuselage Main, Floor BeamSDR SWAA2025052770756Floor Panel · pulledFLOOR PANEL 241CF HAS AREAS OF PULLED STRANDS. CORRECT PANEL NUMBER IS 241EF.<[01] FLOOR PANEL 241EF WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL PER SRM 53-00-50-2R-0 DUE TO AMOUNT OF ALL DAMAGE.May 13, 2025 · N8690A · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2025052770865Panel · crackedLT WING TRAILING EDGE SPANWISE PANEL BETWEEN SPOILER PANELS 5 AND 6 CRACKED IN UPPER RADIUS. (PN 115A2512-29)<[01] REMOVED AND REPLACED ANGLE P/N 115A2156-7 IAW SRM 51-40-02 AND AIPC 57-50-00-36A;[02] CORRECTIVE ACTION COMPLETED.May 13, 2025 · N8690A · Boeing 7378H4 · SpoilersSDR SWAA2025032408177Flashlight · inoperativeFA FWD JUMP SEAT FLASHLIGHT INOP <[01]. RESEATED FWD FA FLASHLIGHT IN CRADLE PER SIP. OPS CHECKS GOOD.Mar 20, 2025 · N8690A · Boeing 7378H4 · Emergency EquipmentSDR SWAA2025011686657Lamp · inoperativeL2 EXTERIOR EMERGENCY LIGHT INOP.<[01] RELAMPED L2 EMERGENCY EXIT LIGHT. OPS CHECK GOOD. ALL WORK PERFORMED PER AMM 33-51-04.Jan 16, 2025 · N8690A · Boeing 7378H4 · Emergency LightingSDR SWAA2025010382394Light · brokenFWD EMERGENCY FO SIDE LIGHT ASSEMBLY BROKEN<[01] R&R EMERGENCY EXIT LIGHT ASSEMBLY OVER WING RH FWD SIDEWALL. OPS CK GOOD PER AMM 33-51-01.Jan 1, 2025 · N8690A · Boeing 7378H4 · Emergency LightingSDR SWAA2024091637771Trim Motor · faultySTABILIZER TRIM INOP<[01] T/S PER FIM 22-15 TASK 821. CYCLED C/B & FAULT WAS INTERMITTENT. PER MOC REQUEST; R&R STAB TRIM MOTOR PER AMM 27-41-71. OPS CHECK GOODSep 14, 2024 · N8690A · Boeing 7378H4 · Stabilizer Control SystemSDR SWAA2024090333182Battery · inoperativeFLIGHT ATTENDANT FORWARD FLASHLIGHT INOP<[01] OK FOR CONTINUE SERVICE PERMEL 25-12-01 SP1B;[02] REMOVED AND REPLACED BATTERY FOR FA FWD FLASHLIGHT PER AMM 25-64-00.Aug 30, 2024 · N8690A · Boeing 7378H4 · Emergency EquipmentSDR SWAA2024061301239Flashlight · failedFLIGHT ATTENDANT FORWARD JUMPSEAT FLASHLIGHT PRESS TO TEST BUTTON NOT WORKING.<[01] PROPERLY POSITIONED FLASHLIGHT IN HOLDER AND OPS CK GOOD PER AMM 25-64-00.Jun 12, 2024 · N8690A · Boeing 7378H4 · Emergency EquipmentSDR SWAA2024060698227Battery Pack · inoperativeFWD O/W EMERGENCY EXIT LIGHTS INOP ON LEFT SIDE<[01] REPLACED EMERGENCY BATTERIES PACK; M1675 PERFORMED GOOD TEST PER AMM 33-51-06-960-805;[02] VERIFIED CORRECTIVE ACTION COMPLETE.<BR>VERIFIED MEASUREMENT TABLE.Jun 4, 2024 · N8690A · Boeing 7378H4 · Emergency LightingSDR SWAA2024060698229Battery Pack · inoperativeCEILING EMERGENCY EXIT LIGHTS; SEVERAL LIGHTS INOP.<[01] REPLACED EMERGENCY BATTERIES PACK; M1672; M1673; PERFORMED GOOD TEST PER AMM 33-51-06-960-805;[02] VERIFIED CORRECTIVE ACTION COMPLETE.<BR>VERIFIED MEASUREMENT TABLE.Jun 4, 2024 · N8690A · Boeing 7378H4 · Emergency LightingSDR SWAA2024060698842Battery Pack · inoperativeCEILING EMERGENCY EXIT LIGHTS; SEVERAL LIGHTS INOP.<[01] REPLACED EMERGENCY BATTERIES PACK; M1672; M1673; PERFORMED GOOD TEST PER AMM 33-51-06-960-805;[02] VERIFIED CORRECTIVE ACTION COMPLETE.<BR>VERIFIED MEASUREMENT TABLE.Jun 4, 2024 · N8690A · Boeing 7378H4 · Emergency LightingSDR SWAA2024060698228Battery Pack · inoperativeO/W FWD AND AFT EMERGENCY EXIT LIGHTS INOP ON RT SIDE<[01] REPLACED EMERGENCY BATTERIES PACK; M1674; PERFORMED GOOD TEST PER AMM 33-51-06-960-805;[02] VERIFIED CORRECTIVE ACTION COMPLETE.<BR>VERIFIED MEASUREMENT TABLE.Jun 4, 2024 · N8690A · Boeing 7378H4 · Emergency LightingSDR SWAA2024060697838Connector · disconnectedDURING FWD CABIN RESTORATION; FOUND FWD GALLEY DOORWAY EMERGENCY EXIT SIGNS; UPPER AND LOWER; INOP.<[01] FOUND CONNECTOR D14812 NOT PROPERLY SEATED. RE-SEATED CONNECTOR PER AMM 33-51-06-960-806. STEP 5.E.(4).(F) OPS CHECK GOOD.<BR><BR>CARD COMPLETE.;[02] VERIFJun 3, 2024 · N8690A · Boeing 7378H4 · Light System WiringSDR SWAA2024060684064Floorbeam · damagedELONGATED HOLE IN FWD FLANGE OF BS 887 FLOOR BEAM; RBL 4; WL 208. DAMAGE WAS FOUND TO A FLOOR PANEL ATTACH HOLE IN THE FWD FLANGE OF THE BS 887 FLOOR BEAM (146A5518-7#C) AT RBL 4. THE DAMAGE WAS REMOVED BY OVERSIZING THE HOLE. THERE ARE NO ALLOWABLE DAMAGE LIMay 9, 2024 · N8690A · Boeing 7378H4 · Fuselage Main, Floor BeamSDR SWAA2024060683900Floorbeam · corrodedCORROSION AROUND FITTING ON FLOOR BEAM BS 947; RBL 50 (MARKED)<[01] REMOVED DAMAGE ON BS 947 RBL 50 FLOOR BEAM UPPER SURFACE IN AN AREA OF 1'X 1'; ORIGINAL THICKNESS IS 0.180' REMAINING THICKNESS IS 0.100' CORROSION FOUND TO BE OUT OF LIMITS I.A.W SRM 53-70-51May 9, 2024 · N8690A · Boeing 7378H4 · Fuselage Main, Floor BeamSDR SWAA2024060683901Floorbeam · corrodedCORROSION AROUND FITTING ON FLOOR BEAM BS 947; LBL 25 (MARKED)<[01] REMOVED DAMAGE ON BS 947 LBL 25 FLOOR BEAM UPPER SURFACE IN AN AREA OF 1'X 1'; ORIGINAL THICKNESS IS 0.180' REMAINING THICKNESS IS 0.105' CORROSION FOUND TO BE OUT OF LIMITS I.A.W SRM 53-70-51May 9, 2024 · N8690A · Boeing 7378H4 · Fuselage Main, Floor BeamSDR SWAA2024060683904Floorbeam · corrodedCORROSION AROUND FITTING ON FLOOR BEAM BS 947; LBL 50 (MARKED)<[01] REMOVED DAMAGE ON BS 947 LBL 50 FLOOR BEAM UPPER SURFACE IN AN AREA OF 1'X 1'; ORIGINAL THICKNESS IS 0.180' REMAINING THICKNESS IS 0.100' CORROSION FOUND TO BE OUT OF LIMITS I.A.W SRM 53-70-51May 9, 2024 · N8690A · Boeing 7378H4 · Fuselage Main, Floor BeamSDR SWAA2024060684067Floor Support · corrodedCORROSION ON FLOOR SUPPORT AT BS 947 RBL 50 WL 208<[01] REMOVED DAMAGE ON BS 947-967 RBL 50 FLOOR SUPPORT UPPER SURFACE IN AN AREA OF 1'X 1'; ORIGINAL THICKNESS IS 0.205' REMAINING THICKNESS IS 0.130' CORROSION FOUND TO BE OUT OF LIMITS I.A.W SRM 53-70-51-1A-1May 9, 2024 · N8690A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024060683902Floor Support · corrodedCORROSION AROUND FITTING ON FLOOR SUPPORT BS 947+3; LBL 50 (MARKED)<[01] REMOVED DAMAGE ON BS 947-967 LBL 50 FLOOR SUPPORT UPPER SURFACE IN AN AREA OF 1'X 1'; ORIGINAL THICKNESS IS 0.205' REMAINING THICKNESS IS 0.105' CORROSION FOUND TO BE OUT OF LIMITS I.A.W May 9, 2024 · N8690A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024060783884Attach Angle · corrodedFWD SERVICE DOOR MOPSILL THRESHOLD ATTACH ANGLE HAS CORROSION AT BS 305; 310; 315; 319 RBL 61 WL 208. INSTALLED NEW FWD SERVICE DOOR MOPSILL THRESHOLD ATTACH ANGLE AT BS 319 RBL 61 WL 208 IAW SRM 51-40-02; DOCUMENT NUMBER:141A8310 TYPE: DWG 0046 REV - & DOCUMay 8, 2024 · N8690A · Boeing 7378H4 · Fuselage Main, Attach FittingsSDR SWAA2024060783886Attach Angle · corrodedCORROSION ON FED MOPSILL THRESHOLD ATTACH ANGLE AT BS 340 LBL 63 WL 208.May 8, 2024 · N8690A · Boeing 7378H4 · Fuselage Main, Attach FittingsSDR SWAA2024060683588Floor Panel · pulledAFT FLOOR PANEL 241XF UPPER SKIN HAS AN AREA OF PULLED STRANDS. (MARKED)<[01] AFT FLOOR PANEL 241XF UPPER SKIN AREA OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION #1May 8, 2024 · N8690A · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2024060683601Support · brokenAFT CARGO BAY FORWARD BULKHEAD FLOOR TO BULKHEAD SUPPORT IS BROKE BS 727+4 LBL 10 TO RBL 10 WL156<[01] IF REPAIR REFERENCE 25-52-10-400-801-NG-01 WAS ORIGINALLY SELECTED BUT IS NO LONGER REQUIRED TO SIGN OFF THE FAULT; MARK THIS STEP AS N/A.<BR>RECEIVED NEW AFMay 8, 2024 · N8690A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024060683593Floor Panel · damagedFWD FLOOR PANEL 221BF O/B AFT CORNER TANG IS MISSING.<[01] FLOOR PANEL 221BF AFT CORNER TANG HAS BEEN REPAIRED IAW SRM 53-00-50-2R-6.May 8, 2024 · N8690A · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2024060683882Channel · crackedFWD ENTRY DOOR MOPSILL IS CRACKED AT BS 303 LBL 57 WL 208<[01] REMOVED AND REPLACED FWD ENTRY MOPSILL IAW SRM 51-40-02-0G-0 AND DWG 140A9810;[02] VERIFIED CORRECTIVE ACTION 1May 8, 2024 · N8690A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024061083267Panel · debondedR/H; AFT AWE; HEADER PANEL FWD SIDE BOTTOM CLIP IS DISBONDED<[01] CORRECTTION SHOULD BE (R/H; AFT OWE; HEADER PANEL FWD SIDE BOTTOM CLIP IS DISBONED);[02] BONDED R/H AFT OVERWING EXIT FWD SIDE BOTTOM CLIP PER SOPM 20-50-12 TYPE 89 & REFERENCE BOEING DRAWING 41May 7, 2024 · N8690A · Boeing 7378H4 · Fuselage Main, StructureSDR SWAA2024060683586Scuff Plate · crackedFORWARD CARGO BAY FWD CORNER SCUFF PLATE IS CRACKED. REPAIRED FWD CARGO BAY FWD CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1.May 7, 2024 · N8690A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024060683587Scuff Plate · crackedAFT CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED. REPAIRED AFT CARGO BAY AFT CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1.May 7, 2024 · N8690A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024060683583Web · corrodedCORROSION FWD CARGO BAY SUB THRESHOLD WEB MULTIPLE AREAS AROUND NUT PLATE HOLES BS440+5' TO BS490' RBL 26 WL156<[01] REMOVED DAMAGED SUB THRESHOLD WEB; LOCATED; DRILLED AND INSTALLED NEW FWD CARGO SUB THRESHOLD WEB PER SRM 51-40-02-0G; SRM 51-40-05-0G-0 AND DWMay 7, 2024 · N8690A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024060683584Web · corrodedCORROSION AFT CARGO BAY SUB THRESHOLD WEB MULTIPLE AREAS AROUND NUT PLATE HOLES BS794 TO BS847 RBL 26 WL156<[01] REMOVED DAMAGED SUB THRESHOLD WEB. LOCATED; DRILLED AND INSTALLED NEW ACB SUB THRESHOLD WEB PER SRM 51-40-02-0G; SRM 51-40-05-0G-0 AND DWG 146A8340May 7, 2024 · N8690A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024060683594Support Plate · corrodedCORROSION AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS727H+19' TO BS787+1' LBL22 WL156<[01] REMOVED DAMAGED SECTION OF FLOOR TO SIDEWALL SUPPORT; FABRICATED; AND INSTALLED FROM BS727H+11' TO BS787+13' IAW SRM 53-00May 7, 2024 · N8690A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024060683585Sidewall Support · corrodedCORROSION AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS AROUND NUT PLATE HOLES BS727C TO BS767 RBL22 WL156<[01] CORROSION ON SUPPORT WAS FOUND TO BE OUT OF LIMITS REMOVED AND REPLACED SUPPORT AS PER SRM 51-40-02 AND DRAWING 146A7500.;[02May 7, 2024 · N8690A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024030457919Power Supply · inoperativeAFT LH EMERGENCY POWER SUPPLY INOP<[01] R/R<BR>01 - REMOVED AND REPLACED PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)]Mar 1, 2024 · N8690A · Boeing 7378H4 · Emergency Lighting
Back to N8690A