N8507C

Service difficulty reports · 77

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 = 'N8507C' 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 SWAA2025112036435Sign · inoperativeRIGHT EMERGENCY SIGN ABOVE OVERWING EMERGENCY DOORS INOPERATIVE. REMOVED AND REPLACED M1695 EMERGENCY EXIT LIGHT BATTERY PACK REF AMM 33-51-06. OPS CHECKED GOOD.Nov 18, 2025 · N8507C · Boeing 7378H4 · Emergency LightingSDR SWAA2025112036434Battery Pack · inoperativeLEFT EMERGENCY SIGN ABOVE OVERWING EMERGENCY DOORS INOPERATIVE. REMOVED AND REPLACED IAW AMM 33-51-06-960-805-NG.Nov 18, 2025 · N8507C · Boeing 7378H4 · Emergency LightingSDR SWAA2025112033159Bracket · crackedL/H WING: PANEL 551FB DUAL NUT PLATE BRACKET IS CRACKED. BRACKET IS ON THE FWD EDGE OF PANEL; JUST INBD OF THE GREEN TEE ANGLE. REMOVED AND REPLACED PANEL 551FB DUAL NUT PLATE BRACKET IAW SRM 51-40-02.Nov 8, 2025 · N8507C · Boeing 7378H4 · Trailing Edge FlapsSDR SWAA2025112030269Seat Track · crackedSEAT TRACK NR 4 ATTACH BRACKET CRACKED ON BOTH INBD & OTBD RADII BS 727B UNDER FLOORBOARD 242DF. HFEC VERIFIED THE ATTACHED BRACKET IS CRACKED IAW NDT PART 6; 51-00-00 PROCEDURE 23. REMOVED AND REPLACED SPLICE STRAP BRACKET IAW SRM 51-10-02, AND SRM 51-40Oct 30, 2025 · N8507C · Boeing 7378H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2025112030268Attach Bracket · crackedSEAT TRACK NR 1 ATTACH BRACKET CRACKED ON BOTH INBD & OTBD RADII AT BS 727B UNDER FLOORBOARD 241FF. HFEC VERIFIED THE ATTACHED BRACKET IS CRACKED AT BOTH LOCATIONS IAW NDT PART 6; 51-00-00, PROCEDURE 23. REMOVED DAMAGED SPLICE STRAP BRACKET AT BS 727B, LBLOct 30, 2025 · N8507C · Boeing 7378H4 · Fuselage Main, Attach FittingsSDR SWAA2025112029386Attach Angle · crackedCRACK FOUND ON BS 663 LT ATTACH ANGLE, LBL 34. REMOVED TANK FASTENERS FROM LBL 34 TO LBL 65. CUT AND REMOVED DAMAGED SECTION OF ATTACH ANGLE IAW SRM 57-10-10-2R-5. CW NDT INSPECTIONS OF HOLES COMMON TO REPAIR IAW PART 6 51-00-00. PROCEDURE 16, AND PERFORMOct 28, 2025 · N8507C · Boeing 7378H4 · Fuselage Main, Attach FittingsSDR SWAA2025112029387Attach Angle · crackedCRACK FOUND ON BS 663 RT ATTACH ANGLE, RBL 34. REMOVED DAMAGED SECTION OF RT STA 663 ATTACH ANGLE FROM APPROX RBL 24 TO RBL 65. COMPLIED WITH STEP 2, COMPLIED WITH REMAINING FASTENER HOLE INSPECTION AT REPAIR HOLES IAW NDT PART 6 51-00-00, PROCEDURE 16. NO Oct 28, 2025 · N8507C · Boeing 7378H4 · Fuselage Main, Attach FittingsSDR SWAA2025112029497Stiffener · crackedNR 2 ENGINE OTBD FAN COWL 424AR, SHELF STIFFENER CRACKED. REMOVED AND REPLACED STIFFENER IAW SRM 51-40-02.Oct 28, 2025 · N8507C · Boeing 7378H4 · Nacelle/Pylon, Main FrameSDR SWAA2025112028732Support Angle · crackedLEFT WING TRAILING EDGE SHELF PANEL AT MAIN FLAP DEFLECTION ROLLER ARM HAS A CRACK IN LATERAL SUPPORT. LOCATED AND DRILLED REPLACEMENT SUPPORT ANGLE IAW SRM 51-40-05.Oct 26, 2025 · N8507C · Boeing 7378H4 · Trailing Edge FlapsSDR SWAA2025102125660Flashlight · inoperativeAFT CABIN GALLEY 1 FLASHLIGHT TEST INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT BATTERY IAW AMM 25-64-00. OPS CHECK GOOD.Oct 18, 2025 · N8507C · Boeing 7378H4 · Emergency EquipmentSDR SWAA2025101523874Flashlight · unsecureAFT FLASHLIGHT NOT BLINKING. FOUND AFT RT INBD FLASHLIGHT NOT PROPERLY SECURED. REINSTALLED IAW AMM 25-64-00. OPS CHECKED GOOD.Oct 12, 2025 · N8507C · Boeing 7378H4 · Emergency EquipmentSDR SWAA2025022598706Lamp · contaminatedAFT PAX DOOR EXTERIOR SLIDE EMERGENCY LIGHT INOP <[01]. RELAMPED AFT PAX DOOR EXTERIOR SLIDE EMERGENCY LIGHT IAW AMM 33-51-04. NO FIX. LIGHT REMAINS INOP.;[02] FOUND AFT LH EXIT DOOR EMERGENCY LIGHT CONTAMINATED WITH DE-ICING FLUID. CLEANED PER SOPM 20-30-03.Feb 23, 2025 · N8507C · Boeing 7378H4 · Emergency LightingSDR SWAA2025022598705Lamp · inoperativeFWD PAX DOOR EXTERIOR SLIDE EMERGENCY LIGHT INOP <[01]. RELAMPED FWD PAX DOOR EXTERIOR SLIDE EMERGENCY LIGHT IAW AMM 33-51-04. OPS CHECK GOOD @ THIS TIME.Feb 23, 2025 · N8507C · Boeing 7378H4 · Emergency LightingSDR SWAA2024102244233Stringer Clip · crackedFWD CARGO STRINGER CLIP AT STA 500I - STRINGER 25L CRACKED AT FASTENER HOLE<[01] REMOVED FWD CARGO STRINGER CLIP AT STA 500I - STRINGER 25L PER SRM 51-40-02.;[02] LOCATED AND DRILLED NEW CLIP PER SRM 51-40-02.;[03] INSTALLED NEW STRINGER CLIP PER SRM 51-40-02.Oct 2, 2024 · N8507C · Boeing 7378H4 · Fuselage Main, Attach FittingsSDR SWAA2024102244224Floor Support · crackedPASSENGER CABIN FLOOR STRUCTURE STA 540 LBL 3 FLOOR SUPPORT INTERCOSTAL CRACKED.<[01] REMOVED AND REPLACED PASSENGER CABIN FLOOR INTERCOSTAL AT STA. 540; FROM LBL 1' TO LBL 24' PER SRM 51-40-02.;[02] INSPECTED WORK ABOVEOct 1, 2024 · N8507C · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024102244225Floor Support · crackedPASSENGER CABIN FLOOR STRUCTURE STA 540 RBL 3 FLOOR SUPPORT INTERCOSTAL CRACKED.<[01] REMOVED AND REPLACED PASSENGER CABIN FLOOR INTERCOSTAL AT STA. 540; FROM RBL 1' TO RBL 24' PER SRM 51-40-02.;[02] INSPECTED WORK ABOVEOct 1, 2024 · N8507C · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024102243864Support Angle · corrodedFLOOR WALL SUPPORT ANGLE ON AFT L/H SIDE AT 986.5+6 LBL 43 IS CORRODED. FLOOR WALL SUPPORT ANGLE ON AFT L/H SIDE CORRODED.<[01] REMOVED ANGLE SUPPORT PER SRM 51-40-02.;[02] REMOVED L/H AFT FLOOR WALL ANGLE PER SRM 51-40-02.;[03] INSTALLED NEW SUPPOR IAW SRM 51Sep 30, 2024 · N8507C · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024102243638Access Door · crackedENG.COWL 414; ACCESS HOLE FOR OIL ACCESS DOOR 414AR; INSIDE WEB CRACKED.<[01] REPLACED COWL 414 ASSY SEE TTG8Q00S5HR7 FOR WORK ACCOMLISHED.;[02] VERIFIED REPLACEMENTSep 30, 2024 · N8507C · Boeing 7378H4 · Nacelle/Pylon Miscellaneous StructureSDR SWAA2024102243202Angle · out of limitsR/H TRANSITION ANGLE REQUIRES REPLACEMENT BETWEEN STA 727 TO STA 767 DUE TO SEVERAL AREAS OUT OF LIMITS.<[01] REMOVED RH TRANSITION ANGLE FORM STA 727 TO 847 PER SRM 51-40-02<BR>LOCATED AND DRILLED NEW RH TRANSITION ANGLE FORM STA 727 TO 847 PER SRM 51-40-02;[Sep 29, 2024 · N8507C · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024102243201Angle · corrodedL/H TRANSITION ANGLE STA 767 TO STA 787 HAS NUMEROUS AREAS OF CORROSION.<[01] REMOVED SURFACE CORROSION AT R/H TRANSITION ANGLE FROM STA. 767 -787. MATERIAL REMOVED .010 AND REMAINING THICKNESS .035 FOUND TO BE OUT OF LIMITED PER SRM 53-00-53-1A-2.;[02] ENTER Sep 29, 2024 · N8507C · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024102243200Angle · out of limitsL/H TRANSITION ANGLE REQUIRES REPLACEMENT BETWEEN STA 727 TO STA 847 DUE TO SEVERAL AREAS OUT OF LIMITS.<[01] REMOVED LH TRANSITION ANGLE FORM STA 727 TO 847 PER SRM 51-40-02;[02] LOCATED AND DRILLED NEW LH TRANSITION ANGLE FORM STA 727 TO 847 PER SRM 51-40-02Sep 29, 2024 · N8507C · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024102243217Floorbeam · corrodedAFT GALLEY WET AREA STRUCTURE HAS LIGHT CORROSION AROUND FASTENER HOLE STA 986.5 LBL 43.<[01] BLENDED OUT DAMAGE PER SRM 53-70-51. ORIGINAL METAL THICKNESS IS .156. REMAINING MATERIAL AFTER DAMAGE REMOVAL .114. DAMAGE OUT OF LIMITS AND REQUIRES REPAIR.;[02] CUSep 29, 2024 · N8507C · Boeing 7378H4 · Fuselage Main, Floor BeamSDR SWAA2024102242920Angle · out of limitsR/H TRANSITION ANGLE REQUIRES REPLACEMENT BETWEEN STA 500A THRU STA 500I DUE TO SEVERAL AREAS OUT OF LIMITS<[01] REMOVED R/H TRANSITION ANGLE FROM STA 500A TO 500I.;[02] DRILLED AND LOCATED HOLES ON NEW TRANSITION ANGLE PER SRM 51-40-05;[03] INSPECTED AS REQUISep 28, 2024 · N8507C · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024102242918Angle · corrodedFWD CABIN WET AREA STRUCTURE HAS LIGHT CORROSION AROUND FASTENER HOLES OF ZEE ANGLE AT FWD SERVICE DOOR STA 294 TO STA 328. RBL 56.<[01] REMOVED CORROSION PER SRM 51-10-02. MAX MATERIAL REMOVED 0.016?. DAMAGE REMOVAL IS OUT OF LIMITS PER SRM 53-10-15-1A-2.;[02Sep 28, 2024 · N8507C · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024102242904Angle · corrodedAFT CARGO; SURFACE CORROSION; LH TRANS. ANGLE STA. 727I TO 727J.<[01] REMOVED SURFACE CORROSION AT L/H TRANSITION ANGLE FROM STA. 727I-727J. MATERIAL REMOVED .005 AND REMAINING THICKNESS .035 FOUND TO BE OUT OF LIMITED PER SRM 53-00-53-1A-2.<BR>SEE WORK CAPTURSep 27, 2024 · N8507C · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024102242900Angle · corrodedAFT CARGO; SURFACE CORROSION; RH TRANS. ANGLE STA. 747 TO 767<[01] REMOVED LIGHT SURFACE CORROSION AT R/H TRANSITION ANGLE FROM STA. 747-767. MATERIAL REMOVED .005 AND REMAINING THICKNESS .035 FOUND TO BE OUT OF LIMITED PER SRM 53-00-53-1A-2.;[02] SEE WORK CAPSep 27, 2024 · N8507C · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024102242909Angle · corrodedAFT CARGO; SURFACE CORROSION; RH TRANS. ANGLE STA. 727G TO 727H<[01] REMOVED LIGHT SURFACE CORROSION AT R/H TRANSITION ANGLE FROM STA. 727G-727H. MATERIAL REMOVED .005 AND REMAINING THICKNESS .035 FOUND TO BE OUT OF LIMITED PER SRM 53-00-53-1A-2.;[02] SEE WORKSep 27, 2024 · N8507C · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024102242898Angle · corrodedAFT CARGO; SURFACE CORROSION; RH TRANS. ANGLE STA. 727H TO 727I<[01] REMOVED SURFACE CORROSION AT R/H TRANSITION ANGLE FROM STA. 727H-727I. MATERIAL REMOVED .005 AND REMAINING THICKNESS .035 FOUND TO BE OUT OF LIMITED PER SRM 53-00-53-1A-2.;[02] SEE WORK CAPTUSep 27, 2024 · N8507C · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024102242899Angle · corrodedAFT CARGO; SURFACE CORROSION; RH TRANS. ANGLE STA. 727J TO 747<[01] REMOVED LIGHT SURFACE CORROSION AT R/H TRANSITION ANGLE FROM STA. 727J-747. MATERIAL REMOVED .005 AND REMAINING THICKNESS .035 FOUND TO BE OUT OF LIMITED PER SRM 53-00-53-1A-2.;[02] SEE WORK CSep 27, 2024 · N8507C · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024102242906Angle · corrodedAFT CARGO; SURFACE CORROSION; RH TRANS. ANGLE STA. 747 TO 767<[01] THIS WORK CAPTURE IS A DUPLICATED FORM WORK CAPTURE # TTG8Q00W429A<BR><BR>SEE WORK CAPTURE # TTG8Q00W4YYT FOR REPLACEMENT OF NEW RH TRANSITION ANGLE FROM STA 727 TO 767;[02] INSPECTED WORK ABOVSep 27, 2024 · N8507C · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024102242283Angle · corrodedFWD CARGO L/H TRANSITION ANGLE CORROSION BETWEEN STA 500E AND 500D<[01] BLENDED AREAS; REMOVED .007' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] 02 - INSPECTED PER [SRM 53-00-53-1A-2-B00297 (PERMANENT (NON-DENT DAMAGE TYPES))];[03] REMOVED Sep 26, 2024 · N8507C · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024102242273Angle · corrodedFWD CARGO R/H TRANSITION ANGLE CORROSION BETWEEN STA 500I AND 500H<[01] REMOVED CORROSION PER SRM 53-00-53-1A-2 FOUND TO BE WITHIN LIMITS . TRANSITION ANGLE TO BE REPLACED. REFERENCE TTG8Q00W4L4E DUE TO THE TRANSITION ANGLE BEING PART OF TRANSITION ANGLE STA 5Sep 26, 2024 · N8507C · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024102242276Angle · corrodedFWD CARGO R/H TRANSITION ANGLE CORROSION BETWEEN STA 500G AND 500F<[01] REMOVED CORROSION PER SRM 53-00-53-1A-2 FOUND TO BE WITHIN LIMITS . TRANSITION ANGLE TO BE REPLACED. REFERENCE TTG8Q00W4L4E DUE TO THE TRANSITION ANGLE BEING PART OF TRANSITION ANGLE STA 5Sep 26, 2024 · N8507C · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024102242282Angle · corrodedFWD CARGO R/H TRANSITION ANGLE CORROSION BETWEEN STA 500E AND 500D<[01] REMOVED CORROSION PER SRM 53-00-53-1A-2 FOUND TO BE WITHIN LIMITS . TRANSITION ANGLE TO BE REPLACED. REFERENCE TTG8Q00W4L4E DUE TO THE TRANSITION ANGLE BEING PART OF TRANSITION ANGLE STA 5Sep 26, 2024 · N8507C · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024102242284Angle · corrodedFWD CARGO R/H TRANSITION ANGLE CORROSION BETWEEN STA 500D AND 500C<[01] REMOVED CORROSION PER SRM 53-00-53-1A-2 FOUND TO BE WITHIN LIMITS . TRANSITION ANGLE TO BE REPLACED. REFERENCE TTG8Q00W4L4E DUE TO THE TRANSITION ANGLE BEING PART OF TRANSITION ANGLE STA 5Sep 26, 2024 · N8507C · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024102242289Angle · corrodedFWD CARGO R/H TRANSITION ANGLE CORROSION BETWEEN STA 500C AND 500B<[01] REMOVED CORROSION PER SRM 53-00-53-1A-2 FOUND TO BE WITHIN LIMITS . TRANSITION ANGLE TO BE REPLACED. REFERENCE TTG8Q00W4L4E DUE TO THE TRANSITION ANGLE BEING PART OF TRANSITION ANGLE STA 5Sep 26, 2024 · N8507C · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024102242294Stringer Clip · crackedFWD CARGO STRINGER CLIP AT STA 500I - STRINGER 25R CRACKED AT FASTENER HOLE<[01] REMOVED FWD CARGO STRINGER CLIP AT STA 500I - STRINGER 25R PER SRM 51-40-02;[02] REMOVED AND REPLACED FWD CARGO STRINGER CLIP AT STA 500I - STRINGER 25R PER SRM 51-10-02 AND SRM 5Sep 26, 2024 · N8507C · Boeing 7378H4 · Fuselage Main, Attach FittingsSDR SWAA2024102242583Angle · corrodedFWD CARGO R/H TRANSITION ANGLE CORROSION STA 500-480<[01] REMOVED CORROSION PER SRM 53-00-53-1A-2 FOUND TO BE WITHIN LIMITS . TRANSITION ANGLE TO BE REPLACED. REFERENCE TTG8Q00W371U DUE TO THE TRANSITION ANGLE BEING PART OF TRANSITION ANGLE STA 500 THRU 500A;[Sep 26, 2024 · N8507C · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024102242292Angle · corrodedFWD CARGO R/H TRANSITION ANGLE CORROSION BETWEEN STA 500A AND 500<[01] REMOVED CORROSION DAMAGE PER SRM 53-00-53-1A-2;[02] REMOVED CORROSION DAMAGE PER SRM 53-00-53-1A-2 FOUND TO BE OUT OF LIMITS ; TRANSITION ANGLE REQUIRES REPLACMENT BETWENN STA 480 THRU 500ASep 26, 2024 · N8507C · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024102242290Angle · corrodedFWD CARGO R/H TRANSITION ANGLE CORROSION BETWEEN STA 500B AND 500A<[01] REMOVED CORROSION PER SRM 53-00-53-1A-2. FOUND TO BE OUT OF LIMITS TRANSITION ANGLE REQUIRES REPLACEMENT BETWEEN STA 500A THRU STA 500B;[02] CORRECT PART NUMBER FOR TRANSITION ANGLE 143A75Sep 26, 2024 · N8507C · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024102242278Angle · corrodedFWD CARGO R/H TRANSITION ANGLE CORROSION BETWEEN STA 500F AND 500E<[01] REMOVED CORROSION PER SRM 53-00-53-1A-2 FOUND TO BE OUT OF LIMITS . TRANSITION ANGLE TO BE REPLACED. REFERENCE TTG8Q00W4L4E DUE TO THE TRANSITION ANGLE BEING PART OF TRANSITION ANGLE STA 5Sep 26, 2024 · N8507C · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024102242275Angle · corrodedFWD CARGO R/H TRANSITION ANGLE CORROSION BETWEEN STA 500H AND 500G<[01] REMOVED CORROSION PER SRM 53-00-53-1A-2 FOUND TO BE OUT OF LIMITS . TRANSITION ANGLE TO BE REPLACED. REFERENCE TTG8Q00W4L4E DUE TO THE TRANSITION ANGLE BEING PART OF TRANSITION ANGLE STA 5Sep 26, 2024 · N8507C · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2024102242593Mount · corrodedAFT L/H LAV; AFT OTBD MOUNT HAS CORROSION; STA 947.<[01] DEPTH OF DAMAGE PRIOR TO BLENDING=.030?. DAMAGE IS OUT OF LIMITS PER SRM 53-70-51-1A-1. ORIGINAL PART THICKNESS = .205?; REMAINING THICKNESS = .175?. MATERIAL LOSS = .030?.;[02] INSPECTED AS REQUIRED. COSep 26, 2024 · N8507C · Boeing 7378H4 · Fuselage, Equipment Attach FittingsSDR SWAA2024102242267Pin · missingL/H AFT OVERWING EXIT DOOR MISSING DOOR UPPER HANDLE PIN INTERNAL<[01] REPLACED PER [SRM 51-40-02-0G-0-B00069 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)]. FINAL INSTALLATION AND TORQUE TO BE ACCOMPLISHED ON TTG8R007PZS2.;[02] 02 - INSSep 26, 2024 · N8507C · Boeing 7378H4 · Emergency ExitsSDR SWAA2024102241764Seal · crackedR/H HORIZONTAL STAB; FWD UPPER SLIDING SEAL CRACKED<[01] REMOVED THE R/H HORIZONTAL STAB; FWD UPPER SLIDING SEAL PER AMM 53-31-31;[02] INSTALLED R/H HORIZONTAL STAB; FWD UPPER SLIDING SEAL IAW AMM <BR>TASK 53-31-31;[03] INSPECTED WORK PERFORMED. R&R R/H HSep 25, 2024 · N8507C · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2024102241768Seal · crackedL/H HORIZONTAL STAB; FWD UPPER SLIDING SEAL CRACKED<[01] REMOVED THE L/H HORIZONTAL STAB; FWD UPPER SLIDING SEAL PER AMM 53-31-31;[02] INSTALLED L/H HORIZONTAL STABILIZER STAB; FWD UPPER SLIDING SEAL PER AMM 53-31-31;[03] PARTS DOCUMENTED ON TTG8Q00W2H64;[04] Sep 25, 2024 · N8507C · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2024072214523Battery Pack · inoperativeEMERGENCY LIGHTS AT ROWS 18 AND 21DEF; AFT RH EMERGENCY EXIT FLOOR; AND RH AFT EXTERIOR OVERWING INOP<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK M1671 IN REF TO AMM 33-51-06. OPS TEST GOOD. NO DEFECTS NOTED AT THIS TIME.Jul 20, 2024 · N8507C · Boeing 7378H4 · Emergency LightingSDR SWAA2024060597850Battery · inoperativeFLIGHT CREW REPORTS FWD FA FLASHLIGHT NOT TESTING<[01] R&R FLASHLIGHT BATTERY PER MM 25-64-00 NO HELP<BR>OK TO CONTINUE PER MEL 25-12-01<BR>SP1B;[02] RESECURED FWD FLASHLIGHT IN CHARGER; TEST NORMAL REF AMM 33-55-00.Jun 3, 2024 · N8507C · Boeing 7378H4 · Emergency EquipmentSDR SWAA2024042579176Battery Pack · inoperativeMULTIPLE INTERIOR AND EXTERIOR EMERGENCY EXIT LIGHTS INOP.<[01] REMOVED AND REPLACED BATTERY PACKS M1670; M1676 AND M2335 IAW AMM 33-51-06.Apr 25, 2024 · N8507C · Boeing 7378H4 · Emergency LightingSDR SWAA2024020849715Light · inoperativeL2 DOOR EXTERIOR EMER LIGHT INOP<[01] R&R L2 EXTERIOR EMER LIGHT PER AMM 33-51-04. OPS CHECK GOOD.Feb 7, 2024 · N8507C · Boeing 7378H4 · Emergency Lighting
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