# Service difficulty reports: N8507C

A list on [N8507C](https://openairdocs.org/aircraft/N8507C.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 · 77 reports

- [SDR SWAA2025112036435](https://openairdocs.org/sdr/SWAA2025112036435.md): Sign · inoperative · Nov 18, 2025 · N8507C · Boeing 7378H4 · Emergency Lighting
  > RIGHT EMERGENCY SIGN ABOVE OVERWING EMERGENCY DOORS INOPERATIVE. REMOVED AND REPLACED M1695 EMERGENCY EXIT LIGHT BATTERY PACK REF AMM 33-51-06. OPS CHECKED GOOD.
- [SDR SWAA2025112036434](https://openairdocs.org/sdr/SWAA2025112036434.md): Battery Pack · inoperative · Nov 18, 2025 · N8507C · Boeing 7378H4 · Emergency Lighting
  > LEFT EMERGENCY SIGN ABOVE OVERWING EMERGENCY DOORS INOPERATIVE. REMOVED AND REPLACED IAW AMM 33-51-06-960-805-NG.
- [SDR SWAA2025112033159](https://openairdocs.org/sdr/SWAA2025112033159.md): Bracket · cracked · Nov 8, 2025 · N8507C · Boeing 7378H4 · Trailing Edge Flaps
  > L/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.
- [SDR SWAA2025112030269](https://openairdocs.org/sdr/SWAA2025112030269.md): Seat Track · cracked · Oct 30, 2025 · N8507C · Boeing 7378H4 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT 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 51-40
- [SDR SWAA2025112030268](https://openairdocs.org/sdr/SWAA2025112030268.md): Attach Bracket · cracked · Oct 30, 2025 · N8507C · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > SEAT 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, LBL
- [SDR SWAA2025112029386](https://openairdocs.org/sdr/SWAA2025112029386.md): Attach Angle · cracked · Oct 28, 2025 · N8507C · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > CRACK 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 PERFORM
- [SDR SWAA2025112029387](https://openairdocs.org/sdr/SWAA2025112029387.md): Attach Angle · cracked · Oct 28, 2025 · N8507C · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > CRACK 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
- [SDR SWAA2025112029497](https://openairdocs.org/sdr/SWAA2025112029497.md): Stiffener · cracked · Oct 28, 2025 · N8507C · Boeing 7378H4 · Nacelle/Pylon, Main Frame
  > NR 2 ENGINE OTBD FAN COWL 424AR, SHELF STIFFENER CRACKED. REMOVED AND REPLACED STIFFENER IAW SRM 51-40-02.
- [SDR SWAA2025112028732](https://openairdocs.org/sdr/SWAA2025112028732.md): Support Angle · cracked · Oct 26, 2025 · N8507C · Boeing 7378H4 · Trailing Edge Flaps
  > LEFT 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.
- [SDR SWAA2025102125660](https://openairdocs.org/sdr/SWAA2025102125660.md): Flashlight · inoperative · Oct 18, 2025 · N8507C · Boeing 7378H4 · Emergency Equipment
  > AFT CABIN GALLEY 1 FLASHLIGHT TEST INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT BATTERY IAW AMM 25-64-00. OPS CHECK GOOD.
- [SDR SWAA2025101523874](https://openairdocs.org/sdr/SWAA2025101523874.md): Flashlight · unsecure · Oct 12, 2025 · N8507C · Boeing 7378H4 · Emergency Equipment
  > AFT FLASHLIGHT NOT BLINKING. FOUND AFT RT INBD FLASHLIGHT NOT PROPERLY SECURED. REINSTALLED IAW AMM 25-64-00. OPS CHECKED GOOD.
- [SDR SWAA2025022598706](https://openairdocs.org/sdr/SWAA2025022598706.md): Lamp · contaminated · Feb 23, 2025 · N8507C · Boeing 7378H4 · Emergency Lighting
  > AFT 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.
- [SDR SWAA2025022598705](https://openairdocs.org/sdr/SWAA2025022598705.md): Lamp · inoperative · Feb 23, 2025 · N8507C · Boeing 7378H4 · Emergency Lighting
  > FWD 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.
- [SDR SWAA2024102244233](https://openairdocs.org/sdr/SWAA2024102244233.md): Stringer Clip · cracked · Oct 2, 2024 · N8507C · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > FWD 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.
- [SDR SWAA2024102244224](https://openairdocs.org/sdr/SWAA2024102244224.md): Floor Support · cracked · Oct 1, 2024 · N8507C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > PASSENGER 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 ABOVE
- [SDR SWAA2024102244225](https://openairdocs.org/sdr/SWAA2024102244225.md): Floor Support · cracked · Oct 1, 2024 · N8507C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > PASSENGER 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 ABOVE
- [SDR SWAA2024102243864](https://openairdocs.org/sdr/SWAA2024102243864.md): Support Angle · corroded · Sep 30, 2024 · N8507C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FLOOR 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 51
- [SDR SWAA2024102243638](https://openairdocs.org/sdr/SWAA2024102243638.md): Access Door · cracked · Sep 30, 2024 · N8507C · Boeing 7378H4 · Nacelle/Pylon Miscellaneous Structure
  > ENG.COWL 414; ACCESS HOLE FOR OIL ACCESS DOOR 414AR; INSIDE WEB CRACKED.<[01] REPLACED COWL 414 ASSY SEE TTG8Q00S5HR7 FOR WORK ACCOMLISHED.;[02] VERIFIED REPLACEMENT
- [SDR SWAA2024102243202](https://openairdocs.org/sdr/SWAA2024102243202.md): Angle · out of limits · Sep 29, 2024 · N8507C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > R/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;[
- [SDR SWAA2024102243201](https://openairdocs.org/sdr/SWAA2024102243201.md): Angle · corroded · Sep 29, 2024 · N8507C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > L/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
- [SDR SWAA2024102243200](https://openairdocs.org/sdr/SWAA2024102243200.md): Angle · out of limits · Sep 29, 2024 · N8507C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > L/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 51-40-02
- [SDR SWAA2024102243217](https://openairdocs.org/sdr/SWAA2024102243217.md): Floorbeam · corroded · Sep 29, 2024 · N8507C · Boeing 7378H4 · Fuselage Main, Floor Beam
  > AFT 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] CU
- [SDR SWAA2024102242920](https://openairdocs.org/sdr/SWAA2024102242920.md): Angle · out of limits · Sep 28, 2024 · N8507C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > R/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 REQUI
- [SDR SWAA2024102242918](https://openairdocs.org/sdr/SWAA2024102242918.md): Angle · corroded · Sep 28, 2024 · N8507C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD 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.;[02
- [SDR SWAA2024102242904](https://openairdocs.org/sdr/SWAA2024102242904.md): Angle · corroded · Sep 27, 2024 · N8507C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT 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 CAPTUR
- [SDR SWAA2024102242900](https://openairdocs.org/sdr/SWAA2024102242900.md): Angle · corroded · Sep 27, 2024 · N8507C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT 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 CAP
- [SDR SWAA2024102242909](https://openairdocs.org/sdr/SWAA2024102242909.md): Angle · corroded · Sep 27, 2024 · N8507C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT 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 WORK
- [SDR SWAA2024102242898](https://openairdocs.org/sdr/SWAA2024102242898.md): Angle · corroded · Sep 27, 2024 · N8507C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT 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 CAPTU
- [SDR SWAA2024102242899](https://openairdocs.org/sdr/SWAA2024102242899.md): Angle · corroded · Sep 27, 2024 · N8507C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT 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 C
- [SDR SWAA2024102242906](https://openairdocs.org/sdr/SWAA2024102242906.md): Angle · corroded · Sep 27, 2024 · N8507C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT 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 ABOV
- [SDR SWAA2024102242283](https://openairdocs.org/sdr/SWAA2024102242283.md): Angle · corroded · Sep 26, 2024 · N8507C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD 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
- [SDR SWAA2024102242273](https://openairdocs.org/sdr/SWAA2024102242273.md): Angle · corroded · Sep 26, 2024 · N8507C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD 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 5
- [SDR SWAA2024102242276](https://openairdocs.org/sdr/SWAA2024102242276.md): Angle · corroded · Sep 26, 2024 · N8507C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD 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 5
- [SDR SWAA2024102242282](https://openairdocs.org/sdr/SWAA2024102242282.md): Angle · corroded · Sep 26, 2024 · N8507C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD 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 5
- [SDR SWAA2024102242284](https://openairdocs.org/sdr/SWAA2024102242284.md): Angle · corroded · Sep 26, 2024 · N8507C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD 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 5
- [SDR SWAA2024102242289](https://openairdocs.org/sdr/SWAA2024102242289.md): Angle · corroded · Sep 26, 2024 · N8507C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD 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 5
- [SDR SWAA2024102242294](https://openairdocs.org/sdr/SWAA2024102242294.md): Stringer Clip · cracked · Sep 26, 2024 · N8507C · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > FWD 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 5
- [SDR SWAA2024102242583](https://openairdocs.org/sdr/SWAA2024102242583.md): Angle · corroded · Sep 26, 2024 · N8507C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD 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;[
- [SDR SWAA2024102242292](https://openairdocs.org/sdr/SWAA2024102242292.md): Angle · corroded · Sep 26, 2024 · N8507C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD 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 500A
- [SDR SWAA2024102242290](https://openairdocs.org/sdr/SWAA2024102242290.md): Angle · corroded · Sep 26, 2024 · N8507C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD 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 143A75
- [SDR SWAA2024102242278](https://openairdocs.org/sdr/SWAA2024102242278.md): Angle · corroded · Sep 26, 2024 · N8507C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD 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 5
- [SDR SWAA2024102242275](https://openairdocs.org/sdr/SWAA2024102242275.md): Angle · corroded · Sep 26, 2024 · N8507C · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD 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 5
- [SDR SWAA2024102242593](https://openairdocs.org/sdr/SWAA2024102242593.md): Mount · corroded · Sep 26, 2024 · N8507C · Boeing 7378H4 · Fuselage, Equipment Attach Fittings
  > AFT 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. CO
- [SDR SWAA2024102242267](https://openairdocs.org/sdr/SWAA2024102242267.md): Pin · missing · Sep 26, 2024 · N8507C · Boeing 7378H4 · Emergency Exits
  > L/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 - INS
- [SDR SWAA2024102241764](https://openairdocs.org/sdr/SWAA2024102241764.md): Seal · cracked · Sep 25, 2024 · N8507C · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous Structure
  > R/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 H
- [SDR SWAA2024102241768](https://openairdocs.org/sdr/SWAA2024102241768.md): Seal · cracked · Sep 25, 2024 · N8507C · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous Structure
  > L/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]
- [SDR SWAA2024072214523](https://openairdocs.org/sdr/SWAA2024072214523.md): Battery Pack · inoperative · Jul 20, 2024 · N8507C · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY 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.
- [SDR SWAA2024060597850](https://openairdocs.org/sdr/SWAA2024060597850.md): Battery · inoperative · Jun 3, 2024 · N8507C · Boeing 7378H4 · Emergency Equipment
  > FLIGHT 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.
- [SDR SWAA2024042579176](https://openairdocs.org/sdr/SWAA2024042579176.md): Battery Pack · inoperative · Apr 25, 2024 · N8507C · Boeing 7378H4 · Emergency Lighting
  > MULTIPLE INTERIOR AND EXTERIOR EMERGENCY EXIT LIGHTS INOP.<[01] REMOVED AND REPLACED BATTERY PACKS M1670; M1676 AND M2335 IAW AMM 33-51-06.
- [SDR SWAA2024020849715](https://openairdocs.org/sdr/SWAA2024020849715.md): Light · inoperative · Feb 7, 2024 · N8507C · Boeing 7378H4 · Emergency Lighting
  > L2 DOOR EXTERIOR EMER LIGHT INOP<[01] R&R L2 EXTERIOR EMER LIGHT PER AMM 33-51-04. OPS CHECK GOOD.

Next page: https://openairdocs.org/aircraft/N8507C/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 = 'N8507C' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8507C/reports

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