# Service difficulty reports: N8675A

A list on [N8675A](https://openairdocs.org/aircraft/N8675A.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 3 · 130 reports

- [SDR SWAA2026093046583](https://openairdocs.org/sdr/SWAA2026093046583.md): Battery · inoperative · Sep 26, 2026 · N8675A · Boeing 7378H4 · Emergency Equipment
  > LEFT AFT INBD FLIGHT ATTENDANT FLASHLIGHT BATTERY INOPERATIVE, OK TO CONTINUE PER MEL 25-12-01. R & R THE FLASHLIGHT BATTERY IAW AMM 25-64-00. OPS CHECKED GOOD.
- [SDR SWAA2026081002003](https://openairdocs.org/sdr/SWAA2026081002003.md): Engine · failed · Aug 4, 2026 · N8675A · Boeing 7378H4 · Engine (Turbine/Turboprop)
  > NR 1 ENGINE FAILED ON TAKEOFF ROLL. REMOVED AND REPLACED THE NR 1 ENG IAW MT 771-00-01. REF TTG8Q008F2S8.
- [SDR SWAA2025121551604](https://openairdocs.org/sdr/SWAA2025121551604.md): Bracket · broken · Dec 11, 2025 · N8675A · Boeing 7378H4 · Emergency Equipment
  > FWD MEGAPHONE BRACKET BROKEN. R & R BRACKET IAW AMM 25--64-00 SIP.
- [SDR SWAA2025110731884](https://openairdocs.org/sdr/SWAA2025110731884.md): Tray · delaminated · Nov 5, 2025 · N8675A · Boeing 7378H4 · Passenger Compartment Equipment
  > PASSENGER CABIN SEAT BACK MOUNTED TRAY TABLE DELAMINATED AT 15E. REMOVED AND REPLACED FOOD TRAY TABLE AT 15E IAW CMM 25-22-46
- [SDR SWAA2025091113312](https://openairdocs.org/sdr/SWAA2025091113312.md): Battery · intermittent · Sep 9, 2025 · N8675A · Boeing 7378H4 · Emergency Equipment
  > CREW REPORTS FWD MEGAPHONE WORK INTERMITTENTLY. R & R FWD MEGAPHONE BATTERIES IN REF TO AMM 25-64-00. NEXT INSPECTION DUE SEP 2026
- [SDR SWAA2025052772867](https://openairdocs.org/sdr/SWAA2025052772867.md): Tab · cracked · May 20, 2025 · N8675A · Boeing 7378H4 · Wing Main, Frame Structure
  > LEFT WING FIXED TRAILING EDGE DEFLECTION ROLLERS ASSEMBLYS PANEL ATTACHMENT TAB HAS A VISIBLE CRACKED 1.7 INCHES IN THE RADIUS FROM THE AFT EDGE.PICTURE ATTACHED. REPAIRED ATTACHMENT TAB ON LH DEFLECTION CONTROL RIB REF SRM 57-51-02-2R-3 REPAIR 3. REINSTALLED
- [SDR SWAA2025042125874](https://openairdocs.org/sdr/SWAA2025042125874.md): Girt Bar · failed · Apr 17, 2025 · N8675A · Boeing 7378H4 · Emergency Equipment
  > FWD ENTRY DOOR GIRT BAR NOT DISARMED WHEN DOOR WAS OPENED. SLIDE CAME PARTIALLY OUT OF DOOR. SLIDE DID NOT DEPLOY. REINSTALLED FORWARD ENTRY ESCAPE SLIDE PER MT 725-60-01
- [SDR SWAA2025012086390](https://openairdocs.org/sdr/SWAA2025012086390.md): Battery Pack · inoperative · Jan 15, 2025 · N8675A · Boeing 7378H4 · Emergency Lighting
  > RT HAND EMERGENCY EXIT DOOR LIGHTS INOP<[01] REMOVED AND REPLACED CHARGER ASSY AND BATTERY IAW AMM 33-51-06 SYSY OPERATION NORMAL;[02] INSPECTED REMOVED AND REPLACED CHARGER ASSY AND BATTERY IAW AMM 33-51-06 SYSY OPERATION NORMAL
- [SDR SWAA2025012084581](https://openairdocs.org/sdr/SWAA2025012084581.md): Angle · cracked · Jan 9, 2025 · N8675A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > IN THE LH AC BAY; L ANGLE AT STA 663; LBL12; RIVET HAS A VERTICAL CRACK EXTENDING FROM IT. VERIFIED WITH HFEC. FABRICATED REPAIR PARTS PER SRM 57-10-10-2R-5;[04] RII: VERIFIED C.A STEP 3 (P. GIETZEN AMT) OF FABRICATED REPAIR PARTS PER SRM 57-10-10-2R-5.;[05]
- [SDR SWAA2025012083721](https://openairdocs.org/sdr/SWAA2025012083721.md): Angle · cracked · Jan 7, 2025 · N8675A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > BAFFLE ATTACH ANGLE CRACKED IN FORWARD CARGO; AFT SIDE OF BS 500H RBL 21.<[01] REMOVED ATTACH ANGLE FROM AIRCRAFT I.A.W SRM 51-40-02 FOR REPLACEMENT.;[02] LOCATED AND DRILLED NEW ATTACH ANGLE PER SRM 51-40-05.;[03] VERIFIED CORRECTIVE ACTION #2;[04] OK TO INST
- [SDR SWAA2025012083722](https://openairdocs.org/sdr/SWAA2025012083722.md): Angle · cracked · Jan 7, 2025 · N8675A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > BAFFLE ATTACH ANGLE CRACKED IN FORWARD CARGO; FWD SIDE OF BS 500H RBL 21.<[01] REMOVED ATTACH ANGLE FROM AIRCRAFT I.A.W SRM 51-40-02 FOR REPLACEMENT.;[02] LOCATED AND DRILLED NEW ATTACH ANGLE PER SRM 51-40-05.;[03] VERIFIED CORRECTIVE ACTION #2;[04] OK TO INST
- [SDR SWAA2025012083723](https://openairdocs.org/sdr/SWAA2025012083723.md): Angle · cracked · Jan 7, 2025 · N8675A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > BAFFLE ATTACH ANGLE CRACKED IN FORWARD CARGO; AFT SIDE OF BS 500G RBL 21.<[01] REMOVED ATTACH ANGLE FROM AIRCRAFT I.A.W SRM 51-40-02 FOR REPLACEMENT.;[02] LOCATED AND DRILLED NEW ATTACH ANGLE PER SRM 51-40-05.;[03] VERIFIED CORRECTIVE ACTION #2;[04] OK TO INST
- [SDR SWAA2025012081294](https://openairdocs.org/sdr/SWAA2025012081294.md): Angle · cracked · Dec 28, 2024 · N8675A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > IN THE LH AC BAY; L ANGLE AT STA 663; LBL12; RIVET HAS A VERTICAL CRACK EXTENDING FROM IT. VERIFIED WITH HFEC. FABRICATED REPAIR PARTS PER SRM 57-10-10-2R-5;[04] RII: VERIFIED C.A STEP 3 OF FABRICATED REPAIR PARTS PER SRM 57-10-10-2R-5.;[05] OK TO INSTALL REP
- [SDR SWAA2025012081291](https://openairdocs.org/sdr/SWAA2025012081291.md): Panel · damaged · Dec 28, 2024 · N8675A · Boeing 7378H4 · Wing, Plate/Skin
  > PANEL 551GB PANEL HAS 2 ELONGATED FASTERNER HOLES. MARKED.<[01] REPAIRED PER SRM 51-70-06-2R-9;[02] INSPECTED REPAIR PER SRM 51-70-06-2R-9.
- [SDR SWAA2025012081293](https://openairdocs.org/sdr/SWAA2025012081293.md): Strap · frayed · Dec 28, 2024 · N8675A · Boeing 7378H4 · Emergency Equipment
  > LEFT EMERGENCY EXIT HATCH ESCAPE STRAP FRAYED<[01] REMOVED AND REPLACED EMERGENCY ESCAPE STRAP PER AMM 25-61-10-400-802.;[02] QC C/W FOR CA#1. WILLIAM DAVIS (TECHNICIAN); 28-DEC-2024 20:55 UTC<BR>REMOVED AND REPLACED EMERGENCY ESCAPE STRAP PER AMM 25-61-10-400
- [SDR SWAA2025012081292](https://openairdocs.org/sdr/SWAA2025012081292.md): Strap · frayed · Dec 28, 2024 · N8675A · Boeing 7378H4 · Emergency Equipment
  > RIGHT EMERGENCY EXIT HATCH ESCAPE STRAP FRAYED<[01] REMOVED AND REPLACED EMERGENCY ESCAPE STRAP PER AMM 25-61-10-400-802.;[02] QC C/W FOR CA#1. WILLIAM DAVIS (TECHNICIAN); 28-DEC-2024 20:50 UTC<BR>REMOVED AND REPLACED EMERGENCY ESCAPE STRAP PER AMM 25-61-10-40
- [SDR SWAA2025012081165](https://openairdocs.org/sdr/SWAA2025012081165.md): Floor Support · cracked · Dec 27, 2024 · N8675A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > PASSENGER COMPARTMENT FLOOR SUPPORT STA. 540 BL 0-RBL 24 CRACKED ON BOTH ENDS AT ATTACHMENT FASTENERS.<[01] 01 - REMOVED AND REPLACED PER SRM 51-40-02.
- [SDR SWAA2025012081166](https://openairdocs.org/sdr/SWAA2025012081166.md): Floor Support · cracked · Dec 27, 2024 · N8675A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > PASSENGER COMPARTMENT FLOOR SUPPORT STA. 540 BL 0-LBL 24 CRACKED ON BOTH ENDS AT ATTACHMENT FASTENERS.<[01] 01 - REMOVED AND REPLACED PER SRM 51-40-02.;[02] CORRECTED FAILURE TYPE LINE FROM NO TO YES PER TELECOM FOR PHONEVILAY VANRACHACK E62007.;[03] CERTIFIED
- [SDR SWAA2025012080925](https://openairdocs.org/sdr/SWAA2025012080925.md): Panel · damaged · Dec 26, 2024 · N8675A · Boeing 7378H4 · Wing, Plate/Skin
  > RIGHT WING LOWER WING L/E PANEL #621FB HAS 2EA ELONGATED HOLES.<[01] REPAIRED PER SRM 51-70-06-2R-9;[02] INSP C/W PER REPAIRED PER SRM 51-70-06-2R-9;[03] RESTORED FINISH TO REPAIRED AREA PER M.M. 51-21-99;[04] 02 - INSPECTED PER [AMM 51-21-99-701-NG (DECORATIV
- [SDR SWAA2025012080922](https://openairdocs.org/sdr/SWAA2025012080922.md): Panel · damaged · Dec 26, 2024 · N8675A · Boeing 7378H4 · Wing, Plate/Skin
  > RIGHT WING LOWER WING L/E PANEL #621PB HAS 1EA ELONGATED HOLES.<[01] REPAIRED PER SRM 51-70-06-2R-9;[02] INSP C/W PER REPAIRED PER SRM 51-70-06-2R-9;[03] RESTORED FINISH TO REPAIRED AREA PER M.M. 51-21-99;[04] 02 - INSPECTED PER [AMM 51-21-99-701-NG (DECORATIV
- [SDR SWAA2025012080926](https://openairdocs.org/sdr/SWAA2025012080926.md): Panel · damaged · Dec 26, 2024 · N8675A · Boeing 7378H4 · Wing, Plate/Skin
  > RIGHT WING LOWER WING L/E PANEL #621VB HAS 2EA ELONGATED HOLES.<[01] REPAIRED PER SRM 51-70-06-2R-9;[02] INSP C/W REPAIRED PER SRM 51-70-06-2R-9;[03] RESTORED FINISH TO REPAIRED AREA PER M.M. 51-21-99;[04] 02 - INSPECTED PER [AMM 51-21-99-701-NG (DECORATIVE EX
- [SDR SWAA2025012080581](https://openairdocs.org/sdr/SWAA2025012080581.md): Angle · cracked · Dec 24, 2024 · N8675A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FOUND 'L' ANGLE CRACKED AT STA 663 R/H SIDE A/C BAY FROM FASTENER HOLE. 5TH FASTENER FROM O/B BULKHEAD DIVIDER.<[01] INSPRJCT: WORK ACCOMPLISHED IN STEPS 1; 2 AND 3 ARE MISSING THE WORK REFERENCE AS REQUIRED PER MPM 51.3.1. WORK ACCOMPLISHED IN STEPS 1; 2 AN
- [SDR SWAA2025012080577](https://openairdocs.org/sdr/SWAA2025012080577.md): Angle · cracked · Dec 24, 2024 · N8675A · Boeing 7378H4 · Wing Miscellaneous Structure
  > L/H WING FIXED T/E ANGLE THAT IS ATTACHED TO THE I/B SIDE OF THE DEFLECTION CONTROL RIB IS CRACKED (MARKED) AFT UPPER T/E<[01] REMOVED OLD ANGLE AND DRILLED NEW ANGLE PER SRM 51-10-02. OK TO INSTALL.;[02] REMOVED OLD ANGLE AND DRILLED NEW ANGLE PER SRM 51-10-0
- [SDR SWAA2025012080580](https://openairdocs.org/sdr/SWAA2025012080580.md): Support Bracket · cracked · Dec 24, 2024 · N8675A · Boeing 7378H4 · Wing Miscellaneous Structure
  > FIXED TRAILING PANEL ABOVE DEFLECTION CONTROL RIB HAS SUPPORT BRACKET (FWD SIDE) CRACK LOCATED AT WBL 190.<[01] REMOVED AND REPLACED SUPPORT BRACKET PER SRM 51-40-02.;[02] VERIFIED
- [SDR SWAA2025012080578](https://openairdocs.org/sdr/SWAA2025012080578.md): Rib · damaged · Dec 24, 2024 · N8675A · Boeing 7378H4 · Wing, Rib/Bulkhead
  > R WING TRAILING EDGE STRUCTURE DEFLECTION CONTROL RIB UPPER TAB HAS ELONGATED FASTENER HOLES.(2EA) [MARKED]<[01] CUT OUT DAMAGE IN UPPER TAB IAW SRM 57-51-02-2R-4.;[02] INSPECTED AND VERIFIED CA#1 DANIEL HONKOMP (TECHNICIAN); 27-DEC-2024 23:47 UTC<BR>CUT OUT D
- [SDR SWAA2025012080345](https://openairdocs.org/sdr/SWAA2025012080345.md): Web · frayed · Dec 22, 2024 · N8675A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO; LEFT OF DOOR- HALF MOON CARGO WEB FRAYING<[01] REPLACED FWD CARGO; LEFT OF DOOR- HALF MOON CARGO NET PER AMM 25-52-12.;[02] 02 - INSPECTED PER [AMM 25-52-12-401-NG (CARGO COMPARTMENT NET - REMOVAL/INSTALLATION - PERMANENT)]
- [SDR SWAA2025012080346](https://openairdocs.org/sdr/SWAA2025012080346.md): Web · frayed · Dec 22, 2024 · N8675A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO; RIGHT OF DOOR- HALF MOON CARGO WEB FRAYING<[01] REPLACED FWD CARGO; RIGHT OF DOOR- HALF MOON CARGO PER AMM 25-52-12.;[02] 02 - INSPECTED PER [AMM 25-52-12-401-NG (CARGO COMPARTMENT NET - REMOVAL/INSTALLATION - PERMANENT)]
- [SDR SWAA2024102452279](https://openairdocs.org/sdr/SWAA2024102452279.md): Girt Bar · out of alignment · Oct 23, 2024 · N8675A · Boeing 7378H4 · Emergency Equipment
  > FLIGHT ATTENDANT REPORTS THAT FWD SERVICE DOOR GIRT BAR IS HARD TO STOW ON HOOKS<[01] RR?D FWD SERVICE DOOR GIRT BAR IAW AMM 25-66-01
- [SDR SWAA2024070106876](https://openairdocs.org/sdr/SWAA2024070106876.md): Lens · unsecure · Jun 27, 2024 · N8675A · Boeing 7378H4 · Emergency Lighting
  > CENTER AISLE EXIT SIGN NOT SECURE<[01] SECURED EXIT SIGN LENS COVER PER M/M 33-51-01
- [SDR SWAA2024020546548](https://openairdocs.org/sdr/SWAA2024020546548.md): Pump · low pressure · Jan 30, 2024 · N8675A · Boeing 7378H4 · Hydraulic Pump (Electric/Engine), Main
  > A HYD SYSTEM FAILURE CREW NOTED LOSS OF A SYSTEM ENGINE PUMP PRESSURE AND LOSS OF 50% OF FLUID. 'FOLLOWING CHECKLIST' RAN ELECTRIC PUMP TILL ZERO PRESSURE AND ZERO QUANTITY INDICATION AT WHICH TIME SHUT OFF ELECTRIC PUMP. NOTED 18% REMAINING AFTER SHUTDOWN AND
- [SDR SWAA2023121832365](https://openairdocs.org/sdr/SWAA2023121832365.md): Filler · missing · Dec 15, 2023 · N8675A · Boeing 7378H4 · Fuselage Main, Structure
  > EXTERNAL ELECTRICAL PLUG CUTOUT; EXTERNAL DOUBLER TAB IS MISSING AT THE LOWER LATCH STRIKER PLATE.<[01] REMOVED FASTENERS AT MISSING FILLER FROM PREVIOUS REPAIR. NO ADDITIONAL DAMAGE NOTED. FABRICATED NEW FILLER PER SRM 53-10-15-2R-4. OK TO INSTALL;[02] INSPEC
- [SDR SWAA2023121531422](https://openairdocs.org/sdr/SWAA2023121531422.md): Battery Pack · inoperative · Dec 13, 2023 · N8675A · Boeing 7378H4 · Emergency Lighting
  > RIGHT AFT SERVICE DOOR EMERGENCY LIGHT INOP<[01] REMOVED AND REPLACED RIGHT AFT GALLEY EMERGENCY LIGHT BATTERY PACK PER MM 33-51-06. OPS CHECKS GOOD PER MM 33-51-00;[02] REMOVED AND REPLACED RIGHT AFT GALLEY EMERGENCY LIGHT BATTERY PACK PER MM 33-51-06. OPS CH
- [SDR SWAA2023121830127](https://openairdocs.org/sdr/SWAA2023121830127.md): Handle · gouged · Dec 10, 2023 · N8675A · Boeing 7378H4 · Service Doors
  > FWD SERVICE DOOR LINER UPPER ASSIST HANDLE IS GOUGED.<[01] REPLACED FWD SERVICE DOOR ASSIST HANDLE MOUNTING CUP IN REFERENCE AMM 52-41-31.;[02] REPLACED FWD SERVICE DOOR ASSIST HANDLE MOUNTING CUP IN REFERENCE AMM 52-41-31. C/W INSPECTION
- [SDR SWAA2023121530128](https://openairdocs.org/sdr/SWAA2023121530128.md): Handle · gouged · Dec 10, 2023 · N8675A · Boeing 7378H4 · Passenger/Crew Doors
  > FWD ENTRY DOOR INTERIOR AFT ASSIST HANDLE IS GOUGED.<[01] REPLACED FWD ENTRY DOOR INTERIOR AFT ASSIST HANDLE MOUNTING CUPS IN REFERENCE AMM 25-21-31-420-802 STEP 3.A; B; (6).;[02] REPLACED FWD ENTRY DOOR INTERIOR AFT ASSIST HANDLE MOUNTING CUPS IN REFERENCE AM
- [SDR SWAA2023121529579](https://openairdocs.org/sdr/SWAA2023121529579.md): Battery Pack · inoperative · Dec 8, 2023 · N8675A · Boeing 7378H4 · Emergency Lighting
  > CABIN BULL NOSE EMERGENCY LIGHT; LEFT SIDE INOP<[01] REMOVED AND REPLACED BATTERY PACKS AT SEATS 7; 13; AND 20ABC; OPS CHECKS GOOD; CABIN BULL NOSE EMERGENCY LIGHTS ARE OPERATIONAL. REF. AMM 33-51-06.;[02] REMOVED AND REPLACED BATTERY PACKS AT SEATS 7; 13; AND
- [SDR SWAA2023121529132](https://openairdocs.org/sdr/SWAA2023121529132.md): Scuff Plate · cracked · Dec 8, 2023 · N8675A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO AFT CORNER SCUFF PLATE IS CRACKED.<[01] REMOVED AND REPLACED AFT CARGO SCUFF PLATE PER AMM 53-11-02
- [SDR SWAA2023121825199](https://openairdocs.org/sdr/SWAA2023121825199.md): Floorbeam · corroded · Nov 27, 2023 · N8675A · Boeing 7378H4 · Fuselage Main, Floor Beam
  > FLOOR BEAM CORRODED AT STA 947 LBL 24 NEAR EDGE OF LAV MOUNT<[01] REMOVED CORROSION IAW SRM 51-10-02. THE REWORKED AREA IS OUT OF LIMIT PER SRM 53-70-51-1A-1 FIG 104 DETAIL N.;[02] REJECT: THERE ARE NUMEROUS MEASUREMENT BLOCKS THAT HAVE N/A LISTED AS THE REASO
- [SDR SWAA2023121525200](https://openairdocs.org/sdr/SWAA2023121525200.md): Radome · cracked · Nov 27, 2023 · N8675A · Boeing 7378H4 · Aerodynamic Fairings
  > NOSE RADOME RUBBER BOOT HAS MULTIPLE CRACKS<[01] REMOVED AND REPLACED RADOME PER MM 53-52-00. SEE CARD [TTG8Q00PX78K FOR TOOLING AND SIGH OFFS.
- [SDR SWAA2023121524848](https://openairdocs.org/sdr/SWAA2023121524848.md): Light · inoperative · Nov 26, 2023 · N8675A · Boeing 7378H4 · Emergency Lighting
  > OPS CHECK EMERGENCY LIGHTS<[01] CABIN EMERGENCY LIUGHTS OPS CHECKS GOOD PER MM 33-51-00
- [SDR SWAA2023121829963](https://openairdocs.org/sdr/SWAA2023121829963.md): Stringer · incorrect · Nov 22, 2023 · N8675A · Boeing 7378H4 · Fuselage Main, Longeron/Stringer
  > BS 727 INNER CHORD AT STRINGER 18A LEFT SIDE THICKNESS OF THE GAP BETWEEN THE INNER CHORD AND STRINGER S-18A RECORDED GAP VALUE.029 (GAP MEASUREMENT IS GREATER THAN 0.006 INCH)<[01] SHIMED GAP PER 5311-E-14577-NG;[02] C/W INSPECTION;[03] C/W INSPECTION
- [SDR SWAA2023121829964](https://openairdocs.org/sdr/SWAA2023121829964.md): Stringer · incorrect · Nov 22, 2023 · N8675A · Boeing 7378H4 · Fuselage Main, Longeron/Stringer
  > BS 727 INNER CHORD AT STRINGER 18A RIGHT SIDE THICKNESS OF THE GAP BETWEEN THE INNER CHORD AND STRINGER S-18A RECORDED GAP VALUE.021 (GAP MEASUREMENT IS GREATER THAN 0.006 INCH)<[01] SHIMED GAP PER 5311-E-14625-NG;[02] C/W INSPECTION;[03] C/W INSPECTION
- [SDR SWAA2023121824197](https://openairdocs.org/sdr/SWAA2023121824197.md): Angle · corroded · Nov 22, 2023 · N8675A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO R/H TRANSITION ANGLE FLOORBOARD HOLE AT 747 + 2 ' APROX AT STA 747 + 2 ' APROX<[01] REMOVED CORROSION FROM AREA PER SRM 53-00-53-1A-2 (0.036' REMAINING THICKNESS). TRANSITION ANGLE IS OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] REMOVED RH
- [SDR SWAA2023121824192](https://openairdocs.org/sdr/SWAA2023121824192.md): Angle · corroded · Nov 22, 2023 · N8675A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO R/H TRANSITION ANGLE AROUND ATTACH HOLE AT STA 767 { MARK }<[01] CORROSION REMOVED PER SRM 51-10-02. DAMAGE OUT OF LIMITS PER SRM 53-00-53-1A-2. TRANSITION ANGLE WAS REMOVED FOR REPLACEMENT FROM STA 727H=+11? - STA 767 PER SRM 51-40-02.;
- [SDR SWAA2023121824203](https://openairdocs.org/sdr/SWAA2023121824203.md): Angle · corroded · Nov 22, 2023 · N8675A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO R/H TRANSITION ANGLE FLOORBOARD HOLE AT BS 727 J + 10 ' APROX<[01] REMOVED CORROSION FROM AREA PER SRM 53-00-53-1A-2 (0.037' REMAINING THICKNESS). TRANSITION ANGLE IS OUT OF LIMITS PER SRM<BR>53-00-53-1A-2.;[02] REMOVED RH TRANSITION ANG
- [SDR SWAA2023121824207](https://openairdocs.org/sdr/SWAA2023121824207.md): Angle · corroded · Nov 22, 2023 · N8675A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO R/H TRANSITION ANGLE FLOORBOARD HOLE AT BS 727 I + 6 ' APROX<[01] REMOVED CORROSION PER SRM 53-0-53-1A-2 (0.037' REMAINING THICKNESS). TRANSITION ANGLE IS OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] REMOVED RH TRANSITION ANGLE (SIDEPLATE)
- [SDR SWAA2023121824208](https://openairdocs.org/sdr/SWAA2023121824208.md): Angle · corroded · Nov 22, 2023 · N8675A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO R/H TRANSITION ANGLE FLOORBOARD HOLE AT BS 727 I + 14 ' APROX<[01] REMOVED CORROSION PER SRM 53-00-53-1A-2 (0.035' REMAINING THICKNESS). TRANSITION ANGLE IS OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] FABRICATED REPAIR PARTS PER SRM 53-00-
- [SDR SWAA2023121824209](https://openairdocs.org/sdr/SWAA2023121824209.md): Angle · corroded · Nov 22, 2023 · N8675A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO R/H TRANSITION ANGLE FLOORBOARD HOLE AT BS 727 I + 18 ' APROX<[01] REMOVED CORROSION PER SRM 53-0-53-1A-2 (0.038' REMAINING THICKNESS). TRANSITION ANGLE IS OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] REMOVED RH TRANSITION ANGLE FROM STA 72
- [SDR SWAA2023121824187](https://openairdocs.org/sdr/SWAA2023121824187.md): Angle · corroded · Nov 22, 2023 · N8675A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO R/H TRANSITION ANGLE FLOORBOARD HOLE AT 747 + 6 ' APROX AT STA 747 + 6 ' APROX<[01] REMOVED CORROSION FROM AREA PER SRM 53-00-53-1A-2 (0.037' REMAINING THICKNESS). TRANSITION ANGLE IS OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] TRANSITION
- [SDR SWAA2023121824188](https://openairdocs.org/sdr/SWAA2023121824188.md): Angle · corroded · Nov 22, 2023 · N8675A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO R/H TRANSITION ANGLE FLOORBOARD HOLE AT 747 +14 ' APROX AT STA 747 +14 ' APROX<[01] REMOVED CORROSION FROM AREA PER SRM 53-00-53-1A-2 (0.036' REMAINING THICKNESS). TRANSITION ANGLE IS OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] TRANSITION
- [SDR SWAA2023121824198](https://openairdocs.org/sdr/SWAA2023121824198.md): Angle · corroded · Nov 22, 2023 · N8675A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO R/H TRANSITION ANGLE FLOORBOARD HOLE AT 747 + 10 ' APROX AT STA 747 + 10 ' APROX<[01] REMOVED CORROSION PER SRM 53-00-53-1A-2 (0.037' REMAINING THICKNESS). TRANSITION ANGLE IS OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] TRANSITION ANGLE IS

Next page: https://openairdocs.org/aircraft/N8675A/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 = 'N8675A' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8675A/reports

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