# Service difficulty reports: N8670A

A list on [N8670A](https://openairdocs.org/aircraft/N8670A.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 · 100 reports

- [SDR SWAA2026092146823](https://openairdocs.org/sdr/SWAA2026092146823.md): Fastener · missing · Sep 16, 2026 · N8670A · Boeing 7378H4 · Elevator Miscellaneous Structure
  > LEFT ELEVATOR OTBD BALANCE WEIGHT INNER MOST TRIM WEIGHT MISSING INBD ATTACH HARDWARE. INSTALLED FASTENER IAW SRM 51-61-04, AND SRM 51-40-02-0G-0-B00387.
- [SDR SWAA2026061611642](https://openairdocs.org/sdr/SWAA2026061611642.md): Girt Bar · out of adjust · Jun 12, 2026 · N8670A · Boeing 7378H4 · Emergency Equipment
  > FLIGHT ATTENDANT REPORTS AFT GALLEY FIRST OFFICER`S SIDE GRIT BAR SKIRT HANGING OUT MORE THEN USUAL. READJUSTED AFT RT SVC DOOR ESCAPE SLIDE GIRT BAR SKIRT AS REQUIRED PER S.I.P
- [SDR SWAA2026060104886](https://openairdocs.org/sdr/SWAA2026060104886.md): Elec Connector · broken · May 20, 2026 · N8670A · Boeing 7378H4 · Light System Wiring
  > RIGHT HAND OWE AFT DOOR LIGHT ASSEMBLY #W4142; D14724 M02838 IS BROKEN (RED CAPPED). REPLACED CONNECTOR D14724 FUNCTIONAL CHECK OF RIGHT AFT OWE EMERGENCY LIGHT TO BE PERFORMED ON CCN TTG8Q01C8JPP NO FURTHER ACTION REQUIRED. CONNECTOR REPLACEDMENT WAS PERFOR
- [SDR SWAA2026060104617](https://openairdocs.org/sdr/SWAA2026060104617.md): Cartridge · cracked · May 19, 2026 · N8670A · Boeing 7378H4 · Wing Main, Frame Structure
  > CRACK FOUND ON LT OUTBOARD AFT FLAP INBOARD CARTRIDGE INNER SURFACE. LEFT WING OUTBOARD AFT FLAP; CARTRIDGE WAS REMOVED AND REPLACED IAW B737 CMM 57-53-08. ASSEMBLY 2.C.(2);
- [SDR SWAA2026031679516](https://openairdocs.org/sdr/SWAA2026031679516.md): Filter · odor · Mar 13, 2026 · N8670A · Boeing 7378H4 · Potable Water System
  > WATER SMELLS OF CHEMICALS. DRAIN POTABLE WATER TANK. R & R GALLEY FILTERS. SERVICED POTABLE WATER PER AMM 38-11-99.
- [SDR SWAA2025123055653](https://openairdocs.org/sdr/SWAA2025123055653.md): Light · detached · Dec 26, 2025 · N8670A · Boeing 7378H4 · Emergency Lighting
  > CENTER AISLE EMERGENCY EXIT SIGN DETACHED. REMOVED AND REPLACED EMERGENCY AISLE LIGHT IAW AMM 33-51-03.
- [SDR SWAA2025122955339](https://openairdocs.org/sdr/SWAA2025122955339.md): Sign · detached · Dec 24, 2025 · N8670A · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY EXIT SIGN MID CABIN DETACHED. PERFORMED TIME LIMIT REPAIR AT EMERGENCY EXIT SIGN MID CABIN IAW M24-133-0096. PERFORMED TIME LIMIT REPAIR AT EMERGENCY EXIT SIGN MID CABIN IAW M24-133-00396.
- [SDR SWAA2025121551849](https://openairdocs.org/sdr/SWAA2025121551849.md): Slide · dislodged · Dec 12, 2025 · N8670A · Boeing 7378H4 · Escape Slide
  > AFT SERVICE DOOR SLIDE FELL OUT BUT DID NOT DEPLOY. RE-PACKED AFT SERVICE DOOR SLIDE IAW MT 725-61-06. ACFT OK FOR SERVICE.
- [SDR SWAA2025032709939](https://openairdocs.org/sdr/SWAA2025032709939.md): Lamp · inoperative · Mar 27, 2025 · N8670A · Boeing 7378H4 · Emergency Lighting
  > FWD LEFT OVERWING INTERIOR EXIT LIGHT HAS A FEW LAMPS INOP<[01] RELAMPED FWD LEFT OVERWING INTERIOR EXIT LIGHT PER AMM 33-51-01. OPS CHECK GOOD.
- [SDR SWAA2025010382711](https://openairdocs.org/sdr/SWAA2025010382711.md): Light · out of adjust · Jan 2, 2025 · N8670A · Boeing 7378H4 · Emergency Lighting
  > EXIT SIGN COVERS KNOCKED OFF<[01] R&R AISLE EXIT LT ASSY PER AMM 33-51-01
- [SDR SWAA2024120272623](https://openairdocs.org/sdr/SWAA2024120272623.md): Panel · cracked · Nov 29, 2024 · N8670A · Boeing 7378H4 · Aerodynamic Fairings
  > WING-TO-BODY FAIRING PANEL 193D GROOVE AND CRACK DAMAGE LOCATED 4.25' FROM FWD EDGE OF PANE<[01] REMOVED AND REPLACED 93D PANEL PER SOPM 20-50-01. PARTS TRANSACTION ON TTG8Q00XB1ST ( 24-153-03309-TLD)
- [SDR SWAA2024120272231](https://openairdocs.org/sdr/SWAA2024120272231.md): Panel · cracked · Nov 27, 2024 · N8670A · Boeing 7378H4 · Fuselage Main, Plate/Skin
  > PANEL 193D HAS 5.5' GROOVE.5' WIDE WITH CRACK IN FACESHEET<[01] C/W EA 24-153-03309.
- [SDR SWAA2024112561582](https://openairdocs.org/sdr/SWAA2024112561582.md): Cover · missing · Nov 19, 2024 · N8670A · Boeing 7378H4 · Emergency Lighting
  > OVERHEAD XIT SIGN AT OVERWING MISSING<[01] LENSE COVER FOUND AND REFITTED IAW AMM 33-51-03
- [SDR SWAA2024111258236](https://openairdocs.org/sdr/SWAA2024111258236.md): Sign · loose · Nov 9, 2024 · N8670A · Boeing 7378H4 · Emergency Lighting
  > AISLE EXIT SIGN MID CAB SIGN LOOSE<[01] RESECURED EXIT SIGN PER SIP
- [SDR SWAA2024110856878](https://openairdocs.org/sdr/SWAA2024110856878.md): Flap System · locked · Nov 4, 2024 · N8670A · Boeing 7378H4 · Trailing Edge Flap Control System
  > FLAPS WOULD NOT GO DOWN PAST 5<[01] FOUND #1 FLAP TRANSMISSION TRIP INDICATOR TRIPPED. RESET PER FIM 27-51 TASK 849.;[02] REPLACED OIL FOR TRAILING EDGE FLAP TRANSMISSION?S 1-8 IAW AMM 12-22-51 (SEE TTG8Q00WV8DF FOR WORK PERFORMED) OPS CHECK GOOD
- [SDR SWAA2024062404817](https://openairdocs.org/sdr/SWAA2024062404817.md): Lens · detached · Jun 22, 2024 · N8670A · Boeing 7378H4 · Emergency Lighting
  > LEFT FORWARD OVER WING EMERGENCY EXIT DOOR SIGN LENS OFF<[01] INSTALLED LENS COVER PER M/M 33-51-01
- [SDR SWAA2024061497825](https://openairdocs.org/sdr/SWAA2024061497825.md): Stiffener · cracked · Jun 3, 2024 · N8670A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACKED STIFFENER BS 540 LBL 1.5 WL 208 (MARKED)<[01] VERIFIED STEP 2 IN PARTIAL.;[02] REMOVED AND REPLACED PASSENGER CABIN STIFFENER AT BS 540 BL0 TO LBL 25 WL 208 IAW SRM 51-40-02 AND DWG 143A524;[03] VERIFIED STEPS 1;2 COMPLETE.;[04] REMOVED AND REPLACED PA
- [SDR SWAA2024061497824](https://openairdocs.org/sdr/SWAA2024061497824.md): Stiffener · cracked · Jun 3, 2024 · N8670A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACKED STIFFENER BS 540 RBL 1.5 WL 208 (MARKED)<[01] VERIFIED STEP 3 IN PARTIAL.;[02] VERIFIED STEPS 2;3 COMPLETE; STEP 1 IN PARTIAL.;[03] REMOVED AND REPLACED STIFFENER BS 540 BL 0 TO RBL 25 WL 208 IAW SRM 51-40-02-0G-0 DWG 143A5240;[04] REMOVED AND REPLACED
- [SDR SWAA2024061491364](https://openairdocs.org/sdr/SWAA2024061491364.md): Attach Angle · cracked · May 29, 2024 · N8670A · Boeing 7378H4 · Fuselage Main, Bulkhead
  > B.S. 663 VAPOR BARRIER UPPER ATTACH ANGLE IS CRACKED AT R.B.L. 10 W.L. 164.<[01] VERIFIED STEPS 8;10 COMPLETE; STEP 9 IN PARTIAL.;[02] VERIFIED STEPS 9;11 COMPLETE.;[03] STEP 12 COMPLETE;[04] REPAIRED BS 663 VAPOR BARRIER UPPER ATTACH ANGLE PER SRM 57-10-10-2R
- [SDR SWAA2024022957111](https://openairdocs.org/sdr/SWAA2024022957111.md): Cover · detached · Feb 27, 2024 · N8670A · Boeing 7378H4 · Emergency Lighting
  > CREW REPORTED OVERWING AREA EMERGENCY EXIT SIGN COVER FELL OFF<[01] REPOSITIONED OVERWING EMERGENCY EXIT SIGN COVER PER AMM 33-51-01 OP CHECK OK
- [SDR SWAA2024020247019](https://openairdocs.org/sdr/SWAA2024020247019.md): Glowstrip · detached · Jan 30, 2024 · N8670A · Boeing 7378H4 · Emergency Equipment
  > PHOTOLUMINESENT STRIP FO SIDE BLUE FLOOR STRIP BY ROW 12 IS COMING OFF<[01] RESEATED GLOW STRIP IAW SIP
- [SDR SWAA2023082392773](https://openairdocs.org/sdr/SWAA2023082392773.md): Battery Pack · inoperative · Aug 23, 2023 · N8670A · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY LIGHT IN AFT CEILING PANEL INOP<[01] FOUND CONNECTOR DISCONNECTED AND TAPED. CONNECTED TO EMERGENCY BATTERY PACK CONNECTOR PER SIP & WDM 33-51-14.
- [SDR SWAA2023052450594](https://openairdocs.org/sdr/SWAA2023052450594.md): Wedge · delaminated · May 21, 2023 · N8670A · Boeing 7378H4 · Wing, Control Surfaces
  > R/H INBOARD FLAP BONDED WEDGE ASSY DELAMANATED<[01] REMOVED WEDGE PER SRM 51-40-02.;[02] RII. OK TO INSTALL NEW WEDGE P/N 113A2500-14.;[03] INSTALLED SERVICABLE R/H INBOARD MAIN FLAP; BONDED WEDGE ASSY IAW SRM 51-40-02; SRM 51-10-02 AND SRM 51-20-05.;[04] INST
- [SDR SWAA2023052547785](https://openairdocs.org/sdr/SWAA2023052547785.md): Fairing · delaminated · May 11, 2023 · N8670A · Boeing 7378H4 · Fuselage Main, Plate/Skin
  > L/H WING #3 FLAP FAIRING 542BB OUTER SKIN IS DELAMINATED ON LOWER OUTBOARD SIDE. (MARKED)<[01] REMOVED DELAMINATED SKIN PER SRM 57-53-70-2R-4.;[02] INSPECTED WORK ACCOMPLISHED IN C/A #1. JOSEPH MARTINI (TECHNICIAN); 11-MAY-2023 21:55 UTC REMOVED DELAMINATED SK
- [SDR SWAA2023052547435](https://openairdocs.org/sdr/SWAA2023052547435.md): Baffle · corroded · May 11, 2023 · N8670A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO BAFFLE AT RBL 22 STA 747-767 HAS CORROSION AROUND FASTENER HOLES.<[01] BLENDED CORROSION PER SRM 51-10-02. BLENDED AREA OUT OF LIMITS PER SRM 53-00?52-1A-2;[02] VERIFIED CA#1 BLENDED CORROSION PER SRM 51-10-02. BLENDED AREA OUT OF LIMITS PER SRM 53-0
- [SDR SWAA2023052447663](https://openairdocs.org/sdr/SWAA2023052447663.md): Battery Pack · inoperative · May 11, 2023 · N8670A · Boeing 7378H4 · Emergency Lighting
  > FWD GALLEY LT EMERGENCY EXIT BATTERY PACK INOP<[01] REMOVED AND REPLACED FOWARD GALLEY BATTERY PACK PER MM 33-51-06; OPS CHECKS GOOD PER MM 33-51-00
- [SDR SWAA2023052546994](https://openairdocs.org/sdr/SWAA2023052546994.md): Skin · pulled · May 9, 2023 · N8670A · Boeing 7378H4 · Nacelle/Pylon Structure
  > #1 ENGINE INLET HAS FASTENER PULLED THROUGH LIP SKIN OUTER SURFACE 2 O'CLOCK POSITION.<[01] PERFORMED NDT ON FASTENER HOLE PER NDT PART 6; 51-00-00 PROCEDURE 16. NO DEFECTS NOTED.;[02] REMOVED LOOSE FASTENER. REAMED HOLE AND COUNTERSUNK FOR OVERSIZE FASTENER I
- [SDR SWAA2023052547102](https://openairdocs.org/sdr/SWAA2023052547102.md): Angle · cracked · May 9, 2023 · N8670A · Boeing 7378H4 · Wing, Control Surfaces
  > L/H WING UPPER TRAILING EDGE PANEL LOWER CHANNEL UNDER PANEL HAS SEVERAL CRACKS I/B OF CASTING FOR I/B FLAP DEFLECTION ROLLERS (MKD)<[01] REMOVED AND REPLACED L/H WING UPPER TRAILING EDGE PANEL ATTACH ANGLE JUST I/B OF DEFLECTION RIB PER SRM 51-40-02;[02] VERI
- [SDR SWAA2023052546187](https://openairdocs.org/sdr/SWAA2023052546187.md): Shield · corroded · May 6, 2023 · N8670A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR SURROUND STRUCTURE LOWER SILL FWD TRANSITION SHIELD STA 767 TO STA 795; RBL 21 TO RBL 27 HAS CORROSION AT UPPER AND LOWER SURFACES AROUND FASTENER HOLES.<[01] BLENDED OUT CORROSION AT AFT CARGO DOOR SURROUND FWD TRANSITION SHIELD UPPER SURFACE P
- [SDR SWAA2023052545319](https://openairdocs.org/sdr/SWAA2023052545319.md): Beam · cracked · May 4, 2023 · N8670A · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > AFT CARGO COMPARTMENT BILGE AREA. SUPPORT ANGLE FOR WASTE TANK ENCLOSURE BEAM IS CRACKED. LOCATED AT STA 867 LBL 13; WL 161. MARKED. AFT CARGO COMPARTMENT BILGE AREA. SUPPORT ANGLE FOR WASTE TANK ENCLOSURE BEAM IS CRACKED. LOCATED AT STA 867 LBL 13 WL 161. MAR
- [SDR SWAA2023052545316](https://openairdocs.org/sdr/SWAA2023052545316.md): Web · corroded · May 4, 2023 · N8670A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR CUTOUT SURROUND STRUCTURE. LOWER MAIN SILL WEB HAS MINOR SURFACE CORROSION AROUND FASTENER HOLES STARTING AT STA 787 TO STA 847 RBL 21 TO RBL 27. MARKED<[01] FAULT DUPLICATED IN ERROR. REFERENCE FAULT TTG8Q00KTSGQ FOR CORRECTIVE ACTION.;[02] C/A
- [SDR SWAA2023052545310](https://openairdocs.org/sdr/SWAA2023052545310.md): Angle · corroded · May 4, 2023 · N8670A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO LH FLOOR TRANSITION ANGLE (SIDEPLATE CHANNEL) HAS CORROSION IN NUMEROUS AREAS ON AND AROUND FASTEN HOLES STA-747 TO 787 (MARKED)<[01] BLENDED OUT CORROSION AT L/H TRANSITION ANGLE STA 747 TO 787; LBL 21 PER REF. SRM 51-10-02. REMAINING MATERIAL THICK
- [SDR SWAA2023052545614](https://openairdocs.org/sdr/SWAA2023052545614.md): Angle · corroded · May 4, 2023 · N8670A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO RH FLOOR TRANSITION ANGLE (SIDEPLATE CHANNEL) CORROSION OUT OF LIMITS BS727I TO 727J.<[01] COMPLIED WITH MEASUREMENTS.;[02] COMPLIED WITH TOOL REQUIREMENT.;[03] REMOVED CORROSION FROM AREA PER SRM 53-00-53-1A-2 (REMAINING THICKNESS 0.036'). TRANSITIO
- [SDR SWAA2023052445612](https://openairdocs.org/sdr/SWAA2023052445612.md): Flap · delaminated · May 4, 2023 · N8670A · Boeing 7378H4 · Trailing Edge Flaps
  > LEFT WING OUTBOARD AFT FLAP HAS A LARGE AREA OF DELIMITATION ON THE INBOARD LOWER SURFACE. (PIC ATTACHED)<[01] REMOVED AND REPLACED OUTBOARD AFT FLAP IAW AMM 27-51-22. SEE STEPS 1-3 FOR INDIVIUAL SIGN OFFS.;[02] INSPECTED WORK PERFORMED
- [SDR SWAA2023052545067](https://openairdocs.org/sdr/SWAA2023052545067.md): Angle · cracked · May 3, 2023 · N8670A · Boeing 7378H4 · Fuselage Main, Plate/Skin
  > FWD CARGO R/H SIDEPLATE HAS POSSIBLE CRACK AT I/B ATTACH FASTENER RBL 21; STA. 500B.<[01] CRACKED FOUND OUT OF LIMIT.I.A.W. SRM 53-00-53-1A-2.;[02] REMOVED RH TRANSITION ANGLE STA 500B-500I PER SRM 51-40-02;[03] LOCATE AND DRILL REPAIR PARTS FROM STA 500B TO
- [SDR SWAA2023052545083](https://openairdocs.org/sdr/SWAA2023052545083.md): Plate · cracked · May 3, 2023 · N8670A · Boeing 7378H4 · Fuselage Main, Plate/Skin
  > FWD CARGO L/H SIDEPLATE HAS POSSIBLE CRACK AT I/B ATTACH FASTENER LBL 21; STA. 500B.<[01] FWD CARGO L/H SIDE PLATE FROM STA 440+10 TO STA 500I REPLACED ON FAULT TTG8Q00KSRV.;[02] CORRECTIVE ACTION #1 ENTERED INCORRECTLY. FWD CARGO L/H SIDE PLATE FROM STA 440+1
- [SDR SWAA2023052545073](https://openairdocs.org/sdr/SWAA2023052545073.md): Structure · corroded · May 3, 2023 · N8670A · Boeing 7378H4 · Fuselage Main, Structure
  > SURFACE CORROSION ON UPPER FLOOR STRUCTURE AROUND O/B AFT LAV MOUNT FOR AFT L/H LAV. (MKD)<[01] DRAIN INTERCOSTAL OUT OF LIMITS PER SRM 53-70-51-1A-1;[02] LOCATED AND DRILLED REPLACEMENT INTERCOSTAL; COUNTERSUNK FASTENER HOLES AS REQUIRED PER REF. SRM 51-40-05
- [SDR SWAA2023052545059](https://openairdocs.org/sdr/SWAA2023052545059.md): Angle · corroded · May 3, 2023 · N8670A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO AFT BULKHEAD PANEL LOWER ATTACH ANGLE HAS CORROSION AT FASTENER HOLES; RBL 11-RBL 24; STA. 500I<[01] REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAGE TO BE.009? IN DEPTH. DAMAGE FOUND TO BE OUT OF LIMITS I.A.W SRM 53-30-08-1A-1.;[02] REMOVED DAMAG
- [SDR SWAA2023052545075](https://openairdocs.org/sdr/SWAA2023052545075.md): Plate · corroded · May 3, 2023 · N8670A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO R/H SIDEPLATE HAS CORROSION AT FASTENER HOLES RBL 24; STA. 500D-500E<[01] REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAGE DEPTH TO BE.010? IN DEPTH. DAMAGE FOUND TO BE OUT OF LIMITS I.A.W SRM 53-00-53-1A-2.;[02] REMOVED RH TRANSITION ANGLE STA 50
- [SDR SWAA2023052545076](https://openairdocs.org/sdr/SWAA2023052545076.md): Plate · corroded · May 3, 2023 · N8670A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO R/H SIDEPLATE HAS CORROSION AT FASTENER HOLES RBL 24; STA. 500E-500F<[01] REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAGE DEPTH TO BE.015?. DAMAGE FOUND TO BE OUT OF LIMITS I.A.W SRM 53-00-53-1A-2.;[02] REMOVED RH TRANSITION ANGLE STA 500B-500H P
- [SDR SWAA2023052545061](https://openairdocs.org/sdr/SWAA2023052545061.md): Plate · corroded · May 3, 2023 · N8670A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO R/H SIDEPLATE HAS CORROSION AT FASTENER HOLES RBL 24; STA. 500F-500G<[01] REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAGE DEPTH TO BE.009?. DAMAGE FOUND TO BE OUT OF LIMITS I.A.W SRM 53-00-53-1A-2.;[02] REMOVED RH TRANSITION ANGLE STA 500B-500H P
- [SDR SWAA2023052545064](https://openairdocs.org/sdr/SWAA2023052545064.md): Threshold · corroded · May 3, 2023 · N8670A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR THRESHOLD CORROSION AT STA 795 TO 847; RBL 27. AFT CARGO DOOR THRESHOLD CORROSION AT STA 795 TO 847 RBL 27.<[01] BLENDED OUT CORROSION AT AFT CARGO DOOR THRESHOLD WEB PER SRM 51-10-02. REMAINING MATERIAL THICKNESS OUT OF LIMITS PER SRM 53-60-15-
- [SDR SWAA2023052545077](https://openairdocs.org/sdr/SWAA2023052545077.md): Plate · corroded · May 3, 2023 · N8670A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO R/H SIDEPLATE HAS CORROSION AT FASTENER HOLES RBL 24; STA. 500H-500I<[01] REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAGE DEPTH TO BE.006?. DAMAGE FOUND TO BE OUT OF LIMITS I.A.W SRM 53-00-53-1A-2.;[02] REMOVED RH TRANSITION ANGLE STA 500B-500I P
- [SDR SWAA2023052545062](https://openairdocs.org/sdr/SWAA2023052545062.md): Plate · corroded · May 3, 2023 · N8670A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO R/H SIDEPLATE HAS CORROSION AT FASTENER HOLES RBL 24; STA. 500G-500H<[01] REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAGE DEPTH TO BE.009?. DAMAGE FOUND TO BE OUT OF LIMITS I.A.W SRM 53-00-53-1A-2.;[02] REMOVED RH TRANSITION ANGLE STA 500B-500H P
- [SDR SWAA2023052545086](https://openairdocs.org/sdr/SWAA2023052545086.md): Threshold · corroded · May 3, 2023 · N8670A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO DOOR THRESHOLD WEB HAS CORROSION RBL 28; STA. 440-492.<[01] REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAGE DEPTH TO BE.006?. DAMAGE FOUND TO BE OUT OF LIMITS I.A.W SRM 53-30-15-1A-1.;[02] LOCATED AND DRILLED NEW WEB PER SRM 51-40-02;[03] LOCATED
- [SDR SWAA2023052545298](https://openairdocs.org/sdr/SWAA2023052545298.md): Beam · corroded · May 3, 2023 · N8670A · Boeing 7378H4 · Fuselage Main, Floor Beam
  > CORROSION ON FLOOR BEAM AT STA 927+10; LBL +52- MARKED. FAULT #1137 CLOSED IN ERROR<[01] DRAIN INTERCOSTAL OUT OF LIMITS PER SRM 53-70-51-1A-1;[02] FAULT TO BE RESOLVED ON ANOTHER FAULT. REF TTG8Q00KTSPA;[03] INSPECTED WORK PERFORMED
- [SDR SWAA2023052545078](https://openairdocs.org/sdr/SWAA2023052545078.md): Plate · corroded · May 3, 2023 · N8670A · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO L/H SIDEPLATE HAS CORROSION AT FASTENER HOLES LBL 24; STA. 500D-500E<[01] REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAGE DEPTH TO BE.018?. DAMAGE FOUND TO BE OUT OF LIMITS I.A.W SRM 53-00-53-1A-2.[08] INSPECTED WORK PERFORMED ON C/A #7;[09] ENGI
- [SDR SWAA2023052545299](https://openairdocs.org/sdr/SWAA2023052545299.md): Intercostal · cracked · May 3, 2023 · N8670A · Boeing 7378H4 · Nacelle/Pylon Miscellaneous Structure
  > LEFT INBOARD FAN COWL HAS CRACKED INTERCOSTAL ON OIL ACCESS DOOR FRAME.<[01] REMOVED AND REPLACED INTERCOSTAL PER ARM. 51-40-02;[02] INSPECTED WORK PERFORMED.
- [SDR SWAA2023052545300](https://openairdocs.org/sdr/SWAA2023052545300.md): Web · cracked · May 3, 2023 · N8670A · Boeing 7378H4 · Nacelle/Pylon Miscellaneous Structure
  > RIGHT OUTBOARD FAN COWL HAS CRACKED INTERCOSTAL ON OIL SERVICE DOOR FRAME.<[01] REMOVED AND REPLACED WEB I.A.W SRM 51-40-02.;[02] INSPECTED WORK PERFORMED
- [SDR SWAA2023052446186](https://openairdocs.org/sdr/SWAA2023052446186.md): Panel · missing · May 3, 2023 · N8670A · Boeing 7378H4 · Fuselage Floor Panel
  > PANEL 221BF HAS FIBERS MISSING<[01] INSTALLED NEW 221BF PANEL PER AMM 53-21-00-401-NG (PASSENGER CABIN FLOORS - REMOVAL/INSTALLATION - PERMANENT);[02] C/W INSPECTION.

Next page: https://openairdocs.org/aircraft/N8670A/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 = 'N8670A' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8670A/reports

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