# Service difficulty reports: N8608N

A list on [N8608N](https://openairdocs.org/aircraft/N8608N.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 · 142 reports

- [SDR SWAA2026080433342](https://openairdocs.org/sdr/SWAA2026080433342.md): Glowstrip · damaged · Jul 31, 2026 · N8608N · Boeing 7378H4 · Emergency Equipment
  > PHOTOLUMINESCENT STRIP AT 13C DAMAGED. OK TO CONTINUE PER MEL 25-10-01 SP1. REMOVED AND REPLACED PHOTOLUMINESCENT STRIP AT 13C PER AMM 33-51-15. FUNCTION TEST GOOD. NO FURTHER DEFECTS NOTED.
- [SDR SWAA2026073061286](https://openairdocs.org/sdr/SWAA2026073061286.md): Slide · partial deploy · Jul 26, 2026 · N8608N · Boeing 7378H4 · Escape Slide
  > SLIDE PACK ON L1 DOOR PARTIALLY DEPLOYED ON OPENING OF L1 DOOR AT THE GATE RE INSTALLED SLIDE PER MT725-61-06.
- [SDR SWAA2026060106452](https://openairdocs.org/sdr/SWAA2026060106452.md): Light · loose · May 26, 2026 · N8608N · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY LIGHTS BY ROW 12 ARE NOT SECURED TO THE FLOOR. REATTACTED STRIP AT ROW 12 PER SIP.
- [SDR SWAA2026041789970](https://openairdocs.org/sdr/SWAA2026041789970.md): Light · detached · Apr 15, 2026 · N8608N · Boeing 7378H4 · Emergency Lighting
  > F/A REPORTS 12C FLOOR LIGHT COMING UP. ATTACHED FLOOR PHOTOLUMINESCENT LIGHT AT 12C PER AMM 33-51-15.
- [SDR SWAA2026041589124](https://openairdocs.org/sdr/SWAA2026041589124.md): Slide · out of position · Apr 13, 2026 · N8608N · Boeing 7378H4 · Escape Slide
  > F/A REPORTS THAT R1 DOOR SLIDE IS OUT OF POSITION IN BUSTLE. ADJUSTED R1 SLIDE PACK WITHIN BUSTLE PER SIP
- [SDR SWAA2026041387888](https://openairdocs.org/sdr/SWAA2026041387888.md): Slide · out of position · Apr 9, 2026 · N8608N · Boeing 7378H4 · Escape Slide
  > L1 DOOR SLIDE FLAP SHOWING. SECURED L1 DOOR SLIDE CAUTION FLAP IAW AMM 25-66-00. OK FOR SERVICE
- [SDR SWAA2026040886209](https://openairdocs.org/sdr/SWAA2026040886209.md): Lamp · inoperative · Apr 4, 2026 · N8608N · Boeing 7378H4 · Emergency Lighting
  > FORWARD SERVICE DOOR LIGHT ASSEMBLY L1186 DOES NOT ILLUMINATE DURING EMERGENCY LIGHTING TEST. TROUBLESHOT TO FAULTY FUSE IN M2816 POWER SUPPLY. REPLACED FUSE CONNECTED TO D14812; PIN 15 PER WDM 33-51-21, WDM 33-51-11, AND AMM 33-51-06-960-804. REPLACED TH
- [SDR SWAA2026040887233](https://openairdocs.org/sdr/SWAA2026040887233.md): Fuse · inoperative · Apr 4, 2026 · N8608N · Boeing 7378H4 · Emergency Lighting
  > FORWARD SERVICE DOOR LIGHT ASSEMBLY L1186 DOES NOT ILLUMINATE DURING EMERGENCY LIGHTING TEST.<[01] TROUBLESHOT TO FAULTY FUSE IN M2816 POWER SUPPLY; REPLACED FUSE CONNECTED TO D14812; PIN 15 PER WDM 33-51-21; WDM 33-51-11; AND AMM 33-51-06-960-804. RELAMPED L1
- [SDR SWAA2026040886411](https://openairdocs.org/sdr/SWAA2026040886411.md): Handle · broken · Apr 1, 2026 · N8608N · Boeing 7378H4 · Passenger/Crew Doors
  > FWD GALLEY ASSIST HANDLE IS BROKEN<[01] REMOVED AND REPLACED BROKEN G1 ASSIST HANDLE IAW SRM 51-40-02;[02] VERIFIED CORRECTIVE ACTION ITEM 1.
- [SDR SWAA2026021369768](https://openairdocs.org/sdr/SWAA2026021369768.md): Radome · delaminated · Feb 10, 2026 · N8608N · Boeing 7378H4 · Aerodynamic Fairings
  > NOSE RADOME HAS A DELAMINATION AT 4 O`CLOCK, 4 INCHES FROM AFT EDGE, MEASURES 9 INCHES BY 14 INCHES. R & R NOSE RADOME IAW AMM 53-52-00.
- [SDR SWAA2025120442045](https://openairdocs.org/sdr/SWAA2025120442045.md): Angle · cracked · Dec 3, 2025 · N8608N · Boeing 7378H4 · Wing Miscellaneous Structure
  > LEFT WING OTBD ANGLE UNDER UPPER INBD FIXED TRAILING EDGE PANEL CRACKED. REMOVED AND REPLACED ANGLE IAW SRM 51-40-02-0G-0-B00069.
- [SDR SWAA2025051267810](https://openairdocs.org/sdr/SWAA2025051267810.md): Lens · wrong part · May 6, 2025 · N8608N · Boeing 7378H4 · Emergency Lighting
  > R1 DOOR EMERGENCY EXIT LIGHT LENS DOESNT MATCH<[01] R&R R1 DOOR EMERGENCY EXIT LIGHT LENS IAW AMM 33-51-01
- [SDR SWAA2025051267809](https://openairdocs.org/sdr/SWAA2025051267809.md): Lens · wrong part · May 6, 2025 · N8608N · Boeing 7378H4 · Emergency Lighting
  > L1 DOOR EMERGENCY EXIT LIGHT LENS DOESNT MATCH<[01] R&R L1 DOOR EMERGENCY EXIT LIGHT LENS IAW AMM 33-51-01
- [SDR SWAA2025022898243](https://openairdocs.org/sdr/SWAA2025022898243.md): Handle · out of adjust · Feb 22, 2025 · N8608N · Boeing 7378H4 · Galley Doors
  > CR RR R2 DOOR ASSIST HANDLE AIRFRAME SIDE NEEDS SECURED. <[01] SECURED R2 DOOR ASSIST HANDLE IAW B737-800 AMM 25-21-420-801; [02] SECURED R2 DOOR ASSIST HANDLE IAW B737-800 AMM 25-21-420-801; [03] SECURED R2 DOOR ASSIST HANDLE IAW B737-800 AMM 25-21-420-801.
- [SDR SWAA2025022797269](https://openairdocs.org/sdr/SWAA2025022797269.md): Battery Pack · failed · Feb 18, 2025 · N8608N · Boeing 7378H4 · Emergency Lighting
  > FORWARD RIGHT-HAND EMERGENCY LIGHTS INOP <[01]. REMOVED AND REPLACED FORWARD R/H BATTERY PACK M02816 AND OPS CHECK GOOD IAW B737-800 AMM 33-51-06-960-805.; [02] REMOVED AND REPLACED FORWARD R/H BATTERY PACK M02816 AND OPS CHECK GOOD IAW B737-800 AMM 33-51-06-9
- [SDR SWAA2025022690572](https://openairdocs.org/sdr/SWAA2025022690572.md): Intercostal · cracked · Jan 29, 2025 · N8608N · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT INTERCOSTAL CLIP STA 500H R/H CRACKED P/N#143A7502-158<[01] REMOVED AND REPLACED FWD CARGO COMPARTMENT INTERCOSTAL CLIPS STA 500H R/H WITH NEW PN: 143A7502U158 PO: 1112667.1 AND PN:143A7502U154 PO: 1112648.1 IAW DWG 143A7505 REV - AND B73
- [SDR SWAA2025022690573](https://openairdocs.org/sdr/SWAA2025022690573.md): Intercostal · cracked · Jan 29, 2025 · N8608N · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT INTERCOSTAL CLIP STA 500H R/H CRACKED P/N 143A7502-154<[01] REMOVED AND REPLACED FWD CARGO COMPARTMENT INTERCOSTAL CLIP STA 500H R/H P/N 143A7502-154 PO: 1112648.1 IAW DWG 143A7505 REV - AND B737-800 SRM 51-40-02;[02] VERIFIED REMOVED AND
- [SDR SWAA2025022890570](https://openairdocs.org/sdr/SWAA2025022890570.md): Baffle · cracked · Jan 28, 2025 · N8608N · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT INTERCOSTAL/BAFFLE STA 500F - STA 500G R/H CRACKED (DOT K570) <[01]. REMOVED AND REPLACED BAFFLE STA 500F IAW B737-800 SRM 51-40-02 AND BOEING DWG 143A7510 REV: B AND REPAIRED IAW 51-70-13-2R-1.; [02] VERIFIED: REMOVED AND REPLACED BAFFL
- [SDR SWAA2025022690568](https://openairdocs.org/sdr/SWAA2025022690568.md): Intercostal · cracked · Jan 28, 2025 · N8608N · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT INTERCOSTAL STA 500D - STA 500E R/H CRACKED (DOT K569)<[01] REMOVED FWD CARGO COMPARTMENT INTERCOSTAL AT STA 500D - STA 500E R/H IAW B737-800 SRM 51-40-02; RECEIVED NEW PART P/N: 143A7510-22 BAFFLE ASSEMBLY; P.O: 1112649.1 IAW BAC DWG 143
- [SDR SWAA2025022690127](https://openairdocs.org/sdr/SWAA2025022690127.md): Transition Panel · corroded · Jan 28, 2025 · N8608N · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT R/H TRANSITION PANEL CORRODED AT FASTENER HOLES THROUGHOUT FROM STA 500C TO STA 500I<[01] EVALUATED FWD CARGO COMPARTMENT R/H TRANSITION PANEL FROM STA 500C TO STA 500I; ORIG. MAT. THK. 0.040'; MATERIAL REMOVED 100% AND FOUND TO BE OUT OF
- [SDR SWAA2025022789739](https://openairdocs.org/sdr/SWAA2025022789739.md): Frame · cracked · Jan 26, 2025 · N8608N · Boeing 7378H4 · Fuselage Main, Frame
  > (CR - VERNON) FOUND FRAME CRACK AT STA 312 BETWEEN S-5L AND S-6L ABOVE L-1 DOOR<[01] REMOVED DAMAGE; FORMED; LOCATED; DRILLED; HFEC CUT OUT; OPEN HOLES AND FPI FORMED ANGLE; NO DEFECTS NOTED; ALODINED; PRIMED; INSTALLED REPAIR ANGLE; AND CIC REF B737-NG SRM 53
- [SDR SWAA2025030387860](https://openairdocs.org/sdr/SWAA2025030387860.md): Panel · corroded · Jan 21, 2025 · N8608N · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > [DOT: Z041] AFT CARGO FLOOR BETWEEN STA 727C AND STA 807; LEFT TRANSITION PANEL CORRODED NUMEROUS PLACES AS MARKED. <FOUND TO BE OUT OF LIMITS ORGINAL MATERIAL IS 0.040IN AND THE MATERIAL REMOVED IS 0.007IN; THE NEW MATERIAL THICKNESS IS 0.033IN. FROM STA 737
- [SDR SWAA2025022787861](https://openairdocs.org/sdr/SWAA2025022787861.md): Transition Panel · corroded · Jan 21, 2025 · N8608N · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > [DOT: Z042] AFT CARGO FLOOR FROM FWD BULKHEAD TO STA 767; RIGHT TRANSITION PANEL CORRODED NUMEROUS PLACES AS MARKED. <[01] REMOVED CORROSION FROM R/H TRANSITION PANEL AT STA 727-STA767 ORIGINAL MATERIAL THICK.040 IAW BAC 1496-377. MATERIAL LOST FROM SAT 727-S
- [SDR SWAA2025022687863](https://openairdocs.org/sdr/SWAA2025022687863.md): Angle · corroded · Jan 21, 2025 · N8608N · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > [DOT: B726] AFT CARGO FLOOR BETWEEN STA 767 AND STA 793; RIGHT SUPPORT Z-ANGLE CORRODED AS MARKED.<[01] REMOVED AND REPLACED AFT CARGO FLOOR BETWEEN STA 767 AND STA 793; RIGHT SUPPORT Z-ANGLE REQUIRES INSTALLATION WITH NEW PN:1468127U12 IAW B737-800 SRM 5
- [SDR SWAA2025022687865](https://openairdocs.org/sdr/SWAA2025022687865.md): Splice Strap · corroded · Jan 21, 2025 · N8608N · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > [DOT: B727] AFT CARGO FLOOR AT STA 847; RBL 19 HAS RAIL SPLICE STRAP CORRODED AS MARKED.<[01] REMOVED AND REPLACED NEW STRAP IAE B737-800 SRM 51-40-02 AAND BAC DWG 146A8120 REV A.;[02] VERIFIED REMOVED AND REPLACED NEW STRAP IAE B737-800 SRM 51-40-02 AAND BAC
- [SDR SWAA2025022887747](https://openairdocs.org/sdr/SWAA2025022887747.md): Intercostal · corroded · Jan 20, 2025 · N8608N · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > MAIN CABIN FWD WET AREA INTERCOSTA AT STA.294.5-312 BL0 IS CORR0DED <[01]. REMOVED DAMAGE; ORIG..063; MATERIAL LOSS.063; REMAINING 0.0; FOUND TO BE OUT OF LIMITS REF B737-NG SRM 53-10-51-1A-1 FIG 105 DETAIL A; REMOVED ALL FASTENERS COMMON TO INTERCOSTAL IAW
- [SDR SWAA2025030391075](https://openairdocs.org/sdr/SWAA2025030391075.md): Panel · corroded · Jan 19, 2025 · N8608N · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD PIT TRANSITON PANELS CORRODED AT FASTENER HOLES FROM STA 500C TO 500I <[01]. L/H TRANSITION PANEL FROM STA 500C TO STA 500I EVALUATED ORIG. MAT. THK. = 0.040'; RMV. MAT. = 0.040'; REM. MAT. THK.= 0.00' AND FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-00-5
- [SDR SWAA2025022887419](https://openairdocs.org/sdr/SWAA2025022887419.md): Seal · cracked · Jan 19, 2025 · N8608N · Boeing 7378H4 · Horizontal Stabilizer Structure
  > R-HORIZONTAL UPPER SLIDING SEAL CRACKED DOT# J149 <[01] REMOVED; LOCATED; DRILLED; AND INSTALLED NEW R/H HORIZONTAL UPPER SLIDING SEAL REF B737-NG AMM 53-31-31-400-802; [02] REMOVED; LOCATED; DRILLED; AND INSTALLED NEW R/H HORIZONTAL UPPER SLIDING SEAL REF B73
- [SDR SWAA2025022887417](https://openairdocs.org/sdr/SWAA2025022887417.md): Seal · cracked · Jan 18, 2025 · N8608N · Boeing 7378H4 · Horizontal Stabilizer Structure
  > L/H HORIZ. STAB TRAILING EDGE; UPPER BLADE SEAL DELAMINATED APPROX. EL STA. 155. <[01] REMOVED AND REPLACED BLADE SEAL P/N 185A1621-115 PO 1111955.1 REF BAC DWG 180A1659 REV A TOOL SCREW GUN T03835-203 DUE 03 JUN 25; [02] REMOVED AND REPLACED BLADE SEAL P/N 1
- [SDR SWAA2025022887154](https://openairdocs.org/sdr/SWAA2025022887154.md): Tail Cone · cracked · Jan 18, 2025 · N8608N · Boeing 7378H4 · Wing, Plate/Skin
  > R-WING FLAP FAIRING #6 AT TAILCONE IS CRACKED AND HAS A HOLE DOT# J148 <[01]. REPAIRED RH WING TAILCONE ON FLAP FAIRING #6 IAW 737-800 SRM 51-70-04-2R-1 REPAIR 1 AND APPLIED TOUCH UP PAINT IAW 737-800 AMM 51-21-99-300-802; [02] REPAIRED RH WING TAILCONE ON FL
- [SDR SWAA2025022887138](https://openairdocs.org/sdr/SWAA2025022887138.md): Intercostal · corroded · Jan 17, 2025 · N8608N · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT WET AREA BS 967 TO 987 LBL 15 +/- INTERCOSTAL CORRODED AS MARKED. <[01] REMOVED DAMGED ON LBL 15 +/- INTERCOSTAL STA 967-987 FOUND TO BE OUT OF LIMITS IAW B737-800 53-70-51-1A-1; BOEING DWG 147A5676 REV:M ORGINAL THICKNESS:.075 REMAINING THICKNESS.064 MAT
- [SDR SWAA2025022887140](https://openairdocs.org/sdr/SWAA2025022887140.md): Floor Support · corroded · Jan 17, 2025 · N8608N · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT WET AREA; BS 995 LBL 38 +/- WEB CORRODED AT FASTENER. AS MARKED. <[01] REMOVED AND REPLACED FLOOR SUPPORT PN:147A5710U1 AT STA. 995 LBL 38. IAW B737-800 SRM 51-40-02 AND BOEING DWG. NO. 147A5700 REV:A; [02] REMOVED AND REPLACED FLOOR SUPPORT PN:147A5710U1
- [SDR SWAA2025022787139](https://openairdocs.org/sdr/SWAA2025022787139.md): Floorbeam · corroded · Jan 17, 2025 · N8608N · Boeing 7378H4 · Fuselage Main, Floor Beam
  > AFT WET AREA; BS 987 LBL 47 +/- FLOORBEAM T CAP CORRODED AT DOME NUT FASTENER. AS MARKED. <[01] REMOVED CORROSION FROM AFT WET AREA; BS 987 LBL 47 +/- FLOOR BEAM T CAP AT DOME NUT FASTENER IAW B 737-800 SRM 51-10-02; ORIGINAL MATERIAL THICK. 0.150 IAW BAC 1518
- [SDR SWAA2025022787142](https://openairdocs.org/sdr/SWAA2025022787142.md): Web · corroded · Jan 17, 2025 · N8608N · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT WET AREA; BS 947 RBL 52 TO LBL 5 +/- FLOORBEAM T CAP CORRODED. WIDE SPREAD AND AS MARKED.<[01] REMOVED DAMAGE; ORIG..180; MATERIAL LOSS.090. REMAINING.090; FOUND TO BE OUT OF LIMITS REF B737-NG SRM 53-70-51-1A-1 FIG 104 DETAIL C; ACCOMP. HFEC TRIMMED ED
- [SDR SWAA2025022787136](https://openairdocs.org/sdr/SWAA2025022787136.md): Support · corroded · Jan 17, 2025 · N8608N · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > MAIN CABIN FWD WET AREA; FLOOR SUPPORT CORRODED BETWEEN BS 328 AND BS 344 APPROX. LBL-24. MARKED <[01]. MAIN CABIN FWD WET AREA; FLOOR SUPPORT CORRODED BETWEEN BS 328 AND BS 344 APPROX. LBL-24; EVALUATED DAMAGE AND FOUND OUT OF LIMITS IAW B737-800 SRM 53-10-5
- [SDR SWAA2025022787129](https://openairdocs.org/sdr/SWAA2025022787129.md): Support · corroded · Jan 17, 2025 · N8608N · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > MAIN CABIN FWD WET AREA; FLOOR SUPPORT CORRODED BETWEEN BS 328 AND BS 344 APPROX. LBL-45. <[01] MAIN CABIN FWD WET AREA; FLOOR SUPPORT CORRODED BETWEEN BS 328 AND BS 344 APPROX. LBL-45. EVALUATED DAMAGE AND FOUND OUT OF LIMITS IAW B737-800 SRM 53-10-51-1A-1
- [SDR SWAA2025022886807](https://openairdocs.org/sdr/SWAA2025022886807.md): Structure · cracked · Jan 16, 2025 · N8608N · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > STA540 R/H FLOORBOARD SUPPORT STRUCTURE CRACKED 2EA AREAS DOT T743 <[01]. REMOVED AND REPLACED PANEL BREAK#143A5240-64 PO#1111708.1 AT STA540 R/H IAW B737-800 SRM 51-40-02 AND BAC DWG#143A0060 REV.A; [02] REMOVED AND REPLACED PANEL BREAK#143A5240-64 PO#1111708
- [SDR SWAA2025022885827](https://openairdocs.org/sdr/SWAA2025022885827.md): Flap · delaminated · Jan 14, 2025 · N8608N · Boeing 7378H4 · Trailing Edge Flaps
  > RIGHT WING OUTBOARD AFT FLAP INBOARD LOWER CORNER IS DELAMINATED <[01]. REMOVED AND REPLACED RIGHT WING OUTBOARD AFT FLAP IAW B737-800 AMM 27-51-22-401-NG.; [02] VERIFIED REMOVED AND REPLACED RIGHT WING OUTBOARD AFT FLAP IAW B737-800 AMM 27-51-22-401-NG.; [03
- [SDR SWAA2025022785833](https://openairdocs.org/sdr/SWAA2025022785833.md): Battery Pack · inoperative · Jan 14, 2025 · N8608N · Boeing 7378H4 · Emergency Lighting
  > R/H AFT EMERGENCY LIGHTS ON R2 DOOR INOP <[01]. REMOVED AND REPLACED R/H AFT EMERGENCY BATTERY AND OPS CHECK GOOD IAW B737-800 AMM 33-51-00-710-801; [02] REMOVED AND REPLACED R/H AFT EMERGENCY BATTERY AND OPS CHECK GOOD IAW B737-800 AMM 33-51-00-710-801. VERI
- [SDR SWAA2025030385504](https://openairdocs.org/sdr/SWAA2025030385504.md): Stand Off · corroded · Jan 13, 2025 · N8608N · Boeing 7378H4 · Wing Miscellaneous Structure
  > L/H WING FIXED L/E; 3 EACH STIAND OFFS FOR OVER HEAT DETECTOR CORRODED BETWEEN RIB #3 AND RIB #4. <[01] REMOVED AND REPLACED 3 EACH STAND OFFS # BACN10TL3A12 PO # 1111371.1 AT L/H WING FIXED L/E IAW B737-800 SRM 51-40-02 AND BAC DWG #116A2130 REV.- TOOL # T886
- [SDR SWAA2024031462046](https://openairdocs.org/sdr/SWAA2024031462046.md): Skin · cracked · Mar 12, 2024 · N8608N · Boeing 7378H4 · Nacelle/Pylon, Plate/Skin
  > #2 ENGINE I/B FAN COWL IS CRACKED 17' LONG AT FWD LOWER FWD END.<[01] REMOVED AND REPLACED #2 ENGINE INBOARD FAN COWL REF. AMM 71-11-02. INSTALLED VORTEX CONTROL DEVICE REF. AMM 71-11-08.
- [SDR SWAA2024021351466](https://openairdocs.org/sdr/SWAA2024021351466.md): Actuator · faulty · Feb 11, 2024 · N8608N · Boeing 7378H4 · Landing Gear Retraction/Extension System
  > ON APPROACH LDG GEAR WAS LOWERED AND LT MAIN DISAGREED WITH HANDLE POSITION. NOSE & RT MAIN GREEN/ LEFT MAIN RED AND NO GREEN GEAR LT ON OVERHEAD FOR LT MAIN. RAN QRH FOR LANDING GEAR DISAGREE; PULLED MANUAL EXTENSION AND GOT GREEN LT ON LT MAIN AND OVERHEAD.<
- [SDR SWAA2023122634741](https://openairdocs.org/sdr/SWAA2023122634741.md): Megaphone · inoperative · Dec 21, 2023 · N8608N · Boeing 7378H4 · Emergency Equipment
  > FWD BULLHORN INOP<[01] R & R?D FWD GALLEY MEGAPHONE PER AMM 25-64-00.
- [SDR SWAA2023022104967](https://openairdocs.org/sdr/SWAA2023022104967.md): Battery · inoperative · Feb 20, 2023 · N8608N · Boeing 7378H4 · Emergency Lighting
  > RIGHT SIDE PASSENGER EMERGENCY LIGHTS INOP<[01] T/S PER FIM 33-50 TASK 801; RR?D BATTER PACK AT ASSY# M1695 PER AMM 33-51-06. NO HELP. RETURNED BACK TO ORIGINAL CONFIGURATION. R/R EMERGENCY LIGHT BATTERY PACKS AT POS M1676 AND M1671 REF AMM 33-51-06. OPS CHE
- [SDR SWAA2023012693543](https://openairdocs.org/sdr/SWAA2023012693543.md): Battery Pack · inoperative · Jan 20, 2023 · N8608N · Boeing 7378H4 · Emergency Lighting
  > R/H EMERGENCY EXIT LIGHTS INOP<[01] REMOVED AND REPLACED 2EA EMERGENCY LIGHT BATTERY PACKS PER AMM 33-51-06. OPERATIONAL CHECK NORMAL OF EMERGENCY LIGHTS PER AMM 33-51-00.;[02] INSPECTED
- [SDR SWAA2023012693544](https://openairdocs.org/sdr/SWAA2023012693544.md): Battery Pack · inoperative · Jan 20, 2023 · N8608N · Boeing 7378H4 · Emergency Lighting
  > R/H AFT SERVICE DOOR EMERGENCY EXIT LIGHT INOP<[01] REMOVED AND REPLACED 2EA EMERGENCY LIGHT BATTERY PACKS PER AMM 33-51-06. OPERATIONAL CHECK NORMAL OF EMERGENCY LIGHTS PER AMM 33-51-00. REFERENCE CARD TTG8Q00HCN6F FOR PARTS INSTALLED.;[02] INSPECTED
- [SDR SWAA2023012692942](https://openairdocs.org/sdr/SWAA2023012692942.md): Balance Weight · corroded · Jan 18, 2023 · N8608N · Boeing 7378H4 · Rudder Structure
  > EVIDENCE OF CORROSION ON THE RUDDER BALANCE WEIGHT.<[01] REMOVED RUDDER WEIGHT PER CMM 55-40-09;[02] INSTALLED RUDDER WEIGHT PER CMM 55-40-09;[03] C/W INSPECTION.;[04] INSTALLED RUDDER WEIGHT PER CMM 55-40-09
- [SDR SWAA2023012692410](https://openairdocs.org/sdr/SWAA2023012692410.md): Track · cracked · Jan 18, 2023 · N8608N · Boeing 7378H4 · Horizontal Stabilizer Structure
  > R/T HORIZONTAL PANEL 343AT FWD TRACK IS CRACKED<[01] R&R TRACK PER SOPM 20-50-01;[02] INSPECTED WORK PERFORMED.
- [SDR SWAA2023012688618](https://openairdocs.org/sdr/SWAA2023012688618.md): Support Beam · cracked · Jan 5, 2023 · N8608N · Boeing 7378H4 · Wing Main, Frame Structure
  > L/H WING FIXED TRAILING EDGE SUPPORT BEAM FWD FASTENER HOLE ADJACENT TO L/H DEFLECTION RIB HAS AN HFEC INDICATION OF A CRACK AT THE FWD SIDE OF THE HOLE SEE ATTACHED PICTURE<[01] REPAIR PER EA #23-157-00063 (N8608N - SWA - REPAIR - L/H WING TRAILING EDGE SUPPO
- [SDR SWAA2023012687231](https://openairdocs.org/sdr/SWAA2023012687231.md): Floor Support · cracked · Jan 3, 2023 · N8608N · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CENTER CABIN STA. 540 LBL 1 FLOOR PANEL SUPPORT ANGLE IS CRACKED AT FASTENER HOLE. MRKD<[01] REMOVED AND REPLACED CABIN FLOOR SUPPORT PER SRM 51-40-02.

Next page: https://openairdocs.org/aircraft/N8608N/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 = 'N8608N' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8608N/reports

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