# Service difficulty reports: N8692F

A list on [N8692F](https://openairdocs.org/aircraft/N8692F.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 · 81 reports

- [SDR SWAA2026021169785](https://openairdocs.org/sdr/SWAA2026021169785.md): Unknown · odor · Feb 11, 2026 · N8692F · Boeing 7378H4 · Air Distribution System
  > VERY STRONG BURNING METAL ODOR IN THE AFT GALLEY, NO SMOKE. COFFEE POT WAS NOT ON. ODOR CAME ON STRONG & THEN DECREASED. PERFORMED AN INSPECTION IAW AMM 05-51-56, AND FIM 21-00-806. NO DEFECT OR ODOR NOTED. SUSPECT FLIGHT PATH OVER KNOW EVERGLADES FIRE TO
- [SDR SWAA2026012964893](https://openairdocs.org/sdr/SWAA2026012964893.md): Light · detached · Jan 26, 2026 · N8692F · Boeing 7378H4 · Emergency Lighting
  > LAST EMERGENCY LIGHTING STRIP ON LEFT SIDE REMOVED. APPROX 3 FEET LONG. REINSTALLED PHOTOLUMINSCENT STRIP IAW MM33-51-15
- [SDR SWAA2025112036811](https://openairdocs.org/sdr/SWAA2025112036811.md): Pump · leaking · Nov 19, 2025 · N8692F · Boeing 7378H4 · Hydraulic Pump (Electric/Engine), Main
  > LOSS OF A HYDRAULICS QUANTITY ZERO R & R SYSTEM A EMDP PUMP IAW AMM 29-11-21-000 IAW SUB TASK 729-PRD-01-01.
- [SDR SWAA2025112037150](https://openairdocs.org/sdr/SWAA2025112037150.md): Actuator · leaking · Nov 19, 2025 · N8692F · Boeing 7378H4 · Drag Control System
  > LOSS OF A HYDRAULICS, QUANTITY ZERO. R & R SYSTEM A ED PUMP IAW AMM 29-11-21-000 IAW SUB TASK 729-PRD-01-01. REMOVED & REPLACED THE NR 1 OTBD GROUND SPOILER ACTUATOR OPS AND LEAK CHECK GOOD IAW AMM 27-62-94. LEAK CHECKED EMDP AND EDP HYDRAULIC PUMPS AND F
- [SDR SWAA2025061780646](https://openairdocs.org/sdr/SWAA2025061780646.md): Lamp · inoperative · Jun 11, 2025 · N8692F · Boeing 7378H4 · Emergency Lighting
  > RIGHT AFTER SERVICE DOOR SLIDE EMERGENCY LIGHT INOPERATIVE. RELAMPED RIGHT AFT SERVICE DOOR SLIDE EMERGENCY LIGHT PER AMM 33-51-04.
- [SDR SWAA2025061779898](https://openairdocs.org/sdr/SWAA2025061779898.md): Light · cracked · Jun 10, 2025 · N8692F · Boeing 7378H4 · Emergency Lighting
  > FWD LAV A EXIT LIGHT BASE CRACKED. REMOVED AND REPLACED PER AMM 33-51-01-960-802-NG.
- [SDR SWAA2025062576835](https://openairdocs.org/sdr/SWAA2025062576835.md): Cowl Door · cracked · Jun 1, 2025 · N8692F · Boeing 7378H4 · Nacelle/Pylon, Main Frame
  > #1 ENGINE INBOARD FAN COWL; 414; STIFFENER AFT OF THE OIL SERVICE DOOR IS CRACKED.<[01] #1 ENG. I/B FAN COWL WILL REPLACED ON MT 7111-E-17063-NG (REP - RIGHT-HALF FAN COWL ASSEMBLY) [TTG8Q00S5GXS]; REFER TO MT FOR ALL WORK ACCOMPLISHED;[02] INSPECTED AS REQUIR
- [SDR SWAA2025062575975](https://openairdocs.org/sdr/SWAA2025062575975.md): Attach Angle · cracked · May 29, 2025 · N8692F · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > BS 663 VAPOR BARRIER ATTACH ANGLE HAS A CRACK AT APPROXIMATELY RBL 9<[01] REMOVED FASTENERS FROM BS 663 VAPOR BARRIER ATTACH ANGLE LOWER LEG PER SRM 57-10-10-2R-5.;[02] INSPECTED WORK PERFORMED ON C/A #1;[03] MEASUREMENT #11 (NDT) ANSWERED INCORRECTLY. NDT IS
- [SDR SWAA2025062475974](https://openairdocs.org/sdr/SWAA2025062475974.md): Attach Angle · cracked · May 29, 2025 · N8692F · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > BS 663 VAPOR BARRIER ATTACH ANGLE HAS A CRACK AT APPROXIMATELY LBL 9. REMOVED FASTENERS FROM BS 663 VAPOR BARRIER ATTACH ANGLE LOWER LEG PER SRM 57-10-10-2R-5. FABRICATED REPAIR ANGLE & SPLICE ANGLE PER SRM 57-10-10-2R-5. TREATED REPAIR PARTS PER SRM 51-20
- [SDR SWAA2025062578653](https://openairdocs.org/sdr/SWAA2025062578653.md): Fitting · loose · May 28, 2025 · N8692F · Boeing 7378H4 · Wing, Attach Fittings
  > LEFT WING TRAILING EDGE - DEFLECTION CONTROL RIB SUPPORT BEAM ATTACHMENT FASTENERS ARE LOOSE AT SERRATED PLATE.<[01] REMOVED INBD AND OUTBD SERRATED PLATES FOR REPLACEMENT IAW SRM 51-40-02.;;[12] INSTALLED TEE FITTING AND UPPER AND LOWER O.B. RADIUS FILLERS PE
- [SDR SWAA2025031103563](https://openairdocs.org/sdr/SWAA2025031103563.md): Flashlight · no test · Mar 9, 2025 · N8692F · Boeing 7378H4 · Emergency Equipment
  > AFT GALLEY FLASH LIGHT WONT TEST AND SEAL BROKEN<[01] REPLACED AFT GALLEY FLASHLIGHT BATTERY REF AMM 25-64-00.
- [SDR SWAA2024121675810](https://openairdocs.org/sdr/SWAA2024121675810.md): Battery Pack · failed · Dec 11, 2024 · N8692F · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY LIGHTING BATTERY PACK FWD OF R/H OVER WING EXIT FAILED THE CAPACITY CHECK.<[01] REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.
- [SDR SWAA2024120273208](https://openairdocs.org/sdr/SWAA2024120273208.md): Light · inoperative · Dec 2, 2024 · N8692F · Boeing 7378H4 · Emergency Lighting
  > AFT ENTRY EXTERIOR EMERGENCY LIGHT INOP<[01] RELAMPED LIGHT PER AMM 33-51-04. OP CHECK GOOD.
- [SDR SWAA2024112060977](https://openairdocs.org/sdr/SWAA2024112060977.md): Flashlight · damaged · Nov 17, 2024 · N8692F · Boeing 7378H4 · Emergency Equipment
  > FWD OTBD FLASHLIGHT UNDER FLIGHT JUMP SEAT UNUSABLE FWD OTBD FLASHLIGHT UNUSABLE<[01] R&R FLASHLIGHT REF MM 25-64-00. THIS CLEARS MEL 25-12-01 #223812
- [SDR SWAA2024092540454](https://openairdocs.org/sdr/SWAA2024092540454.md): Bulb · inoperative · Sep 23, 2024 · N8692F · Boeing 7378H4 · Emergency Lighting
  > R2 SERVICE DOOR SLIDE LIGHT INOP. REMOVED AND REPLACED BULB FOR R2 EMERGENCY SLIDE-EXTERIOR. REPLACED IAW AMM 33-51-01.
- [SDR SWAA2024081225069](https://openairdocs.org/sdr/SWAA2024081225069.md): Sign · cracked · Aug 9, 2024 · N8692F · Boeing 7378H4 · Emergency Lighting
  > OVERWING CIELING EXIT SIGN COVER CRACKED<[01] R&R OVERWING CIELING EXIT SIGN COVER PER AMM 33-51-01
- [SDR SWAA2024061802689](https://openairdocs.org/sdr/SWAA2024061802689.md): Connector · disconnected · Jun 17, 2024 · N8692F · Boeing 7378H4 · Light System Wiring
  > EMERGENCY LIGHT ON BACK OF FWD LAV INOP<[01] FOUND EMERGENCY LIGHT ON BACK OF FWD LAV UNPLUGGED; PLUGGED BACK IN AS PER AMM 33-51-01-960-801;[02] VERIFIED STEP 1.
- [SDR SWAA2024061802021](https://openairdocs.org/sdr/SWAA2024061802021.md): Battery Pack · inoperative · Jun 15, 2024 · N8692F · Boeing 7378H4 · Emergency Lighting
  > SEVERAL PAX CABIN EMERGENCY LIGHTS INOPERATIVE<[01] OPENED ACCESS PANEL TO PERFORM CABIN EMERGENCY LIGHTS; PERFORMED T/S AND FOUND M1676(R); M2335(L); M1694(L); M1670(L); AND M1671(R); BATTERY PACKS DEFECTED. REF. TO B 737 AMM 21-23-03-000-801 FIM 33-50 TASK 8
- [SDR SWAA2024061801294](https://openairdocs.org/sdr/SWAA2024061801294.md): Floor Panel · damaged · Jun 13, 2024 · N8692F · Boeing 7378H4 · Fuselage Floor Panel
  > FABRICATION OF FLOOR PANEL #120CF AT FWD CARGO COMPARTMENT<[01] FABRICATED FWD CARGO FLOOR PANEL 120CF PER AMM 25-52-01-201-801 AND DWG # 453A1610 INSTALLATION OF PANEL WILL BE ACCOMPLISH ON TTG8Q00T34E7;[02] VERIFIED STEP:1<BR>AUDIT C/W REF MPM 52.02.02
- [SDR SWAA2024062102105](https://openairdocs.org/sdr/SWAA2024062102105.md): Panel · damaged · Jun 12, 2024 · N8692F · Boeing 7378H4 · Wing Main, Frame Structure
  > LEFT WING DEFLECTOR CONTROL RIB UPPER COMPOSITE PANEL HAS 4 EACH ELONGATED HOLES AS MARKED<[01] ACCOMPLISHED REPAIR AT LEFT WING DEFLECTOR CONTROL RIB UPPER COMPOSITE PANEL 4 EACH FASTENER HOLES AND TOPCOATED PER SRM 51-70-04-2R-9 AMM 51-21-73-370-803;[02] VER
- [SDR SWAA2024061897820](https://openairdocs.org/sdr/SWAA2024061897820.md): Floor Panel · delaminated · Jun 3, 2024 · N8692F · Boeing 7378H4 · Fuselage Floor Panel
  > LEFT PASSENGER CABIN FLOOR PANEL 221AF; SURFACE DELAMINATED.<[01] RECEIVED PANEL 221AF; PART #: 141A5810-728; PANEL WILL BE CLOSED ON TASK [TTG8Q00T3487];[02] VERIFIED STEP:1<BR>AUDIT C/W REF MPM 52.02.02
- [SDR SWAA2024062097326](https://openairdocs.org/sdr/SWAA2024062097326.md): Floor Panel · cracked · Jun 2, 2024 · N8692F · Boeing 7378H4 · Fuselage Floor Panel
  > FLOOR PANEL 221BF CRACKED AT CORNER ON BOTTOM LEFT SIDE<[01] THIS FAULT WIIL BE RESOLVED IN ANOTHER FAUL (TTG8Q00TPJPY).;[02] FINAL INSPECTION; VERIFIED STEP #1.<BR> AUDIT C/W REF. MPM 52.02.02.
- [SDR SWAA2024061897613](https://openairdocs.org/sdr/SWAA2024061897613.md): Floor Panel · corroded · Jun 2, 2024 · N8692F · Boeing 7378H4 · Fuselage Floor Panel
  > FWD CARGO COMPARTMENT FLOOR PANEL#120CF HAS CORROSSION AROUND THE EDGES.<[01] RECIEVED MATERIAL 2024 T3 CLAD.071' P/O # 1749056; FABRICATION WILL BE ACCOMPLISH ON TTG8Q00TXVK4;[02] VERIFIED STEP:1<BR>AUDIT C/W REF MPM 52.02.02
- [SDR SWAA2024061897614](https://openairdocs.org/sdr/SWAA2024061897614.md): Floor Panel · corroded · Jun 2, 2024 · N8692F · Boeing 7378H4 · Fuselage Floor Panel
  > AFT CARGO COMPARTMENT FLOOR PANEL#140DF AFT OF STA. 890 UPPER SURFACE EDGE HAS CORROSION.<[01] NEW PART (AFT CARGO FLOOR PANEL 140 DF) RECEIVED; FOR INSTALLATION SEE TTG8Q00T34FQ;[02] VERIFIED STEP 1.
- [SDR SWAA2024061897612](https://openairdocs.org/sdr/SWAA2024061897612.md): Floor Panel · corroded · Jun 2, 2024 · N8692F · Boeing 7378H4 · Fuselage Floor Panel
  > FWD CARGO COMPARTMENT FLOOR PANEL#120BF HAS CORROSSION AROUND THE EDGES.<[01] AUDIT C/W REF MPM 52.02.02
- [SDR SWAA2024061897615](https://openairdocs.org/sdr/SWAA2024061897615.md): Floor Panel · corroded · Jun 2, 2024 · N8692F · Boeing 7378H4 · Fuselage Floor Panel
  > FWD CARGO COMPARTMENT FLOOR PANEL#120DF HAS CORROSSION AROUND THE EDGES.<[01] RECEIVED NEW FWD CARGO COMPARTMENT FLOOR PANEL#120DF; INSTALLATION WILL BE ACCOMPLISH ON TTG8Q00T34E5;[02] VERIFIED STEP:1<BR>AUDIT C/W REF MPM 52.02.02
- [SDR SWAA2024061897316](https://openairdocs.org/sdr/SWAA2024061897316.md): Floor Panel · cracked · Jun 1, 2024 · N8692F · Boeing 7378H4 · Fuselage Floor Panel
  > FWD WET AREA PANEL CRACK # 141A5810-729<[01] REVEIVED NEW PANEL 221BF; PART #: 141A5810-729; PANEL WILL BE CLOSED ON TASK [TTG8Q00TPJPY].;[02] REVEIVED NEW PANEL 221BF; PART #: 141A5810-729; PANEL WILL BE CLOSED ON TASK [TTG8Q00T3485].;[03] VERIFIED STEP:2<BR>
- [SDR SWAA2024061897315](https://openairdocs.org/sdr/SWAA2024061897315.md): Floor Panel · delaminated · Jun 1, 2024 · N8692F · Boeing 7378H4 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL#241#AF DELAMINATED<[01] RECEIVED NEW FLOORPANEL PN. 144A5810-127; PANEL WILL BE CLOSED ON TTG8Q00T33ZX.;[02] FINAL INSPECTION; VERIFIED STEP #1 SUB -1.<BR>AUDIT C/W REF. MPM 52.02.02.
- [SDR SWAA2024061897320](https://openairdocs.org/sdr/SWAA2024061897320.md): Floor Panel · delaminated · Jun 1, 2024 · N8692F · Boeing 7378H4 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL#231XF DELAMINATED<[01] RECEIVED NEW FLOOR PANEL P.N# 144A5810-126; PANEL WILL BE CLOSED ON TTG8QOOT343M.;[02] VERIFIED STEP:1<BR>AUDIT C/W REF MPM 52.02.02;[03] RECEIVED NEW FLOOR PANEL P.N# 144A5810-126; PANEL WILL BE CLOSED ON TTG8Q00T
- [SDR SWAA2024061897321](https://openairdocs.org/sdr/SWAA2024061897321.md): Floor Panel · delaminated · Jun 1, 2024 · N8692F · Boeing 7378H4 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL#241DF DELAMINATED<[01] RECEIVED NEW FLOOR PANEL #144A5810-128; PANEL WILL BE CLOSED ON TTG8T33ZT.;[02] CORRECTING STE 1:RECEIVED NEW FLOOR PANEL #144A5810-128; PANEL WILL BE CLOSED ON TTG8Q00T33ZT.;[03] VERIFIED STEP:2 AUDIT C/W REF MPM
- [SDR SWAA2024061897319](https://openairdocs.org/sdr/SWAA2024061897319.md): Channel · corroded · Jun 1, 2024 · N8692F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FORWARD CARGO COMPARTMENT Z CHANNEL L/H HAS CORROSION FROM STA 500 TO STA 500E<[01] REMOVED AND REPLACED L/H Z CHANNEL FORWARD CARGO COMPARTMENT FROM STA 480+8 TO STA 500I PER REF SRM 51-40-02-0G-0 AND SRM 53-00-53-2R-5;[02] REMOVED AND REPLACED L/H Z CHANNEL
- [SDR SWAA2024061897322](https://openairdocs.org/sdr/SWAA2024061897322.md): Channel · corroded · Jun 1, 2024 · N8692F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FORWARD CARGO COMPARTMENT Z CHANNEL L/H HAS CORROSION FROM STA 500E TO STA 500I<[01] THIS N/R WILL BE CLOSED ON TTG8Q00TPJQH;[02] (RII) FINAL INSPECTION; VERIFIED STEP #1.<BR> AUDIT C/W REF. MPM 52.02.02.
- [SDR SWAA2024061894392](https://openairdocs.org/sdr/SWAA2024061894392.md): Not Reported · corroded · May 31, 2024 · N8692F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION AT MAIN CABIN AFT WET AREA STA 947 RBL 50 UNDER HARD POINT<[01] ACCOMPLISHED REPAIR AT MAIN CABIN AFT WET AREA STA 947 RBL 50 UNDER HARD POINT SRM 51-40-02-0G-0 AND SRM 53-70-51-2R-8;[02] FINAL INSPECTION; VERIFIED STEP #1.<BR> AUDIT C/W REF. MPM 52.
- [SDR SWAA2024061896979](https://openairdocs.org/sdr/SWAA2024061896979.md): Web · corroded · May 31, 2024 · N8692F · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION FOUND AFT CARGO DOOR CUTOUT LOWER WEB FROM STA 787 + 16 TO STA 847 RBL 27 WL 155.5 HAS SPOTS OF CORROSION.<[01] EVALUATED DAMAGE AT AFT CARGO DOOR CUTOUT LOWER WEB FROM STA 787 + 16 TO STA 847 RBL 27 WL 155.5; PART WAS FOUND OUT OF LIMITS DUE TO EXF
- [SDR SWAA2024061891704](https://openairdocs.org/sdr/SWAA2024061891704.md): Doubler · deteriorated · May 30, 2024 · N8692F · Boeing 7378H4 · Fuselage Main, Structure
  > EXTERNAL POWER RECEPTACLE CUT-OUT; AT LOWER EDGE DOBLER SKIN MISSING. FABRICATED AND INSTALLED NEW REPAIR PARTS AND RUBBING BLOCK AT EXTERNAL POWER RECEPTACLE CUT-OUT AT LOWER EDGE PER SRM 51-40-02-0G-0 AND 53-10-15-2R-4.
- [SDR SWAA2024061891700](https://openairdocs.org/sdr/SWAA2024061891700.md): Skin · delaminated · May 30, 2024 · N8692F · Boeing 7378H4 · Trailing Edge Flaps
  > LEFT WING O/B MAIN FLAP AFT FLAP; I/B LOWER SKIN SECTION DELAMINATED DOT 223-LWAF11.<[01] REMOVED AND INSTALLED NEW LEFT WING O/B AFT FLAP. AS PER AMM 27-51-22-000-801 AND AMM 27-51-22-400-801.;[02] RII:<BR>VERIFIED STEP 1<BR>AUDITED PER MPM 52.02.02
- [SDR SWAA2024061891706](https://openairdocs.org/sdr/SWAA2024061891706.md): Skin · delaminated · May 30, 2024 · N8692F · Boeing 7378H4 · Trailing Edge Flaps
  > RIGHT WING O/B MAIN FLAP AFT FLAP; I/B LOWER SKIN SECTION DELAMINATED DOT 223-LWAF18.<[01] REMOVED AND INSTALLED NEW RIGHT WING O/B AFT FLAP. AS PER AMM AMM 27-51-22-000-801 AND AMM 27-51-22-400-801.;[02] RII:<BR>VERIFIED STEP 1<BR>AUDITED CW PER MPM 52.02.02
- [SDR SWAA2024061891701](https://openairdocs.org/sdr/SWAA2024061891701.md): Post · corroded · May 30, 2024 · N8692F · Boeing 7378H4 · Fuselage Main, Structure
  > MAIN CABIN LAVATORY D FWD WALL PANEL DOOR POST CORRORED.<[01] REMOVED AND REINSTALLED MAIN CABIN LAVATORY D FWD WALL PANEL DOOR IN REF B737 CMM 25-40-42.;[02] VERIFIED STEP:1<BR>AUDIT C/W REF MPM 52.02.02;[03] CORRECTION: UPDATED MEASUREMENT TABLE;[04] VERIFIE
- [SDR SWAA2024061891702](https://openairdocs.org/sdr/SWAA2024061891702.md): Post · corroded · May 30, 2024 · N8692F · Boeing 7378H4 · Fuselage Main, Structure
  > MAIN CABIN LAVATORY E FWD WALL PANEL DOOR POST CORRORED.<[01] REMOVED LAVATORY E FWD WALL PANEL AS PER REF CMM 25-40-44;[02] REMOVED AND REINSTALLED MAIN CABIN LAVATORY E FWD WALL PANEL DOOR IN RE B737 CMM 25-40-44;[03] VERIFIED STEP:2<BR>AUDIT C/W REF MPM 52.
- [SDR SWAA2024061901021](https://openairdocs.org/sdr/SWAA2024061901021.md): Angle · cracked · May 29, 2024 · N8692F · Boeing 7378H4 · Wing Miscellaneous Structure
  > RIGHT WING O/B DEFLECTION CONTROL RIB PANEL; LOWER HORIZONTAL SEAL RETAINER ANGLE CRACK.<[01] REMOVED AND REPLACED RIGHT WING O/B DEFLECTION CONTROL RIB PANEL; LOWER HORIZONTAL SEAL RETAINER ANGLE PER REF SRM 51-40-02-0G-0;[02] FINAL INSPECTION; VERIFIED STEP
- [SDR SWAA2024061902102](https://openairdocs.org/sdr/SWAA2024061902102.md): Retainer · cracked · May 29, 2024 · N8692F · Boeing 7378H4 · Wing Main, Frame Structure
  > LEFT WING O/B DEFLECTION CONTROL RIB PANEL; LOWER HORIZONTAL SEAL RETAINER ANGLE CRACK.<[01] INSTALLED L LOWER HORIZONTAL SEAL RETAINER ANGLE AT LEFT WING O/B DEFLECTION CONTROL RIB PANEL AS PER BOEING 737-800 SRM 51-40-02-0G-0 USED TOOL B/C 173324;[02] REMOVE
- [SDR SWAA2024061891307](https://openairdocs.org/sdr/SWAA2024061891307.md): Post · corroded · May 29, 2024 · N8692F · Boeing 7378H4 · Fuselage Main, Structure
  > MAIN CABIN LAV A DOOR POST CORRORED AT THE BOTTOM.<[01] REMOVED AND REPLACED DOOR POST AT MAIN CABIN AFT LAV A IN REF B737 CMM 25-40-40;[02] FINAL INSPECTION; VERIFIED STEP #1.<BR> AUDIT C/W REF. MPM 52.02.02.
- [SDR SWAA2024061891308](https://openairdocs.org/sdr/SWAA2024061891308.md): Post · corroded · May 29, 2024 · N8692F · Boeing 7378H4 · Fuselage Main, Structure
  > MAIN CABIN AFT LAV D DOOR POST CORRORED AT THE BOTTOM.<[01] REMOVED AND REPLACED DOOR POST AT MAIN CABIN AFT LAV D IN REF B737 CMM 25-4042;[02] CORRECT STEP 2:REMOVED AND REPLACED DOOR POST AT MAIN CABIN AFT LAV D IN REF B737 CMM 25-40-42;[03] FINAL INSPECTION
- [SDR SWAA2024061891309](https://openairdocs.org/sdr/SWAA2024061891309.md): Post · corroded · May 29, 2024 · N8692F · Boeing 7378H4 · Fuselage Main, Structure
  > MAIN CABIN AFT LAV E DOOR POST CORRORED AT THE BOTTOM.<[01] REMOVED AND REPLACED LAV E DOOR POST AT MAIN CABIN AFT E IN REF B737 CMM 25-40-44;[02] FINAL INSPECTION; VERIFIED STEP #1.<BR> AUDIT C/W REF. MPM 52.02.02.
- [SDR SWAA2024052288708](https://openairdocs.org/sdr/SWAA2024052288708.md): Controller · failed · May 22, 2024 · N8692F · Boeing 7378H4 · Cabin Pressure Controller
  > CABIN CLIMB/ PRESSURIZATION FAIL<[01] FOUND #2 CPC FAULTING CABIN PRESS CONTROL MODULE. R&R'D OVERHEAD CABIN PRESS CONTROL MODULE. SWEEP TEST PASS. NO FAULTS NOTED.
- [SDR SWAA2024032768165](https://openairdocs.org/sdr/SWAA2024032768165.md): Megaphone · damaged · Mar 27, 2024 · N8692F · Boeing 7378H4 · Emergency Equipment
  > AFT MEGAPHONE DAMAGED<[01] REMOVED AND REPLACED AFT MEGAPHONE AND CKS OK. REF AMM 25-64-00
- [SDR SWAA2024032166273](https://openairdocs.org/sdr/SWAA2024032166273.md): Battery Pack · inoperative · Mar 21, 2024 · N8692F · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY EXIT SIGN ABOVE L2 DOOR IS INOP.<[01] 01 - REMOVED AND REPLACED BATTERY PACK FOR THE EMERGENCY EXIT SIGN ABOVE L2 DOOR; PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)]. OPS CHECK GOOD.
- [SDR SWAA2024011240321](https://openairdocs.org/sdr/SWAA2024011240321.md): Light · inoperative · Jan 12, 2024 · N8692F · Boeing 7378H4 · Emergency Lighting
  > LH AFT EXIT DOOR EMERGENCY LIGHT IS INOP.<[01] REPLACED TERMINAL FOR LEFT AFT DOOR EMERGENCY LIGHT IAW SWPM 20-30-11
- [SDR SWAA2023120126582](https://openairdocs.org/sdr/SWAA2023120126582.md): Flashlight · inoperative · Nov 30, 2023 · N8692F · Boeing 7378H4 · Emergency Equipment
  > FWD FA JUMP SEAT FLASHLIGHT INOP<[01] RESECURED LIGHT. OPS CH GOOD PER AMM 33-55-00
- [SDR SWAA2023101710542](https://openairdocs.org/sdr/SWAA2023101710542.md): Fairing · cracked · Oct 14, 2023 · N8692F · Boeing 7378H4 · Nacelle/Pylon, Main Frame
  > #2 ENGINE PYLON AFT STRUT SUPPORT FAIRING ASSY CRACK - PERMANENT REPAIR<[01] R&R AFT PYLON STRUT FAIRING ASSY PER SRM 51-40-02 AND 51-10-02

Next page: https://openairdocs.org/aircraft/N8692F/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 = 'N8692F' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8692F/reports

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