# Service difficulty reports: N536AS

A list on [N536AS](https://openairdocs.org/aircraft/N536AS.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 6 · 269 reports

- [SDR ASAA2026091168687](https://openairdocs.org/sdr/ASAA2026091168687.md): Sign · detached · Sep 11, 2026 · N536AS · Boeing 737890 · Emergency Lighting
  > EXIT SIGN FELL FROM 17A,. GROUNDED - YES. REF AMM 33-51-01/201 REPLACED EXIT SIGN ASSY. OPS TESTED GOOD.
- [SDR ASAA2026050866010](https://openairdocs.org/sdr/ASAA2026050866010.md): Door · unstable · May 8, 2026 · N536AS · Boeing 737890 · Passenger/Crew Doors
  > L1 DOOR UNSTABLE DURING OPENING. GROUNDED - YES. PERFORMED GVI ON L1 DOOR NO VISIBLE DEFECTS NOTIFIED SYS TEST IAW AMM 52-41-00.
- [SDR ASAA2026031165405](https://openairdocs.org/sdr/ASAA2026031165405.md): Transition Panel · corroded · Mar 11, 2026 · N536AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > AFT CARGO SIDEPLATE TRANSITION PANEL IS CORRODED MULTIPLE SPOTS LH SIDE STA 727 - 727I. GROUNDED - YES. REMOVED CORROSION, FOUND OUT OF LIMITS IAW B737-800 SRM 53-00-53-1A-2 FIG 103, REPAIRED AND REPLACED SIDE PLATE TRANSITION FROM STA 727 TO 747+11 IAW B737-8
- [SDR ASAA2026031165404](https://openairdocs.org/sdr/ASAA2026031165404.md): Transition Panel · corroded · Mar 11, 2026 · N536AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > AFT CARGO SIDEPLATE TRANSITION PANEL IS CORRODED MULTIPLE SPOTS RH SIDE STA 727E - 767. GROUNDED - YES. REMOVED CORROSION & FOUND 100% MATERIAL LOSS AT FASTENERS HOLE LOCATIONS REPLACED SECTION & REQUIRED R/H SIDEPLATE TRANSTION STA 727-767 IAW BOEING 737-800
- [SDR ASAA2026030564727](https://openairdocs.org/sdr/ASAA2026030564727.md): Lamp · inoperative · Mar 5, 2026 · N536AS · Boeing 737890 · Emergency Lighting
  > AFT RH DOOR EMERGENCY EXTERIOR LIGHT INOP. GROUNDED - YES. RE-LAMPED AFT RH DOOR EMERGENCY EXTERIOR LIGHT REF AMM 33-51-04 OPS CK GOOD.
- [SDR ASAA2025102561891](https://openairdocs.org/sdr/ASAA2025102561891.md): Sign · detached · Oct 25, 2025 · N536AS · Boeing 737890 · Emergency Lighting
  > MID CABIN EXIT SIGN CEILING 13 HANGING BY WIRE. GROUNDED - YES. REATTACHED LIGHT ASSEMBLY PER AMM 33-51-01 OPS CHECK GOOD.
- [SDR ASAA2024111953926](https://openairdocs.org/sdr/ASAA2024111953926.md): Skin · corroded · Nov 19, 2024 · N536AS · Boeing 737890 · Fuselage Main, Plate/Skin
  > WATER SERVICE DOOR CUTOUT SKIN HAS SIGNS OF CORROSION GROUNDED - YES. ACCOMPLISHED CATEGORY B MINOR REPAIR TO FUSELAGE SKIN PANEL 147A3400-4 AT STA 907-927 STGR 25R- 27R AT WATER SERVICE PANEL CUTOUT IAW EA#800-53EA-27860 REV00
- [SDR ASAA2024111953946](https://openairdocs.org/sdr/ASAA2024111953946.md): Skin · corroded · Nov 19, 2024 · N536AS · Boeing 737890 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN AT STA 1016 FROM STGR 27R TO 24L HAS SIGNS OF CORROSION GROUNDED - YES. ACCOMPLISHED CATEGORY B MAJOR REPAIR TO FUSELAGE SKIN PANEL 147A3400-4 AT STA 1016 BETWEEN STGR 24L-26R IAW EA 800-53EA-27863 REV 00
- [SDR ASAA2024111953927](https://openairdocs.org/sdr/ASAA2024111953927.md): Skin · corroded · Nov 19, 2024 · N536AS · Boeing 737890 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN AT STA 1088 STGR 15R TO STGR 17R HAS SIGNS OF CORROSION GROUNDED - YES. ACCOMPLISHED CATEGORY A MINOR REPAIR TO AFT FUSELAGE SKIN P/N 148A3321-13 AND P/N 148A3820-2 AT STA 1088 SGTR 16AR-17R IAW EA 800-53EA-27872 REV 00
- [SDR ASAA2024111853873](https://openairdocs.org/sdr/ASAA2024111853873.md): Skin · corroded · Nov 18, 2024 · N536AS · Boeing 737890 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN AT STA 1088 BETWEEN STGR 12L TO STGR 21L HAS SIGNS OF CORROSION SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY A MINOR REPAIR AT FUSELAGE SKIN PANEL 148A3311-12 AT STA 1088 BETWEEN STGR 16L AND 17L IAW EA#800-53EA-27874 REV 00 SRXR430X.
- [SDR ASAA2024111853872](https://openairdocs.org/sdr/ASAA2024111853872.md): Skin · corroded · Nov 18, 2024 · N536AS · Boeing 737890 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN AT STA 992.8 TO STA 1006 BETWEEN STGR 24L TO STGR 25L HAS SIGNS OF CORROSION SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY A MINOR REPAIR AT FUSELAGE SKIN 147A3400-4 STA 992-1006 STGR 24L-25L IAW EA 800-53EA-27858 REV00
- [SDR ASAA2024111853871](https://openairdocs.org/sdr/ASAA2024111853871.md): Skin · corroded · Nov 18, 2024 · N536AS · Boeing 737890 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN AT STA 1088 BETWEEN STGR 12L TO STGR 21L HAS SIGNS OF CORROSION SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY A MINOR REPAIR AT FUSELAGE SKIN PANEL 148A3311-12 AT STA 1088 BETWEEN STGR 16L AND 17L IAW EA#800-53EA-27874 REV 00
- [SDR ASAA2024111153947](https://openairdocs.org/sdr/ASAA2024111153947.md): Skin · corroded · Nov 11, 2024 · N536AS · Boeing 737890 · Fuselage Main, Plate/Skin
  > TOILET VENT BETWEEN STR 21L AND 22L HAS SIGNS OF CORROSION. GROUNDED - YES. ACCOMPLISHED CATEGORY B MAJOR REPAIR TO FUSELAGE SKIN PANEL 147A3110-3 AT STA 20L-23L AT AFT LAV VENT CUTOUT IAW EA 800-53EA-27859 REV 00.
- [SDR ASAA2023102845903](https://openairdocs.org/sdr/ASAA2023102845903.md): Unknown · unknown · Oct 28, 2023 · N536AS · Boeing 737890 · Windshield/Door Rain/Ice Removal
  > L FWD WINDOW HEAT CAUTION AT CRUISE. GROUNDED - YES. FOUND WHCU SHOWING SENSOR FAULT IN BITE. PERFORMED TEMPERATURE SENSOR RESISTANCE MEASUREMENT PER AMM TASK 30-41-21-760-801. FOUND PRIMARY SENSOR ON L1 WINDOW OPEN. SWITCHED WINDOW TO SPARE SENSOR AND SENSOR
- [SDR ASAA2023102645877](https://openairdocs.org/sdr/ASAA2023102645877.md): Windshield · cracked · Oct 26, 2023 · N536AS · Boeing 737890 · Windshield/Door Rain/Ice Removal
  > RIGHT FWD WINDOW OVERHEAT LIGHT FOLLOWED BY RIGHT FWD WINDSHEILD CRACK ON OUTER PANEINIDRATED MIG 2C 40-0052475 37813 10-26-2023. GROUNDED - YES. AIR TURNBACK - REMOVED # 1 FO WINDOW, REF AMM 56-11-11. INSTALLED FO WINDOW FOUND WINDOW DIMENSIONS TO BE OUT OF L
- [SDR ASAA2023101845726](https://openairdocs.org/sdr/ASAA2023101845726.md): Unknown · unknown · Oct 18, 2023 · N536AS · Boeing 737890 · Fuel Controlling System
  > WHILE ACCOMPLISHING T/C 7827300, FOUND FAULT MSG 73-31712 ON #2 ENG. GROUNDED - YES. ACCOMPLISHED FIM TASK 73-28 TASK 801. #2 ENG BITE EEC TESTED GOOD W/O FAULTS. POSSIBLE INTERMITTENT FAULT.
- [SDR ASAA2023083044856](https://openairdocs.org/sdr/ASAA2023083044856.md): Oil Cooler · leaking · Aug 30, 2023 · N536AS · Boeing 737890 · APU Oil System
  > WHLE PERFORMING TSR #TSR714852FOUND APU OIL COOLER LEAKING. GROUNDED - YES. REPLACED APU OIL COOLER. REF. AMM 49-91-41. INSTALLATION/LEAK CHECK GOOD. PLACARDS REMOVED. THIS CLEARS MEL 49-1B. SEAMC TODD NOTIFIED.
- [SDR ASAA2023071043964](https://openairdocs.org/sdr/ASAA2023071043964.md): Unknown · unknown · Jul 10, 2023 · N536AS · Boeing 737890 · Airborne Auxiliary Power Unit (APU) System
  > LOW OIL PRESSURE INDICATED ON APU AFTER START ATTEMPT. GROUNDED - YES. PERFORMED APU BITE PER FIM 49-60 TASK 801NO FAULTS FOUND. APU OPS CHK GOOD.
- [SDR ASAA2023070943938](https://openairdocs.org/sdr/ASAA2023070943938.md): Unknown · unknown · Jul 9, 2023 · N536AS · Boeing 737890 · Flight Management Computing Hardware System
  > AFTER LANDING DURING TAX-IN FMC FAILED. FMC ON MENU PAGE AND VTK FLAG INTERMITTENT FLASHING. GROUNDED - YES. ACCOMPLISHED B737-800 FIM 34-61 TASK 801, L FMC LOGGED PGM FAULT. ACCOMPLISHED FIM 34-61 TASK 807, L FMC OPS NML.
- [SDR ASAA2023061043511](https://openairdocs.org/sdr/ASAA2023061043511.md): Unknown · unknown · Jun 10, 2023 · N536AS · Boeing 737890 · HF Communications System
  > VERIFICATION FLIGHT UNSATISFACTORY. UNABLE TO TRANSMIT ON HF1 & HF2. GROUNDED - YES. CHECKED ALL (8) RAYCHEM PLUGS FOR SECURITY ON FACE OF E8-1 RACK. BOTH HF COAX CONNECTIONS ON THE SIDE OF E8-1 RACK WERE JUST FINGER TIGHT AND INSTALLED TO THE WRONG POSITIONS.
- [SDR ASAA2023053043428](https://openairdocs.org/sdr/ASAA2023053043428.md): Actuator · faulty · May 30, 2023 · N536AS · Boeing 737890 · Cabin Cooling System
  > RH PACK ILLUMINATES AFTER RECALL BUT EXTINGUISHES AFTER MASTER CAUTION RESET. GROUNDED - YES. REMOVED AND REPLACED R/H RAM AIR INLET ACTUATOR IAW B737-800 AMM 21-51-21 OPS CHECK GOOD.
- [SDR ASAA2023052243316](https://openairdocs.org/sdr/ASAA2023052243316.md): Harness · damaged · May 22, 2023 · N536AS · Boeing 737890 · Engine Fuel System Wiring
  > WHILE PERFORMING ASA T/C N8420001, FOUND HARNESSES MW0235, MW0311 & J9 DAMAGED BEYOND LIMITS #2 ENG. GROUNDED - YES. REMOVED & REPLACE HARNESS MW0235 PER B737-800 AMM TASKS 73-21-06-000-803-F00 + 73-21-06-400-803-F00. OPS CHECK GOOD. REMOVED & REPLACED HARNESS
- [SDR ASAA2023051543261](https://openairdocs.org/sdr/ASAA2023051543261.md): Unknown · unknown · May 15, 2023 · N536AS · Boeing 737890 · Cabin Temperature Control System
  > CONT CAB ZONE TEMP LIGHT ON RECALL, EXTINGUISH ON RESET. GROUNDED - YES. ON DEFERRAL.
- [SDR ASAA2023050443124](https://openairdocs.org/sdr/ASAA2023050443124.md): Unknown · unknown · May 4, 2023 · N536AS · Boeing 737890 · Communications System
  > BOTH HF RADIO'S WOULD TUNE ON ALL APPROPRIATE FREQUENCIES BUT NEITHER PILOT COULD TRANSMIT ON ANY HF FREQ. SELCAL WORKED NOTE NEITHER PILOT COULD WE COULD HEAR ATC AND OTHER TRAFFIC ON ALL HG FREQ'S BUT COULD NOT TRANSMIT. GROUNDED - YES. ON DEFERRAL. ATB
- [SDR ASAA2023040543181](https://openairdocs.org/sdr/ASAA2023040543181.md): Battery Pack · inoperative · Apr 5, 2023 · N536AS · Boeing 737890 · Emergency Lighting
  > LEFT OVERWING AND SLIDE EXTERNAL EMERGENCY LIGHTS INOP. GROUNDED - YES. REMOVED AND REPLACED AND OP CHECKED GOOD BATTERY PACKS FOR LEFT OVERWING AND SLIDE LIGHTS IAW B737-800 AMM 33-51-06-960-805.
- [SDR ASAA2023031442503](https://openairdocs.org/sdr/ASAA2023031442503.md): Skin · cracked · Mar 14, 2023 · N536AS · Boeing 737890 · Horizontal Stabilizer Structure
  > RIGHT HORIZONTAL STABILIZER LOWER SKIN IS CRACKED AT THE I/B SIDE OF RIB STA 129.50 APPROX 9 INCHES FWD OF REAR SPAR. GROUNDED - YES. REMOVED DAMAGE AND REPAIRED RH HORIZ STAB LOWER SKIN AT STA 129.5 AT LOCATIONS APPROX 9 INCHES AND 17 INCHES FWD OF REAR SPAR
- [SDR ASAA2023031242522](https://openairdocs.org/sdr/ASAA2023031242522.md): Baffle · cracked · Mar 12, 2023 · N536AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT BAFFLE CLIP STA 500H AFT SIDE UNDER L/H TRANSITION PANEL CRACKED. GROUNDED - YES. REMOVED AND REPLACED BAFFLE CLIP STA 500H AFT SIDE AT L/H TRANSITION PANEL IAW B737-800 SRM 51-40-02-0G-0.
- [SDR ASAA2023031042524](https://openairdocs.org/sdr/ASAA2023031042524.md): Floorbeam · corroded · Mar 10, 2023 · N536AS · Boeing 737890 · Fuselage Main, Structure
  > AFT WET AREA FLOOR BEAM STA 986 HAS CORROSION AT RH END AROUND GIRT BAR FITTING NUTPLATE. GROUNDED - YES. PREFORMED SURFACE BLEND AND REMOVED DAMAGE ON FLOOR BEAM 986 RH FASTNER HOLE FOUND TO BE OUT OF LIMITS REPAIRED FLOOR BEAM IAW B737-800 SRM 53-70-51-2R-6W
- [SDR ASAA2023031042452](https://openairdocs.org/sdr/ASAA2023031042452.md): Floorbeam · corroded · Mar 10, 2023 · N536AS · Boeing 737890 · Fuselage Main, Structure
  > AFT WET AREA FLOOR BEAM STA 986 HAS CORROSION AT LH END AROUND GIRTBAR FITTING NUTPLATE. GROUNDED - YES. PREFORMED SURFACE BLEND REMOVED CORROSION ON FLOOR BEM STA 986 LH FASTNER HOLE FOUND TO BE OUT OF LIMITS INSTALLED REPAIR PARTS RESTORED FINISH IAW B737-80
- [SDR ASAA2023030942525](https://openairdocs.org/sdr/ASAA2023030942525.md): Track · corroded · Mar 9, 2023 · N536AS · Boeing 737890 · Fuselage Main, Attach Fittings
  > AFT PIT RH CARGO TRACK IS CORRODED BETWEEN STA 787-807. GROUNDED - YES. REMOVED DAMAGE WITH SURFACE BLEND FOUND TO BE OUT OF LIMITS REPAIRED CARGO TRACK FROM STA 887 TO STA 767 IAW B737-800 SRM 53-00-53-2R-3W=1 O=.072 R=.059 L=2 D=.033.
- [SDR ASAA2023030942541](https://openairdocs.org/sdr/ASAA2023030942541.md): Baffle · cracked · Mar 9, 2023 · N536AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > BAFFLE CLIP STA 500H FWD SIDE AT L/H TRANSITION PANEL CRACKED. GROUNDED - YES. REMOVED AND REPLACED BAFFLE CLIP STA 500H FWD SIDE AT L/H TRANSITION PANEL IAW B737-900 SRM 51-40-02-0G-0.
- [SDR ASAA2023030942526](https://openairdocs.org/sdr/ASAA2023030942526.md): Support · corroded · Mar 9, 2023 · N536AS · Boeing 737890 · Fuselage Structure (General)
  > R/H TRANSITION PANEL STA 500C TO 500E HAS CORROSION. GROUNDED - YES. CORROSION FOUND TO BE BEYOND LIMITS IAW B737-800 SRM 53-00-53-1A-2 FIG 103 CUTOUT DAMAGED SECTION AND PERFORMED SIDEPLATE REPAIR IAW B737-800 SRM 53-00-53-2R-5W-.4 O-.040 R- 0 L-.5 D-.040
- [SDR ASAA2023030942523](https://openairdocs.org/sdr/ASAA2023030942523.md): Cargo Track · corroded · Mar 9, 2023 · N536AS · Boeing 737890 · Fuselage Main, Attach Fittings
  > AFT PIT RH CARGO TRACK IS CORRODED BETWEEN STA 787-807. GROUNDED - YES. REMOVED DAMAGE WITH SURFACE BLEND FOUND TO BE OUT OF LIMITS REPAIRED CARGO TRACK FROM STA 887 TO STA 767 IAW B737-800 SRM 53-00-53-2R-3W=1 O=.072 R=.059 L=2 D=.033.
- [SDR ASAA2023030942453](https://openairdocs.org/sdr/ASAA2023030942453.md): Floor Support · corroded · Mar 9, 2023 · N536AS · Boeing 737890 · Fuselage Miscellaneous Structure
  > AFT WET AREA FLOOR SUPPORT STA 947 TO 947 LBL 32 IS CORRODED. GROUNDED - YES. PERFORMED SURFACE BLEND REMOVED CORROSION ON FLOOR SUPPORT AT LBL 32 STA 647-967 FOUND TO BE OUT OF LIMITS REPLACED FLOOR SUPPORT IAQW B737-800 SRM 53-70-51-1A-1, SRM 51-40-02-0G-0W=
- [SDR ASAA2023030842451](https://openairdocs.org/sdr/ASAA2023030842451.md): Web · corroded · Mar 8, 2023 · N536AS · Boeing 737890 · Fuselage Main, Structure
  > AFT CARGO THRESHOLD SILL WEB IS CORRODED. GROUNDED - YES. REMOVED AND REPLACED AFT CARGO THRESHOLD SILL WEB IAW B737-800 SRM 51-40-02-0G-0, 51-40-05-0G-0.
- [SDR ASAA2023030742449](https://openairdocs.org/sdr/ASAA2023030742449.md): Web · corroded · Mar 7, 2023 · N536AS · Boeing 737890 · Cargo/Baggage Doors
  > FWD CARGO THRESHOLD PAN IS CORRODED IN SEVERAL SPOTS. GROUNDED - YES. REMOVED CORROSION AND CHECKED LIMITS FOUND THRESHOLD WEB (PANS) OUT OF LIMITS IAW B737-800 SRM 53-30-15-1A-1. REMOVED AND REPLACED WEB IAW B737-800 SRM 51-40-02-06-0W- 1.0 O-.045 R-.039 L-
- [SDR ASAA2023030342641](https://openairdocs.org/sdr/ASAA2023030342641.md): Battery Pack · discharged · Mar 3, 2023 · N536AS · Boeing 737890 · Emergency Lighting
  > EMREGENCY LIGHTS BATTERY PACK FOR EXTERIOR FWD LH OVERWING ESCAPE LIGHT FAILS CAP CHECK. GROUNDED - YES. REMOVED AND INSTALLED SERVICEABLE BATTERY PACK OPS CHECK GOOD IAW B737-800 AMM 33-51-06-960-805 CH E 33-51-06-960-006 5J6.
- [SDR ASAA2023021642003](https://openairdocs.org/sdr/ASAA2023021642003.md): Exciter · faulty · Feb 16, 2023 · N536AS · Boeing 737890 · Ignition Harness (Distribution)
  > #1 ENG HAS NO EGT RISE AFTER START LEVER TO IDLE WITH IGN R. #1 ENG STARTS OK WITH IGN L. GROUNDED - YES. REMOVED AND REPLACED MAIN IGNITER PLUG #1 ENGINE REFB737-800 AMM 74-21-02. OPS CHECK OOD. NO DEFECTS NOTED. REMOVED AND REPLACED #1 ENGINE TOP IGNITION E
- [SDR ASAA2023020441825](https://openairdocs.org/sdr/ASAA2023020441825.md): Circuit Breaker · inoperative · Feb 4, 2023 · N536AS · Boeing 737890 · Windshield/Door Rain/Ice Removal
  > F/O ' 2 WINDOW HEAT INOP. GROUNDED - YES. FOUND CIRCUIT BREAKER P6-11 B8 WINDOW HEAT POWER BROKEN. REPLACED CIRCUIT BREAKER C393 P6-11 B8 PER B737-800 WDM 30-41-11-2. PERFORMED WINDOW HEAT OPERATIONAL TEST PER B737-800 AMM 30-41-00-710-801.
- [SDR ASAA2023020241830](https://openairdocs.org/sdr/ASAA2023020241830.md): Not Reported · not reported · Feb 2, 2023 · N536AS · Boeing 737890 · Flight Management Computing Hardware System
  > CAPTAIN'S SIDE MCDU WENT BLANK FOR 5-10 SECONDS DURING CRUISE AT FL 360.ALL WARNING LIGHTS ON SIDES OF KEYPAD ILLUMINATED.WHEN SCREEN CAME BACK, MCDU WENT INTO BITE TEST MODE FOR ABOUT 10 SECONDS AND RETURNED TO NORMAL OPS.NO SIGN OF FMC FAILURE. GROUNDED - YE
- [SDR ASAA2022122041204](https://openairdocs.org/sdr/ASAA2022122041204.md): Fmc · faulted · Dec 20, 2022 · N536AS · Boeing 737890 · Flight Management Computing Hardware System
  > BETWEEN HALLI AND HELOP WAYPOINTS AT FL350, BOTH FMCS FAILED. VTK DISPLAYED ON BOTH ND SCREENS, BOTH MAPS DISAPPEARED FROM BOTH MCDU MENU PAGES. EVERYTHING RETURNED TO NORMAL OPERATIONS AFTER APPROX. 2 MINUTES. GROUNDED - YES. BITE CHECKED BOTH FMC'S IAW FIM
- [SDR ASAA2022110440670](https://openairdocs.org/sdr/ASAA2022110440670.md): Valve · leaking · Nov 4, 2022 · N536AS · Boeing 737890 · Engine Cooling System
  > STATIC FUEL LEAK FROM #2 ENG HPTCCV DRAIN LINE, APPROX 10 DROPS PER MIN. GROUNDED - YES. PERFORMED IDLE ENG RUN. NO LEAK FOUND FROM HPTCCV DRAIN. OK FOR SERVICE. IAW AMM 71-71-00-200-801-F00, STEP 2.A(2). REMOVED AND REPLACED #2 ENG HPTACC VALVE REF AMM 75-21
- [SDR ASAA2022110340644](https://openairdocs.org/sdr/ASAA2022110340644.md): Contactor · faulted · Nov 3, 2022 · N536AS · Boeing 737890 · Electrical Power System Wiring
  > LEFT GEN DRIVE LIGHT ILLUMINATED. DISCONNECTED DRIVE IAW CHECK LIST. GROUNDED - YES. REPLACED C804 BUS TIE BREAKER 1 PER B737-800 AMM 24-21-41.
- [SDR ASAA2022110140643](https://openairdocs.org/sdr/ASAA2022110140643.md): Idg · faulted · Nov 1, 2022 · N536AS · Boeing 737890 · AC Generator-Alternator
  > AFTER ENGINE START DRIVE LIGHT ON ENG #2 ILLUMINATED ENGINE SHUT DOWN. GROUNDED - YES. PERFORMED B737-800 AMM 24-11-11-080-801 AND FOUND FILTERS CONTAMINATED. REMOVED #2 IDG REF AMM 24-11-11-000-801, REMOVED #2 ENG IDG AIR/OIL COOLER LINES REF AMM 24-11-21. FL
- [SDR ASAA2022110140561](https://openairdocs.org/sdr/ASAA2022110140561.md): Idg · faulted · Nov 1, 2022 · N536AS · Boeing 737890 · AC Generator-Alternator
  > AFTER ENGINE START, GENERATOR #1 WOULD NOT CONNECT OPENED #1 ENGINE FAN COWL TO FOM. GROUNDED - YES. REMOVED #1 IDG REF B737-800 AMM 24-11-11. REPLACED #1 IDG REF AMM 24-11-11.
- [SDR ASAA2022102740524](https://openairdocs.org/sdr/ASAA2022102740524.md): Indicator · inoperative · Oct 27, 2022 · N536AS · Boeing 737890 · Fuel Quantity Indicator
  > #2 MAIN TANK REFUELING INDICATOR POSITION DIGIT IS INOP DOES NOT SHOW 2 AT BOTTOM OF GAUGE. GROUNDED - YES. REPLACED #2 TANK REFUELING INDICATOR INSTALLATION TEST PASSES REF B737-800 AMM 28-41-61-400-801.
- [SDR ASAA2022102740512](https://openairdocs.org/sdr/ASAA2022102740512.md): Compensator · out of limits · Oct 27, 2022 · N536AS · Boeing 737890 · Fuel Indicating System
  > #1 FQIS FAILS SYSTEM TEST AT 404.7 PICO FARADS, REF AMM TASK 28-41-00-730-801. COMPENSATOR, TU1, TU2, TU3, TU7 AND TU10 ARE OUT OF ACCEPTABLE LIMITS. GROUNDED - YES. REMOVED AND REPLACED PROBES - COMPENSATOR, TU1, TU2, TU3, TU7, AND TU10 REF B737-800 AMM 28-
- [SDR ASAA2022102640488](https://openairdocs.org/sdr/ASAA2022102640488.md): Probe · failed · Oct 26, 2022 · N536AS · Boeing 737890 · Fuel Indicating System
  > WITH CENTER TANK PUMPS ON, RIGHT FUEL QUANTITY IS BEING BURNED AT ABOUT 150 LBS/HR CAUSING A FUEL IMBALANCE OF ABOUT 600 LBS. BEFORE CENTER TANK IS EMPTY. FUEL BURNS WERE NORMAL INDICATING NO LEAK. LEFT AND CENTER TANKS DID NOT SHOW A CORRESPONDING INCREASE AS
- [SDR ASAA2022102540485](https://openairdocs.org/sdr/ASAA2022102540485.md): Warning Message · false indication · Oct 25, 2022 · N536AS · Boeing 737890 · Fuel Indicating System
  > INITIALLY UPON LEVELING IN CRUISE FLIGHT, BOTH MAIN TANKS WERE BALANCED. AS THE FLIGHT PROGRESSED AND CONTINUING TO BURN FROM CENTER TANK, THE RIGHT MAIN TANK SLOWLY DROPPED TO 8000 LBS WHILE THE LEFT MAIN TANK INCREASED FROM 8300 LBS TO 8600 LBS. CONTINUED CO
- [SDR ASAA2022093040121](https://openairdocs.org/sdr/ASAA2022093040121.md): Control Panel · failed · Sep 30, 2022 · N536AS · Boeing 737890 · Autopilot System
  > VERTICAL SPEED WHEEL IS INOP WITH CAPTAIN FD (1) ENGAGED. OPERATES NORMAL WITH FIRST OFFICER (2) FD ENGAGED. NO OTHER ANOMALIES. GROUNDED - YES. REMOVED & REPLACED DFCS MODE CONTROL PANEL REF B737-800 AMM 22-11-34.

Next page: https://openairdocs.org/aircraft/N536AS/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 = 'N536AS' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N536AS/reports

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