Boeing 737-890

Service difficulty reports · 23,033

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Query with SQL
duckdb -csv -c "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 aircraft_model_key = '737890'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR ASAA2026050866644Transition Panel · corrodedAFT CARGO R/H TRANSITION CORRODED FROM STA 727 TO 727G. GROUNDED - YES. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-00-53-1A-2. REPAIRED TRANSITION IAW B737-800 SRM 53-00-53-2R-5W: 1" O: .040" R: .033" L: 1" D: .007".May 8, 2026 · N558AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2026050866523Web · corrodedAFT CARGO SILL WEB CORRODED. GROUNDED - YES. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A-1. REMOVED AND REPLACED WEB IAW SRM 51-40-02-0G-0.May 8, 2026 · N584AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2026050866053Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 143A5810-533 IS DELAMINATED. GROUNDED - YES. FABRICATED NEW MAIN CABIN FLOOR PANEL 143A5810-533 IAW ASA B737-800 SRM 53-00-50-2R-0 AND AIPC 53-21-51-58B.May 8, 2026 · N537AS · Boeing 737890 · Fuselage Floor PanelSDR ASAA2026050866052Floor Panel · damagedMAIN CABIN FLOOR PANEL 147A5810-123 HAS MISSING INSERTS. GROUNDED - YES. ACCOMPLISHED PERMAMENT REPAIR OF TWO (2) EA MISSING DAMAGED INSERTS IAW ASA B737-800 SRM 53-00-50-2R-0 AND AIPC 53-21-51-56.May 8, 2026 · N537AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2026050866010Door · unstableL1 DOOR UNSTABLE DURING OPENING. GROUNDED - YES. PERFORMED GVI ON L1 DOOR NO VISIBLE DEFECTS NOTIFIED SYS TEST IAW AMM 52-41-00.May 8, 2026 · N536AS · Boeing 737890 · Passenger/Crew DoorsSDR ASAA2026050866003Sign · detachedEXIT SIGN OVERHEAD 16/17 DEF FALLING OFF. GROUNDED - YES. SECURED EXIT SIGN OVERHEAD 16/17 DEF OK FOR SERVICE.May 8, 2026 · N557AS · Boeing 737890 · Emergency LightingSDR ASAA2026050766649Web · corrodedFWD CARGO SILL WEB CORRODED STA 440 TO STA 492. GROUNDED - YES. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-30-15-1A-1. REMOVED AND REPLACED SILL WEB IAW B737-800 SRM 51-40-02-0G-0W= 1.25 O= .045 R= .035 L= 3.75 D= .010.May 7, 2026 · N558AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2026050766643Transition Panel · corrodedFWD CARGO R/H TRANSITION CORRODED FROM STA 500A TO 500E. GROUNDED - YES. REMOVED AND REPLACED DAMAGED SECTION FWD CARGO R/H TRANSITION BETWEEN STA 500A TO 500E IAW B737-800 SRM 51-40-02-0G-0W 1" O .040" R .030 L 4" D .010".May 7, 2026 · N558AS · Boeing 737890 · Fuselage Main, StructureSDR ASAA2026050766642Transition Panel · corrodedFWD CARGO R/H TRANSITION CORRODED FROM STA 500F TO 500I. GROUNDED - YES. REMOVED AND REPLACED DAMAGED SECTION FWD CARGO R/H TRANSITION BETWEEN STA 500F TO 500I IAW B737-800 SRM 51-40-02-0G-0W 1" O .040" R .030" L 4" D .010".May 7, 2026 · N558AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2026050766641Transition Panel · corrodedFWD CARGO L/H TRANSITION CORRODED FROM STA 500B TO 500I. GROUNDED - YES. REMOVED AND REPALCED DAMAGED SECTION FWD CARGO L/H TRANSITION FROM STA 500B TO 500I IAW B737-800 SRM 51-40-02-0G-0W 1" O .040" R .032" L 3" D .008".May 7, 2026 · N558AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2026050766336Shield · corrodedFWD CARGO R/H AFT SHIELD CORRODED. GROUNDED - YES. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-30-15-1A-1. REMOVED AND REPLACED SHIELD IAW B737-800 SRM 51-40-02-0G-0.W: 2" O: .032" R: .025" L: 2" D: 007".May 7, 2026 · N558AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2026050765970Light · detachedFA REPORTS EXIT SIGN IN AFT GALLEY MISSING SCREWS AND HANGING BY THE WIRES. GROUNDED - YES. (RESOLVED ON W/O: 2100997 TASKCARD: N/R-00004 ) REMOVED AND REPLACED EXIT SIGN ASSEMBLY INSTALLED NEW UNIT. OPS CHECKS NORMAL. REF: AMM 33-51-01 SEAMC FELIX NOTIFIED. TMay 7, 2026 · N581AS · Boeing 737890 · Emergency LightingSDR ASAA2026050765947Power Supply · inoperativeFORWARD RT GALLEY EMERGENCY LIGHTS INOP. GROUNDED - YES. REMOVED AND REPLACED POWER SUPPLY M02816 REF AMM 33-51-06. FORWARD R/H GALLEY EMERGENCY LIGHTS OPS CHECK GOOD REF AMM 33-51-06.May 7, 2026 · N538AS · Boeing 737890 · Emergency LightingSDR ASAA2026050765946Power Supply · inoperativeLEFT HAND OVERWING EMERGENCY EXIT SIGNS ABOVE DOORS, FORWARD LEFT-HAND LOWER EXIT LIGHT AND FORWARD RIGHT-HAND LOWER EXIT LIGHT INOP. GROUNDED - YES. REMOVED AND REPLACED EMERGENCY POWER SUPPLY M1694 AND OPS CHECK GOOD IAW B737 AMM 33-51-06-960-806.May 7, 2026 · N538AS · Boeing 737890 · Emergency LightingSDR ASAA2026050666650Beam · crackedBEAM BELOW HANDLE BOX ON THE R1 DOOR IS CRACKED IN THE RADIUS NEXT TO MOUNT BOLTS MARKED WITH DOT. GROUNDED - YES. REMOVED AND INSTALLED NEW BEAM ON BELOW HANDLE BOX ON THE R1 DOOR IAW B737-800 SRM 51-40-02-0G-0.May 6, 2026 · N558AS · Boeing 737890 · Service DoorsSDR ASAA2026050666273Web · corrodedAFT CARGO DOOR THRESHOLD HAS CORROSION ON UPPER SURFACE. GROUNDED - YES. REMOVED CORROSION, EVALUATED REMAINIG THICKNESS, ORIGINAL THICKNESS .050, REMOVED .007, REMAING THICKNESS .043 FOUND TO BE OUT OF LIMITS, REMOVED AFT CARGO WEB, LOCATED AND DRILLED NEW WMay 6, 2026 · N537AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2026050465904Power Supply · faultyDURING TAKEOFF ROLL EMERGENCY LIGHTS AT R2 DOOR AND DOWNLIGHTS UNDER OVERHEAD BINS AT 28C AND 30C CAME ON AND STAYED ON FOR ABOUT ONE MINUTE. GROUNDED - YES. PER WDM 33-51-14 ALL AFFECTED LIGHTS GO TO THE M1672 EMERGENCY BATTERY POWER SUPPLY. INSP OF P/S SHOWEMay 4, 2026 · N532AS · Boeing 737890 · Emergency LightingSDR ASAA2026050365872Lamp · inoperativeL1 EXIT PATH LIGHT INOP. GROUNDED - YES. RELAMPED L1 EXIT PATH LIGHT . REF AMM 33-51-00. OPS CHECK GOOD.May 3, 2026 · N548AS · Boeing 737890 · Emergency LightingSDR ASAA2026043065810Rib · crackedR1 DOOR LOWER CENTER RIB BY THE HANDLE HOUSING ATTACH BOLTS RADIUS APPEARS TO BE CRACKED. GROUNDED - YES. REMOVED & REPLACE R1 DOOR LOWER CENTER RIB BEAM IAW B737-800 SRM 51-40-02-0G-0.Apr 30, 2026 · N527AS · Boeing 737890 · Passenger/Crew DoorsSDR ASAA2026042865806Transition Panel · corrodedFWD CARGO LT SIDE TRANSITION PANEL STA 500B+10 TO 500G+10 IS CORRODED. GROUNDED - YES. REMOVED THE CORROSION FROM THE FWD PIT L/H TRANSITION PANEL AT STA 500B+10 TO 500G+10 IAW B737-800 SRM 53-00-53-1A-2.4(2) ORIG THICKNESS IS .040" IAW B737-800 SRM 53-30-53-0Apr 28, 2026 · N528AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2026042165876Mount · corrodedPASSENGER CABIN STA 916.5 LBL 51.55 DUAL FLOOR MOUNT ATTACHING INTERCOSTAL HAS CORROSION AROUND MOUNT. GROUNDED - YES. REMOVED AND REPLACED 147A5690-8 INTERCOSTAL IAW BAC DWG 147A5680 REV - AND B737-800 SRM 51-40-02. ALLOWABLE LIMITS IN SRM FOUND DEEMED OUT OFApr 21, 2026 · N597AS · Boeing 737890 · Fuselage, Equipment Attach FittingsSDR ASAA2026042065603Fire Detector · malfunctionedMOMENTARY WHEEL WELL FIRE WARNINGS ON CLIMBOUT. GOT BELL, MASTER FIRE, AND WW FIRE INDICATION. NO MASTER CAUTION. GROUNDED - YES. AFTER CREW CONSULT WHEEL WELL WARNING WAS ONLY MOMENTARY THEN EXTINGUISHED PERFORMED BITE CHECK OF OVERHEAT DETECTOR CONTROL MODUApr 20, 2026 · N557AS · Boeing 737890 · Fire DetectionSDR ASAA2026041765554Power Supply · inoperativeEMERGENCY LIGHTS ASSOCIATED WITH POWER SUPPLY M1676 ARE INOP. GROUNDED - YES. REMOVED AND REPLACED POWER SUPPLY M1676 S/N 0644 AND TEST PASSED IAW B737-800 AMM 33-51-06-960-806.Apr 17, 2026 · N586AS · Boeing 737890 · Emergency LightingSDR ASAA2026041765553Power Supply · inoperativeEMERGENCY LIGHTS ASSOCIATED WITH POWER SUPPLY M2335 ARE INOP. GROUNDED - YES. REMOVED AND REPLACED POWER SUPPLY M2335 S/N 15801 AND TEST PASSED IAW B737-800 AMM 33-51-06-960-806.Apr 17, 2026 · N586AS · Boeing 737890 · Emergency LightingSDR ASAA2026041665820Intercostal · crackedPASS CABIN, FWD WET AREA, INTERCOSTAL BETWEEN STA 360-344 IS DAMAGED. GROUNDED - YES. REMOVED AND REPLACED PASS CABIN, FWD WET AREA INTERCOSTAL BETWEEN STA 360-344 I.A.W. B737-800 SRM 51-40-02-06-0.Apr 16, 2026 · N527AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2026041665571Light · detachedFWD OVERHEAD EMERGENCY EXIT PLASTIC COVER KEEPS FALLING OFF. GROUNDED - YES. REPLACED FOWARD EXIT SIGN LIGHT ASSEMBLY PER AMM 33-51-01. LIGHT ASSEMBLY OP CHECKS GOOD.Apr 16, 2026 · N588AS · Boeing 737890 · Emergency LightingSDR ASAA2026041265945Cargo Track · corrodedAFT PIT CARGO TRACK HAS CORROSION IB OF DOOR AT STA 787-827. GROUNDED - YES. REPLACED AFT PIT CARGO TRACK I/B OF DOOR AT STA 787-827 IAW B737-800 SRM 53-00-53-2R-3W- 1" O- .070" R- .040" L- 2" D- .030".Apr 12, 2026 · N527AS · Boeing 737890 · Fuselage, Seat/Cargo Attach FittingsSDR ASAA2026041265944Support · corrodedFWD PIT LOWER AFT BULKHEAD SUPPORT R/H IS CORRODED. GROUNDED - YES. REMOVED AND REPLACED FWD PIT LOWER AFT BULKHEAD SUPPORT R/H I.A.W. B737-800 SRM 51-40-02-0G-0 STEP 4.B AND 7.C.Apr 12, 2026 · N527AS · Boeing 737890 · Fuselage Main, StructureSDR ASAA2026041265943Support · corrodedFWD PIT LOWER L/H AFT BULKHEAD SUPPORT IS CORRODED. GROUNDED - YES. REMOVED AND REPLACED FWD PIT LOWER L/H AFT BULKHEAD SUPPORT I.A.W. B737-800 SRM 51-40-02-0G-0 STEP 4.B AND 7.C.Apr 12, 2026 · N527AS · Boeing 737890 · Fuselage Main, StructureSDR ASAA2026041265822Support · corrodedFWD PIT LOWER AFT BULKHEAD SUPPORT MIDDLE PIECE IS CORRODED. GROUNDED - YES. REMOVED AND REPLACED FWD PIT LOWER AFT BULKHEAD SUPPORT MIDDLE I.A.W. B737-800 SRM 51-40-02-0G-0 STEP 4.B AND 7.CW- 1" O- .063" R- 0" L- 2" D- .063".Apr 12, 2026 · N527AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2026041265821Web · crackedFWD PIT SILL WEB HAS CORROSION. GROUNDED - YES. REMOVED AND REPLACED FWD PIT SILL WEB IAW B737-800 SRM 51-40-02-0G-0W: 1" O: .045" R: .039" L: 2" D: .006".Apr 12, 2026 · N527AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2026041265813Web · corrodedAFT PIT SILL WEB HAS CORROSION. GROUNDED - YES. REMOVED AND REPLACED AFT PIT SILL WEB IAW B737-800 SRM 51-40-02-0G-0W: 1" O: .050" R: .043" L: 2" D: .007.Apr 12, 2026 · N527AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2026041265812Plate · corrodedFWD PIT SIDEPLATE R/H SIDE IS CORRODED AT STA 500A-500I. GROUNDED - YES. REMOVED AND REPLACED FWD PIT SIDEPLATE R/H SIDE AT STA 500A-500I IAW BOEING 737-800 SRM 53-00-53-2R-5W: 1" OT: 0.040" RT: 0.032 L: 2" D: 0.008".Apr 12, 2026 · N527AS · Boeing 737890 · Fuselage Main, StructureSDR ASAA2026041265811Plate · corrodedFWD PIT LT SIDEPLATE HAS CORROSION AT STA 500H-500I. GROUNDED - YES. REMOVED AND REPLACED FWD PIT L/H SIDEPLATE STA 500H-500I. IAW B737-800 SRM 51-40-02-0G-0W 1" O .040 R .036 L 2" D .014.Apr 12, 2026 · N527AS · Boeing 737890 · Fuselage Main, StructureSDR ASAA2026041265809Plate · corrodedAFT PIT SIDEPLATE RT SIDE AT STA 727G TO 767 HAS CORROSION. GROUNDED - YES. REMOVED & REPLACE AFT PIT SIDEPLATE R/H SIDE AT STA 727G TO 767 IAW B737-800 SRM 51-40-02-0G-0W 1 1/2 O .040 R .020 L 1 1/2 D .020.Apr 12, 2026 · N527AS · Boeing 737890 · Fuselage Main, StructureSDR ASAA2026041265808Plate · corrodedAFT PIT L/H SIDEPLATE HAS CORROSION AT STA 727-747. GROUNDED - YES. REMOVED AND REPLACED AFT PIT L/H SIDEPLATE FROM STA 727 TO 747 IAW BOEING SRM 53-00-53-2R-5WI: 1" OT: 0.040" RT: 0.027" L: 0.013" D: 0.007".Apr 12, 2026 · N527AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2026040965745Shield · corrodedMULTIPLE SPOTS OF CORROSION ON THE SHIELD ON THE RIGHT HAND SIDE OF THE AFT CARGO PIT BETWEEN STATIONS 767 AND 787,18 INCHES FROM THE BUTT LINE. GROUNDED - YES. REMOVED CORROSION FROM THE AFT PIT, FWD SHIELD FROM STA 767 TO 787 IAW B737-800 SRM 53-60-15-1A-1.2Apr 9, 2026 · N528AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2026040865805Transition Panel · corrodedFWD CARGO LH SIDE TRANSITION PANEL STA 500G+10 TO 500I IS CORRODED. GROUNDED - YES. REMOVED THE CORROSION FROM THE FWD PIT L/H TRANSITION PANEL AT STA 500G+10 TO 500I IAW B737-800 SRM 53-00-53-1A-2.2.D. ORIG THICKNESS IS .040" IAW B737-800 SRM 53-30-53-01-2 TAApr 8, 2026 · N528AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2026040865725Transition Panel · corrodedMULTIPLE SPOTS OF CORROSION ON THE RIGHT HAND TRANSITION STRAP IN THE AFT CARGO PIT BETWEEN STATIONS 727B AND 767. GROUNDED - YES. UPON EVALUATION 100% MATERIAL LOSS FOUND THROUGHOUT THE RH AFT PIT TRANSITION PANEL FROM STA 727B TO 767, AND IS OUT OF LIMITS IAApr 8, 2026 · N528AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2026040865724Transition Panel · corrodedFWD CARGO RT SIDE TRANSITION PANEL STA 500G+10 TO 500I IS CORRODED. GROUNDED - YES. REMOVED CORROSION FROM FWD PIT R/H TRANSITION PANEL AT STA 500G+10 TO 500I IAW B737-800 SRM 53-00-53-1A-2.2.D. ORIG THICKNESS IS .040" IAW B737-800 SRM 53-30-53-01-2. TABLE 2 RApr 8, 2026 · N528AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2026040865644Floor Support · corrodedCORROSION ON THE STRINGER ON THE RIGHT HAND SIDE OF THE AFT CARGO PIT BETWEEN STATIONS 767 AND 787 12 INCHES FROM THE BUTT LINE. GROUNDED - YES. REMOVED CORROSION FROM THE AFT PIT FLOOR RAIL AT STA 772, RBL 13.84 IAW B737-800 SRM 53-00-53-1A-2.2.D ORIG THICKNEApr 8, 2026 · N528AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2026040865640Channel · corrodedMULTIPLE SPOTS OF CORROSION ON THE LEFT HAND TRANSITION STRAP IN THE AFT CARGO PIT BETWEEN STATIONS 787 AND THE FORWARD BULKHEAD. GROUNDED - YES. REMOVED CORROSION FROM THE L/H AFT PIT TRANSITION PANEL AT STA 787 TO FWD BULKHEAD IAW B737-800 SRM 53-00-53-1A-2.Apr 8, 2026 · N528AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2026040765726Web · corrodedAFT CARGO DOOR CUTOUT SUB SCUFF PLATE STRUCTURE HAS MULTIPLE SPOTS OF CORROSION. GROUNDED - YES. REMOVED CORROSION FROM THE AFT PIT DOOR CUT OUT LOWER WEB. ORIG MATERIAL WAS .045" IAW B737-800 SRM 53-60-15-01-1. REMOVED .019", REMAINING IS .26" AND IS FOUND TOApr 7, 2026 · N528AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2026040765490Transition Panel · corrodedAFT CARGO L/H TRANSITION CORRODED STA 727G-10 TO 727J+5. GROUNDED - YES. REMOVED DAMAGE FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-00-53-1A-2, REMOVED AND REPLACED L/H TRANSITION IAW B737-800 SRM 53-00-53-2R-5. W= 2 O= .040 R= .000 L= 1 D= .040.Apr 7, 2026 · N532AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2026040765487Transition Panel · corrodedFWD CARGO LT TRANSITION CORRODED STA 500H TO 500I. GROUNDED - YES. REMOVED DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. FABRICATED, LOCATED AND DRILLED NEW FWD CARGO L/H TRANSITION STA 500 4 TO 5 IAW SRM 53-00-53-2R-5. W: 2 O: .040 R: .033 L: 1 D: Apr 7, 2026 · N532AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2026040665524Stop Fitting · gougedWHILE PERFORMING AFT ENTRY DOOR HEALTH CHECK FOUND STOP PIN FITTING GAUGED AT TOP FWD CORNER. SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY "A" MINOR REPAIR TO AFT ENTRY DOOR P/N 147A6116-26 S/N 002595 UPPRER FWD DOOR STOP FITTING P/N 147A6128-53 IAW EA 800-Apr 6, 2026 · N596AS · Boeing 737890 · Passenger/Crew DoorsSDR ASAA2026040665482Skin · crackedRIGHT HORIZONTAL STAB LOWER SKIN IS CRACKED AT THE I/B SIDE OF RIB # 10 STA166.30 INLINE WITH THE DRAIN HOLE.262A001. GROUNDED - YES. REPAIRED RIGHT HORIZONTAL STAB LOWER SKIN IAW B737-800 SRM 55-10-01-2R-11.Apr 6, 2026 · N516AS · Boeing 737890 · Horizontal Stabilizer, Plate/SkinSDR ASAA2026040565340Battery Pack · inoperativeEMERGENCY LIGHT AT RIGHT HAND SIDE BETWEEN ROWS 19-24 AND OVERWING AFT AND BEHIND WING FAILED CAPACITY TEST. SRXR430X. GROUNDED - YES. REMOVED AND REPLACED BATTERY PACK EMERGENCY LIGHT AT RIGHT HAND SIDE BETWEEN ROWS 19-24 AND OVERWING AFT AND BEHIND WING (M16Apr 5, 2026 · N596AS · Boeing 737890 · Emergency LightingSDR ASAA2026040465642Stub Beam · gougedL1 DOOR UPPER STUB BEAM GOUGED. GROUNDED - YES. REMOVED DAMAGED STUB BEAM AND INSTALLED NEW STUB BEAM IAW B737-800 SRM 51-40-02, BAC DWG#141A6260 REV B AND BAC DWG#141A6143 REV-.Apr 4, 2026 · N528AS · Boeing 737890 · Passenger/Crew DoorsSDR ASAA2026040465641Stop Fitting · out of limitsR2 DOOR FWD UPPER STOP FITTING GOUGED BS. GROUNDED - YES. BLENDED DAMAGED AREA FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED UPPER FWD STOP FITTING IAW BAC DWG 147A6502 REV A AND REV F, B737-800 SRM 51-40-02 AND APPLIED TOPCOAT IAW B737-800 AMM 51-21-99.Apr 4, 2026 · N528AS · Boeing 737890 · Passenger/Crew Doors
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