N127DU

Service difficulty reports · 46

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N127DU' AND registry_match = 'registration'
  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 DALA2025080705927Skin · gougedAFT SERVICE DOOR- EXTERIOR SKIN HAS 2 SMALL GOUGES AT THE DOOR HANDLE CUTOUT FROM THE HANDLE CONTACTING THE SKIN. "M" SEE PIC. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0819:5246-2004/002 00275 REPAIRED PER PRIS Aug 4, 2025 · N127DU · Airbus BD5001A10 · Service DoorsSDR DALA2025072905701Door Sill · corrodedAIRCRAFT AFT SERVICE DOOR SILL, BOLT HOLE #4 HAS CORROSION EMITTING FROM IT. (P)(M). SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0546:5360-2024/002 00539 REMOVED AND REPLACED FORWARD CORNER STRIKER REF A220 ASRP 52-42-21. (LP# 1112326)Jul 29, 2025 · N127DU · Airbus BD5001A10 · Fuselage Main, StructureSDR DALA2025072905697Duct · damagedAPU HIGH PRESSURE BLEED DUCT HAS PLY SEPARATION AT FIRE LOOP STANDOFF, 10 INCHES FWD OF FRAME 85. PER AMDS, REQUIRES CUSTOMER RESPONSE CENTER NOTIFICATION. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 066-0001:3610-2002Jul 24, 2025 · N127DU · Airbus BD5001A10 · APU Bleed Air SystemSDR DALA2025072205496Seat Track · corrodedREAR BARREL SEAT TRACKS. AT LH FR 71 IB MULTIPLE AREAS OF CORROSION ON THE SEAT TRACK. REPLACED SEAT TRACK REF. A220 ASRP 51-42-00 AND A220 DWG C01342700. (LP# 1095019)Jul 20, 2025 · N127DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025072205495Seat Track · corrodedREAR BARREL SEAT TRACKS. AT LH FR 71 OB MULTIPLE AREAS OF CORROSION ON THE SEAT TRACK (M). REPLACED SEAT TRACK REF. A220 DWG C01342700 AND A220 ASRP 51-42-00. (LP# 1095032)Jul 20, 2025 · N127DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025072205494Seat Track · corrodedREAR BARREL SEAT TRACKS. AT RH FR 71 OB MULTIPLE AREAS OF CORROSION ON THE SEAT TRACK (M). REPLACED SEAT TRACK REF. A220 ASRP 51-42-00 AND A220 DWG C01342700.Jul 20, 2025 · N127DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025072205493Seat Track · corrodedREAR BARREL SEAT TRACKS. AT RH FR 71 IB MULTIPLE AREAS OF CORROSION ON THE SEAT TRACK (M). SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0584:5300-2015/002 00502 REPLACED SEAT TRACK REF. A220 DWG C01342700 AND A220 AJul 19, 2025 · N127DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025070104903Slide · no discrepancyLH OWEED SLIDE REQUIRES DEPLOYMENT REF AMDS 2561-9101. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0402:2561-9101/001 00003 DEPLOYED SLIDE PER AMDS 2561-9005 STEP 1-4. SLIDE INSTALL WILL BE COMPLETED ON THE REMAINDJun 26, 2025 · N127DU · Airbus BD5001A10 · Escape SlideSDR DALA2025070104895Slide · no discrepancyRH OWEED SLIDE REQUIRES DEPLOYMENT REF AMDS 2561-9101. DEPLOYED SLIDE PER AMDS 2561-9006 STEP 1-4. SLIDE INSTALL WILL BE COMPLETED ON THE REMAINDER OF AMDS 2561-9006. (LP# 1047913)Jun 26, 2025 · N127DU · Airbus BD5001A10 · Escape SlideSDR DALA2024121111657Light · inoperativeRT EXTERNAL REAR EMERGENCY LIGHT INOP. REMOVED AND REPLACED R/H AFT EXTERNAL LIGHT ASSEMBLY. OPS CHECKS GOOD REF A220 AMP 33-55.Dec 8, 2024 · N127DU · Airbus BD5001A10 · Emergency LightingSDR DALA2024120511474Fan · abnormalRECIRC AIR FAIL MSG DURING ENG START FA IN AFT GALLEY REPORTED ELECTRICAL SMELL AT SAME TIME. R/R BOTH RECIRC FILTERS PER A220 AMP 21-22-03. REMOVED RECIRC FAN PER A220 AMP 21-22-01. INSTALLED PER A220 AMP 21-22. NO HELP. T/S PER EFIM INSTALLED DCM 1A SLOT 567Dec 1, 2024 · N127DU · Airbus BD5001A10 · Air Distribution FanSDR DALA2024082208371Slat Track · corrodedRH SLAT TRACK NUMBER 4 PINION TEETH (2EA) HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-010287-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 21AUG24 2157 UTC 02 CORR BY MUNOZ 02379974 IAH 21AUG24 ATA 5742 Aug 21, 2024 · N127DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024082208370Slat Track · corrodedRH SLAT TRACK NBR 4 UPPER AFT I/B SIDE HAS EVIDENCE OF A ROLLER WEAR MARK WITH REWORK REF 5742-01028-02B. MEASUREMENT DEPTH IS 0.011", OUTSIDE OF SPECIFIED RESTRICTIONS. LIAISON ENGINEERING WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED RH SLAT TRACK #4 UPPEAug 21, 2024 · N127DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024082208369Slat Track · corrodedRH SLAT TRACK NUMBER 4 RACK TEETH (2EA) HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 21AUG24 2204 UTC 02 CORR BY MUNOZ 02379974 IAH 21AUG24 ATA 5742 RIIAug 21, 2024 · N127DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2025070204956Tape · peelingLH WINGLET TIP LEADING EDGE EROSION TAPE FOUND PEELED UP. REQUIRES REPAIR. INSPECTED LH WINGLET TIP L E WHERE EROSION TAPE WAS DAMAGED & FOUND NO UNDERLYING DAMAGE. TRIMMED OFF EXCESS EROSION BOOT MATERIAL TO MEET AERODYNAMIC SMOOTHNESS IAW ASRP 55-32-01-01AAAAug 19, 2024 · N127DU · Airbus BD5001A10 · Wing Miscellaneous StructureSDR DALA2024052805555Landing Gear · faultedSHIP 8127 - MISC/DE - DECLARED EMERGENCY DUE TO GEAR FAIL MSG. CREW DID RECEIVE ALL 3 GEARS DOWN AND LOCKED INDICATING GREEN. FLIGHT LANDED SAFELY. CORRECTIVE ACTION: R/R LGCL PER A220 AMP 32-31-07. PERFORMED ALTERNATE GEAR EXTENSION CHECK ON LGSCU 1A AND 2A PMay 23, 2024 · N127DU · Airbus BD5001A10 · Landing Gear Retraction/Extension SystemSDR DALA2025070805079Tape · peelingON WALK AROUND FOUND VERT STAB EROSION TAPE PEELED. GVI OF PAINT OK. FWD TO MON IAW A220 ASRP 55-32-01-01AAA-662A-A FOR 8500 FLT HRS. GVI DUE IN 850 FLT HRS. PERFORMED GVI IAW A220 ASRP 51-10-01-01AAA- 018A-A. NO FURTHER DEFECTS FOUND. OK TO CONT. ON MON.REMOVMar 10, 2024 · N127DU · Airbus BD5001A10 · Vertical StabilizerSDR DALA2024010310787Unknown · unknownL/H SLAT TRACK NBR 10 LOWER SURFACE HAS EVIDENCE OF CORROSION & PREVIOUS REWORK. REF AA6742-01028-02A. LIAISON ENGINEERING WILL. REPAIRED L/H SLAT TRACK NBR 10 LOWER SURFACE PER ER/A 607781- 14AD REV A AND PRI REV 0. (LP# 0131986)Dec 30, 2023 · N127DU · Bombdr BD1001A10 · Leading Edge DevicesSDR DALA2024010310786Unknown · unknownL/H SLAT TRACK NBR 1 UPPER SURFACE HAS EVIDENCE OF CORROSION & NO EVIDENCE OF PREVIOUS REWORK REF AA 5742-01028-02A LIASON ENGINEERING SUPPORT WILL BE REQ'D BEFORE FURTHER FLT. REPAIRED L/H SLAT TRACK NBR 1 UPPER SURFACE PER ER/A 607781-14AD REV A AND PRI REV Dec 30, 2023 · N127DU · Bombdr BD1001A10 · Leading Edge DevicesSDR DALA2024010310785Unknown · unknownL/H SLAT TRACK # 7 LOWER AFT SURFACE HAS WEAR AND PREVIOUSLY REWORK. REF AA5742-01028-02A. LIASON ENGINEERING WILL BE REQ'D BEFORE FURTHER FLT. REPAIRED L/H SLAT TRACK NBR 7 LOWER AFT SURFACE PER ER/A 607781- 14AD REV A AND PRI REV 0. (LP# 0131992)Dec 30, 2023 · N127DU · Bombdr BD1001A10 · Leading Edge DevicesSDR DALA2024010310784Unknown · unknownL/H SLAT TRACK NBR 8 UPPER SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF AA 5742-01028-02A. LIASON ENGINEERING SUPPORT WILL BE REQ'D BEFORE FURTHER FLT. REPAIRED LH SLAT TRACK NBR 8 UPPER SURFACE PER ER/A 607781-14AD REV A AND PRI REV 0. (LP# 0131Dec 30, 2023 · N127DU · Bombdr BD1001A10 · Leading Edge DevicesSDR DALA2024010310783Unknown · unknownL/H SLAT TRACK NBR 7 UPPER SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA 5742-01028-02A. LIASON ENGINEERING SUPPORT WILL BE REQ'D BEFORE FURTHER FLT. REPAIRED L/H SLAT TRACK NBR 7 UPPER SURFACE PER ER/A 607781-14AD REV A AND PRI REV 0. (LP# 0131Dec 30, 2023 · N127DU · Bombdr BD1001A10 · Leading Edge DevicesSDR DALA2024010310782Unknown · unknownL/H SLAT TRACK NBR 2 UPPER SURFACE HAS EVIDENCE OF CORROSION NO EVIDENCE OF PREVIOUS REWORK REF AA 5742-01028-02A LIASON ENGINEERING SUPPORT WILL BE REQ'D BEFORE FURTHER FLT. REPAIRED L/H SLAT TRACK NBR 2 UPPER SURFACE PER ER/A 607781-14AD REV A AND PRI REV 0.Dec 30, 2023 · N127DU · Bombdr BD1001A10 · Leading Edge DevicesSDR DALA2024010310781Unknown · unknownR/H SLAT TRACK NBR 6 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION WITH PREVIOUS RE-WORK. REF. 5742-01028-02B LIASON ENGINEERING SUPPORT WILL BE REQ'D BEFORE FURTHER FLT. REPAIRED RH SLAT TRACK NDR 6 UPPER AFT SURFACE PER ER/A 607782- 14AD REV B AND PRI REV 0. (Dec 30, 2023 · N127DU · Bombdr BD1001A10 · Leading Edge DevicesSDR DALA2024010310780Unknown · unknownR/H SLAT TRACK NBR 10 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION WITH PREVIOUS REWORK REF. 5742-01028-02B LIASON ENGINEERING SUPPORT WILL BE REQ'D BEFORE FURTHER FLT. REPAIRED RH SLAT TRACK #10 UPPER AFT SURFACE PER ER/A 607782- 14AD REV B AND PRI REV 0. (LP#Dec 30, 2023 · N127DU · Bombdr BD1001A10 · Leading Edge DevicesSDR DALA2023051203780Unknown · unknownWET SOCK SMELL NOTICED FROM PAX & CREW. C/W A220 NO-GO ODI 21-72. C/W W/C 0550-2001 +0550-6001. REF LOG 4086590 FOR FINDINGS. WHILE PERFORMING B.S.I. ON #2 ESN 736235 IAW AMDS 0550-6001 STEP (8), FOUND EVIDENCE OF OIL WETNESS @ HPC VARIABLE INLET GUIDE VANES. May 11, 2023 · N127DU · Bombdr BD1001A10 · Air Conditioning SystemSDR DALA2023041102849Unknown · unknownAIRCRAFT 8127, AD/ERA REQUIRES L/H WING SLAT RIGGING PER AMP 27-81-17, AND THE "SLAT CONTOUR CHECK" AS DESCRIBED IN OPTION #2. CORRECTIVE ACTION: ACCOMPLISHED L/H WING SLAT RIGGING PER A220 AMP 27-81-17, AND THE "SLAT CONTOUR CHECK" AS DESCRIBED IN OPTION #2. Apr 8, 2023 · N127DU · Bombdr BD1001A10 · Leading Edge DevicesSDR DALA2023041102848Unknown · unknownAIRCRAFT 8127, AD/ERA REQUIRES R/H WING SLAT RIGGING PER AMP 27-81-17, AND THE "SLAT CONTOUR CHECK" AS DESCRIBED IN OPTION #2. CORRECTIVE ACTION: ACCOMPLISHED L/H WING SLAT RIGGING PER A220 AMP 27-81-17 AND ERA 607782 AND THE "SLAT CONTOUR CHECK" AS DESCRIBED Apr 8, 2023 · N127DU · Bombdr BD1001A10 · Leading Edge DevicesSDR DALA2023041102847Unknown · unknownAIRCRAFT 8127, ERA 607781-14AD SECTION I ISSUED FOR REPAIR TO LH SLAT TRACKS FOLLOW ON ACTION REQUIRED. CORRECTIVE ACTION: ERA 607781-14AD REV O SECTION I COMPLETED FOR L/H SLAT TRACK CORROSION REWORK. (TIME LIMITED REPAIR) RII STEP 3 WAS ACCOMPLISHED. (LP 270Apr 8, 2023 · N127DU · Bombdr BD1001A10 · Wing StructureSDR DALA2023020300859Not Entered · not enteredSHIP 8127 - DIV - TO LIT DUE TO "R ELEVATOR FAIL" CAUTION MESSAGE. CORRECTIVE ACTION: REPLACED #3 REU. (LP# 9432468)Feb 1, 2023 · N127DU · Bombdr BD1001A10 · Flight Control SystemSDR DALA2022110807220Hinge Bracket · crackedR/H HORIZONAL /ELEVATOR HINGE BRACKET # 3 CRACKED IN LWR AFT CORNER IN RADIUS.SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0260:2090-2039-RH/ 003 00114 COMPLIED WITH ER/A PRI 603293-14 REV. 1 AND FINAL ERA 603293-14 REV. ORIGINAL. C/W ERA PRI 603293-14 REV ORNov 5, 2022 · N127DU · Bombdr BD1001A10 · Horizontal Stabilizer, Spar/RibSDR DALA2022110807219Hinge Bracket · crackedR/H HORIZONAL /ELEVATOR HINGE BRACKET # 2 CRACKED IN LWR AFT CORNER IN RADIUS.SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0260:2090-2039-RH/ 002 00113 COMPLIED WITH ER/A PRI 603292-14 REV. 1 AND FINAL ERA 603292-14 REV. ORIGINAL. C/W PRI 603292-14 REV ORIGINNov 5, 2022 · N127DU · Bombdr BD1001A10 · Horizontal Stabilizer, Spar/RibSDR DALA2022110407168Frame · corrodedAIRCRAFT 8127, UPPER CORNER OF FRAME 75 HAS CORRODED SPOT FORWARD OF WASTE BOX. CORRECTIVE ACTION: REPLACED WASTE BOX PAN, INBD HINGE FITTINGS, INBD HINGE ARM FITTINGS, AND REMOVED CORROSION ON WASTE B=DOOR DOUBLER PER ER/A 603257-14. LP 2481206Nov 3, 2022 · N127DU · Bombdr BD1001A10 · Fuselage Main, FrameSDR DALA2022110407167Pan · corrodedAIRCRAFT 8127, CORROSION FOUND ON FORWARD EDGE OF LAV PAN, 2 LOCATIONS. CORRECTIVE ACTION: REPLACED WASTE BOX PAN, INBD HINGE FITTINGS, INBD HINGE ARM FITTINGS, AND REMOVED CORROSION ON WASTE B=DOOR DOUBLER PER ER/A 603257-14. LP 2481199Nov 3, 2022 · N127DU · Bombdr BD1001A10 · Fuselage Miscellaneous StructureSDR DALA2022110407166Access Door · corrodedAIRCRAFT 8127, CORROSION FOUND ON FWD EDGE OF LAV WASTE SERVICE DOOR (146 BR). CORRECTIVE ACTION: REPLACED WASTE BOX PAN, INBD HINGE FITTINGS, INBD HINGE ARM FITTINGS, AND REMOVED CORROSION ON WASTE B=DOOR DOUBLER PER ER/A 603257-14. LP 2481194Nov 3, 2022 · N127DU · Bombdr BD1001A10 · Fluid Service DoorsSDR DALA2022110407165Hinge · corrodedAIRCRAFT 8127, BOTH HINGES ON LAV WASTE SERVICE DOOR (146 BR) CORRODED. CORRECTIVE ACTION: REPLACED WASTE BOX PAN, INBD HINGE FITTINGS, INBD HINGE ARM FITTINGS, AND REMOVED CORROSION ON WASTE B=DOOR DOUBLER PER ER/A 603257-14. LP 2481191Nov 3, 2022 · N127DU · Bombdr BD1001A10 · Fuselage, Door HingeSDR DALA2022110407164Pan · corrodedAIRCRAFT 8127, SEVERAL AREAS CORRODED ON LAV PAN WASTE BOX (MARKED). CORRECTIVE ACTION: REPLACED WASTE BOX PAN, INBD HINGE FITTINGS, INBD HINGE ARM FITTINGS, AND REMOVED CORROSION ON WASTE B=DOOR DOUBLER PER ER/A 603257-14. LP 2481177Nov 3, 2022 · N127DU · Bombdr BD1001A10 · Fuselage Miscellaneous StructureSDR DALA2022110407163Doubler · corrodedAIRCRAFT 8127, CORROSION FOUND ON FWD SECTION OF THE WASTE ACCESS INTERNAL DOUBLER. CORRECTIVE ACTION: REPLACED WASTE BOX PAN, INBD HINGE FITTINGS, INBD HINGE ARM FITTINGS, AND REMOVED CORROSION ON WASTE B=DOOR DOUBLER PER ER/A 603257-14. LP 2481175Nov 3, 2022 · N127DU · Bombdr BD1001A10 · Fluid Service DoorsSDR DALA2023022801499None · noneERA 603257-14AD SECTION I ACCOMPLISHED IN MSPDURING C CHECK TO THE WASTE BOX AREA. FOLLOW ON ACTION IS REQUIRE. ACCOMPLISH ERA 603257-14AD SECTION II EVERY 850 FH AFTER SECTION I ACCOMPLISHMENT.ERA 603257-14AD SECTION I REPAIR IS ACCEPTABL E FOR 8500 FH. FURTHNov 1, 2022 · N127DU · Bombdr BD1001A10 · Fuselage Internal Mounting StructureSDR DALA2021091505503Radome · damagedRADOME REPAIR PER ERA 588183-14. RADOME SKIN/CORE REPAIRED PER ERA 588183-14. REPETITIVE INSPECTION PER ERA 588183-14 SECTION II REQUIRED EVERY 850 HRS UNTIL ACCOMPLISHMENT OF PERMANENT REPAIR PER SECTION III AT 8500 HRS. ASSOCIATED ER/A 14-588183 ADDED. (LP# Sep 10, 2021 · N127DU · Airbus BD5001A10 · Aerodynamic FairingsSDR DALA2020101903384Bottle · low pressureDURING SVC CK FOUND L2 DOOR EOAM PRESSURE LOW. SERVICED L2 DOOR EOAM PER A220 AMP 52-11. C/W RII VERIFIED DOOR SAFTY PIN STOWED PER A220 AMP 52-11.Oct 19, 2020 · N127DU · Bombdr BD1001A10 · Emergency EquipmentSDR DALA2020101903385Bottle · low pressureL1 DOOR EOAM IN YELLOW. SERVICED L1 DOOR EOAM PER A220 AMP 52-11. OK FOR SVC. C/W RII. VERIFIED DOOR SAFTY PIN STOWED PER A220 AMP 52-11.Oct 17, 2020 · N127DU · Bombdr BD1001A10 · Emergency EquipmentSDR DALA2020020430875Bottle · low pressureL-1 DOOR EOAM PSI BELOW MINIMUMS. ACTUATOR SAFETY PIN INSTALLED FOR MAINT. SERVICED L-1 DOOR EOAM ACTUATOR PER A220 AMP 52-11. COMPLIED WITH RII REQUIREMENTS PER A220 AMP BD500-A-J52-11-08-01AAA-214A-A. VERIFIED L1 DOOR ASSIST ACTUATOR REARMED AND SAFETY PIN RJan 31, 2020 · N127DU · Bombdr BD1001A10 · Emergency EquipmentSDR DALA2020012870629Damper · low pressureL1 DOOR EOAM FORWARD PASSENGER DOOR DAMPER IS IN THE RED BAND REQUIRES RII AND SERVICING. SERVICED PASSENGER ENTRY DOOR L1 EOAM I.A.W CE SERIES AMP TASK BD500-A-J52-12-08-01AAA-21A-A. SERVICED TO GREEN BAND. (LP# 6527185)Jan 27, 2020 · N127DU · Airbus BD5001A10 · Passenger/Crew DoorsSDR DALA2020012800631Fairing · crackedDURING A CHECK FOUND BELLY FAIRING CRACKED AT MID E&E ACCESS DOOR. REMOVED LONGERON PER AMP 53-82. INSTALLED LONGERON TO AFT WTBF LH SUPPORT STRUCTURE P/N C02383111-0010DL PER ERA 583461-14 AND ASRP C SERIES 51-42 THIS IS PERMANENT REPAIR. (LP# 6527164)Jan 22, 2020 · N127DU · Airbus BD5001A10 · Aerodynamic FairingsSDR DALA2019110206394B-Nut · loose#2 ENG FIRE EXTINGUISHING HOSE B NUT LOSE AND TORQUE STRIPE BROKEN ON ENGINE CONNECTING SIDE OF THE HOSE. REPLACE HOSE ACCORDING TO AD RELATED TASK CARD 2620-01223-01B. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 024-0Nov 2, 2019 · N127DU · Bombdr BD1001A10 · Extinguishing System
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