N136DQ

Service difficulty reports · 55

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 = 'N136DQ' 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 DALA2026041002301Heater · odorDIVERTED TO OAK DUE TO DIRTY SOCK SMELL. DECLARING AN EMERGENCY. DEFERRED AFT GALLEY FAN AND GALLEY HEATER. LATER, AFT GALLEY HEATER WAS REPLACED. (LP 7963269, 7963271 - AIRCRAFT WAS GROUNDED)Apr 8, 2026 · N136DQ · Airbus BD5001A10 · Heating SystemSDR DALA2026031801872Skin · puncturedPUNCTURE TO LH SIDE FUSELAGE SKIN BETWEEN FR69-FR70 AND BETWEEN STR 33L AND 34L. REPAIRED DAMAGE SKIN ON L/H SIDE FUSELAGE BETWEEN FR69-FR70 AND BETWEEN STR 33L AND 34L PER ER/A# 633137-14AD REV-ORIGINAL. ASSOCIATED ER/A 14-633137 ADDED FOR AC 8136. (LP# 14956Mar 15, 2026 · N136DQ · Airbus BD5001A10 · Fuselage Main, Plate/SkinSDR DALA2026031701847Doubler · corrodedWHILE PERFORMING DVI OF ER/A 610625-14 REV ORIGINAL SECTION II OF CC JOB#136-2882877 CORROSION WAS FOUND AT INTERNAL DOUBLER AFT EDGE CORNERS OF WASTE BOX CUTOUT. C/W ER/A 610625-14 REV A ASSOCIATED ER/A 14-610625 ADDED FOR AC 8136. LOG TO REFLECT SDR YES. (LPMar 13, 2026 · N136DQ · Airbus BD5001A10 · Fuselage Main, Plate/SkinSDR DALA2026041502390Skin · corrodedER/A 610625-14 REV A; A220 / LOWER AFT FUSELAGE / FR75-76 / WASTE SERVICE COMPARTMENT/CORROSION. SUBJECT REPAIR REQUIRES FOLLOW-ON ACTION. ACCOMPLISH 610625-14 REV A, SECTION II REPETITIVE INSPECTION WITHIN EVERY 1,000 FLIGHT HOURS FROM 14,667 TOTAL AIRCRAFT FMar 11, 2026 · N136DQ · Airbus BD5001A10 · Fuselage Main, Plate/SkinSDR DALA2026030901609Access Panel · corrodedCORROSION, FLOOR ACCESS PANEL AT THE R/H SERVICE DOOR AT FR76 NEAR RBL 43.5. REMOVED DAMAGED FLOOR ACCESS PANEL R/H SERVICE DOOR (ASD) AND REPLACED PER A220 AMP BD500-A-J53-00-47-14AAA-720A-A. (LP# 1485104)Mar 8, 2026 · N136DQ · Airbus BD5001A10 · Fuselage Main, StructureSDR DALA2026030901610Support Fitting · corrodedCORRODED FLOOR PANEL SUPPORT FITTING AT RBL 23, FR 79. REMOVED AND REPLACED DOOR PANEL SUPPORT FITTING AT RBL 23 FR79 PER A220 ASRP BD500-A-J51-42-20-00AAA-078A-A AND BOMBARDIER PL# C01342700 REV T. (LP# 1482159)Mar 6, 2026 · N136DQ · Airbus BD5001A10 · Fuselage Miscellaneous StructureSDR DALA2026030401493Floor Panel · corrodedCORRODED FLOOR PANEL SUPPORT BETWEEN RBL 23 AND RBL 43.2 AT FR 76. REMOVED DAMAGED SUPPORT AND INSTALLED NEW FLOOR SUPPORT AT FR 76 -78 RBL 39" IAW BOMBARDIER DRAWING# PL C01342700 AND A220ASRP BD500-A-J51-42-06-00AAA-078A-A. (LP# 1477333)Mar 3, 2026 · N136DQ · Airbus BD5001A10 · Fuselage Floor PanelSDR DALA2026030401487Seat Track · corrodedCORROSION ON SEAT TRACK AT FR74, LBL44, WL151. REMOVED SEAT TRACK DAMAGED AND INSTALLED NEW SEAT TACK AT FR 74 TO FR61 LBL 44, WL 151 IAW A220 ASRP BD500-A-J51-42-20-00AAA- 078A-A AND DWG BOMBARDIER PL C01342701 REV-G. (LP# 1475749)Mar 2, 2026 · N136DQ · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026022601374Seat Track · corrodedCORROSION FOUND ON FUSELAGE SEAT TRACK AT STA FR20 RBL 23. REMOVED DAMAGED SEAT TRACK AT STA FR20 TO FR30 RBL 23 AND INSTALLED NEW SEAT TRACK PER A220 ASRP BD500-A-J51-42-21-00AAA- 078A-A AND DWG BOMBARDIER PL C02312600 REV-E. (LP# 1463021)Feb 22, 2026 · N136DQ · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026022401322Support · corrodedLOWER FAIRING SUPPORT STRUCTURE AT FR 48 FROM BL0 TO LBL 13 WITH POSSIBLE CORROSION. REMOVED AND REPLACED LOWER FAIRING SUPPORT FRAME AT STA FR 48 FROM BL0 TO LBL 74 PER A220 ASRP BD500-A-J51-42-21-00AAA-078A-A AND BOMBARDIER DWG# C01363100 REV-E. (LP# 1461955Feb 21, 2026 · N136DQ · Airbus BD5001A10 · Fuselage Miscellaneous StructureSDR DALA2026022401321Seat Track · corrodedCORROSION FOUND ON FUSELAGE SEAT TRACK AT STA FR20 RBL 43.5. REMOVED AND REPLACED SEAT TRACK AT RBL 43.5 FROM STA FR 20 TO STA FR 30 IAW A220 ASRP BD500-A-J51-42-21-01AAA-078A-A AND BOMBARDIER DWG# C02312600. (LP# 1461439)Feb 20, 2026 · N136DQ · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026022401320Floor Panel · corrodedCORROSION FWD SERVICE DOOR ENTRY FLOOR PANEL WITH CORROSION ON AFT I/B CORNER. REMOVED AND REPLACED FWD SERVICE DOOR ENTRY FLOOR PLANE IAW ASRP BD500-A-J51-40-00-AA-028A-A & PER A220 AMP BD500-A-J53-00- 47-12AAA-720A-A. (LP# 1457200)Feb 18, 2026 · N136DQ · Airbus BD5001A10 · Fuselage Floor PanelSDR DALA2026010200036Valve · faultedAFTER ENGINE START, TRIM AIR WAS VERY HOT IN CKPT AND AFT DUCTS. 188+F IN CKPT, 184+F AFT. CYCLED TRIM AIR SWITCH AND FUNCTIONED NORMALLY. AT CRUISE, FA REPORTED SMELLING ELECTRICAL SMELL AT L1 DOOR. POSSIBLE SMELL AROUND 2L DOOR. ODOR MAY BE ASSOCIATED WITH TJan 1, 2026 · N136DQ · Airbus BD5001A10 · Cabin Temperature Control SystemSDR DALA2025121209101Longeron · crackedCRACK IN WTB FAIRING LONGERON P/N 53-1111-501 AT LBL 40.0. CRACK SPREAD BETWEEN TWO NUT PLATES ON OUTBOARD SIDE OF LONGERON FORWARD OF FRAME AT FS 973. CRACK MEASURES 6 1/8" LONG BY 1/2 " WIDE. AD RELATED REF WORK CARD 5352-01038-01A. COMPLIED WITH WORK CARD 5Dec 8, 2025 · N136DQ · Airbus BD5001A10 · Aerodynamic FairingsSDR DALA2025121209100Longeron · damagedFOUND LONGERON DAMAGED. REMOVED LONGERON PER A220 DWG C02382100 REV A. INSTALLED LONGERON PER A220 DWG C02382100 REV A. ONE FASTENER STILL REQUIRED. (HR 259148) FINISHED INSTALLING LONGERON PER A220 C02382100 REV A. (LP# 1342239)Dec 8, 2025 · N136DQ · Airbus BD5001A10 · Fuselage Main, Longeron/StringerSDR DALA2025121009037Seal · failedDIV TO LAX DUE TO A "L PACK LEAK". FOUND FAULT CODE 3621F0024. FOUND LEAK ON LT UROSEAL UNDER BLUE INSULATION OVER FORWARD END OF SEAL. R/R LT DUCT UROSEAL, ITEM J PER A220 AMP 36-16-05-02. C/W LEAK CHECK. (LP# 8084381, 7823376)Dec 4, 2025 · N136DQ · Airbus BD5001A10 · Cabin Cooling SystemSDR DALA2025111208279Engine · making metalLEFT ENGINE IFSD INTO SLC, DECLARED EMERGENCY. LEFT ENGINE OIL TEMP BEGAN TO RISE AND OIL PRESSURE STARTED TO DROP. CREW THEN RECEIVED AN OIL DEBRIS OVER LIMIT MESSAGE AND SHUT DOWN THE ENGINE PER THE QRH. NR 1 ENGINE REPLACED. (LP# 8223999)Nov 11, 2025 · N136DQ · Airbus BD5001A10 · Engine (Turbine/Turboprop)SDR DALA2025090206508Egt Indication · illuminatedRIGHT ENGINE AUTO SHUTDOWN ON DESCENT WITH EGT EXCEEDANCE. RT ENGINE REPLACED. (LP# 7823306)Aug 26, 2025 · N136DQ · Airbus BD5001A10 · Engine EGT/TIT Indicating SystemSDR DALA2025061804588Circuit Breaker · trippedAFTER C/B CDC5-7-6 TRIPPED, FA REPORTED BURNING PLASTIC SMELL FUMES IN AFT GALLEY. FUMES DISSIPATED AFTER AFT GALLEY HEATER/ FAN WAS TURNED OFF BY FA. C/W AMDS WORK CARDS 0550-2003 & 0550-2001. FOUND SOURCE OF SMELL TO BE AFT GALLEY HEATER. DEFERRED AFT GALLEYJun 14, 2025 · N136DQ · Airbus BD5001A10 · Air Conditioning System WiringSDR DALA2025061704573Heater · odorMUSTY SMELL REPORTED IN THE AFT GALLEY BY FA'S AFTER TURNING GALLEY HEATER ON. ODOR DISSIPATED ABOUT 15-20 MINUTES AFTER TURNING HEATER BACK OFF. C/W NO GO ODI. ODOR IS ISOLATED TO AFT GALLEY HEATER. R/R AFT GALLEY HEATER IAW A220 AMP 12-42. OPS CHECKS GOOD. Jun 11, 2025 · N136DQ · Airbus BD5001A10 · Heating SystemSDR DALA2025060304235Seat Track · corrodedAIRCRAFT 8136, CORROSION ON SEAT TRACK LBL 23 AFT OF FRAME 72. CORRECTIVE ACTION: CUTAWAY DAMAGE SEAT TRACK LBL 23 TO CUT LOCATION PER ER/A#623168-14TR REV O. ACCOMPLISHED HFEC CUTLINE PER ANDTPBD500-A-J51-01-08-01AAD-353A-A. NO CRACKS FOUND. FIT NEW SEAT TRACJun 2, 2025 · N136DQ · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025060304234Seat Track · corrodedAIRCRAFT 8136, CORROSION ON SEAT TRACK RBL 23 AFT OF FRAME 72. CORRECTIVE ACTION: CUT & REMOVED DAMAGED SEAT TRACK RBL 23.0 AT LOCATION A PER ER/A 623169-14TR REV ORIG. ACCOMPLISHED HFEC OF CUT LINE PER ANDTP BD500-A-J51-01-08-01AAA-353A-X NO CRACKS FOUND. RECJun 2, 2025 · N136DQ · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025060104196Seat Track · corrodedAIRCRAFT 8136, CORROSION ON SEAT TRACK LBL 43.5 AFT OF FRAME 72. CORRECTIVE ACTION: CUT AND REMOVED DAMAGED SEAT TRACK LBL 43.5 AT LOCATION B PER ER/A 623167-14TR REV ORIG. ACCOMPLISHED HFEC OF CUTLINE PER ANDTP BD500-A-J51-01-08-01 AAA-353A-A NO CRACKS FOUND.Jun 1, 2025 · N136DQ · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025020300800Battery Pack · inoperativeL2 DOOR EMERGENCY EXIT SIGN INOP. R/R EPSU BATTERY PACK PER A220 AMP 33-51. OPS CHECK PASSED. A/C OK FOR RETURN TO SERVICE. (LP# 6384381)Jan 27, 2025 · N136DQ · Airbus BD5001A10 · Emergency LightingSDR DALA2024010800263Not Reported · not reportedR/H SLAT TRACK NBR 7 UPPER AFT SURFACE HAVE EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED RH SLAT TRACK #7 UPPER AFT PER ER/A 607815-14AD REV A AND PRI REV 0 MATCHED.Jan 4, 2024 · N136DQ · Bombdr BD1001A10 · Leading Edge DevicesSDR DALA2024010800262Not Reported · not reportedR/H SLAT TRACK NBR 6 LWR AFT SURFACE HAVE EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED RH SLAT TRACK #6 LOWER AFT PER ER/A 607815-14AD REV A AND PRI REV 0 MATCHED. (Jan 4, 2024 · N136DQ · Bombdr BD1001A10 · Leading Edge DevicesSDR DALA2024010800261Not Reported · not reportedR/H SLAT TRACK NBR 6 UPPER AFT SURFACE HAVE EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED RH SLAT TRACK #6 UPPER AFT PER ER/A 607815-14AD REV A AND PRI REV 0 MATCHED.Jan 4, 2024 · N136DQ · Bombdr BD1001A10 · Leading Edge DevicesSDR DALA2024010800260Not Reported · not reportedR/H SLAT TRACK NBR 5 LWR FWD SURFACE HAVE EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED RH SLAT TRACK #5 LOWER FWD PER ER/A 607815-14AD REV A AND PRI REV 0 MATCHED. (Jan 4, 2024 · N136DQ · Bombdr BD1001A10 · Leading Edge DevicesSDR DALA2024010800259Not Reported · not reportedR/H SLAT TRACK NBR5 LWR AFT SURFACE HAVE EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED RH SLAT TRACK #5 LOWER AFT PER ER/A 607815-14AD REV A AND PRI REV 0 MATCHED. (LJan 4, 2024 · N136DQ · Bombdr BD1001A10 · Leading Edge DevicesSDR DALA2024010800258Not Reported · not reportedR/H SLAT TRACK NBR 5 UPPER FWD SURFACE HAVE EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED RH SLAT TRACK #5 UPPER PER ER/A 607815-14AD REV A AND PRI REV 0 MATCHED. (LPJan 4, 2024 · N136DQ · Bombdr BD1001A10 · Leading Edge DevicesSDR DALA2024010800257Not Reported · not reportedR/H SLAT TRACK NBR 5 UPPER AFT SURFACE HAVE EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED RH SLAT TRACK #5 UPPER PER ER/A 607815-14AD REV A AND PRI REV 0 MATCHED. (LPJan 4, 2024 · N136DQ · Bombdr BD1001A10 · Leading Edge DevicesSDR DALA2024010800256Not Reported · not reportedR/H SLAT TRACK NBR 3 LWR AFT SURFACE HAVE EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED RH SLAT TRACK #3 LOWER PER ER/A 607815-14AD REV A AND PRI REV 0 MATCHED. (LP# Jan 4, 2024 · N136DQ · Bombdr BD1001A10 · Leading Edge DevicesSDR DALA2024010800255Not Reported · not reportedR/H SLAT TRACK NBR 2 LWR AFT SURFACE HAVE EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED RH SLAT TRACK #2 LOWER PER ER/A 607815-14AD REV A AND PRI REV 0 MATCHED. (LP# Jan 4, 2024 · N136DQ · Bombdr BD1001A10 · Leading Edge DevicesSDR DALA2024010800254Not Reported · not reportedR/H SLAT TRACK NBR 1 LWR AFT SURFACE HAVE EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED RH SLAT TRACK NBR 1 LOWER AFT SURFACE PER ER/A 607815- 14AD REV A AND PRI REV Jan 4, 2024 · N136DQ · Bombdr BD1001A10 · Leading Edge DevicesSDR DALA2024010800253Not Reported · not reportedR/H SLAT TRACK NBR 1 UPPER AFT SURFACE HAVE EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-0102-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED RH SLAT TRACK #1 UPPER AFT SURFACE PER ER/A 607814-14AD REV A AND PRI REV 0 MJan 4, 2024 · N136DQ · Bombdr BD1001A10 · Leading Edge DevicesSDR DALA2024010800252Not Reported · not reportedL/H SLAT TRACK NBR 9 UPPER AFT SURFACE HAVE EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-0102-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED LH SLAT TRACK #9 UPPER AFT SURFACE PER ER/A 607814-14AD REV A AND PRI REV 0 MJan 4, 2024 · N136DQ · Bombdr BD1001A10 · Leading Edge DevicesSDR DALA2024010800251Not Reported · not reportedL/H SLAT TRACK NBR 8 UPPER AFT SURFACE HAVE EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-0102-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED LH SLAT TRACK #8 UPPER AFT SURFACE PER ER/A 607814-14AD REV A AND PRI REV 0 MJan 4, 2024 · N136DQ · Bombdr BD1001A10 · Leading Edge DevicesSDR DALA2024010800250Not Reported · not reportedL/H SLAT TRACK NBR 6 LWR AFT SURFACE HAVE EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-0102-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED LH SLAT TRACK #6 LOWER AFT SURFACE PER ER/A 607814-14AD REV A AND PRI REV 0 MATJan 4, 2024 · N136DQ · Bombdr BD1001A10 · Leading Edge DevicesSDR DALA2024010800249Not Reported · not reportedL/H SLAT TRACK NBR 4 LWR AFT SURFACE HAVE EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-0102-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED LH SLAT TRACK #2 LOWER AFT SURFACE PER ER/A 607814-14AD REV A AND PRI REV 0 MATJan 4, 2024 · N136DQ · Bombdr BD1001A10 · Leading Edge DevicesSDR DALA2024010800248Not Reported · not reportedL/H SLAT TRACK NBR 3 LWR AFT SURFACE HAVE EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-0102-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED LH SLAT TRACK #3 LOWER AFT SURFACE PER ER/A 607814-14AD REV A AND PRI REV 0 MATJan 4, 2024 · N136DQ · Bombdr BD1001A10 · Leading Edge DevicesSDR DALA2024010800247Not Reported · not reportedL/H SLAT TRACK NBR 3 UPPER FWD SURFACE HAVE EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-0102-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED LH SLAT TRACK #3 UPPER FWD SURFACE PER ER/A 607814-14AD REV A AND PRI REV 0 MJan 4, 2024 · N136DQ · Bombdr BD1001A10 · Leading Edge DevicesSDR DALA2024010800246Not Reported · not reportedL/H SLAT TRACK NBR 2 LWR FWD SURFACE HAVE EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-0102-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED LH SLAT TRACK #2 LOWER FWD SURFACE PER ER/A 607814-14AD REV A AND PRI REV 0 MATJan 4, 2024 · N136DQ · Bombdr BD1001A10 · Leading Edge DevicesSDR DALA2024010800245Not Reported · not reportedL/H SLAT TRACK NBR 2 LWR AFT SURFACE HAVE EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-0102-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED LH SLAT TRACK #2 LOWER AFT SURFACE PER ER/A 607814-14AD REV A AND PRI REV 0 MATJan 4, 2024 · N136DQ · Bombdr BD1001A10 · Leading Edge DevicesSDR DALA2024010800244Not Reported · not reportedL/H SLAT TRACK NBR 2 UPPER FWD SURFACE HAVE EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF AA 5742-01028-02A LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. REPAIRED LH SLAT TRACK #2 UPPER FWD SURFACE PER ERA 607814-14AD REV A AND PRI REV 0 MAJan 4, 2024 · N136DQ · Bombdr BD1001A10 · Leading Edge DevicesSDR DALA2024010800243Not Reported · not reportedL/H SLAT TRACK NBR 2 UPPER AFT SURFACE HAVE EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF AA 5742-01028-02A LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. REPAIRED LH SLAT TRACK #1 UPPER AFT SURFACE PER ERA 607814-14AD REV A AND PRI REV 0 MAJan 4, 2024 · N136DQ · Bombdr BD1001A10 · Leading Edge DevicesSDR DALA2024010800242Not Reported · not reportedL/H SLAT TRACK NBR 1 LOWER AFT SURFACE HAVE EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF AA 5742-01028-02A LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. REPAIRED LH SLAT TRACK #1 LOWER AFT SURFACE PER ERA 607814-14AD REV A AND PRI REV 0 MAJan 4, 2024 · N136DQ · Bombdr BD1001A10 · Leading Edge DevicesSDR DALA2024010800241Not Reported · not reportedL/H SLAT TRACK NBR 1 LOWER FWD SURFACE HAVE EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF AA 5742-01028-02A LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. REPAIRED LH SLAT TRACK #1 LOWER FWD SURFACE PER ERA 607814-14AD REV A AND PRI REV 0 MAJan 4, 2024 · N136DQ · Bombdr BD1001A10 · Leading Edge DevicesSDR DALA2024010800240Not Reported · not reportedL/H SLAT TRACK NBR 1 UPPER AFT SURFACE HAVE EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF AA 5742-01028-02A LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. REPAIRED LH SLAT TRACK #1 UPPER AFT SURFACE PER ERA 607814-14AD REV A AND PRI REV 0 MAJan 4, 2024 · N136DQ · Bombdr BD1001A10 · Leading Edge DevicesSDR DALA2023081506641Unknown · unknownSHIP 8136 -DIV- DIVERTED TO SFO DUE TO LEFT ENGINE OPERATION DEGRADED MESSAGE WITH LEFT ENGINE FAULT. CORRECTIVE ACTION: REPLACED EEC, PERFORMED GROUND TEST AND IDLE RUN, NO FURTHER FAULTS. (LP# 4662724)Aug 10, 2023 · N136DQ · Bombdr BD1001A10 · Fuel Controlling SystemSDR DALA2023073106173Unknown · unknownWASTE BOX CORRODED AT LOWER FWD CUT OUT AREA. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0085:5360-2017/001 00102 COMPLIED WITH ER/A 610625-14 PRI REV 0, ER/A 610625-14 PRI REV 1, AND FINAL ER/A 610625-14 REV ORIGINAL. SUMMARY SEE NR FOR ADDITIONAL INFORMATJul 29, 2023 · N136DQ · Bombdr BD1001A10 · Fuselage Structure (General)
Back to N136DQ