# Service difficulty reports: N136DQ

A list on [N136DQ](https://openairdocs.org/aircraft/N136DQ.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 · 55 reports

- [SDR DALA2026041002301](https://openairdocs.org/sdr/DALA2026041002301.md): Heater · odor · Apr 8, 2026 · N136DQ · Airbus BD5001A10 · Heating System
  > DIVERTED 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)
- [SDR DALA2026031801872](https://openairdocs.org/sdr/DALA2026031801872.md): Skin · punctured · Mar 15, 2026 · N136DQ · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > PUNCTURE 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# 14956
- [SDR DALA2026031701847](https://openairdocs.org/sdr/DALA2026031701847.md): Doubler · corroded · Mar 13, 2026 · N136DQ · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > WHILE 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. (LP
- [SDR DALA2026041502390](https://openairdocs.org/sdr/DALA2026041502390.md): Skin · corroded · Mar 11, 2026 · N136DQ · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > ER/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 F
- [SDR DALA2026030901609](https://openairdocs.org/sdr/DALA2026030901609.md): Access Panel · corroded · Mar 8, 2026 · N136DQ · Airbus BD5001A10 · Fuselage Main, Structure
  > CORROSION, 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)
- [SDR DALA2026030901610](https://openairdocs.org/sdr/DALA2026030901610.md): Support Fitting · corroded · Mar 6, 2026 · N136DQ · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > CORRODED 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)
- [SDR DALA2026030401493](https://openairdocs.org/sdr/DALA2026030401493.md): Floor Panel · corroded · Mar 3, 2026 · N136DQ · Airbus BD5001A10 · Fuselage Floor Panel
  > CORRODED 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)
- [SDR DALA2026030401487](https://openairdocs.org/sdr/DALA2026030401487.md): Seat Track · corroded · Mar 2, 2026 · N136DQ · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION 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)
- [SDR DALA2026022601374](https://openairdocs.org/sdr/DALA2026022601374.md): Seat Track · corroded · Feb 22, 2026 · N136DQ · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION 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)
- [SDR DALA2026022401322](https://openairdocs.org/sdr/DALA2026022401322.md): Support · corroded · Feb 21, 2026 · N136DQ · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > LOWER 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# 1461955
- [SDR DALA2026022401321](https://openairdocs.org/sdr/DALA2026022401321.md): Seat Track · corroded · Feb 20, 2026 · N136DQ · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION 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)
- [SDR DALA2026022401320](https://openairdocs.org/sdr/DALA2026022401320.md): Floor Panel · corroded · Feb 18, 2026 · N136DQ · Airbus BD5001A10 · Fuselage Floor Panel
  > CORROSION 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)
- [SDR DALA2026010200036](https://openairdocs.org/sdr/DALA2026010200036.md): Valve · faulted · Jan 1, 2026 · N136DQ · Airbus BD5001A10 · Cabin Temperature Control System
  > AFTER 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 T
- [SDR DALA2025121209101](https://openairdocs.org/sdr/DALA2025121209101.md): Longeron · cracked · Dec 8, 2025 · N136DQ · Airbus BD5001A10 · Aerodynamic Fairings
  > CRACK 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 5
- [SDR DALA2025121209100](https://openairdocs.org/sdr/DALA2025121209100.md): Longeron · damaged · Dec 8, 2025 · N136DQ · Airbus BD5001A10 · Fuselage Main, Longeron/Stringer
  > FOUND 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)
- [SDR DALA2025121009037](https://openairdocs.org/sdr/DALA2025121009037.md): Seal · failed · Dec 4, 2025 · N136DQ · Airbus BD5001A10 · Cabin Cooling System
  > DIV 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)
- [SDR DALA2025111208279](https://openairdocs.org/sdr/DALA2025111208279.md): Engine · making metal · Nov 11, 2025 · N136DQ · Airbus BD5001A10 · Engine (Turbine/Turboprop)
  > LEFT 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)
- [SDR DALA2025090206508](https://openairdocs.org/sdr/DALA2025090206508.md): Egt Indication · illuminated · Aug 26, 2025 · N136DQ · Airbus BD5001A10 · Engine EGT/TIT Indicating System
  > RIGHT ENGINE AUTO SHUTDOWN ON DESCENT WITH EGT EXCEEDANCE. RT ENGINE REPLACED. (LP# 7823306)
- [SDR DALA2025061804588](https://openairdocs.org/sdr/DALA2025061804588.md): Circuit Breaker · tripped · Jun 14, 2025 · N136DQ · Airbus BD5001A10 · Air Conditioning System Wiring
  > AFTER 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 GALLEY
- [SDR DALA2025061704573](https://openairdocs.org/sdr/DALA2025061704573.md): Heater · odor · Jun 11, 2025 · N136DQ · Airbus BD5001A10 · Heating System
  > MUSTY 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.
- [SDR DALA2025060304235](https://openairdocs.org/sdr/DALA2025060304235.md): Seat Track · corroded · Jun 2, 2025 · N136DQ · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > AIRCRAFT 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 TRAC
- [SDR DALA2025060304234](https://openairdocs.org/sdr/DALA2025060304234.md): Seat Track · corroded · Jun 2, 2025 · N136DQ · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > AIRCRAFT 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. REC
- [SDR DALA2025060104196](https://openairdocs.org/sdr/DALA2025060104196.md): Seat Track · corroded · Jun 1, 2025 · N136DQ · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > AIRCRAFT 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.
- [SDR DALA2025020300800](https://openairdocs.org/sdr/DALA2025020300800.md): Battery Pack · inoperative · Jan 27, 2025 · N136DQ · Airbus BD5001A10 · Emergency Lighting
  > L2 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)
- [SDR DALA2024010800263](https://openairdocs.org/sdr/DALA2024010800263.md): Not Reported · not reported · Jan 4, 2024 · N136DQ · Bombdr BD1001A10 · Leading Edge Devices
  > R/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.
- [SDR DALA2024010800262](https://openairdocs.org/sdr/DALA2024010800262.md): Not Reported · not reported · Jan 4, 2024 · N136DQ · Bombdr BD1001A10 · Leading Edge Devices
  > R/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. (
- [SDR DALA2024010800261](https://openairdocs.org/sdr/DALA2024010800261.md): Not Reported · not reported · Jan 4, 2024 · N136DQ · Bombdr BD1001A10 · Leading Edge Devices
  > R/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.
- [SDR DALA2024010800260](https://openairdocs.org/sdr/DALA2024010800260.md): Not Reported · not reported · Jan 4, 2024 · N136DQ · Bombdr BD1001A10 · Leading Edge Devices
  > R/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. (
- [SDR DALA2024010800259](https://openairdocs.org/sdr/DALA2024010800259.md): Not Reported · not reported · Jan 4, 2024 · N136DQ · Bombdr BD1001A10 · Leading Edge Devices
  > R/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. (L
- [SDR DALA2024010800258](https://openairdocs.org/sdr/DALA2024010800258.md): Not Reported · not reported · Jan 4, 2024 · N136DQ · Bombdr BD1001A10 · Leading Edge Devices
  > R/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. (LP
- [SDR DALA2024010800257](https://openairdocs.org/sdr/DALA2024010800257.md): Not Reported · not reported · Jan 4, 2024 · N136DQ · Bombdr BD1001A10 · Leading Edge Devices
  > R/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. (LP
- [SDR DALA2024010800256](https://openairdocs.org/sdr/DALA2024010800256.md): Not Reported · not reported · Jan 4, 2024 · N136DQ · Bombdr BD1001A10 · Leading Edge Devices
  > R/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#
- [SDR DALA2024010800255](https://openairdocs.org/sdr/DALA2024010800255.md): Not Reported · not reported · Jan 4, 2024 · N136DQ · Bombdr BD1001A10 · Leading Edge Devices
  > R/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#
- [SDR DALA2024010800254](https://openairdocs.org/sdr/DALA2024010800254.md): Not Reported · not reported · Jan 4, 2024 · N136DQ · Bombdr BD1001A10 · Leading Edge Devices
  > R/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
- [SDR DALA2024010800253](https://openairdocs.org/sdr/DALA2024010800253.md): Not Reported · not reported · Jan 4, 2024 · N136DQ · Bombdr BD1001A10 · Leading Edge Devices
  > R/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 M
- [SDR DALA2024010800252](https://openairdocs.org/sdr/DALA2024010800252.md): Not Reported · not reported · Jan 4, 2024 · N136DQ · Bombdr BD1001A10 · Leading Edge Devices
  > L/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 M
- [SDR DALA2024010800251](https://openairdocs.org/sdr/DALA2024010800251.md): Not Reported · not reported · Jan 4, 2024 · N136DQ · Bombdr BD1001A10 · Leading Edge Devices
  > L/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 M
- [SDR DALA2024010800250](https://openairdocs.org/sdr/DALA2024010800250.md): Not Reported · not reported · Jan 4, 2024 · N136DQ · Bombdr BD1001A10 · Leading Edge Devices
  > L/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 MAT
- [SDR DALA2024010800249](https://openairdocs.org/sdr/DALA2024010800249.md): Not Reported · not reported · Jan 4, 2024 · N136DQ · Bombdr BD1001A10 · Leading Edge Devices
  > L/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 MAT
- [SDR DALA2024010800248](https://openairdocs.org/sdr/DALA2024010800248.md): Not Reported · not reported · Jan 4, 2024 · N136DQ · Bombdr BD1001A10 · Leading Edge Devices
  > L/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 MAT
- [SDR DALA2024010800247](https://openairdocs.org/sdr/DALA2024010800247.md): Not Reported · not reported · Jan 4, 2024 · N136DQ · Bombdr BD1001A10 · Leading Edge Devices
  > L/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 M
- [SDR DALA2024010800246](https://openairdocs.org/sdr/DALA2024010800246.md): Not Reported · not reported · Jan 4, 2024 · N136DQ · Bombdr BD1001A10 · Leading Edge Devices
  > L/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 MAT
- [SDR DALA2024010800245](https://openairdocs.org/sdr/DALA2024010800245.md): Not Reported · not reported · Jan 4, 2024 · N136DQ · Bombdr BD1001A10 · Leading Edge Devices
  > L/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 MAT
- [SDR DALA2024010800244](https://openairdocs.org/sdr/DALA2024010800244.md): Not Reported · not reported · Jan 4, 2024 · N136DQ · Bombdr BD1001A10 · Leading Edge Devices
  > L/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 MA
- [SDR DALA2024010800243](https://openairdocs.org/sdr/DALA2024010800243.md): Not Reported · not reported · Jan 4, 2024 · N136DQ · Bombdr BD1001A10 · Leading Edge Devices
  > L/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 MA
- [SDR DALA2024010800242](https://openairdocs.org/sdr/DALA2024010800242.md): Not Reported · not reported · Jan 4, 2024 · N136DQ · Bombdr BD1001A10 · Leading Edge Devices
  > L/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 MA
- [SDR DALA2024010800241](https://openairdocs.org/sdr/DALA2024010800241.md): Not Reported · not reported · Jan 4, 2024 · N136DQ · Bombdr BD1001A10 · Leading Edge Devices
  > L/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 MA
- [SDR DALA2024010800240](https://openairdocs.org/sdr/DALA2024010800240.md): Not Reported · not reported · Jan 4, 2024 · N136DQ · Bombdr BD1001A10 · Leading Edge Devices
  > L/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 MA
- [SDR DALA2023081506641](https://openairdocs.org/sdr/DALA2023081506641.md): Unknown · unknown · Aug 10, 2023 · N136DQ · Bombdr BD1001A10 · Fuel Controlling System
  > SHIP 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)
- [SDR DALA2023073106173](https://openairdocs.org/sdr/DALA2023073106173.md): Unknown · unknown · Jul 29, 2023 · N136DQ · Bombdr BD1001A10 · Fuselage Structure (General)
  > WASTE 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 INFORMAT

Next page: https://openairdocs.org/aircraft/N136DQ/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 = 'N136DQ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N136DQ/reports

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