# Service difficulty reports: N606AL, cancelled Oct 6, 2014 A list on [N606AL, cancelled Oct 6, 2014](https://openairdocs.org/deregistered/N606AL-2014-10-06.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 9 · 446 reports - [SDR IXXA20121127032O](https://openairdocs.org/sdr/IXXA20121127032O.md): Connector · loose · Nov 27, 2012 · N606AL · Doug DC873F · Landing Gear System Wiring > ON APPROACH, RT MLG DOWN GREEN LIGHT DID NOT ILLUMINATE, NO RED LIGHTS ILLUMINATED. CYCLED LANDING GEAR AND GREEN LIGHT ILLUMINATED. RESEATED CONNECTOR PLUG ON RT MLG DOWNLOCK SWITCH IAW MM 32-60-0. OPS CHECKS GOOD. - [SDR IXXA110048O](https://openairdocs.org/sdr/IXXA110048O.md): Connector · dirty · Jun 10, 2011 · N606AL · Doug DC873F · Light System Wiring > ON FINAL APPROACH WITH LANDING GEAR LEVER DOWN, RT LANDING LIGHT DID NOT ILLUMINATE. THE CREW CYCLED THE GEAR AND GEAR LIGHT ILLUMINATED 10 SECONDS AFTER GEAR CYCLE. THEY LANDED WITHOUT FURTHER INCIDENT. MX REMOVED AND CLEANED THE CONNECTOR PLUG ON THE DOWN - [SDR IXXA110027O](https://openairdocs.org/sdr/IXXA110027O.md): Mec · defective · Mar 11, 2011 · N606AL · Doug DC873F · Turbine Engine Compressor Section > AT THE TOP OF CLIMB OUT AT FLIGHT LEVEL 36,000 FT WHEN THROTTLES WERE PULLED BACK FROM CLIMB POWER TO CRUISE POWER NR 3 ENG MOMENTARILY COMPRESSOR STALLED. ALL OTHER ENGINES PARAMETERS WERE NORMAL AND NR 3 COMPRESSOR STALLED AGAIN 10 MINUTES LATER AT CRUISE W - [SDR IXXA110026O](https://openairdocs.org/sdr/IXXA110026O.md): Sensor · defective · Mar 7, 2011 · N606AL · Doug DC873F · Engine Indicating System > DURING CRUISE NR 3 ENG COMPRESSOR STALLED. CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX REPLACED (CIT) SENSOR. OPS CHECK GOOD IAW CFM MM 73-21-20. ACFT WAS RETURNED TO SERVICE. - [SDR IXXA110021O](https://openairdocs.org/sdr/IXXA110021O.md): Engine · flamed out · Feb 11, 2011 · N606AL · Doug DC873F · Engine (Turbine/Turboprop) > AFTER TAKEOFF, WHEN THROTTLES WERE RETARDED AT FL 37.0 NR 3 ENGINE FLAMED OUT. BEFORE THE CREW COULD ACCOMPLISH FLAME OUT CHECK LIST, THE ENG RELIT WITH NO PROBLEMS THE REMAINDER OF THE FLIGHT, LANDED WITHOUT FURTHER INCIDENT. MX ACCOMPLSHED TREE FAULT 51 WITH - [SDR IXXA110006O](https://openairdocs.org/sdr/IXXA110006O.md): Unknown · unknown · Jan 22, 2011 · N606AL · Doug DC873F · Standard Practices/Structures > DURING TAKEOFF ROLL, ACFT PULLED HARD LEFT. CREW WAS UNABLE TO MAINTAIN DIRECTIONAL CONTROL WITH FULL RT RUDDER. THEY ABORTED TAKEOFF AND RETURNED TO BLOCKS WITH OUT FURTHER INCIDENT. MX INSPECTED THE NOSE GEAR, WHEELS, BRAKES, NOSE WHEEL STEERING, NOSE STEE - [SDR IXXA10SMN095S](https://openairdocs.org/sdr/IXXA10SMN095S.md): Spar Cap · cracked · Sep 30, 2010 · N606AL · Doug DC873F · Wing Spar > DURING ROUTINE C-CHECK INSP FOUND RT WING T/E SPAR CAP UPPER PART CRACKED AT STA XRS 74.000. REMOVED CRACKED UPPER SPAR CAP. FABRICATED NEW UPPER SPAR CAP. CLEANED, TREATED, PRIMED AREA AND REPAIR PART. INSTALLED NEW UPPER SPAR CAP IAW DWG 5611440, 5616128, - [SDR IXXA10SMN094S](https://openairdocs.org/sdr/IXXA10SMN094S.md): Skin · cracked · Sep 25, 2010 · N606AL · Doug DC873F · Wing, Plate/Skin > DURING ROUTINE C-CHECK INSP, FOUND LT WING OUTER WING OTBD L/E LOWER SKIN CRACKED AT STA XFS 847.500. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. PERFORMED NDT INSP. NO CRACKS OR CORROSION NOTED. FABRICATED NEW SKIN, FILLERS AND DOUB - [SDR IXXA10SMN093S](https://openairdocs.org/sdr/IXXA10SMN093S.md): Support Angle · corroded · Sep 22, 2010 · N606AL · Doug DC873F · Wing Miscellaneous Structure > DURING ROUTINE C-CHECK INSP, FOUND RT WING UPPER PANEL SUPPORT ANGLE CORRODED AT STA XW 5.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED ANGLE. FABRICATED NEW ANGLE. CLEANED, TERATED, AND PRIMED AREA. I - [SDR IXXA10SMN092S](https://openairdocs.org/sdr/IXXA10SMN092S.md): Skin · damaged · Sep 22, 2010 · N606AL · Doug DC873F · Wing, Plate/Skin > DURING ROUTINE C-CHECK INSP, FOUND LT WING NR 2 STUB WING LOWER SKIN ELONGATED HOLES AT STA XFS 247.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED SPLICE DOUBLER AND NEW SKIN. PERFORMED NDT INSP. NO CRACKS OR CORROSION NOT - [SDR IXXA10SMN091S](https://openairdocs.org/sdr/IXXA10SMN091S.md): Skin · cracked · Sep 21, 2010 · N606AL · Doug DC873F · Wing, Plate/Skin > DURING ROUTINE C-CHECK INSP FOUND LT WING NR 2 STUB WING LOWER SKIN CRACKED AT STA XFS 200.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED SPLICE DOUBLER AND NEW SKIN. PERFORMED NDT INSP. NO CRACKS OR CORROSION NOTED. - [SDR IXXA10SMN090S](https://openairdocs.org/sdr/IXXA10SMN090S.md): Fitting · cracked · Sep 17, 2010 · N606AL · Doug DC873F · Fuselage Main, Attach Fittings > DURING ROUTINE C-CHECK INSP, FOUND AFT CARGO COMPARTMENT SPLICE FITTING CRACKED AT STA 1390.000 LONGERON 30 LT. REMOVED CRACKED FITTING. FABRICATED NEW SPLICE FITTING. CLEANED, TREATED, PRIMED AREA AND SPLICE FITTING. INSTALLED NEW SPLICE FITTING IAW SRM 53- - [SDR IXXA10SMN089S](https://openairdocs.org/sdr/IXXA10SMN089S.md): Fitting · cracked · Sep 17, 2010 · N606AL · Doug DC873F · Fuselage Main, Attach Fittings > DURING ROUTINE C-CHECK INSP, FOUND AFT CARGO COMPARTMENT SPLICE FITTING CRACKED AT STA 1370.000, LONGERON 31 LT. R & R SPLICE FITTING IAW SRM 51-1-20D AND SRM 51-3-1. - [SDR IXXA10SMN088S](https://openairdocs.org/sdr/IXXA10SMN088S.md): Fitting · cracked · Sep 17, 2010 · N606AL · Doug DC873F · Wing, Attach Fittings > DURING ROUTINE C-CHECK INSP, FOUND LT WING T/E UPPER FITTING CRACKED AT STATION XRS 409.000. R & R CRACKED FITTING IAW SRM 51-1-21. - [SDR IXXA10SMN086S](https://openairdocs.org/sdr/IXXA10SMN086S.md): Doubler · cracked · Sep 16, 2010 · N606AL · Doug DC873F · Wing, Plate/Skin > DURING ROUTINE C-CHECK INSP FOUND LT WING NR 2 STUB WING EXTERNAL LOWER REPAIR DOUBLER CRACKED. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CRACKED DOUBLER. FABRICATED EXTERNAL AND INTERNAL DOUBLERS. PERFORMED HEAT TREATMENT. CLEANED, TREATED, PRIME - [SDR IXXA10SMN087S](https://openairdocs.org/sdr/IXXA10SMN087S.md): Skin · cracked · Sep 16, 2010 · N606AL · Doug DC873F · Ailerons > DURING ROUTINE C-CHECK INSP, FOUND LT OTBD AILERON LOWER SKIN CRACKED AT STA 761.695. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CRACKED SKIN. FABRICATED NEW SKIN AND DOUBLERS BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED, AND PRIMED AREA A - [SDR IXXA10SMN085S](https://openairdocs.org/sdr/IXXA10SMN085S.md): Frame · cracked · Sep 16, 2010 · N606AL · Doug DC873F · Fuselage Main, Frame > DURING ROUTINE C-CHECK INSP FOUND MAIN CARGO COMPARTMENT FRAME FLANGE CRACKED AT STA 1580.000 LONGERON20-21 RT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED FRAME. FABRICATED FRAME SEGMENT. PERFORMED HEAT TREATMENT. CLEANED,TREATED, AND P - [SDR IXXA10SMN084S](https://openairdocs.org/sdr/IXXA10SMN084S.md): Support Fitting · cracked · Sep 15, 2010 · N606AL · Doug DC873F · Wing, Landing Gear Attach Fittings > DURING ROUTINE C-CHECK INSP FOUND RT WING MLG SUPPORT FITTING EXTERNAL FACE CRACKED. R & R RT MLG SUPPORT FITTING IAW AD 89-10-04, DACO S/B, DC8-57-094, REV 04 DATED 03-24-2000, DWG 5611021, 5611440, 5611425, 5616128, 5641112, 5893930, AND EO NR 2010556. - [SDR IXXA10SMN083S](https://openairdocs.org/sdr/IXXA10SMN083S.md): Web · cracked · Sep 15, 2010 · N606AL · Doug DC873F · Nacelle/Pylon Miscellaneous Structure > DURING ROUTINE C-CHECK INSP FOUND NR 4 PYLON TEE DOUBLER HORIZ FLANGE CRACKED IN UPPER INTERNAL PART AT STA YN 335.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO CRACKS OR CORROSION NOTED. FABRICATED SPACER. - [SDR IXXA10SMN082S](https://openairdocs.org/sdr/IXXA10SMN082S.md): Skin · worn · Sep 15, 2010 · N606AL · Doug DC873F · Trailing Edge Flaps > DURING ROUTINE C-CHECK INSP FOUND LT WING INBD FLAP UPPER EXTERNAL SKIN WORN AT STA XW 104.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND BONDED DOUBLERS. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED - [SDR IXXA10SMN081S](https://openairdocs.org/sdr/IXXA10SMN081S.md): Skin · dented · Sep 15, 2010 · N606AL · Doug DC873F · Trailing Edge Flaps > DURING ROUTINE C-CHECK INSP, FOUND LT WING INBD FLAP UPPER EXTERNAL SKIN DENTED AT STATION XW 104.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED, AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW - [SDR IXXA10SMN080S](https://openairdocs.org/sdr/IXXA10SMN080S.md): Skin · cracked · Sep 15, 2010 · N606AL · Doug DC873F · Trailing Edge Flaps > DURING ROUTINE C-CHECK INSP FOUND LT WING INBD FLAP LOWER EXTERNAL SKIN CRACKED AT STATION XCW 64.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CRACKED SKIN. FABRICATED NEW SKIN AND DOUBLERS. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREAT - [SDR IXXA10SMN078S](https://openairdocs.org/sdr/IXXA10SMN078S.md): Skin · corroded · Sep 15, 2010 · N606AL · Doug DC873F · Trailing Edge Flaps > DURING ROUTINE C-CHECK INSP FOUND RT OTBD FLAP UPPER SKIN CORRODED AT STATION XF 304.000 - 333.0000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORRODED SKIN. FABRICATED NEW SKIN AND DOUBLERS. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED - [SDR IXXA10SMN076S](https://openairdocs.org/sdr/IXXA10SMN076S.md): Skin · corroded · Sep 14, 2010 · N606AL · Doug DC873F · Fuselage Main, Plate/Skin > DURING ROUTINE C-CHECK INSP, FOUND EXTERNAL FUSELAGE LOWER PART BUTT JOINT SKIN CORRODED AT STA 1690.000 BETWEEN LONGERON 34 RT- LONGERON 34 LT. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED NEW SKIN, DOUBLERS, FINGER DOUBLERS AND FI - [SDR IXXA10SMN077S](https://openairdocs.org/sdr/IXXA10SMN077S.md): Skin · worn · Sep 14, 2010 · N606AL · Doug DC873F · Trailing Edge Flaps > DURING ROUTINE C-CHECK INSP, FOUND RT INBD FLAP SKIN WORN AT STA XW 104.000 - 115.0000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED, AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND RE - [SDR IXXA10SMN075S](https://openairdocs.org/sdr/IXXA10SMN075S.md): Doubler · misrepaired · Sep 11, 2010 · N606AL · Doug DC873F · Fuselage Main, Structure > DURING ROUTINE C-CHECK INSP, FOUND IMPROPER REPAIR AT STATION FS 1560, LONGERON 20.5 RT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR DOUBLER. FABRICATED NEW SKIN, INTERNAL AND EXTERNAL DOUBLERS AND FILLER. CLEANED, TREATED, PRIMED - [SDR IXXA100044O](https://openairdocs.org/sdr/IXXA100044O.md): Switch · broken · Sep 8, 2010 · N606AL · Doug DC873F · Landing Gear Position and Warning > DURING CLIMBOUT, AFTER GEAR RETRACTION, THE "DOOR NOT LATCH" LIGHT REMAINED ON. CREW CYCLED THE GEARS AND WAS UNABLE TO DETERMINE CONDITION OF MAIN GEAR DOORS. THEY CONTINUED FLIGHT AND LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED THE MAIN GEAR DOOR WARNING - [SDR IXXA090075O](https://openairdocs.org/sdr/IXXA090075O.md): Generator · failed · Dec 16, 2009 · N606AL · Doug DC873F · AC Generation System > DURING CLIMB OUT FROM DEPARTURE NR 3 GENERATOR BUSS FAILURE, VOLTS AND FREQUENCIES AT ZERO. THE CREW ACCOMPLISHED COM PROCEDURES AND RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX RESET NR 3 GENERATOR BUS FAULT RESET SWITCH. OPS CHECK GOOD IAW MM 24-20-0. - [SDR IXXA090040S](https://openairdocs.org/sdr/IXXA090040S.md): Tee Fitting · cracked · Aug 14, 2009 · N606AL · Doug DC873F · Fuselage Main, Attach Fittings > DURING INSP IAW AD2007-21-18 AND SB DC8-53A081 FOUND AFT PRESSURE BULKHEAD TEE FITTING CRACKED AT LONGERON 9 RT TO LONGERON 10 RT. STOP DRILLED CRACK IAW SRM 53-2-5. - [SDR IXXA090039S](https://openairdocs.org/sdr/IXXA090039S.md): Tee Fitting · cracked · Aug 14, 2009 · N606AL · Doug DC873F · Fuselage Main, Attach Fittings > DURING INSP IAW AD2007-21-18 AND SB DC8-53A081 FOUND AFT PRESSURE BULKHEAD TEE FITTING CRACKED AT LONGERON 11 LT TO LONGERON 13 LT. STOP DRILLED CRACK IAW DACO DC8 SRM 53-2-5. - [SDR IXXA090028O](https://openairdocs.org/sdr/IXXA090028O.md): Cable · defective · Apr 27, 2009 · N606AL · Doug DC873F · Engine Indicating System Wiring > DURING CLIMB-OUT FROM KTOL NUMBER TWO ENGINE EGT WENT TO 914 DEGREE FOR TWO TO FIVE SECONDS. THE CREW RETARDED THE THROTTLE AND EGT INDICATOR DECREASED AND ALL OTHER ENGINES PARAMETER WERE NORMAL. THE CREW RETURNED TO KTOL AND LANDED WITHOUT FURTHER INCIDENT - [SDR IXXA090005O](https://openairdocs.org/sdr/IXXA090005O.md): Tube · clogged · Feb 16, 2009 · N606AL · Doug DC873F · Fuel Control/Turbine Engines > DURING DESCENT INTO ETAR NUMBER 2 ENGINE FLAME OUT. WITH THROTTLE REDUCTION, MILD VIBRATION, AND FUEL FLUCTUATION. THE CREW LANDED IN ETAR WITHOUT FURTHER INCIDENT. MAINTENANCE ACCOMPLISHED CFM TROUBLESHOOTING TREE FAULT 51 AND FOUND CDP TUBES CLOGGED. MAI - [SDR IXXA080016O](https://openairdocs.org/sdr/IXXA080016O.md): Fire Loop · shorted · May 1, 2008 · N606AL · Doug DC873F · Fire Detection > DURING CRUISE FROM KTOL, NUMBER THREE ENGINE FIRE WARNING LIGHT AND BELL CAME ON INTERMITTENTLY. THE CREW ACCOMPLISHED THE ENGINE FIRE CHECKLIST AND DISCHARGED BOTH BOTTLES. AFTER BOTH BOTTLES WERE DISCHARGED THE FIRE WARNING CAME ON STEADY AND STAYED ON JUS - [SDR IXXA080004O](https://openairdocs.org/sdr/IXXA080004O.md): Switch · defective · Jan 24, 2008 · N606AL · Doug DC873F · Landing Gear Position and Warning > DURING CLIMB FROM KTOL, AFTER GEAR WAS RETRACTED DOOR NOT LATCH LIGHT CAME ON, THE CREW CYCLED THE GEAR THE LIGHT STAYED ON. THE CREW ACCOMPLISHED UPLATCH CHECK AND CYCLED THE GEAR A SECOND TIME THE LIGHT STAYED ON. THE CREW CLIMB TO 32,000 FEET CYCLED THE G - [SDR IXXA07SMN224S](https://openairdocs.org/sdr/IXXA07SMN224S.md): Structure · misrepaired · Aug 21, 2007 · N606AL · Doug DC873F · Fuselage Main, Structure > DURING ROUTINE C CHECK INSPECTION, FS 1345, LONGERON 30.5 LEFT. DOUBLER BELOW AND AFT OF AFT EMERGENCY EXIT DOOR. REPAIR NUMBER 606 AL-R36. PROBLEM: SIDE 2, 2ND ROW EXCEEDS MAS RIVET SPACING. DISPOSITION: ADD RIVETS TO BRING INTO LIMITS OR UPGRADE. - [SDR IXXA07SMN223S](https://openairdocs.org/sdr/IXXA07SMN223S.md): Fitting · corroded · Aug 21, 2007 · N606AL · Doug DC873F · Fuselage Main, Attach Fittings > DURING ROUTINE C CHECK INSPECTION, MAIN CARGO LT CUSP EXTRUSION, FITTING WITH CORROSION AT STA 80.000, L-21L. - [SDR IXXA07SMN225S](https://openairdocs.org/sdr/IXXA07SMN225S.md): Longeron · misrepaired · Aug 21, 2007 · N606AL · Doug DC873F · Fuselage Main, Longeron/Stringer > DURING ROUTINE C CHECK INSPECTION, FS 1367, LONGERON 30.5 LEFT, DOUBLER BELOW AND AFT OF AFT EMERGENCY EXIT DOOR. REPAIR NUMBER 606AL-R37. PROBLEM: SIDE 2 ENDS ON LONGERON WITHOUT FINGER DOUBLER. DISPOSITION: UPGRADE IAW SRM. - [SDR IXXA07SMN217S](https://openairdocs.org/sdr/IXXA07SMN217S.md): Fitting · cracked · Aug 17, 2007 · N606AL · Doug DC873F · Fuselage Main, Attach Fittings > DURING ROUTINE C CHECK INSPECTION, MAIN CARGO CMPT AFT FITTING SHOWS CRACK 2" BETWEEN STA 1220.000 AND L-19R. REPLACED CRACKED FITTING WITH NEW FITTING IAW DC8 SRM 51-1-20D. - [SDR IXXA07SMN222S](https://openairdocs.org/sdr/IXXA07SMN222S.md): Spar · cracked · Aug 17, 2007 · N606AL · Doug DC873F · Wing Spar > DURING ROUTINE C CHECK INSPECTION, NR 2 MAIN TANK WEB OF CENTRAL SPAR (LWR SIDE) CRACKED 2 1/2" AT STA XRS 172.000 BETWEEN S-61 AND S-62. - [SDR IXXA07SMN212S](https://openairdocs.org/sdr/IXXA07SMN212S.md): Skin · dented · Aug 17, 2007 · N606AL · Doug DC873F · Trailing Edge Flaps > DURING ROUTINE C CHECK INSPECTION, LT WING INBD FLAP UPPER SKIN SHOWS DENT AT XW 88.000. - [SDR IXXA07SMN211S](https://openairdocs.org/sdr/IXXA07SMN211S.md): Longeron Splice · cracked · Aug 17, 2007 · N606AL · Doug DC873F · Fuselage Main, Longeron/Stringer > DURING ROUTINE C CHECK INSPECTION, MAIN CARGO CMPT LONGERON SPLICE FITTING CRACKED AT STA 1690.000 L-36. - [SDR IXXA07SMN221S](https://openairdocs.org/sdr/IXXA07SMN221S.md): Spar Cap · cracked · Aug 17, 2007 · N606AL · Doug DC873F · Wing Spar > DURING ROUTINE C CHECK INSPECTION, NR 2 MAIN TANK LOWER CAP OF CENTER SPAR 3" CRACKED AT STA ZRS 172.000 BETWEEN S-61 AND S-62. - [SDR IXXA07SMN214S](https://openairdocs.org/sdr/IXXA07SMN214S.md): Skin · corroded · Aug 17, 2007 · N606AL · Doug DC873F · Horizontal Stabilizer, Plate/Skin > DURING ROUTINE C CHECK INSPECTION, LT HORIZONTAL STABILIZER, POINTS OF CORROSION ON UPPER SKIN FROM STA XE 28.843 TO STA XE 30.000. - [SDR IXXA07SMN216S](https://openairdocs.org/sdr/IXXA07SMN216S.md): Fitting · cracked · Aug 17, 2007 · N606AL · Doug DC873F · Fuselage Main, Attach Fittings > DURING ROUTINE C CHECK INSPECTION, MAIN CARGO CMPT FWD FITTING SHOWS CRACK 1" BETWEEN STA 1152.000 AND L-20R. - [SDR IXXA07SMN218S](https://openairdocs.org/sdr/IXXA07SMN218S.md): Fitting · cracked · Aug 17, 2007 · N606AL · Doug DC873F · Fuselage Main, Attach Fittings > DURING ROUTINE C CHECK INSPECTION, MAIN CARGO CMPT AFT FITTING SHOWS CRACK 2" AT STA 759.000 AND L-18.8L. - [SDR IXXA07SMN215S](https://openairdocs.org/sdr/IXXA07SMN215S.md): Fitting · cracked · Aug 17, 2007 · N606AL · Doug DC873F · Horizontal Stabilizer, Attach Fittings > DURING ROUTINE C CHECK INSPECTION, RT HORIZ STABILIZER FITTING SHOWS CRACK 2" FRONT PART AT STA NFS 60.000. - [SDR IXXA07SMN220S](https://openairdocs.org/sdr/IXXA07SMN220S.md): Spar · cracked · Aug 17, 2007 · N606AL · Doug DC873F · Wing Spar > DURING ROUTINE C CHECK INSPECTION, NR 1 MAIN TANK CTR SPAR WEB LWR SIDE, CRACK 4" AT STA XRS 255.000 BETWEEN S-61 AND S-62. - [SDR IXXA07SMN219S](https://openairdocs.org/sdr/IXXA07SMN219S.md): Spar · cracked · Aug 17, 2007 · N606AL · Doug DC873F · Wing Spar > DURING ROUTINE C CHECK INSPECTION, NR 1 MAIN TANK, CTR SPAR LWR CAP, CRACKED 3" AT STA XRS 255.000 BETWEEN S-61 AND S-62. - [SDR IXXA07SMN213S](https://openairdocs.org/sdr/IXXA07SMN213S.md): Skin · dented · Aug 17, 2007 · N606AL · Doug DC873F · Trailing Edge Flaps > DURING ROUTINE C CHECK INSPECTION, LT WING INNER FLAP, UPPER SKIN SHOWS DENT BETWEEN STA XF 112.000 TO STA XF 120.000. - [SDR IXXA07SMN209S](https://openairdocs.org/sdr/IXXA07SMN209S.md): Skin · dented · Aug 13, 2007 · N606AL · Doug DC873F · Elevator, Plate/Skin > DURING ROUTINE C CHECK INSPECTION, RT ELEVATOR OIL CANNING LOWER PANEL, PLATING AT STA XE 279.000 STA XE 306.000. Next page: https://openairdocs.org/deregistered/N606AL-2014-10-06/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 = 'N606AL' AND deregistration_id = 'N606AL-2014-10-06' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N606AL-2014-10-06/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.