N866AT, cancelled Aug 12, 2005

Service difficulty reports · 52

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 = 'N866AT' AND deregistration_id = 'N866AT-2005-08-12'
  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 AT0200047Actuator · stickingFORWARD NOSE GEAR DOOR REMAINED OPEN ON DEPARTURE/BURNED DOWN FUEL, RETURNED TO BASE. FOUND NOSE GEAR DOOR MANUAL ACTUATOR STICKING, LUBED ACTUATOR AND MANUALLY OPERATION PERFORMED GOOD, AIRCRAFT GOOD TO CONTINUE IAW M/M 32-00 AND 12-90.Apr 9, 2002 · N866AT · Doug DC932 · Landing Gear Door ActuatorSDR AT0200028Wire · brokenDURING EMERGENCY LIGHTING CHECK OUT FOUND TAIL CONE EMERGENCY RELEASE HANDLE LIGHT INOP. FURTHER INVESTIGATION REVEALED POSITIVE WIRE CUT IN HALF 2 FEET FROM LIGHT.Mar 3, 2002 · N866AT · Doug DC932 · Light System WiringSDR AT0100236Battery · dischargedFOUND EMERGENCY LIGHTS WILL NOT EXTINGUISH. CORRECTIVE ACTION: REMOVED AND REPLACED NICAD BATTERY PACK, D5-28, B5-27. IAW DC9 MM 33-50Nov 29, 2001 · N866AT · Doug DC932 · Emergency LightingSDR AT0100176Proximity Sensor · out of adjAIRCRAFT WOULD NOT TRANSFER TO FLIGHT MODE. AIRCRAFT WAS FERRIED FOR TROUBLESHOOTING. RIGGED AND ADJUSTED GROUND SENSE MECHANISM AND SERVICED NOSE STRUT IAW DC9 MM 32-23-1, 32-21-2.Feb 12, 2001 · N866AT · Doug DC932 · Landing Gear Position and WarningSDR AT0100001Strut · dischargedUNABLE TO RAISE GEAR ON TAKEOFF. SUSPECT SQUAT SWITCH PROBLEM. TRIED GEAR LEVER SEVERAL TIMES. SERVICED NOSE STRUT WITH NITROGEN IAW MM 32-21. PERFORMED CHECK OF GROUND SENSING SWITCHES IAW MM 32-23-01.Jan 12, 2001 · N866AT · Doug DC932 · Nose/Tail Landing Gear Strut/AxleSDR AT0000504Smoke Detector · damagedFOUND JUST AFTER TAKE OFF 'A' LOOP SMOKE DETECTOR IN FORWARD CARGO COMPARTMENT LIGHT ILLUMINATED. RETURNED TO CAK AIRPORT LIGHT EXTINGUISHED AFTER LANDING. CORRECTIVE ACTION: MAINTENANCE CHECKED DETECTION SYSTEM, FOUND DETECTORS DAMAGED FODec 15, 2000 · N866AT · Doug DC932 · Smoke DetectionSDR AT0000502Skin · crackedFOUND CRACKED EXTERIOR SKIN IN LOWER AFT DOOR JAMB CORNER OF FORWARD SERVICE DOOR. CUT OUT CRACKED SECTION, FABRICATED REPAIR DOUBLERS, SHIMS AND FILLERS. IAW DC9 SRM 51-10-2, 51-10-3, 51-10-4, 51-30-2, AND 51-30-5, DRAWING SR0953017C AND E.O. 095310-29-E14Oct 29, 2000 · N866AT · Doug DC932 · Fuselage Main, Plate/SkinSDR AT0000475Frame · corrodedFOUND VERTICAL STABILIZER LEADING EDGE UPPER KNEE CUP HAS CORROSION. REMOVED AND REPLACED VERTICAL STABILIZER LEADING EDGE HORSESHOE FORMER IAW DC9 SRM 51-10-02, 51-10-3, 51-10-4, 55-31-0 FIGURE 4.Oct 21, 2000 · N866AT · Doug DC932 · Vertical Stabilizer, Spar/RibSDR AT0000469Longeron · corrodedFOUND CORROSION ON LEFT LONGERON NR 20 AT THE OUTBOARD MEMBER SURFACE. CORROSION WAS OUT OF LIMITS, REMOVED CORRODED SECTION. FABRICATED AND INSTALLED LONGERON SPLICE AND STRAP IAW DC9 SRM 51-10-4, 51-10-3, 53-02 FIGURE 9A.Oct 7, 2000 · N866AT · Doug DC932 · Fuselage Main, Longeron/StringerSDR AT0000468Floorbeam · corrodedFOUND FLOOR SUPPORT BEAM AT BS 1012 RBL 24 TO LBL 24 WAS CORRODED. MECHANICALLY REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REMOVED LEFT AND RIGHT BEAM AND LOWER DOOR JAMB. FABRICATED AND INSTALLED NEW JAMB, PANELS AND ANGLES IAW DC9 SRM 51-30-2, 53-01 FOct 6, 2000 · N866AT · Doug DC932 · Fuselage Main, Floor BeamSDR AT0000466Skin · corrodedFOUND FLOOR BOARD NR 80 CORRODED ON SKIN. REMOVED CORROSION AND FOUND 3 CRACKS. REPAIRED SKIN, REMOVED AND INSTALLED HATS, AND REINSTALLED FLOOR BOARD IAW DC9 MM 53-20-1, DC9 SRM 53-21-0, 51-10-03, 51-30-2, 53-20-1.Oct 6, 2000 · N866AT · Doug DC932 · Fuselage Main, Plate/SkinSDR AT0000465Floor Panel · crackedFOUND FLOORBOARD NR 67 TEMPORARY PATCH INSTALLED. REMOVED FLOOR PANEL NR 67, FABRICATED REPAIR SKIN. REPLACED HAT CHANNELS AND INSTALLED REPAIR SKIN. REINSTALLED FLOOR PANEL IAW DC9 MM 53-20-1, DC9 SRM 51-10-3, 51-30-2.Oct 6, 2000 · N866AT · Doug DC932 · Fuselage Floor PanelSDR AT0000474Floor Panel · corrodedFOUND FLOOR PANEL 4692 CORRODED AND HAT CHANNELS CRACKED. REMOVED FLOOR PANEL AND REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. FABRICATED, TREATED, AND INSTALLED NEW FLOOR PANEL AND HAT CHANNELS IAW DC9 MM 53-20-1 DC9 SRM 51-10-3.Oct 5, 2000 · N866AT · Doug DC932 · Fuselage Floor PanelSDR AT0000467Floor Panel · corrodedFOUND FLOOR BOARD NR 4695 WAS CORRODED. BLENDED OUT CORROSION, FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED HATS AND FABRICATED AND INSTALLED FLOOR PANEL IAW DC9 MM 53-20, DC9 SRM 53-01 FIGURE 1, 51-10-2, 51-10-4, 51-30-2, 53-20-1.Oct 5, 2000 · N866AT · Doug DC932 · Fuselage Floor PanelSDR AT0000490Panel · corrodedFOUND PANEL 1211 AT RIGHT WING LOWER LEADING EDGE HAS AREA OF CORROSION ON OUTER SURFACE. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS, FORMED REPAIR DOUBLER, TREATED, PRIMED AND INSTALLED. IAW DC9 SRM 51-10-3, 51-30-1, 51-30-2, 57-01 FIGURE 2A, FIGURE 1Oct 3, 2000 · N866AT · Doug DC932 · Wing, Plate/SkinSDR AT0000125Connector · disconnectedNO RIGHT MAIN LANDING GEAR GREEN LIGHT FOR THE LANDING GEAR DOWN INDICATION. CORRECTIVE ACTION: CORRECTED OPEN WIRE AT RT GEAR DOWN LIMIT CONNECTOR (P1-129).Mar 20, 2000 · N866AT · Doug DC932 · Landing Gear Position and WarningSDR AT0000127Light · dislodgedEMERGENCY PATH LIGHTING IN BUSINESS CLASS IS OUT OF TRACK. CORRECTIVE ACTION: RESECURED LIGHT.Mar 18, 2000 · N866AT · Doug DC932 · Emergency LightingSDR AT0000057Light · failedFOUND TAIL CONE LEFT STAIR EMERGENCY LIGHT WOULD NOT ILLUMINATE. RELAMPED UNIT IAW DC9 MM 33-50.Jan 25, 2000 · N866AT · Doug DC932 · Emergency LightingSDR AT0000038Strut · dischargedFOUND LANDING GEAR UPLATCH RELEASE OR GROUND SHIFT DID NOT WORK AND WOULD NOT RAISE. ON FINAL AT BUF (BUFFALO). GROUND SHIFT OR THE UPLATCH RELEASE WAS HEARD TO HAVE RELEASED. PERFORMED GEAR SWING. NOSE LANDING GEAR FOUND TO BE UNDER SERVICED WITH FLUID ANJan 23, 2000 · N866AT · Doug DC932 · Nose/Tail Landing Gear Strut/AxleSDR AT0000037Strut · dischargedFOUND AFTER TAKEOFF AIRCRAFT WOULD NOT PRESSURIZE AND GEAR WOULD NOT COME UP. RETURNED TO BMI (BLOOMINGTON-NORMAL). STEERING IN AIR WOULD TURN. INSPECTED AIRCRAFT AND FOUND NOSE STRUT FLAT. SERVICED STRUT IAW DC9 MM 32-30.Jan 21, 2000 · N866AT · Doug DC932 · Nose/Tail Landing Gear Strut/AxleSDR AT0000008Engine · fodON CLIMB-OUT, NOISE AND VIBRATION WERE NOTED FROM NUMBER 2 ENGINE. NR 2 ENGINE SHUT DOWN, AIRCRAFT RETURNED FOR LANDING. REMOVED AND REPLACED NR 2 ENGINE AND CONFIRMED BIRD STRIKE.Jan 3, 2000 · N866AT · Doug DC932 · Engine (Turbine/Turboprop)SDR AT9900895Glide Slope · inoperativeDURING CLIMB-OUT, NR 2 NAV BECAME INOPERATIVE AND ALL FLOURESCENT LIGHTS FLICKERED. RESEATED NR 2 NAV CONTROL PANEL IAW DC9 MM 34-32 AND TESTED LIGHTING IAW DC9 MM 33-10.Dec 21, 1999 · N866AT · Doug DC932 · Glide Slope SystemSDR AT9900722Clamp · failedINBOUND TO ATL LOST CABIN PRESSURIZATION AT 14,000 FT, PASSENGER OXYGEN MASKS DEPLOYED. BOTH AIR CONDITIONING PACKS QUIT AT THE SAME TIME. BOTH PACKS WERE RESTARTED BUT THEY QUIT AGAIN. FOUND RIGHT AIR CYCLE MACHINE DISCHARGE DUCT BLOWN. RE-SECURED BLOWN DOct 9, 1999 · N866AT · Doug DC932 · Cabin Cooling SystemSDR AT9900637Rib · gougedSCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND GOUGED ON THE LEADING EDGE NR 3 SLAT RIB AT XOS 288.193. BLEND OUT GOUGED AREA, TREAT, PRIMED, AND REFINISH IAW DC9 SRM 57-01-0 FIG 1, SHEET 3, 57-21-1 FIG 1, AND TIMCO EO NR 99-1238.Sep 5, 1999 · N866AT · Doug DC932 · Leading Edge DevicesSDR AT9900587Skin · corrodedDURING A ROUTINE INSPECTION AT TIMCO LAKE CITY FL, FOUND EXTERIOR FUSELAGE SKIN HAS BULGE AT BS 990 L25L. REMOVED CORROSION AT BS 976-996. FABRICATED, TREATED, PRIMED AND INSTALLED REPAIR DOUBLERS IAW TIMCO EO NR 99-1213 AND DC9 SRM 51-10-3 AND 53-01 FIG 1.Aug 14, 1999 · N866AT · Doug DC932 · Fuselage Main, Plate/SkinSDR AT9900586Skin · corrodedDURING A ROUTINE INSPECTION AT TIMCO LAKE CITY FL, FOUND EXTERIOR FUSELAGE SKIN OF AFT CARGO DOOR AT BS 935 CORRODED. CUT OUT CORRODED AREA. FORMED, DRILLED, COUNTERSUNK, DEBURRED, TREATED, PRIMED AND INSTALLED DOUBLER IAW DC9 SRM 51-10-4, 51-10-3, 51-20-0, Aug 13, 1999 · N866AT · Doug DC932 · Fuselage Main, Plate/SkinSDR AT9900570Longeron · chafedDURING SCHEDULED INSPECTION AT TIMCO, FOUND FLANGE OF LONGERON AT RT BOTTOM OF BS 1076 CHAFED. BLENDED OUT CHAFED AREA. FABRICATED AND INSTALLED EXTERNAL STRAP REPAIR AND FILLER IAW DC9 SRM 51-30-5 AND EO NR 99-1216.Aug 9, 1999 · N866AT · Doug DC932 · Fuselage Main, Longeron/StringerSDR AT9900569Panel · corrodedDURING SCHEDULED INSPECTION AT TIMCO LAKE CITY FL, FOUND CORROSION ON INNER FLANGE LT PANEL NR 2108A. CLEANED CORROSION ON INNER FLANGE. FABRICATED, TREATED, PRIMED AND INSTALLED STRIPS ON INNER FLANGE IAW DC9 SRM 51-10-3, 51-10-2, 51-10-4.Aug 6, 1999 · N866AT · Doug DC932 · Wing, Plate/SkinSDR AT9900564Fixed Vane · corrodedDURING SCHEDULED CHECK AT TIMCO LAKE CITY FL, FOUND SPOTS OF CORROSION ON UNDERSIDE OF RT WING FLAP FIXED VANE. REMOVED CORROSION. FABRICATED FILLERS AND DOUBLER. BONDED REPAIR. ALODINED AND SEALED IAW DC9 SRM 57-50-9 IG 2, 51-50-2.Jul 31, 1999 · N866AT · Doug DC932 · Wing Miscellaneous StructureSDR AT9900567Floor · corrodedDURING SCHEDULED CHECK AT TIMCO LAKE CITY FL, FOUND FWD ENTRY FLOOR PANEL AT BS 160-200 RT CORRODED. FABRICATED NEW PANEL IAW DC9 SRM 53-20-0, 51-10-4.Jul 29, 1999 · N866AT · Doug DC932 · Fuselage Floor PanelSDR AT9900563Floor · corrodedDURING SCHEDULED CHECK AT TIMCO LAKE CITY FL, FOUND FLOOR PANEL ON RT SIDE AT BS 280 CORRODED. FABRICATED NEW PANEL AND INSTALLED IAW DC9 SRM 51-21-0, 51-30-1.Jul 29, 1999 · N866AT · Doug DC932 · Fuselage Floor PanelSDR AT9900562Fixed Vane · corrodedDURING SCHEDULED CHECK AT TIMCO LAKE CITY FL, FOUND OUTBOARD FIXED VANE ON RT WING CORRODED. FABRICATED FILLER AND DOUBLER. INSTALLED IAW DC9 SRM 57-50-1, 51-70-2, 51-10-3, 51-30-2.Jul 29, 1999 · N866AT · Doug DC932 · Wing Miscellaneous StructureSDR AT9900561Panel · corrodedDURING SCHEDULED CHECK AT TIMCO LAKE CITY FL, FOUND RT WING LOWER LEADING EDGE PANEL CORRODED. REMOVED CORROSION. FABRICATED DOUBLERS, TREATED, PRIMED AND INSTALLED IAW SRM 57-01 FIG3, 51-10-03, 51-20-0, 51-30-2.Jul 29, 1999 · N866AT · Doug DC932 · Wing, Plate/SkinSDR AT9900541Fitting · corrodedSCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND THE FORWARD CABIN GALLEY AREA AT BS 149 L-18R AT CUSP LINE LOWER FRAME WEB AND ATTACH FITTING CORRODED. REMOVED AND REPLACED FITTING, CLEAN CORROSION ON LOWER WEB WITHIN LIMITS, TREATED AND PRIMED AREAS IAW DJul 29, 1999 · N866AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT9900540Web · crackedSCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND THE LEFT CUSP WEB AT BS 737-756 WITH CORROSION AND CRACKS. FABRICATED NEW CUSP WEB, TRIMMED AND DRILLED TO FIT, ALODINED AND PRIMED IAW DC9 SRM 51-10-3, AND 51-10-4.Jul 29, 1999 · N866AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT9900545Floor · corrodedSCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND THE FORWARD ENTRY FLOOR PANEL AT BS 180-200 CORRODED. FABRICATED FLOOR BOARD, DRILLED, DEBURRED, COUNTERSUNK, DRILLED AND INSTALLED HAT CHANNELS PARTS, AND INSULATION IAW DC9 SRM 53-01 FIG.1, 51-10-4, 51-30-Jul 27, 1999 · N866AT · Doug DC932 · Fuselage Floor PanelSDR AT9900546Skin · corrodedSCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND THE RIGHT WING LEADING EDGE PANEL NR 1219A CORRODED AND ANGLE SUPPORT CHAFFED. REMOVED CORROSION, BLEND OUT GOUGE, FABRICATED DOUBLER, TREATED, PRIMED, AND INSTALLED IAW DC9 SRM 51-10-3, 51-30-2, AND 57-01 FIJul 25, 1999 · N866AT · Doug DC932 · Wing, Plate/SkinSDR AT9900565Fitting · corrodedDURING SCHEDULED CHECK AT TIMCO LAKE CITY FL, FOUND LONGERON END FITTING AT BS 990 L-25L CORRODED. DRILLED NEW LONGERON END FITTING IAW DC9 SRM 51-10-2, 51-10-3, 51-10-4.Jul 24, 1999 · N866AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT9900535Floor · corrodedDURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND FWD ENTRY RT FLOOR PANEL AT BS 200-280 CORRODED. 3 HAT CHANNELS CRACKED, ELONGATED HOLES AND INSULATION MISSING. FABRICATED NEW FLOOR PANEL AND HAT CHANNELS IAW DC9 SRM 53-21-0, 51-10-4. REINSTALLEJul 23, 1999 · N866AT · Doug DC932 · Fuselage Floor PanelSDR AT9900544Skin · corrodedSCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND THE RIGHT WING FLAP 25 AND 27 INCHES OUTBOARD OF INBOARD FLAP ACTUATOR CORRODED. REMOVED FASTENERS, BURNISHED CORROSION, FABRICATED DOUBLER, DRILLED, DEBURRED, TRIMMED, TREATED, PRIMED AND INSTALLED IAW DC9 SJul 22, 1999 · N866AT · Doug DC932 · Trailing Edge FlapsSDR AT9900607Floor · corrodedSCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND RIGHT FLOOR PANEL AT BS 160-180 CORRODED. FABRICATED FLOORBOARD PANEL, DRILLED, DEBURRED, DIMPLED, ALODINED, PRIMED, AND INSTALLED NUT PLATES IAW DC9 SRM 53-21 FIG D, 51-10-4, 51-10-3, AND 51-30-2.Jul 21, 1999 · N866AT · Doug DC932 · Fuselage Floor PanelSDR AT9900536Frame · corrodedDURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND CANTED FRAME AT BS 1074 CORRODED ON FWD SURFACE BELOW L-2L. REMOVED OLD WEB. FABRICATED WEB REPAIR. DRILLED, DEBURRED, TREATED, PRIMED AND INSTALLED WEB REPAIR IAW DC9 SRM 53-01 FIG 1, 51-30-2, 51-Jul 21, 1999 · N866AT · Doug DC932 · Fuselage Main, FrameSDR AT9900534Floor · corrodedDURING A SCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND FLOOR PANEL NR 4693 AT BS 180-200 CORRODED ON TOP SIDE OF PANEL AND INSULATION TORN. REMOVED CORROSION, PANEL OUT OF LIMITS. FABRICATED NEW FLOOR PANEL IAW 53-21-0, 51-10-3, 51-30-2.Jul 21, 1999 · N866AT · Doug DC932 · Fuselage Floor PanelSDR AT9900560Fitting · corrodedDURING SCHEDULED CHECK AT TIMCO LAKE CITY FL, FOUND LONGERON END FITTING CORRODED AT BS 990 L24L. OBTAINED NEW END FITTING. DRILLED AND DEBURRED IAW SRM 51-10-2, 51-10-3, 51-10-4.Jul 20, 1999 · N866AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT9900513Floor · corrodedSCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND FLOOR PANEL AT BS 200-280 LEFT CORRODED ALONG EDGE UPPER AND LOWER FLANGE. CRACKS ON END HOLES IN PANEL. HAT CHANNEL CORRODED ENTIRE LENGTH. UPON FURTHER EVALUATION, FLOOR PANEL HAD EXFOLIATION CORROSION. Jul 19, 1999 · N866AT · Doug DC932 · Fuselage Floor PanelSDR AT9900543Seat Track · corrodedSCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND THE CABIN RIGHT INBOARD SEAT TRACK AT 198-206 RBL-22 CORRODED. REMOVED SEAT TRACK, LOCATED AND DRILLED, TRIMMED, COUNTERSUNK, DEBURRED, TREATED, PRIMED, AND INSTALLED IAW DC9 SRM 51-10-4, 51-30-1, 51-10-3, ANJul 18, 1999 · N866AT · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR AT9900542Seat Track · corrodedSCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND THE FORWARD CABIN OUTBOARD SEAT TRACK AT BS 198-205 RBL-44 CORRODED. REMOVED SEAT TRACK, CUT, DRILLED, TRIMMED SECTION, ALODINED, PRIMED AND INSTALLED SPLICE IAW DC9 SRM 53-20-1, 53-05 FIG 4F, 51-10-3, AND 51Jul 18, 1999 · N866AT · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR AT9900640Pan · corrodedSCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND THE RIGHT SIDE AFT CARGO PIT DOOR CUT OUT CORRODED. REPAIRED THE AFT CARGO DOOR FUSELAGE CUT OUT PAN AFT CORNER BY REMOVING CORROSION AND FABRICATING AND INSTALLING REPAIR DOUBLER IAW DC9 SRM 51-10-3, 51-10-4Jul 17, 1999 · N866AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT9900599Panel · corrodedDURING A ROUTINE INSPECTION AT TIMCO LAKE CITY FL, FOUND EXTERIOR FUSELAGE LT SIDE AT BS 237-303 HAS SPOTS OF SURFACE CORROSION AROUND WINDOW FRAME BELT. HFEC AND DYE PENETRANT INSPECTION PERFORMED BEFORE REMOVAL OF PANEL. BLEND OUT CORROSION, REMOVED AND REJul 17, 1999 · N866AT · Doug DC932 · Fuselage Main, Plate/SkinSDR AT9900337Duct · looseTAIL COMPARTMENT TEMPERATURE HIGH LIGHT CAME ON AFTER TAKEOFF, LIGHT WENT OUT WHEN LEFT THROTTLE PULLED BACK TO IDLE. AIR RETURN. RESECURED DUCT BEFORE LEFT HAND AIR CYCLE MACHINE PER MM 36-10. OPS CHECK AND LEAK CHECK GOOD PER 36-10.Apr 27, 1999 · N866AT · Doug DC932 · Pneumatic Distribution System
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