Pratt & Whitney Canada JT15D-1 series

Service difficulty reports · 84

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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 engine_model_key = 'JT15D1'
  ORDER BY difficulty_date DESC"

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SDR 5JHA20250930231Compressor · stalledWHILE IN CRUISE FLIGHT AT FL370 (37,000 FT) THE LEFT ENGINE SUFFERED A SUSPECTED COMPRESSOR STALL WHICH SUBSEQUENTLY LEAD TO THE COMPLETE FAILURE/FLAMEOUT OF THE LEFT ENGINE. ALL REQUIRED QRH PROCEDURES WERE ACCOMPLISH ALONG WITH AN ATTEMPTED RELIGHT/RESTART Sep 30, 2025 · N16NL · Cessna 501 · Turbine Engine Compressor SectionSDR 2017FA0000394Pump · failedLEFT ENGINE OIL PUMP HAD INTERNAL FAILURE. UPON START OF THE LEFT ENGINE, NO TURBINE SPEED OR OIL PRESSURE INDICATION .Feb 13, 2017 · N91VB · Cessna 550 · Turbine Engine Oil SystemSDR CA141218002Engine · shutdown(CAN) DURING CRUISE, PILOT OBSERVED NR 1 ENGINE OIL PRESSURE LIGHT ON AND A FEW SECONDS LATER THE OIL PRESSURE GAUGE SHOWED "ZERO" PSI. PILOT IN COMMAND SHUT DOWN THE ENGINE AND CONTINUED FLIGHT TO THE INTERNATIONAL AIRPORT WHERE AN UNEVENTFUL LANDING WAS MADEDec 3, 2014 · Engine (Turbine/Turboprop)SDR CA140318001Tube · defective(CAN) MS9382-04 TEE TUBE, AN OIL LEAK WAS NOTED DURING A ROUTINE LEAK CHECK PERFORMED BY ASSEMBLY AND TEST. FOLLOWING INVESTIGATION, THE LEAK WAS ATTRIBUTED TO A TEE TUBE, PN MS9382-04 ASSEMBLED INTO A TUBE ASSEMBLY. RECEIVED THIS INDUSTRY STANDARD PART FROMMar 18, 2014 · Turbine Engine Oil SystemSDR 2013FA0000056Transmitter · brokenACFT DECLARED AN EMERGENCY, LANDING WITH THE RT ENGINE SHUTDOWN AND REPORTED THAT THE ENGINE FLAMED OUT ON TAKEOFF. THERE WAS A SMALL AMOUNT OF FUEL IN THE COWLING. ON REMOVAL OF THE COWLING IT WAS DISCOVERED THAT THE FUEL FLOW TRANSMITTER WAS BROKEN (TWO SCJan 25, 2013 · N84EC · Cessna S550 · Engine Fuel Indicating SystemSDR L7OA2012F00165Indicator · inoperativeLEFT ENGINE INSTRUMENT DISPLAY INOPERATIVE.Aug 14, 2012 · N347MH · Cessna 501 · Engine Indicating SystemSDR K45A2012070202Skin Panel · dentedACFT WAS INSPECTED TO CHECK OUT BASE MX (FOD INSPECTION). A 3" BY 5" DENT .125" DEEP WAS DISCOVERED 2 FT INBD OF STALL STRIP UNDER THE DEICE BOOT. DAMAGE WILL BE REPAIRED IAW EA RECOMMENDATIONS.Jun 29, 2012 · N980AG · Cessna 560CESSNA · Wing, Plate/SkinSDR K45A2012070201Liner · damagedENGINE WAS INSPECTED TO CHECK OUT BASE MX (FOD INSPECTION). ABRADABLE MATERIAL WAS FOUND MISSNG FROM LOW COMPRESSOR CASE FTO 9 O`CLOCK THROUGH OUT 10:30 O`CLOCK POSITION. BELIEVE THE MATERIAL WAS LOOSENED BY THE BIRD STIKE BUT NOT EASILY DETECTED. THE MATERJun 29, 2012 · N980AG · Cessna 560CESSNA · Turbine Engine Compressor SectionSDR DXTR2012009Inlet · crackedLT ENGINE INLET FAN FLANGE CRACKED APPROX AT 9 OCLOCK POSITION, CRACK IS 4" IN LENGTH.Jan 31, 2012 · N819QS · Cessna 560CESSNA · Engine Air Intake SystemSDR CA110928011Line · damaged(CAN) OPERATOR REPORTED PERSISTENT SERVICING REQUIREMENT OF THE OXYGEN SYSTEM. INVESTIGATION FOUND A PINHOLE LEAK IN THE SOLDER JOINT AT THE BULKHEAD ATTACH END OF THE LINE ASSY-PRESSURE BULKHEAD TO OXYGEN GAGE. PN 9912057-7 (ALT S1721-20).Sep 7, 2011 · Cessna 500CESSNA · Passenger Oxygen SystemSDR CA110412003Line · misinstalled(CAN) RIGID FUEL LINE, WAS MAKING CONTACT WITH THE LOWER COWL ASSY AND SUBSEQENTLY WEARING THE SKIN. INVESTIGATION SHOWS THE FUEL LINE MAY NOT HAVE BEEN INSTALLED CORRECTLY. THE FUEL LINE HAS 1 SHORTER TUBE THAT SHOULD BE SECURED TO THE ENGINE DRIVEN FUEL PApr 11, 2011 · Cessna 560XL · Aircraft Fuel Distribution SystemSDR FDEA201010264174Valve · inoperativeRT AIR MIX VALVE STUCK FULL COLD. FOLLOWED BY LOSS OF CABIN PRESSURIZATION. RAN PACKS INDIVIUALY AND TOGETHER. PERFORMED LEAK CK OF DUCTS, PACKS, MIX VLVS. NO DEFECTS NOTED. PERFORMED BITE TEST OF 35 DEG VALVE AND WATCHED VALVES OPERATE. PULLED C/B ON Oct 26, 2010 · N466FE · Boeing 727225 · Cabin Pressure Control SystemSDR DXTA2010081804198Engine · flamed outENGINE 1 HAD A UNCOMMANDED FLAME OUT ON THE RAMP PRIOR TO TAXI. ALL ENGINE INDICATIONS WERE NORMAL PRIOR TO THE FLAMEOUT. REMOVED COWL, INSPECTED ENGINES, FOUND THE IDLE DETENT FRICTION OUT OF ADJUSTMENT. AJUSTED IDLE DETENT FRICTION TO PROPER AJUSTMENT. RAAug 17, 2010 · N348QS · Cessna 560CESSNA · Engine (Turbine/Turboprop)SDR FDEA201008032789Skin · gougedMCD INNER SURROUND SKIN GOUGED STA 620-630, STR 16L. REPAIRED MCD INNER SURROUND SKIN IAW EA 7-5330-135571.Aug 3, 2010 · N466FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR DXTA20082870Landing Gear · malfunctionedUPON RETRACTION OF LANDING GEAR, GEAR UNSAFE LIGHT ILLUMINATED. JACKED AND SWUNG GEAR TEN TIMES WITH NO FAULTS. LUBED ALL UP LOCK ROLLERS AND GEAR. OPS CHECKED GOOD IAW MM CH32-01-00.Feb 12, 2008 · N375QS · Cessna 560CESSNA · Landing Gear Retraction/Extension SystemSDR DXTA200802810Hose · leakingDURING TOUCHDOWN AT PDK, COPILOT'S LT BRAKE PEDAL WENT COMPLETELY TO THE FLOOR. REMOVED AND REPLACED BOTH CO-PILOTS UPPER MASTER CYLINDER HOSES. IAW MM CHAP 32-42-02. ALSO COMPLETED APPROVED BLEEDING PROCEDURES CHAP 32-42-00.Jan 30, 2008 · N375QS · Cessna 560CESSNA · Landing Gear Brake SystemSDR DXTA200702661Brake Assy · weakBRAKES PULL AIRCRAFT NOSE HARD LT WHEN EQUAL PRESSURE IS APPLIED TO BOTH BRAKE PEDALS DURING LANDING ROLLOUT. BLED BRAKES IAW C560 M/M 32-42-00. TAXI CHECKED/BRAKE CHECKED A/C. OPS CHECKS NORM.Dec 8, 2007 · N348QS · Cessna 560CESSNA · Landing Gear Brake SystemSDR DXTA200702370Engine · malfunctionedLT ENGINE QUIT AFTER NORMAL START SEQUENCE AND STABILIZATION. AFTER PERFORMING GENERATOR CHECK NOTICED LT FUEL BOOST PUMP ANNUNCIATOR ON, THEN N2 ROLLING DOWN. THROTTLE LEVER WAS PLACED ON GATE AND NEVER MOVED. PERFORMED LEFT ENGINE START PROCEDURES PER NJJul 31, 2007 · N303QS · Cessna 560CESSNA · Engine (Turbine/Turboprop)SDR 2007FA0000070Attach Fitting · crackedUPPER CHAIR BASE ASSEMBLY CRACKED AT CHAIR BACK ATTACH POINTS. CHAIR WAS REPAIRED IAW STC ST01042WI STRUCTURAL SEAT REPAIR. (K)Jan 8, 2007 · N117TW · Cessna 500CESSNA · Passenger Compartment EquipmentSDR 2006FA0001196Line · corrodedINVESTIGATING SOFT BRAKE CONDITION IT WAS NOTED THAT BRAKE FLUID WAS LEAKING FROM AROUND THE BELLY BEACON AND THE BEACON LENS WAS FULL OF FLUID. REMOVED THE INTERIOR AND THE CENTER AISLE FLOOR PANELS. HYDRAULIC FLUID WAS NOTED DRIPPING FROM RIDGE BRAKE LINE Nov 29, 2006 · N501LH · Cessna 500CESSNA · Hydraulic System, MainSDR CA060706003Connecting Rod · worn(CAN) PRATT & WHITNEY CANADA OVERHAUL MANUAL 3037323 REV.22, SECTION 72-30-07, PARAGRAPH 88-4 MISTAKENLY CALLS FOR NICKEL PLATING IN ACCORDANCE WITH SPOP 62. SPOP 62 IS A FLORESCENT PENETRANT INSPECTION PROCEDURE. IT IS UNDERSTOOD THAT THE MANUAL SHOULD RATHERJul 4, 2006 · Compressor Bleed ValveSDR 2006FA0000168Actuator · leakingHYDRAULIC LEAK AT SWITCH ACTUATOR ENTRY INTO NLG ACTUATOR AT 231 CYCLES INSTALLED AND 4224 CYCLES SOH/NEW. DEPELETED HYDRAULIC SYSTEM ON LANDING. (K)Feb 16, 2006 · N502BE · Cessna 500CESSNA · Landing Gear ActuatorSDR 2006FA0000000Tire · leakingREPLACED THE FRONT TIRE, WITH THIS NEW TIRE AND HAVE HAD A SLOW LEAK EVER SINCE. TOOK THE TIRE BACK OFF AND SUBMERGED THE TIRE AND WHEEL UNDER WATER, FOUND 10 VERY SMALL PINHOLES IN THE TIRE SIDEWALL CLOSE TO THE RIM EQUALLY SPACED AROUND THE SIDEWALL, THE PIDec 21, 2005 · N94LH · Beech 400A · TireSDR 2005FA0001457Transmitter · out of adjustFLAP ASYMMETRY ANNUNCIATOR ILLUMINATED DURING APPROACH. FOUND MIDBOARD ASYMMETRY DETECTOR READING 5.7 VOLTS. FOUND IB ASYMMETRY DETECTOR READING 7.8 VOLTS. ADJUSTED LT AND RT FLAP POSITION TRANSMITTERS AS REQUIRED IAW MM TO BRING VOLTAGES TO 5.8 VOLTS +/- 0Oct 10, 2005 · N419CW · Beech 400A · Trailing Edge Flap Control SystemSDR 2005FA0001369Torque Tube · crackedNOSE LANDING GEAR DOORS WERE OBSERVED TO BE DROOPING SLIGHTLY. NOSE GEAR RETRACT LINKAGE WAS INSPECTED AND TORQUE TUBE WAS OBSERVED TO HAVE A BROKEN WELD AT ONE END CAP. RECOMMEND INSPECTING WELDS CAREFULLY DURING PERIODIC INSPECTIONS. (K)Sep 23, 2005 · N561JS · Cessna 560CESSNA · Nose/Tail Landing GearSDR 2005FA0001321Line · damagedDURING COMPLIANCE WITH INSPECTION PORTION OF SB NOTED CHAFE DAMAGE TO PN 128580101-1 NOTED CHAFE DAMAGE TO PN 128-580101-1 HYDRAULIC BRAKE LINE FROM ADJACENT FLOORBOARD ATTACH SCREW. DAMAGE FOUND LESS THAN 10 PERCENT OF TUBING WALL THICKNESS. RECOMMEND THATSep 12, 2005 · N907JE · Beech 400A · Landing Gear Brake SystemSDR AJC2005F00012Squat Switch · defectiveDEPARTED, ENROUTE, AFTER TAKEOFF THE CREW REPORTED THAT THE LANDING GEAR HANDLE WAS LOCKED IN THE DOWN POSITION AND THEY COULD NOT RETRACT THE GEAR. THE LANDING GEAR DOWN LOCK OVER RIDE WAS ENGAGED AND THE GEAR RETRACTED NORMALLY. ON DESCENT, THE CREW REPORTAug 26, 2005 · N400HS · Beech 400A · Landing Gear Position and WarningSDR AJC2005F00009Valve · failedAIR RETURNED DUE TO AIR CONDITIONING FAIL LIGHT ILLUMINATED AND CABIN REVERTED TO EMERGENCY PRESSURIZATION MODE. AIRCRAFT ISSUED SPECIAL FLIGHT PERMIT, FOR MAINTENANE AT SERVICE CENTER. MAINTENANCE FOUND THE CABIN TEMPERATURE CONTROL VALVE TO BE DEFECTIVE. RJul 27, 2005 · N127BW · Beech 400A · Cabin Temperature Control SystemSDR SFO2005F00003Heat Shield · failedINSP, A LOUD SCRAPING NOISE WAS HEARD WHEN FAN WAS TURNED. BORESCOPE OF TURBINE SEC., AFTER EXHAUST DUCT WAS REMOVED, NR 4 BRG HSG HEAT SHIELD WAS FOUND BROKEN, TWISTED, IN 3 SEPARATE PIECES, WAS RUBBING ON AFT FACE OF NR 3 LOW PRESSURE TURBINE DISC. DISC WAJun 21, 2005 · N27SF · Cessna 500CESSNA · Engine (Turbine/Turboprop)SDR 2005FA0000864Clamp · defectiveDURING FLIGHT, THE CREW HEARD A POP AFTER WING DEICE HAD BEEN TURNED ON. THEY PERFORMED THE NESSARY PROCEDURES ACCORDING TO THE CHECKLIST. DETAILED INSPECTION REVEALED THAT THE SUSPECT CLAMP HAD SEPARATED AND CAUSED ENGINE BLEED AIR TO DUMP INTO THE AFT EQUIMay 21, 2005 · N234DK · Beech 400A · Pneumatic SystemSDR 2005FA0000630Relay · looseCREW SQUAWKED ELEC FUMES AND FOUL ODOR IN COCKPIT. ODOR SEEMED TO LET UP AFTER BATTERY PLACED IN EMERG AND BOTH GENERATORS PLACED IN EMERG. MAINT FOUND RT WINDSHIELD HEAT CURRENT SENSE RELAY (L102S) TERMINAL B AND APPROX 2 INCHES OF WIRE INSULATION TO OVERHEJan 27, 2005 · N430CW · Beech 400A · Windshield/Door Rain/Ice RemovalSDR 2005FA0000098Heat Shield · damagedPILOT REPORTED, HE HAD HIT AN OBJECT ON RUNWAY DUE TO IMPACT SOUND HEARD ON LT SIDE OF AC AND BRAKE ANTI-SKID FAIL INDICATION. INVESTIGATED LT WHEEL AREA AND DISCOVERED THAT TIRE HEAT SHIELD HAD PARTIALLY DISLOGED FROM WHEEL ASSY. INSPECTED AREA AND FOUND PANov 7, 2004 · N567EA · Cessna 500CESSNA · TireSDR O2G2004F00008Bearing · wornRUMBLE FROM LT MAIN GEAR. REMOVED AND REPLACED MAIN WHEEL BEARING, WHEEL AND TIRE.Oct 22, 2004 · N23YZ · Cessna 560CESSNA · Wheel/Ski/FloatSDR 2004FA0000676Battery · explodedWHILE ATTEMPTING TO PERFORM AN ENGINE START A LOUD NOISE WAS HEARD AND THE START WAS ABORTED. AN INVESTIGATION REVEALED THE MAIN BATTERY HAD EXPLODED. SEVEN OF THE TWELVE CELL CAPS WERE BLOWN OFF AND THE TOP COVER WAS BROKEN AND BLOWN OFF. BATTERY ELECTROLYAug 6, 2004 · N999AM · Cessna 500CESSNA · Battery/Charger SystemSDR R2J2004F00000Brace · mismanufacturedWHILE REINSTALLING LT WING FLAP CABLES DURING PHASE 5 INSPECTION, NOTICED CABLE RUN TOO CLOSE TO STRUCTURE. INVESTIGATION AND NOTIFIED MFG TECH SUPPORT. IT WAS DETERMINED LT BRACE 5511037-3 AND RIB 5525130, CABLE PASS THRU WERE INCORRECTLY LOCATED DURING MANJun 29, 2004 · N501CF · Cessna 501 · Trailing Edge FlapsSDR R2J2004F00001Control Cable · misinstalledDURING PHASE 5 INSPECTION, UPON REINSTALLING LT WING FLAP CABLES, NOTICED AIRCRAFT WAS DIFFERENT THAN MM DATA AS TO ROUTING OF FLAP CABLES ON LT OB BELLCRANK. EXPERIMENTED AND CONTACTED MFG TECH SUPPORT. FOUND DATA ON PG 27-50-01 PG 203 FIG 201 (SHEET 2) SHOJun 29, 2004 · N501CF · Cessna 501 · Trailing Edge Flap Control SystemSDR JEM2004F00001Bracket · crackedDURING A SCHEDULED INSPECTION OF THE HORIZONTAL STABILIZER SIDE ROLLER BRACKET ASSY AND AREA, IT WAS DISCOVERED THAT THE SUPPORTING BRACKETS BEHIND THE RIB AS WELL AS THE RIB ON THE LT AND RT SIDE ROLLER BRACKET WERE CRACKED. THE INSPECTION WAS ACCOMPLISHED UJun 17, 2004 · N250AJ · Beech 400A · Horizontal Stabilizer StructureSDR JEM2004F00002Bracket · crackedDURING A SCHEDULED INSPECTION OF THE HORIZONTAL STABILIZER SIDE ROLLER BRACKET ASSY AND AREA, IT WAS DISCOVERED THAT THE SUPPORTING BRACKETS BEHIND THE RIB AS WELL AS THE RIB ON THE LT AND RT SIDE ROLLER BRACKET WERE CRACKED. THE INSPECTION WAS ACCOMPLISHED UJun 17, 2004 · N250AJ · Beech 400A · Horizontal Stabilizer StructureSDR JEM2004F00003Rib · crackedDURING A SCHEDULED INSPECTION OF THE HORIZONTAL STABILIZER SIDE ROLLER BRACKET ASSY AND AREA, IT WAS DISCOVERED THAT THE SUPPORTING BRACKETS BEHIND THE RIB AS WELL AS THE RIB ON THE LT AND RT SIDE ROLLER BRACKET WERE CRACKED. THE INSPECTION WAS ACCOMPLISHED Jun 17, 2004 · N250AJ · Beech 400A · Horizontal Stabilizer, Spar/RibSDR JEM2004F00004Rib · crackedDURING A SCHEDULED INSPECTION OF THE HORIZONTAL STABILIZER SIDE ROLLER BRACKET ASSY AND AREA, IT WAS DISCOVERED THAT THE SUPPORTING BRACKETS BEHIND THE RIB AS WELL AS THE RIB ON THE LT AND RT SIDE ROLLER BRACKET WERE CRACKED. THE INSPECTION WAS ACCOMPISHED UJun 17, 2004 · N250AJ · Beech 400A · Horizontal Stabilizer, Spar/RibSDR JEM2004F00005Rib · crackedDURING A SCHEDULED INSPECTION OF THE HORIZONTAL STABILIZER SIDE ROLLER BRACKET ASSY AND AREA, IT WAS DISCOVERED THAT THE SUPPORTING BRACKETS BEHIND THE RIB AS WELL AS THE RIB ON THE LT AND RT SIDE ROLLER BRACKET WERE CRACKED. THE INSPECTION WAS ACCOMPLISHED Jun 17, 2004 · N250AJ · Beech 400A · Horizontal Stabilizer, Spar/RibSDR JEM2004F00006Rib · crackedDURING A SCHEDULED INSPECTION OF THE HORIZONTAL STABILIZER SIDE ROLLER BRACKET ASSY AND AREA, IT WAS DISCOVERED THAT THE SUPPORTING BRACKETS BEHIND THE RIB AS WELL AS THE RIB ON THE LT AND RT SIDE ROLLER BRACKET WERE CRACKED. THE INSPECTION WAS ACCOMPLISHED Jun 17, 2004 · N250AJ · Beech 400A · Horizontal Stabilizer, Spar/RibSDR YNO2004F00002Uplock Switch · inoperativeON APRIL 12, 2004 AT APPROX 10:30 AM, AIRCRAFT WAS DEPARTING WHEN GEAR WAS SELECTED UP, THE RT MAIN GEAR WOULD NOT COME UP AND LOCK. THE PILOTS COMPLETED THE CHECKLIST, THE GEAR WAS SELECTED DOWN AND HAD AN ALL GEAR SAFE CONDITION. THE AIRCRAFT DIVERTED AND Apr 12, 2004 · N62NS · Cessna S550 · Landing Gear Position and WarningSDR CWQ2004F00008Piccolo Tube · corrodedDURING ROUTINE PHASE 1-4 INSP, THE MECH GRABBED THE LIP BLEED AIR FEED TUBE NR 1 ENGINE AND APPLIED PRESSURE BACK AND FORTH, A NOISE WAS HEARD BANGING AT EACH STROKE. AFTER FURTHER DISASSEMBLY (REMOVAL OF LIP) FOUND THE 6552502-3, PICCOLO ASSY ATTACH LEGS (2 Mar 3, 2004 · N348QS · Cessna 560CESSNA · Airfoil Anti/De-ice SystemSDR 40188138Bracket · crackedBALANCE WEIGHT ARM FOR ELEVATOR CONTROL SYSTEM IS CRACKED.Feb 26, 2004 · N26NS · Cessna 500CESSNA · Elevator StructureSDR GVR2004F00000Seat Back · crackedUPPER CHAIR BASE ASSEMBLY CRACKED AT CHAIR BACK ATTACH POINTS. STRESS ON CHAIR BACK AND METAL FATIGUE PROBABLE CAUSE. ALSO, CHAIR BASE HAS HAD PREVIOUS INAPPROPRIATE REPAIR MADE. CHAIR WAS REPAIRED.Jan 15, 2004 · N13ST · Cessna 501 · Passenger Compartment EquipmentSDR KBM2003F00080Window · crackedLT FORWARD WINDOW CRACKED AND CRAZED. REMOVED AND REPLACED.Oct 29, 2003 · N677JM · Cessna 501 · Flight Compartment WindowsSDR CA030604002Hose · ruptured(CAN) WHILE PREPARING TO REFUEL THE AIRCRAFT, PILOT NOTED A LARGE QUANTITY OF HYDRAULIC FLUID ON THE RT ENGINE/THRUST REVERSER AREA. THE AFT HYDRAULIC HOSE CONNECTING THE TAIL ROTOR TO THE PYLON HAD BURST AT APPROXIMATELY MID LENGTH. (THIS IS THE AREA WHERE THMay 20, 2003 · Cessna 560CESSNA · Engine Thrust ReverserSDR AUS20030484Engine · seized(AUS) RT ENGINE FAILED AND COULD NOT BE RESTARTED. INVESTIGATION FOUNDTHE ENGINE SEIZED.Apr 17, 2003 · Cessna 500CESSNA · Engine (Turbine/Turboprop)SDR 03FDEA00386Warning Light · failedEQUIPMENT COOLING LIGHT CAME ON IN FLIGHT. PULLED RADIO ALT CB VIA THE QRH AND LIGHT WENT OUT FOR A FEW MINUTES. LIGHT THEN CAME BACK ON STEADY. QHR SAID LAND, ASAP. ON RETURN TO MEMPHIS, LIGHT WENT OUT A COUPLE OF TIMES IN THE DESCENT BUT WAS ON MOST OF Apr 4, 2003 · N234FE · Boeing 727200 · Cabin Temperature Indicator
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