N726DH, cancelled Mar 4, 2005

Service difficulty reports · 223

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 = 'N726DH' AND deregistration_id = 'N726DH-2005-03-04'
  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 DHL2003726012Engine · failedDURING T/O FROM ATL, ENGINE NR 2 EGT CLIMBED TO 620 C WITH EPR SET AT 1.95, N1 = 94 PERCENT, REDUCED THRUST TO 1.72 EPR, N1 = 89.5, EGT = 580 C, N2 = 92.8, FF = 6800, PERFORMED EGT OVER TEMPERATURE ABNORMAL PROCEDURE IAW 727 A.O.M. SHUTDOWN NR 2 ENGINE. ENGINESep 3, 2003 · N726DH · Boeing 727228 · Engine Temperature Indicating SystemSDR DHL2003726011Control Handle · dirtyWHEN GEAR WAS CYCLED DOWN, ALL 3 GREEN AND ALL 3 RED GEAR LIGHTS STAYED ON. DOORS LIGHT OUT. SECONDARY INDICATIONS CONFIRMED ALL GEAR DOWN. FOUND GEAR HANDLE SLIGHTLY STICKY ON SLIDE FUNCTION. CLEANED AND LUBRICATED HANDLE. CYCLED 3 TIMES ALL NORMAL PER MJul 22, 2003 · N726DH · Boeing 727228 · Landing Gear SelectorSDR DHL2003726010Latch · lack of lubeDURING LANDING ROLL OUT, CAPTAIN'S SLIDING WINDOW CAME UNSEATED LOST PROPER SEAL. FOUND WINDOW HANDLE LOCKING MECHANISM STICKING. LUBED HANDLE. OPS CHECKED GOOD IAW M/M 12-25-71.Jul 15, 2003 · N726DH · Boeing 727228 · Flight Compartment WindowsSDR DHL2003726009Tee Fitting · leakingON CLIMBOUT, NR 3 ENGINE OIL QUANTITY DECREASING RAPIDLY. WHEN OIL PSI WENT BELOW 40 PSI, PERFORMED IN FLIGHT ENGINE SHUTDOWN ABNORMAL PROCEDURES. FOUND PLUG ON NR 3 ENGINE OIL COOLER SUPPLY T-FITTING PARTIALLY INSTALLED/THREADS IN FITTING WERE STRIPPED. REJun 11, 2003 · N726DH · Boeing 727228 · Engine Oil Temperature RegulatorSDR DHL2003726008Connector · looseLEFT GEAR DOOR LIGHT DOES NOT ILLUMINATE ON S/O'S ANNUNCIATOR PANEL DURING GEAR RETRACTION OR EXTENSION. LIGHT TESTS OK. CLEANED AND RE-SECURED CONNECTOR. OPS CHECKED GOOD IAW B727 M/M 32-62.Jun 4, 2003 · N726DH · Boeing 727228 · Landing Gear Position and WarningSDR DHL2003726007Actuator · malfunctionedUPON FLAP RETRACTION NR 2 FLAP FAILED TO RETRACT PERFORMED ABNORMAL PROCEDURE DID NOT FIX PROBLEM. PERFORMED DETAILED CHECK OF SLAT SYSTEM WIRING. FOUND NO DEFECTS IAW B-727 WDM 27-81-02. REMOVED AND REPLACED NR 2 SLAT ACTUATOR IAW B-727 MM 27-81-0. OP'S CMay 28, 2003 · N726DH · Boeing 727228 · Leading Edge Slat Position Indicating SystemSDR DHL2003726006Slat · malfunctionedDURING CLIMB, UPON FLAP RETRACTION NR 2 SLAT FAILED TO RETRACT. PERFORM ABNORMAL PROCEDURES. DID NOT FIX PROBLEM. AIRCRAFT TURNED BACK AND RETURNED TO BASE. INSPECTED NR 2 L/E SLAT ROLLERS TRACKS ACTUATOR ATTACH POINTS IAW B-727 MM. NO DEFECTS NOTED. INSP. LMay 28, 2003 · N726DH · Boeing 727228 · Leading Edge Slat ActuatorSDR DHL2003726005Fire Loop · shortedENGINE NR 3 SYSTEM-B FIRE DETECTION LIGHT ILLUMINATED. TRANSFERRED TO DMI NR 12942 PER DHL MEL 26-13-1 CAT-C. PLACARD INSTALLED. MAINTENANCE CONTROL WAS NOTIFIED. REF DMI NR 12942 NR 3 ENGINE SYSTEM B-LOOP FIRE DETECTION. TROUBLESHOT TO SHORTED FIRE WALL May 15, 2003 · N726DH · Boeing 727228 · Fire DetectionSDR DHL2003726004Fire Loop · shortedENGINE NR 3 SYSTEM B-FIRE DETECTION LIGHT ILLUMINATED. PERFORMED ABNORMAL PROCEDURE CHECK LIST. SWITCHED TO SYSTEM-A SYSTEM TESTED NORMALLY. FOUND SHIELD FOR FIRE LOOP CONTACTING B-LOOP. CLEARED SHIELD, OPS TESTED NORMALLY.May 14, 2003 · N726DH · Boeing 727228 · Fire DetectionSDR DHL2003726003Connector · dirtyENGINE SYSTEM-B FIRE DETECTION LIGHT ILLUMINATED. SWITCHED TO SYSTEM-A FIRE DETECTION LIGHT TESTED NORMALLY. CLEANED NR 3 FIRE LOOP CONNECTOR AND RESET B-SYSTEM TEST BUTTON OPS CHECKED NORMAL IAW 727 M/M 26-11-0.May 14, 2003 · N726DH · Boeing 727228 · Fire DetectionSDR DHL2003726002Seat Track · damagedS/O'S SEAT WILL NOT LOCK INTO RAIL FOR SIDEWAY MOVEMENT. CLEANED AND LUBRICATED SEAT RAILS AND LOCKING MECHANISM PER M/M 2510. OPS NORMAL.Apr 4, 2003 · N726DH · Boeing 727228 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2003726001Fire Detector · will not testAPU FIRE WARNING WILL NOT TEST. TROUBLESHOT SYSTEM, VERIFIED INTEGRITY OF THE SENSOR/RESPONDER, TEST SWITCH, OPERATING POWER UNIT, AND WIRING UP TO SENSOR/RESPONDER PER B727 MM 26-15-00. PLACED ITEM ON DEFERRAL, DMI NR 11766, PER MEL 26-11-1 C.Jan 25, 2003 · N726DH · Boeing 727228 · Fire DetectionSDR DHL2002726007Power Unit1) AFTER HOLDING THE APU FIRE TEST S/W TO THE TEST POS. FOR 60 SEC. THE TEST DOES NOT ACTIVATE2) TRANSFER'D TO DMI #11007 MEL 26-11 PLACARD INSTALL'D COMPLIED WITH SP 26-113) REF DMI# 11007, APU FIRE TEST DON'T TEST.4) R&R FIRE TEST POWER UNIT, OPS. CK. GNov 19, 2002 · N726DH · Boeing 727228 · Fire Protection SystemSDR DHL2002726006Smoke Detector1) FORWARD LOWER CARGO COMPARTMENT FIRE DETECTOR S/N 1698 INOP AMBER & GREEN LIGHTS ILLUMINATED ON DETECTION SYS DISPLAY.2) DEFERRED LOWER CARGO COMPARTMENT FIRE DETECTOR S/N 1698 PER DHL MEL 26-19-1 CAT B DMI#10927. PLACARD INSTALLED.3) REF. DMI #10927 "FONov 9, 2002 · N726DH · Boeing 727228 · Smoke DetectionSDR DHL2002726005Fire Warning · malfunctionedAFTER APU SHUT DOWN FIRE WARNING ILLUMINATED WITH NO BELL. BELL WOULD NOT TEST. DISCHARGED BOTTLE EMERGENCY PROCEDURE. DEFERRED PER MEL 49-1 CAT. "C" PLACARD 10665 INSTALLED. MAINTENANCE WAS NOTIFIED. REF. DMI #10665 - AFTER APU SHUTDOWN FIRE WARNING LIGHT IOct 16, 2002 · N726DH · Boeing 727228 · Fire DetectionSDR DHL2002726004Valve · failedANTI-ICE DUCT OVERHEAT LIGHT ILLUMINATED AT TAKE-OFF. APPEARS TO BE NR 3 ENGINE. REMOVED & REPLACED NR 3 WING ANTI-ICE VALVE. OPS CHECKED IAW B727 M/M 30-11-31. OPS CHECKED GOOD. REJECTED TAKE-OFF! TAKE-OFF WEIGHT - 144,000 LBS, AIRSPEED - 40 KNOTS, TEMPEROct 1, 2002 · N726DH · Boeing 727228 · Airfoil Anti/De-ice SystemSDR DHL2002726003Smoke Detector · will not testNR 5 CABIN SMOKE DETECTOR WILL NOT TEST. REMOVED AND REPLACED LAMP TEST BULB OF DETECTOR 5R. OPS TEST GOOD IAW MM 26-17-00.Jul 24, 2002 · N726DH · Boeing 727228 · Smoke DetectionSDR DHL2002726002Smoke Detector · inoperativeNR 3 LEFT SMOKE DETECTOR WILL NOT TEST. RELAMPED DETECTOR TEST LOOP. OPS CHECK OK 26-16-0.Jul 3, 2002 · N726DH · Boeing 727228 · Smoke DetectionSDR DHL2002726520Skin · dentedDURING C-CHECK, NR 5 LEADING EDGE SLAT HAS A DENT AT SLAT AT STA 355. CUT OUT DENTED SECTION OF SLAT SKIN IAW B-727 SRM 57-50-1 FIG 1, FABRICATED REPAIR PARTS IAW B-727 SRM 57-50-3 FIG 1, AND INSTALLED DOUBLER AND FILLER REPAIR ON NR 5 LEADING EDGE SLAT IAW BMay 1, 2002 · N726DH · Boeing 727228 · Leading Edge DevicesSDR DHL2002726512Stringer · corrodedDURING C-CHECK, STRINGER 27R AT BS 710 HAS CORROSION. CUT OUT DAMAGED AREA IAW B-727 SRM 53-10-3 FIG 1. FABRICATED AND INSTALLED NEW STRINGER SECTIONS IAW SRM 53-10-2 FIG 9 SHEET 1.Apr 25, 2002 · N726DH · Boeing 727228 · Fuselage Main, Longeron/StringerSDR DHL2002726517Floorbeam · corrodedDURING C CHECK, BS 930 FLOORBEAM IS EXFOLIATED ON THE AFT SIDE OF THE BEAM AT THE INTERSECTION WITH THE BS 930 LT FORGING LBL 62, WL 203. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW B-727 SRM 53-10-2 FIG 8 SHEET 3 DETAIL III. FABRICATED REPAIR PART IAW Apr 23, 2002 · N726DH · Boeing 727228 · Fuselage Main, Floor BeamSDR DHL2002726508Angle · corrodedDURING C CHECK, C-1 CARGO DOOR INTERIOR STRUCTURE, 10 ANGLE HAS SEVERE EXFOLIATION CORROSION. REMOVED ANGLE FROM C-1 DOOR INTERIOR STRUCTURE AND REPLACED IAW B-727 SRM 51-40-4. REMOVED ANGLE FROM C-1 DOOR INTERNAL STRUCTURE IAW B-727 SRM 51-30-2. REPLACED AApr 22, 2002 · N726DH · Boeing 727228 · Cargo/Baggage DoorsSDR DHL2002726515Tab · puncturedDURING C-CHECK, LT AND ELEVATOR CONTROL TAB SHOW PUNCTURED HOLE TOP SIDE STA 73.0 APPROX. CUT OUT PUNCTURED AREA ON LT ELEVATOR TAB, IAW B-727 SRM 55-20-1 FIG 1 AND 51-40-10 FIG 2. INSTALLED REPAIR IAW B-727 SRM 51-40-10 FIG 2. OPS CHECK GOOD IAW B-727 MM 2Apr 20, 2002 · N726DH · Boeing 727228 · Elevator, Tab StructureSDR DHL2002726519Doubler · crackedDURING C-CHECK, MCD AFT UPPER CORNER FRAME DOUBLER (INTERNAL) CRACKED, AS VIEWED THROUGH THE MCD UPPER AFT LIGHTENING HOLE. REMOVED AFT UPPER FRAME CORNER DOUBLER IAW B-727 SRM 51-30-2. FABRICATED AND INSTALLED PART IAW B-727 SRM.Apr 18, 2002 · N726DH · Boeing 727228 · Cargo/Baggage DoorsSDR DHL2002726506Cowling · crackedDuring C Check "discrepancy" as follows, #3 engine upper cowling gouged/chaffed on the #12 rib O/B section.Corrective action as follows,Cut-out damaged area on #3 engine cowl upper #12 rib I.A.W. B-727 SRM 54-10-2. Fabricated repair from 7075-T6 .050 P.O.# 991Apr 18, 2002 · N726DH · Boeing 727228 · Nacelle/Pylon, Main FrameSDR DHL2002726505Skin · damagedDURING C-CHECK, EXTERNAL FUSELAGE REPAIR AT BS 1223, STR 21R IS INSTALLED WITH BLIND FASTENERS. REMOVED REPAIR IAW B-727 SRM 51-30-2. FABRICATED AND INSTALLED NEW DOUBLER IAW B-727 SRM 51-30-2.Apr 18, 2002 · N726DH · Boeing 727228 · Fuselage Main, Plate/SkinSDR DHL2002726503Skin · crackedDURING C-CHECK, NR 1 ENGINE UPPER COWL SKIN IS CRACKED AT NR 3 LATCH. FABRICATED AND INSTALLED DOUBLER IAW B-727 SRM 51-30-2.Apr 18, 2002 · N726DH · Boeing 727228 · Engine Cowling SystemSDR DHL2002726502Plate · crackedDURING C-CHECK, NR 1 ENGINE LOWER COWL NR 5 O/B U-BOLT COVER PLATE IS CRACKED. REMOVED COVER PLATE. FABRICATED AND INSTALLED NEW PLATE IAW B-727 SRM 51-30-2.Apr 18, 2002 · N726DH · Boeing 727228 · Engine Cowling SystemSDR DHL2002726518Hinge · crackedDURING C-CHECK, MAIN CARGO DOOR HINGE (UPPER FUSELAGE SIDE) IS CRACKED, 2ND LOBE FROM AFT. VERIFIED BY HFEC. REMOVED CRACKED UPPER HINGE IAW B-727 SRM 51-30-2. INSTALLED NEW HINGE FOR MCD IAW PEMCO DWG 52-487-1.Apr 17, 2002 · N726DH · Boeing 727228 · Fuselage, Door HingeSDR DHL2002726516Stringer · crackedDURING C-CHECK, CABIN BS 720B STR 15 L IS CRACKED FWD OF WING LIGHT. FABRICATED NEW ANGLE CHANNEL AND DOUBLER IAW 53-10-3 FIG 5. INSTALLED NEW ANGLE CHANNEL IAW B-727 SRM 51-30-2 SRM 53-10-3 FIG 5. PRESSURE CHECK GOOD IAW B-727 21-30-0.Apr 17, 2002 · N726DH · Boeing 727228 · Fuselage Main, Longeron/StringerSDR DHL2002726514Panel · crackedDURING C-CHECK, NLG WW LT SIDEWALL PANEL IS CRACKED BS 290 WL 198 APPROX UNDERNEATH FITTING SUPPORT DOOR ACTUATOR 2 PLACES CRACKED (NDT CONFIRMED). ROUTED OUT CRACKED AREA. NDT INSP AROUND ROUTED OUT AREA PER NDT MANUAL, NO CRACKS NOTED. FABRICATED DOUBLER Apr 17, 2002 · N726DH · Boeing 727228 · Fuselage Miscellaneous StructureSDR DHL2002726511Pressure Panel · crackedDURING C-CHECK, NOSE WHEEL WELL L/SIDE WALL PANEL CRACKED BS 280 AND UPPER CHORD ANGLE SEEN FROM INSIDE (NDT VERIFIED). FABRICATED AND INSTALLED REPAIR PARTS IAW B-727 SRM 51-30-2.Apr 17, 2002 · N726DH · Boeing 727228 · Fuselage Main, BulkheadSDR DHL2002726513Rib · crackedDURING C-CHECK, RT WING FIXED L/E RIB HAS A CRACK AT WS 572. CUT OUT DAMAGED AREA IAW B-727 SRM 51-40-3. FABRICATED AND INSTALLED REPAIR IAW B-727 SRM 51-30-2 AND 51-40-3.Apr 16, 2002 · N726DH · Boeing 727228 · Wing, Rib/BulkheadSDR DHL2002726501Skin · dentedDURING C-CHECK, DENT ON C-1 DOOR SKIN AT BS 590, STR 20 R. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER IAW B-727 SRM 51-30-2.Apr 16, 2002 · N726DH · Boeing 727228 · Passenger/Crew DoorsSDR DHL2002726522Support · corrodedDURING C-CHECK, COCKPIT FLOOR STA 265 LBL 3, PANEL IN FLOOR BULGED WITH PULLING RIVETS AT I/B END OF F/E SEAT TRACK. REMOVED AND REPLACED F/E SEAT TRACK SUPPORT IAW B-727 SRM 51-30-5/ 51-30-8/ 51-30-2. BULGING FOUND TO BE CORROSION OF F/E SEAT TRACK SUPPORT.Apr 15, 2002 · N726DH · Boeing 727228 · Fuselage Miscellaneous StructureSDR DHL2002726521Door Frame · corrodedDURING C-CHECK, RT AND AFT EMERGENCY EXIT FUSELAGE CUTOUT LWR FWD CORNER INTERIOR EXFOLIATED CORROSION. REMOVED CORROSION ON RT AFT EMERGENCY EXIT LWR FWD CORNER IAW B-727 SRM 51-30-1. FOUND TO BE OUT OF LIMITS IAW B-727 SRM 53-30-1. FABRICATED AND INSTALLEApr 15, 2002 · N726DH · Boeing 727228 · Fuselage Main, StructureSDR DHL2002726510Pressure Panel · crackedDURING C-CHECK, NOSE WHEEL WELL LEFT SIDEWALL BULKHEAD BS 243, WL 150 CRACK INDICATION ABOUT 2.5 INCH LONG. NDT VERIFIED. CUT-OUT DAMAGED AREA. FABRICATED AND INSTALLED REPAIR PARTS IAW B-727 SRM 51-30-2.Apr 15, 2002 · N726DH · Boeing 727228 · Fuselage Main, BulkheadSDR DHL2002726509Skin · dentedDURING C-CHECK, VENTRAL STAIRS ASSY STA 1315 TO 1335, AFT EXT SKIN HAS 3 DENTS. FABRICATED AND INSTALLED DOUBLER REPAIRS.Apr 15, 2002 · N726DH · Boeing 727228 · Entrance StairsSDR DHL2002726504Pressure Panel · crackedDURING C-CHECK, RT NLG W/W FWD BULKHEAD LOWER I/B CORNER HAS 4 INCH CRACK. CUT OUT CRACKED WEB & INSTALLED A WEB REPAIR DOUBLER. CUT OUT CRACKED SECTION OF LOWER EXTRUSION ANGLE & INSTALLED AN EXTRUSION ANGLE REPAIR.Apr 15, 2002 · N726DH · Boeing 727228 · Fuselage Main, BulkheadSDR DHL2002726500Attach Fitting · crackedDURING C-CHECK, NR 2 ENGINE LT UPPER ENGINE MOUNT FITTING ATTACH ANGLE FITTING INSIDE (PANEL 5201) HAS A 3 INCH LONG CRACK. REMOVED AND REPLACED ATTACH FITTING IAW B-727 SRM 51-30-2. REMOVED AND REPLACED LT UPPER SUPPORT CHORD. REMOVED NR 2 ENGINE LT UPPER Apr 14, 2002 · N726DH · Boeing 727228 · Engine Mount SectionSDR DHL2002726001Windshield Wiper · out of adjustRIGHT WIPER DOES NOT FUNCTION. WINDSHIELD WIPER KNOB FELL OFF. REPLACED SET SCREWS IAW B727 M/M 30-42-01. RECLOCKED RIGHT WINDSHIELD WIPER IAW BMM 30-42-01, OPERATIONAL CHECK IS GOOD.Mar 16, 2002 · N726DH · Boeing 727228 · Windshield/Door Rain/Ice RemovalSDR DHL2001726008Downlock Sensor · failedON GEAR EXTENSION GOT UNSAFE LEFT GEAR LIGHT ON FWD INST PANEL AND CONSTANT GEAR WARNING HORN WITH FLAPS AT 25 OR 30 DEG. SECONDARY GEAR INDICATION LIGHTS (S/O PANEL) NORMAL. COMPLIED WITH ABNORMAL CHECKLIST. CYCLED GEAR 3 TIMES, HAND CRANKED LEFT MAIN, CONDUNov 17, 2001 · N726DH · Boeing 727228 · Landing Gear Position and WarningSDR DHL2001726007Stringer · crackedFCD INSP - AIR COND DISTRIBUT BAY STRING 27R SHOW CRACK CORROSION AND BULGING FROM BS 720F THRU BS 740. CUT OUT AND REMOVED 8.5 SECTION OF CRACKED & CORRODED STR 27R STA 740 TO STA 720F IAW B727 SRM 53-10-3 FIG 1. REMOVED SURFACE CORROSION ON SKIN .001 FOUND Oct 6, 2001 · N726DH · Boeing 727228 · Fuselage Main, Longeron/StringerSDR DHL2001726006Stringer · crackedFCD INSPECTION- AIR CONDITIONING BAY STR 26R SHOW BULGING AND CRACK CORROSION AT DIFFERENT SPOTS FROM 720 THRU 740. CUT OUT AND REMOVED CRACKED AND CORRODED SECTION OF STRINGER 26R FROM STA 740 TO STA 720 IAW B727 SRM 53-10-3 FIG 1. REMOVED SURFACE CORROSIONOct 6, 2001 · N726DH · Boeing 727228 · Fuselage Main, Longeron/StringerSDR DHL2001726005Smoke Detector · inoperativeAFT LOWER CARGO SMOKE DETECTOR INOP. RESET 7110 SMOKE DETECTOR AFT CARGO COMPARTMENT IAW MM SUP 26-16-00. OPS CHECKED NORMAL.Aug 23, 2001 · N726DH · Boeing 727228 · Smoke DetectionSDR DHL2001726004Light1) ON SERVICE CHECK FOUND L-1 DOOR EMERGENCY EXIT LIGHT DIM.2) REMOVED AND REPLACED L-1 DOOR EXIT LIGHT ASSY. OPS CK NORMAL IAW M/M 33-50-111STATUS: CLOSEDAug 15, 2001 · N726DH · Boeing 727228 · Emergency LightingSDR DHL2001726003Overheat Loop · faultyLOWER AFT BODY LIGHT ILLUMINATED DURING CLIMB AT 15000 FT. PERFORMED ABNORMAL PROCEDURE. UPON REDUCING THRUST ON NR 1 ENGINE, LIGHT EXTINGUISHED. RETURNED TO CVG. R&R OVERHEAT DETECTION SENSING ELEMENT WITH SERVICEABLE UNIT IAW B MM 26-14-1.Aug 5, 2001 · N726DH · Boeing 727228 · Overheat DetectionSDR DHL2001726002Circuit Breaker · failedNR 1 FWD SMOKE DETECTOR LIGHT CAME ON ON PUSH BACK. MAIN DECK CARGO DETECTOR LOOP 2 CIRCUIT BKR WOULD NOT RESET AFTER BEING PULLED TO RESET ISOLATION VALVES. R&R C/B 9001WH PER WDM 26-11-14. OPS CK SERVICEABLE. SMOKE DET SERVICEABLE PER 26-11-00.Aug 5, 2001 · N726DH · Boeing 727228 · Smoke DetectionSDR DHL2000726005Connector · failedON TAKEOFF ROLL AT 65 KTS FLAP LED WENT FROM GREEN TO AMBER BACK TO GREEN-AMBER. TAKEOFF REJECTED. TS L/E FLAP AND SLAT INDICATION SYS FOUND BAD CANNON PLUG INSERT NR 4 K FLAP SWITCH. PERFORMED SPECIAL PROCEDURE IN MEL 27-6. TRF TO DMI 2497 OK PER MEL 27-6Sep 23, 2000 · N726DH · Boeing 727228 · Leading Edge Slat Control SystemSDR DHL2000726100Warning System · false indicationCLIMBING THROUGH FL 190 A LOUD THUMP FOLLOWED BY A RED MAIN CARGO DOOR ILLUMINATED ON SO''S ANNUNCIATOR PANEL. RETURNED TO CVG. CABIN APPROX 7.0 PSI WHEN THUMP OCCURR RED. LIGHT REMAINED ILLUMINATED THROUGH 1 PSI EXTINGUISHED AT ZERO PSI. CREW REPORTED L1 Aug 24, 2000 · N726DH · Boeing 727228 · Door Warning System
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