Boeing 727-224

Service difficulty reports · 2,252

Newest first. General aviation reporting is voluntary.

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 aircraft_model_key = '727224'
  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 DHL2006745525Seat Track · corrodedMC DECK, 24L SEAT TRACK FROM BS 460 TO BS 660 SHOWS SURFACE CORROSION. REMOVED SEAT TRACK BS 460-660, RBL 24 FOR REPLACEMENT IAW B727 SRM 51-30-2, FAB NEW SEAT TRACK FROM P/N BAC1520-792, PO NR 9003607 APPROX DIM 17' 5" IAW B727 SRM 53-10-5, FIG 1, TREATED ANSep 1, 2006 · N745DH · Boeing 727224 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2006745521Frame · dentedFWD CARGO COMPT, FRAME AT STA 700 IS DENTED IN 3 PLACES BETWEEN STR 22R-26R. CUT OUT DAMAGE AREA 2 EA 2 3/4" BY 1" AND 1 3/4" BY 1" IAW B727 SRM 53-10-1. FABRICATED REPAIR DOUBLER FROM 7075.0, .071, PO NR 9003189 DIM 24" BY 3 5/8" IAW B727 SRM 53-10-2, HEATSep 1, 2006 · N745DH · Boeing 727224 · Fuselage Main, FrameSDR DHL2006745520Frame · dentedFWD CARGO COMPT, FRAME AT STA 520 IS DENTED IN UPPER FLANGE AND HAS OPEN FASTENER HOLES BETWEEN STR 23R-25R. CUT OUT DAMAGED AREA OF FRAME APPROX DIM 9" BY 1" IAW B727 SRM 51-40-3 FIG 1. FAB ANGLE DOUBLER REPAIR FROM P/N 7075-0, .050, PO NR 9003749 APPROX DISep 1, 2006 · N745DH · Boeing 727224 · Fuselage Main, FrameSDR DHL2006745535Frame · dentedREF ASTAR N/R 56426. DISCREPANCY: FWD CARGO COMPT, FRAME AT STA 660 IS DENTED AT UPPER FLANGE ABOVE STR 23R. CORRECTIVE ACTION: CUT OUT DAMAGED AREA APPROX DIM 3.7 INCH X 1 INCH IAW SRM 51-40-3 FIG 1, FAB REPAIR DOUBLER FROM P/N 7075-0, .071, PO NR 9003189Aug 29, 2006 · N745DH · Boeing 727224 · Fuselage Main, FrameSDR DHL2006745510Frame · dentedAFT CARGO COMP BS 950B ABOVE STR 25R HAS FRAME INNER FRAME CHORD DENTED. CUT OUT DAMAGED AREA APPROX DIM 1" BY 1.5" AND 1" BY .75" IAW B727 SRM 51-40-3, FIG 1. FABRICATED DOUBLER FROM 7075-0 .071, PO NR 9003110, APPROX DIM 28" BY 4" IAW B727 SRM 51-40-3 FIG Aug 29, 2006 · N745DH · Boeing 727224 · Fuselage Main, FrameSDR DHL2006745519Frame · dentedAFT CARGO COMPARTMENT BS 950C LT HAS 3 DENTS IN RADIUS OF FRAME. CUT OUT DAMAGED SECTION 2" BY 1" AT AFT CARGO FRAME BS 950C LT STR 26L IAW B727 SRM 51-40-3 FIG 1. REMOVED FASTENERS FOR FRAME REPAIR IAW B727 SRM 51-30-2. FAB REPAIR DOUBLER FROM P/N 7075-0 .Aug 29, 2006 · N745DH · Boeing 727224 · Fuselage Main, FrameSDR DHL2006745518Frame · dentedAFT CARGO COMP BS 950C ABOVE STR 25RT, HAS FRAME INNER CHORD DENTED. REMOVED FASTENERS FOR FRAME REPAIR AT BS 950C, STR 25R IAW B727 SRM 51-30-2. CUT OUT DAMAGED AREA APPROX DIM 1" BY 1 1/4" IAW B727 SRM 51-40-3 FIG 1. FAB REPAIR DOUBLER FROM P/N 7075-0 .07Aug 29, 2006 · N745DH · Boeing 727224 · Fuselage Main, FrameSDR DHL2006745540Spar · damagedLT HORIZ STAB LWR AFT REAR SPAR CHORD (75% CHORD) FROM ELEVATOR STA 50.5 TO 136.5 HAS MISS DRILLED SEAL HOLES MISSING FASTENERS & SEAL IS LOSE IN SEVERAL PLACES. (PREVIOUSLY REJECTED ON N/R 056346) WRONG HARDWARE & CRAFTMANSHIP. CUT OUT DAMAGED AREA AT RT HOAug 22, 2006 · N745DH · Boeing 727224 · Horizontal Stabilizer, Spar/RibSDR DHL2006745527Seat Track · corrodedMAIN CARGO DECK AT BS 680-720F 45L SEAT TRACK HAS CORROSION AND MISDRILLED HOLE AT BS 690. REMOVED SEAT TRACK FROM BS 660-740 LBL45 IAW B727 SRM 51-30-2, FAB NEW SEAT TRACK P/N BAC1520-792 PO NR 9003607 APPROX DIM 17'3" IAW B727 SRM 53-10-05 FIG 1 AND SRM 53-Aug 16, 2006 · N745DH · Boeing 727224 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2006745506Frame · dentedAFT CARGO COMPT LT STA 1130 HAS DENT IN RADIUS OF FRAME. CUTOUT DAMAGED SECTION 3/4" BY 1" AT AFT CARGO FRAME 1130 LT AS PER B727 SRM 51-40-3 FIG 1. FABRICATED DOUBLER 7075-0 .063 PO NR 9003418 APPROX 6.5" BY 4" IAW B727 SRM 53-10-2 FIG 5 AND SRM 51-40-3 FIGAug 13, 2006 · N745DH · Boeing 727224 · Fuselage Main, FrameSDR DHL2006745532Stringer Splice · corrodedASTAR N/R 056414-FWD CARGO COMPT. STR. 27L SPLICE IS CORRODED WITH EXFOLIATION BS 680. REMOVED CORR AT FWD CARGO COMPT. BS 680,STR. 27L. AREA FOUND TO BE OUT OF ALLOWABLE LIMITS. CUT OUT DAMAGED AREA AT STR. 27L, DIM. 4.5 INCH AND FAB NEW SPLICE FROM P/N BAV14Aug 12, 2006 · N745DH · Boeing 727224 · Fuselage Main, Longeron/StringerSDR DHL2006745531Stringer Splice · corrodedASTAR N/R 056419-FWD CARGO COMP. STR. 28L SPLICE IS CORRODED BETWEEN STA 680-700. REMOVED CORR FOUND OUT OF ALLOWABLE LIMITS. REMOVED EXISTEN SPLICE CUT OUT DAMAGED AREA AT STR. 28L DIM. 4 INCH, FAB NEW SPLICE FROM P/N BAC 1498-132 7075T6 PO NR 423185 DIM. 16Aug 12, 2006 · N745DH · Boeing 727224 · Fuselage Main, Longeron/StringerSDR DHL2006745526Frame · dentedFWD CARGO COMPT FRAME AT STA 700 IS DENTED IN 2 PLACES BETWEEN STR 23L-25L. CUTOUT DAMAGE AREA AT BS 700 STR 23L TO 25L 2EA DIM 1.10" BY 1" IAW SRM 53-10-1. FABRICATED FRAME REPAIR USING 7075 "0" .071 PO NR 9003189 DIM19" NR 4 1/2" IAW B727 SRM 53-10-2. HEAAug 12, 2006 · N745DH · Boeing 727224 · Fuselage Main, FrameSDR DHL2006745512Lap Joint · chafedFUSELAGE EXTERIOR BS 720E PLUS 10", STR 19R, LAP SEAM AREA, CHAFED AREA WORN, OUT OF LIMITS. CUT OUT DAMAGE AREA APPROX DIM 4.5" BY 2.5" AT BS 720E PLUS 10", STR 19R IAW B727 SRM 53-30-3 FIG 5. FABRICATED REPAIR DOUBLER FROM 2024-T3, .080, PO NR 509622, APPRAug 12, 2006 · N745DH · Boeing 727224 · Fuselage Main, Plate/SkinSDR DHL2006745511Frame · dentedFWD CARGO COMP FRAME AT BS 740, STR 24R DENTED IN TWO LOCATIONS. CUT OUT DAMAGED AREA APPROX DIM 4" BY 1" IAW B727 SRM 51-40-3 FIG 1. FABRICATED REPAIR DOUBLER FROM 7075-0 .071, PO NR 9003189, APPROX DIM 14" BY 4" IAW B727 SRM 51-40-3 FIG 1. HEAT TREATED MAAug 12, 2006 · N745DH · Boeing 727224 · Fuselage Main, FrameSDR DHL2006745509Frame · dentedAFT CARGO COMPARTMENT BS 950F BETWEEN STR 25L AND 26L, FRAME INNER CHORD DENTED. FAB REPAIR DOUBLER FROM 7075, 0.063, PO NR 900348 APPROX DIM 17 BY 4 INCHES IAW B727 SRM 53-10-2 FIGURE 5 AND 51-40-3 FIGURE 1. HEAT TREATED MATERIAL TO T6 CONDITION IAW FLIGHTSAug 12, 2006 · N745DH · Boeing 727224 · Fuselage Main, FrameSDR DHL2006745517Frame · dentedFWD CARGO COMPT FRAME AT STA 500 IS DENTED IN SEVERAL PLACES OF THE UPPER FLANGE BETWEEN STR 23R-24R. CUT OUT DAMAGED SECTION 1" BY 2 1/2", 1" BY 2',1" BY 3' AT FWD CARGO FRAME STA 500 BETWEEN STR 23R-24R PER B727 SRM 51-40-3 FIG 1. FABRICATED DOUBLER 7075-0Aug 12, 2006 · N745DH · Boeing 727224 · Fuselage Main, FrameSDR DHL2006745515Frame · dentedFWD CARGO COMP FRAME AT STA 720 IS DENTED IN 3 PLACES BETWEEN STR 24L-25L. REMOVED DAMAGED SECTION 1" BY 1",1.10" BY 1" AT STA 720 BETWEEN STR 24L-25L PER B727 SRM 51-40-3 FIG 1. FABRICATED DOUBLER 7075-0 .071 P.O. 9003189 15.5" BY 4" PER B727 SRM 51-40-3 FIAug 12, 2006 · N745DH · Boeing 727224 · Fuselage Main, FrameSDR DHL2006745514Frame · dentedAFT CARGO COMPT BS 990 BETWEEN STR 25L AND 26L HAS FRAME INNER CHORD DENTED. CUT OUT DAMAGE SECTION 2 AREAS 1" BY 2" AT AFT CARGO BS 990 BETWEEN STR 25L-26L UPPER FLANGE AS PER B727 SRM 51-40-3 FIG 1. FABRICATED DOUBLER FROM 7075 .071 5" BY 22" IAW B727 SRM Aug 12, 2006 · N745DH · Boeing 727224 · Fuselage Main, FrameSDR DHL2006745505Frame · damagedAFT CARGO COMPT BS 1110 BET STR 25L AND 26L HAS FRAME INNER CHORD DENTED AND BENT. FABBED REPAIR DOUBLER FROM 7075-0 .063 PO NR 9003418 APPROX DIM 14" BY 4.25" IAW B727 SRM 53-10-2 FIG 5 AND SRM 51-40-3 FIG 1, HEAT TREATED MATERIAL TO T6 IAW FLIGHTSTAR A/C SEAug 12, 2006 · N745DH · Boeing 727224 · Fuselage Main, FrameSDR DHL2006745504Frame · dentedFWD CARGO COMPT FRAME AT STA 680 IS DENTED IN SEVERAL PLACES BETWEEN STR 22L-24L. CUTOUT DAMAGED SECTIONS 1.5" BY 1", 3.25" BY 1" AT FS 680 STR 22L-24L FRAME AREA AS PER B727 SRM 51-40-3 FIG 1. FABRICATED DOUBLER 7075-0 .071 PO NR 9003110 19.125" BY 2.25 AS Aug 12, 2006 · N745DH · Boeing 727224 · Fuselage Main, FrameSDR DHL2006745502Frame · damagedAFT CARGO COMPT BS 1050 BETWEEN STR 25L-26L HAS FRAME INNER CHORD DENTED AND BENT. CUTOUT DAMAGE SECTIONS 1" BY 1", 3/4" BY 1" AT AFT CARGO BS 1050 BETWEEN STR 25L-26L FRAME AS PER SRM 51-40-3 FIG 1. FABRICATED DOUBLER 7075-0 .071 PO NR 90031189, 11" BY 3 3Aug 12, 2006 · N745DH · Boeing 727224 · Fuselage Main, FrameSDR DHL2006745501Frame · dentedFOUND FWD CARGO COMPT FRAME AT STA 680 IS DENTED AT UPPER FLANGE BETWEEN STR 23R - 24R. CUTOUT DAMAGED AREA 3 1/2" BY 1" AT FWD CARGO STA 680 STR 23R-24R IAW SRM 51-40-3 FIG 1. FABRICATED DOUBLER WITH 7075-0 .071 SIZE 12 1/2" BY 2" PO NR 9003110 AS PER B727 Aug 12, 2006 · N745DH · Boeing 727224 · Fuselage Main, FrameSDR DHL2006745500Lap Joint · chafedFUSELAGE EXTERIOR BS 720E +10 AND STR 19L LAP SEAM AREA CHAFED, AREA WORN. CUTOUT DAMAGED SECTION 4.5" BY 2 7/8" AT FS SKIN BS 720E +10 STR 19L IAW B727 SRM 53-30-3 FIG 5. FABBED REPAIR DOUBLER FROM 2024 T3 .080 PO NR 509622 APPROX DIM 11" BY 10.5. FABBED SAug 10, 2006 · N745DH · Boeing 727224 · Fuselage Main, Plate/SkinSDR DHL2006745513Skin · crackedBS 254 BELOW STR 10R, FUSELAGE SKIN CRACKED AT FASTENER. REMOVED FASTENERS FOR SKIN REPAIR AT BS 254 BELOW STR 10R IAW B727 SRM 51-30-2 AND 53-30-3, FIG 29. FABRICATED REPAIR DOUBLER FROM 2024-T3, 0.80, PO NR 9003641, APPROX DIM 14" BY 13" IAW B727 SRM 53-30Aug 9, 2006 · N745DH · Boeing 727224 · Fuselage Main, Plate/SkinSDR DHL2006745508Structure · crackedRIGHT INBD MIDFLAP AFT LWR CHORD, WBL 100, 2 CRACK INDICATIONS. REMOVED DAMAGED LWR CHORD AT WBL 100 IAW B727 SRM 51-30-2. FAB NEW LWR CHORD SECTION FROM P/N BAC1517-1507 APPROX DIM 4 BY 1 BY 7/8 INCHES IAW B727 SRM 57-50-2 FIGURE 5 AND SRM 51-20-1 FIGURE 2.Aug 9, 2006 · N745DH · Boeing 727224 · Trailing Edge FlapsSDR DHL2006745507Flap · delaminatedDELAMINATION OF LEFT INBD MID-FLAP, WBL 140 THRU WBL 243, TE. CLEANED AND PREPPED 8 DISBONDED AREAS ON LT I/B MIDFLAP T/E, APPLIED ADHESIVE AND CURED IAW B727 SRM 51-40-21. CUT OUT DELAMINATED AREAS APPROX 4.2 INCHES BY 5.4 INCHES, FABRICATED FILLER APPROX 4.Aug 9, 2006 · N745DH · Boeing 727224 · Trailing Edge FlapsSDR DHL2006745516Flap · delaminatedRT INBOARD MID FLAP SHOW DELAM ARE FROM T/E WBL 130. CUT OUT DELAMINATED AREA ON RT I/B MID FLAP APPROX 4.2" BY 6.2". FABRICATED FILLER APPROX 4.2" BY 6.2" AND DOUBLERS (2 EA) APPROX 3' BY 4.2" FROM 7075-T6 .016, PO 9003142. CLEANED, PREPPED, BONDED, CLEANEAug 9, 2006 · N745DH · Boeing 727224 · Trailing Edge FlapsSDR DHL2006745503Angle · crackedLT INBD MID-FLAP AFT LOWER CHORD SHOW 3 CRACK INDICATION WBL 100-120. REMOVED DAMAGED LWR CHORD ANGLE AT LT I/B MIDFLAP AFT LWR AREA WBL100-120 AS PER B727 SRM 51-30-2. FABRICATED NEW CHORD ANGLE BAC1503-100046 14'9"X 2" PO NR 900385 AS PER B727 57-50-2 FIG Aug 9, 2006 · N745DH · Boeing 727224 · Trailing Edge FlapsSDR DHL2006745528Pressure Panel · crackedNOSE WHEEL WELL PANEL CRACK INDICATION AROUND FASTENERS BS 286 LBL4. VERIFIED INDICATION AS MARKED IAW NDT M PT6 51-00-00 FIG 23. REMOVED FASTENERS FOR REPAIR AT NOSE WHEEL WELL BS286 IAW B727 SRM 51-30-2, CUTOUT DAMAGED AREA APPROX DIM 3/4" BY 3" IAW B727 SAug 8, 2006 · N745DH · Boeing 727224 · Fuselage Main, BulkheadSDR DHL2006746002Battery · inoperativeFOUND EMERGENCY EXIT LIGHT ABOVE FWD ENTRY DOOR DOES NOT ILLUMINATE DURING STBY PWR CHECK. REPLACED BOTH BATTERIES IN EMERG EXIT LIGHT IAW B727 MM 33-50-10. SYS OP'S CK SERVICEABLE, P/N: 37067-001.Aug 1, 2006 · N746DH · Boeing 727224 · Emergency LightingSDR GAIA06023STFrame · dentedNO FLIGHT: DURING INSPECTION THE FRAME AT STATION 380 WAS FOUND DENTED BETWEEN STRINGERS S5L AND S6L. REPAIRED FRAME WITH DOUBLER REPAIR IAW SRM. AIRCRAFT RETURNED TO SERVICE. (K)Jul 11, 2006 · N69735 · Boeing 727224 · Fuselage Main, FrameSDR GAIA06024STFrame · dentedNO FLIGHT: DURING INSPECTIO THE FRAME AT STATION 400 WAS FOUND DENTED BETWEEN STRINGERS S6L AND S7L. REPAIRED FRAME WITH DOUBLER REPAIR SRM. AIRCRAFT RETURNED TO SERVICE. (K)Jul 11, 2006 · N69735 · Boeing 727224 · Fuselage Main, FrameSDR GAIA06025STFrame · dentedNO FLIGHT: DURING INSPECTION THE FRAME AT STATION 560 WAS FOUND DENTED BETWEEN STRINGERS S5R AND S6R. REPAIRED FRAME WITH DOUBLER REPAIR IAW SRM. AIRCRAFT RETRUNED TO SERVICE. (K)Jul 11, 2006 · N69735 · Boeing 727224 · Fuselage Main, FrameSDR GAIA06026STFrame · dentedNO FLIGHT: DURING INSPECTION THE FRAME AT STATION 600 WAS FOUND DENTED BETWEEN STRINGERS S6R AND S7R. REPAIRED FRAME WITH DOUBLER REPAIR SRM. AIRCRAFT RETURNED TO SERVICE. (K)Jul 11, 2006 · N69735 · Boeing 727224 · Fuselage Main, FrameSDR DHL2006747002Fairing · damagedMX RELEASE FOR DROP IN VISIT FOR DAMAGE TO LT AFT BODY FAIRING AND FAIRING SUPPORT. MX RELEASE DONE ON 3-13-06 UNDER WORK ORDER 5001328.Mar 13, 2006 · N747DH · Boeing 727224 · Aerodynamic FairingsSDR DHL2006747001Pin · installedNOSE GEAR FAILED TO RETRACT. RETURNED TO FIELD NOSE GEAR PIN FOUND INSTALLED ON POST FLIGHT. DURING POST FLT FOUND ONE MAIN GEAR PIN MISSING. REMOVED NOSE GEAR PIN AND STOWED IAW ASTAR GMM 20.7. VERIFIED MAIN GEAR PINS REMOVED FROM GEAR. ENTERED MISSING GMar 1, 2006 · N747DH · Boeing 727224 · Main Landing GearSDR GAIA06005Turbine · failedDURING TAKEOFF AFTER V- THE FLIGHT CREW FELT A DULL THUD ON AN ENGINE THE NR 1 ENGINE THEN FAILED. THE FLIGHT CREW DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. AN UNEVENTFUL LANDING WAS MADE. INSPECTION REVEALED TURBINE BLADE DAMAGE ON THE NR 1 ENGINE. Feb 16, 2006 · N69735 · Boeing 727224 · Turbine SectionSDR DHL2006745003Battery · dischargedEMERGENCY EXIT LIGHT FWD ENTRY WAY DEAD. REMOVED AND REPLACED EXIT LIGHT BATTERIES IAW MM 33-50-71, OPS CKS GOOD P/N MISC-062.Feb 14, 2006 · N745DH · Boeing 727224 · Emergency LightingSDR DHL2006745001Engine · malfunctionedEPR INDICATIONS ERRATIC ON NR 2 ENGINE DURING TAKEOFF. REJECTED AC WEIGHT 156.9 LBS OPT 0 DEGREES C BRAKE ENERGY CHART REFERENCED RAN ENGINE AFTER SELECTING EAI AND EPR INDICATIONS WERE NORMAL. DEPARTED NORMALLY. NOTED BY MAINTENANCE REJECTED T/O, PAPERWORKJan 19, 2006 · N745DH · Boeing 727224 · Engine (Turbine/Turboprop)SDR DHL2006746001Structure · ground damageRT WING TIP AND OUTBOARD AILERON TRAILING EDGE STRUCK BY UPS TRUCK. REMOVED RT WING TIP, PERFORMED HFEC INSPECTION IAW B727 AMM 5-51-61, HARD LANDING INSPECTION AND NDT MANUAL D6-48875. INSTALLED NEW WING TIP, P/N 65-24965-2 IAW B727 SRM 57-40-10 AND 51-10-3Jan 7, 2006 · N746DH · Boeing 727224 · Wing Main, Frame StructureSDR GAIA05040OPOil Filter · bypassingDURING CRUISE, DURING FLIGHT VIBRATION AND NOISE FOLLOWED BY OIL FILTER BYPASS LIGHT ON NR 3 ENGINE. NR 3 EINGINE SHUTDOWN AND ENGINE WINDMILLING PROCEDURE FOLLOWED (OIL FILTER BYPASS LIGHT WENT OUT BELOW 25 PERCENT, N2) NOTE: ENGINE WINDMILLED FOR 38 MIN AT Dec 22, 2005 · N69735 · Boeing 727224 · Engine Oil System (Airframe Furnished)SDR GAIA05039OPFilter · bypassingDURING CLIMB, OIL FILTER BYPASS LIGHT ILLUMINATED. RETARDING THROTTLE DID NOT EXTINGUISH. PERFORMED PRECAUTIONARY ENGINE SHUTDOWN IAW ABNORMAL PORCEDURES. NOTE: THE ENGINE WAS WINDMILLING FOR ABOUT 15-20 MIN AND OIL PRESSURE WAS ABOUT 20-25 PSI. FLIGHT RETDec 22, 2005 · N69735 · Boeing 727224 · Engine Oil System (Airframe Furnished)SDR DHL2005745014Accessory Unit · malfunctionedWHEN GEAR WAS SELECTED UP RED NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED. ALL DOORS LIGHTS WERE OUT. CYCLED GEAR AS DIRECTED BY MX. NOSE GEAR UNSAFE LIGHT WENT OUT. T/S TO LG ACCESSORY UNIT. REMOVED AND REPLACED LG ACCESSORY UNIT WITH SERVICEABLE UNIT. Dec 19, 2005 · N745DH · Boeing 727224 · Landing Gear Position and WarningSDR DHL2005747003Connector · looseAFTER FLAPS WERE RETRACTED TO 0 THE AMBER LE FLAPS LIGHT ILLUMINATED ON FWD PANEL SO PANEL READ NR5 LE FLAP IN TRANSIT ABNORMAL PROCEDURE COMPLETE PROBLEM REMAINED. FOUND CONNECTOR LOOSE FOR SWITCH CLEANED, RESECURED SWITCH CONNECTOR PLUG RAN FLAPS OPS CK NMLDec 16, 2005 · N747DH · Boeing 727224 · Leading Edge Slat Control SystemSDR FX7A200500011Actuator · inoperativeFLIGHT CREW REPORTED THAT DURING FLAP RETRACTION, THE NR 4 SLAT DID NOT RETRACT FROM 5 TO 2 FLAP SETTINGS, FUEL DUMPING WAS ACCOMPLISHED. LOG PAGE # 36436. REMOVED AND REPLACED THE NR 4 SLAT ACTUATOR ASSEMBLY AND THE SLAT SWITCH, IAW 727 MM REF 27-81-22 AND Dec 10, 2005 · N79749 · Boeing 727224 · Leading Edge Slat ActuatorSDR DHL2005746005Light · looseCABIN DOOR EMERGENCY LIGHT CAME ON AFTER T/O AND STAYED ON. RESECURED AND TESTED EMERGENCY LIGHT IAW MM CHP 33-50-01. OPS CK NORMAL AT THIS TIME.Dec 7, 2005 · N746DH · Boeing 727224 · Emergency LightingSDR DHL2005745013Switch · malfunctionedDURING TAKEOFF ENG NR 2 WAS NOT MAKING TAKEOFF THRUST. ENG NR1, NR3 WERE NORMAL AT 80 KTS WITH THRUST LEVERS MATCH, NR2 EPR WAS AT 1.6 NOT INCREASING, N1 WAS ABOVE RED LINE. REJECTED T/O AT 80KTS,170,000 LBS 3860 PRESSURE. ENGINE RUNUP PERFORMED IAW JRH. NNov 23, 2005 · N745DH · Boeing 727224 · Engine (Turbine/Turboprop)SDR DHL2005745012Switch · out of adjustRED DOORS LIGHT ON FORWARD PANEL FLICKERS IN FLIGHT AND CORRESPONDING L GEAR DOOR LIGHT ON FLIGHT ENGINEERS PANEL FLICKERS. NO VIBRATION FELT. ADJUSTED LEFT MAIN GEAR DOOR SWITCH IAW B727 M/M 32-62-0, OPS CHECK GOOD.Nov 22, 2005 · N745DH · Boeing 727224 · Landing Gear Position and WarningSDR DHL2005745011Indicator · inoperativeCAPTAINS AIRSPEED INDICATOR INOP. STBY AIRSPEED INDICATOR INDICATIONS NOT NOTED. ABORTED TAKEOFF AT APPROXIMATELY 70 KIAS PRESSURE ALT 26FT. AIRCRAFT WEIGHT 137,100 LB REVERSE THRUST NOT USED. REMOVED AND REPLACED CAPT A/S IND IAW M/M 34-12-21. REMOVED ANNov 16, 2005 · N745DH · Boeing 727224 · Airspeed/Mach Indicator
Back to Boeing 727-224