Boeing 727-247

Service difficulty reports · 2,669

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  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = '727247'
  ORDER BY difficulty_date DESC"

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SDR FDEA201011124368Skin · corrodedBULGE EXTERIOR FUSELAGE, INCLUDING SHEARED RIVET HEAD STA 990 - STA 970 STR 28L. CUTOUT DAMAGED SKIN DIM: 12 1/2" X 1 7/8 IAW SRM 53-30-3 FIG 3 AND 53-30-2 FIG 2. FABRICATED REPAIR DOUBLER AND FILLER FROM 2024 T3 .125" DIM 24 1/2" X 10 3/4" AND 12 1/2 X 1 1Nov 12, 2010 · N233FE · Boeing 727247 · Fuselage Main, Plate/SkinSDR FDEA201011124370Stringer · corrodedSTRINGER 28L CORRODED STA 990 - 970 CUTOUT DAMAGED STRINGER DIM: 19 1/2" IAW SRM 53-10-1 FIG 1 AND 53-10-3 FIG 1. FABRICATED STRINGER SECTION FROM BAC 1498-145 7075 T6 DIM: 19 1/2" IN LENGTH AND (2 EA. ) SPLICE SECTIONS FROM BAC 1498-131 7075 T6 DIM: 19 1/14"Nov 12, 2010 · N233FE · Boeing 727247 · Fuselage Main, Longeron/StringerSDR FDEA201007262686Light · failedMAINT PRE-FLT FOUND LT ENTRY DOOR, EMERGENCY LIGHT INOP. NEW BATTERIES NO HELP. REPLACED LIGHT ASSY IAW AMM 33-50-101-2-0. OPS CKS GOOD. PREMATURE REMOVAL/INSTALLATION OFF.Jul 26, 2010 · N233FE · Boeing 727247 · Emergency LightingSDR CA100622024Bolt · shearedA PORTION OF THE BOLT AND A BUSHING (PN NAS72-7E007) WAS DISCOVERED ON A TAXIWAY USED BY ACFT EARLIER IN THE DAY. THE ACFT WAS INSPECTED, AND THE PART WAS FOUND BE MISSING FROM THE LT WING, INBD FLAP, OTBD FLAP CARRIAGE ASSY. THE ACFT WAS TAKEN OUT OF SERVICJun 21, 2010 · Boeing 727247 · Trailing Edge FlapsSDR CA091224001Window · cracked(CAN) DISCREPANCY: AT FL 37.0 VERY LOUD CRACKING NOISE FROM VICINITY OF F/O NR 3 WINDOW DESCENT TO 10,000 AND DEPRESSURIZED AIRCRAFT. MX NOTE: AS PER CREW COMMENTS AIRCRAFT DID NOT LOOSE CABIN PRESSURE DUE TO THIS INCIDENT AND AS A PRECAUTIONARY MEASURE AIRCDec 24, 2009 · Boeing 727247 · Flight Compartment WindowsSDR CA091009003Warning Switch · faulty(CAN) IN POSITION ON RWY FOR DEPARTURE. THRUST LEVERS ADVANCED TO TAKEOFF THRUST FOLLOWED BY THE TAKEOFF WARNING HORN. THRUST RETARTED TO IDLE. FLAPS RESELECTED UP THEN BACK TO FLAPS 15, STAB TRIM MOVED TO ZERO THEN BACK TO TAKEOFF POSITION, SPD BRAKES DEPLOYEOct 8, 2009 · Boeing 727247 · Stabilizer Position IndicatingSDR CA090625006Clamp · leaking(CAN) ENROUTE, HAD AN ENGINE FIRE WARNING. ENG NR 3 DRILL AND CHECK LIST COMPLETED AND NR 1 BOTTLE DISCHARGED. TROUBLESHOOTING CARRIED OUT AND COULD NOT FAULT ON GROUND. WITH ENGINE RUNNING, CARRIED OUT A LEAK CHECK OF PNEUMATIC DUCTS ON THE ENG AND AROUNDJun 24, 2009 · Boeing 727247 · Engine Bleed Air SystemSDR CA090625004Actuator · failed(CAN) DISCREPANCY ON DESCENT. HYD SYS A, ENG 1 PUMP LOW PRESSURE LIGHT ILLUMINATED WHEN FLAPS WERE EXTENDED. PRESSURE READ NORMAL QUANTITY 0. ENGINE NR 2 PUMP LIGHT ILLUMINATED. BOTH LIGHTS THEN EXTINGUISHED. FLAPS AND GEAR EXTENDED BY NORMAL SYS. ACFT Jun 24, 2009 · Boeing 727247 · Trailing Edge Flap ActuatorSDR FDEA200902210628Keelbeam · corroded29R KEEL BEAM AT STA.950C TO 950E IS CORRODED. REPAIRED KEELBEAM AREA AT STA 950C-950E BY REMOVING CORROSION AND INSTALLED STRAP REPAIR IAW EA NR 7-5310-124065.Feb 21, 2009 · N237FE · Boeing 727247 · Fuselage Main, KeelSDR FDEA200902210627Stringer · corrodedLOWER FWD CARGO COMPARTMENT HEAVY CORROSION ON SKIN LAP, STR 26R FROM 720D - 720E 18 AND FRAME FS 720E AT 26R REPAIRED STR 26 FROM 720D-740 IAW SRM 53-10-3 FIG I. REPAIRED SKIN AT LAP JOINT STA 720D-720E IAW SRM 53-30-3 FIG 24.Feb 21, 2009 · N237FE · Boeing 727247 · Fuselage Main, Longeron/StringerSDR FDEA200902210626Stringer · corrodedAT STA 720D LT SIDE STR 22L HAS LIGHT CORROSION. REPAIRED STRINGER 22L STA 720D LT SIDE IAW SRM 53-10-3 FIG 1, REPAIR PART FABRICATED ON TRAVELER T8/781589.Feb 21, 2009 · N237FE · Boeing 727247 · Fuselage Main, Longeron/StringerSDR FDEA200902210625Structure · crackedLT WING T/E COVE AREA FALSE SPAR WEB CRACKED OTBD OF NR 7 SPOILER ACTUATOR. REPAIRED SPAR WEB IAW SB 727-57-158 PARTS FABRICATED ON TRAVELERS T9/780969,T9/780970,T9/780968,T9/780971,AND T9/780967. REPAIR DOUBLER FABRICATED.Feb 21, 2009 · N237FE · Boeing 727247 · Wing Miscellaneous StructureSDR FDEA200902180573Seat Track · crackedMAIN DECK SEAT TRACK EXT EXTENSION AT STA.850-870 RBL 45-63 CRACKED . REMOVED SEAT TRACK EXTENSION AND BUSHINGS IAW SRM 51-30-2. FABRICATED SEAT TRACK EXTENSION IAW DWG 69-24621. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED SEAT TRACK EXTENSION AND BUSHIFeb 18, 2009 · N237FE · Boeing 727247 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200902100500Shear Tie · corrodedLOWER FWD CARGO COMPARTMENT, FRAME SHEAR TIE CORRODED AT FS 720F BETWEEN STR 26 AND 27 L. REMOVED AND INSTALLED NEW SHEAR TIE IAW SRM 51-30-2. FABRICATED NEW SHEAR TIE ON MAE TRAVELER NR T9/780298.Feb 10, 2009 · N237FE · Boeing 727247 · Fuselage Internal Mounting StructureSDR CA081112005Connector · damaged(CAN) AT APPROX 700 FT, AGL T/O YHZ FIRE WARNING LIGHTS ON GLARE SHIELD WERE DIMMLY ILLUMINATED. NO AURAL WARNING. APU FIRE HANDLE ILLUMINATED. SWITCH PULLED AND BOTTLE DISCHARED. ACFT RETURNED TO DEPARTURE. RECTIFICATION AFTER TROUBLESHOOTING FOUND APU FINov 7, 2008 · Boeing 727247 · Fire Protection System WiringSDR DHLA200800124Fuel Tank · leakingKEROSENE SMELL WHEN TURNING ON PACKS AFTER T/O. FOUND FUEL LEAK NR 2 TANK.Nov 6, 2008 · N793DH · Boeing 727247 · Fuel StorageSDR DHLA200800122Unknown · odorPIREP: KEROSENE SMELL AFTER TAKEOFF IN ILN. DOWNLOADED A/C VISUALLY INSPECTED MAIN CARGO DECK & FWD & AFT PITS NO EVIDENCE OF LEAKS OR SMELL IAW BMM 5-51-0 & 12-40.Nov 5, 2008 · N793DH · Boeing 727247 · Air Distribution SystemSDR DHLA200800119Unknown · odorDURING CLIMB-OUT A STRONG KEROSENE ODOR WAS IN THE COCKPIT FOR TWO TO THREE MINUTES AND THEN WENT AWAY. RESOLUTION, GROUND RUN OF APU IAW 49-00-00 AND GROUND RUN OF LEFT AND RIGHT PACKS IAW MM 21-55-00 COULD NOT ODOR KEROSENE OR ANY OTHER ABNORMAL ODORS, NO NOct 30, 2008 · N793DH · Boeing 727247 · Air Distribution SystemSDR CA081009007Switch · failed(CAN) JUST AFTER DEPARTURE FROM YYZ, THE PILOTS NOTICED WHEN SELECTING FLAPS 5 TO FLAPS 2, THE LEADING EDGE FLAP INDICATOR ON THE FORWARD PANEL WENT MOMENTARILY GREEN THEN BACK TO AMBER. THE LEADING EDGE INDICATOR ON THE REAR PANEL INDICATED THE NR 1 LEADING Oct 9, 2008 · Boeing 727247 · Leading Edge Slat Position Indicating SystemSDR CA080917003Shutoff Valve · failed(CAN) DURING CLIMBOUT, SEPT 16 2008, PRESSURIZATION FAILED TO OPERATE NORMALLY. WHEN CLIMBING THROUGH 23,000 FT, CABIN ALTITUDE EXCEEDED 10000 FT. FUEL DUMP CARRIED OUT IN ORDER FOR ACFT TO RETURN TO DEPARTURE. CABIN PRESSURIZATION LEAK CHECK CARRIED OUT, NO Sep 16, 2008 · Boeing 727247 · Pressure Regulator/Outflow ValveSDR CA080911005O-Ring · leaking(CAN) WHILE CLIMBING OUT, NOTICED ENG NR 1 OIL QUANTITY INDICATOR SLOWLY DECREASING, QUANTITY WAS 1 GALLON AT TOP OF CLIMB. AT MID POINT, QUANTITY DECREASED TOWARD ZERO. ENGINE SHUTDOWN DRILL AND CHECK LIST COMPLETED. ENGINE WINDMILLING SUPPLEMENT COMPLETEDSep 11, 2008 · Boeing 727247 · Engine Oil Distribution (Airframe Furnished)SDR DHL2008F00032Unknown · unknownDURING TAKEOFF ROLL OVERSPEED WARNING SOUND AT 70 KTS . DEFERRED IAW MEL 34-4-3 PULLED IAW CREW REQUEST. AIRCRAFT WAS GROUNDED. (K)Sep 11, 2008 · N793DH · Boeing 727247 · Central WarningSDR CA080418002Fire Detector · false indication(CAN) AFTER TAKEOFF, AT APPROX 1,000 FEET AGL, THERE WAS A FIRE WARNING ON THE NR 1 ENGINE. THRUST LEVER RETARDED, LIGHT REMAINED ON. EMERGENCY DRILL COMPLETED AND LIGHT EXTINGUISHED AFTER FIRE BOTTLE DISCHARGED. AC RETURNED AND LANDED WITHOUT FURTHER INCIDENApr 17, 2008 · Boeing 727247 · Fire DetectionSDR CA080124002Swivel · leaking(CAN) AC WAS DISPATCHED AND DURING CRUISE FLIGHT, THE FLIGHT ENGINEER NOTICED THAT THE (A) SYS HYDRAULICS INDICATED .1250 OF A TANK REMAINING. THE CREW DECIDED TO DECLARE AN EMERGENCY AND THE LANDING GEAR NEEDED TO BE CRANKED DOWN. THE AC LANDED SAFELY AND WASJan 24, 2008 · Boeing 727247 · Hydraulic System, MainSDR CA080115007Pcu · frozen(CAN) THE AC ARRIVED AT DESTINATION AND WAS ON A TURN-AROUND WHEN THE CREW NOTICED ON TAXI OUT, THAT THE AILERONS HAD FROZEN UP. THE AC RETURNED TO THE RAMP WHERE MAINT INSPECTED THE SYS. IT WAS DETERMINED THAT THE AILERON POWER CONTROL UNIT HAD FROZEN UP. HEJan 15, 2008 · Boeing 727247 · Aileron Control SystemSDR CA080109004Uplock Switch · faulted(CAN) FLIGHT WAS DEPARTING AND THEN DURING THE TAKEOFF ROLL, THE CREW SELECTED THE LANDING GEAR UP. WHEN THE GEAR HAD CYCLED UP THERE REMAINED A RED NOSE GEAR UNSAFE LIGHT. THE CREW CYCLED THE LANDING GEAR 3 TIMES BEFORE THE UNSAFE LIGHT EVENTUALLY WENT OUT. TJan 8, 2008 · Boeing 727247 · Landing Gear Position and WarningSDR DHL2007793027Shear Tie · corrodedINTERGRANULAR CORROSION NOTED ON BS 700 FRAME LOWER LIP BETWEEN STRINGERS 27R AND 28R FORWARD PIT. CUT OUT DAMAGE. FABRICATED AND INSTALLED A DOUBLER REPAIR IAW SRM 53-10-4 FIGURE 13 AND 53-10-2 FIGURE 2. HEAT TREATED TO T6 CONDITION IAW FAS0115 REV 11 AND Dec 12, 2007 · N793DH · Boeing 727247 · Fuselage Internal Mounting StructureSDR DHL2007793032Nose Cowl · crackedNR 1 ENGINE NOSE COWL EXTERIOR SKIN SURFACE AT 12 O'CLOCK POSITION JUST OUTBOARD OF INSPECTION PANEL HAS A 2" LONG CRACK RUNNING FROM RIVET HEAD. CUT OUT DAMAGED SECTION. FABRICATED AND INSTALLED DOUBLER REPAIR IAW SRM 54-30-3 FIGURE 3 AND 3A.Dec 11, 2007 · N793DH · Boeing 727247 · Nacelle/Pylon, Main FrameSDR 07FDEA05030Valve · malfunctionedNR 2 FUEL TANK CROSS FEED WOULD NOT OPEN UP IN FLIGHT. ACN RELEASED FOR SERVICE. CLEANED AND RESEATED NR 2 FUEL CROSSFEED MAINIFOLD VALVE CONNECTOR PER SMP. TRANSFERED FUEL FROM NR 2 INTO 1&3 TANKS. PERFORMED TEST OF VALVE PER AMM 28-22-011-4. SYS CHECKS NORDec 11, 2007 · N237FE · Boeing 727247 · Aircraft Fuel Distribution SystemSDR DHL2007793006Hinge · crackedMAIN CARGO DOOR AFT HINGE APPEARS TO BE CRACKED, BS 640 STRINGER 4L. HFEC VERIFIED CRACK IAW B-727 NDTM PT 6-51-00-00 FIGURE 23. REMOVED AT MAIN CARGO DOOR AFT HINGE BS 640 STRINGER 4L AS REQUIRED IAW AEI BOEING 727-200 FREIGHTER M/M FIGURE 5201B REV G. FABDec 8, 2007 · N793DH · Boeing 727247 · Fuselage, Door HingeSDR DHL2007793021Stringer · corrodedSURFACE CORROSION ON STRINGER 30 FROM BS 1150 TO 1166. REMOVED CORROSION IAW SRM 51-10-6. AREA FOUND WITH IN LIMITS IAW SRM 53-10-1 FIGURE 1 AND 53-10-2 FIGURE 9. FOUND CORROSION BETWEEN BS 1150-1155 TO BE OUT OF LIMITS IAW SRM 53-10-1 FIGURE 1 AND 53-10-2 Dec 8, 2007 · N793DH · Boeing 727247 · Fuselage Main, Longeron/StringerSDR DHL2007793020Stringer · corrodedSTRINGER SPLICE CORRODED ON STRINGER 27L AT STATION 1130 IN CHANNEL AND AFT OUTBOARD FLANGE EXFOLIATED. CUT OUT DAMAGE IAW SRM 53-10-23 FIGURE 1. FABRICATED REPAIR IAW SRM 53-10-3 FIGURE 1. TREATED AND PRIMED PART AND AREA IAW SRM 51-10-2. INSTALLED STRINGDec 8, 2007 · N793DH · Boeing 727247 · Fuselage Main, Longeron/StringerSDR DHL2007793017Seat Track · corrodedCABIN SEAT TRACK HAS CORROSION AT BS 500 TO 680 LBL45. REMOVED SEAT TRACK IAW SRM 51-30-2. FABRICATED 2 EACH SECTION SEAT TRACKS , 2 ANGLE REPAIRS, AND 1 STRAP IAW SRM 53-10-5 FIGURE 1. TREATED AND PRIMED PART IAW SRM 51-10-2. INSTALLED 2 SECTION SEAT TRACKDec 7, 2007 · N793DH · Boeing 727247 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2007793016Seat Track · corrodedCABIN SEAT TRACK HAS CORROSION AT BS 740 TO 830 RBL 24. REMOVED SECTION AS REQUIRED IAW SRM 51-30-2. FABRICATED NEW SECTION IAW SRM 51-20-1 AND 53-10-2 FIGURE 7. TREATED AND PRIMED NEW SECTION IAW SRM 51-10-2. INSTALLED NEW SECTION IAW SRM 51-30-2.Dec 7, 2007 · N793DH · Boeing 727247 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2007793028Shear Tie · corrodedCORROSION ON SHEAR TIE AT STATION 1130 BETWEEN STRINGER 29R AND 30. REMOVED SHEAR TIE AT AFT CARGO COMPARTMENT STATION 1130 STRINGER 29R TO 30 AS REQUIRED IAW B-727 SRM 53-10-4 FIGURE 15. FABRICATED NEW SHEAR TIE ANGLE MATERIAL USED 7075-T6 0.063" PO NR 9006Dec 6, 2007 · N793DH · Boeing 727247 · Fuselage Internal Mounting StructureSDR DHL2007793031Floorbeam · corrodedEXFOLIATED CORROSION ON FLOORBEAM BS 276 RBL 14. CUT OUT CORRODED SECTION OF FLOORBEAM IAW SRM 51-40-4 FIGURE 1. FABRICATED FILLER, 1 ANGLE AND FILLER FOR VERTICAL STIFFENER IAW SRM 51-40-4. TREATED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLED REPAIR PARTDec 5, 2007 · N793DH · Boeing 727247 · Fuselage Main, Floor BeamSDR DHL2007793022Nose Cowl · dentedNR 3 ENGINE NOSE COWL HAS DENTS ON INBOARD SIDE 3 O'CLOCK POSITION NAC STATION 99.3. CUT OUT DAMAGE AREA AT NR 3 ENGINE NOSE COWL INBOARD SIDE AT 3 O'CLOCK POSITION. FABRICATED DOUBLER OUT 2024-T3 0.040" IAW B-727 SRM 54-30-3 AND 54-30-2. FABRICATED FILLER Dec 4, 2007 · N793DH · Boeing 727247 · Engine Air Intake SystemSDR DHL2007793015Shear Tie · chafedFRAME AT BS 344 CHAFING AT 9G BARRIER SHEAR TIE STRINGER 12R. REMOVED AND REPLACED ATTACH ANGLE (SHEAR TIE) AT STRINGER 3R P/N 2942-3 PO NR 734151 IAW DRAWING NR 2936 REV B AND MM CHAPTER 25 PAGE 20 REV G MARCH 28, 2005 ON 9G BARRIER.Dec 4, 2007 · N793DH · Boeing 727247 · Fuselage Internal Mounting StructureSDR DHL2007793014Shear Tie · chafedFRAME AT BS 344 CHAFING AT 9G BARRIER SHEAR TIE STRINGER 11R. REMOVED AND REPLACED ATTACH ANGLE (SHEAR TIE) AT STRINGER 3R P/N 2942-3 PO NR 734151 IAW DRAWING NR 2936 VENTURA AEROSPACE REV B AND AEI BOEING 727-200 FREIGHTER M/M CHAPTER 25 PAGE 20 REV G MARCH Dec 4, 2007 · N793DH · Boeing 727247 · Fuselage Internal Mounting StructureSDR DHL2007793012Shear Tie · chafedFRAME AT BS 344 CHAFING AT 9G BARRIER SHEAR TIE STRINGER 9R. REMOVED AND REPLACED ATTACH ANGLE (SHEAR TIE) AT STRINGER 3R P/N 2942-3 PO NR 734151 IAW DRAWING NR 2936 VENTURA AEROSPACE REV B AND AEI BOEING 727-200 FREIGHTER M/M CHAPTER 25 PAGE 20 REV G MARCH 2Dec 4, 2007 · N793DH · Boeing 727247 · Fuselage Internal Mounting StructureSDR DHL2007793011Shear Tie · chafedFRAME AT BS 344 CHAFING AT 9G BARRIER SHEAR TIE STRINGER 8R. REMOVED AND REPLACED ATTACH ANGLE (SHEAR TIE) AT STRINGER 3R P/N 2942-3 PO NR 734151 IAW DRAWING NR 2936 VENTURA AEROSPACE REV B AND AEI BOEING 727-200 FREIGHTER M/M CHAPTER 25 PAGE 20 REV G MARCH 2Dec 4, 2007 · N793DH · Boeing 727247 · Fuselage Internal Mounting StructureSDR DHL2007793010Shear Tie · chafedFRAME AT BS 344 CHAFING AT 9G BARRIER SHEAR TIE STRINGER 6R. REMOVED AND REPLACED ATTACH ANGLE (SHEAR TIE) AT STRINGER 3R P/N 2942-3 PO NR 734151 IAW DRAWING NR 2936 VENTURA AEROSPACE REV B AND AEI BOEING 727-200 FREIGHTER M/M CHAPTER 25 PAGE 20 REV G MARCH 2Dec 4, 2007 · N793DH · Boeing 727247 · Fuselage Internal Mounting StructureSDR DHL2007793009Shear Tie · chafedFRAME AT BS 344 CHAFING AT 9G BARRIER SHEAR TIE STRINGER 5R. REMOVED AND REPLACED ATTACH ANGLE (SHEAR TIE) AT STRINGER 3R P/N 2942-3 PO NR 734151 IAW DRAWING NR 2936 VENTURA AEROSPACE REV B AND AEI BOEING 727-200 FREIGHTER M/M CHAPTER 25 PAGE 20 REV G MARCH 2Dec 4, 2007 · N793DH · Boeing 727247 · Fuselage Internal Mounting StructureSDR DHL2007793008Shear Tie · chafedFRAME AT BS 344 CHAFFING AT 9G BARRIER SHEAR TIE STRINGER 4R. REMOVED AND REPLACED ATTACH ANGLE (SHEAR TIE) AT STRINGER 3R P/N 2942-3 PO NR 734151 IAW DRAWING NR 2936 VENTURA AEROSPACE REV B AND AEI BOEING 727-200 FREIGHTER M/M CHAPTER 25 PAGE 20 REV G MARCH Dec 4, 2007 · N793DH · Boeing 727247 · Fuselage Internal Mounting StructureSDR DHL2007793007Shear Tie · chafedFRAME AT BS 344 CHAFING AT 9G BARRIER SHEAR TIE STRINGER 3R. REMOVED AND REPLACED ATTACH ANGLE (SHEAR TIE) AT STRINGER 3R P/N 2942-3 PO NR 734151 IAW DRAWING NR 2936 VENTURA AEROSPACE REV B AND AEI BOEING 727-200 FREIGHTER M/M CHAPTER 25 PAGE 20 REV G MARCH 2Dec 4, 2007 · N793DH · Boeing 727247 · Fuselage Internal Mounting StructureSDR DHL2007793005Skin · crackedDENT RT FUSELAGE SKIN BS 1220 ABOVE STRINGER 19R. EVALUATED DENT AND FOUND IT TO BE WITHIN LIMITS IAW SRM 53-30-1 FIGURE 1. HFEC SHOW CRACK AT DENT AREA IAW NDT PT 6 51-00-00 FIGURE 23. CUT OUT DAMAGE AREA IAW SRM 53-30-3 FIGURE 1. FABRICATED DOUBLER REPDec 4, 2007 · N793DH · Boeing 727247 · Fuselage Main, Plate/SkinSDR CA071204004Accessory Unit · unserviceable(CAN) SHORTLY AFTER TAKEOFF WHEN GEAR WAS BEING RETRACTED, CREW NOTICED THAT THE RT MAIN GEAR RED LIGHT WAS STILL ILLUMINATED. CREW CYCLED THE LANDING GEAR (3) TIMES WITH THE SAME RESULTS. THE CREW ADVISED THAT AIR NOISE COULD BE HEARD. GEAR WAS SELECTED DOWN Dec 4, 2007 · Boeing 727247 · Landing Gear Retraction/Extension SystemSDR DHL2007793030Seat Track · corrodedCABIN SEAT TRACK CORRODED AT BS 870 TO 959 LBL45. FABRICATED NEW SEAT TRACK SECTION IAW SRM 53-10-5 FIGURE 1. TREATED AND PRIMED PART IAW SRM 51-10-2. INSTALLED NEW SECTION IAW SRM 53-10-5 FIGURE 1.Dec 2, 2007 · N793DH · Boeing 727247 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2007793019Skin · dentedDENT, UNDERNEATH ELEVATOR SKIN PANEL AT ELEVATOR STATION 50.50 LT. CUT OUT DAMAGE AREA AT LT ELEVATOR LOWER SKIN IAW SRM 55-20-3 FIGURE 4. FABRICATED REPAIR DOUBLER IAW SRM 55-20-3 FIGURE 4 AND 55-20-3 FIGURE 1. PART AND AREA TREATED AND PRIMED IAW SRM 51-1Dec 2, 2007 · N793DH · Boeing 727247 · Elevator, Plate/SkinSDR DHL2007793026Frame · dentedAFT CARGO COMPARTMENT FRAME AT STATION 1090 UPPER FLANGE IS DENTED BETWEEN STRINGER 27L TO 26L. CUT OUT DAMAGE AREA AT AFT CARGO COMPARTMENT FRAME STATION 1090 BETWEEN STRINGER 27L TO 26L IAW B-727 SRM 51-40-3 FIGURE 1 DIMENSION CUT OUT .75" BY .75". FABRICADec 1, 2007 · N793DH · Boeing 727247 · Fuselage Main, Frame
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