Boeing 727-223

Service difficulty reports · 5,313

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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 aircraft_model_key = '727223'
  ORDER BY difficulty_date DESC"

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SDR DHL2008746017Shear Tie · corrodedDURING C CHECK, AFT PIT BS 970 SHEAR TIE CORROSION BETWEEN STRINGER 29L AND 28L. FOUND CORROSION OUT OF LIMITS IAW SRM 53-10-1 FIG 1, CUT OUT DAMAGE AREA DIMENSION 6.5" BY 1" IAW SRM 51-10-1, 53-10-1 FIG 1 AND 53-10-4 FIG 11. FABRICATED SHEAR TIE REPAIR IAW Jan 10, 2008 · N749DH · Boeing 727223 · Fuselage Internal Mounting StructureSDR DHLA200700073Battery · inoperativeCOCKPIT EMERGENCY EXIT LIGHT INOP WITH EMERGENCY EXIT LIGHT SWITCH ON AND DURING STANDBY POWER CHECK. REMOVED AND REPLACED COCKPIT EMERGENCY LIGHT BATTERIES PER MM 33-50-101 CK GOOD, P/N MISC062 (2 EACH).Dec 2, 2007 · N749DH · Boeing 727223 · Emergency LightingSDR DHLA200700072Light · inoperativeRE INSTALL EMERG EXIT LIGHT. REINSTALLED COCKPIT EMERGENCY LIGHT ASSY OVER DOOR PER MM 33-50-71, OPS CKS GOOD.Nov 30, 2007 · N749DH · Boeing 727223 · Emergency LightingSDR DHLA200700069Battery · inoperativeFWD ENTRY DOOR ESCAPE SLIDE LIGHT REMAINS ILLUMINATED. DEFERRED IAW MEL 33-16-2A CAT-B PLACARD INSTALLED. REMOVED AND REPLACED BATTERY ASSY OPS CHECK GOOD IAW MM 33-50-01 THIS CLEARS DMI 30900 PLACARD REMOVED PN 60-1321-1Nov 27, 2007 · N753DH · Boeing 727223 · Emergency LightingSDR C8GA20070012Helicoil · damagedFLT 708 FROM TOL TO MCI - DURING CRUISE OPERATION AT FLT LEVEL 320, THE NR 3 ENGINE LOW OIL PSI LIGHT ILLUMINATED. OIL QUANTITY WAS OBSERVED TO BE DECREASING FOLLOWED BY A DECREASE IN OIL PSI. THE NR 3 ENGINE WAS SHUT DOWN AND THE AIRCRAFT DIVERTED TO STL WHNov 20, 2007 · N713AA · Boeing 727223 · Turbine Engine Accessory DriveSDR DHLA200700065Panel · defectiveESCAPE ROPE ACCESS PANEL ON CAPT SIDE WILL NOT CLOSE. SECURED ESCAPE ROPE PANEL ON CAPT SIDE, OPS CHECK GOOD PER MM 25-60-00.Nov 18, 2007 · N749DH · Boeing 727223 · Emergency EquipmentSDR DHLA200700064Battery · dischargedEMERGENCY EXIT LIGHTS ILLUMINATE THEN IMMEDIATELY EXTINGUISH WHEN TURNED ON AND DURING STAND BY POWER CHECK. REMOVED AND REPLACED BOTH EMERGENCY EXIT LIGHT BATTERIES, OPS CHECK GOOD PER MM 33-50-01 P/N MISC062 QTY 4.Nov 18, 2007 · N749DH · Boeing 727223 · Emergency LightingSDR CA071122006Accessory Unit · inoperative(CAN) THE CREW DISCOVERED THAT THE LANDING GEAR HANDLE WOULD NOT MOVE PAST THE (OFF) POSITION WITHOUT THE USE OF THE OVERRIDE TRIGGER. AT THE TERMINATING STATION, MAINTENANCE REPLACED THE LANDING GEAR ACCY UNIT AND RETURNED THE AIRCRAFT TO SERVICE. (TC NR 2007Nov 9, 2007 · Boeing 727223 · Landing Gear Retraction/Extension SystemSDR DHLA200700063Lamp · inoperativeEMERG EXIT LTS UNARMED LIGHT INOP. RELAMPED EMERG EXIT LTS. UNARMED LIGHT (P/N 313). OPS CHECKS NORMAL IAW MM CH 33-50-01.Oct 31, 2007 · N754DH · Boeing 727223 · Emergency LightingSDR DHLA200700057Pump · failedAT START OF TAKEOFF, 1.4 EPR NR 2 ENGINE FAILED COMPLETED ABNORMAL PROCEDURE. REPLACED NR 2 ENG FUEL PUMP IAW PRATT AND WHITNEY JT8D M/M GROUND RAN AND LEAK CK GOOD AT THIS TIME IAW 73-11-01. PERFORMED MPA RUN PER JRH 7.7.Oct 18, 2007 · N754DH · Boeing 727223 · Engine Fuel PumpSDR C8GA20070010Line · leakingFLT 811 FROM SJU TO MCO - DURING CLIMB OPERATION, THE AIRCRAFT EXPERIENCED NR 2 ENGINE "A" SYSTEM HYDRAULIC FAILURE/FLUID LOSS. THE AIRCRAFT RETURNED TO SJU WERE AN EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION REVEALEOct 13, 2007 · N715AA · Boeing 727223 · Hydraulic System, MainSDR DHL2007749002Web · crackedWHILE AT FLIGHTSTAR AIRCRAFT SERVICES FOR A CHECK, REF N/R 099780, DISCREPANCY, RT AIRSTAIR TORQUE BOX CRACKED AT LIGHTNING HOLE ATBS 1233. STOPPED DRILLED HOLE AT THE END OF CRACK WITH .250 IAW SRM 51-10-01, C/W HFEC IAW NDTM PT 6, 51-00-00 FIG 23, CRACK TERSep 24, 2007 · N749DH · Boeing 727223 · Fuselage Miscellaneous StructureSDR DHL2007749001Web · crackedWHILE AT FLIGHTSTAR AIRCRAFT SERVICES FOR A CHECK, REF N/R 099780, DISCREPANCY, RT AIRSTAIR TORQUE BOX CRACKED AT LIGHTNING HOLE AT BS 1233. STOPPED DRILLED HOLE AT THE END OF CRACK WITH .250 IAW SRM 51-10-01, C/W HFEC IAW NDTM PT 6, 51-00-00 FIG 23, CRACK TESep 24, 2007 · N749DH · Boeing 727223 · Fuselage Miscellaneous StructureSDR DHL2007749006Torque Box · crackedDURING "A" CHECK, REF N/R 099779 , DISCREPANCY, RT AIRSTAIR TORQUE BOX CRACKED AT LIGHTING HOLE BS 1228. STOP DRILLED AT THE END OF CRACK WITH .250" IAW B727 SRM 51-10-01. C/W HFEC IAW B727 NDTM, PT 6 51-00-00, FIG 23, CRACK TERMINATE IN STOP DRILL HOLE. FSep 24, 2007 · N749DH · Boeing 727223 · Fuselage Main, StructureSDR DHL2007749005Torque Box · crackedWHILE AT FLIGHTSTAR AIRCRAFT SERVICES FOR A CHECK, REF N/R 099780, DISCREPANCY, RT AIRSTAIR TORQUE BOX CRACKED AT LIGHTNING HOLE ATBS 1233. STOPPED DRILLED HOLE AT THE END OF CRACK WITH .250 IAW SRM 51-10-01, C/W HFEC IAW NDTM PT 6, 51-00-00 FIG 23, CRACK TERSep 24, 2007 · N749DH · Boeing 727223 · Fuselage Miscellaneous StructureSDR C8GA20070009Control Valve · malfunctionedFLT 720 FROM TOL TO ATL, DURING CRUISE OPERATION THE AIRCRAFT EXPERIENCED ICING CONDITIONS WITH BOTH ENGINE AND WING ANTI-ICE ON, THE LOWER AFT CARGO SMOKE DETECTOR BELL RANG AND INDICATED A FIRE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCISep 14, 2007 · N899AA · Boeing 727223 · Engine Anti-Icing SystemSDR C8GA20070008Rod · brokenFLT 723 FROM ROC TO TOL, AFTER TAKEOFF WHEN GEAR WAS RAISED THE RIGHT MAIN LANDING GEAR GREEN AND RED INDICATIONS LIGHTS REMAINED ON, SECONDARY RIGHT MAIN GEAR LIGHT ON FO'S PANEL REMAINED ON. ALL INDICATIONS WERE NORMAL WITH GEAR DOWN. AIRCRAFT RETURNED TO Aug 7, 2007 · N898AA · Boeing 727223 · Landing Gear Position and WarningSDR CA070813002Pitot Tube · blocked(CAN) THE AIRCRAFT BEGAN TO DEPART ON THE TAKE-OFF ROLL WHEN THE FLIGHT CREW OBSERVED THAT THE CAPTAINS AIRSPEED INDICATION HAD FAILED. THE TAKE-OFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE WITH NO ADDITIONAL PROBLEMS. UPON INSPECTION OF THE CAPTAINS Jul 30, 2007 · Boeing 727223 · Pitot/Static SystemSDR DHL2007753001Skin · delaminatedSMALL AREA OF DELAMINATION ON RT I/B MID FLAP T/E. CUT OUT DELAMINATED AREA ON RT I/B MID FLAP, APPROX 4 1/4" BY 5". FABBED FILLER APPROX 4 1/4" BY 5" AND DOUBLER APPROX 3" BY 4 1/4" FROM 7075-T6 .016" PO NR 9003988. CLEANED, PREPPED, PRIMED, BONDED, CLEANJul 15, 2007 · N753DH · Boeing 727223 · Trailing Edge FlapsSDR DHL2007753500Structure · chafedRIGHT WING INBD FORE FLAP HAS O/B OF L/E DEEP CHAFE. REMOVED RT INBD FORE FLAP TO FOM IAW B727 MM 27-51-1. CUT OUT DAMAGED AREA I/B FORE FLAP R/WING. DIM CUT OUT 3/4" BY 3/4" AS REQUIRED IAW B727 SRM 57-50-4 FIG 1. FABBED DOUBLER REPAIR FROM P/N 2024-T3 .Jul 14, 2007 · N753DH · Boeing 727223 · Trailing Edge FlapsSDR DHLA200700022Compressor · stalledREJECTED TAKEOFF AT APPROX 20 KNOTS DUE TO AN AUTOPACK TRIP AND AN APPARENT COMPRESSOR STALL.Apr 18, 2007 · N754DH · Boeing 727223 · Turbine Engine Compressor SectionSDR DHLA200700023Compressor · stalledDEPARTING RNWY 22R AT ILN, NR 2 ENG COMPRESSOR STALL OCCURRED AT AN EPR OF 2.05. WIND WERE 290DEG AT 14 GUSTING TO 26 (70DEG X-WIND) IAS -0, OAT - 13DEG, PA - 1077 A/C GW 178.8. FOR INFORMATION ONLY. INSPECTED INLET AND EXHAUST OF NR 2 ENG PER AOM CHPT 1.8 PApr 4, 2007 · N754DH · Boeing 727223 · Turbine Engine Compressor SectionSDR ASTAR20070014Switch · out of adjustWHEN THRUST LEVERS WERE BEING ADVANCED FOR T/O NR 3 ENG THRUST REVERSER LIGHT ILLUMINATED. REJECTED T/O AT ABOUT 20 KTS. PERFORMED RTO CHECKLIST AND ABNORMAL PROCEDURE. NORMAL OPERATION RESTORED. ADJUSTED NR 3 THRUST REV OPERATING LIGHT SWITCH IAW B727 MM Mar 21, 2007 · N752DH · Boeing 727223 · Engine Thrust ReverserSDR C8GA20070004Gearbox · leakingFLT 715 FROM HRL TO MEM. DURING CRUISE OPERATION NR 2 LOW OIL PSI LIGHT ILLUMINATED FOLLOWED BY A DECREASE IN OIL PSI AND OIL QUANTITY. PERFORMED APPROPRIATE CHECKLIST AND SHUT DOWN NR 2 ENGINE. AIRCRAFT DIVERTED TO IAH WHERE IT LANDED WITHOUT INCIDENT. POSMar 20, 2007 · N708AA · Boeing 727223 · Turbine Engine Accessory DriveSDR DHL2007780003Unknown · unknownRTO INFO 146800 LBS 80 KTS -11C, PA 1077, NORMAL AT 80 KTS, HEARD A THUMP, SAW A FLASH, ENG FAIL LIGHTS ILLUMINATED, AUTO PACK TRIP ACTIVATED. TAKEOFF WAS REJECTED. INSPECTED ENG INLET/ C-1. NO DAMAGE NOTED. SUSPECT X-WIND COND 24 KTS NOTED, PER AOM CH 1 8Feb 14, 2007 · N780DH · Boeing 727223 · Engine (Turbine/Turboprop)SDR CA070213003Contact · burned(CAN) DURING CLIMB OUT ALL 4 CB`S POPPED FOR TANK 2 FUEL BOOST PUMPS, AIRCRAFT RETURNED TO AIRPORT. DETERMINED NR 3 GENERATOR VOLTAGE FLUCTUATING, (THE PUMP FAULT WAS ATTRIBUTED TO THE POWER FLUCTUATION WHICH WAS POWERING THE (ESSENTIAL POWER) AND THE (SYNC BUFeb 6, 2007 · Boeing 727223 · Electrical Power System WiringSDR DHL2006780134Skin · crackedVERTICAL STAB, LWR RUDDER HAS DENT CLUSTER NEAR L/E AFT OF RUDDER HINGELINE, FIN STA 110.4. NDT INSP REVEALED CRACKS IN DENTS. REMOVED AND FABRICATED NEW DOUBLER REPAIR FROM 301 1/2 HARD CRES, .025" BY 23" BY 12", PO NR 9003982, PER B727 SRM 55-40-3 FIG 1. Dec 3, 2006 · N780DH · Boeing 727223 · Rudder, Plate/SkinSDR DHL2006780133Stringer · corrodedFWD CARGO COMPT, CORROSION ON STRINGER 28L AT BS 580. CUT OUT DAMAGED AREA APPROX 16.25" LONG PER B727 SRM 53-10-3 FIG 1. FABRICATED REPAIR SPLICE FROM BAC1498-132, 8.063" LONG, 2 PO NR 9003866, AND FILLER FROM BAC1498-138, 16.25" LONG, PO NR 6260178, PER B7Dec 3, 2006 · N780DH · Boeing 727223 · Fuselage Main, Longeron/StringerSDR DHL2006780132Skin · corrodedFWD CARGO COMPT, BS 700 HAS SKIN CORRODED BETWEEN STR 26R AND 27R. CORROSION FOUND OUT OF LIMITS PER B727 SRM 53-30-1 FIG 1. CUT OUT DAMAGED AREA APPROX 9.5" BY 5", FABRICATED: REPAIR DOUBLER FROM 2024-T3, .071" BY 14.5" BY 16", PO NR 9004067; TRIPLER FROM Dec 3, 2006 · N780DH · Boeing 727223 · Fuselage Main, Plate/SkinSDR DHL2006780131Frame · corrodedCORROSION ON FRAME LWR FLANGE AFT SIDE BS 990, STR 29L TO 29R. BLENDED, CORROSION OUT OF LIMITS IN 2 AREAS PER B727 SRM 53-30-1. CUT OUT DAMAGED AREA OF FRAME AND FABRICATED SHEAR TIE REPAIR DOUBLERS, 2, FROM 7075-T0, .063" BY 3" BY 4" AND .063" BY 3" BY 4.5Dec 3, 2006 · N780DH · Boeing 727223 · Fuselage Main, FrameSDR DHL2006780130Door Frame · corrodedE/E DOOR SURROUND AFT FRAME CORRODED, BS 450, BL 0. CORROSION AT AFT FRAME OUT OF LIMITS PER B727 SRM 51-10-6 AND 53-30-1 FIG 1. REMOVED AND FABRICATED NEW FRAME SECTION (FROM SAMPLE) FROM 7075-TO, .040", PO NR 9003849, PER B727 SRM 53-10-2. HEAT TREATED TODec 3, 2006 · N780DH · Boeing 727223 · Fuselage Main, StructureSDR DHL2006780129Skin · corrodedAFT CARGO COMPT, BS 950F, STR 28L, SKIN HAS EXFOLIATING CORROSION ON SKIN. CORROSION ON SKIN AND STR 28L FOUND OUT OF LIMITS PER B727 SRM 53-30-1 FIG 1 AND 53-30-3 FIG 3. CUT OUT DAMAGED SKIN, 8.25" BY 3.25", AND CUT OUT DAMAGED STR, 14" LONG, IAW B727 SRM 5Dec 3, 2006 · N780DH · Boeing 727223 · Fuselage Main, Plate/SkinSDR DHL2006780127Spar · damagedLT HORIZ STAB HAS 1 DAMAGED SCREW HOLES AT STAB STA 172 APPROX. CUT OUT DAMAGED AREA, 3 PLACES AT 9.75" BY 1" BY 1", PER B727 SRM 55-10-5 FIG 1. FABBED REPAIR ANGLE FROM 7075-T6, .080" BY 9' BY 1" BY 1.75", PO NR 9003505, PER B727 SRM 55-10-5 FIG 1. TREATEDDec 1, 2006 · N780DH · Boeing 727223 · Horizontal Stabilizer, Spar/RibSDR DHL2006780126Stringer · corrodedFWD CARGO COMPT, CORROSION ON STRINGER, BS 510, STR 28L. CORROSION OUT OF LIMITS: REMOVED STR 28L FROM BS 480 TO 515 PER B727 SRM 51-30-2 AND 53-10-1. FABRICATE: STRINGER SECT FROM BAC1498-138, 34" LONG, FOR BS 450-480, PO NR 6260178; STRINGER SECT FROM P/Dec 1, 2006 · N780DH · Boeing 727223 · Fuselage Main, Longeron/StringerSDR DHL2006780125Fillet · gougedRT WING L/E UPPER SECTION SLAT AREA DAMAGED FILLET, RWS 652. BLENDED OUT SHARP EDGES. FABRICATED REPAIR DOUBLER FROM 2024-T3, .125" BY 3.5" BY 7.5", PO NR 9003898 IAW B727 SRM 57-50-3 FIG 10. TREATED, PRIMED, AND INSTALLED DOUBLER PER B727 SRM 57-50-3 FIG 1Dec 1, 2006 · N780DH · Boeing 727223 · Leading Edge DevicesSDR DHL2006780124Spar · corrodedLT HORIZ STAB, LOWER AFT SPAR 75 PERCENT CHORD HAS CORROSION AT LWR FLANGE, LSTAB STA 168. REMOVED CORROSION ON 75 PERCENT CHORD LWR FLANGE AT LSTAB STA 168, MATERIAL LOSS OUT OF LIMITS PER B727 SRM 55-10-1 FIG 1 AND 55-10-2 FIG 2. CUT OUT AFFECTED AREA, APPNov 30, 2006 · N780DH · Boeing 727223 · Horizontal Stabilizer, Spar/RibSDR DHL2006780123Stringer · corrodedAFT CARGO COMPT, CORROSION ON STRINGER AND ADJACENT SKIN AT BS 1010, STR 28L. REMOVED EXISTING STR SPLICE AND REMOVED CORROSION ON SKIN PER B727 SRM 51-10-6. MATERIAL REMOVED, .010", REMAINING, .116", ORIGINAL MATERIAL THICKNESS, .126", WITHIN LIMITS PER B72Nov 30, 2006 · N780DH · Boeing 727223 · Fuselage Main, Longeron/StringerSDR DHL2006780121Seat Track · corrodedCABIN SEAT TRACK BS 830, LBL 45 HAS CORROSION AND IS GOUGED AS MARKED. REMOVED SEAT TRACK SECTION FROM BS 747.45 TO BS 852.95, LBL 45 AND FABRICATED NEW SEAT TRACK FROM BAC1520-841, 95" LONG, PO NR 9004051 IAW B727 SRM 53-10-2 FIG 7, 51-30-5, AND 51-30-2. TRNov 30, 2006 · N780DH · Boeing 727223 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2006780122Frame · corrodedAFT CARGO COMPT, CORROSION ON FRAME BS 950F, STR 28L. CUT OUT DAMAGED AREA APPROX 2" BY 1.5", AND FABRICATED REPAIR ANGLE FROM 7075-T6, .040" BY 4.25" BY 3", PO NR 634724, PER B727 SRM 51-40-3 FIG 1 AND 53-10-2 FIG 5. TREATED, PRIMED, AND INSTALLED REPAIR ANNov 30, 2006 · N780DH · Boeing 727223 · Fuselage Main, FrameSDR DHL2006780221Seat Track · corrodedCABIN SEAT TRACK BS 830, LBL 45 HAS CORROSION AND IS GOUGED AS MARKED. REMOVED SEAT TRACK SECTION FROM BS 747.45 TO BS 852.95, LBL 45 AND FABRICATED NEW SEAT TRACK FROM BAC1520-841, 95" LONG, PO NR 9004051 IAW B727 SRM 53-10-2 FIG 7, 51-30-5, AND 51-30-2. TRNov 30, 2006 · N780DH · Boeing 727223 · Fuselage, Seat/Cargo Attach FittingsSDR CA061218013Switch · malfunctioned(CAN) NOSE GEAR GREEN LIGHT DID NOT ILLUMINATE WITH LANDING GEAR SELECTED DOWN. VISUALLY INSPECTED TO ENSURE NOSE GEAR WAS DOWN AND LOCKED THROUGH VIEWPORT AND CONFORMED NOSE GEAR WAS DOWN AND LOCKED. AS A PRECAUTIONARY ACTION NOSE GEAR LOCK SWITCH REMOVED ANov 29, 2006 · Boeing 727223 · Landing Gear Position and WarningSDR DHL2006752004Smoke Detector · malfunctionedNR 5 CARGO SMOKE DETECTOR ILLUMINATED IN FLIGHT. REMOVED AND REPLACED NR 5 SMOKE DETECTOR. OPS CK OF SMOKE DETECTOR SYS CKS GOOD IAW MM 26-13-00, NO EVIDENCE OF FIRE DETECTED.Nov 29, 2006 · N752DH · Boeing 727223 · Smoke DetectionSDR DHL2006780117Skin · corrodedAFT CARGO COMPT, CORROSION ON SKIN BS 1025 OUTBOARD OF STR 29L. REMOVED CORROSION AS REQ AT BS 1025, MATERIAL LOSS EXCEEDS LIMITS PER B727 SRM 53-30-1 FIG 1. CUT OUT DAMAGED AREA, DIM 1.5" BY 1" IAW B727 SRM 53-30-3 FIG 1. FABRICATED DOUBLER FROM 2024-T3, .Nov 28, 2006 · N780DH · Boeing 727223 · Fuselage Main, Plate/SkinSDR CA061219003Disc · detached(CAN) WHILE TOWING AIRCRAFT TO LINE IT WAS REPORTED THAT NR 1 BRAKE WAS TRYING TO LOCK UP. UPON REMOVAL OF BRAKE ASSEMBLY THE DISC RING WAS FOUND DETACHED FROM THE ASSEMBLY. A RIVET WAS FOUND SHEARED AND THE DISC RING CAME APART. FURTHER TO FOLLOW AFTER STRIPNov 22, 2006 · Boeing 727223 · BrakeSDR CA061120009Duct · ruptured(CAN) ENROUTE TO DESTINATION, #2 ENGINE FIRE WARNING. CHECKLIST ACCOMPLISHED, ENGINE SHUTDOWN. 13TH STAGE SADDLE DUCT FOUND RUPTURED, REPLACED AND AIRCRAFT RETURNED TO SERVICE. (TC# 20061120009)Nov 18, 2006 · Boeing 727223 · Turbine Engine Compressor SectionSDR CA061219002Window · cracked(CAN) DURING SERVICING THE L4 WINDOW WAS FOUND CRACKED. WINDOW REPLACED IAW MM 56-11-31, FUNCTION CHECKED SERVICEABLE WITH NO FURTHER FAULTS REPORTED. (TC NR 20061219002)Nov 16, 2006 · Boeing 727223 · Flight Compartment WindowsSDR DHL2006780118Structure · dentedLEFT INBD AFT FLAP IS DENTED INBD OF INBD ACTUATOR ROD. REMOVED DAMAGED AREA FROM LT INBD AFT FLAP 1/4" AREA IAW B727 SRM 57-50-4. FAB PART 2024-0 .050 6" BY 12" PO NR 9003505 IAW B727 SRM 57-50-4 AND HEAT TREATED TO 2024T4 IAW FLIGHTSTAR A/C SERV ER# 2-3715Nov 14, 2006 · N780DH · Boeing 727223 · Trailing Edge FlapsSDR DHL2006780120Seat Track · gougedCABIN SEAT TRACK BS 520 RBL 45 HAS DEEP GOUGE (AREA MARKED). BLENDED OUT GOUGE AT CABIN SEAT TRACK BS 520 RBL 45 PER B727 SRM 51-10-6, MAT LOSS .063, ORIGINAL THICKNESS .800, MAT REMAINING .737 AREA FOUND BEYOND LIMITS. REMOVED FLOOR ROW E AND F BS 420-720A Nov 13, 2006 · N780DH · Boeing 727223 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2006780119Skin · delaminatedLEFT WING I/B MID FLAP IS DELAMINATED AT TE LOWER SURFACE. REMOVED DELAMINATED AREA APPROX 7" BY 4.2". FAB FILLER APPROX 7" BY 4.2", FILLERS (2EA) 3" BY 4.2" AND STRAP 1" BY 4.4" FROM 7075T6 .016 PO NR 526029, ALODINED AND PRIMED REPAIR PARTS AND AREA TO BE Nov 13, 2006 · N780DH · Boeing 727223 · Trailing Edge FlapsSDR DHL2006780114Skin · delaminatedLEFT WING, INBD FORE FLAP, UPPER SURFACE, INBD SIDE DELAMINATED. CUTOUT DELAMINATED SKIN AND HONEYCOMB CORE APPROX 2.5 BY 8. FABRICATED FILLER APPROX 2.5" BY 8" AND DOUBLER APPROX 4 BY 9.5 FROM P/N 2024-T3, .016, PO NR 9003189 AND HONEYCOMB P/N 3.1 3/16 5052Nov 13, 2006 · N780DH · Boeing 727223 · Trailing Edge Flaps
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