Boeing 727-2Q9

Service difficulty reports · 830

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  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = '7272Q9'
  ORDER BY difficulty_date DESC"

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SDR DHL2001740003Warning Light · illuminatedUPON NR 1 ENGINE STARTUP UNDER EXCITED SYSTEM NR 1, LIGHT ILLUMINATED ON S/O AUX PANEL. DEFERRED PER MEL 24-1. DMI 4988 PLACARD INSTALLED. SP C/W. STATUS-OPEN.Apr 3, 2001 · N740DH · Boeing 7272Q9 · Central WarningSDR DHL2001740002Doubler · looseNR 19. LT WING TOP AILERON REPAIR IS COMING LOOSE FWD. AND INBD NR 7 SPOILER(DOT) RII CORRECTIVE ACTION: ACOMPLISHED REPAIR IAW AERONAUTICAL SOLUTIONS REPORT 00-003 IR 03-26-01 AND SRM 51-30-02.SEE ITEM 9M FOR REPLACEMENT INSTRUCTIONS. INTERIM REPAIR INSTALLEDMar 25, 2001 · N740DH · Boeing 7272Q9 · AileronsSDR DHL2001740001Indicator · malfunctionedS.O. ELEC. ANNUNCE. PANEL HAS OVEREXITED AND UNDEREXITED SYS. 1, LIGHTS ILLUMINATED WHEN RESET BUTTON IS PUSHED THE LIGHT EXTINGUISH AND THE LIGHT FOR NR 2 DIFF. FAULT LIGHT ILLUMINATES. WHEN RESET BUTTON IS RELEASED AND THE SAME NR 1 SYS.LIGHTS RE-ILLUMINATEMar 23, 2001 · N740DH · Boeing 7272Q9 · Central WarningSDR DHL2001741518Stop Fitting · damagedC2 CARGO DOOR FRAME LOWER AFT DOOR STOP HAS A CRACK INDICATION. REMOVED LOWER AFT DOOR STOP AND FASTENERS OF SEAL RETAINERS FOR S/M ACCESS AS PER B727SRM 51-30-2. PERFORMED HFEC INSP PER B727NDT MANUAL PART 6 51-00-00 FIG 4 NO CRACK INDICATION FOUND. FABRICMar 19, 2001 · N741DH · Boeing 7272Q9 · Fuselage Main, StructureSDR DHL2001741511Spar · corrodedRIGHT WING, LOWER SPAR HAS EXFOLIATED CORROSION UNDER CAVITY CUTOUT FOR NR 8 LEADING EDGE SLATACTUATOR. REMOVED L/E ACCESS PANELS 6542; 6543 6546 AND 6540 AT RIGHT WING LOWER SURFACEAS PER B727 SRM 51-30-2. REMOVED FUEL ACCESS PANELS AT RT WING LOWER SURFACMar 19, 2001 · N741DH · Boeing 7272Q9 · Wing SparSDR DHL2001741515Skin · crackedNR 3 ENGINE UPPER COWL O/B AFT CORNER SKIN AND ATTACH SUPPORT FOR RUB SEAL RETAINER ARE GOUGED AND CRACKED. STOP DRILLED CRACKS PER B727 SRM 51-10-1 ON THE NR 3 ENGINE UPPER COWL O/B AFT CORNER SKIN. PERFORMED HFEC INSP PER B727 NDT MANUAL PART 6-51-00-00 FIMar 15, 2001 · N741DH · Boeing 7272Q9 · Engine Cowling SystemSDR DHA2001741513Skin · crackedNR 1 ENG UPPER COWL OUTER SKIN DAMAGED AT 3RD LATCH CUTOUT FROM OUTBOARD FWD SIDE. REMOVED LOWER ROW OF FASTENERS AND STOP DRILL CRACK AS PER SRM 51-10-1 (COWL SKIN) NR 1 ENG 0.50, FABRICATED DOUBLER AS PER SRM 54-10-3 MATERIAL 7075-T6 ML 207155, INSTALLED DOMar 15, 2001 · N741DH · Boeing 7272Q9 · Engine Cowling SystemSDR DHL2001741514Attach Angle · crackedNR 3 ENGINE LOWER COWL LEFT I/B SIDE FWD NR 1 LATCH CUTOUT ATTACH ANGLE CRACKED AT O/B RADIUS. REMOVED ATTACH ANGLE AT LEFT I/B SIDE FWD OF NR 1 LATCH CUTOUT AS PER B727 SRM 51-30-2. FABRICATE NEW ATTACH ANGLE AS PER B727 SRM 54-10-2 FIG 2. MAT USED 7075 -OMar 14, 2001 · N741DH · Boeing 7272Q9 · Engine Cowling SystemSDR DHL2001741505Fuel Tank · corrodedCORROSION AT CTR WING TANK LWR SURFACE, INSIDE RT A/C BAY PLENUM, APPROX BS 830. REMOVED FASTENERS FOR ACCESS AS PER B727 SRM 51-30-2. REMOVED RT PRIMARY AND SECONDARY HEAT EXCHANGER AND PLENUM ASSY FOR SM ACCESS B727 MM 21-50-21. REMOVED CORROSION AT CTR WMar 12, 2001 · N741DH · Boeing 7272Q9 · Fuel StorageSDR DHL2001741507Spar · corrodedRIGHT WING LOWER SPAR HAS EXFOLIATED CORROSION UNDER CAVITY CUT OUT FOR NR 8 LEADING EDGE SLAT ACTUATOR. REMOVE L/E ACCESS PANELS 6542, 6543, 6546, AND 6540 AT RIGHT WING LOWER SURFACE AS PER B727 SRM 51-30-2. REMOVED FUEL ACCESS PANELS 17, 18, 19 AT RIGHT WMar 10, 2001 · N741DH · Boeing 7272Q9 · Wing SparSDR DHL2001741501Skin · crackedNR 3 ENGINE UPPER COWL, O/B NR 4 LATCH CUTOUT IS CRACKED IN 2 CORNERS. CUT OUT DAMAGED AREA AT NR 3 ENG UPPER COWL O/B NR 4 LATCH CUT-OUT CRACK AS PER B727 SRM 54-10-3 FIG 5 MAT LOSS 1 X.5 INCH. REMOVED EXISTING REPAIR IAW B727 SRM 51-30-2. INSTALLED EXTERNMar 10, 2001 · N741DH · Boeing 7272Q9 · Engine Cowling SystemSDR DHL2001741517Floorboard · corrodedCORROSION ON FLOORBOARDS AND FLOOR SUPPORT STRUCTURE FROM FS STA 303 TO FS 344 AND FROM RBL 16 TO RBL 55 (UNDER FWD LAV). REMOVED CORROSION AS PER B727 SRM 51-10-6 MATERIAL LOSS .030 FOUND OUT OF LIMITS AS PER B727 SRM 53-30-1. REPLACED FLOORBOARDS SUPPORT PMar 9, 2001 · N741DH · Boeing 7272Q9 · Fuselage Floor PanelSDR DHL2001741516Floor Support · corrodedFWD LAV COMPARTMENT FLOOR SUPPORT CORRODED IN SEVERAL AREAS AND AROUND NUT PLATES (BLUE WATER STAINS). REMOVED CORROSION AS PER B727 SRM 51-10-6. MATERIAL LOSS .030 FOUND OUT OF LIMITS AS PER B727 SRM 53-30-1. CUT OUT DAMAGED AREA ON FLOORBEAM AT BS 312RBL 3Mar 9, 2001 · N741DH · Boeing 7272Q9 · Fuselage Miscellaneous StructureSDR DHL2001741506Skin · delaminatedRT I/B MID FLAP UPPER SURFACE DELAMINATED AREA AT I/B TRAILING EDGE AREA (MKD). INSTALLED BOND REPAIR TO I/B MID FLAP UPPER SURFACE AT I/B TRAILING EDGE AREA AS PER B727 SRM 51-40-6 PAGE 7 MATERIAL USED ADHESIVE AF 163-2K 085 PO 2429 AND ALUMINUM 7075-T6 016 Mar 9, 2001 · N741DH · Boeing 7272Q9 · Trailing Edge FlapsSDR DHL2001741502Floorboard · corrodedCORROSION ON AND FLOOR SUPPORT STRUCTURE FROM FS STA 303 TO FS 344 AND FROM RBL 16 TO RBL 55 (UNDER FWD LAV). REMOVED CORROSION AS PER B727 SRM 51-10-6 MATERIAL LOSS .030 FOUND OUT OF LIMITS AS PER B727 SRM 53-30-01. REPLACED FLOORBOARDS SUPPORT PO 8B12244 LMar 9, 2001 · N741DH · Boeing 7272Q9 · Fuselage Floor PanelSDR DHL2001741500Skin · crackedNR 1 ENGINE NOSE COWL EXTERNAL SKIN HAS CRACK BETWEEN TWO FASTENERS EXTENDING INTO EXISTING DOUBLER REPAIR 9:00 POSITION NACELLE STA 80. REMOVED EXISTING DOUBLER REPAIR PER 727 SRM 57-30-2. CUT OUT ACCESS HOLE 8 INCHES DIA PER SRM 54-30-3 FIG 3. CUT OUT DELMar 9, 2001 · N741DH · Boeing 7272Q9 · Engine Cowling SystemSDR DHL2001741510Fuel Tank · corrodedCORROSION AT CTR WING TANK LOWER SURFACE, INSIDE RT A/C BAY PLENUM, APPROX BS 830. REMOVED FASTENERS FOR ACCESS AS PER B 727 SRM 51-30-2. REMOVED RT PRIMARY 7 SECONDARY HEAT EXCHANGER AND PLENUM ASY FOR S/M ACCESS B 727 MM 21-50-2. REMOVED CORROSION AT CENTMar 8, 2001 · N741DH · Boeing 7272Q9 · Fuel StorageSDR DHL2001741508Support Bracket · corrodedLT WING NR 7 SPOILER HINGE SUPPORT ROD IS LOOSE AND CORRODING AT LOWER ATTACH TO LOWER COVER PANEL SUPPORT RIB. REMOVED LOWER ATTACH SUPPORT BRACKET AT LEFT WING NR 7 SPOILER OUTBOARD HINGE SUPPORT ROD AS PER B727 SRM 51-30-2. FABRICATE NEW SUPPORT BRACKET AMar 8, 2001 · N741DH · Boeing 7272Q9 · SpoilersSDR DHL2001741504Web · corrodedCABIN FLOOR WEB CORRODED AT SEVERAL AREAS FROM STA 1183 TO 1148 LBL 24 TO LBL 62. CUT OUT DAMAGED AREAS AT CABIN FLOOR WEB STA 1183 TO 1148 LBL 24 TO LBL 62 IN SEVERAL SECTIONS IAW B727 SRM 51-40-2 FIG 1 MAT USING 2024-T3 .063 10 X 38 INCHES PO 83110575 LOT 8Mar 8, 2001 · N741DH · Boeing 7272Q9 · Fuselage Miscellaneous StructureSDR DHL2001741503Floor Support · crackedCABIN FLOOR SUPPORT STA 743 LBL 24.75 TO 45.5 HAS A CRACK. REMOVED AND REPLACED MED STRAP-FLOOR SUPPORT STA 743 LBL 24.75 TO 45.5. MAT USED 7075T6 .040 PO 8311935 LOT 219081 SIZE 16.5 X 2 INCHES AS PER B 727 SRM 51-20-2. TREATED, ALODINED AND PRIMER AS PER BMar 8, 2001 · N741DH · Boeing 7272Q9 · Fuselage Miscellaneous StructureSDR DHA2001741512Web · corrodedCABIN FLOOR WEB 1183 TO 1166 RBL 24 TO 45 HAS SEVERAL ELONGATED HOLES AND CORROSION AT FASTENERS. CUT OUT DAMAGED AREA AT CABIN FLOOR WEB STA 1183 TO STA 1166 RBL 24 TO 45 IN SEVERAL SECTIONS IAW B727 SRM 51-40-2. INSTALLED DOUBLER REPAIR AT CABIN FLOOR WEB Mar 7, 2001 · N741DH · Boeing 7272Q9 · Fuselage Miscellaneous StructureSDR DHL2001741509Panel · crackedNR 3 L/E SLAT ACTUATOR ROD END ATTACH AREA ADJACENT PANEL CRACKED. REMOVED INTERNAL PANEL AT NR 3 L/E SLOT ACTUATOR AS PER B 727 SRM 51-30-2. ROUTE OUT CRACK AS PER B 727 SRM 51-10-1, MAT LOSS .010. INSTALLED DOUBLER REPAIR AS PER B 727 SRM 51-40 2 FIG AT. Mar 7, 2001 · N741DH · Boeing 7272Q9 · Leading Edge DevicesSDR DHL2001741003Indicator · malfunctionedF/O AIRSPEED INDICATOR GOT MACH AND UMO FLAGS IN VIEW DURING TAXI-OUT. UMO FLAG IN VIEW ON F/O MACH A/S INDICATOR NR 2 MACH A/S AURAL WARNING WOULD NOT TEST. UMO FLAG MOVED TO ITEM 2M, MACH FLAG DEF PER MEL 34-3-2 CTRL NR 4287 CAT C PLA INSTALLED. SEE RESTRFeb 6, 2001 · N741DH · Boeing 7272Q9 · High Speed WarningSDR DHL2001740C14Attach Angle · corrodedNR 5 L/E SLAT I/B TRACK ROLLER SUPPORT O/B VERTICAL ATTACH ANGLE HAS CORROSION AT LOWER SPAR. INSTALLED NEW VERTICAL ATTACH ANGLE PER B727 SRM 57-10-2 AND 51-30-2.Jan 25, 2001 · N740DH · Boeing 7272Q9 · Leading Edge DevicesSDR DHL2001740C20Angle · corrodedLEFT WING FRONT SPAR LOWER CHORD ANGLE LOWER SECTION WHERE L/E PANELS ATTACH, CORROSION ON TWO SECTIONS APPROX BETWEEN WS 383.0 AND 477.0. FABRICATED AND INSTALLED REPAIR PLATE 18.375 X 2.875 INCHES. INSTALLED PER AVITAS EO AVHM-0186 RO-1FORM 337 FILED BY AVJan 24, 2001 · N740DH · Boeing 7272Q9 · Wing SparSDR DHL2001740C23Panel · bulgedEXTERIOR LOWER FUSELAGE, PANEL 3420 BULGE. INSTALLED NEW SKIN FUSELAGE PANEL NR 3420 PER B727 SRM 53-50-1 AND 51-30-2. SIZE OF MATERIAL USED 19.25 X 20.25 INCHES.Jan 18, 2001 · N740DH · Boeing 7272Q9 · Fuselage Main, Plate/SkinSDR DHL2001740C22Structure · gougedLEFT WING INBOARD FORE FLAP OUTBOARD END HAS DEEP GOUGE IN PREVIOUS REPAIR DOUBLER. INSTALLED DOUBLER PER B727 SRM 51-30-2. SIZE OF MATERIAL USED 5 X 6 INCHES.Jan 18, 2001 · N740DH · Boeing 7272Q9 · Leading Edge DevicesSDR DHL2001740C26Skin · tornMAIN CARGO DOOR CUTOUT FWD LOWER CORNER IS TORN BY DOOR SILL. REMOVED DOOR CUTOUT FWD LOWER CORNER SILL IAW B727SRM-51-30-2. FABRICATE AND INSTALLED NEW WEB AT MAIN CARGO DOOR FWD LOWER CUTOUT AS PER B727 SRM 53-10-2 FIG 5 AND 51-30-2. MAT USED 7075T6 .063 Jan 17, 2001 · N740DH · Boeing 7272Q9 · Fuselage Main, Plate/SkinSDR DHL2001740C24Angle · crackedFOUND SMALL CRACK LOCATED AT A/C BAY AREA RAM AIR DOORS UPPER OUTBOARD CORNER AT BS 720B. REMOVED AND REPLACED UPPER ANGLE AT BS 720B PER B727 SRM 51-10-1, 5110-2 AND 51-30-2. SIZE OF ANGLE 1.5 X 29 INCHES.Jan 17, 2001 · N740DH · Boeing 7272Q9 · Fuselage Miscellaneous StructureSDR DHL2001741002Gcu · failedNR 1 ENGINE GEN WOULD NOT COME ON LINE, NR 6B FAILS TO CLOSE. SWAPPED NR 1 AND APU GCU''S RAN ENG, SYS OPS GOOD PER M/M 24-20.Jan 17, 2001 · N741DH · Boeing 7272Q9 · AC Generation SystemSDR DHL2001740C27Floor Support · corrodedAFT CARGO STA 950A RBL 4 FLOOR SUPPORT ANGLE HAS CORROSION AND DOUBLE HOLES. ROUTED OUT CORROSION AND DOUBLE HOLES AT STA 950A FLOOR SUPPORT B727 SRM 51-40-4. INSTALLED ANGLE REPAIR AT FS 950A RBL 4 FLOOR SUPPORT AS PER B727 SRM 51-40-21, PO 8318692, LOT 747Jan 16, 2001 · N740DH · Boeing 7272Q9 · Fuselage Miscellaneous StructureSDR DHL2001740C28Bracket · crackedLEFT MLG W/W PARKING BRAKE SHUTTLE VALVE MOUNT BRACKET CRACKED AT STATION 930 AT KEEL BEAM. REMOVED VALVE FOR S/M REPAIR BRAKE IAW B727 M/M 32-40-0 LT TO W/W. REMOVED DAMAGED MOUNT BRACKET FOR LT MLG PARKING BRAKE SHUT OFF VALVE AND FABRICATED REPLACEMENT IAJan 16, 2001 · N740DH · Boeing 7272Q9 · Landing Gear Brake SystemSDR DHL2001740C08Floorbeam · corrodedAFT CARGO CROSS SECTION FLOOR ANGLE AT STA 950 HAS CORROSION AND TOO MANY DOUBLE HOLES. INSTALLED NEW ANGLE 50 X 4.75 INCHES PER B727 SRM53-10-2 AND 51-30-2.Jan 16, 2001 · N740DH · Boeing 7272Q9 · Fuselage Main, Floor BeamSDR DHL2001740C07Angle · chafedHYD COMP B-SYS SUPPORT FRAME AT FWD SIDE OF ENTRY ACCESS HAS 2 CHAFE HOLES. INSTALLED ANGLE PER B727 SRM 51-40-3 PG 3 SIZE OF MATERIAL 6 X 3 INCHES.Jan 16, 2001 · N740DH · Boeing 7272Q9 · Fuselage Miscellaneous StructureSDR DHL2001740C29Structure · corrodedFUS LOWER AREA, UPPER WALL OF AIR CONDITIONING RAM AIR PLENUM AT LT PRIMARY HEAT EXCHANGER AREA WITH SIGNS OF CORROSION (RED MARKS). REMOVED FASTENERS FOR S/M ACCESS AS PER B727 SRM 51-30-2. REMOVED CORROSION AT RAM AIR PLENUM LT LOWER EXTERNAL SKIN AS PER BJan 15, 2001 · N740DH · Boeing 7272Q9 · Fuselage Main, StructureSDR DHL2001740C21Skin · dentedLEFT WING INBOARD FORE FLAP HAS DENT AT CENTER ACCESS PANEL 8442 MAKING CONTACT WITH NR 6 SPOILER ACTUATOR ROD END. INSTALLED NEW ACCESS PANEL PER B727 SRM 51-30-2. SIZE OF REPAIR 8 X 8 INCHES.Jan 15, 2001 · N740DH · Boeing 7272Q9 · Leading Edge DevicesSDR DHL2001740C17Skin · splitRIGHT WING OUTBOARD FLAP AFT FLAP T/E SPLITTING. INSTALLED BOND REPAIR PER B727 SRM 51-40-6. SIZE OF REPAIR 10 X 4 INCHES.Jan 15, 2001 · N740DH · Boeing 7272Q9 · Trailing Edge FlapsSDR DHL2001740C12Skin · crackedRIGHT WING TIP ASSY FWD INBOARD TOP CORNER HAS CRACKS. FABRICATE REPAIR PER B727 SRM 57-20-5, MATERIAL LOSS 4 X 2.5 INCHES.Jan 14, 2001 · N740DH · Boeing 7272Q9 · Wing, Plate/SkinSDR DHL2001740C19Fairing · crackedNR 4 FLAP TRACK FWD FAIRING CRACKED IN 2 PLACES. REPAIRED TRACK FAIRING PER B727 SRM 51-30-2. SIZE OF MATERIAL 19 X 2 INCHES.Jan 11, 2001 · N740DH · Boeing 7272Q9 · Trailing Edge FlapsSDR DHL2001740C16Fairing · tornNR 5 FLAP TRACK MID FAIRING SKIN TORN AT FWD END. REPLACED SKIN AT NR 5 FLAP TRACK MIN FAIRING PER B727 SRM 51-30-2 AND 51-10-2. SIZE OF MATERIAL 13 X 6 INCHES.Jan 11, 2001 · N740DH · Boeing 7272Q9 · Trailing Edge FlapsSDR DHL2001740C15Fairing · crackedNR 5 FLAP TRACK FWD FAIRING CRACKED AND CHAFING AT SEVERAL SPOTS ALONG THE EDGE. REPAIRED PER B727 SRM 51-30-2. SIZE OF MATERIAL 13 X 1.5 INCHES.Jan 11, 2001 · N740DH · Boeing 7272Q9 · Trailing Edge FlapsSDR DHL2001740C11Floor Support · corrodedCORROSION UNDER SEALING TAPE AT LAVATORY AREA FWD FROM BS 304 TO 343. REPLACED ANGLE.Jan 11, 2001 · N740DH · Boeing 7272Q9 · Fuselage Miscellaneous StructureSDR DHL2001740C13Bracket · crackedREFUELING BAY ACCESS DOOR HOLD OPEN LINKAGE ATTACH BRACKET IS CRACKED. REPLACED BRACKET PER B727 SRM 51-10-2, MATERIAL USED 9 X 2 X 1 INCHES.Jan 10, 2001 · N740DH · Boeing 7272Q9 · Fluid Service DoorsSDR DHL2001740C25Skin · crackedAFT AIRSTAIRS CUTOUT EXTERNAL SKIN HAS A CRACK AT FWD CORNER. STOP DRILL CRACK AT AFT AIRSTAIRS CUTOUT EXTERNAL SKIN AS PER SRM 51-10-1. REMOVED FASTENERS FOR INSTALL DOUBLER AS PER SRM 51-30-2. INSP IAW B727NDT MANUAL PART 6-51-00-00 FIG 4, FOUND NO CRACKSJan 9, 2001 · N740DH · Boeing 7272Q9 · Fuselage Main, Plate/SkinSDR DHL2001740C18Fairing · crackedNR 4 FLAP TRACK CENTER FAIRING CRACKED AT PREVIOUS REPAIR. REPAIRED TRACK FAIRING PER B727 SRM 51-30-2. SIZE OF REPAIR 7 X 3 INCHES.Jan 9, 2001 · N740DH · Boeing 7272Q9 · Trailing Edge FlapsSDR DHL2001740C10Floor Support · corrodedFLOOR SUPPORT ANGLE IS CORRODED BETWEEN STA 312 AND 328 RBL-4. INSTALLED NEW T-ANGLE FLOOR SUPPORT. MATERIAL USED 20 INCHES.Jan 9, 2001 · N740DH · Boeing 7272Q9 · Fuselage Miscellaneous StructureSDR DHL2001740C09Floorboard · corrodedCORROSION ON LOWER SURFACE OF CABIN FLOOR AT FS 1166 LBL 52. FABRICATED AND INSTALLED NEW FLOOR BOARD PER B727 SRM 51-30-2. MATERIAL USED 18 X 68 INCHES.Jan 9, 2001 · N740DH · Boeing 7272Q9 · Fuselage Floor PanelSDR DHL2001741001Strut · underservicedON TAXI-OUT LOUD BANGING NOISE FROM NOSE WHEEL AREA ESPECIALLY WHEN TAXING OVER SMALL BUMPS. SERVICED NOSE STRUT WITH 5606 AND NITROGEN PER M/M CHPT 32Jan 9, 2001 · N741DH · Boeing 7272Q9 · Nose/Tail Landing Gear Strut/AxleSDR DHL2000740006Apu · fireAPU WOULD NOT SHUT DOWN. EVIDENCE OF SMOKE AND FIRE. DEFERRED AND INSPECTED. STATUS - OPEN. APU HAS 90 SECOND SHUT DOWN DELAY PER M/M CHAP 49.APU OPS NORMAL. FIRE AND SMOKE CONFIRMED APU EXHAUST. DMI 3365 WAS CLEARED ON LOG PAGE 216393.Dec 7, 2000 · N740DH · Boeing 7272Q9 · APU Core EngineSDR DHL200074006Switch · failedWHEN FLAPS WERE EXTENDED TO 5 DEG THE AMBER LIGHT ON THE FWD PANEL STAYED ON AND THE CHRISTMAS TREE VERIFIED THE NR 3 L/E FLAP WAS NOT EXTENDED. REMOVED AND REPLACED SWITCH AND ROD WITH BUSHINGS ON NR 3 L/E FLAP. CHECKED GOOD PER M/M 27-82-1.Sep 19, 2000 · N740DH · Boeing 7272Q9 · Leading Edge Slat Position Indicating System
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