Boeing 727-264

Service difficulty reports · 617

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  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = '727264'
  ORDER BY difficulty_date DESC"

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SDR DHL2008765013Skin · gougedDURING C CHECK, LT OUTBOARD FORE FLAP OUTBOARD LEADING EDGE REPAIR IS GOUGED 2 PLACES. REMOVED OLD DOUBLER REPAIR IAW SRM 51-30-2. FABRICATED NEW DOUBLER REPAIR IAW SRM 57-50-2 FIG 4. TREATED AND PRIMED NEW DOUBLER IAW SRM 51-10-2. INSTALLED NEW DOUBLER IAJan 15, 2008 · N765AT · Boeing 727264 · Trailing Edge FlapsSDR DHL2008765007Skin · dentedDURING C CHECK, RT WING WS 760 NR 8 SLAT UPPER SURFACE HAS A DENT AROUND FASTENER. EVALUATED AND FOUND DENT OUT OF LIMITS IAW SRM 57-50-1 FIG 2 DUE TO DENT BEING ON FASTENER. CUT OUT DAMAGED AREA DIMENSION 1.75" BY 1.125" IAW SRM 57-50-3 FIG 1. FABRICATED DJan 15, 2008 · N765AT · Boeing 727264 · Leading Edge DevicesSDR DHL2008765008Intercostal · crackedDURING C CHECK, AFT CARGO COMPARTMENT BS 950A + 19" INTERCOSTAL LBL 5" HAS FASTENERS POPPED AND METAL CRACKED. REMOVED INTERCOSTAL AT AFT CARGO PIT IAW SRM 51-30-2. FABRICATED NEW INTERCOSTAL IAW SRM 53-10-2 FIG 5 AND 51-20-1. LOCATED AND DRILLED NEW INTERCJan 12, 2008 · N765AT · Boeing 727264 · Fuselage Miscellaneous StructureSDR DHL2008765027Skin · crackedDURING C CHECK, NR 3 SPOILER NR 3 HINGE CUT OUT ON LT WING TRAILING EDGE IS CRACKED. STOP DRILLED CRACK 0.250 IAW SRM 51-10-1. FABRICATED DOUBLER REPAIR IAW SRM 51-20-1, 51-30-5 AND 57-30-4 FIG 10. ALODINED AND PRIMED DOUBLER AND AREA IAW SRM 51-10-2. INSTJan 11, 2008 · N765AT · Boeing 727264 · SpoilersSDR DHL2008765029Skin · crackedDURING C CHECK, NR 4 SPOILER NR 2 HINGE CUT OUT ON LT WING TRAILING EDGE CRACKED. STOP DRILLED CRACK DIAMETER 0.250 INCH AND FABRICATED REPAIR DOUBLER IAW SRM 51-10-1 AND 57-30-4 FIG 10, NDT CONFIRMED STOP DRILL END STOP CRACK IAW NDT MM CH 51-00-00 PART 6 FIJan 9, 2008 · N765AT · Boeing 727264 · SpoilersSDR DHL2008765028Skin · crackedDURING C CHECK, NR 4 SPOILER NR 3 HINGE CUT OUT ON LEFT WING TRAILING EDGE CRACKED. STOP DRILLED CRACK DIAMETER 0.250" IAW SRM 51-10-1 AND 57-30-4 FIG 10, NDT STOP DRILL CONFIRMED END OF CRACK IAW NDT MM CH 51-00-00 PART 6. FABRICATED REPAIR DOUBLER IAW SRM Jan 9, 2008 · N765AT · Boeing 727264 · SpoilersSDR DHL2008765019Stringer · crackedDURING C CHECK, VERTICAL STABILIZER NR 8 STRINGER CRACKED FIN STATION 133. REMOVED PREVIOUS REPAIR FROM AREA IAW SRM 51-30-2. FABRICATED 2 EACH REPAIR ANGLES IAW SRM 55-30-5 FIGURE 1 AND 55-30-2 FIGURE 2. HFEC VERIFIED CRACK TERMINATES IN FASTENER HOLE IAW Jan 9, 2008 · N765AT · Boeing 727264 · Vertical Stabilizer, Spar/RibSDR DHL2007763002Panel · delaminated7 BY 5 INCH AREA OF DELAMINATION ON PANEL JUST O/B OF NR 1 SPOILER. DELAMINATION LOCATED JUST ABOVE JACKSCREW GEAR BOX, PANEL NR 8155.Dec 18, 2007 · N763AT · Boeing 727264 · Wing, Plate/SkinSDR DHL2007765001Web · crackedA-8 CHECK REF N/R 054239 AFT AIRSTAIR AREA LT TORQUE BOX AT STA 1263 LWR LIGHTING HOLE SKIN HAS 1 INCH CRACK AT 11:00 POSITION. CUT OUT DAMAGED AREA AT AFT AIRSTAIRS AREA LT TORQUE BOX STA 1263 LWR LIGHTING HOLE SKIN DIMENSION 3/4" BY 1/4" IAW B727 SRM 51-40-Nov 24, 2007 · N765AT · Boeing 727264 · Fuselage Miscellaneous StructureSDR DHL2007763001Web · crackedA-6 CHECK, DISCREPANCY: AFT AIR STAIRS RT FWD LWR LIGHTING HOLE TORQUE BOX SKIN AREA IS CRACKED. ROUTED OUT CRACK IAW SRM 51-10-1 FABRICATED REPAIR DOUBLER FROM 7075-T6 .025 X 2 INCH X 4 INCH IAW SRM 51-40-2 AND 53-10-2, PN 9003505 ALODINED AND PRIMED IAW SRM Nov 10, 2007 · N763AT · Boeing 727264 · Fuselage Miscellaneous StructureSDR DHLA200700046Light · dislodgedFOUND UPPER EMERG EXIT LIGHT DISLODGED. RE INSTALLED UPPER EMERGENCY EXIT LIGHT PER MM 33-50-00.Sep 26, 2007 · N765AT · Boeing 727264 · Emergency LightingSDR DHLA200700048Pitot Tube · obstructedON TAKEOFF ACCELERATION AT 80 KTS NO AIRSPEED INDICATION ON F/O AIRSPEED. A/C WT 131.7 AS 90KTS 27 DEGREES C ALT 0 FT COMPLETE RTO FLOW CHART BRAKE ENERGY NORMAL RANGE RWY 18R MCO. FOUND FOREIGN OBJECT IN F/O PITOT TUBE REMOVED OBJECT PERFORMED PITOT STATICSep 15, 2007 · N751DH · Boeing 727264 · Pitot/Static SystemSDR DHLA200700041Light · looseEMERGENCY LIGHT ILLUMINATED ON TAKEOFF. FOUND COCKPIT EMERGENCY LIGHT ASSY LOOSE. RESECURED IN PLACE PERFORMED GROUND TEST IAW M/M33-50-01,TEST OKAug 31, 2007 · N765AT · Boeing 727264 · Emergency LightingSDR DHL2007751519Keelbeam · crackedLT FWD KEEL BEAM, BS 870, HAS A CRACK BETWEEN TWO FASTENERS. VERIFIED CRACK FROM BS 870 TO BS 873. GAINED ACCESS AS REQ, CUT OUT DAMAGED AREA 1.875" BY 1" PER SB B727-53-0208. FABRICATED REPAIR DOUBLER FROM 15.5 PH STEEL, .071" BY 8.5" BY 3.75", PO NR 65222Mar 20, 2007 · N751DH · Boeing 727264 · Fuselage Main, KeelSDR DHL2007751518Support Angle · corrodedINT E/E AT BS 300, ON RT CRAWLWAY HAS I/B CORRODED ON LOWER SURFACE (NLG TRUNNION SUPPORT). GAINED ACCESS, REMOVED CORROSION, WITH MATERIAL LOSS EXCEEDING LIMITS AS PER B727 SRM 53-10-1 (MAT REMOVED <.085"). REMOVED AND REPLACED RT MID CHORD ANGLE PER B727 SMar 20, 2007 · N751DH · Boeing 727264 · Fuselage Miscellaneous StructureSDR DHL2007751517Support Fitting · corrodedLT NLG TRUNNION FITTING AND LOWER CAP HAVE SURFACE CORROSION. REMOVED SURFACE CORROSION AT FITTING PER B727 SRM 53-40-1 FIG 2; ORIG BORE DIA 2.498", FINAL BORE DIA 2.587", REWORK WITHIN CONTINUED SERV LIMITS PER B727 SRM 53-40-1 FIG 2. REWORK SURFACE TREATEMar 20, 2007 · N751DH · Boeing 727264 · Fuselage, Landing Gear Attach FittingsSDR DHL2007751516Frame · corrodedAFT CARGO COMPT FRAME AT STA 950C IS CORRODED AT BOTTOM BETWEEN STR 29L AND 30L. CORROSION DMG EXCEEDS LIMITS PER B727 SRM 53-10-2 FIG 5. CUT OUT DAMAGE, FABRICATED SHEAR TIE REPAIR FROM 7075-T0, .080" BY 4.5" BY 1.5" BY 1", PO NR 9002619 PER B727 SRM 53-10-Mar 9, 2007 · N751DH · Boeing 727264 · Fuselage Main, FrameSDR DHL2007751515Frame · corrodedAFT CARGO COMPT FRAME AT STA 1148 IS CORRODED AT BOTTOM BETWEEN STR 29R AND 30R. CUT OUT DAMAGED AREA 4" BY 1" BY 1". FABRICATED REPAIR SHEAR TIE (.063" BY 4.875" BY 3.5" BY 1") AND SHIM (.063" BY 3.5" BY 1.2") FROM 7075-T6 PO NR 9004690; TREATED AND PRIMEDMar 9, 2007 · N751DH · Boeing 727264 · Fuselage Main, FrameSDR DHL2007751509Intercostal · corrodedIN "C" CHECK, AFT CARGO COMPT INTERCOSTAL BETWEEN STA 1050-1070 STR 27L CORRODED. REMOVED INTERCOSTAL UPPER ANGLE IAW B727 SRM 51-30-2. FAB NEW ANGLE IAW B727 SRM 53-10-2 USING 2024T3 .050 PO NR 9004174 DIM 19" BY 2" ALODINE AND PRIME PART IAW B727 IAW B727 Mar 4, 2007 · N751DH · Boeing 727264 · Fuselage Miscellaneous StructureSDR DHL2007751505Angle · crackedIN "C" CHECK, NOSE WW INSIDE LT UPPER PRESSURE PANEL ACCESS, "L" ANGLE IS CRACKED AT STA.259 LBL 12. REMOVED CRACKED ANGLE IAW B727 SRM 51-30-2. FAB NEW ANGLE FROM 2024T3 0.040 PO NR 9004539 DIM 6 1/2" BY 1"BY 1" IAW B727 SRM 53-10-2 FIG 1 AND 51-20-1. TREAMar 2, 2007 · N751DH · Boeing 727264 · Fuselage Miscellaneous StructureSDR DHL2007751504Angle · crackedIN "C" CHECK, NOSE WW INSIDE LT UPPER PRESSURE PANEL ACCESS "L" ANGLE IS CRACKED AT STA 258 LBL 6. REMOVED CRACKED ANGLE IAW B727 SRM 51-30-2. FAB NEW ANGLE FROM 2024T3 0.040 PO NR 9004539 DIM 10 1/4" BY 1"BY 1" IAW B727 SRM 53-10-2 FIG 1 AND 51-20-1. TREATMar 2, 2007 · N751DH · Boeing 727264 · Fuselage Miscellaneous StructureSDR DHL2007751511Frame · damagedFOUND INTERIOR E/E COMPARTMENT, BS 318, RBL 18-24, WL 160, LEVELING COMPOUND BLOWN UP AT FASTENERS BY FRAME WALKWAY BEAM INTERSECTION. REMOVED LEVELING COMPOUND FOR CORROSION EVAL IAW B727 SRM 51-10-6. CORROSION FOUND OUT OF LIMITS AT FRAME SHEAR TIE IAW B72Feb 28, 2007 · N751DH · Boeing 727264 · Fuselage Main, FrameSDR DHL2007751503Skin · dentedA/C IN "C" CHECK, NR 7 SLAT UPPER SKIN IS DENTED AT RIVET WS 601. REMOVED FASTENERS IN AFFECTED AREA IAW B727 SRM 51-30-2. CUTOUT DAMAGED AREA (DIM.1" BY 1") IAW B727 SRM 57-50-3 FIG 1. FAB REPAIR DOUBLER FROM 2024T3 0.080 PO NR 9004617 (DIM.5 1/4" BY 4 1/4Feb 28, 2007 · N751DH · Boeing 727264 · Leading Edge DevicesSDR DHL2007751510Skin · damagedIN "C", RT WING OB FORE FLAP UPPER SURFACE HAS 3" GOUGE, HITTING SCREWS ON SPOILERS, WS 575. CUT OUT GOUGED/DELAMINATED AREA ON RT OB FORE FLAP UPPER SURFACE APPROX 2" BY 4". FAB FILLER APPROX 2" BY 4" AND DOUBLER APPROX 6"BY 6 3/4" FROM 2024T3 .016 PO NR 90Feb 27, 2007 · N751DH · Boeing 727264 · Trailing Edge FlapsSDR DHL2007751513Frame · corrodedA/C IN "C" CHECK, AFT CARGO COMPT FRAME AT STA 950C IS CORRODED AT BOTTOM BETWEEN STR 29L-28L. REPLACED DAMAGED SHEAR TIE AT BS 950C BETWEEN STR 29L-28L. FABRICATED NEW PART 7075-0 .080 PO NR 9002619 IAW B727 SRM 53-10-4 FIG 15 AND 53-10-2 FIG 5. HEAT TREATFeb 26, 2007 · N751DH · Boeing 727264 · Fuselage Main, FrameSDR DHL2007751512Frame · puncturedIN "C" CHECK, AFT CARGO COMPT FRAME AT STA 1090 IS PUNCTURED IN UPPER FLANGE RADIUS ABOVE STR 27L. REMOVAL TRANSITION PANEL FOR ACCESS IAW B727 SRM 51-30-2, FAB FRAME REPAIR FROM 7075-0 .063 PO NR 9004384 DIM 8" BY 3 1/2"BY 1" BY 1" IAW B727 SRM 53-10-2 FIG 1Feb 26, 2007 · N751DH · Boeing 727264 · Fuselage Main, FrameSDR DHL2007751508Frame · dentedIN "C", FWD CARGO COMPT FRAME STA 660 HAS DEEP DENT AT UPPER FLANGE BETWEEN STR.23R-24R. CUT OUT DAMAGED AREA APPROX DIM 1 1/4" IAW B727 SRM 51-40-3. FAB DOUBLER REPAIR FROM 7075-0 .063 PO NR 9004384 APPROX DIM 13" IAW B727 SRM 51-40-3 PAGE 1 AND 3 AND SRM 5Feb 26, 2007 · N751DH · Boeing 727264 · Fuselage Main, FrameSDR DHL2007751507Frame · dentedIN "C" CHECK, FWD CARGO COMPT FRAME STA 700 HAS 3 DENTS AT UPPER FLANGE BETWEEN STR 24L-25L. CUT OUT DAMAGED AREA APPROX 1" BY 3/4" IAW B727 SRM 51-40-3 FIG 1. FAB REPAIR ANGLE FROM 7075-0 .063 PO NR 9004384 APPROX DIM 11.7" BY 4" IAW B727 SRM 51-40-3 FIG 1 Feb 26, 2007 · N751DH · Boeing 727264 · Fuselage Main, FrameSDR DHL2007751506Frame · dentedIN "C" CHECK, FWD CARGO COMPT FRAME STA 520 IS DENTED AT UPPER FLANGE ABOVE STR 24R. CUT OUT DAMAGED AREA APPROX DIM 1" BY 3/4" IAW B727 SRM 51-40-3 FIG 1. FAB REPAIR ANGLE FROM 7075-0 .050 PO NR 9004219 APPROX DIM 10 1/4" BY 3 1/4" IAW B727 SRM 51-40-3 FIG Feb 26, 2007 · N751DH · Boeing 727264 · Fuselage Main, FrameSDR DHL2007751502Frame · dentedWHILE IN "C" CHECK, FWD CARGO COMPT FRAME STA 500 IS DENTED IN TWO PLACES AT UPPER FLANGE BETWEEN STR 23R-24R. CUTOUT DAMAGED AREA AT FWD CARGO COMPT BS 500 BETWEEN STR 23R AND 24R APPROX DIM 1 1/2" BY 1" IAW B727 SRM 51-40-3 FIG 1. FAB REPAIR ANGLE FROM 707Feb 26, 2007 · N751DH · Boeing 727264 · Fuselage Main, FrameSDR DHL2007751501Frame · dentedWHILE IN "C" CHECK, AFT CARGO COMPT FRAME AT STA1050 IS DENTED BETWEEN STR 26L AND 27L IN THE UPPER FLANGE. CUTOUT DENTED AREA (DIM 7" BY 2 1/2" BY 1 1/2") IAW B727 SRM 51-40-3 FIG 1. FABRICATED FRAME REPAIR ANGLE FROM 7075-0 0.063 (D.7"X 2 1/2") PO NR 9004Feb 26, 2007 · N751DH · Boeing 727264 · Fuselage Main, FrameSDR DHL2006764003Light · inoperativeSECURITY CHECK COCKPIT EMERG EXIT LIGHT INOP. REMOVED AND REPLACED COCKPIT EMERG EXIT LIGHT ASSY IAW B727 M/M 33-50-101. OPS CHECK GOOD.Dec 18, 2006 · N764AT · Boeing 727264 · Emergency LightingSDR DHL2006751004Skin · dentedACFT SUSTAINED DAMAGE ON LEFT SIDE OF NOSE AT APPROX STA 230, BETWEEN STR 23L AND 25L. CUT OUT DAMAGED AREA, 6.25" BY 9.875". FABRICATED DOUBLER FROM 2024-T3, .071" BY 16.5" BY 14", PO NR 9004067, AND FILLER FROM 2024-T3, .063" BY 13.75" BY 15.5", PO NR 9004Dec 6, 2006 · N751DH · Boeing 727264 · Fuselage Main, Plate/SkinSDR DHL2006751003Rib · crackedLT SIDE FUSELAGE AT BS 233.8, AND STR 25L, SUPPORT RIB CRACKED. REMOVED AND FABRICATED SUPPORT RIB FROM 7075-T6, .050" BY 14" BY 5", PO NR 9003817, AND ANGLE FROM 7075-T6, .032" BY 1" BY 1" BY 14", PO NR 9004042, PER B727 SRM 53-10-2 FIG 1 AND 51-20-1 FIG 8. Dec 6, 2006 · N751DH · Boeing 727264 · Fuselage Main, StructureSDR DHL2006751001Skin · dentedACFT SUSTAINED DAMAGE ON LEFT SIDE OF NOSE AT APPROX BS 197, 8" ABOVE STR 25L. CUT OUT DAMAGED SECTION OF FUSE, 5.75" BY 2.25" AT BS 197. FABRICATED; DOUBLER FROM 2024-T3, .071" BY 11.5" BY 9.562", PO NR 9004067, AND FILLER FROM 2024-T3, .063" BY 12.5" BY 9Dec 6, 2006 · N751DH · Boeing 727264 · Fuselage Main, Plate/SkinSDR DHL2006751002Support Channel · bentLT SIDE FUSE AT BS 230, AND 8" ABOVE STR 25L, HORIZ "T" SUPPORT CHANNEL BENT (REF ASTAR LOG PG 119403, ITM 6M FOR CAUSE). REMOVED AND FABRICATED "T" SUPPORT, FROM BS 227.8 TO 259.5, FROM BAC1505-100360, 32" IN LENGTH, PO NR 6452255, PER B727 SRM 53-10-2 FIG 2Dec 6, 2006 · N751DH · Boeing 727264 · Fuselage Miscellaneous StructureSDR DHL2006763006Relay · failedEMERG LTS COME ON IN ARMED POS. REPLACED R-70 RELAY AND CHECK SERV PER B-727 M/M 33-50-101 P/N 9524-6508.Nov 26, 2006 · N763AT · Boeing 727264 · Emergency LightingSDR DHL2006763005Battery · dischargedFWD ENTRY DOOR EMERGENCY LIGHTS INOP. REPLACED BATTERIES P/N 37067-001 2 EA IAW B727 M/M 33-50-101. OPS CHECK SERVICEABLE.Nov 26, 2006 · N763AT · Boeing 727264 · Emergency LightingSDR DHL2006765004Brake Assy · noisyLEFT BRAKE MAKES NOISE WHEN DEPRESSED AND AIRCRAFT SHAKES. BLED LEFT MLG BRAKES PER B727 MM CH 32-41-00. OPS AND LEAK CHECK GOOD.Nov 1, 2006 · N765AT · Boeing 727264 · Landing Gear Brake SystemSDR DHL2006763004Coalescer Bag · dirtyVERY STRONG ODOR, LIKE BURNING OIL COMING FROM PACKS DURING T/O AND CLIMB, GOES AWAY AFTER APPROX 20 MIN. REMOVED AND CLEANED BOTH WATER SEPARATOR COALESCER SOCKS. OPS CHECK GOOD. NO ODOR NOTED IAW AMM 21-55-51.Oct 31, 2006 · N763AT · Boeing 727264 · Humidity Control SystemSDR DHL2006765003Indicator · failedNR 3 OIL PRESSURE WENT TO 100 PSI ON T/O ROLL. ABORTED T/O AT 10 KTS. REMOVED AND REPLACED NR 3 OIL PRESSURE IND IAW MM 79-32-00. OPS CHECK GOOD IAW JRH 5.2.Sep 22, 2006 · N765AT · Boeing 727264 · Engine Oil PressureSDR DHL2006764007Skin · damagedREF. ASTAR LOG PAGE 098862 ITEM 1P. BELT LOADER STRUCK A/C AFT OF FWD BELLY LEFT 17 INCH GASH. C/W ASTAR JC EA53100140-001-B REPAIR SKIN (FS680-690). ACCOMPLISHED ASTAR JC EA53100140-001-B WO 600017273 REPAIR SKIN (FS680-690) EXT. B727 AND DWG NR 53100140-001Sep 16, 2006 · N764AT · Boeing 727264 · Fuselage Main, Plate/SkinSDR DHL2006764004Skin · damagedCREASE IN SKIN STA 660 STR 26R-27R IAW ITEM 1P LP 098862. CUTOUT DAMAGE AREA DIM. 3 INCH X 1 INCH, FAB. DOUBLER MAT. USED 2024T3 .063 PO NR 9003898 DIM. 11.3750 INCH X 9.7500 INCH. FAB TRIPLER MAT USED 2024T3 .071 PO NR 9003866 DIM. 12.1250 INCH X 10 INCH. Sep 16, 2006 · N764AT · Boeing 727264 · Fuselage Main, Plate/SkinSDR DHL2006764006Web · damagedWEB DAMAGED BELOW STR 27R BETWEEN STA 680-700 REF. ITEM 1P LP 098862. REMOVED DAMAGED WEB, FABRICATED PO NR 900245 DIM. 18.1250 INCH X 7.1250 INCH, INSTALLED, PRIMED AND TREATED IAW SRM 51-30-2 & 51-10-2 AT STA 680-700 BELOW STR 27R.Sep 16, 2006 · N764AT · Boeing 727264 · Fuselage Miscellaneous StructureSDR DHL2006764005Skin · damagedSTRINGERS 28R AND 27R DAMAGED BETWEEN STA 680-700. REF. ITEM 1P LP 098862. CUTOUT DAMAGED SECTIONS STR 27R 26.5 INCH AND STR 28R 7.5 INCH. FAB. NEW FROM BAC1498-144. SPLICE FROM BAC1498-132 STR 27R 12INCH AND STR 28R 22.5 INCH PO INCH 623185 AND PO INCH 423185Sep 16, 2006 · N764AT · Boeing 727264 · Fuselage Main, Plate/SkinSDR DHL2006763003Connector · damagedON DEPARTURE LANDING GEAR WOULD NOT GO PAST OFF ABNORMAL PROCEDURES WAS PERFORMED HORN SOUNDED AT FLAPS 2 FLAPS WERE SELECTED BACK TO 5 AND GEAR HANDLE SELECTED DOWN AT CONNECTOR 1890B INTERMITTENT REPLACED PIN 35 AND 36 IAW SWPM 20-60-02 AND GEAR MODULE SSep 7, 2006 · N763AT · Boeing 727264 · Landing Gear System WiringSDR DHL2006763002Accessory Unit · failedON DEP F/O WENT TO RAISE GEAR, GEAR HANDLE WOULD NOT GO PAST OFF. F/O PULLED LEVER LATCH TO RAISE GEAR. ON FLAP RETRACTION WARNING HORN SOUNDED ON FLAPS UP, COMPLIED WITH ABNORMAL PROCEDURES. REMOVED & REPLACED LANDING GEAR ACCESSORY BOX IAW B727 MM 32-09-1Sep 7, 2006 · N763AT · Boeing 727264 · Landing Gear Retraction/Extension SystemSDR DHL2006764002Battery · dischargedCOCKPIT EMERGENCY EXIT LIGHT WILL NOT ILLUM. DURING SBY PWR CHECK. R&R EMERGENCY EXIT LIGHT BATTERIES 2 EACH P/N38931-002. INSTALLED, OPS CHECK SERVICEABLE PER B-727 M/M 33-50-00.Jun 29, 2006 · N764AT · Boeing 727264 · Emergency LightingSDR DHL2006785007Wire · looseLEFT MAIN GEAR RED UNSAFE LIGHT TESTS GOOD BUT FAILS TO ILLUMINATE WHEN GEAR IS RETRACTED OR EXTENDED. ALL OTHER GEAR INDICATIONS WORK GOOD. VERIFIED PROBLEM. T/S, FOUND LOOSE WIRE ON LIGHT ASSY SOCKET. CLEANED CONTACTS & TIGHTENED. OPS CHECK GOOD. MM REJun 29, 2006 · N785AT · Boeing 727264 · Landing Gear System WiringSDR DHL2006765002Engine · malfunctionedON ENG START - START WAS NORMAL. ENG ACCELERATED TO 30 PERCENT N1, 520 EGT 52 PERCENT N2. GRD PERSONNEL REPORTED ENG SMOKING & ENG FLAMED-OUT. ENG FAILURE CHECKLIST COMPLETE. FLOW CHART COMPLETE. INSP INLET & EXHAUST - NO DAMAGE NOTED. OPENED COWLING & IJun 27, 2006 · N765AT · Boeing 727264 · Engine (Turbine/Turboprop)
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