Boeing 727-2Q9

Service difficulty reports · 830

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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 = '7272Q9'
  ORDER BY difficulty_date DESC"

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SDR DHL2003740006Odor · detectedHOT SMELL COMING FROM AIR CONDITIONING PACK TEMPERATURE AND DUCT TEMPERATURE NORMAL. RAN ENGINES AND PACKS IAW JRH & M/M 21-20-01. NO DEFECTS NOTED. CAN NOT DUPLICATE, OK TO CONTINUE.Nov 7, 2003 · N740DH · Boeing 7272Q9 · Air Distribution SystemSDR DHL2003740005Strap · misinstalledCABIN ENTRY DOOR HARD TO CLOSE. FOUND DOOR TO BE BINDING ON WARNING STRAP DUE TO INCORRECT INSTALLATION OF STRAP. INSTALLED STRAP IAW B-727 M/M 52-11-01. OPS CHECK OF FORWARD ENTRY DOOR IAW B-727 M/M 52-11-01.Oct 25, 2003 · N740DH · Boeing 7272Q9 · Passenger/Crew DoorsSDR DHL2003741010Light · inoperativeCREW ENTRY DOOR GALLEY EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED GALLEY EMERGENCY LIGHT PER M/M 33-50-01. OPS CHECKED GOOD.Oct 18, 2003 · N741DH · Boeing 7272Q9 · Emergency LightingSDR DHL2003741009Screw · looseCOCKPIT DOOR IS DIFFICULT TO OPEN AND CLOSE. TIGHTENED SCREWS ON DOOR FRAME AND DOOR. OPS CHECKED GOOD IAW 20-80-1 AND 52-50-1.Oct 2, 2003 · N741DH · Boeing 7272Q9 · Fixed Inner DoorsSDR DHL2003741008Switch · malfunctionedRIGHT GEAR DOOR OPENED WHEN GEAR HANDLE MOVED TO THE OFF POSITION. CYCLED HANDLE UP-OFF. DOOR REMAINED CLOSED ON SECOND ATTEMPT. REMOVED AND REPLACED LANDING GEAR DOOR WARNING SWITCH RT GEAR DOOR IAW M/M 32-62-11. SWITCH P/N: 1EN161RB1 TESTED IAW M/M 32-62Aug 29, 2003 · N741DH · Boeing 7272Q9 · Door Warning SystemSDR DHL2003741007Switch · dirtyTHE RIGHT MAIN GEAR DOOR WENT DOWN WITH GEAR HANDLE ON THE OFF POSITION. ABNORMAL PROCEDURE COMPLETED, THE DOOR WENT BACK UP WITH HANDLE ON UP POSITION. TROUBLESHOT RIGHT MAIN LANDING GEAR DOOR IAW M/M 32-61-01. CLEANED DOOR SWITCH IAW WPM 20-60-01. TESTEDAug 27, 2003 · N741DH · Boeing 7272Q9 · Landing Gear Position and WarningSDR DHL2003741006Smoke Detector · faultyCARGO SMOKE LIGHT ILLUMINATED DURING DESCENT. CYCLED SWITCH OFF THEN ON AND LIGHT EXTINGUISHED. REMOVED AND REPLACED NR 6 CARGO SMOKE DETECTOR IAW M/M 26-16-01. OPS CHECKED NORMAL.Jul 18, 2003 · N741DH · Boeing 7272Q9 · Smoke DetectionSDR DHL2003741005Smoke Warning · false activationCARGO SMOKE LIGHT ILLUMINATED ON FINAL APPROACH. PERFORMED OPERATIONAL CHECK. COULD NOT DUPLICATE OK FOR SERVICE. CARGO LIGHT IS NOT ILLUMINATED.Jul 18, 2003 · N741DH · Boeing 7272Q9 · Smoke DetectionSDR DHL2003740004Handle · inoperativeFORWARD ENTRY DOOR EXTERIOR HANDLE WILL NOT STAY IN THE FLUSH POSITION. HANDLE WAS OUT OF FLUSH POSITION OR 90 DEGREES OUT OF DETENT. CLEANED AND LUBRICATED EXTERIOR AND INTERIOR DOOR HANDLES, CLEANED VENTILATION HOLE HANDLE EXTERIOR CHECKED OPS GOOD IAW M/Jun 28, 2003 · N740DH · Boeing 7272Q9 · Passenger/Crew DoorsSDR DHL2003741004Warning Horn · activatedREJECTED TAKEOFF CVG DUE TO TAKEOFF WARNING HORN. TOGW 128.4, KIAS 0-2K, OAT 17 DEGREES C, PA 900, BRAKE ENERGY CHART, NORMAL STAB TRIM FOR T/O SET AT 2.8 PRIOR TO NEXT T/O, RECYCLED STAB TRIM FULL NOSE DOWN AND FULL NOSE UP, THEN BACK TO 2.8. NO FURTHER PROJun 5, 2003 · N741DH · Boeing 7272Q9 · Central WarningSDR DHL2003741003Smoke Detector · will not testNR 6 SMOKE DETECTOR IN MAIN CABIN DOES NOT TEST. REMOVED AND REPLACED SMOKE DETECTOR IAW B-727 26-16-01.Jun 3, 2003 · N741DH · Boeing 7272Q9 · Smoke DetectionSDR DHL2003740003Light · inoperativeEMERGENCY EXIT LIGHT IN ENTRYWAY VERY DIM. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSEMBLY IAW B727 M/M 33-50-111. OPS CHECKED SATISFACTORY.May 2, 2003 · N740DH · Boeing 7272Q9 · Emergency LightingSDR DHL2003740002Handle · lack of lubeMAIN ENTRY DOOR HANDLE EXTREMELY HARD TO TURN TO LOCKED POSITION FROM THE INSIDE. LUBED MAIN ENTRY DOOR HANDLE AND LATCHES OK PER M/M 52-11-01.Apr 5, 2003 · N740DH · Boeing 7272Q9 · Passenger/Crew DoorsSDR DHL2003741519Floorbeam · crackedDURING (C) CHECK, FUSELAGE INTERIOR FLOORBEAMS BS 640 AND BS 660 SPLICE PLATE TO MCD LWR. BEAMS ARE CRACKED 2 EACH NDT CONFIRMED.CA: 1) REMOVED FWD. PIT LT UPPER SIDEWALL GILLINER SUPPORTS FROM BS 580 TO 680. REMOVED LWR JAMB WEB ANGLE LWR EDGE FOR WEB REMMar 25, 2003 · N741DH · Boeing 7272Q9 · Fuselage Main, Floor BeamSDR DHL2003741516Frame · corrodedDURING (C) CHECK DISCREPANCY AS FOLLOWS, FUSELAGE C-1 DOOR CUT-OUT FWD. FRAME WEB BS 560 CORROSION THRU FASTENERS HOLES OF NR 6 DOOR STOP ALSO AT WEB. C/A: REMOVED PREVIOUS REPAIR C-1 DOOR FWD. FRAME WEB BS 560 FOR CORROSION REMOVAL IAW B-727 SRM 51-30-2. 2) Mar 22, 2003 · N741DH · Boeing 7272Q9 · Fuselage Main, FrameSDR DHL2003741518Skin · dentedDURING (C) CHECK DISCREPANCY AS FOLLOWS, FUSELAGE SKIN HAS DENTS AT BS 1090 STR'S 18, 19, AND 20 L. C/A: 1) REMOVED PAINT I.A.W. B-727 M.M. 51-20-01. 2) EVALUATE 5 EACH DENTS, 2 EACH OUT OF LIMITS, 3 EACH IN LIMITS WITH A/Y RATIOS OF 1/.013 =76, .6/.009 = 66Mar 20, 2003 · N741DH · Boeing 7272Q9 · Fuselage Main, Plate/SkinSDR DHL2003741517Skin · damagedDURING (C) CHECK DISCREPANCY AS FOLLOWS, FUSELAGE SKIN HAS PILLOWING BETWEEN BS 294 AND 312 AT STR. 24 R. REMOVED RT FLOOR PANEL IN DOG HOUSE FOR ACCESS STA. 294 TO 330 RBL 30 IAW B-727 SRM 51-30-3. 2) CUT-OUT 2 EACH DAMAGE AREA 5 INCHES X 1.7500 INCH OF 8 INMar 20, 2003 · N741DH · Boeing 7272Q9 · Fuselage Main, Plate/SkinSDR DHL2003741002Connector · contaminatedIN CRUISE, FL290 BOTH AFT BOOST PUMP LOW PSI LIGHTS ILLUMINATED IN THE FUEL TANK NR 2 AT THE SAME TIME BOTH CIRCUIT BREAKERS POPPED. PERFORMED ABNORMAL PROCEDURES. INSPECTED FUEL PUMPS AND PLUG CONNECTIONS, CLEANED AND RESET PLUGS, RESET BREAKERS, OPERATED PMar 1, 2003 · N741DH · Boeing 7272Q9 · Fuel System WiringSDR DHL2003740530Skin · damagedSKIN CREASED BELOW STR 23R AT BS 1060. CUT OUT DAMAGED AREA DIM 6 INCHES X 3 INCHES AT BS 1060 STR 23R AND FABRICATED ONE DOUBLER DIMENSIONS 9.25 INCHES X 15.5 INCHES USING .071 2024T3 PO 9912182 IAW SRM 53-30-3 FIG 1. ALODINED AND PRIMED IAW SRM 57-10-2, INFeb 28, 2003 · N740DH · Boeing 7272Q9 · Fuselage Main, Plate/SkinSDR DHL2003740529Skin · gougedSKIN GOUGED AT STR 19R BS 1130-1148. DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-30-1 FIG 1. CUT OUT DAMAGED AREA 4.2 INCHES X 1 INCH AND FABBED DOUBLER FROM 2024T3 .071 PO 9912182 DIM 11.3 INCHES X 10.5 INCHES IAW SRM 53-30-2 FIG 2 & 53-30-3 FIG 1. DOUBLERFeb 28, 2003 · N740DH · Boeing 7272Q9 · Fuselage Main, Plate/SkinSDR DHL2003740527Spar · crackedRT ELEVATOR TAB HAS 3 O/B HINGES LOOSE AT ELEVATOR REAR SPAR ATTACH POINT, CHECK FOR SPAR CRACKS PER S/B 55-0089. REMOVED DAMAGED SPAR AND INSTALLED NEW SPAR (P/N 65C30825-24) PO 301742 IAW S/B 727-55-0089 FIG 6 AND SUPPORT FITTINGS.Feb 26, 2003 · N740DH · Boeing 7272Q9 · Elevator, Spar/RibSDR DHL2003740528Web · corrodedC-1 DOOR LOWER CUTOUT WEB HAS CORROSION. CORROSION ON WEB FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1 FIG 1. REMOVED WEB FROM C1 DOOR LWR CUTOUT FOR REPLACEMENT IAW SRM 51-30-2, FABRICATED NEW WEB DIMENSIONS 60 INCHES X 4 INCHES USING 2024T3 .071 PO 9912182 IAFeb 21, 2003 · N740DH · Boeing 7272Q9 · Fuselage Miscellaneous StructureSDR DHL2003740525Door Frame · crackedAFT CARGO COMPT, C-2 DOOR LOWER CUTOUT LOWER FRAME IS CORRODED AND CRACKED IN 3 AREAS. REMOVED THRESHOLD MOUNT FITTINGS FROM C-DOOR FOR ACCESS IAW SRM 51-30-2. REMOVED 2 EA PREVIOUS REPAIRS SPLICE PLATES FROM LWR TEE CHORD IAW SRM 51-30-2. REMOVED FWD AFT, Feb 21, 2003 · N740DH · Boeing 7272Q9 · Fuselage Main, StructureSDR DHL2003741001Motor · failedA-SYSTEM HYDRAULIC FAILURE. COMPLETED ABNORMAL PROCEDURE. END NR 2 FLUID SHUTOFF FOR 20 MIN. LT WHEEL WELL FLAP HYDRAULIC MOTOR REMOVED AND REPLACED IAW B727 M/M 27-51-62. A-SYSTEM CASE DRAINS AND MOD FILTERS CHECKED FOR CONTAMINATION, NONE NOTED. RESERVIFeb 14, 2003 · N741DH · Boeing 7272Q9 · Hydraulic System, MainSDR DHL2003740502Frame · dentedFWD CARGO FRAME HAS 3 DENTS AT BS 700 STR 38 L. REMOVED FASTENERS FOR ACCESS PER SRM 51-10-2. CUT OUT DAMAGED AREA PER SRM 57-40-3. FABRICATED REPAIR 7075-T6 .063 PER SRM 53-10-3 FIG 3. ALODINED AND PRIMED PER SRM 51-10-2, INSTALLED REPAIR PER SRM 57-40-3 Feb 13, 2003 · N740DH · Boeing 7272Q9 · Fuselage Main, FrameSDR DHL2003740510Frame · dentedFUSELAGE FRAME AT STA 1090 BETWEEN STR 16R AND 17R HAS DENT AND ELONGATED HOLE. CUT OUT DAMAGED AREA PER SRM 51-40-3 FIG 1. FABRICATED REPAIR DOUBLER (7075-T6-.090) PER SRM 51-10-2. TREATED, PRIMED AND PAINTED AREA PER SRM 51-10-2. INSTALLED REPAIR PER SRMFeb 4, 2003 · N740DH · Boeing 7272Q9 · Fuselage Main, FrameSDR DHL2003740503Frame · crackedFUESLAGE UPPER MAIN DECK CARGO DOOR FUSLAGE FRAME 480 CRACKED FWD SIDE WHERE ATTACH TO FUSELAGE SKIN. CUT OUT DAMAGED FLANGE AND FABRICATED REPAIR FROM 7075-T6 AND FILLER FROM 7075-T6 .063 PER SRM 53-10-4 FIG 1. PARTS TREATED AND PRIMED PER SRM 51-10-2. INSFeb 4, 2003 · N740DH · Boeing 7272Q9 · Fuselage Main, FrameSDR DHL2003740517Frame · dentedFUESLAGE FRAME AT STA 540 IS DENTED BETWEEN STR 16R-17R. CUT OUT DENTED AREA AND FABRICATED REPAIR PER SRM 51-40-3. TREATED AND PRIMED REPAIR PARTS AND INSTALLED PER SRM 51-40-1 FIG 1.Feb 3, 2003 · N5311 · Boeing 7272Q9 · Fuselage Main, FrameSDR DHL2003740519Frame · dentedIN FWD CARGO FRAME HAS A DENT INTO THE RADIUS AT BS 680 STR 24 LT. REMOVED FASTENERS AT FRAME BS 680 STR 24L PER SRM 57-30-2. CUT OUT DAMAGED FRAME AREA PER SRM 57-40-3 FIG 1. FABRICATED FRAME REPAIR FROM 7075-T6 0.063 (12.5 X 6 INCH) PER SRM 51-40-3 FIG 1.Feb 3, 2003 · N740DH · Boeing 7272Q9 · Fuselage Main, FrameSDR DHL2003740518Frame · crackedFUSELAGE FRAME AT STA 580 IS DENTED AND CRACKED BETWEEN STR 16R-17R. REMOVED DAMAGED AREA, NO CRACK FOUND. FABRICATED REPAIR PART FROM 7075-T6 .063 AL PER SRM 51-40-3. TREATED, PRIMED AND INSTALLED PER SRM 51-40-3 FIG 1.Feb 3, 2003 · N740DH · Boeing 7272Q9 · Fuselage Main, FrameSDR DHL2003740515Floorbeam · crackedAFT CARGO COMPT AFT PIT FLOORBEAM AT RBL 15 IS CRACKED AT NUT PLATE STA 950E. REMOVED FASTENERS PER SRM 51-30-2. FABRICATED DOUBLER ANGLES (2024-T3 .050) PER SRM 51-40-3. TREATED AND PRIMED PER SRM 51-10-2. INSTALLED REPAIR PER SRM 51-30-2.Feb 3, 2003 · N740DH · Boeing 7272Q9 · Fuselage Main, Floor BeamSDR DHL2003740513Frame · dentedFUSELAGE FRAME AT STA 660 IS DENTED BETWEEN STR 16 R - 17 R. CUT OUT DAMAGED AREA, FABRICATED REPAIR PART (7075-T6 .063) PER SRM 51-40-3. CLEANED, TREATED AND PRIMED PER SRM 51-10-2. INSTALLED REPAIR PER SRM 51-40-1.Feb 3, 2003 · N740DH · Boeing 7272Q9 · Fuselage Main, FrameSDR DHL2003740507Frame · dentedFWD CARGO FRAME HAS 3 DENTS INTO THE RADIUS AT BS 680 STR 23 & 24R. REMOVED FASTENERS FOR ACCSESS PER SRM 51-30-2. FABRICATED REPAIR DOUBLER USING .063 7075-T6 PER SR 53-10-2 FIG 11. TREATED, PRIMED AND INSTALLED PER SRM 51-40-3.Feb 3, 2003 · N740DH · Boeing 7272Q9 · Fuselage Main, FrameSDR DHL2003740506Floorbeam · crackedAFT CARGO COMPT AFT PIT FLOORBEAM AT RBL 15 IS CRACKED AT NUT PLATE STA 950E. REMOVED FASTENERS PER SRM 57-30-2. CUT OUT DAMAGED AREA 2 PLACES PER SRM 51-40-3 FIG 3. FABRICATED DOUBLER ANGLES (2024 T3) .050 PER SRM 51-30-2. TREATED AND PRIMED PER SRM 51-30Feb 3, 2003 · N740DH · Boeing 7272Q9 · Fuselage Main, Floor BeamSDR DHL2003740505Frame · dentedIN FWD CARGO FRAME HAS 2 DENTS INTO THE RADIUS AT BS 660 STR 24 R. REMOVED FASTENERS FOR ACCSES PER SRM 51-10-2. CUT OUT DAMAGED AREA PER SRM 52-10-3. FABRICATED FRAME REPAIR 7076-T6 .063 PER SRM 53-10-3 PG 3. TREATED AND PRIMED PER SRM 51-10-2. INSTALLEDFeb 3, 2003 · N740DH · Boeing 7272Q9 · Fuselage Main, FrameSDR DHL2003740504Frame · crackedFUSELAGE FRAME AT STA 600 IS DENTED AND CRACKED BETWEEN STR 16R-17R. CUT OUT DAMAGED FRAME AND FABRICATED REPAIR FROM 7075-T6 .063. CLEANED, TREATED AND PRIMED AND INSTALLED REPAIR PER SRM 51-40-1.Feb 3, 2003 · N740DH · Boeing 7272Q9 · Fuselage Main, FrameSDR DHL2003740514Channel · chafedCABIN BS 1166 STR 10.3 LT ATTACHING GILLINER SUPPORT SHOWS CHAFE MARK. CUT OUT DAMAGED AREA (2.5 X 1 INCH) AND FABRICATED DOUBLER (7075-T6 .090) PER SRM 53-10-2 AND 51-40-3. TREATED AND PRIMED PARTS PER SRM 51-10-2. INSTALLED DOUBLER PER SRM 51-30-2.Feb 2, 2003 · N740DH · Boeing 7272Q9 · Fuselage Main, Attach FittingsSDR DHL2003740512Frame · crackedCABIN BS 1166 FRAME CRACKED AND BENT 3 INCHES ABOVE FLOOR STRINGER 17 L. CUT OUT DAMAGED AREA 2 X 1.5 INCH, FABRICATED DOUBLER (7075-T6 .090) PER SRM 51-40-3 FIG 1. ALODINED AND PRIMED PER SRM 51-10-2. INSTALLED DOUBLER PER SRM 51-30-2.Feb 2, 2003 · N740DH · Boeing 7272Q9 · Fuselage Main, FrameSDR DHL2003740511Channel · chafedCABIN BS 1166 AND 1148 STR 7.5 LT EACH HAVE GILLINER ATTACHING SUPPORT CHAFE MARKS INTO FRAME. CUT OUT DAMAGED AREA AT STA 1166 3 X 1 INCH, AND 1148 3 X 1 INCH PER SRM 51-40-3. FABRICATED DOUBLERS (7075-T6 .100) PER SRM 53-10-2 FIG 5. TREATED PARTS AND AREAFeb 2, 2003 · N740DH · Boeing 7272Q9 · Fuselage Main, Attach FittingsSDR DHL2003740509Skin · damagedSMALL SKIN CREASE LT SIDE OF FUSLAGE BS 620 STR 25L. MADE CUT OUT IN DAMAGED SKIN PER SRM 53-30-3 FIG 2. FABRICATED REPAIR DOUBLER 2024-T3 .063. FABRICATED FILLER 2024-T3 .050 PER SRM 53-30-3 FIG 2. TREATED AND PRIMED REPAIR PARTS PER SRM 51-10-2. INSTALLFeb 1, 2003 · N740DH · Boeing 7272Q9 · Fuselage Main, Plate/SkinSDR DHL2003740001Window · burnedL-2 WINDOW BURNED AND OUTER PANE CRACKED. REMOVED AND REPLACED L-2 WINDOW IAW M/M 56-12-11. OPS CHECKED GOOD. NO LEAKS NOTED.Jan 21, 2003 · N740DH · Boeing 7272Q9 · Flight Compartment WindowsSDR DHL2002741022Smoke Detector · failed1) NR 5 SMOKE DETECTOR DOES NOT TEST. (NO LIGHT) REPLACED NR 5 SMOKE DETECTOR IAW B-M/M 26-17-000. OPS CHECKED GOOD.Dec 18, 2002 · N741DH · Boeing 7272Q9 · Smoke DetectionSDR DHL2002741021Power Unit · malfunctionedAPU FIRE WARNING WILL NOT TEST. TRANSFERRED TO DMI 11242 PER MEL 26-11, CAT. "C". PLACARD INSTALLED. REF. DMI 11242 - APU FIRE WARNING WILL NOT TEST. REMOVED AND REPLACED APU FIRE TEST RELAY, IAW BMM 26-15-0. NO HELP, DMI 11242 STILL IN EFFECT. REF. DMI Dec 14, 2002 · N741DH · Boeing 7272Q9 · Fire DetectionSDR DHL2002741020Stop · out of adjustMAIN ENTRY DOOR DIFFICULT TO CLOSE PROPERLY. MAIN ENTRY DOOR 2ND FROM BOTTOM AFT STOP NOT CONTACTING. ADJUSTED 2ND FROM BOTTOM AFT ON MAIN ENTRY DOOR OPS CHECKED OK AS PER M/M 52-11-01.Dec 7, 2002 · N741DH · Boeing 7272Q9 · Passenger/Crew DoorsSDR DHL2002741019Snubber1) FWD ENTRY DOOR LEVER GRINDS AND IS DIFFICULT TO OPERATE.2) INSTALLED SERVICEABLE SNUBBER IAW CHAPTER 52-11-33.Dec 7, 2002 · N741DH · Boeing 7272Q9 · Passenger/Crew DoorsSDR DHL2002741018Wire · looseLOWER AFT BODY OVERHEAT WILL NOT TEST. TRANSFERRED TO DMI LIST IAW MEL 26-10-2 SP APPLY REF. DMI 11103. DOES NOT EFFECT SAFE OPERATION OF A/C. REF. DMI 11103 / LOWER AFT BODY OVERHEAT WILL NOT TEST. RESECURED WIRE CONNECTORS ON S/W ON OVERHEAT S/W PER Dec 1, 2002 · N741DH · Boeing 7272Q9 · Fire Protection System WiringSDR DHL2002741017Latch · lack of lubeDOOR OPEN LATCH ON FORWARD ENTRY DOOR IS DIFFICULT TO RELEASE. LUBRICATED "HOLD OPEN" LATCH ON FORWARD ENTRY DOOR. OPS CHECKED GOOD.Nov 13, 2002 · N741DH · Boeing 7272Q9 · Passenger/Crew DoorsSDR DHL2002741016Switch1) AILERON "B" SYSTEM LOW PRESSURE LIGHT ILLUMINATED ON FORWARD PANEL. RTO AT 20 KTS, SL, 174.3 K LBS, 27 DEGREE C. BEC NORMAL SEE DISCREPANCY 1P FOR RTO REASON.2) ENTERED ON DMI #10731 AS PER MEL 27-16 CAT "C". PLACARD INSTALLED. FOR INFORMATION ONLY.3) ROct 23, 2002 · N741DH · Boeing 7272Q9 · Aileron Control SystemSDR DHL2002741015Cap1) "A" SYSTEM HYDRAULIC FAILURE AFTER TAKE-OFF, "0" QUANTITY FOLLOWED ABNORMAL PROCEDURE.2) INSPECTED & FOUND ELEVATOR FEEL COMPUTER "A" SYSTEM FILTER CAP CRACKED. R & R "A" SYSTEM CAP & SEAL PER M/M 27-30-101. INSPECTED #1 & #2 ENGINE HYDRAULIC PUMP CASE DROct 16, 2002 · N741DH · Boeing 7272Q9 · Hydraulic System, MainSDR DHL2002740005Light1) EMERGENCY EXIT LIGHT OVER MAIN ENTRANCE DOOR FOUND INOPERATIVE DURING PREFLIGHT.2) REMOVED AND REPLACED EXIT LIGHT BATTERIES IAW BMM CHAPTER 33-50-71, NO HELP, REMOVED AND REPLACED EXIT LIGHT ASSEMBLY IAW BMM REF. 33-50-71, OPS CHECKED GOOD.Oct 8, 2002 · N740DH · Boeing 7272Q9 · Emergency Lighting
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