Boeing 727-227

Service difficulty reports · 5,082

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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 = '727227'
  ORDER BY difficulty_date DESC"

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SDR DHL2005781537Hinge · crackedDURING A C-CHECK, NR 3 SPOILER HINGE CUTOUT CRACKED (MARKED) LT WING UPPER SURFACE. REMOVED NR 3 SPOILER PANEL TO FACILITATE OTHER MAINTENANCE IAW B727 SRM 27-62-01. REMOVED FASTENERS FOR ACCESS FOR REPAIR IAW B727 SRM 57-30-4 FIG 10. CRACK TERMINATED AT FAFeb 14, 2005 · N781DH · Boeing 727227 · SpoilersSDR DHL2005782537Hinge · crackedDURING A C-CHECK, NR 3 SPOILER HINGE CUTOUT CRACKED (MARKED) LT WING UPPER SURFACE. REMOVED NR 3 SPOILER PANEL TO FACILITATE OTHER MAINTENANCE IAW B727 SRM 27-62-01. REMOVED FASTENERS FOR ACCESS FOR REPAIR IAW B727 SRM 57-30-4 FIG 10. CRACK TERMINATED AT FAFeb 14, 2005 · N781DH · Boeing 727227 · SpoilersSDR DHL2005781535Stop Fitting · wornDURING A C-CHECK, LT W/W AFT DOOR STOP FITTING BS 950 HAS PLAY. REMOVED LT W/W AFT BODY FAIRING AT BS 950 AND FUEL VENT TUBE IAW B727 SRM 51-30-2. FABRICATED ANGLES (2EA) FAIRING FROM 2024T3-050 PO 9001576 DIM 19.375 X 3.3125 X .75 X .75 (2EA) IAW B727 SRM 5Feb 14, 2005 · N781DH · Boeing 727227 · Fuselage Main, StructureSDR DHL2005781534Skin · gougedDURING A C-CHECK, 4 HAND FUSELAGE 4 E AREA IS GOUGED APPROX STA 720E (MARKED) STR 19L. REMOVED PREVIOUS AT LT/HAND FUSELAGE L/E AREA STA 720E STR 19L IAW B727 SRM 51-30-2. FABRICATED DOUBLER REPAIR MAT USED 2024T3 .071 PO 9001978 DIM 17 X 12 INCH AND 1 EA FIFeb 14, 2005 · N781DH · Boeing 727227 · Fuselage Main, Plate/SkinSDR DHL2005781533Skin · gougedDURING A C-CHECK, RT FUSELAGE L/E AREA IS GOUGED APPROX STA 720 E (MARKED). REMOVED PREVIOUS REPAIR AT RT FUELAGE L/E AREA STA 720E STR 19R IAW B727 SRM 51-30-2. FABRICATED DOUBLER REPAIR MAT USED 2024T3 .071 PO 9001765 DIM 10.5 X 9.5 INCH AND FILLER MAT USEFeb 14, 2005 · N781DH · Boeing 727227 · Fuselage Main, Plate/SkinSDR DHL2005781532Skin · crackedDURING A C-CHECK, NR 4 SLAT CRACKED AT I/B & O/B OF ACTUATOR ROD ATTACH POINT (IN LIGHTENING HOLE). REMOVED AND REPLACED NR 4 SLAT WEB (RIBS) IAW B727 SRM 51-30-2, P/N 65-17276-9, PO441715 & P/N 65-17276 PO441715.Feb 14, 2005 · N781DH · Boeing 727227 · Leading Edge DevicesSDR DHL2005781509Skin · delaminatedDURING A "C" CHECK, RT WING OUTBD MID FLAP INBD END IS DELAMINATED AT TRAILING EDGE, WBL 300. REMOVED RT O/B MID FLAP I/B FAIRING TO F.D.M IAW B727 SRM 51-30-2. CUT OUT DELAM AREA UPPER SKIN AT T/E APPROX 7 INCH BY 3 1/2 INCH IAW B727 SRM 51-40-20 FIG 30. Feb 14, 2005 · N781DH · Boeing 727227 · Trailing Edge FlapsSDR DHL2005781522Rib · crackedDURING A "C" CHECK, RT WING LEADING EDGE RIB AT SLAT, STA 260 IS CRACKED. REMOVED AT RT WING LEADING EDGE RIB AT STA 260 FOR FAB IAW B727 SRM 51-30-2, FABRICATED NEW RIB, MAT'L USED 2024-T3 .050 PO NR 9001873,DIM.15 INCH BY 1 1/2 INCH IAW B727 SRM 57-20-2 FIFeb 13, 2005 · N781DH · Boeing 727227 · Leading Edge DevicesSDR DHL2005781521Angle · crackedDURING A "C" CHECK: RT WING LEADING EDGE COVE PANEL INBD SUPPORT ANGLE IS CRACKED AT WS 130. REMOVED R/W L/E COVE PNL SUPPORT ANGLE AND FABBED NEW FROM 2024-T3 .050 PO NR 9001417 DIM 17 1/2 INCH BY 1 1/2 INCH IAW 727 SRM 57-20-2 FIG 1. NEW ANGLE TREATED AND Feb 13, 2005 · N781DH · Boeing 727227 · Wing Miscellaneous StructureSDR DHL2005781520Frame · dentedDURING A "C" CHECK, AFT CARGO DENT FRAME STA 1110 AT STA 23 LT. REMOVED FASTENERS FOR ACCESS AT AFT CARGO STA 1110 AT STA 23 LT IAW B727 SRM 51-30-2. CUT OUT DAMAGE AREA DIMENSION 2 INCH BY 1 INCH IAW B727 SRM 51-40-3 FIG 1. FABRICATED FRAME REPAIR MAT USEDFeb 13, 2005 · N781DH · Boeing 727227 · Fuselage Main, FrameSDR DHL2005781519Intercostal · corrodedDURING A "C" CHECK, AFT CARGO CORROSION ON INTERCOSTAL STA 1150 TO 1166 O/B OF 26R. EVALUATED ANGLE FROM BS 1150 TO 1166 AND FOUND IT TO BE OUT OF LIMITS IAW 727 SRM 53-10-1 FIG 5. REMOVED ANGLE FROM BS 1150 TO 1166 IAW 727 SRM 51-30-2. FABRICATED ANGLE FROFeb 13, 2005 · N781DH · Boeing 727227 · Fuselage Miscellaneous StructureSDR DHL2005781518Skin · crackedDURING A "C" CHECK, L1 DOOR UPPER HINGE CUTOUT IS CRACKED AT BS 303. REMOVED EXISTING FASTENERS, CUT OUT DAMAGED AREA DIM 1.5 X .5. ACCOMPLISHED NDT INSPECTION AROUND CUTOUT, NO CRACK NOTED. FABRICATED DOUBLER FROM 301 CRESS 1/2 HARD .063, PO 900125 DIM. 16Feb 13, 2005 · N781DH · Boeing 727227 · Fuselage Main, Plate/SkinSDR DHL2005781510Skin · gougedDURING A "C" CHECK, RT WING TIP LOWER INBD EDGE IS GOUGED BY NR 8 SLAT AND WEB IS DENTED SLAT STA 434.5. REMOVED R/WING TIP AND WEB SLAT STA 434.5 IAW B727 SRM 51-30-2. REMOVED AREA TO ORIGINAL CONTOUR IAW B727SRM 51-40-1. ACCOMPLISHED NOT HFEC AT REMOVED Feb 13, 2005 · N781DH · Boeing 727227 · Wing, Plate/SkinSDR DHL2005781517Hinge · crackedDURING A "C" CHECK, MAIN CARGO DOOR, LT AFT HINGE CRACKED. REMOVED AFT HINGE SECTION AT MCD IAW B727 SRM 51-30-2, DRILLED NEW HINGE P/N MS20001-16-7200 PO 9001289 DIM.18 INCH BY 2 INCH AND 12 INCH BY 2 INCH IAW S/B AEJ 01-01,TREATED AND PRIMED HINGE AND AREA Feb 12, 2005 · N781DH · Boeing 727227 · Fuselage, Door HingeSDR DHL2005781531Skin · crackedDURING A C-CHECK, NR 1 SLAT SKIN CRACKED AT I/B TRACK ATTACH POINT (MARKED). STOP DRILLED WITH .25 INCH DIAMETER DRILL IAW B727 SRM 51-10-1 FAB. DOUBLER REPAIR WITH 2024T3 0.80 SIZE 6.5 X 6.5 INCH PO 9001502 IAW B727 SRM 57-50-3 FIG 1 & 57-50-2 FIG 2. TREATFeb 11, 2005 · N781DH · Boeing 727227 · Leading Edge DevicesSDR DHL2005781530Skin · gougedDURING A C-CHECK, NR 2 SLAT SKIN GOUGED AT I/B SLAT HOOK (MARKED). REMOVED FASTENERS FOR ACCESS AT NR 2 SLAT SKIN AT I/B SLAT HOOK IAW B727 SRM 51-30-2. FABRICATED DOUBLER REPAIR MAT USED 2024T3 .125 PO 9001068 DIM 5.5 X 3.5 INCH IAW B727 SRM 57-50-3 FIG 10.Feb 11, 2005 · N781DH · Boeing 727227 · Leading Edge DevicesSDR DHL2005781529Panel · dentedDURING A C-CHECK, VERT STAB RT SIDE TRAPIZOIDAL PANEL HAS 3 SHARP DENTS BELOW PREVIOUS REPAIR. CUT OUT DENTED AREA ON RT VERT TRAPAZOID PANEL APPROX 2 INCH DIA AND REMOVED PREVIOUS REPAIR APPROX 3 X 3.5 INCH, FABRICATED FILLERS, 1- APPROX 2 INCH DIA AND 2 - AFeb 11, 2005 · N781DH · Boeing 727227 · Vertical StabilizerSDR DHL2005781525Skin · dentedDURING A "C" CHECK, NR 1 SLAT L/E EXTERIOR SKIN DENTED AND SCRATCHED AT WSTA 760 (MARKED). CUT OUT DAMAGED AREA APROX 1 INCH BY 2 1/4 INCH AT NR 1 SLAT LE EXT SKIN W STA 760 IAW B727 SRM 57-50-3. FAB DOUBLER REPAIR WITH 2024T3 .080 SIZE 5 1/4 INCH BY 4.5 INFeb 11, 2005 · N781DH · Boeing 727227 · Leading Edge DevicesSDR DHL2005781523Skin · gougedDURING A "C" CHECK, LT WING UPPER SURFACE GOUGED 1 INCH AFT OF NR 2 SLAT O/B SLAT HOOK RETAINER. REMOVED PAINT AT AFFECTED AREA IAW B727 B772 51-20-1. INSPECTED AREA USING C/3 ULTRSONIC THICKNESS GOUGE ORIGINAL THICKNESS OF 0.040 MATERIAL LOSS OF 0.0102 INCHFeb 11, 2005 · N781DH · Boeing 727227 · Wing, Plate/SkinSDR DHL2005781516Skin · dentedDURING A "C" CHECK, LT L/E SKIN DENTED 15 INCH I/B OF NR 4 SLAT I/B TRACK. CUT OUT DAMAGED AREA AT LT WING L/E SKIN I/B NR 4 SLAT, I/B TRACK DIM.3/4 BY 3/4 IAW B727 SRM 57-30-4 FIG.1. FABRICATED DOUBLER REPAIR MAT'L 2024 T3 .050 PO 9001873 DIM 3 1/4 BY 3 3Feb 11, 2005 · N781DH · Boeing 727227 · Leading Edge DevicesSDR DHL2005781505Skin · crackedDURING A C-CHECK, NR 3 SLAT SKIN AT TRACK ATTACH POINT CRACKED. MAKE 2 EA STOP DRILLS WITH .25 DIA DRILL AT NR 3 SLAT SKIN AT I/B TRACK IAW B727 SRM 57-5-3 FIG 1. ACCOMPLISHED 727 HFEC INSPECTION 51-00-00 FIG 4, CRACK CONTAINMENT CONFIRMED. FAB REPAIR DOUBLFeb 11, 2005 · N781DH · Boeing 727227 · Leading Edge DevicesSDR DHL2005781502Skin · dentedDURING A C-CHECK, LT WING L/E SKIN DENTED 15 INCHES I/B OF NR 4 SLAT I/B TRACK. CUT OUT DAMAGED AREA LT WING LEADING EDGE SKIN I/B NR 4 SLAT I/B TRACK DIM .75 X .75 INCH IAW B727 SRM 57-30-4 FIG 1. FABRICATED DOUBLER REPAIR MATL USED 2024-T3 .050 PO 9001873 Feb 11, 2005 · N781DH · Boeing 727227 · Leading Edge DevicesSDR DHL2005781501Skin · gougedDURING AN C-CHECK, NR 2 SLAT SKIN GOUGED AT I/B SLAT HOOK. REMOVED FASTENERS FOR ACCESS AT NR 2 SLAT SKIN AT I/B SLAT HOOK IAW B727 SRM 51-30-2, FABRICATED DOUBLER REPAIR, MAT USED 2024-T3 .125 PO 9001068, DIM 5.5 X 3.5 INCHES IAW B727 SRM 57-50-3 FIG 10. ALFeb 11, 2005 · N781DH · Boeing 727227 · Leading Edge DevicesSDR DHL2005781515Nose Cowl · dentedDURING A "C" CHECK, NR 1 ENG NOSE COWL EXTERIOR SKIN HAS DENT AT 6 O'CLOCK POSITION; DENT OUT OF LIMITS BY A/Y RATIO A.1.9 .075=25 IAW B727SRM 54-30-1 FIG 1. REMOVED INTERNAL ANTI-ICE DUCTS TO FOLICATE S/M WORK IAW B727 M/M 30-21-14. REMOVED FASTENERS FOR Feb 10, 2005 · N781DH · Boeing 727227 · Engine Cowling SystemSDR DHL2005781514Skin Panel · scratchedDURING A "C" CHECK, THREE SCRATCHES EXTERIOR SURFACE AT STA 460, STR 5 RIGHT. REMOVED PAINT AFFECTED AREA BS 440 TO BS 460 AT STR 3 TO STR 6 RT SIDE IAW B727 M/M 51-20-1, SCRATCHED AREA FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-30-1 FIG 1. CUT OUT DAMAGED AFeb 10, 2005 · N781DH · Boeing 727227 · Fuselage Main, Plate/SkinSDR C8GA20050004Pitot Line · looseFLT 739 FROM CLT TO BNA, ON TAK OFF, F/O AIRSPEED INDICATOR SHOWED NO INDICATION. ABORTED TAKEOFF AND RETURNED TO GATE. FOUND PITOT/STATIC LINE TO INDICATOR DISCONNECTED. RECONNECTED LINE. SYSTEM OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICEJan 26, 2005 · N89427 · Boeing 727227 · Pitot/Static SystemSDR DHL2005784003Warning Light · false indicationFIRE PROTECTION SYSTEM ENG NR 3 DETECTION CIRCUIT LIGHT ILLUMINATED. COULD NOT DUPLICATE. PERFORMED VISUAL INSPECTION NO DEFECTS NOTED. OPS NORMAL IAW 26-11-0.Jan 26, 2005 · N784DH · Boeing 727227 · Fire DetectionSDR DHL2005784002Oil Cap · looseOIL QUANTITY ENGINE 32 4.25 DECREASED TO 1.25 INFLIGHT PERFORMED ABNORMAL PROC. INSPECTED 32 ENG OIL QTY FOUND OIL CAP LOOSE RESECURED. SERVICED 32 ENG TO FULL. RESECURED OIL CAP REF M/M 12-15-1.Jan 21, 2005 · N784DH · Boeing 727227 · Turbine Engine Oil SystemSDR C8GA20050003Isolation Valve · malfunctionedFLT 712 FROM TOL TO DEN, IN CRUISE AT 31000 FEET, AIRCRAFT RAPIDLY DEPRESSURIZED. CREW EMERGENCY DESCENDED TO 14000 FEET AND STABILIZED PRESSURE AT 5 PSID. AIRCRAFT CONTINUED TO DEN AND LANDED WITHOUT INCIDENT. SWAPPED ENGINE BLEED VALVES WITH NR 2 ISOLATIOJan 19, 2005 · N308AS · Boeing 727227 · Cabin Pressure Control SystemSDR DHL2005782001Pcu · failedAFTER GEAR RETRACTION LOST ALL A-SYS HYD FLUID, PERFORMED ABNORMAL CHECKLIST. RIGHT ELEVATOR PCU FAILED. REPLACED PER 27-30-81. TESTS SERV PER 27-30-81. SERV HYD PER M/M 12-12-0. RAN ENG'S PER JRH 5.2 AND PURGED FLT CONTROLS. NO FURTHER DEFECTS NOTEDJan 15, 2005 · N782DH · Boeing 727227 · Elevator Control SystemSDR DHL2005784001Brake · failedAC REQUIRES EXCESSIVE POWER TO TAXI AND CAME TO A COMPLETE STOP TWICE W/ NO BRAKE APPLICATION AT LESS THAN 150.0 LBS. REMOVED AND REPLACED NR 4 BRAKE AND T/W ASSY IAW B-727-200 MM CH 32-41-32 AND 32-45-1, LEAKS CHECK GOOD IAW 32-41-32.Jan 11, 2005 · N784DH · Boeing 727227 · BrakeSDR DHL2005781001Shutoff Valve · malfunctionedAT FL 270 CABIN ALTITUDE AURAL WARNING SOUNDED AND ALTITUDE ALERTER ILLUMINATED AND AURAL WARNING SOUNDED. UNABLE TO CONTROL CABIN ALTITUDE EXECUTED EMERGENCY DESCENT RETURNED TO DEPARTURE AIRPORT. (AUS) T/S SYS, RAN ENGINES AND PERF DECAY CK PER M/M 05-51-7Jan 4, 2005 · N781DH · Boeing 727227 · Cabin Pressure Control SystemSDR DHL2004784007Switch · dirtyON TAKEOFF, WHEN LANDING GEAR HANDLE RAISED THE FWD ENTRY DOOR LIGHT ILLUMINATED RETURNED FOR LANDING. PERFORMED FWD DOOR ENTRY INDICATOR SWITCH CLEANED AND TIGHTENED SAME TEST OK LT OFF IN CLOSED POS IAW AMM 52-11-01.Dec 31, 2004 · N784DH · Boeing 727227 · Door Warning SystemSDR XN0A1227Warning Light · illuminatedNR 3 ENGINE CSD LOW PRESSURE WARNING LIGHT ON WITH NO FREG. DISCONNECTED NR 3 CSD DEFERRED NR 3 GENERATOR INOP IAW ENA B727 MEL 24-1 PROCEDURES DMI 4858 CAT-B ITEM. PLACARDS INSTALLED.Dec 24, 2004 · N76752 · Boeing 727227 · Antenna/Radome Anti-Ice/De-Ice SystemSDR DHL2004783016Engine · flamed outENGINE NUMBER 1 FLAMED-OUT AFTER START, ATTEMPTED SECOND START, NO LIGHT OFF, ON SECOND START. ACCOMPLISHED NO LIGHT OFF ABNORMAL PROCEDURE. REMOVED CONNECTOR, CLEANED CONNECTION FOR FUNCTIONAL CHECK OF VALVE, ALL INDICATION NORMAL IAW 28-22-01. ENGINE RUN Dec 9, 2004 · N783DH · Boeing 727227 · Engine (Turbine/Turboprop)SDR XNOA1215Actuator · malfunctionedON CLIMB-OUT, LEADING EDGE DEVICES WOULD NOT INDICATE UP AND LOCKED. X-FERRED TO DMI 4798, MEL 27-6 CAT "C". PLACARDS INSTALLED AS REQUIRED. R/R NR 2 SLAT ACTUATOR, OPS CK GOOD ON GROUND IAW B727 MM 27-81-32. THIS ACTION CLEARS DMI 4798. PLACARDS REMOVED. (SDec 7, 2004 · N793A · Boeing 727227 · Leading Edge Slat ActuatorSDR DHL2004782013Battery · inoperativeBOTH EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERIES IAW MM 33-50-71, OPS CK NORMAL P/N MIOSC062 (4 EA).Dec 7, 2004 · N782DH · Boeing 727227 · Emergency LightingSDR DHL2004781005Light · looseEMERGENCY EXIT LIGHT OVER COCKPIT DOOR FLASHES INTERMITTENTLY. RESECURED ASSY, OPS CK GOOD IAW 33-50-101. `Dec 2, 2004 · N781DH · Boeing 727227 · Emergency LightingSDR 04FDEA03205Transmitter · failedDURING CLIMB THROUGH 17,000 FT, NOTICED NR 1 ENG OIL PRESS AT 27 PSI. SHUT ENG DOWN IAW RED TABS LANDED IN MEM. ENT BY: 206208 RPT BY: 111069, SWAPED NR 1 AND NR 2 OIL PRES IND, RAN NR 1 ENG OIL PRES IND STUCK AT 27PSI, LOP LIGHT WAS OUT ALL OTHER IND WERE Nov 25, 2004 · N478FE · Boeing 727227 · Engine Oil QuantitySDR DHL2004783015Connector · detachedR GEAR DOOR LIGHT ILLUMINATED WHEN HANDLE SELECTED OFF. PER ABNORMAL, RECYCLE HANDLE LIGHT OFF. CLEANED AND RESECURED CONNECTOR ON RT MLG DOOR SWITCH, TESTED RT MLG DOOR SWITCH IAW B-727 MM 32-62-11, NO DEFECTS NOTED.Nov 20, 2004 · N783DH · Boeing 727227 · Landing Gear System WiringSDR DHL2004783014Relay · failedEMERGENCY EXIT LIGHTS ILLUMINATED AFTER GOING TO SHIPS POWER. DEFER APU DUE TO EXTERNAL PWR RELAY STICKING AND GEN RELAY PER MEL REF 49-1, CONTROL NR 18533 , PLACARD INSTALLED. DEFER APU DUE TO EXTERNAL PWR RELAY STICKING AND GEN RELAY PER MEL REF 49-1, CONTNov 19, 2004 · N783DH · Boeing 727227 · Emergency LightingSDR DHL2004782012Engine · leakingAT 10 KTS ON THE TAKEOFF ROLL RWY 35L WINDS CALM TEMP +1C A LOUD BOOM WAS HEARD THE AUTOPACK TRIP TRIPPED AND THE TAKEOFF REJECTED. THE A/C WAS TAXIED OFF THE RUNWAY AND THE NR 3 ENGINE OIL WAS DECREASING THE NR 3 ENGINE WAS SHUT DOWN RETURNED TO THE BLOCKS RNov 13, 2004 · N782DH · Boeing 727227 · Engine (Turbine/Turboprop)SDR DHL2004782011Pressure Switch · malfunctionedNR 2 START VALVE ILLUMINATED IN FLIGHT SHUT DOWN NR 2 ENGINE AS PRECAUTION. TRANSFERED NR 2 START VALVE OPEN LIGHTS TO DMI NR 18276 PER MEL 80-1-1B PLACARD INSTALLED. REMOVED AND REPLACED START VALVE PRESSURE SWITCH PER 80-11-11. GROUND CHECKS GOOD CLEAR DMOct 28, 2004 · N782DH · Boeing 727227 · Engine StarterSDR XNOA1205Switch · damagedNR 6 LED FAILED TO RETRACT AFTER T/O. FOUND PUSHED PIN AT NR 6 LED FLAP POS SWITCH. RESEATED PIN IAW MM CH. 20-11-07. OPS CHECKS GOOD IAW MM CH. 27-82-11.Oct 27, 2004 · N76753 · Boeing 727227 · Leading Edge Slat Control SystemSDR XNOA1204Position Switch · out of adjustNR 6 LED FAILED TO RETRACT. ADJUSTED NR 6 LEADING EDGE FLAP POS SWITCH IAW MM CH. 27-82-11.Oct 27, 2004 · N76753 · Boeing 727227 · Leading Edge Slat Position Indicating SystemSDR 04FDEA02970Indicator · malfunctionedINBOARD FLAP ASYM INDICATION UPON RETRACTION. REMOVED AND REPLACED INBD FLAP POSITION INDICATOR PER MM 27-52-021-2, OPS CHECK NORMAL. R/I FROM FACT PREMATURE REMOVAL/INSTALLATION OFF MFG 18-1299-5-2F1 POS 2 SRL 0778AN TAG 680660 ON MFG 2061-13-1 SRL 252 TAOct 22, 2004 · N487FE · Boeing 727227 · Trailing Flap Position Indicating SystemSDR CA041020002Fitting · cracked(CAN) DURING ROUTINE MAINTENANCE A CRACK WAS FOUND IN THE LEFT HAND MLG UPLOCK FITTINGIN THE FORWARD RADIUS. NDT CONFIRMED THE CRACK. FITTING WAS REPLACED AND GEAR RETRACTIONS CARRIED OUT.Oct 16, 2004 · Boeing 727227 · Landing Gear Position and WarningSDR CA041007001Wire · chafed(CAN) JUST PRIOR TO ENGINE START AT AN OUTBASE, THE A/C APU SHUT DOWN ON ITS OWN. GROUND EQUIPMENT WAS USED TO POWER AND START THE A/C, AND THE FLIGHT CONTINUED. AT THE TERMINATING BASE, MAINTENANCE PERSONNEL FOUND 2 WIRES AT THE APU THAT HAD CHAFED AND SHORTOct 5, 2004 · Boeing 727227 · APU System WiringSDR DHL2004782010Brake Assy · malfunctionedLEFT BRAKE SQUEALS, SHUDDERS AND GRABS ON APPLICATION. INSPECTED LT BRAKES, NO DEFECTS NOTED. BLED LEFT BRAKES AS A PRECAUTIONARY. WORK DONE IAW B-727 MM 32-41-0. TAXIED AIRCARFT, BRAKES OPS CHECKED GOOD.Sep 25, 2004 · N782DH · Boeing 727227 · Landing Gear Brake SystemSDR CA040922002Rod End · sheared(CAN) DURING ROUTINE OPENING OF THE CARGO DOOR FOR LOADING OF THE AIRCRAFT, A WIND GUST BLEW THE DOOR FULLY OPEN, AND SHEARED ALL FOUR ACTUATOR LINK RODS. THE DOOR ENDED UP IN A VERTICAL POSITION. THE WIND VELOCITY AND GUSTS WERE CHECKED WITH THE CONTROL TOWERSep 15, 2004 · Boeing 727227 · Cargo/Baggage Doors
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