Boeing 727-264

Service difficulty reports · 617

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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 = '727264'
  ORDER BY difficulty_date DESC"

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SDR MZZA99056Web · wornTNN - DURING 1/2D CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, WORN WAS FOUND ON RIGHT SIDE AFTER AIRSTAIR TORQUE BOX HORIZONTAL WEB AT BS 1320. THE DAMAGED WEB OF AFTER AIRSTAIR TORQUE BOX HORIZONTAL WEB WAS REPAIRED PER B727 SRM 51-40-2 FIGURE 1. (M)Mar 15, 1999 · N625DH · Boeing 727264 · Fuselage Miscellaneous StructureSDR MZZA99058Stringer · crackedTNN - DURING 1/2D CHECK INSPECTION ON AIRCRFT AT AIR ASIA, .4375 INCH LONG CRACK WAS FOUND ON LEFT WING UPPER S-9 STRINGER/RIB ATTACH HOLE AT WS 656.5. THE CRACK WAS STOP DRILLED AND REPAIRED PER CMI EA 5762-01050 PART 3 (SB 727-57A159 FIGURE 18).Mar 14, 1999 · N625DH · Boeing 727264 · Wing, Longeron/StringerSDR MZZA99057Web · wornTNN - DURING 1/2D CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, WORN WAS FOUND ON LEFT SIDE AFTER AIRSTAIR TORQUE BOX HORIZONTAL WEB AT BS 1273. THE DAMGED WEB OF AFTER AIRSTAIR TORQUE BOX HORIZONTAL WEB WAS REPAIRED PER B727 SRM 51-40-2 FIGURE 1. (M)Mar 12, 1999 · N625DH · Boeing 727264 · Fuselage Miscellaneous StructureSDR 99ZZZM302Battery Charger · inoperativeDURING PREFLIGHT, FOUND THE FIRST TEN ROWS OF EGRESS LIGHTS INOPERATIVE. REMOVED AND REPLACED FORWARD BATTERY CHARGER PER MM 33-50. (M)Feb 3, 1999 · N764AT · Boeing 727264 · Emergency LightingSDR MZZA98186Accessory Unit · failedFLT 891 - MNL - AFTER TAKEOFF GEAR LEVER WOULD NOT RETRACT. GEAR HANDLE WOULD NOT PASS OFF POSITION. DUMP FUEL AND RETURN TO MNL. MAINTENANCE T/S SYSTEM FOUND L/G ACCESSORY UNIT AT FAULT. REMOVED AND REPLACED L/G ACCESSORY UNIT AND PERFORMED OPS CHECKED PEJul 20, 1998 · N623DH · Boeing 727264 · Landing Gear Retraction/Extension SystemSDR MZZA98160Actuator · rupturedMNL - FLT 876/27 - AIRCRAFT AIR RETURNED DUE TO LOSS OF A-SYSTEM HYDRAULIC FLUID. FOUND NR 1 LE FLAP ACT RUPTURED. LOG PAGE REMAINS OPEN AND NOT ENTERED, AWAITING SPARES. FLIGHT CONTINUED USING AIRCRAFT 435. (X)May 27, 1998 · N625DH · Boeing 727264 · Leading Edge Slat ActuatorSDR MZZA98158Skin · puncturedDURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, PUNCTURE WAS FOUND ON RT ELEVATOR TAB UPPER SKIN AT ELEV STA 110. THE DAMAGED SKIN 0.5 INCH DIAMETER WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. (X)Apr 30, 1998 · N625DH · Boeing 727264 · Elevator, Tab StructureSDR MZZA98157Skin · gougedTNN - DURING S-CHECK INSPECTION, ON AIRCRAFT AT AIR ASIA, GOUGE WAS FOUND ON RT WING T/E INBOARD FOREFLAP UPPER SKIN EXISTING REPAIR DOUBLER AT WBL 88. THE DAMAGED EXITING REPAIR DOUBLER WAS REMOVED AND REPAIRED PER B727 SRM 51-40-6. (X)Apr 30, 1998 · N625DH · Boeing 727264 · Trailing Edge FlapsSDR MZZA98155Skin · delaminatedTNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON RT WING INBOARD T/E FOREFLAP T/E LOWER SKIN AT WBL 88. THE DAMAGED SKIN 4 INCHES BY 5 INCHES IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. (X)Apr 30, 1998 · N625DH · Boeing 727264 · Trailing Edge FlapsSDR MZZA98154Skin · gougedTNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, GOUGE WAS FOUND ON RT WING T/E INBOARD FOREFLAP NOSE SKIN AT WBL 240. THE GOUGED SKIN WAS STOP DRILLED AND REPAIRED PER B727 SRM 57-50-4 FIGURE 1. (X)Apr 30, 1998 · N625DH · Boeing 727264 · Trailing Edge FlapsSDR MZZA98156Skin · delaminatedTNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON RT WING NR 8 SPOILER T/E UPPER SKIN. THE DAMAGED SKIN 9 INCHES BY 11.5 INCHES IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. (X)Apr 28, 1998 · N625DH · Boeing 727264 · SpoilersSDR MZZA98153Web · cannedTNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, OIL CANNING FOUND ON AFT AIRSTAIR RT TORQUE BOX INBOARD WEB. RT SIDE BETWEEN BS 1233 AND BS 1253. RT SIDE BETWEEN BS 1282 AND BS 1313. THE AFT AIRSTAIR RT TORQUE BOX INBOARD WEB OIL CANNING AREAS AND Apr 28, 1998 · N625DH · Boeing 727264 · Fuselage Miscellaneous StructureSDR MZZA98152Web · cannedTNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIS, OIL CANNING WAS FOUND ON AFT AIRSTAIR LT TORQUE BOX INBOARD WEB. LT SIDE BETWEEN BS 1293 AND BS 1323. LT SIDE BETWEEN BS 1243 AND BS 1283. REF: OPERATOR CONTROL NR 98ZZZX____. (X)Apr 28, 1998 · N625DH · Boeing 727264 · Fuselage Miscellaneous StructureSDR 98ZZZX2201Web · cannedTNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIS, OIL CANNING WAS FOUND ON AFT AIRSTAIR LT TORQUE BOX INBOARD WEB. LT SIDE BETWEEN BS 1293 AND BS 1323. LT SIDE BETWEEN BS 1243 AND BS 1283. REF: OPERATOR CONTROL MZZA98152.Apr 28, 1998 · N625DH · Boeing 727264 · Fuselage Miscellaneous StructureSDR 98ZZZX2200Web · cannedTNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, OIL CANNING FOUND ON AFT AIRSTAIR RT TORQUE BOX INBOARD WEB. RT SIDE BETWEEN BS 1233 AND BS 1253. RT SIDE BETWEEN BS 1282 AND BS 1313. THE AFT AIRSTAIR RT TORQUE BOX INBOARD WEB OIL CANNING AREAS AND Apr 28, 1998 · N625DH · Boeing 727264 · Fuselage Miscellaneous StructureSDR MZZA98101Control Cable · misinstalledKUL - RT AILERON BODY CABLE SYSTEM, AFT QUADRANT ABOVE RT WHEEL WELL FOUND TO HAVE CABLES INSTALLED ON WRONG GROOVES IAW MM 27-61-11, PARA 71 PLS NOTE THAT RETAINERS STILL HAD ORIGINAL BOEING TAMPER PROOF SEALANT. CABLES SWAPPED IN GROOVES IAW MM 27-62-11, BOMar 2, 1998 · N623DH · Boeing 727264 · Aileron Control SystemSDR 98ZZZM361Battery Pack · dischargedDURNG P/F, FOUND RT AFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK. (M)Feb 27, 1998 · N763AT · Boeing 727264 · Emergency LightingSDR 98ZZZM360Light · inoperativeDURING P/F, FOUND EMERGENCY LIGHT OVER L-1 DOOR INOP. REMOVED AND REPLACED EMERGENCY LIGHT OVER L-1 DOOR. (M)Feb 27, 1998 · N763AT · Boeing 727264 · Emergency LightingSDR MZZA98103Mounting Box · crackedKUL - CRACK ON NR 2 KRUEGER FLAP ACTUATOR MOUNTING BOX ON LOWER OUTBOARD SIDE. LEFT WING NR 2 LE FLAP ACTUATOR MOUNTING BOX OUTBOARD WEB FABRICATED IAW 727 DWG 65-16275. ALODINED AND PRIMED IAW MM 51-20-2. REMOVED AND INSTALLED WITH NEW WEB IAW SRM 51-30-2.Feb 23, 1998 · N623DH · Boeing 727264 · Leading Edge Slat ActuatorSDR MZZA98097Spring · brokenKUL - RIGHT INBOARD FOREFLAP INBOARD SEQUENCE CARRIAGE TOGGLE DETENT SPRING BROKEN. SPRING REPLACED IAW MM 27-51-4. FUNCTIONAL CHECK CUTOUT SATISFACTORY. (M)Feb 23, 1998 · N623DH · Boeing 727264 · Trailing Edge Flap Control SystemSDR MZZA98098Bushing · corrodedKUL - LEFT MLG AFT RUNNION BUSHING FOUND, HAS SIGN OF CORROSION. LEFT MLG AFT TRUNNION BUSHING REPLACED IAW SRM 20-50-03. (M)Feb 21, 1998 · N623DH · Boeing 727264 · Main Landing Gear Attach SectionSDR MZZA98102Drum · crackedKUL - LOST MOTION DEVICE UPPR CABLE DRUM FOUND CRACKED AT CABLE RETAINER SLOT. DRUM REPLACED IN LOST MOTION DEVICE IAW OHM 27-10-03. (M)Feb 20, 1998 · N623DH · Boeing 727264 · Aileron Control SystemSDR MZZA98108Sill · corrodedKUL - AFT CARGO DOOR LOWER SILL T-CHORD BADLY CORRODED ON PREVIOUS BLENDED OUT AREAS. REPAIR CARRYOUT PER ECRA EC 5310-02509. (M)Feb 19, 1998 · N623DH · Boeing 727264 · Fuselage Miscellaneous StructureSDR MZZA98105Web · failedKUL - WEB BUCKLED BETWEEN STA 28L AND 28R AT FS 620 FWD CARGO. FABRICATED REPAIR DOUBLER AND INSTALLED IAW SRM 51-40-3 FIG 1. (M)Feb 19, 1998 · N623DH · Boeing 727264 · Fuselage Miscellaneous StructureSDR MZZA98100Stringer · crackedKUL - CRACK AT 'Z' SECTION AT WS 686.5 AT AFT OF VENT BOX, MOUNTING POINT BETWEEN 'Z' SECTION AND WEB LEFT WING. FABRICATED EXTRUSION IAW EA 5762-01050. ALODINED AND PRIME IAW 51-20-2. INSTALLED EXTRUSION IAW EA 5762-01050. (M)Feb 18, 1998 · N623DH · Boeing 727264 · Wing, Longeron/StringerSDR MZZA98099Stringer · crackedKUL - CRACK AT 'Z' SECTION AT WS 656.5 AT AFT OF VENT BOX, MOUNTING POINT BETWEEN 'Z' SECTION AND WEB LT WING. FABRICATED EXTRUSION IAW EA 5762-01050. ALODINED AND PRIME IAW 51-20-2. INSTALLED EXTRUSION IAW EA 5762-01050. (M)Feb 18, 1998 · N623DH · Boeing 727264 · Wing, Longeron/StringerSDR MZZA98096Gasket · missingKUL - ALL LEFT AND RT NON STRESSED WING FUEL TANK PANELS FOUND WITH MISSING KNITTED BONDING GASKETS, FOLLOWING PANEL REMOVAL. NEW KNITTED GASKETS INSTALLED IAW MM 28-11-21. (M)Feb 18, 1998 · N623DH · Boeing 727264 · Fuel StorageSDR MZZA98111Sill · corrodedKUL - AFT CARGO SILL FWD CORNER AREA BADLY CORRODED. WEB REPAIR CARRYOUT PER SRM 53-10-1. (M)Feb 17, 1998 · N623DH · Boeing 727264 · Fuselage Miscellaneous StructureSDR MZZA98104Rib · crackedKUL - NR 6 SLAT HAS CRACKING IN THE FOLLOWING PLACES UPPER SKIN AT OUTBOARD HOOK AFT FASTENER HOLE (2 CRACKS), EYE END ATTACH INBOARD RIB AT UPPER FWD CORNER AND LOWER AFT CORNER. REPAIR CARRIED OUT TO THE UPPER SKIN OF OUTBOARD HOOK AS PER SRM 57-50-3. REPLFeb 17, 1998 · N623DH · Boeing 727264 · Leading Edge DevicesSDR MZZA98095Angle · crackedKUL - NR 6 KRUEGER LEADING EDGE FLAP ACTUATOR TRUNNION MOUNTING BOX STRUCTURE FOUND CRACKED AT INBOARD LOWER AND OUTBOARD UPPER CORNERS. INBOARD AND OUTBOARD ANGLES FABRICATED IAW BOEING DRAWING 65-16275 AND INSTALLED IAW SRM 51-30-2. ACTUATOR REINSTALLED ANFeb 17, 1998 · N623DH · Boeing 727264 · Wing Miscellaneous StructureSDR MZZA98110Beam · corrodedKUL - LEFT HORIZONTAL STAB TRAILING EDGE UPPER BEAM IS CORRODED EXFOLIATED AT FWD H/CHANNEL. CORROSION REMOVED IAW SRM 51-10-6 FOUND OUT OF LIMITS SRM 51-10-1 PAGE 1 FLANGE THICKNESS LIMIT. LEFT H/STAB, TRAILING EDGE UPPER REPLACED, NEW ROWS OF RIVET INSTALLFeb 15, 1998 · N623DH · Boeing 727264 · Horizontal Stabilizer StructureSDR MZZA98076Pcu Cover · crackedKUL - Q-CHECK - DURING REASSEMBLY OF AILERON PCU LINKAGE ASSEMBLY, LOWER COVER WAS FOUND CRACKED AT LOWER RIG PIN HOLE. REPAIR TO LOWER COVER CUT-OUT IAW ECRA 5270C072. PLEASE REFER TO ROUTINE CARD NR 552 FOR REASSEMBLY OF PCU LINKAGES. (X)Feb 9, 1998 · N622DH · Boeing 727264 · Aileron Control SystemSDR MZZA98075Bracket · damagedKUL - Q-CHECK - DURING REPLACEMENT OF RT AILERON BUS CABLE, FOUND RT AILERON BUS CABLE TURNAROUND PULLEY BRACKET DAMAGED. PLATES FABRICATED AND INSTALLED IAW BOEING DRAWING 69-25882. REFER HNRC 869821 FOR CABLE REPLACEMENT. (X)Feb 9, 1998 · N622DH · Boeing 727264 · Aileron Control SystemSDR MZZA98071Pin · missingKUL - Q-CHECK - LEADING EDGE SLAT/FLAP CONTROL VALVE FOUND TO HAVE MISSING SPLIT PIN IN INPUT LEVER BOLT AND NUT INSTALLED FINGER TIGHT. BOLT AND NUT TORQUED AND SPLIT PINNED IAW MM 27-81-81. (X)Feb 2, 1998 · N622DH · Boeing 727264 · Leading Edge Slat Control SystemSDR MZZA98069Gasket · missingKUL - Q-CHK - FOLLOWING REMOVAL OF ALL NON-STRESSED WING FUEL TANK ACCESS PANELS FOUND NO PANELS HAD ALUMINUM KNITTED GASKETS FITTED. BONDING GASKET REINSTALLED PRIOR TO PANEL REPLACEMENT. FUEL LEAK CHECK CARRIED OUT. (X)Feb 2, 1998 · N622DH · Boeing 727264 · Fuel StorageSDR MZZA98077Rib · crackedKUL - Q-CHECK - RIGHT WING OUTBOARD F/FLAP CENTER STABILIZING TRACK - SUPPORT FITTING INBOARD AND OUTBOARD TRACK RIBS - OUTBOARD RIB HAS .50 INCH CRACK AT FORWARD RIVET HOLE AND INBOARD RIB HAS EXCESSIVE WEAR IN LUG RADIUS. BOTH FITTINGS REPLACED IAW SRM 51-3Jan 29, 1998 · N622DH · Boeing 727264 · Wing, Rib/BulkheadSDR 98ZZZX1074Rib · crackedKUL - Q-CHECK - RIGHT WING OUTBOARD F/FLAP CENTER STABILIZING TRACK - SUPPORT FITTING INBOARD AND OUTBOARD TRACK RIBS - OUTBOARD RIB HAS .50 INCH CRACK AT FORWARD RIVET HOLE AND INBOARD RIB HAS EXCESSIVE WEAR IN LUG RADIUS. BOTH FITTINGS REPLACED IAW SRM 51-3Jan 29, 1998 · N622DH · Boeing 727264 · Wing, Rib/BulkheadSDR MZZA98078Angle · crackedKUL - Q-CHK - NR 6 KRUEGER LEADING EDGE FLAP ACTUATOR TRUNNION MOUNTING BOX IS CRACKED AT LOWER INBOARD CORNER. FORMED SECTION FABRICATED IAW BOEING DRAWING AND INSTALLED IAW SRM 51-30-2. ACTUATOR REINSTALLED AND FUNCTIONAL CHECK CARRIED OUT. (X)Jan 26, 1998 · N622DH · Boeing 727264 · Leading Edge Slat ActuatorSDR MZZA98073Angle · crackedKUL - Q-CHECK - NR 2 SLAT LOWER SKIN ATTACH ANGLE FOUND WITH TWO CRACKS AT TAI DUCT CUT-OUT AT SLAT STA 271. FORMED SECTION REPAIR CUT-OUT IAW ECRA 5750-02901. (X)Jan 26, 1998 · N622DH · Boeing 727264 · Leading Edge DevicesSDR MZZA98072Rib · crackedRIGHT OUTBOARD AILERON INBOARD HINGE SUPPORT AT WBL 498.4 - UPPER AFT FLANGE OF CHORD IS CRACKED. FORMED SECTION REPAIR CUT-OUT IAW ECRA EC 5720-00196. (X)Jan 25, 1998 · N622DH · Boeing 727264 · AileronsSDR MZZA98070Nut · missingKUL - Q-CHECK - DURING INSPECTION OF RT WING HIP TANK, FOUND A BOLT MIGRATED AND BOTH NUTS MISSING OFF SUPPORT STRUT AT WBL 74 THAT SECURES RT AFT WING TERMINAL BOTTLE PIN FITTING. MIGRATED BOLT INSPECTED AND REINSTALLED. BOTH NUTS REPLACED IAW SRM 51-30-2. Jan 25, 1998 · N622DH · Boeing 727264 · Wing, Fuselage Attach FittingsSDR MZZA98074Stiffener · corrosionKUL - C-CHECK - CORROSION FOUND AT RT WING SPAR STIFFENER OF FRONT SPAR NR 2 FROM WS 251 (NR 5 KRUGER FLAP AREA). CORROSION REMOVED AND FOUND BEYOND LIMIT IAW SRM 57-10-1 AREA 3 INCHES BY 1.5 INCHES BY 0.024 INCH. STIFFENER REPLACED IAW SRM 51-30-2. HYDRAULJan 21, 1998 · N622DH · Boeing 727264 · Wing Miscellaneous StructureSDR 98ZZZM407Light · inoperativeIND - DURING PRE-FLIGHT, THE AFT ENTRY FOR AIRSTAIR EGRESS LIGHT IS INOP. REMOVED AND REPLACED LIGHT ASSY AND OPS CHECK NORMAL. (M)Jan 4, 1998 · N765AT · Boeing 727264 · Emergency LightingSDR MZZA97266Floor Panel · corrodedHKG - ON WALK AROUND DISCOVER CORROSION AT STATION 440 BETWEEN STRINGER STRINGER 28R AND STRINGER 27R. OPENED FORWARD CARGO FLOOR PANEL AND INSEPCTED DAMAGED AREA. THERE IS NO DAMAGE TO THE STRINGER AND FRAME WEB ASSEMBLY. CUTOUT DAMAGED AREA 2.4 INBY BY 2.Oct 29, 1997 · N624DH · Boeing 727264 · Fuselage Floor PanelSDR MZZA97262Mounting Plate · leakMANILA - FLT 0875 - LOG PAGE 7967654 - ON APPROACH INTO MANILA, CREW NOTICED A-HYDRAULIC SYSTEM DROPPED TO 1-3/4 GALLONS. CREW THEN FOLLOWED ABNORMAL PROCEDURES AND LANDED WITH NO ABNORMALITIES. MAINTENANCE FOUND FLUID LOSS DUE TO LEAKAGE AT LOWER RUDDER PCUSep 30, 1997 · N623DH · Boeing 727264 · Rudder Control SystemSDR EISA97202Stiffener · crackedRIGHT PYLON VERTICAL STIFFENER CRACKED THROUGH AT BOTTOM HOLE. REMOVED STIFFENER AND FABRICATED NEW. INSTALLED PER SRM 55-30-04. TT, 55,940:30 HOURS. TC: 32,713. (X)Sep 22, 1997 · N15DF · Boeing 727264 · Nacelle/Pylon StructureSDR EISA97201Seat Track · corrodedSEAT TRACK CORRODED FS 950A TO FS 1010, LT OTBD TRACK. INSTALLED NEW SEAT TRACK FROM FS 950A - FS 1010 PER SRM 53-10-05. TT, 55,940:30 HOURS. TC: 32,713. (X)Sep 22, 1997 · N15DF · Boeing 727264 · Fuselage, Seat/Cargo Attach FittingsSDR EISA97200Seat Track · corrodedSEAT TRACK CORROSION FS 950B LT INBD TRACK. INSTALLED NEW TRACK SECTION PER SRM 53-10-05. TT, 55,940:30 HOURS. TC: 32,713. (X)Sep 22, 1997 · N15DF · Boeing 727264 · Fuselage, Seat/Cargo Attach FittingsSDR EISA97199Seat Track · corrodedSEAT TRACK CORROSION FS 950 RT INBD TRACK. REMOVED CORROSION SECTION AND INSTALLED REPAIR SECTION PER SRM 53-10-05. TT, 55,940:30 HOURS. TC: 32,713. (X)Sep 22, 1997 · N15DF · Boeing 727264 · Fuselage, Seat/Cargo Attach FittingsSDR EISA97198Seat Track · corrodedSEAT TRACK CORROSION FS 890 RT INBD TRACK. REMOVED CORROSION SECTION AND INSTALLED REPAIR SECTION PER SRM 53-10-05. TT, 55,940:30 HOURS. TC: 32,713. (X)Sep 22, 1997 · N15DF · Boeing 727264 · Fuselage, Seat/Cargo Attach Fittings
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