Boeing 727-225

Service difficulty reports · 4,226

Newest first. General aviation reporting is voluntary.

Query with SQL
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 = '727225'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR MYW2003F00000Light · inoperativeDURING PRE-FLIGHT TRANSIT CHECK FLIGHT TRANSIT AFT AIRSTAIRS OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED AFT AIRSTRAIRS OVERHEAD EMERGENCY LIGHT ASSY IAW MM. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.Jan 2, 2003 · N804MA · Boeing 727225 · Emergency LightingSDR 2003F00110Battery Pack · dischargedDURING PREFLIGHT TRANSIT CHECK FLIGHT TRANSIT RIGHT CENTER OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED RIGHT OVERWING EMERGENCY LIGHT BATTERY PACK ASSEMBLY IAW MM 33-50-0. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)Jan 2, 2003 · N804MA · Boeing 727225 · Emergency LightingSDR SDR020040Shaft · shearedDURING CLIMB OUT, THROUGH 1000 FT ALT ENGINE NR 1 FLAMED OUT. (FUEL FLOW AND EPR WENT TO ZERO. DURING TAKEOFF ALL ENGINE INDICATIONS WERE NORMAL. C/W AOM PROCEDURES AND RETURNED TO AIRPORT. REMOVED AND REPLACED FUEL CONTROL UNIT AND FUEL PUMP FUEL PUMP UNIDec 24, 2002 · N802MA · Boeing 727225 · Fuel Control/Turbine EnginesSDR DHL2002755011Bulb · burned outAFT CARGO SMOKE INDICATOR ON FORWARD PANEL WILL NOT TEST AS PER AOM. LIGHT WILL NOT PUSH TO TEST EITHER. RESET LAMP ON GLARE SHIELD IAW B-MM 26-16-001. OPS CHECKED GOOD.Dec 17, 2002 · N755DH · Boeing 727225 · Instrument PanelSDR DHL2002755010Switch1) FIRE WARNING BELL FOR ENGINE AND WHEELWELL DETECTOR INTERMITTENT, LIGHTS OK.2) REMOVED AND REPLACED FAULTY BELL CUT-OUT SWITCH & OPS CHECKED IAW B727 M/M 26-11-0. OPS CHECKED GOOD.Dec 12, 2002 · N755DH · Boeing 727225 · Detection SystemSDR DHL2002743015Seat · damagedS/O SEAT NEARLY IMPOSSIBLE TO RELEASE FROM FULL FORWARD POSITION. LUBRICATED S/O SEAT IAW M/M 25-10-41. OPS CHECKED GOOD.Dec 12, 2002 · N743DH · Boeing 727225 · Flight Compartment EquipmentSDR DHL2002743014Seat1) F/O SEATBACK POPS BACKWARD WHEN PRESSURE EXERTED AGAINST IT.2) REMOVED AND REPLACED F/O'S SEAT IAW B-727 M/M 25-10-42. OPS CHECKED GOOD.Dec 12, 2002 · N743DH · Boeing 727225 · Flight Compartment EquipmentSDR DHL2002743517Fuel Control · malfunctionedDURING ACCEPTANCE FLIGHT AFTER C CHECK, AFTER LANDING BROUGHT ENGINE INTO REVERSE THRUST. TOOK ENGINE OUT OF REVERSER PUSH THRUST LEVERS FORWARD AND ENGINE NR 3 FLAMED OUT. REMOVED AND REPLACED NR 3 ENGINE FCU AND FUEL PUMP, FUEL HEATER ASSY. OPS AND LEAK CHDec 8, 2002 · N743DH · Boeing 727225 · Fuel Control/Turbine EnginesSDR DHL7432002515Stringer · corrodedDURING C-CHECK, STRINGER 27 LEFT STATION 1010-1030 IS CORRODED AT FASTENER HOLES. CUT-OUT DAMAGED STRINGER BS 1010-1030 APPROXIMATELY 20 INCHES IAW B-727 SRM 53-10-3 FIG 1. FABBED NEW STRINGER AND SPLICES 2 EACH IAW B-727 SRM 53-10-3 FIG 1. INSTALLED REPAIRNov 24, 2002 · N743DH · Boeing 727225 · Fuselage Main, Longeron/StringerSDR DHL2002742010Clamp · looseFIRE DETECTOR CIRCUIT GROUND NR 3 LIGHT ILLUMINATED IN FLIGHT. FOUND FIRE DETECTOR LOOP MOUNT CLAMP UNSECURED, RESECURED OPS CHECKED GOOD IAW 26-11-01.Nov 23, 2002 · N742DH · Boeing 727225 · Fire DetectionSDR 2003F00136Battery Pack · dischargedDURING P/T FOUND DOOR 2 AISLE EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT BATTERY PACK, LIGHTS OPS CHECKS GOOD IAW AMM 33-50-00. (M)Nov 17, 2002 · N889MA · Boeing 727225 · Emergency LightingSDR 2003F00105Light · inoperativeDURING P/T FOUND FORWARD MOST E-PATH LIGHT STRIP OUT. REMOVED AND REPLACED E-PATH LIGHT STRIP, OPS CHECK NORMAL. (M)Nov 17, 2002 · N889MA · Boeing 727225 · Emergency LightingSDR DHL2002743516Skin · crackedDURING C CHECK, UPPER RUDDER TAB LE SKIN CLOSE OUT IS CRACKED AND CORRODED. REMOVED UPPER RUDDER TAB FOR ACCESS IAW B-727 M.M. 27-20-11. REMOVED 6 DAMAGED SKINS, LOCATED, AND DRILLED NEW SKINS IAW B-727 SRM 55-40-2. PARTS ALODINED AND PRIMED IAW B-727 SRM Nov 16, 2002 · N743DH · Boeing 727225 · Rudder, Plate/SkinSDR DHL2002743513Frame · corrodedDURING C CHECK, AFT SIDE OF BS 1166 FRAME, STR 27 LT TO 28 LT IS CORRODED. REMOVED LOWER ANGLE AND STIFFNER FOR ACCESS AND FOUND CORRODED OUT OF LIMITS IAW B-727 SRM 53-10-1 CUT-OUT DAMAGE ON WEB AND FABRICATED FILLER AND NEW STIFFNER REPAIR DOUBLER IAW B-727Nov 16, 2002 · N743DH · Boeing 727225 · Fuselage Main, FrameSDR 2002F01122Battery Pack · dischargedDURING PREFLIGHT TRANSIT, FOUND LEFT AFT OUTSIDE EGRESS LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. OPERATIONAL CHECKED GOOD IAW MM 33-50-01. (M)Nov 13, 2002 · N803MA · Boeing 727225 · Emergency LightingSDR GAIA02155OPActuator · crackedDURING CLIMB-OUT OF SCHEDULE FLIGHT NR 705 FROM IAH-FWA, THE CREW NOTICED THE LOSS OF SYSTEM 'A' HYDRAULIC QUANTITY, AND PRESSURE WENT TO ZERO. THE CREW DECLARED AND EMERGENCY AND RETURNED IAH. THE AIRCRAFT LANDED WITHOUT ANY INCIDENT. MAINTENANCE FOUND THENov 12, 2002 · N936PG · Boeing 727225 · Leading Edge Slat ActuatorSDR DHL2002743509Frame · chafedDURING C CHECK, HYDRAULIC SUPPLY LINE CHAFED INTO 1150 FRAME AT STR 20 LT DUE TO CLAMP STAND-OFF BRACKET. CLEANED CHAFED AREA IAW B-727 SRM 51-10-6. FOUND TO BE OUT OF LIMITS IAW B-727 SRM 53-10-1. CUT-OUT DAMAGE FRAME IAW B-727 SRM 53-10-4. AND FABRICATEDNov 12, 2002 · N743DH · Boeing 727225 · Fuselage Main, FrameSDR DHL2002743506Frame · bentDURING C CHECK, STA. 950F FRAME IS BENT AND BUCKLED AT STR. 26 LT IN AFT CARGO BAY. CUT-OUT DAMAGE FRAME IAW B-727 SRM 53-10-4. FABRICATED REPAIR ANGLE IAW B-727 SRM 53-10-2. TREATED AND PRIMED IAW B-727 SRM 51-10-2. INSTALLED REPAIR ANGLE IAW B-727 SRMNov 12, 2002 · N743DH · Boeing 727225 · Fuselage Main, FrameSDR DHL2002743501Frame · dentedDURING C CHECK, FWD. CARGO FRAME BS 600 HAS A DENT INTO THE RADIUS AT STR 25 LT. PART ALODINED AND PRIMED IAW B-727 SRM 51-10-2. INSTALLED PART IAW B-727 SRM 51-30-2. REMOVED AND REPLACED FRAME SPLICE IA/W B-727 SRM 53-10-2 FIG. 3.Nov 12, 2002 · N743DH · Boeing 727225 · Fuselage Main, FrameSDR DHL2002743500Skin · corrodedDURING C CHECK, AFT CARGO BAY HAS A CORROSION SPOT ON FRAME TO FUSELAGE BS 1070 STR 29R FWD SIDE. REMOVED SURFACE CORROSION WITH A MATERIAL LOSS 0.28 AND IS OUT OF LIMITS IAW B-727 SRM 53-10-1. FABRICATED ANGLE REPAIR DIMENSIONS 3 X 2 X 1 INCHES. ALODINEDNov 12, 2002 · N743DH · Boeing 727225 · Fuselage Main, Plate/SkinSDR DHL2002743514Fitting · crackedDURING C CHECK, LT WING NR 4 SLAT ACTUATOR PISTON END ATTACH FITTING LOOSE FASTENERS ALSO INTERNAL ANGLES 2 EACH PLUS RIB ARE CRACKED. REMOVED NR 4 SLAT IAW B-727 M.M. 27-81-11. CUT-OUT AREA IN AFT LOWER. SKIN IAW B-727 SRM 57-50-3 AND REMOVED 2 DAMAGED REPANov 11, 2002 · N743DH · Boeing 727225 · Leading Edge DevicesSDR DHL2002743512Duct · corrodedDURING C CHECK, NR 2 ENGINE INLET "S" DUCT LOWER. ACCESS DOOR, INSIDE INTERIOR DOOR SKIN IS CORRODING PLUS PEELING ALONG DOOR SKIN EDGES. REMOVED CENTER ENGINE INLET ACCESS DOOR IAW B 727 MM 52-40-31. REMOVED INNER SKIN, LOCATED, AND DRILLED NEW SKIN AS PER SNov 11, 2002 · N743DH · Boeing 727225 · Engine Air Intake SystemSDR DHL2002743510Angle · crackedDURING C CHECK, LT WING LE LOWER STA 130.7 ANGLE CRACKED ABOUT 1 1/2 INCHES LONG. REMOVED NR 3 LT FLAP IAW B-727 MM 27-81-1. CUTOFF ANGLE LT WING LE STA. 130.7 IAW B-727 SRM 51-10-3. MADE NEW ANGLE FILLER AND ANGLE REPAIR IAW B-727 SRM 51-40-3. RE-INSTALNov 11, 2002 · N743DH · Boeing 727225 · Leading Edge DevicesSDR DHL2002743511Structure · lightning strikeDURING C CHECK, LIGHTNING STRIKE AT FS 198, STR 19 LT. MECHANICALLY REMOVED PAINT FOR ACCESS IAW B-727 M/M 51-20-1. BLEND LIGHTNING STRIKE IAW B-727 53-30-1 FOUND TO BE OUT OF LIMITS IAW B-727 SRM 53-30-1. CUT OUT DAMAGED AREA (UPPER SKIN) AND MADE STRUCTUNov 9, 2002 · N743DH · Boeing 727225 · Fuselage Main, StructureSDR DHL2002743503Skin · gougedDURING C CHECK, GOUGE IN FUSELAGE SKIN AT FS 1195 STR. 25 LT, CHEMICALLY REMOVED POINT FOR ACCESS IAW B-727 M/M 51-20-2. BLENDED GOUGE ON FUSELAGE SKIN IAW B-727 SRM 53-30-3 MEASURE DAMAGE AREA AS PER 51-30-1 FABRICATED DOUBLER FOR CUT-OUT IAW B-727 SRM 5Nov 9, 2002 · N743DH · Boeing 727225 · Fuselage Main, Plate/SkinSDR DHL2002743508Skin · gougedDURING C CHECK, SEVERAL GOUGES IN FUSELAGE SKIN FS 360 TO 380 STR. 18 LT. DAMAGE FOUND TO BE OUT OF LIMITS IAW B-727 SRM 53-30-3. REMOVED FASTENER AT FUSELAGE SKIN BS 360 TO 380 ABOVE STR 18 LT IAW B-727 SRM 51-30-2. CUT-OUT DAMAGED AREA IAW B-727 SRM 53-Nov 8, 2002 · N743DH · Boeing 727225 · Fuselage Main, Plate/SkinSDR DHL2002743507Stringer · lightning strikeDURING C CHECK, LIGHTNING STRIKE AT STA. 227 STR. 19 LT. CHEMICALLY REMOVED PAINT FOR ACCESS MM 51-20-1, BLENDOUT IAW B-727 SRM 53-30-1. MATERIAL LOSS FOUND OUT OF LIMITS IAW B-727 SRM 53-10-1. CUT-OUT DAMAGE AREA, FABRICATED DOUBLER IAW B-727 SRM 53-30-3. Nov 8, 2002 · N743DH · Boeing 727225 · Fuselage Main, Longeron/StringerSDR DHL2002743504Skin · dentedDURING C CHECK, C-1 DOOR EXTERIOR SKIN DENTED AT LOWER AFT CORNER. CUT-OUT DAMAGE AREA AND FABRICATED NEW DOUBLER IAW B-727 SRM 52-00-3 TREATED AND PRIMED IAW B-727 SRM 51-10-2.Nov 8, 2002 · N743DH · Boeing 727225 · Cargo/Baggage DoorsSDR DHL2002743502Skin · dentedDURING C CHECK, DENT IN FUSELAGE SKIN AT FS 1120 SRT 18RT. CUT-OUT DAMAGE AREA, AND FABRICATED FILLER IAW B-727 SRM 53-30-3 AND FABRICATED DOUBLER IAW B-727 SRM 53-30-3. ALODINED AND PRIMED IAW B-727 SRM 51-10-2. INSTALLED FILLER AND DOUBLER IAW B-727 SRM 51Nov 8, 2002 · N743DH · Boeing 727225 · Fuselage Main, Plate/SkinSDR CA021122005Thrust Reverser · damaged(CAN) ON LANDING IT WAS OBSERVED THE TRAIL SKID INDICATOR ILLUMINATED INDICATING A TAIL STRIKE. THE AIRCRAFT HAD LANDED WITHOUT INCIDENT. A DETAILED INSPECTION FOUND DAMAGE TO THE FOLLOWING: TAIL SKID ASSEMBLY, NR 3 VHF COMM. ANTENNA, NR 2 ENGINE THRUST RENov 7, 2002 · Boeing 727225 · Engine Thrust ReverserSDR 2003F00142Power Supply · dischargedDURING PREFLIGHT TRANSIT, FOUND EPL SYSTEM INOPERATIVE AT L2 DOOR AND ROWS 26 ABC THROUGH 30 ABC. TROUBLESHOT EPL SYSTEM. REMOVED AND REPLACED EPL POWER SUPPLY. OPERATIONAL CHECKED IAW 33-59-00. AIRCRAFT RETURNED TO SERVICE. (M)Nov 4, 2002 · N804MA · Boeing 727225 · Emergency LightingSDR C7WA200200039Duct · looseNR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED ON TAKEOFF WHILE CLIMBING 200 FEET. EPRS 2.08/2.11. THROTTLES BACKED OFF TO 1.7 EPR LIGHT EXTINGUISHED. TROUBLESHOOTING FOUND DUCT CONNECTION TO NR 3 ENGINE PRECOOLER LOOSE. TIGHTENED, NO FURTHER LEAKS, MM 36-11Oct 31, 2002 · N8887Z · Boeing 727225 · Pneumatic Distribution SystemSDR C7WA200200038Bracket · misinstalledUPON GEAR RETRACTION, RED RIGHT GEAR LIGHT AND RED DOORS LIGHT REMAIN ILLUMINATED, AS WELL AS SECOND OFFICERS AMBER RIGHT GEAR DOOR LIGHT, CYCLED GEAR. UPON TROUBLESHOOTING FOUND INBOARD DOOR DRIVE ROD BRACKET INSTALLED BACKWARDS. REPOSITIONED BRACKET AS PEROct 31, 2002 · N8887Z · Boeing 727225 · Landing Gear Door Retract SectionSDR DHL2002755008Fire Warning · will not testWHEN TESTING FIRE WARNING SYSTEM, SWITCH TO RIGHT NR 2 & 3 ENGINE FIRE WARNING CAPSULES DO NOT LIGHT. PERFORMED OPS CHECK OF ENGINE FIRE WARNING SYSTEM IAW B727 M/M 26-11-01. NO DEFECTS NOTED.Oct 31, 2002 · N755DH · Boeing 727225 · Fire DetectionSDR C7WA200200037Clamp · looseNR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED ON TAKEOFF, EPRS 2.01/2.03 WHEN THROTTLES BACKED OFF TO 1.7 EPR LIGHT EXTINGUISHED. TIGHTENED LOOSE CLAMP IN STRUT AREA PER MM 75-00 AND 20-80-1. (M)Oct 30, 2002 · N8887Z · Boeing 727225 · Pneumatic Distribution SystemSDR C7WA200200036Door · out of rigUPON GEAR RETRACTION RED RIGHT GEAR LIGHT AND RED DOORS LIGHT REMAIN ILLUMINATED. CYCLED GEAR 3 TIMES, NO HELP. AIR TURNBACK. RE-RIGGED RIGHT GEAR DOOR PER MM 32-12-1, PAGE 501-502. GROUND TEST OK. (M)Oct 30, 2002 · N8887Z · Boeing 727225 · Landing Gear Door Retract SectionSDR 2002F01022Pump · malfunctionedDURING ASCENT FROM MIA 30 MINUTES INTO FLIGHT NR 2 'B' SYSTEM HYDRAULIC LOW PRESSURE LIGHT ILLUMINATED. PERFORMED ABNORMAL CHECKLIST, NO BREAKERS POPPED. AIRCRAFT RETURNED TO MIAMI. TROUBLESHOT HYDRAULIC SYSTEM. FOUND CURRENT DRAWS FROM RELAY ON PUMP NR 1 Oct 25, 2002 · N803MA · Boeing 727225 · Hydraulic Pump, AuxiliarySDR GAIA02151STSkin · crackedDURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE RIGHT WING UPPER OUTBOARD LEADING EDGE AT WS 430 HAD A ROW OF FASTENERS WITH CRACKS RUNNING FROM HEAD HOLES AT THE NR 5 SLAT LEADING EDGE. REPAIR WAS ACCOMPLISHED IAW BOEING 727 SRM 57-30-3, FIGURE 4. TOct 24, 2002 · N936PG · Boeing 727225 · Leading Edge DevicesSDR GAIA02150STDoor Frame · crackedDURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE C-1 DOOR CUTOUT AFT RIGHT FRAME HAD A CRACK IN THE SKIN IN TWO PLACES AT STRINGER S26R. REPAIR WAS ACCOMPLISHED IAW BOEING 727 SRM 51-40-2, FIGURE 1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Oct 24, 2002 · N936PG · Boeing 727225 · Fuselage Main, StructureSDR GAIA02149STFrame · dentedDURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE FRAME AT BS 560, STRINGER S25L WAS DENTED. REPAIR WAS ACCOMPLISHED IAW BOEING 727 SRM 51-40-3, FIGURE 1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Oct 24, 2002 · N936PG · Boeing 727225 · Fuselage Main, FrameSDR GAIA02148STFrame · dentedDURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE FRAME AT BS 580, AND IN BETWEEN STRINGER S24L AND S25L WAS DENTED. REPAIR WAS ACCOMPLISHED IAW BOEING 727 SRM 51-40-3, FIGURE 1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Oct 24, 2002 · N936PG · Boeing 727225 · Fuselage Main, FrameSDR GAIA02147STBushing · deterioratedDURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE LEFT AFT BOTTLE PIN BUSHINGS WERE DETERIORATED. THE BUSHINGS WERE REPLACED IAW THE BOEING 727 MM 57-41-11 AND 57-41-1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Oct 24, 2002 · N936PG · Boeing 727225 · Wing, Fuselage Attach FittingsSDR GAIA02146STSkin · crackedDURING A ROUTINE INSPECTION AT FLIGHTSTAR IN JAX, IT WAS DISCOVERED THAT THE C-1 DOOR CUT OUT INNER SKIN WAS CRACKED AT BS 620, STRINGER S25R. REPAIR WAS ACCOMPLISHED IAW BOEING 727 SRM 51-40-2, FIGURE 1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Oct 24, 2002 · N936PG · Boeing 727225 · Fuselage Main, Plate/SkinSDR GAIA02145STSkin · crackedDURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE VENTRAL STAIR CUTOUT, FORWARD RIGHT SIDE HAD A CRACK IN THE RADIUS. REPAIR WAS ACCOMPLISHED IAW BOEING 727 SRM 53-30-3, FIGURE 13. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Oct 24, 2002 · N936PG · Boeing 727225 · Fuselage Main, Plate/SkinSDR GAIA02144STSkin · dentedDURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE LEFT WING NR 2 SLAT NOSE UPPER SURFACE SHOWS A LARGE DENTED AREA ON THE SKIN. REPAIR WAS ACCOMPLISHED IAW BOEING 727 SRM 57-50-3, FIGURE 4. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Oct 24, 2002 · N936PG · Boeing 727225 · Leading Edge DevicesSDR GAIA02143STRib · crackedDURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE LEFT WING NR 4 SLAT INTERIOR RIB WAS CRACKED AT WS 410, OUTBOARD OF THE ACTUATOR ATTACH POINT. REPAIR WAS ACCOMPLISHED IAW BOEING 727 SRM 57-50-3, FIGURE 9. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Oct 24, 2002 · N936PG · Boeing 727225 · Leading Edge DevicesSDR GAIA02142STSkin · crackedDURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE LEFT WING LEADING EDGE UPPER SKIN AT THE NR 3 SLAT GUIDE FITTING CUT OUT WAS CRACKED AND HAD LOOSE FASTENERS. REPAIR WAS ACCOMPLISHED IAW BOEING 727 SRM 57-30-4, FIGURE 9. THE AIRCRAFT WAS RETURNED TO SOct 24, 2002 · N936PG · Boeing 727225 · Wing, Plate/SkinSDR GAIA02141STSkin · delaminatedDURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE LEFT WING NR 7 GROUND SPOILER PANEL WAS DELAMINATED AND HAD HOLES ON THE BOTTOM SIDE OF THE PANEL. REPAIR WAS ACCOMPLISHED IAW BOEING 727 SRM 57-50-6, FIGURE 5. THE AIRCRAFT WAS RETURNED TO SERVICE. (MOct 24, 2002 · N936PG · Boeing 727225 · SpoilersSDR GAIA02140STSkin · crackedDURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE FUSELAGE SKIN WAS CRACKED AT THE FORWARD ENTRY DOOR LOWER HINGE CUT OUT. REPAIR WAS ACCOMPLISHED IAW BOEING 727 SERVICE BULLETIN 727-53-198. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Oct 24, 2002 · N936PG · Boeing 727225 · Fuselage Main, Plate/SkinSDR GAIA02139STFrame · dentedDURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT IN THE FORWARD CARGO LOWER BILGE BS 600, IN BETWEEN STRINGER S28L AND S29L, THE FRAME WAS DENTED. REPAIR ACCOMPLISHED IAW BOEING 727 SRM 51-40-3, FIGURE 1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Oct 24, 2002 · N936PG · Boeing 727225 · Fuselage Main, Frame
Back to Boeing 727-225