Boeing 727-200

Service difficulty reports · 2,835

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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 = '727200'
  ORDER BY difficulty_date DESC"

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SDR 03FDEA01185Skin · gougedNOSE WHEEL WELL SKIN GOUGED AROUND PANEL OPENING 3223 (4 PLACES) 247 - 250. BLENDED GOUGE IN WW SKIN AT BS 237. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. DAMAGE WILL BE REPAIRED ON N00468.Jul 31, 2003 · N215FE · Boeing 727200 · Fuselage Main, BulkheadSDR 03FDEA01183Skin · dentedDENT IN FUSELAGE SKIN BS 1336 ABOVE STR 17R. DENT IN FUSELAGE SKIN BS 1336 ABOVE STR 17R WAS FOUND TO BE OUT OF LIMITS PER SRM 53-30-1. CUT OUT DAMAGE AS PER SRM 53-30-3. FABRICATED REPAIR DOUBLER. ALODINED & PRIMED PER SRM 53-30-3 AND INSTALLED PER SRM Jul 31, 2003 · N215FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 03FDEA01182Keelbeam · crackedRT KEEL BEAM UPPER FLANGE INSIDE APU CUTOUT STA 873 RBL 6 CRACKED. REPAIRED CRACKED RT KEEL BEAM UPPER FLANGE AT BS 873 PER EA 7-5310-54931.Jul 31, 2003 · N215FE · Boeing 727200 · Fuselage Main, KeelSDR 03FDEA01181Skin · gougedNOSE WHEEL WELL SKIN GOUGED AROUND PANEL OPENING 3124 BS 249 LT.Jul 31, 2003 · N215FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 03FDEA01180Skin · gougedNOSE WHEEL WELL SKIN GOUGED AROUND PANEL OPENING NR 3124, BS 247.Jul 31, 2003 · N215FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 03FDEA01177Proximity Sensor · out of adjustLEVEL FL 190 280 KTS OCN LT TURB MAIN CARGO DOOR WARNING LIGHT ILLUMINATED STEADY THEN WENT DIM AND EXTINGUISHED AFTER 30 SEC AS WE COMPLIED WITH RED TABS. CHECKED OPERATION AND INDICATION OF MAIN CARGO DOOR, ONLY DISCREPANCY NOTED WAS INCORRECT ADJUSTMENT Jul 30, 2003 · N280FE · Boeing 727200 · Door Warning SystemSDR 03FDEA01157Floorbeam · bulgedPLATE ON 25G BEAM UNDER FE'S SEAT BULGED. ACCESSED FLOOR PANELS; REMOVED 25G BEAM; REPLACED WITH NEW PART; PER SRM 51-30- 2; REINSTALLED ACCESSED GROUP.Jul 28, 2003 · N494FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 03FDEA01156Frame · damagedDAMAGED FASTENER HOLE ON FRAME AT BS 1070, LBL 22, WL 152. DAMAGED FASTENER HOLES ON FRAME AT BS 1070, LBL-22, WL-152 FOUND TO BE OUT OF LIMITS PER SRM 53-10-1, CUT OUT DAMAGED MATERIAL AND REPAIRED IAW SRM5 1-40-3, FED- EX EA 7-5310-54913.Jul 28, 2003 · N494FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA01154Frame · damagedELONGATED FASTENER HOLE AT B/S 1070, 1050, 1110, LBL-22, WL-152. REPAIRED FRAME AT B.S. 1070, 1050, 1110, LBL 22 (WL 152) IAW SRM 51-40-3 AND EA 7-5310-54911.Jul 28, 2003 · N494FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA01155Frame · damagedDAMAGED FASTENER HOLES ON FRAME AT BS 1110, LBL 22, WL 152. CUT OUT MATERIAL FROM FRAME THAT HAD DAMAGED FASTENERS HOLES AT BS 1110, LBL 22, WL 152. FABRICATED REPAIR FROM HFAB53-FR-011, AND INSTALLED ALL IAW SRM 53-10-1, 51- 40-3, 51-30-5, 51-30-2, AND 51Jul 28, 2003 · N494FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA01141Warning Light · illuminatedAFTER LANDING GEAR RETRACTION, RT MLG DOOR LIGHT REMAINED ILLUMINATED (F/O PANEL+S/O PANEL). RECYCLED GEAR PER RED TABS BUT LIGHT REMAINED ILLUMINATED. R/R RT MLG DOOR WARN SWITCH. R/R CONNECTORS D752 & D4660P.Jul 25, 2003 · N479FE · Boeing 727200 · Landing Gear Position and WarningSDR 03FDEA01131Warning Light · false activationDURING CRUISE GOT LOWER AFT BODY OVERHEAT LIGHT. ENGINE ANTI-ICE WAS OPEN. RED TABS COMPLETED DETERMINED NR 2 ENG ANTI-ICE WAS CAUSE OF OVERHEAT LIGHT. WHEN NR 2 ENGINE ANTI-ICE CLOSED DUCT TEMP DECREASED BELOW 50 DEGREES C OVERHEAT LIGHT WENT OUT. RAN ENJul 24, 2003 · N492FE · Boeing 727200 · Overheat DetectionSDR 03FDEA01132Hydraulic Line · leakingPASSING 17,000 FEET IN A NORMAL CLIMB BOTH HYDRAULIC SYSTEM "A" PUMP LOW PRESSURE LIGHTS CAME ON, FOLLOWED BY A COMPLETE LOSS OF SYSTEM "A" QUANITY. PERFORMED STABILIZERS EXECUTED CHECKLIST IAW QRH. DECLARED IFE AND LANDED UNEVENTFULLY AT IAH. INSTALLED NEWJul 24, 2003 · N246FE · Boeing 727200 · Hydraulic System, MainSDR 03FDEA01130Uplock Sensor · failedAFTER TAKEOFF LEFT GEAR UNSAFE LIGHT REMAINED ILLUMINATED. COMPLIED WITH QRH AND LIGHT REMAINED ILLUMINATED. REMOVED AND REPLACED LEFT MAIN GEAR UP AND LOCKED PROX SENSOR (M827) IAW 727 WDM 32-60-01 SENSOR NEEDS TO BE REINSTALLED AND OP'S CHECKED. REPLACED LJul 23, 2003 · N220FE · Boeing 727200 · Landing Gear Position and WarningSDR 03FDEA01126Light · illuminatedAFT AIRSTAIR LIGHT (AMBER) ILLUMINATED ON DEPARTURE WHILE PASSING 5000 FT -SLAT CLIMB POWER. REMAINED ON AT ALL POWER SETTINGS FOR REMAINDER OF FLIGHT. LIGHT EXTINGUISHED AT TOUCHDOWN.Jul 23, 2003 · N484FE · Boeing 727200 · Door Warning SystemSDR 03FDEA01125Accessory Unit · malfunctionedAFTER TAKEOFF LANDING GEAR LEVER RAISED TO UP POSTION. LANDING GEAR WARNING HORN STAYS ON STEADY WITH RED UNSAFE LIGHTS IN NOSE, LT AND RT LANDING GEAR ANNUNCIATOR. COMPLIED WITH QRH. AFTER 5 MIN IN FLT LIGHTS EXTINGUISHED AND HORN STOPPED. RE-RACKED LANDIJul 22, 2003 · N483FE · Boeing 727200 · Landing Gear Position and WarningSDR 03FDEA01120Shear Tie · corrodedCORROSION ON SHEAR TIE AFT SIDE BS 1130, BETWEEN STR 29 AND 28 LT. REMOVED CORROSION ON SHEAR TIE AFT SIDE 2.20 X 1.80 X .007 INCH MAX, IAW SRM 51-10-6. ORIGINAL MATERIAL .050, OUT OF LIMITS IAW SRM 53-10-1 FIG 1. FABRICATED REPAIR SHEAR TIE OF 7075 T6 .0Jul 21, 2003 · N494FE · Boeing 727200 · Fuselage Main, StructureSDR 03FDEA01121Structure · wornNR 2 ENGINE LT FWD COWL FWD FUSELAGE MATING SURFACE WORN THROUGH AT BS 1350.Jul 21, 2003 · N494FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 03FDEA01119Regulator · malfunctionedSMOKE OR FUMES IN COCKPIT CLIMBING THRU FL 180 NO INDICATION ON S/O PANEL EXCEPT VERY HIGH DUCT PRESSURE L AND R ABOVE 65 PSI. BLEED SWAPPED TO 2 AND 3 LOWERED PRESSURE TO NORMAL RANGE (BETWEEN 30 40 PSI). REMOVED AND REPLACED HIGH PRESSURE SHUT OFF VALVE USJul 19, 2003 · N207FE · Boeing 727200 · Pneumatic Distribution SystemSDR 03FDEA01116Fire Warning · false activationSHORTLY AFTER TAKEOFF WHILE CLIMBING THROUGH 3000 FEET THE FIRE WARNING LIGHT ON THE CENTER FWD PANEL ILLUMINATED, ACCOMPANIED BY THE FIRE WARNING BELL. THE WARNING LASTED FOR APPROXIMATELY 2-3 SECONDS WITH NO OTHER INDICATIONS AND DISCONTINUED SPONTANEOUSLJul 19, 2003 · N266FE · Boeing 727200 · Fire DetectionSDR 03FDEA01108Skin · gougedSKIN GOUGED IN 3 PLACES BS 384 BELOW STR 24L. REPAIRED SKIN BS 384 BELOW STR 25L IAW SRM 53-30-3 DETAIL 1.Jul 18, 2003 · N494FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 03FDEA01112Shear Tie · corrodedCORROSION ON FRAME SHEAR TIE AND FUSE SKIN AT BS 720C LBL 12, WL 150. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REPAIRED SHEAR TIE PER SRM, 51-30-2, 51-10-1, 53-10-1, 51-10-2, 51-10-3.Jul 18, 2003 · N494FE · Boeing 727200 · Fuselage Main, StructureSDR 03FDEA01111Skin · wornNR 2 ENGINE LT FWD COWL FWD FUSELAGE MATING SURFACE WORN THROUGH AT BS 1350. FOUND AREA ON 1350 RING CHORD TO HAVE 100 PERCENT MATERIAL LOSS AND CRACKED OUT OF LIMITS. REMOVED 1350 RING CHORD. DRILLED UP AND INSTALLED NEW 1350 CHORD IAW SRM 51-30-2, 51-30Jul 18, 2003 · N494FE · Boeing 727200 · Nacelle/Pylon, Plate/SkinSDR 03FDEA01109Shear Tie · corrodedCORROSION ON SHEAR TIE AFT SIDE BS 1130, BETWEEN STR 29 AND 28 LT. REMOVED CORROSION ON SHEAR TIE AFT SIDE 2.20 X 1.80 X .007 INCH MAX, IAW SRM 51-10-6. ORIGINAL MATERIAL .050, OUT OF LIMITS IAW SRM 53-10-1 FIG 1. FABRICATED REPAIR SHEAR TIE OF 7075 T6 .050Jul 18, 2003 · N494FE · Boeing 727200 · Fuselage Main, StructureSDR 03FDEA01105Fire Warning · malfunctionedAT 900FT ON CLIMBOUT, FIRE WARNING BELL SOUNDED AND ENGINE FIRE WARNING LIGHTS ON INSTRUMENT PANEL ILLUMINATED FOR 2 SECONDS. NO OTHER INDICATIONS AND ALL OTHER SYSTEMS OPERATED NORMALLY. PERFORMED ENGINE FIRE WARNING TEST. TESTED GOOD. COULD NOT DUPLICATEJul 17, 2003 · N498FE · Boeing 727200 · Fire DetectionSDR 03FDEA01098Control Box · malfunctionedGOT LOWER BODY OVERHEAT LIGHT ON CLIMBOUT UPON DESCENT, LIGHT EXTINGUISHED WITH THROTTLE REDUCTION. T/S IAW 26-14-000-1, FOUND AFT STAIR LT LOOP RUBBING AGAINST STREAMER OF A/C. REPOSITIONED SAME, RERACKED FIRE AND OVERHEAT CONTROL BOX. RAN ENGINES AT GAJul 15, 2003 · N278FE · Boeing 727200 · Detection SystemSDR 03FDEA01096Structure · noisyPASSING 10K MSL, EXTREMELY LOUD SQUEAL APPEARED IN COCKPIT. PRESSURIZATION NORMAL. CLIMBED TO 14K AND SQUEAL REMAINED ON. NOISE WENT OUT PASSING 10K MSL IN DESCENT. SHUT OFF ALL RADIOS & COULD NOT ISOLATE PROBLEM. PRESSURIZED A/C TO 8.5 PSI NO SQUEAL OR HJul 13, 2003 · N283FE · Boeing 727200 · Aircraft StructuresSDR 03FDEA01094Floorbeam · corrodedCORROSION ON FLOOR SUPPORT BS 344, LBL 45, WL 208. CORROSION ON FLOORBEAM BS 344, LBL 45, WL 208. REPAIRED FLOORBEAM IAW SRM 53-10- 1, 51-10-1, 51-30-2 & 53-10-8.Jul 11, 2003 · N467FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 03FDEA01093Skin · lightning strikeN00177 LIGHTNING STRIKE BS 350 BETWEEN STR 2L AND STR 3L. FOUND LIGHTNING STRIKE DAMAGE TO BE OUT OF LIMITS. REPAIRED DAMAGE IAW SRM 53-30-3 AT BS 350 BETWEEN STR 2L AND 3L.Jul 11, 2003 · N467FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 03FDEA01095Switch · defectiveMAIN CARGO DOOR LIGHT ILLUMINATED INFLIGHT AFTER T/O PSI DIFFERENTIAL WAS 1 PSID PACKS OFF, AIRCRAFT DEPRESS MAIN CARGO DOOR LIGHT WENT OUT. AIR TURNBACK, MAIN CARGO DOOR LIGHT WAS INTERMITTENT ON TAXI BACK TO GATE. ADJUSTED THE LOCK SWITCHES PER EO (.040" GJul 11, 2003 · N270FE · Boeing 727200 · Door Warning SystemSDR 03FDEA01082Fire Detector · failedTEN MIN AFTER TAKEOFF THE RED LIGHT IN THE APU FIRE SHUTOFF HANDLE ILLUMINATED. THERE WAS NO RINGING OF THE FIRE BELL IN ACCORDANCE WITH QRH. THE APU FIRE HANDLE WAS PULLED AND APU BOTTLE DISCHARGE BUTTON PUSHED. THE RED LIGHT IN THE APU FIRE HANDLE REMAINEJul 10, 2003 · N477FE · Boeing 727200 · Fire DetectionSDR 03FDEA01085Scavenge Pump · inoperativeNR 2 ENGINE SHUT DOWN IN FLIGHT DUE TO OIL QUANTITY SLOWLY DECREASING TO ZERO. AS OIL QUANTITY DROPPED TO ZERO OIL PRESSURE DROPPED BELOW 40 PSI AND OIL TEMP WAS INCREASING. R & R NR 2 ENG OIL PUMP IAW PRATT & WHITNEY, ENGINE MANUAL 72-00-61. RAN ENGINE AND Jul 10, 2003 · N258FE · Boeing 727200 · Turbine Engine Oil SystemSDR 03FDEA01083Door · missingHYDRAULIC SERVICE AREA ACCESS PANEL MISSING FROM A/C. REPLACED DOOR IAW SMP. OK FOR SERVICE.Jul 10, 2003 · N220FE · Boeing 727200 · Hydraulic Compartment DoorsSDR 03FDEA01084Tripler · wornMDIS 284 53-30 0005339 07JUL03 BFM CLOSER COMPLY WITH EA 7-5330-70973 FUSELAGE-MAIN CARGO DOOR TRIPLER WEAR,P/N 53FX1301-7/-9 (AD 2002-16-19). FACT 10JUL03 10:28 BFM R COMPLIED WITH E.A. NR 7-5330-70973 FUSELAGE-MAIN CARGO DOOR TRIPLER WEAR, P/N Jul 10, 2003 · N284FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 03FDEA01081Skin · dentedEXTERIOR SKIN HAS DENT AT BS 203 RBL 14 STR 26R. SKIN DENT BS 203, RBL 14, STR 26R OUT OF LIMITS PER SRM 53-30-1. REPAIRED SKIN PER SRM 53-30-3.Jul 9, 2003 · N467FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 03FDEA01080Skin · lightning strikeEXTERIOR SKIN HAS SEVERAL LIGHTNING STRIKES FROM BS 334 TO BS 351 STR 25R TO STR 27R. REMOVED DAMAGE ON 7EA LIGHTNING STRIKES BS 334-351, STR 25-27 RT 5EA AREA. REMOVED DAMAGE BY DRILLING OUT DAMAGE AND INSTALLING FASTENERS PER SRM 53-30-3, 1EA AREA FOUND TJul 9, 2003 · N467FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 2003F00486Engine · leakingDURING DESCENT AT FORT LAUDERDALE (KFLL), THE CREW SHUTDOWN NR 3 ENGINE DUE TO EXCESSIVELY HIGH OIL TEMPERATURE, FLICKERING FILTER BYPASS LIGHT, LOW OIL PRESSURE ON THE GATE AND LOW OIL PRESSURE LIGHT ON STEADY AS WELL AS DECREASING OIL PRESSURE. LANDED AT KFJul 5, 2003 · N875AA · Boeing 727200 · Turbine Engine Oil SystemSDR 03FDEA01029Frame · dentedFRAME DENTED BS 500 STR 24L. REPAIRED DENTED FRAME AT BS 500, STR 24L PER SRM 51-40-3.Jul 3, 2003 · N467FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA01033Frame · dentedFRAME DENTED BS 540 STR 24L. CUT OUT DENTED SECTION OF FRAME STR 24L BS 540 2.2 X 1 X .050 INCH. FABRICATED REPAIR AND INSTALLED IAW SRM 51-40-3.Jul 3, 2003 · N467FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA01036Frame · dentedAFT CARGO BAY BS 990 FRAME IS DENTED AT STR 26L. REPAIRED FRAME AT BS 990, STR 26L PER SRM 51-40-3, FIG 1.Jul 3, 2003 · N467FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA01035Frame · dentedFRAME DENTED BS 580 BETWEEN STR 23L TO STR 5L. CUT OUT DAMAGED AREA ON BS 580 FRAME, 2 AREAS BETWEEN STR 23L AND 25L, 1.4 X 1 AND 3.8 X 1 INCH. FABRICATED REPAIR DOUBLER. ALODINED, PRIMED AND INSTALLED PER FED EX SRM 51-40-3.Jul 3, 2003 · N467FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA01034Frame · dentedFRAME DENTED BS 560 STR 22L TO 24L. REMOVED DAMAGED AREA OF DENTED FRAME BS 560, STR 22L TO 24L. FABRICATED, ALODINED, PRIMED AND INSTALLED REPAIR PART. ALL IAW SRM 53-10-1 FIG 1, 51-40-3 FIG 1, 51-20-04 PGS 3 AND 4, FED EX MM 51-20-000-7.Jul 3, 2003 · N467FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA01032Frame · dentedFRAME DENTED BS 520 STR 24L. INSPECTED DENTS AT BS 520, STR 24L. FOUND TO BE OUT OF LIMITS PER SRM 53-10-1, FIG 1, DETAIL II, NOTE [S]. CUT OUT AND REPAIRED DAMAGE PER SRM 51-40-3, FIG 1.Jul 3, 2003 · N467FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA01038Frame · dentedAFT CARGO BAY BS 950F FRAME IS DENTED IN 3 PLACES BETWEEN STR 26L AND 25L. REPAIRED FRAME AT BS 950F BETWEEN STRS 25L & 26L PER SRM 51-40-3 FIG 1.Jul 3, 2003 · N467FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA01037Frame · dentedAFT CARGO BAY BS 970 FRAME IS DENTED AT STR 26L AND 25L AND 23L. REPAIRED FRAME AT BS 970, STR 25L - 26L AND STR 23L PER SRM 51-40-3 FIG 1.Jul 3, 2003 · N467FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA01031Frame · dentedFRAME DENTED BS 500 STR 22R. FRAME AT BS 500, STR 22R DENT OUT OF LIMITS PER SRM 53-10-1. REPAIRED FRAME PER SRM 51-40-3.Jul 3, 2003 · N467FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA01030Frame · dentedFRAME DENTED BS 520 STR 22R TO 24R. REPAIRED FRAME BS 520, STR 22R TO 24R PER SRM 51-40-03.Jul 3, 2003 · N467FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA01000Skin · damagedMDIS 463 53-30 0005661 26JUN03 BFM CLOSE R COMPLY WITH EA NR 7-5330-70964 FUSELAGE-SKIN-PRE-EXISTING ELONGATED HOLES UNDER MCD HINGE (AD 2002-16-19).. FACT 29JUN03 17:38 BFM U COMPLIED WITH EA NR 7-5330-70964 FUSELAGE-SKIN-PRE-EXISTING ELONGJun 29, 2003 · N463FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 03FDEA00993Control Unit · faultyREPEAT WRITEUP. ENG NR 1 STRUT OVERHEAT LIGHT ILLUMINATED ON CLIMBOUT. COMPLIED WITH RED TABS AND LIGHT EXTINGUISHED WHEN NR 1 BLEED AIR SWITCH CLOSED AND LEFT, PACK TURNED OFF. REMAINED OFF FOR REST OF FLIGHT. INSPECTED NR 1 STRUT OVHT. DETECTOR SENSOR CJun 28, 2003 · N481FE · Boeing 727200 · Overheat DetectionSDR 03FDEA00995Fitting · gougedMDIS 463 53-10 0005658 24JUN03 BFM CLOSE R COMPLY WITH EA NR 7-5310-70960, FUSELAGE - MAIN CARGO DOOR ACTUATOR FITTING GOUGE REPAIR P/N 53FX1428-1. FACT 27JUN03 13:57 BFM R COMPLIED WITH EA NR 7-5310-70960,FUSELAGE-MAIN CARGO DOOR ACTUATOR FJun 28, 2003 · N463FE · Boeing 727200 · Fuselage Main, Attach Fittings
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