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 03FDEA01395Engine · leakingAT FL 330 NR 1 OIL QTY WENT RAPIDLY TO ZERO. OIL PRESS DROPPED TO 30 PSI. ENGINE SHUTDOWN IAW RED TABS. REMOVED AND REPLACED NR 1 ENG ASSY AS PER WORK CARD 70T0001-01, A/C OK FOR SERVICE.Aug 27, 2003 · N481FE · Boeing 727200 · Turbine Engine Oil SystemSDR 03FDEA01385Support Fitting · corrodedCORROSION ATTACH FITTING ON BS 228 BULKHEAD, AFT SIDE, LBL 10, 6 INCHES BELOW UPPER PRESSURE DECK IS CORRODED ON UPPER SIDE. REMOVED AND REPLACED SUPPORT FITTING PER SRM 51-30-5 & 51-30-2.Aug 26, 2003 · N220FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 03FDEA01388Frame · dentedFWD CARGO BAY, DENT IN FRAME, BS 500, AT STR 24L. REMOVED, REPLACED AND INSTALLED FRAME SECTION BS 500 AT STR 21L TO STR 25L. ALL WORK DONE IAW SRM 51-30-5, SRM 51-30-2, SRM 51-10-2 AND MM 51-20-151-7 PG 1.Aug 26, 2003 · N220FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA01389Frame · dentedFWD CARGO BAY, DENTS IN FRAME, BS 520, AT STR 23L TO STR 25L. REMOVED FRAME SECTION, BS 520, STR 21-25, INSTALLED NEW FRAME SECTION BETWEEN SPLICES. ALL WORK DONE PER SRM 51-30-2, SRM 51-30-5, SRM 51-10-2 & MM 51-20-151-7 PG 1.Aug 26, 2003 · N220FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA01386Skin · dentedSTA 720A STR 24L SKIN HAS A DENT. REMOVED DAMAGED SKIN AT 720A, STR 24L AND REPAIRED. WORK DONE IAW BOEING 727 SRM 53-30-3 FIG 3.Aug 26, 2003 · N220FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 03FDEA01390Frame · corrodedCORROSION ON FRAME STA 950E BETWEEN STR 28L & 29L. REPAIRED FRAME BS 950E, STR 28L-29L IAW SRM 53-10-4 FIG 13 AND EA 7-5310-54947.Aug 26, 2003 · N275FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA01391Panel Support · chafedVERTICAL STAB LT TEE SUPPORT IS CHAFED WHERE PANEL 8603 LWR ATTACHMENT ANGLE, ATTACHES TO THE PANEL SUPPORT. CUT OUT DAMAGED AREA 3 X 1 INCH ON LT VERTICAL STAB SUPPORT AT PANEL 9603'S AFT ATTACH ANGLE MOUNT HOLE. FABRICATED AND INSTALLED REPAIR IAW SRM 55Aug 26, 2003 · N275FE · Boeing 727200 · Vertical StabilizerSDR 03FDEA01360Frame · corrodedCORROSION (C53-113-01, 2) ON FRAME STA 970 BETWEEN STR 28L & 29L. CORROSION ON FRAME BS 970, STR 28L-29L WAS FOUND OUT OF LIMITS PER SRM 53-10-1. REMOVED DAMAGED FRAME SECTION AT SHEAR TIE SKIN ATTACHMENT, FABRICATED REPAIR PARTS, AND INSTALLED PER SRM 53-10Aug 22, 2003 · N275FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA01358Skin · gougedEMPENNAGE SKIN GOUGED, STA 1348, 12 INCHES ABOVE LEFT AFT AIRSTAIR CORNER. REMOVED DAMAGE AT SKIN AT BS 1348. FOUND TO BE OUT OF LIMITS. FABRICATED THE REPAIR DOUBLER, AND INSTALLED THE REPAIR PART IAW SRM 54-30-3.Aug 22, 2003 · N491FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 03FDEA01362Stiffener · corrodedSTIFFENER INSIDE DELTA BEAM AT BS 789, RBL 3, WL 154 IS CORRODED. REMOVED AND REPLACED STIFFENER IAW SRM 51-30-2.Aug 22, 2003 · N220FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 03FDEA1361Skin · damagedSIX PREVIOUSLY PLUGGED HOLES IN SKIN AT BS 400 BETWEEN STR 14 - 15 LT ADJACENT TO EXISTING FASTENERS.Aug 22, 2003 · N275FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 03FDEA01359Skin · dentedDENT IN SKIN BS 380 BETWEEN STR 14L AND STR 15L. CUT OUT DAMAGE, INSTALLED REPAIR DOUBLER (EXTERNAL) PER EA 7-5330-70501.Aug 22, 2003 · N275FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 03FDEA01352Frame · corrodedCORROSION ON CHORDS IN NLG BAY AT B/S 284, LBL 18 INSIDE TORQUE BOX O/B OF STRUT DOOR FWD HINGE. REMOVED AND REPLACED LT CHORD AT B.S. 284, LBL 18 PER SRM 51-30-02. PERFORMED FUNCTIONAL TEST OF NLG PER M/M 32-22-001-5. FUNCTIONAL TEST GOOD.Aug 21, 2003 · N220FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA01351Floorbeam · corrodedCORROSION (C53-224-03(1/2) AT BS 344, LBL 40, WL 208, ON TOP OF FLOORBEAM. REMOVED CORROSION BS 344, WL 208, LBL 40. FOUND TO BE OUT OF LIMITS. REMOVED FLOORBEAM UPPER CHORD BS 344, BL 0 TO LBL 70 & INSTALLED REPAIR. ALL IAW SRM 53-10-1 & 53-10-8, FIG Aug 21, 2003 · N220FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 03FDEA01350Skin · corrodedCORROSION (C53-113-01) ON FLOOR FUSELAGE SKIN STA 703 BL 0 WL 148. REPAIRED SKIN B.S 703, WL 148, BL 0, IAW SRM 53-30-3 FIG 1.Aug 21, 2003 · N220FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 03FDEA01342Frame · chafedCHORD AT BS 1352 IS CHAFED ALONG ENTIRE CIRCUMFERENCE AND RUB STRIPS ARE MISSING. FOUND FLANGE ON 1352 CHORD TO BE OUT OF LIMITS. REMOVED DAMAGED CHORD, DRILLED UP AND INSTALLED NEW 1352 CHORD IAW SRM 53-10-1, 51-30-2, 51-30-5.Aug 19, 2003 · N220FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA01338Skin · dentedDENT IN SKIN BS 268 BETWEEN STR 16-17L. DENT IN SKIN AT BS 268 BETWEEN STR 16-17L WAS OUT OF LIMITS. AREA WAS REPAIRED PER SRM 53-30-3 FIG 1.Aug 19, 2003 · N491FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 03FDEA01339Skin · dentedDENT IN SKIN AT EDGE OF MAIN CARGO DOOR CUTOUT BS 620 ABOVE STR 17L. REWORKED DENT IN SKIN AT EDGE OF MAIN CARGO DOOR CUTOUT, BS 620, ABOVE STR 17L PER EA 7-5330-70490.Aug 19, 2003 · N491FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 03FDEA01337Pressure Panel · gougedNOSE LANDING GEAR FWD RT PRESSURE ACCESS PANEL SKIN CUTOUT IS GOUGED. REPAIRED FWD RT PRESSURE ACCESS PANEL SKIN AT NOSE LANDING GEAR. ALL WORK DONE IAW SRM 51-40-2.Aug 19, 2003 · N491FE · Boeing 727200 · Fuselage Main, BulkheadSDR 03FDEA01341Skin · gougedAFT AIRSTAIR, HAS A GOUGE ON THE EXTERNAL SKIN, 40 INCHES FROM THE LOWER END. EVALUATED GOUGE ON AFT AIRSTAIR EXTERNAL SKIN 40 INCHES FROM LOWER END. FOUND GOUGE TO BE .012 INCHES DEEP. ORIGINAL THICKNESS IS .040. FOUND TO BE OUT OF LIMITS PER SRM 52-00-2. Aug 19, 2003 · N220FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 03FDEA01343Structure · crackedBS 1225 RBL 20 WL 185 STRUCTURE UNDER AIRSTAIR ACTUATOR MOUNT IS CRACKED. REMOVED, DRILLED UP & INSTALLED REPLACEMENT "L" ANGLE SUPPORT BS 1265, WL 185, RBL 20-45 IAW SRM 51-30-2, 51-30-5.Aug 19, 2003 · N220FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 03FDEA01340Fitting · corrodedCORROSION ON UPPER SURFACE OF NLG DOOR UPPER FITTING ON BS 227.9 BULKHEAD LBL 8, WL 180. REMOVED NLG UPPER FITTING AND LOCATED AND BACK DRILLED NEW FITTING. INSTALLED FITTING WET WITH SEALANT IAW SRM 51-30-2.Aug 15, 2003 · N491FE · Boeing 727200 · Landing Gear DoorsSDR 03FDEA01321Keelbeam · corrodedCORROSION ON LT KEELBEAM CORD AT STA 950D, WL 148. ACCESSED LT KEELBEAM. REMOVED CORROSION ON L/HKEEL BEAM CORD AT BS 950D+15, WL 148. CORROSION FOUND TO BE OUT OF LIMITS. REPAIRED KEELBEAM IAW FED EX EA 7- 5310-72313. PERFOMRED SHEAR TIE REPAIR AND RAug 15, 2003 · N491FE · Boeing 727200 · Fuselage Main, KeelSDR 03FDEA01319Floorbeam · corrodedCORROSION (C53-224-02) ON FLOORBEAM AT BS 480, RBL 3 - RBL 10, WL 207.9 ON LOWER SIDE OF TOP FLANGE. CORROSION OUT OF LIMITS. REPLACED FLOORBEAM UPPER CHORD BS 480, LBL 38 - RBL 65, WL 207.9 IAW FED EX EA 7-5310-72538.Aug 15, 2003 · N215FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 03FDEA01320Skin · damagedGRAVEL DAMAGE ON FUSELAGE BELLY SKIN, BS 1050-1060 BETWEEN STR 26R AND 28R. REMOVED DAMAGED SKIN AT BS 1050-1060 BETWEEN STR 26 RT AND 28 RT AND INSTALLED REPAIR DOUBLER PER SRM 53-30-3 & EA 7-5330-70493.Aug 15, 2003 · N491FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 03FDEA01322Web · corrodedCORROSION ON WEB AT STA 986, STR 29R, WL 148 . REPAIRED WEB AT B.S. 986, STR 29R, WL 148 IAW SRM 53-10-4 FIG 15.Aug 15, 2003 · N491FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 03FDEA01323Frame · corrodedCORROSION ON FRAME AT STA 1010, STR 29R TO 29L, WL 138. BLENDED OUT CORROSION ON FRAME AT STA 1010, STR 29R TO 29L, WL 138. FOUND OUT OF LIMITS I.A.W. BOEING 727 SRM 53-10-1. REPAIRED BLEND OUTS PER BOEING 727 SRM 53-10-4, FIG 15, BOEING 727 SRM 51-10-Aug 15, 2003 · N491FE · Boeing 727200 · Fuselage Main, StructureSDR 03FDEA01326Keelbeam · corrodedKEEL BEAM (STR 29R OUTBD FLANGE) IS CORRODED BEYOND LIMITS. REPAIRED RT KEEL BEAM OUTBD FLANGE AT BS 950F-970 PER SR 27-53-023A.Aug 15, 2003 · N275FE · Boeing 727200 · Fuselage Main, KeelSDR C8GA20030020Pump · defectiveDEPARTED STL HAD NO INDICATION OF A PROBLEM UNTIL 150 MILES OUT OF TOL. A-SYSTEM QUANTITY GAUGE SHOWED A SUDDEN LOSS OF INDICATED HYDRAULIC QUANTITY. FOLLOWED CCIA “A” SYSTEM FAIL PROCEDURE, ADVISED ATC AND DECLARED AN EMERGENCY AND LANDED AT OUR FINAL DESTINAAug 15, 2003 · N713AA · Boeing 727200 · Hydraulic Pump (Electric/Engine), MainSDR 03FDEA01325Stringer · corrodedSTRINGER HAS CORROSION, WHILE WORKING ON CARD NR N00150, FOUND CORROSION ON STRINGER 27R AT BS 1056.Aug 15, 2003 · N491FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 03FDEA01316Latch · stuckAFTER T/O FROM KGEG F2 F/O COULD NOT RAISE THE LANDING GEAR LEVER BEYOND THE OFF POSITION. FOLLOWED RED TABS LANDING GEAR LEVER LATCH FAILED TO RELEASE. CHECKLIST, CHECK 2F RESET P6- 3 LANDING GEAR 2 LEVER LATCH 2 FLIGHT CB. LANDING GEAR THEN RETRACTED.Aug 15, 2003 · N206FE · Boeing 727200 · Landing Gear SelectorSDR 03FDEA01303Switch · failedDURING FLAP RETRACTION L/E FLAP AMBER LIGHT REMAINED ILLUMINATED 26 S/O PANEL SHOWED 237 L/E SLAT NOT RETRACTED. REMOVED AND REPLACED BOTH RETRACT & EXTEND SWITCHES ON NR 7 SLAT ACTUATOR IAW 727-200 M/M 27-82-011-4. TESTED AS PER SAME REFER. OPS CHECKS GOODAug 14, 2003 · N280FE · Boeing 727200 · Leading Edge Slat Control SystemSDR 03FDEA01301Clamp · looseDURING CLIMBOUT PASSING APPROX FL270 22 ENG 1 STRUT OVERHEAT 22 LIGHT ILLUMINATED. PERFORMED THE APPROPIATE RED TAB PROCEDURE AND LIGHT EXTINGUISHED. AFTER CLOSING N1 BLEED. SUSPECT AIR BLEED LEAK ITS ON THE FUSELAGE SIDE OF THE BLEED AIR VALVE PER RED Aug 14, 2003 · N218FE · Boeing 727200 · Pneumatic Indicating SystemSDR 03FDEA01302Fan · shortedGASPER FAN C/B POPPED IN FLT IMMEDIATELY FOLLOWING MILD SMOKEY ODOR IN COCKPIT. DID NOT RESET C/B ODOR WENT AWAY. REMOVED AND REPLACED GASPER FAN PER 727-200 M 2FM 21-23-011-4 2C, OPS CHECK OK.Aug 14, 2003 · N207FE · Boeing 727200 · Air Distribution FanSDR 03FDEA01304Indicator · failedON CLIMBOUT OF TUS, CABIN CONTINUED TO CLIMB TO 2000 27QRH PROCEDURES WERE PERFORMED AND CABIN PRESSURE DID NOT RESPOND.Aug 14, 2003 · N469FE · Boeing 727200 · Cabin Pressure Control SystemSDR 03FDEA01253Frame · bentFWD CARGO BAY 680 FRAME BENT AT RBL 35 BETWEEN STR 24R 26 25R. FRAME AT BS 680, RBL 35 BETWEEN STR 24 & 25 RT OUT OF LIMITS. REPAIRED FRAME IAW FED EX EA 7-5310-72507, SRM 53-10-1 & 51-40-3 FIG 1.Aug 12, 2003 · N215FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA01254Floorbeam · chafedBS 740 FLOORBEAM UPR CHORD CHAFED ALONG AFT EDGE LBL 44 -RBL 44 WL 208 . BLENDED DAMAGE PER EA 7-5310-72307.Aug 12, 2003 · N215FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 03FDEA01256Door Frame · crackedWHILE WORKING CARD N00281 2C FOUND CRACK ON 2FH LWR CORNER WEB OF ENTRY DOOR.Aug 12, 2003 · N215FE · Boeing 727200 · Fuselage Main, StructureSDR 03FDEA01255Floorbeam · corrodedCORROSION AFT CARGO BAY FLOORBEAM LOWER FLANGE HAS CORROSION AT FASTENER HOLES BS 1070 WL 200 2C LBL 40 TO RBL 53. BLENDED DAMAGE. COMPLIED WITH EA 7-5310-72306. REPAIRED 1070 FLOORBEAM AT BS 1070 WL 200, LBL 40 TO RBL 40.Aug 12, 2003 · N215FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 03FDEA01258Floorbeam · corrodedCORROSION ON LOWER FLANGE OF FLOORBEAM BS 720 LBL 46 TO RBL 46 WL 200. REMOVED CORROSION ON BS 720 FLOORBEAM LOWER CHORD LBL 46 TO RBL 46, WL 200. ALL AREAS WITHIN LIMITS EXCEPT AT LBL 5 AND THIS AREA WAS REPAIRED PER FED EX EA 7- 5310-72309.Aug 12, 2003 · N215FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 03FDEA01257Floorbeam · corrodedFASTENER HOLES ON FLOORBEAM LOWER SIDE OF FLANGE STA 560 LBL -25 WL 208 CORRODED. REMOVED CORROSION ON FLOORBEAM LOWER SIDE OF UPPER TEE BS 560, LBL 0-25, WL 208. REPAIRED IAW FED EX EA 7-5310-72311.Aug 12, 2003 · N215FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 03FDEA01261Floorbeam · corrodedCORROSION 28 C53-224-01 281 29 29 AT FASTENER HOLE 2C ON FLOORBEAM 2C LOWER SIDE OF FLANGE 2C STA 680 2C RBL 41 WL 208. REMOVED CORROSION BS 680, RBL 41 AND RBL 37 OUT OF LIMITS. REPAIRED FLOORBEAM IAW SRM 53-10-1 AND EA 7-5310-54933.Aug 12, 2003 · N215FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 03FDEA01252Control Panel · malfunctionedIN CRZ FLT LOWER AFT BODY OVERHEAT LIGHT CAME ON BLINKING AT VARIOUS RATES. ACCOMPLISHED QRH L.A.B. OVERHEAT CHECKLIST TO INCLUDE CLOSING NR 3 ENG. BLEED. BLINKING SLOWED THEN STOPPED. SYSTEM TESTED GOOD. CONTINUED IN CRUISE WITH NR 3 BLEED CLOSED. R7R Aug 10, 2003 · N208FE · Boeing 727200 · Overheat DetectionSDR 03FDEA01219Frame · bentFWD CARGO BAY 680 FRAME BENT AT RBL 35 BETWEEN STR 24R & 25R. FRAME AT BS 680, RBL 35 BETWEEN STR 24 & 25 RT OUT OF LIMITS. REPAIRED FRAME IAW FEDEX EA 7-5310-72507, SRM 53-10-1 & 51-40-3 FIG 1.Aug 7, 2003 · N215FE · Boeing 727200 · Fuselage Main, FrameSDR C1HA200396013Battery · inoperativeAFT AIRSTAIRS OVERHEAD EMERGENCY LIGHT INOP. REMOVED AND REPLACED AFT BATTERY, OPS CHECK NORMAL.Aug 4, 2003 · N696CA · Boeing 727200 · Emergency LightingSDR C1HA200396014Battery · inoperativeAFT AIRSTAIRS OVERHEAD EMERGENCY LIGHT INOP. REMOVED AND REPLACED FWD BATTERY, OPS CHECK NORMAL.Aug 4, 2003 · N696CA · Boeing 727200 · Emergency LightingSDR DHL2003749008Hydraulic Line · leakingHYDRAULIC SYSTEM-B FAILED EN ROUTE MTY-CVG. LOST ALL B-SYSTEM HYDRAULIC QUANTITY. ALL ABNORMAL PROCEDURES/CHECKLIST ACCOMPLISHED PER M/M 29-00-00. REMOVED AND REPLACED B-SYSTEM HOSE ASSEMBLIES TO AND FROM NR 2 HYDRAULIC PUMP. SERVICED HYDRAULICS. OPS AND Aug 2, 2003 · N749DH · Boeing 727200 · Hydraulic System, AuxiliarySDR 03FDEA01201Bushing · wornAFTER RETRACTING FLAPS TO 2 THE RED L/E ANNUNCIATOR LIGHT REMAINED ILLUMINATED. POSITION TEST SHOWED NR 2 L/E FLAP INTRANSIT. RED TABS COMPLETED AND LIGHT WENT OUT, AFTER 1 MIN RED L/E FLAPS LIGHT ILLUMINATED AGAIN (WITH FLAPS IN THE UP POSITION). RED TABS Aug 1, 2003 · N268FE · Boeing 727200 · Leading Edge DevicesSDR 03FDEA01196Fire Loop · false indicationENGINE FIRE LIGHT (DASHBOARD AND FIRE HANDLE) NUMBER 1 ENGINE ILLUMINATED MOMENTARILY INFLIGHT ON APPROACH (APPROX 11,000FT AND 300K), ACCOMPANIED BY FIRE BELL. LIGHT AND BELL WENT OUT, FIRE TEST CHECK OK, ALL ENGINE INDICATIONS NORMAL. APPROXIMATELY 3 MINAug 1, 2003 · N281FE · Boeing 727200 · Fire DetectionSDR 03FDEA01184Skin · gougedNOSE WHEEL WELL GOUGE AROUND PANEL OPENING 3124, BS 237 LT. BLENDED GOUGE TO NEW SKIN AT BS 237. FOUND TO BE OUT OF LIMITS IAW 53-10-1. DAMAGE WILL BE REPAIRED ON CARD N00468.Jul 31, 2003 · N215FE · Boeing 727200 · Fuselage Main, Plate/Skin
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