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 03FDEA01820Skin · gougedDENT WITH GOUGE IN EXTERNAL FUSELAGE SKIN AT BS 500 AT STR 25 RIGHT. REWORKED DENT AND BLENDED GOUGE IN REWORKED AREA ON EXTERNAL FUSELAGE SKIN AT BS 500 AT STR 25 RIGHT. AREA REMOVED 1 X .8 X .020 INCH. FOUND TO BE OUT OF LIMITS. FABRICATED, ALODINED, PRIOct 29, 2003 · N270FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 03FDEA01823Floorbeam · corrodedCORROSION (C53-111-01, 3) LWR CHORD OF FLOORBEAM BS 1110, RBL 38, WL 201. *S/D* REMOVED CORROSION AREA 1.5 X 3 X .029 INCH DEEP FROM ORIGINAL .150 FOUND OUT OF LIMITS PER SRM 53-10-1 FIG 4. REPAIRED LWR CHORD OF FLOORBEAM BS 1110 RBL 38 WL 201 PER SRM 53-Oct 29, 2003 · N270FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 03FDEA01825Stringer · corrodedCORROSION (C53-111-01, 2) FWD CARGO COMPARTMENT STR 28R BS 680 RBL 6 WL 148. FWD CARGO BAY STR 28R BS 680 WAS OUT OF LIMITS. FABRICATED NEW STRINGER SPLICE & INSTALLED PER SRM 51-30-02.Oct 29, 2003 · N270FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 03FDEA01826Floorbeam · corrodedCORROSION (C53-224-01, 3) FLOORBEAM BS 1050, LBL 27, WL 208. BLENDED CORROSION ON TOP CHORD OF FLOORBEAM IN A 1 X 1 X .029 INCH FOUND TO BE OUT OF LIMITS PER SRM 53-10-1 FIG 4. REMOVED TOP OF CHORD FROM LBL 19 TO 30.5 AND INSTALLED REPAIR PER SRM 53-10-8 FIGOct 29, 2003 · N270FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 03FDEA01828Clamp · out of positionFLIGHT TEST: NOSE GEAR INDICATOR LIGHT FLICKERS & IS INTERMITTENTLY OFF WITH GEAR DOWN & LOCKED. FOUND IF PRESSURE IS APPLIED TO INBOARD EDGE OF MASTER DIM AND TEST SWITCH, LIGHTS (NOSE GEAR AND NR 3 OIL PRESSURE LIGHT) WOULD FLICKER, LOOSENED PANEL, AND FOOct 29, 2003 · N217FE · Boeing 727200 · Landing Gear Position and WarningSDR 03FDEA01827Floorbeam · corrodedCORROSION WHILE WORKING N01449 FOUND CORROSION ON TOP SURFACE OF UPPER CHORD OF FLOORBEAM BS 1070 RBL 23 WL 208.Oct 29, 2003 · N270FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 03FDEA01824Floorbeam · corrodedCORROSION ON LOWER SECTION OF FLOORBEAM BS 1070, LBL 1-42, WL 201. REMOVED CORROSION LOWER SECTION OF FLOORBEAM BS 1070, LBL 1-42, WL 201 (14 AREAS) 1 X 1 X NO MORE THAN .018 FROM ORIGINAL .150 EXCEPT AREAS AT LBL 28 .208 REMOVED AND LBL 38 .082 REMOVED. Oct 29, 2003 · N270FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 03FDEA01822Skin · bulgedOUTER EXTERIOR SKIN HAS BULGE AT STA 1050 STR 28L. REMOVED CORROSION ON SKIN STA 1050 STR 28L, FOUND OUT OF LIMITS PER SRM 53-30-01. REPAIRED STRINGER PER SRM 53-10-03 FIG. 1.Oct 29, 2003 · N270FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 03FDEA01821Skin · dentedOUTER EXTERIOR SKIN IS DENTED AT STA 1148 BETWEEN STR 24L AND 25L. REPAIRED OUTER EXTERIOR SKIN AT STA 1148 BETWEEN STR 24L AND 25L. ALL WORK DONE IAW SRM 53-30-1, SRM 53-30-3.Oct 29, 2003 · N270FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR C8GA20030025Pitot Tube · obstructedFLT 717 FROM ELP TO STL. ON TAKEOFF ROLL, THE CAPTAIN'S AIRSPEED INDICATOR READ 30 KNOTS LESS THAN THE FIRST OFFICER POSITION. ABORTED TAKEOFF AND AIRCRAFT RETURNED TO RAMP WITHOUT FURTHER INCIDENT. INSPECTED CAPTAIN'S PITOT PROBE AND FOUND DEBRIS LODGED INOct 28, 2003 · N713AA · Boeing 727200 · Stall Warning SystemSDR 03FDEA01819Connector · looseON FINAL FOR LANDING WITH FLAPS 30 AND GEAR DOWN THE NOSEWHEEL GREEN DOWN AND LOCKED ILLUMINATED INTERMITTENTLY CAUSING THE GEAR WARNING HORN TO GIVE A STEADY AURAL WARNING. A GO-AROUND WAS ACCOMPLISHED AND QRH CHECK LIST WAS RUN. AFTER RECYCLING, HAD 3 GREEOct 28, 2003 · N203FE · Boeing 727200 · Landing Gear Position and WarningSDR 03FDEA01806Support Beam · corrodedCORROSION AROUND NOSE GEAR SUPPORT BEAM PANEL ATTACHMENT FLANGE CORROSION ON TEE CHORD FLANGE AT NOSE GEAR SUPPORT BEAM PANEL ATTACHMENT FLANGE FOUND TO BE OUT OF LIMITS. REMOVED TEE CHORD AND SENT OUT FOR FABRICATION. INSTALLED NEW TEE CHORD IN PLACE Oct 27, 2003 · N493FE · Boeing 727200 · Fuselage, Landing Gear Attach FittingsSDR 2003F00605Powerpack · inoperativeAISLE EMERGENCY EXIT LIGHT AT ROW 20 INOPERATIVE. REMOVED AND REPLACED BATTERY POWER PACK AT ROW 20 IAW B727 MM, 335071. (M)Oct 26, 2003 · N910PG · Boeing 727200 · Emergency LightingSDR XNOA1161Pressure Switch · leakingNR 2 ENG LOW OIL PRESS WARNING LT & LOSS OF OIL PRESS. SHUT DOWN ON TAXI OUT. FOUND NR 2 ENG OIL PRESS SWITCH LEAKING. REMOVED AND REPLACED NR 2 LOW OIL PRESS SWITCH AS REQ IAW B727 MM REF 79-33-1, OPS AND LEAK CHECK. DURING TROUBLESHOOTING FOUND LOW OIL POct 24, 2003 · N793A · Boeing 727200 · Engine Oil PressureSDR 03FDEA01796Structure · corrodedCOMPLY WITH EA 7-5310-73206 FUSELAGE - MAIN FRAME - BS 950 BULKHEAD LOWER STRUCTURE CORROSION REPAIR, P/N 65-16338-7. COMPLIED WITH EA 7-5310-73206 FUSELAGE - MAIN FRAME - BS 950 BULKHEAD LOWER STRUCTURE CORROSION REPAIR P/N 65-16338-7, AT MAE.Oct 23, 2003 · N269FE · Boeing 727200 · Fuselage Main, BulkheadSDR 03FDEA01790Pitot Tube · obstructedF/O AIRSPEED INDCATOR INOP ON T/O UPON ARRIVAL CHECKED FOR OBTRUCTIONS IN BOTH CAPTS & F/O'S PITOT TUBES NO BLOCKAGE NOTED. R&R F/O'S AIRSPEED INDICATOR.OPS CHECKS GOOD PER B727-200_M.M. CHAPT.34-12-000-5.Oct 22, 2003 · N206FE · Boeing 727200 · Pitot/Static SystemSDR 03FDEA01791Fitting · chafedCOMPLY WITH EA 7-5310-73211 FUSELAGE - MAIN FRAME - NLG DRAG BRACE SUPPORT CHAFE REPAIR P/N 65-17673. COMPLIED WITH EA 7-5310-73211 FUSELAGE - MAIN FRAME - NLG DRAG BRACE SUPPORT CHAFE REPAIR P/N 65-17673, AT MAE.Oct 22, 2003 · N269FE · Boeing 727200 · Fuselage, Landing Gear Attach FittingsSDR 03FDEA01792Flap · out of rigUPON TAKEOFF WHILE RETRACTING THE FLAPS FROM 5 DEGREES TO 2, BOTH FLAP INDICATIONS STUCK BETWEEN 5 AND 2 AND INTRANSIT LIGHT SHOWED AMBER, THE S/O'S VERIFICATION PANEL SHOWED ALL LED'S DOWN. AFTER APPROX 5 MIN THE LED'S RANDOMLY SEQUENCED TO 2, 3, 6, 7 AND Oct 21, 2003 · N479FE · Boeing 727200 · Trailing Edge Flap Control SystemSDR 03FDEA01788Keelbeam · damagedCOMPLY WITH EA 7-5310-73207 FUSELAGE - MAINFRAME - KEEL BEAM T-ANGLE REPAIR. COMPLIED WITH EA 7-5310-73207 FUSELAGE - MAIN FRAME - KEEL BEAM T-ANGLE REPAIR AT MAE.Oct 21, 2003 · N269FE · Boeing 727200 · Fuselage Main, KeelSDR 03FDEA01787Hinge · chafedCOMPLY WITH EA 7-5230-73214 DOORS - MAIN CARGO - WEAR/CHAFING ON 2 EACH LOBES OF MCD HINGE ASSY. COMPLIED WITH EA 7-5230-73214 DOORS - MAIN CARGO - WEAR/CHAFING ON 2 EACH LOBES OF MCD HINGE ASSY.Oct 21, 2003 · N269FE · Boeing 727200 · Cargo/Baggage DoorsSDR 03FDEA01785Switch · malfunctionedON FLAP RETRACTION FROM 5 DEG TO 2 DEG, LED NR 5 (RT SIDE) DID NOT FULLY RETRACT. AMBER LIGHT ILLUMINATED ON LED POSITION INDICATOR AFT BULKHEAD. COMPLIED WITH RED TABS, DID NOT CORRECT PROBLEM. REMOVED AND REPLACED NR 5 L/E FLAP POSITION SWITCH IAW MM 27-8Oct 21, 2003 · N273FE · Boeing 727200 · Leading Edge Slat Control SystemSDR 03FDEA01783Skin · misrepairedFUSELAGE SKIN PRE-EXISTING OPEN HOLES NEAR MAIN CARGO DOOR CUTOUT. FUSELAGE SKIN PRE-EXISTING OPEN HOLES NEAR MAIN CARGO DOOR CUTOUT. (INITIAL ACTION, PART 1 COMPLIED WITH ONLY).Oct 21, 2003 · N269FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR XNOA1160Windshield · failedCRACKED R-1 WINDSHIELD, ARCING AS WELL. REMOVED AND REPLACED F/O R-1 WINDSHIELD IAW B727MM 56-11-11 AS REQ NO DEFECTS NOTED. (STATUS: ORIG/CLOSED)Oct 18, 2003 · N793A · Boeing 727200 · Flight Compartment WindowsSDR 2003F00599Power Unit · failedAPU FIRE ALARM DID NOT TEST ON GROUND. REMOVED AND REPLACED OPERATING POWER UNIT IAW B727 MM 26-15-00. OPERATIONALLY CHECKED GOOD. (M)Oct 17, 2003 · N906PG · Boeing 727200 · Smoke DetectionSDR 03FDEA01765Floorbeam · damagedSTA 950F, WL 208, LBL 30 & 36 FLOORBEAM HAS TOOL MARKS. BLENDED TOOL MARKS FROM 950F FLOORBEAM WL 208, LBL 30-36, REMOVED 1 X1 X.150 & 1 X2 X.045 FROM ORIGINAL OF .225 . OUT OF LIMIT PER SRM 51-10-1. CUT OFF DAMAGE SECTION OF FLOOR BEAM, AFT UPPER Oct 17, 2003 · N217FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 03FDEA01764Skin · corrodedCORROSION FOUND ON AIRCRAFT SKIN, UNDER STRINGER 28 LT AT BS 950E, 950E+9, AND 950F+6. FOUND SKIN TO BE OUT OF LIMITS AT 950E, 950E 9 AND 950F 6. CUT OUT CORRODED SKIN AND REPAIRED PER 727 SRM 53-30-3 FIG 3Oct 17, 2003 · N493FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 03FDEA01759Stringer · corrodedCORROSION ON STRINGER 28 LT, BS 950E 3, OUTBOARD SIDE OF STRINGER.Oct 16, 2003 · N493FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 03FDEA01747Bolt · missingAFTER SEVERAL SUCCESSFUL FLAP RETRACTION CYCLES, OUTBOARD FLAPS STOPPED AT 5 DEG & STAYED THERE WHILE FLAPS 2 WERE COMMANDED, ALTERNATE FLAP SELECTION WAS UNABLE TO MOVE THEM FURTHER UP OR DOWN. USE OF NORMAL HYD MOTOR WAS ABLE TO DRIVE OUTBOARDS DOWN. BUT Oct 15, 2003 · N468FE · Boeing 727200 · Trailing Edge FlapsSDR 03FDEA01739Skin · corrodedCORROSION (C53-113-01(2) ON EXTERNAL SKIN BS 1054 AT STR 28L. COMING CUT OUT & REMOVED DAMAGED SKIN B/S 1054. FABRICATED & INSTALLED REPAIR IAW SRM 53- 30-3 FIG 3. (STR 28L).Oct 15, 2003 · N493FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 03FDEA01738Lap Joint · chafedCHAFING ON LAP JOINT SKIN STR19R, BS720D PLUS 10 INCHES. BLENDED OUT LAP JOINT SKIN STR 19R, BS 720D 10, 2 X 2 X .022 FROM ORIGINAL OF .060. FOUND TO BE OUT OF LIMITS PER SRM 53-30-1 CUT OUT DAMAGE FROM LAP AND REPAIRED PER SRM 53-30-3,Oct 15, 2003 · N217FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 03FDEA01742Skin · corrodedEXTERIOR SKIN 12 INCH FORWARD OF BS 1183 BETWEEN STRINGERS 22L AND 23L CORRODED AND FASTENERS CORRODED AND AREA BULGED. REPAIRED DOUBLER FOR AFT LAV SERVICE PAN AREA IAW EA 7-5330-55022.Oct 15, 2003 · N223FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 03FDEA01743Floorbeam · damagedSTA 1163 FLOORBEAM REPAIR NOT IAW STANDARD REWORK DRAWING. REWORKED FLOORBEAM REPAIR STA 1163 IAW EA 7-5310-55026Oct 15, 2003 · N223FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 03FDEA01744Attach Angle · corrodedATTACH ANGLE ABOVE AFT LAV SERVICE PAN CORRODED. REMOVED AND REPLACED IAW EA 7-5320-55012.Oct 15, 2003 · N223FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 03FDEA01745Fitting · corrodedSTA 1183 STR 20L UPPER AND LOWER TERMINATING FITTINGS HAVE CORROSION AND GOUGES AT FASTENER HOLES. REMOVED AND REPLACED STRINGER 20 TERMINATING FITTINGS IAW B727 SRM 51-30-2 AND 727-200 AMM 20-80-001-2Oct 15, 2003 · N223FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 03FDEA01746Bolt · corrodedSTA 1183, FORWARD BULKHEAD LOWER TENSION FITTINGS STR 26L, 27L, 26R, 27R, AND 29R HAVE CORRODED .3750 INCH BOLTS. REMOVED AND REPLACED BOLTS IAW WORK CARD 71C716-00Oct 15, 2003 · N223FE · Boeing 727200 · FastenersSDR 03FDEA01737Skin · chafedCHAFING ON LAP JOINT SKIN STR 19L B/S 720D PLUS 10 INCHS. BLENDED CHAFFE FOUND TO BE OUT OF LIMITS, CUT OUT DAMAGED AREA AND REPAIRED. PER SRM 53-30-3 FIG 14.Oct 14, 2003 · N217FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 03FDEA01736Stringer · bulgedBULGE ON EXTERNAL SKIN BS 1050 AT STR 27L. CUT OUT & REMOVED DAMAGED STRINGER BS 1040-1060 STR 27L. FABRICATED & INSTALLED REPAIR IAW SRM 53-10-3 FIG 1.Oct 14, 2003 · N493FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 03FDEA01713Floorbeam · corrodedCORROSION BS 320-340, RBL 40, WL 208 ON TOP OF FLOORBEAM AND INTERCOSTAL REMOVED AND REPLACED FLOORBEAM.Oct 8, 2003 · N217FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 03FDEA01706Floorbeam · corrodedCORROSION (C53-111-01(3)) ON BS 1148 FLOORBEAM LOWER CHORD BL 0, WL 200. *S/D* CORROSION ON FLOORBEAM AT BS 1148 LOWER CHORD BL 0 WL 200 WAS FOUND TO BE OUT OF LIMITS. REPAIRED FLOORBEAM PER FED EX EA 7-5310-55019.Oct 7, 2003 · N468FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 03FDEA01707Skin · gougedRT FUSELAGE SKIN GOUGE STRINGER 19R LAP BS 720D 14. REPAIRED RT FUSELAGE SKIN GOUGE PER SRM 53-30-3, AND SR DRAWING SR 27-57-056.Oct 7, 2003 · N468FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 03FDEA01708Keelbeam · corrodedCORROSION ON RT KEEL BEAM BS 950F 8 O/B FLANGE. *S/D* BLENDED CORROSION ON RT KEEL BEAM BS 950F 8 O/B FLANGE AND FOUND OUT OF LIMITS. FABRICATED REPAIR STRAP AND INSTALLED REPAIR STRAP. ALL WORK DONE IAW SR 27-53- 023A.Oct 7, 2003 · N217FE · Boeing 727200 · Fuselage Main, KeelSDR 2003F00597Charger · failedBATTERY CHARGER FOR L1 EMERGENCY EXIT LIGHTING NOT CHARGING. REMOVED AND REPLACED CHARGER UNIT PER MM 33-50-51. (M)Oct 6, 2003 · N288SC · Boeing 727200 · Emergency LightingSDR 03FDEA01696Frame · dentedFWD CARGO SIDE FRAME DENTED STA 680, LBL 33, WL 160 . OUT OF LIMITS. CUT OUT DAMAGE & REPAIRED FRAME BS 680, LBL 33, WL 160 PER SRM 53-10- 1, 51-40-3 FIG 1 AND FED EX EA 7-5310-55028.Oct 3, 2003 · N217FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA01700Frame · dentedFWD CARGO SIDE FRAME DENTED STA 680 RBL 30 WL 157. FWD CARGO SIDE FRAME DENTED STA 680, RBL 30, WL 157 FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REPAIR FRAME PER SRM 51-40-3.Oct 3, 2003 · N217FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA01698Frame · dentedFWD CARGO SIDE FRAME DENTED STA 720 LBL 34 WL 160. DENT OUT OF LIMITS. CUT OUT DAMAGE AND REPAIRED FRAME BS 720, LBL 34, WL 160 IAW SRM 53-10-1, 51-40-3 FIG 1 AND FED EX EA 7-5310-55029.Oct 3, 2003 · N217FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA01697Frame · dentedFWD CARGO SIDE FRAME DENTED STA 700 LBL 50 WL 166 FWD CARGO FRAME DENTED AT STA 700, LBL 50, WL 166 FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REPAIRED DAMAGE FRAME PER SRM 51-40-3. ALSO REPAIRED PER FED EX EA 7-5310-55031.Oct 3, 2003 · N217FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA01699Frame · dentedFWD CARGO SIDE FRAME DENTED STA 660 RBL 35 WL 160 ** SD ** COMINGOct 3, 2003 · N217FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA01691Keelbeam · corrodedCORROSION ON OB FLANGE OF S28-R KEELBEAM, STA 720E TO 720F. REPAIRED PER E.A. 7-5310-55007.Oct 2, 2003 · N469FE · Boeing 727200 · Fuselage Main, KeelSDR 03FDEA01690Keelbeam · corrodedCORROSION ON OUTBOARD FLANGE OF S28-L KEELBEAM, STA 720E TO 720F. REPAIRED PER E.A. 7-5310-55007.Oct 2, 2003 · N469FE · Boeing 727200 · Fuselage Main, KeelSDR 03FDEA01682Vent · crackedLT WING FWD VENT BOX TAB CRACKED AT STA. 656.60. REPAIRED IAW EA 7-5710-55011.Oct 2, 2003 · N468FE · Boeing 727200 · Wing Miscellaneous Structure
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