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 05FDEA04187Seal Depressor · chafedLOWER FWD CARGO DOOR, LOWER DOOR FRAME IS CHAFED. REMOVED AND REPLACED LWR FWD CARGO DOOR FRAME PER SRM 51-30-2.Dec 8, 2005 · N485FE · Boeing 727200 · Cargo/Baggage DoorsSDR 05FDEA04186Stringer · corrodedSTR 28L BS 950-1009 HAS SEVERAL AREAS OF CORROSION. REMOVED DAMAGED STRINGER 28L FROM BS 950-1009 AND REPLACED PER SRM 53-10-3 FIG 1 AND SRM 51-30-02Dec 8, 2005 · N485FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 05FDEA04185Repair · improperREPAIR LOCATED AT STA 950F - 970 STRINGER 29-R REQUIRES EVALUATION FOR MAJOR / MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED REPAIR AT STA BS 950F - 970 STRINGER 29R IAW B727 SRM 51-30-2. FABRICATED NEW REPAIR PARTS IAW Dec 8, 2005 · N486FE · Boeing 727200 · Fuselage Main, StructureSDR 05FDEA04184Floorbeam · corrodedREWORK OF FEDEX SNRM N00773 DUE TO IMPROPER SRM REPAIR APPLICABILITY MAIN DECK FLOORBEAM CORRODED ON TOP TWO PLACES AT STA BS 312 BETWEEN LBL 4 AND LBL 20. REMOVED IMPROPER REPAIR IAW B727 SRM 51-30-2. FABRICATED REPAIR ANGLES AND TEE CAP SECTION IAW B727 SRDec 8, 2005 · N486FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 05FDEA04182Skin · corrodedAFT PIT HAS EXFOLIATED SKIN AT STA 1044 TO 1050 STR 29R-28R. REMOVED DAMAGE IAW B727 SRM 53-30-3 FIG 3 SHEET 1. FABRICATED AND INSTALLED DOUBLER IAW B727 SRM 53-30-3 FIG 3, 51-10-2 AND 51-30-2, MECH NR 7990 QC 362, MAJOR REPAIR.Dec 8, 2005 · N220FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 05FDEA04177Rib · gougedWHILE WORKING CARD NR N00763 FOUND RT NR 5 ELEVATOR HINGE, SUPPORT RIB L/E GOUGED. REPAIRED RIB PER FED EX EA 7-5510-91427.Dec 8, 2005 · N485FE · Boeing 727200 · Elevator, Spar/RibSDR 05FDEA04172Skin · bulgedN00204 BS 206, STR 24-24L, 2 INCH CREASED BULGE IN THE SKIN. REPAIRED FUSELAGE SKIN AT BS 206, STR 24L-25L AS PER FED EX EA 7-5310-91431Dec 7, 2005 · N485FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 05FDEA04157Floor Support · corrodedN00770 CORROSION (C53-221-01) BS 304, WL 208, LBL 12 TO 50 HOZ FLOOR SUPPORT UPPER FLANGE. REPAIRED FLOOR SUPPORT IAW SRM 51-30-2.Dec 6, 2005 · N490FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 05FDEA04159Strap · corrodedCORROSION ON TENSION STRAP BS 1070 RBL 45 WL 201. REPAIRED TENSION STRAP IAW SRM 53-10-8 FIG 6.Dec 6, 2005 · N490FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 05FDEA04145Flap Track · corrodedN01126 LT WING IB FLAP OB FLAP TRACK CORRODED ON AFT ATTACH POINT. ** SD ** COMING REPLACED FLAP TRACK IAW W/C 27X5705-03Dec 5, 2005 · N485FE · Boeing 727200 · Trailing Edge FlapsSDR 05FDEA04144Intercostal · crackedINTERCOSTAL CRACKED BS 950B-2, STR 29R WL 155. REPAIRED IAW SRM 51-40-2.Dec 5, 2005 · N485FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 05FDEA04143Window · brokenPDIS 237 56-10 0007743 04DEC05 FSD CLOSE R AT FL200, CAPT'S NR1 WINDSCREEN OUTER PANE CRACKED. TURNED CAPT'S WINDOW HEAT OFF AND COMPLIED WITH QRH PROCEDURE. FACT 04DEC05 23:58 FSD U REMOVED AND REPLACED L-1 WINDOW IAW AMM 56-11-011-4. ALSO REMOVED Dec 5, 2005 · N237FE · Boeing 727200 · Flight Compartment WindowsSDR 05FDEA04109Union · leakingAFTER T/O WHEN GEAR LVR WAS RAISED TO THE UP POS THE HYD SYS (A) RESERVOIR WENT TO ZERO. THE GEAR REMAINED DOWN AND FLAPS STAYED AT 15 DEG. REMOVED AND REPLACED PACKING AND UNION FOR THE OB TE FLAP CONTROL VALVE IAW IPC REF 27-50-00-30AZZ ITEM 145. LEAK ANDec 3, 2005 · N240FE · Boeing 727200 · Hydraulic System, MainSDR 05FDEA04052Panel · misinstalledINCORRECT REFERENCE WAS USED TO DETERMINE IF HORZ STAB REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA - PREVIOUS REPAIR ON LEFT HORIZONTAL STABILIZER AT STAB STA 115, 3" WIDE X 3" LONG, 15" AFT OF STAB REAR SPAR. ** SD ** COMING REPLACED PREVIODec 1, 2005 · N466FE · Boeing 727200 · Horizontal Stabilizer StructureSDR 05FDEA04023Flap Track · corrodedRIGHT WING INB FLAP OUTB TRACK FORWARD MOUNT HOLE "D" HAS PITTING IN INNER BORE. REMOVED PITTING , FABRICATED AND INSTALLED REPAIR BUSHING AND FINAL REAM ID IAW BAC OHM57-40-01.Nov 29, 2005 · N220FE · Boeing 727200 · Trailing Edge FlapsSDR 05FDEA03999Skin · chafedLOWER AFT CARGO DOOR OUTER SKIN IS CHAFED ALONG FAIRING RUB STRIP. REPAIRED LOWER AFT CARGO DOOR OUTER SKIN PER 52-00-3 FIG 4.Nov 28, 2005 · N485FE · Boeing 727200 · Cargo/Baggage DoorsSDR 05FDEA03998Skin · dentedN00222 BS 1170 STR. 23-24L DENT IN SKIN ** SD ** COMING DENT ON SKIN WAS FOUND TO BE OUT OF LIMITS, REPAIRED DENT ON SKIN AT BS 1170, STR 23L-24L, IAW SRM 53-30-3.Nov 28, 2005 · N485FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 05FDEA04001Frame · dentedAFT CARGO COMPARTMENT, DENT IN FRAME BS 950C RBL 36 WL 152. REMOVED DENT DAMAGE AREA, FABRICATED REPAIR PART AND INSTALLED IAW SRM 51-40-3.Nov 28, 2005 · N485FE · Boeing 727200 · Fuselage Main, FrameSDR 05FDEA04000Stringer Clip · damagedMECHANICAL DAMAGE TO STRINGER CLIP BS 950C STRINGER 5 RT. REPAIRED STRINGER CLIP PER SRM 53-10-1, 51-30-2.Nov 28, 2005 · N485FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 05FDEA03962Switch · malfunctionedAMBER AFT AIRSTAIR LIGHT ILLUMINATED DURING CLIMB THROUGH 27,000 MSL. ACCOMPLISHED QRH. LANDED UNEVENTFULLY. OPENED AFT AIRSTAIRS, CLEANED SWITCHES, AND CHECKED DOOR WARNING SYSTEM PER M/M 52-70-001-5. OPS CHECKS NORMAL. OK FOR SERVICE.Nov 26, 2005 · N288FE · Boeing 727200 · Door Warning SystemSDR 05FDEA03961Door Frame · corrodedCORROSION ALONG INSIDE OF NR 3 LOWER CARGO DOOR CUTOUT ATF LOWER CORNER. REPAIRED PER E.A 7-5310-92359 FUSELAGE CORROSION ON AFT FRAME OF NR 3 CARGO DOOR OPENING.Nov 25, 2005 · N266FE · Boeing 727200 · Fuselage Main, StructureSDR 72000002Jackscrew · jammedSTRONG SHUDDER IN AIRCRAFT, TRIM THEN RAN AWAY. SHUDDER LASTED FOR APPROX 10-15 SECONDS. TRIM THEN JAMMED BUT WAS MANUALLY OPERATIONAL AFTER PROCEDURES. EMERGENCY LANDING, DIVERTED FROM ROC TO SYR DUE TO WEATHER.Nov 23, 2005 · N720CK · Boeing 727200 · Stabilizer Control SystemSDR A0512001Jackscrew · failedON APPROACH, WITH FLAPS SELECTED TO 5 DEG, STAB TRIM WHEEL RAN AWAY FROM APPROX 5 UNITS NOSE UP TO 0 DEG AND BUFFETING WAS FELT IN FLT CONTROLS. AC STARTED A 2000 TO 4000 RPM RATE OF DESCENT, PILOTS TRIED TO INPUT UP ELEVATOR TO ARREST SINK RATE, THERE WAS NONov 22, 2005 · N720CK · Boeing 727200 · Flight Control SystemSDR 05FDEA03942Engine · malfunctionedAFTER 20 MINUTES AT CRUISE, NR 3 OIL PRESSURE READ 34 PSI. WENT TO QRH, RETARDED THROTTLE AND OIL TEMP ROSE TO 120 C. ALL OTHER INDICATIORS WERE GOOD. SHUT ENGINE DOWN IAW QRH, DIVERTED TO CVG.Nov 22, 2005 · N482FE · Boeing 727200 · Engine Oil QuantitySDR 05FDEA03924Engine · malfunctionedON CLIMBOUT NR 3 ENG OIL PRESS WENT TO 30PSI AND OIL T EMP WENT TO 130C. SHUT DOWN ENG NR 3 IAW QRH AND RETURNED TO MEMPHIS. ACCOMP ENG WINDMILLING CK AND R&R OIL FILTER PER M/M 72-00-00, PG 531. RAN ENG AND OPS CKS GOOD AT IDLE. ADJ OIL PRESS RELIEF VALNov 20, 2005 · N482FE · Boeing 727200 · Engine Oil QuantitySDR 72000001Stabilizer · jammedAIRCRAFT TOOK OFF FROM KATL TOWARD KYIP. STABILIZER JAMMED IN A VERY NARROW RANGE FROM 2 DEG UP TO 2 DEG DOWN. CREW ELECTED TO RETURN TO KATL.Nov 19, 2005 · N720CK · Boeing 727200 · Stabilizer Control SystemSDR 05FDEA03897Skin · misdrilledLT IB TE MIDFLAP LWR AFT SKIN HAS NUMEROUS FASTENER HOLES DOUBLE DRILLED OR EXCESSIVELY COUNTERSUNK, O/B OF O/B FLAP TRACK. REPAIRED LT IB MIDFLAP LOWER AFT SKIN PER SRM 51-40-2.Nov 18, 2005 · N466FE · Boeing 727200 · Trailing Edge FlapsSDR 05FDEA03872Repair · unknownEXISTING EXTERNAL REPAIR ON FUSELAGE BS 860-880 STR 8R-10R. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. ALL WORK WAS ACCOMPLISHED IAW FED EX E.A. 7-5330-91421. REPAIR WAS DETERMINED TO BENov 18, 2005 · N466FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 05FDEA03871Shear Tie · corrodedEXERNAL FUSELAGE SKIN PILLOWING AROUND SHEAR TIE FASTENERS AT BS 1090, STR 28 - 29 LEFT. REMOVED SHIM BETWEEN SHEAR TIE & FUSELAGE SKIN AT BS 1090 STR 28-29L FABRICATED NEW SHIM & INSTALLED PER SRM 51-10-2, 51-30-2.Nov 18, 2005 · N485FE · Boeing 727200 · Fuselage Internal Mounting StructureSDR 05FDEA03860Repair · undamagedFOUND ROUND REPAIR AT STA 370 STR 16L. REPAIR REQUIRES EVALUATION FOR MAJOR / MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR AT STA 370 STR 16L WAS DETERMINED TO BE IAW FEDEX EO 7-5100-7-2307H - DATE 0Nov 17, 2005 · N266FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 05FDEA03857Skin · corrodedEXTERNAL FUSELAGE SKIN PILLOWING AROUND FASTENER HEADS AT BS 1051, STR 29 LEFT. SUSPECT CORRODED STRINGER. REMOVED CORROSION FOUND OUT OF LIMITS. REMOVED AREA OF DAMAGE, FABRICATED REPAIR DOUBLER AND FILLER AND ISNTALLED, IAW SRM 53-30-3.Nov 17, 2005 · N485FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 05FDEA03845Depressor · crackedUPON REMOVAL OF AFT CARGO DOOR LOWER SEAL DEPRESSOR, FOUND STUB FRAME CRACKED AT BS 950F, RBL 40, WL 148 SECOND FRAME AFT FROM FWD SIDE OF DOOR. REMOVED AND REPLACED STUB FRAME AT BS 950F, RBL 40 WL 148 IAW SRM 51-30-2 AND SRM 51-30-5.Nov 16, 2005 · N466FE · Boeing 727200 · Cargo/Baggage DoorsSDR 05FDEA03846Repair · properFOUND 2 REPAIRS ON LOWER AFT CARGO DOOR. REPAIRS REQUIRE EVALUATION FOR MAJOR / MINOR DETERMINATION AND IF REPAIRS WERE ACCOMPLISHED USING FAA APPROVED DATA. TWO PREVIOUSLY INSTALLED REPAIRS ON LOWER AFT CARGO DOOR NR 3 WERE DETERMINED TO BE IAW SRM 52-00-3 Nov 16, 2005 · N266FE · Boeing 727200 · Cargo/Baggage DoorsSDR 05FDEA03841Frame · dentedAFT CARGO COMPARTMENT, FRAME IS DENTED BS 950B LBL 27 WL 148. REPAIRED FRAME PER SRM 51-40-3.Nov 16, 2005 · N485FE · Boeing 727200 · Fuselage Main, FrameSDR 05FDEA03840Frame · dentedAFT CARGO COMPARTMENT, FRAME IS DENTED BS 1010 LBL 27 TO LBL 30 WL 150 TO WL 153. DENT IN FRAME FOUND TO BE OUT OF LIMITS, CUT OUT DAMAGE FABRICATED DOUBLER, ALODIEND & PRIMED, INSTALLED FASTENERS IN REPAIR SRM 51-30-2.Nov 16, 2005 · N485FE · Boeing 727200 · Fuselage Main, FrameSDR 05FDEA03844Stringer · corrodedCORROSION (C53-111-01) AFT CARGO COMPARTMENT ON STR 29 STA 1050. REPAIRED STR 30 BS 1050 PER SRM 53-10-3.Nov 16, 2005 · N485FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 05FDEA03843Keelbeam · corrodedSTR 29L KEEL BEAM BS 950C TO 950D WL 148 HAS CORROSION (C53-113-01).Nov 16, 2005 · N485FE · Boeing 727200 · Fuselage Main, KeelSDR 05FDEA03842Frame · dentedAFT CARGO COMPARTMENT, FRAME IS DENTED BS 990 LBL 29 WL 150. REPAIRED FRAME, BS 990, LBL 29, WL 150 PER SRM 51-40-3.Nov 16, 2005 · N485FE · Boeing 727200 · Fuselage Main, FrameSDR 05FDEA03837Indicator · inoperativeCREW REPORTS NR 3 EPR IND INOP/ERRATIC ON TAKEOFF ROLL. REPORTS ALL OTHER INDICATIONS NORMAL. RELEASED FOR SERVICE PER MEL/CDL: 77-01-01. MEL 77-01-01: NR 3 ENGINE EPR INDICATOR INOP. PLACED ON MEL DEFERRAL 77-01-01. EXPIRES 19 NOV 2005. OK FOR SERVICE. Nov 16, 2005 · N287FE · Boeing 727200 · Engine Pressure Ratio (EPR)SDR DHL2005749027Stringer · damagedACCOMPLISH IDENTIFICATION OF EXISTING STRINGER SPLICE REPAIR AT STA 600 STR 28L. EXISTING REPAIR FOUND TO BE NON COMPLIANT IAW 727 SRM 53-10-3 FIG 1 TABLE I. REMOVED EXISTING REPAIR IAW 727 SRM 51-30-2 FABBED AND INSTALLED NEW STR SECTIONS 2EA FROM BAC1498-Nov 9, 2005 · N749DH · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 05FDEA03716Stringer · damagedEXISTING STRINGER REPAIR IN FWD CARGO BAY BS 480-530 S28R. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED AND REPLACED AFT SPLICE PER SRM 53-10-3.Nov 8, 2005 · N466FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 05FDEA03715Shear Tie · unknownEXISTING FRAME SHEAR TIE REPAIR AT BS 680 STR 26L-27L. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR WAS ACCOMPLISHED PER SRM 53-10-4.Nov 8, 2005 · N466FE · Boeing 727200 · Fuselage Internal Mounting StructureSDR DHL2005749026Seat Track · corrodedFOUND CORROSION ON SEAT TRACK AT RBL24 BS 770-800. CLEANED CORROSION IAW B727 SRM 51-0-6 AND FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-10-1 FIG 3. REMOVED SEAT TRACK SECTION AT RBL 24 BS 757-852 IAW B727 SRM 51-30-2 TREAT AT PRIMED AREA IAW B727 SRM 51-10-2.Nov 7, 2005 · N749DH · Boeing 727200 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2005749025Seat Track · corrodedFOUND CORROSION ON SEAT TRACK AT RBL 45 BS 770-850. REMOVED SEAT TRACK BS 757-852 RBL 45 AND FABBED NEW FROM BAC 1520-841 PO 9002277 DIM 95" IN LENGTH IAW B727 SRM 53-10-2 FIG 7 AND 53-10-5 FIG 2 LWR SURFACED TREATED AND PRIMED IAW B727 SRM 51-10-2. INSTALLENov 7, 2005 · N749DH · Boeing 727200 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2005749023Skin · crackedDISCREPANCY NR113286 AS FOLLOWS; GAIN INTERNAL ACCESS TO 3 REPAIRS ON EMP SKIN AT AIR START DOOR, LT AIRSTAIR CUT OUT AND RT AIRSTAIR CUT OUT. REMOVED AIRSTAIRS CUT OUT TORQUE BOX WEB FOR ACCESS IAW B727 SRM 51-30-2 AND FOUND RT SKIN ATTACH ANGLE CRACKED. RENov 7, 2005 · N749DH · Boeing 727200 · Fuselage Main, Plate/SkinSDR 05FDEA03697Stringer · unknownMAPPED EXISTING REPAIR ON STRINGER, BS 720 F-740, STR 26R. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. STRINGER REPAIR AT BS 720F-740 STR 26 RT ORIGINAL THICKNESS IS 0.080 HAT SECTION INov 7, 2005 · N466FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 05FDEA03696Stringer · unknownEXISTING STRINGER REPAIR IN FWD CARGO BAY AT BS 643-674 S28R. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIRED STRINGER AT BS 643-674, STR 28R PER SRM 53-10-3.Nov 7, 2005 · N466FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 05FDEA03694Frame · damagedSTA 312 STR 22L, FRAME CRACKED AT PREVIOUS REPAIR. REMOVED AND REPLACED FRAME WEB BS 312 STR 21-23L PER SRM 51-30-2Nov 7, 2005 · N466FE · Boeing 727200 · Fuselage Main, FrameSDR 05FDEA03693Floorbeam · damagedEXISTING UPPER FLOOR BEAM REPAIR AT BS 1030 LBL 10 WL 208, REPAIR REQUIRED EVALUATION FOR MAJ OR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USIING FAA APPROVED DATA. EVALUATED EXISTING REPAIR TO BS 1030 UPPER FLOORBEAM LBL 10 WL 208, TO BE A MAJORNov 7, 2005 · N466FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 05FDEA03692Frame · damagedSTA 321 STR 22L, FRAME CRACKED AT PREVIOUS REPAIR. REMOVED PREVIOUS REPAIR DOUBLER, FABRICATED, DRILLED, ALODINED, PRIMED REPAIR DOUBLER CAP, AND INSTALLED BS 321 STR 22L PER SRM 51-40-3.Nov 7, 2005 · N466FE · Boeing 727200 · Fuselage Main, Frame
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