Boeing 727-200

Service difficulty reports · 2,835

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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 = '727200'
  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 05FDEA01924Stringer Clip · crackedCRACKED STRINGER CLIP BS 990 AT STRINGER 28L FWD SIDE OF FRAME. REPLACED CRACKED STRINGER CLIP PER SRM 51-10-1.Jul 13, 2005 · N218FE · Boeing 727200 · Fuselage Main, Attach FittingsSDR 05FDEA01923Stringer Clip · crackedFUSELAGE UPPER LOBE, STRINGER CLIP IS CRACKED, BS 680, STR 7R. REMOVED, FABRICATED AND INSTALLED STRINGER CLIP AT BS 680 STR 7R IAW SRM 51-30-02 AND DRAWING 65-45313.Jul 13, 2005 · N218FE · Boeing 727200 · Fuselage Main, Attach FittingsSDR 05FDEA01922Stringer Clip · missingFUSELAGE UPPER LOBE STRINGER CLIP MISSING FRAME ATTACH FASTENERS BS 680, STR 6L. REMOVED, FABRICATED AND INSTALLED STRINGER CLIP AT BS 680 STR 6L IAW SRM 51-20-1, 51- 30-02 AND 51-10-02.Jul 13, 2005 · N218FE · Boeing 727200 · Fuselage Main, Attach FittingsSDR 05FDEA01920Stringer Clip · crackedFUSELAGE UPPER LOBE, STRINGER CLIP IS CRACKED, BS 660, STR 8R. REMOVED FABRICATED AND INSTALLED STR. CLIP AT BS 660 STR 8R IAW SRM 51-20-1 & 51-30- 02.Jul 13, 2005 · N218FE · Boeing 727200 · Fuselage Main, StructureSDR 05FDEA01919Stringer Clip · crackedFUSELAGE UPPER LOBE, STRINGER CLIP IS CRACKED, BS 700, STR 6. REMOVED FABRICATED AND REPLACED STRINGER CLIP AT BS 700 STR 6R PER SRM 51-30-02, 51-20-1, 51-10-02Jul 13, 2005 · N218FE · Boeing 727200 · Fuselage Main, Attach FittingsSDR 05FDEA01918Stringer Clip · crackedFUSELAGE UPPER LOBE, STRINGER CLIP CRACKED, BS 640, STR. 9 RT.Jul 13, 2005 · N218FE · Boeing 727200 · Fuselage Main, Attach FittingsSDR 05FDEA01832Plate · gougedMAIN CARGO DOOR BS 460 TO 640 LBL 45 WL 295 DOOR CUTOUT INNER PLATE HAS NUMEROUS GOUGES. *S/D* BLENDED AND REPAIRED GOUGES IN MAIN CARGO DOOR INNER PLATE IAW EA 7-5330-89309.Jul 7, 2005 · N263FE · Boeing 727200 · Fuselage Main, StructureSDR 05FDEA01830Plate · gougedMAIN CARGO DOOR BS 460 TO 480 LBL 24 WL 287 DOOR CUTOUT INNER PLATE HAS NUMEROUS GOUGES. *S/D* BLENDED NUMEROUS GOUGES IN DOOR CUTOUT INNER PLATE IAW EA 7-5330-89309.Jul 7, 2005 · N263FE · Boeing 727200 · Fuselage Main, StructureSDR 05FDEA01828Skin · gougedMAIN CARGO DOOR BS 620 TO 640 LBL 24 WL 287 DOOR CUTOUT INNER PLATE HAS NUMEROUS GOUGES. *S/D* BLENDED NUMEROUS GOUGES AT MAIN CARGO DOOR CUTOUT INNER PLATE PER EA 7-5330-89309.Jul 7, 2005 · N263FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 05FDEA01824Skin · lightning strikeLIGHTNING STRIKE IN SKIN AT BS 441 1.5 X 1.5 INCH AT STR 23. *S/D* REPAIRED LIGHTNING STRIKES IAW SRM 53-30-3.Jul 7, 2005 · N263FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 05FDEA01822Skin · gougedFUSELAGE EXTERNAL SKIN, SECTION 48, BS 1329 LBL 22 3 INCHES O/B OF AFT AIRSTAIR CUTOUT GOUGED. *S/D* GOUGED IN EXTERNAL SKIN OF THE AFT AIRSTAIR CUTOUT AT BS 1329 LBL 22 WAS OUT OF LIMITS IAW SRM 53-30-1. CUT OUT DAMAGE AND FABRICATED REPAIR IAW SRM 51-10Jul 7, 2005 · N263FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 05FDEA01778Seat Track · corrodedSEAT TRACK LBL 24 HAS CORROSION AT 500 TO 520 AND STA 620. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-10-5 FIG 1 PG 4Jul 2, 2005 · N272FE · Boeing 727200 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA01776Tee Fitting · corrodedTEE CHORD 760 -787 RBL 45 IS CORRODED. REMOVED AND REPLACED TEE CHORD IAW SRM 51-30- 2Jul 1, 2005 · N272FE · Boeing 727200 · Fuselage Main, StructureSDR 05FDEA01775Tee Fitting · corrodedTEE FITTING APPROX STA 760-787 RBL 45 IS CORRODED. REMOVED AND REPLACED TEE FITTING IAW SRM 51-30-2Jul 1, 2005 · N272FE · Boeing 727200 · Fuselage Main, StructureSDR 05FDEA01774Seat Track · corrodedSEAT TRACK STA 740-760 LBL 24 IS CORRODED. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-1.Jul 1, 2005 · N272FE · Boeing 727200 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA01759Transmitter · malfunctionedON TAKEOFF WITH STANDARD EPR SET NR3 N1,N2 AND FUEL FLOW WERE LOW. AC RELEASED FOR SERVICE IAW MEL/CDL: 77-01-01 01JUL05 14:55 ORF REMOVED PT2 SENSOR FROM ENG, BLEW AIR THROUGH LINE TO INSURE NO OBSTRUCTIONS PRESENT. RE-INSTALLED SAME. DISCONNECTED NR3 Jul 1, 2005 · N465FE · Boeing 727200 · Power Indicating SystemSDR 05FDEA01767Compressor · stalledON TAKEOFF ROLL THROTTLES SMOOTHLY ADVANCED TO T/O PWR NR 2 ENGINE HAD AVERY PRONOUNCED COMPRESSOR STALL APPROX. 5-8 SEC. INTO TAKEOFF ROLL REJECTED T/O AND CLEARED RUNWAY. INSPECTED INLET AND EXHAUST NO DAMAGE NOTED. PERFORMED TAKEOFF POWER EPR TEST REF Jun 30, 2005 · N488FE · Boeing 727200 · Turbine Engine Compressor SectionSDR 05FDEA01751Warning Light · false indicationDURING CLIMBOUT AT FL 220 HAD INTERMITTENT MASTER FIRE WARNING LIGHT AND TESTED ENGINE AND CARGO FIRE SYSTEMS, ALL TESTED OK. DURING CRUISE AT 330 ABOUT 30 MINS LATER, APU FIRE LIGHT ILLUMINATED. NO WARNING BELL JUST THE LIGHT IN THE HANDLE. RAN RED TABS PULLEJun 30, 2005 · N461FE · Boeing 727200 · Fire DetectionSDR 05FDEA01748Seat Track · corrodedSEAT TRACK LBL 24 IS CORRODED 690 - 740. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-30-2Jun 30, 2005 · N272FE · Boeing 727200 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA01747Seat Track · corrodedSEAT TRACK STA 480 - 690 AT LBL 45 HAS CORROSION . REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-2Jun 30, 2005 · N272FE · Boeing 727200 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA01723Cover · crackedPANEL RACK NR 1 ENGINE UPPER AFT THRUST REVERSER PANEL CRACKED AND GOUGED AT BOTH ENDS. REPLACED PART TO BE INSTALLED DURING C-CHECK.Jun 28, 2005 · N203FE · Boeing 727200 · Engine Thrust ReverserSDR 05FDEA01722Antenna · delaminatedNR 1 ADF LOOP ANTENNA IS DELAMINATED. REMOVED AND REPLACED NR 1 ADF ANTENNA IAW MM 34-37-012-4. OPS CHECKED GOOD IAW M/M 34-37-001-5Jun 28, 2005 · N203FE · Boeing 727200 · Long-Range Navigation (LORAN) SystemSDR 05FDEA01721Floor Support · corrodedAFT PIT BS 950A BL 0 FLOOR SUPPORT ANGLE HAS CORROSION UNDER NUT PLATES. REPLACED FLOOR SUPPORT ANGLE IAW SRM 51-30-2Jun 28, 2005 · N203FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 05FDEA01720Frame · crackedCOCKPIT LT FRAME STA 277 BTWN STR S-14 TO S-16 FRAME WEB ANGLES CRACKED AT FWD & AFT SIDE OF FRAME AT 6 EA PLACES AS MARKED. REPAIRED FRAME WEB ANGLE IAW SRM 53-10-4 MAJOR REPAIRJun 28, 2005 · N203FE · Boeing 727200 · Fuselage Main, FrameSDR 05FDEA01719Hinge Fitting · crackedAFT FLAP RT INBD AT HINGE FITTING 111.0 FROM INBD, LE LWR SKIN CRACKED (.450 LONG) REPLACED FLAP ON W/C 76C071-00Jun 28, 2005 · N203FE · Boeing 727200 · Trailing Edge FlapsSDR 05FDEA01718Frame · chafed344 FRAME CHAFED AT STR'S 4R,6R & 8R. FABRICATED AND INSTALLED REPAIR CHANNEL IAW SRM 51-40-3Jun 28, 2005 · N272FE · Boeing 727200 · Fuselage Main, FrameSDR 05FDEA01715Support Angle · chafedLT MLG FWD TRUNNION I/B SUPPORT ANGLE IS CHAFED ON LWR EDGE. REPAIR (BLENDED), STRESS RELIEVED AND REFINISHED LT MLG FWD TRUNNION SUPPORT ANGLE ON LWR EDGE IAW SRM 51-10-1, SOPM 20-10-03 AND FED EX EA 7-5710-86323 REPAIR WITHIN LIMITS IAW EA - 7-5710-86323Jun 28, 2005 · N263FE · Boeing 727200 · Main Landing GearSDR 05FDEA01646Spar · corrodedCORROSION ON RT WING FUEL CELL FWD SPAR WEB FWD FACE AROUND CUTOUT 7540R. *S/D* REPAIRED RIGHT WING FUEL CELL FWD SPAR WEB FACE AROUND PANEL 7540 PER FED EX EA 7-5710-86300.Jun 22, 2005 · N482FE · Boeing 727200 · Wing SparSDR 05FDEA01645Control Valve · lack of lubeL/E DEVICES WOULD NOT RETRACT AT FLAPS 2 DEGREES. PERFORMED ADJUSTMENT AND TEST OF FLAP 2 DEG SWITCH AS PER M/M 27-82-021-2, OPS CK GOOD. INSPECTED PULLEYS ROD END GOING TO FLAP CONTROL VALVE AND LUBED AS NEEDED. FLAPS AND LEADING EDGE DEVICES GROUND CKS NOJun 22, 2005 · N211FE · Boeing 727200 · Trailing Edge Flap Control SystemSDR 05FDEA01628Floorbeam · corrodedCORROSION ON FLOORBEAM LBL 25 - RBL 25 BS 620. CORROSION FOUND TO BE OUT OF LIMITS REPAIRED FLOORBEAM IAW SRM 53-10-8 FIG 3Jun 21, 2005 · N264FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 05FDEA01629Floorbeam · corrodedCORROSION ON FLOORBEAM LBL 12 BS 480. FABRICATED AND INSTALLED FLOORBEAM REPAIR LBL 12, BS 480 PER SRM 53-10-08 FIG 3Jun 21, 2005 · N264FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 05FDEA01619Attach Angle · damagedNR 2 SPOILER ACTUATOR LWR ATTACH ANGLE HOLES ARE ELONGATED. *S/D* REPLACED NR 2 SPOILER ACTUATOR SUPPORT FITTING PER SRM 51-30-2.Jun 19, 2005 · N482FE · Boeing 727200 · SpoilersSDR 05FDEA01617Frame · damagedWHILE WORKING N01404 FOUND HOLES IN FRAME AT BS 520 RBL 65 WL 201 DAMAGE. *S/D* REMOVED AND REPLACED BS 520 FRAME SEGMENT STR 13R TO 25R, FOUND TO BE A MAJOR REPAIR PER SRM 51-30-5 AND 51-30-2.Jun 17, 2005 · N482FE · Boeing 727200 · Fuselage Main, FrameSDR 05FDEA01616Keelbeam · corrodedAFT CARGO CORROSION ON KEELBEAM STA 950D TO 950E, STR 29L. BLENDED CORROSION AT KEELBEAM STA 950D TO 950E OUT OF LIMITS. INSTALLED REPAIR IAW SR27-53-023A. FOUND TO BE A MINOR REPAIR.Jun 17, 2005 · N263FE · Boeing 727200 · Fuselage Main, KeelSDR 05FDEA01612Stringer · crackedCRACKED STRINGER INSIDE VERTICAL STAB AT STRINGER 7 FIN STATION 157.2 LT. REPAIRED STRINGER PER SRM 55-30-4 FIG 1.Jun 16, 2005 · N477FE · Boeing 727200 · Vertical Stabilizer, Spar/RibSDR 05FDEA01613Stringer · corrodedFOUND STRINGER 27R TO BE CORRODED BS 1178.Jun 16, 2005 · N477FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 05FDEA01611Skin · dentedLEFT HORIZONTAL STAB UPPER SURFACE HAS DENT WITH GOUGE 17.5 INCHES FROM I/B END AND 16.5 INCHES FROM AFT END. REPAIRED PER FED EX EA 7-5510-86317.Jun 15, 2005 · N477FE · Boeing 727200 · Horizontal Stabilizer, Plate/SkinSDR 05FDEA01610Stringer · crackedWHILE WORKING N00525, FOUND RT WING UPPER STRINGER NR 10 CRACKED AT WS 686.5 RIB BOLT. REPAIRED STRINGER PER FED EX EA 7-5710-86308.Jun 15, 2005 · N477FE · Boeing 727200 · Wing Main, Frame StructureSDR 05FDEA01609Flap Track · corrodedNR 3 FLAP TRACK HAS CORROSION EMINATING FROM AFT ATTACH AREA. REPLACED NR 3 FLAP TRACK PER MM 27-51-031-4Jun 15, 2005 · N482FE · Boeing 727200 · Trailing Edge FlapsSDR 05FDEA01603Frame · damagedN01425 BS 360, STR 2R BS 360 S2R FRAME IS DAMAGED AT TOOLING HOLE. REPAIRED FRAME PER SRM 51-40-3Jun 14, 2005 · N482FE · Boeing 727200 · Fuselage Main, FrameSDR 05FDEA01607Skin · corrodedAFT FUSELAGE LOWER SKIN EXTERNAL SURFACE APPROX FS 1010 BETWEEN STRINGERS 27L AND 28L AREA IS EXFOLIATED CORROSION. REPAIRED DAMAGED AREA IAW SRM 53-30-3 FIG 3, MAJOR REPAIR.Jun 14, 2005 · N266FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 05FDEA01606Skin · delaminatedRIGHT WING UPPER SURFACE PANEL AT APU EXHAUST HAS DELAMINATION, CORROSION AND OLD REPAIR TORN OFF JUST AFT OF EXHAUST PORT. FABRICATED NEW PANEL AND INSTALLED NEW PANEL IAW SRM 51-30-5 & 51-30-2.Jun 14, 2005 · N262FE · Boeing 727200 · Wing, Plate/SkinSDR 05FDEA01604Doubler · gougedCOMPLY WITH EA 7-5330-87786, FUSELAGE -PLATING -GOUGE IN MAIN CARGO DOOR CUTOUT REINFORCEMENT DOUBLER AND TRIPLER. COMPLIED WITH EA 7-5330-87786 - FUSELAGE PLATING GOUGED IN MAIN CARGO DOOR CUTOUT REINFORCEMENT DOUBLER & TRIPLER (MINOR REPAIR).Jun 14, 2005 · N262FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 05FDEA01597Floor Support · crackedAFT CARGO COMPT FLOOR SUPPORT IS CRACKED AT FS 1030-1050 RBL 11. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 27-53-039.Jun 13, 2005 · N262FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 05FDEA01596Floor Panel · crackedCOCKPIT F/O OUTBOARD RUDDER PEDAL FLOOR PANEL CRACKED. REMOVED AND REPLACED PANEL IAW SRM 51-30-2.Jun 13, 2005 · N203FE · Boeing 727200 · Fuselage Floor PanelSDR 05FDEA01602Antenna · corrodedFWD LOWER FUSE ADF ANT BASE CORRODED. REMOVED AND REPLACED ADF ANTENNA IAW MM 34-37-012-4, OPS CHECKS GOOD.Jun 13, 2005 · N262FE · Boeing 727200 · Long-Range Navigation (LORAN) SystemSDR 05FDEA01601Antenna · corrodedAFT LOWER FUSE ADF LOOP ANT BASE CORRODED. REMOVED AND REPLACED ADF ANTENNA IAW MM 34-37-012-4, OPS CHECKS GOOD.Jun 13, 2005 · N262FE · Boeing 727200 · Long-Range Navigation (LORAN) SystemSDR 05FDEA01599Frame · crackedNR 1 ENG FIXED COWL AFT LWR END SKIN AND FRAME IS CRACKED. TRIMMED DAMAGE SKIN IAW SRM 54-30-1 FIG 1 DETAIL 6. REMOVED AND REPLACED FRAME IAW SRM 51-10-1 AND SRM 51-30-2.Jun 13, 2005 · N262FE · Boeing 727200 · Nacelle/Pylon, Main FrameSDR 05FDEA01593Actuator · leakingLOSS SYSTEM-A HYDRALICS IN FLIGHT. COMPLETED QRH/RED TAB PROCEDURES. SYSTEM-A FLUID SHUTOFF SWITCHED CLOSED AT 1032, LANDED AT 1048. *S/D* REMOVED AND REPLACED A-HYD SYS PRESS FILTERS PER M/M 29-11-062-3, NO CONTAMINATION FOUND. REMOVED AND REPLACED A-HYD Jun 13, 2005 · N213FE · Boeing 727200 · Leading Edge Slat ActuatorSDR 05FDEA01585Frame · damagedUPPER FUSELAGE STA 360, MULTIPLE OPEN HOLES IN CIRCUM FRAME, FROM BL 0 TO STR 5L. *S/D* REPAIRED MULTIPLE OPEN HOLES IAW SRM 51-40-3 AND 51-30-02.Jun 10, 2005 · N482FE · Boeing 727200 · Fuselage Main, Frame
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