Boeing 727-227

Service difficulty reports · 5,082

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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 = '727227'
  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 95FDEA01773Stringer · damagedWHILE WORKING NR 0137, FOUND DAMAGED STRINGER 24L AT BS 600.Nov 17, 1995 · N490FE · Boeing 727227 · Fuselage Main, Longeron/StringerSDR 95FDE01755Frame · dentedFWD BAY, FRAME DENTED AT BS 600 BETWEEN STR 22 TO 25L. REPAIRED DENTED FRAME IN FWD BAY AT BS 600 BETWEEN STR 22 TO 25L IAW FEDEX SRM 51-40-3.Nov 17, 1995 · N490FE · Boeing 727227 · Fuselage Main, FrameSDR 95FDEA01772Web · crackedCRACKED WEB AND SUPPORT ANGLES BETWEEN WING STA 70.5 AND 80.5 IN L/W PIE SECTION.Nov 16, 1995 · N490FE · Boeing 727227 · Wing Miscellaneous StructureSDR 95FDEA01766Floorbeam · damagedMECHANICAL DAMAGE TO FLOORBEAM LOWER SURFACE OF UPPER FLANGE BS 600 RBL 11 WL 207. THE DAMAGE WAS FOUND TO BE OUT OF LIMITS. REPAIRED FLOORBEAM AT BS 600 RBL 11 WL 207 PER FEDEX SRM 53-10-1 AND 53-10-8.Nov 16, 1995 · N490FE · Boeing 727227 · Fuselage Main, Floor BeamSDR 95FDEA01765Frame · dentedFWD BAY FRAME DENTED AT BS 500 BETWEEN STR 23 TO 22L AND DENT FOUND TO BE OUT OF LIMITS. REPAIRED DENTED FRAME AT BS 500 BETWEEN STR 23 TO 22L PER FEDEX SRM 51-40-3 AND 53-10-1.Nov 16, 1995 · N490FE · Boeing 727227 · Fuselage Main, FrameSDR 95FDEA01764Clip · crackedSTR CLIP IS CRACKED BS 660 STR 15L. REPLACED OLD STR CLIP AT BS 660 STR 15L WITH NEW STR CLIP.Nov 16, 1995 · N490FE · Boeing 727227 · Fuselage Miscellaneous StructureSDR 95FDEA01750Frame · dentedFRAME DENTED AT BS 500 BETWEEN STR 24 TO 25R AND DENT WAS FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE AREA FROM FRAME, FABRICATED, TREATED AND INSTALLED DOUBLER PER FEDEX SRM 53-10-1 AND 51-40-3.Nov 16, 1995 · N490FE · Boeing 727227 · Fuselage Main, FrameSDR 95FDEA01763Clip · crackedSTR CLIP IS CRACKED BS 680 STR 3L. REMOVED STR CLIP AT BS 680 STR 3L AND REPLACED WITH NEW STR CLIP AT ABOVE AREA.Nov 15, 1995 · N490FE · Boeing 727227 · Fuselage Miscellaneous StructureSDR 95FDEA01762Clip · crackedSTR CLIP IS CRACKED BS 680 STR 2L. REMOVED STR CLIP AT BS 680 STR 2L AND REPLACEMENT WITH NEW STR CLIP AT ABOVE AREA.Nov 15, 1995 · N490FE · Boeing 727227 · Fuselage Miscellaneous StructureSDR 95FDEA01761Clip · crackedSTR CLIP IS CRACKED BS 660 STR 8L. REMOVED CRACKED STR CLIP AND REPLACED WITH NEW STR CLIP AT BS 660 STR 8L.Nov 15, 1995 · N490FE · Boeing 727227 · Fuselage Miscellaneous StructureSDR 95FDEA01760Frame · dentedFWD CARGO BAY BS 700 BETWEEN STR 22 TO 25R DENTED ON FRAME. REMOVED DAMAGED AREA OF FRAME AT BS 700 BETWEEN STR 22 TO 25R, FABRICATED AND INSTALLED REPAIR PARTS PER FEDEX SRM 51-40-3.Nov 15, 1995 · N490FE · Boeing 727227 · Fuselage Main, FrameSDR 95FDEA01756Srtinger · corrosionCORROSION (C53-224-01, 2), ON STR 4L AT BS 765. ACCOMPLISHED STR REPAIR AT BS 765 STR 4L IAW FEDEX SRM 53-10-3.Nov 15, 1995 · N490FE · Boeing 727227 · Fuselage Main, Longeron/StringerSDR 95FDEA01755Frame · dentedFWD BAY, FRAME DENTED AT BS 600 BETWEEN STR 22 AND 25L.Nov 15, 1995 · N490FE · Boeing 727227 · Fuselage Main, FrameSDR CAL951043Eel · inoperativeIAH - FLT 0384 - INSPECTION FOUND THE COCKPIT EMERGENCY EXIT LIGHT INOPERATIVE. THE COCKPIT EMERGENCY EXIT LIGHT WAS REMOVED AND REPLACED. (X)Nov 14, 1995 · N99763 · Boeing 727227 · Emergency LightingSDR 95FDEA01758Nutplate Strip · damagedCORROSION (C53-111-01-1), ON PRESSURIZATION NUTPLATE DOMES AT BS 720B LBL 5 TO RBL 5 IN BILGE. REMOVED NUTPLATE STRIP AT BS 720B LBL 5. REMOVED .5 INCH BY 1 INCH BY .026 INCH. CORROSION WAS DETERMINED TO BE OUT OF LIMITS IAW FEDEX SRM 53-10-6. FABRICATED NNov 14, 1995 · N490FE · Boeing 727227 · Fuselage Miscellaneous StructureSDR 95FDEA01757Skin · corrodedCORROSION (53-111-01-3), ON SKIN AT BS 950F PLUS 10 STR 28L WHILE WORKING ON CARD NR0208, CORROSION OUT OF LIMITS. CUT OUT DAMAGE, FABRICATED DOUBLER AND FILLER, INSTALLED PER FEDEX SRM 53-30-3.Nov 14, 1995 · N490FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR 95FDEA01752Skin · corrosionCORROSION (C53-111-01-1), ON EXTERIOR SKIN SURFACE AT BS 720A PLUS 10 TO 720C, BL 0 WL 145. CORROSION FOUND WHILE ACCESSING NR0481 BENEATH RAM AIR DOOR'S SPLITTER VALVE. BLENDED CORROSION ON EXTERIOR SKIN BS 720A TO 720C BL 0 WL 145 BENEATH RAM AIR SPLITTER Nov 14, 1995 · N490FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR 95FDEA01751Channel · corrodedCORROSION (C53-224-01), ON HAT CHANNEL BS 328 WL 208 RBL 13. REMOVED CORRODED HAT CHANNEL, FABRICATED AND INSTALLED HAT CHANNEL AT BS 303 TO 344 RBL 10 TO 15 WL 208.Nov 14, 1995 · N490FE · Boeing 727227 · Fuselage Miscellaneous StructureSDR 95FDEA01749Frame · dentedFWD BAY FRAME DENTED AT BS 680 AT STR 24 L.Nov 14, 1995 · N490FE · Boeing 727227 · Fuselage Main, FrameSDR 95FDEA01748Frame · dentedFWD CARGO BAY BS 700 BETWEEN STR 22 TO 25R DENT ON FRAME.Nov 14, 1995 · N490FE · Boeing 727227 · Fuselage Main, FrameSDR 95FDEA01746Stringer · corrosionCORROSION (C53-111-01-1), ON STR 27R AT BS 720B PLUS 10, INSIDE BAY. REMOVED CORROSION 1 INCH BY 2 INCH BY .005 INCH DEEP AT BS 720 PLUS 10 STR 27R, ORIGINAL THICKNESS 0.89. FOUND WITHIN ALLOWABLE LIMITS PER FEDEX SRM 53-10-1, CLEANED AND TREATED.Nov 14, 1995 · N490FE · Boeing 727227 · Fuselage Main, Longeron/StringerSDR 95FDEA01735Stringer · corrosionCORROSION (53-111-01-1), ON STR AT BS 720 A PLUS 10 STR 27R, INSIDE BAY. REMOVED CORROSION 1.5 INCH BY 1.5 INCH BY .011 INCH DEEP AT BS 720A PLUS 2 TO 720A PLUS 17 STR 27R, ORIGINAL THICKNESS .084. FOUND WITHIN ALLOWABLE LIMITS PER FEDEX SRM 53-10-1, CLEANENov 14, 1995 · N490FE · Boeing 727227 · Fuselage Main, Longeron/StringerSDR 95FDEA01733Floor Support · corrosionCORROSION (C53-111-01-1), ON UNDERSIDE OF FLOOR SUPPORT AROUND RIVNUT BS 480 WL 155 LBL 13.5. REMOVED CORROSION ON UNDERSIDE OF FLOOR SUPPORT AROUND RIVNUT BS 480 WL 155 LBL 13.5. REMOVED .003 INCH BY 1 INCH BY 1.125 INCH FROM ORIGINAL THICKNESS OF .071. Nov 14, 1995 · N490FE · Boeing 727227 · Fuselage Miscellaneous StructureSDR 95FDEA01732Skin · corrodedCORROSION (C53-111-01-2), ON SKIN AT BS 700 WL 145 RBL 8 O/B OF STR 28R FOUND ON INNER SURFACE WHILE WORKING NR0235. CORROSION ON SKIN AT BS 700 WL 145 RBL 8 O/B OF STR 28R WAS FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-30-1. REMOVED DAMAGED AREA, FABRICATENov 14, 1995 · N490FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR 95FDEA01731Skin · dentedDENT ON I/B UPPER SURFACE OF LEFT WING I/B AILERON. REMOVED, REPAIRED AND REINSTALLED SERVICEABLE LEFT WING I/B AILERON IAW FEDEX MM 27-10-1, FUNCTIONAL TESTED IAW FEDEX MM 27-10-00.Nov 14, 1995 · N490FE · Boeing 727227 · AileronsSDR 95FDEA01730Stringer · corrodedCORROSION (C53-111-01-3), ON STR AT BS 950F PLUS 10, STR 28L, WHILE WORKING ON NR 0208.Nov 14, 1995 · N490FE · Boeing 727227 · Fuselage Main, Longeron/StringerSDR 95FDEA01729Keel Beam · crackedPOSSIBLE CRACK FOUND ON SIDE OF RT KEEL BEAM APPROX 2 INCHES LONG AT BS 950E PLUS 3 STR 29R WL 145. REPAIRED CRACKED KEEL BEAM AFT CARGO BAY BS 950E PLUS 3 STR 29R WL 145 PER PER EA 7-5310-26741.Nov 14, 1995 · N490FE · Boeing 727227 · Fuselage Main, KeelSDR 95FDEA01727Frame · damagedPUNCTURED FRAME BS 1090 STR 7L WL 281. REPAIRED DAMAGED FRAME AT BS 1090 STR 7L WL 281 PER FEDEX SRM 53-10-4 FIG 2.Nov 14, 1995 · N490FE · Boeing 727227 · Fuselage Main, FrameSDR 95FDEA01725Blkhd Angle · corrosionCORROSION (C53-111-01-2), ON BULKHEAD SUPPORT ANGLE AROUND NUTPLATE HOLES BS 720D LBL 28 WL 156. CORROSION WAS FOUND TO BE OUT LIMITS. REMOVED BULKHEAD SUPPORT AND INSTALLED NEW BULKHEAD SUPPORT ANGLE AT BS 720D LBL 28 WL 156.Nov 14, 1995 · N490FE · Boeing 727227 · Fuselage Main, BulkheadSDR 95FDEA01724Blkhd Angle · corrosionCORROSION ON BULKHEAD SUPPORT ANGLE AT BS 480 RBL 24 TO 39 WL 155. CORROSION OUT OF LIMIT ON BULKHEAD SUPPORT ANGLE AT BS 480 RBL 24 TO 39. ROBBED SERVICEABLE BULKHEAD SUPPORT FROM N489FE AND REMOVED AND REPLACED SERVICEABLE BULKHEAD SUPPORT.Nov 14, 1995 · N490FE · Boeing 727227 · Fuselage Main, BulkheadSDR SCNA95270Fire Loop · out of positionTHE NUMBER 3 ENGINE FIRE DETECTION LIGHT ILLUMINATED DURING FLIGHT. REPOSITIONED NUMBER 3 ENGINE DETECTOR, SYSTEM CHECKED GOOD IAW MM 26-11-00 PAGE 501.Nov 13, 1995 · N275AF · Boeing 727227 · Fire DetectionSDR 95FDEA01726Frame · dentedIN THE AFT CARGO BAY THE FRAME IS DENTED AT STA 1039 BETWEEN STR 25 TO 26L. REPAIRED FRAME AT BS 1030 BETWEEN STR 25 TO 26L PER FEDEX SRM STR 40-3. ALODINED, PRIMED AND PAINTED, REPAIR DOUBLER FRAME WAS FOUND TO BE OUT OF LIMITS PER SRM 53-10-1.Nov 13, 1995 · N490FE · Boeing 727227 · Fuselage Main, FrameSDR 95FDEA01716Floorbeam · corrodedFLOORBEAM AT STA 380 RBL 47 WL 208.1 HAS CORROSION, CORROSION REMOVED FOUND OUT OF LIMITS. CUT OUT CORRODED SECTION OF FLOORBEAM AND INSTALLED FLOORBEAM PER SRM 53-10-8.Nov 13, 1995 · N485FE · Boeing 727227 · Fuselage Main, Floor BeamSDR 95FDEA01711Support · corrodedMAIN CARGO, FLOOR BOARD SUPPORT CORRODED AT STA 1035 AT 12 RBL. INSTALLED NEW PART PER SRM 51-10-1.Nov 13, 1995 · N485FE · Boeing 727227 · Fuselage Miscellaneous StructureSDR 95FDEA01710Rib · crackedSTA 760 RT RIB CHORD, HFEC INDICATES CRACKS TOP AND BOTTOM FWD HOLE. INSTALLED REPAIR PER BOEING DRAWING 65-68492-18.Nov 13, 1995 · N485FE · Boeing 727227 · Wing, Rib/BulkheadSDR 95FDEA01707Floorbeam · corrodedFLOORBEAM AT STA 380 RBL 47 WL 208.1 HAS CORROSION. CORROSION REMOVED FOUND OUT OF LIMITS. CUT OUT CORRODED SECTION OF FLOORBEAM AND INSTALLED FLOORBEAM PER SRM 53-10-8.Nov 13, 1995 · N485FE · Boeing 727227 · Fuselage Main, Floor BeamSDR 95FDEA01705Pack Valve · malfunctionedON CLIMBOUT OF DSM PASSING 3,000 FT, THE NR 5 MAIN CARGO SMOKE DETECTOR ILLUMINATED. DETECTOR REMAINED ON APPROXIMATELY 2 MINUTES, THEN EXTINGUISHED. APPROXIMATELY 4 MINUTES LATER THE NR 5 LIGHT ILLUMINATED AGAIN. FOUND PACK C/B TRIPPED. REMOVED AND REPLACNov 11, 1995 · N484FE · Boeing 727227 · Cabin Cooling SystemSDR 95FDEA01715Floorbeam · corrodedCABIN FLOORBEAM UPPER CHORD LWR SURFACE CORRODED AROUND SCREW HOLE STA 344 LBL 25.5 RBL 20. SPLICED IN NEW SECTION PER FEDEX DRAWING SR 27-53-007. REMOVED CORROSION OUTSIDE OF SPLICE SECTION PER SRM 51-10-6.Nov 10, 1995 · N485FE · Boeing 727227 · Fuselage Main, Floor BeamSDR 95FDEA01714Floorbeam · crackedCABIN FLOORBEAM UPPER AFT CHORD CRACKED AT SCREW HOLE STA 344 LBL 25. REMOVED CRACKED SECTION OF CHORD. SPLICED IN NEW SECTION OF CHORD PER FEDEX DRAWING NR SRM 27-53-007.Nov 10, 1995 · N485FE · Boeing 727227 · Fuselage Main, Floor BeamSDR 95FDEA01713Floorbeam · corrodedCORROSION ON FLOORBEAM STA 344 BL O LBL 22.5. CORROSION BEYOND LIMITS, REMOVED T-CHORD FROM LBL 2 TO 32 SPLICED IN NEW SECTION PER FEDEX DRAWING SR 27-53-007.Nov 10, 1995 · N485FE · Boeing 727227 · Fuselage Main, Floor BeamSDR 95FDEA01712Angle · crackedLT FLOOR BOARD CHORD ANGLE AT 750 TO 760 LBL 62 IS CRACKED. REMOVED CRACKED CHORD ANGLE, REPLACED LT 760 CHORD ANGLE PER SRM 51-10-1.Nov 10, 1995 · N485FE · Boeing 727227 · Fuselage Miscellaneous StructureSDR SCNA95265Fire Loop · out of positionTHE NUMBER 3 ENGINE FIRE DETECTION LIGHT ILLUMINATED DURING FLIGHT. THE A-CIRCUIT BREAKER WAS PULLED AND THE LIGHT EXTINGUISHED. REPOSITIONED NUMBER 3 ENGINE FIRE WARNING ELEMENT AND THE SYSTEM TESTED GOOD.Nov 9, 1995 · N275AF · Boeing 727227 · Fire DetectionSDR SCNA95260Battery Pack · dischargedTHE AFT OVERWING LOWER EMERGENCY EXIT SIGNS WERE FOUND TO BE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK FOR FAULTY EXIT SIGNS AND SYSTEM TESTED GOOD PER 33-50-01.Nov 7, 1995 · N275AF · Boeing 727227 · Emergency LightingSDR SCNA95261Fire Loop · out of positionTHE NUMBER 3 ENGINE FIRE DETECTOR LIGHT ILLUMINATED. REPOSITIONED THE NUMBER 3 FIRE WARNING ELEMENT AND SYSTEM TESTED GOOD IAW MM 26-11-00.Nov 6, 1995 · N275AF · Boeing 727227 · Fire DetectionSDR CAL951019Eel Wire · failedEWR - FLT 0539 - A PRE-FLIGHT INSPECTION FOUND THE AFT AIRSTAIR EMERGENCY OVERHEAD LIGHTS INOPERATIVE. MAINTENANCE FOUND A BAD SPLICE ON POWER WIRE IN BUNDLE. THE WIRE WAS RE-SPLICED AND OPERATION OF THE AFT AIRSTAIR EMERGENCY OVERHEAD LIGHTS WAS RESTORED. (Nov 3, 1995 · N76752 · Boeing 727227 · Emergency LightingSDR 95FDEA01669Module · light inopWHEN GEAR LEVER DOWN, LEFT MAIN GREEN DOWN AND LOCK LIGHT DID NOT ILLUMINATE AND OTHER LIGHTS OK. RECYCLED GEAR, THREE GREEN DOWN AND LOCKED LIGHTS OK. FOUND LEFT GEAR LIGHT INOPERATIVE. REPLACED LANDING GEAR MODULE, OPERATIONAL CHECK GOOD.Nov 2, 1995 · N479FE · Boeing 727227 · Landing Gear Position and WarningSDR 95FDEA01664Frame · crackedFORWARD LOWER CARGO FUSE FRAME STA 640 CRACKED AT RBL 8 FLOOR STR ATTACH. STOP DRILLED ENDS OF CRACK, CONFIRMED CRACK ENDS AT STOP DRILL WITH DYE PENETRANT. INSTALLED REPAIR DOUBLER PER SRM 51-40-3.Nov 1, 1995 · N485FE · Boeing 727227 · Fuselage Main, FrameSDR 95FDEA01708Skin · corrodedSTA 965 STR 30L FASTENER HEAD PULLED AND SKIN BULGING SUSPECT CORROSION. CUT OUT CORROSION STA 965 STR 30L AND INSTALLED FILLER AND DOUBLER PER SRM 53-30-3 PG 11.Oct 31, 1995 · N485FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR 95FDEA01644Floor Beam · corrodedFLOOR BEAM AT STA 380, RBL 47, WL 208.1, HAS CORROSION. CORROSION REMOVED AND FOUND TO BE OUT OF LIMITS .086 INCH. SHOULD BE .100 INCH.Oct 31, 1995 · N485FE · Boeing 727227 · Fuselage Main, Floor BeamSDR 95FDEA01643Floor Beam · corrodedAFT LOWER CARGO FLOOR BEAM LOWER FWD FLANGE CORRODED BEYOND SRM LIMITS STA 1070, RBL 12. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 51-10-6.Oct 31, 1995 · N485FE · Boeing 727227 · Fuselage Main, Floor Beam
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