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 05FDEA03898Floorbeam · damagedFOUND DOUBLE HOLE IN FLOORBEAM BS 740 LBL 47 WL 208. REPAIRED PER FED EX EA 7-5810-91429.Nov 18, 2005 · N485FE · Boeing 727227 · Fuselage Main, Floor BeamSDR DHL2005782004Indication Sys · malfunctionedAFTER GEAR RETRACTION RED DOOR LIGHT AND LEFT/RIGHT RED DOOR LIGHTS REMAINED ILLUMINATED (AND L GEAR /R GEAR AMBER LIGHTS ILLUMINATED ON S/O PANEL) TAIL SKID AMBER LIGHT ILLUMINATED BUT WENT OUT AFTER A MINUTE COMPLETED ABNORMAL PROCEDURE, LIGHTS SAME AS ABONov 17, 2005 · N782DH · Boeing 727227 · Landing Gear Position and WarningSDR 05FDEA03826Stringer · corrodedFOUND CORROSION ON STRINGER 21R BS 310-317. FOUND CORROSION ON STR 21R BS 310-317 TO BE OUT OF LIMITS. REMOVED CORRODED PORTION OF STR. REPAIRED STRINGER IAW SRM 53-10-3 FIG 1.Nov 15, 2005 · N485FE · Boeing 727227 · Fuselage Main, Longeron/StringerSDR 05FDEA03818Skin · bentFOUND FORWARD ENTRY DOOR, UPPER AFT CORNER SKIN IS BENT OUTWARDS. REPAIRED FORWARD ENTRY DOOR UPPER AFT CORNER SKIN PER SRM 52-00-3.Nov 15, 2005 · N485FE · Boeing 727227 · Passenger/Crew DoorsSDR 05FDEA03605Warning Light · illuminatedON DEPARTURE AFT AIRSTAIR LIGHT ILLUMINATED ON S/O PANEL, RETURNED TO MEM, LIGHT EXTINGUISHED ON TOUCHDOWN. ACN RELEASED FOR SERVICE PER MEL/CDL: 52-06-B CATEGORY: C EXPIRATION:Nov 2, 2005 · N481FE · Boeing 727227 · Entrance StairsSDR XN0A1274Engine · failedNR 1 ENGINE FAULT ON T/O ROLL AT STEWART, LOUD BAND HEARD FOLLOWED BY EPR REDUCTIVE TOWARDS 0. ALL OTHER ENGINE INDICATIONS NORMAL DURING T/O ROLL.Oct 28, 2005 · N79754 · Boeing 727227 · Engine (Turbine/Turboprop)SDR DHL2005783006Switch · dirtyDURING CLIMB-OUT, RT DOOR WARNING LT ILLUMINATED S/O PANEL SHOWED RT GEAR DOOR COMPLIED WITH ABNORMAL PROCEDURE LIGHT OUT WITH GEAR HANDLE UP. CLEANED AND ADJUSTED RT DOOR WARNING SWITCH IAW M/M 32-62-11. OPS CKS GOOD.Oct 27, 2005 · N783DH · Boeing 727227 · Landing Gear Position and WarningSDR DHL2005782003Switch · lack of lubeAFTER TAKEOFFF WHEN GEAR HANDLE MOVED TO OFF R GEAR DOOR LIGHT ILLUM. ON S/O PANEL AND RED DOOR LIGHT ON FORWARD PANEL. PERFORMED ABNORMAL PROCEDURE. NO HELP. GEAR HANDLE HAD TO REMAIN IN UP TO KEEP LIGHTS OUT. CLEAN AND LUBED RT MLG DOOR SWITCH, OPS CK GOct 25, 2005 · N782DH · Boeing 727227 · Landing Gear Position and WarningSDR 05FDEA03426Duct · looseENG 3 STRUT OVERHEAT LIGHT ILLUMINATED, COMPLETED QRH PROC AND ISOLATED ENG NR 3 BLEED AIR. LIGHT EXTINGUISHED WHEN NR 3 BLEED AIR SW AND NR 2 PACK SW TURNED OFF AND NR 3 THROTTLE RETURNED TO IDLE. LIGHT REMAINED OFF THROUGH REST OF FLIGHT. 13 OCT 05 REMOVEOct 13, 2005 · N489FE · Boeing 727227 · Engine Bleed Air SystemSDR 05FDEA03316Hinge · crackedRT OB AILERON 2ND FROM I/B HINGE ASSY FLANGE SECTION MISSING. REMOVED AND REPLACED HINGE ASSY IAW SRM 51-30-2.Oct 9, 2005 · N484FE · Boeing 727227 · Wing Main, Frame StructureSDR XNOA1271Outflow Valve · malfunctionedAIRCRAFT FAILED TO PRESSURIZE MORE THAN 2 PSI DIFFERENTIAL. R & R THE RT FLOW CONTROL VALVE IAW MM 36-12-61, SYSTEMS OPS CHECK GOOD. (STATUS:ORIG/CLOSED)Oct 6, 2005 · N793A · Boeing 727227 · Pressure Regulator/Outflow ValveSDR DHL2005781004Stabilizer · out of adjustAIRCRAFT ROTATES 15 KTS BEFORE VR AND THEN REQUIRES 1.0 UNIT DOWN TRIM TO MAINTAIN V2 +10 ON CLIMBOUT.Oct 3, 2005 · N781DH · Boeing 727227 · Stabilizer Control SystemSDR XN0A1270Transmitter · malfunctionedCREW O2 TO 0 PSI IN TAXI OUT SWF, BACK TO THE RAMP. RESET PRESS TRANSMITTER ON CREW BOTTLE, CHECK GOOD IAW 35-11-00.Oct 1, 2005 · N73751 · Boeing 727227 · Crew Oxygen SystemSDR DHL2005783005Battery · inoperativeEMERGENCY EXIT LIGHT OVER COCKPIT DOOR DOES NOT ILLUMINATE DURING STBY POWER CHECK. INSTALLED NEW BATTERIES IN EMERGENCY EXIT LIGHT P/N 38931-002. LIGHT OP CHECKS GOOD IAW B727 M/M 33-50-00.Sep 28, 2005 · N783DH · Boeing 727227 · Emergency LightingSDR 05FDEA03040Panel · gougedRT HORIZONTAL STABILIZER UPPER T/E PANEL INNER SIDE IS GOUGED JUST 3 INCHES I/B OF NR 7 RIB. REPAIRED PER E.A. 7-5510-91362.Sep 21, 2005 · N483FE · Boeing 727227 · Horizontal Stabilizer, Plate/SkinSDR XN0A1267Hydraulic System · leakingLOSS (A) SYS HYD ON TAKEOFF. (ORIG/OPEN)Sep 21, 2005 · N793A · Boeing 727227 · Hydraulic System, MainSDR 05FDEA03007Structure · corrodedAFTER REMOVAL OF NR 7 FLAP TRACK FWD FITTING ON N00421, FOUND EXISTING DAMAGE IN AFT INBOARD ATTACH FITTING HOLE. REPAIRED PER SRM 51-20-1, 51-30-2.Sep 20, 2005 · N483FE · Boeing 727227 · Trailing Edge FlapsSDR 05FDEA02982Web · crackedVERTICAL STABILIZER 1303 WEB IS CRACKED AT LOWER LT CORNER. REPAIRED VERT STAB 1303 WEB IAW SRM 51-40-2.Sep 18, 2005 · N483FE · Boeing 727227 · Ventral StructureSDR 05FDEA02929Depressor · dentedNR 1 CARGO DOOR LWR CENTER SEAL DEPRESSOR DENTED AT AFT END. REPAIRED PER SRM 52-00-2.Sep 15, 2005 · N483FE · Boeing 727227 · Cargo/Baggage DoorsSDR 05FDEA02886Skin · crackedN00364 - R-1 DOOR SKIN IS CRACKED AT UPPER HINGE.Sep 14, 2005 · N483FE · Boeing 727227 · Service DoorsSDR 05FDEA02887Rib · gougedLEFT HORIZONTAL STAB NR 3 BALANCE BAY OB RIB IS GOUGED FROM CONTACT WITH IDLER HINGE PIN. REMOVED AND REPLACED L/HORIZ. STAB NO. 3 BALANCE BAY OUTBD RIB IAW EA 7-5510-70689, PART 1 AND 727 SRM 51-30-2 AND 51-30-5.Sep 14, 2005 · N483FE · Boeing 727227 · Horizontal Stabilizer, Spar/RibSDR 05FDEA2886Skin · crackedR-1 DOOR SKIN IS CRACKED AT UPPER HINGE.Sep 14, 2005 · N483FE · Boeing 727227 · Service DoorsSDR XN0A1263Cabin Pressure · malfunctionedAIRCRAFT WOULD NOT PRESSURIZE IN ANY MODE - AUTO, STANDBY OR MANUAL AC OR DC. TRANSFERRED TO MEL 5718 IAW MEL 21-16-2D. PLACARDS INSTALLED CAT-C.Sep 13, 2005 · N76752 · Boeing 727227 · Cabin Pressure Control SystemSDR 05FDEA02825Skin · gougedFUSELAGE SKIN HAS SEVERAL GOUGES FROM BS 990-1050 STRINGER 27L - 26R. REPAIRED PER SRM 53-30-3Sep 9, 2005 · N483FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR 05FDEA02806Attach Fitting · corrodedRIGHT WING, NR 7 FLAP TRACK FWD ATTACH FITTING INBOARD FACE CORRODED (27X5709-02). REPAIRED PER E.A. 7-5710-91348.Sep 7, 2005 · N483FE · Boeing 727227 · Trailing Edge FlapsSDR 05FDEA02710Support · corrodedCORROSION ON COCKPIT FLOOR STRUCTURE BS 268 LBL 8 WL 207. REMOVED FABRICATED AND INSTALLED WEB AND TEE CHORD IAW SRM 51-30-3, 51-30-6 AND 51-10-3.Aug 29, 2005 · N483FE · Boeing 727227 · Fuselage Main, StructureSDR 05FDEA02711Floor Support · corrodedCORROSION ON COCKPIT FLOOR STRUCTURE BS 266 LBL 2 WL 207. REMOVED, FABRICATED AND INSTALL REPAIR PER SRM 51-20-1Aug 29, 2005 · N483FE · Boeing 727227 · Fuselage Miscellaneous StructureSDR 05FDEA02709Floor Support · corrodedCORROSION ON COCKPIT FLOOR STRUCTURE BS 268 LBL 8 WL 207. REMOVED FABRICATED AND INSTALLED WEB AND TEE CHORD IAW SRM 51-30-3, 51-30-6 AND 51-10-3.Aug 29, 2005 · N483FE · Boeing 727227 · Fuselage Miscellaneous StructureSDR 05FDEA02708Frame · dentedFORWARD CARGO BAY, FRAME IS DENTED AT BS 580 BETWEEN STRINGER LT 24 AND LT 23. REPAIRED FRAME IAW SRM 51-40-3.Aug 29, 2005 · N483FE · Boeing 727227 · Fuselage Main, FrameSDR DHL2005781003Relay · failedEMERGENCY EXIT LIGHTS ON WITH SWITCH IN THE ARMED POSITION. REMOVED AND REPLACED R70 EMERGENCY EXIT RELAY IAW WD 33-51-00, GROUND OPS CHECK NORMAL. P/N 10-60450-3 USED.Aug 27, 2005 · N781DH · Boeing 727227 · Emergency LightingSDR DHL2005783003Switch · failedUPON RETRACTING FLAPS FROM 5 TO 2 DEG LED IN TRANSIT LIGHT REMAINED ILLUMINATED. CHECKED SO PANEL, NR 5 LE FLAP IN TRANSIT. PERFORMED ABNORM PROCEDURE, NO CHANGE RETURNED TO CVG. REMOVED AND REPLACED NR 5 L/E FLAP SWITCH IAW MM 27-82-01, OPS CHECK GOOD.Aug 26, 2005 · N783DH · Boeing 727227 · Leading Edge Slat Control SystemSDR XN0A1260Door · out of adjustPILOT REPORT, COULD NOT PRESSURIZE A/C. RE-ADJUSTED EE DOOR IAW MM 52-40-11.Aug 25, 2005 · N79754 · Boeing 727227 · Electrical/Electronic Compartment DoorsSDR 05FDEA02636Keelbeam · crackedUPPER FLANGE ON KEELBEAM, IS CRACKED AT FASTENER HOLE, STA 874, LBL 6. FABRICATED & INSTALLED STEEL DOUBLER AT BS 870 LBL 6 PER ECA 7-5310-70687 AND BOEING SERVICE BULLITEN 727-53-0208.Aug 24, 2005 · N483FE · Boeing 727227 · Fuselage Main, KeelSDR 05FDEA02595Stringer · dentedWHILE WORKING N01449, FOUND STRINGER 20R BS 419 TO BE DENTED. REPAIRED PER SRM 53-10-3 FIG 1.Aug 23, 2005 · N483FE · Boeing 727227 · Fuselage Main, Longeron/StringerSDR 05FDEA02592Stringer · damagedAT STA 435 STR 19R, FOUND CRACK AT FASTENER HOLES, 2ND HOLE FWD OF STRINGER SPLICE. REPAIRED PER SRM 53-10-3, MAJOR REPAIR. [CLOSED]Aug 23, 2005 · N483FE · Boeing 727227 · Fuselage Main, Longeron/StringerSDR 05FDEA02577Attach Fitting · corrodedNR 7 FLAP TRACK FWD ATTACH FITTING IS CORRODED. REPLACED NR 7 FLAP TRACK FWD ATTACH FITTING IAW BOEING DWG 65-17357, OHM 20-50-03, MM 28-11-00.Aug 19, 2005 · N489FE · Boeing 727227 · Wing, Attach FittingsSDR DHL2005781002Indicator · malfunctionedREJECTED TO RNY 30L STL DUE TO NR 1 EGT EXCEEDING 620 DEGREES AT CALCULATED EPR OF 2.11 GW 178,400, PA 540 A/S 120 KNTS TEMP 25 DEGREES. REPLACED NR 1 EGT INDICATOR AND PERFORMED GROUND CHECK PER JRH 7.1 CHECK NORMAL.Aug 19, 2005 · N781DH · Boeing 727227 · Engine EGT/TIT Indicating SystemSDR 05FDEA02498Rib · crackedRIGHT WING, NR 5 SLAT, LEADING EDGE RIB CRACKED OUTBOARD OF OUTBOARD MAIN TRACK. REMOVED AND REPLACED RIB IAW SRM 51-30-5, 51-30-2.Aug 17, 2005 · N483FE · Boeing 727227 · Leading Edge DevicesSDR 05FDEA02499Stringer Clip · damagedFUSELAGE, UPPER LOBE, STA 680 STR 2L, STRINGER CLIP DAMAGED. REPLACED STRINGER CLIP AT BS 680, STR 2L PER SRM 51-30-2.Aug 17, 2005 · N483FE · Boeing 727227 · Fuselage Main, Attach FittingsSDR 05FDEA02497Frame · bentFRAME BENT STA 1070 STR 25L - 2L. REMOVED DAMAGED AREA, FABRICATED REPAIR ANGLE, TREATED AND PRIMED, INSTALLED REPAIR IAW SRM 51-30-2, 51-40-3, 51-10-2.Aug 17, 2005 · N483FE · Boeing 727227 · Fuselage Main, FrameSDR XN0A1257Generator · overtempAC GEN DRIVE OIL TEMP IN CAUTION RANGE GEN NR 2. CLEANED CONNECTORS AT BOTH TEMP BULB. CHECKED MAG PLUG - NO CONTAMINATION. CHANGED CSD OIL & OPS CHECK GOOD IAW MM 24-10-0 & 24-20-0. (ORIG/CLOSED).Aug 17, 2005 · N793A · Boeing 727227 · AC Generation SystemSDR 05FDEA02469Stringer · damagedSTRINGER AT BS 1090 STR 7LT IS DAMAGED. REPAIRED STRINGER PER SRM 53-10-1, 53-10-3 FIG 3 MAJOR REPAIR.Aug 16, 2005 · N483FE · Boeing 727227 · Fuselage Main, Longeron/StringerSDR 05FDEA02470Stringer Clip · brokenFUSELAGE UPPER LOBE, STA 660, STRINGER CLIP 8L BROKEN. REMOVED AND REPLACED STRINGER CLIP AT STR 8L BS 660 IAW SRM 51-30-2.Aug 16, 2005 · N483FE · Boeing 727227 · Fuselage Main, Attach FittingsSDR 05FDEA02446Vertical Beam · unknownREPAIR ON VERTICAL BEAM AT STA 1183, RBL 36.83, WL 230, PREVIOUS REPAIR NEEDS ENG EVALUATION TO DETERMINE IF MAJOR OR MINOR AND IF REPAIR IS IAW FAA APPROVED DATA. NO ENGINEERING ASSISTANCE NEEDED. THIS IS A MODIFICATION COMPLIED WITH PER DRAWING 65C29080. Aug 12, 2005 · N479FE · Boeing 727227 · Fuselage Miscellaneous StructureSDR 05FDEA02445Skin · unknownREPAIR LOCATED ON FUSELAGE AT NR 3 ENG, PREVIOUS REPAIR AT STA 1243 BELOW NR 3 PYLON NEEDS ENG EVALUATION TO DETERMINE IF MAJOR OR MINOR AND IF REPAIR IS IAW FAA APPROVE DATA.Aug 12, 2005 · N479FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR 05FDEA02444Skin · unknownREPAIR LOCATED ON FUSELAGE AT NR 3 ENG, PREVIOUS REPAIR AT STA 1243 BELOW NR 3 PYLON NEEDS ENG EVALUATION TO DETERMINE IF MAJOR OR MINOR AND IF REPAIR IS IAW FAA APPROVE DATA. NO ENGINEERING NEEDED. THIS IS A MODIFICATION COMPLETED BY DRAWING B27-53-020 REV Aug 12, 2005 · N479FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR 05FDEA02443Skin · unknownREPAIR LOCATED ON FUSELAGE AT NR 1 ENGINE, PREVIOUS REPAIR AT FS 1243 BELOW NR 1 PYLON NEEDS ENG EVALUATION TO DETEMINE IF MAJOR OR MINOR AND IF REPAIR IS IAW FAA APPROVED DATA. NO ENGINEERING NEEDED. THIS IS A MODIFICATION INSTALLED IAW DRAWING B27-53-020. Aug 12, 2005 · N479FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR 05FDEA02442Skin · unknownREPAIR LOCATED AT APPROX BS 1140 TO 1183 STR 21L TO 23L, PREVIOUS REPAIR AT STA 1140 TO 1183 STR 21L TO 23L NEEDS ENG EVALUATION TO DETERMINE IF MAJOR OR MINOR AND IF REPAIR IS IAW FAA APPROVED DATA. NO ENGINEERING EVALUATION REQUIRED. REPAIR HAS BEEN COMPLIAug 12, 2005 · N479FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR 05FDEA02441Floorbeam · unknownREPAIR ON FLOORBEAM AT STA 1130 BL 0 THRU RBL 18, PREVIOUS REPAIR AT STA 1130 , BL 0 TO RBL 18 NEEDS ENG EVALUATION TO DETERMINE IF MAJOR OR MINOR AND IF REPAIR IS IAW FAA APPROVED DATA. NO ENGINEERING NEEDED. THE REPAIR IS WAS INSTALLED IAW SRM 53-10-8 ANDAug 12, 2005 · N479FE · Boeing 727227 · Fuselage Main, Floor BeamSDR 05FDEA02440Frame · unknownREPAIR LOCATED AT APPROX BS 1010 TO 1016 BETWEEN 23L AND 24L, PREVIOUS REPAIR AT STA 1010 TO 1016 BETWEEN STR 23L AND 24L NEEDS ENG EVALUATION TO DETERMINE IF MAJOR OR MINOR AND IF REPAIR IS IAW WITH FAA APPROVED DATA. NO ENGINEERING NEEDED. THIS REPAIR WAS Aug 12, 2005 · N479FE · Boeing 727227 · Fuselage Main, Frame
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