N189FE, cancelled Aug 2, 2007

Service difficulty reports · 42

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N189FE' AND deregistration_id = 'N189FE-2007-08-02'
  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 05FDEA04351Door · obstructedON DEPARTURE, FORWARD CARGO DOOR LIGHT ILLUMINATED, COULD NOT PRESSURIZE AIRCRAFT, RETURNED TO MEM. FOUND DOOR LATCH HANDLE STOWED, DOOR CL0SED BUT NOT LOCKED OVER CENTER. ALSO, FOUND BUNGEE STUCK IN DOOR LATCH MECHANISM ON FWD SIDE OF DOOR. OPENED DOOR, PUDec 16, 2005 · N189FE · Boeing 72722 · Cargo/Baggage DoorsSDR 04FDEA00242Fan · malfunctionedACRID BURNING ODOR WHEN GASPER FAN IS TURNED ON. MAINTENANCE WAS NOTIFIED AND NOTICED AN UNUSUAL SOUND WHEN GASPER FAN WAS TURNED ON. REMOVED AND REPLACED GASPER FAN, OPS CHECK GOOD PER 727-100 MM 21-23-011-4.Jan 28, 2004 · N189FE · Boeing 727100 · Air Distribution FanSDR 03FDEA00493Control Unit · failedDURING TAXI INTO IND, LWR AFT CARGO SMOKE ALARM ACTIVATED WITH AFT SMOKE LIGHT AND ARMED LIGHT. PERFORMED CHECKLIST ITEMS, INCLUDING DISCHARGE OF BOTH BOTTLES. NO OTHER INDICATIONS OF SMOKE OR FIRE; SYS TEST INDICATES FAULT IN AFT SYSTEM. REMOVED AND REPLACApr 17, 2003 · N189FE · Boeing 727100 · Fire DetectionSDR 02FDEA00970Lap Joint · bulgedFUSELAGE SKIN BETWEEN STA 595 AND 620 ALONG STR 14R SKIN LAP JOINT IS BULGING AT RIVETS. REPAIRED IAW EA.Dec 26, 2002 · N189FE · Boeing 727100 · Fuselage Main, Plate/SkinSDR 02FDEA00971Stringer · crackedLOWER FUSELAGE, STRINGER 21R, IS CRACKED AT STA 400. REMOVED DAMAGED SECTION OF STRINGER FROM STATION 390-410 AND REPLACED IAW SRM.Dec 26, 2002 · N189FE · Boeing 727100 · Fuselage Main, Longeron/StringerSDR 02FDEA00969Stringer · corrodedAFT CARGO COMPARTMENT, STA 1070 TO 1090, STRINGER 29R IS CORRODED. REMOVED AND REPLACED STRINGER SECTION IAW SRM.Dec 26, 2002 · N189FE · Boeing 727100 · Fuselage Main, Longeron/StringerSDR 02FDEA00968Stringer · crackedLOWER FUSELAGE, STRINGER 21R, IS CRACKED AT STA 400.Dec 26, 2002 · N189FE · Boeing 727100 · Fuselage Main, Longeron/StringerSDR 02FDEA00623Switch · failedAIRPLANE DIVERTED TO TPA. MAIN CARGO DOOR WARNING ON S/O'S ANNUNCIATOR CAME ON IN FLIGHT. REPLACED LOCK BAR CLOSED SWITCH PER M/M 52-34-009-5. OPS CHECK OK.Sep 5, 2002 · N189FE · Boeing 727100 · Door Warning SystemSDR 01FDEA00835Actuator · failedLEADING EDGE FLAP LIGHT CAME ON AT 10L FT WITH FLAPS UP. REMOVED AND REPLACED NR 2 & 6 SLAT ACTUATORS PER MM 27-81-032-4.Sep 14, 2001 · N189FE · Boeing 72722 · Leading Edge Slat ActuatorSDR 01FDEA00562Engine · faultyENGINE FIRE NR 3 AFT T/O AT 100 FT. FIRED BOTH BOTTLES. *S/D* REMOVED AND REPLACED NR 3 ENG PER WORK CARD 70T0501-03. OK FOR SERVICE.Jul 13, 2001 · N189FE · Boeing 72722 · Engine (Turbine/Turboprop)SDR 01FDEA00323Pump · failedON T/O NR 1 ENG SHUTDOWN. ENG MET ALL RESTART PREM. REMOVED AND REPLACED NR 1 ENG FUEL CONTROL UNIT AND FUEL PUMP PER JRH, LEAK CK GOOD. OK FOR SERVICE.May 2, 2001 · N189FE · Boeing 72722 · Engine Fuel PumpSDR 00FDEA00778Warning System · activatedDURING CLIMBOUT ALTITUDE WARN WENT OFF. PERFORMED AIR CONDITIONING AND PRESSURIZATION OPERATION TEST. CHECKED GOOD TWO TIMES. AC OK FOR SERVICE PER B727 JET RUN HANDBOOK 7-13.Nov 14, 2000 · N189FE · Boeing 72722 · Cabin Pressure Control SystemSDR 00FDEA00493Annunciator · inoperativeGREEN NOSE GEAR DOWN AND LOCKED IND INOP ON EXTENSION. RED TABS COMPLETED WITH NO JOY. NORMAL LANDING. *S/D* REMOVED AND REPLACED PER WIRING DIAGRAM 32-64-01 & 32-64 PG 4. REMOVED AND REPLACED GEAR WARNING ANNUNCIATOR PNL, OPS CK NORM PER 727-100 MM 32-61Jul 27, 2000 · N189FE · Boeing 72722 · Landing Gear Position and WarningSDR 00FDEA00474Rib · crackedDURING ROUTINE INSPECTION, NR 4 LEAD EDGE SLAT FOUND CRACKED AT I/B ACTUATOR ATTACH RIB. STOP DRILL, FAB AND INSTALLED PER IAW SRM 51-40-3 & SRM 51-30-2.Jul 17, 2000 · N189FE · Boeing 72722 · Leading Edge DevicesSDR 00FDEA00473Window Post · crackedDURING ROUTINE INSPECTION, RT E-N WINDOW POST FOUND CRACKED. REPAIRED E-N WINDOW POST IAW FEDEX EO 7-5330-7-3354, PT 5.Jul 17, 2000 · N189FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 00FDEA00472Cover · crackedDURING ROUTINE INSPECTION, FWD ENTRY DOOR EMERGENCY ESCAPE SLIDE LWR CASE FOUND CRACKED AT BOTH SIDES OF STOW HOOKS. REMOVED AND REPLACED WELD PER IAW BAC 5975, MM 25-60-13.Jul 17, 2000 · N189FE · Boeing 72722 · Escape SlideSDR 00FDEA00471Web · crackedDURING ROUTINE INSPECTION, WEB AT LEFT WING LEAD EDGE BS 920 FOUND CRACKED ADJACENT TO BOTTLE BOLT. REMOVED AND REPLACED PER IAW SRM 51-40-2.Jul 17, 2000 · N189FE · Boeing 72722 · Wing Miscellaneous StructureSDR 00FDEA00470Structure · corrodedDURING ROUTINE INSPECTION, NR 6 LEAD EDGE FLAP CORRODED BEYOND ALLOWED LIMITS ON THE OUTER SURFACE. REMOVED AND REPLACED PER IAW MM 27-81-1. OPS CK GOOD IAW MM 27-81-1.Jul 17, 2000 · N189FE · Boeing 72722 · Leading Edge DevicesSDR 00FDEA00469Pressure Panel · crackedDURING ROUTINE INSPECTON, RIGHT WHEEL WELL FOUND CRACKED AT I/B WEB AT BS 920. REMOVED AND REPLACED PER IAW SRM 51-40-2.Jul 17, 2000 · N189FE · Boeing 72722 · Fuselage Main, BulkheadSDR 00FDEA00468Heat Shield · crackedDURING ROUTINE INSPECTION, NR 3 ENGINE PRE-COOLER HEAT SHIELD FOUND CRACKED ON UPPER I/B SIDE. STOP DRILLED CRACK, FAB, AND INSTALLED PER IAW SRM 51-40-2.Jul 17, 2000 · N189FE · Boeing 72722 · Turbine SectionSDR 00FDEA00467Light · inoperativeDURING ROUTINE INSPECTION, FWD ENTRY DOOR EMERGENCY EXIT LIGHT FOUND INOP WHEN SWITCH IS IN THE ARM POSITION. REMOVED AND REPLACED PER IAW MM 33-50-1.Jul 17, 2000 · N189FE · Boeing 72722 · Emergency LightingSDR 00FDEA00466Battery Pack · crackedDURING ROUTINE INSPECTION, FWD ENTRY DOOR ESCAPE SLIDE LIGHT BATTERY PACK FOUND CRACKED. REMOVED AND REPLACED PER IAW MM 33-50-112.Jul 17, 2000 · N189FE · Boeing 72722 · Escape SlideSDR 00FDEA00465Rib · crackedDURING ROUTINE INSPECTION, THE NR 5 LEAD EDGE SLAT FOUND CRACKED AT O/B ACTUATOR ATTACH RIB. STOP DRILLED CRACK, FAB REPAIR, AND INSTALLED IAW SRM 51-40-3 & SRM 51-30-2.Jul 17, 2000 · N189FE · Boeing 72722 · Leading Edge DevicesSDR 99FDEA00198Transmitter · failed99-121 - ON ROTATION, STICK SHAKER ACTUATED, 2ND REPEAT WRITE UP. REMOVED AND REPLACED RIGHT INBD FLAP TRANSMITTER PER MM 27-52-001 OPER CK GOOD.May 29, 1999 · N189FE · Boeing 72722 · Trailing Flap Position Indicating SystemSDR 98FDEA00231Forging · corrodedWHILE WORKING NR 0441, FOUND CORROSION ON BS 870 FORGING, RBL 57, WL 168. *S/D* REMOVED AND REPLACED RIGHT HAND BS 870 FITTING STR 9 TO WL 156 IAW FED-EX NR 7-5310-38683.Apr 3, 1998 · N189FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 98FDEA00203Splice · crackedNR 0439 014, BS 870 LT UPPER SPLICE PLATE FOR UPPER CHORD HAS 2 CRACKED HOLES AND 1 DAMAGED HOLE AOG ACCESS REQUIRED. REMOVED AND REPLACED BS 870 LT UPPER SPLICE PLATE PER BOEING DRAWING 64-8336.Mar 18, 1998 · N189FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 98FDEA00181Strap · corrodedCORROSION (C53-132-02-1, 2) ON LOAD TENSION STRAP BS 870, RBL 35 TO 50. *S/D* REPAIRED BS 870 LOAD TENSION STRAP AT RBL 30 TO 60 IAW FED-EX EA 7-5310-37605.Mar 12, 1998 · N189FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 98FDEA00092Frame · corrodedNR 0433 012, WHILE WORKING NR0301, FOUND FRAME TO BE CORRODED AT BS 680, RBL 24, WL 155 (STR 26). REMOVED DAMAGE AT BS 680, RBL 24 FROM STR 22-26 RT. FOUND TO BE OUT OF LIMITS IAW FED-EX SRM 53-10-1. REPAIRED DAMAGED FRAME AT BS 680, RBL 24, STR 22-26 RT IAFeb 10, 1998 · N189FE · Boeing 72722 · Fuselage Main, FrameSDR 98FDEA00054Stiffener · corrodedCORROSION (C53-224-03-1/2) ON NOSE WHEEL WELL HORIZONTAL STIFFENER BS 303, RBL 8, WL 180. *S/D* REMOVED AND REPLACED HORIZONTAL STIFFENER BS 303, RBL 8, WL 180 IAW FEDEX DRAWING NR 65-18417.00.Jan 26, 1998 · N189FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 98FDEA00035Tee Fitting · corrodedWHILE WORKING NR0328, FOUND CORROSION ON TEE FITTING AT BS 336, LBL 17, WL 150. *S/D* REMOVED AND REPLACED TEE FITTING AT BS 336, LBL 17, WL 155 IAW FED-EX DRAWING 65-18415.Jan 15, 1998 · N189FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 98FDEA00031Floorbeam · gougedUPON REMOVAL OF RADIUS FILLER, FOUND DEEP GOUGE AT BS 880, LBL 15, WL 201.5. *S/D* BLENDED OUT GOUGE, CRACK AND CORROSION AT BS 880, LBL 15, WL 201.5 ORIGINAL THICKNESS WAS .1, MATERIAL REMOVED WAS .045. BLENDOUT AREA IS .3 X .2, FOUND TO BE OUT OF LIMITS PJan 15, 1998 · N189FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 98FDEA00028Chord · corrodedWHILE WORKING NR 0329, FOUND FRAME FAIL-SAFE CHORD CORRODED AT BS 312, LBL 19, WL 153. *S/D* FOUND CORROSION DAMAGE ON FAIL-SAFE CHORD AT BS 312, LBL 19, WL 153 TO BE OUT OF LIMITS IAW FEDEX SRM 53-10-1. REMOVED CHORD LBL 19 TO LBL 42. FABRICATED NEW PART AJan 12, 1998 · N189FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 98FDEA00027Floorbeam · corrodedNR 0429 007, WHILE WORKING NR0408, FOUND CORROSION ON FLOORBEAM BS 344, RBL 17 OUT OF LIMITS AND DOUBLE HOLE DRILLED AT RBL 38, WL 208. REMOVED AND REPLACED BS 344 BEAM UPPER CHORD LBL 17 TO RBL 65 PER FED-EX DRAWING SR 27-53-007.Jan 12, 1998 · N189FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 98FDEA00026Bulkhead Web · corrodedCORROSION (C53-132-02-1, 2) IN NUMEROUS AREAS ON BS 870 BULKHEAD WEB OF CENTER WING SECTION. *S/D* REMOVED AND REPLACED 870 BULKHEAD WEB OF CENTER WING SECTION PER EA 7-5710-38653.Jan 12, 1998 · N189FE · Boeing 72722 · Wing, Rib/BulkheadSDR 98FDEA00025Spar Chord · corrodedCORROSION (C53-132-02-1, 2) ALONG VERTICAL FLANGE OF BS 870 UPPER SPAR CHORD WL 180, RBL 65- LBL 65. *S/D* REMOVED AND REPLACED 870 UPPER SPAR CHORD WL 180, RBL 65 - LBL 65 IAW FED-EX EA 7-5100-37367 AND 7-5710-38653.Jan 12, 1998 · N189FE · Boeing 72722 · Wing SparSDR 98FDEA00018Angle · corrodedNR 0329 004, CORROSION C53-111-03-1/2 ON LT LOWER NOSE CHORD BS 336 TO 350, LBL 17, WL 149. FOUND CORROSION ON LT LOWER NOSE ANGLE BS 336 TO 350, LBL 17, WL 149 TO BE OUT OF LIMITS IAW FED-EX SRM 53-10-01. REMOVED AND REPLACED ANGLE BS 284 TO BS 350, LBL 17,Jan 8, 1998 · N189FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 98FDEA00017Chord · corrodedNR 0328 003, CORROSION C53-111-03 1/2 ON RT LOWER NOSE CHORD BS 336 TO 350, RBL 17, WL 149. FOUND CORROSION ON RT LOWER NOSE CHORD BS 336 TO BS 350, RBL 17, WL 149 TO BE OUT OF LIMITS IAW FED-EX SRM 53-10-1. REMOVED AND REPLACED CHORD BS 284 TO BS 350 RT, RBJan 8, 1998 · N189FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 98FDEA00011Chord · corrodedCORROSION (C53-224-03 1, 2) ON RT MID CHORD BS 315 TO 335, RBL 15, WL 169 WILL REQUIRE REMOVAL OF NOSE LANDING GEAR TO GAIN ACCESS. *S/D* REMOVED DAMAGED CHORD AND INSTALLED NEW CHORD BS 259 TO 351, WL 169, RBL 15 IAW FEDEX DRG 65-18415.Jan 7, 1998 · N189FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 98FDEA00010Stringer · corrodedCORROSION ON STR 29 LT KEEL BEAM LT BS 1080, WL 140. *S/D* REMOVED CORROSION ON STR 29L AT BS 1080 TO 1095, WL 140. FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1. REMOVED CORRODED PIECE IAW FEDEX SRM 53-10-3. FABRICATED REPAIR PARTS PER FEDEX SRM 53-10-Jan 7, 1998 · N189FE · Boeing 72722 · Fuselage Main, Longeron/StringerSDR 96FDEA01656Gcu · water contamNR 1 GENERATOR TRIPPED OFF LINE 2-3 MINUTES AFTER TAKEOFF. BUS TIE WOULD NOT CLOSE PER CHECKLIST. FINALLY DID CLOSE BUT FIELD WOULD THEN NOT CLOSE WITH GOOD RESIDUAL VOLTS. REMOVED AND CLEANED WATER FROM GCU. REINSTALLED, OPS CHECKED NORMAL PER JRH 8-3.Nov 7, 1996 · N189FE · Boeing 72722 · AC RegulatorSDR 96FDEA01052Door Switch · failedAT FLT LEVEL 310, MCD ANNUNCIATOR LIGHT ILLUMINATED. ACCOMPLISHED CHECKLIST AND DEPRESSURIZED A/C IN DESCENT. LIGHT REMAINED ILLUMINATED UNTIL 2,000 FEET ABOVE GROUND LEVEL ON APPROACH, THEN WENT OUT. NO OTHER SYMPTOMS WERE NOTED, NO NOISE OR LOSS OF PRESSUMay 29, 1996 · N189FE · Boeing 72722 · Door Warning SystemSDR 96FDEA00196Retract Mech · failedDURING FLAP RETRACTION, L/E DEVICES FAILED TO RETRACT PROPERLY. ARRIVED WITH THE L/E DEVICES AND FLAP HANDLE IN THE 2 DEGREE POSITION AMBER LIGHT WAS STILL ON, NO GREEN LIGHT. CYCLED FLAPS AND OPS CHECK NORMAL.Feb 9, 1996 · N189FE · Boeing 72722 · Leading Edge Slat Control System
Back to N189FE, cancelled Aug 2, 2007