N185FE, cancelled May 23, 2007

Service difficulty reports · 114

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 = 'N185FE' AND deregistration_id = 'N185FE-2007-05-23'
  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 06FDEA2569Blade · damagedAS POWER WAS ADVANCED TO MAX POWER FOR T/O, THERE WAS A LOUD BANG AND THUMP IN THE THROTTLE QUADRANT, FOLLOWED BY THE SOUND OF A CABLE UNWINDING. T/O WAS DISCONTINUED AND AIRCRAFT RETURNED TO MX. AFTER DEBRIEFING FLIGHT CREW PROCEEDED TO INSPECT NR 2 ENGINE Jul 15, 2006 · N185FE · Boeing 727100 · Engine (Turbine/Turboprop)SDR 06FDEA1659Attach Fitting · damagedFORWARD TRUNNION ATTACH FTG OVERSIZE HOLE REWORK. COMPLIED WITH EA 7-5710-7-92417 WINGS MAIN FRAME MLG TRUNNION ATT FITTING OVERSIZE HOLE REWORK RII:573074.May 1, 2006 · N185FE · Boeing 72722 · Wing, Landing Gear Attach FittingsSDR 06FDEA1658None · noneTRUNNION ATTACH FITTING MODIFICATION. COMPLIED WITH EO 7-5710-7-2314D PT5 WINGS MLG TRUNNION ATTACH FITTING.May 1, 2006 · N185FE · Boeing 72722 · Standard Practices/StructuresSDR 06FDEA1657Attach Fitting · crackedCOMPLY WITH EO 7-5710-7-2314D PT6 EOCN D1 WINGS - MLG TRUNNION ATTACH FITTING MODIFICATION BOEING S/B 72 7-57AD132 R3 AD 2004-18-08. COMPLIED WITH EO 7-5710-7-2314D PT6 RII:536327.May 1, 2006 · N185FE · Boeing 727100 · Wing, Landing Gear Attach FittingsSDR 06FDEA0308Lamp · inoperativeLT MLG GREEN LIGHT DID NOT ILLUMINATE FOR LANDING. CREW REPORTED GEAR WAS DOWN BY VISUAL INSPECTION UPON ARRIVAL RE-LAMPED LEFT MAIN GEAR GREEN LIGHT OPS CHECK GOOD IAW MMSP.Jan 21, 2006 · N185FE · Boeing 727100 · Landing Gear Position and WarningSDR 05FDEA01270Wire · brokenEXTENDING GEAR, DID NOT GET RIGHT MAIN GEAR GREEN LIGHT. TAIL SKID LIGHT ON S/O PANEL WAS ALSO ILLUMINATED. CHECKLIST LEAD US TO TEST GREEN LIGHT, LIGHT WAS WORKING. CB PRESS TO TEST AND LIGHTS WERE RESET PER CHECKLIST. VERIFIED RIGHT MAIN DOWN WITH MANUALMay 13, 2005 · N185FE · Boeing 72722 · Landing Gear System WiringSDR 05FDEA00093Fairing · missingON ARRIVAL FOUND AFT CARGO DOOR MOVABLE FAIRING MISSING FROM AIRCRAFT. INSTALLED AFT CARGO DOOR MOVABLE FAIRING PER 727-100 MM 52-33-00-4. OPS CHECK GOOD.Jan 14, 2005 · N185FE · Boeing 727100 · Aerodynamic FairingsSDR 04FDEA03199Control Unit · malfunctionedLOWER AFT CARGO SMOKE WARNING ILLUMINATED IN FLIGHT. RAN QRH. DISCHARGED BOTTLE-1, LANDED IN LCK IN 20 MIN. SECOND BOTTLE DID NOT AUTO-FIRE AS PER 25 MIN REQUIREMENT. CFR CREWS DETERMINED NO FIRE PRESENT. FOUND ALL TEST LIGHTS ON AFT LOWER CARGO COMPARTNov 24, 2004 · N185FE · Boeing 72722 · Smoke DetectionSDR 04FDEA02265Skin · corrodedCORROSION ON INNER SKIN AT AFT CARGO DOOR AFT CUTOUT LOWER CORNER. REPAIRED INNER SKIN AT AFT CARGO DOOR AFT CUT OUT LOWER CORNER PER FED EX E.A. 7-5310-55341.Jul 28, 2004 · N185FE · Boeing 727100 · Fuselage Main, Plate/SkinSDR 04FDEA02264Door Frame · corrodedCORROSION AFT CARGO DOORWAY AFT FRAME AT CORNER THRESHOLD CONTINUING UNDER FILLER. REPAIRED AFT CARGO DOORWAY AFT FRAME AT CORNER THRESHOLD PER FED EX E.A. 7-5310- 55341.Jul 28, 2004 · N185FE · Boeing 727100 · Fuselage Main, StructureSDR 04FDEA02263Stringer · corrodedCORROSION ON UPPER SURFACE OF STRINGER 7L STA 876. CORROSION DAMAGE ON UPPER SURFACE OF STRINGER 7L, STA 876 WAS FOUND TO BE OUT OF LIMITS PER SRM 53-10-1 FIG 1. REMOVED DAMAGED STRINGER SECTION BS 870 - 890+10, STR 7L PER SRM 51-10-5 AND 51-30-2. FAJul 28, 2004 · N185FE · Boeing 727100 · Fuselage Main, Longeron/StringerSDR 04FDEA02266Skin · crackedCRACK IN SKIN AT EDGE OF LAP JOINT BS 1064 RBL 26 STR 26R.Jul 28, 2004 · N185FE · Boeing 727100 · Fuselage Main, Plate/SkinSDR 04FDEA02180Skin · dentedDENT IN FUSELAGE SKIN BS 320-330 AND 2 INCHES ABOVE STR 21R. REPAIRED THE FUSELAGE SKIN AT BS 320 TO 330 2 INCHES ABOVE STR 21R PER EA 7-5330- 70671Jul 26, 2004 · N185FE · Boeing 727100 · Fuselage Main, Plate/SkinSDR 04FDEA02191Stringer · crackedWHILE WORKING CARD N00533, FOUND CRACKED STRINGER AT BS 1114 STR 25 RT. *S/D* REPAIRED STRINGER 25 RT AT BS 1107-1115 PER SRM 53-10-3 FIG 1.Jul 26, 2004 · N185FE · Boeing 727100 · Fuselage Main, Longeron/StringerSDR 04FDEA02190Seat Track · corrodedCORROSION AROUND SEAT TRACK LINK AFT ATTACH BOLT BS 870 LBL 25 WL 205. *S/D* CORROSION ON AROUND SEAT TRACK LINK ATTACH BOLT AT BS 870 LBL 25 WL 205 WAS FOUND TO BE IN LIMITS. CORROSION ON LINK AT BS 870 LBL 25 WL 208 WAS OUT OF LIMITS. REMOVED & REPLACED Jul 26, 2004 · N185FE · Boeing 727100 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA02189Seat Track · corrodedCORROSION SEAT TRACK BS 870-950, RBL 45, WL 208. CORROSION ON SEAT TRACK AT BS 870-950 RBL 45 WL 208 WAS FOUND TO BE OUT OF LIMITS. REMOVED & REPLACED SEAT TRACK PER SRM 53-10-5.Jul 26, 2004 · N185FE · Boeing 727100 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA02188Seat Track · corrodedCORROSION SEAT TRACK BS 760-840 RBL 22 WL 208. REMOVED AND REPLACED LONGITUDAL BEAM STA 760-848 RBL 22, WL 208 IAW SRM 51-30-02, 51-30-5.Jul 26, 2004 · N185FE · Boeing 727100 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA02187Seat Track · corrodedCORROSION SEAT TRACK BS 760-840 LBL 25 WL 208 AT FASTENER HOLES. REMOVED CORROSION ON SEAT TRACK FROM BS 760-840 LBL 25 WL 208 FOUND SEAT TRACK TO BE OUT OF LIMITS. LOCATED AND DRILLED HOLES ON NEW LONGITUDAL BEAM AND INSTALLED IAW SRM 51-30-2.Jul 26, 2004 · N185FE · Boeing 727100 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA02186Seat Track · damagedCORROSION SEAT TRACK BS 870, LBL 45, WL 208. REMOVED CORROSION ON SEAT TRACK STA 870 LBL 45, WL 208. REMOVED .040, 1 INCH X 1 INCH FROM .080. OUT OF LIMITS. REMOVED DAMAGED SEAT TRACK, LOCATED AND DRILLED, ALODINED AND PRIMED NEW SEAT TRACK, INSTALLED NEW SEAJul 26, 2004 · N185FE · Boeing 727100 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA02185Angle · dentedFWD CARGO COMPARTMENT J-ANGLE DENTED OUT OF LIMITS AT BS 500 LBL 28 WL 155. *S/D* FOUND J-ANGLE DENTED OUT OF LIMITS AT BS 500 LBL 28 WL 155. REMOVED, FABRICATED AND INSTALLED NEW J-ANGLE IAW SRM 53-10-1 PG 2 FIG 1 SHEET 2, SRM 51-30-2.Jul 26, 2004 · N185FE · Boeing 727100 · Fuselage Miscellaneous StructureSDR 04FDEA02184Seat Track · corrodedCORROSION AROUND SEAT TRACK LINK FWD ATTACH BOLT BS 742 RBL 48 WL 205. *S/D* CORROSION ON LINK AT BS 742 WAS OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK LINK AND FWD ATTACH BOLT AT BS 742 RBL 48 WL 205 PER SRM 51-30-2, 53-10-1 & 53-10-5 & AT BS 740-760 RJul 26, 2004 · N185FE · Boeing 727100 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA02183Seat Track · corrodedCORROSION AROUND SEAT TRACK LINK FWD ATTACH BOLT BS 742 LBL 25 WL 205. *S/D* REMOVED AND REPLACED SEAT TRACK LINK BS 740 TO BS 760, LBL 25, IWL 205 IAW SRM 51-30-2.Jul 26, 2004 · N185FE · Boeing 727100 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA02182Stringer · corrodedCORROSION WHILE WORKING CARD N00233 FOUND CORROSION ON STRINGER 26 LEFT LBL 20 BS 1135. CORROSION ON STA 26 LEFT BS 1135 WAS FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED STR 26 LEFT BS 1120-1140 AND INSTALLED NEW STRINGER & REPAIR SPLICE PER SRM 53-10-Jul 26, 2004 · N185FE · Boeing 727100 · Fuselage Main, Longeron/StringerSDR 04FDEA02181Floorbeam · corrodedCORROSION FLOORBEAM BS 344, BS LBL 60 - RBL 12, WL 208. *S/D* REMOVED AND REPLACED FLOORBEAM SECTION AT BS 344 LBL 7 TO LBL 65 WL 208 PER SRM 53-10-8.Jul 26, 2004 · N185FE · Boeing 727100 · Fuselage Main, Floor BeamSDR 04FDEA02142Fitting · crackedCRACKED STR FITTING AT BS 874 STR 9R. REMOVED AND REPLACED STRINGER 9R FITTING AT BS 874 IAW BOEING 727 SRM 51-30-5, BOEING 727 SRM 51-30-2.Jul 20, 2004 · N185FE · Boeing 727100 · Fuselage Main, Attach FittingsSDR 04FDEA02143Stringer · damagedMECHANICAL DAMAGE IN MAIN CARGO ON STRINGER AT BS 442 STR 5L. REMOVED DAMAGE AND FABRICATED A REPAIR IAW SRM 53-10-3, 51-30-2, 51-10-2 AND 51-10-6. INSTALLED REPAIR PARTS PER SRM 51-10-6 AND 51-30-2.Jul 20, 2004 · N185FE · Boeing 727100 · Fuselage Main, Longeron/StringerSDR 04FDEA02138Frame · damagedDAMAGE AT REPAIR DOUBLER AT BS 930, 3 INCHES ABOVE STR 14 LT, AFT SIDE OF FRAME. REMOVED AND REPLACED REPAIR DOUBLER AT BS 930, 3 ABOVE STR 14 LT PER SRM 51-30-2, 53-10-3.Jul 19, 2004 · N185FE · Boeing 727100 · Fuselage Main, FrameSDR 04FDEA02096Skin · corroded(C54-451-01, 2) EXTERNAL FUSELAGE SKIN PILLOWED & EMINATING POWDER AT BUTT JOINTS BS 1363-1379, 6 INCHES OVER NR 2 ENGINE CUTOUT, RT SIDE. REMOVED DAMAGE SKIN PANEL AT BS 1363 TO 1379 AND FABRICATED NEW PANEL. ALODINE, PRIMED AND PAINTED NEW PANEL. INSTALLJul 16, 2004 · N185FE · Boeing 727100 · Fuselage Main, Plate/SkinSDR 04FDEA02095Stringer · crackedFWD CARGO COMPARTMENT, STR 21 LT BS 488 IS CRACKED. REMOVED DAMAGE PORTION OF STR 21 LT, BS 488. FABRICATED REPAIR PARTS. ALODINED, PRIMED AND INSTALLED IAW SRM 53-10-3 FIG 1.Jul 16, 2004 · N185FE · Boeing 727100 · Fuselage Main, Longeron/StringerSDR 04FDEA02094Floorbeam · corrodedCORROSION 870 FLOORBEAM UPPER SECTION RBL 20 & RBL 26 WL 208. REMOVED CORROSION ON 870 BEAM UPPER CHORD, RBL 20 TO RBL 26, WL 208. FOUND 870 BEAM UPPER CHORD, RBL 20 TO RBL 26, WL 208 TO BE IN LIMITS IAW SRM 53-10-1, FIG 8.Jul 16, 2004 · N185FE · Boeing 727100 · Fuselage Main, Floor BeamSDR 04FDEA02093Floor Panel · corrodedCORROSION ON FLOOR WEB BS 620, LBL 48-55, WL 208, AND ELONGATED FASTENER HOLES. COMPLIED WITH FED EX E.A. 7-5310-70670 ON THE 620 FLOORBEAM LBL 48-55 WL 208.Jul 16, 2004 · N185FE · Boeing 727100 · Fuselage Floor PanelSDR 04FDEA02092Stringer · damagedMECHANICAL DAMAGE IN MAIN CARGO ON STRINGER AT BS 442, STR 6L. REMOVED AND REPLACED DAMAGED SECTION OF STRINGER 6L BS 442 I.A.W. BOEING 727 SRM 53-10-3 FIG 3.Jul 16, 2004 · N185FE · Boeing 727100 · Fuselage Main, Longeron/StringerSDR 04FDEA02089Floorbeam · corrodedCORROSION FLOORBEAM LWR FWD AT BS 1050 LBL 1 TO 22 WL 201. REMOVED DAMAGE ON FLOORBEAM LWR FWD AT BS 1050, LBL 1-22. FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE. FABRICATED REPAIR PARTS. ALODINED, PRIMED AND INSTALLED IAW SRM 53-10-8, 51-10-1.Jul 15, 2004 · N185FE · Boeing 727100 · Fuselage Main, Floor BeamSDR 04FDEA02088Floorbeam · corrodedCORROSION FLOORBEAM FASTENER HOLES BS 1110 LBL 21 WL 208. REMOVED AND REPLACED FLOORBEAM UPPER CHORD SECTION AT BS 1110 LBL 20-22.5 WL 208 PER SRM 53-10-8Jul 15, 2004 · N185FE · Boeing 727100 · Fuselage Main, Floor BeamSDR 04FDEA02087Crease Beam · corrodedCORROSION ON CREASE BEAM BS 1080 LBL 65 WL 208. CORROSION ON CREASE BEAM BS 1080, LBL 65, WL 208 FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED DAMAGED CREASE BEAM. INSTALLED NEW CREASE BEAM IAW 51-30-2, 51- 20-4.Jul 15, 2004 · N185FE · Boeing 727100 · Fuselage Main, StructureSDR 04FDEA02085Crease Beam · corrodedCORROSION ON CREASE BEAM BS 1010 - 1050 LBL 65 WL 208. CORROSION ON CREASE BEAM BS 1010 TO BS 1050, LBL 65, WL 208 FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVE DAMAGED CREASE BEAM, INSTALLED NEW CREASE BEAM IAW SRM 51-30- 2, 51-20-4.Jul 15, 2004 · N185FE · Boeing 727100 · Fuselage Main, StructureSDR 04FDEA02090Floorbeam · corrodedCORROSION ON LOWER FLOORBEAM FASTENERS BS 1110 RBL 1-12 WL 201. REMOVED CORROSION ON FLOORBEAM LWR CHORD BS 1110 RBL 6 WL 201, 2 X 1 MAXIUMUN MATERIAL LOSS .036 ORIGINAL THICKNESS .125 OUT OF LIMMITS PER SRM 51-10-6, 53-10-2 CUT OUT DAMAGE LWR FLANGE BS 1110 AJul 15, 2004 · N185FE · Boeing 727100 · Fuselage Main, Floor BeamSDR 04FDEA02078Beam · corrodedCORROSION ON RT HORIZONTAL STAB UPPER T/E BEAM UPPER SURFACE, ABOVE NR 7 HINGE. REMOVED AND REPLACED RT HORIZONTAL STAB UPR T/E BEAM IAW SRM 51-10-2, 51-30-2, 51- 30-5, 51-30-8 AND SOPM 20-50-01 AND EA 7-5510-72372.Jul 14, 2004 · N185FE · Boeing 727100 · Horizontal Stabilizer StructureSDR 04FDEA02077Stringer · corrodedCORROSION ON STR 23R BS 740. FOUND CORROSION TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED DAMAGED SECTION OF STRINGER PER SRM 53-10-3. FABRICATED REPAIR PER SRM 53-10-3 FIG. 1. INSTALLED REPAIR ONS TR 23R BS 740 PER SRM 53-10-3 AND SRM 53-30-2.Jul 14, 2004 · N185FE · Boeing 727100 · Fuselage Main, Longeron/StringerSDR 03FDEA00942Flap · malfunctionedNR 4 LEADING EDGE FLAP WOULD NOT RETRACT WHEN WE MOVED FROM FLAP 5 TO 2 WHILE INFLIGHT. INSTALLED JUMPER CABLE ON NR 4 L/E FLAP. UPON INSP FOUND NR 4 LE FLAP LIGHT ON AT S/O'S. PANEL WHEN NR 4 LE FLAP FULLY RETRACTED. INSTALLED ADAPTER CABLE ON NR 4 LE FLJun 21, 2003 · N185FE · Boeing 727100 · Leading Edge Slat Control SystemSDR 01FDEA00583Actuator · inoperative01-243 AFT DEPART WHEN FLAPS WERE RETRACTED TO 2 DEG #5 SLAT W/N RETRACT. R&R ACTUATOR PER 27-81-032-4. LEAK OPS CK GOOD.Jul 19, 2001 · N185FE · Boeing 72722 · Leading Edge Slat Control SystemSDR 00FDEA00181Switch · bentNR 5 LEAD EDGE FLAP SHOW INTRANSIT ABOUT 5 MIN AFT T/O. DID RED TABS, EXT TO 5 DEG AND BACK TO 0 AND LIGHT WENT OUT. REMOVED AND REPLACED MICRO SWITCH PER MM 27-81.Mar 28, 2000 · N185FE · Boeing 72722 · Leading Edge Slat Control SystemSDR 99FDEA00417Switch · malfunction99-248 REPEAT, LEFT MAIN GEAR IND GREEN LIGHT MALFUNCTION. SUSPECT DOWN LOCK SWITCH. REPLACED DOWNLOCK SWITCH PER 727 MM 32-61-021-4. PERF ADJUST AND TEST PER MM 32-61-021-5, OPER CK GOOD. OK FOR SERV.Oct 8, 1999 · N185FE · Boeing 72722 · Landing Gear Position and WarningSDR 99FDEA00416Connector · dirty99-247 - LEFT MAIN GEAR NOT DOWN AND LOCKED WITH HANDLE DOWN. NEGATIVE G PER RED TABS LOCK DOWN GEAR. CLEANED CANNON PLUG ON DOWN LOCK SWITCH LEFT GEAR. OPER CK GOOD PER GENERAL MM.Oct 8, 1999 · N185FE · Boeing 72722 · Landing Gear Position and WarningSDR 99FDEA00414Frame · corrodedNR 991, CORROSION ON BELTFRAME EXTRUSION BS 333 AT LT SKATE ANGLE. CUT OUT DAMAGE AND INSTALLED REPAIR PER DRAWING 65C 15724.Sep 14, 1999 · N185FE · Boeing 72722 · Fuselage Main, FrameSDR 99FDEA00413Bulkhead · corrodedNR 991 - CORROSION ON BULKHEAD BS 348 IN NOSE W/W IN AREA OF DRAG BRACE FITTING. REMOVED AND REPLACED PER EA 7-5310-45369 DATED AUG 16, 1999.Sep 14, 1999 · N185FE · Boeing 72722 · Fuselage Main, BulkheadSDR 99FDEA00411Frame · crackedNR 544, BS 804, STR 5R FRAME HAS VISUAL IND OF CRACK AT STR ATTACH RIVETS. CONFIRMED CRACK WITH DYE PENATRANT. REMOVED (CUTOUT) DAMAGED AREA. INSTALL REPAIR ANGLE PER SRM 53-10-4.Sep 14, 1999 · N185FE · Boeing 72722 · Fuselage Main, FrameSDR 99FDEA00408Stringer · damagedNR 522, STR 4L DAMAGED O/B SIDE BS 680 4 GOUGES IN 3 SECTION, 1 GOUGE THROUGH STR. REPAIR STR PER SRM 53-10-3 FIG 3.Sep 14, 1999 · N185FE · Boeing 72722 · Fuselage Main, Longeron/StringerSDR 99FDEA00406Bulkhead · crackedNR 379, CRACK IN 1183 BULKHEAD LT DOOR FRAME WEB AT WL 263. INSTALLED NEW BEAM SECTION AND SPLICED PER EA 7532045307 DATED 7/16/99 AND SB 727-53-210.Sep 14, 1999 · N185FE · Boeing 72722 · Fuselage Main, BulkheadSDR 99FDEA00405Frame · crackedNR 543, CRACK IN BELLFRAME BS 822 AT STR 5R. CUT OUT CRACKED AREA AND INSTALL .090 DOUBLER ALL PER 53-10-4 FIG 2.Sep 14, 1999 · N185FE · Boeing 72722 · Fuselage Main, Frame
Back to N185FE, cancelled May 23, 2007