N180FE, cancelled Sep 29, 2006

Service difficulty reports · 30

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 = 'N180FE' AND deregistration_id = 'N180FE-2006-09-29'
  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 06FDEA0016O-Ring · leakingJUST AFTER LEVEL OFF AT 16000 EXPERIENCED COMPLETE SYS-A HYD FAILURE. QTY AND PRESSURE BOTH WENT IMMEDIATELY TO ZERO. RAN QRH CHECKLIST, TIMED SYS-A FLUID SHUTOFF SWITCHES OFF FOR 55 MIN TO LANDING. LED NR 5 AMBER AND GREEN LIGHTS ON, ALL SLATS AND LED LIGHJan 4, 2006 · N180FE · Boeing 727100 · Hydraulic System, MainSDR 05FDEA02219Indicator · spinningNR 3 EPR GAUGE ERRATIC SPINNING RAPIDLY WHEN T/O POWER SET. AFTER RTO, OPERATELY NORMALLY ON SECOND ATTEMPT. INFO NOTED PER CREW, OPS CHECK GOOD ON GROUND, NO DEFECTS NOTED OK TO CONTINUE.Aug 3, 2005 · N180FE · Boeing 72722 · Engine Pressure Ratio (EPR)SDR 05FDEA01745Hydraulic System · leakingAT ROTATION A-SYS HYD FLUID WENT TO ZERO, RAN QRH, KEPT GEAR DOWN AND FLAPS 15, HAD A-SYS FLUID SHUT OFF SWITCHED OFF 23 MIN. DECLARED EMERGENCY. R & R INBOARD FLAP FLOW LIMITING VALVE PER MM. R & R NR 1 & 2 ENGINE PUMP CASE DRAIN FILTERS PER MM. R & R BOTHJun 29, 2005 · N180FE · Boeing 727100 · Hydraulic System, MainSDR 97FDEA00395Frame · crackedNR 0646 013 WHILE WORKING CUSTOMER CARD NR 0607, FOUND FRAME CRACKED BS 1110, WL 153, RBL 25. REPAIRED CRACKED FRAME AT BS 1110, WL 153, RBL 25. ALL WORK DONE PER FED-EX SRM 51-40-3.Jul 8, 1997 · N180FE · Boeing 72722 · Fuselage Main, FrameSDR 97FDEA00365Frame · crackedCRACK IN FRAME BS 680, STR 22L IN FORWARD CARGO BAY. *S/D* REMOVED DAMAGED FRAME AREA 2.75 DIAMETER AREA. HFEC NOTED NO CRACKS FOUND. FABRICATED REPAIR PARTS FROM 7075-0 .050, IAW FED-EX SRM 51-40-3. TREATED AND PRIMED REPAIR PARTS PER FED-EX SRM 51-10-2.Jun 24, 1997 · N180FE · Boeing 72722 · Fuselage Main, FrameSDR 97FDEA00362Skin · disbondedSKIN IS DISBONDED AT BS 1143 TO 1166 BETWEEN STR 24R TO 25R. *S/D* ACCESSED AREA, REMOVED EXISTING DOUBLERS, REMOVED SKIN BS 1080 TO 1183, STR 20 TO 26R. DRILLED, TREATED MATERIAL AND INSTALLED. FABRICATED DOUBLERS, TREATED AND INSTALLED IAW FED-EA 7-5330Jun 20, 1997 · N180FE · Boeing 72722 · Fuselage Main, Plate/SkinSDR 97FDEA00361Chord · crackedRIGHT MAIN GEAR WELL, BS 950, RBL 3, WL 180, - 75 CRACK TOP OF AFT VERTICAL CHORD. *S/D* REMOVED DAMAGED VERTICAL CHORD, FABRICATED AND INSTALLED NEW VERTICAL CHORD AT BS 950, RBL 3, WL 150 TO 180 PER BOEING DRAWING 65-18636 AND FEDEX SRM 51-30-2.Jun 19, 1997 · N180FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 97FDEA00357Skin · disbondedNR 0577 007, SKIN IS DISBONDED AT BS 1143 TO 1183 RT BETWEEN STR 18, 19 AND 20. *S/D* REPAIRED DISBONDED SKIN AT BS 1143 TO 1183 RT BETWEEN STR 18, 19 AND 20 RT PER FED-EX SRM 53-30-4.Jun 19, 1997 · N180FE · Boeing 72722 · Fuselage Main, Plate/SkinSDR 97FDEA00356Stringer · corrodedNR 0124 008 CORROSION (C53-224-01(3)) ON STRINGER 2 RT AT BS 967. REPAIRED CORRODED STRINGER NR 2 RT AT BS 967. ALL WORK DONE PER FED-EX SRM 51-40 AND 53-10-3.Jun 19, 1997 · N180FE · Boeing 72722 · Fuselage Main, Longeron/StringerSDR 97FDEA00350Floorbeam · corrodedNR 0573 006 WHILE WORKING NR 0172 FOUND CORROSION EMANATING FROM UNDER CEILING SUPPORT STRAP BS 540, RBL 25, WL 200. REPAIRED FLOORBEAM AT BS 540, RBL 25, WL 200 IAW FED-EX SRM 53-10-8.Jun 17, 1997 · N180FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 97FDEA00346Chord · corrodedNR 0571 004, CORROSION (C53-100-01,1) ON UPPER CHORD OF FRAME AT BS 220, RBL 21, WL 148. *S/D* REMOVED DAMAGED UPPER CHORD. FABRICATED AND INSTALLED NEW UPPER CHORD BS 220, RBL 28 TO LBL 28, WL 148 PER BOEING DRAWING 65-16305.Jun 13, 1997 · N180FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 97FDEA00338Floorbeam · corrodedNR 0215 002 CORROSION EMANATING FROM UNDER NUT PLATE BS 600 FLOORBEAM UPPER CHORD AT RBL 17, WL 208. REMOVED DAMAGED FLOORBEAM UPPER FLANGE REPAIRED PER FED-EX SRM 53-10-8 FIG 3.Jun 11, 1997 · N180FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 97FDEA00347Frame · crackedNR 0558 005, FRAME CRACKED AT BS 680, STR 26R FWD CARGO BAY. *S/D* STOP DRILLED CRACK, FABRICATED DOUBLER AND INSTALLED AT BS 680, STR 26R AS PER FED-EX SRM 51-40-3.Jun 5, 1997 · N180FE · Boeing 72722 · Fuselage Main, FrameSDR 97FDEA00345Angle · corrodedNR 0504 003, CORROSION ON SHEAR TIE AFT SIDE OF BS 660, STR 27 TO 28 RT. *S/D* REMOVED CORRODED SHEAR TIE ANGLE FROM BS 660 FRAME, AFT SIDE BETWEEN STR 27 TO 28 RT. CORROSION FOUND TO BE OUT OF LIMITS PER FED-EX SRM 53-10-1. FABRICATED, DRILLED, ALODINED, Jun 5, 1997 · N180FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 97FDEA00329Frame · dentedNR 0502 001, BS 660 FRAME DENTED BETWEEN STR 24 TO 23 LT. *S/D* REPAIRED DENTED FRAME BS 660 BETWEEN STR 24 AND 23L PER FED-EX SRM 51-40-3.Jun 5, 1997 · N180FE · Boeing 72722 · Fuselage Main, FrameSDR 97FDEA00360Beam · crackedNR 0214 FORWARD ENTRY DOOR LOWER GATE BEAM IS CRACKED IN RADIUS ON AFT SIDE. REMOVED AND INSTALLED NEW FORWARD ENTRY DOOR LOWER GATE BEAM IAW FED-EX SRM 51-30-2, 51-30-5, AND 51-30-8.Jun 1, 1997 · N180FE · Boeing 72722 · Passenger/Crew DoorsSDR 95FDEA00849Post · crackedRIGHT NR 2 WINDOW CUT OUT DOUBLER IS CRACKED IN THE UPPER AFT RADIUS. REPAIRED CRACK IN DOUBLER IAW EO 7-5330-7-3354 PART 5.Jun 28, 1995 · N180FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 95FDEA00848Spar · corrodedCORROSION FOUND ON UPPER REAR SPAR CHORD BS 870 AT RBL 20 AND LBL 10. REMOVED AND REPLACED UPPER REAR SPAR CHORD AT BS 870 PER EA NR 95-2684 AND DWG NR 65C21531-2.Jun 28, 1995 · N180FE · Boeing 72722 · Wing SparSDR 95FDEA00847Keel Beam · corrodedRIGHT KEEL BEAM CORRODED, BS 953, RBL 6, WL 156. CUT ACCESS HOLE IN SKIN, REMOVED AND REPLACED KEEL BEAM THEN REPAIRED HOLE IN SKIN. REF: TCO EWO NR 95-2710 AND SRM 53-30-3 FIG 3.Jun 28, 1995 · N180FE · Boeing 72722 · Fuselage Main, KeelSDR 95FDEA00846Frame · crackedAFT CARGO BAY BS 1130 STR 27L, FRAME IS CRACKED. CUT OUT DAMAGE AND REPAIR PER SRM 51-40-3.Jun 28, 1995 · N180FE · Boeing 72722 · Fuselage Main, FrameSDR 95FDEA00845Fitting · corrodedSTA 351, CORROSION ON STR 26R DOG BONE FITTING. REMOVED AND REPLACED STR 26R STA 351. FITTING IAW FEDEX SRM 51-30-2.Jun 28, 1995 · N180FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 95FDEA00844Frame · damagedFOUND FIGURE EIGHT HOLE IN FRAME FLANGE AT STA 1030 STR 27R. TRIMMED OUT DAMAGED PORTION OF FRAME, FABRICATED REPAIR PART AND INSTALLED WET WITH SEAL AS PER SRM 51-40-3.Jun 28, 1995 · N180FE · Boeing 72722 · Fuselage Main, FrameSDR 95FDEA00843Frame · crackedCRACKED FRAME AT BS 1070 STR 27L. REMOVED AND REPLACED FRAME AT BS 1070 STR 24-27L AND TREATED IAW FEDEX SRM 51-40-03, FEDEX MM 51-20-31 AND 51-20-21.Jun 28, 1995 · N180FE · Boeing 72722 · Fuselage Main, FrameSDR 95FDEA00842Frame · crackedCRACKED FRAME AT BS 1090 STR 27L. REMOVED AND REPLACED FRAME BS 1090 STR 24-27L AND TREATED IAW FEDEX SRM 57-40-03, FEDEX MM 51-20-31 AND 51-20-21.Jun 28, 1995 · N180FE · Boeing 72722 · Fuselage Main, FrameSDR 95FDEA00841Stringer · crackedSTR 23L IS CRACKED AT STA 380. REMOVED AND REPLACED STR 23L STA 360-384 IAW FEDEX SRM 53-10-3.Jun 28, 1995 · N180FE · Boeing 72722 · Fuselage Main, Longeron/StringerSDR 95FDEA00840Stringer · crackedPOSSIBLE CRACKS ON STR 24L BS 380. REMOVED DAMAGED STR, FABRICATED REPAIR PARTS AND INSTALLED IAW FEDEX SRM 53-10-3.Jun 28, 1995 · N180FE · Boeing 72722 · Fuselage Main, Longeron/StringerSDR 95FDEA00839Skin · gougedFORWARD CARGO BAY DOORWAY CUT OUT BS 523 BETWEEN STR 22 AND 23R, 2 EACH GOUGES MAXIMUM DEPTH OF .030 INCH. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW FEDEX SRM 53-30-3, AT FWD CARGO BAY DOORWAY CUT OUT BS 523 BETWEEN STR 22 AND 23R.Jun 28, 1995 · N180FE · Boeing 72722 · Fuselage Main, Plate/SkinSDR 95FDEA00838Skin · dentedDENT APPROXIMATELY .100 INCH DEEP IN SKIN AT BS 461 WL 210 RT SIDE. CUT OUT DENT AT BS 461 WL 210 AND FABRICATED A REPAIR DOUBLER AND INSTALLED AS PER FEDEX SRM 53-30-3 FIG 1.Jun 28, 1995 · N180FE · Boeing 72722 · Fuselage Main, Plate/SkinSDR 95FDEA00837Tie · crackedWEB TO FRAME TIE FOUND TO BE CRACKED AT STA 823 RBL 67 WL 208. REMOVED FRAME TIE AT STA 823 RBL 67 WL 208 FABRICATED NEW TIE ALODINED AND PRIMED, INSTALLED PER FEDEX SRM 51-20-1 AND SRM 51-10-2.Jun 28, 1995 · N180FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 95FDEA00836Skin · gougedGOUGE LESS THAN .004 INCH DEEP IN SKIN AT BS 410 WL 156 LT SIDE. FOUND GOUGE TO BE OUT OF LIMITS, REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER AT BS 410 WL 156 LT SIDE IAW FEDEX SRM 53-30-3.Jun 28, 1995 · N180FE · Boeing 72722 · Fuselage Main, Plate/Skin
Back to N180FE, cancelled Sep 29, 2006