N270FE, cancelled Dec 17, 2008

Service difficulty reports · 94

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 = 'N270FE' AND deregistration_id = 'N270FE-2008-12-17'
  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 08FDEA04355Stringer Clip · crackedMAIN CABIN UPPER LOBE STA 680 STR 4L CLIP CRACKED REMOVED CLIP STA 680 STR L4 REF SRM 51-30-02 P1. INSTALLED CLIP STA 680 STR L4 REF SRM 51-30-02 P1. THIS IS CLASSIFIED AS A MAJOR REPAIR.Oct 15, 2008 · N270FE · Boeing 727233 · Fuselage Main, Attach FittingsSDR 08FDEA04354Stringer Clip · corrodedFWD PIT BILGE BODY FRAME STR CLIP IS CORRODED BS 700, STR 26L, WL 153. REMOVED STRINGER CLIP, CORROSION ON CLIP WAS EXFOLIATED BEYOND REPAIR. FABRICATED, TREATED, AND PRIMED NEW CLIP, P/N 69-47375-2. INSTALLED CLIP REF SRM 51-30-2, PG 1-4/BOEING DWG NR 69-4Oct 15, 2008 · N270FE · Boeing 727233 · Fuselage Main, Attach FittingsSDR 07FDEA04686Switch · failedON FLAP RETRACTION TO 2 DEGREES, NR 2 LE FLAP REMAINS EXTENDED. NORMAL HYDRAULICS. RECYCLED TO 5 DEGREES AND BACK TO 2 DEGREES IAW QRH. NO LUCK. NO ASYMMETRIC CONTROL FORCES NOTED. OBTAINED NORMAL FLAPS 30 LANDING CONFIGURATION. REMOVED AND REPLACED NROct 25, 2007 · N270FE · Boeing 727233 · Leading Edge Slat Control SystemSDR 07FDEA03586Valve · leakingCALLED BACK BY RAMP. MX NOTICED HYD LEAK/PUDDLE ON GND AFTER WE TOOK OFF. REPLACED NR 3 BRAKE SHUTTLE VALVE PER B727 AMM 32-41-051-4. LK CKS GOOD.Sep 11, 2007 · N270FE · Boeing 727233 · Master Cylinder/Brake ValveSDR 07FDEA02367Control Knob · misalignedCLIMBING THRU 10,000' NOTICED NR 3 FUEL TANK SHOWED HAVING ALL IT'S FUEL AND NR 2 SHOWED HAVING BURNED TWICE THE AMOUNT IT SHOULD HAVE. AFTER FURTHER ANALYSIS CONCLUDED THE NR 3 CROSSFEED VALVE WAS NOT OPERATING AS THE INDICATOR SWITCH WAS SHOWING. WHEN THE Jul 3, 2007 · N270FE · Boeing 727233 · Fuel Quantity IndicatorSDR 06FDEA1959Repair · unknownFOUND PREVIOUSLY REPAIR ON LT INBD MID FLAP LOWER SURFACE INBD OF INBD CARRIAGE FAIRING IS NOT CONFORMED TO FAA APPROVED DATA. REMOVED EXISTING REPAIR AND REINSTALLED REPAIR PARTS IAW EA 7-5710-92428. REPAIR IS CLASSIFED AS MAJOR PER FEDEX GMM 6-2-100.May 18, 2006 · N270FE · Boeing 72722 · Wing Main, Frame StructureSDR 06FDEA1786None · noneFOUND PREVIOUSLY REPAIR INSTALLED AT LT ELEVATOR INBOARD UPPER SURFACE WAS ACCOMPLISHED IAW SRM 55-20-3 FIG 1 PAGE 1, BASED ON AN EXTERNAL EVALUATION, CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER SPACING AND NUMBER, GENERAL WORKMANSMay 11, 2006 · N270FE · Boeing 727233 · Standard Practices/StructuresSDR 06FDEA1784Repair · misinstalledFOUND EXISTING REPAIR INSTALLED AT STA 270 STR 17L IS NOT CONFORMED TO FAA APPROVED REPAIR DATA. REMOVED EXISTING REPAIR, FABRICATED REPAIR DOUBLER IAW SRM 53-30-3, FIG 3A. INSTALLED REPAIR DOUBLER IAW SRM 51-30-2 AND SRM 53-30-3 FIG 3A. REPAIR IS CLASSIFMay 11, 2006 · N270FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 06FDEA1783Repair · misinstalledFOUND PREVIOUSLY REPAIR INSTALLED AT STA 280 STR 22R IS NOT CONFORMED TO FAA APPROVED REPAIR DATA. REMOVED EXISTING REPAIR, FABRICATED NEW REPAIR DOUBLER IAW SRM 53-30-2 FIG 4. INSTALLED REPAIR DOUBLER IAW SRM 53-30-2 AND SRM 53-30-3. REPAIR IS CLASSIFIED AMay 11, 2006 · N270FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 06FDEA1753Repair · misinstalledFOUND PREVIOUSLY REPAIR INSTALLED AT STA 765 STR 8R IS NOT CONFORMED TO FAA APPROVED DATA, REMOVED EXISTING REPAIR AND REINSTALLED REPAIR DOUBLER AND FILLER IAW SRM 53-30-3 AND SRM 51-30-2. REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6- 2-100.May 9, 2006 · N270FE · Boeing 727233 · Fuselage Main, StructureSDR 06FDEA1745Repair · misinstalledFOUND PREVIOUSLY REPAIR INSTALLED ON NR 7 LEADING EDGE SLAT IS NOT COMPLIED WITH FAA APPROVED DATA. REMOVED EXISTING REPAIR AND REINSTALLED REPAIR DOUBLER IAW SRM 57-50-3, FIG 1. REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.May 8, 2006 · N270FE · Boeing 727233 · Leading Edge DevicesSDR 06FDEA1722None · nonePREVIOUSLY REPAIR INSTALLED AT STA 710, STR 21L WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 2 PAGE 9. BASED ON AN EXTERNAL EVALUATION, CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER SPACING AND NUMBERS.May 5, 2006 · N270FE · Boeing 727233 · Standard Practices/StructuresSDR 06FDEA1721None · noneFOUND PREVIOUSLY REPAIR INSTALLED AT LT FWD ENTRY DOOR HINGE CUTOUTS WAS ACCOMPLISHED IAW EA 7-5330-28325, BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SIZE, SHAPE, MATERIAL THICKNESS AND TYPE, FASTENER SPACING AND NUMBERS, GENERAL WORKMANSHIP May 5, 2006 · N270FE · Boeing 727233 · Standard Practices/StructuresSDR 06FDEA1706None · noneFOUND REPAIR LOCATED AT STA 410 STR 15 RT, REPAIR REQUIRES EVALUATION FOR MAJOR / MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR WAS DETERMINED TO BE IAW SRM 53-30-3 FIG 1 BASED ON EXTERNAL VISUAL EVALUATION WITH REPAIR INSMay 5, 2006 · N270FE · Boeing 727200 · Standard Practices/StructuresSDR 06FDEA1707None · noneFOUND REPAIR LOCATED AT STA 203 STR 28R REPAIR REQUIRES EVALUATION FOR MAJOR / MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR WAS DETERMINED TO BE IAW SRM 53-30-3 FIG 1. REPAIR CLASSIFIED AS MAJOR BASED ON GMM 6-2-100 CRITMay 5, 2006 · N270FE · Boeing 727200 · Standard Practices/StructuresSDR 06FDEA1708None · noneFOUND REPAIR LOCATED AT STA 1050 STR 29L REPAIR REQUIRES EVALUATION FOR MAJOR / MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR WAS DETERMINED TO BE IAW SRM 53-30-3 FIG 2, REPAIR CLASSIFIED AS MAJOR BASED ON GMM 6-2-100 May 5, 2006 · N270FE · Boeing 727200 · Standard Practices/StructuresSDR 06FDEA1705None · noneFOUND REPAIR LOCATED ON AFT CARGO DOOR REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR DETERMINED TO BE IAW SRM 52-00-3 FIG 3 BASED ON EXTERNAL VISUAL EVALUATION WITH REPAIR INSTALLMay 4, 2006 · N270FE · Boeing 727233 · Standard Practices/StructuresSDR 05FDEA00089Control Unit · contaminatedCARGO SMOKE IN LOWER, FORWARD CARGO COMPARTMENT. DISCHARGED NR 1 BOTTLE. CARGO SMOKE ON FRONT PANEL AND S/O'S PANEL ILLUMINATED FOR APPROXIMATELY 2 SECONDS. REMOVED AND REPLACED NR 1 LOWER CARGO COMPMENT FIRE BOTTLE, TESTS GOOD. FOUND LOWER CARGO COMPMENT Jan 13, 2005 · N270FE · Boeing 727200 · Fire DetectionSDR 04FDEA01706Control Unit · failedDISCHARGED BOTH LOWER CARGO COMPT FIRE BOTTLES, INDICATION OF FWD LOWER CARGO FIRE. AFTER CHECKING COMPARTMENT AND WHILE BEING TOWED HAD ANOTHER ACTIVATION OF LOWER CARGO FIRE WARNING. REMOVED AND REPLACED LWR FWD CARGO COMPT FIRE SUPP/SMOKE DET CONTROL ELECJun 13, 2004 · N270FE · Boeing 727200 · Fire DetectionSDR 04FDEA01696Control Unit · malfunctionedFORWARD LOWER CARGO COMPARTMENT FIRE INDICATION ON TAXI OUT. NO ACTUAL FIRE REPORTED BY FIRE DEPARTMENT AFTER FIRE BOTTLES DISCHARGED INTO FWD LOWER CARGO COMPARTMENT. REMOVED AND REPLACED BOTH NR 1 AND NR 2 FIRE BOTTLES AND THE CARTRIDGES PER MM 26-17-014-Jun 11, 2004 · N270FE · Boeing 727200 · Fire DetectionSDR 04FDEA00379Warning Horn · false activationLOWER CARGO SMOKE WARNING BELL ACTIVATED TWICE AT ALTITUDE FOR 1-2 SECONDS. WARNING LIGHTS AND HORN WENT OUT IMMEDIATELY WITHOUT ACTIVATING THE DISCHARGE BUTTON. BEGAN IMMEDIATE DESCENT INTO YMX. WARNING CAME ON CONTINUOUS AT 500 FT, PUSH BOTTLE DISCHARGE BFeb 7, 2004 · N270FE · Boeing 727200 · Fire DetectionSDR 03FDEA01906Attach Angle · corrodedWHILE WORKING NRC N01585 FOUND CORROSION AT STA 950 10 RBL 11 TO 50 WL 148, RT MLG BANANA FAIRING ATTACH ANGLE. CORROSION AT BS 950 10, RBL 11 TO 50, WL 148 FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE, FABRICATED REPAIR ANGLES AND FILLERS AND INSTALLED FOR RT Nov 12, 2003 · N270FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 03FDEA01905Frame · gougedGOUGE ON BS 540 FRAME, I/B FLANGE, ONE INCH ABOVE STR 22L. BLENDED GOUGE AREA ON FRAME AT BS 540 ABOVE STR 22L, 1 X 1 X .008 INCH ORIGINAL THICKNESS .045 INCH. FOUND TO BE OUT OF LIMITS PER SRM 53-10-1 PG 1 FIG 1, DETAIL I. REMOVED AND REPLACED LOWER LEFT FNov 11, 2003 · N270FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA01903Keelbeam · corrodedCORRODED KEEL BEAM STR 29L, O/B FLANGE BS 950D - 1004. CORROSION ON KEEL BEAM STR 29L O/B FLANGE BS 950D-1004 REPAIRED PER EA 7-5310- 55109 & SR 27-53-023A.Nov 11, 2003 · N270FE · Boeing 727200 · Fuselage Main, KeelSDR 03FDEA01902Spar · chafedVERTICAL STAB STRINGER 7 CHAFED UNDER AFT CORNER OF ACCESS PANEL 9601. REPAIRED DAMAGE TO LT VERTICAL FIN MID SPAR AT FIN STA 229 PER SRM 55-30-06 FIGURE 3.Nov 11, 2003 · N270FE · Boeing 727200 · Vertical Stabilizer, Spar/RibSDR 03FDEA01904Floorbeam · corrodedCORROSION (C53-224-04) BS 1130 FLOORBEAM UPPER CHORD AROUND HOLES AND UNDER NUT PLATES, LBL 48, WL 208.Nov 11, 2003 · N270FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 03FDEA01899Hinge · corrodedCORROSION ON FASTENERS ALONG UPPER LT GEAR BODY DOOR HINGE AREA ENTIRE LENGTH. *S/D* CORROSION ALONG UPPER LT GEAR BODY DOOR HINGE AREA ENTIRE LENGTH. ORIG THICKNESS .020. LOWEST READING .078, FOUND TO BE IN LIMITS IAW SRM 53-10-1.Nov 10, 2003 · N270FE · Boeing 727200 · Landing Gear DoorsSDR 03FDEA01898Frame · dentedFWD LWR CARGO FRAME IS DENTED AT STA 600, STR 24L. REMOVED AND REPLACED DAMAGED FRAME SECTION BS 600, STR 21L TO STR 25L PER SRM 51-30-2.Nov 10, 2003 · N270FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA01886Failsafe · crackedCRACKED FAILSAFE CHORD, BS 804 AT STR 14L.Nov 7, 2003 · N270FE · Boeing 727200 · Fuselage Main, StructureSDR 03FDEA01887Floorbeam · corrodedWHILE WORKING CARD N01482, FOUND CORROSION ON FLOORBEAM, STA 328 LBL 23 WL 208.Nov 7, 2003 · N270FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 03FDEA01888Floorbeam · corrodedWHILE DRILLING UP NEW SEAT TRACK AT BS 1050 LBL 25 DRILLED THROUGH RADIUS OF FLOORBEAM REPAIR ANGLE.Nov 7, 2003 · N270FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 03FDEA01876Frame · corrodedCORROSION FOUND ON FORWARD SIDE OF 950E FRAME AT STRINGER 29 LT. REPAIRED PER B727 SRM 53-10-4 FIG 15.Nov 5, 2003 · N270FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA01871Floorbeam · corrodedWHILE WORKING CARD NR N01362, FOUND CORROSION ON FLOORBEAM STA 312, RBL 14, WL 208. FLOORBEAM AT BS 312 WAS OUT OF LIMITS. REMOVED DAMAGED BEAM & REPAIRED. INSTALLED NEW SECTION PER SRM 53-10-8 FROM RBL 14 TO LBL 65.Nov 5, 2003 · N270FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 03FDEA01873Frame · dentedFWD LWR CARGO FRAME IS DENTED AT STA 660 STR 22L. FWD LOWER CARGO FRAME IS DENTED AT STR 22L AT BS 660. FOUND TO BE OUT OF LIMITS PER SRM5 3-10-1. REPAIRED DAMAGE FRAME PER SRM 51-40-3.Nov 5, 2003 · N270FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA01879Skin · crackedFUSELAGE UPPER LOBE, BS 720B 15.5, STR 15R, CRACKED BS 720B 15.5, STR 16 R/H CRACK FOUND TO BE OUT OF LIMITS. REPAIR DAMAGE STR. 15 RT PER SRM 53-10-3.Nov 5, 2003 · N270FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 03FDEA01870Shear Tie · corrodedCORROSION ON FWD CARGO COMPARTMENT SHEAR TIE ON AFT SIDE OF BS 700 FRAME RBL 9 WL 148. REPAIR PER SRM 53-10-4 FIG 13 SHT 1 AT BS 700, RBL 9, WL 148.Nov 5, 2003 · N270FE · Boeing 727200 · Fuselage Main, StructureSDR 03FDEA01880Frame · corrodedCORROSION FOUND ON FORWARD SIDE OF 970 FRAME AT STR 29 LT. OPENNov 5, 2003 · N270FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA01878Skin · bulgedN00148 OUTER EXTERIOR SKIN HAS BULGE AT STA 1050 STR 28L ** SD ** COMINGNov 5, 2003 · N270FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 03FDEA01877Frame · dentedN00509) DENT IN FRAME BS 1050 ABOVE STR 25L ** SD ** COMINGNov 5, 2003 · N270FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA01875Floorbeam · corrodedN01453 CORROSION WHILE WORKING N01449 FOUND CORROSION ON TOP SURFACE OF UPPER CHORD OF FLOORBEAM BS 1070, RBL 23, WL 208 ** SD ** COMINGNov 5, 2003 · N270FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 03FDEA01874Frame · dentedN00817) FWD LWR CARGO FRAME DENTED AT STA 520 STR 22L TO 25L ** SD ** COMINGNov 5, 2003 · N270FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA01872Floorbeam · corrodedN01482 CORROSION WHILE WORKING CARD NO N00939, FOUND CORROSION ON FLOORBEAM, STA 344 RBL 13-53 WL 208. ** SD ** COMINGNov 5, 2003 · N270FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 03FDEA01863Stringer · crackedFUSELAGE UPPER LOBE, BS 720B 4.5, STR 15R, CRACKED. REMOVED DAMAGED SECTION OF STRINGER 15R, BS 720B 4.5 AND REPAIRED STRINGER PER SRM 53-10-3 FIG 5.Nov 3, 2003 · N270FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 03FDEA01865Stringer Clip · crackedCRACKED STR CLIP BS 950C STR 5R. REMOVED AND REPLACED CRACKED STRINGER CLIP BS 950C, STRINGER 5R PER SRM 51-30-2. LOCATED AND DRILLED HOLES PER SRM 51-30-5.Nov 3, 2003 · N270FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 03FDEA01859Keelbeam · corrodedCORROSION ON LOWER CROSS BRACE INSIDE DELTA KEELBEAM, BS 762, WL 148. REMOVED CORROSION ON LOWER CROSS BRACE INSIDE DELTA KEELBEAM BS 762, WL 148. FABRICATED NEW L-ANGLE AND REPLACED CORRODED PART WITH NEW PART PER 727 SRM 53-30-2, 51-40-2, 51-10-2, 51-Nov 3, 2003 · N270FE · Boeing 727200 · Fuselage Main, KeelSDR 03FDEA01857Frame · dentedFWD LWR CARGO FRAME IS DENTED AT STA 560 STR 24 LT. REMOVED DAMAGE AREA AT FRAME IN AREA 1 X 2, AT BS 560, STR 24 LT. FABRICATE THE DOUBLER MADE FROM 7075-T6 0.063, AND INSTALLED REPAIR DOUBLER IAW SRM 51-40-3.Nov 3, 2003 · N270FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA01858Frame · dentedFORWARD LOWER CARGO FRAME IS DENTED AT STA 580 STR 24L. REMOVED DAMAGE AT FRAME IN AREA OF 1 X 3 INCHES AT BS 580, STR 24L. FABRICATE THE DOUBLER MADE FROM 7075-T6 0.063 AND INSTALLED THE REPAIR DOUBLER IAW SRM 51-40-3.Nov 3, 2003 · N270FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA01860Shear Tie · corrodedCORROSION (C53-111-01, 2) FWD CARGO COMPARTMENT SHEAR TIE ON AT SIDE OF BS 700 FRAME LBL 9 WL 148.Nov 3, 2003 · N270FE · Boeing 727200 · Fuselage Main, StructureSDR 03FDEA01861Floorbeam · corrodedCORROSION AROUND SEVERAL NUT PLATE HOLES IN LONGITUDINAL FLOORBEAM, LBL 25, WL 208, BS 760 - 850.Nov 3, 2003 · N270FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 03FDEA01862Floorbeam · corrodedCORROSION BS 400 FLOORBEAM TOP CHORD CORRODED, LBL 6 TO LBL 10, WL 208.Nov 3, 2003 · N270FE · Boeing 727200 · Fuselage Main, Floor Beam
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