N279FE, cancelled Mar 19, 2013

Service difficulty reports · 56

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 = 'N279FE' AND deregistration_id = 'N279FE-2013-03-19'
  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 FDEA200902230670Structure · crackedRT WING INBD MID FLAP REAR CHORD CRACKED AT 2ND CUTOUT FROM INBD WBL 96. REMOVED MID FLAP LWR SKIN FOR ACCESS, REMOVED DAMAGED EXTRUDED SECTION. FABRICATED NEW EXTRUDED SECTION USING 7075T-6 PO NR 8306161 DIMS 48 INCH LONG AND INSTALLED NEW EXTRUDED SECTION,Feb 23, 2009 · N279FE · Boeing 727233 · Trailing Edge FlapsSDR FDEA200902120511Intercostal · damagedMCD INNER CENTER BEAM HAS MISDRILLED HOLE AND GOUGED INTO INTERCOSTAL REMOVED DAMAGE INTERCOSTAL IAW SRM 51-30-2, FABRICATED NEW INTERCOSTAL IAW HAYES INTERNATIONAL CORP DRAWING NR 52FX518 REV A, HEAT TREATED PART IAW FAS ENGINEERING REPORT NR 2-37153-801 REV Feb 12, 2009 · N279FE · Boeing 727233 · Cargo/Baggage DoorsSDR FDEA200902060476Skin · crackedTWO CRACKS ON FWD ENTRY DOOR HINGE CUT OUT BODY SKIN EDGE RADII, LOWER HINGE. REPAIRED CRACKS IAW EO 7-5330-7-2345F PART 2.Feb 6, 2009 · N279FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA200901310407Skin · crackedRIGHT WING NR 8 SLAT OTBD TRACK SKIN IS CRACKED. STOP DRILLED CRACK IAW DRAWING SR27-57-034 REV A AND SRM 51-10-1. FABRICATED REPAIR DOUBLER FROM 2024-T3 0.071 DIM 9 1/2" BY 6" IAW DRAWING SR27-57-034 REV A. INSTALLED DOUBLER IAW DRAWING SR27-57-034 REV A AJan 31, 2009 · N279FE · Boeing 727233 · Leading Edge DevicesSDR FDEA200901290389Structure · corrodedPOSSIBLE CORROSION AT DOG HOUSE LOWER LEFT CHORD STA 312 UNDER LEVELING COMPOUND. REMOVED LEVELING COMPOUND AND CORROSION FROM AREA IAW SRM 51-10-6 AND SOPM 20-30-03, FOUND CHORD OUT OF LIMITS IAW SRM 53-10-1 FIG 1, REMOVED AND REPLACED CHORD IAW SRM 51-30-Jan 29, 2009 · N279FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR FDEA200901290386Angle · crackedRIGHT WING LOWER CHORD ANGLE CRACKED AT NR 8 SPOILER FITTING.Jan 29, 2009 · N279FE · Boeing 727233 · Wing, Attach FittingsSDR FDEA200901290385Angle · crackedLEFT WING LOWER CHORD ANGLE CRACKED AT NR 7 SPOILER FITTING.Jan 29, 2009 · N279FE · Boeing 727233 · Wing Miscellaneous StructureSDR FDEA200901290384Skin · canningC1 DOOR LOWER AFT SKIN IS OIL CANNED. CUT OUT DAMAGED AREA IAW 52-00-03 FIG 3. FABRICATED DOUBLER REPAIR IAW SRM 52-00-03 FIG 3 AND 52-30-01 FIG. 7. INSTALLED REPAIR DOUBLER IAW SRM 51-30-2.Jan 29, 2009 · N279FE · Boeing 727233 · Cargo/Baggage DoorsSDR FDEA200901290383Structure · crackedCRACK ON LEFT INBD MID FLAP CHORD AT WBL 114. CUT OUT DAMAGED AREA IAW SRM 51-40-3 FIG 1. FABRICATED LOWER SECTION USING EXTRUSION AND SPLICE IAW SRM 51-40-3 FIG 1 AND 57-50-2 FIG 5. INSTALLED REPAIR PARTS IAW SRM 51-30-2.Jan 29, 2009 · N279FE · Boeing 727233 · Trailing Edge FlapsSDR FDEA200901290382Frame · gougedFWD PIT FRAME AT BS 520 STRINGER 22L IS GOUGED AT RADIUS. CUT OUT DAMAGED IAW SRM 51-40-3 FIG. 1. FABRICATED REPAIR DOUBLER, STRUCTURAL FILLER, AND 1 FILLER IAW SRM 53-10-2 FIG. 3 AND 51-40-3 FIG. 1. HEAT TREATED PART FROM 7075-O TO 7075-T6 IAW FAS ENGINEERINJan 29, 2009 · N279FE · Boeing 727233 · Fuselage Main, FrameSDR FDEA200901290380Skin · gougedRIGHT WING INBD FORE FLAP IS GOUGED AT OTBD LEADING EDGE IN TWO PLACES. REMOVED PREVIOUS REPAIR IAW SRM 51-30-2. FABRICATED NEW REPAIR PARTS IAW SRM 57-50-2 FIG 3 AND 57-50-4 FIG 1. INSTALLED NEW REPAIR IAW SRM 51-30-2.Jan 29, 2009 · N279FE · Boeing 727233 · Trailing Edge FlapsSDR FDEA200901280343Angle · crackedLEFT WING LOWER CHORD ANGLE CRACKED AT NR 7 SPOILER FITTING. REMOVED AND DISCARDED DOUBLER IAW FEDEX DRAWING SR27-57-038 REV C. TRIMMED WEB AND LOWER CHORD IAW FEDEX DRAWING SR27-57-038 REVC. FABRICATED NEW WEB FROM 7075-T6 0.032 DIM. 12 1/8" BY 9 1/2". Jan 28, 2009 · N279FE · Boeing 727233 · SpoilersSDR FDEA200901280347Frame · crackedNR 1 ENGINE NOSE COWL AFT EDGE IS CRACKED AND SECTION TORN AT 4 O'CLOCK POSITION BS 1200 CUT OUT DAMAGED AREA IAW SRM 51-10-1. FABRICATED REPAIR PARTS AND 1 FILLER IAW SRM 54-10-2 FIG 1 AND 54-10-3 FIG 3. INSTALLED REPAIR PARTS IAW SRM 51-30-2.Jan 28, 2009 · N279FE · Boeing 727233 · Nacelle/Pylon, Main FrameSDR FDEA200901280344Skin · damagedLEFT AFT EMERGENCY EXIT HATCH HAS DEEP SCRATCH ON OUTER SKIN. CUT OUT DAMAGED AREA IAW SRM 52-00-03 FIG 3. FABRICATED REPAIR DOUBLER IAW SRM 52-00-03 FIG 3 AND 52-20-01 FIG 1. INSTALLED REPAIR DOUBLER IAW SRM 51-30-2.Jan 28, 2009 · N279FE · Boeing 727233 · Emergency ExitsSDR FDEA200901280342Angle · crackedRIGHT WING LOWER CHORD ANGLE CRACKED AT NR 8 SPOILER FITTING. REMOVED AND DISCARDED DOUBLER IAW DRAWING SR27-57-038 REV C. TRIMMED WEB AND LOWER CHORD IAW DRAWING SR27-57-038 REV C. FABRICATED NEW INBD WEB, FABRICATED NEW INBD LOWER CHORD, FABRICATED NEW STJan 28, 2009 · N279FE · Boeing 727233 · Wing Miscellaneous StructureSDR FDEA200901280345Skin · damagedRIGHT FWD EMERGENCY EXIT HATCH OUTER SKIN HAS DEEP SCRATCH. CUT OUT DAMAGED AREA DIM 4 1/4 BY 1 1/4 INCH IAW B727 SRM 52-00-03 FIG 3. FABRICATED DOUBLER REPAIR MAT USED 2024-T3 0.080" PO NR 9008077 DIM 11 1/8 BY 7" IAW B727 SRM 52-00-03 FIG 3 AND 52-20-01 Jan 28, 2009 · N279FE · Boeing 727233 · Emergency ExitsSDR FDEA200901090107Actuator · failedAFTER TAKEOFF WHILE RAISING FLAPS NR 1 LEADING EDGE DEVICE REMAINED EXTENDED AT 2 DEG AND 0 DEG FLAP SETTING. RAN QRH PROBLEM REMAINED. RETURNED TO BASE FOR NORMAL LANDING. LEADING EDGE DEVICE RETRACTED ON SCHEDULE AFTER LANDING CLEAN UP. VISUAL INSPECTION Jan 9, 2009 · N279FE · Boeing 727233 · Leading Edge Slat ActuatorSDR FDEA200901080103Actuator · failedAFTER TAKEOFF WHILE RAISING FLAPS NR 1 LEADING EDGE DEVICE REMAINED EXTENDED AT 2 DEG AND 0 DEG FLAP SETTING. RAN QRH PROBLEM REMAINED. RETURNED TO BASE FOR NORMAL LANDING. LED RETRACTED ON SCHEDULE AFTER LANDING CLEAN UP. VISUAL INSPECTION OF NR 1 LEADINGJan 8, 2009 · N279FE · Boeing 727233 · Leading Edge Slat ActuatorSDR 07FDEA01502Connector · damagedNR 1 ENG FIRE DETECTION A LOOP INOP. MEL 03APR07 00:03 YOW ACN RELEASED FOR SERVICE PER MEL/CDL: 26-06-B. REMOVABLE ON P6 AREA, APU START PANEL, L/E ANNUNC. PANEL, GEN. FAULT ANNUNC. PANEL. REMOVED RELAY R730, DEPINNED PIN 9 FROM D5220J, DEPINNED PINS 6Apr 12, 2007 · N279FE · Boeing 727200 · Detection SystemSDR 06FDEA03463Switch · stickingDURING GEAR EXTENSION NOSE GEAR DOOR WARNING LIGHT ILLUMINATED AFTER EXTENSION WITH DOOR LIGHT ON S/O PANEL. LIGHT WENT OUT AFTER 2 MINUTES. INSPECTED SWITCH ASSY ON NOSE WHEEL GEAR DOOR SWITCH. FOUND PLUNGERS STICKING. CLEANED AND LUBED SWITCH. OPS CHECSep 27, 2006 · N279FE · Boeing 727233 · Landing Gear Position and WarningSDR FDEA200607212648Warning Light · illuminatedMAIN CARGO DOOR "B" LT ILLUMINATED IN FLIGHT, FL250 WITH VENT DOOR WARNING LT IN GALLEY AREA ILLUMINATED.Jul 21, 2006 · N279FE · Boeing 727233 · Door Warning SystemSDR 06FDEA2648Warning Light · illuminatedMAIN CARGO DOOR "B" LT ILLUMINATED IN FLIGHT, FL250 WITH VENT DOOR WARNING LT IN GALLEY AREA ILLUMINATED.Jul 21, 2006 · N279FE · Boeing 727233 · Door Warning SystemSDR 06FDEA1420Fitting · looseNR 1 ENGINE FAILED TO MAKE STANDARD EPR ON TAKEOFF ROLL TARGET EPR 2.08, MADE ONLY 1.8 WITH THRUST LEVER AT FORWARD STOP. ENGINE WAS VERY SLOW TO ACCELERATE. NO OTHER PARAMETERS EXCEEDED. RUNWAY 27, WEATHER: 190/4KTS, 1ONM VIS, TEMP19*C, DEW POINT 11*C, 30.Apr 12, 2006 · N279FE · Boeing 727233 · Engine (Turbine/Turboprop)SDR 04FDEA01001Web · corrodedCENTER WEB AND CHORD IS CORRODED UNDER FLOOR PANEL AT BS 1176 FWD OF AFT AIR STAIRWAY IN MAIN CARGO COMPT. REMOVED AND REPLACED WEB AND CHORD IAW SRM 51-30-2 AT MAE.Apr 17, 2004 · N279FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 04FDEA001000Bracket · crackedNR 8 SPOILER INBOARD STOP BRACKET LWR MOUNTING CRACKED. REMOVED AND REPLACED STOP BRACKET IAW SRM 51-30-2 AT MAE.Apr 17, 2004 · N279FE · Boeing 727200 · SpoilersSDR 04FDEA001001Floor Panel · corrodedCENTER WEB AND CHORD IS CORRODED UNDER FLOOR PANEL AT BS 1176 FWD OF AFT AIR STAIRWAY IN MAIN CARGO COMPT. REMOVED AND REPLACED WEB AND CHORD IAW SRM 51-30-2 AT MAE.Apr 17, 2004 · N279FE · Boeing 727200 · Fuselage Floor PanelSDR 04FDEA00849Duct · crackedCOMPLY WITH EA 7-7254-77153 ENGINE - FAN EXHAUST OUTER DUCT NR 6 OIL SUPPLY TUBE EGRESS BOSS WELD REPAIR. COMPLIED WITH EA 7-7254-77153 ENGINE - FAN EXHAUST OUTER DUCT NR 6 OIL SUPPLY TUBE EGRESS BOSS WELD REPAIR AT MAE.Apr 7, 2004 · N279FE · Boeing 727200 · Engine Exhaust SystemSDR 02FDEA00755Door Seal · defectiveON APPROACH TO CID-EXTENDED LAND GEAR, NOSE DOOR AMBER LT ON S/O PANEL & RED DOORS LIGHT ON. ELECTED TO DO MISS APPROACH & RECYCLE GEAR. LT WENT OUT. ON RE-EXTENSION RED GEAR DOOR LT WENT OUT. BELOW 200 KTS ON RECYCLE. CHECKED QRH. NO OTHER PROBLEM. FOUOct 23, 2002 · N279FE · Boeing 727200 · Landing Gear DoorsSDR 02FDEA00201Wire · chafedHYD A-SYS OVERHEAT LIGHT CAME ON. BOTH PUMPS WERE OFF PER CK LIST. REPEAT WRITEUP. REMOVED AND REPLACED CHAFED WIRE WITH TEFLON TAPE PER CHAPTER 20 STANDARD PRACTICES.Mar 14, 2002 · N279FE · Boeing 727233 · Hydraulic Power System WiringSDR 01FDEA00965Floorbeam · corrodedCORROSION (C53-224-01, 1) ON TOP OF FLOORBEAM AT FASTENER HOLES BS 312, LBL 3 TO LBL 50, WL 208. REMOVED AND REPLACED FLOORBEAM PER SRM 53-10-8, FIG 9.Nov 6, 2001 · N279FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 01FDEA00959Beam · chafedLT HORIZ STAB LOWER TRAILING EDGE BEAM HAS CHAFE DAMAGE AND MISSING SPACER.Nov 3, 2001 · N279FE · Boeing 727233 · Horizontal Stabilizer StructureSDR 01FDEA00952Floorbeam · corrodedCORROSION (C53-224-01) ON TOP OF FLOORBEAM BS 344, RBL 3 - LBL 31, WL 208. REMOVED AND REPLACED FLOORBEAM PER SRM 51-10-6.Nov 2, 2001 · N279FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 01FDEA00935Stringer · damagedSTRINGER 27L EDGE DAMAGE BS 480, WL 149. REMOVED AND REPLACED STRINGER PER EA 7-5310-59896.Oct 29, 2001 · N279FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR 01FDEA00932Floorbeam · corrodedCORROSION ON FLOORBEAM BS 1070, LBL 45, WL 208. REMOVED AND REPLACED FLOORBEAM PER SRM 53-10-8 FIG 3.Oct 26, 2001 · N279FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 01FDEA00921Beam · chafedLEFT HORIZ STAB LOWER TRAILING EDGE BEAM HAS CHAFE DAMAGE AND MISSING SPACER BLOCK AT THE 3RD RUB PAD FROM O/B END. REMOVED AND REPLACED BEAM PER EA 7-5510-60563.Oct 26, 2001 · N279FE · Boeing 727233 · Horizontal Stabilizer StructureSDR 01FDEA00927Floorbeam · corrodedCORROSION (C53-224-01, 2) ON LWR CHORD OF FLOORBEAM, BS 1110, RBL 41, WL 200. REMOVED AND REPLACED CORROSION PER EA 7-5310-59897.Oct 26, 2001 · N279FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 01FDEA00922Floorbeam · corrodedCORROSION C53-224-01,1 ON TOP CHORD OF BS 720A FLOORBEAM RBL 7 OUT OF LIMITS. REMOVED AND REPLACED FLOORBEAM PER EA 7-5310-60567.Oct 26, 2001 · N279FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 01FDEA00958Floorbeam · corrodedCORROSION ON FLOORBEAM BS 1970, LBL 45, WL 208.Oct 26, 2001 · N279FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 01FDEA00928Skin · dentedEMPENNAGE SKIN DENT AT BS 1338, 38' BELOW VERT STAB LT SIDE. REMOVED AND REPLACED SKIN PER SRM 51-40-2.Oct 26, 2001 · N279FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 01FDEA00929Skin · crackedCRACK IND IN EXTERNAL FUSE SKIN AFT I/B CORNER. REMOVED AND REPLACED SKIN PER DWG SR 27-53-024 & EA.Oct 26, 2001 · N279FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 01FDEA00923Floorbeam · corrodedCORROSION ON UPPER CHORD OF FLOORBEAM BS 1050, RBL 35 AND RBL 55, WL 208. REMOVED AND REPLACED FLOORBEAM PER SRM 53-10-8 & 51-30-2.Oct 26, 2001 · N279FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 01FDEA00925Keelbeam · corrodedCORROSION ON KEEL BEAM AT BS 934, STR 29 RIGHT O/B. REMOVED AND REPLACED BEAM PER DWG SR 27-53-023.Oct 26, 2001 · N279FE · Boeing 727233 · Fuselage Main, KeelSDR 01FDEA00926Frame · dentedFRAME DENTED BS 660 JUST ABOVE STR 24L. REMOVED AND REPLACED FRAME PER SRM 51-40-3.Oct 26, 2001 · N279FE · Boeing 727233 · Fuselage Main, FrameSDR 01FDEA00920Stringer · crackedVERTICAL STAB MAIN BOX INTERIOR STRINGER IS CRACKED AT FIN STA 110.4, STR 9 LT. REMOVED AND REPLACED STRINGER PER SRM 55-30-4 FIG 1 & EA 7-5530-59892.Oct 25, 2001 · N279FE · Boeing 727233 · Vertical Stabilizer, Spar/RibSDR 01FDEA00919Frame · crackedVERTICAL STABILIZER MAIN BOX INTERIOR CHORD IS CRACKED AT FIN BS 157.2, STR 8 LT. REMOVED AND REPLACED CHORD PER SRM 55-30-5 FIG 1 & EA 7-5530-59891.Oct 25, 2001 · N279FE · Boeing 727233 · Vertical StabilizerSDR 01FDEA00918Stringer · crackedVERTICAL STABILIZER MAIN BOX INTERIOR STRINGER IS CRACKED AT FIN BS 157.2, STR 8 RT. REMOVED AND REPLACED STRINGER PER SRM 55-30-4 & EA 7-5530-59891.Oct 25, 2001 · N279FE · Boeing 727233 · Vertical Stabilizer, Spar/RibSDR 01FDEA00916Spar · crackedRIGHT WING I/B MIDFLAP, AFT FLAP CONTROL ROD CUT OUT IN THE LWR SPAR CHORD CRACKED. REMOVED AND REPLACED CHORD PER SRM 51-40-4, 51-30-2.Oct 25, 2001 · N279FE · Boeing 727233 · Wing SparSDR 01FDEA00917Skin · chafedBS 720, STR 19 LT FUSELAGE EXTERNAL SKIN CHAFED. REMOVED AND REPLACED SKIN PER SRM 53-30-3.Oct 25, 2001 · N279FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 01FDEA00956Floorbeam · corrodedCORROSION ON LOWER CHORD OF FLOORBEAM AROUND NUT PLATE HOLES. REMOVED AND REPLACED FLOORBEAM PER EA 7-5310-59894.Oct 21, 2001 · N279FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 01FDEA00801Switch · failed01-299 DUR DEPART #2 L/E DEVICE FAILED TO RETRACT. R&R #2 LED SWITCH PER MM 27-82-001. OPS CK OK.Sep 5, 2001 · N279FE · Boeing 727233 · Leading Edge Slat Control System
Back to N279FE, cancelled Mar 19, 2013