N276FE, cancelled Aug 10, 2015

Service difficulty reports · 60

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 = 'N276FE' AND deregistration_id = 'N276FE-2015-08-10'
  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 FDEA200812295313Shear Tie · corrodedAFT CARGO COMPARTMENT - CORROSION ON SHEAR TIE AT BS 1166 AFT SIDE BETWEEN STRINGERS 29L AND 28L. CORROSION ON SHEAR TIE 100% MATERIAL LOSS & OUT OF LIMITS IAW SRM 53-10-1 FIG 1. REMOVED SHEAR TIE IAW SRM 51-30-2 AND FABRICATED NEW PART IAW SRM 51-20-1 FIGDec 29, 2008 · N276FE · Boeing 727233 · Fuselage Internal Mounting StructureSDR FDEA200812245280Frame · gougedGOUGED FRAME ON STA 580, STR 3L REMOVED FASTENERS IAW SRM 51-30-2, BLENDED OUT DAMAGE AREA IAW SRM 51-10-1. UT AREA IAW NDTM 51-00-00 FIG 2 PT 4. HFEC AREA IAW NDTM 51-00-00 FIG 23 PT 6. NO DEFECTS NOTED. FOUND TO BE OUT OF LIMITS IAW FDX SRM 53-10-1 FIG 1ADec 24, 2008 · N276FE · Boeing 727233 · Fuselage Main, FrameSDR FDEA200812165177Skin · gougedPREVIOUS REPAIR AT BS 312 STR 24R HAS IMPROPERLY INSTALLED FASTENERS, AND FOUND GOUGES, AND TOOLING MARKS. REMOVED PREVIOUS REPAIR AT BS 312 STR 24R IAW SRM 51-30-2. CUT OUT DAMAGED AREA IAW SRM 51-10-1. CUT OUT DIMENSIONS 3.8" X 4.1". FABRICATED REPAIR FILDec 16, 2008 · N276FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA200812165176Sill · corrodedC-2 DOOR SILL CHORD O/B FLANGE CORRODED. REMOVED CORROSION PER B727 SRM 51-10-6 AND PERFORMED UT INSP OF AREA IAW NDTM 51-00-00 FIG 3 PART 4. (ORIG: .220 REMAIN : .170 LOSS: .050). REPORTED FINDINGS TO ENGINEERING AND EA 7-5310-126874 DATED 15 DEC 08 ISSUEDec 16, 2008 · N276FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR FDEA200812125129Skin · crackedSKIN BULGING AND CRACKED STA 1010 STR 27L CUT DAMAGE AREA IAW SRM 53-30-3 , FIG 3A. FABRICATED FILLER AND DOUBLER IAW SRM 53-30-3 FIG 3A. TREATED & PRIMED REPAIR PARTS IAW SRM 51-10-2. INSTALLED REPAIR PARTS IAW SRM 51-30-2.Dec 12, 2008 · N276FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA200812125128Spar · crackedCRACKED CHORD FALSE SPAR UNDER NR 7 SPOILER FITTING. REMOVED LOWER SECTION OF CHORD IAW DRWG SR27-57-038 REV C AND FABRICATED NEW LOWER SECTION, 2 REPAIR ANGLES, 1 REPAIR STRAP, AND WEB IAW DWG SR27-57-038 REV C. TREATED AND PRIMED REPAIR PARTS IAW SRM 51-1Dec 12, 2008 · N276FE · Boeing 727233 · Wing SparSDR FDEA200812125127Spar · crackedFALSE SPAR CHORD CRACKED UNDER NR 8 SPOILER . TRIMMED INBRD WEB SECTION IAW DRAWING SR 27-57-038 REV C. TRIMMED LOWER STRUCTURE IAW DRAWING SR 27-57-038. LOCATED, DRILLED, DEBURRED LOWER ANGLE IAW 51-30-5 & DWG SR 27-57-038 REV C. FABRICATED 2 EA ANGLES ADec 12, 2008 · N276FE · Boeing 727233 · Wing SparSDR FDEA200809163907Connector · damagedLT GEAR (RED AND GREEN) INDICATOR LIGHTS ILLUMINATED IN FLIGHT. ON APPROACH WHEN LANDING GEAR LEVER PLACED DOWN, UNSAFE LIGHT REMAIN ON, RAN QRH AND CHECKED MANUAL MAIN GEAR EXTENSION DOWNLOCKS. FOUND PIN 31 IN PLUG D4658P PUSHED BACK AND LOCK BROKEN. REPLSep 16, 2008 · N276FE · Boeing 727233 · Landing Gear System WiringSDR 08FDEA03907Connector · damagedLEFT GEAR (RED AND GREEN) INDICATOR LIGHTS ILLUMINATED IN FLIGHT. ON APPROACH WHEN LANDING GEAR LEVER PLACED DOWN, UNSAFE LIGHT REMAIN ON. RAN QRH AND CHECKED MANUAL MAIN GEAR EXTENSION DOWNLOCKS. FOUND PIN 31 IN CONNECTOR D4658P PUSHED BACK AND LOCK BROKENSep 16, 2008 · N276FE · Boeing 727233 · Landing Gear System WiringSDR 08FDEA03256Connector · damagedDURING CRUISE AT FL 350 THE RUDDER LOAD LIMITER LIGHT AND BOTH THE RED AND GREEN LEFT GEAR LIGHTS ILLUMINATED AT THE SAME TIME. DURING THE DESCENT THE RED AND GREEN LEFT GEAR LIGHTS ILLUMINATED INTERMITTENTLY WHILE THE RUDDER LOAD LIMITER REMAINED ILLUMINATAug 5, 2008 · N276FE · Boeing 727233 · Landing Gear System WiringSDR 08FDEA00870Controller · unknownCLIMBING OUT OF LAX, PRESSURE CONTROLLER INDICATED -100 FPM (DESCENT) UNTIL 8000'MSL. F/O COMPLAINED OF PAIN IN EARS/TEETH ALMOST IMMEDIATELY. CAPTS EARS ALSO PAINFUL. AT 8000' CABIN BEGAN TO CLIMB PASSING 12000, F/O STILL UNCOMFORTABLE. DIRECTED S/O TO SWITCMar 11, 2008 · N276FE · Boeing 727233 · Cabin Pressure ControllerSDR 06FDEA2144Repair · misinstalledFOUND PREVIOUSLY REPAIR INSTALLED AT STA 188 BELOW STR 24L IS NOT CONFORMED TO FAA APPROVED DATA. REMOVED EXISTING REPAIR, FABRICATED REPAIR DOUBLER IAW SRM 53-30-3 FIG 3 AND REINSTALLED REPAIR PARTS PER SRM 51-10-2 AND MM 51-20-151-7. REPAIR IS CLASSIFIED AMay 31, 2006 · N276FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 06FDEA2143Repair · improperFOUND PREVIOUSLY REPAIR LOCATED AT STA 990 STR 24R IS NOT CONFORMED TO FAA APPROVED DATA. REMOVED EXISTING REPAIR, FABRICATED REPAIR PART DOUBLER IAW SRM 53-30-3 FIG 1. INSTALLED REPAIR DOUBLER IAW SRM 53-30-3 FIG 1 AND SRM 51-30-2. REPAIR IS CLASSIFIED AS May 31, 2006 · N276FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 06FDEA2095Skin · misrepairedFOUND PREVIOUSLY REPAIR LOCATED AT NR 3 CARGO DOOR EXTERNAL SKIN UPPER AFT EDGE IS NOT CONFORMED TO FAA APPROVED DATA. REMOVED EXISTING REPAIR, FABRICATED REPAIR PARTS IAW SRM 52-00-3 FIG 3. INSTALLED REPAIR PART IAW SRM 52-00-3, FIG 3. REPAIR IS CLASSIFIEDMay 31, 2006 · N276FE · Boeing 727233 · Cargo/Baggage DoorsSDR 06FDEA2081None · noneFOUND PREVIOUSLY REPAIR INSTALLED FROM STA 970-990, STR 29R WAS DETERMINED TO BE ACCOMPLISHED PER BOEING SB 727-53-0179, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SIZE, SHAPE, MATERIAL TYPE AND THICKNESS, FASTENERS SPACING AND NUMBERS, GENEMay 30, 2006 · N276FE · Boeing 727233 · Standard Practices/StructuresSDR 06FDEA2080None · noneFOUND PREVIOUSLY REPAIR INSTALLED AT STA 950D, STR 18R WAS DETERMINED TO BE ACCOMPLISHED IAW FEDEX EA 5310-57265, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER SPACING AND NUMBERS, GENERAL WORKMay 30, 2006 · N276FE · Boeing 727233 · Standard Practices/StructuresSDR 06FDEA2079None · noneFOUND PREVIOUSLY REPAIR INSTALLED BETWEEN STA 950-950C, STR 29L WAS DETERMINED TO BE ACCOMPLISHED IAW FEDEX EA 5380-55160, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENERS SPACING AND NUMBERS, GEMay 30, 2006 · N276FE · Boeing 727233 · Standard Practices/StructuresSDR 06FDEA2078None · noneFOUND PREVIOUSLY REPAIR DOUBLER/TRIPLER INSTALLED AT STA 1090 FWD LOWER SIDE OF AFT CARGO DOOR CUT OUT WAS DETERMINED TO BE ACCOMPLISHED IAW EA 7-5330-55172 BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SIZE, SHAPE, MATERIAL TYPE AND THICKNESS,May 30, 2006 · N276FE · Boeing 727233 · Standard Practices/StructuresSDR 06FDEA2077None · noneFOUND PREVIOUSLY REPAIR LOCATED AT STA 178, FWD SIDE OF BULKHEAD, LT BOTTOM WAS DETERMINED TO BE ACCOMPLISHED PER SRM 53-10-9, FIG 3, BASED ON AN EXTERNAL EVALUATION, CONSIST OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER SPACING AND NUMBERS,May 30, 2006 · N276FE · Boeing 727233 · Standard Practices/StructuresSDR 06FDEA2076None · noneFOUND PREVIOUSLY REPAIR INSTALLED AT STA 196.5, STR 24R WAS DETERMINED TO BE ACCOMPLISHED IAW SRM 53-30-3 FIG. 6, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER SPACING AND NUMBERS AND GENERAL WMay 30, 2006 · N276FE · Boeing 727233 · Standard Practices/StructuresSDR 04FDEA01392Position Switch · failedNR 1 L/E FLAP FAILED TO RETRACT AFTER T/O. FOLLOWED RED TABS AND RETURNED TO LAND. REMOVED AND REPLACED NR 1 L/E FLAP POSITION SWITCH PER MM 27-82-001-4. OPS CHECK GOOD PER MM. ACFT OK FOR SERVICE.May 21, 2004 · N276FE · Boeing 727200 · Leading Edge Slat Position Indicating SystemSDR 03FDEA02150Skin · gougedLOWER FUSELAGE, BS 1090, 1 INCH ABOVE AND 4 INCHES BELOW STR 24 RT, EXTERNAL SKIN IS DENTED, GOUGED AND POSSIBLY CRACKED. DAMAGE ON SKIN FOUND TO BE OUT OF LIMITS. REPAIRED SKIN IAW FED-EX EA 7-5330-55172.Dec 9, 2003 · N276FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 03FDEA02157Fuel Tank · corrodedFOUND CORROSION ON UPPER SURFACE OF WING CENTER TANK BS 825 RBL 12. REMOVED CORROSION ON UPPER SURFACE OF WING CENTER TANK AT BS 825, RBL 12 PER SRM 51-10-06. FOUND DAMAGE AREA TO BE OUT OF LIMITS PER SRM 53-10-1, FIG 1. REMOVED DAMAGE AND REPAIRED PER SDec 9, 2003 · N276FE · Boeing 727200 · Fuel StorageSDR 03FDEA02149Frame · crackedCRACKED FRAME AT BS 640, RBL 9, WL 155.5. CUT OUT CRACK ON FRAME AT BS 640, RBL 9, WL 155.5. REMOVED 2 X 2 INCHES. FABRICATED REPAIR PARTS FROM 7075-T6 .063 LOT 516678. ALODINED, PRIMED AND INSTALLED IAW SRM 51-30- 2, 53-10-1, 51-40-3.Dec 9, 2003 · N276FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA02127Keelbeam · corrodedCORROSION AFT CARGO BAY LEFT KEELBEAM LWR O/B FLANGE BS 1000, STR 29L . FOUND CORRODED KEELBEAM OUT OF LIMITS PER SRM 53-10-1. REMOVED AND REPLACED STR 29L KEELBEAM IAW FED EX EA 7-5330-55160.Dec 8, 2003 · N276FE · Boeing 727200 · Fuselage Main, KeelSDR 03FDEA02039Frame · crackedCRACKED FRAME AT BS 640, RBL 9, WL 155.5. CUT OUT CRACK ON FRAME AT BS 640, RBL 9, WL 155.5. REMOVED 2X2 INCH. FABRICATED REPAIR PARTS FROM 7075-T6 .063 INCH, LOT 516678. ALODINED, PRIMED AND INSTALLED IAW SRM 51-30- 2, 53-10-1, 51-40-3. (CLOSED)Dec 3, 2003 · N276FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA02038Stringer Clip · corrodedCORROSION ON STRINGER CLIP AT BS 540, STR 28L. REMOVED CORROSION ON STRINGER CLIP AT B.S. 54O STR 28L. FOUND OUT OF LIMITS. REPLACED STRINGER CLIP PART 65-45313-6 ALL WORK DONE IAW SRM 51-30-2, SRM 53-10-1, SRM 51-30- 5, SRM 51-30-6.Dec 3, 2003 · N276FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 02FDEA00868Door · missingDURING POST FLIGHT WALK AROUND FOUND HYD SERVICE DOOR MISSING. INSPECTED AREA FOR DAMAGE FROM DOOR COMING OFF. NO DAMAGE FOUND. INSTALLED SERVICEABLE DOOR IAW STANDARD MAINT PRACTICES, OK FOR SERVICE.Nov 21, 2002 · N276FE · Boeing 727200 · Hydraulic Compartment DoorsSDR 01FDEA00527Actuator · failedWHEN RETRACT FLAPS FROM 2 DEG TO 0 NR 7 LED FAILED TO RETRACT. REMOVED AND REPLACED RIGHT WING NR 7 SLAT ACTUATOR PER MM 27-81-032-4. OPS AND LEAK CK GOOD.Jul 10, 2001 · N276FE · Boeing 727233 · Leading Edge Slat ActuatorSDR 01FDEA00436Actuator · faultyIN CRUISE NR 2 FUEL PUMPS ON, ALL CROSS FEEDS OPEN, TANK NR 1 & 3 FUEL PUMP OFF. FUEL STILL BURN TANK TO ENG. *S/D* REMOVED AND REPLACED ACT ASSY PER MM 28-22-011-4, REMOVED AND REPLACED CANNON PLUG D40 REF 727-200 MM CH 20.Jun 13, 2001 · N276FE · Boeing 727233 · Aircraft Fuel Distribution SystemSDR 01FDEA00389Door Frame · dentedNR 3 CARGO DOORWAY FWD FRAME AT BS 1090 IS DENTED WITH A GOUGE IN THE CTR LOCATED BETWEEN NR 1 STOP PAD AND LATCH PLATE. R&R PER FEDEX EA 7-5310-56599, SRM 51-10-2, 51-20-4, 51-30-2.May 25, 2001 · N276FE · Boeing 727233 · Fuselage Main, StructureSDR 01FDEA00388Floorbeam · corroded(C53-111-01) CORROSION ON FASTENER HOLES IN THE FLOORBEAM LWR CHORD BS 1130, RBL 44.5 TO LBL 44.5, WL 200. *S/D* REMOVED AND REPLACED DAMAGED FLOORBEAM PER IAW FEDEX EA 7-5310-57249.May 25, 2001 · N276FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 01FDEA00379Floorbeam · corrodedCORROSION AT FASTENER HOLES ON FLOORBEAM AT BS 344, LBL 60 - RBL 60, WL 208. R&R PER FEDEX DWG 27-53-007 & SRM 51-30-2May 22, 2001 · N276FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 01FDEA00376Frame · dentedFRAME DENTED BS 580 BETWEEN STR 16 - 17R, WL 213. *S/D* Removed and replaced PER FEDEX SRM 51-40-3 FIG 1.May 21, 2001 · N276FE · Boeing 727233 · Fuselage Main, FrameSDR 01FDEA00374Spar · chafedVERTICAL STAB LT STR 7, MID SPAR CHORD IS CHAFED 3 inches IN FRONT OF SLIDING SEAL. *S/D* Removed and replaced PER FEDEX SRM 55-30-6 FIG 3, FEDEX EA 7-5530-54061.May 16, 2001 · N276FE · Boeing 727233 · Vertical Stabilizer, Spar/RibSDR 01FDEA00373Spar · chafedVERTICAL STAB, RT STR 7 MID SPAR CHORD IS CHAFED 3 inches IN FRONT OF SLIDING SEAL. *S/D* Removed and replaced PER FEDEX SRM 55-30-3 FIG 3, FEDEX EA 7-5530-54061.May 16, 2001 · N276FE · Boeing 727233 · Vertical Stabilizer, Spar/RibSDR 01FDEA00375Skin · damagedEXTERNAL FUSELAGE SKIN CREASED BS 1327, STR 17 LT 18 LT. *S/D* REMOVED, REPLACED AND FAB PER IAW FEDEX SRM 53-30-3, 51-30-2, 51-30-5, 51-30-8 & FEDEX MM 51-21-151.May 16, 2001 · N276FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 01FDEA00366Skin · damagedUPON REMOVAL OF FAIRING BRACKET FOR FAIRING 3619 BS 950D, STR 18R FOUND HOLE IN FUSELAGE SKIN ELONGATED. *S/D* removed and replaced per fedex ea 7-5310-57265, srm 51-10-2, 53-10-3, 51-10-2, 51-30-5, 51-30-2.May 15, 2001 · N276FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 01FDEA00354Frame · dentedDENTED FRAME AT BS 580, LBL 47, WL 165 PER FEDEX EA 7-5310-29267. R&R PER FEDEX SRM 51-40-3.May 15, 2001 · N276FE · Boeing 727233 · Fuselage Main, FrameSDR 01FDEA00359Frame · dentedFWD CARGO BAY LT FRAME AT BS 520 HAS TWO DENTS SIDE BY SIDE LBL 38. R&R FRAME PER IAW FEDEX SRM 51-40-3.May 15, 2001 · N276FE · Boeing 727233 · Fuselage Main, FrameSDR 01FDEA00357Frame · dentedDENTED FRAME BS 680, LBL 38, WL 162 PER FEDEX EA 7-5310-29267. R&R PER FEDEX SRM 51-40-3.May 15, 2001 · N276FE · Boeing 727233 · Fuselage Main, FrameSDR 01FDEA00365Stringer · crackedSTR 27L CRACKED AT BS 480 (FWD SIDE OF 480 FRAME). R&R STRINGER PER FEDEX SRM 53-10-3.May 15, 2001 · N276FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR 01FDEA00363Frame · dentedDENTED FRAME AT BS 560, LBL 35, WL 160 PER FEDEX EA 7-5310-29267. R&R PER IAW FEDEX EA 7-5310-29267, SRM 51-40-3.May 15, 2001 · N276FE · Boeing 727233 · Fuselage Main, FrameSDR 01FDEA00360Frame · dentedFWD CARGO BAY LT FRAME AT BS 500, LBL 40 HAS A DENT IN TOP FLANGE. REMOVED AND REPLACED PER FEDEX SRM 51-40-3. ALODINED AND PRIMED PER FEDEX 51-20-151.May 15, 2001 · N276FE · Boeing 727233 · Fuselage Main, FrameSDR 01FDEA00361Frame · dentedDENTED FRAME AT BS 540, LBL 40, WL 164 PER EA 7-5310-29267. REMOVED AND REPLACED PER FEDEX SRM 51-40-3. ALODINED AND PRIMED PER FEDEX 51-20-151.May 15, 2001 · N276FE · Boeing 727233 · Fuselage Main, FrameSDR 01FDEA00362Frame · dentedDENTED FRAME AT BS 560, LBL 47, WL 168 PER EA 7-5310-29267. R&R PER IAW FEDEX EA 7-5310-29267, SRM 51-40-3.May 15, 2001 · N276FE · Boeing 727233 · Fuselage Main, FrameSDR 01FDEA00367Floorbeam · corroded(C53-221-01) AT UPPER SURFACE OF 25-G BEAM BS 270, WL 208, LBL 1-6.May 15, 2001 · N276FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 01FDEA00355Frame · dentedDENTED BS 580, LBL 33, WL 159 PER FEDEX EA 7-5310-29267. R&R PER FEDEX SRM 51-40-3May 15, 2001 · N276FE · Boeing 727233 · Fuselage Main, FrameSDR 01FDEA00356Frame · dentedDENTED FRAME AT BS 600, LBL 33, WL 159. R&R PER FEDEX SRM 51-40-3May 15, 2001 · N276FE · Boeing 727233 · Fuselage Main, FrameSDR 01FDEA00364Floorbeam · corrodedCORROSION ON FLOORBEAM AT FASTENER HOLES BS 560 BETWEEN RBL 25 & LBL 25, WL 208. REMOVED, REPLACED AND FAB PER IAW FEDEX SRM 53-10-1, 53-10-8, 51-10-2, 51-20-4 & 51-30-2.May 15, 2001 · N276FE · Boeing 727233 · Fuselage Main, Floor Beam
Back to N276FE, cancelled Aug 10, 2015