Boeing 727-277

Service difficulty reports · 627

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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 aircraft_model_key = '727277'
  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 VGCA20140624004Fairing · damagedFAIRING ADJACENT TO LEFT PACK COOLING DOOR DAMAGED.Jun 24, 2014 · N251FL · Boeing 727277 · Aerodynamic FairingsSDR FDEA201306151306Unknown · unknownENROUTE, BOTH ALTIMETERS SHOWED LEVEL AT FL350 ATC STATED THE RETURN WAS SHOWING 400' HIGH. TRANSPONDER WAS SELECTED NR 1. PERFORMED TEST ON NR 1 & 2 TRANSPONDERS REF MM 34-54-001-2 NO FAULTS FOUND. PERFORMED SELF TESTS ON ADDU AND CADC REF MM 34-12-001-Jun 15, 2013 · N481FE · Boeing 727277 · Altimeter, Barometric/EncoderSDR VGCA20130528005Support Beam · corrodedCORROSION ON LT MLG BEAM AT NR 4 FLAP TRACK ATTACH POINT AROUND BOLTS.May 28, 2013 · N251FL · Boeing 727277 · Fuselage, Landing Gear Attach FittingsSDR VGCA20130528004Support Beam · corrodedCORROSION ON BOTTOM SIDE OF RT MLG SUPPORT BEAM AT NR 5 FLAP TRACK ATTACH POINT.May 28, 2013 · N251FL · Boeing 727277 · Fuselage, Landing Gear Attach FittingsSDR VGCA20130528003Support Fitting · corrodedCORROSION ON LT WING FUSELAGE TERMINAL FITTING.May 28, 2013 · N251FL · Boeing 727277 · Fuselage Miscellaneous StructureSDR VGCA20130528002Fuel Tank · corrodedRIGHT SIDE AFT UPPER SURFACE OF FUEL TANK AT FS 850 CORRODED.May 28, 2013 · N251FL · Boeing 727277 · Fuel StorageSDR VGCA20130528001Support Fitting · corrodedCORROSION ON LT WING FUELAGE TERMINAL FITTING.May 28, 2013 · N251FL · Boeing 727277 · Fuselage Miscellaneous StructureSDR VGCA20121010Skin · damagedUPPER FUSELAGE SKIN DAMAGED.Oct 10, 2012 · N251FL · Boeing 727277 · Fuselage Main, Plate/SkinSDR VGCA20120207Door Frame · crackedTHREE INCH CRACK FOUND ON NR 3 CARGO DOOR FWD FRAME AT S-26R ON FRAME 1090 WHILE COMPLYING WITH AD2006-13-01/SB 53A0169.Feb 7, 2012 · N251FL · Boeing 727277 · Fuselage Main, StructureSDR FDEA201108173307Light · inoperativeFLIGHT DECK EMERGENCY EXIT LIGHT INOPERATIVE. R & R FLIGHT DECK EMERGENCY EXIT LIGHT REF MM 33-50-101-2-0. OPS CHECKED NORMAL.Aug 17, 2011 · N244FE · Boeing 727277 · Emergency LightingSDR FDEA201107303035Flex Hose · leakingAT ABOUT 60-70 KNOTS ON TAKEOFF ROLL S/O CALLED A-SYS HYD QTY WAS ZERO. REJECTED TAKEOFF. PRESSURE ON A SYS WAS NORMAL UNTIL THE RUNWAY CLEARED, THEN LOST HYD PRESSURE. STOPPED ACFT AND SHUTDOWN ENGINES. FOUND A SYS HYD FLEX HOSE FROM THE A SYS HYD MODULE Jul 30, 2011 · N241FE · Boeing 727277 · Hydraulic System, MainSDR FDEA201107232914Thermal Switch · failedDURING CRUISE AT FL360 ENGINE 3 BLEED AIR TRIP OFF LIGHT ILLUMINATED AND THE NR 3 BLEED AIR VALVE CLOSED, SYS WOULD NOT RESET VIA QRH PROCEDURES ( LIGHT STAYED ON ). CABIN ALTITUDE WAS RAPIDLY INCREASING THROUGH 10000FT AND AFTER DONNING OXYGEN AND DESCENDIJul 23, 2011 · N245FE · Boeing 727277 · Engine Bleed Air SystemSDR FDEA201010224147Engine · failedWHILE ADVANCING POWER FOR TAKEOFF, AT 80 PERCENT N1 ON ENG NR 2. EPR SLOW TO INCREASE, COMPRESSOR STALL OCCURED. TOWER WITNESSED FLAMES FROM NR 2 ENGINE. R & R NR 2 ENGINE IAW WORK CARD 70T0002. INSTALLED ENGINE IAW WORK CARD 70T0002.Oct 22, 2010 · N245FE · Boeing 727277 · Compressor Bleed ControlSDR FDEA201008203055Receiver · failedVOR'S CHECKED GOOD ON PREFLIGHT. DURING CLIMBOUT BOTH VOR'S SHOWED A 30 DEGREE SPLIT ON VOR STA COULD NOT CTR EITHER CDI ON VOR STATION. TRIED ANOTHER VOR STA, SAME SITUATION. BOTH RMI'S HAD VOR NEEDLES 30 - 40 ' SPLIT. COMPASS SYS MATCHED. HAD TO RELY ON ATAug 20, 2010 · N244FE · Boeing 727277 · Visual Omnirange (VOR) SystemSDR FDEA201001150180Seat Track · corrodedCABIN SEAT TRACK AT STA 695 RBL 24 INBD FLANGE AND SPLICE CORRODED REMOVED SEAT TRACK SECTION BETWEEN STA 690 TO 740 RBL24 AND 1 EA SPLICER IAW SRM 51-30-2, FABRICATED NEW SEAT TRACK SECTION FROM BAE 1526-729-7178 T6 511 PO NR 9006020, DIM 172" LONG IAW SRM 5Jan 15, 2010 · N489FE · Boeing 727277 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200908072929Indicator · failedSTANDBY ADI PRECESSED 20 MIN. AFTER TAKE OFF, AT CRUISE. RECAGED BUT 2-3 MIN. LATER, PRECESSED AGAIN. 20-30 DEG RIGHT BANK, 10 DEG NOSE HIGH. REMOVED AND REPLACED STANDY BY ATTITUDE INDICATOR IAW MM 34-25-011-4. SYSTEM OPS CHECKED NORMAL. OK TO CONTAug 7, 2009 · N245FE · Boeing 727277 · Attitude Gyro and Indicating SystemSDR FDEA200906011866Floorbeam · corrodedMAIN CABIN FLOORBEAM BS 312, LBL 6 IS EXFOLIATED ON AFT LIP OF UPPER CHORD. CUT OUT DAMAGED AREA 2 BY 1 INCH IAW DWG NR SR27-53-017 REV A. FABRICATED 2 REPAIR ANGLES AND REPAIR FILLER IAW DWG NR SR27-53-017 REV A. HEAT TREATED REPAIR ANGLES FROM TO T6 IAW FJun 1, 2009 · N244FE · Boeing 727277 · Fuselage Main, Floor BeamSDR FDEA200905311899Skin · damagedRT WING INBD FOREFLAP, OUTBD END, PREVIOUS REPAIR IS GOUGED REMOVED PREVIOUS REPAIR IAW SRM 51-30-2. FABRICATED REPAIR DOUBLER IAW SRM 57-50-2 FIG 4 AND 57-50-4 FIG. ALODINED AND PRIMED DOUBLER IAW SRM 51-10-2. INSTALLED DOUBLER IAW SRM 57-50-11 FIG 1.May 31, 2009 · N245FE · Boeing 727277 · Wing, Plate/SkinSDR FDEA200905301857Fuel Tank · damagedDAMAGE AT STA 744 ON CTR TANK WEB RBL 60. REPAIRED CENTER TANK WEB IAW EA 7-5710-126825. REPAIR BY CUTTING OUT DAMAGED AREA, FABRICATED DOUBLER AND INSTALLED IAW EA 7-5710-126825.May 30, 2009 · N245FE · Boeing 727277 · Fuel StorageSDR FDEA200905301858Stringer · corrodedAFT CARGO COMPARTMENT, CORROSION AROUND FASTENERS IN STRINGER 30 AT BS 990. REMOVED CORROSION AND FOUND OUT OF LIMITS, FABRICATED NEW STRINGER SECTION, FABRICATED NEW SPLICE AND INSTALLED PARTS IAW SRM 51-10-6, 53-10-1, 51-30-2, 53-10-3, AND 51-30-5.May 30, 2009 · N245FE · Boeing 727277 · Fuselage Main, Longeron/StringerSDR FDEA200905291863Rib · crackedNR 5 SLAT HAS CRACKED RIB ON INBOARD SIDE OF ACTUATOR FORWARD MOUNT. REMOVED AND REPLACED RIBS WITH NEW RIBS IAW SRM 51-30-2.May 29, 2009 · N245FE · Boeing 727277 · Leading Edge DevicesSDR FDEA200905291846Stringer · corrodedSTRINGER 27L CORRODED STA'S 950F TO 1030 REMOVED CORROSION AND FOUND OUT OF LIMITS, REMOVED DAMAGED STRINGER AND FABRICATED NEW STRINGER SECTIONS. FABRICATED REPAIR SPLICES AND INSTALLED REPAIR PARTS IAW SRM 53-10-3, 53-10-2 AND 51-30-2.May 29, 2009 · N245FE · Boeing 727277 · Fuselage Main, Longeron/StringerSDR FDEA200905271940Frame · damagedSTATION 520 FRAME DAMAGED AT STRINGER 21L TO 26L. REMOVED DAMAGED FRAME, FABRICATED NEW FRAME, HEAT TREATED TO T6 CONDITION, AND INSTALLED PARTS IAW SRM 51-30-2, 53-10-2.May 27, 2009 · N245FE · Boeing 727277 · Fuselage Main, FrameSDR FDEA200905271898Skin · crackedRMLG WING DOOR SKIN CRACKED FWD OF AFT HINGE POINT REMOVED FILLER AND DOUBLER IAW SB 727-32-318 HFEC SHOWS AREA OF CUT OUT FREE OF CRACKS IAW NDTM 51-00-00 FIG 23 FABRICATED FILLER AND DOUBLER, ALODINED AND PRIMED PARTS IAW SRM 51-10-2 OPENED INNER SKIN May 27, 2009 · N245FE · Boeing 727277 · Landing Gear DoorsSDR FDEA200905271865Seat Track · corrodedSEAT TRACK CORRODED STA 690-720 LBL 45. REMOVED DAMAGED SEAT TRACK, FABRICATED NEW ONE, REPAIR SPLICES, STRAP, AND INSTALLED REPAIR PARTS IAW 53-10-5 AND 53-10-2.May 27, 2009 · N245FE · Boeing 727277 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200905271815Shear Tie · corrodedFWD PIT BS 720C BETWEEN ST 25RT TO 26RT SHEAR TIE CORRODED.May 27, 2009 · N245FE · Boeing 727277 · Fuselage Internal Mounting StructureSDR FDEA200905271814Shear Tie · corrodedFWD PIT BS 720C BETWEEN STR 25L TO 26L SHEAR TIE CORRODEDMay 27, 2009 · N245FE · Boeing 727277 · Fuselage Internal Mounting StructureSDR FDEA200905261900Skin · crackedLEFT MLG WING DOOR CRACKED FWD OF AFT HINGE POINT REMOVED FILLER AND DOUBLER IAW SB B727-32-318 AND SRM 51-30-2 HFEC SHOWS AREA FREE OF CRACKS IAW NDTM 51-00-00 FIG 23 FABRICATED NEW FILLER AND DOUBLER IAW SB 727-32-318 ALODINED AND PRIMED PARTS IAW SRM 51-May 26, 2009 · N245FE · Boeing 727277 · Landing Gear DoorsSDR FDEA200905231868Stringer Splice · corrodedCORROSION ON STRINGER SPLICE AT STRINGER 30, BS 950. REMOVED DAMAGED ANGLE, LOCATED, DRILLED AND INSTALLED NEW ANGLE PN 69-44177-1 IAW SRM 51-30-2, AND 51-30-5.May 23, 2009 · N245FE · Boeing 727277 · Fuselage Main, Longeron/StringerSDR FDEA200905231867Fitting · corrodedCORROSION ON STRINGER 29L KEELBEAM EXTENSION FITTING AT BS 950. FOUND OUT OF LIMITS, REMOVED FITTING AND LOCATED, DRILLED AND INSTALLED NEW FITTING PART NR 69-51272-1 IAW SRM 51-30-2 AND 53-10-1.May 23, 2009 · N245FE · Boeing 727277 · Fuselage Main, Attach FittingsSDR FDEA200905211765Seat Track · corrodedMAIN CABIN FUSELAGE SEAT TRACK AT BS 1110, LBL 24 IS CORRODED. REMOVED CORRODED SECTION OF SEAT TRACK IAW 51-30-2 FABRICATED NEW SECTION IAW DRAWING 53FX976 REV B. TREATED & PRIMED SECTION IAW SRM 51-10-2 INSTALLED SEAT TRACK SECTION IAW SRM 51-30-2May 21, 2009 · N244FE · Boeing 727277 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200905211760Stringer · corrodedART PIT STR 27L CORRODED IN CHANNEL BETWEEN BS 950E-950F. REMOVED CORROSION IAW SRM 51-10-6. UT INSPECTED AREA FOUND OUT OF LIMITS. CUT OUT DAMAGE AREA IAW SRM 53-10-3 FIG 1. FABRICATED REPAIR PARTS AND 2 SPLICES IAW SRM 53-10-2 FIG 9. TREATED AND PRIMEMay 21, 2009 · N244FE · Boeing 727277 · Fuselage Main, Longeron/StringerSDR FDEA200905211759Stringer · corrodedAFT PIT STR 27L CORRODED IN CHANNEL BETWEEN BS 970-990. REMOVED CORROSION IAW SRM 51-10-6. INSPECTED AREA AND FOUND OUT OF LIMITS IAW SRM 53-10-1. FIG 1. CUT OUT DAMAGED AREA IAW SRM 53-10-3, FIG. 1. FABRICATED STRINGER, & SPLICERS IAW SRM 53-10-3 FIG. 1. ANMay 21, 2009 · N244FE · Boeing 727277 · Fuselage Main, Longeron/StringerSDR FDEA200905191757Skin · crackedL-1 DOOR LOWER HINGE SKIN DOUBLER IS CRACKED. REPAIRED L-1 DOOR LOWER HINGE SKIN IAW EO 7-5330-7-2345 PART 2.May 19, 2009 · N245FE · Boeing 727277 · Passenger/Crew DoorsSDR FDEA200905191741Frame · crackedFORWARD CARGO DOOR, STA 540, STRINGER 21L-22L, CRACK ON STUB FRAME EXTENSION RADIUS. REMOVED DAMAGED STUB FRAME, FABRICATED NEW ONE AND INSTALLED IAW SRM SRM 51-20-1, 51-30-2 AND DWG 53FX1350.May 19, 2009 · N245FE · Boeing 727277 · Cargo/Baggage DoorsSDR FDEA200905191740Frame · crackedFORWARD CARGO DOOR, STA 520, STRINGER 21L-22L, CRACK ON STUB FRAME EXTENSION RADIUS. REMOVED DAMAGED STUB FRAME AND INSTALLED NEW FABRICATED ONE IAW SRM 51-30-2, 51-20-1 AND DWG 53FX1350.May 19, 2009 · N245FE · Boeing 727277 · Cargo/Baggage DoorsSDR FDEA200905191739Frame · crackedFORWARD CARGO DOOR, STA 500, STRINGER 21L-22L, CRACK ON STUB FRAME EXTENSION RADIUS. REMOVED AND INSTALLED IAW SRM SRM 51-20-1, 51-30-2 AND DWG 53FX1350.May 19, 2009 · N245FE · Boeing 727277 · Cargo/Baggage DoorsSDR FDEA200905191738Frame · crackedFORWARD CARGO DOOR, STA 560, STRINGER 21-22L, CRACK ON STUB FRAME EXTENSION RADIUS. REMOVED DAMAGED STUB FRAME EXTENSION, FABRICATED NEW STUB FRAME, HEAT TREATED TO T-6 AND INSTALLED IAW SRM SRM 51-20-1, 51-30-2 AND DWG 53FX1350.May 19, 2009 · N245FE · Boeing 727277 · Fuselage Main, StructureSDR FDEA200905181842Seat Track · corrodedCORROSION ON SEAT TRACK FLANGE BS 1110-1116 LBL47. CORROSION ON SEAT TRACK OUT OF LIMITS, REMOVED SEAT TRACK, FABRICATED NEW SEAT TRACK AND INSTALLED IAW SRM 51-30-2, 53-10-5 AND 51-10-2.May 18, 2009 · N245FE · Boeing 727277 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200905181713Stringer · corrodedFWD PIT CORROSION ON STR 26 L STA 720B. CUT OUT DAMAGE AREA IAW SRM 53-10 3 FIG 1. FABRICATED REPAIR PART AND 2 SPLICES IAW SRM 53-10-2 FIG 1 AND 53-10-2 FIG 9. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED REPAIR PARTS IAW SRM 51-30-2.May 18, 2009 · N244FE · Boeing 727277 · Fuselage Main, Longeron/StringerSDR FDEA200905181712Stringer · corrodedFWD PIT - CORROSION ON STR 26 L BETWEEN STA 700 AND 720. CUT OUT DAMAGE AREA IAW SRM 53-10-3 FIG 1. FABRICATED STRINGER AND 1 SPLICE IAW SRM 53-10-2 FIG 9. TREATED AND PRIMED IAW SRM 51-10-2, INSTALLED REPAIR PARTS IAW B727 SRM 51-30-2.May 18, 2009 · N244FE · Boeing 727277 · Fuselage Main, Longeron/StringerSDR FDEA200905181714Fitting · corrodedCORROSION ON STRINGER 29 R KEEL BEAM EXTENSION FITTING AT BS 950. FOUND CORROSION ON FITTING OUT OF LIMITS, REMOVED FITTING AND LOCATED, DRILLED AND INSTALLED NEW FITTING PN 69-51272-2 IAW SRM 51-30-2 AND 53-10-1.May 18, 2009 · N245FE · Boeing 727277 · Fuselage Main, Attach FittingsSDR FDEA200905171699Skin · crackedRT WING INBD MID FLAP AFT LOWER ANGLE HAS 2 CRACKS, WBL 90. REMOVED R / WING I/B MID FLAP LOWER INNER SKIN PANEL IAW SRM 51-30-2. CUT OUT DAMAGE AREA ANGLE SECTION SRM 51-10-1 AND 51-40-4. FABRICATED REPAIR ANGLE AND SPLICE IAW SRM 57-50-2. TREAT AND PRIMEDMay 17, 2009 · N245FE · Boeing 727277 · Trailing Edge FlapsSDR FDEA200905171702Angle · crackedNR 3 SLAT AFT LOWER ANGLE IS CRACKED AT ACTUATOR ATTACHMENT. UPON FURTHER INVESTIGATION SLAT REPAIR NOT FEASIBLE, SLAT REMOVED AND REPLACED.May 17, 2009 · N245FE · Boeing 727277 · Wing, Control Surface Attach FittingsSDR FDEA200905171701Spar · crackedLT WING FALSE SPAR LOWER CHORD IS CRACKED AT WBL 118. CUTOUT SECTION, FABRICATED NEW SECTION, FABRICATED WEB, FABRICATED 2 ANGLES, HEAT TREAT ANGLES IAW FASI ER 2-32153-801 REV. A, FABRICATED STRAP, 2 RADIUS FILLERS, LOCATED AND DRILLED NEW PARTS, ALODINED ANMay 17, 2009 · N245FE · Boeing 727277 · Wing SparSDR FDEA200905171700Keelbeam · crackedLT W/W, LT KEEL BEAM IS CRACKED AT 2ND FASTENER STA 875, LBL 6. TRIMMED OUT CRACK DIMS 2 INCH X 1 INCH, FABRICATED DOUBLER, HEAT TREATED AND CADMIUM PLATED DOUBLER AND INSTALLED IAW EA 7-5310-127963.May 17, 2009 · N245FE · Boeing 727277 · Fuselage Main, KeelSDR FDEA200905171697Skin · corrodedRT WING LEADING EDGE HAS BULGING SEALANT AND CORROSION AT WS 510 UPPER SURFACE ABOVE SPAR. FABRICATED REPAIR FILLERS & DOUBLER IAW B727 SRM 57-30-4 FIG 6. TREATED & PRIMED PARTS & AREA IAW SRM 51-10-2. FLAP SHOT PEEN AREA IAW EA 7-5710-127964. INSTALLEDMay 17, 2009 · N244FE · Boeing 727277 · Wing, Plate/SkinSDR FDEA200905161690Skin · damagedFUSELAGE SKIN AT STA 300 STRINGER 21LT IS GOUGED BLENDED OUT DAMAGED AREA IAW SRM 51-10-1, FOUND TO BE OUT OF LIMITS IAW SRM 53-30-1 FIG 1 AND 2, CUT OUT DAMAGED AREA IAW SRM 51-10-1, FABRICATED REPAIR DOUBLER IAW SRM 53-30-3 FIG 1 AND 53-30-2 FIG 2, TREATEDMay 16, 2009 · N244FE · Boeing 727277 · Fuselage Main, Plate/SkinSDR FDEA200905161693Angle · crackedNR 6 SLAT AFT LOWER CHORD ANGLE IS CRACKED AT INBD UPSTOP PAD REMOVED NR 6 SLAT COVE ACCESS PANELS IAW SRM 51-30-2. CUT OUT DAMAGED AREA IAW SRM 51-10-1. FABRICATED NEW ANGLE AND SPLICE IAW SRM 51-40-4 AND 57-50-2 FIG. 2. ALODINED AND PRIMED REPAIR PARTS IAWMay 16, 2009 · N245FE · Boeing 727277 · Wing, Plate/SkinSDR FDEA200905151681Skin · crackedRIGHT FOREFLAP, INBOARD WBL 124, CRACK ON SKIN ABOVE CARRIAGE ATTACH FITTING CUT OUT DAMAGED AREA IAW SRM 51-10-1, FABRICATED REPAIR DOUBLER & FILLER IAW SRM 57-50-2 FIG 4 AND 57-50-2 FIG 1, TREATED AND PRIMED IAW SRM 51-10-2 INSTALLED REPAIR IAW SRM 51-30-2May 15, 2009 · N244FE · Boeing 727277 · Trailing Edge Flaps
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