N258FE, cancelled Aug 10, 2015
Service difficulty reports · 87
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 = 'N258FE' AND deregistration_id = 'N258FE-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.
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 = 'N258FE' AND deregistration_id = 'N258FE-2015-08-10' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR FDEA201109063775Slide · dislodgedCLOSED L1 DOOR, DOOR SLIDE FELL OFF LAYING IN A HEAP AGAINST LAV DOOR. R & R L1 DOOR SLIDE REF MM 25-60-015-2. FINAL CLOSEDSDR FDEA200907112582Power Unit · leakingSYS B HYD SYS FAILED INFLT B HYD INDICATED ZERO GAL & PRESSURE BEGAN TO DECREASE BELOW 200 PSI. EVALUATION SHOWS LEAK FROM UPPER RUDDER AREA. F/E NOTED DECREASING "B" SYS QTY & MONITORED QTY & PRESSURE. AS PRESSURE DECREASED, AS SOON AS NR 2 "B" PUMP LOW PSDR FDEA200905141663Bypass Valve · failedON DEPARTURE, FLAP RETRACTION NOT NORMAL, SPLIT FLAPS, OUTBOARD FLAPS IN AGREEMENT W/HANDLE AT FLAPS 5 DEG INBOARD FLAPS STAYED AT 15 DEG. RAN QRH, SOME SLATS EXTENDED. ATTEMPTED FLAP MASTER & RAISE INBD FLAPS, ALT FLAP MOTOR INBD C/B POPPED. RTB. INBD FLASDR FDEA200902210623Web · crackedAFT AIRSTAIR RT WEB AT BS 1223 LIGHTENING HOLE HAS A CRACK. ROUTED OUT CRACKED AREA OF RT TORQUE BOX WEB AT STA 1223 IAW SRM 51-10-1. FABRICATED REPAIR DOUBLER IAW SRM 51-40-2. TREATED AND PRIMED NEW PARTS IAW SRM 51-10-2 AND INSTALLED IAW SRM 51-40-2 FIG 1SDR FDEA200902200614Skin · gougedC2 DOOR LOWER AFT CORNER IS GOUGED BS 990 S26R. ROUTED OUT DAMAGED EDGE IAW SRM 51-10-1. FABRICATED REPAIR DOUBLER & 2 FILLERS IAW SRM 52-00-03 FIG 4 & 52-30-1 FIG 8. HFEC INSPECTION PERFORMED IAW NDTM PT6 & 51-00-00 FIG 11. NO CRACKS NOTED. OVERSIZED CRISDR FDEA200902200613Frame · crackedFRAME CRACKED BS 970 ABOVE STR 26L AFT PIT. REMOVED INTERCOSTAL AND PREVIOUS REPAIR FOR ACCESS IAW SRM 51-30-2, CUTOUT DAMAGED AREA ON FRAME IAW SRM 51-10-1. FABRICATED FILLERS & DOUBLER IAW SRM 53-102 FIG 5 AND 51-40-3 FIG 1. HEAT TREATED FILLERS & DOUBLER SDR FDEA200902200612Frame · crackedFRAME CRACKED BS 990 ABOVE STR 26L AFT PIT. CUTOUT DAMAGED AREA IAW SRM 51-10-1, FABRICATED FILLER & DOUBLER IAW SRM 53-10-2 FIG 5 & 51-40-3 FIG 1. HEAT TREATED FILLER & DOUBLER TO 7075 T-6 IAW FAS ENG REPORT 2-37153-001 REV A. LOCATED DRILLED, DEBURRED FILLSDR FDEA200902190584Skin · dentedOIL CANNING RT FUSELAGE SKIN BS 675 BETWEEN STR 22R AND STR 23R. CUT-OUT DAMAGE AREA IAW SRM 53-30-3 FIG 1. FABRICATED DOUBLER REPAIR IAW SRM 53-30-3 FIG 1 AND 53-30-2 FIG 2. TREATED AND PRIMED NEW PARTS IAW SRM 51-10-2. INSTALLED PARTS IAW SRM 51-30-2 ANDSDR FDEA200902190587Hinge · crackedEXTERIOR FUSELAGE MCD AFT HINGE AFT END HAS LARGE CRACK TO ATTACH SCREW HOLE, FROM LOBE. REPLACED HINGE SEGMENT IAW SRM 51-30-5, 51-30-2 & IAW DWG 52FX1433 REV E & INSTALLED NEW HINGE PIN IAW SRM 51-30-2 & DRAWING 52FX1433 REV E. OPS CHECK GOOD IAW MM 52-34-0SDR FDEA200902190585Skin · corrodedEXTERIOR FUSELAGE, CORROSION ON SKIN LAP AT BS 690 STR 26R. REMOVED CORROSION IAW SRM 51-10-6. OUT OF LIMITS IAW SRM 53-30-1 FIG 1. CUT-OUT DAMAGED AREA, FABRICATED DOUBLER, & FILLER. TREATED AND PRIMED ALL REPAIR PARTS IAW SRM 51-10-2. INSTALLED REPAIR IASDR FDEA200810074263Transmitter · failedNR 1 ENG SHUTDOWN IN FLIGHT FOR HIGH OIL PRESSURE (60 PSI) IAW QRH. WINDMILLED FOR 15 MINUTES IN GREEN BAND AND BELOW. REMOVED AND REPLACED OIL PRESSURE TRANSMITTER PER BOEING MM 79-33-001-4 RAN ENGINE FOR LEAK CHECK AND PRESSURE CHECKS. CHECK OIL PRESSURE SDR 08FDEA04263Transmitter · failedNR 1 ENGINE SHUTDOWN INFLT FOR HIGH OIL PRESSURE (60 PSI) IAW QRH. WINDMILLED FOR 15 MINUTES IN GREEN BAND AND BELOW. REMOVED AND REPLACED OIL PRESSURE TRANSMITTER PER MM 79-33-001-4. RAN ENGINE FOR LEAK AND PRESSURE CHECKS. CHECK OIL PRESSURE WITH DIRECT SDR 07FDEA04996Blocker Door · out of adjustMAIN CARGO DOOR "A" OPEN LIGHT ILLUMINATED INFLIGHT, PRESSURIZATION NORMAL INITIALLY, FLICKERED AT FL 200 THEN REMAINED ON STEADY IN DESCENT UNTIL SHORT FINAL THEN WENT OUT. ACN RELEASED FOR SERVICE PER MEL/CDL: 52-15-01 CATEGORY: C EXPIRATION: 14DEC07 "MELSDR 05FDEA00661Warning Light · illuminatedLOWER CARGO SMOKE LIGHT ILLUMINATED ON T/O 70 KTS. RTO, NO OTHER INDICATIONS, LIGHT WENT OUT DURING DECELERATION. MEL 26MAR05, RELEASED FOR SERVICE PER MEL/CDL: 26-19-C CATEGORY: C EXPIRATION: 05APR05 MEL 26-19-C: SMOKE DETECTION IN THE AFT LOWER CARGO COMPASDR 05FDEA00660Warning Light · illuminatedLOWER CARGO SMOKE LIGHT ILLUMINATED ON T/O AT 70 KTS, RTO NO OTHER INDICATIONS LIGHT WENT OUT DURING DECELERATION. RELEASED FOR SERVICE PER MEL/CDL: 26-19-A CATEGORY: C EXPIRATION: 05APR05 MEL 26-19-A: SMOKE DETECTION IN THE FWD LOWER CARGO COMPARTMENT INOPSDR 05FDEA00631Lamp · malfunctionedLOWER CARGO SMOKE LIGHT ILLUMINATED ON T/O AT 90 KTS, RTO- NO OTHER INDICATION ON CARGO PANEL OR BELL. BOTH FWD AFT COMPARTMENTS CHECK CLEAR. RELAMPED INDICATOR OPS TEST NORMAL IAW MM 26-17-012-2 OK FOR SERVICE.SDR 05FDEA00280Skin Panel · corrodedOVERWING BOX, TANK TOP, HAS CORROSION AT BODY STATION 840 RIGHT BUTT LINE 12.0. REPAIRED OVERWING BOX FUEL TANK, STATION 840 AT RIGHT BUTT LINE 12.0 IAW FEDEX EA 7-5730-83992, WINGS-UPPER SKIN PANEL, CENTER TANK CORROSION-REPAIR.SDR 04FDEA02006Smoke Detector · malfunctionedCLIMBING THROUGH 16,000 FT, NR 4 MAIN CARGO SMOKE LIGHT ILLUMINATED. RAN QRH PROCEDURES. LIGHT EXTINGUISHED. SHORTLY AFTER LEVELING AT FL 230, NR 4 SMOKE WARNING REOCCURRED. TEST OF SYSTEM SHOWED BAD NR 4 SENSOR, IE TEST NOT GOOD. REMOVED AND REPLACED NRSDR 04FDEA00762Control Box · inoperativeMAIN GEAR ANTI SKID OUTBOARD INOP & INBD INOP LIGHTS INTERMITTEN ON TAKEOFF ROLL WITH NO BRAKES APPLIED. REMOVED AND REPLACED ANTI SKID CONTROL BOX, OPS CHECK AND SELF TEST GOOD AT THIS TIME IAW 727 MM 32-42-001-5.SDR 04FDEA00685Bear Strap · corrodedMAIN FRAME, FWD LWR CARGO DOOR BEAR STRAP CORRODED (AD 98-11-03R1). COMPLIED WITH EA 7-5310-73889A FUSELAGE - MAIN FRAME, FWD LWR CARGO DOOR BEAR STRAP CORROSION REPAIR (AD 98-11-03 R1).SDR 03FDEA01085Scavenge Pump · inoperativeNR 2 ENGINE SHUT DOWN IN FLIGHT DUE TO OIL QUANTITY SLOWLY DECREASING TO ZERO. AS OIL QUANTITY DROPPED TO ZERO OIL PRESSURE DROPPED BELOW 40 PSI AND OIL TEMP WAS INCREASING. R & R NR 2 ENG OIL PUMP IAW PRATT & WHITNEY, ENGINE MANUAL 72-00-61. RAN ENGINE AND SDR 03FDEA00732Tripler · wornCOMPLY WITH E.A. 7-5330-70385 FUSELAGE-MAIN CARGO DOOR TRIPLER WEAR. FACT 15MAY03 21:19 BFM U COMPLIED WITH E.A. 7-5330-70385 FUSELAGE-MAIN CARGO DOOR TRIPLER WEAR.SDR 03FDEA00135Actuator · failedAFTER TAKEOFF, WHEN RETRACTING FROM FLAPS, 5 DEG TO 2 DEG, LEADING EDGE FLAPS AMBER REMAINED ON, RIGHT SIDE LEADING EDGE FLAP NR 4 REMAINED OUT. AFTER FOLLOWING RED TABS, AT FLAPS, 2 DEG LEADING EDGE, NR 5 REMAINED OUT. WITH FLIGHT CONTROL WHEEL RELAXED, A/SDR 02FDEA00308Position Switch · failedRIGHT INBOARD LEADING EDGE FLAP NR 5 FAILED TO RETRACT WHEN FLAPS 2 SELECTED. REMOVED AND REPLACED NR 5 LEADING EDGE FLAP POSITION SWITCH PER MM 27-80-001-4. OPS CHECK NORMAL.SDR 02FDEA00307Flap · failed02-108 RIGHT INBD LEADING EDGE FLAP #5 FAILED TO RETRACT WHEN FLAPS 2 WAS SELECTED. ** S/D ** COMINGSDR 01FDEA00822Support · crackedN 1137 L/W I/B SPOILER SUPPORT BEAM CRACKED OF I/B END. ** S/D ** COMINGSDR 01FDEA00850Skin · corrodedN 490 CORROSION ON FUSELAGE SKIN INNER SIDE BS 498, RBL 7, WL 148. R&R SKIN PER EA 7-5330-59857.SDR 01FDEA00851Stringer · corrodedN 489 STRINGER 28R CORRODED AT BS 498. R&R STRINGER PER SRM 53-10-1 FIG 1.SDR 01FDEA00852Floorbeam · misdrilledN 783 FLOORBEAM LWR FLANGE HAS DRILL HOLE IN RADIUS BS 460, RBL 45, WL 208. R&R FLOORBEAM PER SR 27-53-034E & SRM 51-30-2.SDR 01FDEA00840Shear Tie · corrodedCORRODED SHEAR TIE BS 1110, RBL 10 - 14. REMOVED AND REPLACED SHEAR TIE PER SRM 51-20-1, 51-10-2 & 51-30-2.SDR 01FDEA00838Floorbeam · corrodedCORROSION (C53-224-1-, 1) ON FLOORBEAM BS 620 LBL 25 TO 45, WL 208. REMOVED AND REPLACED CORROSION ON FLOORBEAM PER SRM 53-10-8.SDR 01FDEA00839Floorbeam · corrodedCORROSION (C53-024-02) ON FLOORBEAM TOP CHORD UPPER AND LOWER FLANGE BS 680, RBL 3 - 25, WL 208. REMOVED AND REPLACED FLOORBEAM PER SRM 53-10-8 FIG 3.SDR 01FDEA00837Frame · dentedN 450 AFT CARGO FRAME DENT AT BS 970, LBL 33. ** S/D ** COMINGSDR 01FDEA00528Damper · faultyEXPERIENCED UNCOMMANDED YAW PULLED UPPER RUDDER YAW DAMPER AC & DC CB YAW DISCONTINUED.SDR 01FDEA00030Circuit Breaker · failedTRAILING EDGE INBOARD FLAPS FAILED TO RETRACT DURING GO-AROUND. RED TABS ACCOMPLISHED. RESET INBOARD FLAP IND CIRCUIT BREAKER. CYCLED FLAPS 4 TIMES WITH NO DISCREPANCY. TEST PER 727-200 MM 27-51-000-1. OK TO CONTINUE.SDR 0FDEA00478Uplock · lack of lubeGEAR RETRACTION WITH GEAR HANDLE IN OFF POSITION RED DOOR LIGHT ON FWD PANEL. PERFORMED GEAR RETRACTION TEST PER MM 32-32-0. RT MLG OPS OK AND IND NORM. TEST SEVERAL TIMES. LUBED RT MLG UPLOCK MECHANISM PER 12-21-1.SDR 00FDEA00404Engine · failedNR 1 ENG - FLAMES AND METAL PARTS REPORTED BY ACFT BEHIND, ON T/O AND TOWER. NR 1 ENG TEMP 610 ON T/O ROLL. ALL OTHER IND NORMAL. *S/D* REMOVED AND REPLACED NR 1 ENGINE PER WORK CARDS 70T0001-01, AND 70T0301-01.SDR 99FDEA00507Controller · malfunctionedCLIMB THRU FLT LEVEL 180 CABIN PRESS START TO DECREASE AT 1200 RPM (4.8 PSID & DECREASING). PERFORMED CABIN PRES CKLIST, NO HELP. *S/D* ACCOMPLISH EXCESS CABIN PRESS LEAKAGE CONDITION, REF B727 MM 05-51-101-2, TEST OK. NO DEFECTS NOTED AT THIS TIME, A/C OKSDR 99FDEA00180Wire · out of positionLWR AFT BODY O/H LIGHT. TEST SYS OK PER RED TABS CLOSE BLD. *S/D* REPOSITIONED WIRE REF LOOP POS 26-14-1 PG 203. REMOVED AND REPLACED MODULATING SHUT OFF VALVE PER MM 36-12-042-4. LEAK CK OK.SDR 99FDEA00177Control Unit · malfunctionedLOWER BODY O/H LIGHT ILLUM, WITH BOTH PACKS ON NR 1 ENG BLD CLOSED NR 2 AND 3 ENG BLD OPEN. RAN RED TABS 2-714 WHEN NR 1 BLD AND LT PACK OFF LIGHT WENT OUT. REMOVED AND REPLACED AFT BODY O/H DETECTION DETECTOR AS PER MM 26-14-0, OPER CK NORM.SDR 99FDEA00158Duct · leaked99-95 - LWR AFT BODY OVERHEAT. STEP 19 IND BLD AIR LEAK IS BETWEEN BLEED VALVE AND PACK VALVE. ENG RUN ON NR 1, 2 AND 3 ENG NO FAULTS PER MM 24-14-1 PG 204CK. INSULATION RESISTANCE ABOVE LOOPS FND IN LIMITS. CTR CONDUCTOR LOOPS M322, M365, M767, M367 FND ISDR 99FDEA00146Overheat Light · illuminatedLOWER AFT BODY OVERHEAT LIGHT ILLUMINATED. CLOSED LEFT PACK SWITCH AND NR 1 ENG BLD VALVE AFT RETARD NR 1, THROTTLE LIGHT WENT OUT AND STAY OUT. RAN NR 1 AND NR 2 ENGINE, NO LEAK FOUND. INSPECTED LOWER AFT BODY OVERHEAT DETECTOR, NORM PER MM 26-14-00.SDR 98FDEA00339Engine · failedON T/O, NR 3 ENG FAILED, SLIGHT SHUDDER ACCOMMP BY LOSS OF EPR AND N1, HIGH EGT AND LOSS OF OIL QTY, SHUTDOWN PER 727 A/C FLT MANUAL. REMOVED AND REPLACED NR 3 ENG PER W/C 70T0001.SDR 97FDEA00833Position Ind · malfunctionedDURING FLAP RETRACTION AT 2 DEGREE ON CLIMBOUT, THE NR 4 RIGHT INBD FLAP DID NOT RETRACT. THE POSITION TEST SELECTOR INDICATED THE SAME. THE LEADING EDGE FLAPS POSITION IND LIGHTS WERE AMBER. PROCEEDED WITH RED TAB CHECK LIST AND MADE A NORMAL LANDING. REMSDR 97FDEA00122Retract Mech · lack of lubeNOSE GEAR DID NOT EXTEND WHEN GEAR HANDLE LOWERED (UNSAFE NOSE GEAR LIGHT AND VISUALLY CONFIRMED NOT DOWN/ DOORS NOT OPEN). RAISED GEAR, INDICATED ALL UP. LOWERED GEAR HANDLE IN CONJUNCTION WITH NEGATIVE 'G', CAME DOWN AND LOCKED. LUBRICATED DRAG BRACE KNUCSDR 96FDEA01664Bonding Jumper · corrodedNR 398 036, CORROSION (C57-562-01-1) NR 1 K-FLAP BULLNOSE O/B BONDING JUMPER UPPER END LOWER ATTACH POINT. *S/D* REPAIRED NR 1 K-FLAP BULLNOSE O/B BONDING JUMPER UPPER END LOWER ATTACH POINT IAW FEDEX EA 7-5750-31262.SDR 96FDEA01663Angle · corrodedNR 640, 035, CORROSION (C53-224-01, 1) ON MOP SILL AT BS 312 TO 360, LBL 62, WL 208.1. *S/D* REMOVED AND REPLACED MOP SILL FROM BS 259 TO 360, LBL 65 WL 208.1 IAW FEDEX SRM 53-10-1, 51-30-2.SDR 96FDEA01666Bullnose · wornNR 0137 038, LOWER RUDDER BULLNOSE WORN AT CONTACT POINT OF RUDDER TO VERTICAL FIN FAIRING, BEYOND LIMITS. RUDDER REMOVAL AND INSTALL REQUIRED). *S/D* REMOVED LOWER RUDDER, INSTALLED DOUBLERS OVER WORN AREAS IAW FEDEX SRM 55-40-3 FIG 1, REINSTALLED RUDDER ISDR 96FDEA01665Bullnose · wornNR 0136 037, UPPER RUDDER BULLNOSE WORN AT CONTACT POINT OF RUDDER TO VERTICAL FIN FAIRING, BEYOND LIMITS. RUDDER REMOVAL AND INSTALL REQUIRED. *S/D* REMOVED UPPER RUDDER, INSTALLED DOUBLER OVER WORN AREA IAW FEDEX SRM 55-40-3 FIG NR 1. REINSTALLED UPPER RSDR 96FDEA01658Window Frame · corrodedNR 0128 034. MAIN CABIN RIGHT HAND WINDOW PLUG BS 640-660 HAS EVIDENCE OF CORROSION BETWEEN PLUG AND WINDOW FRAME LOWER AFT CORNER. *** S/D *** COMING.
Back to N258FE, cancelled Aug 10, 2015