# Service difficulty reports: N258FE, cancelled Aug 10, 2015

A list on [N258FE, cancelled Aug 10, 2015](https://openairdocs.org/deregistered/N258FE-2015-08-10.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 2 · 87 reports

- [SDR FDEA201109063775](https://openairdocs.org/sdr/FDEA201109063775.md): Slide · dislodged · Sep 6, 2011 · N258FE · Boeing 727233 · Escape Slide
  > CLOSED 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 CLOSED
- [SDR FDEA200907112582](https://openairdocs.org/sdr/FDEA200907112582.md): Power Unit · leaking · Jul 11, 2009 · N258FE · Boeing 727233 · Hydraulic System, Main
  > SYS 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 P
- [SDR FDEA200905141663](https://openairdocs.org/sdr/FDEA200905141663.md): Bypass Valve · failed · May 14, 2009 · N258FE · Boeing 727200 · Trailing Edge Flap Control System
  > ON 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 FLA
- [SDR FDEA200902210623](https://openairdocs.org/sdr/FDEA200902210623.md): Web · cracked · Feb 21, 2009 · N258FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > AFT 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 1
- [SDR FDEA200902200614](https://openairdocs.org/sdr/FDEA200902200614.md): Skin · gouged · Feb 20, 2009 · N258FE · Boeing 727233 · Cargo/Baggage Doors
  > C2 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 CRI
- [SDR FDEA200902200613](https://openairdocs.org/sdr/FDEA200902200613.md): Frame · cracked · Feb 20, 2009 · N258FE · Boeing 727233 · Fuselage Main, Frame
  > FRAME 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 FDEA200902200612](https://openairdocs.org/sdr/FDEA200902200612.md): Frame · cracked · Feb 20, 2009 · N258FE · Boeing 727233 · Fuselage Main, Frame
  > FRAME 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 FILL
- [SDR FDEA200902190584](https://openairdocs.org/sdr/FDEA200902190584.md): Skin · dented · Feb 19, 2009 · N258FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > OIL 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 AND
- [SDR FDEA200902190587](https://openairdocs.org/sdr/FDEA200902190587.md): Hinge · cracked · Feb 19, 2009 · N258FE · Boeing 727233 · Fuselage, Door Hinge
  > EXTERIOR 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 52-34-0
- [SDR FDEA200902190585](https://openairdocs.org/sdr/FDEA200902190585.md): Skin · corroded · Feb 19, 2009 · N258FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > EXTERIOR 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 IA
- [SDR FDEA200810074263](https://openairdocs.org/sdr/FDEA200810074263.md): Transmitter · failed · Oct 7, 2008 · N258FE · Boeing 727233 · Engine Oil Quantity
  > NR 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 08FDEA04263](https://openairdocs.org/sdr/08FDEA04263.md): Transmitter · failed · Oct 7, 2008 · N258FE · Boeing 727233 · Engine Oil Quantity
  > NR 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 07FDEA04996](https://openairdocs.org/sdr/07FDEA04996.md): Blocker Door · out of adjust · Dec 4, 2007 · N258FE · Boeing 727200 · Door Warning System
  > MAIN 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 "MEL
- [SDR 05FDEA00661](https://openairdocs.org/sdr/05FDEA00661.md): Warning Light · illuminated · Mar 28, 2005 · N258FE · Boeing 727200 · Fire Detection
  > LOWER 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 COMPA
- [SDR 05FDEA00660](https://openairdocs.org/sdr/05FDEA00660.md): Warning Light · illuminated · Mar 26, 2005 · N258FE · Boeing 727200 · Fire Detection
  > LOWER 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 INOP
- [SDR 05FDEA00631](https://openairdocs.org/sdr/05FDEA00631.md): Lamp · malfunctioned · Mar 24, 2005 · N258FE · Boeing 727* · Fire Detection
  > LOWER 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 05FDEA00280](https://openairdocs.org/sdr/05FDEA00280.md): Skin Panel · corroded · Feb 12, 2005 · N258FE · Boeing 727233 · Wing, Plate/Skin
  > OVERWING 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 04FDEA02006](https://openairdocs.org/sdr/04FDEA02006.md): Smoke Detector · malfunctioned · Jul 7, 2004 · N258FE · Boeing 727233 · Smoke Detection
  > CLIMBING 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 NR
- [SDR 04FDEA00762](https://openairdocs.org/sdr/04FDEA00762.md): Control Box · inoperative · Mar 27, 2004 · N258FE · Boeing 727200 · Brake Anti-Skid Section
  > MAIN 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 04FDEA00685](https://openairdocs.org/sdr/04FDEA00685.md): Bear Strap · corroded · Mar 22, 2004 · N258FE · Boeing 727200 · Fuselage Main, Plate/Skin
  > MAIN 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 03FDEA01085](https://openairdocs.org/sdr/03FDEA01085.md): Scavenge Pump · inoperative · Jul 10, 2003 · N258FE · Boeing 727200 · Turbine Engine Oil System
  > NR 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 03FDEA00732](https://openairdocs.org/sdr/03FDEA00732.md): Tripler · worn · May 15, 2003 · N258FE · Boeing 727200 · Fuselage Main, Plate/Skin
  > COMPLY 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 03FDEA00135](https://openairdocs.org/sdr/03FDEA00135.md): Actuator · failed · Feb 18, 2003 · N258FE · Boeing 727200 · Trailing Edge Flap Control System
  > AFTER 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 02FDEA00308](https://openairdocs.org/sdr/02FDEA00308.md): Position Switch · failed · May 6, 2002 · N258FE · Boeing 727200 · Leading Edge Slat Position Indicating System
  > RIGHT 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 02FDEA00307](https://openairdocs.org/sdr/02FDEA00307.md): Flap · failed · May 3, 2002 · N258FE · Boeing 727233 · Leading Edge Slat Control System
  > 02-108 RIGHT INBD LEADING EDGE FLAP #5 FAILED TO RETRACT WHEN FLAPS 2 WAS SELECTED. ** S/D ** COMING
- [SDR 01FDEA00822](https://openairdocs.org/sdr/01FDEA00822.md): Support · cracked · Oct 5, 2001 · N258FE · Boeing 727233 · Trailing Edge Flap Control System
  > N 1137 L/W I/B SPOILER SUPPORT BEAM CRACKED OF I/B END. ** S/D ** COMING
- [SDR 01FDEA00850](https://openairdocs.org/sdr/01FDEA00850.md): Skin · corroded · Sep 18, 2001 · N258FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > N 490 CORROSION ON FUSELAGE SKIN INNER SIDE BS 498, RBL 7, WL 148. R&R SKIN PER EA 7-5330-59857.
- [SDR 01FDEA00851](https://openairdocs.org/sdr/01FDEA00851.md): Stringer · corroded · Sep 18, 2001 · N258FE · Boeing 727233 · Fuselage Main, Structure
  > N 489 STRINGER 28R CORRODED AT BS 498. R&R STRINGER PER SRM 53-10-1 FIG 1.
- [SDR 01FDEA00852](https://openairdocs.org/sdr/01FDEA00852.md): Floorbeam · misdrilled · Sep 17, 2001 · N258FE · Boeing 727233 · Fuselage Main, Floor Beam
  > N 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 01FDEA00840](https://openairdocs.org/sdr/01FDEA00840.md): Shear Tie · corroded · Sep 17, 2001 · N258FE · Boeing 727233 · Fuselage Main, Structure
  > CORRODED SHEAR TIE BS 1110, RBL 10 - 14. REMOVED AND REPLACED SHEAR TIE PER SRM 51-20-1, 51-10-2 & 51-30-2.
- [SDR 01FDEA00838](https://openairdocs.org/sdr/01FDEA00838.md): Floorbeam · corroded · Sep 17, 2001 · N258FE · Boeing 727233 · Fuselage Main, Floor Beam
  > CORROSION (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 01FDEA00839](https://openairdocs.org/sdr/01FDEA00839.md): Floorbeam · corroded · Sep 17, 2001 · N258FE · Boeing 727233 · Fuselage Main, Floor Beam
  > CORROSION (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 01FDEA00837](https://openairdocs.org/sdr/01FDEA00837.md): Frame · dented · Sep 17, 2001 · N258FE · Boeing 727233 · Fuselage Main, Structure
  > N 450 AFT CARGO FRAME DENT AT BS 970, LBL 33. ** S/D ** COMING
- [SDR 01FDEA00528](https://openairdocs.org/sdr/01FDEA00528.md): Damper · faulty · Jul 10, 2001 · N258FE · Boeing 727233 · Autopilot System
  > EXPERIENCED UNCOMMANDED YAW PULLED UPPER RUDDER YAW DAMPER AC & DC CB YAW DISCONTINUED.
- [SDR 01FDEA00030](https://openairdocs.org/sdr/01FDEA00030.md): Circuit Breaker · failed · Jan 20, 2001 · N258FE · Boeing 727233 · Trailing Edge Flap Control System
  > TRAILING 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 0FDEA00478](https://openairdocs.org/sdr/0FDEA00478.md): Uplock · lack of lube · Jul 19, 2000 · N258FE · Boeing 727233 · Landing Gear Position and Warning
  > GEAR 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 00FDEA00404](https://openairdocs.org/sdr/00FDEA00404.md): Engine · failed · Jun 23, 2000 · N258FE · Boeing 727233 · Engine (Turbine/Turboprop)
  > NR 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 99FDEA00507](https://openairdocs.org/sdr/99FDEA00507.md): Controller · malfunctioned · Dec 22, 1999 · N258FE · Boeing 727233 · Cabin Pressure Control System
  > CLIMB 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 OK
- [SDR 99FDEA00180](https://openairdocs.org/sdr/99FDEA00180.md): Wire · out of position · May 14, 1999 · N258FE · Boeing 727233 · Overheat Detection
  > LWR 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 99FDEA00177](https://openairdocs.org/sdr/99FDEA00177.md): Control Unit · malfunctioned · May 12, 1999 · N258FE · Boeing 727233 · Overheat Detection
  > LOWER 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 99FDEA00158](https://openairdocs.org/sdr/99FDEA00158.md): Duct · leaked · Apr 23, 1999 · N258FE · Boeing 727233 · Pneumatic Distribution System
  > 99-95 - 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 I
- [SDR 99FDEA00146](https://openairdocs.org/sdr/99FDEA00146.md): Overheat Light · illuminated · Apr 17, 1999 · N258FE · Boeing 727233 · Overheat Detection
  > LOWER 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 98FDEA00339](https://openairdocs.org/sdr/98FDEA00339.md): Engine · failed · May 12, 1998 · N258FE · Boeing 727233 · Engine (Turbine/Turboprop)
  > ON 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 97FDEA00833](https://openairdocs.org/sdr/97FDEA00833.md): Position Ind · malfunctioned · Nov 14, 1997 · N258FE · Boeing 727233 · Leading Edge Slat Position Indicating System
  > DURING 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. REM
- [SDR 97FDEA00122](https://openairdocs.org/sdr/97FDEA00122.md): Retract Mech · lack of lube · Feb 25, 1997 · N258FE · Boeing 727233 · Landing Gear Retraction/Extension System
  > NOSE 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 KNUC
- [SDR 96FDEA01664](https://openairdocs.org/sdr/96FDEA01664.md): Bonding Jumper · corroded · Nov 11, 1996 · N258FE · Boeing 727233 · Leading Edge Devices
  > NR 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 96FDEA01663](https://openairdocs.org/sdr/96FDEA01663.md): Angle · corroded · Nov 11, 1996 · N258FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > NR 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 96FDEA01666](https://openairdocs.org/sdr/96FDEA01666.md): Bullnose · worn · Nov 9, 1996 · N258FE · Boeing 727233 · Rudder, Plate/Skin
  > NR 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 I
- [SDR 96FDEA01665](https://openairdocs.org/sdr/96FDEA01665.md): Bullnose · worn · Nov 9, 1996 · N258FE · Boeing 727233 · Rudder, Plate/Skin
  > NR 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 R
- [SDR 96FDEA01658](https://openairdocs.org/sdr/96FDEA01658.md): Window Frame · corroded · Nov 6, 1996 · N258FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > NR 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.

Next page: https://openairdocs.org/deregistered/N258FE-2015-08-10/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/deregistered/N258FE-2015-08-10/reports

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