# Service difficulty reports: N257FE, cancelled Aug 10, 2015

A list on [N257FE, cancelled Aug 10, 2015](https://openairdocs.org/deregistered/N257FE-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 · 89 reports

- [SDR FDEA201303080529](https://openairdocs.org/sdr/FDEA201303080529.md): Battery Pack · inoperative · Mar 8, 2013 · N257FE · Boeing 727233 · Emergency Lighting
  > PERFORMED SERVICE CHECK, L1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED L1 DOOR EMERGENCY EXIT LIGHT BATTERIES, OPS TEST IAW MM33-50-001-2.
- [SDR FDEA201212064255](https://openairdocs.org/sdr/FDEA201212064255.md): Skin · damaged · Dec 6, 2012 · N257FE · Boeing 727233 · Vertical Stabilizer, Plate/Skin
  > ACFT HAS BEEN INVOLVED IN AN ACFT STRIKE, THE RT SIDE OF THE VERTICAL STABILIZER HAS SUSTAINED DAMAGE. INITIAL INSPECTION SHOWS NUMEROUS RIBS AND STIFFENERS BROKEN INTERNAL TO VERTICAL FIN. ALSO, HAS DAMAGED HYD LINES INTERNAL OF STAB, OUTER DAMAGE INCLUDES
- [SDR FDEA201211204106](https://openairdocs.org/sdr/FDEA201211204106.md): Panel · unsecure · Nov 20, 2012 · N257FE · Boeing 727233 · Fuselage Main, Structure
  > IN FLIGHT, ACFT WOULD NOT PRESSURIZE IN AUTO, STANDBY OR MANUAL MODE. WITH ACFT AT 10000 FT PRESSURE CONTROLLER WOULD HOLD ABOUT 7000 FT CABIN ALTITUDE IN MANUAL WITH OUTFLOW VALVE FULLY CLOSED OR IN STANDBY MODE. DURING PRESSURIZATION CHECK, FOUND AIR LEAK
- [SDR FDEA201209203362](https://openairdocs.org/sdr/FDEA201209203362.md): Oxygen Mask · failed · Sep 20, 2012 · N257FE · Boeing 727233 · Crew Oxygen System
  > SECOND OBSERVER OXYGEN MASK FAILED PREFLIGHT CHECK. THE FLOW INDICATOR SHOWED RED DURING TEST. REPLACED SECOND OBSERVER`S OXYGEN MASK, OP CHECKED NORMAL IAW 35-12-000-4.
- [SDR FDEA201206062107](https://openairdocs.org/sdr/FDEA201206062107.md): Slide · unwanted deploy · Jun 6, 2012 · N257FE · Boeing 727233 · Escape Slide
  > FORWARD CARGO SLIDE DEPLOYED FROM DOOR BEING OPENED EXTERNALLY. STOWED SLIDE AS REQUIRED IN REF TO AMM 25-60-015-2. ACFT IS OK FOR SERVICE.
- [SDR FDEA201203291170](https://openairdocs.org/sdr/FDEA201203291170.md): Oil System · leaking · Mar 29, 2012 · N257FE · Boeing 727233 · Turbine Engine Oil System
  > 45 MIN AFTER TAKEOFF NR 3 ENG HAD LOST APPROX 1 GAL DOWN TO 1.5 GALS FROM 2.6 GAL AT TAKEOFF. OIL PRESSURE & TEMP WERE NORMAL ON NR 3. LANDED WITH GAL 1.25 GAL / 42 PSI PRESS / 10C OIL TEMP. ENT BY: 152952 RPT BY: 434068 SHGN 28MAR12 23:57 MEM U OPENE
- [SDR FDEA201108093162](https://openairdocs.org/sdr/FDEA201108093162.md): Stringer · corroded · Aug 9, 2011 · N257FE · Boeing 727233 · Fuselage Main, Longeron/Stringer
  > STRINGER 28L CORRODED BS 540. CUT OUT DAMAGED STRINGER DIM 17 AND 1/4 INCHES LONG IAW SRM 53-10-3 FIG 1. FABRICATED STRINGER REPAIR PARTS IAW SRM 53-10-3 FIG 1 AND 53-10-2 FIG 9. INSTALLED STRINGER REPAIR PARTS IAW SRM 51-30-2 AND 53-10-3 FIG 1.
- [SDR FDEA201108053124](https://openairdocs.org/sdr/FDEA201108053124.md): Skin · dented · Aug 5, 2011 · N257FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > DENT AT FRAME 360 AT STRINGER 19, RT SIDE OF EXTERIOR SURFACE. CUT OUT DAMAGED AREA, FABRICATED 3EA REPAIR FILLERS, REPAIR DOULBER, AND STRUCTURAL FILLER, AND INSTALLED 3EA REPAIR FILLERS, REPAIR DOUBLER, AND STRUCTURAL FILLER AT FRAME BS 360 STR 19R EXTERI
- [SDR FDEA201107303042](https://openairdocs.org/sdr/FDEA201107303042.md): Skin · corroded · Jul 30, 2011 · N257FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > CORROSION UNDER ANTENNA STRUCTUAL DOUBLER STA.550 BETWEEN STR 28 RIGHT AND 28 LEFT REMOVED ANTENNA STRUCTURAL DOUBLER STA 550 BETWEEN STR 28R TO 28L IAW SRM 51-30-2. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-30-01 FIG 1. FABRICATED REPAIR DOUBLE
- [SDR FDEA201107283003](https://openairdocs.org/sdr/FDEA201107283003.md): Floorbeam · cracked · Jul 28, 2011 · N257FE · Boeing 727233 · Fuselage Main, Floor Beam
  > FLOORBEAM HAS CRACK AT LOWER FWD RADIUS BL 0, CRACK DOES NOT EXTEND. BEYOND SECOND FASTENER EITHER SIDE OF BL 0. STOP DRILLED CRACK IN BS 900 FLOORBEAM LWR FWD RADIUS AT BL 0 IAW EO 7-5300-7-2309 G PT 3. FABRICATED REPAIR ANGLE, 2 FILLERS, AND 2 RADIUS FILLE
- [SDR FDEA201107273002](https://openairdocs.org/sdr/FDEA201107273002.md): Structure · cracked · Jul 27, 2011 · N257FE · Boeing 727233 · Trailing Edge Flaps
  > RT WING INBD MID FLAP T/E CHORD CRACKED AT INBD CABLE CONTROL DRUM CUTOUT. CUT OUT DAMAGE TRAILING EDGE CHORD RIGHTHAND WING INBOARD MID FLAP IAW SRM 51-40-4 FIG 3. FABIRCATED LOCATED AND DRILLED NEW CHORD AND SPLICE IAW 51-40-4 FIG 3 AND 57-50-2. INSTALLE
- [SDR FDEA201107232921](https://openairdocs.org/sdr/FDEA201107232921.md): Frame · cracked · Jul 23, 2011 · N257FE · Boeing 727233 · Fuselage Main, Frame
  > RIGHT FRAME, BS 760.95 CRACK IN WEB PILOT HOLE. REPAIRED RT FRAME BS 760.95 IAW EO 7-5310-7-3367 PT 9.
- [SDR FDEA201107232920](https://openairdocs.org/sdr/FDEA201107232920.md): Frame · cracked · Jul 23, 2011 · N257FE · Boeing 727233 · Fuselage Main, Frame
  > RT FRAME BS 760.95, CRACK IN 2ND HOLE ABOVE FLOOR AND CRACK IN 3RD HOLE ABOVE FLOOR. REPAIRED RT FRAME BS 760.95 IAW FED EX EO 7-5310-7-3367 PT9.
- [SDR FDEA201107212887](https://openairdocs.org/sdr/FDEA201107212887.md): Structure · damaged · Jul 21, 2011 · N257FE · Boeing 727233 · Trailing Edge Flaps
  > LT WING OTBD MID FLAP INBD T/E IS CHIPPED. FOUND TO BE UNREPAIRABLE IAW SRM 57-50-1 FIG 3. REMOVED AND REPLACED LT O/B MID FLAP ASSEMBLY IAW AMM 27-51-011-4-0.
- [SDR FDEA201107202847](https://openairdocs.org/sdr/FDEA201107202847.md): Stringer · corroded · Jul 20, 2011 · N257FE · Boeing 727233 · Fuselage Main, Longeron/Stringer
  > STR 28L AT BS 510 HAS CORROSION INSIDE HAT CHANNEL. CUT OUT DAMAGED AREA IAW SRM 53-10-1 FIG.1. FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 53-10-3 FIG.1 AND 53-30-2.
- [SDR FDEA201107202825](https://openairdocs.org/sdr/FDEA201107202825.md): Seat Track · corroded · Jul 20, 2011 · N257FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
  > SURFACE CORROSION ON SEAT TRACK, RBL 26, BS 1170. REMOVED SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED, LOCATED, AND DRILLED NEW SEAT TRACK SECTION IAW SRM 53-10-2 FIG 7A. INSTALLED NEW SEAT TRACK SECTION IAW SRM 51-30-2.
- [SDR FDEA201107202862](https://openairdocs.org/sdr/FDEA201107202862.md): Seat Track · corroded · Jul 20, 2011 · N257FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
  > MULTIPLE AREAS OF CORROSION ON SEAT TRACK FLANGES LBL 26, BS 772-850. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-10-1 FIG 1. REMOVED SEAT TRACK IAW SRM 51-30-2 FABRICATED NEW SEAT TRACK IAW SRM REV 103 51-30-5 AND 53-10-2 FIG 7. INSTALLED NEW SE
- [SDR FDEA201107202855](https://openairdocs.org/sdr/FDEA201107202855.md): Seat Track · corroded · Jul 20, 2011 · N257FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SEAT TRACK AT LBL 24 IS CORRODED ON LWR SURFACE BTWN BS 480-500. REMOVED SEAT TRACK SECTION IAW SRM 51-30-2, FABRICATED NEW SEAT TRACK SECTION AND 2 EA. REPAIR SPLICE ANGLES AND STRAP IAW SRM 53-10-2 FIG 7A, SRM 53-10-5 FIG 1 & 51-30-5. INSTALLED NEW
- [SDR FDEA201107202852](https://openairdocs.org/sdr/FDEA201107202852.md): Frame Splice · cracked · Jul 20, 2011 · N257FE · Boeing 727233 · Fuselage Main, Frame
  > CABIN FRAME SPLICE AT BS 930, STR 14R HAS CRACK INDICATING AT SPLICE. CUT OUT DAMAGED AREA IAW SRM 53-10-4 FIG 1. FABRICATED REPAIR PARTS IAW SRM 53-10 4 FIG 1. INSTALLED REPAIR PARTS IAW SRM 51-30-2 AND 53-10-4 FIG 1
- [SDR FDEA201107202863](https://openairdocs.org/sdr/FDEA201107202863.md): Floorbeam · corroded · Jul 20, 2011 · N257FE · Boeing 727233 · Fuselage Main, Floor Beam
  > SURFACE CORROSION ON FLOORBEAM BS 950D, LBL 20. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-10-1 FIG. 1. CUTOUT DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED REPAIR PARTS IAW SRM 53-10-8 FIG 8.
- [SDR FDEA201107202857](https://openairdocs.org/sdr/FDEA201107202857.md): Seat Track · corroded · Jul 20, 2011 · N257FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SEAT TRACK FLANGE STA 480 - STA 530, RBL 25. REMOVED SEAT TRACK & SPLICE SECTION IAW SRM 51-30-2, FABRICATED NEW SEAT TRACK AND SPLICE ANGLES AND SPLICE STRAP IAW SRM 53-10-2 FIG 7A & SRM 53-10-5 FIG 1 AND INSTALLED NEW SEAT TRACK AND SPLICE PARTS
- [SDR FDEA201107202848](https://openairdocs.org/sdr/FDEA201107202848.md): Seat Track · corroded · Jul 20, 2011 · N257FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
  > MULTIPLE AREAS OF CORROSION ON SEAT TRACK FLANGE LBL 50 BS 780-870. REMOVED DAMAGED SEAT TRACK IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK IAW SRM 53-10-2 FIG 7 AND 51-30-5. INSTALLED NEW SEAT TRACK IAW SRM 51-30-2.
- [SDR FDEA201107202840](https://openairdocs.org/sdr/FDEA201107202840.md): Skin · damaged · Jul 20, 2011 · N257FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > RT SIDE OF FUSELAGE HAS LIGHTNING STRIKE DAMAGE AT BS 580, STRINGER 7R. CUT OUT DAMAGED AREA OF FUSELAGE SKIN IAW SRM REV.103 53-30-3 FIG 3. FABRICATED REPAIR DOUBLER IAW SRM 53-30-3 FIG 3 AND 53-30-2 FIG. 2. INSTALLED REPAIR DOUBLER IAW SRM 53-30-3 FIG 3.
- [SDR FDEA201107202838](https://openairdocs.org/sdr/FDEA201107202838.md): Skin · damaged · Jul 20, 2011 · N257FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > RT SIDE OF FUSELAGE HAS LIGHTNING STRIKE DAMAGE AT BS 690, STRINGER 7R. CUT OUT DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED DOUBLER IAW SRM 51-30-4 FIG. 6 AND 53-30-3 FIG. 1
- [SDR FDEA201107202827](https://openairdocs.org/sdr/FDEA201107202827.md): Skin · damaged · Jul 20, 2011 · N257FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > RT SIDE OF FUSELAGE HAS LIGHTING STRIKE DAMAGE AT BS 265 BELOW STR 4R. CUT OUT DAMAGED AREA, FABRICATED REPAIR PARTS, AND INSTALLED DOUBLER IAW SRM 53-30-3 FIG. 3 AND 53-30-2 FIG. 1.
- [SDR FDEA201107202826](https://openairdocs.org/sdr/FDEA201107202826.md): Floorbeam · corroded · Jul 20, 2011 · N257FE · Boeing 727233 · Fuselage Main, Floor Beam
  > MAIN CABIN BS 1110 FLOORBEAM HAS CORROSION ON UPPER SURFACE BETWEEN BL0 AND LBL26. CUT OUT DAMAGED AREA IAW SRM 53-10-8 FIG. 3, FABRICATED REPAIR PARTS IAW SRM 53-10-8 FIG. 3, AND INSTALLED REPAIR PARTS IAW B727 51-30-2.
- [SDR FDEA201107202858](https://openairdocs.org/sdr/FDEA201107202858.md): Seat Track · corroded · Jul 20, 2011 · N257FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SEAT TRACK FLANGE STA 370-480, LBL 24. REMOVED SEAT TRACK SECTION IAW SRM 51-30-2, FABRICATED NEW SEAT TRACK SECTION IAW SRM 53-10-2 FIG 7A & SRM 53-10-2 FIG 7, INSTALLED SEAT TRACK SECTION IAW SRM 51-30-2 & 51-10-2.
- [SDR FDEA201107202867](https://openairdocs.org/sdr/FDEA201107202867.md): Seat Track · corroded · Jul 20, 2011 · N257FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SEAT TRACK FLANGE STA 383 - 480, LBL 45. REMOVED SEAT TRACK AND SPLICE PARTS AND WEB FOR ACCESS IAW SRM 51-30-2, FABRICATED NEW SEAT TRACK SECTION IAW SRM 53-10-2 FIG 7A, SRM 51-30-5 & 53-10-2 FIG 7, TREATED AND PRIMED, AND INSTALLED SEAT TRACK SECT
- [SDR FDEA201107202866](https://openairdocs.org/sdr/FDEA201107202866.md): Seat Track · corroded · Jul 20, 2011 · N257FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SEAT TRACK FLANGE STA 380 - 480, RBL 45. REMOVED SEAT TRACK SECTION AND FABRICATED NEW SEAT TRACK SECTION AND INSTALLED IAW SRM 51-30-2 AND SRM 53-10-2 FIG 7A.
- [SDR FDEA201107202861](https://openairdocs.org/sdr/FDEA201107202861.md): Seat Track · corroded · Jul 20, 2011 · N257FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SEAT TRACK SPLICE PLATE BS 480-498, LBL 45. FOUND SEAT TRACK SPLICE AND SEAT TRACK SECTION OUT OF LIMITS IAW SRM REPORT 2489. REMOVED SEAT TRACK SECTION AND SPLICE PARTS IAW SRM 51-30-2 AND FABRICATED NEW SEAT TRACK SECTION AND SPLICE ANGLES, AND
- [SDR FDEA201107202860](https://openairdocs.org/sdr/FDEA201107202860.md): Seat Track · corroded · Jul 20, 2011 · N257FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SEAT TRACK FLANGE STA 480 - 550, RBL 45. REMOVED SEAT TRACK SECTION AND SPLICE PARTS AFTER FOUND OUT OF LIMITS IAW SRMR 2489 & SRM 51-30-2. FABRICATED NEW SEAT SECTION AND SPLICE PARTS IAW SRM 53-10-2 FIG 7A & SRM 53-10-5 FIG 1. INSTALLED NEW SE
- [SDR FDEA201107202856](https://openairdocs.org/sdr/FDEA201107202856.md): Seat Track · corroded · Jul 20, 2011 · N257FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SEAT TRACK FLANGE STA 600 - 720, BL 0. REMOVED OUT OF LIMITS SEAT TRACK IAW SRM REPORT 2489 AND SRM 51-30-2. FABRICATED NEW SEAT TRACK SECTION IAW SRM 53-10-2 FIG 7A AND SRM 51-30-5. INSTALLED NEW SEAT TRACK SECTION IAW SRM 51-30-2.
- [SDR FDEA201107202854](https://openairdocs.org/sdr/FDEA201107202854.md): Seat Track · corroded · Jul 20, 2011 · N257FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SEAT TRACK FLANGE BS 344-390, RBL 25. REMOVED SEAT TRACK SECTION AFTER FOUND OUT OF LIMITS IAW SRM 51-30-2 & SRM REPORT 2489, FABRICATED NEW SEAT TRACK SECTION IAW SRM 53-10-2 FIG 7A, INSTALLED NEW SEAT TRACK SECTION IAW SRM 51-30-2.
- [SDR FDEA201107202853](https://openairdocs.org/sdr/FDEA201107202853.md): Seat Track · corroded · Jul 20, 2011 · N257FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SEAT TRACK FLANGE STA 480-600, BL 0. REMOVED OUT OF LIMITS SEAT TRACK IAW SRM 51-30-2 AND SRM 2489. FABRICATED NEW SEAT TRACK SECTION IAW SRM 53-10-2 FIG 7A AND SRM 51-30-5. INSTALLED NEW SEAT TRACK IAW SRM 51-30-2.
- [SDR FDEA201107202865](https://openairdocs.org/sdr/FDEA201107202865.md): Beam · misinstalled · Jul 20, 2011 · N257FE · Boeing 727233 · Fuselage Main, Structure
  > AFT PIT BS 1183 VERTICAL BEAM LBL 17.8 SEVERAL FASTENERS HAVE LOW SPACING. TRIMMED OFF BEAM AFT FLANGE AND WEB, FABRICATED REPAIR PARTS, TREATED, PRIMED AND INSTALLED IAW EA 7-5310-136787.
- [SDR FDEA201107202846](https://openairdocs.org/sdr/FDEA201107202846.md): Skin · corroded · Jul 20, 2011 · N257FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > BS 510 BL 0 IN FWD CARGO BAY FUSELAGE SKIN HAS CORROSION AROUND ANTENNA DOUBLER. REMOVED ANTENNA STRUCTURAL DOUBLER BS 510, BL 0 IAW SRM 51-30-2. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-30-01, FIG 1, FABRICATED REPAIR DOUBLER IAW EA 7-5330-1541
- [SDR FDEA201107202841](https://openairdocs.org/sdr/FDEA201107202841.md): Stringer · corroded · Jul 20, 2011 · N257FE · Boeing 727233 · Fuselage Main, Longeron/Stringer
  > STR 28L AT BS 510 HAS CORROSION INSIDE HAT CHANNEL. CUT OUT DAMAGED AREA IAW SRM 53-10-1 FIG 1. FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 53-10-3 FIG 1 AND 53-30-2.
- [SDR FDEA201107202839](https://openairdocs.org/sdr/FDEA201107202839.md): Frame · dented · Jul 20, 2011 · N257FE · Boeing 727233 · Fuselage Main, Frame
  > BS 500 FRAME DENTED BTWN STR 24R-25R AT UPPER FLANGE. FOUND AREA DENTED AND OUT OF LIMITS IAW SRM 53-10-1 FIGURE 1. TRIMMED OUT DAMAGE, FABRICATED REPAIR FILLER AND REPAIR DOUBLER SPLICE AND INSTALLED IAW EA 7-5310-152426.
- [SDR FDEA201107202824](https://openairdocs.org/sdr/FDEA201107202824.md): Seat Track · corroded · Jul 20, 2011 · N257FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
  > SURFACE CORROSION ON SEAT TRACK BL 0 BS 1140 TO 1180. REMOVED SEAT TRACK IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK IAW SRM 53-10-2, FIG 7A. INSTALLED NEW SEAT TRACK SECTION IAW SRM 51-30-2.
- [SDR FDEA201107192823](https://openairdocs.org/sdr/FDEA201107192823.md): Floorbeam · corroded · Jul 19, 2011 · N257FE · Boeing 727233 · Fuselage Main, Floor Beam
  > SURFACE CORROSION ON TOP OF FLOORBEAM BS 950, RBL 50. REMOVED UPPER TEE CAP IAW SRM 51-30-2. FABRICATED NEW TEE CAP IAW SRM 53-10-2 FIGURE 7 AND SRM 51-30-5. INSTALLED TEE CAP IAW SRM 51-30- 2 AND SRM 51-30-5.
- [SDR FDEA201107192818](https://openairdocs.org/sdr/FDEA201107192818.md): Floorbeam · corroded · Jul 19, 2011 · N257FE · Boeing 727233 · Fuselage Main, Floor Beam
  > SURFACE CORROSION ON FLOORBEAM, LOWER SIDE LBL58, BS 950. FLOORBEAM REPLACED ON NR NOO538.
- [SDR FDEA201107192815](https://openairdocs.org/sdr/FDEA201107192815.md): Frame · damaged · Jul 19, 2011 · N257FE · Boeing 727233 · Fuselage Main, Frame
  > RT FRAME BS 783.95, SECOND AND THIRD HOLE ABOVE FLOOR HAVE DOUBLE DRILLED HOLES. REPAIRED RIGHT HAND FRAME BS 783.95 IAW EA 7-5310-152422.
- [SDR FDEA201107192804](https://openairdocs.org/sdr/FDEA201107192804.md): Keelbeam · cracked · Jul 19, 2011 · N257FE · Boeing 727233 · Fuselage Main, Keel
  > RT KEELBEAM IS CRACKED AT SECOND HAND, THIRD FASTENER, BS 880, RBL 6. REPAIRED RT KEELBEAM AT BS 880 RBL 6 IAW EA 7-5310-152421.
- [SDR FDEA201107192805](https://openairdocs.org/sdr/FDEA201107192805.md): Keelbeam · cracked · Jul 19, 2011 · N257FE · Boeing 727233 · Fuselage Main, Keel
  > LT KEEL BEAM IS CRACKED AT SECOND FASTENER BS 880 LBL 6. REPAIRED LT KEELBEAM BS 880 LBL6 IAW EA 7-5310-152421.
- [SDR FDEA201107192802](https://openairdocs.org/sdr/FDEA201107192802.md): Floorbeam · corroded · Jul 19, 2011 · N257FE · Boeing 727233 · Fuselage Main, Floor Beam
  > CORROSION TOP TEE ON FLOORBEAM STA 620, LBL 45 - 25. CUT OUT DAMAGE IAW SRM 53-10-8 FIG.3. FABRICATED REPAIR PARTS IAW SRM 53-10-8 FIG.3. INSTALLED ALL REPAIR PARTS IAW SRM 51-30-2
- [SDR FDEA201107192807](https://openairdocs.org/sdr/FDEA201107192807.md): Skin · damaged · Jul 19, 2011 · N257FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > LT SIDE OF FUSELAGE SKIN IS DENTED AND CHAFED AT LAP SEAM BS 950, PLUS 10", STRINGER 26L. CUT OUT DAMAGE AREA IAW SRM 53-30-3 FIG.14. FABRICATED REPAIR PARTS DOUBLER AND STRUCTURAL FILLER IAW SRM 53-30-3 FIG.14 AND 53-30-2 FIG.2. INSTALLED DOUBLER AND STRUC
- [SDR FDEA201107192803](https://openairdocs.org/sdr/FDEA201107192803.md): Floorbeam · corroded · Jul 19, 2011 · N257FE · Boeing 727233 · Fuselage Main, Floor Beam
  > CORROSION TOP TEE CAP FLOORBEAM STA 380, RBL 25 - RBL 45. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-10-1 FIG. 4B. FABRICATED REPAIR PARTS AND REPAIRED TOP TEE CAP OF FLOORBEAM BS 380 IAW SRM 53-10-8 FIG. 3 AND 51-30-2.
- [SDR FDEA201107192999](https://openairdocs.org/sdr/FDEA201107192999.md): Skin · damaged · Jul 19, 2011 · N257FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > RT SIDE OF FUSELAGE HAS LIGHTNING STRIKE DAMAGE AT BS 198, STR 13 R. CUTOUT DAMAGED AREA IAW SRM 53-30-3 FIG 13, FABRICATED DOUBLERS & FILLERS IAW SRM 53-30-3 FIG 13 & 53-30-2 FIG 1. INSTALLED REPAIR PARTS IAW SRM 51-30-2 AT RT SIDE OF FUSELAGE AT BS 198 AND
- [SDR FDEA201107192821](https://openairdocs.org/sdr/FDEA201107192821.md): Floorbeam · corroded · Jul 19, 2011 · N257FE · Boeing 727233 · Fuselage Main, Floor Beam
  > SURFACE CORROSION TOP OF FLOORBEAM, BS 950F, LBL 18. CUTOUT DAMAGED AREA IAW SRM 53-10-8 FIG 3 AND FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-10-8 FIG 3.
- [SDR FDEA201107192819](https://openairdocs.org/sdr/FDEA201107192819.md): Seat Track · corroded · Jul 19, 2011 · N257FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
  > SURFACE CORROSION ON SEAT TRACK RBL 26, BS 870 AND 950. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-10-1 FIG 3 AND REMOVED SEAT TRACK SECTION IAW SRM 51-30-2, FABRICATED NEW SEAT TRACK SECTION IAW SRM 53-10-2 FIG 7 & SRM 51-30-5, AND INSTALLED NEW

Next page: https://openairdocs.org/deregistered/N257FE-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 = 'N257FE' AND deregistration_id = 'N257FE-2015-08-10'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N257FE-2015-08-10/reports

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