# Service difficulty reports: N495FE, cancelled Aug 21, 2014

A list on [N495FE, cancelled Aug 21, 2014](https://openairdocs.org/deregistered/N495FE-2014-08-21.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 3 · 116 reports

- [SDR FDEA201305110972](https://openairdocs.org/sdr/FDEA201305110972.md): Slide · loose · May 11, 2013 · N495FE · Boeing 727227 · Escape Slide
  > L1 MAIN ENTRY DOOR SLIDE WAS FOUND LOOSE IN THE SLIDE COVER. REMOVED & REINSTALLED L1 DOOR SLIDE ASSY IAW AMM 25-60-015-2. OK FOR SERVICE.
- [SDR FDEA201201200279](https://openairdocs.org/sdr/FDEA201201200279.md): Control Unit · failed · Jan 20, 2012 · N495FE · Boeing 727227 · Fire Detection
  > AT ALTITUDE, RECEIVED WHEELWELL LIGHT & BELL, PERFORMED PHASE 1, LOWERED GEAR & OPENED MAIN GEAR DOORS, LIGHT REMAINED ON, ON TEST, BELL DID NOT SOUND. AFTER ACFT PULL IN THE GATE, INSPECTED WHEEL WELL TIRES AND BRAKES NO DISCREPANCY FOUND. INSPECTED FIRE
- [SDR FDEA201201190271](https://openairdocs.org/sdr/FDEA201201190271.md): Controller · malfunctioned · Jan 19, 2012 · N495FE · Boeing 727227 · Overheat Detection
  > PRIOR TO TAKEOFF, WHEEL WELL FIRE LIGHT AND BELL CAME ON INTERMITTENTLY APPROX 5 TIMES. AFTER WHICH WHEEL WELL FIRE WARNING WOULD NOT TEST. CHECKED MLG WW WIRING & SENSING ELEMENTS IAW WDM 26-12-01 & MM 26-12-001, ALL CHECKED GOOD. POWER & GROUND TO FIRE &
- [SDR FDEA201106302504](https://openairdocs.org/sdr/FDEA201106302504.md): Frame · damaged · Jun 30, 2011 · N495FE · Boeing 727227 · Fuselage Main, Frame
  > AFT PIT STA 990, STR 26R HAS (3) RIVETS GROUPED TOGETHER IN FRAME. REPAIRED AFT PIT BS990 STRINGER 26R FRAME WEB AND LOWER CHORD IAW EA 7-5310-153050.
- [SDR FDEA201106292496](https://openairdocs.org/sdr/FDEA201106292496.md): Skin · gouged · Jun 29, 2011 · N495FE · Boeing 727227 · Fuselage Main, Plate/Skin
  > INNER SURROUND SKIN GOUGED NUMEROUS PLACES STA 620 - 640, S4-10L. REMOVED INNER SKIN IAW SRM 51-30-2. FABRICATED INNER SKIN IAW SRM 53-10-2, FIG 3A AND DWG 53FX1551. INSTALLED MCD AFT UPPER INNER SKIN IAW SRM 51-30-2.
- [SDR FDEA201106292495](https://openairdocs.org/sdr/FDEA201106292495.md): Floorbeam · corroded · Jun 29, 2011 · N495FE · Boeing 727227 · Fuselage Main, Floor Beam
  > MAIN CABIN, FLOORBEAM UPPER SURFACE HAS EXFOLIATION CORROSION AT BS 950, BTW LBL 24.75 AND LBL 45.50. REMOVED TEE SECTION OF FLOORBEAM IAW SRM 51-30-2. FABRICATED, LOCATED, AND DRILLED NEW TEE SECTION IAW SRM 51-30-5. INSTALLED TEE SECTION IAW SRM 51-30-2
- [SDR FDEA201106272451](https://openairdocs.org/sdr/FDEA201106272451.md): Skin · damaged · Jun 27, 2011 · N495FE · Boeing 727227 · Fuselage Main, Plate/Skin
  > 3 HOLES AT STR 26L INBD SIDE, STA 480. REPAIRED FUSELAGE SKIN AT BS 480 STRINGER 26LEFT IAW EA 7-5330-136776
- [SDR FDEA201106272449](https://openairdocs.org/sdr/FDEA201106272449.md): Frame · cracked · Jun 27, 2011 · N495FE · Boeing 727227 · Fuselage Main, Frame
  > FWD LOWER CARGO COMPARTMENT BS 680 FRAME HAS A DENT AT STRINGER 24R REWORKED DENTED AREA AND FOUND CRACKED AND OUT OF LIMITS IAW SRM 53-10-1, FIGURE 1, CUTOUT DAMAGE ( 1.5" X 1") AND FABRICATED REPAIR ANGLE FROM 7075-0 0.063 DIM 12.2500" X 3" IAW SRM 51-40
- [SDR FDEA201106272450](https://openairdocs.org/sdr/FDEA201106272450.md): Seat Track · corroded · Jun 27, 2011 · N495FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SEAT TRACK AT BS 950 TO 950A, RBL 25 HAS CORRODED SPLICE. REMOVED CORRODED SEAT TRACK SPLICES IAW SRM 51-30-2, FABIRCATED 2 EA. NEW SPLICE ANGLES FROM BAC 1503-160122 DIM 15" X 2.5" EACH AND 1 SPLICE STRAP FROM 7075T6 0.0250 DIM 9" X 2" IAW SRM 53-10-5
- [SDR FDEA201106262427](https://openairdocs.org/sdr/FDEA201106262427.md): Angle · cracked · Jun 26, 2011 · N495FE · Boeing 727227 · Leading Edge Devices
  > LT WING NR 1 SLAT HAS CRACKED LOWER ANGLE AT INBD SIDE OF SLAT, OTBD UPPER STOP PAD. REMOVED NR 1 SLAT ANGLE AND FABRICATED NEW ANGLE AND SPLICE. IAW SRM 57-50-2 FIG 2 AND 51-40-4 FIG 1. INSTALLED NEW ANGLE AND SPLICE IAW SRM 51-30-2
- [SDR FDEA201106252421](https://openairdocs.org/sdr/FDEA201106252421.md): Stringer · corroded · Jun 25, 2011 · N495FE · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > STRINGER 28R CORRODED JUST AFT OF E AND E DOOR STA 450. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW IAW SRM 53-10-1, FIG 1 & 51-10-6. REMOVED STRINGER SECTION BS 440 TO BS 469, STR 28R IAW SRM 51-30-2, FABRICATED NEW STRINGER SECTION FROM BAC 1498-138 7075
- [SDR FDEA201106212426](https://openairdocs.org/sdr/FDEA201106212426.md): Floorbeam · corroded · Jun 21, 2011 · N495FE · Boeing 727227 · Fuselage Main, Floor Beam
  > FLOORBEAM, BS 620, BL0 TO LBL 25 UPPER SURFACE HAS CORROSION. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 51-10-6 - FLOORBEAM BS 620 BL 0 - LBL 25. CUTOUT DAMAGE AREA FLOORBEAM IAW SRM 53-10-8 - FABRICATED REPAIR PARTS IAW SRM 53-10-8 FIG 3. TREATED &
- [SDR FDEA201106202350](https://openairdocs.org/sdr/FDEA201106202350.md): Frame · dented · Jun 20, 2011 · N495FE · Boeing 727227 · Fuselage Main, Frame
  > RT SIDE OF FUSELAGE FRAME HAS A DENT AT BS 1030 ABOVE STR 26R. CUTOUT DAMAGED AREA AND FABRICATED REPAIR PARTS IAW SRM 51-40-3 FIG 1. INSTALLED REPAIR PARTS IAW SRM 51-30-2.
- [SDR FDEA201106202424](https://openairdocs.org/sdr/FDEA201106202424.md): Shear Tie · corroded · Jun 20, 2011 · N495FE · Boeing 727227 · Fuselage Internal Mounting Structure
  > AFT PIT STA 990, SHEAR TIE AT STR 30 T0 28R HAS LIGHT SURFACE CORROSION. CUTOUT DAMAGED AREA IAW SRM 51-40-3 FIG 1. FABRICATED REPAIR SHEAR TIE IAW SRM 53-10-4 FIG 11. INSTALLED SHEAR TIE REPAIR IAW SRM 51-30-2.
- [SDR FDEA201106182337](https://openairdocs.org/sdr/FDEA201106182337.md): Seat Track · corroded · Jun 18, 2011 · N495FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT BS 480-680, LBL 45 HAS CORROSION. REMOVED SEAT TRACK BS 480 TO 690 LBL 45 IAW SRM, REV 103, 51-30-2. FABRICATED AND INSTALLED NEW SEAT TRACK AND SPLICES IAW SRM 51-30-2 AND 53-10-5 FIG 1.
- [SDR FDEA201106182336](https://openairdocs.org/sdr/FDEA201106182336.md): Seat Track · corroded · Jun 18, 2011 · N495FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT BL 0 LT FLANGE CORRODED BTWN BS 950D-950F. FOUND OUT OF LIMITS IAW SRM 53-10-1. REMOVED DAMAGED SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED AND INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-10-2 AND SRM 51-30-2.
- [SDR FDEA201106182335](https://openairdocs.org/sdr/FDEA201106182335.md): Seat Track · corroded · Jun 18, 2011 · N495FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT BS 720E-740 BL0 HAS CORROSION. REMOVED SEAT TRACK SECTION IAW SRM 51-30-2 REV 103, FABRICATED NEW SEAT TRACK IAW SRM 53-10-2 FIG7A, INSTALLED NEW SEAT TRACK IAW SRM 51-30-02
- [SDR FDEA201106182334](https://openairdocs.org/sdr/FDEA201106182334.md): Seat Track · corroded · Jun 18, 2011 · N495FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT BS 720A-720B, RBL 45 HAS CORROSION. REMOVED SEAT TRACK SECTION IAW SRM 51-30-2 REV 103. FABRICATED NEW SEAT TRACK IAW SRM 53-10-5 FIG 1. INSTALLED SEAT TRACK SECTION IAW SRM 51-30-2
- [SDR FDEA201106182329](https://openairdocs.org/sdr/FDEA201106182329.md): Seat Track · corroded · Jun 18, 2011 · N495FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT BS 480-690, LBL 25 HAS CORROSION. FOUND OUT OF LIMITS IAW SRM 53-10-1. REMOVED DAMAGED SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED AND INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-10-5 FIG1 AND SRM 51-30-2.
- [SDR FDEA201106172328](https://openairdocs.org/sdr/FDEA201106172328.md): Seat Track · corroded · Jun 17, 2011 · N495FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT BS 690 -740, LBL 25 HAS CORROSION. FOUND OUT OF LIMITS IAW SRM PF 53-30-1 FIG 3A. REMOVED SEAT TRACK SECTION, FABRICATED NEW SEAT TRACK SECTION FROM BAC1520-792 7178-T6511 DIM. 172" LONG IAW SRM 53-10-2 FIG 7. TREATED AND PRIMED NEW SEAT TRACK
- [SDR FDEA201106172327](https://openairdocs.org/sdr/FDEA201106172327.md): Seat Track · corroded · Jun 17, 2011 · N495FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT BS 600 -700 BL0 HAS CORROSION. CORROSION OUT OF LIMITS IAW SRM 53-10-1. REMOVED DAMAGED SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED AND INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-10-2 AND SRM 51-30-2.
- [SDR FDEA201106172325](https://openairdocs.org/sdr/FDEA201106172325.md): Floorbeam · damaged · Jun 17, 2011 · N495FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > UPON REMOVAL OF SEAT TRACK FOUND DOUBLE DRILLED HOLE AT MAIN CABIN FLOORBEAM BS 520, BL 0. CUT OUT DAMAGED AREA DIM 1" X 0.800" AND FABRICATED 2EA REPAIR ANGLES FROM 7075-O 0.090" DIM 15 1/8" X 3" AND 11 1/2" X 2 7/8" AND 1EA REPAIR FILLER FROM 7075-T6 0.12
- [SDR FDEA201106172326](https://openairdocs.org/sdr/FDEA201106172326.md): Seat Track · corroded · Jun 17, 2011 · N495FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT BL0 RT FLANGE CORRODED BETWEEN BS 950F-970. CORROSION OUT OF LIMITS IAW SRM 53-10-1. REMOVED DAMAGED SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED AND INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-10-2 AND SRM 51-30-2.
- [SDR FDEA201106162283](https://openairdocs.org/sdr/FDEA201106162283.md): Frame · corroded · Jun 16, 2011 · N495FE · Boeing 727227 · Fuselage Main, Frame
  > FRAME CORRODED AT BS 1130 AT STR 17R. REMOVED CORROSION IAW SRM 51-10-6. FABRICATED REPAIR PLATE IAW SRM 51-40-3 FIG 1. INSTALLED REPAIR PLATE IAW SRM 51-30-2.
- [SDR FDEA201106162282](https://openairdocs.org/sdr/FDEA201106162282.md): Frame · dented · Jun 16, 2011 · N495FE · Boeing 727227 · Fuselage Main, Frame
  > RT SIDE OF FUSELAGE, FRAME HAS A DENT AT BS 1130 BETWEEN STRINGER 25R AND 26R. CUTOUT DAMAGED AREA, FABRICATED REPAIR ANGLE, AND INSTALLED REPAIR IAW SRM 51-40-3 FIG 1.
- [SDR FDEA201106162307](https://openairdocs.org/sdr/FDEA201106162307.md): Shear Tie · corroded · Jun 16, 2011 · N495FE · Boeing 727227 · Fuselage Internal Mounting Structure
  > BS 950E SHEAR TIE CORRODED STRINGER 28L TO 29L. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 51-10-6 AND 53-10-1 FIG 1. REMOVED SHEAR TIE IAW SRM 51-30-2, FABRICATED NEW SHEAR TIE IAW SRM 53-10-4 FIG 11 AND 53-10-2 FIG 5. HEAT TREATED SHEAR TIE TO T6, L
- [SDR FDEA201106162306](https://openairdocs.org/sdr/FDEA201106162306.md): Seat Track · corroded · Jun 16, 2011 · N495FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT BS 480-690, RBL 45 HAS CORROSION. FOUND OUT OF LIMITS IAW SRM 53-10-1. REMOVED DAMAGED SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED AND INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-10-2 AND SRM 51-30-2.
- [SDR FDEA201106162305](https://openairdocs.org/sdr/FDEA201106162305.md): Seat Track · corroded · Jun 16, 2011 · N495FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT BS 480-600 BL 0 HAS CORROSION. REMOVED SEAT TRACK SECTION IAW SRM51-30-2, REV 103. FABRICATED NEW SEAT TRACK IAW SRM 53-10-2 FIG 7A. INSTALLED SEAT TRACK SECTION IAW SRM 51-30-2.
- [SDR FDEA201106162304](https://openairdocs.org/sdr/FDEA201106162304.md): Seat Track · corroded · Jun 16, 2011 · N495FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT BS 480-690 RBL 25 HAS CORROSION. CORROSION OUT OF LIMITS IAW SRM 53-10-1. REMOVED DAMAGED SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED AND INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-10-2 AND SRM 51-30-2.
- [SDR FDEA201106162303](https://openairdocs.org/sdr/FDEA201106162303.md): Seat Track · corroded · Jun 16, 2011 · N495FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT BS 360-480 RBL 25 HAS CORROSION. CORROSION OUT OF LIMITS IAW SRM 53-10-1. REMOVED SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED AND INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-10-2, 53-42-00-04 AND SRM 51-30-2.
- [SDR FDEA201106162302](https://openairdocs.org/sdr/FDEA201106162302.md): Seat Track · corroded · Jun 16, 2011 · N495FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT BS 380-480 LBL 25 HAS CORROSION. CORROSION OUT OF LIMITS IAW SRM 53-10-1. REMOVED DAMAGED SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED AND INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-10-2 AND SRM 51-30-2.
- [SDR FDEA201106162289](https://openairdocs.org/sdr/FDEA201106162289.md): Seat Track · corroded · Jun 16, 2011 · N495FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT BS 720D-740, RBL 25 HAS CORROSION. CORROSION. CORROSION OUT OF LIMITS IAW SRM 53-10-1. REMOVED DAMAGED SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED AND INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-10-5 FIG1 AND SRM 51-30-2.
- [SDR FDEA201106162288](https://openairdocs.org/sdr/FDEA201106162288.md): Seat Track · corroded · Jun 16, 2011 · N495FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT BS 348-480, BL 0 HAS CORROSION. CORROSION OUT OF LIMITS IAW SRM 53-10-1. REMOVED DAMAGED SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED AND INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-10-2 AND SRM 51-30-2.
- [SDR FDEA201106162287](https://openairdocs.org/sdr/FDEA201106162287.md): Skin · gouged · Jun 16, 2011 · N495FE · Boeing 727227 · Fuselage Main, Plate/Skin
  > GOUGE LWR FUS. STA 410 BELOW STR 23R. BLENDED AREA AND FOUND OUT OF LIMITS IAW SRM 51-10-1 AND 53-30-1. CUT OUT DAMAGED AREA IAW SRM 53-30-3. FABRICATED DOUBLER AND INSTALLED IAW SRM 53-30-3.
- [SDR FDEA201106162286](https://openairdocs.org/sdr/FDEA201106162286.md): Seat Track · corroded · Jun 16, 2011 · N495FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT BS 360-480, LBL 45 HAS CORROSION. CORROSION OUT OF LIMITS IAW SRM 53-10-1. REMOVED DAMAGED SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED AND INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-10-2 AND SRM 51-30-2.
- [SDR FDEA201106162284](https://openairdocs.org/sdr/FDEA201106162284.md): Seat Track · corroded · Jun 16, 2011 · N495FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT BS 360-480, RBL 45 HAS CORROSION. CORROSION OUT OF LIMITS IAW SRM 53-10-1. REMOVED DAMAGED SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED AND INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-10-2 AND SRM 51-30-2.
- [SDR FDEA201106142285](https://openairdocs.org/sdr/FDEA201106142285.md): Frame · dented · Jun 14, 2011 · N495FE · Boeing 727227 · Fuselage Main, Frame
  > ZEE FRAME DENTED AT STA 660 JUST OTBD OF STR 25R. CUTOUT DAMAGE AREA IAW SRM 51-40-3 FIG 1, FABRICATED REPAIR IAW SRM 51-40-3 FIG FIG1, HEAT TREATED REPAIR TO T6 IAW FASI REPORT 2-37153-801 REV A, TREATED & PRIMED REPAIR IAW SRM 51-10-2, INSTALLED REPAIR I
- [SDR FDEA201106142425](https://openairdocs.org/sdr/FDEA201106142425.md): Floorbeam · corroded · Jun 14, 2011 · N495FE · Boeing 727227 · Fuselage Main, Floor Beam
  > FLOORBEAM AT BS 680, LBL 45 TO RBL 25 HAS CORROSION. REMOVED CORROSION, CUTOUT DAMAGED AREA IAW SRM 51-10-6, FABRICATED REPAIR PARTS IAW SRM 53-10-8, INSTALLED REPAIR PARTS IAW SRM 51-30-5, 51-10-2, 51-30- 2.
- [SDR FDEA201106102374](https://openairdocs.org/sdr/FDEA201106102374.md): Skin · dented · Jun 10, 2011 · N495FE · Boeing 727200 · Fuselage Main, Plate/Skin
  > AFT AIRSTAIRS LT TORQUE BOX EXTERIOR SKIN AT STA 1308, LIGHTING CUT-OUT, SKIN HAS DENT AND CRACK ALONG EDGE. CUTOUT DAMAGED AREA & FABRICATED REPAIR DOUBLER IAW SRM 51-40-2 FIG 1 & 53-10-2 FIG 6, TREATED & PRIMED PARTS IAW SRM 51-10-2, INSTALLED REPAIR DOUBLE
- [SDR FDEA200812075102](https://openairdocs.org/sdr/FDEA200812075102.md): Skin · corroded · Dec 7, 2008 · N495FE · Boeing 727227 · Fuselage Main, Plate/Skin
  > BS 1183 TO 1148 AT STR 26L HAS SURFACE CORROSION ON INNER SKIN REMOVED CORROSION AND FOUND OUT OF LIMITS REPAIRED SKIN IAW EA 7-5330-126867.
- [SDR FDEA200812035061](https://openairdocs.org/sdr/FDEA200812035061.md): Skin · damaged · Dec 3, 2008 · N495FE · Boeing 727227 · Fuselage Main, Plate/Skin
  > NUMEROUS FASTENERS WITH IMPROPER ED AND SPACING STA 440 STR'S 8L TO 10L. REPAIRED THE AFFECTED AREA IAW FEDEX EA NR 7-5330-126864, FUSELAGE SKIN AD 98-11-03R1. MCD CUTOUT REINFORCEMENT DOUBLER AND FUSELAGE SKIN LAP JOINT REPAIR AT STA 440, S10L.
- [SDR FDEA200812035063](https://openairdocs.org/sdr/FDEA200812035063.md): Spar · corroded · Dec 3, 2008 · N495FE · Boeing 727227 · Fuselage Main, Structure
  > CORROSION IN NLG LT STRUT DOOR SPAR BOX, APPX FUSELAGE STA 290. REMOVED WEB IAW SRM 51-30-2 AND REMOVED CORROSION IAW SRM 51-10-6. FOUND OUT OF LIMITS IAW SRM 53-10-1 FIG 1. REMOVED 2ND WEB LT AREA FOR ACCESS IAW SRM 51-30-2 AND REMOVED NLG SPAR IAW SRM 51
- [SDR FDEA200812035062](https://openairdocs.org/sdr/FDEA200812035062.md): Skin · corroded · Dec 3, 2008 · N495FE · Boeing 727227 · Fuselage Main, Plate/Skin
  > BS 1183 - 1148 OB AND STR 26L HAS SURFACE CORROSION. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-30-1 FIG 1 AND 2 AND 53-30-2 FIG 2. REPAIRED SKIN IAW EA NR 7-5330-126867 FUSELAGE SKIN AD 98-11-03 R1, STA 1152 STA 1175 STR 26L 65-54583 LAP JOINT UPP
- [SDR FDEA200812035060](https://openairdocs.org/sdr/FDEA200812035060.md): Failsafe · corroded · Dec 3, 2008 · N495FE · Boeing 727227 · Fuselage Main, Frame
  > AFT CARGO COMP BS 950 AT STR 29R OTBD SIDE HAS LEVELING COMPOUND CRACKED, BELOW FAILSAFE. CORROSION ON FAILSAFE BS 950 STR 29R TO STR 28R. REMOVED LEVELING COMPOUND AND FOUND CORROSION OUT OF LIMITS IAW SRM 53-10-1 FIG 1. CUT OUT DAMAGE AREA IAW SRM 51-10-1
- [SDR FDEA200812015024](https://openairdocs.org/sdr/FDEA200812015024.md): Skin · dented · Dec 1, 2008 · N495FE · Boeing 727227 · Service Doors
  > E&E DOOR DENTED & HAS GOUGE MARKS AT LH EDGE OF DOOR EXTERIOR SKIN. DENTS FOUND TO BE OUT OF LIMITS BY MECHANICAL MEANS IAW SRM 52-100-2. CUT OUT DAMAGE (DIMS: 2 1/8 X 1 1/8) IAW SRM 52-00-3 FIG 1. FABRICATED DOUBLER AND FILLER REPAIR IAW SRM 52-00-3 FIG A
- [SDR FDEA200812015028](https://openairdocs.org/sdr/FDEA200812015028.md): Shear Tie · corroded · Dec 1, 2008 · N495FE · Boeing 727227 · Fuselage Internal Mounting Structure
  > NLG W/W WEB AT STA 312 UPPER SECTION OF SHEAR TIE WEB IS CORRODED AT LBL 22. CUT OUT DAMAGE AREA DIM: 5 1/2 BY 4 AND REPAIRED NLG W/W WEB AT STA 312 SHEAR TIE LBL 22 IAW B727 SRM 53-10-4 FIG 11 AND 53-10-2 FIG 1.
- [SDR FDEA200812015027](https://openairdocs.org/sdr/FDEA200812015027.md): Shear Tie · cracked · Dec 1, 2008 · N495FE · Boeing 727227 · Fuselage Internal Mounting Structure
  > NLG W/W SHEAR TIE AT STA 312 BETWEEN STR 24R - 25R IS CRACKED AT BOTTOM HOLE. REMOVED FASTENERS A ND CUT OUT SHEAR TIE IAW B727 SRM 51-30-2 AND 53-10-4 FIG 15. REPAIRED NLG W/W SHEAR TIE AT BS 312 BETWEEN STR 24R AND STR 25R IAW B727 SRM 53-10-4 FIG 15. TRE
- [SDR 08FDEA04942](https://openairdocs.org/sdr/08FDEA04942.md): Skin · eroded · Nov 20, 2008 · N495FE · Boeing 727227 · Nacelle/Pylon, Plate/Skin
  > NR 1 NOSE COWL L/E SKIN AT BOTTOM HAS AREAS OF EROSION AND 3 CRACKS. REMOVED ACCESS PANEL IAW B727 SRM 51-30-2, CUT OUT DAMAGE DIMS 9 3/4 BY 3/4 IAW B727 SRM 54-30-3 FIG 3. FAB DOUBLER MAT 2024T3.050 PO NR 9007861 DIMS 19 3/8 BY 3 1/2 AND FILLER MATERIAL 2
- [SDR 08FDEA04941](https://openairdocs.org/sdr/08FDEA04941.md): Skin · corroded · Nov 20, 2008 · N495FE · Boeing 727227 · Fuselage Main, Plate/Skin
  > AFT CARGO COMP BS 950F - 970 OUTBD OF STR 28L HAS SURFACE CORROSION RUNNING AFT BEHIND INTERCOSTAL. REMOVED FLOOR SUPPORT AND INTERCOSTAL FOR ACCESS IAW SRM 51-30-2. CUT OUT DAMAGE AREA. FABBED DOUBLER REPAIR AND 2 FILLER IAW SRM 53-30-3 FIG 3 AND 53-30-2 F
- [SDR 08FDEA04939](https://openairdocs.org/sdr/08FDEA04939.md): Skin · cracked · Nov 20, 2008 · N495FE · Boeing 727227 · Trailing Edge Flaps
  > RT WING L/E SLAT NR 6 LOWER SURFACE SKIN IS CRACKED AROUND RIVET HOLE. REMOVED RT NR 6 SLAT COVE PNL FOR ACCESS IAW SRM 51-30-2. FABRICATED REPAIR DOUBLE IAW SRM 57-50-3 FIG 1. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED REPAIR IAW SRM 57-50-3 FIG 1, REI

Next page: https://openairdocs.org/deregistered/N495FE-2014-08-21/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 = 'N495FE' AND deregistration_id = 'N495FE-2014-08-21'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N495FE-2014-08-21/reports

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