# Service difficulty reports: N286FE, cancelled Aug 27, 2013

A list on [N286FE, cancelled Aug 27, 2013](https://openairdocs.org/deregistered/N286FE-2013-08-27.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 6 · 271 reports

- [SDR FDEA201108253475](https://openairdocs.org/sdr/FDEA201108253475.md): Skin · damaged · Aug 25, 2011 · N286FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DAMAGED, INSTALLED REPAIR IAW EA 7-5330-153076 PART 1 AND ATTACHED REPAIR SKETCH.
- [SDR FDEA201106212370](https://openairdocs.org/sdr/FDEA201106212370.md): Turbine Blades · damaged · Jun 21, 2011 · N286FE · Boeing 727233 · Turbine Section
  > SETTING T/O POWER HAD LOUD BANG AND ALL ENG NR 1 INSTRUMENTS DROPPED. REPEATED T/O PRIOR TO T/O. REJECTED T/O PRIOR TO T/O POWER BEING SET. ENG NR1 WAS RUNNING ROUGH AND SMOOTHED OUT AS ENG WOUND DOWN. OPEN COWLING FOUND MASSIVE AMOUNT OF OIL IN COWL. INSP
- [SDR FDEA201009223652](https://openairdocs.org/sdr/FDEA201009223652.md): Battery Pack · inoperative · Sep 22, 2010 · N286FE · Boeing 727233 · Emergency Lighting
  > DURING PRE-DISPATCH CHECKS FOUND FWD ENTRY DOOR ESCAPE LIGHT INOP. DEN R RELEASED FOR SERVICE IAW MEL: 33-16-02-A CATEGORY: B EXPIRATION: 24SEP10 "MEL 33-16-02-A: FWD ESCAPE SLIDE LIGHT - INOP." L/E-LAMPED IAW SMP NO HELP.ITEM IS DEFFERED. R & R EMERGENCY
- [SDR FDEA201003140819](https://openairdocs.org/sdr/FDEA201003140819.md): Valve · unknown · Mar 14, 2010 · N286FE · Boeing 727233 · Engine Bleed Air System
  > SHORTLY AFTER T/O HEARD LOUD POP. OBSERVED FLUCTUATING EPR ON ENG NR 2 WITH OIL TEMP APPROX 115 DEGREES C. RESTARTED NR 2 ENG AT REDUCED POWER SETTING REMAINDER OF FLIGHT WITH NORMAL INDICATIONS INCLUDING NORMAL OIL TEMP. INSPECTED INLET AND EXHAUST OF NR 2
- [SDR FDEA201002090366](https://openairdocs.org/sdr/FDEA201002090366.md): Engine · power loss · Feb 9, 2010 · N286FE · Boeing 727233 · Engine (Turbine/Turboprop)
  > DURING STANDARD PWR TAKEOFF AT 2000 FT, EXPERIENCED SUDDEN VIBRATION IN CTR PEDESTAL ACCOMPANIED BY ABNORMAL NOISE. DISCOVERED RETARDING NR 2 THROTTLE RESOLVED VIBRATION. ALL ENGINE INDICATIONS NORMAL. ENG HAS BEEN APPROVED FOR REMOVAL BY POWERPLANT ENGINE
- [SDR FDEA200910053479](https://openairdocs.org/sdr/FDEA200910053479.md): Stringer · corroded · Oct 5, 2009 · N286FE · Boeing 727233 · Fuselage Main, Longeron/Stringer
  > CORROSION ON OTBD SIDE OF STR 28L BETWEEN STA 490 AND 500. CUT OUT DAMAGED AREA, FABRICATED 2 REPAIR SPLICES, FABRICATED STRINGER FILLERS AND INSTALLED IAW SRM 53-10-3 AND 51-30-2.
- [SDR FDEA200910053478](https://openairdocs.org/sdr/FDEA200910053478.md): Skin · corroded · Oct 5, 2009 · N286FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > CORROSION ON SKIN AT STA 496 OTBD OF STR 28L. CUT OUT DAMAGED AREA, FABRICATED DOUBLER AND INSTALLED REPAIR PARTS IAW SRM 53-30-3, 53-30-2 AND 51-30-2.
- [SDR FDEA200910013455](https://openairdocs.org/sdr/FDEA200910013455.md): Stiffener · cracked · Oct 1, 2009 · N286FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > NLG LT TRUNNION FITTING AFT VERTICAL STIFFNER CRACKED. REMOVED VERTICAL STIFFNER IAW SRM 51-30-2. LOCATED AND DRILLED NEW VERTICAL STIFFNER PN 65-19863-5 PO NR 29105141 IAW SRM 51-30-5. INSTALLED NEW VERTICAL STIFFNER IAW SRM 51-30-2.
- [SDR FDEA200909293427](https://openairdocs.org/sdr/FDEA200909293427.md): Seat Track · corroded · Sep 29, 2009 · N286FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK BS 480 - 380 BL0 IS CORRODED AT I/B FLANGE. FABRICATED NEW SEAT TRACK SECTION FROM BS 380 TO BS 480 BL 0 USING PN BAC 1520-792 PO NR 9006020 APPROX 109.6250 INCH FABRICATED REPAIR SPLICE ANGLES AND REPAIR STRAP IAW SRM 53-10-5 FIG 1, TRE
- [SDR FDEA200909283433](https://openairdocs.org/sdr/FDEA200909283433.md): Support Fitting · missing · Sep 28, 2009 · N286FE · Boeing 727233 · Fuselage Main, Attach Fittings
  > MAIN CABIN SEAT TRACK SUPPORT FITTING MISSING, STA 1183, LBL 24.75. INSTALLED MISSING MAIN CABIN SEAT TRACK SUPPORT FITTING IAW SRM 51-30-2, 51-30-5 AND DWG 65-19606.
- [SDR FDEA200909263456](https://openairdocs.org/sdr/FDEA200909263456.md): Skin · damaged · Sep 26, 2009 · N286FE · Boeing 727233 · Nacelle/Pylon, Plate/Skin
  > NR 2 ENGINE "S" DUCT INLET NOSE COWL CAP HAS DENT AT 8 O'CLOCK POSITION, BS 1101. EVALUATED DENT AND FOUND OUT OF LIMITS, CUT OUT DAMAGED AREA, FABRICATED 2 DOUBLERS AND LIP SKIN FILLER, HEAT TREATED PARTS TO T4 CONDITION AND INSTALLED IAW SRM 54-30-1, 54-
- [SDR FDEA200909253388](https://openairdocs.org/sdr/FDEA200909253388.md): Structure · corroded · Sep 25, 2009 · N286FE · Boeing 727233 · Fuselage Main, Structure
  > NLG WHEEL WELL UPPER STRUCTURE - CORROSION ON MID CHORD UPPER SURFACE AT APPROX STA 350, LT SIDE, ( INSIDE FWD WALKWAY ACCESS). REMOVED CORROSION AND FOUND OUT OF LIMITS, REMOVED CHORD, LOCATED AND DRILLED NEW CHORD PN 5312412 PO NR 29105100 AND INSTALLED IAW
- [SDR FDEA200909243430](https://openairdocs.org/sdr/FDEA200909243430.md): Skin · gouged · Sep 24, 2009 · N286FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > FWD PIT - SKIN GOUGED AT BS 480, AFT SIDE, BETWEEN STRINGERS 27L AND 26L. CUT OUT DAMAGED TEAR STRAP, CUT OUT SKIN, FABRICATED SKIN DOUBLER, TRIPLER, STRUCTURAL FILLER, FILLER, TEAR STRAP REPAIRS AND SHEAR TIE REPAIR, HEAT TREATED PART TO T6 CONDITION IAW
- [SDR FDEA200909233371](https://openairdocs.org/sdr/FDEA200909233371.md): Seat Track · corroded · Sep 23, 2009 · N286FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
  > CORR AT SEAT TRACK LBL 45, STA 852-STA 870 REMOVED OLD SEAT TRACK ON LBL 45 STA 852 TO STA 870 IAW SRM 51-30-2, FABRICATED NEW SEAT TRACK FROM BAC 1520-1466 PO 8205123 DIM: 16 INCHES X 4 INCHES IAW SRM 53-10-2 TREATED AND PRIMED NEW SEAT TRACK IAW SRM 51-10-2
- [SDR FDEA200909223426](https://openairdocs.org/sdr/FDEA200909223426.md): Seat Track · corroded · Sep 22, 2009 · N286FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK BS 440-460, LBL 24 IS CORRODED. REMOVED DAMAGED SEAT TRACK SECTION, FABRICATED ANGLES, ONE STRAP, AND NEW SEAT TRACK SECTION AND INSTALLED PARTS IAW SRM 53-10-5 AND 51-30-2.
- [SDR FDEA200909223350](https://openairdocs.org/sdr/FDEA200909223350.md): Skin · gouged · Sep 22, 2009 · N286FE · Boeing 727233 · Cargo/Baggage Doors
  > MCD DOOR AFT LWR SIDE GOUGED AT OLD REPAIR REMOVED OLD DOUBLER OUT OF LIMITS IAW SRM 51-30-2, FAB NEW DOUBLER USING MAT 301.1/2HD.063 PO NR 29067392, DIM: "8.5 X 4.8750" IAW PF SDMCER 01-049 REV H AND 52-30-2 FIG 2A. PAINTED IAW SRM 51-10-2, INSTALLED NEW DO
- [SDR FDEA200909173428](https://openairdocs.org/sdr/FDEA200909173428.md): Skin · chafed · Sep 17, 2009 · N286FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > FWD ENTRY DOOR FRAME AT BS 303.9, STR 15 AND16 WEB CUT OUTS HAS JAGGED EDGES AND RUBBING AGAINST DOOR STRAP. TRIMMED OUT EDGE UPPER SECTION ON FRAME STR 15L DIM:.063 AND STR 16L DIM:.090 IAW SRM 51-10-1 AND EA 7-5310-126849. HFEC AREA IAW NDTM 51-00-00,
- [SDR FDEA200909173317](https://openairdocs.org/sdr/FDEA200909173317.md): Angle · cracked · Sep 17, 2009 · N286FE · Boeing 727233 · Trailing Edge Flaps
  > LT INBD MID FLAP LWR T/E ON ACT ROD CUTOUT WBL 106 ANGLE IS CRACKED. REMOVED ANGLE CRACKED FROM LT I/B MID FLAP IAW SRM 51-30-2, FABRICATED NEW ANGLE IAW SRM 51-40-4 FIG 1 SRM 57-50-2 FIG 5. INSTALLED NEW ANGLE IAW SRM 51-30-2 SRM 57-20-2 INSTALLED LOWER SKI
- [SDR FDEA200909173363](https://openairdocs.org/sdr/FDEA200909173363.md): Skin · misinstalled · Sep 17, 2009 · N286FE · Boeing 727233 · Fuselage Main, Structure
  > MAIN CARGO AREA, STA 660, STR 4L, ABOVE STRINGER, RIVETS WITH NO SPACING. CUT OUT DAMAGED AREA OF STRAP, FABRICATED DOUBLER, TRIPLER, STRUCTURAL FILLER, 2 FILLERS, TEAR STRAP REPAIR, SHIMS, AND INSTALLED PARTS IAW SRM 51-30-2, 53-30-3, 51-30-5 AND 53-30-
- [SDR FDEA200909173362](https://openairdocs.org/sdr/FDEA200909173362.md): Skin · misinstalled · Sep 17, 2009 · N286FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > MAIN CARGO AREA, STA 660, STR 4L, BELOW STR, RIVETS WITH NO SPACING. CUT OUT DAMAGED AREA OF STRAP DIMS 3 INCHES X 5.5 INCHES, CUT OUT DAMAGED AREA OF SKIN, FABRICATED DOUBLER, TRIPLER, STRUCTURAL FILLER, 2 FILLERS, TEAR STRAP REPAIR, SHIMS, AND INSTALLED PAR
- [SDR FDEA200909173319](https://openairdocs.org/sdr/FDEA200909173319.md): Doubler · gouged · Sep 17, 2009 · N286FE · Boeing 727233 · Leading Edge Devices
  > RT WING INBD FORE FLAP OTBD L/E HAS DEEP GOUGE FROM LONG SCREW IN WING LWR T/E. STOP DRILLED DEEP GOUGE AT RT WING INBD FORE FLAP OTBD L/E IAW SRM 51-10-1 REV 101. HFEC INSPECTED AREA IAW NDTM 51-00-00, FIG 23 PART 6, NO DEFECTS NOTED. FABRICATED REPAIR P
- [SDR FDEA200909173318](https://openairdocs.org/sdr/FDEA200909173318.md): Angle · cracked · Sep 17, 2009 · N286FE · Boeing 727233 · Trailing Edge Flaps
  > RT WING INBD MID-FLAP, AFT LWR CHORD ANGLE IS CRACKED IN 2 PLACES AT WBL 100. REMOVED LWR SKIN PANEL IAW SRM 51-30-2. REMOVED LWR CHORD ANGLE ON IB MID FLAP IAW SRM 51-30-2 REV 101. FABRICATED NEW CHORD ANGLE 5 FT X 1.5 INCHES FROM BAC1503-100046 7075 T6,
- [SDR FDEA200909173316](https://openairdocs.org/sdr/FDEA200909173316.md): Skin · cracked · Sep 17, 2009 · N286FE · Boeing 727233 · Landing Gear Doors
  > RT MLG WING DOOR SKIN CRACKED UNDER UPPER SEAL RETAINER AFT HINGE AREA. REPAIRED MLG WING DOOR IAW EO 7-5280-7-4301 PART 4.
- [SDR FDEA200909163384](https://openairdocs.org/sdr/FDEA200909163384.md): Frame · damaged · Sep 16, 2009 · N286FE · Boeing 727233 · Fuselage Main, Frame
  > AFT PIT BS 1090 FRAME IS PUNCTURED IN THE UPPER FLANGE ABOVE STR 27L. CUT-OUT DAMAGED AREA IAW SRM 51-10-1 REV 101. FABRICATED REPAIR DOUBLER IAW SRM 51-40-3 FIG 1. HEAT TREATED 7075-0 TO T6 CONDITION IAW ER 2-37153-801 REV A. CW CONDUCTIVITY TEST IAW NDTM
- [SDR FDEA200909163434](https://openairdocs.org/sdr/FDEA200909163434.md): Support Fitting · missing · Sep 16, 2009 · N286FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK SUPPORT FITTING MISSING, STA 1183, RBL 24.75. INSTALLED MISSING MAIN CABIN SEAT TRACK SUPPORT FITTING PART IAW SRM 51-30-2, 51-30-5 AND DWG 65-19606.
- [SDR FDEA200909163431](https://openairdocs.org/sdr/FDEA200909163431.md): Seat Track · corroded · Sep 16, 2009 · N286FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AT SEAT TRACK STA 740 TO STA 870, LBL 24. REMOVED OLD SEAT TRACK, FABRICATED NEW SEAT TRACK AND INSTALLED IAW DWG 65-16279 AND SRM 51-30-2.
- [SDR FDEA200909163383](https://openairdocs.org/sdr/FDEA200909163383.md): Frame · punctured · Sep 16, 2009 · N286FE · Boeing 727233 · Fuselage Main, Frame
  > AFT PIT BS 1050 FRAME PREVIOUS REPAIR DOUBLER IS PUNCTURED ABOVE STR 27R. REMOVED PREVIOUS REPAIR DOUBLER, FABRICATED NEW DOUBLER, HEAT TREATED DOUBLER TO T-6 CONDITION IAW FASI FORM 2-37153- 801 REV A, AND INSTALLED IAW SRM 51-40-3, 53-10-2 AND 51-30-2.
- [SDR FDEA200909153429](https://openairdocs.org/sdr/FDEA200909153429.md): Skin · gouged · Sep 15, 2009 · N286FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > MAIN CARGO AREA, STA 620-640, STR 4L, INNER SKIN HAS DEEP GOUGE. CUT OUT DAMAGED AREA, FABRICATED REPAIR DOUBLER AND FILLER AND INSTALLED PARTS IAW SRM 51-10-1 AND EA 7-5310-126850.
- [SDR FDEA200909153345](https://openairdocs.org/sdr/FDEA200909153345.md): Skin · damaged · Sep 15, 2009 · N286FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > LT SIDE OF FUSELAGE, OUTER SKIN, SCRATCHES BETWEEN STA 1070 TO STA 1130, AND STR 23L TO STR 27L. REPAIRED LT SIDE OF FUSELAGE OUTER SKIN STA. 1086 TO 1097 BETWEEN STR 24L TO 25L IAW SRM 53-30-3 FIG 1 REV 101, 53-30-3, FIG 1, AND 51-30-2..
- [SDR FDEA200909123346](https://openairdocs.org/sdr/FDEA200909123346.md): Web · cracked · Sep 12, 2009 · N286FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > AFT AIRSTAIR STA 1275 LIGHTNING HOLE LT SIDE OF AIRSTAIR CRACKED. TRIMMED OUT DAMAGED AREA, FABRICATED REPAIR DOUBLER FROM 7075-T6.032 PO NR 9008186 APPROX DIM: 4 INCHES X 2.3750 INCHES AND INSTALLED NEW REPAIR DOUBLER AT BS 1275 LH AFT AIRSTAIR WEB IAW SRM 5
- [SDR FDEA200909123315](https://openairdocs.org/sdr/FDEA200909123315.md): Spar · cracked · Sep 12, 2009 · N286FE · Boeing 727233 · Trailing Edge Flaps
  > RT WING LWR T/E, FALSE SPAR IS CRACKED AT INBD END, WBL 118. REMOVED LWR CHORD SECTION IAW DWG 27-57-038 REV C & DOUBLER IAW DWG SR27-57-038 REV C. TRIMMED OUT INBD AREA IAW DWG SR27-57-038, REV C & FABRICATED 2 ANGLES & HEAT TREATED ANGLES TO T6 IAW ER NR 2
- [SDR FDEA200909123314](https://openairdocs.org/sdr/FDEA200909123314.md): Spar · cracked · Sep 12, 2009 · N286FE · Boeing 727233 · Trailing Edge Flaps
  > LT WING LOWER T/E, FALSE SPAR IS CRACKED AT INBD END, WBL 118. REMOVED DOUBLER, CUT-OUT LOWER CHORD, FABRICATED NEW WEB, 2 EACH ANGLES, NEW LWR CHORD, NEW DOUBLER, STRAPS, 2 FILLERS AND INSTALLED PARTS IAW DWG SR27-57-038 REV C.
- [SDR FDEA200901100120](https://openairdocs.org/sdr/FDEA200901100120.md): Valve · failed · Jan 10, 2009 · N286FE · Boeing 727233 · Hydraulic Pump (Electric/Engine), Main
  > TOTAL LOSS OF A HYDRAULICS UPON GEAR RETRACTION, (LEVEL AND PRESSURE 0). A PUMPS RAN AMAX OP 3 MINS BEFORE SHUTOFF. REMOVED AND REPLACED LT GEAR LOCK SEQUENCE VALVE IAW MM 32-32-031-4. PERFORMED GEAR SWING IAW AMM 32-32-00-005. REMOVED BOTH NR1 AND NR 2 HY
- [SDR 07FDEA03255](https://openairdocs.org/sdr/07FDEA03255.md): Skin · corroded · Aug 30, 2007 · N286FE · Boeing 727233 · Elevator, Plate/Skin
  > RT HORIZONTAL STAB ELEVATOR, OB MOST UPPER SURFACE STATIC WICK. CORROSION ON SKIN SURFACE, AROUND AND UNDER STATIC WICK BASE, AND ON WICK BASE ALSO REMOVED CORROSION ON UPPER RT OUTBOARD ELEVATOR STATIC WICK, FOUND TO BE OUT OF LIMITS BY NDT. MATERIAL LOSS
- [SDR 07FDEA03241](https://openairdocs.org/sdr/07FDEA03241.md): Seat Track · damaged · Aug 30, 2007 · N286FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
  > UPPER MAIN DECK FLOOR STRUCTURE, UPPER BEAM CAP HAS MULTIPLE DRILL HOLES UNDER REMOVED SEAT TRACK STA 1166, RBL 25. INSTALLED TWO FREEZE PLUGS IN 1166 FLOORBEAM. PLUG TWO HOLES IN 1166 FLOORBEAM. DRILLED TWO HOLES IN 1166 FLOORBEAM. DRILLED TWO TO BLUE
- [SDR 07FDEA03231](https://openairdocs.org/sdr/07FDEA03231.md): Floorbeam · corroded · Aug 29, 2007 · N286FE · Boeing 727233 · Fuselage Main, Floor Beam
  > AFT UPPER MAIN DECK, CORROSION ON UPPER SURFACE OF UPPER T- CAP ON FLOOR BEAM, STA 950, LBL 10.5 AND LBL 21". REMOVED CORROSION FROM SURFACE ON UPPER T-CAP REF SRM 51-10-01. REMOVED SEAT TRACK SRM 51-30-2. REMOVED WEB SUPPORT AND BRACKET AT 950. REMOVED TW
- [SDR 07FDEA03175](https://openairdocs.org/sdr/07FDEA03175.md): Stringer · damaged · Aug 28, 2007 · N286FE · Boeing 727233 · Fuselage Main, Longeron/Stringer
  > BS 740, VERTICAL ANGLE AND BULKHEAD SKIN, ABOVE STR S-28 HAS 2 EA PLUG RIVETS THROUGH ALL PARTS (PREVIOUS DAMAGE) ACCOMPLISHED WORK INSTRUCTION ON EA NR 7-5310-11068 FOR REPAIR OF 2 (EA) PLUG RIVETS THROUGH VERTICAL ANGLE, AND BULKHEAD.
- [SDR 07FDEA03123](https://openairdocs.org/sdr/07FDEA03123.md): Skate Angle · cracked · Aug 25, 2007 · N286FE · Boeing 727233 · Trailing Edge Flaps
  > LT WING IB TE NR 3 FLAP TRACK FWD FRG IB SKATE ANGLE IS CRACKED AT 2 WING SKIN FASTENERS WBL 199, 3" FWD AND AFT OF SPAR. REPAIRED NR 3 FLAP TRACK SKATE ANGLE IAW B 272-200 SRM 51-40-3 AND 51-30-2. ALL LEAK CK'S GOOD. THIS IS CLASSIFIED AS A MINOR REPAIR.
- [SDR 07FDEA03124](https://openairdocs.org/sdr/07FDEA03124.md): Skin · damaged · Aug 25, 2007 · N286FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > FOUND DOUBLE DRILLED HOLE AT STA 720F PLUS 5", STR 27R IN NEW SKIN. REMOVED DAMAGE, FABRICATED REPAIR FILLER, STRUCTURAL FILLER AND REPAIR DOUBLER. TREATED AND PRIMED ALL REPAIR PARTS. INSTALLED ALL REPAIR PARTS. REF SRM 53-30-3/FIG NR 3/PAGES 12-14, C
- [SDR 07FDEA03122](https://openairdocs.org/sdr/07FDEA03122.md): Frame · corroded · Aug 25, 2007 · N286FE · Boeing 727233 · Fuselage Main, Frame
  > FWD PIT BILGE, BODY FRAME CHORD IS CORRODED, BS 740, STR 27L- 28L, WL149 REMOVED AND REPLACED CHORD ANGLE REF B727 SRM 51-30-02 PG 2 DUE TO CORROSION BEING OUT OF LIMITS REF SRM 727 SRM 51-10-1, CLASSIFIED AS A MAJOR REPAIR.
- [SDR 07FDEA03121](https://openairdocs.org/sdr/07FDEA03121.md): Stringer · cracked · Aug 25, 2007 · N286FE · Boeing 727233 · Fuselage Main, Longeron/Stringer
  > LWR FWD CARGO PIT FUSELAGE STRINGER UPPER O/B FLANGE HAS CRACK, STA 720 PLUS 14.5" STR 25R. REMOVED DAMAGE REF SRM 53-10-3. FABRICATED REPAIR REF SRM 53-10-3 FIG 2, SHEET 2. INSTALLED REPAIR REF 51-30-2 PG 1, PG 1-3, THIS IS CLASSIFIED AS A MAJOR REPAIR.
- [SDR 07FDEA03120](https://openairdocs.org/sdr/07FDEA03120.md): Frame · corroded · Aug 25, 2007 · N286FE · Boeing 727233 · Fuselage Main, Frame
  > LWR FUSELAGE RT SIDE STA 743, RBL 7", SUPPORT FRAME AT IB SIDE OF ACCESS DOOR 3449R IS CORRODED OB SIDE REMOVED BEACON, REMOVED PANELS 3449R AND 3346. CORROSION THROUGH SUPPORT FRAME. REMOVED SUPPORT FRAME. FABRICATED NEW PARTS, ASSEMBLED NEW FRAME. INSTAL
- [SDR 07FDEA03117](https://openairdocs.org/sdr/07FDEA03117.md): Skin · cracked · Aug 25, 2007 · N286FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > FWD ENTRY DOOR CUTOUT, UPPER HINGE CUTOUT REPAIR, 5 HOLES ARE CRACKED NEED EVALUATION PER WIC 53308429 ITEM 5, HOLES ARE CIRCLED IN BLACK. ALSO FUSELAGE SKIN IS CRACKED OUT OF THE MAIN ENTRY DOOR CUTOUT UPPER HINGE ON WO NR 36352/N00076 COMPLIED WITH EA NR 7-
- [SDR 07FDEA03116](https://openairdocs.org/sdr/07FDEA03116.md): Skin · cracked · Aug 25, 2007 · N286FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > FWD ENTRY DOOR CUTOUT, LOWER HINGE REPAIR, 3 HOLES ARE CRACKED. NEED ENGINEERING EVALUATION PER WIC 53308429 ITEM 5. HOLES CIRCLE IN BLACK, ALSO ON NR00077 LT FUSELAGE SKIN IS CRACKED OUT OF THE MAIN ENTRY DOOR CUTOUT LWR HINGE CUTOUT. REPAIR OF LOWER HING
- [SDR 07FDEA03115](https://openairdocs.org/sdr/07FDEA03115.md): Stringer Splice · corroded · Aug 24, 2007 · N286FE · Boeing 727233 · Fuselage Main, Longeron/Stringer
  > AFT PIT BILGE BODY FRAME STR SPLICE IS CORRODED, BS 1008-1012, STR 29L, WL 140. REMOVED STRINGER SPLICE, CLEANED DAMAGE HOLE, HFEC STRINGER, FABRICATED STRINGER SPLICE. FABRICATED STRINGER CLIPS, TREATED AND PRIMED PARTS, PERFORMED HIDDEN DAMAGE INSPECTION.
- [SDR 07FDEA03114](https://openairdocs.org/sdr/07FDEA03114.md): Floor Support · corroded · Aug 24, 2007 · N286FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > FWD CARGO AREA, STA 718, STR 29L, ABOUT LBL 2, FLOOR SUPPORT IS CORRODED ON REPAIR ANGLE REMOVED DAMAGE. FABRICATION REPAIR PART, TREATED AND PRIMED REPAIR PARTS AND INSTALLED. THIS REPAIR IS CLASSIFIED AS MINOR.
- [SDR 07FDEA03113](https://openairdocs.org/sdr/07FDEA03113.md): Stringer Clip · corroded · Aug 24, 2007 · N286FE · Boeing 727233 · Fuselage Main, Attach Fittings
  > FUSELAGE, BS 740, S-27L, 2 STR CLIPS CORRODED REMOVED CLIPS, REMOVED CORROSION AND CLIPS ARE OUT OF LIMITS. FABRICATED NEW CLIPS, TREATED AND PRIMED AND INSTALLED. REF BOEING DOCUMENT DRAWING NR 69-45628/ID NR 0001/FRAME NR 1 CLASSIFIED AS A MAJOR REPAIR.
- [SDR 07FDEA03112](https://openairdocs.org/sdr/07FDEA03112.md): Stringer Clip · corroded · Aug 24, 2007 · N286FE · Boeing 727233 · Fuselage Main, Attach Fittings
  > FWD LWR CARGO PIT BILGE STRINGER TIE, ON PRESSURE BULKHEAD HAS CORROSION, STA 740, STR 27R. REMOVED CORRODED STRINGER TIES, FABRICATED NEW STRINGER TIES, AND INSTALLED. REF BOEING DRAWING NR 69-45628 AND SRM 51-30-02. THIS IS CLASSIFIED AS A MAJOR REPAIR.
- [SDR 07FDEA03111](https://openairdocs.org/sdr/07FDEA03111.md): Angle · cracked · Aug 24, 2007 · N286FE · Boeing 727233 · Fuselage Main, Structure
  > FWD PIT BILGE BODY SKIN STIFFENER IS BUCKLED/CRACKED, BS 720B PLUS 13" 5", IB OF STR 28R, WL 148. REMOVED DAMAGE SUPPORT ANGLE AND INSTALLED NEW SUPPORT ANGLE, REF BOEING DWG NR 65-54577 AND SRM 51-30-2, THIS IS CLASSIFIED AS A MAJOR REPAIR.
- [SDR 07FDEA03099](https://openairdocs.org/sdr/07FDEA03099.md): Angle · corroded · Aug 24, 2007 · N286FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > FWD LOWER CARGO BAY REINFORCING ANGLE DOUBLER AT AT BS 740 BULKHEAD STR S-27R IS CORRODED REMOVED CORRODED REINFORCING ANGLE. REMOVED CORROSION AND ANGLE WAS OUT OF LIMITS. FABRICATED NEW REINFORCING ANGLE ON SNRM NR N01045, 8130 FORM TRACKING 2007-06-143.

Next page: https://openairdocs.org/deregistered/N286FE-2013-08-27/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 = 'N286FE' AND deregistration_id = 'N286FE-2013-08-27'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N286FE-2013-08-27/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.