# Service difficulty reports: N284FE, cancelled Dec 19, 2013

A list on [N284FE, cancelled Dec 19, 2013](https://openairdocs.org/deregistered/N284FE-2013-12-19.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 4 · 167 reports

- [SDR FDEA201110264651](https://openairdocs.org/sdr/FDEA201110264651.md): Wire Harness · burned · Oct 26, 2011 · N284FE · Boeing 727233 · Hydraulic Power System Wiring
  > CARGO COMPARTMENT AFT SERVICE LIGHTS C/B POPPED WHILE T/S FOR HYD LEAK IN SERVICE BAY. FOUND WIRE BUNDLE BEHIND B MOD PACK WITH APPROX 5, BURNED WIRES IN IT. PERMANENTLY REPAIRED WIRING IAW SWP TO B PUMP LOW S1 AND 2 OF THE SWITCHES INCLUDING NEW PINS. R &
- [SDR FDEA201110044315](https://openairdocs.org/sdr/FDEA201110044315.md): Battery · inoperative · Oct 4, 2011 · N284FE · Boeing 727233 · Emergency Lighting
  > CAN NOT GET EMERGENCY EXIT LIGHTS TO ILLUMINATE EITHER BY GOING TO ON OR WITH ESS POWER IN STBY. REPLACED BATTERIES ON THE LIGHT ASSY ABOVE FWD ENTRY DOOR. OPS CHECKS GOOD IAW MM 33-50-101-2-0.
- [SDR FDEA201109133873](https://openairdocs.org/sdr/FDEA201109133873.md): Battery Pack · failed · Sep 13, 2011 · N284FE · Boeing 727233 · Emergency Lighting
  > DURING TRANSIT CHECK, FOUND EXTERNAL FWD ENTRY DOOR ESCAPE SLIDE LIGHT INOP. RELAMPED WITH 1619 BULB, NO FIX. R & R EMERGENCY ESCAPE SLIDE LIGHT BATTERY PACK IAW MM REF 33-50-051-2. OPS CHECKED GOOD. OK FOR FLIGHT.
- [SDR FDEA201007212633](https://openairdocs.org/sdr/FDEA201007212633.md): Valve · failed · Jul 21, 2010 · N284FE · Boeing 727233 · Engine Oil Indicating System
  > ON CLIMBOUT NOTICED NR 1 OIL TEMP IN YELLOW RANGE. RAN THE QRH AND AFTER 15 MINUTES WE SHUT DOWN THE NR 1 ENGINE PER THE QRH. OPERATED NR 1 ENG FUEL HEAT SWITCH VALVE NO INDICATION NOTED.VISUALLY CHECKED FUEL HEAT VALVE, FOUND OPEN.REMOVED AND REPL ACED V
- [SDR FDEA201006152014](https://openairdocs.org/sdr/FDEA201006152014.md): Fire Warning · false activation · Jun 15, 2010 · N284FE · Boeing 727233 · Smoke Detection
  > ON CLIMBOUT, GLARESHIELD FIRE WARNING LIGHTS ILLUMINATED DIMLY, FOLLOWED A MINUTE LATER BY AN APU FIRE WARNING LIGHT. FIRE WARNING LIGHTS STAYED ON APPROX 15-20 SECONDS. APU FIRE WARNING REMAINED ON UNTIL IN CHOCKS. PULLED APU FIRE HANDLE, DISCHARGED APU FIR
- [SDR FDEA201003170859](https://openairdocs.org/sdr/FDEA201003170859.md): Actuator · failed · Mar 17, 2010 · N284FE · Boeing 727233 · Leading Edge Slat Actuator
  > NR 1 LED FAILS TO RETRACT BETWEEN 5 AND 2 DEGREES. INSTALLED JUMPER AND NO HELP. AMBER LIGHT STAYED ON IN RETRACT POSITION. R & R NR 1 L/E SLAT ACTUATOR IAW AMM 27-81-032-4. LEAK AND OPS CHECK NORMAL. L/E FLAP LIGHT OUT. RETURN TO SERVICE. PREMATURE REMO
- [SDR FDEA200907102578](https://openairdocs.org/sdr/FDEA200907102578.md): Angle · corroded · Jul 10, 2009 · N284FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > FUSELAGE LWR BODY AT PANEL CUTOUT BTW STA 277 AND STA 351 CORROSION SKIN AND NUTPLATES. REMOVED NUTPLATES AND CORROSION IAW SRM 51-10-6 AND 51-30-2 AND FOUND OUT OF LIMITS IAW SRM 53-10-1 FIG1. REMOVED T-ANGLE AND FABRICATED NEW T-ANGLE IAW DWG NR 65-10936.
- [SDR FDEA200907072515](https://openairdocs.org/sdr/FDEA200907072515.md): Skin · gouged · Jul 7, 2009 · N284FE · Boeing 727233 · Trailing Edge Flaps
  > RT OTBD FOREFLAP WBL 442, GOUGE FWD OF ATTACH FITTING BURNISHED AREA IAW SRM 51-10-1 AND FOUND OUT OF LIMITS IAW SRM 57-50-1 FIG 23. REMOVED FOREFLAP BRACKET FOR ACCESS IAW SRM 51-30-4, FIG 4. CUT DAMAGED AREA IAW SRM 57-50-4, FIG 4 FABRICATED 2 EA DOUBLERS
- [SDR FDEA200906242279](https://openairdocs.org/sdr/FDEA200906242279.md): Seat Track · gouged · Jun 24, 2009 · N284FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN FLOOR SUPPORT GOUGE AT SEAT TRACK STA 1090 NR RBL 24.5. BLENDED OUT DAMAGE AND FOUND OUT OF LIMITS IAW SRM 51-10-1 AND 53-10-1 FIG 3. REMOVED DAMAGED SEAT TRACK AND FABRICATED NEW TRACK SECTION. TREATED AND PRIMED NEW TRACK AND INSTALLED IAW SRM 51-30
- [SDR FDEA200906172140](https://openairdocs.org/sdr/FDEA200906172140.md): Attach Fitting · cracked · Jun 17, 2009 · N284FE · Boeing 727233 · Fuselage Main, Attach Fittings
  > MAIN CABIN UPPER FUSELAGE RT SIDE AT STA 360, STR 7 R AT 9G BULKHEAD ATTACHMENT TO STRINGER - STR 7R IS CRACKED AT LWR END RADIUS. REMOVED FASTENERS ON STRINGER ACESS AND STRAP SUPPORT IAW SRM 51-30-2. STOP-DRILLED CRACK IAW SRM 53-10-3 FIG 2. C/W HFEC-VERIF
- [SDR FDEA200906172139](https://openairdocs.org/sdr/FDEA200906172139.md): Skin · cracked · Jun 17, 2009 · N284FE · Boeing 727200 · Wing, Plate/Skin
  > LT OTBD FORE FLAP WBL 442, CRACK ON CUTOUT FWD OF ATTACH FITTING. TRIMMED OUT CRACKED AREA, DIM 0.100 INCH LENGTH IAW SRM 51-10-1. FOUND WITHIN LIMITS IAW SRM 57-50-1. FIG 3 TREATED AND PRIMED IAW SRM 51-10-2.
- [SDR FDEA200906172134](https://openairdocs.org/sdr/FDEA200906172134.md): Shear Tie · damaged · Jun 17, 2009 · N284FE · Boeing 727200 · Fuselage Internal Mounting Structure
  > FWD PIT- EXTRA HOLE IN SHEAR TIE AT BS 660, BETWEEN STRINGERS 28L AND 27L. REMOVED FASTENERS FOR ACCESS IAW SRM 51-30-2. REMOVED DAMAGED SECTION OF SHEAR TIE IAW SRM 53-10-4 FIG 15. FABRICATED NEW SHEAR TIE IAW SRM 53-10-4 FIG 15. FABRICATED RADIUS FILLER I
- [SDR FDEA200906152116](https://openairdocs.org/sdr/FDEA200906152116.md): Stiffener · misinstalled · Jun 15, 2009 · N284FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > AFT PIT - VERTICAL STIFFENER HAS 3 EACH PLACES WHERE FASTENERS AVE NO EDGE DISTANCE AT BS 1183, LBL 17.8. REPAIRED IAW EA 7-53-126832 - FUSELAGE AD 98-11-03 R1, BS 1183 BULKHEAD, VERTICAL BEAM WITH UNSUFFICIENT FASTENER SPACING AT LBL 20 BELOW WL 190 REPAIR.
- [SDR FDEA200906152115](https://openairdocs.org/sdr/FDEA200906152115.md): Frame · cracked · Jun 15, 2009 · N284FE · Boeing 727200 · Fuselage Main, Frame
  > FWD CARGO AREA, STA 540, STR 21-22L, LWR STUB FRAME EXTENSION, CRACK ON RADIUS. REPAIRED FORWARD CARGO COMPARTMENT LOWER STUB FRAME EXTENSION IAW EA 7-5310-126829.
- [SDR 07FDEA00523](https://openairdocs.org/sdr/07FDEA00523.md): Accessory Unit · failed · Feb 18, 2007 · N284FE · Boeing 727233 · Landing Gear Position and Warning
  > DURING GEAR RETRACTION, AN AUDIO HORN SOUNDS WITH A CORRESPONDING RED GEAR LIGHTS AND RED DOOR LIGHT. NOTE: RED DOOR LIGHT EXTINGUISHES AFTER AN APPROPRIATE TIME. BEFORE TAKEOFF, AIRCREW CYCLED FLAPS TO 30 DEGREES AND BACK TO 15 DEGREES. TRIED SAME SEQU
- [SDR 07FDEA00519](https://openairdocs.org/sdr/07FDEA00519.md): Module · faulty · Feb 17, 2007 · N284FE · Boeing 727233 · Landing Gear Position and Warning
  > ON TAKEOFF WHEN GEAR RETRACTED, RED DOOR AND ALL RED GEAR LIGHTS WITH GEAR WARNING HORN. DOORS LIGHT EVENTUALLY GO OUT, BUT RED GEAR LIGHTS AND AURAL HORN STAYS ON. TROUBLESHOT SYSTEM REF MM 32-61-001-1. REPLACED LGAU MODULE REF MM 32-09-121-4. LANDING GEA
- [SDR 07FDEA00439](https://openairdocs.org/sdr/07FDEA00439.md): Hinge Pin · damaged · Feb 9, 2007 · N284FE · Boeing 727233 · Cargo/Baggage Doors
  > MAIN CARGO DOOR HINGE PIN HAS A.2 INCH GAP BETWEEN THE RETENTION NUT AND WASHER ON THE AFT END OF THE HINGE (PIN CRACKED/BROKEN). INSTALLED NEW HINGE PIN UPON DOOR INSTALL REF MM 52-34-009-4-1 PAGE 1, MM 52-34-009- 5 PAGE 1, NASI SUP FXV-727-MM14 CLASSIFIE
- [SDR 07FDEA00431](https://openairdocs.org/sdr/07FDEA00431.md): Sill · corroded · Feb 9, 2007 · N284FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > FOUND MAIN DECK 1R DR CUTOUT LWR SILL CREASE BEAM SCUFF PLATE IB SUPPORT UPPER FLANGE IS CORRODED. BLENDED CORROSION, HFEC, NO DEFECTS NOTED. ALODINED AND PRIMED, REF EA NR 7-5310-106989, PART 1.
- [SDR 07FDEA00388](https://openairdocs.org/sdr/07FDEA00388.md): Web · tool damage · Feb 8, 2007 · N284FE · Boeing 727233 · Cargo/Baggage Doors
  > MAIN CARGO DOOR UPPER AFT CORNER WEB BS.590-640 HAS MULTIPLE TOOLING MARKS ON INNER SURFACE REMOVED GILL LINER AND PARTIALLY REMOVED INNER SKIN WEB FOR ACCESS. REMOVED REPAIR DOUBLER REF SRM 51-30-2, CUT OUT DAMAGE AREA REF. 51-10-1 HFEC CUT OUT, IAW B727 NDT
- [SDR 07FDEA00387](https://openairdocs.org/sdr/07FDEA00387.md): Intercostal · cracked · Feb 8, 2007 · N284FE · Boeing 727233 · Cargo/Baggage Doors
  > MAIN CARGO DOOR INTERCOSTAL IS CRACKED AT DOME NUT FOR UPPER BOLT TO FORWARD UPPER HOIST ATTACH POINT. INSTALLED NEW INTERCOSTAL REF SRM 51-30-2 PAGE 2 ITEM 4B. CLASSIFIED AS A MAJOR REPAIR.
- [SDR 07FDEA00386](https://openairdocs.org/sdr/07FDEA00386.md): Angle · cracked · Feb 8, 2007 · N284FE · Boeing 727233 · Emergency Exits
  > LT AFT W/W EMERGENCY EXIT HATCH SEAL ANGLE FLANGE HAS 2 CRACKED OUT FASTENERS HOLES ONE LOCATED UPPER SEAL ANGLE, ANOTHER LOCATED LOWER AFT SEAL ANGLE. REMOVED AND REPLACED 1 ANGLE. REMOVED FABRICATED, HEAT TREATED, TREATED AND PRIMED 1 ANGLE REF SRM 51-30
- [SDR 07FDEA00385](https://openairdocs.org/sdr/07FDEA00385.md): Angle · cracked · Feb 8, 2007 · N284FE · Boeing 727233 · Emergency Exits
  > RT FWD O/W EMERGENCY EXIT HATCH SEAL ANGLE UPPER FORWARD CORNER 3 EACH HOLES ARE CRACKED OUT. REMOVED AND REPLACED 1 ANGLE. REMOVED, FABRICATED, HEAT TREATED AND PRIMED 1 ANGLE. REF SRM 51-30-2 PGS 1-7. REPAIR CLASSIFIED AS MAJOR. REF SRM 51-10-2 PAGE 2
- [SDR 07FDEA00384](https://openairdocs.org/sdr/07FDEA00384.md): Angle · cracked · Feb 8, 2007 · N284FE · Boeing 727233 · Emergency Exits
  > RT AFT WO EMERGENCY EXIT HATCH SEAL ANGLE HAS 5 EACH HOLES THAT ARE CRACKED OUT ALONG FWD EDGE OF HATCH. FABRICATED NEW SEAL ANGLE REF DWG 50-7978. TREATED AND PRIMED ANGLE REF SRM 51-10-2 AND MM 51-20-031-7 AND INSTALLED ANGLE REF SRM 51-30-2.
- [SDR 07FDEA00383](https://openairdocs.org/sdr/07FDEA00383.md): Angle · corroded · Feb 8, 2007 · N284FE · Boeing 727233 · Emergency Exits
  > RT FORWARD O/W EMERGENCY EXIT HATCH, 5 EACH SEAL ANGLES ARE CORRODED. VERIFIED ORIGINAL MATERIAL ON ALL 5 ANGLES TO BE.040". THE FOLLOWING ANGLES WERE OUT OF LIMITS: P/N'S 50-7978-65 AT.031", 50-7978-67 AT.029", 50-7978-72 AT.029". ANGLE P/N'S 50-7978
- [SDR 07FDEA00382](https://openairdocs.org/sdr/07FDEA00382.md): Angle · corroded · Feb 8, 2007 · N284FE · Boeing 727233 · Emergency Exits
  > LT AFT OW EMERGENCY EXIT HATCH 5 EACH SEAL ANGLES ARE CORRODED BLENDED 4 EACH SEAL ANGLES AND FOUND WITHIN LIMITS AND TREATED AND PRIMED. REMOVED AND REPLACED 1 EACH SEAL ANGLE REF SRM 51-10-6 PAGE 2, SRM 51-30-2 PAGE 2 AND SRM 51-10-1 PAGE 7.
- [SDR 07FDEA00381](https://openairdocs.org/sdr/07FDEA00381.md): Web · damaged · Feb 8, 2007 · N284FE · Boeing 727233 · Passenger/Crew Doors
  > MAIN ENTRY DOOR L1, INTERNAL SKIN WEB DAMAGED LOCATED AFT EDGE JUST ABOVE 8TH STOP PIN FROM THE TOP. REMOVED DAMAGE, FABRICATED REPAIR PIECES, TREAT, AND PRIMED AND INSTALLED REPAIR PARTS REF SRM 51-40-2. CLASSIFIED AS A MAJOR REPAIR.
- [SDR 07FDEA00363](https://openairdocs.org/sdr/07FDEA00363.md): Seat Track · corroded · Feb 7, 2007 · N284FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK FLOOR SEAT TRACK I/B FLANGE IS CORRODED BS 380-400, LBL 44, WL208 BLENDED CORROSION, ACCOMPLISHED HFEC NO DEFECTS NOTED. FLAP PEENED ALL BLENDED AREAS. ALODINED AND PRIMED, AS NEEDED REF EA NR 7-5310-108847 A.
- [SDR 07FDEA00362](https://openairdocs.org/sdr/07FDEA00362.md): Skin · delaminated · Feb 7, 2007 · N284FE · Boeing 727233 · Trailing Edge Flaps
  > LT IB FOREFLAP AT IB END UPPER SURFACE IS WORN AND DELAMINATED REPAIRED LT IB FOREFLAP REF SRM 51-40-20 PGS 1-63 AND REBONDED RUBSTRIP REF SRM 51-20-4 PGS 1 AND 2. TAP CHECKS GOOD. CLASSIFIED AS A MAJOR REPAIR.
- [SDR 07FDEA00354](https://openairdocs.org/sdr/07FDEA00354.md): Frame · damaged · Feb 6, 2007 · N284FE · Boeing 727233 · Fuselage Main, Frame
  > AFT PIT FRAME AT STA 1148, LOWER CHORD HAS MISDRILLED HOLE JUST BELOW STR 23L REMOVED DAMAGE NDT. NO DEFECTS NOTED, FABBED AND INSTALLED SHEAR TIE ANGLE REPAIR REF SRM 51-30-2 PG 1-12, SRM 51-40-3 PG 2 FIG 1, SRM 53-10-4 PG 46-49 AND BOEING DWG 65-16348. CLA
- [SDR 07FDEA00351](https://openairdocs.org/sdr/07FDEA00351.md): Floor Panel · cracked · Feb 6, 2007 · N284FE · Boeing 727233 · Fuselage Floor Panel
  > LWR AFT CARGO COMPT NR 4 FLOOR PANEL HAS SEVERAL DEEP GOUGES AND IS CRACKED THROUGH AT BS 1035 BL ''0'' CUT SHEETMATAL TO FORM OF OLD FLOOR PNL. JOGGLED EDGED, TRANSFERED FASTENER HOLES FOR PANEL, PRIMED BACK (UNDERSIDE) OF PNL. INSTALLED FASTENERS SECURING
- [SDR 07FDEA00350](https://openairdocs.org/sdr/07FDEA00350.md): Structure · failed · Feb 6, 2007 · N284FE · Boeing 727233 · Wing Main, Frame Structure
  > RT WING INBD T/E WAFFLE BOARD HAS PANEL FASTENERS PULLED THROUGH AT LWR SPAR FLANGE JUST FWD OF MLG MAIN ACTUATOR REMOVED DAMAGE WAFFLE BOARD AND INSTALLED NEW SEAL AND WAFFLE BOARD IN AREA, REF SRM 51-30-2 PG 2-5.
- [SDR 07FDEA00349](https://openairdocs.org/sdr/07FDEA00349.md): Rib · gouged · Feb 6, 2007 · N284FE · Boeing 727233 · Nacelle/Pylon, Frame/Spar/Rib
  > NR 3 ENGINE UPPER COWL 2ND FROM FWD END RIB IS GOUGED ACCOMPLISHED TYPICAL FORMED REPAIR ON NR 3 ENG UPPER COWL REB REF SRM 51-43-3, PG 1-3 FIG 1. REINSTALLED NR 3 ENG UPPER COWL REF MM 71-10-011-4.
- [SDR 07FDEA00348](https://openairdocs.org/sdr/07FDEA00348.md): Stiffener · cracked · Feb 6, 2007 · N284FE · Boeing 727233 · Fuselage Main, Keel
  > LT MLG WHEEL WELL KEEL BEAM STIFFENER IS CRACKED AT BL 0, STA 930, WL 198. REMOVED CRACKED STIFFENER, FABRICATED AND INSTALLED NEW STIFFENER REF SRM 51-30-2 PG 2. CLASSIFIED AS MAJOR REPAIR.
- [SDR 07FDEA00347](https://openairdocs.org/sdr/07FDEA00347.md): Panel · gouged · Feb 6, 2007 · N284FE · Boeing 727233 · Wing, Plate/Skin
  > RT WING INBD TE LWR SURFACE PANEL JUST OB OF MLG FWD TRUNNION, DELAMINATED ON UPPER SURFACE FWD EDGE. OIL SOAKED REMOVED DAMAGED PANEL ASSY. TRIED TO REMOVE DAMAGE REF SRM 51-40-9 PG 4 AND DAMAGE WAS MORE THEN 25% OF PANEL, BEYOND REPAIRABLE LIMITS REF SRM
- [SDR 07FDEA00338](https://openairdocs.org/sdr/07FDEA00338.md): Structure · damaged · Feb 5, 2007 · N284FE · Boeing 727233 · Nacelle/Pylon, Main Frame
  > NR 1 PYLON HOLE ''E'' IS CONICAL IN SHAPE AND ITS MAXIMUM HOLE DIAMETER IS OUT OF LIMITS. NDT HOLE, REAMED, FABRICATED CONICAL WASHER AND INSTALLED WASHER AND FASTENER REF WRI NR 54508487 AND EA NR 7-5450-106973.
- [SDR 07FDEA00337](https://openairdocs.org/sdr/07FDEA00337.md): Floorbeam · corroded · Feb 5, 2007 · N284FE · Boeing 727233 · Fuselage Main, Floor Beam
  > FLT DECK FLOORBEAM AT BS 277 HAS SEVERAL AREAS OF CORROSION ON UPPER SURFACE BETWEEN RBL 13 AND LBL 13. REMOVED CORROSION REF SRM 51-10-1 PG 5, MAT LOSS =.007'' HFEC, ROTO PEENED, TREATED, PRIMED, REF EA NR 7-5310-107610 AND AAR EA NR I070063.
- [SDR 07FDEA00336](https://openairdocs.org/sdr/07FDEA00336.md): Floorbeam · gouged · Feb 5, 2007 · N284FE · Boeing 727233 · Fuselage Main, Floor Beam
  > FLT DECK FLOORBEAM AT BS 277 UPPER SURFACE OF UPPER CHORD GOUGED AT LBL 14.5 BLEND DAMAGE, ORIGINAL THICKNESS.090'' AMOUNT REMAINING 0.075'' HFEC IAW EA# I070063, ROTO PEENED, TREATED, PRIMED, REF FED EX EA NR 7-5310-107610.
- [SDR 07FDEA00332](https://openairdocs.org/sdr/07FDEA00332.md): Floor Support · corroded · Feb 5, 2007 · N284FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > FLT DECK FLOOR SUPPORT UPPER SURFACE CORRODED BETWEEN BS 277-266.75 AT RBL 13 REMOVED CORROSION REF SRM 51-10-1 PG 5. MAT LOSS IS.007''. HFEC IAW AAR EA I070063 REF FED EX EA NR 7-5310-107610/ WO#35039.
- [SDR 07FDEA00331](https://openairdocs.org/sdr/07FDEA00331.md): Skin · dented · Feb 5, 2007 · N284FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > EXTERNAL FUSELAGE, STA 1422 LT SIDE. SKIN DENTED 4.0'' BELOW VERTICAL FIN Y=.080'' A=1.25'' A/Y = 15, REMOVED DAMAGE, FABRICATED REPAIR DOUBLER AND FILLER. INSTALLED REPAIR, REF SRM 51-40-2, PG 1-6.
- [SDR 07FDEA00322](https://openairdocs.org/sdr/07FDEA00322.md): Handle · damaged · Feb 5, 2007 · N284FE · Boeing 727233 · Cargo/Baggage Doors
  > FUSELAGE LOWER LOBE, NR 1 CARGO DOOR EXT HANDLE HAS EXCESSIVE PLAY AT CONTROL ROD FWD END REPLACED DOOR REF MM 52-35-011-4, PG 3 B. OPS CHECKED GOOD.
- [SDR 07FDEA00316](https://openairdocs.org/sdr/07FDEA00316.md): Pan · gouged · Feb 5, 2007 · N284FE · Boeing 727233 · Cargo/Baggage Doors
  > FUSELAGE LOWER LOBE NR 1 CARGO DOOR EXT HANDLE PAN LOWER SIDE IS GOUGED FROM CONTACT WITH CONTROL ROD FWD EYE BOLT AT BS 569 REF N01095. REPLACED DOOR REF MM 52-35-011-4, OPS CHECKED GOOD.
- [SDR 07FDEA00299](https://openairdocs.org/sdr/07FDEA00299.md): Skin · misrepaired · Feb 3, 2007 · N284FE · Boeing 727233 · Leading Edge Devices
  > LT WING NR 4 SLAT REPAIR AT O/B TRACK SKIN DOES NOT CONFORM TO FEDX DWG SR 27-57-034 REMOVED AND REPLACED LT NR 4 SLAT REF MM 27-81-011.
- [SDR 07FDEA00298](https://openairdocs.org/sdr/07FDEA00298.md): Floorbeam · corroded · Feb 3, 2007 · N284FE · Boeing 727233 · Fuselage Main, Floor Beam
  > FOUND MAIN DECK FLOORBEAM UPPER FLANGE IS CORRODED BS 620 LBL 4-20, WL 208. INSTALLED REPAIR ON MAIN DECK FLOORBEAM UPPER CHORD AT STA 620, LBL 4 THRU 20, WL 208 REF B727 SRM 53-10-8 PG 18-23 AND DWG 53FX1547. CLASSIFIED AS A MAJOR REPAIR.
- [SDR 07FDEA00297](https://openairdocs.org/sdr/07FDEA00297.md): Frame · tool damage · Feb 3, 2007 · N284FE · Boeing 727233 · Fuselage Main, Frame
  > MAIN CABIN BS 620 BETWEEN STR S-3L AND S-4L UPPER SILL TO FRAME SPLICE AREA HAS 2. MISDRILLED HOLES AND 1 OVER CHAMFERED HOLE (VIEW FROM AFT SIDE) COMPLIED WITH EA NR 7-5310-106977 (WRI53108462) AND AAR WO NR 11701/2400/0004 PART 1, ITEM 1 THRU 10 ACCOMPLISH
- [SDR 07FDEA00296](https://openairdocs.org/sdr/07FDEA00296.md): Intercostal · tool damage · Feb 3, 2007 · N284FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT BS 1086, JUST ABOVE STRINGER 23R HAS A HOLE DRILLED IN RADIUS. HOLE LOCATED BELOW NUT PLATE ATTACH RIVET. DAMAGED INTERCOSTAL REMOVED NEW PART FABRICATED AND INSTALLED REF BAC DWG 65-56131, SRM 51-30-2, SRM 51-10-2 PG 7. CLASSIFIED AS A MAJOR
- [SDR 07FDEA00295](https://openairdocs.org/sdr/07FDEA00295.md): Web · gouged · Feb 3, 2007 · N284FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > FOUND MAIN DECK FLOOR WEB UPPER SURFACE IS GOUGED BS 617-620, LBL 57-60, SL 208. FABRICATED NEW WEB REF DWG 53FX1565 AND SRM 51-30-2 P3 1-12.
- [SDR 07FDEA00294](https://openairdocs.org/sdr/07FDEA00294.md): Stringer Clip · gouged · Feb 3, 2007 · N284FE · Boeing 727233 · Fuselage Main, Attach Fittings
  > FOUND STRINGER CLIP HAS BEEN GROUND AT RADIUS CUT OUT BS 660 STRINGER 8L. REPLACED STRINGER CLIP, REF SRM 51-30-2 PG 2. CLASSIFIED AS A MAJOR REPAIR.
- [SDR 07FDEA00293](https://openairdocs.org/sdr/07FDEA00293.md): Stringer Clip · cracked · Feb 3, 2007 · N284FE · Boeing 727233 · Fuselage Main, Attach Fittings
  > FOUND STRINGER CLIP CRACKED IN CUT OUT RADIUS AT BS 680 STR 7L. REMOVED AND REPLACED STR CLIP AT STA 680 STR 7L REF SRM 51-30-02 CLASSIFIED AS A MAJOR REPAIR.
- [SDR 07FDEA00292](https://openairdocs.org/sdr/07FDEA00292.md): Stringer Clip · gouged · Feb 3, 2007 · N284FE · Boeing 727233 · Fuselage Main, Attach Fittings
  > STRINGER CLIP HAS BEEN GROUND AT THE RADIUS CUT OUT BS 440 STR 3L REMOVED STR CLIP STA 440 STR 3L. RECEIVED CLEARANCE AND INSTALLED STR CLIP REF SRM 51-30-2 PG 1. CLASSIFIED AS MAJOR REPAIR.
- [SDR 07FDEA00291](https://openairdocs.org/sdr/07FDEA00291.md): Stringer Clip · gouged · Feb 3, 2007 · N284FE · Boeing 727233 · Fuselage Main, Attach Fittings
  > STRINGER CLIP HAS BEEN GROUND AT RADIUS CUT OUT BS 440 STR 1 BLENDED RADIUS ON STR CLIP REF SRM 53-10-4 PG 3. DAMAGE OUT OF LIMITS, REMOVED STR CLIP REF SRM 51-30-2 PG 2. VERIFY MATERIAL FOR FABRICATION OF NEW STR CLIP 7075-T6-.032 (A02779) REF BOEING DW

Next page: https://openairdocs.org/deregistered/N284FE-2013-12-19/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 = 'N284FE' AND deregistration_id = 'N284FE-2013-12-19'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N284FE-2013-12-19/reports

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