# Service difficulty reports: N479FE, cancelled Aug 10, 2015

A list on [N479FE, cancelled Aug 10, 2015](https://openairdocs.org/deregistered/N479FE-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 3 · 145 reports

- [SDR FDEA201205231945](https://openairdocs.org/sdr/FDEA201205231945.md): Shaft · worn · May 23, 2012 · N479FE · Boeing 727227 · Passenger/Crew Doors
  > MAIN ENTRY DOOR HARD TO SHUT FROM INSIDE AND NOT POSSIBLE TO CLOSE AND STORE HANDLE FROM OUTSIDE. FOUND ENTRY DOOR HANDLE SPLINE SHAFT WORN. R & R SHAFT IAW MM 52-11-001-5. OPS CHECKED GOOD.
- [SDR FDEA201201170208](https://openairdocs.org/sdr/FDEA201201170208.md): Controller · malfunctioned · Jan 17, 2012 · N479FE · Boeing 727227 · Cabin Pressure Controller
  > UPON LEVELING AT FL360, "CAB ALT" WARNING HORN SOUNDED. CAB ALT WAS 10,000' & CLIMBING. ACCOMPLISHED PHASE 1'S, RAN QRH, & WAS UNABLE TO REMEDY LACK OF PRESSURIZATION. ELECTED TO RETURN. CREW REPORTED DURING DEBRIEF THAT THEY COULD NOT CONTROL THE RT PAC
- [SDR FDEA201201130142](https://openairdocs.org/sdr/FDEA201201130142.md): Sensor · failed · Jan 13, 2012 · N479FE · Boeing 727227 · Elevator Control System
  > DURING CRUISE FLIGHT WITH AUTOPILOT ELEVATOR SERVO "A" ENGAGED, ACFT HAD PITCH OSCILLATIONS GREATER THAN PLUS/MINUS 2 DEGREES INTERMITTENTLY. OSCILLATIONS SEEMED MORE PRONOUNCED DURING TURBULENCE OR WHEN ELEVATOR WAS LOADED IN A TURN. A/P SERVO INDICATOR S
- [SDR FDEA201112075212](https://openairdocs.org/sdr/FDEA201112075212.md): Mechanism · damaged · Dec 7, 2011 · N479FE · Boeing 727227 · Passenger/Crew Doors
  > FWD DOOR ENTRY SEAL DID NOT APPEAR TO SEAL UNTIL PASSING 6000 ALT. FWD ENTRY DOOR WOULD NOT OPEN ON LDL. CREW REPORTED THAT DOOR WAS VERY DIFFICULT TO CLOSE LEAVING LAST STATION AND THAT IT MADE SOME POPPING NOISES WHILE CLIMBING. UPON CREW DEBRIEF DOOR WOUL
- [SDR FDEA201004081100](https://openairdocs.org/sdr/FDEA201004081100.md): Seat Track · gouged · Apr 8, 2010 · N479FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > GOUGED LOBE SEAT TRACK MAIN CABIN BS 681 RBL 62 REMOVED DAMAGED SEAT TRACK FROM ST 660 T0 STA 740 RBL 62 AT EXISTING SPLICES IAW SRM 51-30-2. DRILLED AND DEBURED NEW SEAT TRACK SIZE 80" IAW SRM 51-30-5 AND SRM 53-10-20 FIG 7A. TREATED AND PRIMED PART IAW SRM 5
- [SDR FDEA201004051058](https://openairdocs.org/sdr/FDEA201004051058.md): Stringer · damaged · Apr 5, 2010 · N479FE · Boeing 727227 · Fuselage Main, Longeron/Stringer
  > UPON REMOVAL OF BS 600 FRAME SUPPORT CLIP, FOUND STR 24 L GOUGED AND PUNCTURED. CUT OUT DAMAGED SECTION OF STRINGER 24L AT BS 600, 17.7500" IN LENGTH IAW SRM, REV 102, 51-10-1 AND 53-10-3 FIG 1. FABRICATED STRINGER FILLER USING BAC1498 -142, 7075-T62, 17.75
- [SDR FDEA201004011047](https://openairdocs.org/sdr/FDEA201004011047.md): Frame · cracked · Apr 1, 2010 · N479FE · Boeing 727227 · Fuselage Main, Frame
  > FWD PIT - UPPER SURFACE OF FRAME IS DENTED AT BS 600, ABOVE STRINGER 24 L. REMOVED CRACKED SECTION OF BS 600 FRAME 1" X 2 1/8" ABOVE STR 24L IAW FED EX B727 SRM REV 102 51-10-1 FABRICATED REPAIR DOUBLER FROM 7075 -0.050 X6" X 12" IAW B727 SRM 53-10-2
- [SDR FDEA201003291044](https://openairdocs.org/sdr/FDEA201003291044.md): Rib · cracked · Mar 29, 2010 · N479FE · Boeing 727227 · Wing, Rib/Bulkhead
  > LEFT WING INBD AND OTBD RIBS ARE CRACKED WHERE NR 3 LE SLAT ACTUATOR MOUNTS TO SLAT. REMOVED ACCESS PANEL FOR ACCESS IAW 727 SRM 51-30-2. REMOVED INBD AND OTBD RIBS IAW SRM 51-10-1. LOCATED AND DRILLED NEW INBD RIB SUPPORT PN NR 65-17294U14 PO NR 20013120 A
- [SDR FDEA201003251012](https://openairdocs.org/sdr/FDEA201003251012.md): Skin · dented · Mar 25, 2010 · N479FE · Boeing 727227 · Fuselage Main, Plate/Skin
  > DENT EXTERIOR FUSELAGE BS 1080 STR. 20L. CUT-OUT DAMAGED AREA DIM: 6.5" X 1.75" AND FABRICATED REPAIR DOUBLER SROM 2024T3.063 PO NR 9009362 DIM: 13.5" X 6.4" & STRUCTURAL FILLER FROM 2024T3.050 PO NR 9009327, DIM: 13.5" X 3.5" IAW SRM 53-30-2 FIG 2 & 53-30-3
- [SDR FDEA201003251011](https://openairdocs.org/sdr/FDEA201003251011.md): Skin · dented · Mar 25, 2010 · N479FE · Boeing 727227 · Fuselage Main, Plate/Skin
  > DENTS 3EA EXTERIOR FUSELAGE BS 1042 STR 24R - 25R. DENTS FOUND OUT OF LIMITS IAW B727 SRM 53-30-1 FIG 1. CUT-OUT DAMAGED AREA DIM: 1" X 1" AND FABRICATED REPAIR DOUBLER FROM 2024T3.071 PO NR 9009120 DIM: 8.6" X 6.7" IAW SRM 53-30-2, FIG 2 AND 53-30-3 FIG 1.
- [SDR FDEA201003241020](https://openairdocs.org/sdr/FDEA201003241020.md): Floorbeam · corroded · Mar 24, 2010 · N479FE · Boeing 727227 · Fuselage Main, Floor Beam
  > CORROSION LOWER SURFACE OF UPPER TEE ON FLOORBEAM STA 1110, BETWEEN RBL 45 AND RBL 65. AREA FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1 FIG 4. CUT-OUT DAMAGED AREA OF UPPER TEE DIM: 6" X 2" AND FABRICATED UPPER TEE FROM BAC1505-100617 7075T6, PO NR 29094137 DIM
- [SDR FDEA201003241014](https://openairdocs.org/sdr/FDEA201003241014.md): Skin · dented · Mar 24, 2010 · N479FE · Boeing 727227 · Fuselage Main, Plate/Skin
  > DENT EXTERIOR FUSELAGE BS 297 STR 23L - 24L DENT FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-30-1 FIG 1. CUT-OUT DAMAGED AREA 3.05 INCH BY 1.2 INCH AND FABRICATED AND INSTALLED REPAIR DOUBLER OF 2024T3.050 PO NR 9009378 DIM: 10.5 INCH BY 8.0 INCH AND STRUCTUR
- [SDR FDEA201003231005](https://openairdocs.org/sdr/FDEA201003231005.md): Skin · dented · Mar 23, 2010 · N479FE · Boeing 727227 · Fuselage Main, Plate/Skin
  > DENTS (2 EA) EXTERIOR FUSELAGE BS 1059 STR 25R.
- [SDR FDEA201003221002](https://openairdocs.org/sdr/FDEA201003221002.md): Seat Track · corroded · Mar 22, 2010 · N479FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SEAT TRACK MAIN CABIN BS 1130 - BS 1180 RBL 45. R & R SEAT TRACK SECTION FROM BS1130 - BS 1180 IAW SRM 51-30- 2. FABRICATED SEAT TRACK IAW DWG NO 53FX976, TREATED AND PRIMED PARTS IAW SRM 51-30-2 & DWG 53FX976.
- [SDR FDEA201003180924](https://openairdocs.org/sdr/FDEA201003180924.md): Frame · corroded · Mar 18, 2010 · N479FE · Boeing 727227 · Fuselage Main, Frame
  > AFT PIT HAS SURFACE CORROSION ON FRAME BS 1030 AT STR 27L AND STR 27R. REMOVED CORROSION AT BS 1030 STRINGER 27L IAW SRM 51-10-6. AREA FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. FORMED REPAIR DOUBLER IAW SRM 53-10-2, FIG 5 AND 51-40-3 FIG 1. LOCATED, DR
- [SDR FDEA201003180923](https://openairdocs.org/sdr/FDEA201003180923.md): Frame · corroded · Mar 18, 2010 · N479FE · Boeing 727227 · Fuselage Main, Frame
  > AFT PIT HAS SURFACE CORROSION ON FRAME BS 950D OTBD OF STR 28L. REMOVED CORROSION ON FRAME AT BS 950D AND STR 28L IAW SRM, REV 102, 51-10-6. C/W U.T. THICKNESS ON AREA IAW NDTM, PT 4, 51-00-00 FIG 3, ORIGINAL MATERIAL.063", MATERIAL REMOVED.033", MATERIAL R
- [SDR FDEA201003180922](https://openairdocs.org/sdr/FDEA201003180922.md): Frame · corroded · Mar 18, 2010 · N479FE · Boeing 727227 · Fuselage Main, Frame
  > AFT PIT HAS SURFACE CORROSION ON FRAME AT BS 950B OTBD OF STR 28L. REMOVED CORROSION AT BS 950B STR 28L IAW SRM 51-10-6. AREA FOUND TO BE OUT OF LIMITS IAW SRM REV 102. FORMED REPAIR DOUBLER IAW SRM 51-40-3 FIG 1 & 53-10-2. LOCATED, DRILLED & DEBURRED DOUBL
- [SDR FDEA201003180910](https://openairdocs.org/sdr/FDEA201003180910.md): Sill · gouged · Mar 18, 2010 · N479FE · Boeing 727227 · Fuselage Miscellaneous Structure
  > UPPER SILL WEB GOUGED AT BS 560, STR 4L. REMOVED INNER SKIN AT UPPER SILL IAW SRM 51-30-2. FABRICATED INNER SKIN USING 2024-T3,.090", PO NR 9009093 APROX DIM 88" X 33.75" IAW SRM 53-10-2, FIG 3A AND DWG NR 53FX1551. INSTALLED INNER SKIN AT BS 526 TO BS 61
- [SDR FDEA201003180907](https://openairdocs.org/sdr/FDEA201003180907.md): Seat Track · corroded · Mar 18, 2010 · N479FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION - RBL 45 SEAT TRACK AT STA 1130, LOWER SURFACE. REMOVED SEAT TRACK IAW SRM 53-10-5, FIG 1. FABRICATED NEW SEAT TRACK SECTIONS FROM BAC 15207927178T6511 IAW SRM 53-10-5, FIG 1 SECTION (1) 99" SECTION AND (2) 74.7500". FABRICATED ANGLE SPLICES 4 EA
- [SDR FDEA201003180905](https://openairdocs.org/sdr/FDEA201003180905.md): Floorbeam · corroded · Mar 18, 2010 · N479FE · Boeing 727227 · Fuselage Main, Floor Beam
  > CORROSION - STA 1030 FLOORBEAM UPPER CHORD, UPPER AND LOWER SURFACE, APPROX RBL 9. CUT-OUT DAMAGED AREA 1.8 INCH STA 1030 RBL 8 IAW SRM 53-10-8 FIG 8. FABRICATED REPAIR ANGLES FROM BAC 1490-2888 7075T6 PO NR 29103176 DIM: 13 INCH 1 AND 9 INCH 1 AND FILLER FR
- [SDR FDEA201003180903](https://openairdocs.org/sdr/FDEA201003180903.md): Floorbeam · corroded · Mar 18, 2010 · N479FE · Boeing 727227 · Fuselage Main, Floor Beam
  > FLOORBEAM ABOVE RT MLG WHEEL WELL FWD SURFACE HAS CORROSION AT BS 880, RBL 44. REMOVED CORROSION ON FLOORBEAM BY MECHANICAL MEANS IAW SRM 51-10-6. AREA UT INSPECTED IAW NDTM 51-00-00 FIG 2 PART 4 WITH ORIGINAL MATERIAL OF.100",.002" REMOVED, REMAINING AREA
- [SDR FDEA201003180901](https://openairdocs.org/sdr/FDEA201003180901.md): Seat Track · corroded · Mar 18, 2010 · N479FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ALONG SEAT TRACK MAIN CABIN BS 510 - BS 690 RBL 24. REMOVED CORROSION AT IB FLANGE IAW SRM 51-10-6 FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1 FIG 3 & 53-10-2. REMOVED SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED SEAT TRACK FROM BAC 1520-7927178-
- [SDR FDEA201003180898](https://openairdocs.org/sdr/FDEA201003180898.md): Seat Track · damaged · Mar 18, 2010 · N479FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > MISSING SCREW WITH HOLE ELONGATED AND EVIDENCE OF MISSING MATERIAL SEAT TRACK SPLICE MAIN CABIN BS 720E 10", BL 0. REMOVED DAMAGED AREA OF SEAT TRACK AT BL 0 FROM STA 720-740 IAW SRM 51-30-2. FABRICATED SEAT TRACK SECTION IAW SRM 53-10-5 FIG 1 AND P - F SRM
- [SDR FDEA201003180896](https://openairdocs.org/sdr/FDEA201003180896.md): Seat Track · corroded · Mar 18, 2010 · N479FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SEAT TRACK LOBE SIDE WALL MAIN CABIN BS 610 - BS 620 RBL 45. REMOVED CORROSION IB FLANGE IAW SRM 51-10-6. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1, FIG 3 & 53-10-2. REMOVED SEAT TRACK SECTION SRM 51-30-2. FABRICATED SEAT TRACK SECTION MATERIA
- [SDR FDEA201003180894](https://openairdocs.org/sdr/FDEA201003180894.md): Seat Track · corroded · Mar 18, 2010 · N479FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ALONG WHOLE SEAT TRACK SECTION BS 480 - BS 690 LBL 45. REMOVED SEAT TRACK STA 480 - STA 690 LBL 45 IAW SRM 51-30-2. FABRICATED SEAT TRACK PN BAC 1520-792-7178T 65, PO 9006020, DIM: 204" X 8" STA 480 - 690 AND FABRICATE ANGLE PN 1503-100-122-7178T6,
- [SDR FDEA201003180891](https://openairdocs.org/sdr/FDEA201003180891.md): Seat Track · corroded · Mar 18, 2010 · N479FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ALONG WHOLE SEAT TRACK SECTION MAIN CABIN BS 480- BS 690, LBL 24. EVALUATED AREA FOUND CORROSION AT SEAT TRACK SECTION BS 480 TO BS 700 OUT OF LIMITS IAW SRM 727-200 NOTED 5.4 AND SRM 53-10-5 FIG 1. R & R SEAT TRACK AT LBL 24 FROM BS 480 TO BS 690
- [SDR FDEA201003180889](https://openairdocs.org/sdr/FDEA201003180889.md): Seat Track · corroded · Mar 18, 2010 · N479FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SEAT TRACK SECTION MAIN CABIN BS 360-480 BL 0. CLEANED AREA IAW BSOPM 20-30-03, EVALUATED AREA NO CORROSION NOTED IAW SRM 51-10-1 AT BS 360-440, REMOVED DAMAGED SECTION BS 430-600 IAW SRM 51-30-2 AND FABRICATED NEW SEAT TRACK SECTION FROM BAC 1520-7
- [SDR FDEA201003180886](https://openairdocs.org/sdr/FDEA201003180886.md): Seat Track · corroded · Mar 18, 2010 · N479FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SEAT TRACK MAIN CABIN BS 370 -BS 390 LBL 45. CLEANED AREA IAW BSOPM 20-30-03 AND EVALUATED AREA NO CORROSION NOTED IAW SRM 51-10-1 AT BS 360- BS 399. EVALUATED AREA FROM BS 400 - BS 480 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1 FIG 3 AND SRM -20
- [SDR FDEA201003180884](https://openairdocs.org/sdr/FDEA201003180884.md): Seat Track · corroded · Mar 18, 2010 · N479FE · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SEAT TRACK SECTION MAIN CABIN BS 360 -BS 480 LBL 24. CLEANED AREA FROM BS 360- BS 480 LBL 24 IAW BSOPM 20-30-03. EVALUATED AREA FOUND CORROSION AT BS 380- BS 480 IAW SRM 51-10-1 OUT OF LIMITS IAW SRM 53-10-1 AND SRM 727-200 9G NOT 5.4. REMOVED DAM
- [SDR FDEA201003180880](https://openairdocs.org/sdr/FDEA201003180880.md): Floorbeam · corroded · Mar 18, 2010 · N479FE · Boeing 727227 · Fuselage Main, Floor Beam
  > CORROSION WITH CRACKING/ LIFTED METAL -STA 1130 FLOORBEAM UPPER CHORD FWD FLANGE, LBL 25 - LBL 45. CUT-OUT DAMAGED AREA FROM 1130 FLOORBEAM UPPER CHORD FWD FLANGE IAW SRM 53-10-8 DETAIL III DIM 12.5 INCH LONG. PERFORMED HFEC ON CUT-OUT IAW NDTM 51-00-00 FIG
- [SDR FDEA201003180872](https://openairdocs.org/sdr/FDEA201003180872.md): Floorbeam · corroded · Mar 18, 2010 · N479FE · Boeing 727227 · Fuselage Main, Floor Beam
  > FLOORBEAM ABOVE RT MLG WHEEL WELL FWD SURFACE HAS CORROSION AT BS 880 RBL 44. REMOVED CORROSION ON FLOORBEAM BY MECHANICAL MEANS IAW SRM 51-10-6. AREA UT INSPECTED IAW NDTM 51-00-00 FIG 2, PART 4 WITH ORIGINAL MATERIAL OF.100",.002" REMOVED, REMAINING A
- [SDR FDEA201003180871](https://openairdocs.org/sdr/FDEA201003180871.md): Floorbeam · cracked · Mar 18, 2010 · N479FE · Boeing 727227 · Fuselage Main, Floor Beam
  > MAIN CABIN OVERWING FLOORBEAM T CHORD CRACKED AT LOWER RADIUS RBL 24 BS 760.9. REMOVED DAMAGED CHORD IAW SRM 51-30-2. FABRICATED NEW CHORD FROM BAC1506-1108 MATERIAL 7075T6 PO NR 20013162 DIM: 110" IAW SRM 51-30-5 & 51-10-1 AND DWG 65-16279 REV F DATED 04/19
- [SDR FDEA201003160962](https://openairdocs.org/sdr/FDEA201003160962.md): Support · cracked · Mar 16, 2010 · N479FE · Boeing 727227 · Fuselage, Landing Gear Attach Fittings
  > CRACK RT FWD STIFFNER NLG TRUNNION SUPPORT. REPLACEMENT OF STIFFENER ACCOMPLISHED ON SNRM NR N00463, WORK ORDER NR 00047694.
- [SDR FDEA201003160961](https://openairdocs.org/sdr/FDEA201003160961.md): Support · cracked · Mar 16, 2010 · N479FE · Boeing 727227 · Fuselage, Landing Gear Attach Fittings
  > CRACK RT AFT STIFFNER NOSE TRUNNION SUPPORT. NO WORK ACCOMPLISHED ON THIS WORK CARD. REPLACEMENT OF STIFFENER ACCOMPLISHED ON SNRM NR N00463, WORK ORDER NR 00047694, SDR TRACKING NR 10-0807.
- [SDR FDEA201003160843](https://openairdocs.org/sdr/FDEA201003160843.md): Floorbeam · corroded · Mar 16, 2010 · N479FE · Boeing 727227 · Fuselage Main, Floor Beam
  > FLOORBEAM ABOVE RT MLG WHEEL WELL CORRODED ON FWD SURFACE BS 890, RBL 22 TO RBL 28. CUT-OUT DAMAGED AREA AT BS 890 RBL 22 TO 28 DIM: 4.125" X 2.750" AND 2" X 2.9" IAW SRM 51-40-4, FIG 1. HFEC INSPECTED CUT-OUT IAW NDTM 51-00-00 FIG 23, PT 6 NO DEFECTS NOTED.
- [SDR FDEA201003160842](https://openairdocs.org/sdr/FDEA201003160842.md): Door Frame · cracked · Mar 16, 2010 · N479FE · Boeing 727227 · Fuselage Main, Structure
  > NR 1 CARGO DOORWAY FRAME, BS 620, STR 25R, WEB CRACKED, ORIGINATING FROM SEAL RETAINER FASTENER HOLE. REMOVED WEB AT BS 620 FRAME FROM STRINGER 16R TO 28R IAW SRM, REV 102, 51-30-2. FABRICATED NEW WEB USING 7075-T6,.071" X 24" X 139.5" IAW MFG DWG NR 65-5
- [SDR FDEA201003160841](https://openairdocs.org/sdr/FDEA201003160841.md): Web · cracked · Mar 16, 2010 · N479FE · Boeing 727227 · Fuselage Main, Structure
  > NR 1 CARGO DOORWAY FRAME, BS 560, STR 19R, WEB CRACKED NEXT TO DOOR STOP FITTING. REMOVED WEB FROM C-1 DOOR CUT OUT FRAME AT BS 560 IAW SRM, REV 102, 51-30-2. FABRICATED NEW WEB USING 7075 -T6,.071" X 80" X 18" IAW SRM 53-10-2 FIG 3 AND DWG NR 65-56100,
- [SDR FDEA201003130812](https://openairdocs.org/sdr/FDEA201003130812.md): Skin · gouged · Mar 13, 2010 · N479FE · Boeing 727227 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN GOUGED AT LAP SEAM, STR 19L, STA 720E. REMOVED FASTENERS AS REQUIRED AND CUT-OUT DAMAGED AREA ON UPPER AND LOWER LAP SEAM DIM: 3" X 4.3750" 2 EA IAW SRM 53-30-3 FIG 6. HEFC INSPECTED AREA IAW NDTM 51-00-00 FIG 23 PART 6, NO DEFECTS NOTED. FA
- [SDR FDEA201003130811](https://openairdocs.org/sdr/FDEA201003130811.md): Skin · chafed · Mar 13, 2010 · N479FE · Boeing 727227 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CHAFED AT LAP SEAM, STR 19R, STA 720E. CUT-OUT DAMAGED AREA DIM: 5.5" X 2.7500" IAW SRM 53-30-3 FIG 6. HFEC INSPECTED AREA IAW NDTM 51-00-00 FIG 23, PART 6, NO DEFECTS NOTED. FABRICATED DOUBLER FROM 2024T3.071 DIM: 13" X 9" AND 2 EA TAPER FIL
- [SDR FDEA201003130814](https://openairdocs.org/sdr/FDEA201003130814.md): Skin · cracked · Mar 13, 2010 · N479FE · Boeing 727227 · Wing, Plate/Skin
  > RT INBD FOREFLAP CARRIAGE ATTACH FITTING AREA AT STA 224, SKIN CRACKED FWD OF ATTACH FITTING. CUT OUT DAMAGED AREA, DIMENSIONS.750" X.218" IAW SRM, REV 102, 57-50-4, FIG. 1. FABRICATED FILLER USING 2024 T-3, PO NR 9002222, DIMENSIONS.050" X.750" X.218"
- [SDR FDEA201003130810](https://openairdocs.org/sdr/FDEA201003130810.md): Skin · dented · Mar 13, 2010 · N479FE · Boeing 727227 · Fuselage Main, Plate/Skin
  > DENT BS 400 STR 17L - 19L EXTERIOR FUSELAGE. EVALUATED DENT AND FOUND TO BE OUT OF LIMITS IAW SRM 53-30-1 FIG 1. CUT-OUT DAMAGED AREA DIM: 2.6250" X 2.8750" IAW SRM 53-30-3 FIG 3. HFEC INSP CUT-OUT AREA IAW NDTM 51-00-00, FIG 23, PART 6, NO DEFECTS NOTED. F
- [SDR FDEA201003130816](https://openairdocs.org/sdr/FDEA201003130816.md): Frame · damaged · Mar 13, 2010 · N479FE · Boeing 727227 · Fuselage Main, Frame
  > FRAME DAMAGED BY TOO LONG HARDWARE INSTALLED IN WIRE BUNDLE STAND OFF CLAMP, STA 500, STR 8R. REMOVED STAND OFF IAW SRM 51-30-2. DRILLED OUT DAMAGED AREA.125 DIA IAW SRM 53-10-1, FIG 1 INSTALLED.1250" SOLID FASTENER IAW SRM 53-10-1 FIG 1 & 51-30-2. INST
- [SDR FDEA201003130815](https://openairdocs.org/sdr/FDEA201003130815.md): Frame · damaged · Mar 13, 2010 · N479FE · Boeing 727227 · Fuselage Main, Frame
  > WIRE BUNDLE STAND OFF BROKEN AND FRAME DAMAGED, STA 460, STR 8R. REMOVED DAMAGED STAND OFF IAW SRM 51-30-2. DRILLED OUT DAMAGE AT FRAME UP TO.125 DIA IAW SRM 53-10-1, FIG 1 AND INSTALLED.1250" SOLID FASTENER AT FRAME IAW SRM 51-30-2. INSTALLED NEW STAND O
- [SDR FDEA201003130813](https://openairdocs.org/sdr/FDEA201003130813.md): Frame · mismanufactured · Mar 13, 2010 · N479FE · Boeing 727227 · Fuselage Main, Frame
  > FASTENERS WITH NO SPACING IN FRAME, STA 344, STR 4L. CUT-OUT DAMAGED AREA, FABRICATED REPAIR ANGLES FROM 7075-0.050 PO NR 9009327 DIM: 7.4" X 3.3" & 7.4" X 3" HEAT TREATED TO 7075T6 IAW ENGINEERING REPORT NR 2-37153-801, REV A. TREATED AND PRIMED IAW SRM 51-
- [SDR FDEA201003130807](https://openairdocs.org/sdr/FDEA201003130807.md): Structure · corroded · Mar 13, 2010 · N479FE · Boeing 727227 · Fuselage Main, Structure
  > E/E COMPARTMENT, RT MID CHORD CORRODED AT STA 294.5. REMOVED CORROSION FROM RT MID CHORD AT STA 294.5 IAW SRM, REV 102, 51-10-6. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1, FIG 1. R & R MID CHORD PN 65-19862-20 AND 2 VERTICAL STIFFENERS, PN 65-19863-10 AND 65
- [SDR FDEA201003110971](https://openairdocs.org/sdr/FDEA201003110971.md): Rib · cracked · Mar 11, 2010 · N479FE · Boeing 727225 · Leading Edge Devices
  > LT WING NR 4 L/E SLAT INBD RIB IS CRACKED WHERE ACTUATOR MOUNTS TO RIB. REMOVED CRACKED RIB IN NO. 4 L/E SLAT WHERE ACTUATOR MOUNTS IAW FED EX B727 SRM, REV102, 51-30-2 AND COVE PANEL FOR ACCESS IAW B727 SRM 51-30-2. LOCATED AND DRILLED TWO RIBS IAW B727 SR
- [SDR FDEA201003110781](https://openairdocs.org/sdr/FDEA201003110781.md): Rib · cracked · Mar 11, 2010 · N479FE · Boeing 727227 · Leading Edge Devices
  > NR 5 SLAT RIB OTBD OF ACTUATOR FWD MOUNT, PREVIOUS REPAIR DOUBLER IS MISSSING 1 FASTENER AND DOUBLER IS INSTALLED ON TOP OF BUTTON HEAD RIVET. ACCOMPLISHED NR 5 SLAT RIBS REPLACEMENT ON NR N00260 SO 00047694, SDR 10-0780
- [SDR FDEA201003110780](https://openairdocs.org/sdr/FDEA201003110780.md): Rib · cracked · Mar 11, 2010 · N479FE · Boeing 727227 · Leading Edge Devices
  > NR 5 SLAT HAS ONE RIB CRACKED INBD SIDE OF ACTUATOR FWD MOUNT. REMOVED WEB PNL FOR ACCESS AND REINSTALLED IAW B727 SRM 51-30-2. REMOVED 2 EA. RIBS FOR CRACKS AND FABRICATED 1 RIB FROM 2024-0.040 PO 24146179 DIMS: 16 3/4" X 6" IAW SRM 57-20-2 FIG 2 & 51-30-
- [SDR FDEA201003110784](https://openairdocs.org/sdr/FDEA201003110784.md): Rib · cracked · Mar 11, 2010 · N479FE · Boeing 727227 · Leading Edge Devices
  > NR 7 SLAT HAS 1 RIB CRACKED ON OTBD SIDE OF ACTUATOR FWD MOUNT.
- [SDR FDEA201003110783](https://openairdocs.org/sdr/FDEA201003110783.md): Angle · cracked · Mar 11, 2010 · N479FE · Boeing 727227 · Leading Edge Devices
  > NR 7 SLAT LOWER AFT CHORD ANGLE IS CRACKED BELOW T-DUCT.

Next page: https://openairdocs.org/deregistered/N479FE-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 = 'N479FE' AND deregistration_id = 'N479FE-2015-08-10'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N479FE-2015-08-10/reports

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