# Service difficulty reports: N463FE, cancelled Dec 19, 2013

A list on [N463FE, cancelled Dec 19, 2013](https://openairdocs.org/deregistered/N463FE-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 · 171 reports

- [SDR FDEA201108273528](https://openairdocs.org/sdr/FDEA201108273528.md): Actuator · inoperative · Aug 27, 2011 · N463FE · Boeing 727225 · Leading Edge Slat Actuator
  > UPON RETRACTION OF FLAP/SLAT FROM 5 DEG TO 2 DEG SLAT NR 8 SHOWED INTRANSIT AMBER LIGHT. FOLLOWED QRH TO NO AVAIL. R & R NR 8 SLAT ACTUATOR. OPS CHECKED GOOD IAW AMM 27-81-032-4.
- [SDR FDEA201103191082](https://openairdocs.org/sdr/FDEA201103191082.md): Control Panel · failed · Mar 19, 2011 · N463FE · Boeing 727225 · External Power System
  > AT FL 290 SMELLED STRONG ELECTRICAL ODOR. NO SMOKE NOTED OR CB'S POPPED. DECLARED EMERGENCY AND LANDED. R & R BUSS PROTECTION PANEL CONTROL BOX IAW AMM 20-10-017-2. R & R THE EXTERNAL POWER CONTACT RELAY IAW AMM 24-20-000-5. RAN ALL 3 ENGINES IAW JRH WITH
- [SDR FDEA201011174401](https://openairdocs.org/sdr/FDEA201011174401.md): Window · cracked · Nov 17, 2010 · N463FE · Boeing 727225 · Flight Compartment Windows
  > L-1 WINDOW CRACKED AND ARCED AT FL 210 DURRING CLIMB OUT. NO WEATHER AS AN ISSUE. SMOOTH AIR AND CLEAR SKIES. 3-4 CRACKS ALL ON OUTER PANE. REMOVED AND REPLACED L-1 WINDOW IAW AMM 56-11-011-4. WINDOW HEAT TEST CHECKED NORMAL IAW 30-41-033-4 RII 236332 R/C A
- [SDR FDEA200908062926](https://openairdocs.org/sdr/FDEA200908062926.md): Frame · corroded · Aug 6, 2009 · N463FE · Boeing 727225 · Fuselage Main, Frame
  > NO. 2 CARGO DOOR AFT FRAME, STA 990, BETWEEN STR 24R & 25R, EXFOLIATION ON FRAME ABOVE DOOR FITTING. FABRICATED ANGLE REPAIR FROM 15-5 PH.080 PO 290342002 DIM: 18 1/4" X 3 1/2", FABRICATED REPAIR FILLER FROM BAC 1505-10046 PO 2901682 DIM: 3 1/8" X 1 1/8
- [SDR FDEA200908042916](https://openairdocs.org/sdr/FDEA200908042916.md): Stiffener · cracked · Aug 4, 2009 · N463FE · Boeing 727225 · Wing, Attach Fittings
  > NR 7 SLAT ACT. ATTACH BRACKET I/B SIDE, INSIDE PLATE IS CRACKED. OPENED PANELS 7613, 7614, 7615 IAW MM 28-11-021-4 AND REMOVED STIFFNER AND PLATE ON NR 7 SLAT ACTUATOR IAW SRM 51-30-2. LOCATED AND DRILLED NEW STIFFNER PART 65-17240-24 IAW SRM 51-30-5 AND
- [SDR FDEA200908042894](https://openairdocs.org/sdr/FDEA200908042894.md): Skin · damaged · Aug 4, 2009 · N463FE · Boeing 727225 · Fuselage Main, Plate/Skin
  > FUSELAGE OUTER SKIN HAS SCRATCHES AT STA 660 TO ST 700, STR 28L TO STR 28R. FABRICATED NEW REPAIR DOUBLER IAW SRM 53-30-2 FIG 2 SRM 53-30-3 FIG 1 CUT OUT DAMAGE AREA IAW SRM 53-30--2 FIG 2 SRM 53-30-3 FIG 1 INSTALLED REPAIR DOUBLER IAW SRM 53-30-3 FIG 1 53-30-
- [SDR FDEA200907292833](https://openairdocs.org/sdr/FDEA200907292833.md): Doubler · cracked · Jul 29, 2009 · N463FE · Boeing 727225 · Landing Gear Doors
  > LT MLG WING DOOR SKIN IS CRACKED FWD OF AFT HINGE AREA ABOVE SEAL RETAINER REMOVED DOUBLER AND FILLER IAW SRM 51-30-2 AND INNER PANEL IAW SRM 51-30-2 FABRICATED DOUBLER AND FILLER FROM 2024 T3.050" PO NR 9008729 DIM 14.5" X 8" FOR DOUBLER AND 11" X 5.5"
- [SDR FDEA200907282878](https://openairdocs.org/sdr/FDEA200907282878.md): Keelbeam · cracked · Jul 28, 2009 · N463FE · Boeing 727225 · Fuselage Main, Structure
  > RT W/W KEEL BEAM CHORD ON RT SIDE IS CRACKED AT BS 870 RBL 6. REMOVED AND DISCARDED GUSSET PLATE AND REMOVED FASTENERS ON CHORD IAW EA 7-5310-126839 HFEC SHOWS HOLES ARE FREE OF CRACKS IAW NDTM 51-00- 00 FIG 23 PART 6 TRIMMED OUT DAMAGED CHORD AREA DIM 2
- [SDR FDEA200907272806](https://openairdocs.org/sdr/FDEA200907272806.md): Angle · cracked · Jul 27, 2009 · N463FE · Boeing 727225 · Leading Edge Devices
  > NR 2 SLAT AFT LWR CHORD ANGLE PREVIOUS REPAIR IS CRACKED BELOW T-DUCT. REMOVED INNER ACCESS PANEL AT NR 2 SLAT IAW SRM 51-30-2. REMOVED CHORD ANGLE AT NR 2 SLAT IAW SRM 51-30-2. FABRICATED NR 2 SLAT AFT LWR CHORD ANGLE USING BAC 1514-1559 2024 T3511, PO NR 2
- [SDR FDEA200907252756](https://openairdocs.org/sdr/FDEA200907252756.md): Angle · cracked · Jul 25, 2009 · N463FE · Boeing 727225 · Fuselage Miscellaneous Structure
  > RT WHEEL WELL VERTICAL ANGLE AT BS 870 IS CRACKED AT RBL 8. REMOVED VERTICAL ANGLE AT RT W/W BS 870 IAW SRM 51-30-2. FABRICATED NEW ANGLE IAW SRM 53-10-2 FIG 4, 51-30-5, 51-20-01 REMOVED KEELBEAM PANELS IAW SRM 51-30-2 ALODINED AND PRIMED ANGLE IAW SR
- [SDR FDEA200907252753](https://openairdocs.org/sdr/FDEA200907252753.md): Angle · cracked · Jul 25, 2009 · N463FE · Boeing 727225 · Trailing Edge Flaps
  > RT WING INBD MID-FLAP, LOWER CHORD ANGLE IS CRACKED BELOW INBD MECHANISM, WBL 90. OPENED INBD MIDFLAP INNER PANEL IAW SRM 51-30-2. CUT OUT DAMAGED SECTION DIM 47" IAW SRM 51-10-1 AND 51-40-4 FABRICATED CHORD SECTION FROM BAC1503-100046, PO NR 9008728 DI
- [SDR FDEA200907252752](https://openairdocs.org/sdr/FDEA200907252752.md): Structure · cracked · Jul 25, 2009 · N463FE · Boeing 727225 · Trailing Edge Flaps
  > LT IB MIDFLAP LWR AFT CHORD IS CRACKED 4 PL. ON IB CARRIAGE TRACK CUT OUT AND IB ACT ROD CUT OUT. REMOVED INNER SKIN AND TEARDROP FAIRING IAW SRM 51-30-2. REMOVED PREVIOUS REPAIR SECTION DIM 48" IAW SRM 51-30-2, FABRICATED NEW ANGLE FROM BAC 1503 - 100046
- [SDR FDEA200907232724](https://openairdocs.org/sdr/FDEA200907232724.md): Frame · cracked · Jul 23, 2009 · N463FE · Boeing 727225 · Fuselage Main, Frame
  > FWD CARGO AREA, BS 540, STR 21L - 22L, CRACK ON STUB FRAME EXTENSION RADIUS. REMOVED GILLINER SUPPORT AND FRAME EXTENSION STUB IAW SRM 51-30-2. FORMED STUB FRAME WITH 7075 'O'.063" PO NR 9008655 IAW DWG 53FX 1350 REV A. HEAT TREATED PART FROM 'O' MATER
- [SDR 07FDEA01374](https://openairdocs.org/sdr/07FDEA01374.md): Support · corroded · Apr 7, 2007 · N463FE · Boeing 727225 · Fuselage Miscellaneous Structure
  > DURING PANEL CLOSE UP ON AFT BULKHEAD IN AFT PIT, CENTER LOWER PANEL, UPPER ANGLE CORRODED AROUND FASTENER HOLES. REMOVED CENTER BULKHEAD PANEL SUPPORT ANGLE, REPAIRED BY INSTALLING 2 ANGLES AND A FILLER. RE-INSTALLED PANEL SUPPORT ANGLE REF SRM 51-40-4/FIG
- [SDR 07FDEA01370](https://openairdocs.org/sdr/07FDEA01370.md): Angle · cracked · Apr 6, 2007 · N463FE · Boeing 727225 · Spoilers
  > RT WING, TE LOWER PANEL, BELOW NR 12 SPOILER PANEL, OTBD ATTACH ANGLE, OF THE OTBD SET IS CRACKED AT SUPPORT ROD. REMOVED DAMAGE ANGLE, VERIFIED REPAIR MATERIAL AS 7075-T6.050 REF IPC 57-30-00 FIG 16 AND DWG 65-21658. FABRICATED REPLACEMENT ANGLE REF FED EX
- [SDR 07FDEA01369](https://openairdocs.org/sdr/07FDEA01369.md): Channel · cracked · Apr 6, 2007 · N463FE · Boeing 727225 · Fuselage Miscellaneous Structure
  > AFT CARGO PIT RT "Z" CHANNEL CRACKED AT RIVET HEAD AT STA 1040 FRAME REPLACED Z-ANGLE REF SRM 51-30-2.
- [SDR 07FDEA01368](https://openairdocs.org/sdr/07FDEA01368.md): Attach Fitting · corroded · Apr 6, 2007 · N463FE · Boeing 727225 · Wing, Attach Fittings
  > LT WING NR 1 KRUGER FLAP ALL 3 HINGES, HARDWARE HAS RUST CENTER CASTING AT ACTUATOR ATTACH, 1 HOLE IS CORRODED EDGE DAMAGED. REPLACED NR 1 KRUGER FLAP REFERENCE MM 27-81-001-4 ADJUSTMENT AND CHECK PERFORMED REF W/C70C007-00.
- [SDR 07FDEA01367](https://openairdocs.org/sdr/07FDEA01367.md): Threshold · cracked · Apr 6, 2007 · N463FE · Boeing 727225 · Fuselage Miscellaneous Structure
  > AFT LOWER CARGO PIT DOOR CUTOUT THRESHOLD HAS 2 CRACKS IN CURVED AREA BETWEEN 27" AND 32" AFT OF FWD EDGE WELD ACCOMPLISHED ON SHOP N/R 11841-8300-0001. VERIFIED MATERIAL WELDED AND SMOOTHED AREA REFERENCE FED EX DWG SR27-53-025C.
- [SDR 07FDEA01366](https://openairdocs.org/sdr/07FDEA01366.md): Skin · damaged · Apr 6, 2007 · N463FE · Boeing 727225 · Fuselage Main, Plate/Skin
  > EXT FUSELAGE BS 420 S-4R 2 PAIRS OF OVERLAPPPING RIVET HEADS AND SEVERAL RIVETS CLOSELY SPACED REMOVED 9 G NET ATTACH STRUCTURE BETWEEN S-4R AND S-5R CUT OUT DAMAGED AREA. FABRICATED REPAIR FILL AND REPAIR DOUBLER AND INSTALLED. REFERENCE EA NR 7-5330-106995
- [SDR 07FDEA01364](https://openairdocs.org/sdr/07FDEA01364.md): Skin · cracked · Apr 5, 2007 · N463FE · Boeing 727225 · Wing, Plate/Skin
  > LEFT WING FAIRING NR 3343 VERIFIED MATERIAL AS 2024-0.050 REF DWG 65-22555 AND SRM 51-40-2 PG 1. STOPPED DRILLED CRACK REF SRM 51-10-PG 13 ITEM 10, HFEC IAW 727NDT MAN PART 6, 51-00-00 FIG 23. TOOL NR IDM 0031 11-30-07. VERIFIED CRACK TO BE CONFINED BY STO
- [SDR 07FDEA01365](https://openairdocs.org/sdr/07FDEA01365.md): Web · corroded · Apr 5, 2007 · N463FE · Boeing 727225 · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR WEB UPPER SURFACE IS CORRODED BS 1147, LBL 52-63, WL 208. REMOVED DAMAGE AREA OF WEB REF SRM 51-40-2 FIG 1, STA 1147, LBL 62, THAT WAS OUT OF LIMITS REF 51-10-1, AFTER BLENDING, MFG AND INSTALLED REPAIR REF SRM 51-40-2 FIG 1 AT LBL 62
- [SDR 07FDEA01363](https://openairdocs.org/sdr/07FDEA01363.md): Keelbeam · corroded · Apr 5, 2007 · N463FE · Boeing 727225 · Fuselage Main, Keel
  > LOWER AFT PIT BILGE, STA 950E 10, LBL 8" O/B LWR FLANGE OF KEEL BEAM CHORD HAS CORROSION, ON PREVIOUS STRAP REPAIR. REMOVED FLOOR SUPPORT AND SHEAR TIE FOR ACCESS, GROUND CORROSION ON EXISTING STRAP AND NDT FOR MATERIAL LOSS. FOUND TO BE OUT OF LIMITS. FA
- [SDR 07FDEA01362](https://openairdocs.org/sdr/07FDEA01362.md): Keelbeam · corroded · Apr 5, 2007 · N463FE · Boeing 727225 · Fuselage Main, Keel
  > LWR AFT PIT BILGE, STA 950A LBL 8" OB LWR FLANGE OF KEEL BEAM CHORD HAS APPROX 6 SQ INCHES OF CORROSION ON UPPER SURFACE. REMOVED CORROSION ON OUTBOARD FLANGE OF KEEL BEAM LWR AFT PIT BILGE STA 950A, 6" LBL 8" FOUND AREA OUT OF LIMITS. FABRICATED, TREATED A
- [SDR 07FDEA01351](https://openairdocs.org/sdr/07FDEA01351.md): Fitting · damaged · Apr 4, 2007 · N463FE · Boeing 727225 · Fuselage Miscellaneous Structure
  > INTERNAL FUSELAGE AT STA 259.BL0 TO RBL 2, CASTING HAS TOOLING DAMAGE REMOVE FLIGHT DECK CEILING TO GAIN ACCESS TO CASTING. REMOVED INTERCOSTAL AND SURROUND STRUCTURE. REMOVED CASTING, DRILLED NEW CASTING AND INSTALLED. RE-INSTALLED ALL STRUCTURE AND CEILIN
- [SDR 07FDEA01350](https://openairdocs.org/sdr/07FDEA01350.md): Skin · cracked · Apr 4, 2007 · N463FE · Boeing 727225 · Fuselage Main, Plate/Skin
  > FUSELAGE UPPER LOBE INTERIOR SKIN IS CRACKED ON BOTH SIDES OF STRINGER AT SKATE ANGLE FASTENERS AT BS 1097, STR 1, LBL 1 - RBL 1. REMOVED DAMAGE AND INSTALLED DOUBLER IN REFERENCE TO SRM 53-30-3, PG 12.
- [SDR 07FDEA01349](https://openairdocs.org/sdr/07FDEA01349.md): Casting · cracked · Apr 4, 2007 · N463FE · Boeing 727225 · Fuselage Miscellaneous Structure
  > MAIN DECK 2 RIGHT DOOR CUT OUT UPPER AFT CORNER SEAL DEPRESSOR CASTING IS CRACKED AT BS 1062 WL 271. REMOVED AND DRILLED UP R2 CORNER SEAL DEPRESSOR CASTING. INSTALLED CASTING REF 51-30-02.
- [SDR 07FDEA01347](https://openairdocs.org/sdr/07FDEA01347.md): Floorbeam · corroded · Apr 4, 2007 · N463FE · Boeing 727225 · Fuselage Main, Floor Beam
  > MAIN DECK FLOORBEAM UPPER FLANGE IS CORRODED AT BS 1110, RBL 22, WL 208 CORROSION DAMAGE REPAIRED REFERENCE EA NR 7-5310-106997.
- [SDR 07FDEA01345](https://openairdocs.org/sdr/07FDEA01345.md): Bracket · corroded · Apr 4, 2007 · N463FE · Boeing 727225 · Escape Slide
  > MAIN ENTRY DOOR EMERG ESCAPE SLIDE, BACK PAN LWR LATCH HINGED RETAINER, MOUNT BLOCK HAS EXFOLIATION CORROSION. INSTALLED NEW BRACKET REF SRM 51-30-2 PG 2.
- [SDR 07FDEA01344](https://openairdocs.org/sdr/07FDEA01344.md): Bracket · cracked · Apr 4, 2007 · N463FE · Boeing 727225 · Wing, Attach Fittings
  > NR 6 FLAP TRACK OTBD FAIRING ATTACH BRACKET IS CRACKED REMOVED AND REPLACED NR 6 FLAP TRACK OTBD BRACKET REF SRM 5130-2 PGS 3, 4 AND 5 AND SRM 51-20-031-7 PGS 1, 3 AND 7.
- [SDR 07FDEA01327](https://openairdocs.org/sdr/07FDEA01327.md): Skin · cracked · Apr 4, 2007 · N463FE · Boeing 727225 · Wing, Plate/Skin
  > RT WING LEADING EDGE UPPER SURFACE CUTOUT AT NR 5 SLAT INBD GUIDE IS GOUGED AND CRACKED AT AFT EDGE REMOVED SLAT SEALS AND COVER FOR ACCESS, DAMAGE REMOVED REF SRM 57-30-2. HFEC FOR CRACKS REF B727 NDT MANUAL PART 6. FABRICATED PART AND INSTALLED REPAIR REF
- [SDR 07FDEA01318](https://openairdocs.org/sdr/07FDEA01318.md): Skin Panel · gouged · Apr 4, 2007 · N463FE · Boeing 727225 · Vertical Stabilizer, Plate/Skin
  > RT VERTICAL STAB SKIN/WEB HAS (2 EA) TOOLING GOUGES LOCATED UNDER PANEL 9706. GOUGES ARE LOCATED NEAR FASTENER ROW FOR L- ANGLE AND 23", 24" FROM FRONT OF PANEL. REMOVED DAMAGE PER EA I070144. VERIFY DAMAGED REMOVED BY HFEC IAW 727 NDT MAN, PART 6, 51-00-00
- [SDR 07FDEA01309](https://openairdocs.org/sdr/07FDEA01309.md): Nacelle · cracked · Apr 3, 2007 · N463FE · Boeing 727225 · Nacelle/Pylon, Attach Fittings
  > NR 1 ENGINE FIXED COWL UPPER SECTION CRACKED AT UPPER FWD CORNER. REPLACED FIXED COWL, NEW COWL INSTALLED ON WC 70T0001-01.
- [SDR 07FDEA01308](https://openairdocs.org/sdr/07FDEA01308.md): Skin · cracked · Apr 3, 2007 · N463FE · Boeing 727225 · Fuselage Main, Plate/Skin
  > FOUND REPAIR AT FUSELAGE STA 1184, LBL 10. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED REPAIR DOUBLER REF SRM 51-30-2. HFEC SKIN IAW 727 NDT MANUAL PART 6, 51-00-00 FIG 23. FOUN
- [SDR 07FDEA01307](https://openairdocs.org/sdr/07FDEA01307.md): Attach Angle · cracked · Apr 3, 2007 · N463FE · Boeing 727225 · Wing, Attach Fittings
  > RT WING TE, LOWER PANEL BELOW NR 13 SPOILER PANEL OTBD ATTACH ANGLE OF THE INBD SET IS CRACKED AT SUPPORT ROD. FABRICATED REPLACEMENT ANGLE ON SHOP WO NR 11841-6300-0002. HEAT TREATED ON 8130- 3 TRACKING NR 2007-03-142. REPLACED ANGLE ATTACHMENT FOR LOWER P
- [SDR 07FDEA01306](https://openairdocs.org/sdr/07FDEA01306.md): Angle · corroded · Apr 3, 2007 · N463FE · Boeing 727225 · Fuselage Miscellaneous Structure
  > LOWER AFT PIT FWD BULKHEAD STA 950A, LBL 12, HORIZONTAL L-ANGLE AT BASE OF WALL SUPPORT HAS CORROSION AT INBD END. REMOVED L ANGLE FROM LBL 6 TO LBL 21, STA 950A. FABRICATED NEW L ANGLE ON AAR SHOP WO NR 11841-1600-0002, BY HEAT TREATING ANGLE REF DWG 65-672
- [SDR 07FDEA01304](https://openairdocs.org/sdr/07FDEA01304.md): Floorbeam · corroded · Apr 3, 2007 · N463FE · Boeing 727225 · Fuselage Main, Floor Beam
  > LOWER AFT PIT FLOORBEAM, VERTICAL CHANNEL HAS CORROSION AT LWR END AROUND FASTENER HEAD AT STA 950E, LBL 8 FABRICATED NEW FLOORBEAM VERTICAL CHANNEL AT STA 950E, LBL 8. HEAT TREATED AND HARDNESS TESTED FOR 7075 T6 CONDITION REF BAC DWG 69-44559 AND BAC 5602 R
- [SDR 07FDEA01301](https://openairdocs.org/sdr/07FDEA01301.md): Frame · corroded · Apr 3, 2007 · N463FE · Boeing 727225 · Fuselage Main, Frame
  > LOWER AFT PIT BILGE, FRAME HAS APPROX 3 SQ INCHES OF CORROSION ON AFT LOWER FACE AT STA. 950A, LBL 8". REMOVED CORROSION REF 51-10-2 AND 53-10-1. NDT'D FOR MATERIAL LOSS, FOUND AREA OUT OF LIMITS REF SRM 53-10-1 FIG 1. REMOVED SUPPORT BRKT, VERT SUPPORT BRK
- [SDR 07FDEA01300](https://openairdocs.org/sdr/07FDEA01300.md): Support Channel · corroded · Apr 3, 2007 · N463FE · Boeing 727225 · Fuselage Miscellaneous Structure
  > LOWER AFT PIT BILGE FWD SIDE OF STA 950A, VERTICAL SUPPORT CHANNEL AT 8" LBL HAS SMALL AMOUNT OF CORROSION AT LOWER OB. REPLACED VERTICAL SUPPORT AT STA 950A. REFERENCE SRM 51-30-2 PAGE 1 - 12.
- [SDR 07FDEA01298](https://openairdocs.org/sdr/07FDEA01298.md): Angle · corroded · Apr 3, 2007 · N463FE · Boeing 727225 · Fuselage Miscellaneous Structure
  > LOWER AFT PIR FWD BULKHEAD STA 950A, RBL 22, L ANGLE AT BASE OF WALL SUPPORTS HAVE CORROSION ON UPPER SURFACE (2 EACH) DAMAGE TO 2 L ANGLES OUT OF LIMITS. ORIGINAL MATERIAL WAS.050", REMAINING MATERIAL.035". FABRICATED 2 REPAIR ANGLES, HEAT TREATED TO T4 O
- [SDR 07FDEA01247](https://openairdocs.org/sdr/07FDEA01247.md): Structure · delaminated · Apr 2, 2007 · N463FE · Boeing 727225 · Spoilers
  > RT WING NR 14 SPOILER T/E IS SPLIT REMOVED AND REINSTALLED NR 14 SPOILER FOR T/E REPAIR REF M/M 27-61-0001-4, M/M 27-61-001-5. SPOILER REPAIRED ON IDM WORK CARD ORDER NR 11841-6000-0004.
- [SDR 07FDEA01246](https://openairdocs.org/sdr/07FDEA01246.md): Skin · delaminated · Apr 2, 2007 · N463FE · Boeing 727225 · Spoilers
  > RT WING NR 9 SPOILER UPPER TE SURFACE HAS DELAM REMOVED NR 9 SPOILER PANEL. SPOILER REPAIRED ON SHOP WO NR 11841-6000-0003 REF SRM 51-40-20. INSTALLED NR 9 SPOILER PANEL REF MM 27-62-001-4 STEP 3-5. ADJUSTED SPOILER REF MM 27-62-001-5 PG 1 STEP 2A-2F AND ST
- [SDR 07FDEA01245](https://openairdocs.org/sdr/07FDEA01245.md): Skin · misrepaired · Apr 2, 2007 · N463FE · Boeing 727225 · Leading Edge Devices
  > FOUND REPAIR AT LT WING NR 1 SLAT. FLUSH REPAIR IS 15" FROM OB END ON TOP SURFACE. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. FOUND REPAIR DID NOT MEET CRITERIA OF SRM 57-50-3 FIG 1. AFT
- [SDR 07FDEA01244](https://openairdocs.org/sdr/07FDEA01244.md): Skin · misrepaired · Apr 2, 2007 · N463FE · Boeing 727225 · Fuselage Main, Plate/Skin
  > FOUND EXTERNAL FUSELAGE REPAIR AT APPROX STA 1223, STR 25R. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. FOUND REPAIR DID NOT CONFORM TO SRM 53-30-3 FIG 3. REMOVED EXTERNAL DOUBLER FROM A
- [SDR 07FDEA01243](https://openairdocs.org/sdr/07FDEA01243.md): Skin · delaminated · Apr 2, 2007 · N463FE · Boeing 727225 · Spoilers
  > RT WING NR 13 SPOILER T/E IS SPLIT NR 13 SPOILER REPAIRED ON WO NR 11841-6000-0005 REFERENCE SRM 51-40-20. INSTALLED NR 13 SPOILER REF MM 27-61-001-4 PG 2-3 STEP 5, TORQUE WRENCH AAR 20026 DATE 8-23-07. CTR BOLT 285 IN LB. OUTBD HINGE BOLT, 130 IN LB TORQUE
- [SDR 07FDEA01242](https://openairdocs.org/sdr/07FDEA01242.md): Skin · delaminated · Apr 2, 2007 · N463FE · Boeing 727225 · Ailerons
  > LT WING OTBD AILERON IS DELAMINATED AT THE OTBD T/E. LT OB AILERON WAS REPAIRED ON SHOP WO NR 11841-5000-0003 REFERENCE SRM 51-40-20. LT OB AILERON IS INSTALLED AND RIGGED ON SNRM NR N00554.
- [SDR 07FDEA01221](https://openairdocs.org/sdr/07FDEA01221.md): Panel · delaminated · Mar 31, 2007 · N463FE · Boeing 727225 · Wing, Plate/Skin
  > RT WING, UPPER SURFACE AT WBL 462, PNL, JUST O/B OF NR 14 SPOILER IS DELAMINATED. REMOVED PANEL AND SENT OUT FOR REPAIR. PANEL REPAIRED ON AAR WO NR 11841/6300/0003. REMOVED DAMAGE AND DELAMINATED SKIN, AND REPAIRED, REF SRM 51-40-20. INSTALLED PANEL REF
- [SDR 07FDEA01220](https://openairdocs.org/sdr/07FDEA01220.md): Plug · corroded · Mar 31, 2007 · N463FE · Boeing 727225 · Flight Compartment Windows
  > THE SECOND WINDOW PLUG AFT OF THE LEFT AFT EMERGENCY ESCAPE HATCH HAS CORROSION UNDER THE SEAL AT THE FWD LOWER PLUG RETAINER REMOVED WINDOW PLUG, REF MM 56-20-000-4 PG 1. DRILLED HOLE IN THE WINDOW PLUG FOR JUMPER STRAP, REF EO NR 7-5620-7-4304. INSTALLED W
- [SDR 07FDEA01219](https://openairdocs.org/sdr/07FDEA01219.md): Skin · gouged · Mar 31, 2007 · N463FE · Boeing 727225 · Cargo/Baggage Doors
  > FWD LOWER CARGO DOOR, FWD LOWER CORNER OF SKIN WORN, GOUGED. INSTALLED REPAIR DOUBLER REF 52-00-3 PG 2, FIG 4, DETAIL F. RESTORED LEVELING, COMPOUND REF SOPM 20-60-04 PG 7.
- [SDR 07FDEA01218](https://openairdocs.org/sdr/07FDEA01218.md): Floorbeam · corroded · Mar 31, 2007 · N463FE · Boeing 727225 · Fuselage Main, Floor Beam
  > FLIGHT DECK FLOORBEAM HAS CORROSION ON TOP OF BEAM LOCATED AT BS 277, RBL 10.5. REMOVED CORROSION, ALL WORK FOR BLEND WAS ACCOMPLISHED ON FED EX EA NR 7-5310-107004.
- [SDR 07FDEA01217](https://openairdocs.org/sdr/07FDEA01217.md): Battery Box · corroded · Mar 31, 2007 · N463FE · Boeing 727225 · Battery Box Structure
  > E/E COMPARTMENT BATTERY TRAY AFT EDGE IS CORRODED. REMOVED, FABRICATED AND ACP HEAT TREAT PROCESS FOR 2024-T4, CONDITION FOR TRAY. REF BAC DWG 69-21649 REV C AND BAC5602 REV (AF) 28 AUG 01 AND BAC 5946 REV (AA) 9 JUL 01. IDENTIFIED TRAY AS FX-69-21649-1. W

Next page: https://openairdocs.org/deregistered/N463FE-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 = 'N463FE' AND deregistration_id = 'N463FE-2013-12-19'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N463FE-2013-12-19/reports

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