# Service difficulty reports: N263FE, cancelled Dec 19, 2013

A list on [N263FE, cancelled Dec 19, 2013](https://openairdocs.org/deregistered/N263FE-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 2 · 95 reports

- [SDR FDEA201106022096](https://openairdocs.org/sdr/FDEA201106022096.md): Slide · dislodged · Jun 2, 2011 · N263FE · Boeing 727233 · Escape Slide
  > BIRD WAS A LAYOVER. WALKING UP CREW STAIRS DURING LINE INSPECTION, FOUND EMERGENCY ESCAPE SLIDE LYING ON CREW STAIRS. REPLACED WITH A "NEW" SLIDE.
- [SDR FDEA201104271652](https://openairdocs.org/sdr/FDEA201104271652.md): Slide · dislodged · Apr 27, 2011 · N263FE · Boeing 727233 · Escape Slide
  > ON PREFLIGHT FOUND SLIDE PACK SITTING ON MAIN DECK FLOOR. R & R EVACUATION SLIDE ASSY ON THE L1 DOOR REF MM 25-60-015-2. ACFT OK TO CONTINUE AT THIS TIME. PREMATURE REMOVAL/INSTALLATION.
- [SDR FDEA200912054398](https://openairdocs.org/sdr/FDEA200912054398.md): Structure · corroded · Dec 5, 2009 · N263FE · Boeing 727233 · Fuselage Main, Structure
  > CORROSION ON CHORD AT STA 1176, LBL 65 TO RBL 65. REMOVED CORROSION AND FOUND OUT OF LIMITS, REMOVED CHORD, LOCATED AND DRILLED NEW CHORD PN 65-31773-1 PO NR 2911891 AND INSTALLED IAW SRM 51-10- 6, 53-10-1, 53-10-2 AND 51-30-2.
- [SDR FDEA200911284210](https://openairdocs.org/sdr/FDEA200911284210.md): Stringer · corroded · Nov 28, 2009 · N263FE · Boeing 727233 · Fuselage Main, Longeron/Stringer
  > C-3 DOOR CUTOUT STR 25R IS CORRODED ON END AT BS 1140. REMOVED CORROSION AND FOUND OUT OF LIMITS, CUT OUT DAMAGED STRINGER DIMS 14" LONG, FABRICATED STRINGER REPAIR, 1 STRINGER SPLICE, AND INSTALLED IAW SRM 51-10-6, 51-30-2, AND 53-10-3.
- [SDR FDEA200911264347](https://openairdocs.org/sdr/FDEA200911264347.md): Attach Fitting · cracked · Nov 26, 2009 · N263FE · Boeing 727233 · Wing, Attach Fittings
  > LT WING STA 686.5 STR TO RIB ATTACHMENT CRACKED AT STR 14. (LWR) REMOVED LWR CHORD AT LT WING STA 686.5 AT STR 14 IAW SRM 51-30-2 REV 101, LOCATED AND DRILLED NEW CHORD IAW SRM 51-30-5, INSTALLED NEW LWR CHORD IAW SRM 51-30-2, REV 101.
- [SDR FDEA200911254187](https://openairdocs.org/sdr/FDEA200911254187.md): Floorbeam · damaged · Nov 25, 2009 · N263FE · Boeing 727233 · Fuselage Main, Floor Beam
  > DOUBLE DRILLED HOLE IN FLOORBEAM UPPER TEE BS 1166, BL 0. CUTOUT DAMAGED AREA DIMS 5 1/4" X 2", FABRICATED UPPER TEE, 2 SUPPORT ANGLES, 3 ANGLE SUPPORTS, REINFORCEMENT STRAP, INSTALLED IAW SRM 53-10-8, 53-10-2 AND 51-30-2.
- [SDR FDEA200911254184](https://openairdocs.org/sdr/FDEA200911254184.md): Stringer · cracked · Nov 25, 2009 · N263FE · Boeing 727233 · Fuselage Main, Longeron/Stringer
  > STRINGER CRACKED AT STA 620 STR 27L. REMOVED DAMAGED STRINGER DIMS 20", FABRICATED NEW STR SECTION, FABRICATED SPLICES AND INSTALLED IAW SRM 51-30-2, 53-10-3 AND 51-10-2.
- [SDR FDEA200911234351](https://openairdocs.org/sdr/FDEA200911234351.md): Skin · gouged · Nov 23, 2009 · N263FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > MCD CUT-OUT INNER SKIN GOUGED STA 620 STR 4L. CUTOUT DAMAGE AREA 3 EA. DIM(7/8" X 7/8") IAW EA 7-5310-135508. HFEC INSPECTED AREA IAW NDTM 51-00-00 FIG 27 PT6 NO DEFECTS NOTED. PERFORMED.040" INSURANCE CUTOUT IAW EA 7-5310-135508, FABRICATED REPAIR DOUBLER
- [SDR FDEA200911234350](https://openairdocs.org/sdr/FDEA200911234350.md): Skin · gouged · Nov 23, 2009 · N263FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > MCD CUT-OUT INNER SKIN GOUGED STA 640, STR 6L. CUT OUT DAMAGED AREAS 2 EA 7/8" AND 1 EA 1" X 2". CW HFEC INSP NO DEFECTS NOTED. MADE.040" INSURANCE CUT, FABRICATED REPAIR DOUBLER AND FILLERS. TREATED AND PRIMED REPAIR PARTS AND INSTALLED REPAIR IAW EA 7-5
- [SDR FDEA200911234349](https://openairdocs.org/sdr/FDEA200911234349.md): Skin · gouged · Nov 23, 2009 · N263FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > MCD CUT-OUT INNER SKIN GOUGED, STA 625, STR 10L. CUT OUT DAMAGED AREA DIM 1" IAW EA 7-5310-135511. CW HFEC INSP, NO DEFECTS NOTED. PERFORMED.040" INSURANCE CUT AND FABRICATED REPAIR DOUBLER IAW EA 7-5310-135511. TREATED AND PRIMED DOUBLER IAW SRM 51-10-2.
- [SDR FDEA200911234188](https://openairdocs.org/sdr/FDEA200911234188.md): Shear Tie · cracked · Nov 23, 2009 · N263FE · Boeing 727233 · Fuselage Internal Mounting Structure
  > FUSELAGE RIB TO SKIN SHEAR TIE WEB CRACKED, PIECE BROKEN OFF, APPROX F/S 328, LBL 14, NLG W/W STRUCTURE AT LWR CHORD ATTACHMENT. CUT OUT DAMAGED AREA DIMS 3" X 2", FABRICATED DOUBLER REPAIR AND INSTALLED IAW SRM 51-30-2, 53-10-4, AND 51-10-2.
- [SDR FDEA200911234127](https://openairdocs.org/sdr/FDEA200911234127.md): Floorbeam · damaged · Nov 23, 2009 · N263FE · Boeing 727233 · Fuselage Main, Floor Beam
  > MIS-DRILLED FASTENER HOLES STA 1166 FLOORBEAM RBL 25 TO RBL 65. CUTOUT DAMAGED AREA DIMS 34" LONG, FABRICATED UPPER TEE, 2 SUPPORT ANGLES, AND 2 REINFORCEMENT STRAPS. INSTALLED IAW SRM 53-10-8, 53-10-2 AND 51-30-2.
- [SDR FDEA200911234126](https://openairdocs.org/sdr/FDEA200911234126.md): Floorbeam · damaged · Nov 23, 2009 · N263FE · Boeing 727233 · Fuselage Main, Floor Beam
  > MIS-DRILLED FASTENER HOLES STA 1166 FLOORBEAM LBL 25 TO LBL 65. CUTOUT DAMAGED AREA DIMS 3 3/4" X 2", FABRICATED UPPER TEE, SUPPORT ANGLES AND 2 REINFORCEMENT STRAPS. INSTALLED IAW SRM 53-10-8, 53-10-2 AND 51-10-2.
- [SDR FDEA200911234125](https://openairdocs.org/sdr/FDEA200911234125.md): Floorbeam · damaged · Nov 23, 2009 · N263FE · Boeing 727233 · Fuselage Main, Floor Beam
  > MIS-DRILLED FASTENER HOLES STA 1148 FLOORBEAM RBL 25 TO RBL 65. CUT OUT DAMAGED AREA DIMS 95 1/8" X 2", FABRICATED UPPER TEE REPAIR, SUPPORT ANGLES, REINFORCEMENT STRAP AND INSTALLED ALL PARTS IAW SRM 53-10-8, 53-10-2 AND 51-30-2.
- [SDR FDEA200911234124](https://openairdocs.org/sdr/FDEA200911234124.md): Floorbeam · damaged · Nov 23, 2009 · N263FE · Boeing 727233 · Fuselage Main, Floor Beam
  > MIS-DRILLED FASTENER HOLES STA 1148 FLOORBEAM LBL 25 TO LBL 65. CUTOUT DAMAGED AREA DIMS 3 3/8" X 2", FABRICATED UPPER TEE, 2 ANGLES AND 2 REINFORCEMENT STRAPS. INSTALLED IAW SRM 53-10-8, 53-10-2, AND 51-30-2.
- [SDR FDEA200911234123](https://openairdocs.org/sdr/FDEA200911234123.md): Floorbeam · damaged · Nov 23, 2009 · N263FE · Boeing 727233 · Fuselage Main, Floor Beam
  > MIS-DRILLED FASTENER HOLES STA 1130 FLOORBEAM RBL 25 TO RBL 65. REMOVED WEB AT STA 1130-1148, CUT-OUT DAMAGED AREA DIMS 2" X 1 1/4", FABRICATED ANGLE, HEAT TREATED PART TO T6 CONDITION IAW FASI ER NR 2-37153-801 REV A ON FASI FORM NR FAS0115 REV 19, MADE I
- [SDR FDEA200911234122](https://openairdocs.org/sdr/FDEA200911234122.md): Floorbeam · damaged · Nov 23, 2009 · N263FE · Boeing 727233 · Fuselage Main, Floor Beam
  > MIS-DRILLED FASTENER HOLES STA 1130 FLOORBEAM LBL 25 TO LBL 65. REMOVED WEB AT STA 1130-1148 FOR ACCESS, CUT OUT DAMAGED AREA DIMS 2" X 1 1/4", FABRICATED ANGLE, HEAT TREATED PART TO T6 CONDITION IAW FASI ENGINEERING REPORT NR 2-37153-801 REV A ON FASI FORM
- [SDR FDEA200911214375](https://openairdocs.org/sdr/FDEA200911214375.md): Skin · chafed · Nov 21, 2009 · N263FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > 5 DOUBLERS ON MCD CUTOUT INNER SKIN DAMAGED FROM CHAFING. DOUBLERS WERE REMOVED ON EA 7-5330-89309. FABRICATED 4 EACH DOUBLERS USING 2024T-3.100 PO NR 9008728 DIMS 6" X 3 3/4", 6" X 3 7/8", 6" X 3 7/8", 9 5/8" X 3 1/2", AND 1 EACH DOUBLER USING 2024T-3.1
- [SDR FDEA200911214374](https://openairdocs.org/sdr/FDEA200911214374.md): Skin · chafed · Nov 21, 2009 · N263FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > 3 DOUBLERS ON MCD CUTOUT INNER SKIN DAMAGED FROM CHAFING. DOUBLERS WERE REMOVED ON EA 7-5330-110787. FABRICATED 3 EACH DOUBLERS USING 2024T-3.140 PO NR 2907573 DIMS 5 5/8" X 5 1/4", 9 3/4" X 3" AND 22 1/8" X 11 1/8" IAW SRM 51-40-02. DOUBLER INSTALLATION
- [SDR FDEA200911214107](https://openairdocs.org/sdr/FDEA200911214107.md): Beam · corroded · Nov 21, 2009 · N263FE · Boeing 727233 · Fuselage Main, Structure
  > CORROSION INDICATION AND LIFTING/ DISBONDING OF LEVELING COMPOUND ON LT HORIZ WALKWAY BEAM ABOUT STA 294, LBL 14, NWW. REMOVED COMPOUND AND FOUND CORROSION OUT OF LIMITS, REMOVED LT NLG LWR SECTION OF BEAM, LOCATED AND DRILLED NEW SECTION AND INSTALLED, RE-AP
- [SDR FDEA200911204416](https://openairdocs.org/sdr/FDEA200911204416.md): Doubler · gouged · Nov 20, 2009 · N263FE · Boeing 727233 · Cargo/Baggage Doors
  > MCD CUTOUT INNER SKIN GOUGED STA 480, STR 4L. CUTOUT DAMAGE AREA 2 EA. DIM (1.9" X 1 1/2") AND (1.45" X 0.65") IAW EA NR 7-5310-135510. HFEC INSPECTED CUTOUT IAW NDTM 51-00-00 FIG 23 PT6 NO DEFECTS NOTED. PERFORMED.040" INSURANCE CUTOUT IAW EA 7-5310-135510
- [SDR FDEA200911204250](https://openairdocs.org/sdr/FDEA200911204250.md): Door Frame · cracked · Nov 20, 2009 · N263FE · Boeing 727233 · Fuselage Main, Structure
  > FWD ENTRY DOOR FRAME STA 303.9 STR 16L CRACK ON THE WEB CUTOUT. REMOVED FWD ENTRY DOOR STOP AND SUPPORT ANGLE IAW SRM 51-30-2. STOP DRILLED CRACK TO.250 DIM IAW 51-10-1. FABRICATED NEW ANGLE AND 2 FILLERS IAW DWG 65C38447 AND EO 7-5310-7-3362 B2 PT7. TRE
- [SDR FDEA200911204103](https://openairdocs.org/sdr/FDEA200911204103.md): Skin · dented · Nov 20, 2009 · N263FE · Boeing 727233 · Trailing Edge Flaps
  > LT WING INBD FOREFLAP INBD L/E DENTED AND GOUGED. REMOVED 2 EACH ACCESS PANELS IAW SRM 51-30-2, CUT OUT DAMAGED AREA DIM 3/4" X 3/4" IAW SRM 51-10-1, FABRICATED REPAIR DOUBLER IAW SRM 57-50-4 FIG 1 AND 57-50-2 FIG 3, TREATED AND PRIMED PARTS IAW SRM 51
- [SDR FDEA200911204102](https://openairdocs.org/sdr/FDEA200911204102.md): Retainer · cracked · Nov 20, 2009 · N263FE · Boeing 727233 · Trailing Edge Flaps
  > LT WING INBD MID FLAP T/E CHORD CRACKED AT WS 195. REMOVED SEAL RETAINER, DISPLACED MID-FLAP SKIN FOR ACCESS, REMOVED DAMAGED CHORD SECTION, FABRICATED NEW SECTION AND INSTALLED, CLOSED MID-FLAP SKIN AND REINSTALLED SEAL RETAINER IAW SRM 51-30-2, 51-40-4 AND
- [SDR FDEA200911204101](https://openairdocs.org/sdr/FDEA200911204101.md): Retainer · cracked · Nov 20, 2009 · N263FE · Boeing 727233 · Trailing Edge Flaps
  > LT INBD MID FLAP T/E CHORD CRACKED AT INBD AFT FLAP TRACK WS 180. REMOVED SEAL RETAINER AND DISPLACED MID-FLAP SKIN FOR ACCESS, REMOVED DAMAGED CHORD SECTION, FABRICATED NEW AND INSTALLED, CLOSED MID-FLAP SKIN AND RE-INSTALLED SEAL RETAINER IAW SRM 51-30-2,
- [SDR FDEA200911194183](https://openairdocs.org/sdr/FDEA200911194183.md): Skin · gouged · Nov 19, 2009 · N263FE · Boeing 727233 · Trailing Edge Flaps
  > LT WING, LT INBD FOREFLAP OTBD END IS GOUGED ON L/E REPAIR, W/S 360 REMOVED PREVIOUS REPAIR IAW SRM 51-30-2, FABRICATED REPAIR DOUBLER IAW SRM 57-50-4 FIG 1 AND 57-50-2 FIG 3, TREATED AND PRIMED IAW SRM 51-10-2, INSTALLED REPAIR DOUBLER IAW SRM 51- 30-2
- [SDR FDEA200911184186](https://openairdocs.org/sdr/FDEA200911184186.md): Skin · bulged · Nov 18, 2009 · N263FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > SKIN BULGE STA 620 STR 27L. CUT OUT DAMAGED AREA DIMS 6.025" X 1.12", FABRICATED DOUBLER REPAIR, TRIPLER REPAIR, STRUCTURAL FILLER, & FILLER IAW SRM 51-30-2, 53-30-3, AND 51-30-8.
- [SDR FDEA200911184019](https://openairdocs.org/sdr/FDEA200911184019.md): Skin · chafed · Nov 18, 2009 · N263FE · Boeing 727233 · Trailing Edge Flaps
  > RT WING, INBD FLAP, FORE FLAP L/E IS GOUGED, JUST INBD OF NR 6 JACKSCREW. CUT OUT DAMAGED AREA DIMS 1 1/2" X 3/4", FABRICATED PLATE USING 2024T-3.063 PO NR 9008875 DIMS 7 1/8" X 4 7/8" AND INSTALLED IAW SRM 57-50-4, 51-10-2 AND 51-30-2.
- [SDR FDEA200911184007](https://openairdocs.org/sdr/FDEA200911184007.md): Skin · cracked · Nov 18, 2009 · N263FE · Boeing 727233 · Leading Edge Devices
  > NR 5 SLAT UPPER SKIN CRACKED AT INBD SLAT HOOK MOUNT SCREW. REMOVED THE HOOK FOR ACCESS IAW SRM 51-30-2. STOP DRILLED CRACK IAW SRM 51-10-1. C/W HFEC INSP IAW NDTM PT 6, 51-00-00 FIG 23. CRACK END IN STOP DRILL HOLE. FAB REPAIR DOUBLER MAT USED 2024 T3.125"
- [SDR FDEA200911184006](https://openairdocs.org/sdr/FDEA200911184006.md): Spar · cracked · Nov 18, 2009 · N263FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > LT WING T/E FALSE SPAR CHORD ANGLE CRACKED WBL 118. REPAIRED LT WING T/E FALSE SPAR CHORD ANGLE IAW DWG SR27-57-038 REV C, REMOVED DOUBLER, CUT-OUT WEB AND CRACKED ANGLE, FABRICATED REPAIR ANGLES, STRAP, NEW CHORD ANGLE, WEB SECTION AND DOUBLER IAW DWG SR27
- [SDR FDEA200911184005](https://openairdocs.org/sdr/FDEA200911184005.md): Spar · cracked · Nov 18, 2009 · N263FE · Boeing 727233 · Wing Spar
  > RT WING T/E EDGE FALSE SPAR CHORD ANGLE CRACKED WBL 118. REPAIRED RT WING T/E FALSE SPAR CHORD ANGLE WBL 118 IAW DWG SR27-57-038 REV C, REMOVED DOUBLER, CUT OUT WEB AND CRACKED ANGLE, FABRICATED REPAIR ANGLES, STRAP, NEW CHORD ANGLE, WEB SECTION AND DOUBLE
- [SDR 08FDEA03984](https://openairdocs.org/sdr/08FDEA03984.md): Seat Track · corroded · Sep 22, 2008 · N263FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT SEAT TRACK HAS CORROSION BETWEEN STA 1765 AND STA 1785, LBL 106. REMOVED CORROSION. FOUND TO BE WITHIN LIMITS IAW SRM 53-70-00. FABRICATED CHANNEL IAW SRM 53-70-00. ALODINED & PRIMED IAW SRM 51-21- 01. INSTALLED CHANNEL REPAI
- [SDR 07FDEA04361](https://openairdocs.org/sdr/07FDEA04361.md): Frame · corroded · Sep 28, 2007 · N263FE · Boeing 727233 · Fuselage Main, Frame
  > AFT CARGO STA 950 S-26L HAS A CRACK AND CORROSION ON FRAME STA 950 REMOVED CORROSION IAW SRM 51-10-6, AREA WITHIN LIMITS IAW EA 7-5310-110790, HFEC ACCOMPLISHED, NO DEFECTS NOTED.
- [SDR 07FDEA04352](https://openairdocs.org/sdr/07FDEA04352.md): Floorbeam · corroded · Sep 27, 2007 · N263FE · Boeing 727233 · Fuselage Main, Floor Beam
  > AFT CARGO STA 950F LBL 44 MAIN DECK FLOORBEAM HAS CORROSION AROUND FASTENER HOLE. REMOVED AND REPLACED T-CAP IAW SRM 51-30 AND SRM 27-53-034.
- [SDR 06FDEA03571](https://openairdocs.org/sdr/06FDEA03571.md): Torque Link · scratched · Oct 3, 2006 · N263FE · Boeing 727233 · Nose/Tail Landing Gear
  > ON LANDING ROLLOUT BELOW 80 KNOTS, FELT A VIOLENT SHUDDERING FROM THE NOSE WHEEL AREA. AFTER BLOCKING A/C AND INSP'ING NOSE GEAR FOUND DAMAGE AS FOLLOWS: GROUND SHIFT ROD BROKEN AT LWR TORQUE LINK,RT FWD GEAR DOOR HAS A HOLE IN IT,LWR TORQUE LINK SCRATCH
- [SDR 05FDEA01832](https://openairdocs.org/sdr/05FDEA01832.md): Plate · gouged · Jul 7, 2005 · N263FE · Boeing 727200 · Fuselage Main, Structure
  > MAIN CARGO DOOR BS 460 TO 640 LBL 45 WL 295 DOOR CUTOUT INNER PLATE HAS NUMEROUS GOUGES. *S/D* BLENDED AND REPAIRED GOUGES IN MAIN CARGO DOOR INNER PLATE IAW EA 7-5330-89309.
- [SDR 05FDEA01830](https://openairdocs.org/sdr/05FDEA01830.md): Plate · gouged · Jul 7, 2005 · N263FE · Boeing 727200 · Fuselage Main, Structure
  > MAIN CARGO DOOR BS 460 TO 480 LBL 24 WL 287 DOOR CUTOUT INNER PLATE HAS NUMEROUS GOUGES. *S/D* BLENDED NUMEROUS GOUGES IN DOOR CUTOUT INNER PLATE IAW EA 7-5330-89309.
- [SDR 05FDEA01828](https://openairdocs.org/sdr/05FDEA01828.md): Skin · gouged · Jul 7, 2005 · N263FE · Boeing 727200 · Fuselage Main, Plate/Skin
  > MAIN CARGO DOOR BS 620 TO 640 LBL 24 WL 287 DOOR CUTOUT INNER PLATE HAS NUMEROUS GOUGES. *S/D* BLENDED NUMEROUS GOUGES AT MAIN CARGO DOOR CUTOUT INNER PLATE PER EA 7-5330-89309.
- [SDR 05FDEA01824](https://openairdocs.org/sdr/05FDEA01824.md): Skin · lightning strike · Jul 7, 2005 · N263FE · Boeing 727200 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE IN SKIN AT BS 441 1.5 X 1.5 INCH AT STR 23. *S/D* REPAIRED LIGHTNING STRIKES IAW SRM 53-30-3.
- [SDR 05FDEA01822](https://openairdocs.org/sdr/05FDEA01822.md): Skin · gouged · Jul 7, 2005 · N263FE · Boeing 727200 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERNAL SKIN, SECTION 48, BS 1329 LBL 22 3 INCHES O/B OF AFT AIRSTAIR CUTOUT GOUGED. *S/D* GOUGED IN EXTERNAL SKIN OF THE AFT AIRSTAIR CUTOUT AT BS 1329 LBL 22 WAS OUT OF LIMITS IAW SRM 53-30-1. CUT OUT DAMAGE AND FABRICATED REPAIR IAW SRM 51-10
- [SDR 05FDEA01715](https://openairdocs.org/sdr/05FDEA01715.md): Support Angle · chafed · Jun 28, 2005 · N263FE · Boeing 727200 · Main Landing Gear
  > LT MLG FWD TRUNNION I/B SUPPORT ANGLE IS CHAFED ON LWR EDGE. REPAIR (BLENDED), STRESS RELIEVED AND REFINISHED LT MLG FWD TRUNNION SUPPORT ANGLE ON LWR EDGE IAW SRM 51-10-1, SOPM 20-10-03 AND FED EX EA 7-5710-86323 REPAIR WITHIN LIMITS IAW EA - 7-5710-86323
- [SDR 05FDEA01708](https://openairdocs.org/sdr/05FDEA01708.md): Skin · damaged · Jun 27, 2005 · N263FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERNAL SKIN OF AFT AIRSTAIR, SECTION 48, AREA FROM LE TO 27 INCH AFT OF LE, LBL 21 TO RBL 21, HAS GRAVEL DAMAGE.
- [SDR 05FDEA01665](https://openairdocs.org/sdr/05FDEA01665.md): Skin · corroded · Jun 23, 2005 · N263FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > AFT CARGO CORROSION ON FUSELAGE SKIN STA 1010, STR 29L. OUT OF LIMITS AREA CUT OUT, INSTALLED SRM REPAIR TO THE SKIN AT STA. 1010, STR 29L, REF SRM 53-30-3 PAGE 14E-14O FIG 3A
- [SDR 05FDEA01648](https://openairdocs.org/sdr/05FDEA01648.md): Skin · gouged · Jun 22, 2005 · N263FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERNAL SKIN GOUGED AT AFT AIRSTAIR CUTOUT, BS 1230, LBL 20. REPAIRED SKIN AT AFT AIR STAIR CUTOUT BS 1230, LBL 20 PER SRM 53-30-3.
- [SDR 05FDEA01616](https://openairdocs.org/sdr/05FDEA01616.md): Keelbeam · corroded · Jun 17, 2005 · N263FE · Boeing 727200 · Fuselage Main, Keel
  > AFT CARGO CORROSION ON KEELBEAM STA 950D TO 950E, STR 29L. BLENDED CORROSION AT KEELBEAM STA 950D TO 950E OUT OF LIMITS. INSTALLED REPAIR IAW SR27-53-023A. FOUND TO BE A MINOR REPAIR.
- [SDR 03FDEA00076](https://openairdocs.org/sdr/03FDEA00076.md): Skin · gouged · Jan 27, 2003 · N263FE · Boeing 727233 · Cargo/Baggage Doors
  > NR 3 CARGO DOOR EXTERIOR SKIN HAS A GOUGE 15 INCHES FROM FWD EDGE 28 INCHES FROM LOWER EDGE. GOUGE ON NR 3 CARGO DOOR EXTERIOR SKIN FOUND TO BE OUT OF LIMITS IAW SRM 52-00-2. REMOVED AND REPLACED NR 3 CARGO DOOR EXTERIOR SKIN IAW EA NR7-5230- 68160, FUNCTI
- [SDR 03FDEA00072](https://openairdocs.org/sdr/03FDEA00072.md): Floorbeam · damaged · Jan 22, 2003 · N263FE · Boeing 727200 · Fuselage Main, Floor Beam
  > MECHANICAL DAMAGE ON FLOORBEAM BS 990 RBL 37.5 WL 207.
- [SDR 03FDEA00071](https://openairdocs.org/sdr/03FDEA00071.md): Shear Tie · dented · Jan 22, 2003 · N263FE · Boeing 727200 · Fuselage Main, Structure
  > DENT IN SKIN AT FRAME BS 460 BETWEEN STR 20R - 21R. FOUND SKIN TO BE WITHIN LIMITS. SHEAR TIE AT BS 460 STR 20R-21R OUT OF LIMITS. REPAIRED SHEAR TIE IAW SRM 51-40-3 FIG 1 AND EA 7-5310-54395.
- [SDR 03FDEA00063](https://openairdocs.org/sdr/03FDEA00063.md): Web · corroded · Jan 22, 2003 · N263FE · Boeing 727200 · Fuselage Miscellaneous Structure
  > CORROSION, FORWARD CARGO DOORWAY LOWER SILL BEAM WEB, STA 560-620 STR 26R, NUMEROUS AREAS OUTBOARD SIDE. REMOVED, FABRICATED, AND INSTALLED FORWARD CARGO DOOR LWR BEAM WEB IAW SRM 53-10-1, 51-20-1, 51-30-2.
- [SDR 03FDEA00062](https://openairdocs.org/sdr/03FDEA00062.md): Seat Track · corroded · Jan 22, 2003 · N263FE · Boeing 727200 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK OUTBOARD FLANGE BS 720D - 720D+10 LBL 25 WL 208. REMOVED AND REPLACED NEW SEAT TRACK IAW SRM 51-30-2.

Next page: https://openairdocs.org/deregistered/N263FE-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 = 'N263FE' AND deregistration_id = 'N263FE-2013-12-19'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N263FE-2013-12-19/reports

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