# Service difficulty reports: N266FE, cancelled Feb 11, 2013

A list on [N266FE, cancelled Feb 11, 2013](https://openairdocs.org/deregistered/N266FE-2013-02-11.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 · 115 reports

- [SDR FDEA201301040015](https://openairdocs.org/sdr/FDEA201301040015.md): Lamp · inoperative · Jan 4, 2013 · N266FE · Boeing 727233 · Emergency Lighting
  > FOUND DURING PRE-DISPATCH CHECK, FWD ENTRY DOOR ESCAPE SLIDE LIGHT INOPERATIVE. LAMPED EMERGENCY LIGHT ASSY IAW MM 33-50-041-2. OPS NORMAL.
- [SDR FDEA201205171826](https://openairdocs.org/sdr/FDEA201205171826.md): Oxygen Mask · damaged · May 17, 2012 · N266FE · Boeing 727233 · Portable Oxygen System
  > DURING PRE-FLIGHT, FOUND PORTABLE O2 MASK HAD A HOLE IN THE HOSE. INSTALLED NEW OXYGEN MASK IAW MM 35-30-000-0. OK FOR SERVICE.
- [SDR FDEA201203130926](https://openairdocs.org/sdr/FDEA201203130926.md): Controller · failed · Mar 13, 2012 · N266FE · Boeing 727233 · Cabin Pressure Controller
  > COULD NOT MAINTAIN PRESSURIZATION ON NR 1 PACK AT 25K, DIFFERENTIAL UP TO 7PSI ON CLIMB BUT SLOWLY LOST PRESSURIZATION TO 3 PSI; COULD ONLY MAINTAIN 7K AT 15K ALTITUDE. LOST COMPLETE PRESSURIZATION AT 4K ALTITUDE, AUTOFAIL & STANDBY LIGHTS, TRIED TO MANUAL VAL
- [SDR FDEA201201210285](https://openairdocs.org/sdr/FDEA201201210285.md): Bottle · low pressure · Jan 21, 2012 · N266FE · Boeing 727233 · Escape Slide
  > FORWARD ENTRY DOOR ESCAPE SLIDE BOTTLE PRESSURE IS LOW. REMOVED AND REPLACED SLIDE ASSY
- [SDR FDEA201112155282](https://openairdocs.org/sdr/FDEA201112155282.md): Actuator · malfunctioned · Dec 15, 2011 · N266FE · Boeing 727233 · Auxiliary Gear (Tail Skid)
  > TAIL SKID LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. COMPLIED WITH QRH. FUEL USAGE INCREASE. REPLACED TAIL SKID ACTUATOR IAW MM 32-71-012-4-0. OPS CHECKED NORMAL. ACFT OK FOR SERVICE.
- [SDR FDEA201108253480](https://openairdocs.org/sdr/FDEA201108253480.md): Gauge · out of position · Aug 25, 2011 · N266FE · Boeing 727233 · Escape Slide
  > PRESSURE GAUGE NOT VISIBLE ON DOOR SLIDE WINDOW. REPOSITIONED SLIDE, GAUGE VISIBLE AT THIS TIME REF MM 25-60-015-2-0.
- [SDR FDEA201012144661](https://openairdocs.org/sdr/FDEA201012144661.md): Duct · damaged · Dec 14, 2010 · N266FE · Boeing 727233 · Pneumatic Distribution System
  > ON DESCENT, WITH WING ANTI ICE ON, RECEIVED LOWER AFT BODY LIGHT, WITH LOST AUTO PRESSURIZATION. RAN QRH, RESET WING ANTI ICE & TRIED AGAIN. RECEIVED LOWER AFT BODY LIGHT & AUTO PRESSURIZATION FAIL LIGHT AGAIN. RAN PRESSURIZATION IN MANUAL. TRIED AUTO PRE
- [SDR FDEA201007082474](https://openairdocs.org/sdr/FDEA201007082474.md): Support Angle · cracked · Jul 8, 2010 · N266FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > RT LOWER TORQUE BOX UPPER SUPPORT ANGLE IS CRACKED AT INBD END BS 1263 REMOVED RT LOWER TORQUE BOX UPPER SUPPORT ANGLE IAW SRM 51-30-2, FABRICATED UPPER SUPPORT ANGLE MATERIAL USED BAC 1514-1617 7075 T6511 PO NR 20105119 DIM 28" X 3.2500" IAW DWG NR 65-1
- [SDR FDEA201007062372](https://openairdocs.org/sdr/FDEA201007062372.md): Rib · cracked · Jul 6, 2010 · N266FE · Boeing 727233 · Wing, Rib/Bulkhead
  > NR 6 SLAT I/B & O/B ACTUATOR ATTACH RIBS CRACKED. REMOVED I/B AND O/B RIBS TO NR 6 SLAT IAW SRM 51-30-2 FABRICATED, LOCATED AND DRILLED NEW I/B AND O/B RIBS, 2024 0 MATERIAL PO 29126300 DIM 16 1/2" X 6" IAW SRM 57-50-2 FIG 2 INSTALLED NEW RIBS 2 EACH IAW S
- [SDR FDEA201007052369](https://openairdocs.org/sdr/FDEA201007052369.md): Skin · bulged · Jul 5, 2010 · N266FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > BULGE EXTERIOR FUSELAGE BS 660 BETWEEN STR 28L TO 28R. CUT OUT DAMAGED AREA 3" X 1.375" AND 1.75" X 1.5" IAW SRM 53-30-3. FABRICATED DOUBLER FROM 2024T3.080" DIM. 17.50" X 10.50" IAW SRM 53-30-3 AND 53-30-2. INSTALLED REPAIR PARTS IAW SRM 53-30-3 AND 51-30-
- [SDR FDEA201006302310](https://openairdocs.org/sdr/FDEA201006302310.md): Attach Bracket · cracked · Jun 30, 2010 · N266FE · Boeing 727233 · Leading Edge Devices
  > NR 8 SLAT ACTUATOR IB & OB ATTACH BRACKETS INSIDE PLATES ARE CRACKED. REMOVED I/B AND O/B BRACKETS IAW SRM 51-30-2. FABRICATED BRACKETS FROM 7075-0.063" DIM. 9" X 4.80 " (2 EA) AND I/B PLATE FROM 7075T6.125" DIM. 3.8" X 7.5" IAW DWG. 65-17255. HEAT TREATED B
- [SDR FDEA201006302309](https://openairdocs.org/sdr/FDEA201006302309.md): Attach Bracket · cracked · Jun 30, 2010 · N266FE · Boeing 727233 · Leading Edge Devices
  > NR 8 SLAT ACT. IB & OB ATTACH BRACKETS INSIDE PLATES ARE CRACKED. REMOVED I/B AND O/B BRACKETS FROM NR 8 SLAT IAW SRM 51-30-2. FABRICATED I/B AND O/B BRACKETS FROM 7075-0.063" DIM. 9" X 4.80 " (2 EA) AND I/B PLATE FROM 7075T6.125" DIM. 3.8" X 7.5" IAW DWG. 6
- [SDR FDEA201006302272](https://openairdocs.org/sdr/FDEA201006302272.md): Skin · dented · Jun 30, 2010 · N266FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > DENT EXTERIOR FUSELAGE BS 1060 STR 20L. CUT OUT DAMAGED AREA DIM. 3.375" X 2.625" IAW SRM 53-30-3. FABRICATED DOUBLER FROM 2024T3.071" DIM. 13.25" X 9.25" AND FILLER FROM 2024T3.063" DIM. 14.75" X 6.5" IAW SRM 53-30-3. INSTALLED REPAIR PARTS IAW SRM 53-30-3.
- [SDR FDEA201006282269](https://openairdocs.org/sdr/FDEA201006282269.md): Web · cracked · Jun 28, 2010 · N266FE · Boeing 727233 · Fuselage Main, Structure
  > AFT AIRSTAIR AREA - RT LOWER TORQUE BOX WEB LIGHTNING HOLE IS CRACKED AT BS 1223. TRIMMED OUT DAMAGED AREA DIM..5" X.25" IAW SRM 51-10-1, FABRICATED REPAIR WEB DOUBLER FROM 2024T3.040" DIM. 4" X 2.625" IAW SRM 51-40-2 AND INSTALLED DOUBLER IAW SRM 51-30-2
- [SDR FDEA201006282271](https://openairdocs.org/sdr/FDEA201006282271.md): Web · cracked · Jun 28, 2010 · N266FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > AFT AIRSTAIR AREA - RT LOWER TORQUE BOX WEB LIGHTNING HOLE IS CRACKED AT BS 1243 TRIMMED OUT DAMAGED AREAS DIM..375" X.5" AND.5" X.75" IAW SRM 51-10-1, FABRICATED WEB REPAIR DOUBLER FROM 2024T3.040" DIM 2.375" X 6.625" IAW SRM 51- 40-2, FIG 1 AND INSTA
- [SDR FDEA201006282270](https://openairdocs.org/sdr/FDEA201006282270.md): Web · cracked · Jun 28, 2010 · N266FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > AFT AIRSTAIR AREA - RT LOWER TORQUE BOX WEB LIGHTNING HOLE IS CRACKED AT BS 1225 TRIMMED OUT DAMAGED AREA DIM..5" X.375" IAW SRM 51-10-1, FABRICATED WEB REPAIR DOUBLER FROM 2024T3.040" DIM. 4" X 2.25" IAW SRM 51-40-2, FIG 1 AND INSTALLED WEB REPAIR DOUBLER
- [SDR FDEA201006262202](https://openairdocs.org/sdr/FDEA201006262202.md): Web · cracked · Jun 26, 2010 · N266FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > AFT AIRSTAIR AREA - RT LOWER TORQUE BOX LIGHTNING HOLE IS CRACKED AT BS 1230 REMOVED DAMAGED AREA IAW SRM 51-40-2 AND 51-10-1, REV 103. FABRICATED DOUBLER IAW SRM 51-40-2 FIG 1 AND 53-10-2. INSTALLED DOUBLER IAW SRM 51-30-2.
- [SDR FDEA201006252194](https://openairdocs.org/sdr/FDEA201006252194.md): Bulkhead · cracked · Jun 25, 2010 · N266FE · Boeing 727233 · Fuselage Main, Bulkhead
  > AFT PIT CRACK IN BS 1183 BULKHEAD AT APPROX. RBL 24 & WL 167. CUT OUT WEB AROUND THE CRACK APPROX. 2.875" X 1.875" IAW EA 7-5310-135559. FABRICATED FILLER FROM 2024T3.050" DIM. 2.75" X 1.75", DOUBLER FROM 2024T3.071" DIM. 7.125" X 6", 3 EACH FILLERS FROM
- [SDR FDEA201006252193](https://openairdocs.org/sdr/FDEA201006252193.md): Doubler · gouged · Jun 25, 2010 · N266FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > GOUGE ON MCD INNER DOUBLER STA. 560 S4L. REMOVED MCD INNER SKIN UPPER CENTER PANEL IAW SRM 51-30-2. FABRICATED NEW MCD INNER SKIN UPPER CENTER PANEL FROM 2024T3.090" DIM. 88" X 34" IAW SRM 53-10-2 FIGURE 3A. INSTALLED NEW MCD INNER SKIN UPPER CENTER PANEL IAW
- [SDR FDEA201006252145](https://openairdocs.org/sdr/FDEA201006252145.md): Skin · damaged · Jun 25, 2010 · N266FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > L-1 DOOR RAIN GUTTER INSTALLED WITH BLIND FASTENERS THROUGH FUSELAGE SKIN WITH NO E.D. WITH SOLID FASTENERS. DRILLED DAMAGED AREAS (3 EACH) TO MINIMUM DIAMETER IAW SRM 51-30-2 AND EA 7-5330-135558. FABRICATED REPAIR DOUBLER FROM 2024T3.090" DIM. 33" X 22.25",
- [SDR FDEA201006242135](https://openairdocs.org/sdr/FDEA201006242135.md): Skin · cracked · Jun 24, 2010 · N266FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > FORWARD GALLEY DOOR CUTOUT, CRACKED ON LOWER AFT CORNER. CUT OUT DAMAGED AREA OF SKIN APPROX. 2.5" X 1" IAW FEDEX EO 7-5313-7-2304 PT2. FABRICATED REPAIR FILLER FROM 2024T3.080" DIM. 2.5" X 1" AND DOUBLER FROM 2024T3.080" DIM. 26.125" X 20.125" IAW EO 7-
- [SDR FDEA201006242144](https://openairdocs.org/sdr/FDEA201006242144.md): Skin · gouged · Jun 24, 2010 · N266FE · Boeing 727233 · Cargo/Baggage Doors
  > GOUGE ON MCD INNER DOUBLER STA. 640 STR. 5L. REMOVED INNER SKIN AFT UPPER PANEL IAW SRM 51-30-2. FABRICATED NEW INNER SKIN FROM 2024T3.125" DIM. 48" X 79" IAW SRM 53-10-2 FIGURE 3A. INSTALLED INNER SKIN IAW SRM 51-30-2
- [SDR FDEA201006232143](https://openairdocs.org/sdr/FDEA201006232143.md): Skin · gouged · Jun 23, 2010 · N266FE · Boeing 727233 · Cargo/Baggage Doors
  > GOUGE ON MCD INNER DOUBLER STA. 480 STR. 4L. REMOVED FORWARD UPPER INNER SKIN IAW SRM 51-30-2. FABRICATED NEW INNER SKIN FROM 2024T3.125" DIM. 48" X 79" IAW SRM 53-10-2 FIGURE 3A. INSTALLED FORWARD UPPER INNER SKIN IAW SRM 51-30-2.
- [SDR FDEA201006232123](https://openairdocs.org/sdr/FDEA201006232123.md): Doubler · gouged · Jun 23, 2010 · N266FE · Boeing 727233 · Cargo/Baggage Doors
  > GOUGES ON MCD INNER DOUBLER STATION 620, STRINGER 9L. REMOVED INNER SKIN DOUBLER "SPLICE" IAW SRM 51-30-2. FABRICATED NEW INNER SKIN DOUBLER "SPLICE" FROM 2024T3.125" DIM. 11" X 22" IAW SRM 53-10-2 FIGURE 3A. INSTALLED INNER SKIN DOUBLER "SPLICE" IAW SRM
- [SDR FDEA201006232276](https://openairdocs.org/sdr/FDEA201006232276.md): Doubler · gouged · Jun 23, 2010 · N266FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > GOUGE ON MCD INNER DOUBLER STA 640, STR 11L. CUT OUT DAMAGED AREA DIM. 28" X 22 IAW EA 7-5330-135557. FABRICATED NEW WEB FROM 2024T3.125" DIM. 28" X 22" AND SPLICE STRAP FROM 2024T3.125" DIM. 22" X 4" IAW EA 7-5330-135557. INSTALLED REPAIR PARTS IAW FEDEX
- [SDR FDEA201006232275](https://openairdocs.org/sdr/FDEA201006232275.md): Skin · gouged · Jun 23, 2010 · N266FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > GOUGE ON MCD INNER DOUBLER STA 620 STR 16L CUT OUT DAMAGED AREA DIM. 2" X 1" IAW EA 7-5330-135557. FABRICATED FILLER FROM 2024T3.125" DIM. 2" X 1" AND DOUBLER FROM 2024T3.125" DIM. 6" X 3" IAW EA 7-5330-135557. INSTALLED REPAIR PARTS IAW IAW EA 7-5330-13555
- [SDR FDEA201005141531](https://openairdocs.org/sdr/FDEA201005141531.md): Switch · misinstalled · May 14, 2010 · N266FE · Boeing 727233 · Leading Edge Slat Control System
  > ON CLEAN UP OF FLAPS. NR 1 PORT L/E FLAPS WOULD NOT RETRACT FROM 5 DEGREES TO 2 DEGREES POSITION. GSP U TRIED JUMPER PLUG NO HELP. ON FURTHER TROUBLESHOOTING FOUND WEAR MARKS WHERE SWITCH LINKAGE WAS CONTACTING AIRFRAME. NR1 L/E FLAP SWITCH IMPROPERLY INST
- [SDR FDEA200911274207](https://openairdocs.org/sdr/FDEA200911274207.md): Actuator · failed · Nov 27, 2009 · N266FE · Boeing 727233 · Autopilot Trim Servo
  > IN CRUISE FLIGHT AT FL310, MACH.84, THE AUTOPILOT WAS PULSING BACK AND FORTH WITH A CORRESPONDING ACFT PITCHING MOVEMENT. DECIDED TO TRY SERVO B, UPON DISCONNECTING AUTOPILOT, DISCOVERED ACFT WAS OUT-OF-TRIM NOSE UP. COULD NOT TRIM THE ACFT NOSE DOWN WITH
- [SDR 08FDEA02923](https://openairdocs.org/sdr/08FDEA02923.md): Module · failed · Jul 16, 2008 · N266FE · Boeing 727233 · Exterior Lighting
  > DURING GEAR EXTENSION RECEIVED UNSAFE NOSEGEAR (NO GREEN LIGHT) ALL GEAR INDICATIONS S/O PANEL NORMAL, NO GEAR WARNING HORN DURING THROTTLE REDUCTION. COMPLIED WITH QRH, MANUAL GEAR EXTENDED. LIGHT REMAINED OUT. AFTER CRANKING NOSEWHEEL TO STOPS, LIGHT REMA
- [SDR FDEA200807152876](https://openairdocs.org/sdr/FDEA200807152876.md): Switch · malfunctioned · Jul 15, 2008 · N266FE · Boeing 727233 · Landing Gear Position and Warning
  > DURING NORMAL LANDING GEAR EXTENSION, RECEIVED UNSAFE NLG INDICATION. C/W QRH, LIGHT TEST OK, USED MANUAL NLG GEAR EXT AND RECEIVED SAFE NLG IND AFTER ONLY.2500 TURN OF HAND CRANK. SWUNG NOSE GEAR SEVERAL TIMES IAW MM. REMOVED AND REPLACED NLG LOCK AND POS
- [SDR 08FDEA02876](https://openairdocs.org/sdr/08FDEA02876.md): Switch · malfunctioned · Jul 15, 2008 · N266FE · Boeing 727233 · Landing Gear Position and Warning
  > DURING NORMAL LANDING GEAR EXTENSION RECEIVED UNSAFE NLG INDICATION. C/W QRH, LIGHT TEST OK, USED MANUAL NLG GEAR EXT AND RECEIVED SAFE NLG IND AFTER ONLY 1/4 TURN OF HAND CRANK. SWUNG NOSE GEAR SEVERAL TIMES PER 727-200 MM 07-11-000-2 CND. REMOVED AND REPL
- [SDR 08FDEA00668](https://openairdocs.org/sdr/08FDEA00668.md): Skin · dented · Feb 29, 2008 · N266FE · Boeing 727233 · Trailing Edge Flaps
  > LT WING I/B AFT FLAP DENTED AND DELAMINATED AT WBL 124 CUT OUT DAMAGED AREA ON LT WING I/B AFT FLAP LWR SURFACE WBL 124 AND REMOVED DAMAGED CORE. FABRICATED DOUBLER AND CORE PLUG IAW SRM 57-50-2. BONDED CORE AND DOUBLER, AND PRIMED AND SEALED IAW SRM 51-40-2
- [SDR 08FDEA00661](https://openairdocs.org/sdr/08FDEA00661.md): Support Beam · cracked · Feb 29, 2008 · N266FE · Boeing 727233 · Wing Miscellaneous Structure
  > NR 7 SPOILER FITTING TO FALSE SPAR ATTACHMENT REPAIR CRACKED AT WS 198. REMOVED ACTUATOR FITTING SRM 51-30-2. REPAIRED NR 7 SPOILER SUPPORT BEAM (FALSE SPAR) IAW DWG NR 5127-57-038 REV C. REINSTALLED SPOILER ACTUATOR FITTING IAW SRM 51-30-2.
- [SDR 08FDEA00660](https://openairdocs.org/sdr/08FDEA00660.md): Support Beam · cracked · Feb 29, 2008 · N266FE · Boeing 727233 · Wing Miscellaneous Structure
  > NR 8 SPOILER FITTING TO FALSE SPAR ATTACHMENT REPAIR CRACKED AT WS 198. REMOVED ACTUATOR FITTING IAW SRM 51-30-2. REPAIRED NR 8 SPOILER SUPPORT BEAM (SPAR) IAW DWG NR SR27-57-038 REV C. REINSTALLED SPOILER ACTUATOR FITTING IAW SRM 51-30-2.
- [SDR 08FDEA00659](https://openairdocs.org/sdr/08FDEA00659.md): Seat Track · corroded · Feb 29, 2008 · N266FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN CARGO COMPARTMENT, SEAT TRACK HAS CORROSION AT STA 950A - 1030, BL 46R. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-10-1 FIG 3. REMOVED SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK SECTION IAW SRM 53-10-5 FIG 1. TREATED
- [SDR 08FDEA00630](https://openairdocs.org/sdr/08FDEA00630.md): Skin · cracked · Feb 27, 2008 · N266FE · Boeing 727227 · Fuselage Main, Plate/Skin
  > LT LWR FUSELAGE EXTERIOR SKIN SURFACE SHOWS CRACK AT STA 520, ABOVE STR 23L, FWD OF THE STATIC PORT. PERFORMED HFEC AND FOUND CRACK 2" IAW B727 NDTM PART 6 51-00-00 FIG23. REPAIRED FUSELAGE, MDCD SURROUND STRUCTURE TRIPLER AT STA 520, STR 23L IAW EA NR 7-533
- [SDR 08FDEA00524](https://openairdocs.org/sdr/08FDEA00524.md): Rib · cracked · Feb 20, 2008 · N266FE · Boeing 727233 · Horizontal Stabilizer, Spar/Rib
  > LT HORIZONTAL STABILIZER MAIN BOX INTERIOR RIB CRACKED AT LIGHTENING HOLE STAB STA 188. CUT OUT DAMAGED AREA IAW SRM 55-10-5 FIG2 NAD 55-10-4 FIG2. FABRICATED REPAIR FOR FWD SPAR WEB IAW SRM 55-10-5 FIG 2 PARTS AND AFFECTED AREAS TREATED AND PRIMED IAW SRM
- [SDR 08FDEA00523](https://openairdocs.org/sdr/08FDEA00523.md): Rib · cracked · Feb 20, 2008 · N266FE · Boeing 727233 · Elevator Structure
  > LT HORIZONTAL STABILIZER MAIN BOX INTERIOR RIB CRACKED AT LIGHTENING HOLE STAB STA 69. CUT OUT FWD WEB FOR ACCESS IAW SRM 55-10-3 FIG2. FABRICATED REPAIR DOUBLER FOR INTERNAL RIB IAW SRM 55-10-4 FIG 2 AND 55-10-2 FIG2. FABRICATED REPAIR DOUBLERS IAW SRM 55-10
- [SDR 08FDEA00525](https://openairdocs.org/sdr/08FDEA00525.md): Spar · damaged · Feb 20, 2008 · N266FE · Boeing 727233 · Wing Spar
  > LT WING LEADING EDGE FRONT SPAR FASTENER HOLE HAS NO EDGE DISTANCE AT WS 167, LE STA 90. REPAIRED IAW EA 7-5710-116957.
- [SDR 08FDEA00471](https://openairdocs.org/sdr/08FDEA00471.md): Seat Track · corroded · Feb 17, 2008 · N266FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN CARGO COMPARTMENT, SEAT TRACK HAS CORROSION FROM STA 950 TO STA 950E, BL 0. REMOVED DAMAGED SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK SECTION IAW SRM ER 01-049, SRM 53-10-5 FIG 7A. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED S
- [SDR 08FDEA00470](https://openairdocs.org/sdr/08FDEA00470.md): Seat Track · corroded · Feb 17, 2008 · N266FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN CARGO COMPARTMENT, SEAT TRACK HAS CORROSION FROM STA 870 TO STA 890, BL 0. REMOVED SEAT TRACK WITH OUT OF LIMIT COROSION IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK IAW SRM (ER 01-049) 53-10-5 AND 53-10-2 FIG7. LOCATED AND DRLLED NEW SEAT TRACK IAW
- [SDR 08FDEA00469](https://openairdocs.org/sdr/08FDEA00469.md): Seat Track · corroded · Feb 17, 2008 · N266FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN CARGO COMPARTMENT, SEAT TRACK HAS CORROSION FROM STA 1070 TO STA 1130, BL 0. REMOVED SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED SEAT TRACK IAW SRM 53-10-5, 53-10-2 FIG 7A (ER 01-049) LOCATED AND DRILL NEW SEAT TRACK IAW SRM 51-30-5. TREATED AND
- [SDR 08FDEA00468](https://openairdocs.org/sdr/08FDEA00468.md): Seat Track · corroded · Feb 17, 2008 · N266FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN CARGO COMPARTMENT, SEAT TRACK HAS CORROSION FROM STA 890 TO STA 950, BL 0. REMOVED AND REPLACED SEAT TRACK IAW SRM ER 01-049 AND SRM 53-10-5 AND 53-10-2 FIG 7A
- [SDR 08FDEA00418](https://openairdocs.org/sdr/08FDEA00418.md): Frame · dented · Feb 13, 2008 · N266FE · Boeing 727233 · Fuselage Main, Frame
  > AFT CARGO COMPARTMENT INTERIOR, FRAME SURFACE HAS DENT AT STA 950F, STR 25L. REMOVED PREVIOUS REPAIR ANGLE IAW SRM 51-30-2. FABRICATED NEW REPAIR ANGLE IAW SRM 51-20-151-40-3 FIG 1 AND 53-10-2 FIG 5. HEAT TREATED ANGLE. TREATED AND PRIMED PART IAW SRM 51-10-2
- [SDR 08FDEA00417](https://openairdocs.org/sdr/08FDEA00417.md): Floorbeam · corroded · Feb 13, 2008 · N266FE · Boeing 727233 · Fuselage Main, Floor Beam
  > MAIN CABIN, FLOORBEAM UPPER SURFACE HAS CORROSION AT STA 846, LBL 48. REMOVED SEAT TRACK AND REMOVED SUPPORT TEE IAW SRM 51-30-2. FABRICATED, LOCATED AND DRILLED NEW TEE BEAM IAW SRM 53-10-2 FIG7 AND 51-30-5.TREATED AND PRIMED AFFECTED AREA IAW SRM 51-10-2. I
- [SDR 08FDEA00414](https://openairdocs.org/sdr/08FDEA00414.md): Skin · dented · Feb 13, 2008 · N266FE · Boeing 727233 · Passenger/Crew Doors
  > AFT FUSELAGE EXTERIOR, NR 3 CARGO DOOR SKIN HAS SEVERAL DENTS AT FWD LWR EDGE BS 1090, S26-27R. EVALUATED DENTS AND FOUND OUT OF LIMITS. CUT OUT DAMAGED SKIN IAW SRM 53-00-03 FIG4. FABRICATED REPAIR DOUBLER AND FILLER IAW SRM 52-30-1 FIG 6. TREATED AND PRIM
- [SDR 08FDEA00413](https://openairdocs.org/sdr/08FDEA00413.md): Seat Track · corroded · Feb 13, 2008 · N266FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CARGO COMPARTMENT, SEAT TRACK HAS CORROSION IN SEVERAL PLACES FROM STA 360 TO STA 380, LBL 48. REMOVED CORROSION IAW SRM 51-10-6 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-2 FIG 7 AND 53-10-1 FIG3 SRM PAG23. REMOVED SEAT TRACK SECTION IAW 51-30-2. FAB
- [SDR 08FDEA00412](https://openairdocs.org/sdr/08FDEA00412.md): Seat Track · corroded · Feb 12, 2008 · N266FE · Boeing 727200 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CARGO COMPARTMENT, SEAT TRACK CORRODED IN NUMEROUS PLACES FROM BS 360-400, LBL 24. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-2 FIG7 AND 53-10-1 FIG3, SRM PAGE 23. REMOVED SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK
- [SDR 08FDEA00411](https://openairdocs.org/sdr/08FDEA00411.md): Skin · damaged · Feb 12, 2008 · N266FE · Boeing 727200 · Fuselage Main, Plate/Skin
  > AFT CARGO COMPARTMENT FRAME SHEAR TIE HAS IMPROPER RIVET INSTALLATION ON FWD SIDE. RIVET INSTALLED THRU ANOTHER RIVET AT STA. 970, STR 25-26L. REMOVED RIVETS FROM SHEAR TIE AND FAIRING ATTACHMENT SUPPORT IAW SRM 51-30-2. CUT-OUT DAMAGED SKIN. FABRICATED REPAI
- [SDR 08FDEA00410](https://openairdocs.org/sdr/08FDEA00410.md): Skin · corroded · Feb 12, 2008 · N266FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > LT WING TO BODY FUSELAGE SKIN SURFACE SHOWS CORROSION AND GOUGE AT LAP JOINT STA 720E, STR 19L. BURNISHED AFFECTED AREA AND FOUND OUT OF LIMITS IAW SRM 53-30-1 FIG1,2. REMOVED FAIRING FOR ACCESS IAW SRM 51-30-2. CUT OUT DAMAGE DIM 43/4 X 23/4. FABRICATED DOUB

Next page: https://openairdocs.org/deregistered/N266FE-2013-02-11/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 = 'N266FE' AND deregistration_id = 'N266FE-2013-02-11'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N266FE-2013-02-11/reports

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