# Service difficulty reports: N262FE, cancelled Dec 18, 2013

A list on [N262FE, cancelled Dec 18, 2013](https://openairdocs.org/deregistered/N262FE-2013-12-18.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 · 157 reports

- [SDR FDEA201110134476](https://openairdocs.org/sdr/FDEA201110134476.md): Switch · damaged · Oct 13, 2011 · N262FE · Boeing 727233 · Landing Gear Position and Warning
  > AFTER GEAR RETRACTION, NOSE GEAR UNSAFE RED LIGHT REMAINED ILLUMINATED. RAN QRH PROCEDURE AND LIGHT REMAINED ILLUMINATED. R & R NOSE GEAR LOCK SWITCH IAW MM32-61-071-4. NOSE GEAR POSITION AND WARNING SYS GROUND OPS CHECK NORMAL IAW MM32-61-071-5. OK FOR S
- [SDR FDEA201109224034](https://openairdocs.org/sdr/FDEA201109224034.md): Retainer · broken · Sep 22, 2011 · N262FE · Boeing 727233 · Emergency Equipment
  > EMERGENCY SLIDE GIRT BAR RETAINER PLASTIC CLIP IS BROKEN LT SIDE. REMOVED SLIDE ASSY FROM L1 DOOR. OPENED SLIDE COMPARTMENT COVER. R & R STOWAGE RETAINER FOR GIRT BAR. CLOSED AND SECURED COVER AND REINSTALLED SLIDE ASSY ON L1 DOOR IAW MM 25-60-015-2.
- [SDR FDEA201104071377](https://openairdocs.org/sdr/FDEA201104071377.md): Valve · leaking · Apr 7, 2011 · N262FE · Boeing 727233 · Engine Bleed Air System
  > DURING CLIMB OUT, NR 1 ENG STRUT LIGHT ON, COMPLIED QRH, RETURN TO MEM LIGHT WENT OUT AFTER APPROX 2 MIN. FOUND CLAMP AND MOD VALVE LEAKING. REMOVED AND REPOSITIONED CLAMP PER SMP. RAN ENG AT IDLE AND NO LEAK NOTED. PERFORMED HIGH POWER ENGINE RUN PER JRH.
- [SDR FDEA201101260370](https://openairdocs.org/sdr/FDEA201101260370.md): Light · inoperative · Jan 26, 2011 · N262FE · Boeing 727233 · Emergency Lighting
  > COCKPIT EMERGENCY EXIT LIGHT ILLUMINATED INTERMITTENTLY DURING CLIMBOUT. REPEAT GRIPE. R & R COCKPIT EMERGENCY EXIT LIGHT IAW MM 33-50-101-2. OPS CHECKED GOOD.
- [SDR FDEA201101250344](https://openairdocs.org/sdr/FDEA201101250344.md): Battery Pack · inoperative · Jan 25, 2011 · N262FE · Boeing 727233 · Emergency Lighting
  > EMERGENCY LIGHTS ILLUMINATED INTERMITTENTLY. R & R EMERGENCY EXIT LIGHT ASSY. INSTALLED NEW BATTERIES IAW MM33-50-001-2, OPS NORMAL.
- [SDR FDEA201010114002](https://openairdocs.org/sdr/FDEA201010114002.md): Contact · dirty · Oct 11, 2010 · N262FE · Boeing 727233 · Light System Wiring
  > CABIN ENTRY EMERGENCY EXIT LIGHT DOES NOT TEST FROM COCKPIT SWITCH. REMOVED LIGHT ASSY CLEANED CONTACTS AND REINSTALLED IAW 33-50-101-2-0. OPS CHECKED GOOD. OK FOR SERVICE. REMOVED LIGHT ASSY CLEANED CONTACTS AND REINSTALLED IAW 33-50-101-2-0. OPS CHECKED GO
- [SDR FDEA200911093923](https://openairdocs.org/sdr/FDEA200911093923.md): Shear Tie · corroded · Nov 9, 2009 · N262FE · Boeing 727233 · Fuselage Internal Mounting Structure
  > INT FUSELAGE BS 303.9 BETWEEN STR 22R-23R SHEAR TIE HAS CORROSION. CUT-OUT DAMAGED AREA APPROX DIM OF CUT-OUT 2" X 5" IAW SRM 53-10-4. FABRICATED SHEAR TIE REPAIR FROM PN 7075T6.050 PO NR 9008963 APPROX DIM: 4" X 5 1/2" IAW SRM 53-10-4 FIG H, 53-10-2 AND 5
- [SDR FDEA200911083920](https://openairdocs.org/sdr/FDEA200911083920.md): Skin · misrepaired · Nov 8, 2009 · N262FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > DOUBLER EXT SKIN BS 440 STR 25L NO EDGE DISTANCE BETWEEN FASTENERS. CUT-OUT DAMAGED AREA UPPER & LWR SKIN, FABRICATED REPAIR DOUBLER, TRIPLER, REPAIR FILLER, BEAR STRAP FILLER, UPPER FILLER, DOUBLER FILLER AND TAPERED FILLER, MILLED BEAR STRAP FILLER, FABRI
- [SDR FDEA200911073886](https://openairdocs.org/sdr/FDEA200911073886.md): Skin · damaged · Nov 7, 2009 · N262FE · Boeing 727233 · Emergency Exits
  > RT FWD OVERWING EMER EXIT HATCH EXTERIOR SKIN HAS SEVERAL AREAS OF SKIN EDGE DAMAGE. REMOVED ACCESS PANEL AND REMOVED COVER SUPPORT IAW SRM 51-30-2. CUT-OUT DAMAGE AREA DIM: 3 1/2" X 4 1/8" IAW SRM 52-00-3 FIG 3, REV 101. FABRICATED REPAIR DOUBLER IAW SRM 5
- [SDR FDEA200910303747](https://openairdocs.org/sdr/FDEA200910303747.md): Stringer · corroded · Oct 30, 2009 · N262FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > INT FUSELAGE BS 312-300 STR 25 RT HAS CORROSION IN CHANNEL. CUT OUT DAMAGED STRINGER APPROX DIM 18" LONG IAW SRM 51-30-2, FABRICATED NEW STRINGER FILLER FROM BAC1498-139 PO#29111206 APPROX DIM 20 5/8" FABRICATED 2 ANGLES, FABRICATED CHANNEL, AND FABRICATED
- [SDR FDEA200910303746](https://openairdocs.org/sdr/FDEA200910303746.md): Stringer · corroded · Oct 30, 2009 · N262FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > INT FUSELAGE BS 300-312 STR 24 RT IS CORRODED IN CHANNEL. REMOVED CORRODED SECTION OF STRINGER 15.6 " LONG IAW SRM REV 101 51-10-1. FABRICATED STRINGER FILLER, 4 ANGLES, 2 CHANNELS, & STRAPS, IAW SRM 53-10-3 FIG 1 AND 53-10-2 FIG 9. INSTALLED REPAIR PARTS I
- [SDR FDEA200910303745](https://openairdocs.org/sdr/FDEA200910303745.md): Skin · damaged · Oct 30, 2009 · N262FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > MAIN CARGO AREA, BS 450, STR 3L, NO EDGE DISTANCE BETWEEN FASTENERS. REMOVED FASTENERS AREA IAW SRM 51-30-2, CUT OUT DAMAGE STRINGER AREA IAW SRM 53-10-3 FIG 3, FABRICATED FILLER. FABRICATED PLATE NR 1. FABRICATED PLATES NR 2 IAW SRM 53-10-3 FIG 3 53-10-2
- [SDR FDEA200910303744](https://openairdocs.org/sdr/FDEA200910303744.md): Skin · corroded · Oct 30, 2009 · N262FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > AFT CARGO COMPARTMENT BS1010 OTBD OF STR 29L LEVELING COMPOUND MISSING AND CORROSION ON SKIN. CUT OUT DAMAGE SECTION IAW SRM 53-10-3 FIG 3A. FABRICATED DOUBLER AND 1EA FILLER IAW SRM 53-30-3 FIG 3A. TREATED AND PRIMED IAW SRM 51-10-2, INSTALLED REPAIR PARTS D
- [SDR FDEA200910283718](https://openairdocs.org/sdr/FDEA200910283718.md): Seat Track · corroded · Oct 28, 2009 · N262FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SEAT TRACK FLANGE BS360 - BS420, LBL 24. REMOVED DAMAGED SEAT TRACK SECTION FROM BS 344-480 LBL 24, FABRICATED NEW SEAT TRACK SECTION FROM BAC 1520-792 PO NR 9006020 APPROX LENGTH 136" AND INSTALLED NEW SEAT TRACK SECTION USING PREVIOUS GOOD CONDIT
- [SDR FDEA200910273852](https://openairdocs.org/sdr/FDEA200910273852.md): Skin · damaged · Oct 27, 2009 · N262FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > DOUBLER EXT SKIN BS 460 STR 27L, NO EDGE DISTANCE BETWEEN FASTENERS. CUT OUT DAMAGE ON LOWER FLANGE OF STRINGER 27L, 3/4" X 3/4" IAW SRM 51- 10-1 REV 101, FABRICATED FILLER FROM BAC1514-1559, AND DOUBLER FROM BAC1509-100146 6 1/2" LONG IAW SRM 51-40-3. I
- [SDR FDEA200910273692](https://openairdocs.org/sdr/FDEA200910273692.md): Angle · cracked · Oct 27, 2009 · N262FE · Boeing 727233 · Fuselage Main, Bulkhead
  > RT W/W VERTICAL ANGLE IS CRACKED AT BS 870, RBL 8. REMOVED CRACKED ANGLE IAW SRM 51-30-2 REV 101. LOCATED DRILLED AND DEBURRED NEW ANGLE IAW SRM 51-30-5. INSTALLED NEW ANGLE IAW SRM 51-30-2.
- [SDR FDEA200910273740](https://openairdocs.org/sdr/FDEA200910273740.md): Angle · cracked · Oct 27, 2009 · N262FE · Boeing 727233 · Wing Miscellaneous Structure
  > LT WING STR CRACKED AT STR TO RIB ATTACH POINT WS 686.5 STR 10 STOP DRILLED CRACK.190 DIA, HFEC INSPECTED STOP DRILL AREA NO DEFECTS NOTED, FABRICATED ANGLES REPAIR. FABRICATED RADIUS FILLER AND INSTALLED REPAIR PARTS AT LT WING STR 10 WS 686.5 IAW EO 7- 5
- [SDR FDEA200910273695](https://openairdocs.org/sdr/FDEA200910273695.md): Skin · dented · Oct 27, 2009 · N262FE · Boeing 727233 · Nacelle/Pylon, Plate/Skin
  > DENT IN NR3 ENGINE NOSE COWL LWR SKIN AT NAC STA 69.00. CUT OUT DAMAGE 3 3/8 X 5 7/8 IAW SRM REV 101, 51-10-1. FABRICATED REPAIR DOUBLER FROM 2024T3,.050 X 7 1/2 X 9 3/8, PO NR 9008452 AND FILLER FROM 2024T3.040 X 5 7/8 X 3 3/8", PO NR 9008875 IAW SRM 54-
- [SDR FDEA200910273691](https://openairdocs.org/sdr/FDEA200910273691.md): Frame · corroded · Oct 27, 2009 · N262FE · Boeing 727233 · Fuselage Main, Frame
  > AFT CARGO COMP BS 1130 OB OF STR 29LT. AFT FRAME FLANGE HAS CORROSION. REMOVED AFT FLANGE ANGLE AT BS 1130 OTBD OF STR 29L IAW SRM REV 101 51-30-2. FABRICATED REPLACEMENT ANGLE FROM 7075T6.063 X 2 1/8" X 6 1/2", PO NR 9008729 IAW SRM 51-20-1, FIG 7 AND 53-
- [SDR FDEA200910213651](https://openairdocs.org/sdr/FDEA200910213651.md): Angle · cracked · Oct 21, 2009 · N262FE · Boeing 727233 · Trailing Edge Flaps
  > LEFT I/B MID FLAP CRACKED AT CUT-OUT IN T/E ANGLE. REMOVED CRACKED SECTION OF LT IB MID FLAP TE ANGLE 46" LONG IAW SRM REV 101, 51-30-2. LOCATED, DRILLED AND DEBURRED NEW SECTION OF TE CHORD IAW SRM 51-30-5. INSTALLED NEW ANGLE IAW SRM 51-30-2.
- [SDR FDEA200910213637](https://openairdocs.org/sdr/FDEA200910213637.md): Seat Track · corroded · Oct 21, 2009 · N262FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SEAT TRACK FLANGE BS 360 - BS 420 BL 0. REMOVED DAMAGED SEAT TRACK SECTION FROM BS 344-480 BL0, FABRICATED NEW SEAT TRACK SECTION FROM BAC 1520-792 PO 9006020 APPROX DIM 136" & INSTALLED NEW SEAT TRACK USING EXISTING GOOD SPLICE IAW SRM 53-10-5 FIG
- [SDR FDEA200910213641](https://openairdocs.org/sdr/FDEA200910213641.md): Torque Box · cracked · Oct 21, 2009 · N262FE · Boeing 727233 · Fuselage Main, Structure
  > AFT AIRSTAIRS, RT LR TORQUE BOX, LWR LIGHTNING HOLE IS CRACKED AT BS 1223. REMOVED DAMAGE 1/4" X 3/4" IN AFT AIRSTAIR RT LWER TORQUE BOX LOWER LIGHTNING HOLE AT BS 1213 IAW SRM REV 101 51-10-1. FABRICATED DOUBLER IAW SRM 51-40-2 FIG 1 AND 53-10-2 FIG 6. INSTA
- [SDR FDEA200910213640](https://openairdocs.org/sdr/FDEA200910213640.md): Torque Box · cracked · Oct 21, 2009 · N262FE · Boeing 727233 · Fuselage Main, Structure
  > AFT AIRSTAIRS, RT LWR TORQUE BOX, LWR LIGHTNING HOLE IS CRACKED AT BOTTOM AT BS 1213. REMOVED DAMAGE 1/4" X 3/4" IN AFT AIRSTAIRS RT LOWER TORQUE BOX LOWER LIGHTNING HOLE AT BOTTOM BS 1213 IAW B727 SRM REV 101 51-10-1. FABRICATED DOUBLER FROM 7075T6.032
- [SDR FDEA200910213639](https://openairdocs.org/sdr/FDEA200910213639.md): Torque Box · cracked · Oct 21, 2009 · N262FE · Boeing 727233 · Fuselage Main, Structure
  > AFT AIR STAIRS, RT LWR TORQUE BOX, LWR LIGHTNING HOLE IS CRACKED AT TOP AT BS 1213. REMOVED DAMAGE 1/4" X 3/4" IN AFT AIRSTAIRS RT LOWER TORQUE BOX LOWER LIGHTNING HOLE AT BS 1213 IAW B727 SRM REV 101 51-10-1. FABRICATED DOULBER FROM 7075T6.032" X 4" X 2
- [SDR FDEA200910213622](https://openairdocs.org/sdr/FDEA200910213622.md): Frame · damaged · Oct 21, 2009 · N262FE · Boeing 727233 · Fuselage Main, Frame
  > STA 303.9 FRAME, WEB CUTOUT AT STR 15L AND STR 16L HAVE SHARP RADIUS. ACCOMPLISHED REPAIR IAW EA NR 7-5310-135505.
- [SDR FDEA200910203736](https://openairdocs.org/sdr/FDEA200910203736.md): Skin · damaged · Oct 20, 2009 · N262FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > TRIPLER EXT SKIN BS 620 STR 25L TWO DRILL STARTS. REMOVED FASTENERS AT EXT SKIN BS 620 STR 25L IAW SRM 51-30-2, CUT OUT DAMAGED AREA APPROX 1.05" X 4.6" IAW SRM 53-30-3 FIG 1A. TREATED & PRIMED REPAIR PARTS IAW SRM 51-10-2. INSTALLED PARTS IAW B727 SRM 51-30
- [SDR FDEA200910203735](https://openairdocs.org/sdr/FDEA200910203735.md): Angle · cracked · Oct 20, 2009 · N262FE · Boeing 727233 · Trailing Edge Flaps
  > RT INBD MID FLAP FWD LWR CHORD ANGLE IS CRACKED 2 PLACES BELOW PULLEY MECHANISM WBL112. REMOVED ACCESS PANEL IAW SRM 51-30-2 AND REMOVED DAMAGED ANGLE IAW SRM 51-40-4. FABRICATED REPAIR ANGLE IAW SRM 51-40-4 TREATED & PRIMED ANGLE IAW B727 SRM 51-10-2. IN
- [SDR FDEA200910203650](https://openairdocs.org/sdr/FDEA200910203650.md): Skin · damaged · Oct 20, 2009 · N262FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > TRIPLER EXTERIOR SKIN BS 480 STR 25L HAS TWO DRILL STARTS CUT OUT DAMAGE 3 1/4 SQ IAW SRM REV H 53-30-3 FIG 1A. FABRICATED REPAIR DOUBLER AND STRUCTURAL FILLER IAW SRM 53-30-3 FIG 1A. INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 53-30-3 FIG 1A.
- [SDR FDEA200910203653](https://openairdocs.org/sdr/FDEA200910203653.md): Seat Track · corroded · Oct 20, 2009 · N262FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SEAT TRACK FLANGE BS 360 - BS 420 RBL 24. REMOVED DAMAGED SEAT TRACK SECTION. FABRICATED NEW SEAT TRACK SECTION & INSTALLED SEAT TRACK IAW SRM 53-10-5 FIG 1, SRM 51- 30-2, AND SRM 53-10-1 FIG 3A.
- [SDR FDEA200910203655](https://openairdocs.org/sdr/FDEA200910203655.md): Skin · damaged · Oct 20, 2009 · N262FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > MAIN CARGO AREA BS 640 STR 3L & STR 4L, NO EDGE DISTANCE. CUT OUT DAMAGED AREA OF SKIN IAW SRM 53-30-3, CUT OUT DAMAGED AREA OF TEAR STRAP IAW SRM 53-30-4 FIG 9. FABRICATED TEAR STRAP REPAIR IAW SRM 53-30-4 & 51-30-5, FABRICATED EXTERNAL REPAIR DOUBLER. FA
- [SDR FDEA200910203654](https://openairdocs.org/sdr/FDEA200910203654.md): Seat Track · corroded · Oct 20, 2009 · N262FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SEAT TRACK FLANGE BS 360 - BS 420 LBL 24.
- [SDR FDEA200910203652](https://openairdocs.org/sdr/FDEA200910203652.md): Seat Track · corroded · Oct 20, 2009 · N262FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SEAT TRACK FLANGE BS 360 - BS 420 BL0.
- [SDR FDEA200910203636](https://openairdocs.org/sdr/FDEA200910203636.md): Skin · gouged · Oct 20, 2009 · N262FE · Boeing 727233 · Trailing Edge Flaps
  > RT WING INBD FORE FLAP OUTBD LEADING EDGE IS GOUGED AT WBL 482. BLENDED GOUGE ON RT WING INBD FORE FLAP LE SKIN AT O/B END IAW FEDEX B727 SRM REV 101, 51-10-1. FABRICATED REPAIR DOUBLER FROM 2024T3.063 X 4 5/8" X 3 7/8" PO#9008729 IAW B727 SRM 57-50-4. IN
- [SDR FDEA200910183605](https://openairdocs.org/sdr/FDEA200910183605.md): Web · cracked · Oct 18, 2009 · N262FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > AFT AIRSTAIR AREA - RT LOWER TORQUE BOX LIGHTNING HOLE IS CRACKED AT BS 1243 - MARKED. CUT OUT DAMAGED AREA IAW SRM 51-10-1 REV 101 FABRICATED REPAIR DOUBLER IAW SRM 53-10-2 FIG 6 AND 51-40-2 FIG 1 INSTALLED REPAIR DOUBLER IN AFT AIRSTAIR RT LOWER TORQU
- [SDR FDEA200910183600](https://openairdocs.org/sdr/FDEA200910183600.md): Web · cracked · Oct 18, 2009 · N262FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > AFT AIRSTAIR AREA - RT LOWER TORQUE BOX LIGHTNING HOLE IS CRACKED BS 1223 - MARKED. CUT OUT DAMAGED AREA IAW SRM 51-10-1 REV 101 FABRICATED REPAIR DOUBLER IAW SRM 53-10-2 FIG 6 AND 51-40-2 FIG 1 INSTALLED REPAIR DOUBLER IN AFT AIRSTAIR RT TORQUE BOX LIGH
- [SDR FDEA200910183604](https://openairdocs.org/sdr/FDEA200910183604.md): Torque Box · cracked · Oct 18, 2009 · N262FE · Boeing 727233 · Fuselage Main, Structure
  > AFT AIRSTAIR AREA - RT LWR TORQUE BOX, LWR LIGHTNING HOLE IS CRACKED BS 1223. CUT OUT DAMAGED AREA IAW SRM 51-10-1 REV 101, FABRICATED DOUBLER IAW SRM 53-10-2 FIG 6 AND 51-40-2 FIG 1. INSTALLED REPAIR DOUBLER ON RT LOWER TORQUE BOX IAW SRM 51-30-2 REV 101.
- [SDR FDEA200910183603](https://openairdocs.org/sdr/FDEA200910183603.md): Angle · cracked · Oct 18, 2009 · N262FE · Boeing 727233 · Trailing Edge Flaps
  > RT WING OTBD MID-FLAP UPPER CHORD ANGLE IS CRACKED ABOVE INBD PULLEY AT WBL 320. REMOVED AND REPLACED RT OTBD MID FLAP ASSY IAW MM 27-51-011-4. ADJUSTED/OPS CHECK GOOD IAW MM 27-51-000-5.
- [SDR FDEA200910153587](https://openairdocs.org/sdr/FDEA200910153587.md): Angle · damaged · Oct 15, 2009 · N262FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > PLUG FOUND NEXT TO FASTENER BS 1183 CHORD ANGLE AFT PIT BETWEEN STR 28L TO STR 29L. TRIMMED OUT BS. 1183 BULKHEAD WEB APPROX DIM: 30 1/2" X 9 1/4", BULKHEAD BEAM CUT-OUT DIM: 33 5/8". FABRICATED BULKHEAD WEB REPAIR DOULBER, & FILLER. FABRICATED BEAM REPAIR
- [SDR FDEA200910153578](https://openairdocs.org/sdr/FDEA200910153578.md): Vertical Beam · misinstalled · Oct 15, 2009 · N262FE · Boeing 727233 · Fuselage Main, Structure
  > FASTENERS HAVE NO SPACING AFT PIT BS 1183 LBL 17.8 VERTICAL BEAM. TRIMMED OUT BS 1183 BULKHEAD WEB APPROX DIM: 30 1/2" X 9 1/4", BULKHEAD BEAM CUT-OUT DIM: 33 5/8". FABRICATED BULKHEAD WEB REPAIR DOUBLERS, FILLER. FABRICATED BEAM REPAIR TEE REPAIR ANGLES, F
- [SDR FDEA200910143601](https://openairdocs.org/sdr/FDEA200910143601.md): Angle · cracked · Oct 14, 2009 · N262FE · Boeing 727233 · Leading Edge Devices
  > NR 8 SLAT LWR AFT CHORD ANGLE IS CRACKED AT INBD UP STOP PAD. FABRICATED ANGLE REPAIR FROM EXTRUSION BAC 1514-1559 2024T3-511, PO NR 29111160, DIM: 11" AND OTHER 6" (2 ANGLES) IAW SRM 51-40-4 FIG 1. TREATED AND PRIMED IAW SRM 51-10-2, INSTALLED REPAIR ANGLES
- [SDR FDEA200901240316](https://openairdocs.org/sdr/FDEA200901240316.md): Valve · malfunctioned · Jan 24, 2009 · N262FE · Boeing 727233 · Landing Gear Brake System
  > THE LEFT BRAKE WILL NOT MODULATE. A GREAT DEAL OF PEDAL EFFORT IS REQUIRED TO ACTIVATE AND THEN MAX BRAKING IS RESULT. REMOVED AND REPLACED LT BRAKE METERING VALVE OPS CHECKED GOOD AS PER MM 32-41-011-4.
- [SDR 07FDEA03867](https://openairdocs.org/sdr/07FDEA03867.md): Frame · corroded · Sep 17, 2007 · N262FE · Boeing 727233 · Fuselage Main, Frame
  > AFT LWR CARGO PIT FUSE. CUTOUT FOR NR 3 DOOR, STA 1130 PLUS 13" AFT SIDE FRAME HAS CORROSION DOWN LOW WHERE SCUFF PLATE MOUNTS AT STR 26R. REMOVED FRAME AT STA 1130 PLUS 13, FROM STRINGER 18R-28. REPLACED WITH NEW FRAME STA 1130 PLUS 13, FROM STRINGER 18R -
- [SDR 07FDEA03873](https://openairdocs.org/sdr/07FDEA03873.md): Support Beam · inoperative · Sep 17, 2007 · N262FE · Boeing 727233 · Wing Miscellaneous Structure
  > LT WING SPOILER SUPPORT BEAM LOWER CHORD ANGLE I/B OF NR 4 FLAP TRACK HAS INCORRECT REPAIR INSTALLED REF SR-27-57-038. REMOVED AND REINSTALLED LOWER WING T/E PANELS, REMOVED EXISTING DOUBLER. REMOVED AND REINSTALLED NR 4 SPOILER ACTUATOR MOUNT, FLAP TORQU
- [SDR 07FDEA03872](https://openairdocs.org/sdr/07FDEA03872.md): Floorbeam · corroded · Sep 17, 2007 · N262FE · Boeing 727233 · Fuselage Main, Floor Beam
  > "PREVIOUS REPAIR'" FLOORBEAM AT STA 620, RBL 29-42 HAS CORROSION ON UNDERSIDE FROM AREA NOT TREATED AND PRIMED. REMOVED DAMAGED PORTION OF UPPER FLOORBEAM AT STA 620, RBL 29-42. FABRICATED AND INSTALLED UPPER CAP REPAIR. REF FED EX EA NR 7-5310-113099, THIS
- [SDR 07FDEA03870](https://openairdocs.org/sdr/07FDEA03870.md): Channel · corroded · Sep 17, 2007 · N262FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > LWR AFT CARGO PIT NR 3 CUTOUT THRESHOLD SUPPORT CHANNEL, STA 1130 STR 26R IS CORRODED. SUPPORT CHANNEL FOR NR 3 DOOR CUTOUT THRESHOLD IS REMOVED AND REPLACE ON WO NR 37678/N00602 ITEM 17 AND 18 ON JPF. THIS IS CLASSIFIED AS A MAJOR REPAIR.
- [SDR 07FDEA03791](https://openairdocs.org/sdr/07FDEA03791.md): Bracket · cracked · Sep 14, 2007 · N262FE · Boeing 727233 · Wing, Attach Fittings
  > LT WING T/E PANEL BRACKET IS CRACKED, 2 EA. PLACES ABOVE AND JUST INBOARD OF THE NR 7 SPOILER ACTUATOR REPLACED PANEL BRACKET AS PER SRM 51-30-02, AT WBL 71 TO 153, LT. THIS IS CLASSIFIED AS A MINOR REPAIR.
- [SDR 07FDEA03789](https://openairdocs.org/sdr/07FDEA03789.md): Frame · dented · Sep 14, 2007 · N262FE · Boeing 727233 · Fuselage Main, Frame
  > FWD PIT FRAME, STA 660 UPPER FLANGE HAS A DENT BETWEEN STR 23R-24R FOUND 3 DENTS ON UPPER FLANGE OF STA 660, BETWEEN S-22R -S-25R AND FOUND OUT OF LIMITS, CUTOUT DAMAGE, FORMED NEW FRAME SPLICE DOUBLER OUT OF 7075 O.050, HEAT TREATED MATERIAL 7075-T6 THEN D
- [SDR 07FDEA03669](https://openairdocs.org/sdr/07FDEA03669.md): Skin · cracked · Sep 13, 2007 · N262FE · Boeing 727233 · Trailing Edge Flaps
  > LEFT WING INBD MID FLAP, LOWER SURFACE, VERY AFT ANGLE STRUCTURE IS CRACKED AT NUTPLATE, 55" FROM INBD EDGE INSTALLED ANGLE IAW 51-40-4 THIS IS CLASSIFIED AS A MINOR REPAIR.
- [SDR 07FDEA03664](https://openairdocs.org/sdr/07FDEA03664.md): Bracket · cracked · Sep 13, 2007 · N262FE · Boeing 727233 · Wing Miscellaneous Structure
  > UPPER TRAILING EDGE PANEL BRACKET IS CRACKED ABOVE ACTUATOR REMOVED AND REINSTALLED UPPER WING ROOT PANEL AT TRAILING EDGE. REMOVED AND REINSTALLED NR 8 SPOILER MOUNT. REMOVED AND REPLACED TRAILING EDGE PANEL BRACKET REPLACED STIFFENERS ON PANEL BRACKET,
- [SDR 07FDEA03721](https://openairdocs.org/sdr/07FDEA03721.md): Beam · corroded · Sep 13, 2007 · N262FE · Boeing 727233 · Wing Main, Frame Structure
  > RT MLG BEAM LOWER SURFACE AND FASTENER HOLES EXPOSED BY REMOVAL OF LOWER T/E PANELS NEED TO BE CLEANED AND INSPECTED. FOUND CORROSION INSIDE HOLES REPAIRED DAMAGE HOLE. REF FED EX EA NR 7-5720-113948 CLEANED HOLES/ REWORKED HOLES REF EA. THIS IS CLASSIFIED

Next page: https://openairdocs.org/deregistered/N262FE-2013-12-18/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 = 'N262FE' AND deregistration_id = 'N262FE-2013-12-18'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N262FE-2013-12-18/reports

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