# Service difficulty reports: N268FE, cancelled Mar 8, 2013

A list on [N268FE, cancelled Mar 8, 2013](https://openairdocs.org/deregistered/N268FE-2013-03-08.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 · 130 reports

- [SDR FDEA201108173308](https://openairdocs.org/sdr/FDEA201108173308.md): Roller Track · out of adjust · Aug 17, 2011 · N268FE · Boeing 727233 · Flight Compartment Windows
  > F/O'S WINDOW TAKES ALOT OF FORCE TO CLOSE. VERY DIFFICULT TO CLOSE. TROUBLESHOOTING. ADJUSTED THE TRACK ROLLERS IAW MM 56-12-011-5-0. OPS CKD NORMAL.
- [SDR FDEA201108173310](https://openairdocs.org/sdr/FDEA201108173310.md): Handle · malfunctioned · Aug 17, 2011 · N268FE · Boeing 727233 · Flight Compartment Windows
  > CAPTAINS SIDE WINDOW HANDLE POPS OPEN, JUST THE HANDLE, IT DOES NOT STAY FLUSH. PROPERLY SECURED STOWED EMERGENCY HANDLE CAPTAINS SIDE IAW STANDARD MAINT PRACTICES. OPS NORMAL.
- [SDR FDEA201006022027](https://openairdocs.org/sdr/FDEA201006022027.md): Fitting · damaged · Jun 2, 2010 · N268FE · Boeing 727233 · Fuselage Main, Structure
  > TAIL STAND FITTING AFT SIDE OF 1183 BULKHEAD, LBL19 HAS A DRILL START REPAIRED TAIL STAND FITTING AFT SIDE OF BS 1183 BULKHEAD, LBL19 IAW EA 7-5310- 135541 ( FUSELAGE AD 98-11-03 R1, BS1183 AFT PRESSURE BULKHEAD VERTICAL BEAM WITH INSUFFICIENT FASTENER SPACIN
- [SDR FDEA201005281703](https://openairdocs.org/sdr/FDEA201005281703.md): Intercostal · cracked · May 28, 2010 · N268FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > NR 1 CARGO DOORWAY FRAMES, BS 560, BETWEEN STR 23R AND 24R, CRACKED INTERCOSTAL. REMOVED INTERCOSTAL NR 1 CARGO DOOR WAY BS 560 STR 23R - 24R IAW SRM 51-30-2. FABRICATED NEW INTERCOSTAL USING 7075 O.063" PO 9009533 DIM 19.7500" X 6.2500" IAW MM 51-20-1
- [SDR FDEA201005241637](https://openairdocs.org/sdr/FDEA201005241637.md): Skin · gouged · May 24, 2010 · N268FE · Boeing 727233 · Trailing Edge Flaps
  > RT INBD FOREFLAP OTBD END L/E PREVIOUS REPAIR, GOUGED. REMOVED PREVIOUS REPAIR ON RT INBD FOREFLAP OTBD END IAW SRM 51-30-2 FABRICATED NEW REPAIR IAW SRM 57-50-4, FIG 1, REV 102. INSTALLED NEW REPAIR IAW SRM 51-30-2.
- [SDR FDEA201005221733](https://openairdocs.org/sdr/FDEA201005221733.md): Rib · cracked · May 22, 2010 · N268FE · Boeing 727233 · Wing, Rib/Bulkhead
  > RIB CRACKED AT OTBD TRACK OF NR 6 SLAT REMOVED RIB IAW SRM 51-30-2. FABRICATED NEW RIB FROM 2024-0.050" DIM 15" X 6" IAW SRM 51-20-1 AND 57-50-2. HEAT TREATED PART FROM 2024-0 TO 2024T4 IAW FAS ENGINEERING REPORT NR 2-37153-801 REV A INSTALLED RIB IAW SRM 51
- [SDR FDEA201005201595](https://openairdocs.org/sdr/FDEA201005201595.md): Angle · cracked · May 20, 2010 · N268FE · Boeing 727233 · Leading Edge Devices
  > NR 6 SLAT LOWER AFT T/E ANGLE IS CRACKED AT OTBD UPSTOP PAD. REMOVED ACCESS PANELS NR 6 SLAT IAW SRM 51-30-2, FABRICATED NEW T/E ANGLE. MATERIAL USED BAC1514-1559 2024T3511 PO 20035137 DIM 9' 6" LONG IAW SRM 57-50-2 FIG 2, 51-30-5 TREATED AND PRIMED IAW
- [SDR FDEA201005201594](https://openairdocs.org/sdr/FDEA201005201594.md): Angle · cracked · May 20, 2010 · N268FE · Boeing 727233 · Leading Edge Devices
  > NR 8 SLAT LOWER T/E ANGLE IS CRACKED AT OTBD UPSTOP PAD. REMOVED NR 8 SLAT LOWER T/E ANGLE IAW SRM REV 102, 51-30-2. FABRICATED NEW ANGLE USING BAC1514-1559, 2024 T3511 86 1/4" LONG IAW SRM 51-30-5 AND 57-50-2 FIG 2. INSTALLED NEW ANGLE IAW 51-30-2.
- [SDR FDEA201005191583](https://openairdocs.org/sdr/FDEA201005191583.md): Stiffener · damaged · May 19, 2010 · N268FE · Boeing 727233 · Fuselage Main, Bulkhead
  > BULKHEAD 1183 HORIZONTAL CHORD AT WL 190 BETWEEN LBL 4 AND RBL 6 HAS NUMEROUS HOLES WITH NO SPACING. CUT OUT, WEB DIM. 29" X 7" AND HORIZ CHORD DIM. 9" IAW EA 7-5310-135541 AND SRM 51-10-1. FABRICATED WEB FROM 7075T6.063" DIM. 51.38" X 17.60", VERTICAL LEG S
- [SDR FDEA201005191582](https://openairdocs.org/sdr/FDEA201005191582.md): Stringer · corroded · May 19, 2010 · N268FE · Boeing 727233 · Fuselage Main, Longeron/Stringer
  > STRINGER CORRODED ON STR 27L AT BS 950F, 10". CORROSION OUT OF LIMITS. CUT OUT DAMAGED SECTION 19", FABRICATED FILLER USING BAC1498-147 7075T-6 DIMS 19", SPLICE USING BAC1498-131 7075T-6 DIMS 14" AND INSTALLED IAW SRM 51-30-2, 53-10-1, 53-10-3 AND 51-10-2.
- [SDR FDEA201005171769](https://openairdocs.org/sdr/FDEA201005171769.md): Beam · damaged · May 17, 2010 · N268FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > AFT PIT BS 1183, VERTICAL BEAM AT LBL 17.8 HAS FASTENERS WITH ZERO SPACING. TRIMMED OUT BEAM AFT FLANGES AND BULKHEAD WEB 8 PLACES IAW EA 7-5310-135541. FABRICATED REPAIR DOUBLER, REPAIR ANGLES, FILLERS, BULKHEAD WEB FILLERS, STRAP DOUBLER, STIFFENER SHIMS,
- [SDR FDEA201005171748](https://openairdocs.org/sdr/FDEA201005171748.md): Doubler · gouged · May 17, 2010 · N268FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > GOUGES ON INNER DOUBLER BS 620, STR 16L. TRIMMED OUT DAMAGED AREA DIM. 1.75" X 1" IAW EA 7-5330-135544. FABRICATED FILLER FROM 2024T3.125" DIM. 1.75" X 1" AND DOUBLER FROM 2024T3.125" DIM. 4.75" X 3.75" IAW EA 7-5330-135544. INSTALLED REPAIR PARTS IAW SRM
- [SDR FDEA201005141731](https://openairdocs.org/sdr/FDEA201005141731.md): Skin · gouged · May 14, 2010 · N268FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > GOUGES IN MCD INNER DOUBLER SKIN STA 620-640 STRINGERS 5L - 8L REMOVED INNER WEB SKIN IAW P-F SRM 51-30-2. FABRICATED INNER WEB SKIN FROM 2024T3.125" DIM. 80" X 48" IAW P-F SRM 53-10-2. INSTALLED INNER WEB SKIN IAW P-F SRM 51-30-2.
- [SDR FDEA201005141592](https://openairdocs.org/sdr/FDEA201005141592.md): Stringer · corroded · May 14, 2010 · N268FE · Boeing 727233 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 27L AT BS 985. CORROSION OUT OF LIMITS. CUT OUT DAMAGED SECTION 15.5", FABRICATED FILLER USING BAC1498-147 7075T-6 DIMS 15.5", SPLICES USING BAC1498-131 7075T-6 DIMS 13.7500" AND 10.2500" AND INSTALLED IAW SRM 51-30-2, 53-10-1, 53-10-3 A
- [SDR FDEA201005141591](https://openairdocs.org/sdr/FDEA201005141591.md): Stringer · corroded · May 14, 2010 · N268FE · Boeing 727233 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 27L AT BS 950B 5". CORROSION OUT OF LIMITS. CUT OUT DAMAGED SECTION 18", FABRICATED FILLER USING BAC1498-147 7075T-6 DIMS 18", SPLICES USING BAC1498-131 7075T-6 DIMS 13" AND 12.5" AND INSTALLED IAW SRM 51-30-2, 53-10-1, 53-10-3 AND 51-
- [SDR FDEA201005131619](https://openairdocs.org/sdr/FDEA201005131619.md): Door Frame · cracked · May 13, 2010 · N268FE · Boeing 727233 · Fuselage Main, Structure
  > L-1 ENTRY DOOR FRAME, STA 303.9, STR 16L, CRACK ON WEB CUTOUT. CUTOUT AREA ON WEB DIM 1.25" X.70" AT BS 303.9 AT STR 16L IAW FEDEX EO 7-5310-7-3362 P7. DRILLED AND LOCATED PARTS FROM FEDEX KIT P/N 5314757 IAW SRM 51-30-5. INSTALLED WEB REPAIR AT BS 303.9 A
- [SDR FDEA1005121525A](https://openairdocs.org/sdr/FDEA1005121525A.md): Bulkhead · cracked · May 12, 2010 · N268FE · Boeing 727233 · Fuselage Main, Bulkhead
  > CRACK FOUND AT BS 1183 BULKHEAD WEB AT RBL 24 WL 170 CUT OUT WEB DIM. 2.8750 " X 1.3750 " IAW EA 7-5310-135543 AND SRM 51-10-1. FABRICATED FILLER FROM 2024T3.050" DIM. 2.7500" X 1.3750", FABRICATED DOUBLER FROM 2024T3.071" DIM 7" X 6", FABRICATED FILLER FROM
- [SDR FDEA201005121523](https://openairdocs.org/sdr/FDEA201005121523.md): Spar · cracked · May 12, 2010 · N268FE · Boeing 727233 · Wing Spar
  > RT WING T/E FALSE SPAR CHORD CRACKED, WBL 118. REMOVED LOWER CHORD DIM. 20.5", WEB AND DOUBLER IAW DWG NR SR 27-57-038, REV C. FABRICATED 2 ANGLES FROM 7075-0.071" DIM. 14.5" X 2.75" AND 12.5" X 2.75" IAW DWG NR SR 27-57-038 REV C. HEAT TREATED ANGLES FROM 7
- [SDR FDEA201005121590](https://openairdocs.org/sdr/FDEA201005121590.md): Skin · damaged · May 12, 2010 · N268FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > MAIN CARGO AREA, BS 660, STR 3L-4L, DOUBLE DRILLED HOLES ON BONDED STRAP. CUT OUT AREA DIM. 1.5" X 3.5" AND 1" X.75" IAW SRM 53-30-3. FABRICATED FILLER FROM 2024T3.090" DIM. 19.5" X 8", DOUBLER FROM 2024T3.080" DIM. 17.6" X 11.5", TRIPLER FROM 2024T3.
- [SDR FDEA201005121589](https://openairdocs.org/sdr/FDEA201005121589.md): Skin · damaged · May 12, 2010 · N268FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > MAIN CARGO DOOR AREA, BS 660, STR 3L, NOT ENOUGH DISTANCE BETWEEN FASTENERS. CUT OUT AREA DIM, 2.75" IAW SRM 53-10-3. FABRICATED STRINGER SECTION FROM BAC-1498-139-7075T6 DIM. 2.75", 2 SHIMS FROM 2024T3.080" DIM..75" X 4", PLATE FROM 2024T3.125" DIM 13" X
- [SDR FDEA201005121525A](https://openairdocs.org/sdr/FDEA201005121525A.md): Bulkhead · cracked · May 12, 2010 · N268FE · Boeing 727233 · Fuselage Main, Bulkhead
  > CRACK FOUND AT BS 1183 BULKHEAD WEB AT RBL 24, WL 170.
- [SDR FDEA201005121525](https://openairdocs.org/sdr/FDEA201005121525.md): Spar · cracked · May 12, 2010 · N268FE · Boeing 727233 · Wing Spar
  > RT WING T/E FALSE SPAR CHORD CRACKED, WBL 118.
- [SDR FDEA201005121521](https://openairdocs.org/sdr/FDEA201005121521.md): Spar · cracked · May 12, 2010 · N268FE · Boeing 727233 · Wing Spar
  > LT WING T/E FALSE SPAR CHORD CRACKED, WBL 118. REPAIRED LT WING T/E FALSE SPAR CHORD WBL 118 IAW DWG NR SR27-57-038, REV C.
- [SDR FDEA200905041529](https://openairdocs.org/sdr/FDEA200905041529.md): Accessory Unit · failed · May 4, 2009 · N268FE · Boeing 727233 · Landing Gear Retraction/Extension System
  > AFTER TAKEOFF, LANDING GEAR HANDLE WOULD NOT MOVE INTO UP POSITION. RAN QRH THROUGH P6-3 L/G LEVER/LATCH C/B PULL/RESET. GEAR WOULD NOT RETRACT. RTB DUE TO FUEL CONSIDERATIONS. REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC MODULE IAW 727-200 AMM 32-09-
- [SDR 08FDEA00004](https://openairdocs.org/sdr/08FDEA00004.md): Support Beam · cracked · Jan 2, 2008 · N268FE · Boeing 727233 · Wing Main, Frame Structure
  > RT WING INBD UPPER WING PANEL SUPPORT BEAM IS CRACKED JUST FWD OF MLG BEAM 10" O/B OF UPLOCK T/T. REMOVED SUPPORT BEAM FROM A/C REF SRM 51-30-2. STOP DRILLED CRACK REF SRM 51-10-1. FABRICATED AND INSTALLED REPAIR ON SUPPORT REF SRM 51-40-2. REINSTALLED SUP
- [SDR 07FDEA05147](https://openairdocs.org/sdr/07FDEA05147.md): Fitting · corroded · Dec 27, 2007 · N268FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > NR 2 LOWER CARGO DOOR THRESHOLD TIEDOWN FITTING 23" FROM AFT EDGE OF CUT OUT CORRODED ON UPPER SURFACE. REMOVED AND REPLACED TIEDOWN FITTING REF DWG 69-47673 REF SRM 51-30-2, THIS IS CLASSIFIED AS A MINOR REPAIR.
- [SDR 07FDEA05143](https://openairdocs.org/sdr/07FDEA05143.md): Skin · gouged · Dec 27, 2007 · N268FE · Boeing 727233 · Trailing Edge Flaps
  > RIGHT WING INBOARD MID FLAP UPPER SURFACE, SKIN GOUGED AT OUTBOARD SIDE. BLENDED DAMAGED AREA, NDT VERIFIED NO DEFECTS. TREATED, PRIMED AND TEFLON PAINTED, REF SRM 57-50-1, SRM 51-10-2, MM 51-20-017-7 AND EA NR 7-5750-113963 THIS IS CLASSIFIED AS A MINOR.
- [SDR 07FDEA05142](https://openairdocs.org/sdr/07FDEA05142.md): Skin · chafed · Dec 27, 2007 · N268FE · Boeing 727233 · Trailing Edge Flaps
  > RIGHT WING INBOARD MID FLAP UPPER SURFACE CHAFED AT INBOARD SIDE BLENDED DAMAGE AREA, NDT VERIFIED NO DEFECTS, TREATED, PRIMED, AND TEFLON PAINTED REF SRM 57-50-1, SRM 51-10-2, MM 51-20-017-7, AND EA 7-5750-113963. THIS IS CLASSIFIED AS A MINOR REPAIR.
- [SDR 07FDEA05122](https://openairdocs.org/sdr/07FDEA05122.md): Floorbeam · corroded · Dec 22, 2007 · N268FE · Boeing 727233 · Fuselage Main, Floor Beam
  > CORROSION AROUND NUT PLATE ON TOP OF FLOORBEAM AT FS 1130, LBL 51, WL 208. REMOVED CORROSION AROUND NUT PLATE ON TOP OF FLOORBEAM STA 1130, LBL 51, FOUND TO BE OUT OF LIMITS REF SRM 53-10-8. SAME LOCATION SEAT TRACK FOUND TO BE OUT OF LIMITS. FABRICATED AND
- [SDR 07FDEA05120](https://openairdocs.org/sdr/07FDEA05120.md): Seat Track · corroded · Dec 21, 2007 · N268FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON I/B SIDE OF SEAT TRACK CROWN AND UNDER DOUBLER PLATE, BS 1137 TO BS 1125M RBL 45, WL 208. REMOVED DAMAGED SECTION OF SEAT TRACK STA 1100 - 1135, RBL 45. FABRICATED AND INSTALLED SEAT TRACK AND REPAIR ANGLES REF SRM 53-10-5 FIG 1 SRM 51-30-2 PG
- [SDR 07FDEA05119](https://openairdocs.org/sdr/07FDEA05119.md): Angle · corroded · Dec 21, 2007 · N268FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > FORWARD LOWER PIT FLOOR STRUCTURE LEFT SIDE STA 570 TO STA 650, Z- ANGLE CORRODED ON LOWER SURFACE REMOVED CORROSION FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR DOUBLER. TREATED AND PRIMED AND INSTALLED. REF SRM 51-40-2 AND SRM 53-10-1.
- [SDR 07FDEA05118](https://openairdocs.org/sdr/07FDEA05118.md): Floorbeam · corroded · Dec 21, 2007 · N268FE · Boeing 727233 · Fuselage Main, Floor Beam
  > CORROSION AROUND NUT PLATE HOLES ON TOP OF FLOORBEAM AT SEVERAL LOCATIONS, FS 1130, LBL 64 TO RBL 64, WL 208. BLENDED DAMAGE AREA STA 1130, RBL 64, FOUND TO BE OUT OF LIMITS, REF SRM 53-10-8 TOOL NR IN17-0023 CAL DATE DUE 2-13-08. REMOVED DAMAGE AREA, REF SR
- [SDR 07FDEA05114](https://openairdocs.org/sdr/07FDEA05114.md): Cargo Track · corroded · Dec 20, 2007 · N268FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK FLOOR TIE DOWN FITTING ASSY IS CORRODED BS 950, RBL 57, WL 208 REMOVED CORROSION ON TIE DOWN FITTING, AND IS OUT OF LIMITS. DRILLED HOLES IN NEW TIE DOWN FITTING AND INSTALLED, REF SRM 51-30-2 AND SRM 51-30-5 THIS IS CLASSIFIED AS A MINOR REPAIR.
- [SDR 07FDEA05108](https://openairdocs.org/sdr/07FDEA05108.md): Channel · corroded · Dec 20, 2007 · N268FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > FORWARD LAV SUPPORT STRUCTURE STA 303 TO 306, RBL 15, HAT CHANNEL CORRODED ON LOWER SURFACE REMOVED CORRODED HAT CHANNEL, FABRICATED NEW CHANNEL, TREATED AND PRIMED AND INSTALLED. REF SRM 51-30-2 AND BAC DWG 65-26173. THIS IS CLASSIFIED AS A MINOR REPAIR.
- [SDR 07FDEA05103](https://openairdocs.org/sdr/07FDEA05103.md): Stringer · damaged · Dec 19, 2007 · N268FE · Boeing 727233 · Fuselage Main, Longeron/Stringer
  > EXT FUSELAGE SKIN 2 RIVETS HAVE LIGHTING STRIKES AT STR S-8R BS 510 AND 513 REMOVED LIGHTNING STRIKE DAMAGE TO SKIN AND STR 8R. INSTALLED SKIN DOUBLER USING.050"2024 T-3 FILLER.040 2024 T-3, REF 53-30-2 FIG 20 STR 8. REPAIRED USING BAC 1598-146 REF SRM 53-
- [SDR 07FDEA05102](https://openairdocs.org/sdr/07FDEA05102.md): Floor Support · corroded · Dec 19, 2007 · N268FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > LWR FWD CARGO PIT, FLOOR SUPPORT Z-ANGLE HAS WIDE SPREAD CORROSION WITH A CRACK AT STA 720 RBL 25" CORROSION FROM 710-720D REMOVED Z-ANGLE AT FWD CARGO PIT STA 720, RBL 25" FROM 710 TO 720D REF SRM 51-30-2. LOCATED AND DRILLED HOLES ON NEW "Z" ANGLE P/N 65C1
- [SDR 07FDEA05101](https://openairdocs.org/sdr/07FDEA05101.md): Stringer · cracked · Dec 19, 2007 · N268FE · Boeing 727233 · Fuselage Main, Longeron/Stringer
  > STR 5L CRACKED ON LOWER SIDE UP RIGHT AT ATTACH RIVET AT STA 353 FABRICATED NEW STINGER, TREATED AND PRIMED REF SRM 51-30-2 AND 51-10-2. INSTALLED STRINGER THIS IS CLASSIFIED AS A MAJOR REPAIR
- [SDR 07FDEA05100](https://openairdocs.org/sdr/07FDEA05100.md): Seat Track · corroded · Dec 19, 2007 · N268FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN FLOOR STRUCTURE, LEFT SIDE STA 560 TO 580, LBL 24 SEAT TRACK, INBOARD FLANGE CORRODED ON UPPER SURFACE, FOUND CORROSION TO BE OUT OF LIMITS. NO CORROSION ALLOWED, IAW P-F SRM 53-10-1, FIG 3A PG 3. REPAIRED SEAT RAIL DAMAGE SECTION, STA 560 TO 670
- [SDR 07FDEA05099](https://openairdocs.org/sdr/07FDEA05099.md): Frame · damaged · Dec 19, 2007 · N268FE · Boeing 727233 · Fuselage Main, Frame
  > MAIN CABIN FRAME HAS DEEP WEAR AT STA 1166 AND STR 8L REMOVED DAMAGE SECTION OF FRAME STA 1166 AT STR 8L. FABRICATED AND INSTALLED REPAIR DOUBLER, REF SRM 51-40-3 FIG 1. TREATED AND PRIMED REPAIR PARTS AND AREA. THIS IS CLASSIFIED AS A MAJOR REPAIR.
- [SDR 07FDEA05098](https://openairdocs.org/sdr/07FDEA05098.md): Spar · cracked · Dec 19, 2007 · N268FE · Boeing 727233 · Vertical Stabilizer, Spar/Rib
  > VERTICAL STAB TIP L/E SPAR, CLOSER WEB HAS CRACK RUNNING THROUGH UPPER MOST FASTENER HOLE OF RIGHT SIDE TERMINAL FITTING LOCATION, 4.5" RBL. FABED DOUBLER, APPLIED ALODINE AND PRIMER AND INSTALLED REF DWG 65-17484, SRM 51- 10-2. CLASSIFIED AS A MINOR REPAIR
- [SDR 07FDEA05097](https://openairdocs.org/sdr/07FDEA05097.md): Stringer Clip · cracked · Dec 19, 2007 · N268FE · Boeing 727233 · Fuselage Main, Attach Fittings
  > STRINGER CLIP IS CRACKED AT STATION 680, STRINGER 10 RIGHT REMOVED, FABRICATED, TREATED AND PRIMED, IDENTIFIED AND INSTALLED STRINGER CLIP IAW SRM 51-10-2, 51-20-1PG 11, 51-30-2 PG4 BAC DWG 60-7232-2 AND FED EX GMM 7-0-1001 P1 ITEM 7B.
- [SDR 07FDEA05096](https://openairdocs.org/sdr/07FDEA05096.md): Longeron · cracked · Dec 19, 2007 · N268FE · Boeing 727233 · Nacelle/Pylon, Frame/Spar/Rib
  > NR 1 ENG LWR COWL DOOR OB LONGERON IS CRACKED AT AFT HINGE CUT OUT. REMOVED, FABRICATED NEW INTERCOSTAL, SENT TO HEAT TREAT ON SNR NR N00829. TREATED AND PRIMED, COMPLETED INSTALLATION, REF SRM 51-30-2, 51-10-2 AND BAC DWG 65-19507.
- [SDR 07FDEA05095](https://openairdocs.org/sdr/07FDEA05095.md): Fairing · cracked · Dec 19, 2007 · N268FE · Boeing 727233 · Nacelle/Pylon, Main Frame
  > NR 1 ENG INBOARD COWLING IS CRACKED THROUGH AT 3RD LATCH FROM THE FRONT (TOP SIDE). REMOVED DAMAGE AND REPAIRED WITH DOUBLER, APPLIED ALODINE AND PRIMER REF SRM 54-10-03, DWG SR27-71-007, 51-10-02, CLASSIFIED AS A MINOR REPAIR.
- [SDR 07FDEA05092](https://openairdocs.org/sdr/07FDEA05092.md): Web · corroded · Dec 19, 2007 · N268FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > CORROSION ON DITCHING WEB FRAMES AT BS 720E AND BS 720F, RT OF MAIN CARGO BAY, WL 208, RBL 67. BLENDED CORROSION ON DITCHING WEB, FOUND TO BE OUT OF LIMITS. ORIGINAL.040", REMOVED.010 " REF SRM 53-10-1 DISPLACED SEAT TRACK FROM STA 720B - 745, RBL 67 REF
- [SDR 07FDEA05091](https://openairdocs.org/sdr/07FDEA05091.md): Retainer · cracked · Dec 19, 2007 · N268FE · Boeing 727233 · Emergency Exits
  > LT FWD OVERWING PRESSURE SEAL CORNER RETAINER ANGLE IS CRACKED. FABRICATED ANGLE REF BAC DWG 50-07978, HEAT TREATED, TREATED AND PRIMED REF SRM 51-10-2. INSTALLED RETAINER REF SRM 51-30-2, THIS IS CLASSIFIED AS A MINOR.
- [SDR 07FDEA05090](https://openairdocs.org/sdr/07FDEA05090.md): Seat Track · corroded · Dec 19, 2007 · N268FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AROUND SEAT TRACK ATTACH SCREW, BS 720E, RBL 64, WL 208. REMOVED DAMAGE SECTION OF SEAT TRACK, REF SRM 51-30-2 FROM STA 720-750, RBL 64. REMOVED CREASE BEAM FROM STA 720C-740, RBL 64 REF SRM 51-30-2. FABRICATED SEAT TRACK, REPAIR PARTS, REF SRM 53
- [SDR 07FDEA05089](https://openairdocs.org/sdr/07FDEA05089.md): Bracket · cracked · Dec 19, 2007 · N268FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > LT WING TO BODY FAIRING ATTACH BRACKET AT STR S-18A, BS 937 IS CRACKED REMOVED CRACKED BRACKET. FABRICATED NEW BRACKET, P/N 65-60789-9, FROM 2024T3 -.063". A TAG A 59659/ PO 1026484. TREATED AND PRIMED AND INSTALLED NEW BRACKET REF SRM 51-30-2 PG 2 AND 8 S
- [SDR 07FDEA05088](https://openairdocs.org/sdr/07FDEA05088.md): Floor Support · corroded · Dec 19, 2007 · N268FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > FWD LAV FLOOR STRUCTURE STA 312 RBL 41 SUPPORT ANGLE CORRODED ON LWR SURFACE. BLENDED CORROSION ON ANGLE. OUT OF LIMITS. REMOVED, FABRICATED NEW ANGLE AND INSTALLED REF BOEING DWG 65-17593, SRM 51-10-2, SRM 53-10-2 AND SRM 51-30-02. THIS IS AS A MINOR REPA
- [SDR 07FDEA05087](https://openairdocs.org/sdr/07FDEA05087.md): Pan · corroded · Dec 19, 2007 · N268FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > CORROSION AROUND ATTACH FWD AND UNDER EDGES OF LAV SINK CABINET FLOOR PAN, BS 304 TO BS 315, RBL 13 TO RBL 41, WL 208. REMOVED CORRODED FLOOR PAN AND FABRICATED NEW PAN REF SRM 51-30-2 PG 3, AND SRM 53-20-1 PG 5 AND 12. TREATED AND PRIMED AND APPLIED TOP COA
- [SDR 07FDEA05086](https://openairdocs.org/sdr/07FDEA05086.md): Attach Angle · cracked · Dec 19, 2007 · N268FE · Boeing 727233 · Fuselage Main, Attach Fittings
  > FWD LAV, I/B WALL, ATTACH ANGLE FROM WALL TO FLOOR STRUCTURE IS CRACKED, BS 315, RBL 15. REMOVED CRACKED ANGLE AND FABRICATED NEW SUPPORT ANGLE REF DWG 65-26173 AND SRM 51-30-2 PG 3. TREATED AND PRIMED AND APPLIED TOP COAT TO NEW ANGLE REF SRM 51-10-2 PG 1.

Next page: https://openairdocs.org/deregistered/N268FE-2013-03-08/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 = 'N268FE' AND deregistration_id = 'N268FE-2013-03-08'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N268FE-2013-03-08/reports

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