N262FE, cancelled Dec 18, 2013

Service difficulty reports · 157

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR FDEA201110134476Switch · damagedAFTER 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 SOct 13, 2011 · N262FE · Boeing 727233 · Landing Gear Position and WarningSDR FDEA201109224034Retainer · brokenEMERGENCY 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.Sep 22, 2011 · N262FE · Boeing 727233 · Emergency EquipmentSDR FDEA201104071377Valve · leakingDURING 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. Apr 7, 2011 · N262FE · Boeing 727233 · Engine Bleed Air SystemSDR FDEA201101260370Light · inoperativeCOCKPIT EMERGENCY EXIT LIGHT ILLUMINATED INTERMITTENTLY DURING CLIMBOUT. REPEAT GRIPE. R & R COCKPIT EMERGENCY EXIT LIGHT IAW MM 33-50-101-2. OPS CHECKED GOOD.Jan 26, 2011 · N262FE · Boeing 727233 · Emergency LightingSDR FDEA201101250344Battery Pack · inoperativeEMERGENCY LIGHTS ILLUMINATED INTERMITTENTLY. R & R EMERGENCY EXIT LIGHT ASSY. INSTALLED NEW BATTERIES IAW MM33-50-001-2, OPS NORMAL.Jan 25, 2011 · N262FE · Boeing 727233 · Emergency LightingSDR FDEA201010114002Contact · dirtyCABIN 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 GOOct 11, 2010 · N262FE · Boeing 727233 · Light System WiringSDR FDEA200911093923Shear Tie · corrodedINT 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 5Nov 9, 2009 · N262FE · Boeing 727233 · Fuselage Internal Mounting StructureSDR FDEA200911083920Skin · misrepairedDOUBLER 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, FABRINov 8, 2009 · N262FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA200911073886Skin · damagedRT 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 5Nov 7, 2009 · N262FE · Boeing 727233 · Emergency ExitsSDR FDEA200910303747Stringer · corrodedINT 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 Oct 30, 2009 · N262FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA200910303746Stringer · corrodedINT 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 IOct 30, 2009 · N262FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA200910303745Skin · damagedMAIN 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 Oct 30, 2009 · N262FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA200910303744Skin · corrodedAFT 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 DOct 30, 2009 · N262FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA200910283718Seat Track · corrodedCORROSION 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 CONDITOct 28, 2009 · N262FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200910273852Skin · damagedDOUBLER 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. IOct 27, 2009 · N262FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA200910273692Angle · crackedRT 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.Oct 27, 2009 · N262FE · Boeing 727233 · Fuselage Main, BulkheadSDR FDEA200910273740Angle · crackedLT 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- 5Oct 27, 2009 · N262FE · Boeing 727233 · Wing Miscellaneous StructureSDR FDEA200910273695Skin · dentedDENT 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-Oct 27, 2009 · N262FE · Boeing 727233 · Nacelle/Pylon, Plate/SkinSDR FDEA200910273691Frame · corrodedAFT 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-Oct 27, 2009 · N262FE · Boeing 727233 · Fuselage Main, FrameSDR FDEA200910213651Angle · crackedLEFT 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.Oct 21, 2009 · N262FE · Boeing 727233 · Trailing Edge FlapsSDR FDEA200910213637Seat Track · corrodedCORROSION 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 FIGOct 21, 2009 · N262FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200910213641Torque Box · crackedAFT 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. INSTAOct 21, 2009 · N262FE · Boeing 727233 · Fuselage Main, StructureSDR FDEA200910213640Torque Box · crackedAFT 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 .032Oct 21, 2009 · N262FE · Boeing 727233 · Fuselage Main, StructureSDR FDEA200910213639Torque Box · crackedAFT 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 Oct 21, 2009 · N262FE · Boeing 727233 · Fuselage Main, StructureSDR FDEA200910213622Frame · damagedSTA 303.9 FRAME, WEB CUTOUT AT STR 15L AND STR 16L HAVE SHARP RADIUS. ACCOMPLISHED REPAIR IAW EA NR 7-5310-135505.Oct 21, 2009 · N262FE · Boeing 727233 · Fuselage Main, FrameSDR FDEA200910203736Skin · damagedTRIPLER 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 51-30Oct 20, 2009 · N262FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA200910203735Angle · crackedRT 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. INOct 20, 2009 · N262FE · Boeing 727233 · Trailing Edge FlapsSDR FDEA200910203650Skin · damagedTRIPLER 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.Oct 20, 2009 · N262FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA200910203653Seat Track · corrodedCORROSION 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.Oct 20, 2009 · N262FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200910203655Skin · damagedMAIN 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. FAOct 20, 2009 · N262FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA200910203654Seat Track · corrodedCORROSION SEAT TRACK FLANGE BS 360 - BS 420 LBL 24.Oct 20, 2009 · N262FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200910203652Seat Track · corrodedCORROSION SEAT TRACK FLANGE BS 360 - BS 420 BL0.Oct 20, 2009 · N262FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200910203636Skin · gougedRT 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. INOct 20, 2009 · N262FE · Boeing 727233 · Trailing Edge FlapsSDR FDEA200910183605Web · crackedAFT 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 TORQUOct 18, 2009 · N262FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR FDEA200910183600Web · crackedAFT 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 LIGHOct 18, 2009 · N262FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR FDEA200910183604Torque Box · crackedAFT 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.Oct 18, 2009 · N262FE · Boeing 727233 · Fuselage Main, StructureSDR FDEA200910183603Angle · crackedRT 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.Oct 18, 2009 · N262FE · Boeing 727233 · Trailing Edge FlapsSDR FDEA200910153587Angle · damagedPLUG 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 REPAIROct 15, 2009 · N262FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR FDEA200910153578Vertical Beam · misinstalledFASTENERS 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, FOct 15, 2009 · N262FE · Boeing 727233 · Fuselage Main, StructureSDR FDEA200910143601Angle · crackedNR 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 ANGLESOct 14, 2009 · N262FE · Boeing 727233 · Leading Edge DevicesSDR FDEA200901240316Valve · malfunctionedTHE 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.Jan 24, 2009 · N262FE · Boeing 727233 · Landing Gear Brake SystemSDR 07FDEA03867Frame · corrodedAFT 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 -Sep 17, 2007 · N262FE · Boeing 727233 · Fuselage Main, FrameSDR 07FDEA03873Support Beam · inoperativeLT 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 TORQUSep 17, 2007 · N262FE · Boeing 727233 · Wing Miscellaneous StructureSDR 07FDEA03872Floorbeam · corroded"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, THISSep 17, 2007 · N262FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 07FDEA03870Channel · corrodedLWR 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.Sep 17, 2007 · N262FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 07FDEA03791Bracket · crackedLT 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.Sep 14, 2007 · N262FE · Boeing 727233 · Wing, Attach FittingsSDR 07FDEA03789Frame · dentedFWD 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 DSep 14, 2007 · N262FE · Boeing 727233 · Fuselage Main, FrameSDR 07FDEA03669Skin · crackedLEFT 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.Sep 13, 2007 · N262FE · Boeing 727233 · Trailing Edge FlapsSDR 07FDEA03664Bracket · crackedUPPER 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, Sep 13, 2007 · N262FE · Boeing 727233 · Wing Miscellaneous StructureSDR 07FDEA03721Beam · corrodedRT 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 Sep 13, 2007 · N262FE · Boeing 727233 · Wing Main, Frame Structure
Back to N262FE, cancelled Dec 18, 2013