Boeing 727-233

Service difficulty reports · 3,034

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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 aircraft_model_key = '727233'
  ORDER BY difficulty_date DESC"

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SDR 07FDEA02826Skin · failedON AGING A/C INSPECTION, FOUND EXISTING REPAIR AT STA 1070-1090, STR 25R-27R, DID NOT CONFORM TO SRM 53-30-03. REMOVED OLD REPAIR, FABRICATED AND INSTALLED NEW SKIN REPAIR FROM 2024-T3, .063 FILLER 2024-T3 .071" DOUBLER PER EA NR I070489 IR,THIS IS CLASSIFIEDAug 10, 2007 · N286FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 07FDEA02824Panel · corrodedRT WING T/E LOWER HINGE PANEL 8506R INNER SURFACE HAS CORROSION AROUND EDGE REPAIRED IAW SRM 51-20-151-7.Aug 10, 2007 · N254FE · Boeing 727233 · Wing, Plate/SkinSDR 07FDEA02823Support · crackedLT WING AT T/E REAR SPAR AREA APROX RS STA 383 UPPER FIXED PANEL LOWER C CHANNEL BRACKET MOUNT SUPPORT HAS A CRACK AT FWD SECTION ABOVE NR 3 TRANS ASSY. REMOVED AND REPLACED C CHANNEL SUPPORT IAW SRM 51-30-2. C CHANNEL SUPPORT, FABRICATED ON TRAVELER NR T7Aug 10, 2007 · N254FE · Boeing 727233 · Wing Miscellaneous StructureSDR 07FDEA02822Skin · crackedLT MLG FLYING DOOR UPPER MID INNER SKIN EDGE CRACKED REPAIRED IAW SRM 51-40-2.Aug 10, 2007 · N254FE · Boeing 727233 · Landing Gear DoorsSDR 07FDEA02815Seat Track · corrodedAFT UPPER MAIN DECK, CORROSION ON SEAT TRACK STA 1166 IN CENTERLINE BL 0" AND LBL 2" ON FLANGE REMOVED, FABRICATED NEW TRACK, INSTALLED SEAT TRACK AT BS 1166 BL 0" PER SRM 51-30-2, 51-30-5, 51-30-08, 51-30-02. THIS IS CLASSIFIED AS A MAJOR REPAIR.Aug 9, 2007 · N286FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA02814Intercostal · corrodedFWD CARGO AREA, STA 702 TO 705 AT STR 28R ABOUT RBL 8 INTERCOSTAL IS CORRODED IN LOWER FWD CORNER. REMOVED STIFFENER AT STA 700 RBL 8, AND STA 720 RBL 8. REMOVED INTERCOSTAL AT RBL 8 BTW STA 700-720. FABRICATED NEW INTERCOSTAL AND INSTALLED. INSTALLED STIFAug 9, 2007 · N286FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 07FDEA02813Angle · crackedUPPER MAIN DECK FLOOR STRUCTURE, ARCHED CLOUSER WEB COVER FWD ATTACH ANGLE IS CRACKED OUT OF NUTPLATE HOLE STA 1178, RBL 50" (VIEW FROM LWR PIT) REMOVED ARCHED CLOSER WEB ASSY. FABRICATED NEW WEB, STIFFENER, AND ANGLE REF DWG 65-29548. TREATED AND PRIMED RAug 9, 2007 · N286FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 07FDEA02812Angle · corrodedLWR AFT CARGO PIT, STA 1166 BULKHEAD WALL STRUCTURE. VERTICAL Z-ANGLE IN CENTERLINE, BL 0" ABOVE DIFFERENTIAL PRESSURE VALVE HAS CORROSION AT LWR AND UPPER LT SIDE. REMOVED DAMAGE AREA, DRILLED NEW PART, Z-ANGLE PN NR 65-67250-34, IAW B727 SRM 51-30- 2 PGAug 9, 2007 · N286FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 07FDEA02811Seat Track · corrodedMAIN CABIN TRACK HAS CORROSION AROUND NUTPLATE HOLES AND OTBD SIDE OF SEAT TRACK FROM BS 774 - 848, LBL 45. REMOVED CORROSION REF SRM 51-10-1, FOUND TO BE OUT OF LIMITS REF SRM 53-10-1, ORIGINAL THICKNESS .090", REMOVED .020", REMAINING .070", REPLACED SEAT TAug 9, 2007 · N286FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA02808Skin · corrodedLWR AFT CARGO PIT DOOR, S/N 508, OUTER SKIN HAS LIGHT PITTING CORROSION ON LWR CONTACT AREA OF BODY FAIRING BLENDED CORROSION, NDT VERIFIED ORIGINAL MATERIAL THICKNESS TO BE .036". MATERIAL LOSS AT DEEPEST POINT IS .002" MATERIAL IS WITHIN LIMITS WITH .034" Aug 8, 2007 · N262FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 07FDEA02807Stringer · crackedPASSENGER CABIN STA 950D, STR 9R STRINGER CLIP CRACKED REMOVED AND REPLACED STRINGER CLIP 950D, STR 9R REF SRM 51-30-2, THIS IS CLASSIFIED AS A MAJOR.Aug 8, 2007 · N262FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR 07FDEA02806Stringer Clip · crackedPASSENGER CABIN STA 780 STR 7R, STRINGER CLIP CRACKED REPLACED STA 780 STR 7R, STRINGER CLIP, IAW SRM 51-30-2. THIS REPAIR CLASSIFIED AS MAJOR.Aug 8, 2007 · N262FE · Boeing 727233 · Fuselage Main, Attach FittingsSDR 07FDEA02801Stringer Clip · crackedSTRINGER CLIP CRACKED AT ATR 9L AND 950 C REMOVED AND REPLACED STRINGER CLIP, STR 9L, STA 950C REF SRM 51-30-2 PG 2 8, THIS IS CLASSIFIED AS A MAJOR REPAIR.Aug 8, 2007 · N262FE · Boeing 727233 · Fuselage Main, Attach FittingsSDR 07FDEA02800Stringer Clip · crackedSTINGER CLIP CRACKED AT STA 800 AND STR 7L REMOVED AND REPLACED STRINGER CLIP AT FS 800 STR 7L, IAW B727 SRM 51-30-2, THIS IS CLASSIFIED AS A MAJOR REPAIR.Aug 8, 2007 · N262FE · Boeing 727233 · Fuselage Main, Attach FittingsSDR 07FDEA02799Stringer Clip · crackedPASSENGER CABIN STA 950E STR 7R, STRINGER CLIP CRACKED REPLACED CRACKED STRINGER CLIP W/NEW, REF SRM 51-30-2, THIS IS CLASSIFIED AS A MAJOR REPAIR.Aug 8, 2007 · N262FE · Boeing 727233 · Fuselage Main, Attach FittingsSDR 07FDEA02798Seat Track · corrodedMAIN DECK SEAT TRACK CORRODED STA 1030-1070, RBL 24 ON CROWN AND FLANGE, WL208. REMOVED CORROSION AT SEAT TRACK STA 1030 TO 1070, RBL 24, IAW 51-10-6, FOUND TO BE OUT OF LIMITS ON STA 1030, ORIGINAL THICKNESS ON FLANGE OF .070" MATERIAL LOSS .030". REMAINIAug 8, 2007 · N262FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA02784Flap Track · corrodedNR 3 (LT) FLAP OB TRACK, HAS RUST AT UPPER MOUNTING SURFACE C/T SPOILER BEAM ATTACH PT. REPLACED NR 3 TRACK, NEW TRACK IS INSTALLED ON W/C 27X5705-03, THIS IS CLASSIFIED AS A MINOR REPAIR.Aug 7, 2007 · N262FE · Boeing 727233 · Trailing Edge FlapsSDR 07FDEA02783Flap Track · corrodedRT WING NR 6 FLAP TRACK UPPER ATTACH POINT AT SPOILER BEAM HAS CORROSION. REPLACED NR 6 TRACK, NEW TRACK IS INSTALLED ON W/C 27X5708-03. THIS IS CLASSIFIED AS A MINOR REPAIR.Aug 7, 2007 · N262FE · Boeing 727233 · Trailing Edge FlapsSDR 07FDEA02782Flap Track · corrodedON NON-ROUTINE, RIGHT OUTBD FLAP INBD FLAP TRACK HAS CORROSION AT THE OUTBD AND CENTER MOUNT HOLES AT MOUNT PAD. ON NON- ROUTINE, OUTBD FLAP INBD FLAP TRACK MOUNT BOLTS ARE WORN AND GOUGED. ON NON-ROUTINE, FLAP TRACK HAS WEAR ON TOP OF FLAP TRACK ON OUAug 7, 2007 · N286FE · Boeing 727233 · Trailing Edge FlapsSDR 07FDEA02781Flap Track · corrodedON NON-ROUTINE, RIGHT OUTBD FLAP TRACK HAS CORROSION. ON NON- ROUTINE, RIGHT OUTBD FLAP TRACK HAS WEAR ON TOP OF TRACK. NON- ROUTINE, RIGHT OUTBD FLAP TRACK HAS LIGHT RUST IN FWD HORIZONTAL HOLE AT MOUNT PAD. REPLACED NR 8 FLAP TRACK. NEW FLAP TRACK IS INAug 7, 2007 · N262FE · Boeing 727233 · Trailing Edge FlapsSDR 07FDEA02739Pump · crackedAPPROX 30 SECS AFTER GOING TO FLAPS 30. TOTAL LOSS OF A HYDRAULIC SYSTEM. ALTERNATE FLAP SYSTEM USED TO RAISE FLAPS TO 15. GPWS SYSTEM INHIBITED. PER CREW DEBRIEF, BOTH HYDRAULIC PUMPS WERE SHUT OFF IMMEDIATELY AFTER PRESSURE LOSS. FOUND NR 1 ENG DRIVEN HAug 3, 2007 · N257FE · Boeing 727233 · Hydraulic Pump (Electric/Engine), MainSDR 07FDEA02756Rib · crackedRT WING L/E SLAT NR 5 INBD END PORK CHOP SEAL MOUNTING PLATE DEFORMED AND CRACKED. REMOVED CRACKED RIB, FABBED NEW RIB ON TRAVLER T/682663. INSTALLED NEW RIB.Aug 3, 2007 · N254FE · Boeing 727233 · Wing, Rib/BulkheadSDR 07FDEA02755Fitting · corrodedAFT PIT CARGO DOOR THRESHHOLD STANCHION FITTINGS STA 950E-990 RBL 22-27 4 EA. FITTINGS CORRODED UPON FURTHER REVIEW 2 FITTINGS WITHIN LIMITS AFTER BLEND OUT PER DWG 69-45577-2 AND 69-45576-3. 2 OUT OF LIMITS. REPLACED AT STA 950F AND 950G, ALL FITTINGS REPLAug 3, 2007 · N286FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 07FDEA02738None · noneAFTER GEAR RETRACTION ON CLIMB-OUT, SYS A HYD ENG NR 1 PUMP LOW PRESS LIGHT ILLUMINATED AND NOTICED HYD SYS A QUANTITY DECREASING. JACKED AIRCRAFT IAW THE B727-200 AMM 07-11-000-2. CYCLED THE LANDING GEAR 15 PLUS TIMES WHILE CYCLING. THE FLT CONTROL NUMEROUAug 2, 2007 · N265FE · Boeing 727233 · Hydraulic System, MainSDR 07FDEA02716Floorbeam · corrodedCABIN STA 950 FLOORBEAM BET RBL 45 AND 62 HAS CORROSION ON UPPER AND LWR, AND AROUND FASTENER HOLES REMOVED CORROSION. HFEC NO DEFECT NOTED, ROTO PEENED REF SOPM 20-10-3. TREATED AND PRIMED REF SRM 51-10-2, LEVEL 1 CORROSION.Aug 2, 2007 · N286FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 07FDEA02737Skin · chafedRT LWR FUSELAGE SKIN CHAFED STA 720D 14" STR 19R FABRICATED AND INSTALLED DOUBLER IAW SRM 53-30-3 FIG 5, PAGE 20-22. THIS IS CLASSIFIED AS A MAJOR REPAIR.Aug 2, 2007 · N286FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 07FDEA02732Skin · gougedAFT LT FUSELAGE, STA 988 TO 990, BETWEEN STR 23L AND 24L HAS 2 DEEP GOUGES. BLENDED GOUGES AND FOUND TO BE OUT OF ALLOWABLE LIMITS REF SRM 53-30-1. TRIMMED OUT DAMAGE, FABRICATED REPAIR DOUBLER AND INSTALLED REF 53-30-1 FIG 1, THIS IS CLASSIFIED AS A MAJOR RAug 2, 2007 · N262FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 07FDEA02724Crease Beam · crackedLT AFT FUSELAGE UNDER REMOVED CENTER ENG SUPPORT EXT SKIN PANEL, CREASE ANGLE IS CRACKED UNDER TRIANGULAR RIB, UPPER IB CORNER ATTACHED TO OB SIDE OF VERT STAB SKIN BS 1360 THE CREASE CHORD WAS REPAIRED REF EO NR 7-5530-7-2303 PRT 5, REV Q. JPF STEPS 20-30 ANDAug 2, 2007 · N286FE · Boeing 727233 · Fuselage Main, StructureSDR 07FDEA02722Threshold · corrodedAFT PIT CARGO DOOR THRESHOLD AREA BEAM WEB CORRODED, STA 950E - 990 RBL 21"-22", WL 145 - 148 REMOVED CORROSION FROM AFT PIT CARGO DOOR THRESHOLD WEB BEAM AREA, FOUND TO BE OUT OF LIMITS. REMOVED Z- ANGLE FWD/AFT FOR ACCESS UPPER CHORD BEAM. FABRICATED AND IAug 2, 2007 · N286FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 07FDEA02715Frame · corrodedAFT PIT FRAME CORRODED AT STA 1010 BETWEEN STR 29-30R. REMOVED FASTENERS REF SRM 51-30-2. REMOVED CORROSION REF SRM 51-10-1. INSTALLED FASTENERS REF SRM 51-30-2. TREATED AND PRIMED REF MM 51-20-013 AND PAINTED REF MM 51-20-013. CORROSION LEVEL 1.Aug 2, 2007 · N286FE · Boeing 727233 · Fuselage Main, FrameSDR 07FDEA02637Hose · failedUPON GEAR RETRACTION AFTER T/O SYS A FLUID QTY WENT TO ZERO. LT MAIN GEAR REMAINED EXTENDED. SYS A PUMPS AND FLUID SHUTOFF SWITCH WERE TURNED OFF FOR APPROX 25 MINS WITH ENGINES RUNNING. GEAR MANUALLY EXTENDED. FOUND RETRACT LINE BLOWN ON LEFT GEAR. REMOVJul 27, 2007 · N265FE · Boeing 727233 · Hydraulic System, MainSDR 07FDEA02636Floorbeam · misrepairedON AGING A/C INSP, FOUND EXISTING REPAIR LOCATED AT BS 620 FLOORBEAM UPPER CHORD FROM LBL 3" TO 19". EVALUATED AND DETERMINED REPAIR NOT TO CONFORM TO FED EX DWG SR27-53-034. REMOVED EXISTING REPAIR, FABRICATED NEW REPAIR ANGLE FROM 17-7 PH .063", HEAT TREATJul 26, 2007 · N286FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 07FDEA02627Skin · gougedAFT LWR EXTERNAL BELLY SKIN HAS NUMEROUS NICKS, FROM STA 950D BACK TO 1050, STR 26L TO 26R BLENDED BELLY SKINS FOR NICKS AND REMOVED CORROSION, SRM 51-10-1, ORIGINAL METAL .075", METAL REMOVED .010 AND METAL REMAINING .065" THIS IS CLASSIFIED AS A MINOR REPAIRJul 26, 2007 · N286FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 07FDEA02622Floorbeam · corrodedFWD CARGO AREA, STA 643 AT STR 28R ABOUT RBL 12, FLOOR SUPPORT CORRODED UNDER NUT PLATE. REMOVED CORROSION BY CUTTING OUT DAMAGED AREA, SRM 51-40 -4 PG 1. FABRICATED REPAIR PARTS SRM 51-40-4 PG 1-5. DRILLED FASTENER HOLES SRM 51-40-4 AND 51-30-2 PG 1- 12. Jul 26, 2007 · N286FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 07FDEA02620Floorbeam · corrodedSTA 848 FLOORBOARD SUPPORT BET BL 0 AND LBL 24, HAS LIGHT CORROSION AT NUTPLATE HOLES, UPPER AND LOWER FLANGES SURFACES REMOVED FLOOR SUPPORT AND INSTALLED NEW FLOORBOARD SUPPORT BL 0 TO LBL 24 NAD INSTALLED INBD AND OTBD SEAT TRACK FLANGE, STA 780 - 850 FER SJul 26, 2007 · N286FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 07FDEA02618Splice · crackedLEFT WING LEADING EDGE OVER WING PANEL 3342, FORWARD SPLICE ANGLE HAS LOOSE/WORKING RIVETS AND IS CRACKED IN HALF. REPLACED FASTENERS AND FAB SPLICE ANGLE REF 51-30-2, GMM 7-0-1001, DWG 65-22555.Jul 26, 2007 · N286FE · Boeing 727233 · Wing Miscellaneous StructureSDR 07FDEA02616Door Frame · gougedUPPER MAIN CARGO DOOR, AFT SIDE FRAME, HAS DEEP GOUGE IN PRIOR REPAIR DOUBLER, 19" UP FROME BOTTOM EDGE REMOVED OLD DOUBLER REF SRM 51-30-2, VERIFIED MATERIAL AS 7075-0-.090, FABRICATED REPAIR DOUBLER REF. PF SRM 52-30-2, HEAT TREATED TO 7075-T6, FIT AND Jul 26, 2007 · N286FE · Boeing 727233 · Cargo/Baggage DoorsSDR 07FDEA02615Seat Track · corrodedMAIN CABIN FLOOR SEAT TRACK IS CORRODED AT STA 1090 RBL 45 REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, .090" REMOVED. VERIFIED MATERIAL BAC1520-792 7178T6511, FABRICATED NEW SEAT TRACK, TREATED AND PRIMED NEW SEAT TRACK. INSTALLED NEW SEAT TRACK REF 27 Jul 26, 2007 · N286FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA02613Fairing · crackedRT WING OB TE NR 8 JACKSCREW FAIRING, CRACK COMING OUT OF FASTENER HOLE AT FWD END. REMOVED DAMAGE AREA REF SRM 57-20-4 FIG 1 PG 5. FAB`D REPAIR PARTS REF SRM 51-30- 05 AND 57-20-4 FIG, 1 PG 5. INSTALLED REPAIR PARTS REF SRM 51-30-02 PG 1 AND REF SRM 57-20-Jul 25, 2007 · N286FE · Boeing 727233 · Wing Miscellaneous StructureSDR 07FDEA02603Solenoid · failedAFTER LIFTOFF AND GEAR RETRACTION LANDING GEAR LEVER WOULD NOT RAISE PAST THE OFF POSITION. THE LEVER LATCH LIGHT CIRCUIT BREAKER IMMEDIATELY OPENED AND THE FORWARD LANDING GEAR ANNUNCIATOR PANEL LIGHTS INDICATED ONLY THE GREEN NOSE GEAR LIGHT. CONSULT QRHJul 25, 2007 · N275FE · Boeing 727233 · Landing Gear Retraction/Extension SystemSDR 07FDEA02612Floorbeam · corrodedCABIN FLOORBEAM AT STA 950 HAS CORROSION ON UPPER SURFACE BET RBL 24 RBL 45 REMOVED CORROSION FROM FLOORBEAM AT STA 950 RBL 24 TO RBL 45 IAW B727 SRM 51-10-1, ORIGINAL .125", REMAINING .120", HFEC. NO DEFECTS NOTED, ROTO PEENED, TREATED AND PRIMED IAW EA NR 7Jul 25, 2007 · N286FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 07FDEA02611Bracket · crackedRT WING FWD NAV LIGHT BRACKET CRACKED. REPLACED RT WING FWD NAV LIGHT BRACKET, REF SRM 51-30-02 P.13.Jul 25, 2007 · N286FE · Boeing 727233 · Wing Miscellaneous StructureSDR 07FDEA02608Skin · misrepairedON AGING AC INSP, FOUND EXISTING REPAIR LOCATED ON NR 3 LOWER CARGO DOOR SKIN 31" FROM BOTTOM EDGE FROM 1" TO 48" FROM FWD EDGE. DID NOT CONFORM TO SRM 52-00-3 FIG 3. REMOVED 2 EXISTING DOUBLER, INSTALLED 1 DOUBLER TO REPAIR AREA REF SRM 52-00-3. THIS IS CLJul 25, 2007 · N286FE · Boeing 727233 · Cargo/Baggage DoorsSDR 07FDEA02607Frame · corrodedAFT PIT FRAME STA 1090 CORRODED FWD FACE, OTBD RADIUS BETWEEN STR 19-20R. REMOVED CORROSION PER EA NRI070450 STEP 1, ROTO PEENED AREA PER EA I070450 STEP 3. ALODINED AND PRIMED PER EA NR I070450 STEP 4, THIS IS CLASSIFIED AS A MINOR REPAIR.Jul 25, 2007 · N286FE · Boeing 727233 · Fuselage Main, FrameSDR 07FDEA02605Skin · chafedRT LWR AFT FUSELAGE EXTERIOR SKIN CHAFED AT AFT CARGO PIT FWD DOOR CUTOUT FWD UPPER CORNER. REMOVED CHAFED DAMAGE IAW SRM 51-10-1, NDT FOR MATERIAL LOSS, IAW NDT MANUAL PART 4 51-00-00 FIG 2, OUT OF LIMITS PER SRM 53-30-1 PG 2C FIG 2, VERIFIED MATERIAL 2024- Jul 25, 2007 · N286FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 07FDEA02604Seat Track · corrodedUPPER MAIN DECK SEAT TRACK HAS CORROSION AT BL- 0, STA 930 LT SEAT TRACK FLANGE. REMOVED OLD SEAT TRACK, FABRICATED NEW TRACK. INSTALLED NEW TRACK AT BS 930 BL 0, REF SRM 51-30-02.Jul 25, 2007 · N286FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA02601Accessory Unit · failedAFTER LOWERING LANDING GEAR, DID NOT GET LEFT OR RIGHT GEAR DOWN LIGHTS. COMPLIED WITH QRH PROCEDURES TO VERIFY GEAR DOWN AND LOCKED. NORMAL LANDING ACCOMPLISHED. REMOVED AND REPLACED LANDING GEAR POSITION/WARNING ACCESSORY UNIT IAW 727-200 AMM 32-09-122-5.Jul 24, 2007 · N275FE · Boeing 727233 · Landing Gear Position and WarningSDR 07FDEA02553Floorbeam · damagedCABIN MAIN DECK FLOORBEAM AT BS 720 RBL 48" HAS A DOUBLE DRILLED HOLE IN FWD FLANGE OF THE UPPER CHORD. REMOVED DAMAGE AREA'S. FAB 2EA REPAIR ANGLES FAB 3EA SHIMS, FAB CHORD, FAB WEB, FAB T-CHORD PN 65-80690 IAW B727 SRM 51-30-2 FIG NR 8. INSTALLED FAB PAJul 20, 2007 · N286FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 07FDEA02552Rib · crackedLT AFT FUSELAGE UNDER REMOVED CENTER ENG SUPPORT EXT SKIN PANEL, TRIANGULAR RIB WEB IS CRACKED AT UPP IB CORNER ATTACHED TO OB SIDE OF VERT STAB SKIN BS 1360. (MKD) REMOVED RIB ASSEMBLY, DISASSEMBLED, FABRICATED AND HEAT TREATED NEW WEB, DRILLED UP NEW WEB, AJul 20, 2007 · N286FE · Boeing 727233 · Nacelle/Pylon, Frame/Spar/RibSDR 07FDEA02551Seat Track · corrodedRBL 24 SEAT TRACK BETWEEN STA 804 TO 848 HAS LIGHT CORROSION AROUND NUT PLATE HOLES ON UPPER AND LWR FLANGE SURFACES (DOT 15) REPLACED T-CAP IAW SRM 51-30-2.Jul 20, 2007 · N286FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
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