Boeing 727-225

Service difficulty reports · 4,226

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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 = '727225'
  ORDER BY difficulty_date DESC"

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SDR 07FDEA01367Threshold · crackedAFT LOWER CARGO PIT DOOR CUTOUT THRESHOLD HAS 2 CRACKS IN CURVED AREA BETWEEN 27" AND 32" AFT OF FWD EDGE WELD ACCOMPLISHED ON SHOP N/R 11841-8300-0001. VERIFIED MATERIAL WELDED AND SMOOTHED AREA REFERENCE FED EX DWG SR27-53-025C.Apr 6, 2007 · N463FE · Boeing 727225 · Fuselage Miscellaneous StructureSDR 07FDEA01366Skin · damagedEXT FUSELAGE BS 420 S-4R 2 PAIRS OF OVERLAPPPING RIVET HEADS AND SEVERAL RIVETS CLOSELY SPACED REMOVED 9 G NET ATTACH STRUCTURE BETWEEN S-4R AND S-5R CUT OUT DAMAGED AREA. FABRICATED REPAIR FILL AND REPAIR DOUBLER AND INSTALLED. REFERENCE EA NR 7-5330-106995Apr 6, 2007 · N463FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR 07FDEA01364Skin · crackedLEFT WING FAIRING NR 3343 VERIFIED MATERIAL AS 2024-0 .050 REF DWG 65-22555 AND SRM 51-40-2 PG 1. STOPPED DRILLED CRACK REF SRM 51-10-PG 13 ITEM 10, HFEC IAW 727NDT MAN PART 6, 51-00-00 FIG 23. TOOL NR IDM 0031 11-30-07. VERIFIED CRACK TO BE CONFINED BY STOApr 5, 2007 · N463FE · Boeing 727225 · Wing, Plate/SkinSDR 07FDEA01365Web · corrodedMAIN DECK FLOOR WEB UPPER SURFACE IS CORRODED BS 1147, LBL 52-63, WL 208. REMOVED DAMAGE AREA OF WEB REF SRM 51-40-2 FIG 1, STA 1147, LBL 62, THAT WAS OUT OF LIMITS REF 51-10-1, AFTER BLENDING, MFG AND INSTALLED REPAIR REF SRM 51-40-2 FIG 1 AT LBL 62Apr 5, 2007 · N463FE · Boeing 727225 · Fuselage Miscellaneous StructureSDR 07FDEA01363Keelbeam · corrodedLOWER AFT PIT BILGE, STA 950E 10, LBL 8" O/B LWR FLANGE OF KEEL BEAM CHORD HAS CORROSION, ON PREVIOUS STRAP REPAIR. REMOVED FLOOR SUPPORT AND SHEAR TIE FOR ACCESS, GROUND CORROSION ON EXISTING STRAP AND NDT FOR MATERIAL LOSS. FOUND TO BE OUT OF LIMITS. FAApr 5, 2007 · N463FE · Boeing 727225 · Fuselage Main, KeelSDR 07FDEA01362Keelbeam · corrodedLWR AFT PIT BILGE, STA 950A LBL 8" OB LWR FLANGE OF KEEL BEAM CHORD HAS APPROX 6 SQ INCHES OF CORROSION ON UPPER SURFACE. REMOVED CORROSION ON OUTBOARD FLANGE OF KEEL BEAM LWR AFT PIT BILGE STA 950A, 6" LBL 8" FOUND AREA OUT OF LIMITS. FABRICATED, TREATED AApr 5, 2007 · N463FE · Boeing 727225 · Fuselage Main, KeelSDR 07FDEA01351Fitting · damagedINTERNAL FUSELAGE AT STA 259.BL0 TO RBL 2, CASTING HAS TOOLING DAMAGE REMOVE FLIGHT DECK CEILING TO GAIN ACCESS TO CASTING. REMOVED INTERCOSTAL AND SURROUND STRUCTURE. REMOVED CASTING, DRILLED NEW CASTING AND INSTALLED. RE-INSTALLED ALL STRUCTURE AND CEILINApr 4, 2007 · N463FE · Boeing 727225 · Fuselage Miscellaneous StructureSDR 07FDEA01350Skin · crackedFUSELAGE UPPER LOBE INTERIOR SKIN IS CRACKED ON BOTH SIDES OF STRINGER AT SKATE ANGLE FASTENERS AT BS 1097, STR 1, LBL 1 - RBL 1. REMOVED DAMAGE AND INSTALLED DOUBLER IN REFERENCE TO SRM 53-30-3, PG 12.Apr 4, 2007 · N463FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR 07FDEA01349Casting · crackedMAIN DECK 2 RIGHT DOOR CUT OUT UPPER AFT CORNER SEAL DEPRESSOR CASTING IS CRACKED AT BS 1062 WL 271. REMOVED AND DRILLED UP R2 CORNER SEAL DEPRESSOR CASTING. INSTALLED CASTING REF 51-30-02.Apr 4, 2007 · N463FE · Boeing 727225 · Fuselage Miscellaneous StructureSDR 07FDEA01347Floorbeam · corrodedMAIN DECK FLOORBEAM UPPER FLANGE IS CORRODED AT BS 1110, RBL 22, WL 208 CORROSION DAMAGE REPAIRED REFERENCE EA NR 7-5310-106997.Apr 4, 2007 · N463FE · Boeing 727225 · Fuselage Main, Floor BeamSDR 07FDEA01345Bracket · corrodedMAIN ENTRY DOOR EMERG ESCAPE SLIDE, BACK PAN LWR LATCH HINGED RETAINER, MOUNT BLOCK HAS EXFOLIATION CORROSION. INSTALLED NEW BRACKET REF SRM 51-30-2 PG 2.Apr 4, 2007 · N463FE · Boeing 727225 · Escape SlideSDR 07FDEA01344Bracket · crackedNR 6 FLAP TRACK OTBD FAIRING ATTACH BRACKET IS CRACKED REMOVED AND REPLACED NR 6 FLAP TRACK OTBD BRACKET REF SRM 5130-2 PGS 3, 4 AND 5 AND SRM 51-20-031-7 PGS 1, 3 AND 7.Apr 4, 2007 · N463FE · Boeing 727225 · Wing, Attach FittingsSDR 07FDEA01331Splice · corrodedAFT PIT STR -30 APPROX STA 1178 EXFOLIATED. REMOVED AND REPLACED SPLICE IAW 51-30-2.Apr 4, 2007 · N461FE · Boeing 727225 · Fuselage Miscellaneous StructureSDR 07FDEA01327Skin · crackedRT WING LEADING EDGE UPPER SURFACE CUTOUT AT NR 5 SLAT INBD GUIDE IS GOUGED AND CRACKED AT AFT EDGE REMOVED SLAT SEALS AND COVER FOR ACCESS, DAMAGE REMOVED REF SRM 57-30-2. HFEC FOR CRACKS REF B727 NDT MANUAL PART 6. FABRICATED PART AND INSTALLED REPAIR REF Apr 4, 2007 · N463FE · Boeing 727225 · Wing, Plate/SkinSDR 07FDEA01318Skin Panel · gougedRT VERTICAL STAB SKIN/WEB HAS (2 EA) TOOLING GOUGES LOCATED UNDER PANEL 9706. GOUGES ARE LOCATED NEAR FASTENER ROW FOR L- ANGLE AND 23", 24" FROM FRONT OF PANEL. REMOVED DAMAGE PER EA I070144. VERIFY DAMAGED REMOVED BY HFEC IAW 727 NDT MAN, PART 6, 51-00-00Apr 4, 2007 · N463FE · Boeing 727225 · Vertical Stabilizer, Plate/SkinSDR 07FDEA01309Nacelle · crackedNR 1 ENGINE FIXED COWL UPPER SECTION CRACKED AT UPPER FWD CORNER. REPLACED FIXED COWL, NEW COWL INSTALLED ON WC 70T0001-01.Apr 3, 2007 · N463FE · Boeing 727225 · Nacelle/Pylon, Attach FittingsSDR 07FDEA01308Skin · crackedFOUND REPAIR AT FUSELAGE STA 1184, LBL 10. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED REPAIR DOUBLER REF SRM 51-30-2. HFEC SKIN IAW 727 NDT MANUAL PART 6, 51-00-00 FIG 23. FOUNApr 3, 2007 · N463FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR 07FDEA01307Attach Angle · crackedRT WING TE, LOWER PANEL BELOW NR 13 SPOILER PANEL OTBD ATTACH ANGLE OF THE INBD SET IS CRACKED AT SUPPORT ROD. FABRICATED REPLACEMENT ANGLE ON SHOP WO NR 11841-6300-0002. HEAT TREATED ON 8130- 3 TRACKING NR 2007-03-142. REPLACED ANGLE ATTACHMENT FOR LOWER PApr 3, 2007 · N463FE · Boeing 727225 · Wing, Attach FittingsSDR 07FDEA01306Angle · corrodedLOWER AFT PIT FWD BULKHEAD STA 950A, LBL 12, HORIZONTAL L-ANGLE AT BASE OF WALL SUPPORT HAS CORROSION AT INBD END. REMOVED L ANGLE FROM LBL 6 TO LBL 21, STA 950A. FABRICATED NEW L ANGLE ON AAR SHOP WO NR 11841-1600-0002, BY HEAT TREATING ANGLE REF DWG 65-672Apr 3, 2007 · N463FE · Boeing 727225 · Fuselage Miscellaneous StructureSDR 07FDEA01304Floorbeam · corrodedLOWER AFT PIT FLOORBEAM, VERTICAL CHANNEL HAS CORROSION AT LWR END AROUND FASTENER HEAD AT STA 950E, LBL 8 FABRICATED NEW FLOORBEAM VERTICAL CHANNEL AT STA 950E, LBL 8. HEAT TREATED AND HARDNESS TESTED FOR 7075 T6 CONDITION REF BAC DWG 69-44559 AND BAC 5602 RApr 3, 2007 · N463FE · Boeing 727225 · Fuselage Main, Floor BeamSDR 07FDEA01301Frame · corrodedLOWER AFT PIT BILGE, FRAME HAS APPROX 3 SQ INCHES OF CORROSION ON AFT LOWER FACE AT STA. 950A, LBL 8". REMOVED CORROSION REF 51-10-2 AND 53-10-1. NDT'D FOR MATERIAL LOSS, FOUND AREA OUT OF LIMITS REF SRM 53-10-1 FIG 1. REMOVED SUPPORT BRKT, VERT SUPPORT BRKApr 3, 2007 · N463FE · Boeing 727225 · Fuselage Main, FrameSDR 07FDEA01300Support Channel · corrodedLOWER AFT PIT BILGE FWD SIDE OF STA 950A, VERTICAL SUPPORT CHANNEL AT 8" LBL HAS SMALL AMOUNT OF CORROSION AT LOWER OB. REPLACED VERTICAL SUPPORT AT STA 950A. REFERENCE SRM 51-30-2 PAGE 1 - 12.Apr 3, 2007 · N463FE · Boeing 727225 · Fuselage Miscellaneous StructureSDR 07FDEA01298Angle · corrodedLOWER AFT PIR FWD BULKHEAD STA 950A, RBL 22, L ANGLE AT BASE OF WALL SUPPORTS HAVE CORROSION ON UPPER SURFACE (2 EACH) DAMAGE TO 2 L ANGLES OUT OF LIMITS. ORIGINAL MATERIAL WAS .050", REMAINING MATERIAL .035". FABRICATED 2 REPAIR ANGLES, HEAT TREATED TO T4 OApr 3, 2007 · N463FE · Boeing 727225 · Fuselage Miscellaneous StructureSDR 07FDEA01247Structure · delaminatedRT WING NR 14 SPOILER T/E IS SPLIT REMOVED AND REINSTALLED NR 14 SPOILER FOR T/E REPAIR REF M/M 27-61-0001-4, M/M 27-61-001-5. SPOILER REPAIRED ON IDM WORK CARD ORDER NR 11841-6000-0004.Apr 2, 2007 · N463FE · Boeing 727225 · SpoilersSDR 07FDEA01246Skin · delaminatedRT WING NR 9 SPOILER UPPER TE SURFACE HAS DELAM REMOVED NR 9 SPOILER PANEL. SPOILER REPAIRED ON SHOP WO NR 11841-6000-0003 REF SRM 51-40-20. INSTALLED NR 9 SPOILER PANEL REF MM 27-62-001-4 STEP 3-5. ADJUSTED SPOILER REF MM 27-62-001-5 PG 1 STEP 2A-2F AND STApr 2, 2007 · N463FE · Boeing 727225 · SpoilersSDR 07FDEA01245Skin · misrepairedFOUND REPAIR AT LT WING NR 1 SLAT. FLUSH REPAIR IS 15" FROM OB END ON TOP SURFACE. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. FOUND REPAIR DID NOT MEET CRITERIA OF SRM 57-50-3 FIG 1. AFTApr 2, 2007 · N463FE · Boeing 727225 · Leading Edge DevicesSDR 07FDEA01244Skin · misrepairedFOUND EXTERNAL FUSELAGE REPAIR AT APPROX STA 1223, STR 25R. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. FOUND REPAIR DID NOT CONFORM TO SRM 53-30-3 FIG 3. REMOVED EXTERNAL DOUBLER FROM AApr 2, 2007 · N463FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR 07FDEA01243Skin · delaminatedRT WING NR 13 SPOILER T/E IS SPLIT NR 13 SPOILER REPAIRED ON WO NR 11841-6000-0005 REFERENCE SRM 51-40-20. INSTALLED NR 13 SPOILER REF MM 27-61-001-4 PG 2-3 STEP 5, TORQUE WRENCH AAR 20026 DATE 8-23-07. CTR BOLT 285 IN LB. OUTBD HINGE BOLT, 130 IN LB TORQUEApr 2, 2007 · N463FE · Boeing 727225 · SpoilersSDR 07FDEA01242Skin · delaminatedLT WING OTBD AILERON IS DELAMINATED AT THE OTBD T/E. LT OB AILERON WAS REPAIRED ON SHOP WO NR 11841-5000-0003 REFERENCE SRM 51-40-20. LT OB AILERON IS INSTALLED AND RIGGED ON SNRM NR N00554.Apr 2, 2007 · N463FE · Boeing 727225 · AileronsSDR 07FDEA01225Skin · crackedLEFT WING SMALL CRACK AND DENT IN WING TIP L/E ADJACENT TO O/B END. REMOVED AND REPALCED WING TIP SKIN PNL IAW SRM 51-30-2, P/N 65-16209-4. PAINTED SKIN IAW MM 51-20-151-7.Apr 1, 2007 · N461FE · Boeing 727225 · Wing, Plate/SkinSDR 07FDEA01224Skin · crackedLEFT WING L/E CRACKED ABOVE NR 3 SLAT O/B TRACK. REPAIRED CRACKED ON LEFT WING ABOVE NR 3 SLAT O/B TRACK IAW SRM 57-30-4 FIG 11.Apr 1, 2007 · N461FE · Boeing 727225 · Wing, Plate/SkinSDR 07FDEA01221Panel · delaminatedRT WING, UPPER SURFACE AT WBL 462, PNL, JUST O/B OF NR 14 SPOILER IS DELAMINATED. REMOVED PANEL AND SENT OUT FOR REPAIR. PANEL REPAIRED ON AAR WO NR 11841/6300/0003. REMOVED DAMAGE AND DELAMINATED SKIN, AND REPAIRED, REF SRM 51-40-20. INSTALLED PANEL REF Mar 31, 2007 · N463FE · Boeing 727225 · Wing, Plate/SkinSDR 07FDEA01220Plug · corrodedTHE SECOND WINDOW PLUG AFT OF THE LEFT AFT EMERGENCY ESCAPE HATCH HAS CORROSION UNDER THE SEAL AT THE FWD LOWER PLUG RETAINER REMOVED WINDOW PLUG, REF MM 56-20-000-4 PG 1. DRILLED HOLE IN THE WINDOW PLUG FOR JUMPER STRAP, REF EO NR 7-5620-7-4304. INSTALLED WMar 31, 2007 · N463FE · Boeing 727225 · Flight Compartment WindowsSDR 07FDEA01219Skin · gougedFWD LOWER CARGO DOOR, FWD LOWER CORNER OF SKIN WORN, GOUGED. INSTALLED REPAIR DOUBLER REF 52-00-3 PG 2, FIG 4, DETAIL F. RESTORED LEVELING, COMPOUND REF SOPM 20-60-04 PG 7.Mar 31, 2007 · N463FE · Boeing 727225 · Cargo/Baggage DoorsSDR 07FDEA01218Floorbeam · corrodedFLIGHT DECK FLOORBEAM HAS CORROSION ON TOP OF BEAM LOCATED AT BS 277, RBL 10.5. REMOVED CORROSION, ALL WORK FOR BLEND WAS ACCOMPLISHED ON FED EX EA NR 7-5310-107004.Mar 31, 2007 · N463FE · Boeing 727225 · Fuselage Main, Floor BeamSDR 07FDEA01217Battery Box · corrodedE/E COMPARTMENT BATTERY TRAY AFT EDGE IS CORRODED. REMOVED, FABRICATED AND ACP HEAT TREAT PROCESS FOR 2024-T4, CONDITION FOR TRAY. REF BAC DWG 69-21649 REV C AND BAC5602 REV (AF) 28 AUG 01 AND BAC 5946 REV (AA) 9 JUL 01. IDENTIFIED TRAY AS FX-69-21649-1. WMar 31, 2007 · N463FE · Boeing 727225 · Battery Box StructureSDR 07FDEA01216Battery Box · corrodedE/E COMPARTMENT BATTERY BOX CORRODED AT FOWARD RT AND LT CORNERS REMOVED CORROSION FROM BATTERY BOX. MATERIAL LOSS WAS OUT OF LIMITS, REF SRM 51-30-2 FIG. REPLACED WITH NEW BATTERY BOX REF MM 24-30-011-4.Mar 31, 2007 · N463FE · Boeing 727225 · Battery Box StructureSDR 07FDEA01207Support · crackedRT WING INBD TE LOWER SURFACE FWD INNER SUPPORT CLIP IS CRACKED AT ATTACH TO REAR SPAR FLANGE OFF PANEL 10" O/B OF O/B END OF MLG BEAM REMOVED DAMAGED CLIP, VERIFIED REPAIR MATERIAL AS 2024-T3-.040 REF DWG NR 65-21656, AND FABRICATED REPLACEMENT CLIP REF DWGMar 30, 2007 · N463FE · Boeing 727225 · Wing Miscellaneous StructureSDR 07FDEA01206Floor Support · crackedFWD CARGO PIT FLOOR SUPPORT AT SRA 717 ABOVE STR 27R IS CRACKED FABRICATED FLOOR SUPPORT REF DWG BAC 1517-1507 REV A. NDT REF BAC 5423, HEAT TREATED AND TESTED HARDNESS REF BAC 5602 AND BAC 5946 FEF TRACKING NR 2007-03-150. REMOVED DAMAGED SECTION OF CARGO FMar 30, 2007 · N463FE · Boeing 727225 · Fuselage Miscellaneous StructureSDR 07FDEA01210Door · wornRT IB FORE FLAP INBD UPPER HINGED LE DOOR HAS DEEP WEAR REMOVED AND REPLACED RT INBD FORE FLAP REF MM 27-51-001-4 PAGE 2. TQ WRNCH NR AAR 19624 DUE 8-19-07.Mar 30, 2007 · N463FE · Boeing 727225 · Trailing Edge FlapsSDR 07FDEA01209Panel · delaminatedVERTICAL STABILIZER PANEL 9511 IS DELAMINATED REMOVED DAMAGE AND REPAIRED PANEL, THEN APPLIED CONDUCTIVE COAT, PRIMED AND PAINTED REFERENCE SRM 51-40-09 PAGE 4, AND MM 51-21-121-7.Mar 30, 2007 · N463FE · Boeing 727225 · Vertical Stabilizer, Plate/SkinSDR 07FDEA01208Skin · delaminatedRT OTBD AILERON OTBD T/E UPPER AND LOWER SURFACE IS DELAMINATED FROM CORE. REMOVED AND REPLACED RT OTBD AILERON REF MM 27-10-031-2.Mar 30, 2007 · N463FE · Boeing 727225 · AileronsSDR 07FDEA01205Fairing · wornNR 1 ENGINE S/N 700479 TAIL PIPE FAIRING HAS GROOVE WORN INTO IT AT 3 O'CLOCK POSITION FROM 1" AFT OF FWD EDGE TO 18" AFT OF FWD EDGE. REPLACED DAMAGED ENG NR 1 I/B TAILPIPE FAIRING REF SRM 51-30-2 ITEM 9.Mar 30, 2007 · N463FE · Boeing 727225 · Engine Collector/Tailpipe/NozzleSDR 07FDEA01204Splice · corrodedLOWER AFT PIT FLOOR STRUCTURE FLOOR PANEL SPLICE STRAP AT STA 980 4" HAS CORROSION ON UNDERSIDE AT MANY NUTPLATES AND CRACKED AT RBL 8. MANUFACTURED STRAP PER BOEING DWG 65-57567. REMOVED AND REPLACED AFT PIT FLOOR SPLICE STRAP REF SRM 51-30-07.Mar 30, 2007 · N463FE · Boeing 727225 · Fuselage Main, Floor BeamSDR 07FDEA01203Angle · crackedLOWER AFT PIT LOWER LT SIDEWALL ATTACH CLIP IS CRACKED AT STA 950F ABOVE STR 26L. FABRICATED AND REPLACED BROKEN CLIP REF BOEING DRAWING 66-12821 AND SRM 51-30-2.Mar 30, 2007 · N463FE · Boeing 727225 · Fuselage Miscellaneous StructureSDR 07FDEA01202Skin · delaminatedNR 5 SLAT FENCE IS DELAMINATED ON LEADING EDGE REMOVED DAMAGE AND REPAIRED AREA REF SRM 51-40-09 PG 3-7. APPLIED CONDUCTIVE COATING REF MM 51-20-051-7. PRIMED AND PAINTED REPAIR REF MM 51-20-151-7.Mar 30, 2007 · N463FE · Boeing 727225 · Leading Edge DevicesSDR 07FDEA01201Cowling · crackedNR 3 ENGINE FIXED COWL AFT UPPER LATCH CUTOUT IS CRACKED AT AFT END NEW COWL ASSY RECEIVED AND REPLACED REF MM 71-10-031-4 AND REF WC 74C300-01.Mar 30, 2007 · N463FE · Boeing 727225 · Nacelle/Pylon, Main FrameSDR 07FDEA01200Skin · dentedLOWER FUSELAGE SKIN IS GOUGED/CREASED AT BS 294-347 STR S-21R, 6" DENT WAS DETERMINED TO BE OUT OF LIMITS. REMOVED DAMAGE, FABRICATED AND INSTALLED EXTERNAL DOUBLER REPAIR REF SRM 53-30-3 FIG 1.Mar 30, 2007 · N463FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR 07FDEA01199Skin · damagedLT WING LE, AT NR 4 SLAT OB HOOK CUTOUT CRACKED REMOVED DAMAGED AREA, REF SRM -30-4, NDT AREA AFTER BLEND OUT, NO DEFECTS NOTED REF B727NDT MANUAL PART 6. FABRICATED AND INSTALLED REPAIR REF SRM 57-30-4 AND SRM 51-30-2.Mar 30, 2007 · N463FE · Boeing 727225 · Leading Edge DevicesSDR 07FDEA01198Skin · dentedNLG CUTOUT FWD EDGE SKIN BENT/CREASED, REMOVED DAMAGE AREA. FABRICATED REPAIR DOUBLER AND INSTALLED REF SRM 53-30-3 FIG 1. THIS REPAIR IS A CATEGORY '"B" REPAIR. INSPECTION THRESHOLD IS 45,000 CYCLES REF SRM 53-30-3 FIG TABLE 3.Mar 30, 2007 · N463FE · Boeing 727225 · Fuselage Main, Plate/Skin
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