Boeing 727-227

Service difficulty reports · 5,082

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  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = '727227'
  ORDER BY difficulty_date DESC"

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SDR DHL2005782506Web · crackedSTA 1243 RT LOWER TORQ BOX WEB IS CRACKED. STOP DRILLED CRACK IAW B727 SRM 51-10-1. HFEC PER NDT PT 6 51-00-00 FIG 23 CRACK ENDS AT STOP DRILL. FABRICATED DOUBLER REPAIR USING 7075 T6 .032 PO NR 900573 DIM 4 3/4 INCH BY 2 1/2 INCH IAW B727 SRM 53-10-2 FIG 6Mar 8, 2005 · N782DH · Boeing 727227 · Fuselage Miscellaneous StructureSDR DHL2005781562Rib · crackedDURING A C-CHECK, RT WING NR 6 SLAT I/B RIB AT ACTUATOR ROD ATTACH POINT IS CRACKED. REMOVED DAMAGED RIB IAW B727 SRM 51-30-2, FABRICATED NEW RIB, MATERIAL USED 2024 T3, .040 PO 9002012 DIM15 X 5.5 INCH IAW B727 SRM 57-50-2 FIG 2 AND 51-20-1 FIG 7. ALODINE AMar 3, 2005 · N781DH · Boeing 727227 · Wing, Rib/BulkheadSDR DHL2005781563Rib · crackedDURING A C-CHECK, RT WING NR 6 SLAT I/B RIB AT ACTUATOR ROD ATTACH POINT IS CRACKED. REMOVED DAMAGED RIB IAW B727 SRM 51-30-2, FABRICATED NEW RIB, MATERIAL USED 2024 T3, .040 PO 9002012 DIM 15 BY 5.50 INCHES IAW B727 SRM 57-50-2 FIG 2 AND 51-20-1 FIG 7. ALODMar 3, 2005 · N781DH · Boeing 727227 · Leading Edge DevicesSDR 05FDEA00349Stringer Clip · misdrilledBONUS HOLES IN STRINGER CLIP AT BS 950A STR 7L. REPLACED PER SRM 51-30-2Mar 3, 2005 · N481FE · Boeing 727227 · Fuselage Main, Attach FittingsSDR 05FDEA00348Stringer Clip · misdrilledBONUS HOLES IN STRINGER CLIP AT BS 950C STR 7L. REPLACED PER SRM 51-30-2Mar 3, 2005 · N481FE · Boeing 727227 · Fuselage Main, Attach FittingsSDR 05FDEA00346Stringer Clip · misdrilledBONUS HOLES IN STRINGER CLIP AT BS 950F STR 7L. REPLACED PER SRM 51-30-2Mar 3, 2005 · N481FE · Boeing 727227 · Fuselage Main, Attach FittingsSDR 05FDEA00335Skin · gougedLT IB MID FLAP UPPER SURFACE IS GOUGED AT OB END 13 INCHES FROM LE. BLENDED GOUGE ON LT IB MIDFLAP OB END PER FEDEX EA 7-5710-86252Mar 2, 2005 · N481FE · Boeing 727227 · Trailing Edge FlapsSDR 05FDEA00337Stringer · tool damageTOOLING DAMAGE AT BS 1010 STRINGER 7L IN STRINGER CLIP AND STRINGER SPLICE. REPAIRED PER SRM 53-10-2 (DUPLICATE ENTRY TO TRACKING NR 05-0336)Mar 2, 2005 · N481FE · Boeing 727227 · Fuselage Main, Longeron/StringerSDR 05FDEA00336Stringer · tool damageTOOLING DAMAGE AT BS 1010 STRINGER 7L IN STRINGER CLIP AND STRINGER SPLICE. REPAIRED PER SRM 53-10-2.Mar 2, 2005 · N481FE · Boeing 727227 · Fuselage Main, Longeron/StringerSDR 05FDEA00334Stringer · corrodedCORROSION IN STRINGER 26R, AFT OF BS 1148, AFT CARGO BAY.Mar 2, 2005 · N481FE · Boeing 727227 · Fuselage Main, Longeron/StringerSDR 05FDEA00327Keelbeam · corrodedFWD CARGO BAY RT KEEL BEAM HAS CORROSION AT NUTPLATES FROM BS 720C PLUS 5 TO PLUS 9, RBL 5, WL 149. REMOVED CORROSION FROM RT KEEL BEAM, FOUND TO BE OUT OF LIMITS, REPAIRED IAW FED EX EA 7-5310-86203.Mar 2, 2005 · N496FE · Boeing 727227 · Fuselage Main, KeelSDR 05FDEA00326Panel · dentedRT HORIZ STAB NR 5 BALANCE BAY UPPER SKIN PANEL HAS A SHARP PROTRUSION ON THE OTBD END. THE PANEL HAS CREASE ON O/B END. THE SRM REPAIRS FOR THIS PANEL ARE FOR CRACKS AND NOT DAMAGE OF THIS SIZE. (APPROX 3 INCH BY 1 1/2 INCH). FED-EX DRAWING SR27-55-0004 AMar 2, 2005 · N496FE · Boeing 727227 · Vertical Stabilizer, Plate/SkinSDR XN0A1230Warning System · malfunctionedTAKEOFF WARNING HORN STEADY INSTEAD OF INTEMITTENT. CLEANED AND RESET, CONNECTOR, WARNING BOX OPS CHECK GOOD AT THIS TIME IAW 727-3100.Mar 1, 2005 · N79754 · Boeing 727227 · Central WarningSDR DHL2005781561Skin · delaminatedDURING A C-CHECK, NR 9 SPOILER HAS TWO SPOTS OF DELAMINATION ON UPPER SURFACE AT TRAILING EDGE AND PHENOLIC RUB STRIP AT BOTTOM TRAILING EDGE IS LOOSE. REMOVED NR 9 SPOILER FOR REPAIR IAW B727 MM. REMOVED PREVIOUS REPAIR AND CUT OUT DAMAGE AREA APROX 30.5 BY Feb 27, 2005 · N781DH · Boeing 727227 · SpoilersSDR DHL2005781560Clip · crackedDURING C-CHECK, VERT STAB FIN STA 157 AT STR 9 LT HAS 2 FRAME CLIPS CRACKED. REMOVED FRAME CLIP BS 157 STR 9 LT IAW B727 SRM 51-30-2. FABRICATED (2 EA) FRAME CLIP MATERIAL USED 7075T6 .050 PO NR 9001777 DIM .750 BY 2.50 BY 5 INCHES IAW B727 SRM 55-30-2 FIG 2Feb 24, 2005 · N781DH · Boeing 727227 · Vertical Stabilizer, Spar/RibSDR DHL2005781559Frame · crackedDURING C-CHECK, VERT STAB FIN STA 133 AT STR 9LT HAS 1 FRAME CLIP CRACKED. REMOVED FRAME CLIP AT VERT STAB FIN STA 133 AT STR 9 LT IAW B727 SRM 51-30-2. FABRICATED NEW CLIP MATERIAL USED 7075T6 .050 PO NR 9001777 DIM 7/8" BY 2.50 BY 5.50 IAW B727 SRM 55-30-2Feb 24, 2005 · N781DH · Boeing 727227 · Vertical Stabilizer, Spar/RibSDR DHL2005781558Frame · crackedDURING A C-CHECK, THE FOLLOWING DISCREPANCY WAS NOTED: VERT STAB FIN STA 133 AT STR 8 LT HAS 1 FRAME CLIP CRACKED. REMOVED FRAME CLIP AT VERT STAB FIN STA 133 AT STR 8 LT IAW B727 SRM 51-30-2. FABRICATED NEW CLIP MATERIAL USED 7075T6 .050 PO NR 9001777 DIM 7Feb 24, 2005 · N781DH · Boeing 727227 · Vertical Stabilizer, Spar/RibSDR DHL2005781557Frame · crackedDURING C-CHECK, VERT STAB FIN STA 55.8 STR 3 LT IS CRACKED AT FRAME ATTACH BOLT. REMOVED FRAME CLIP BS 55.8 STR 3 LT IAW B727 SRM 51-30-2. FABRICATED CLIP MATERIAL USED 7075-T6 .050 PO NR 9001777 DIM .750 INCH 2.5 INCH X 5 INCHES IAW B727 SRM 55-30-2 FIG 2 Feb 24, 2005 · N781DH · Boeing 727227 · Vertical Stabilizer, Spar/RibSDR XN0A1229Fire Warning · malfunctionedON TAKEOFF ROLL MAIN CARGO FIRE WARNING AND BELL CAME ON. PERFORMED FUNCTIONAL CHECK OF MAIN DECK CARGO SYS, SDU'S SYSTEM CHECKED NORMAL IAW SECURE A PLANE. INSPECTED MAIN CARGO DECK FOR DEFECTS, NONE FOUND.Feb 24, 2005 · N79754 · Boeing 727227 · Fire DetectionSDR DHL2005781504Pressure Panel · crackedDURING A C-CHECK; NLG W/W BAY UPPER RT INSIDE NOSE PRESSURE ACCESS PANEL CAVITY AREA ABOVE CABLE RUNS, LWR UNDERSIDE COCKPIT FLOOR, ATTACH ANGLE AT BS 230 AT LBL 10 ATTACH ANGLE HAS EDGE CRACKED, GOING TO BUCKTAIL FASTENER HOLE AND BEYOND (EXTENDING PASS HOLE)Feb 21, 2005 · N781DH · Boeing 727227 · Fuselage Main, BulkheadSDR DHL2005781506Web · crackedDURING A C-CHECK, LEFT MLG W/W 950 WEB CRACKED AT AFT DOOR STOP FITTING. CUT OUT DAMAGED AREA 3.25 X 7.25, AT LEFT W/W STA 950 WEB AFT DOOR STOP FITTING IAW B727 SRM 51-40-2 FIG 1. FABRICATED REPAIR DOUBLER FROM 2024-T3 .040 PO 9001634 DIM 7.75 X 4.25 AND FIFeb 20, 2005 · N781DH · Boeing 727227 · Fuselage Miscellaneous StructureSDR DHL2005781524Stringer · crackedDURING A "C" CHECK, STRINGER 30 AT STA 1175 CRACKED AND EXFOLIATED. REMOVED REINFORCEMENT ANGLE FOR ACCESS IAW B727 SRM 51-30-2 BS 1175 TO 1183 STR 30 EVALUATED STRINGER 30 AT BS 1175 TO 1183. NO CORROSION NOTED. EVALUATED REINFORCEMENT ANGLE FROM BS 1175 TFeb 18, 2005 · N781DH · Boeing 727227 · Fuselage Main, Longeron/StringerSDR DHL2005781556Frame · crackedDURING A C-CHECK, AFT PIT FRAME DENTED BS 1130 STR 26 RT. CUT OUT DAMAGED AREA FROM FRAME BS 1130 STR 26 RT IAW 727 SRM 53-10-1 FIG 1. FABRICATED DOUBLER FROM 7075-T6 .063 PO NR 9001660 8.5 X 3 INCHES & STRIP FROM 7075T6 .063 PO NR 9001660 8.5 X 1 INCHES ANDFeb 17, 2005 · N781DH · Boeing 727227 · Fuselage Main, FrameSDR DHL2005781513Skin · crackedDURING A "C" CHECK, CRACKED PANEL SURROUNDING NR 7 SLAT I/B UPSTOP BOLT STOP PAD. REMOVED CRACKED PANEL IAW B727 SRM 51-30-2. FABRICATED PANEL SURROUNDING NR 7 SLAT I/B UPSTOP BOLT STOP PAD MAT USED 2024T3 .050 PO NR 9001684 DIM 18 3/4 INCH BY 8 1/4 INCH IAWFeb 17, 2005 · N781DH · Boeing 727227 · Leading Edge DevicesSDR DHL2005781565Skin · damagedDURING A C-CHECK, ACCOMPLISH IDENTIFICATION OF EXISTING REPAIR ON UPPER RUDDER RT SKIN AT STA 156 PER ASTAR J/C FCD500001-010-B. DISCONNECTED UPPER RUDDER ACTUATOR ROD END THROUGH BOLT FOR S/M ACCESS IAW B727 MM 27-20-14. REMOVED PREVIOUS REPAIR NOT COMPLIANFeb 16, 2005 · N781DH · Boeing 727227 · Rudder, Plate/SkinSDR DHL2005781555Frame · crackedDURING A C-CHECK, VERT STAB FIN STA 133 STR 9 LT IS CRACKED AT FRAME ATTACH BOLT. REMOVED FASTENERS FOR ACCESS, CUT-OUT DAMAGED DIM 4.5 X 3 INCHES STIFFENER AND REMOVED FILLER IAW B727 SRM 55-30-4 FIG 1. FABRICATED STIFFENER REPAIR. INSTALLED STIFFENER REPAFeb 16, 2005 · N781DH · Boeing 727227 · Vertical Stabilizer, Spar/RibSDR DHL2005781554Frame · crackedDURING A C-CHECK, VERT STAB FIN STA 133 STR S-8LT IS CRACKED AT FRAME ATTACH BOLT. REMOVED FASTENERS FOR ACCESS, CUT OUT DAMAGED DIM 4.50 X 3 INCHES STIFFENER AND REMOVED FILLER IAW B727 SRM 55-30-4 FIG 1. FABRICATED STIFFENER REPAIR. INSTALLED STIFFENER REFeb 16, 2005 · N781DH · Boeing 727227 · Vertical Stabilizer, Spar/RibSDR DHL2005781553Frame · crackedDURING A C-CHECK, VERT STAB FIN STA 133 STR 7 LT IS CRACKED AT FRAME ATTACH BOLT. REMOVED FASTENERS FOR ACCESS, CUT-OUT DAMAGED STIFFENER IAW B727 SRM 55-30-4 FIG 1 (4 X 5 INCHES). FABRICATED REPAIR STIFFENER. INSTALLED REPAIR STIFFENER IAW B727 SRM 55-30-4Feb 16, 2005 · N781DH · Boeing 727227 · Vertical Stabilizer, Spar/RibSDR DHL2005781551Frame · crackedDURING A C-CHECK, VERT STAB AT FIN STA 157 STR 9 LT IS CRACKED AT FRAME ATTACH BOLT. REMOVED FASTENERS FOR ACCESS, CUT OUT DAMAGED 6 X 3 INCHES STIFFENER & REMOVED FILLER IAW B727 SRM 55-30-4 FIG 1, FABRICATED STIFFENER REPAIR PN BAC1517-1367, PO NR 501953 DIFeb 16, 2005 · N781DH · Boeing 727227 · Vertical Stabilizer, Spar/RibSDR DHL2005781550Frame · crackedDURING A "C" CHECK, FOLLOWING DISCREPANCIES WERE NOTED;VERT STAB FIN STA 180 STR 6R IS CRACKED AT FRAME ATTACH BOLT. REMOVED PANEL NR 9504 FOR ACCESS TPM FOR SHEET METAL REPAIR IAW B727 SRM 51-30-2. REMOVED FASTENERS FOR ACCESS, CUT OUT DAMAGED STIFFENER ANDFeb 16, 2005 · N781DH · Boeing 727227 · Vertical Stabilizer, Spar/RibSDR DHL2005781549Stiffener · crackedDURING A C-CHECK,THE FOLLOWING DISCREPANCIES WERE NOTED; VERT STA FIN STA 180, STR 5-8 LT IS CRACKED AT FRAME ATTACH BOLT. REMOVED FASTENERS FOR ACCESS, CUT OUT DAMAGE, DIM 5 X 3 STIFFENER AND REMOVED FILLER IAW B 727 SRM 55-30-4 FIG 1. FABRICATED STIFFENEFeb 16, 2005 · N781DH · Boeing 727227 · Vertical StabilizerSDR DHL2005781548Stiffener · crackedDURING A C-CHECK, VERT STAB FIN STA 180, STR 5-8 RT IS CRACKED AT FRAME ATTACH BOLT. REMOVED FASTENERS FOR ACCESS, CUT OUT DAMAGED STIFFENERS AND REMOVED FILLER IAW B727 SRM 55-30-4 FIG 1 (5 X 3). FABRICATED STIFFENER REPAIR P/N BAC1517-1367 PO 501953 DIM 5 Feb 16, 2005 · N781DH · Boeing 727227 · Vertical StabilizerSDR DHL2005781547Skin · crackedDURING A C-CHECK, VERT STAB FIN STA 194 LOWER RUDDER LT SIDE UPPER T/E AT END IS CRACKED. REMOVED CRACKED BRACKET, FABRICATED NEW BRACKET FROM 2024 T3 .025 PO 9001310 DIM 3.5 X 3.5 INCH. TREATED, PRIMED AND INSTALLED BRACKET IAW B727 SRM 51-30-2, 55-30-2 FIFeb 16, 2005 · N781DH · Boeing 727227 · Rudder, Plate/SkinSDR DHL2005781546Frame · crackedDURING A C-CHECK, RIGHT O/B MID FLAP LWR INTERNAL FRAME CRACKED AT WS 520. REMOVED ANGLE SUPPORT INTERNAL FRAME IAW B727 SRM 51-30-2. REMOVED RIGHT O/B MIDFLAP O/B FLAP ACTUATING MECHANISM CABLE (AFA) TO FACILITATE S/M REPAIR PSC B727 M/M 27-51-71. REMOVED Feb 16, 2005 · N781DH · Boeing 727227 · Trailing Edge FlapsSDR DHL2005781503Skin · gougedDURING A C-CHECK, ACCOMPLISH INDENTIFICATION OF EXISTING REPAIR ON LT WING NR 4 SLAT SKIN, WS 436, PER ASTAR J/C FCD 500001-018-B. REMOVED PREVIOUS REPAIR WITH NON-COMPLIANT PER SRM AT LT WING NR 4 SLAT SKIN WS 434 IAW B727 SRM 51-30-2. FABRICATED NEW REPAIRFeb 16, 2005 · N781DH · Boeing 727227 · Leading Edge DevicesSDR DHL2005781545Skin · corrodedDURING A C-CHECK, VERT STAB FIN STA 204 RT SIDE UPPER RUDDER SKIN FWD HAS SURFACE CORROSION. REMOVED CORROSION FOUND TO BE BEYOND LIMITS, REMOVED EXISTING RIVETS, CUT OUT DAMAGED AREA DIM 3.5 X 2.25 INCH, FABRICATED REPAIR DOUBLER FROM 2024 T3 .032 PO 9001634Feb 15, 2005 · N781DH · Boeing 727227 · Rudder, Plate/SkinSDR DHL2005781543Skin · dentedDURING A C-CHECK, DENT AT SKIN OF AFT AIRSTAIR CUTOUT AFT OF STA 1323 BELOW STR 26R. REMOVED FASTENERS AND CUT OUT DAMAGED ARE DIM 2.875 X 1.375 INCH IAW B727 SRM 53-30-3 FIG 3. FABRICATED FILLER FROM 2024T3 .050 PO 9001873 DIM 2.875 X 1.375 INCH AND DOUBLERFeb 15, 2005 · N781DH · Boeing 727227 · Fuselage Main, Plate/SkinSDR DHL2005781542Rib · gougedDURING A C-CHECK, RT WING L/E CAVITY RIB GOUGED WSTA 734. REMOVED DAMAGED ANGLE IAW B727 SRM 51-30-2. FABRICATED ANGLE 20 24 T3 .040 9001634 (16 X 1.875 INCH) IAW B727 SRM 57-20-2 FIG 1 AND 51-20-1. TREATED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED NEW ANFeb 15, 2005 · N781DH · Boeing 727227 · Wing, Rib/BulkheadSDR DHL2005781541Frame · dentedDURING A C-CHECK, RIGHT FUSE AFT CARGO COMPT DOOR BOTH FWD & AFT LWR DOOR FRAME CORNER SECTIONS ARE FLAT SPOTTED & DENTED. REMOVED AND REPLACED AT RIGHT FUSE AFT CARGO COMPARTMENT DOOR BOTH FWD AND AFT LWR DOOR FRAME CORNER IAW 727 SRM 51-30-2 PO 501944, P/N Feb 15, 2005 · N781DH · Boeing 727227 · Cargo/Baggage DoorsSDR DHL2005781540Door Frame · gougedDURING A C-CHECK, FWD CARGO COMPT C-1 DOOR LWR FWD CORNER DOOR FRAME IS GOUGED, PUNCTURE & FLAT SPOTTED. REMOVED AND REPLACED A/C DOOR LWR FWD CORNER DOOR FRAME PO4496403, P/N 65-57146-4 IAW B727 SRM 51-30-2.Feb 15, 2005 · N781DH · Boeing 727227 · Cargo/Baggage DoorsSDR DHL2005781539Skin · damagedDURING A C-CHECK, SEVERAL DENTS ON SKIN OF AFT AIRSTAIR STA 1263. REMOVED FASTENERS ON SKIN OF AFT AIRSTAIR STA 1263 IAW B727 SRM 51-30-2. CUT OUT DAMAGE SKIN DIM 42 X 5 INCH IAW B727 SRM 52-10-2 FIG 4. FABRICATED SKIN REPAIR MAT USED 2024T3 .040 PO 9001765Feb 15, 2005 · N781DH · Boeing 727227 · Fuselage Main, Plate/SkinSDR DHL2005781538Skin · gougedDURING A C-CHECK, LT WING I/B FORE FLAP GOUGED AT O/B LEADING EDGE. REMOVED PREVIOUS REPAIR IAW B727 SRM 51-30-2. FAB DOUBLER FORM 2029-T3 .063 PO 9001634 BY 4.95 X 3.1 IAW B727 SRM 57-50-4 FIG 1. TREAT AND PRIME DOUBLER AREA IAW B727 SRM 51-10-2. INSTALL Feb 15, 2005 · N781DH · Boeing 727227 · Trailing Edge FlapsSDR DHL2005781528Torque Box · lightning strikeDURING A C-CHECK, PREVIOUS REPAIR ON LOWER TORQUE BOX LIGHTENING HOLE IMPROPERLY DONE R/SIDE AT FWD STA 1243. REMOVED PREVIOUS REPAIR ON LOWER TORQUE BOX LIGHTENING HOLE R/SIDE AT FWD STA 1243 IAW B727 SRM B727 SRM 51-30-2. STOP DRILL CRACK 250 TERIMINATED AFeb 15, 2005 · N781DH · Boeing 727227 · Fuselage Main, StructureSDR DHL2005781527Frame · dentedDURING A "C" CHECK, FRAME DENTED AT S25L BS950F. REMOVED FASTENER FOR ACCESS AT STA S25L BS950F IAW B727 SRM 51-30-2. CUT OUT DAMAGE AREA DIM 1.5 INCH BY 1 INCH IAW B727 SRM 51-40-3 FIG1. FABRICATED FRAME REPAIR MAT USED 7075T6 .071 PO NR 900573 DIM 9 3/4 IFeb 15, 2005 · N781DH · Boeing 727227 · Fuselage Main, FrameSDR DHL2005781526Frame · dentedDURING A "C" CHECK AT FLIGHTSTAR AIRCRAFT SERVICES IN JACKSONVILLE FLORIDA, THE FOLLOWING DISCREPANCY WAS NOTED; FRAME DENTED ABOVE S25R BS1050. REMOVED FASTENERS FOR ACCESS AT S25R BS 1050 IAW B727 SRM 51-30-2. CUT OUT DAMAGED AREA DIM 1 1/2 BY 1 INCH IAW BFeb 15, 2005 · N781DH · Boeing 727227 · Fuselage Main, FrameSDR DHL2005781512Skin · gougedDURING A"C" CHECK, LEFT O/B FOREFLAP I/B UPPER L/E GOUGED. REMOVED PREV REPAIR LEFT O/B FOREFLAP I/B UPPER LT IAW B727 SRM 51-30-2. FABRICATE DOUBLER METAL IS 2024-T3 .063 5.0 BY 4.75 PO 9001634 IAW B727 SRM 57-50-2 FIG 4 57-50-4M FIG 1. TREAT PRIME AREA DOFeb 15, 2005 · N781DH · Boeing 727227 · Trailing Edge FlapsSDR DHL2005781511Skin · gougedDURING A "C" CHECK, LT WING INBD FOREFLAP GOUGED ABOVE NR 3 FLAP CARRIAGE (MARKED). REMOVED PREV REPAIR ON L/WING I/B FOREFLAP IAW B727 SRM 51-30-2. FABRICATED REPAIR DOUBLER FROM 2024-T3 .063 IS 8.2 BY 6.4 PO 9001634 IAW B727 SRM 57-50-4 FIG 1 57-50-2 FIG 3Feb 15, 2005 · N781DH · Boeing 727227 · Trailing Edge FlapsSDR DHL2005781508Torque Box · crackedDURING A "C" CHECK, CRACK AT LIGHNING HOLE TORQUE BOX L/SIDE AFT OF STA 1323. REMOVED FASTENERS AT LIGHTENING HOLE LOWER TORQUE BOX L/SIDE AFT OF STA 1323 IAW B727 SRM 51-30-2. STOP DRILL CRACK .250 TERMINATED AT END OF CRACK IAW B727 SRM 51-10-1. FABRICATFeb 15, 2005 · N781DH · Boeing 727227 · Fuselage Miscellaneous StructureSDR DHL2005781507Torque Box · crackedDURING A "C" CHECK, CRACK AT LIGHTENING HOLE LOWER TORQUE BOX L/SIDE AFT OF STA 1223 (MARKED). STOP DRILL CRACK AT LIGHTENING HOLE LOWER TORQUE BOX LT SIDE AFT OF STA 1223, .250 TERMINATED AT END OF CRACK IAW B727 SRM 51-10-1 ACCOMPLISHED 727 HFEC 51-00-00 FFeb 15, 2005 · N781DH · Boeing 727227 · Fuselage Miscellaneous StructureSDR DHL2005781544Skin · delaminatedDURING A C-CHECK, RT WING I/B MID FLAP O/B END, TRAILING EDGE IS DELAMINATED WBL 2400. REMOVED RT WING I/B MID FLAP O/B FAIRING. CUT OUT DELAM UPPER SURFACE SKIN AREA AFT APPROX 8 X 4.25 INCH. FABRICATED ONE SKIN REPLACEMENT APPROX 8 X 4.25 INCH & ONE SPLICFeb 14, 2005 · N781DH · Boeing 727227 · Trailing Edge Flaps
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