Boeing 727-227

Service difficulty reports · 5,082

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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 = '727227'
  ORDER BY difficulty_date DESC"

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SDR DHL2007784520Rib · crackedRT WING STA 233.5, NR 5 SLAT INBD ACTUATOR ATTACH RIB CRACKED. REMOVED 2 DAMAGED RIBS IAW B727 SRM 51-30-5. FABRICATED NEW RIB SUPPORTS FROM 7075T6, .071, 12 BY 2.50 IAW B727 SRM 57-50-2, FIG 2 AND 51-20-1. TREATED, PRIMED AND INSTALLED RIB SUPPORTS IAW B72Jul 8, 2007 · N784DH · Boeing 727227 · Leading Edge DevicesSDR DHL2007784514Skin · burnedEXTERNAL FUSELAGE BS 660 AT STR 7R HAS A LIGHTNING BURN. BLENDED OUT AREA OF LIGHTNING STRIKE IAW B727 SRM 53-30-3, FIG 20. MATERIAL LOSS OVER 30 PERCENT AND LIGHTNING STRIKE STILL PRESENT AND OUT OF LIMITS IAW B727 SRM 53-30-1. CUT OUT DAMAGED AREA DIM 4.5Jul 8, 2007 · N784DH · Boeing 727227 · Fuselage Main, Plate/SkinSDR DHL2007784513Skin · scratchedEXTERNAL FUSELAGE BS 475 AT STR 8R HAS A LIGHTNING BURN ON A FASTENER. BLENDED OUT AREA OF LIGHTNING STRIKE IAW B727 SRM 53-30-3, FIG 20. MATERIAL LOSS OVER 30 PERCENT AND LIGHTNING STRIKE STILL PRESENT AND OUT OF LIMITS IAW B727 SRM 53-30-1. CUT OUT DAMAGEJul 8, 2007 · N784DH · Boeing 727227 · Fuselage Main, Plate/SkinSDR DHL2007784512Skin · damagedEXTERNAL FUSELAGE BS 520 AT STR 8R HAS A LIGHTNING BURN. BLENDED OUT AREA OF LIGHTNING STRIKE IAW B727 SRM 53-30-3, FIG 20. MATERIAL LOSS OVER 30 PERCENT AND LIGHTNING STRIKE STILL PRESENT AND OUT OF LIMITS IAW B727 SRM 53-30-1. CUT OUT DAMAGED AREA DIM. 4 Jul 8, 2007 · N784DH · Boeing 727227 · Fuselage Main, Plate/SkinSDR DHL2007784511Skin · delaminatedRT INBD MID FLAP, OUTBD T/E DELAMINATED UPPER AND LOWER SURFACE, RWBL 239 TO 243.93. REMOVED DAMAGED AREA 3.5 BY 3.6, CLEANED AND PREPPED AREA TO BE REPAIRED IAW B727 SRM 51-40-20, PARA 7, FIG 3. FABRICATED FILLER 3.5 BY 3.6 AND DOUBLER 6.5 BY 5.1 FROM .012,Jul 8, 2007 · N784DH · Boeing 727227 · Trailing Edge FlapsSDR DHL2007784507Skin · crackedLT INBD AFT FLAP LE CRACKED AT NR 2 TRACK CUTOUT PREVIOUS DOUBLER, LWBL 60. REMOVED PREVIOUS REPAIR DOUBLER IAW B727 SRM 51-10-2, 51-30-2. HFEC IAW B727 NDTM PT.6 51-00-00, FIG.23, NO CRACKS INDICATED. FABRICATED REPAIR DOUBLER, MATERIAL USED 7075T6, 050, 3Jul 8, 2007 · N784DH · Boeing 727227 · Trailing Edge FlapsSDR DHL2007784503Web · crackedBS 1243, WL 196, RBL 21, RT TORQUE BOX UPPER HOLE CRACKED AT 12 O`CLOCK POSITION. CUT OUT DAMAGED AREA DIM .25 BY .25 IAW B727 SRM 51-40-2, FIG 1. FABRICATED DOUBLER REPAIR, MATERIAL USED 7075T6, 040, 3.8 BY 3 IAW B727 SRM 51-40-2, FIG 1 AND 53-10-2, FIG 6. Jul 8, 2007 · N784DH · Boeing 727227 · Fuselage Miscellaneous StructureSDR DHL2007784502Skin · crackedLT INBD AFT FLAP LE CRACKED AT NR 3 TRACK CUTOUT, LWBL 112. STOP DRILLED CRACK AT LT INBD AFT FLAP AT NR 3 TRACK CUTOUT, LWBL 112 IAW B727 SRM 57-50-4, FIG 1. HFEC VERIFIED CRACK STOPPED IAW B727 NDTM 51-00-00 PT 6, FIG 23. FABRICATED REPAIR DOUBLER, MATERIJul 8, 2007 · N784DH · Boeing 727227 · Trailing Edge FlapsSDR DHL2007784501Skin · gougedFUSELAGE SKIN GOUGED AT BS 720 PLUS 15, STR 19R. REMOVED GOUGED FILLER AT FUSELAGE SKIN AT PREVIOUS REPAIR. FILLER DIM. 5.5 BY 2.75 IAW B727 SRM 53-30-3, FIG 14. FABRICATED NEW FILLER, MATERIAL USED 2024T3, 063, 5.5 BY 2.75 IAW B727 SRM 53-30-3, FIG 14 ANDJul 8, 2007 · N784DH · Boeing 727227 · Fuselage Main, Plate/SkinSDR DHL2007784521Nose Cowl · crackedNR 3 ENGINE NOSE COWL INTERNAL TAI DUCT SUPPORT BRACKET BROKEN AT APPROX 8 O`CLOCK POSITION, NAC STA 77.5, NAC LBL 28, NAC WL 180. CUT ACCESS HOLE IN NOSE COWL AT 9 O`CLOCK POSITION TO FOM 6 IN DIA IAW B727 SRM 54-30-3, FIG 3. REMOVED BROKEN SUPPORT BRACKET Jul 7, 2007 · N784DH · Boeing 727227 · Nacelle/Pylon, Main FrameSDR 07FDEA02395Stringer · corrodedAFT PIT STRINGER 27R CORRODED FROM STA 1030-1060, BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS. REMOVED SHEAR TIE AND DAMAGED SECTION OF STRINGER. FABRICATED STRINGER REPAIR PARTS AND DRILLED TO FIT. TREATED AND PRIMED REPAIR PARTS. INSTALLED STRINGER Jul 7, 2007 · N481FE · Boeing 727227 · Fuselage Main, Longeron/StringerSDR 07FDEA02394Shear Tie · corrodedAFT PIT SHEAR TIE CORRODED STA 950F BETWEEN STR 27 R-28R RBL 17 - 22 REMOVED CORROSION AT STA 950F, STR 27-28R, RBL 17-22, IAW SRM 53-10-1 PG 2, NDT FOR MATERIAL LOSS, ORIGINAL THICKNESS .063". REMAINING THICKNESS IS .058" . WITHIN 10% LIMIT IAW SRM 53-1Jul 7, 2007 · N481FE · Boeing 727227 · Fuselage Internal Mounting StructureSDR 07FDEA02393Skin · corrodedFWD CARGO BAY INNER SKIN HAS CORROSION, BS 720C TO 720C 6 ", LBL 205" TO 5" WL 148.5. CUT OUT DAMAGE SKIN AT BS 720C TO 726C IAW B727 SRM 53-30-3.Jul 7, 2007 · N481FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR DHL2007784527Frame Splice · crackedMAIN CABIN FRAME BS 783.95, LBL 70, WL 204 IS CRACKED LWR END OF WEB AREA, CRACK ABOUT 1.5 NDT FINDING. REMOVED FASTENERS AT MAIN CABIN FRAME AT LWR END IAW B727 SRM 51-30-2. STOP DRILLED CRACK .250 IAW B727 SRM 51-10-1. HFEC VERIFIED STOP DRILL IAW B727 NDJul 6, 2007 · N784DH · Boeing 727227 · Fuselage Main, FrameSDR 07FDEA02380Skin · gougedAFT FUSELAGE EXT SKIN BS 1208 STR S-23R SKIN IS GOUGED. INSTALLED REPAIR ON EXT SKIN, AFT FUSELAGE STA 1208 STR 23R REF B727 SRM 53-30-3, PG 6 FIG 1.Jul 6, 2007 · N481FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR 07FDEA02379Liner · crackedNR 1 ENGINE HUSH KIT INNER LINER DISBONDED AND CRACKED AT 9 O'CLOCK POS. VERIFIED MATERIAL (INCONEL) REF. 78 -38-41 PREP FOR WELD REF 78-38-41, WELD WITH AMS 5837, A29984 INSPECT REF 78-38-41.Jul 6, 2007 · N481FE · Boeing 727227 · Engine Collector/Tailpipe/NozzleSDR DHLA200700034Warning System · inoperativeWITH FORWARD ENTRY DOOR OPEN, FORWARD ENTRY DOOR LIGHT IS NOT ILLUMINATED.Jul 5, 2007 · N783DH · Boeing 727227 · Door Warning SystemSDR 07FDEA02374Seal Depressor · crackedLT WING TE PNL 8155 SEAL DEPRESSOR IS FRETTED, CRACKED ALONG INBD EDGE. REPLACED SEAL DEPRESSOR IAW SRM 51-30-2.Jul 5, 2007 · N481FE · Boeing 727227 · Wing Miscellaneous StructureSDR 07FDEA02373Skate Angle · crackedRT WING AT NR 6 FLAP TRACK FWD FAIRING, I/B SKATE ANGLE IS CRACKED. REMOVED DAMAGE, FABRICATED NEW 2 REPAIR ANGLE AND INSTALLED 2 REF. REPAIR ANGLES, REF SRM 51-40-3 PG 1-6.Jul 5, 2007 · N481FE · Boeing 727227 · Wing Miscellaneous StructureSDR 07FDEA02372Rib · crackedVERTICAL STABLIZER RIB NUMBER 2 LT OTBD CHORD CRACKED AT STRINGER 7. REMOVED DAMAGE, FABRICATED REPAIR PARTS, SENT TO HEAT TREAT, TRACKING NR 2007-06-203, DRILLED, TREATED, AND PRIMED REPAIR PARTS. INSTALLED REPAIR PARTS REF SRM 55-30-5 FIG 1.Jul 5, 2007 · N481FE · Boeing 727227 · Vertical Stabilizer, Spar/RibSDR 07FDEA02355Flap · delaminatedRT WING, I/B FLAPS, AFT FLAP O/B END T/E IS DELAMINATED. REMOVED, REPAIRED, AND REINSTALLED RT WING I/B FLAP, AFT FLAP ASSY REF'S MM 27-51-002-4 AND SRM 51-40-20. THIS IS CLASSIFIED AS A MAJOR REPAIR. PLAY AND POSITION CHECK TO BE PERFORMED ON ROUTINE CARD Jul 2, 2007 · N481FE · Boeing 727227 · Trailing Edge FlapsSDR 07FDEA02357Wedge · debondedLT I/B MID FLAP AFT WEDGE HAS DISBONDED JUST O/B OF THE AFT FLAP TRACK. REMOVED LT I/B AFT FLAP REF M/M 27-51-001-4 REPAIRED MID FLAP REF SRM 51-40-21 PARA 4D AND 4E AND SRM 51-40-20 PARA 7, 14, 15, 18, 20, 21, 22 LT I/B AFT FLAP ASSY INSTALLED ON SNRM N00328.Jul 2, 2007 · N481FE · Boeing 727227 · Trailing Edge FlapsSDR 07FDEA02356Flap · delaminatedRT WING, I/B FLAPS, AFT FLAP O/B END T/E IS DELAMINATED. REMOVED, REPAIRED, AND REINSTALLED RT WING I/B FLAP, AFT FLAP ASSY REF'S MM 27-51-002-4 AND SRM 51-40-20 THIS IS CLASSIFIED AS A MAJOR REPAIR. PLAY AND POSITION CHECK TO BE PERFORMED ON ROUTINE CARD W/Jul 2, 2007 · N481FE · Boeing 727227 · Trailing Edge FlapsSDR 07FDEA02354Rib · crackedRT WING INBD L/E FORMER WEB CRACKED AT AFT UPPER AREA INBD SIDE. FORMER LOCATED AT O/B END OF NR 6 FLAP. FABRICATED REPAIR DOUBLER, ON RT WING INBD L/E FORMED WEB TREATED AND PRIMED, AND INSTALLED IAW B727 SRM 51-40-2 FIG 1, 51-10-2, 51-30-2, CLASSIFIED MIJul 2, 2007 · N481FE · Boeing 727227 · Wing, Rib/BulkheadSDR 07FDEA02346Channel · crackedLEFT WING FIXED TRAILING PANEL SUPPORT BRACKETS, ARE CRACKED AT SUPPORT ROD. SUPPORT ROD ATTACHS TO, TWO PANELS LOCATED JUST INBD OF THE NR 2 SPOILER. REMOVED, LOCATED, DRILLED AND INSTALLED Z BRACKET LT WING T/E PANEL SUPPORT BRACKET INBD OF NR 2 SPOILER PEJun 30, 2007 · N481FE · Boeing 727227 · Wing Miscellaneous StructureSDR 07FDEA02314Skin · delaminatedLT WING, PNL JUST AFT OF NR 2 KRUGER FLAP IS DELAMED AROUND VENT. REPAIRED DELAMED ON LT WING PNL JUST AFT OF NR 2 KRUGER FLAP REF SRM 51-40-9 PG 9 PARA 7.Jun 28, 2007 · N481FE · Boeing 727227 · Leading Edge DevicesSDR 07FDEA02303Stringer · corrodedFWD CARGO BAY BS 720+10 TO 720+14, S27R FWD END OF ORIGINAL CUT STR UNDER SPLICE IS CORRODED. I/B AND OB SIDE REMOVED S27R SPLICE AT BS 720. REMOVED DAMAGE SECTION STR-27R, AFT OF SPLICE. REMOVED DAMAGE SKIN, FABRICATED NEW STRINGER SECTION SPLICE, TREATED Jun 28, 2007 · N481FE · Boeing 727227 · Fuselage Main, Longeron/StringerSDR 07FDEA02302Skin · damagedFWD CARGO BAY BS 720 13 STR S-23R FUSELAGE SKIN FASTENER HOLE DAMAGED. FABRICATED FILLER AND DOUBLER FOR FWD CARGO BAY BS 720 13" STR S-27R FUSELAGE SKIN REF SRM 53-30-03, 53-10-03, 53-30-02, SEALANT 51-20-04.Jun 28, 2007 · N481FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR 07FDEA02301Stringer · crackedFWD CARGO PIT STRINGER IS CRACKED AT RIVET IN LOWER CHANNEL BS 72 10, STR 27R. REMOVED STRINGER SPLICE AT BS 720 10". FABRICATED, LOCATED AND DRILLED AND DEBURRED NEW STRINGER SPLICE USING BAC1498-132 MATERIAL. TREATED AND PRIMED AND INSTALLED STRINGER AT BJun 28, 2007 · N481FE · Boeing 727227 · Fuselage Main, Longeron/StringerSDR 07FDEA02264Bulkhead · crackedRT LOWER FUSELAGE AFT OF RT WHEEL WELL, FUSELAGE PANEL NR 3622 IS CRACKED AT INNER I/B AREA. REMOVED CRACK ON UNDER SIDE OF PANEL NR 3622 REF SRM 51-40-9 PARAGRAPHS 4A AND4E.Jun 23, 2007 · N481FE · Boeing 727227 · Fuselage Main, BulkheadSDR 07FDEA02255Actuator · failedUPON LOWERING LANDING GEAR HANDLE, NOSE GEAR DID NOT COME DOWN INITIALLY WITH RED NOSE GEAR LIGHT AND NO NOSE GEAR DOOR LIGHT ON FE'S ANNUNCIATOR PANEL. AFTER APPROX 20 SECONDS, COULD HEAR NOSE GEAR DOORS OPEN AND NOSE GEAR COME DOWN AND LOCKED. LANDING GEARJun 22, 2007 · N479FE · Boeing 727227 · Landing Gear ActuatorSDR DHL2007783528Shear Tie · corrodedAFT CARGO COMPARTMENT, CORROSION ON SHEAR TIE BS 1166 BETWEEN STR 29R AND 30R. CUT OUT DAMAGED SHEAR TIE 4 BY 2. FABRICATED AND INSTALLED SHEAR TIE IAW B727 SRM 53-10-4, FIG 5. MATERIAL USED 7075T6, .090, 4.7 BY 5.5 AND 5.5’ BY 2. TREATED, PRIMED PARTS ANDJun 21, 2007 · N783DH · Boeing 727227 · Fuselage Internal Mounting StructureSDR DHL2007783525Channel · crackedCRACK AT VHF NR 3 ANT CHANNEL LT SIDE BETWEEN STR 30R AND 29R STA 1040. REMOVED VHF NR 3 ANTENNA IAW B727 51-30-2. REMOVED ANTENNA CHANNEL IAW B727 SRM 51-30-2. FABRICATED NEW CHANNEL FROM MATERIAL 7075-T6, .050, DIM 20” BY 7.5 IAW B727 SRM 51-20-1 AND EC-0Jun 21, 2007 · N783DH · Boeing 727227 · Fuselage Miscellaneous StructureSDR DHL2007783524Intercostal · corrodedASTAR N/R 062541: FWD CARGO COMPARTMENT STA 580 THRU 600, INTERCOSTAL AT STR 29L HAS CORROSION ON LWR INBD SIDE. REMOVED INTERCOSTAL AT SRT 29L BETWEEN STA 580-600 IAW B727 SRM 53-10-1. FABRICATED NEW INTERCOSTAL FROM 7075-T6, .032, DIM 19.5 BY 19.5 IAW B727 Jun 21, 2007 · N783DH · Boeing 727227 · Fuselage Miscellaneous StructureSDR 07FDEA02246Indicator · failedDURING CLIMB-OUT STBY ATT IND 5 MORE NOSE UP THAN CAT/FO ADI'S SHORTLY THERE AFTER STBY ATT IND RAPID PRECESSION TO -25 WITH INAPPRECIATE BANK INDICATIONS. FOR TROUBLESHOOTING RECAGED TWICE RESET BREAKER. PROBLEM REOCCURRED. REPLACED STANDBY ARTIFICIAL HORIJun 21, 2007 · N491FE · Boeing 727227 · Turn and Bank/Rate of Turn IndicatorSDR DHL2007783522Support Angle · crackedVERTICAL STAB INTERNAL WEB LT UPPER ANGLE IS CRACKED STA 1323, SHORT WEB ANGLE W/L 259. REMOVED DAMAGED ANGLE VERITCAL STAB INTERIOR WEB IAW B727 SRM 51-30-2, FIG 7. VERIFIED MATERIAL TO BE 7075T6 IAW HARDNESS TESTER B727 SRM 51-10-3, FIG 2. FABRICATED NEW Jun 20, 2007 · N783DH · Boeing 727227 · Vertical Stabilizer, Spar/RibSDR DHL2007783518Skin · delaminatedRT WING INBD FOR FLAP WS 230, HAS LARGE DENT. CUT OUT DENTED/DELAMINATED APPROX AREA DIM 5 BY 10.5, REMOVED DAMAGED CORE DIM. 5 BY 10.5, APPLIED VACUUM AND HEAT TO REMOVE MOISTURE IAW B727 SRM 57-50-2, FIG 3 AND 51-40-20, PARA 7. FABRICATED COVE PLUG 5.1 BY Jun 13, 2007 · N783DH · Boeing 727227 · Trailing Edge FlapsSDR C8GA20070006Connector · looseFLT 716 FROM TOL TO MEM, AFTER TAKEOFF, NR 2 ENGINE OIL TEMPERATURE PEGGED HIGH. CREW PERFORMED PRECAUTIONARY ENGINE SHUT DOWN, DECLARED EMERGENCY, AND RETURNED TO TOL. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND OIL TEMP BULB CONNECTOR BACKJun 8, 2007 · N308AS · Boeing 727227 · Engine Oil System WiringSDR DHL2007783521Skin · dentedFUSELAGE SKIN AT MOVABLE AIRSTAIRS BS 1250 CREASED AND DENTED. REMOVED DAMAGED SECTION OF AFT AIRSTAIRS EXTERNAL SKIN FROM BS 1223 TO BS 1329 IAW B727 SRM 52-10-2, FIG 4. FABRICATED NEW SKIN SECTION, FROM 2024T3 .040, 106 BY 52.5 IAW B727 SRM 52-10-1 FIG 3 AJun 7, 2007 · N783DH · Boeing 727227 · Fuselage Main, Plate/SkinSDR DHL2007783508Intercostal · corrodedFOUND CORROSION AT INTERCOSTAL BETWEEN STA 1150 TO 1166, JUST ABOVE STR 27R. REMOVED INTERCOSTAL BETWEEN STA 1150 TO 1166, JUST ABOVE STR 27R IAW B727 SRM 51-30-2. FOUND CORROSION TO BE OUT OF LIMITS IAW B727 SRM 53-10-1, FIG 1. FABRICATED NEW INTERCOSTAL FJun 7, 2007 · N783DH · Boeing 727227 · Fuselage Miscellaneous StructureSDR DHL2007783506Cargo Track · corrodedCABIN SEAT TRACK CORRODED BETWEEN BS 690 TO BS 560, RBL 45. REMOVED SEAT TRACK SECTION BS 590 TO BS 690, RBL 45 IAW B727 SRM 53-10-5, FIG 5. FABRICATED NEW SEAT TRACK, MATERIAL USED BAC1520-792-7178T6511, DIM. 99” LONG AND 2 EACH ANGLES, MATERIAL USED BAC150Jun 7, 2007 · N783DH · Boeing 727227 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2007783505Stringer · corrodedAFT CARGO PIT BETWEEN BS 950E AND 950F, STRINGER 28L HAS CORROSION AT OUTBD BOTTOM FLANGE. CUT OUT DAMAGED STR 28L STA 950D PLUS 10 TO 950F PLUS 10 AS REQUIRED IAW B727 SRM 53-10-3, FIG 1. FABRICATED STRINGER REPAIR 2 EACH MATERIAL USED BAC1498-145-7075T6, DJun 6, 2007 · N783DH · Boeing 727227 · Fuselage Main, Longeron/StringerSDR DHL2007783526Bulkhead · corrodedEXFOLIATION CORROSION IN FWD BILGE, STA 740 BULKHEAD LWR CHORD AT STR 27R, (INBD OF STR 27R). FOUND SKIN SUPPORT ANGLE IN FWD BILGE AT STA 740 BULKHEAD TO BE BEYOND LIMITS AT STR 27R. FABRICATED AND INSTALLED NEW SKIN SUPPORT ANGLE IAW B727 SRM 51-30-2 AND BJun 5, 2007 · N783DH · Boeing 727227 · Fuselage Main, BulkheadSDR DHL2007783527Web · crackedLEFT WING TIP, VERTICAL WEB SHOWS MULTIPLE CRACKS BY FWD NAV LIGHT, WBL 640. CUT OUT DAMAGED AREA OF LEFT WING TIP, VERTICAL WEB AT NAV LIGHT AREA IAW B727 SRM 51-40-3, DIM 7.875 BY 3. FABRICATED AND INSTALLED REPAIR DOUBLER IAW B727 SRM 51-40-3, MATERIAL IDJun 5, 2007 · N783DH · Boeing 727227 · Wing Miscellaneous StructureSDR DHL2007783519Shear Tie · corrodedPILLOWING AT FASTENERS ON LWR FUSELAGE STR 27L, BS 620. REMOVED SHEAR TIE AT STA 620 BETWEEN STR 26L AND 27L IAW B727 SRM 51-30-2. FABRICATED NEW T-ANGLE SHEAR TIE FROM BAC1505-100246 7075T6, .063, 6.50 BY 2 IAW B727 SRM 53-10-2, FIG 3 AND 51-10-3, FIG 1. TJun 5, 2007 · N783DH · Boeing 727227 · Fuselage Internal Mounting StructureSDR DHL2007783517Door Frame · corrodedNR 2 CARGO DOOR CUT-OUT AFT FRAME, BS 990, RBL 22, WL 147.6 INNER CHORD SHOWS CORROSION SPOTS INNER SIDE AND DENT FROM OUTER SIDE. BLENDED OUT DAMAGED AREA AT NR 2 CARGO DOOR CUT OUT AFT FRAME BS 990 IAW B727 SRM 51-10-1, MATERIAL LOSS .017, ORIGINAL MATERIALJun 5, 2007 · N783DH · Boeing 727227 · Fuselage Main, StructureSDR DHL2007783515Angle · crackedCRACK AT UPPER SUPPORT ANGLE INSIDE VERT STAB LT PANEL 9701, FIN STA 239.1, WL 472.6. REMOVED STAB PANELS 9701 AND 9707 TO FOM IAW B727 SRM 51-30-2. REMOVED, FABRICATED NEW ANGLE INSIDE VERT STAB PANEL 9701 FROM 7075T6, .050, 3.25 BY 6 IAW B727 SRM 51-30-2, Jun 5, 2007 · N783DH · Boeing 727227 · Vertical Stabilizer Miscellaneous StructureSDR DHL2007783514Door Frame · dentedNR 2 CARGO DOOR CUT-OUT FWD FRAME, BS 950E INNER CHORD IS DENTED BETWEEN STR 25R AND 26R. REMOVED CORROSION RT NR 2 CARGO DOOR CUT OUT IAW B727 SRM 57-10-1, FIG 1. MATERIAL LOSS, .027, ORIGINAL THICKNESS .150, MATERIAL REMAINING .113 OUT OF LIMITS IAW B727 SJun 5, 2007 · N783DH · Boeing 727227 · Fuselage Main, StructureSDR DHL2007783513Web · crackedLT SIDE AIRSTAIRS WEB PANEL CRACKED AT LIGHTING HOLE, BS 1223, WL 156, LBL 21. CUT OUT DAMAGED AREA DIM .5 BY .5 IAW B727 SRM 51-40-2, FIG 1. FABRICATED DOUBLER REPAIR, MATERIAL USED 7075T6, 040, 4 BY 2.50 IAW B727 SRM 51-40-2, FIG 1 AND 53-10-2, FIG 6. TREJun 4, 2007 · N783DH · Boeing 727227 · Fuselage Miscellaneous StructureSDR DHL2007783512Web · crackedRT SIDE AIRSTAIRS WEB PANEL CRACKED AT LIGHTING HOLE, BS 1223, WL 156, RBL 21. CUT OUT DAMAGED AREA DIM .5 BY .5 IAW B727 SRM 51-40-2, FIG 1. FABRICATED DOUBLER REPAIR, MATERIAL USED 7075T6, 040, 4” BY 2.50 IAW B727 SRM 51-40-2, FIG 1 AND 53-10-2, FIG 6. TRJun 4, 2007 · N783DH · Boeing 727227 · Entrance Stairs
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