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"

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 07FDEA02993Controller · malfunctionedCABIN ALT WARNING CLIMBING THROUGH FL270, CABIN ALT SHOWED 10,000, CLOSED CARGO HEAT OUTFLOW VALVE, NO CHANGE IN CABIN ALTITUDE. PERFORMED QRH CABIN ALT WARNING CHECKLIST. THEN PERFORMED FAILURE OF PRESSURIZATION OF CONTROL CHECKLIST. SYSTEM WOULD NOT PRESSAug 20, 2007 · N479FE · Boeing 727227 · Cabin Pressure ControllerSDR DHL2007784538Skin · damagedBLIND FASTENERS INSTALLED IN REPAIR AT STA 1215, BL 0. REMOVED BLIND FASTENERS ON REPAIR IAW B727 SRM 51-30-2. CUT 4 ACCESS HOLE IN AFT AIRSTAIRS STA 1194 RBL 60 AT TORQUE BOX UPPER WEB IAW B727 SRM 51-40-2. OVER SIZED BLIND FASTENER HOLES .03125 IAW B727 SJul 31, 2007 · N784DH · Boeing 727227 · Fuselage Main, Plate/SkinSDR DHL2007784537Skin · damagedBLIND FASTENERS INSTALLED IN REPAIR AT STA 1194, STR 19R. REMOVED BLIND FASTENERS ON REPAIR IAW B727 SRM 51-30-2. CUT 4 ACCESS HOLE IN AFT AIRSTAIRS STA 1194 RBL 60 AT TORQUE BOX UPR WEB IAW B727 SRM 51-40-2. OVER SIZED BLIND FASTENER HOLES .03125 IAW B727 SJul 31, 2007 · N784DH · Boeing 727227 · Fuselage Main, Plate/SkinSDR DHL2007784536Skin · crackedEXTERIOR FUSELAGE STA 1223, RBL 10, STR 30 A PREVIOUS REPAIR IS CRACKED. REMOVED PREVIOUS REPAIR IAW B727 SRM 51-30-2. FABRICATED NEW REPAIR FROM 2024T3,.050, 8.5 BY 8.5 IAW B727 SRM 53-30-2, FIG 3 AND 53-30-3, FIG 1. TREATED, PRIMED AND INSTALLED NEW ANGLEJul 23, 2007 · N784DH · Boeing 727227 · Fuselage Main, Plate/SkinSDR DHL2007784535Seat Track · corrodedFUSELAGE INTERIOR SEAT TRACK FROM BS 760 TO BS 850, LBL 45.50, WL 208.5 IS CORRODED. REMOVED SEAT TRACK OUT OF LIMITS STA 760 TO 850 IAW B727 SRM 51-30-2. FABRICATED NEW SEAT TRACK FROM P/N BAC1520-841-7178T6, DIM 94.875 IAW B727 SRM 53-10-5, FIG 2. TREATEDJul 22, 2007 · N784DH · Boeing 727227 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2007784518Angle · crackedSUSPECT CRACKED ANGLE AT RT ELEVATOR INBD AFT END, R ELEV STA 36.91 TO 53.91. OPENED END CAP ON RT ELEVATOR INBD SIDE FOUND ANGLE CRACKED AND OPENED ELEVATOR SKIN PANEL. CUT OUT DAMAGED AREA OF ANGLE, REAR SPAR 1 BY 2 IAW B727 SRM 51-40-3. FABRICATED REPAIRJul 19, 2007 · N784DH · Boeing 727227 · Elevator StructureSDR DHL2007784519Skin · distortedRT ELEVATOR, LWR SKIN IS OIL CANNING ON INBD DRAIN HOLE SKIN, 11 FWD OF ELEVATOR T/E, R ELEV STA 17.20. REMOVED DAMAGED AREA DIM .5 BY .75 IAW B727 SRM 55-20-3, FIG 1. FABRICATED DOUBLER REPAIR, MATERIAL USED 2024T3, 032, 5 BY 5 IAW B727 SRM 55-20-3, FIG 1. Jul 19, 2007 · N784DH · Boeing 727227 · Elevator, Plate/SkinSDR 07FDEA02515Shear Tie · corrodedAFT PIT STA 1010 BUTT JOINT SPLICE SHEAR TIE CORRODED BETWEEN STR 27-28R BLENDED CORROSION, ORIGINAL MATERIAL THICKNESS WAS .075" BETWEEN 0.001" AND 0.017 IS THE MATERIAL LOSS. OUT OF LIMITS REF SRM 53-30-01 FIG 1. FABRICATED AND INSTALLED FILLER AND DOUBLERJul 18, 2007 · N481FE · Boeing 727227 · Fuselage Internal Mounting StructureSDR 07FDEA02511Frame · crackedGALLEY DOOR (R-1) CUTOUT UPPER FWD SIDE STATION 380 FRAME CRACKED ON FORWARD SIDE BETWEEN STR 7R AND 8R. REMOVED FASTENERS IN DAMAGED AREA, CUTOUT DAMAGE, NDT VERIFIED NO DEFECTS. FABRICATED STRAP AND FILLER, TREATED, PRIMED REPAIR PARTS. INSTALLED REPAIR PJul 18, 2007 · N481FE · Boeing 727227 · Fuselage Main, FrameSDR 07FDEA02503Rib · damagedCOMPLY WITH EA 7-5710-110753, RT SIDE ONLY, WINGS- (AD 90-06-09 AND AD 94-07-08) MAIN FRAME, RIB UPPER CHORD REPAIR EO 7-5710-7-2308 PART 2. COMPLIED WITH EA 7-5710-110753 RT SIDE IAW SB 727-57-0112.Jul 17, 2007 · N241FE · Boeing 727227 · Wing, Rib/BulkheadSDR 07FDEA02502Rib · misalignedCOMPLY WITH EA NR 7-5710-110754 WING, (AD 90-06-09: 94-07-08: 98-11-03) RBL 70.5 RIB UPPER CHORD REPAIR DEVIATIONS. COMPLIED WITH EA NR 7-5710-110754 WING, (AD 90-06-09: 94-07-08: 98-11-03) RBL 70.5 RIB UPPER REPAIR DEVIATIONS.Jul 17, 2007 · N241FE · Boeing 727227 · Wing, Rib/BulkheadSDR 07FDEA02501Rib · misalignedWING RBL 70.5 RIB UPPER CHORD REPAIR DEVIATIONS EA NR 7-5710-110754. COMPLIED WITH EA NR 7-5710-110754 WING, AD 90-06-09: 94-07-08: 98-11-03) RBL 70.5 RIB UPPER CHORD REPAIR DEVIATIONS.Jul 17, 2007 · N241FE · Boeing 727227 · Wing, Rib/BulkheadSDR 07FDEA02500Web · corrodedMAIN DECK FLOOR SHEAR WEB AT BS 1165-1166 RBL 48" TO 49" WL 208 HAS CORROSION ON UPPER SURFACE. REMOVED CORROSION AND NDT AREA. REMOVED DAMAGED AREA INSTALLED DOUBLER AND FILLER PER SRM 51-40-02 FIGURE NR 1. REINSTALLED DISTURBED AREA PER MM 53-20-012-4, SRJul 17, 2007 · N481FE · Boeing 727227 · Fuselage Miscellaneous StructureSDR 07FDEA02499Web · corrodedMAIN DECK FLOOR SHEAR WEB AT BS 1165-1166 RBL 48" TO 49" WL 208 HAS CORROSION ON UPPER SURFACE. REMOVED CORROSION AND NDT AREA. REMOVED DAMAGED AREA INSTALLED DOUBLER AND FILLER PER SRM 51-40-02 FIGURE NR 1. REINSTALLED DISTURBED AREA PER MM 53-20-012-4, SRJul 17, 2007 · N481FE · Boeing 727227 · Fuselage Miscellaneous StructureSDR 07FDEA02487Depressor · gougedFWD LWR CARGO DOOR LOWER EDGE SEAL DEPRESSOR I/B SURFACE IS GOUGED IN 2 PLACES 26" AND 33" FROM AFT END OF DOOR. REPLACED SEAL DEPRESSOR IAW SRM 52-30-1.Jul 16, 2007 · N481FE · Boeing 727227 · Cargo/Baggage DoorsSDR 07FDEA02486Panel · delaminatedRT WING OB TE PANEL 8855, LWR SKIN HAS LARGE AREA OF DISBOND IN CENTER OF PANEL. INSTALLED NEW PANEL IAW SRM 51-30-02 PG 1 AND PG 13-14.Jul 16, 2007 · N481FE · Boeing 727227 · Wing, Plate/SkinSDR 07FDEA02485Frame · corrodedAFT PIT STA 970 SHEAR TIE CORRODED BETWEEN STRINGER 25R-26R RBL 17-22 REMOVED CORRRODED SHEAR TIE. FAB`D REPAIR SHEAR TIE AND INSTALLED PER SRM 53-10- 4 FIG 11 PAGE 43 THR 45.Jul 16, 2007 · N481FE · Boeing 727227 · Fuselage Main, FrameSDR DHL2007784509Cargo Track · gougedMAIN CARGO NICKS AND GOUGES ON SEAT TRACK, RBL 45, BS 850 TO BS 870. REMOVED SEAT TRACK IAW B727 SRM 51-30-2 AND B727 AMM 53-10-1. FABRICATED NEW SEAT TRACK, MATERIAL USED BAC1520-146-7178T6511, DIM 17 LONG IAW B727 SRM 53-10-2, FIG 7 AND 51-30-5. TREATED, Jul 13, 2007 · N784DH · Boeing 727227 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2007784508Cargo Track · corrodedMAIN CARGO, NICKS, GOUGES AND CORROSION ON SEAT TRACK, RBL 24, BS 850 TO BS 870. REMOVED DAMAGED SEAT TRACK SECTION IAW B727 SRM 51-30-2 AND B727 AMM 53-10-1. FABRICATED NEW SEAT TRACK, MATERIAL USED BAC1520-146-7178T6511, DIM. 17 LONG IAW B727 SRM 53-10-2, Jul 13, 2007 · N784DH · Boeing 727227 · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA02450Panel · delaminatedRT WING O/B T/E PANEL 8855, LWR SKIN HAS LARGE AREA OF DISBOND IN CENTER OF PANEL. INSTALLED NEW PANEL IAW SRM 51-30-2 PG 1 & PG 13-14.Jul 13, 2007 · N481FE · Boeing 727227 · Wing, Plate/SkinSDR 07FDEA02456Keelbeam · corrodedAFT PIT KEEL BEAM CHORD/STR 29L CORRODED STA 990-1010 REMOVED CORROSION. FOUND TO BE OUT OF LIMITS TREATED AND PRIMED BLENDED AREA REF SRM 51-10-2. FABBED REPAIR STRAP REF DWG SR 27-53-023. TREATED AND PRIMED REF SRM 51-10-2. INSTALLED REPAIR REF DWG SR 27Jul 13, 2007 · N481FE · Boeing 727227 · Fuselage Main, KeelSDR 07FDEA02455Skin · gougedFWD LWR CARGO DOOR INNER SKIN IS GOUGED 2 " FROM TOP 19 " FROM AFT EDGE. BLENDED DAMAGE PER SRM 51-10-1 PG 3-4 IT WAS OUT OF LIMITS PER SRM 52-00-2 PG 1 STEP 1B, REMOVED DOUBLER AND MANUFACTURED NEW DOUBLER OUT OF 7075-T6 .050. INSTALLED ON DOOR AND INSTALLEJul 13, 2007 · N481FE · Boeing 727227 · Cargo/Baggage DoorsSDR 07FDEA02454Web · crackedMAIN DECK ARCHED WEB AND ANGLE AT BS 1180 LBL38" WL 208 IS CRACKED. ABOVE SNRM WAS SOILED. FABRICATED NEW WEB, ANGLES AT BS 1180 LBL 38" WL 208 IAW B727 DWG 65-29567. TREATED AND PRIMED, INSTALLED IAW B727 SRM 51-10-2, 51-30-2.Jul 13, 2007 · N481FE · Boeing 727227 · Fuselage Miscellaneous StructureSDR 07FDEA02453Frame · crackedFWD CARGO PIT LT SIDE BS 600 STR 21L FRAME EXTENSION CRACKED ON O/B EDGE ABOVE STR 21L. REMOVED FRAME SPLICE REF SRM 51-30-02. FORMED NEW FRAME SPLICE USING .063 7075-O A 66693 PO NR 1008655 REF DWG 53FX1350 REV A. RECEIVED HEAT TREATED REPAIR SPLICE REF FOJul 13, 2007 · N481FE · Boeing 727227 · Fuselage Main, FrameSDR 07FDEA02452Panel · crackedMAIN DECK ARCHED WEB BETWEEN BS 1176-1183 RBL 36" TO 47" HAS SEVERAL CRACKS AND SEPARATED COMPOSITE PATCH. REMOVED DAMAGED PART AND FABRICATED NEW FROM 2024-O .032 MATERIAL AND SENT FOR HEAT TREAT. TREATED AND PRIMED REF M/M 51-20-151-7. INSTALLED NEW PARTSJul 13, 2007 · N481FE · Boeing 727227 · Fuselage Miscellaneous StructureSDR 07FDEA02451Panel · crackedUPPER MAIN DECK STA. 1176-1183 RBL 27", ARCHED FLOOR WEB CLOSURE, INBD ANGLE IS DAMAGED. REMOVED DAMAGED ANGLE, FABRICATED NEW AND SENT FOR HEAT TREAT. TREATED AND PRIMED REF M/M 51-20-151-7. INSTALLED NEW ANGLE REF SRM 51-30-02.Jul 13, 2007 · N481FE · Boeing 727227 · Fuselage Miscellaneous StructureSDR 07FDEA02449Intercostal · corrodedAFT PIT STA 970 STR 27R-28R INTERCOSTAL. REMOVED INTERCOSTAL REF SRM 51-30-2, REMOVED STIFFENERS REF SRM 51-30-2. FABRICATED AND HEAT TREATED NEW INTERCOSTAL REF WO 2007-07-027 PN 69-44880-12. TREATED AND PRIMED INTERCOSTAL REF SRM 51-10-2. INSTALLED NEW IJul 13, 2007 · N481FE · Boeing 727227 · Fuselage Miscellaneous StructureSDR DHL2007784534Frame · corrodedAFT CARGO COMPARTMENT BS 990, FWD AND AFT SIDES OF FRAME STR 29L-28L HAS WEB AND FRAME SURFACE CORROSION. CUT OUT DAMAGED SHEAR TIE AREA DIM 7 BY 1 IAW B727 SRM 53-10-4, FIG 13. FABRICATED NEW SHEAR TIE FROM 7075T0 .071 DIM 8 BY 4.25 IAW B727 SRM 53-10-4, FIJul 11, 2007 · N784DH · Boeing 727227 · Fuselage Main, FrameSDR DHL2007784516Support Angle · crackedCRACK AT BS 1342 WEB AND LT SUPPORT ANGLE INSIDE VERT STAB PANEL 9504. REMOVED CRACKED SUPPORT ANGLE INSIDE VERT STAB PANEL 9504 IAW B727 SRM 51-30-2. FABRICATED NEW SUPPORT ANGLE FROM .040, 7075T6, DIM. 3.75 BY 8.25 IAW B727 SRM 51-10-2. TREATED, PRIMED ANJul 11, 2007 · N784DH · Boeing 727227 · Vertical Stabilizer Miscellaneous StructureSDR DHL2007784515Frame · crackedAFT CARGO COMPARTMENT BS 970, STR 29L-28L HAS FRAME FLANGE CRACKED OUT WITH CORROSION. CUT OUT DAMAGED SHEAR TIE AT BS 970, BETWEEN STR 28L-29L IAW B727 SRM 53-10-4, FIG 13. FABRICATED SHEAR TIE REPAIR MATERIAL USED 7075T6 .071” DIM 6.50” BY 7 IAW B727 SRM Jul 11, 2007 · N784DH · Boeing 727227 · Fuselage Main, FrameSDR DHL2007784510Stringer Splice · corrodedAFT CARGO COMPARTMENT BS 1010, STR 28R, DOUBLER HAS SURFACE CORROSION.CORRECTIVE ACTION: REMOVED AFT CARGO COMPARTMENT STR 28R DOUBLER IAW B727 SRM 51-30-2. FABRICATED NEW DOUBLER, MATERIAL USED BAC 1498-131-7075T6, DIM 12 LONG IAW B727 SRM 53-10-2, FIG 9 ANDJul 11, 2007 · N784DH · Boeing 727227 · Fuselage Main, Longeron/StringerSDR DHL2007784505Support · crackedNR 6 K-FLAP ACTUATOR SUPPORT IS CRACKED AT INBD CORNERS, W/S 304. REMOVED NR 6 K-FLAP ACTUATOR TRUNNION SUPPORT ANGLES INBD AND OUTBD IAW B727 SRM 51-30-2. FABRICATED SUPPORT ANGLES FROM 7075T6, .071, 8.25 BY 6.25 IAW B727 SRM 57-20-2, FIG 1 AND 51-20-1, FIGJul 11, 2007 · N784DH · Boeing 727227 · Wing, Attach FittingsSDR 07FDEA02424Plate · crackedAFT CARGO PIT THRESHOLD PLATE IS CRACKED BY WELD. REPAIR ACCOMPLISHED ON N/R N00477, PER SR 27-53-025C.Jul 11, 2007 · N481FE · Boeing 727227 · Fuselage Miscellaneous StructureSDR DHL2007784533Seat Track · gougedMAIN CARGO NICKS AND GOUGES ON SEAT TRACK TOP SURFACE, BS 741 TO 868, RBL 45, WL 208.5 AS MARKED. REMOVED SEAT TRACK OUT OF LIMITS STA 760 TO 850 IAW B727 SRM 51-30-2. LOCATED AND DRILLED NEW SEAT TRACK FROM P/N BAC1520-541-7170T6511, DIM. 99.25 IAW B727 SRMJul 10, 2007 · N784DH · Boeing 727227 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2007784532Seat Track · corrodedMAIN CARGO NICKS AND GOUGES ON SEAT TRACK BOTTOM SURFACE, BS 540 TO BS 689, LBL 45, WL 208.5 AS MARKED. REMOVED SEAT TRACK STA 550 TO BS 690 IAW B727 SRM 51-30-2. FABRICATED NEW SEAT TRACK FROM P/N BAC1520-792-7170T6511, DIM 11’8 AND TWO EACH ANGLES FROM BACJul 10, 2007 · N784DH · Boeing 727227 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2007784530Seat Track · corrodedMAIN CARGO GOUGES AND CORROSION ON SEAT TRACK LBL 24, BS 480 TO BS 690, WL 208.5 ON ENTIRE TRACK. REMOVED FLOORBOARDS AT MAIN CABIN ROW B AND C, STA 480 TO 720C AND SEAT TRACK OUT OF LIMITS STA 740 TO BS 720B PLUS 10 IAW B727 SRM 51-30-2. FABRICATED THREE EAJul 10, 2007 · N784DH · Boeing 727227 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2007784531Seat Track · corrodedMAIN CARGO GOUGES AND CORROSION ON SEAT TRACK LBL 45, BS 480 TO BS 690, WL 208.5 ON ENTIRE TRACK. REMOVED FLOOR BOARDS AT MAIN CABIN ROW A, STA 480 TO 720C AND SEAT TRACK STA 480 TO BS 690 IAW B727 SRM 51-30-2. FABRICATED TWO EACH SEAT TRACKS FROM P/N BAC152Jul 10, 2007 · N784DH · Boeing 727227 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2007784529Shear Tie · corrodedAFT CARGO COMPARTMENT BS 1166, STR 29L TO 27L, FRAME SHEAR TIE HAS CORROSION ON BOTH SIDES OF FRAME. REMOVED DAMAGED SHEAR TIE DIM 13.5 BY 2.75 IAW B727 SRM 53-10-4, FIG 13. FABRICATED SHEAR TIE REPAIR, FROM 7075T0 .071, 13.25 BY 7.5 AND ONE EACH FILLER ANGLJul 10, 2007 · N784DH · Boeing 727227 · Fuselage Internal Mounting StructureSDR DHL2007784525Skin · burnedDENT ON LOWER FUSELAGE SKIN BS 630 STR 27L. CUT OUT DAMAGED AREA DIM 1.5 BY 1.5 IAW B727 SRM 53-30-3, FIG 3. FABRICATED DOUBLER FROM 2024T3, .063, DIM. 10 BY 8 IAW B727 SRM 53-30-3, FIG 3. TREATED, PRIMED AND INSTALLED REPAIR IAW B727 SRM 51-10-2 AND 53-30-Jul 10, 2007 · N784DH · Boeing 727227 · Fuselage Main, Plate/SkinSDR DHL2007784522Seat Track · gougedMAIN CARGO COMPARTMENT NICKS, GOUGES AND CORROSION ON SEAT TRACK RBL 24 BS 740 TO BS 868, WL 208.5 ON UPPER AND LOWER TRACK SURFACES. REMOVED DAMAGED SEAT TRACK STA 760 TO BS 850 IAW B727 SRM 51-30-2. LOCATED AND DRILLED NEW SEAT TRACK P/N BAC1520-841-7178T6Jul 10, 2007 · N784DH · Boeing 727227 · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA02414Frame · crackedFWD CARGO PIT LT SIDE BS 600 STR 21L FRAME EXTENSION CRACKED ON O/B EDGE ABOVE STR 21L. REMOVED FRAME SPLICE REF SRM 51-30-2. FORMED NEW FRAME SPLICE USING .063 7075-O A66693 PO NR 1008655 REF DWG 53FX1350 REV A. RECEIVED HEAT TREATED REPAIR SPLICE REF FORMJul 10, 2007 · N481FE · Boeing 727227 · Fuselage Main, FrameSDR 07FDEA02413Stringer · corrodedFWD CARGO BAY STR S-28R I/B UPPER FLANGE IS CORRODED AT BS 530. REMOVED CORROSION. ORIGINAL MATERIAL THICKNESS WAS .063". REMAINING MATERIAL IS OUT OF LIMITS AT .043". FABBED, TREATED, AND PRIMED REPAIR PART, P/N BAC1498-132. INSTALLED REPAIR PART AND NUTJul 10, 2007 · N481FE · Boeing 727227 · Fuselage Main, Longeron/StringerSDR 07FDEA02412Angle · corrodedAFT PIT FWD BULKHEAD BRACKET AT STA 950 WL 146 RBL 21-24 CORRODED. REPLACED ANGLE IAW SRM 53-10-1 THIS IS CLASSIFIED AS A MINOR REPAIR REF BAC65-58600, SRM 51-30-2.Jul 10, 2007 · N481FE · Boeing 727227 · Fuselage Miscellaneous StructureSDR DHL2007784517Skin · dentedC-1 DOOR SKIN HAS DENT AT AFT UPPER CORNER, STA 610-618, W/L 183. CUT OUT DAMAGED SKIN 3” BY 2.5 IAW B727 SRM 52-00-3, FIG 3. FABRICATED REPAIR DOUBLER, FROM 2024T3, 080, 8” BY 8.50 IAW B727 SRM 52-00-3, FIG.3 AND 52-30-1, FIG 7. TREATED, PRIMED AND INSTALLJul 9, 2007 · N784DH · Boeing 727227 · Service DoorsSDR DHL2007784506Stringer · corrodedAFT CARGO CORROSION ON STRINGER 28L, BS 960C. CUT OUT DAMAGED STR 28L STA 950C PLUS 10 AS REQUIRED IAW B727 SRM 53-10-3, FIG 1, DET I. FABRICATED REPAIR PARTS, 1 EACH FILLER MATERIAL USED BAC1498-147-7075T6, .090, 5 LONG AND 1 EACH SPLICE, MATERIAL USED BACJul 9, 2007 · N784DH · Boeing 727227 · Fuselage Main, Longeron/StringerSDR DHL2007784504Stringer · corrodedBULGE IN FUSELAGE SKIN AT STA 1050 PLUS 4 AND STR 27R. REMOVED INTERCOSTAL BETWEEN STA 950 TO 970, IAW B727 SRM 51-30-2. CUT OUT DAMAGED STRINGER DIM 16 LONG IAW B727 SRM 53-10-3, FIG 1. FABRICATED FILLER, MATERIAL USED BAC 1498-145-7075T6, DIM 16 LONG AND Jul 9, 2007 · N784DH · Boeing 727227 · Fuselage Main, Longeron/StringerSDR DHL2007784528Door Frame · crackedMCD HINGE AFT SEGMENT (FUSELAGE SIDE) HAC ONE LOBE CRACKED STA 620, WL 291, LBL 29. REMOVED DAMAGED MCD AFT HINGE SEGMENT IAW B727 SRM 51-30-2. DRILLED UP NEW HINGE SEGMENT PARTS IAW B727 SRM 51-30-5 AND AEI AMM CH. 52, FIG 5210, P/N MS20001-16-7200. TREATEJul 8, 2007 · N784DH · Boeing 727227 · Fuselage Main, StructureSDR DHL2007784526Skin · burnedEXTERNAL FUSELAGE BS 188 BELOW STR 13R HAS A LIGHTNING STRIKE BURN. BLENDED OUT AREA OF LIGHTNING STRIKE IAW B727 SRM 53-30-3, FIG 20. MATERIAL LOSS OVER 30 PERCENT OUT OF LIMITS IAW B727 SRM 53-30-1. CUT OUT DAMAGED SKIN AREA DIM. 2.5 BY 2 IAW B727 SRM 53-Jul 8, 2007 · N784DH · Boeing 727227 · Fuselage Main, Plate/SkinSDR DHL2007784524Skin · burnedEXTERNAL FUSELAGE BS 259.5 AT STR 12R HAS A LIGHTING STRIKE BURN. BLENDED OUT AREA OF LIGHTNING STRIKE IAW B727 SRM 53-30-3, FIG 20. MATERIAL LOSS OVER 30 PERCENT, LIGHTNING STRIKE STILL PRESENT AND OUT OF LIMITS IAW B727 SRM 53-30-1. CUT OUT DAMAGED SKIN ARJul 8, 2007 · N784DH · Boeing 727227 · Fuselage Main, Plate/SkinSDR DHL2007784523Skin · damagedEXTERNAL FUSELAGE BS 680 AT STR 7R HAS SKIN BUTT JOINT WITH A LIGHTING STRIKE 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. CJul 8, 2007 · N784DH · Boeing 727227 · Fuselage Main, Plate/Skin
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