Boeing 727-227

Service difficulty reports · 5,082

Newest first. General aviation reporting is voluntary.

Query with SQL
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 DHL2005782551Shear Tie · corrodedSHEAR TIE AFT STA 1166 BETWEEN STR 18-19R CORRODED. REMOVED SHEAR TIE IAW B727 SRM 51-30-2 CUT OUT DAMAGE ON FRAME SIZE 2 1/2 INCH BY 2 INCH IAW B727 SRM 53-10-1. FABRICATED FILLER SIZE 2 1/2 BY 2 INCH MAT USED 7075 T6 .063 PO NR 900860 AND DOUBLER MAT USED Mar 16, 2005 · N782DH · Boeing 727227 · Fuselage Internal Mounting StructureSDR DHL2005782550Frame · bentFRAME AT STR 26 R STA 1110 BENT. CUT OUT DAMAGE AREA IAW B727 SRM 53-10-1 SIZE 2" BY 1". FABRICATED FRAME DOUBLER USING 7075 T6 .071 PO NR 9001298 DIM 10" BY 4" IAW B727 SRM 53-10-2 FIG 5 AND 51-40-3 FIG 1. ALODINE AND PRIMED IAW B727 SRM 51-10-2. INSTALLEMar 16, 2005 · N782DH · Boeing 727227 · Fuselage Main, FrameSDR DHL2005782549Frame · bentFRAME BETWEEN STR 25-26 R AT STA 1050 BENT. CUT OUT DAMAGE AREA SIZE 1 1/2 INCH BY 1 INCH IAW B727 SRM 53-10-1. FABRICATED FRAME REPAIR USING 7075-T6 .071 PO NR 9002012 DIM 8 INCH BY 4 INCH IAW B727 SRM 53-10-2 FIG 5 AND 51-40-3 FIG 1. ALODINE AND PRIMED PAMar 16, 2005 · N782DH · Boeing 727227 · Fuselage Main, FrameSDR DHL2005782548Bracket · crackedVERT STAB FRAME CLIP CRACKED FIN STA 157.2 BETWEEN STR 8L AND 9L. REMOVED DAMAGED CLIP AT FIN STA 157.2 BETWEEN STR 8-9L IAW 727 SRM 51-30-2. FABBED NEW FROM 7075 T6 .050 PO NR 90014147 DIM 6 5/8" BY 3" IAW 727 SRM 55-30-2 FUG 2 NEW CLIP TREATED PRIMED AND IMar 16, 2005 · N782DH · Boeing 727227 · Vertical StabilizerSDR DHL2005782547Stringer · crackedVERT STAB STR 6L CRACKED AT FIN STA 180.6. REMOVED FASTENERS CUT OUT DAMAGED AREA FABBED NEW STIFFENER FROM BAC 1517-1367 PO NR 501953 DIM 5 1/8" BY 3 INCH SPLICE FROM AND 10133-1401 PO NR 501952 DIM 21 3/8" BY 2" SPLICE FROM AND 10134-1201 PO NR 501952 DIM 2Mar 16, 2005 · N782DH · Boeing 727227 · Vertical Stabilizer, Spar/RibSDR DHL2005782545Skin · crackedNR 6 SLAT IB TRACK SEAL CUTOUT CRACKED WS474 R/W L/E. REMOVED NR 6 SLAT ASSY TO FROM IAW B727 W/W 27-81-41. REMOVED FASTENERS AT NR 6 SLAT I/B TRACK SEAL WS 474 R/W L/E FOR ACCESS IAW B727 SRM 51-30-2. STOP DRILL CRACK IAW B727 SRM 51-10-1. HFEC INSP PER NMar 15, 2005 · N782DH · Boeing 727227 · Leading Edge DevicesSDR DHL2005782544Web · crackedCRACKS IN WEBBING OF RIB LOCATED INSIDE THE BOTTOM END OF THE VERTICAL FIN BS 1303 (MARKED IN RED). JFEC INSPECTED WEB CRACK TERMINATED AT 1ST FASTENER HOLE IAW B727 NDT MAN PT 6 51-00-00 IIS 23, FABRICATED NEW DOUBLER REPAIR MATERIAL USED 7050 T6 .050 PO NR Mar 15, 2005 · N782DH · Boeing 727227 · Vertical StabilizerSDR DHL2005782543Skin · damagedREPLACE INTERIM REPAIR LOCATED ON THE RT VERTICAL STABILIZER BY REPLACING THE PANEL AFT OF THE REAR SPAR WITH A SERVICEABLE PANEL. REMOVED AND REPLACED VERTICAL STAB SKIN PANEL RT AFT OF THE REAR SPAR PN 6517561-234 PO NR 503010 IAW 727 SRM 51-30-2.Mar 15, 2005 · N782DH · Boeing 727227 · Vertical Stabilizer, Plate/SkinSDR DHL2005782542Stringer · crackedSTRINGER 9R CRACKED AT FIN STA 157.2 INSIDE VERTICAL FIN. REMOVED FASTENERS CUT OUT DAMAGED AREA FABBED NEW STIFFENER FROM BAC 1517-1387 PO NR 501953 DIM 4 3/8 INCH BY 3 INCH SPLICE FROM AND 10133-1401 PO NR 501952 DIM 17 3/8" BY 2" SPLICE FROM AND 10134-1201Mar 14, 2005 · N782DH · Boeing 727227 · Vertical Stabilizer, Spar/RibSDR DHL2005782541Skin · dentedDENT ON NR 8 SLAT EXTERNAL SKIN (MARKED). CUT OUT DAMAGE AREA SIZE 1 INCH BY 1 1/2 INCH IAW B727 SRM 57-50-1 FIG 2. FABRICATED DOUBLER REPAIR USING 2024 T3 .080 PO NR 90020125126 DIMENSIONS 6" BY 5" IAW B727 SRM 57-50-2 FIG 2 AND 57-50-3 FIG 1. ALODINE AND Mar 14, 2005 · N782DH · Boeing 727227 · Leading Edge DevicesSDR DHL2005782540Skin · dented4 DENTS ON NR 7 SLAT EXTERNAL SKIN (MARKED). MEASURED 4 DENTS ON NR 7 SLAT IAW B727 SRM 53-30-1 FIG 1 AND FOUND 3 MOST INBOARD DENTS WITHIN LIMITS, A.4/Y.013=30.7, A.2/Y.003=66.6, A.2/Y.002=100 AND OUTBOARD DENT OUT OF LIMITS A.4/Y.O41=9.7. CUT OUT DAMAGED AMar 14, 2005 · N782DH · Boeing 727227 · Leading Edge DevicesSDR DHL2005782539Skin · dentedDENT ON RT WING L/E ABOVE NR 5 KFLAP (MARKED). CUT OUT DAMAGED AREA DIMENSIONS 1 1/2" BY 1/2" AND FABRICATED REPAIR DOUBLER MATERIAL USE 2024 T3 0.080 PO NR 9002012 DIMENSIONS 5 1/4" BY 5 1/4" IAW B727 SRM=57-30-4 FIG NR 1, PARTS TREATED AND PRIMED IAW B727 SMar 14, 2005 · N782DH · Boeing 727227 · Wing, Plate/SkinSDR DHL2005782505Clip · crackedANGLED SHEAR TIE CRACKED JUST BELOW STRINGER 9L AT FIN STA 180.6 INSIDE VERTICAL FIN. REMOVED DAMAGED CLIP AT FIN STA 180.6 BELOW STR 9L IAW 727 SRM 51-30-2. FABBED NEW CLIP FROM 7075 T6 .050 PO NR 9001417 DIM 5 3/4 INCH BY 3 INCHES IAW 727 SRM 727 55-30-2 FMar 14, 2005 · N782DH · Boeing 727227 · Vertical Stabilizer Miscellaneous StructureSDR DHL2005782504Stringer · crackedSTRINGER 9L CRACKED AT FIN STA 180.6 INSIDE VERTICAL FIN. REMOVED FASTENERS, CUTOUT DAMAGED AREA, FABBED NEW STIFFENER FROM BAC 1517-1367 PO NR 501953 DIM 5 1/2" BY 3", SPLICE FROM AND 10133-1401 PO NR 501952 DIM 19 1/8" BY 2" SPLICE FROM 10134-1201 PO NR 501Mar 14, 2005 · N782DH · Boeing 727227 · Vertical StabilizerSDR DHL2005782568Skin · dentedC-CHECK, DENT NR 1 ENGINE PYLON SKIN UPPER SURFACE 7 INCHES AFT OF STA 1303 STR 14L. DENT IS CREASED, FOUND TO BE OUT OF LIMITS ON PYLON NR 1 UPPER SKIN SURFACE 7 INCHES AFT OF STA 1303 STR 14L IAW B727 SRM 54-10-1 FIG 1. CUT OUT DAMAGE AREA SIZE .75 INCH X Mar 13, 2005 · N782DH · Boeing 727227 · Nacelle/Pylon, Plate/SkinSDR DHL2005782535Skin · dentedNR 3 ENG NOSE COWL, EXTERIOR SKIN AT 3 O'CLOCK AFT SKIN SURFACE EDGE IS DENTED, ERODED AND SEPARATING. DAMAGE ON NR 3 ENG NOSE COWL EXTERIOR SKIN 3 O'CLOCK AFT SKIN FOUND TO BE OUT OF LIMITS IAW 727 SRM 54-30-1 FIG 1. CUT OUT DAMAGED AREA, FABBED FILLER FROMMar 13, 2005 · N782DH · Boeing 727227 · Nacelle/Pylon, Main FrameSDR DHL2005782533Nose Cowl · dentedNR 3 ENGINE NOSE COWL, EXTERIOR SKIN AT 9 O'CLOCK FWD OF LOWER LATCH HANDLE, SKIN IS DENTED. DAMAGE ON NR 3 ENGINE NOSE COWL EXTERIOR SKIN AT 9 O'CLOCK FWD OF LOWER LATCH HANDLE OUT OF LIMITS IAW 727 SRM 54-30-1 FIG 1. CUTOUT DAMAGED AREA DIM 1 INCH BY 3/4 IMar 13, 2005 · N782DH · Boeing 727227 · Nacelle/Pylon, Main FrameSDR DHL2005782536Skin · chafedRT IB FOREFLAP LOWER OB END CHAFFED THROUGH REPAIR PATCH. REMOVED FASTENERS AND PREVIOUS REPAIR FOR ACCESS IAW 727 SRM 51-30-2. HFEC INSPECTED AREA WITH NO CRACKS NOTED IAW B727 NDT MAN. PT. 6 51-00-00 FIG 23. FABRICATED REPAIR DOUBLER FROM 2024T3 .071 PO NMar 12, 2005 · N782DH · Boeing 727227 · Trailing Edge FlapsSDR DHL2005782531Skin · delaminatedRT IB T/E FLAP IS DELAMINATED ON THE UPPER SURFACE OF THE AFT FLAP INBOARD EDGE CORRECTIVE ACTION: CUT OUT DELAM AREAS 3 APPROX 3 INCH DIAM, 2 INCH DIAM AND 2 INCH BY 4 1/4 AND CUT OUT PUNCTURED SKIN APPROX 2 INCH IAW B727 SRM 51-40-20 FIG 30. FABBED 2 FILLERMar 12, 2005 · N782DH · Boeing 727227 · Trailing Edge FlapsSDR DHL2005782569Strip · missingLEFT I/B FORE FLAP WBL 70 UPPER SURFACE HAS CHAFE STRIP MISSING. REMOVED AND INSTALLED LEFT I/B FORE FLAP AFTER SHEET METAL REPAIR IAW B727 MM 27-51-1, OP CHECK GOOD IAW B727 27-51-0. CUT OUT DAMAGE SKIN, FABBED FILLER 3.5 X 2.5 INCH & DOUBLER 5 X 4 INCH FROMar 11, 2005 · N782DH · Boeing 727227 · Trailing Edge FlapsSDR DHL2005782532Skin · debondedLT OB AFT FLAP IB UPPER SURFACE WBL 300 HAS DISBOND AT EDGE OF EXISTING REPAIR. FOUND 2 EACH DISBONDED AREA OF LOWER SKIN, ALSO REMOVED PREVIOUS REPAIR FROM LOWER SKIN AND CUTOUT DAMAGED AREA APPROX 48 SQ IN IAW B727 SRM 51-40-20 FIG 31. FABRICATED ON FILLERMar 11, 2005 · N782DH · Boeing 727227 · Trailing Edge FlapsSDR DHL2005782530Skin · crackedR/WING UPPER SURFACE CRACKED AT NR 12 SPOILER HINGE CUTOUT. STOP DRILLED CRACK SIZE .250 IAW B72 SRM 51-10-1. FABRICATED DOUBLER REPAIR USING 7075T6 .071 PO# 9002012 DIM. 6" BY 3 3/4" IAW B727 SRM 57-30-4 FIG 10. ALODINE AND PRIMED PART AND AREA IAW B727 51Mar 11, 2005 · N782DH · Boeing 727227 · Wing, Plate/SkinSDR DHL2005782529Skin · crackedR/WING UPPER SURFACE CRACKED OUT AT NR 11 SPOILER HINGE CUTOUT. REMOVED SPOILER PANEL FOR ACCESS IAW 727 MM 27-61-1. STOPPED DRILLED CRACK IAW 727 SRM 51-10-1. FABBED DOUBLER FROM 7075T6 .071 PO NR 9001737 DIM 5" BY 4" IAW 727SRM 57-30-4 FIG10. DOUBLER TREMar 11, 2005 · N782DH · Boeing 727227 · Wing, Plate/SkinSDR DHL2005782526Skin · gougedLT OB FORE FLAP L/E IB AT WBL 314 HAS GOUGES IN REPAIR DOUBLER SURFACE. REMOVED DOUBLER IAW B727 SRM 51-30-2. FABRICATED NEW DOUBLER USING 2024T3 .063 PO# 9001978 DIM. 7 1/2" BY 3 1/2" IAW B727 SRM 57-50-2 FIG 3 AND 57-30-4 FIG 1. ALODINE AND PRIMED PART ANMar 11, 2005 · N782DH · Boeing 727227 · Trailing Edge FlapsSDR DHL200578228Skin · gougedLT OB FORE FLAP L/E IB AT WBL 314 HAS 2 GOUGES IN REPAIR DOUBLER SURFACE. REMOVED DOUBLER IAW B727 SRM 51-30-2 FABRICATED NEW DOUBLER USING 2024T3 .063 PO NR 9001978 DIM 7 1/2" BY 3 1/2" IAW B727 SRM 57-50-2 FIG 3 AND 57-30-4 FIG 1. ALODINE AND PRIMED PART AMar 11, 2005 · N782DH · Boeing 727227 · Trailing Edge FlapsSDR DHL2005782528Skin · scratchedLT ELEV INBD BOTTOM SIDE HAS ALONG SCRATCH MARK. BURNISHED AREA ON LT ELEV I/B LOWER SKIN AND FOUND AREA CRACKED AND OUT OF LIMITS IAW 727 SRM 55-20-1 FIG 1. CUT OUT DAMAGED AREA DIM 5/8" AND 1/2" AND FABBED DOUBLER FROM 2024T3 .032 PO NR 9002034 DIM 2 1/2" Mar 11, 2005 · N782DH · Boeing 727227 · Elevator, Plate/SkinSDR DHL2005782527Skin · dentedLT ELEV STA 136 HAS 3 DENTS EACH. EVALUATED DENTS AT LT ELEVATOR STA 136 1ST A/Y=1.25/.017=73, 2ND 2.75/.03=91, WITHIN LIMITS AND 3RD OUT OF LIMITS IAW 727 SRM 55-20-1 FIG 1. CUT OUT DAMAGED AREA DIM 5/8" BY 1/2" AND FABBED DOUBLER FROM 2024T3 .032 PO AND 90Mar 11, 2005 · N782DH · Boeing 727227 · Elevator, Plate/SkinSDR DHL2005782525Skin · dentedLT ELEV IB BOTTOM AFT HAS 2 DENTS. EVALUATED 2 DENTS 1ST A/Y=1/.02=50 AND WITHIN LIMITS, 2ND IS OUT OF LIMITS IAW 727 SRM 55-20-1 FIG 1. CUT OUT DAMAGED AREA DIM 5/8" BY 1/2"AND FABBED DOUBLER FROM 2024T3 .032 PO NR 9002034 DIM 2 1/2" BY 2 1/4" IAW 727 SRM 5Mar 11, 2005 · N782DH · Boeing 727227 · Elevator, Plate/SkinSDR DHL2005782524Skin · crackedCRACK IN RT WING ROOT UPPER SKIN LE STA 95. CUT OUT DAMAGED AREA AND FABRICATED FILLER FROM 2024T3 .050 DIM. 7.5 INCH BY 7.5 INCH PO NR 9002012, DOUBLER FROM 2024T3 .040 DIM. 3.7 INCH BY .75 INCH PO NR 9001938 IAW 727 SRM 57-30-4 FIG 5. REPAIR PARTS TREATED Mar 11, 2005 · N782DH · Boeing 727227 · Wing, Plate/SkinSDR DHL2005782567Panel · dentedDURING AN A-CHECK, THE FOLLOWING DISCREPANCES WERE NOTED LWR VERTICAL PNL LT SIDE HAS 2 EA DENTS. CUT OUT DAMAGED AREAS APPROX 1 INCH ROUND AND 2 INCHES ROUND IAW B727 SRM 51-40-2 FIG 30, FABRICATED ONE FILLER 1 INCH ROUND AND ONE FILLER 2 INCHES ROUND AND ONMar 10, 2005 · N782DH · Boeing 727227 · Vertical Stabilizer, Plate/SkinSDR DHL2005782517Skin · bulgedBULGE L/SIDE FUSELAGE SKIN AFT OF STA 580 BELOW STA 24L. DAMAGED FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-30-1 FIG 1. CUTOUT DAMAGE AREA FABBED FILLER FROM 2024T3 .050 PO NR 9001684 DIM 7 1/2 INCH BY 6 1/2 INCH IAW B727 SRM 53-30-2 FIG2 53-30-3 FIG 2. TREAMar 10, 2005 · N782DH · Boeing 727227 · Fuselage Main, Plate/SkinSDR DHL2005782523Skin · crackedSKIN CRACKED ON UPPER SKIN CUT OUT FOR NR 5 SLAT IB TRACK, RT WING LE WS 375. STOP DRILLED CRACK SIZE 1/4 AT UPPER SKIN CUT OUT NR 5 SLAT IB TRACK RT WING LE IAW B727 SRM 51-10-1. FABRICATE DOUBLER REPAIR USING 2024T3 .063 PO NR 9001634 SIZE 7 1/2 INCH BY 6.Mar 10, 2005 · N782DH · Boeing 727227 · Leading Edge DevicesSDR DHL2005782522Rib · crackedRIB CRACKED ON FWD BOTTOM EDGE, RT WING LE WS 130. REMOVED NR 4 K-FLAP FOR ACCESS IAW B727 MM 27-81-01. STOP DRILLED CRACK IAW 727 SRM 51-10-1 AND FABBED REPAIR ANGLE FROM 7075T6 .063 PO NR 900861 DIM. 6" BY 1 3/4" IAW 727 SRM 57-20-2 FIG 1 AND 51-40-3 FIG 1Mar 10, 2005 · N782DH · Boeing 727227 · Wing, Rib/BulkheadSDR DHL2005782521Skin · dentedSEVERAL DENTS RT SIDE FUSELAGE SKIN AFT OF STA 178 BELOW RADOME. CUT OUT DAMAGE AREA IAW B727 SRM 1 1/2" BY 1 1/2" IAW B727 SRM 53-30-2. FABRICATED DOUBLER USING 2024T3 .050 PO NR 9002093 DIM. 10" BY 8" IAW B727 SRM 53-30-2 FIG. 1 AND 53-30-3 FIG. 1. ALODINMar 10, 2005 · N782DH · Boeing 727227 · Fuselage Main, Plate/SkinSDR DHL2005782520Skin · dentedNR 2 SLAT EXTERNAL SKIN DENTED (3) PLACES. MEASURED DENT AT WS 656.3 ON NR 2 SLAT AND FOUND IN LIMITS A.2/Y.005=40 IAW SRM 53-30-1 FIG 1. MEASURED DENT AT WS 684.3 ON NR 2 SLAT AND FOUND TO BE OUT OF LIMITS A.4/Y.32=28.1 IAW B727 SRM 53-30-1 FIG 1 AND REPAIMar 10, 2005 · N782DH · Boeing 727227 · Leading Edge DevicesSDR DHL2005782519Skin · bulgedBULGE UNDERNEATH FUSELAGE SKIN FWD OF STA 1050 STR 29R. DAMAGE FOUND TO BE OUT OF LIMITS IAW 727 SRM 53-30-1 FIG 1. CUT OUT DAMAGED AREAS DIM 3 3/4 INCH BY 1 7/8 INCH AT BS 1040 STR 29R AND 3 1/8 INCH BY 3 3/4 INCH ATBS 1040 STR 29L. FABBED 2 FILLERS FROM 2Mar 10, 2005 · N782DH · Boeing 727227 · Fuselage Main, Plate/SkinSDR DHL2005782518Skin · dentedDENT RT SIDE FUSELAGE SKIN FWD OF STA 480 BELOW STR 21R. DAMAGE FOUND ON PREVIOUS REPAIR FILLER AND OUT OF LIMITS IAW 727 SRM. REMOVED DAMAGED FILLER AND FABBED NEW FROM 2024T3 .040 PO NR 9001417 DIM 43.5 INCH BY 23 INCH IAW 727 SRM 53-30-2 FIG 1 AND COTNEY Mar 10, 2005 · N782DH · Boeing 727227 · Fuselage Main, Plate/SkinSDR DHL2005782516Skin · damagedCREASE LT SIDE FUSELAGE SKIN STA 1148 STR 26L. REMOVED INTERCOSTAL IAW B727 SRM 51-30-2. CUT OUT DAMAGED AREA SIZE 2 INCHES BY 1 9/16 INCH IAW B727 SRM 53-30-3 FIG 24. FABBED FILLER SIZE 2 INCHES BY 1 9/16 INCH USING 2024T3 .100 PO NR 9001576 STRUCTURE FILLMar 10, 2005 · N782DH · Boeing 727227 · Fuselage Main, Plate/SkinSDR DHL2005782515Skin · dentedDENT R/SIDE FUSELAGE SKIN AFT OF STA 1110 ABOVE STR 20. DAMAGED FOUND TO BE OUT OF LIMITS IAW 727 SRM 53-30-1 FIG 1. REMOVED 2 EA EXISTING REPAIRS FOR INCORPORATION INTO 1 BS 1130 STR 20R CUT OUT 2 3/4 INCH BY 1 1/2 INCH BY 2 : BS 1110-1130 STR 21 CUT OUTS 3Mar 10, 2005 · N782DH · Boeing 727227 · Fuselage Main, Plate/SkinSDR DHL2005782514Skin · dentedDENT LT SIDE FUSELAGE SKIN ABOVE STR 17L, AFT OF STA 1324.4. CUTOUT DAMAGED AREA IAW B727 SRM 54-30-1 FIG 1. FABRICATED DOUBLER REPAIR USING 2024T3 .063 PO NR 9001978 DIMENSION 15 INCHES BY 5 5/8 INCH IAW B727 SRM 54-30-2 FIG 7. ALODINED AND PRIMED PART IAWMar 10, 2005 · N782DH · Boeing 727227 · Fuselage Main, Plate/SkinSDR DHL2005782513Skin · dented3 DENTS L/FUSELAGE SKIN AFT OF STA 1342.4 BETWEEN STR 14L AND 13L. CUT OUT DAMAGED 2 EACH SIZE 1 INCH BY 1 INCH AND 1 INCH BY 1 INCH IAW B727 SRM 54-30-1. FABRICATED DOUBLER USING 2024T3 .063 PO NR 9002039 DIM 14 5/8" BY 10 1/4" IAW B727 SRM 54-30-2. ALODINMar 10, 2005 · N782DH · Boeing 727227 · Fuselage Main, Plate/SkinSDR DHL2005782512Skin · dentedSEVERAL DENTS R/SIDE FUSELAGE SKIN WITHIN 1INCH OF AECH OTHER FWD OF STA 1263 ABOVE STR 21R. REMOVED FASTENERS FOR ACCESS AT RT SIDE FUSELAGE SKIN STA 1263 STR 21R IAW B727 SRM 51-30-2. CUT OUT DAMAGE AREA DIMENSION 1 7/8 INCH BY 3 INCHES IAW B727 SRM 53-30-Mar 10, 2005 · N782DH · Boeing 727227 · Fuselage Main, Plate/SkinSDR DHL2005782510Skin · damagedCREASE R/SIDE FUSELAGE SKIN AT STA 1342.2 BELOW 21R. CUT OUT DAMAGED AREA AT FUSELAGE SKIN AT STA 1342 IAW B727 SRM 54-30-1 SIZE 1/2 INCH BY 2 INCH. FABRICATED DOUBLER REPAIR USING 2024T3 .063 PO NR 9001978 SIZE 10 INCH BY 9 INCH IAW B727 SRM 54-30-2 FIG 4ANMar 10, 2005 · N782DH · Boeing 727227 · Fuselage Main, Plate/SkinSDR DHL2005782509Skin · bulgedBULGE R/SIDE FUSELAGE SKIN FWD OF STA 1050 BETWEEN STR 27R AND 26R. DAMAGED FOUND TO BE OUT OF LIMITS IAW 727 SRM 53-30-1 FIG1. CUTOUT DAMAGED AREA DIM 2 1/4 INCH BY 1 7/8 INCH IAW B727 SRM 53-30-3 FIG 3. FABRICATED DOUBLER FROM 2024T3 .071 PO NR 7001978 DIMar 10, 2005 · N782DH · Boeing 727227 · Fuselage Main, Plate/SkinSDR DHL2005782508Skin · crackedFWD ENTRY DOOR OUTBOARD SIDE TOP RT CORNER SKIN DENTED. STOP DRILLED CRACK SIZE .250 IAW B727 SRM 51-10-1. FABRICATED DOUBLER REPAIR USING 2024T3 .050 PO NR 9001873 SIZE 5 3/4" BY 4 3/4" IAW B727 SRM 52-10-1 FIG 1AND 52-00-3 FIG 3. TREATED AND PRIMED AREA AMar 10, 2005 · N782DH · Boeing 727227 · Passenger/Crew DoorsSDR DHL2005782503Skin · damagedBULGE L/SIDE FUSELAGE SKIN AFT OF STA 580 BELOW STR 24L. DAMAGE FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-30-1 FIG 1. CUT OUT DAMAGE AREA FABBED FILLER FROM 2024 T3 .050 PO NR 9001684 DIM 1 1/2 INCH BY 1 1/2 INCH AND DOUBLER FROM 2024 T3 .063 PO NR 9001634 DMar 10, 2005 · N782DH · Boeing 727227 · Fuselage Main, Plate/SkinSDR DHL2005782502Skin · damagedCREASE L/SIDE FUSELAGE SKIN STA 1148 STR 26L. REMOVED INTERCOSTAL IAW B727 SRM 51-30-2 CUT OUT DAMAGED AREA IAW B727 SRM 53-30-3 FIG 24. FAB FILLER SIZE 2" BY 19/16 USING 2024 T3 .100" PO NR 9001576 STRUCTURAL FILLER USING 2024 T3 .063 INCH PO NR 9002039 SIZMar 10, 2005 · N782DH · Boeing 727227 · Fuselage Main, Plate/SkinSDR DHL2005782501Skin · crackedCRACK ON NR 4 SLAT SKIN AT I/B UP STOP BLOCK FASTENER. STOP DRILLED CRACK AT NR 4 SLAT SKIN AT I/B UPSTOP IAW B727 SRM 51-10-1. ACCOMPLISHED 727 HFEC INSPECTION 51-00-00 CRACK CONTIMENT CONFIRMED. FABRICATED REPAIR DOUBLER MAT USED 2024-T3 .80 DIMENSION 11 Mar 10, 2005 · N782DH · Boeing 727227 · Leading Edge DevicesSDR DHL2005782507Skin · damagedREMOVED 2EA RIVETS BS 500-520 STR 24-25R [MS20470 AD-8] AND INSTALL B727 SRM 53-30-3 FIG 23. REPAIR PER ASTAR J/C MSI53300277-001-B. REMOVED 2EA MS20470D-8 FASTENERS IAW 727 SRM 51-30-2. FABBED REPAIR DOUBLER FROM 2024T3 .080 PO NR 9002012 DIM 63 3/4 INCH BMar 9, 2005 · N782DH · Boeing 727227 · Fuselage Main, Plate/SkinSDR DHL2005782534Skin · dentedAFT AIRSTAIR EXTERIOR SKIN AT STA 1303 IS DENTED. REMOVED FASTENER DOOR S/M. REPAIR AT AFT AIRSTAIR EXT SKIN IAW B727 SRM 51-10-2 FIG 4. FABRICATED FILLER SKIN MAT USED 2024T3 040 PO NR 9002012 DIMENSION 61 1/2' BY 42' AND 1 EA STRAP MAT USED 2024T3 0.40 POMar 8, 2005 · N782DH · Boeing 727227 · Entrance Stairs
Back to Boeing 727-227