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 DHL2005748547Frame · dentedDENT ON FRAME ABOVE STR 17R AT BS 680. CUT OUT DAMAGED AREA OF FRAME 1 BY 1.5 FAB REPAIR CHANNEL 8 1/2 BY 2 1/2 7075 T6 PO 9001777 IAW B727 SRM 53-10-4 FIG1. TREATED AND PRIMED ALL BARE SURFACES IAW B727 51-10-2. INSTALLED NEW FRAME REPAIR B727 SRM 53-10-4 Sep 2, 2005 · N748DH · Boeing 727225 · Fuselage Main, FrameSDR DHL2005748546Frame · bentBENT FRAME ABOVE STR 17R AT BS 660. CUT OUT DAMAGED AREA OF FRAME 1.2 BY 1.7 FAB REPAIR CHANNEL 8 1/2 BY 2 1/2 7075 T6 PO NR 9001777 IAW B727 SRM 53-10-4 FIG 1. TREATED AND PRIMED ALL BARE SURFACES IAW B727 51-10-2. INSTALLED NEW CHANNEL FRAME REPAIR IAW B7Sep 2, 2005 · N748DH · Boeing 727225 · Fuselage Main, FrameSDR DHL2005748545Frame · bentBENT FRAME ABOVE STR 17R AT BS 640. CUT OUT DAMAGED AREA OF FRAME 1.3 BY 1.2 FAB REPAIR CHANNEL 8 1/2 BY 2 1/2 7075 T6 PO NR 9001777 IAW B727 SRM 53-10-4 FIG 1. TREATED AND PRIMED ALL BARE SURFACES IAW B727 51-10-2. INSTALLED NEW CHANNEL FRAME REPAIR IAW B7Sep 2, 2005 · N748DH · Boeing 727225 · Fuselage Main, FrameSDR DHL2005748544Frame · bentBENT FRAME ABOVE STR 17R AT BS 600. CUT OUT DAMAGED AREA OF FRAME 2.3 BY 1.7 FAB REPAIR CHANNEL 10 BY 4 .050 7075 T6 PO 9001777 IAW B727 SRM 53-10-4 FIG 1. TREATED AND PRIMED ALL BARE SURFACES IAW B727 SRM 51-10-2. INSTALLED REPAIR CHANNEL IAW B727 SRM 53-1Sep 2, 2005 · N748DH · Boeing 727225 · Fuselage Main, FrameSDR DHL2005748543Frame · bentBENT FRAME ABOVE STR 17R AT BS 580. CUT OUT DAMAGED AREA OF FRAME 1.8 BY 1.7 FAB REPAIR CHANNEL 10 BY 4 .050 7075 T6 PO NR 9001777 IAW B727 SRM 53-10-4 FIG 1. TREATED AND PRIMED ALL BARE SURFACES IAW B727 SRM 51-10-2. INSTALLED REPAIR CHANNEL IAW B727 SRM 5Sep 2, 2005 · N748DH · Boeing 727225 · Fuselage Main, FrameSDR DHL2005748542Frame · bentBENT FRAME ABOVE STR 17R AT BS 560. CUT OUT DAMAGED AREA OF FRAME 1.3 BY 1.2 FAB REPAIR CHANNEL 10" BY 4" .050 7075 T6 PO NR 9001777 IAW B727 SRM 53-10-4 FIG 1. TREATED AND PRIMED ALL BARE SURFACES IAW B727 SRM 51-10-2. INSTALLED REPAIR CHANNEL IAW B727 SRMSep 2, 2005 · N748DH · Boeing 727225 · Fuselage Main, FrameSDR DHL2005748541Frame · dentedDENT ON FRAME ABOVE STR 17R AT BS 540. CUT OUT DAMAGED AREA OF FRAME 1.5 BY 1.2 FAB REPAIR CHANNEL .050 7075 T6 PO NR 9001777 IAW B727 SRM 53-10-4 FIG 1. TREATED AND PRIMED ALL BARE SURFACES IAW B7272 SRM 51-10-2. INSTALLED REPAIR CHANNEL IAW B727 SRM 53-10Sep 2, 2005 · N748DH · Boeing 727225 · Fuselage Main, FrameSDR DHL2005748540Frame · dentedREFERENCE FLIGHTSTAR AIRCRAFT SERVICES NR 110156, DENT ON FRAME ABOVE STR 17R AT BS 500. CUT OUT DAMAGED AREA OF FRAME 1.3 BY 1.2 FAB REPAIR CHANNEL .050 7075 T6 PO NR 9001777 IAW B727 SRM 53-10-4 FIG1. TREATED AND PRIMED ALL BARE SURFACES IAW B727 SRM 51-10Sep 2, 2005 · N748DH · Boeing 727225 · Fuselage Main, FrameSDR DHL2005748539Frame · dentedREFERENCE FLIGHTSTAR AIRCRAFT SERVICES NR 110155, DENT ON FRAME ABOVE STR 17R AT BS 520. CUT OUT DAMAGED AREA OF FRAME 1.6 BY 1.2 FAB REPAIR CHANNEL /050 7075 T6 PO NR 9001777 IAW B727 SRM 53-10-4 FIG 1. TREATED AND PRIMED ALL BARE SURFACES IAW B727 SRM 51-1Sep 2, 2005 · N748DH · Boeing 727225 · Fuselage Main, FrameSDR 05FDEA02736Skin · tornLEFT WING OUTBORD FORE FLAP UPPER SKIN SECTION MISSING (HONEYCOMB EXPOSED). REMOVED AND REPLACED LEFT WING OUTBORD FORE FLAP ASSEMBLY ON FEDEX SNRM N00079. REFERENCE NON ROUTINE N00007.Sep 2, 2005 · N464FE · Boeing 727225 · Trailing Edge FlapsSDR DHL2005478537Stringer · crackedAFT CARGO STR 30 AT BS 950A IS CRACKED. CUT OUT DAMAGED SECTION OF STR 30 DIM 15 1/2" IAW B727 53-10-3 FIG 1. FAB REPAIR PARTS AND REPLACED STR SECTIONS IAW B727 SRM 53-10-3 FIG 1 AND COTNEY AERO INC DWG NR AA00-53-R01 REV IR. TREATED AND PRIMED REPAIR PARTAug 31, 2005 · N748DH · Boeing 727225 · Fuselage Main, Longeron/StringerSDR DHL2005748536Skin · corrodedAFT CARGO AT BS 950F + 6, STR 28R IS CORRODED. CUT OUT DAMAGED AREA OF STR 28R AT BS950F +6 DIM 39". REPLACED WITH FILLER P/N BAC 1509-100204 PO NR 5314211 7075T6 39" AND 2EA SPLICES 7075T6 PO NR 5314245 PART FLT 092205 21 1/2" IAW B727 SRM 51-10-3 FIG1 ANAug 25, 2005 · N748DH · Boeing 727225 · Fuselage Main, Plate/SkinSDR DHL2005748535Channel · brokenNR 1 SLAT ACTUATOR ROD END CHANNEL BRACKET IS BROKEN. REMOVED BROKEN ROD END CHANNEL AND BUSHINGS IAW B727 SRM 51-30-2 LOCATED AND DRILLED NEW CHANNEL P/N 65-17327-7 PO NR 5314113 IAW B727 SRM 51-40-5. TREATED AND PRIMED PARTS IAW B727 SRM 51-10-2. INSTALLEAug 24, 2005 · N748DH · Boeing 727225 · Wing, Attach FittingsSDR DHL2005748534Angle · crackedINNER WEB FWD OF NR 1 SLAT ACTUATOR ROD END IS CRACKED. CUT OUT SECTION OF WEB TO GAIN ACCESS DIM 7.75 BY 1.50 IAW B727 SRM 51-40-2. CUT CRACKED SECTION OF ANGLE IAW B727 SRM 51-40-3 FIG 1. FAB REPAIR ANGLE PO NR 9081237 .040 2024T3 2" BY 10" IAW B727 SRM 5Aug 24, 2005 · N748DH · Boeing 727225 · Wing, Attach FittingsSDR PCSA823200501Door · misalignedON CLIMBOUT, AIRCRAFT WOULD NOT PRESSURIZE, CREW REPORTED LOUD AIRFLOW NOISE COMING FROM CABIN. AIRCRAFT RETURNED TO DEPARTURE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE L-1 MAIN CABIN ENTRY DOOR AFT END OF DOOR WITH A GAP, THE L-1 DOOR WAS ADJAug 23, 2005 · N604AJ · Boeing 727225 · Passenger/Crew DoorsSDR DHL2005748533Skin · delaminatedLT WING I/B FOREFLAP UPPER SURFACE DELAMINATED APPROX 16" O/B OF I/B END. CUT OUT DELAMINATED UPPER SKIN APPROX 6 1/2" BY 5". CUT OUT DAMAGED CORE APPROX 6 1/2" BY 5". FABED SEPTUM APPROX 6 1/2 BY 5 AND REPAIR CORE APPROX 6 1/2 BY 5 FROM DUR-5052-4.4-3/16 Aug 19, 2005 · N748DH · Boeing 727225 · Trailing Edge FlapsSDR DHL2005748532Support Angle · crackedNR 2 K FLAP LWR O/B ACTUATOR MOUNTING SUPPORT ANGLE CRACKED IN L/WING L/E. REMOVED O/B ACTUATOR MOUNTING SUPPORT ANGLE IAW B727 SRM 51-30-2 FAB NEW SUPPORT ANGLE FROM 7075 T6 .063 PO 9001417 8" X8" IAW B727 SRM 57-10-2 FIG 3. TREATED AND PRIMED NEW PARTS IAWAug 18, 2005 · N748DH · Boeing 727225 · Leading Edge DevicesSDR DHL2005748531Skin · dentedAFT CARGO COMP C2 DOOR LWR FWD CORNER IS DENTED STA 950E. REMOVED AND REPLACED AFT CARGO C2 DOOR LWR FWD CORNER RETAINER P/N 65-59947-501 PO 531498 IAW B727 SRM 51-30-2.Aug 17, 2005 · N748DH · Boeing 727225 · Cargo/Baggage DoorsSDR DHL2005748530Depressor · damagedC1 DOOR AFT LWR BS 610 SEAL DEPRESSOR GAUGE. REMOVED AND REPLACED SEAL DEPRESSOR P/N 65-57146-3 PO 5314122 IAW B727 SRM 51-30-2 LEAK CK GOOD IAW B727 MM 5-51-101.Aug 17, 2005 · N748DH · Boeing 727225 · Cargo/Baggage DoorsSDR DHL2005748529Skin · crackedAFT CARGO (C2) DOOR LWR AFT CORNER IS CRACKED AND DENTED STA 990 STR 26R. REMOVED AND REPLACED AFT LWR DOOR CORNER ON AFT CARGO DOOR IAW B727 SRM 51-30-07. REMOVED AND REPLACED LEVELING COMPOUND IAW B727 MM 20-60-01 PN 65-59948-502 PO 5314173.Aug 17, 2005 · N748DH · Boeing 727225 · Cargo/Baggage DoorsSDR DHL2005748526Skin · bentA/C L1 DOOR UPPER HINGE AREA DOOR SKIN BENT. EVAL BENT AREA FOUND CRACK AND STOP DRILLED CRACK DIA 250 IAW B727 SRM 51-10-1. FAB DOUBLER REPAIR 2024T3 .063 8" BY 7 1/4" PO 9001634 IAW B727 SRM 52-00-3 FIG 3 SHEETS 1-4. TREATED AND PRIMED DOUBLER AND AREA IAug 17, 2005 · N748DH · Boeing 727225 · Passenger/Crew DoorsSDR DHL2005748525Hinge · crackedL1 DOOR LWR HINGE CUT OUT CRACKED (HFEC CONFIRMED). REMOVED DOOR TRIM FWD SIDE AND FASTENERS AS NEEDED IAW B727 SRM 51-30-2, CUT OUT DAMAGED SKIN AND DOUBLER AT L1 DOOR LOWER HINGE CUT OUT IAW S/B 727-53A0198 FIG 3 REV 2 1 3/8" BY 2 5/8" CRACK WAS 1.75 LONG Aug 17, 2005 · N748DH · Boeing 727225 · Fuselage, Door HingeSDR DHL2005748524Skin · delaminatedRT WING INBD FORE FLAP DELAMINATED ON UPPER SURFACE 70" FROM OTBD END. CUT OUT DELAMINATED AREA RT I/B FORE FLAP UPPER SURFACE 70" FROM O/B END APPROX 4" DIA FAB FILLER APPROX 4" DIA AND DOUBLER APPROX 7" DIA FROM 2024 T3 .016 PO 9002273, CLEANED PREPPED APPLAug 16, 2005 · N748DH · Boeing 727225 · Trailing Edge FlapsSDR DHL2005748523Angle · crackedANGLE CRACKED AT T/E OF RT WING INBD MID FLAP 36" FROM INBD END. CUT OUT CRACKED SECTION OF ANGLE 8 1/2" AND FAB DOUBLER FROM AND 10133-1401, 7075 T6 .063 EXTRUSION 17 3/8" PO501952 FILLER FROM BAC 1509-10861 .050 8 1/2" PO 5079108 IAW B727 SRM 57-50-2 FIG 5 Aug 16, 2005 · N748DH · Boeing 727225 · Trailing Edge FlapsSDR DHL2005748522Skin · dentedDENT ON LWR SURFACE OF RT WING INBD AFT FLAP 70" FROM OTBD END. REMOVED EXISTING REPAIR AND CUT OUT DAMAGED AREA 8.0 BY 2.25 AND FAB DOUBLER .050 7075 T6 PO 9002507 5.25 BY 11.25 IAW B727 SRM 57-50-4 FIG 5. TREATED AND PRIMED REPAIR PART AND AREA IAW B727 SRAug 16, 2005 · N748DH · Boeing 727225 · Wing, Plate/SkinSDR DHL2005748521Skin · corrodedFOUND CORROSION AFT CARGO COMP STA 950F+6 BETWEEN STR 28R AND 27R. CUT OUT 1.875" BY 6.875" SECTION OF FUSE SKIN AT STR 28R AND STA 950F+6 MAT LOSS .038 REMAINING THICKNESS OF .106 BEYOND LIMITS IAW B727 SRM 53-30-2 AND 53-30-30 FIG 3. FAB DOUBLER FROM 2024TAug 16, 2005 · N748DH · Boeing 727225 · Fuselage Main, Plate/SkinSDR DHL2005748520Shear Tie · corrodedAFT CARGO COMP HAS CORROSION AT SHEAR TIE STA 990 STR 29R. CUT DAMAGED AREA 6" BY 1" FAB REPAIR DOUBLER AND FILLER 7075T6 .071 PO 5096275 IAW B727 SRM 53-10-4 FIG 13 (DOUBLER DIM 6 1/2 BY 3 1/8") (FILLERS 3 1/2 BY 1 1/2) (2" BY 1") & (4" BY 1"). TREATED ANDAug 16, 2005 · N748DH · Boeing 727225 · Fuselage Internal Mounting StructureSDR DHL2005748519Hinge · crackedMAIN CARGO DOOR AFT HINGE SEGMENT CRACKED. REMOVED AFT SECTION OF AFT HINGE IAW AEI CHAPTER 52 FIG 5201A CUT NEW HINGE SECTION FROM NS20001-16-7200 PO9002527 18" DRILLED COUNTERSINK TREATED AND PRIMED NEW HINGE SECTION IAW AEI CHAPTER 52 FIG 5201A. INSTALLEDAug 16, 2005 · N748DH · Boeing 727225 · Fuselage, Door HingeSDR DHL2005748518Skin · wornRT WING OTBD FORE FLAP WORN AT L/E 12" FROM INBD END. REMOVED EXISTING REPAIR ON RT WING O/B FORE FLAP L/E IAW B727 SRM 51-30-2 FAB NEW DOUBLER FROM 2024T3 .050 4" BY 5 1/2" PO9002507 IAW B727 SRM 57-50-4 FIG 1. TREATED AND PRIMED DOUBLER IAW B727 SRM 51-10-Aug 16, 2005 · N748DH · Boeing 727225 · Trailing Edge FlapsSDR DHL2005748517Skin · crackedRT WING UPPER TE PANEL CRACK NOTED FWD OF NR 11 SPOILER HINGE CUT OUT WS 464 AND REAR SPAR. STOP DRILLED CRACK .250 DIA IAW B727 SRM 51-10-1 FAB FROM 7075 T6 .071 6 3/4" BY 4" PO 900989 IAW B727 SRM 57-30-04 FIG10 DETAIL III. TREATED AND PRIMED DOUBLER IAW BAug 16, 2005 · N748DH · Boeing 727225 · Wing, Plate/SkinSDR DHL2005748516Skin · dented8 SLAT LE LWR SKIN SHOW DENT WS 716 (MARKED). CUT OUT DAMAGED AREA OF SKIN 2.5" BY 1.7" AND FAB DOUBLER 3.3" BY 5.7" .040 2024T3 PO 9051237 IAW B727 IAW B727 SRM 57-50-3. FAB FILLER 2.5 BY 1.6 .040 2024T3 PO 9051237 IAW B727 SRM 57-50-3. TREATED AND PRIMED Aug 16, 2005 · N748DH · Boeing 727225 · Leading Edge DevicesSDR DHL2005748515Skin · damagedNR 8 SLAT LE LWR SKIN CREASE AND DENTED TO O/B END WS760. CUT OUT DAMAGED AREA OF SKIN 6" BY 4" AND FAB FILLER 6.0" BY 4.0 .050 2024 T3 PO 9002435 IAW B727 SRM 57-50-3 FIG 1 FAB SPLICE STRAPS 5 BY 2.2 2EACH 3.3 BY 2.2 2EACH 2.4 BY 3.5 1EACH .080 2024 T3 PO 50Aug 16, 2005 · N748DH · Boeing 727225 · Leading Edge DevicesSDR DHL2005748514Trunnion · crackedNR 6 K FLAP ACTUATOR TRUNNION BRACKETS SUPPORT 2EA BOTH L/R ARE CRACKED. NOT CONFIRMED. FAB LEFT AND RIGHT NR 6 K FLAP ACTUATOR TRUNNION BRACKET SUPPORT FROM 7075 T6 .063 PO 9001920 DIM FOR RIGHT SIDE 8" BY 3 1/2" DIM FOR LEFT SIDE 8" BY 3 1/2" IAW B727 SRM Aug 16, 2005 · N748DH · Boeing 727225 · Trailing Edge FlapsSDR DHL2005748599Vertical Beam · crackedVERTICAL BEAM AT BS.1183, RBL 36, WL 240, APPROX, SHOWS CRACK AT CHORD ANGLE. STOP DRILLED CRACK IAW SRM 51-10-1,LOCATED,DRILLED AND INSTALLED REPAIR KIT P/N 65C34406-15,PO NR 531481 IAW S/B 727-53-0192 REV 1,MAY 30,1991Aug 15, 2005 · N748DH · Boeing 727225 · Fuselage Main, StructureSDR DHL2005748501Vertical Beam · crackedVERTICAL BEAM AT BS1183 RBL 36.WL 240, APPROX, SHOWS CRACK AT CHORD ANGLE. STOP DRILLED CRACK IAW SRM 51-10-1,LOCATED,DRILLED AND INSTALLED REPAIR KIT P/N 65C34406-15,PO NR 531481 IAW S/B 727-53-0192 REV 1,MAY 30,1991.Aug 15, 2005 · N748DH · Boeing 727225 · Fuselage Main, StructureSDR DHL2005748510Actuator · crackedNR 1 SLAT ACT TO SLAT ATTACH POINT CRACKED AT I/B RIB. OPENED ACCESS PANELS TO FACILITATE MAINT IAW B727 SRM 51-30-2. REMOVED DAMAGED RIB IAW B727 SRM 51-30-2. LOCATED & DRILLED NEW RIB P/N 65-17327-3 PO NR 531452 IAW B727 SRM 51-30-5 TREATED & PRIMED PARTAug 15, 2005 · N748DH · Boeing 727225 · Leading Edge Slat ActuatorSDR DHL2005748508Skin · delaminatedL/WING I/B FORE FLAP I/B END DELAM. CUT OUT DELAMINATED AREA OF UPPER I/B END OF L/WING I/B FOREFLAP APPROX 3 1/2" BY 14" AFTER RUBSTEP REMOVAL CUT OUT DAMAGED CORE APPROX 8 1/2" BY 2 3/4" FABBED SEPTUM APPROX 8 1/2" BY 2 3/4" REPAIR SKIN APPROX 3 1/2" BY 14"Aug 15, 2005 · N748DH · Boeing 727225 · Trailing Edge FlapsSDR DHL2005748507Skin · dentedL/WING O/B AFT FLAP DENTED ON L/E I/B END. CUT OUT DAMAGED AREA DIM 1" BY 2 1/4" FABRICATED NEW PART PO NR 9001938 2024T3 .050 IAW SRM 57-50-4 FIG 9 5" BY 3 1/2" TREATED AND PRIMED NEW PART IAW B727 SRM 51-10-2. INSTALLED NEW PART IAW SRM 57-50-4.Aug 15, 2005 · N748DH · Boeing 727225 · Trailing Edge FlapsSDR DHL2005748506Skin · dentedFUSELAGE HAS A DENT FWD BS 1144 ABOVE STR 24R. CUT OUT DAMAGED AREA DIMS 2" BY 1 1/2" AND FABRICATED REPAIR DOUBLER FROM MATERIAL USE 2024T3 .080 PO NR 900-2255 DIMS 11" BY 8" IAW B727 SRM 53-30-3 FIG 1 TREATED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED NEW Aug 15, 2005 · N748DH · Boeing 727225 · Fuselage Main, Plate/SkinSDR DHL2005748505Skin · dentedREFERENCE FLIGHTSTAR AIRCRAFT SERVICES NR 109558, FUSE HAS A DENT BS 460 ABOVE STR 26R. CUT OUT DAMAGED AREA DIMS 3" BY 3 1/2 AND FABRICATED REPAIR DOUBLER FROM MATERIAL USE 2024T3 .080 PO NR 900-2255 AND FILLER FROM MATERIAL USE 2024T3 .080 PO NR 900-22-55 DAug 15, 2005 · N748DH · Boeing 727225 · Fuselage Main, Plate/SkinSDR DHL2005748512Skin · corrodedAFT CARGO BILGE SKIN AREA HAS CORROSION AT STA 990 BETWEEN STR 28R AND 29R WCT 1312. CUT OUT DAMAGED AREA (3' BY 2 1/2") AT BS 970 AND REMOVED PREVIOUS DOUBLER AT BS 990 STR 29R -28R WITH PREVIOUS CUT OUT 5 1/2" BY 4" FABRICATED DOUBLER 2024T3 .125 PO 9002678Aug 14, 2005 · N748DH · Boeing 727225 · Fuselage Main, Plate/SkinSDR DHL2005748511Shear Tie · corrodedAFT CARGO COMPARTMENTS CORROSION AT SHEAR TIE STA 950F BETWEEN STR 30 29L (MARKED). CUT OUT DAMAGED AREA 6 1/8 BY 1" IAW B727 SRM 53-10-4 FIG 13. FAB DOUBLER 6 1/2 BY 3 AND FILLERS (2" BY 1") (4 BY 1/2) AND (1" BY 4") MAT ID 7075T6 .071 PO5096275 IAW B727 SAug 14, 2005 · N748DH · Boeing 727225 · Fuselage Internal Mounting StructureSDR DHL2055748504Skin · bulgedFUSELAGE HAS A BULGE AT BS 1010 BETWEEN STR 29R AND STR 30. REMOVED FASTENERS AT DAMAGED AREA BS 1010 STR 30 IAW B727-SRM 51-30-2 EVALUATED SKIN AND EXFOLIATED BEYOND LIMITS PER SRM 53-30-1 FIG 1 B727. CUT OUT DAMAGED AREA 3 1/2" BY 2 1/2" IAW B727 SRM 53-30Aug 13, 2005 · N748DH · Boeing 727225 · Fuselage Main, Plate/SkinSDR 05FDEA02423Transmitter · malfunctionedON TAKEOFF ROLL, NR 2 EPR WOULD NOT ADVANCE PAST 1.4. ALL OTHER ENG INDICATIONS WERE NORMAL. REMOVED AND REPLACED NR 2 ENGINE EPR TRANSMITTER IAW AMM 77-11-011-4. NO HELP. RAN NR 2 ENG TO MAX PWR AND EPR INDICATION WOULD GO TO 1.6 EPR AND DROP TO 1.4 EPR WAug 11, 2005 · N466FE · Boeing 727225 · Engine Pressure Ratio (EPR)SDR DHL2005748503Stringer · corrodedAFT CARGO COMPT LOWER FUSELAGE STR 29L IS CORRODED BETWEEN STA 970 AND STA 990. REMOVED STR 29L KEEL BEAM CHORD FROM BS 950-1010 DRILLED AND LOCATED NEW KEEL BEAM CHORD P/N 65-56441-7 PO NR 53143 IAW S/B 727-53-179 FIG 12 TREATED AND PRIMED AREA AND CHORD IAWAug 7, 2005 · N748DH · Boeing 727225 · Fuselage Main, Longeron/StringerSDR DHL2005748502Skin · bulgedLOWER FUSELAGE AT APPROX STA 950E BELOW AFT CARGO DOOR HAS RIVET HEAD CORRODED OFF AND BULGE IN SKIN. REMOVED STR 29R KEEL BEAM CHORD FROM BS 950 TO BS 1010 REMOVED CORR AND CLEANED AREA BELOW STR 29R FROM SKIN MAT LOSS .007 AT BS 950E ORIGINAL THICKNESS .135Aug 7, 2005 · N748DH · Boeing 727225 · Fuselage Main, Plate/SkinSDR CA050713005Forging · crackedDURING SCHEDULED MLG REPLACEMENT, THE RETRACTION ACTUATOR END CAP FORGING WAS FOUND CRACKED, AND BROKE APART ON REMOVAL OF THE ACTUATOR. PRIOR TO THE GEAR CHANGE THERE WAS NO INDICATIONS OF ANY RETRACTION OR EXTENSION PROBLEMS. THE NATURE OF THE INSTALLATION Jul 6, 2005 · Boeing 727225 · Landing Gear ActuatorSDR 72400003Seat Track · corroded1 X 1 AREA OF CORROSION SEAT TRACK.Jun 20, 2005 · N724CK · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR 72400002Frame · cracked1 INCH CRACK ON FRAME REPLACEMENTJun 19, 2005 · N724CK · Boeing 727225 · Fuselage Main, FrameSDR 72400001Frame · cracked2 INCH CRACK ON FUSE FRAME CHORD REPLACEMENTJun 19, 2005 · N724CK · Boeing 727225 · Fuselage Main, Frame
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