Boeing 727-228

Service difficulty reports · 1,323

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  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = '727228'
  ORDER BY difficulty_date DESC"

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SDR DHL2002727009Power Unit1) APU WOULD NOT PERFORM A FIRE TEST. 2) TROUBLESHOT SYSTEM AND FOUND APU OPERATING POWER UNIT FAULTY. REMOVED & REPLACED POWER UNIT AND OPS CHECKED, WITH NO DEFECTS, PER B727 MM 26-23-00.Aug 7, 2002 · N727DH · Boeing 727228 · Detection SystemSDR DHL2002721512Skin · dentedDURING C-CHECK, FOUND 2 DENTS ON SECTION 41 SKIN AT 6 O'CLOCK POSITION FWD OF FWD E/E BAY DOOR. CUT OUT SECTION OF DAMAGED FUSELAGE SKIN 6 O'CLOCK POSITION AT STA 186 FWD OF FWD E & E DOOR IAW B-727 SRM 53-30-3 FIG 4. REMOVED EXISTING FLUSH REPAIR FWD OF CUTAug 6, 2002 · N721DH · Boeing 727228 · Fuselage Main, Plate/SkinSDR DHL2002721505Skin · crackedDURING C-CHECK DISCREPANCY AS FOLLOWS, FUSELAGE SKIN CRACKED SECTION 41 LEFT SIDE BS 243 WL 215. CUTOUT CRACKED SECTION OF FUSELAGE SKIN IAW B-727 SRM 53-30-3. FABRICATED REPAIR DOUBLER IAW B-727 SRM 53-30-3 FIG 3 AND S/B 53-0183. INSTALLED DOUBLER AND FILLAug 6, 2002 · N721DH · Boeing 727228 · Fuselage Main, Plate/SkinSDR DHL2002721514Seat Track · corrodedDURING C-CHECK, CABIN SEAT TRACK AT LBL 45 IS CORRODED AT STA 1148 AND STA 1156. REMOVED CABIN SEAT TRACK SECTION FROM STA 1148 TO STA 1156-LBL 45 IAW B-727 SRM 51-30-2. FABRICATED NEW SECTION OF SEAT TRACK IAW B-727 SRM 53-10-5 FIG 1. INSTALLED NEW SEAT TRAug 5, 2002 · N721DH · Boeing 727228 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2002721508Seat Track · corrodedDURING C-CHECK, CABIN SEAT TRACK AT RBL 45 IS CORRODED AT STA 1177. REMOVED CABIN SEAT TRACK AT STA 1177 AND RBL 45 IAW B-727 SRM 51-30-2. FABRICATED NEW SEAT TRACK IAW B-727 SRM 53-10-5 FIG 1. INSTALLED SECTION OF SEAT TRACK IAW B-727 SRM 53-10-5 FIG 1.Aug 5, 2002 · N721DH · Boeing 727228 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2002721507Seat Track · corrodedDURING C-CHECK, CABIN SEAT TRACK AT LBL 24 IS CORRODED AT STA 1136 AND STA 1156. REMOVED CABIN SEAT TRACK SECTION IAW B 727 SRM 51-30-2. FABRICATED A NEW SECTION OF SEAT TRACK IAW B-727 SRM 57-10-5 FIG 1. INSTALLED NEW SEAT TRACK IAW B-727 SRM 53-10-5 FIG 1Aug 5, 2002 · N721DH · Boeing 727228 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2002721506Intercostal · corrodedDURING C-CHECK, CABIN INTERCOSTAL AT RBL 24 IS CORRODED AT STA 1148. REMOVED INTERCOSTAL AT STA 1148 AND RBL 24 IAW B-727 SRM 51-30-2. FABRICATED NEW INTERCOSTAL IAW B-727 SRM 53-10-5. INSTALLED NEW INTERCOSTAL AT STA 1148 RT FROM RBL 20 TO RBL 65 IAW B-727Aug 5, 2002 · N721DH · Boeing 727228 · Fuselage Miscellaneous StructureSDR DHL2002721501Stringer · corrodedDURING C-CHECK DISCREPANCY AS FOLLOWS, IN FWD CARGO AFT 640, STR 23R HAS CORROSION. REMOVED SECTION OF STRINGER. FABRICATED A NEW SECTION OF STRINGER IAW B-727 SRM 53-10-3 FIG 1 AND SRM 53-10-2. INSTALLED NEW STRINGER AND SPLICE IAW B-727 SRM 53-10-3 FIG 1.Aug 5, 2002 · N721DH · Boeing 727228 · Fuselage Main, Longeron/StringerSDR DHL2002721500Floor Support · crackedDURING C-CHECK, DISCREPANCY AS FOLLOWS, CRACK IN FLOOR SUPPORT UNDER (FWD) COCKPIT ENTRY FLOOR BETWEEN DOOR AND MANUAL EXTENSION PANELS. REMOVED CRACK FLOOR SUPPORT FROM COCKPIT FLOOR BETWEEN ENTRY DOOR AND MANUAL EXT PANELS IAW B-727 SRM 51-30-2. FABRICATEDAug 5, 2002 · N721DH · Boeing 727228 · Fuselage Miscellaneous StructureSDR DHL2002721518Frame · crackedDURING C-CHECK, LEFT WHEEL WELL CASTING FRAME BS 930 CRACKED. REMOVED CRACKED STA 930 FRAME LT. LOCATED AND DRILLED-UP NEW STA 930 FRAME LT. INSTALLED NEW STA 930 FRAME LT.Aug 3, 2002 · N721DH · Boeing 727228 · Fuselage Main, FrameSDR DHL2002721513Frame · crackedDURING C-CHECK, RT WHEEL WELL CASTING FRAME BS 930 CRACKED TO O/B FWD FLANGE, O/B AFT FLANGE ALSO I/B FLANGE. REMOVED CRACKED STA 930 FRAME RT. LOCATED AND DRILLED-UP NEW STA 930 FRAME R. INSTALLED NEW STA 930 FITTING RT.Aug 3, 2002 · N721DH · Boeing 727228 · Fuselage Main, FrameSDR DHL2002721510Pressure Panel · corrodedDURING C-CHECK, NOSE WHEEL WELL HORIZONTAL PRESS MID CHORD CORROSION AT APPROX STA 320 & 355 RT AT DOGHOUSE TO CATWALK JUST AFT OF RT NOSE TRUNNION. FOUND RT AND N/W/W PRESSURE WEB MID CHORD TO BE CORRODED BEYOND ALLOWABLE LIMITS AND REMOVED. LOCATED AND DRIAug 3, 2002 · N721DH · Boeing 727228 · Fuselage Main, BulkheadSDR DHL2002721007Light · defectiveS/O`S OVERHEAD TABLE LIGHT INOP, WHEN ADJUSTED SPARKS CAME OUT OF SOCKET. FOUND S/O'S FWD TABLE LIGHT SOCKET BROKEN. REPLACED S/O'S FWD TABLE LIGHT ASSEMBLY. OPS CHECK NORMAL. DURING START UP SMOKE APPEARED COMING FROM TABLE LIGHT AREA. TURNED OFF TABLE LJul 25, 2002 · N721DH · Boeing 727228 · Flight Compartment LightingSDR DHL2002721006Light · out of positionEMERGENCY EXIT LIGHT ABOVE ENTRY DOOR FELL OFF. REINSTALLED EMERGENCY EXIT LIGHT AS PER MAINTENANCE MANUAL 33-50-71. OPS CHECK GOOD.Jul 25, 2002 · N721DH · Boeing 727228 · Emergency LightingSDR DHL2002726003Smoke Detector · will not testNR 5 CABIN SMOKE DETECTOR WILL NOT TEST. REMOVED AND REPLACED LAMP TEST BULB OF DETECTOR 5R. OPS TEST GOOD IAW MM 26-17-00.Jul 24, 2002 · N726DH · Boeing 727228 · Smoke DetectionSDR DHL2002721005Battery · dischargedEMERGENCY EXIT LIGHT OVER AIRCRAFT ENTRY DOOR INOP DURING STANDBY POWER CHECK. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERIES, OPS CHECKS GOOD IAW B727 MM 33-50-71.Jul 21, 2002 · N721DH · Boeing 727228 · Emergency LightingSDR DHL2002721004Panel · bentOVERWING EMERGENCY EXIT DOOR PANEL IS BENT AT LOWER AFT CORNER. RESECURED INTERIOR EMERGENCY EXIT PANEL WITH GILLINER TAPE IAW B727 M/M 52-21-00, CHECKS GOOD.Jul 17, 2002 · N721DH · Boeing 727228 · Emergency ExitsSDR DHL2002721003Power Unit1) WHILE PERFORMING APU FIRE WARNING TEST APU BLT C/B POPPED. 2) R/R APU OPERATING POWER UNIT IAW WDM 49-41-01 APU FIRE WARNING GRD OP CK GOOD.Jul 16, 2002 · N721DH · Boeing 727228 · Detection SystemSDR DHL2002726002Smoke Detector · inoperativeNR 3 LEFT SMOKE DETECTOR WILL NOT TEST. RELAMPED DETECTOR TEST LOOP. OPS CHECK OK 26-16-0.Jul 3, 2002 · N726DH · Boeing 727228 · Smoke DetectionSDR DHL2002720003Connector · dirtyON PREFLIGHT, APU WILL NOT FIRE TEST. CLEANED ELECTRICAL CONNECTOR SENSOR/RESPONDER OPS. CHECKS NORMAL IAW DHL B727A MM 26-15-0.Jul 3, 2002 · N720DH · Boeing 727228 · Fire DetectionSDR DHL2002727008Light1) EMERGENCY EXIT LIGHT IN COCKPIT FELL AND BROKE.2) R&R EMERGENCY EXIT LIGHT ASSY. IAW BMM CH 33-50-01, OPS CK GOOD.Jul 2, 2002 · N727DH · Boeing 727228 · Emergency LightingSDR DHL2002720002Smoke Detector · will not testCOCKPIT TEST SMOKE NR 1 LEFT INOP. REMOVED AND REPLACED NR 1 LEFT SMOKE DETECTOR IAW B727 MM 26-16-01, OPS CHECKS NORMAL.Jun 20, 2002 · N720DH · Boeing 727228 · Smoke DetectionSDR DHL2002727006Battery Pack · out of positionCOCKPIT EMERGENCY EXIT LIGHT INOP. RERACKED BATTERY PACKED OPS CK GOOD MM 33-00.May 6, 2002 · N727DH · Boeing 727228 · Emergency LightingSDR DHL2002726520Skin · dentedDURING C-CHECK, NR 5 LEADING EDGE SLAT HAS A DENT AT SLAT AT STA 355. CUT OUT DENTED SECTION OF SLAT SKIN IAW B-727 SRM 57-50-1 FIG 1, FABRICATED REPAIR PARTS IAW B-727 SRM 57-50-3 FIG 1, AND INSTALLED DOUBLER AND FILLER REPAIR ON NR 5 LEADING EDGE SLAT IAW BMay 1, 2002 · N726DH · Boeing 727228 · Leading Edge DevicesSDR DHL2002726512Stringer · corrodedDURING C-CHECK, STRINGER 27R AT BS 710 HAS CORROSION. CUT OUT DAMAGED AREA IAW B-727 SRM 53-10-3 FIG 1. FABRICATED AND INSTALLED NEW STRINGER SECTIONS IAW SRM 53-10-2 FIG 9 SHEET 1.Apr 25, 2002 · N726DH · Boeing 727228 · Fuselage Main, Longeron/StringerSDR DHL2002727005Power Unit · malfunctionedAPU FIRE WARNING DOES NOT TEST. RERACKED APU FIRE DETECTION OPERATING POWER UNIT, OP'S CHECKED GOOD IAW B-MM 26-15-0.Apr 24, 2002 · N727DH · Boeing 727228 · Fire DetectionSDR DHL2002726517Floorbeam · corrodedDURING C CHECK, BS 930 FLOORBEAM IS EXFOLIATED ON THE AFT SIDE OF THE BEAM AT THE INTERSECTION WITH THE BS 930 LT FORGING LBL 62, WL 203. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW B-727 SRM 53-10-2 FIG 8 SHEET 3 DETAIL III. FABRICATED REPAIR PART IAW Apr 23, 2002 · N726DH · Boeing 727228 · Fuselage Main, Floor BeamSDR DHL2002726508Angle · corrodedDURING C CHECK, C-1 CARGO DOOR INTERIOR STRUCTURE, 10 ANGLE HAS SEVERE EXFOLIATION CORROSION. REMOVED ANGLE FROM C-1 DOOR INTERIOR STRUCTURE AND REPLACED IAW B-727 SRM 51-40-4. REMOVED ANGLE FROM C-1 DOOR INTERNAL STRUCTURE IAW B-727 SRM 51-30-2. REPLACED AApr 22, 2002 · N726DH · Boeing 727228 · Cargo/Baggage DoorsSDR DHL2002726515Tab · puncturedDURING C-CHECK, LT AND ELEVATOR CONTROL TAB SHOW PUNCTURED HOLE TOP SIDE STA 73.0 APPROX. CUT OUT PUNCTURED AREA ON LT ELEVATOR TAB, IAW B-727 SRM 55-20-1 FIG 1 AND 51-40-10 FIG 2. INSTALLED REPAIR IAW B-727 SRM 51-40-10 FIG 2. OPS CHECK GOOD IAW B-727 MM 2Apr 20, 2002 · N726DH · Boeing 727228 · Elevator, Tab StructureSDR DHL2002727004Battery Pack · not seatedMAIN ENTRY DOOR EMERGENCY EXIT LIGHT DIM. RESEATED BATTERY PACK IN EXIT LIGHT ASSY. OPS CHECKS NORMAL IAW B727 M/M CH 33-50.Apr 20, 2002 · N727DH · Boeing 727228 · Emergency LightingSDR DHL2002726519Doubler · crackedDURING C-CHECK, MCD AFT UPPER CORNER FRAME DOUBLER (INTERNAL) CRACKED, AS VIEWED THROUGH THE MCD UPPER AFT LIGHTENING HOLE. REMOVED AFT UPPER FRAME CORNER DOUBLER IAW B-727 SRM 51-30-2. FABRICATED AND INSTALLED PART IAW B-727 SRM.Apr 18, 2002 · N726DH · Boeing 727228 · Cargo/Baggage DoorsSDR DHL2002726506Cowling · crackedDuring C Check "discrepancy" as follows, #3 engine upper cowling gouged/chaffed on the #12 rib O/B section.Corrective action as follows,Cut-out damaged area on #3 engine cowl upper #12 rib I.A.W. B-727 SRM 54-10-2. Fabricated repair from 7075-T6 .050 P.O.# 991Apr 18, 2002 · N726DH · Boeing 727228 · Nacelle/Pylon, Main FrameSDR DHL2002726505Skin · damagedDURING C-CHECK, EXTERNAL FUSELAGE REPAIR AT BS 1223, STR 21R IS INSTALLED WITH BLIND FASTENERS. REMOVED REPAIR IAW B-727 SRM 51-30-2. FABRICATED AND INSTALLED NEW DOUBLER IAW B-727 SRM 51-30-2.Apr 18, 2002 · N726DH · Boeing 727228 · Fuselage Main, Plate/SkinSDR DHL2002726503Skin · crackedDURING C-CHECK, NR 1 ENGINE UPPER COWL SKIN IS CRACKED AT NR 3 LATCH. FABRICATED AND INSTALLED DOUBLER IAW B-727 SRM 51-30-2.Apr 18, 2002 · N726DH · Boeing 727228 · Engine Cowling SystemSDR DHL2002726502Plate · crackedDURING C-CHECK, NR 1 ENGINE LOWER COWL NR 5 O/B U-BOLT COVER PLATE IS CRACKED. REMOVED COVER PLATE. FABRICATED AND INSTALLED NEW PLATE IAW B-727 SRM 51-30-2.Apr 18, 2002 · N726DH · Boeing 727228 · Engine Cowling SystemSDR DHL2002726518Hinge · crackedDURING C-CHECK, MAIN CARGO DOOR HINGE (UPPER FUSELAGE SIDE) IS CRACKED, 2ND LOBE FROM AFT. VERIFIED BY HFEC. REMOVED CRACKED UPPER HINGE IAW B-727 SRM 51-30-2. INSTALLED NEW HINGE FOR MCD IAW PEMCO DWG 52-487-1.Apr 17, 2002 · N726DH · Boeing 727228 · Fuselage, Door HingeSDR DHL2002726516Stringer · crackedDURING C-CHECK, CABIN BS 720B STR 15 L IS CRACKED FWD OF WING LIGHT. FABRICATED NEW ANGLE CHANNEL AND DOUBLER IAW 53-10-3 FIG 5. INSTALLED NEW ANGLE CHANNEL IAW B-727 SRM 51-30-2 SRM 53-10-3 FIG 5. PRESSURE CHECK GOOD IAW B-727 21-30-0.Apr 17, 2002 · N726DH · Boeing 727228 · Fuselage Main, Longeron/StringerSDR DHL2002726514Panel · crackedDURING C-CHECK, NLG WW LT SIDEWALL PANEL IS CRACKED BS 290 WL 198 APPROX UNDERNEATH FITTING SUPPORT DOOR ACTUATOR 2 PLACES CRACKED (NDT CONFIRMED). ROUTED OUT CRACKED AREA. NDT INSP AROUND ROUTED OUT AREA PER NDT MANUAL, NO CRACKS NOTED. FABRICATED DOUBLER Apr 17, 2002 · N726DH · Boeing 727228 · Fuselage Miscellaneous StructureSDR DHL2002726511Pressure Panel · crackedDURING C-CHECK, NOSE WHEEL WELL L/SIDE WALL PANEL CRACKED BS 280 AND UPPER CHORD ANGLE SEEN FROM INSIDE (NDT VERIFIED). FABRICATED AND INSTALLED REPAIR PARTS IAW B-727 SRM 51-30-2.Apr 17, 2002 · N726DH · Boeing 727228 · Fuselage Main, BulkheadSDR DHL2002726513Rib · crackedDURING C-CHECK, RT WING FIXED L/E RIB HAS A CRACK AT WS 572. CUT OUT DAMAGED AREA IAW B-727 SRM 51-40-3. FABRICATED AND INSTALLED REPAIR IAW B-727 SRM 51-30-2 AND 51-40-3.Apr 16, 2002 · N726DH · Boeing 727228 · Wing, Rib/BulkheadSDR DHL2002726501Skin · dentedDURING C-CHECK, DENT ON C-1 DOOR SKIN AT BS 590, STR 20 R. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER IAW B-727 SRM 51-30-2.Apr 16, 2002 · N726DH · Boeing 727228 · Passenger/Crew DoorsSDR DHL2002726522Support · corrodedDURING C-CHECK, COCKPIT FLOOR STA 265 LBL 3, PANEL IN FLOOR BULGED WITH PULLING RIVETS AT I/B END OF F/E SEAT TRACK. REMOVED AND REPLACED F/E SEAT TRACK SUPPORT IAW B-727 SRM 51-30-5/ 51-30-8/ 51-30-2. BULGING FOUND TO BE CORROSION OF F/E SEAT TRACK SUPPORT.Apr 15, 2002 · N726DH · Boeing 727228 · Fuselage Miscellaneous StructureSDR DHL2002726521Door Frame · corrodedDURING C-CHECK, RT AND AFT EMERGENCY EXIT FUSELAGE CUTOUT LWR FWD CORNER INTERIOR EXFOLIATED CORROSION. REMOVED CORROSION ON RT AFT EMERGENCY EXIT LWR FWD CORNER IAW B-727 SRM 51-30-1. FOUND TO BE OUT OF LIMITS IAW B-727 SRM 53-30-1. FABRICATED AND INSTALLEApr 15, 2002 · N726DH · Boeing 727228 · Fuselage Main, StructureSDR DHL2002726510Pressure Panel · crackedDURING C-CHECK, NOSE WHEEL WELL LEFT SIDEWALL BULKHEAD BS 243, WL 150 CRACK INDICATION ABOUT 2.5 INCH LONG. NDT VERIFIED. CUT-OUT DAMAGED AREA. FABRICATED AND INSTALLED REPAIR PARTS IAW B-727 SRM 51-30-2.Apr 15, 2002 · N726DH · Boeing 727228 · Fuselage Main, BulkheadSDR DHL2002726509Skin · dentedDURING C-CHECK, VENTRAL STAIRS ASSY STA 1315 TO 1335, AFT EXT SKIN HAS 3 DENTS. FABRICATED AND INSTALLED DOUBLER REPAIRS.Apr 15, 2002 · N726DH · Boeing 727228 · Entrance StairsSDR DHL2002726504Pressure Panel · crackedDURING C-CHECK, RT NLG W/W FWD BULKHEAD LOWER I/B CORNER HAS 4 INCH CRACK. CUT OUT CRACKED WEB & INSTALLED A WEB REPAIR DOUBLER. CUT OUT CRACKED SECTION OF LOWER EXTRUSION ANGLE & INSTALLED AN EXTRUSION ANGLE REPAIR.Apr 15, 2002 · N726DH · Boeing 727228 · Fuselage Main, BulkheadSDR DHL2002726500Attach Fitting · crackedDURING C-CHECK, NR 2 ENGINE LT UPPER ENGINE MOUNT FITTING ATTACH ANGLE FITTING INSIDE (PANEL 5201) HAS A 3 INCH LONG CRACK. REMOVED AND REPLACED ATTACH FITTING IAW B-727 SRM 51-30-2. REMOVED AND REPLACED LT UPPER SUPPORT CHORD. REMOVED NR 2 ENGINE LT UPPER Apr 14, 2002 · N726DH · Boeing 727228 · Engine Mount SectionSDR DHL2002727003Door · jammedMAIN CABIN DOOR WILL NOT CLOSE. FREED JAMMED ENTRY DOOR AND OPERATED NORMALLY SEVERAL TIMES IAW M/M 52-00 INSPECTION REVEALED NO DISCREPANCIES WITH DOOR.Mar 28, 2002 · N727DH · Boeing 727228 · Passenger/Crew DoorsSDR DHL2002724003Bottle · dischargedAPU FIRE BOTTLE PRESSURE INDICATES 50 PSI. APU DEFERRED, PLACARD INSTALLED. REF: DMI 8873 APU FIRE BOTTLE PRESSURE INDICATES 50 PSI. REMOVED AND REPLACED APU FIRE BOTTLE. CHECKS GOOD. THIS CLEARS DMI 8873. PLACARD REMOVED.Mar 27, 2002 · N724DH · Boeing 727228 · Fire Bottle, FixedSDR DHL2002726001Windshield Wiper · out of adjustRIGHT WIPER DOES NOT FUNCTION. WINDSHIELD WIPER KNOB FELL OFF. REPLACED SET SCREWS IAW B727 M/M 30-42-01. RECLOCKED RIGHT WINDSHIELD WIPER IAW BMM 30-42-01, OPERATIONAL CHECK IS GOOD.Mar 16, 2002 · N726DH · Boeing 727228 · Windshield/Door Rain/Ice Removal
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