Boeing 727-30C

Service difficulty reports · 931

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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 = '72730C'
  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 DHL9970235CSkin · crackedC CHECK, RT WING O/B AILERON, I/B UPPER SKIN CRACKED AT I/B TAB BOND WIRE ATTACHMENT FASTENER. REMOVED AILERON TAB, CUT OUT DAMAGED AREA, INSTALLED DOUBLER REPAIR 5 BY 7 PER SRM 57-50-5. BALANCEED PER SRM 51-80-4. NO WEIGHT REQUIRED. N/R 2103.Jun 24, 1999 · N702DH · Boeing 72730C · Aileron TabsSDR DHL9970221CFitting · crackedC CHECK NR 6 SPOILER ACTUATOR SUPPORT FITTING IS CRACKED AT TOP FLANGE. CUT OUT DAMAGED AREAS I/B AND O/B SIDE OF NR 6 SPOILER ACT FITTING IAW AVITAS ENG. REPAIR ORDER NR 99AVHM .045R0-1 REV 1R SIZE OF CUT OUT 1 BY 1.5. EDDY CURRENT PER B727 NDT MAN. PART 6Jun 24, 1999 · N702DH · Boeing 72730C · Drag Control ActuatorSDR DHL9970216CAnge · crackedC CHECK, NR 2 ENG PYLON, ANGLE CRACKED AT AFT OF ENG-MOUNT. REMOVED ANGLE AT NR 2 ENG PYLON AT AFT OF ENG MOUNT IAW B727 SRM 51-30-2. REPLACED ANGLE AT NR 2 ENG PYLON AT AFT OF ENG MOUNT. MAT USES 7075-00. 050. PO NR 8315267 LO NR 219081 SIZED 8 BY 3 IAW B7Jun 24, 1999 · N702DH · Boeing 72730C · Nacelle/Pylon StructureSDR DHL9970245CWeb · corrodedC-CHECK, MAIN CABIN SHEAR WEB PLATE HAS CORROSION BELOW THE PLATE BS 1176 LBL 26. REMOVED FASTENERS ON HAT CHANNEL ANGLE AT BS 1176 LBL26 AS PER SRM 51-30-2. CUTOUT DAMAGE CORRODED AREA AS PER 727 SRM 51-40-2 SIZE CUT OUT 14 BY 15. INSTALLED A WEB REPAIR ASJun 23, 1999 · N702DH · Boeing 72730C · Fuselage Miscellaneous StructureSDR DHL9970242CBracket · crackedC-CHECK, RT WING T/E COVE PNL SUPPORT BRACKET CRACK AT FASTENER HOLE, I/B END OF NR 11 SPOILER PNL AND BELOW. REPLACED BRACKET AT I/B END OR NR 11 SPOILER PNL AS PER B77 SRM 51-10-1 PAR 4 AND 51-30-2. N/R 2083.Jun 23, 1999 · N702DH · Boeing 72730C · Wing Miscellaneous StructureSDR DHL9970234CPanel · crackedC CHECK, LW PANEL ON TOP WING HAS I/B SIDE WITH CRACK AND WORN, O/B SIDE OF NR 5 SPOILER. REMOVED CRACKED METAL STRIP ON L/W PANEL O/B OF NR 5 SPOILER PER B727 SRM 51-30-2. REPLACED METAL STRIP ON L/W PANEL O/B OF NR 5 SPOILER PER B727 SRM 51-40-2. TREATED Jun 23, 1999 · N702DH · Boeing 72730C · Wing, Plate/SkinSDR DHL9970229CSupport · crackedC CHECK, RT WING L/E STRUCTURE, CEILING CROSS SUPPORT CRACKED AT O/B END, L/E STA 130.7. REMOVED UNSERVICEABLE CROSS SUPPORT AND REPLACED WITH NEW EXTRUSION ANGLE AS PER B727 CHAP 51-30-2 MAT USED 7075-T6 .75 BY3.75 BY X 16 LOT NR 354192 PO NR 831451. ALODINJun 23, 1999 · N702DH · Boeing 72730C · Wing Miscellaneous StructureSDR DHL9970224CFitting · corrodedC-CHECK RT WING L/E FLAP NR 6, MIDDLE HINGE UPPER FITTING SUPPORT (MAGNESIUM) HAS SEVERAL AREAS OF CORROSION OR EROISION (MRKD). REMOVED UPPER HINGE FITTING AND ATTCH LINK FOR INC NR 6 L/E FLAP PER B727 SRM 51-30-2. INSTALLED UPPER HINGE FITTING AT RT L/E FLJun 23, 1999 · N702DH · Boeing 72730C · Leading Edge DevicesSDR DHL9970223CDoor · misrepairedC CHECK, FWD CARGO COMPARTMENT DOOR, IMPROPER REPAIR DOUBLER INSUFFICIENT AMOUNT OF FASTENERS AND IMPROPERLY COVERING AREA OF DAMAGE. FS 550 AFT BOTTOM SEEN THROUGH THE INSIDE. REMOVED AND REPLACED DAMAGE AREA AT FWD CARGO COMP DOOR AFT BOTTOM INTERIOR OF DOJun 23, 1999 · N702DH · Boeing 72730C · Cargo/Baggage DoorsSDR DHL9970222CSupport · crackedC CHECK, RT WING L/E STRUCTURE WBL 92.8 VERT SUPPORT CRACKED AT BOTTOM WITH SEVERAL STOP DRILLED HOLES. CUT OUT DAMAGED SECTON, INSTALLED ANGLE REPAIR 1 BY 1.5 BY 7 PER SRM 51-40-3, N/R 2055.Jun 23, 1999 · N702DH · Boeing 72730C · Wing Miscellaneous StructureSDR DHL9970210CDoubler · crackedC CHECK, FWD CARGO COMPARTMENT DOOR HAS A CRACKED DOUBLER AT THE AFT BOTTOM INTERIOR OF DOOR. THIS CAN BE SEEN WITH THE DOOR CLOSED AND INSIDE THE CARGO COMPARTMENT AT FS 560. REMOVED AND REPLACED DAMAGE AREA AT FWD CARGO COMP DOOR AFT BOTTOM INTERIOR OF DOORJun 23, 1999 · N702DH · Boeing 72730C · Cargo/Baggage DoorsSDR DHL9970207CSkin · corrodedC CHECK, LW L/B AFT FLAP HAS CORROSION AND DELAMINATION AT I/B SIDE TOP SKIN. CUT-OUT SMALL CORROSION AND DELAMINATION AREA AND INSTALLED FIBERGLASS OVERLAY REPAIR AT LW I/B AFT FLAP AS PER B727 SRV 51-40-8 FIG 1 MATERIAL USED RES 50-A HARDENER 946 BATCH NR AJun 23, 1999 · N702DH · Boeing 72730C · Trailing Edge FlapsSDR DHL9970206CSkin · corrodedC CHECK, LW NR 2 FLAP (1/B) HAS MID FLAP WITH CORROSION AND DELAMINATION ON TOP SKIN ON TOP OF SECOND TRACK FOR AFT FLAP. CUT-OUT SMALL CORROSION AND DELAMINATION AREA AND INSTALLED FIBERGLASS OVERLAY REPAIR AT LW NR 2 FLAP (I/B) MID FLAP PER BOEING 727 SRM 5Jun 23, 1999 · N702DH · Boeing 72730C · Trailing Edge FlapsSDR DHL9970205CFrame · crackedC CHECK, NR 2 ENG R4 FWD COWLING FRAME IS CRACKED AT NR 1 GUIDE AREA. CUT OUT DAMAGED SECTION, INSTALLED REPAIR DOUBLER PER SRM 51-40-3, 13 BY 5, N/R 6041.Jun 23, 1999 · N702DH · Boeing 72730C · Engine Cowling SystemSDR DHL9970201CCasting · crackedC-CHECK, GALLEY DOOR CUTOUT LOWER AFT CORNER CASTING HAS CRACK AND GOUGE. REPLACED CASTING AT DOOR CUT OUT LOWER AFT CORNER IAW B77 SRM 51-30-2, N/R 3121.Jun 23, 1999 · N702DH · Boeing 72730C · Fuselage Miscellaneous StructureSDR DHL9970243CSkin · crackedC-CHECK, NR 1 ENG INLET COWL CRACKED OUTER SKIN IN POSITION CRACK CONFIRMED BY NDT PART 6-51-00-00 HFEC JRT NDTI58. CUT OUT DAMAGED AREA ON NR 1 ENG NOSE COWL 17 AFT OF L/E AT 12:30 PR B727 SRM 54-30-3, 2.75 BY 8. PERFORMED HFEC INSP PER B7272 HDT MAN PART 6Jun 22, 1999 · N702DH · Boeing 72730C · Engine Cowling SystemSDR DHL9970238CAngle · crackedC-CHECK, NLG W/W AFT, SUPPORT ANGLE IS CRACKED AT STA 3441, ABOVE LOCK DOWN MECHANISM. REMOVED ANGLE, FOUND WEB CRACKED. CUT OUT DAMAGED AREA OF WEB, HFEC OF AREA. INSTALLED DOUBLER REPAIR PER SRM 51-40-2, 6 BY 7. REPLACED ANGLE PER SRM 51-30-2, 4 BY 12, NJun 22, 1999 · N702DH · Boeing 72730C · Fuselage Miscellaneous StructureSDR DHL9970237CSkin · damagedC-CHECK, AFT UPPER AIRSTAIRS WELL TOP TORQUE BOX SKIN IS OIL CAN BS 1285. CUT OUT DAMAGED AREA AT AFT UPPER AIRSTAIRS WELL, TOP TORQUE BOX SKIN. MAT CUT OUT 18 BY 20 AS PER B727 SRM 51-40-2. INSTALLED DOUBLER REPAIR AT AFT AIRSTAIR TORQUE BOX AREA TOP HORIZJun 22, 1999 · N702DH · Boeing 72730C · Fuselage Main, Plate/SkinSDR DHL9970236CSkin · damagedC-CHECK, RT UPPER AIRSTAIRS AREA, TOP TORQUE BOX SKIN IS OIL CAN BS 1263 TO 1243. CUT OUT DAMAGED AREA AT RT UPPER AIRSTAIR AREA TOP TORQUE BOX SKIN MAT CUT OUT 15 BY 4 AS PER B727 SRM 51-40-2. INSTALLED DOUBLER REPAIR AT UPPER AIRSTAIR AREA AT RT UPPER SKINJun 22, 1999 · N702DH · Boeing 72730C · Fuselage Main, Plate/SkinSDR DHL9970233CFloor · crackedC CHECK, AFT CARGO COMPARTMENT AFT BULKHEAD AREA BOTTOM OF CABIN FLOOR HAS AREA OF CORROSION AND A CRACK LEFT SIDE. REMOVED FASTENERS AFT CARGO AFT BULKHEAD BOTTOM AREA AS PER 727 SRM 51-30-2. CUT OUT DAMAGE CORRODED AREA AS PER 727 SRM 51-40-2 SIZE CUT OUT Jun 22, 1999 · N702DH · Boeing 72730C · Fuselage Floor PanelSDR DHL9970232CSeat Track · corrodedC-CHECK, AFT CARGO COMPT STA 1166 RT SEAT TRACK CRACKED. CUT OUT DAMAGED SECTION FROM STA 1166 TO 1130 AS PER B727 SRM 53-10-5 FIG 8. INSTALLED NEW SECTION OF SEAT TRACK FROM STA 1130 TO STA 1166 AND INSTALLED REPAIR PER B727 SRM 53-10-5 FIG 8 AT STA 1130 MAJun 22, 1999 · N702DH · Boeing 72730C · Fuselage, Seat/Cargo Attach FittingsSDR DHL9970231CSeat Track · corrodedC CHECK, AFT CARGO BIN SEAT TRACK CRACKED STA 970 RT SIDE. CUT AND TRIMMED NEW SECTION OF FLOOR TRACK, MADE SPLICE STRIPS, PICKED UP EXISTING FASTENER HOLES AND ADDED NEW ATTACH FASTENER HOLES, TREATED N/R 3096 AND PRIMED ALL NEW AND EXISTING PIECES IAW B727Jun 22, 1999 · N702DH · Boeing 72730C · Fuselage, Seat/Cargo Attach FittingsSDR DHL9970227CPanel · delaminatedC-CHECK, RT WING LOWER SURFACE ACCESS PANEL NR 8505 T/E DELAMINATED (MRK). REMOVED PANEL NR 8505 RT WING LOWER SURFACE FOR FIBERGLASS REPAIR IAW B727-200 12-30-0. INSTALLED BONDING REPAIR AT RT WING LOWER SURFACE ACCESS PANEL NR 8505 T/E AS PER B727 SRM 51-4Jun 22, 1999 · N702DH · Boeing 72730C · Wing, Plate/SkinSDR DHL9970220CFrame · crackedC CHECK, RIGHT SERVICE DOOR, THE DOOR FRAME HAS .5 INCH CRACK AREA OF FORWARD NR 2 STOP FROM THE BOTTOM. REMOVED RT SERVICE DOOR IAW B727 MM 52-40-0. INSTALLED RT SERVICE DOOR IAW B727 M/M 52-12-0. ADJUSTED RT SERV DOOR PER B727 M/M 52-12-0. LEAK OK IAW B7Jun 22, 1999 · N702DH · Boeing 72730C · Service DoorsSDR DHL9970213CSkin · crackedC CHECK, LT/W O/B UPPER T/E PANEL O/B OF NR 1 SPOILER, I/B EDGE OLD REPAIR HAS CRACK AT FASTENER HOLE WS620. REPLACED O/D REPAIR STRAP PR B727 SRM 57-30-4 FIG 10 MATL USED 040 2024T3 APPROX 2 BY 10 LOT NR 44044T25 PMS PO NR 8313480. ALODINED PRIMED TREATED AJun 22, 1999 · N702DH · Boeing 72730C · SpoilersSDR DHL9970209CSupport · damagedC CHECK, FAIRING SUPPORTS AT B5 600 AND 610 ARE BENT AND CRACKED AT LEFT SIDE STRINGER 281. CUT OUT DAMAGED RIB WEB INSTALLED REPAIR PER B727 SRM 51-40-2 AT BS 600 AND BS610 FAIRING SUPPORT MAT USED .040 2024T3 LOT NR 58599511 PMS PO NR 831125 2 PCS APPROX 6 Jun 22, 1999 · N702DH · Boeing 72730C · Fuselage Miscellaneous StructureSDR DHL9970208CDoor · delaminatedC-CHECK HYD COMPARTMENT B-SYSTEM DOOR IS DELAM. INSTALLED FIBRGLASS OVERLAY REPAIR AT HYD COMPARTMENT B SYSTEM DOOR AS PER B727 SRM 51-40-8 FIG 1 MATERIAL USED RESIR 50-A HARDENER 946 BATCH NR AK9CP8011K PO NR 8315299 PLUS FIBERGLASS CLOTH STYLE 7781 PO NR 93Jun 22, 1999 · N702DH · Boeing 72730C · Hydraulic Compartment DoorsSDR DHL9970241CSkin · corrodedC-CHECK, FUS EXTERIOR SKIN BULGED BS 1045 TO 1180 RT SIDE OF S DUCT. REMOVED PREVIOUS DBLR AT STR 4 RT BS 1100 TO 1180 FOR ACCESS TO BULGED AREA PER B727 SRM 51-30-2. CUT OUT DAMAGED AREA AT FUS EXTERIOR SKIN RT 1145 TO 1180 RT SIDE OF S-DUCT DAMAGED AT 4 BYJun 21, 1999 · N702DH · Boeing 72730C · Fuselage Main, Plate/SkinSDR DHL9970240CAngle · corrodedC-CHECK, RIGHT SIDE AIR CONDITIONING COMPARTMENT THROUGH GROUND AIR INLET DOOR AT STA 700 SUPPORT ANGLE FOR BODY FAIRING HAS CORROSION. CUT OUT DAMAGED AREA, INSTALLED ANGLE REPAIR, SUPPORT RIB, PER SRM 51-40-3, .75 BY 1.25 BY .75 LENGTH 10 AND DOUBLERS 2Jun 21, 1999 · N702DH · Boeing 72730C · Fuselage Miscellaneous StructureSDR DHL9970239CSkin · damagedC-CHECK, NR 3 ENG PYLON, UPPER FIXED COWL PANEL I/B OF UPPER MOUNT YOKE, DAMAGED AT UPPER FWD END. REPLACED DAMAGED ANGLE PER B727 SRM 51-40-3 FIG 1 & 54-10-2 ON NR 3 ENG PYLON UPPER FIXED COWL. I/B OF UPPER MOUNT YOKE AT UPPER FWD END. MAT USED 2024-0 .050 Jun 21, 1999 · N702DH · Boeing 72730C · Engine Cowling SystemSDR DHL9970230CSkin · gougedC CHECK, FUS EXTERIOR BS 970 S7L GOUGED SKIN. CUT OUT DAMAGES AREA OF SKIN AT STA 970 BETWEEN STR 6-72 3.0 BY 4.0 IAW 3727 SRM 53-30-3 FIG 1. INSTALLED DOUBLER REPAIR 12 BY 20 PER 13727 SRM 53-30-3 FIG 1 2024T3 .080 PO NR 8314392 LOT NR 362671. TREATED AND Jun 21, 1999 · N702DH · Boeing 72730C · Fuselage Main, Plate/SkinSDR DHL9970228CSupport · crackedC CHECK, LT/W L/E, NR 1 FLAP ACTUATOR FRONT SPAR ATTACH. O/B VERTICAL SUPPORT LWR FLANGE CRACKED STA 307. REMOVED LT/W, L/E NR 1 FLAP ACTUATOR FOR S/M REPAIR IAW B727 MM 27-81-22. REPLACED DAMAGED (CRKD) ANGLE LT/W AT 1 FLAP ACTUATOR FRONT SPAR ATTACH O/B SJun 21, 1999 · N702DH · Boeing 72730C · Leading Edge Slat ActuatorSDR DHL9970226CSupport · crackedC-CHECK, LT/W L/E, NR 1 SLAT ACTUATOR FRONT SPAR ATTACH I/B VERTICAL SUPPORT PREVIOUS REPAIR AT BOLT HOLE STH 734. REMOVED LT/W L/E NR 1 SLAT ACTUATOR FOR S/M REPAIR IAW B727 MM 27-81-32. REPLACED LT/W L/E NR 1 SLAT ACTUATOR FRONT STAR I/B VERTICAL SUPPORT PJun 21, 1999 · N702DH · Boeing 72730C · Leading Edge Slat ActuatorSDR DHL9970225CMount · crackedC CHECK, NR 1 SLAT ACTUATOR MOUNTS CRACKED. REMOVED NR 1 SLAT ACTUATOR FOR S/M REPAIR IAW B727 MM 27-81-32. REPLACED NR 1 SLAT ACTUATOR MOUNTS AS PER B727 SRM 51-30-02 AND SB727 57-0130 MATERIAL USED 7075-T6 .063 SIZE 10 BY 5 PO NR 8314735 LOT NR 64454495. RJun 21, 1999 · N702DH · Boeing 72730C · Leading Edge Slat ActuatorSDR DHL9970219CSkin · corrodedC-CHECK, FUS EXTERIOR SKIN BULGED BUTT JOINT 440 S2R. CUT OUT DAMAGED AREA, FROM STR 4L TO 4R, PERFORMED HFEC, VISUAL INSPECTED. PERFORMED INSURANCE CUT. INSTALLED REPAIR PARTS PER BOEING TELEX 32-9430, 5 BY 60, N/R 3027.Jun 21, 1999 · N702DH · Boeing 72730C · Fuselage Main, Plate/SkinSDR DHL9970212CWeb · crackedC-CHECK, NOSE WW HORIZ WEB CRACKED ABOVE RT GEAR DOOR FWD HINGE BS290R. REMOVED HORIZ WEB AT NOSE WW RT GEAR DOOR FWD HINGE AREA BS 290R AS PER B727 SRM 51-30-2. REPLACED ENTIRE WEB SECTION AT NOSE WW HORIZ WEB AREA ABOVE RT GEARDOOR FWD HINGE ARA BS 290R. Jun 21, 1999 · N702DH · Boeing 72730C · Fuselage Main, Plate/SkinSDR DHL9970204CInlet · crackedC CHECK, NR 1 ENG INLET, AFT FLANGE CRACKED, OUTBD AFT SIDE WHILE COWLING MATES TO INLET. CUT OUT DAMAGED AREA, INSTALLED DOUBLER REPAIR 8 BY 1 BY 1 FT PER SRM 51-40-2, N/R 6019.Jun 21, 1999 · N702DH · Boeing 72730C · Turbine Engine Air Inlet SectionSDR DHL9970218CWeight · crackedC CHECK, LT ELEVATOR TAB HAS BALANCE WEIGHTS CRACKED. REMOVED AND REPLACED LEFT ELEVATOR TAB WEIGHTS BALANCE AS PER S/B 727-55-0040 FIG NR 1, N/R 4004.Jun 20, 1999 · N702DH · Boeing 72730C · Elevator, Tab StructureSDR DHL9970217CWeight · crackedC-CHECK, RT ELEVATOR TAB HAS BALANCE WEIGHT CRACKED. REPLACED RT ELEVATOR TAB BALANCE WEIGHTS PER B727 SRM 51-10-1 PAR 5 AND B727 SRM 51-30-2 AND S/B 727 55-0040 FIG 1, N/R4005.Jun 20, 1999 · N702DH · Boeing 72730C · Elevator, Tab StructureSDR DHL9970202CSupport · crackedTWO CRACKS ON LEFT MLG DOOR ACTUATOR LINK SUPPORT MOUNTED AT THE 870 BULKHEAD, LB22. REMOVED CRACKED ANGLES. REPLACED 3 BRACKETS PER SRM 51-40-3, 8.5 BY 5.5 AND 5 BY 9, 4 BY 3.25, N/R 7032.Jun 19, 1999 · N702DH · Boeing 72730C · Landing Gear Door ActuatorSDR DHL9970215CHinge · crackedC CHECK, R MLG FUSELAGE DOOR FORWARD HINGE (MOUNTED TO KEEL BEAM) IS CRACKED AT FORWARD LOBE AFT CORNER. CRACK IS CONFIRMED BY NDT (MARKED). REMOVED AND REPLACED ON RT MLG FUS DOOR FWD HINGE AS PER B727 CHAP 51-30-2. N/R 7016.Jun 17, 1999 · N702DH · Boeing 72730C · Landing Gear DoorsSDR UPS99229833Light · missingINSPECTION TYPE:N/A, FLIGHT DECK EMERGENCY LIGHT MISSING. REPLACED EMERGENCY LIGHT PACK IAW MM 33-50-01, OPS CKS GOOD PER MM 33-50-01. (P/N 10-0067-9), (S/N 10894) INSTALLED.Jun 12, 1999 · N919UP · Boeing 72730C · Emergency LightingSDR UPS99229619Battery Pack · dischargedINSPECTION TYPE:N/A, COCKPIT EMERGENCY LIGHTS ABOVE DOOR INOP, FAILED TO TEST. REMOVED UNIT FROM A/C, PUT BATTERIES ON CHARGE, REINSTALLED BATTS IN A/C AND OPS OK.May 17, 1999 · N918UP · Boeing 72730C · Emergency LightingSDR UPS99229477Switch · out of adjustCARGO DOOR ANNUNCIATOR ILLUMINATED INLIGHT. AIRCRAFT PRESSURIZATION NORMAL. ATB 0245Z DOOR WARNING SYSTEM DEFERRED. CONTROL NR M171685, MEL 5-2-4. DOOR VISUALLY CHECKED BY RFD MX. AT SDF, ADJUSTED FWD CARGO DOOR SWITCH PER M/M 52-70-01. OPS CHECK NORApr 30, 1999 · N919UP · Boeing 72730C · Door Warning SystemSDR DHL9970153DFitting · crackedAT D-CHECK, LEFT WING O/B AILERON O/B HINGE FITTING CRACKED AT AFT UPPER END AT SKIN ATTACH FLANGE. REMOVED O/B HINGE FITTING AT LEFT WING PER SRM 51-30-2. REPLACED O/B HINGE FITTING PER SRM 57-30-2.Apr 16, 1999 · N701DH · Boeing 72730C · AileronsSDR UPS99229358Engine · malfunctionedINSPECTION TYPE:N/A ON TEST FLIGHT, PERFORMED TEST EVENT SHUT DOWN OF NR 2 ENGINE. ENGINE NR 2 WAS THEN RESTARTED WITH ALL PARAMETERS NORMAL. MINUTES LATER AS NR 2 ENGINE WAS ADVANCED TO CRUISE SETTING, ENGINE WOULD NOT RESPOND TO THROTTLE MOVEMENT. PRECAUTApr 15, 1999 · N906UP · Boeing 72730C · Engine (Turbine/Turboprop)SDR DHL9970165DStringer · crackedAT D-CHECK, EAR CRACKED ON AFT SIDE OF FWD VENT STRINGER WS 601. INSTALLED REPAIR PER S/B 57A159, 11 INCHES LONG.Apr 12, 1999 · N701DH · Boeing 72730C · Wing, Longeron/StringerSDR DHL9970162DBracket · crackedAT D-CHECK, BRACKET SUPPORT FOR AFT CARGO COMPT UP LATCH CRACKED. REMOVED BRACKET SUPPORT, REPLACED SUPPORT PER SRM 51-10-1, 17 X 7.Apr 12, 1999 · N701DH · Boeing 72730C · Fuselage Miscellaneous StructureSDR DHL9970112DSkin · dentedAT D-CHECK, FUSELAGE SKIN DENTED AT APPROX STA 1343 FROM STR 21R TO S-20R. CUT OUT DAMAGED AREA, INSTALLED DOUBLER REPAIR 12 X 8' PER SRM 53-30-3.Apr 8, 1999 · N701DH · Boeing 72730C · Fuselage Main, Plate/SkinSDR DHL9970105DFloorbeam · corrodedAT D-CHECK, FUSE FLOORBEAM CORRODED AT STA 380 BL 49L. CUT OUT FLOORBEAM TO LBL 49. CUT FLOORBEAM CAP OUT FROM LBL 12 TO O/B END. FABRICATED NEW FLOORBEAM TOP CAP WITH SPLICED DOUBLERS PER SRM 53-10-8, 59.5 LONG.Apr 6, 1999 · N701DH · Boeing 72730C · Fuselage Main, Floor Beam
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