N707DH, cancelled May 21, 2015

Service difficulty reports · 121

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N707DH' AND deregistration_id = 'N707DH-2015-05-21'
  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 DHL2002707003Accessory Unit · malfunctionedAFTER GEAR RETRACTION MOVED GEAR HANDLE TO OFF, GEAR DOOR LIGHT FORWARD PANEL AND RIGHT MAIN GEAR DOOR LIGHT S/O PANEL ILLUMINATED. MOVED GEAR HANDLE TO UP, LIGHTS OUT, HANDLE TO OFF, LIGHTS OUT NORMAL OPS. ACCOMPLISHED POWER OFF RERACK OF LDG ACCY UNIT, CLEApr 30, 2002 · N707DH · Boeing 72722 · Landing Gear Retraction/Extension SystemSDR DHL2002707002Switch · inoperativeFIRE ALARM BELL DOES NOT WORK FOR ANY ALARM FUNCTION. REMOVED AND REPLACED THE S41 CUTOFF SWITCH WITH SERVICEABLE SWITCH, OPS CHECK GOOD IAW BOEING WM 26-11-01.Jan 30, 2002 · N707DH · Boeing 72722 · Fire DetectionSDR DHL2002707001Sensor · failedAPU FIRE TEST INOP. REMOVED AND REPLACED FIRE DETECTOR SENSOR IAW DHL 727 MM 26-15-002. SYSTEM OPS CHECKED GOOD.Jan 22, 2002 · N707DH · Boeing 72722 · Fire DetectionSDR DHL2001707015Autopilot Sys · malfunctionedWHILE ON FINAL APPROACH COURSE WITH BOTH LOCALIZERS AND GLIDESLOPE INITIALLY CAPTURED ON AUTOPILOT, THE AUTOPILOT WAS NOT CAPABLE OF FLYING THE GLIDESLOPE. AIRCRAFT DOVE FOR THE GROUND. PERFORMED OPERATIONAL CHECK OF AUTOPILOT SYSTEM IAW 727 MM CH 22-00 AND Dec 14, 2001 · N707DH · Boeing 72722 · Autopilot SystemSDR DHL2001707014Windshield Wiper · out of adjRANGE OF MOTION ON WINDSHIELD WIPERS, BOTH CAPT AND F/O ARE INADEQUATE FOR NORMAL FIELD OF VISION (DO NOT COME UP HIGH ENOUGH). WINDSHIELD WIPERS NEED REPLACING (BLADES). TESTED AND ADJUSTED NR 1 AND NR 2 WIPER ASSB IAW 727 MM CHP 30-42. GROUND CKS NORMAL ADec 14, 2001 · N707DH · Boeing 72722 · Windshield/Door Rain/Ice RemovalSDR DHL2001707013Switch · inoperativeNOSE GEAR UNSAFE LIGHT DOES NOT ILLUMINATE DURING GEAR RETRACTION OR EXTENSION, LIGHT TEST OK. REMOVED NLG POSITION SWITCH AND LINKAGE PER M/M 32-61-71. INSTALLED NLG POSITION SWITCH IAW B727 MM 32-61-71. OPS CHECK GOOD.Sep 19, 2001 · N707DH · Boeing 72722 · Landing Gear Position and WarningSDR DHL2001707012Battery · dischargedEMERGENCY EXIT LIGHTS WILL NOT ILLUMINATE. REMOVED AND REPLACED BATTERIES IN EMERGENCY EXIT LIGHTS IAW B-M/M 33-50-71.Sep 15, 2001 · N707DH · Boeing 72722 · Emergency LightingSDR DHL2001707011Bulkhead · crackedON DROP IN CHECK, FWD CARGO COMPT, WING CENTER SECTION FWD BULKHEAD WEB CRACKED (APPROX 1 INCH) RBL 29 APPROX 14 INCHES ABOVE PRESS SPAL BETWEEN VERTICAL ROW OF FASTENERS. STOP DRILLED CRACK 2 PLACES IN FWD CARGO COMPL, WING CENTER SECTION FWD BULKHEAD WEB ATSep 1, 2001 · N707DH · Boeing 72722 · Fuselage Main, BulkheadSDR DHL2001707010Switch · malfunctionedNR 2 ENGINE OIL PRESSURE LIGHT CAME ON DIM DURING FLIGHT. COULD EXTINGUISH LIGHT BY RETARDING THRUST TO IDLE INITIALLY. BUT EVENTUALLY CAME ON AT IDLE. OIL TEMP READING 135. QUANTITY DECREASED FROM 4.2 GAL AT T/O. R&R MAIN OIL FILTER, FOUND SOME CARBON BB'S NOAug 4, 2001 · N707DH · Boeing 72722 · Engine Oil Indicating SystemSDR DHL2001707009Bleed Valve · failedT/O THRUST LEFT MANIFOLD DUCT PRESSURE ROSE TO 100PSI DEFERRED PER MAINT. CONTROL 36-11-1 MB. WHEN ATTEMPTING TO START ENGINES TO CHECK PRESSURIZATION, NR 1 ENG WOULD NOT START. NO DUCT PRESSURE DROP AND START VALVE OPEN LIGHT DID NOT ILLUMINATE. RESET C/B- Aug 4, 2001 · N707DH · Boeing 72722 · Compressor Bleed ValveSDR DHL2001707008Brake · malfunctionedAT 38 DEGREES C IN SMF, ANTI-SKID REPEATEDLY RELEASED AS T/O THRUST WAS SET WITH BRAKES ON. FORWARD MOVEMENT OF ACFT WAS MINIMAL. DID NOT OBSERVE RELEASE LIGHTS (DID NOT LOOK). ANTI-SKID NORMAL ON LANDING. ANTI-SKID SYS IS DEFERRED PER MEL32-5, ASSIGNED DMIJun 21, 2001 · N707DH · Boeing 72722 · Brake Anti-Skid SectionSDR DHL2001707007Autopilot Sys · malfunctionedWHEN OPERATING AUTOPILOT IN MANUAL MODE USING TURN MODE AUTOPILOT WILL NOT TURN RIGHT. ALL OTHER FUNCTIONS NORMAL. DEFFERED TO DMI 5936, PER MEL 22-1 CAT B, ITEM PLACARD. OPS CHECKED IAW MM 22-11-01, SYSTEM GROUND CHECKS GOOD. PER CREW COMMENT & B727 AUTO-Jun 8, 2001 · N707DH · Boeing 72722 · Autopilot SystemSDR DHL2001707006Computer · malfunctionedWITH AUTOPILOT IN AUTO G/S MODE, AND GLIDE SLOPE CAPTURED, THE AIRCRAFT PITCHES UP AND DOWN AND MAY OR MAY NOT RECOVER TO GLIDE PATH. REPLACED PITCH CHANNEL COMPUTER WITH A SERVICABLE UNIT IAW B727 M/M 22-11-121. CHECKS GOOD AT THIS TIME IAW B727 M/M 22-11-0May 19, 2001 · N707DH · Boeing 72722 · Autopilot ComputerSDR DHL2001707005Light · damagedRIGHT TAIL NAV LIGHT ASSY DAMAGED BY BAGGAGE CART. REPLACED RT WING TIP ASSY IAW MM 57-20-0. STATUS: CLOSED.Apr 10, 2001 · N707DH · Boeing 72722 · Exterior LightingSDR DHL2001707003Panel · debondedUPON ROUTINE A-CHECK INSPECTION, FOUND THE 10 FLIGHT SPOILER PANEL LOWER SKIN SEPARATED FROM PANEL. THE OUTBOARD EDGE WAS COMPLETELY OPEN AND APPEARED THAT SKIN BONDING HAD FAILED. WHEN ATTEMPTING TO MOVE THE PANEL BY HAND, THE PANEL WOULD BUCKLE UNDER PRESSMar 30, 2001 · N707DH · Boeing 72722 · SpoilersSDR DHL2001707002Fastener · looseDURING A/C RECEIVING INSPECTION FOUND LOOSE BLIND FASTENERS ON EXTERNAL SKIN REPAIR BS 218, STRINGER 25R. REMOVED EXTERNAL SKIN REPAIR AND BLIND FASTENERS. INSTALLED EXTERNAL REPAIR WITH SOLID FASTENERS AT BS 218, STRINGER 25R IAW B727 SRM 53-30-3.Feb 12, 2001 · N707DH · Boeing 72722 · Fuselage Main, StructureSDR DHL2001707001Motor · inoperativeCAPTS WINDSHIELD WIPERS INOP IN ALL SPEEDS. REMOVED AND REPLACED CAPTS WIPER MOTOR IAW MM 30-42-11.Feb 7, 2001 · N707DH · Boeing 72722 · Windshield/Door Rain/Ice RemovalSDR DHL2000707037Skin · damagedHOLE IN FUSELAGE, FWD RT SIDE OF NOSE, AFT OF RADOME. REPAIR SKIN USING PROCEDURES OUTLINED IN THE SRM 53-30-3 PG 74C -- 74F. THIS IS AN INTERM REPAIR.Sep 19, 2000 · N707DH · Boeing 72722 · Fuselage Main, Plate/SkinSDR DHL2000707031Turbine · failedNR 3 ENGINE FAILED ON T/O, ENGINE SHUT DOWN (POWER LOSS). EMERGENCY DECLARED, RETURNED TO BWI. INITIAL INSPECTION INDICATES TURBINE FAILURE.Aug 31, 2000 · N707DH · Boeing 72722 · Turbine SectionSDR DHL2000707032Engine · failedNR 3 ENG FAILED ON L/O. ENGINE SHUT DOWN, EMERGENCY WAS DECLARED AND RETURN TO BWI. A/C WAS FERRIED TO CVG FOR ENG CHANGE. REMOVED AND REPLACED NR 3 ENGINE.Aug 31, 2000 · N707DH · Boeing 72722 · Engine (Turbine/Turboprop)SDR DHL2000707030Indicator · failedREJECTED TAKE OFF, NO AIRSPEED INDICATION ON CAPTAIN SIDE.VERIFIED NO OBSTRUCTION IN CAPT PITOT.REMOVED AND REPLACED MACH AIR SPEED INDR.AND OPS CHKD IAW MM 34-11-10 AND 34-11-40.Jul 7, 2000 · N707DH · Boeing 72722 · Airspeed/Mach IndicatorSDR DHL2000707029Warning Light · illuminatedON TACK OFF ROLL THE RIGHT INBD MAIN LANDING GEAR ANTI-SKID LIGHT ILLUMINATED AT 60 KTS,REJECTED TAKE OFF. PLACED ON D M I PER MEL 32-05.Jul 7, 2000 · N707DH · Boeing 72722 · Brake Anti-Skid SectionSDR DHL200070729CPanel · chippedAT C CK; RT VERTICAL STAB PANEL 9604-HONEYCOMB SHOWING THRU AND CHIPPED SURFACE. INSTALLED FIBERGLASS CLOTH OVERLAY REPAIR PER B727 SRM 51-40-8 FIG. 1. PAINTED RH VERT STAB IAW B727 M/M 51-20-0. REF: N/R 4543.Jun 8, 2000 · N707DH · Boeing 72722 · Vertical Stabilizer, Plate/SkinSDR DHL200070728CSkin · delaminatedAT C CK; AFT CARGO DOOR MOVABLE FAIRING EXTERNAL SKIN HAS DELAMINATION ON DIFFERENT PLACES. INSTALLED FIBERGLASS OVERLAY REPAIR AFT CARGO DOOR FAIRING EXTERNAL SKIN PER B727 SRM 51-40-8 FIG. 1, PAINTED AS REQUIRED IAW B727 M/M 51-20-0. REF: N/R 3347.Jun 8, 2000 · N707DH · Boeing 72722 · Aerodynamic FairingsSDR DHL200070726CSupport Bracket · crackedFWD CARGO BAY, LT SIDE WALL SUPPORT, CRACKED STA 540 ABOVE STR 26 LT. REMOVED DAMAGED SECTION OF SIDE WALL LINER SUPPORT FROM STA 480 TO STA 530 ABOVE STR 26 LT. REPLACED SIDE WALL SUPPORT STA 480 STR 26L TO STA 530 STR 26 LT. TREATED AND PRIMED SIDE WALL SUPJun 1, 2000 · N707DH · Boeing 72722 · Fuselage Miscellaneous StructureSDR DHL200070733CTab · delaminatedAT C CK; LWR RUDDER TAB LWR LT & RT SURFACE DELAMINATED. ACCOMPLISHED FIBERGLASS CLOTH OVERLAY REPAIR PER B727 SRM 51-40-8 FIG 1. REF: N/R 4545.May 26, 2000 · N707DH · Boeing 72722 · Rudder, Tab StructureSDR DHL200070730CCowling · wornAT C CK; NR 2 ENGINE RT/AFT COWLING WORN AT LOWER SIDE OF NR 7 RIB. CUTOUT WORN AREA AT NR 2 ENGINE RT AFT COWLING AT RIB NR 7, 6 INCH X 1&1/8 INCH PER B727 SRM 51-30-2, FABRICATED AND INSTALLED DOUBLER REPAIR PER B727 SRM 54-10-3. REF: N/R 6142.May 26, 2000 · N707DH · Boeing 72722 · Engine Cowling SystemSDR DHL200070704CFitting · crackedFS 870 RT TERMINAL FITTING AT SPLICE FWD BETWEEN STR 9 & 10 SHOWS CRACK. REMOVED FASTENERS FWD OF SPLICE STA 870 RT STR 9 & 10. REMOVED FWD SPLICE FOR INSP SRM 51-30-2. FWD SPLICE AT 870 RT FWD SIDE CRACK COMING FROM LOWER HOLE FWD ROW OF SPLICE. ACCOMP HFMay 24, 2000 · N707DH · Boeing 72722 · Fuselage Miscellaneous StructureSDR DHL200070725CLap Joint · damaged1080 LAP JOINT HAS + 10 PERCENT INDICATION OF CORROSION BELOW S-2 LT, FROM LBL 13 TO 14 AFT OF AFT FASTNER ROW. REMOVED FASTENERS AND CUT OUT DAMAGED AREA OF AFT SKIN BS 1080 FROM STR 4 LT TO 4 RT, 1/4 IN X 4 1/8 IN. VISUAL INSPECTION FROM S 10 LT TO S 10 RTMay 23, 2000 · N707DH · Boeing 72722 · Fuselage Main, Plate/SkinSDR DHL200070711CAngle · brokenNR 2 ENGINE FWD MOUNTS REAR AREA BS 1400 APROX METAL ANGLE STRIP BROKEN. REMOVED AND REPLACED ANGLE STRIP PER SRM 51-30-2. TREATED AND PRIMED PER SRM 51-10-2.May 23, 2000 · N707DH · Boeing 72722 · Fuselage Miscellaneous StructureSDR DHL200070708CSkin · corroded1080 CIR JOINT HAS + 10 PERCENT CORROSION LOSS IND FROM LBL 7 AFT OF FASTENER ROW. REMOVED FASTENERS AND CUT OUT DAMAGED SECTION OF AFT SKIN BS 1080 FROM STR 4L TO STR 4R 59.25 X 4.125 PER S/B 727-53-0109. VISUAL INSP COMPLEATED FROM STA 102 TO 10R, NO FURTHMay 23, 2000 · N707DH · Boeing 72722 · Fuselage Main, Plate/SkinSDR DHL200070732CSkin · crackedAT C CK; CABIN SERVICE DOOR HAS CRACK ON EXTERNAL SKIN ON UPPER HINGE AREA. STOP DRILLED CRACK PER B727 SRM 51-10-1, PERFORMED HFEC PER NDT M/M 51-00-00 PART 6 FIG 4, NO CRACK INDICATIONS NOTED, INSTALLED DOUBLER REPAIR PER B727 SRM 51-40-2. (SIZE OF REPAIR-3 May 20, 2000 · N707DH · Boeing 72722 · Service DoorsSDR DHL200070720CDoubler · crackedCORRUGATED DOUBLER CRACKED AT T/E AREA L/W SPAR LOWER SECTION APPROX WS 546.5 (I/B SECTION OF STATION). STOP DRILLED CRACK AT CORRUGATED STRAP AT FT WING REAR SPAR AT WS 546.5 PER SRM 51-10-1. PERFORMED HFEC INSP PER NDT MAN PART 6-51-00-00 FIG 4. NO CRACK May 20, 2000 · N707DH · Boeing 72722 · Wing Miscellaneous StructureSDR DHL200070715CSkin · crackedCABIN SERVICE DOOR HAS CRACK ON EXTERNAL SKIN ON UPPER HINGE PANEL. STOP DRILLED CRACK AT CABIN SERVICE DOOR ON UPPER HINGE AREA PER SRM 51-10-1.PERFORMED HFEC INSP PER NDT MAN 51-00-00 FIG 4, NO CRACK INDICATION NOTED. INSTALLED DOUBLER REPAIR AT CABIN SERVMay 19, 2000 · N707DH · Boeing 72722 · Passenger/Crew DoorsSDR DHL200070724CPlate · crackedMAIN CARGO DOOR CUT OUT SCUFF PLATE AND ADJACENT COVER WORN AND CRACKED AT FWD LOWER CORNER. SMOOTHED OUT SCUFF PLATE AT CARGO DOOR, FWD LOWER CUT OUT AS PER SRM 51-10-1. MATERIAL LOST .003 INCH, WITHIN LIMITS IAW SRM 53-10-1. REMOVED AND REPLACED COVER PER SMay 18, 2000 · N707DH · Boeing 72722 · Fuselage Miscellaneous StructureSDR DHL200070723CSkin · crackedLT HORIZ STAB L/E SKIN HAS A CRACK AT RIVET HEAD STA 47.3. PERFORMED HFEC INSP AND CONFIRMED CRACK PER NDT MAN 51-00-00 PART 6 FIG 4. CUT OUT DAMAGED AREA 2.5 X 1.75 INCH PER SRM 55-10-3. APPLIED ALODINE AND PRIMER PER SRM 51-10-2. INSTALLED REPAIR AT LT HMay 18, 2000 · N707DH · Boeing 72722 · Horizontal Stabilizer, Plate/SkinSDR DHL200070707CFrame · crackedRT MAIN LANDING GEAR WING DOOR LOWER END FRAME IS CRACKED ON O/B BEND RADIUS AT FWD END. REMOVED CRACKED END FRAME AT RT MLG WING DOOR LWR END AS PER SRM 51-30-2. INSTALLED NEW END FRAME AT RT MLG WING DOOR LOWER END FWD SIDE PER SRM 51-30-2. TREATED AND PRMay 18, 2000 · N707DH · Boeing 72722 · Landing Gear DoorsSDR DHL200070706CSkin · corroded1808 CR JOINT HAS +10 PERCENT IND OF CORROSION BELOW S 2L FROM LBL 13 TO 14 AFT OF AFT FASTENER ROW. REMOVED FASTENERS AND CUT OUT DAMAGED SECTION OF SKIN BS 1080 FROM STR 4L TO 4R AS PER S/B 727-53-0109. VISUAL INSP ACCOMPLISHED, NO FURTHER CORROSION NOTED.May 18, 2000 · N707DH · Boeing 72722 · Fuselage Main, Plate/SkinSDR DHL200070703CSkin · corroded1080 CIR JOINT HAS 2090 CORR LOSS FROM S-8R TO S10R AFT OF AFT FASTENER ROW. REMOVED FASTNERS AND CUT OUT DAMAGED SECTION OF AFT SKIN 13S 1080 FROM STR 10R TO STR 4R 59 .375 X 4.125 AS PER S/B 53-0109 R 4. VISUAL INSP ACCOMP FROM 10L STRINGER TO 10R STRINGERMay 18, 2000 · N707DH · Boeing 72722 · Fuselage Main, Plate/SkinSDR DHL200070719CPanel · crackedNR 6 L/E SLAT ANTI-ICE TELOSCOPIC DUCT FAIRING PANEL CRACKED. REMOVED AND REPLACED ANTI ICE DUCT PANEL ON NR 6 L/E SLAT PER SRM 51-30-2. ALODINED AND PRIMED PER SRM 51-10-2.May 17, 2000 · N707DH · Boeing 72722 · Leading Edge DevicesSDR DHL200070718CSkin · scratchedRT WING UPPER SKIN HAS DEEP SCRATCH AT WS 546.5 APPROX. CUT OUT DAMAGED AREA AT L/E RT WING UPPER SKIN AS PER 727 SRM 57-30-4 FIG 2, CUT DIMENSIONS 4 X 2 IN. INSTALLED FLUSH REPAIR AT RT WING L/E AS PER SRM 57-30-4 FIG 2. ALODINED AND PRIMED AS PER SRM 51-1May 17, 2000 · N707DH · Boeing 72722 · Wing, Plate/SkinSDR DHL200070716CAngle · chafedAFT CARGO COMPT FLOORBEAM SUPPORT ANGLE IS WORN (CHAFED) ON TOP BS 111073 ABOVE STR 29R. CUT OUT DAMAGED AREA AT CARGO SUPPORT ANGLE AT AFT CARGO COMPT SUPPORT ANGLE AT BS 1110 STR 29R. CUT OUT SIZE 3 X 1 IN AS PER SRM 51-40-3. INSTALLED ANGLE REPAIR AT CARMay 17, 2000 · N707DH · Boeing 72722 · Fuselage Miscellaneous StructureSDR DHL200070710CRib · crackedTAIL CONE INTERIOR RIB CROSS SUPPORT ANGLE CRACKED. REMOVED FIBERGLASS RIB CROSS SUPPORT ANGLE AT TAIL CONE PER SRM 51-30-2. APPLIED FIBERGLASS CLOTH OVERLAY REPIAR TO INTERIOR RIB CROSS SUPPORT ANGLE PER SRM 51-40-8 FIG 1. INSTALLED RIB SUPPORT ANGLE PER SMay 17, 2000 · N707DH · Boeing 72722 · Aerodynamic FairingsSDR DHL200070702CRivet · looseNR 1 ENG, LWR COWLING SHOWS 8 WORKING RIVETS AT LOWER MID AREA. CUT OUT DAMAGED AREA 13.5 IN X 2.5 IN PER SRM 54-10-3 FIG 5. CLEANED, ALODINED AND PRIMED PER SRM 51-10-2. INSTALLED REPAIR PARTS PER SRM 54-10-3 FIG 5.May 17, 2000 · N707DH · Boeing 72722 · Engine Cowling SystemSDR DHL200070721CSlat Track · crackedTHE NR 2 SLAT O/B TRACK TO SLAT ATTACH CLIP IS CRACKED ON THE I/B RADIUS. REPLACED ATTACH CLIP AT NR 2 SLAT O/B TRACK TO SLAT PER SRM 51-30-2.May 16, 2000 · N707DH · Boeing 72722 · Leading Edge DevicesSDR DHL200070709CAngle · crackedLEFT W/W, VERT ANGLE BETWEEN BULKHEAD 870 AND KEEL BEAM HAS CRACK, FWD SIDE OF APU. VERIFIED CRACK PER NDT M/M PART 6-51-00 FIG 4. REMOVED VERT ANGLE PER SRM 51-30-2. INSTALLED NEW VERT ANGLE AT LEFT W/W PER SRM 53-10-2. ALODINED AND PRIMED PER SRM 51-10-2May 16, 2000 · N707DH · Boeing 72722 · Fuselage Miscellaneous StructureSDR DHL200070727CSkin · delaminatedLT HORIZONTAL STAB, ELEVATOR UPPER SURFACE, HAS SEVERAL AREAS DELAMINATED. OPENED ACCESS PANEL FOR EVALUATION. REMOVED LT HORIZONTAL STAB ELEVATER UPPER SKIN FROM STA 151.81 TO STA 188.65. INSTALLED PANEL SKIN.INSTALLED BALANCE PANEL SEALED PANEL REBALANCED ELMay 15, 2000 · N707DH · Boeing 72722 · Horizontal Stabilizer, Plate/SkinSDR DHL200070713CSeat Track · wornSEAT TRACK LBL 24 HAS LOCK LUG WORN STA 850. REMOVED SEAT TRACK PER SRM 51-30-2. INSTALLED NEW SEAT TRACK FROM STA 850 TO 870 PER SRM 53-10-5. ALODINED AND PRIMED PER SRM 51-10-2.May 15, 2000 · N707DH · Boeing 72722 · Fuselage, Seat/Cargo Attach FittingsSDR DHL200070712CSeat Track · wornSEAT TRACK AT LBL 45 HAS LOCK LUG WORN AT STA 860. REMOVED SEAT TRACK AT BS 860 LBL 45 PER SRM 51-30-2. INSTALLED SEAT TRACK SECTION PER M/M 53-4-0 AND SRM 51030-2. MATERIAL USED SEAT TRACK 91 IN 1778 T6 511. ALODINED AND PRIMED PER SRM 51-10-2.May 15, 2000 · N707DH · Boeing 72722 · Fuselage, Seat/Cargo Attach FittingsSDR DHL200070722CFairing · tornNR 7 FLAP JACKSCREW FAIRING TORN AT I/B EDGE, UPPER SURFACE. CUT OUT DAMAGED AREA AT NR 7 JACKSCREW FAIRING I/B EDGE PER SRM 51-40-2. MATRL LOSS .5 INCH. INSTALLED EXTERNAL DOUBLER PER SRM 51-4-02 FIG 1. ALODINED AND PRIMED AREA PER 51-10-2.May 13, 2000 · N707DH · Boeing 72722 · Wing Miscellaneous Structure
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