N752DH

Service difficulty reports · 115

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 = 'N752DH' AND registry_match = 'registration'
  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 DHLA2008752001Skin · crackedNR 3 K-FLAP HAS TWO SEPARATE CRACKS AT BOTTOM CENTER JUST ABOVE BULLNOSE APPROX WS 171.5. REMOVED AND REPLACED NR 3 K-FLAP OPERATIONAL CHECK GOOD. IAW M/M 27-81-01.Nov 21, 2008 · N752DH · Boeing 727223 · Leading Edge DevicesSDR DHLA200800127Light · malfunctionedL1 DOOR EMERGENCY EXIT LIGHT REMAINS ON WHEN SWITCH IS IN THE OFF POSITION.Nov 15, 2008 · N752DH · Boeing 727223 · Emergency LightingSDR DHLA20087521022BWedge · delaminatedRIGHT WING INBD T/E FLAP ASSY MID FLAP T/E HAS AREA OF DELAMINATION AT OUTER T/E. 337 FILED AND MP9 FILED NR 26945. ALL REPAIR WORK COMPLIED WITH IAW BOEING SRM 51-40-20 PARA 7, 8, 10, 14, 20, 22. REMOVED DAMAGED AREA APPROX 4 INCH BY 4 INCH AND FABRICATED Oct 22, 2008 · N752DH · Boeing 727223 · Trailing Edge FlapsSDR DHLA20087521022AWedge · delaminatedLEFT WING INBD T/E FLAP ASSY INBD MID FLAP T/E APPROX 64 INCHES FROM OUTBOARD EDGE HAS AREA OF DELAMINATION AT PREVIOUS REPAIR. 337 FILED AND MP9 NR 26944 FILED. ALL REPAIR WORK COMPLIED WITH IAW BOEING SRM 51-40-20 PARA 7, 8, 9, 10, 14, 20, 22. AREA OF DAMOct 22, 2008 · N752DH · Boeing 727223 · Trailing Edge FlapsSDR DHLA200800075Battery Pack · inoperativeEMERGENCY ENT LIGHTS INSIDE LIGHT INOP. REMOVED AND REPLACED BATTERIES IN LIGHT PACK, OPS CHECK GOOD IAW MM 33-50-71. FLT 119. A/C WAS GROUNDED. (A)Jun 17, 2008 · N752DH · Boeing 727223 · Emergency LightingSDR DHLA200800050Actuator · leakingFLIGHT 1612 ON TAKEOFF ROLL, A/C SUSTAINED HYD A-SYSTEM FAILURE PRIOR TO 60 KIAS. FOUND NR 5 KRUEGER FLAP LEAKING. REMOVED AND REPLACED NR 5 KRUEGER FLAP ACTUATOR. SERVICED A-SYS. INSP NR 1 & 2 CASE DRAIN FILTERS. OPS CHECK GOOD. NO FURTHER LEAKS NOTED. Jun 1, 2008 · N752DH · Boeing 727200 · Leading Edge Slat ActuatorSDR DHL2008752511Skin · crackedNR 3 NOSE COWL O/B T/E SKIN CRACKED ABOVE COWL LATCH. INSTALLED REPAIR IAW B727 SRM 54-30-2 FIG 1.Feb 26, 2008 · N752DH · Boeing 727223 · Engine Cowling SystemSDR DHL2008752609Skin · crackedNR 3 NOSE COWL O/B T/E SKIN CRACKED ABOVE COWL LATCH. INSTALLED REPAIR IAW B727 SRM 54-30-2 FIG 1.Feb 26, 2008 · N752DH · Boeing 727223 · Engine Air Intake SystemSDR DHL2008752509Flap · delaminatedRT INBD MIDFLAP HAS DELAM AT LOWER OUTBD TRAILING EDGE (AT WBL 238.0). CUT OUT DELAMINATED AREA ON RT I/B MIDFLAP APPROX 1.5 INCH DIAMETER APPLIED POTTING COMPOUND AND CURED AND SANDED SMOOTH. FABRICATED DOUBLER APPROX 3.5 DIAMETER FROM 7075T6 .020 PO NR 728Feb 23, 2008 · N752DH · Boeing 727223 · Trailing Edge FlapsSDR DHL2008752508Rib · crackedNR 1 SLAT ACTUATOR INBD ATTACHING RIB (AT SLAT) CRACKED. REMOVED RIB AND "U" CHANNEL FOUND CRACK IAW B727SRM 51-30-2 LOCATED, DRILLED AND DEBURRED RIB P/N 65-17327U3 PO 7375239 IAW B727 SRM 51-30-5. FABRICATED CHANNEL USING 2024-T3 .071 PO 9005922 DIM 6.5 INFeb 23, 2008 · N752DH · Boeing 727223 · Leading Edge DevicesSDR DHL2008752606Attach Fitting · crackedNR 1 SLAT ACTUATOR INBD ATTACHING RIB (AT SLAT) CRACKED. REMOVED RIB AND "U" CHANNEL FOUND CRACK IAW B727 SRM 51-30-2. LOCATED, DRILLED AND DEBURRED RIB P/N 65-17327U3 PO 7375239 IAW B727 SRM 51-30-5. FABRICATED CHANNEL USING 2024-T3 .071 PO 9005922 DIM 6.5Feb 23, 2008 · N752DH · Boeing 727223 · Wing, Attach FittingsSDR DHL2008752607Attach Fitting · crackedNR 1 SLAT ACTUATOR INBD ATTACHING RIB (AT SLAT) CRACKED. REMOVED RIB AND "U" CHANNEL FOUND CRACK IAW SRM 51-30-2. LOCATED, DRILLED AND DEBURRED RIB IAW SRM 51-30-5. FABRICATED CHANNEL IAW BDW NR 65-17327 AND SRM 51-20-01, 51-20-2, 51-30-5. INSTALLED RIB ANFeb 23, 2008 · N752DH · Boeing 727223 · Leading Edge DevicesSDR DHL2008752506Frame · dentedAFT PIT STA1130 HAS DENT IN RADIUS OF FRAME AT S-26L. CUTOUT DAMAGED AREA AT AFT CARGO COMP STA 1130 STR 26L DIMENSION 3/4 INCH BY 1/2 INCH IAW B727SRM 51-40-3 FIG 1. FABRICATED FRAME REPAIR MATERIAL USED 7075-O .071 PO NR 9006377 DIMENSION 9" BY 4" IAW B727Feb 8, 2008 · N752DH · Boeing 727223 · Fuselage Main, FrameSDR DHL2008752512Angle · crackedRT WING I/B L/E AREA AT FSS 107.2 FWD WING SPAR TERMINAL JOINT ANGLE CRACK AT BOTTOM. STOP DRILLED CRACK DIM .250 IAW B727 SRM 51-10-1 HFEC VERIFIED THAT CRACK END ON STOP DRILL HOLE IAW B727 NDTM PT6 51-00-00 FIG 23. FABRICATED NEW ANGLE USING 7075-T6 .063 Feb 8, 2008 · N752DH · Boeing 727223 · Wing Miscellaneous StructureSDR DHL2008752505Frame · dentedAFT PIT STA1130 HAS DENT IN RADIUS OF FRAME AT S-26L. CUTOUT DAMAGED AREA AT AFT CARGO COMP STA 1130 STR 26L DIMENSION 3/4 INCH BY 1/2 INCH IAW B727SRM 51-40-3 FIG1. FABRICATED FRAME REPAIR MATERIAL USED 7075-O .071 PO NR 9006377 DIMENSION 9 INCH BY 4 INCH IFeb 8, 2008 · N752DH · Boeing 727223 · Fuselage Main, FrameSDR DHL2008752610Spar · crackedRT WING INBOARD L/E AREA AT FSS 107.2 FWD WING SPAR TERMINAL JOINT ANGLE CRACK AT BOTTOM. STOP DRILLED CRACK DIM .250 IAW B727 SRM 51-10-1. HFEC VERIFIED THAT CRACK END ON STOP DRILL HOLE IAW B727 NDTM PT6 51-00-00 FIG 23. FABRICATED NEW ANGLE USING 7075-T6Feb 8, 2008 · N752DH · Boeing 727223 · Wing SparSDR DHL2008752603Frame · dentedAFT PIT STA1130 HAS DENT IN RADIUS OF FRAME AT S-26L. CUTOUT DAMAGED AREA AT AFT CARGO COMP STA 1130 STR 26L DIMENSION 3/4" BY 1/2" IAW B727 SRM 51-40-3 FIG 1. FABRICATED FRAME REPAIR MATERIAL USED 7075-O .071 PO NR 9006377 DIMENSION 9 INCH BY 4 INCHES IAW BFeb 8, 2008 · N752DH · Boeing 727223 · Fuselage Main, FrameSDR DHL2008752604Frame · dentedAFT PIT STA1130 HAS DENT IN RADIUS OF FRAME AT S-26L. CUTOUT DAMAGED AREA AT AFT CARGO COMP STA 1130 STR 26L DIMENSION 3/4" BY 1/2" IAW B727 SRM 51-40-3 FIG 1. FABRICATED FRAME REPAIR MATERIAL USED 7075-O .071 PO NR 9006377 DIMENSION 9" BY 4" IAW B727 SRM 51Feb 8, 2008 · N752DH · Boeing 727223 · Fuselage Main, FrameSDR DHL2008752510Skin · delaminatedLT OB AILERON TAB UPPER SURFACE HAS DELAMINATED AREA. CUTOUT DELAMINATED AREA 2 INCHES DIA ON LT O/B AIL TAB UPPER SURFACE. FABRICATED FILLER AND DOUBLER IAW B727SRM 57-50-2, BONDED FILLER AND DOUBLER IAW B727SRM 51-40-20.Feb 6, 2008 · N752DH · Boeing 727223 · Aileron TabsSDR DHL2008752507Structure · crackedLT WING UPPER T/E WBL 320 NR 4 SPOILER INBOARD CENTER HINGE CUTOUT IS CRACKED FWD. REMOVED FASTENERS AT LT WING UPPER T/E WBL 320 NR 4 SPOILER INBOARD CENTER HINGE CUTOUT IAW B727SRM 51-30-2. STOP DRILLED 0.250" DIA AT END OF CRACK IAW B727 SRM 57-30-4 FIG 1Feb 6, 2008 · N752DH · Boeing 727223 · Wing Miscellaneous StructureSDR DHL2008752608Skin · delaminatedLT OB AILERON TAB UPPER SURFACE HAS DELAMINATED AREA. CUTOUT DELAMINATED AREA 2 INCHES DIA ON LT O/B AILERON. TAB UPPER SURFACE FABRICATED FILLER AND DOUBLER IAW B727 SRM 57-50-2, BONDED FILLER AND DOUBLER IAW B727SRM 51-40-20.Feb 6, 2008 · N752DH · Boeing 727223 · Aileron TabsSDR DHL2008752605Skin · crackedLT WING UPPER T/E WBL 320 NR 4 SPOILER INBOARD CENTER HINGE CUTOUT IS CRACKED FWD. REMOVED FASTENERS AT LT WING UPPER T/E WBL 320 NR 4 SPOILER INBOARD CENTER HINGE CUTOUT IAW B727 SRM 51-30-2. STOP DRILLED 0.250" DIA AT END OF CRACK IAW B727 SRM 57-30-4 FIG Feb 6, 2008 · N752DH · Boeing 727223 · Wing, Plate/SkinSDR DHL2008752502Structure · crackedRT WING NR 5 L/E SLAT WING L/E I/B BULKSEAL HAS SURFACE CRACKED. REMOVED FASTENERS AT RT WING NR 5 L/E SLAT WING L/E I/B BULK SEAL IAW SRM 51-30-2. STOP DRILLED 0.250 AT END OF CRACK IAW SRM 51-10-1. FABRICATED DOUBLER REPAIR AT L/E SLAT MATERIAL USED 2024TFeb 4, 2008 · N752DH · Boeing 727223 · Leading Edge DevicesSDR DHL2008752504Web · crackedLT SIDE OF AIRSTAIR WEB CRACKED AT LIGHTING HOLE BS 1223. CUTOUT DAMAGED AREA AT LT SIDE OF AIRSTAIR WEB SAT 1223 IAW SRM 51-40-2 FIG 1. FABRICATED DOUBLER MAT USED 7075T6 0.032 DIMENSION 2.5 INCH BY 2.5 INCH PO NR 9006457 IAW SRM 51-40-2 FIG 1 AND SRM 53-10Feb 4, 2008 · N752DH · Boeing 727223 · Entrance StairsSDR DHL2008752503Structure · crackedRT WING NR 5 L/E SLAT WING L/E I/B BULKSEAL HAS SURFACE CRACKED. REMOVED FASTENERS AT RT WING NR 5 L/E SLAT WING L/E I/B BULK SEAL IAW SRM 51-30-2. STOP DRILLED 0.250 AT END OF CRACK IAW SRM 51-10-1. FABRICATED DOUBLER REPAIR AT NR 5 L/E SLAT MATERIAL USED Feb 4, 2008 · N752DH · Boeing 727223 · Leading Edge DevicesSDR DHL2008752501Structure · crackedRT WING NR 5 L/E SLAT WING L/E I/B BULKSEAL HAS SURFACE CRACKED. REMOVED FASTENERS AT RT WING NR 5 L/E SLAT WING L/E I/B BULK SEAL IAW SRM 51-30-2. STOP DRILLED 0.250 AT END OF CRACK IAW SRM 51-10-1. FABRICATED DOUBLER REPAIR AT L/E SLAT MATERIAL USED 2024TFeb 4, 2008 · N752DH · Boeing 727223 · Leading Edge DevicesSDR DHL2008752570Structure · crackedRT WING NR 5 L/E SLAT WING L/E I/B BULKSEAL HAS SURFACE CRACKED. REMOVED FASTENERS AT RT WING NR 5 L/E SLAT WING L/E I/B BULK SEAL IAW B727 SRM 51-30-2. STOP DRILLED 0.250 AT END OF CRACK IAW B727 SRM 51-10-1. FABRICATED DOUBLER REPAIR AT L/E SLAT MATERIAL Feb 4, 2008 · N752DH · Boeing 727223 · Leading Edge DevicesSDR DHL2008752550Structure · crackedRT WING NR 5 L/E SLAT WING L/E I/B BULKSEAL HAS SURFACE CRACKED. REMOVED FASTENERS AT RT WING NR 5 L/E SLAT WING L/E I/B BULK SEAL IAW B727 SRM 51-30-2. STOP DRILLED 0.250 AT END OF CRACK IAW B727 SRM 51-10-1. FABRICATED DOUBLER REPAIR AT L/E SLAT MATERIAL Feb 4, 2008 · N752DH · Boeing 727223 · Leading Edge DevicesSDR DHL2008752500Structure · crackedRT WING NR 5 L/E SLAT WING L/E I/B BULKSEAL HAS SURFACE CRACKED. REMOVED FASTENERS AT RT WING NR 5 L/E SLAT WING L/E I/B BULK SEAL IAW B727 SRM 51-30-2. STOP DRILLED 0.250 AT END OF CRACK IAW B727 SRM 51-10-1. FABRICATED DOUBLER REPAIR AT L/E SLAT MATERIAL Feb 4, 2008 · N752DH · Boeing 727223 · Leading Edge DevicesSDR DHL2008752602Web · crackedLT SIDE OF AIRSTAIR WEB CRACKED AT LIGHTING HOLE BS 1223. CUTOUT DAMAGED AREA AT LT SIDE OF AIRSTAIR WEB STA 1223 IAW SRM 51-40-2 FIG1. FABRICATED DOUBLER IAW SRM 51-40-2 FIG1 AND SRM 53-10-2 FIG 6. TREATED AND PRIMED AREA IAW SRM 51-10-2. INSTALLED DOUBLEFeb 4, 2008 · N752DH · Boeing 727223 · Fuselage Miscellaneous StructureSDR DHL2008752600Slat · crackedRT WING NR 5 L/E SLAT WING L/E I/B BULKSEAL HAS SURFACE CRACKED. REMOVED FASTENERS AT RT WING NR 5 L/E SLAT WING L/E I/B BULK SEAL IAW SRM 51-30-2. STOP DRILLED 0.250 AT END OF CRACK IAW SRM 51-10-1. FABRICATED DOUBLER REPAIR AT L/E SLAT MATERIAL USED 2024TFeb 4, 2008 · N752DH · Boeing 727223 · Wing, Plate/SkinSDR DHL2008752515Beam · crackedRT WING T/E UPPER "J" BEAM IS CRACKED AT WBL 118. ACCOMPLISHED REPAIR TO CRACKED RT WING T/E UPPER "J" BEAM WBL 118. REPLACED MATERIAL USED J BEAM P/N BAC1506-860 7075T6 DIM 80.625" IAW EC-00795-001, DWG NR 65-21655 REV J DATED 12/4/78, B727 SRM 51-30-2.Feb 3, 2008 · N752DH · Boeing 727223 · Wing Miscellaneous StructureSDR DHL2008752513Angle · crackedCRACK AT RT MLG WHEEL WELL STATION 870 FWD INBD LWR BULKHEAD 18: LEFT OF LOAD CONTROL VALVE 8 INCHES RIGHT OF CENTER. REMOVED AND REPLACED ANGLE AT RT MLG W/W STA 870 FWD I/B LOWER BULKHEAD IAW B727SRM 51-30-2.Feb 3, 2008 · N752DH · Boeing 727223 · Fuselage Miscellaneous StructureSDR DHL2008752611Angle · crackedCRACK AT RT MLG WHEEL WELL STATION 870 FWD INBD LWR BULKHEAD 18: LEFT OF LOAD CONTROL VALVE 8" RIGHT OF CENTER. REMOVED AND REPLACED ANGLE AT RT MLG W/W STA 870 FWD INBOARD LOWER BULKHEAD IAW B727 SRM 51-30-2.Feb 3, 2008 · N752DH · Boeing 727223 · Fuselage Miscellaneous StructureSDR ASTAR20070014Switch · out of adjustWHEN THRUST LEVERS WERE BEING ADVANCED FOR T/O NR 3 ENG THRUST REVERSER LIGHT ILLUMINATED. REJECTED T/O AT ABOUT 20 KTS. PERFORMED RTO CHECKLIST AND ABNORMAL PROCEDURE. NORMAL OPERATION RESTORED. ADJUSTED NR 3 THRUST REV OPERATING LIGHT SWITCH IAW B727 MM Mar 21, 2007 · N752DH · Boeing 727223 · Engine Thrust ReverserSDR DHL2006752004Smoke Detector · malfunctionedNR 5 CARGO SMOKE DETECTOR ILLUMINATED IN FLIGHT. REMOVED AND REPLACED NR 5 SMOKE DETECTOR. OPS CK OF SMOKE DETECTOR SYS CKS GOOD IAW MM 26-13-00, NO EVIDENCE OF FIRE DETECTED.Nov 29, 2006 · N752DH · Boeing 727223 · Smoke DetectionSDR DHL2006752Support · corrodedWHILE COMPLYING WITH THE VISUAL INSPECTION OF THE UPPER WING SURFACE A BULGE WAS NOTICED JUST AFT OF THE AFT SPAR CAP AT APPROX STA 523 ON THE RIGHT WING. AFTER FURTHER CHECKING THE STOP SUPPORT FOR THE SPOILERS WAS FOUND TO BE CORRODED. THE PART WAS REPLACEAug 31, 2006 · N752DH · Boeing 727223 · Wing Miscellaneous StructureSDR DHL2006752003Light · inoperativeL-1 EXIT LIGHT INOP. REMOVED EMERGENCY LIGHT ASSY. INSTALLED SERVICEABLE EMERGENCY LIGHT ASSY IAW ASTAR MM 33-50-00, OPS CHECK GOOD.Jun 30, 2006 · N752DH · Boeing 727223 · Emergency LightingSDR DHL2006752002Skin · dentedFOUND LEFT WING TEMP REPAIR ON LARGE DENT O/B OF INBD. LANDING LIGHT, BIRD STRIKE. REMOVED AND REPLACED L/W FIXED LEADING EDGE, FROM WS.130 TO WS.349, IAW B727 SRM 51-30-2. OPS CHECKED AND LEAKED CHECKED WING ANTI-ICE SYSTEM, NO LEAKS NOTED IAW B727 MM 30-1Mar 31, 2006 · N752DH · Boeing 727223 · Leading Edge DevicesSDR DHL2006752001Battery · inoperativeEMERGENCY EXIT LIGHTS DID NOT ILLUMINATE DURING STANDBY POWER CHECK. REMOVED AND REPLACED BATTERIES IN EMERGENCY EXIT ASSY. OPS CK NORMAL IAW M/M 33-50-101, P/N MISC-062.Mar 17, 2006 · N752DH · Boeing 727223 · Emergency LightingSDR DHL2006752515Rib · crackedFOUND NR 111086; REMOVED NR 1 SLAT O/B RIB WS 720 FOR ACCESS FOUND CRACK ON RIB. REMOVED NR 1 SLAT O/B RIB WS 720 IAW B727 SRM 51-30-2 AND FABBED RIB FROM 7075-0.040 SIZE 5.5 X 16 INCH PO 9001602 IAW B727 SRM 57-50-2 FIG 2. HEAT TREATED AND PRIMED RIB IAW B7Jan 14, 2006 · N752DH · Boeing 727223 · Wing, Rib/BulkheadSDR DHL2006752514Rib · crackedFOUND NR 111077; NR 2 SLAT, RIB NR 8 AT SLAT STA 180 IS CRACKED. REMOVED DAMAGED PART IAW B727 SRM 51-30-2 AND FABBED NEW RIB AREA NR 2 SLAT RIB NR 8 SLAT 180 DIM 16 X 5 INCH MAT USED 70750.0.40 PO 9001602 IAW B727 SRM 57-50-2 FIG 2 & 51-20-1. PART TREATED AJan 13, 2006 · N752DH · Boeing 727223 · Wing, Rib/BulkheadSDR DHL2006752513Rib · crackedFOUND NR 111076; NR 2 SLAT, RIB 7 SLAT STA 190 IS CRACKED. REMOVED DAMAGED PART IAW B727 SRM 51-30-2 AND FABBED NEW RIB AREA NR 2 SLAT RIB 7 SLAT STA 180 DIM 16 X 5 INCH MAT USED 7075.0:0.40 PO 9001602 IAW B727 SRM 57-50-2 FIG 2 & 51-20-1. PART TREATED AND PJan 13, 2006 · N752DH · Boeing 727223 · Leading Edge DevicesSDR DHL2006752512Skin · crackedNR 2 SLAT RIB NR 1 AT SLAT STA 234.0 IS CRACKED. REMOVED DAMAGED PART IAW B727 SRM 51-30-2 AND FABBED NEW RIB AREA NR 2 SLAT RIB NR 1 SLAT 180 DIM 16 BY 5 MAT USE 7075.0 0.40 PO 9001602 IAW B727 SRM 57-50-2 FIG NR 2 AND 51-20-1 PART TREATED AND PRIMED IAW B7Jan 13, 2006 · N752DH · Boeing 727223 · Leading Edge DevicesSDR DHL2006752511Hinge · crackedMCD HINGE CRACKED FROM AFT SECTION BS 650 NDT CONFIRMED. REMOVED AND REPLACED MCD AFT HINGE SECTION P/N MS20001-16-7200 PO 9002527 IAW B727 AEI M/M CHAPTER 25, FIG 5201B REV F DATED 01-22-2001. THIS REPAIR A CAT "A".Jan 13, 2006 · N752DH · Boeing 727223 · Fuselage, Door HingeSDR DHL2006572512Slat · crackedDISCREPANCY FOUND NR 111075; NR 2 SLAT RIB NR1 AT SLAT STA 234.0 IS CRACKED. REMOVED DAMAGED PART IAW SRM 51-30-2 AND FABBED NEW RIB AREA NR 2 SLAT RIB NR 1 SLAT 180 DIM 16 X 5 MAT USE 7075.0 0.40 PO 9001602 IAW SRM 57-50-2 FIG NR 2 AND 51-20-1 PART TREATEDJan 13, 2006 · N752DH · Boeing 727223 · Wing StructureSDR DHL2006572511Hinge · crackedFOUND NR 111073; MCD HINGE CRACKED FROM AFT SECTION BS 650 NDT CONFIRMED. REMOVED AND REPLACED MCD AFT HINGE SECTION P/N MS20001-16-7200 PO 9002527 IAW AEI M/M CHAPTER 25, FIG 5201B REV F DATED 01-22-2001. THIS REPAIR A CAT (A).Jan 13, 2006 · N752DH · Boeing 727223 · Electrical/Electronic Compartment DoorsSDR DHL2006752522Repair · noneFOUND NR 111057; ACCOMPLISH IDENTIFICATION OF EXISTING FUSELAGE SKIN REPAIR AT BS 1155 & BETWEEN STR 29R-30R. ACCOMPLISHED IDENTIFICATION OF EXISTING FUSELAGE SKIN REPAIR AT BS 1155 & BETWEEN STR 29R-30R. INSTALLATION PERFORMED IAW B727 SRM 53-30-3 FIG 3. VJan 10, 2006 · N752DH · Boeing 727223 · Standard Practices/StructuresSDR DHL2006752521Skin · unknownFOUND NR 111056; ACCOMPLISH IDENTIFICATION OF EXISTING FLUSH FUSELAGE SKIN REPAIR AT BS 499 & BETWEEN STR 19R-20R. ACCOMPLISHED IDENTIFICATION OF EXISTING FLUSH FUSELAGE SKIN REPAIR AT BS 499 & BETWEEN STR 19R-20R. INSTALLATION PERFORMED IAW B727 SRM 53-30-3Jan 10, 2006 · N752DH · Boeing 727223 · Fuselage Main, Plate/SkinSDR DHL2006752520Repair · noneFOUND NR 111055; ACCOMPLISH IDENTIFICATION OF EXISTING EXTERNAL FUSELAGE SKIN REPAIR AT BS 437 & STR 18R. ACCOMPLISHED IDENTIFICATION OF EXISTING EXTERNAL FUSELAGE SKIN REPAIR AT BS 437 & STR 18R. INSTALLATION PERFORMED IAW B727 SRM 53-30-3 FIG 3A. VERIFIEDJan 10, 2006 · N752DH · Boeing 727223 · Standard Practices/Structures
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