# Service difficulty reports: N752DH

A list on [N752DH](https://openairdocs.org/aircraft/N752DH.md).

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

Page 1 of 3 · 115 reports

- [SDR DHLA2008752001](https://openairdocs.org/sdr/DHLA2008752001.md): Skin · cracked · Nov 21, 2008 · N752DH · Boeing 727223 · Leading Edge Devices
  > NR 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.
- [SDR DHLA200800127](https://openairdocs.org/sdr/DHLA200800127.md): Light · malfunctioned · Nov 15, 2008 · N752DH · Boeing 727223 · Emergency Lighting
  > L1 DOOR EMERGENCY EXIT LIGHT REMAINS ON WHEN SWITCH IS IN THE OFF POSITION.
- [SDR DHLA20087521022B](https://openairdocs.org/sdr/DHLA20087521022B.md): Wedge · delaminated · Oct 22, 2008 · N752DH · Boeing 727223 · Trailing Edge Flaps
  > RIGHT 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
- [SDR DHLA20087521022A](https://openairdocs.org/sdr/DHLA20087521022A.md): Wedge · delaminated · Oct 22, 2008 · N752DH · Boeing 727223 · Trailing Edge Flaps
  > LEFT 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 DAM
- [SDR DHLA200800075](https://openairdocs.org/sdr/DHLA200800075.md): Battery Pack · inoperative · Jun 17, 2008 · N752DH · Boeing 727223 · Emergency Lighting
  > EMERGENCY 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)
- [SDR DHLA200800050](https://openairdocs.org/sdr/DHLA200800050.md): Actuator · leaking · Jun 1, 2008 · N752DH · Boeing 727200 · Leading Edge Slat Actuator
  > FLIGHT 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.
- [SDR DHL2008752511](https://openairdocs.org/sdr/DHL2008752511.md): Skin · cracked · Feb 26, 2008 · N752DH · Boeing 727223 · Engine Cowling System
  > NR 3 NOSE COWL O/B T/E SKIN CRACKED ABOVE COWL LATCH. INSTALLED REPAIR IAW B727 SRM 54-30-2 FIG 1.
- [SDR DHL2008752609](https://openairdocs.org/sdr/DHL2008752609.md): Skin · cracked · Feb 26, 2008 · N752DH · Boeing 727223 · Engine Air Intake System
  > NR 3 NOSE COWL O/B T/E SKIN CRACKED ABOVE COWL LATCH. INSTALLED REPAIR IAW B727 SRM 54-30-2 FIG 1.
- [SDR DHL2008752509](https://openairdocs.org/sdr/DHL2008752509.md): Flap · delaminated · Feb 23, 2008 · N752DH · Boeing 727223 · Trailing Edge Flaps
  > RT 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 728
- [SDR DHL2008752508](https://openairdocs.org/sdr/DHL2008752508.md): Rib · cracked · Feb 23, 2008 · N752DH · Boeing 727223 · Leading Edge Devices
  > NR 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 IN
- [SDR DHL2008752606](https://openairdocs.org/sdr/DHL2008752606.md): Attach Fitting · cracked · Feb 23, 2008 · N752DH · Boeing 727223 · Wing, Attach Fittings
  > NR 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 6.5
- [SDR DHL2008752607](https://openairdocs.org/sdr/DHL2008752607.md): Attach Fitting · cracked · Feb 23, 2008 · N752DH · Boeing 727223 · Leading Edge Devices
  > NR 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 AN
- [SDR DHL2008752506](https://openairdocs.org/sdr/DHL2008752506.md): Frame · dented · Feb 8, 2008 · N752DH · Boeing 727223 · Fuselage Main, Frame
  > AFT 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 B727
- [SDR DHL2008752512](https://openairdocs.org/sdr/DHL2008752512.md): Angle · cracked · Feb 8, 2008 · N752DH · Boeing 727223 · Wing Miscellaneous Structure
  > RT 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
- [SDR DHL2008752505](https://openairdocs.org/sdr/DHL2008752505.md): Frame · dented · Feb 8, 2008 · N752DH · Boeing 727223 · Fuselage Main, Frame
  > AFT 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 I
- [SDR DHL2008752610](https://openairdocs.org/sdr/DHL2008752610.md): Spar · cracked · Feb 8, 2008 · N752DH · Boeing 727223 · Wing Spar
  > RT 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-T6
- [SDR DHL2008752603](https://openairdocs.org/sdr/DHL2008752603.md): Frame · dented · Feb 8, 2008 · N752DH · Boeing 727223 · Fuselage Main, Frame
  > AFT 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 B
- [SDR DHL2008752604](https://openairdocs.org/sdr/DHL2008752604.md): Frame · dented · Feb 8, 2008 · N752DH · Boeing 727223 · Fuselage Main, Frame
  > AFT 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 51
- [SDR DHL2008752510](https://openairdocs.org/sdr/DHL2008752510.md): Skin · delaminated · Feb 6, 2008 · N752DH · Boeing 727223 · Aileron Tabs
  > LT 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.
- [SDR DHL2008752507](https://openairdocs.org/sdr/DHL2008752507.md): Structure · cracked · Feb 6, 2008 · N752DH · Boeing 727223 · Wing Miscellaneous Structure
  > LT 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 1
- [SDR DHL2008752608](https://openairdocs.org/sdr/DHL2008752608.md): Skin · delaminated · Feb 6, 2008 · N752DH · Boeing 727223 · Aileron Tabs
  > LT 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.
- [SDR DHL2008752605](https://openairdocs.org/sdr/DHL2008752605.md): Skin · cracked · Feb 6, 2008 · N752DH · Boeing 727223 · Wing, Plate/Skin
  > LT 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
- [SDR DHL2008752502](https://openairdocs.org/sdr/DHL2008752502.md): Structure · cracked · Feb 4, 2008 · N752DH · Boeing 727223 · Leading Edge Devices
  > RT 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 2024T
- [SDR DHL2008752504](https://openairdocs.org/sdr/DHL2008752504.md): Web · cracked · Feb 4, 2008 · N752DH · Boeing 727223 · Entrance Stairs
  > LT 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 53-10
- [SDR DHL2008752503](https://openairdocs.org/sdr/DHL2008752503.md): Structure · cracked · Feb 4, 2008 · N752DH · Boeing 727223 · Leading Edge Devices
  > RT 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
- [SDR DHL2008752501](https://openairdocs.org/sdr/DHL2008752501.md): Structure · cracked · Feb 4, 2008 · N752DH · Boeing 727223 · Leading Edge Devices
  > RT 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 2024T
- [SDR DHL2008752570](https://openairdocs.org/sdr/DHL2008752570.md): Structure · cracked · Feb 4, 2008 · N752DH · Boeing 727223 · Leading Edge Devices
  > RT 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
- [SDR DHL2008752550](https://openairdocs.org/sdr/DHL2008752550.md): Structure · cracked · Feb 4, 2008 · N752DH · Boeing 727223 · Leading Edge Devices
  > RT 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
- [SDR DHL2008752500](https://openairdocs.org/sdr/DHL2008752500.md): Structure · cracked · Feb 4, 2008 · N752DH · Boeing 727223 · Leading Edge Devices
  > RT 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
- [SDR DHL2008752602](https://openairdocs.org/sdr/DHL2008752602.md): Web · cracked · Feb 4, 2008 · N752DH · Boeing 727223 · Fuselage Miscellaneous Structure
  > LT 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 DOUBLE
- [SDR DHL2008752600](https://openairdocs.org/sdr/DHL2008752600.md): Slat · cracked · Feb 4, 2008 · N752DH · Boeing 727223 · Wing, Plate/Skin
  > RT 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 2024T
- [SDR DHL2008752515](https://openairdocs.org/sdr/DHL2008752515.md): Beam · cracked · Feb 3, 2008 · N752DH · Boeing 727223 · Wing Miscellaneous Structure
  > RT 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.
- [SDR DHL2008752513](https://openairdocs.org/sdr/DHL2008752513.md): Angle · cracked · Feb 3, 2008 · N752DH · Boeing 727223 · Fuselage Miscellaneous Structure
  > CRACK 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.
- [SDR DHL2008752611](https://openairdocs.org/sdr/DHL2008752611.md): Angle · cracked · Feb 3, 2008 · N752DH · Boeing 727223 · Fuselage Miscellaneous Structure
  > CRACK 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.
- [SDR ASTAR20070014](https://openairdocs.org/sdr/ASTAR20070014.md): Switch · out of adjust · Mar 21, 2007 · N752DH · Boeing 727223 · Engine Thrust Reverser
  > WHEN 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
- [SDR DHL2006752004](https://openairdocs.org/sdr/DHL2006752004.md): Smoke Detector · malfunctioned · Nov 29, 2006 · N752DH · Boeing 727223 · Smoke Detection
  > NR 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.
- [SDR DHL2006752](https://openairdocs.org/sdr/DHL2006752.md): Support · corroded · Aug 31, 2006 · N752DH · Boeing 727223 · Wing Miscellaneous Structure
  > WHILE 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 REPLACE
- [SDR DHL2006752003](https://openairdocs.org/sdr/DHL2006752003.md): Light · inoperative · Jun 30, 2006 · N752DH · Boeing 727223 · Emergency Lighting
  > L-1 EXIT LIGHT INOP. REMOVED EMERGENCY LIGHT ASSY. INSTALLED SERVICEABLE EMERGENCY LIGHT ASSY IAW ASTAR MM 33-50-00, OPS CHECK GOOD.
- [SDR DHL2006752002](https://openairdocs.org/sdr/DHL2006752002.md): Skin · dented · Mar 31, 2006 · N752DH · Boeing 727223 · Leading Edge Devices
  > FOUND 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 30-1
- [SDR DHL2006752001](https://openairdocs.org/sdr/DHL2006752001.md): Battery · inoperative · Mar 17, 2006 · N752DH · Boeing 727223 · Emergency Lighting
  > EMERGENCY 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.
- [SDR DHL2006752515](https://openairdocs.org/sdr/DHL2006752515.md): Rib · cracked · Jan 14, 2006 · N752DH · Boeing 727223 · Wing, Rib/Bulkhead
  > FOUND 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 B7
- [SDR DHL2006752514](https://openairdocs.org/sdr/DHL2006752514.md): Rib · cracked · Jan 13, 2006 · N752DH · Boeing 727223 · Wing, Rib/Bulkhead
  > FOUND 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 A
- [SDR DHL2006752513](https://openairdocs.org/sdr/DHL2006752513.md): Rib · cracked · Jan 13, 2006 · N752DH · Boeing 727223 · Leading Edge Devices
  > FOUND 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 P
- [SDR DHL2006752512](https://openairdocs.org/sdr/DHL2006752512.md): Skin · cracked · Jan 13, 2006 · N752DH · Boeing 727223 · Leading Edge Devices
  > NR 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 B7
- [SDR DHL2006752511](https://openairdocs.org/sdr/DHL2006752511.md): Hinge · cracked · Jan 13, 2006 · N752DH · Boeing 727223 · Fuselage, Door Hinge
  > 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 B727 AEI M/M CHAPTER 25, FIG 5201B REV F DATED 01-22-2001. THIS REPAIR A CAT "A".
- [SDR DHL2006572512](https://openairdocs.org/sdr/DHL2006572512.md): Slat · cracked · Jan 13, 2006 · N752DH · Boeing 727223 · Wing Structure
  > DISCREPANCY 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 TREATED
- [SDR DHL2006572511](https://openairdocs.org/sdr/DHL2006572511.md): Hinge · cracked · Jan 13, 2006 · N752DH · Boeing 727223 · Electrical/Electronic Compartment Doors
  > FOUND 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).
- [SDR DHL2006752522](https://openairdocs.org/sdr/DHL2006752522.md): Repair · none · Jan 10, 2006 · N752DH · Boeing 727223 · Standard Practices/Structures
  > FOUND 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. V
- [SDR DHL2006752521](https://openairdocs.org/sdr/DHL2006752521.md): Skin · unknown · Jan 10, 2006 · N752DH · Boeing 727223 · Fuselage Main, Plate/Skin
  > FOUND 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 53-30-3
- [SDR DHL2006752520](https://openairdocs.org/sdr/DHL2006752520.md): Repair · none · Jan 10, 2006 · N752DH · Boeing 727223 · Standard Practices/Structures
  > FOUND 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. VERIFIED

Next page: https://openairdocs.org/aircraft/N752DH/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/aircraft/N752DH/reports

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