# Service difficulty reports: N703DH, cancelled Jun 11, 2013

A list on [N703DH, cancelled Jun 11, 2013](https://openairdocs.org/deregistered/N703DH-2013-06-11.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 · 110 reports

- [SDR DHL2001703003](https://openairdocs.org/sdr/DHL2001703003.md): Switch · faulty · May 26, 2001 · N703DH · Boeing 72730C · Landing Gear Position and Warning
  > UPON FIRST GEAR EXTENSION INTO CVG NOSE GEAR GREEN LIGHT WAS INTERMITTENT. RECYCLED LANDING GEAR AND ALL INDICATIONS NORMAL. REMOVED AND REPLACED NOSE POSITION SWITCH IAW B727 MM 32-61-21, OPS CHECK OK.
- [SDR DHL2001703002](https://openairdocs.org/sdr/DHL2001703002.md): Indicator · inoperative · Mar 23, 2001 · N703DH · Boeing 72730C · Hydraulic Indicating System
  > A-SYSTEM HYDRAULIC QUANTITY INDICATOR INOP. PLACED ON DEFERRAL PER DMI 4858. MEL REF 29-14 CAT C.
- [SDR DHL2001703001](https://openairdocs.org/sdr/DHL2001703001.md): Skin · corroded · Feb 20, 2001 · N703DH · Boeing 72730C · Fuselage Main, Plate/Skin
  > STRINGER 19 RIGHT AT FS 369 TO FS 400 LAP SEAM HAS BULGING SKIN AROUND SEVERAL FASTENERS. CUT OUT DAMAGED AREA, INSTALLED DOUBLER AND FILLER 12.55 X 7.05 INCH DOUBLER. REWORKED LAP AT STA 360 TO 390 WORK DONE IAW SRM 53-30-3.
- [SDR DHL2000703007](https://openairdocs.org/sdr/DHL2000703007.md): Reservoir · low · Dec 19, 2000 · N703DH · Boeing 72730C · Hydraulic Reservoir, Main
  > DURING TAXI WITH FLAPS EXTENDED "A" HYD SYS QUANTITY DECREASED TO 1.9 GALLONS, ON RETURN TAXI QUANTITY INCREASED TO 2.4 GALS WITH FLAPS RETRACTED. C/W A VISUAL INSP OF THE WING FLAP SYS (NO EXTERNAL LEAKS NOTED) FOUND RESERVOIR QUANTITY LOW. SERVICED RESERV
- [SDR DHL2000703006](https://openairdocs.org/sdr/DHL2000703006.md): Tire · failed · Oct 31, 2000 · N703DH · Boeing 72730C · Tire
  > O/B LEFT MAIN TIRE BLOWN. REPLACED LEFT MAIN O/B AND I/B TIRES PER M/M 32-40.
- [SDR DHL2000703005](https://openairdocs.org/sdr/DHL2000703005.md): Adc · intermittent · Oct 6, 2000 · N703DH · Boeing 72730C · Air Data Computer
  > INTERMITTENT GYRO FLAG ON CAPTAINS ADI AND FLIGHT DIRECTOR FLAGS ON BOTH CAPTAINS AND F/OS. REMOVED AND REPLACED FLIGHT DIRECTOR COMPUTER.
- [SDR DHL2000703004](https://openairdocs.org/sdr/DHL2000703004.md): Gyro · failed · Oct 6, 2000 · N703DH · Boeing 72730C · Attitude Gyro and Indicating System
  > INTERMITTENT GYRO FLAG AND FLIGHT DIRECTOR FLAG. REMOVED AND REPLACED VERTICAL GYRO AND FLIGHT INSTRUMENT AMPLIFIER.
- [SDR DHL2000703003](https://openairdocs.org/sdr/DHL2000703003.md): Brake · malfunctioned · Sep 29, 2000 · N703DH · Boeing 72730C · Brake Anti-Skid Section
  > AFTER ROTATION PRIOR TO GEAR RETRACTION THE LEFT I/B AND RIGHT O/B ANTI SKID RELEASE LIGHTS ILLUMINATED. PLACED ANTI SKID SYS ON DMI 2456 PER MEL 32-5. TROUBLESHOT SYS PER M/M 32-42-0, SYS CHKS OK. SWAPPED TRANSDUCERS FOR T/S. TEST OK PER M/M 32-42-0.
- [SDR DHL2000703002](https://openairdocs.org/sdr/DHL2000703002.md): Bullet · contaminated · Sep 12, 2000 · N703DH · Boeing 72730C · Engine Pressure Ratio (EPR)
  > NR 3 ENGINE EPR READS HIGH N1 AND N2 LOW NR 3 THROTTLE 3 & 1/2 BEHIND NR 1 AND NR 2. BLEW DEBRIS FROM NR 3 BULLET. PERFORMED ENGINE RUN. OPS CHECK GOOD.
- [SDR DHLA200070301](https://openairdocs.org/sdr/DHLA200070301.md): Stringer · corroded · Aug 18, 2000 · N703DH · Boeing 72730C · Fuselage Main, Longeron/Stringer
  > FOUND LOCALIZED CORROSION AT STATION 650 STRINGER 18R IN LAP JOINT. INSTALLED FLUSH DOUBLER REPAIR ON LAP SEAM AT STR 18 RIGHT FROM BS 615 TO BS 621. REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 53-30-3 FIG 15A. MATERIAL USED 7075-T6 0.080 SIZED 14 X 4 INCHES
- [SDR DHL9970334C](https://openairdocs.org/sdr/DHL9970334C.md): Track · cracked · Aug 6, 1999 · N703DH · Boeing 72730C · Trailing Edge Flaps
  > AT C CHECK, NR 3 FLAP TRACK MOVABLE FAIRING O/B TRACK CRACKED. REMOVED AND REPLACED TRACK PER SRM 51-30-2, N/R 5107.
- [SDR DHL9970342C](https://openairdocs.org/sdr/DHL9970342C.md): Hinge Fitting · cracked · Jul 30, 1999 · N703DH · Boeing 72730C · Auxiliary Gear (Tail Skid)
  > AT C CHECK, RT TAIL SKID DOOR HINGE FITTING CRACKED. REMOVED AND REPLACED RT TAIL SKID DOOR HINGE FITTING PER SRM 51-30-2, N/R 3198.
- [SDR DHL9970341C](https://openairdocs.org/sdr/DHL9970341C.md): Hinge Fitting · cracked · Jul 30, 1999 · N703DH · Boeing 72730C · Auxiliary Gear (Tail Skid)
  > AT C-CHECK, LEFT TAIL SKID DOOR HINGE FITTING CRACKED. REMOVED AND REPLACED LEFT TAIL SKID DOOR HINGE FITTING AS PER SRM 51-30-2, N/R 3197.
- [SDR DHL9970336C](https://openairdocs.org/sdr/DHL9970336C.md): Bulkhead Skin · cracked · Jul 30, 1999 · N703DH · Boeing 72730C · Fuselage Main, Bulkhead
  > AT C CHECK, CRACK AT BS 1183 BULKHEAD SKIN AFT CARGO COMPT WL 182 LBL 15. REMOVED FASTENERS AND STOP DRILLED CRACK PER SRM 51-30-2, AND 51-10-1 PG NR 7. PERFOMRED HFEC INSPECT. NO CRACK IND PAST STOP DRILLS. CUT OUT DAMAGED AREA PER SB 727-53-0175. REMOVE
- [SDR DHL9970335C](https://openairdocs.org/sdr/DHL9970335C.md): Bulkhead Skin · cracked · Jul 30, 1999 · N703DH · Boeing 72730C · Fuselage Main, Bulkhead
  > C-CK, CRACK BS 1183 BULKHEAD SKIN, AFT BAG COMPT WL 182 RBL 15. OVERSIZED HOLE BY.015625 TO REMOVE INDAT WL190 RBL 15.5 AND ACCOMP PER SRM 51-10-1, VERIFIED CRACK NOT VISIBLE NDT PROCEDURE HFEC B727, PER NDT MANUAL PART 6510000 FIG 4. NO CRACK IND. DRILLED
- [SDR DHL9970348C](https://openairdocs.org/sdr/DHL9970348C.md): Bulkhead · damaged · Jul 29, 1999 · N703DH · Boeing 72730C · Fuselage Main, Bulkhead
  > AT C CHECK, REPLACED TEMP REPAIR WITH PERMANENT REPAIR BS 870 BULKHEAD WEB. REF: AVITAS ENG LETTER 98 PMS 1.213D-1. REMOVED TEMPORARY REPAIR AT BS 870. REMOVED OLD PRIMER AND PRC AROUND DAMAGED AREA. PERFORMED HFEC INSP OF STOP DRILL AT BS 870 AND WEB IAW N
- [SDR DHL9970347C](https://openairdocs.org/sdr/DHL9970347C.md): Skin · damaged · Jul 29, 1999 · N703DH · Boeing 72730C · Horizontal Stabilizer, Plate/Skin
  > AT C CHECK, LT INBD HORIZONTAL STABILIZER LEADING EDGE DAMAGED. REMOVED LEADING EDGE FOR APPROX STA 20 LE TO LE STA 147.32 PER SRM 51-30-2. REMOVED RIBS TO AID IN MAINTAINING CONTOUR OF LEADING EDGE IAW SRM 51-30-2. CUT OUT DAMAGED AREA AT LT LEADING I/B HO
- [SDR DHL9970344C](https://openairdocs.org/sdr/DHL9970344C.md): Angle · cracked · Jul 29, 1999 · N703DH · Boeing 72730C · Fuselage Miscellaneous Structure
  > C-CK, LT WING BS 930 LBL 64 VERT ANG CRACKED. R & R FITTING AT LT STA 930 LBL 64, ALOD & PRIM. INSTALL SPLICES STA 920 STR 15/16 RT. INSTALL REPAIR STR 14 & SUB FLOOR WEBS STA 930-940 & 920-930. REPLACED FLOOR PANEL, INSTALL LT W/W EMERG GEAR EXTEN AND FAS
- [SDR DHL9970328C](https://openairdocs.org/sdr/DHL9970328C.md): Bolts · cracked · Jul 27, 1999 · N703DH · Boeing 72730C · Leading Edge Devices
  > AT C CHECK, 2 EA SLAT ROLLER BOLTS CRACKED AT LUBE HOLE AND 6 EA SLAT ROLLER BOLTS WORN. REPLACED PER MM 27-81-11, N/R 2074.
- [SDR DHL9970329C](https://openairdocs.org/sdr/DHL9970329C.md): Skin · cracked · Jul 23, 1999 · N703DH · Boeing 72730C · Wing, Plate/Skin
  > AT C CHECK, RT WING FIXED LEADING EDGE CUT OUT FOR THE NR 5 SLAT INBD TRACK IS CRACKED. REMOVED SEALS TO GAIN ACCESS TO BACKSIDE OF LEAD EDGE OF WING PER SRM 57-30-4, MADE EXTERNAL DOUBLER PICKED UP EXISTING HOLES 2 EA NEW HLOES ONTO NEW DOUBLER PER SRM 57-30
- [SDR DHL9970330C](https://openairdocs.org/sdr/DHL9970330C.md): Hinge · cracked · Jul 22, 1999 · N703DH · Boeing 72730C · Spoilers
  > AT C CHECK, LW NR 7 SPOILER PANEL CENTER HINGE CASTING OUTBOARD LEG CRACKED AT AFT HOLE. CUT OUT CRACK FROM HINGE CASTING 2 LONG PER SRM 51-10-1, DYE PENETRANT INSPECTED CUTOUT PER MIL 68-66B. NO CRACK NOTED, INSTALLED FILLER AND REINFORCING STRAP AT LEFT WI
- [SDR DHL9970317C](https://openairdocs.org/sdr/DHL9970317C.md): Tail Cone · delaminated · Jul 22, 1999 · N703DH · Boeing 72730C · Aerodynamic Fairings
  > AT C CHECK, TAIL CONE HAS DELAMINATION AT LEFT TOP AREA. REMOVED VERTICAL STABILIZER TAILCONE PER SRM 51-30-2. INSTALLED FIBERGLASS OVERLAY REPAIR PER SRM 51-40-8 FIG 1, USED RESIN 50-A AND CLOTH STYLE 720 10 INCH BY 6 INCH, PRIMED ALL REAS PER SRM 51-10-2.
- [SDR DHL9970345C](https://openairdocs.org/sdr/DHL9970345C.md): Door · corroded · Jul 21, 1999 · N703DH · Boeing 72730C · Galley Doors
  > AT C CHECK, GALLEY DOOR UPPER FLAP HINGE HAS CORROSION. REMOVED GALLEY DOOR UPPPER FLAP PER MM 20-10-1. INSTALLED GALLEY DOOR UPPER FLAP (GATE ASSY) PER MM 52-12-0. REMOVED AND REPLACED PIN STOP ON GALLEY DOOR UPPER FLAP PER 52-12-0. SEALED OUTSIDE OF DOOR
- [SDR DHL9970332C](https://openairdocs.org/sdr/DHL9970332C.md): Bulkhead Panel · crushed · Jul 21, 1999 · N703DH · Boeing 72730C · Fuselage Main, Bulkhead
  > AT C CHECK, RT BS 1183 BULKHEAD PANEL IS CRUSHED AT LOWER END. REPLACED RT STA 1183 BLKHD PANEL PER 53-20-11 MATERIAL USED P/N AE4155-81162, APPROXIMATELY 7X4N/R 5118.
- [SDR DHL9970331C](https://openairdocs.org/sdr/DHL9970331C.md): Mount · cracked · Jul 21, 1999 · N703DH · Boeing 72730C · Engine Mount Section
  > AT C CHECK, ENGINE NR 1 GEARBOX FWD MOUNT CRACKED. REMOVED G/B PER MM-72-00, INSTALLED O/H G/B PER MM-72-0. INSTALLED FUEL LINE FROM FUEL OIL COOLER PER MM 28-40-3, LEAK CHECK, NO LEAK FOUND. OPS CHECKED ENGINE RUN AND TRIM, N/R 6179.
- [SDR DHL9970325C](https://openairdocs.org/sdr/DHL9970325C.md): Longeron · cracked · Jul 21, 1999 · N703DH · Boeing 72730C · Engine Cowling System
  > AT C CHECK, NR 1 LOWER COWL OUTBOARD LONGERON IS CRACKED UNDER RUB PLATE BY NR 3 LATCH V-BOLT CUTOUT. ALSO, SKIN IS BENT AND CRACKED AROUND CUTOUT. REWORKED SKIN AT NR 1 ENG LOWER COWL NR 3 LATCH U-BOLT CUT OUT PER SRM 51-10-1. NO SIGNIFICANT MATERIAL LOSS
- [SDR DHL9970320C](https://openairdocs.org/sdr/DHL9970320C.md): Skin · corroded · Jul 21, 1999 · N703DH · Boeing 72730C · Wing, Plate/Skin
  > AT CHECK, RT WING UPPER SURFACE SKIN BULGES ALONG ROW OF FASTENERS JUST FWD OF THE NR 8 SPOILER PANEL. REMOVED PANEL FOR REAIR, CLEANED MATING SURFACE ON WING, NO CORROSION NOTED, TREATED AND PRIMED AREA PER SRM 51-10-2. INSTALLED BONDED REPAIR AT R/WING UPP
- [SDR DHL9970319C](https://openairdocs.org/sdr/DHL9970319C.md): Bracket · cracked · Jul 21, 1999 · N703DH · Boeing 72730C · Cargo/Baggage Doors
  > AT C CHECK, FWD CARGO DOOR UPLOCK SUPPORT BRACKET IS CRACKED. REMOVED FWD CARGO DOOR UP LOCK SUPPORT BRACKET PER SRM 51-30-2. REPLACED FWD CARGO DOOR UPLOCK SUPPORT BRACKET PER SRM 51-30-2 AND 51-40-2, MATERIAL USED 2024T3.040 6 BY 3, ALODINED AND PRIMED PE
- [SDR DHL9970318C](https://openairdocs.org/sdr/DHL9970318C.md): Structure · cracked · Jul 21, 1999 · N703DH · Boeing 72730C · Passenger/Crew Doors
  > AT C CHECK, FWD ENTRY DOOR INTERIOR FWD UPPER CORNER IS CRACKED. REMOVED INTERIOR FWD ENTRY DOOR PER SRM 51-30-2, FABRICATED NEW LINER SUPPORT FWD CORNER PER SRM 52-10-1 FIG 1 USED.050 2024-0 HEAT TREATED TO 2024T3 PER 99PMSI 247 PG-01. ALODINED AND PRIMED P
- [SDR DHL9970316C](https://openairdocs.org/sdr/DHL9970316C.md): Fairing · delaminated · Jul 21, 1999 · N703DH · Boeing 72730C · Vertical Stabilizer
  > AT C CHECK, V STABILIZER HAS FAIRING DELAMINATED ON BOTH SIDES BELOW TAIL CONE. INSTALLED BONDING REPAIR AT VERTICAL STABILIZER FAIRINGS BELOW TAIL CONE PER SRM 51-20-3 FIG 1, MATERIAL USED EPOCAST 1652 A/B, N/R 4127.
- [SDR DHL9970314C](https://openairdocs.org/sdr/DHL9970314C.md): Cowl · chaff · Jul 21, 1999 · N703DH · Boeing 72730C · Fuselage Main, Longeron/Stringer
  > AT C CHECK, NR 1 TOP COWL OUTBOARD LONGERON HAS DEEP CHAFED SPOTS AT 46 AND 54 INCHES FROM AFT EDGE. REPLACED COLGERON SECTION PER SRM 51-40-2 AND 54-10-2 ON NR 1 TOP COWL, USED 2024T3.050 20 BY 4, TREATED AND PRIMED AREA PER SRM 51-10-2, N/R 6206.
- [SDR DHL9970313C](https://openairdocs.org/sdr/DHL9970313C.md): Skin · chafed · Jul 21, 1999 · N703DH · Boeing 72730C · Engine Cowling System
  > AT C CHECK, ENGINE NR 2 FWD RT COWL LOWER FWD INSIDE CORNER DOUBLER CHAFFED THROUGH. REMOVED FASTENER AND DAMAGED DOUBLER PER SRM 51-30-2, CLEANED AND PRIMED ARE PER SRM 51-10-2. REPLACED DOUBLER PER SRM 51-30-2 USED.040 14 BY 5 2024-0 HEAT TREATED TO 2024T
- [SDR DHL9970310C](https://openairdocs.org/sdr/DHL9970310C.md): Depressor · damaged · Jul 21, 1999 · N703DH · Boeing 72730C · Cargo/Baggage Doors
  > AT C CHECK, SEAL DEPRESSOR AT MCD AFT OF NR 6 LATCH HAS A SQUARE.25 OF MATERIAL MISSING REQUIRES REPAIR. SMOOTHED DAMAGED SECTION PER SRM 51-40-1. ALODINED AND PRIMED PER SRM 51-10-2. FABRICATED L ANGLE REPAIR PER SRM 51-40-3 FIG 1 USING.063 2024-0 HEAT T
- [SDR DHL9970308C](https://openairdocs.org/sdr/DHL9970308C.md): Panel · cracked · Jul 21, 1999 · N703DH · Boeing 72730C · Vertical Stabilizer, Plate/Skin
  > AT C CHECK, V STAB ACCESS PANEL NR 9774 HAS REPAIRS CRACKING UP L/S. INSTALLED FIBERGLASS OVERLAY REPAIR PER SRM 51-40-8 FIG 1 USING RESIN 1304, 6 INCH BY 4 INCH, N/R 4128.
- [SDR DHL9970305C](https://openairdocs.org/sdr/DHL9970305C.md): Fairing · corroded · Jul 21, 1999 · N703DH · Boeing 72730C · Wing Miscellaneous Structure
  > AT C CHECK, LEFT WING NR 1 MOVABLE FAIRING SKIN CORRODED AT FWD I/B SIDE AT FAIRING ATTACH POINT. REMOVED PAINT FROM SKIN CORRODED AREA PER MM 51-20-0, CUT 6 INCH BY 5 INCH SECTION OF SKIN AWAY AND INSTALLED REPAIR SKIN AND SPLICE PLATE PER SRM 53-50-1 FIG 1
- [SDR DHL9970340C](https://openairdocs.org/sdr/DHL9970340C.md): Carriage · loose · Jul 20, 1999 · N703DH · Boeing 72730C · Trailing Edge Flaps
  > LS NR 4 FLAP CARRIAGE HAS THRUST NUT LOOSE, IT HAS EXCESS CLEARANCE BETWEEN SHIMS AND FLAP FITTING. REMOVED LEFT INBOARD FLAP ASSY PER MM 27-51-3. FOUND LEFT INBOARD THRUST BEARING CASTING OUT OF LIMITS PER MM 27-51-3. REMOVED CARRIAGES FROM OLD FLAP AND TR
- [SDR DHL9970339C](https://openairdocs.org/sdr/DHL9970339C.md): Angle · cracked · Jul 20, 1999 · N703DH · Boeing 72730C · Wing Miscellaneous Structure
  > AT C-CHECK, LEFT WING LEADING EDGE CAVITY AREA FSS 115.0 VERTICAL ANGLE CRACKED LOSER SECTION. CUTOUT DAMAGED SECTION 3 BY 2 PER SRM 51-40-3. FABRICATED NEW VERTICAL ANGLE PER SRM 51-40-3 FIGURE 1, MATERIAL USED 7075-0.071 3 BY 8,.375 INCH, HEAT TREATED 7
- [SDR DHL9970327C](https://openairdocs.org/sdr/DHL9970327C.md): Skin · damaged · Jul 20, 1999 · N703DH · Boeing 72730C · Wing, Plate/Skin
  > AT C CHECK, LW TOP SKIN PANEL HAS FIBERGLASS REPAIR NOT FINISHED BETWEEN WING AND FUSELAGE. REMOVED LW TOP SKIN PANEL LOCATED BETWEEN WING AND FUSELAGE PER SRM 51-30-2. INSTALLED BONDED REPAIR AT LW TOP PANEL PER SRM 51-40-6 FIG 1 MAT USED 2024 T3.020, 202
- [SDR DHL9970326C](https://openairdocs.org/sdr/DHL9970326C.md): Stiffener · cracked · Jul 20, 1999 · N703DH · Boeing 72730C · Wing Miscellaneous Structure
  > AT C CHECK, LW VERT STIFFENER IS CRACKED AT LOWER END AT FALSE SPAR BELOW NR 5 SPOILER O/B SIDE. STOP DRILLED 1 CRACK PER SRM 57-50-6. REMOVED APPROX 6 OF FASTENERS PER SRM 57-50-6, MADE NEW L ANGLE DOUBLER PER SRM 57-50-6. PICKED UP EXISTING FASTENER HOLE
- [SDR DHL9970323C](https://openairdocs.org/sdr/DHL9970323C.md): Bolt · sheared · Jul 20, 1999 · N703DH · Boeing 72730C · Leading Edge Slat Actuator
  > AT C CHECK, LT WING NR 3 LE SLAT ACTUATOR TIE DOWN BOLT IB LOWER BOLT SHEARED. REPLACE THE IB LOWER BOLT ON NR 3 LE SLAT ACTUATOR PER MM 20-80-1, N/R 1199.
- [SDR DHL9970322C](https://openairdocs.org/sdr/DHL9970322C.md): Skin · corroded · Jul 20, 1999 · N703DH · Boeing 72730C · Trailing Edge Flaps
  > AT C CHECK, RT WING INBOARD FORE FLAP HAS SURFACE CORROSION ON LOWER SKIN APPROXIMATELY 12 FROM OUTBD END. REMOVED CORROSION AT RT WING PER SRM 51-10-6, OUT OF LIMITS PER SRM 57-50-1 FIG 3 DETAIL 3. INSTALLED FG OVERLAY REPAIR PER SRM 51-40-8 FIG 1 ON RT WIN
- [SDR DHL9970321C](https://openairdocs.org/sdr/DHL9970321C.md): Skin · delaminated · Jul 20, 1999 · N703DH · Boeing 72730C · Wing, Plate/Skin
  > AT C CHECK, RT WING UPPER SURFACE SKIN BULGES ALONG PANEL 10 FORWARD OF NR 9 AND NR 10 SPOILER PANEL. REMOVED FASTENERS AT RT WING PANEL PER SRM 51-30-2. FOUND DELAMINATED SKIN IN UPPER PANEL, CLEANED MATING SURFACE ON AIRCRAFT TRATED AND PRIMED. NO CORROSI
- [SDR DHL9970315C](https://openairdocs.org/sdr/DHL9970315C.md): Plate · cracked · Jul 20, 1999 · N703DH · Boeing 72730C · Cargo/Baggage Doors
  > AT C CHECK, MAIN CARGO DOOR INTERIOR LOWER PLATE COVER FWD TO AFT SECTION HAS SEVERAL CRACKS AND DENTS ON SURFACE. REMOVED PLATE AT MAIN CARGO DOOR INTERIOR LOWER PLATE COVER REPAIRED PER SRM 51-30-2 AND 51-10-1. ALODINED AND PRIMED PER SRM 51-10-2 USED 2024
- [SDR DHL9970312C](https://openairdocs.org/sdr/DHL9970312C.md): Longitudinal · cracked · Jul 20, 1999 · N703DH · Boeing 72730C · Fuselage Miscellaneous Structure
  > AT C CHECK, E3 ELECTRONIC RACK UPPER RT LONGITUDINAL IS CRACKED 2 PLACES. STOP DRILLED CRACKS PER SRM 51-10-1 2 PLACES. INSTALLED DOUBLER PER SRM 51-40-2 FIG 1 USING 2024T3.050 6 BY 4 2 EA, ALODINED AND PRIMED PER SRM 51-10-2, N/R 3126.
- [SDR DHL9970309C](https://openairdocs.org/sdr/DHL9970309C.md): Floor · cracked · Jul 20, 1999 · N703DH · Boeing 72730C · Fuselage Floor Panel
  > AT C CHECK, NOSE W/W PRESS FLOW HAS CRACK AT BS 284.5. REMOVED FLOOR PANEL AT FWD PER SRM 51-30-2. REMOVED 2 EACH OLD DOUBLERS PER SRM 51-30-2. CUT OUT DAMAGED AREA AT BS 284.5 4 BY 1 PER S/B 53-0145, HFEC INSPECTED CUTOUT IAW 51-00-0 FIG 4. NO CRACKS NOTE
- [SDR DHL9970307C](https://openairdocs.org/sdr/DHL9970307C.md): Angle · cracked · Jul 20, 1999 · N703DH · Boeing 72730C · Wing Miscellaneous Structure
  > AT C CHECK, RT WING TRAILING EDGE COVER PANEL INBOARD SUPPORT ANGLE IS CRACKED AT WS 447.90 JUST INBOARD OF NR 11 SPOILER ACTUATOR. REMOVED AND REPLACED SUPPORT ANGLE AT RT WING AT WS 447.90 PER SRM 51-10-1 PAR 4 AND 51-30-2, N/R 2044.
- [SDR DHL9970302C](https://openairdocs.org/sdr/DHL9970302C.md): Angle · cracked · Jul 20, 1999 · N703DH · Boeing 72730C · Wing Miscellaneous Structure
  > AT C CHECK, RT WING TRAILING EDGE COVE PANEL OUTBOARD SUPPORT ANGLE IS CRACKED AT WS 498.08 INBOARD OF THE NR 12 SPOILER ACTUATOR. REPLACED COVER PANEL OUTBRD SUPPORT WS 498.08 PER SRM 51-30-2, 51-10-1 PAR 4 N/R 2045.
- [SDR DHL9970301C](https://openairdocs.org/sdr/DHL9970301C.md): Circumferential · cracked · Jul 20, 1999 · N703DH · Boeing 72730C · Fuselage Main, Frame
  > AT C CHECK, FWD CARGO COMPT, CRACK AT CIRCUMFERENTIAL STA 640 STRINGER 26L. REMOVED OLD REPAIR, STOP DRILLED CRACK, HFEC. INSTALLED REPAIR PARTS PER SRM 53-10-4, 12 BY 6, N/R 3121.
- [SDR DHL9970338C](https://openairdocs.org/sdr/DHL9970338C.md): Bulkhead · cracked · Jul 19, 1999 · N703DH · Boeing 72730C · Fuselage Main, Bulkhead
  > AT C-CHECK, CRACK AT 1183 BULKHEAD SKIN AFT CARGO COMPT WL 172 RBL 8. REMOVED FASTENERS AND STOP DRILL CRACK AT 1183 BLKD WL 172 RBL 8. PERFORMED HFEC INSPECTION PER NDT MANUAL PART 6 51-00-00 FIG 4. NO CRACK IND PAST STOP DRILLS, CUT OUT DAMAGED AREA PER S
- [SDR DHL9970311C](https://openairdocs.org/sdr/DHL9970311C.md): Receptacle · cracked · Jul 19, 1999 · N703DH · Boeing 72730C · Fuselage Miscellaneous Structure
  > AT C CHECK, BARRIER NET ATTACH RECEPTACLE AT BS 364 BETWEEN STRINGERS 5L AND 6L UPPER MOUNT BRACKET MISSING ATTACH RIVET AND CRACKED. REMOVED BRACKET SUPPORT PER SRM 51-30-2. REPLACED BRACKET SUPPORT PER SRM 51-30-2 USED 7075T0.071 AND 2024T3.050, ALODINED

Next page: https://openairdocs.org/deregistered/N703DH-2013-06-11/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 = 'N703DH' AND deregistration_id = 'N703DH-2013-06-11'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N703DH-2013-06-11/reports

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