# Service difficulty reports: N717DH, cancelled Dec 16, 2013

A list on [N717DH, cancelled Dec 16, 2013](https://openairdocs.org/deregistered/N717DH-2013-12-16.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 6 · 262 reports

- [SDR DHL2002717001](https://openairdocs.org/sdr/DHL2002717001.md): Fire Loop · inoperative · Mar 7, 2002 · N717DH · Boeing 72723 · Fire Detection
  > NR 3 ENG FIRE TEST INOP. REMOVED AND REPLACED NR 3 ENG FIRE LOOP IAW B727 OHM 71-02-01, OPS CHECKS SERVICEABLE.
- [SDR DHL2001717022](https://openairdocs.org/sdr/DHL2001717022.md): Battery Pack · discharged · Sep 21, 2001 · N717DH · Boeing 72723 · Emergency Lighting
  > DURING STBY POWER CHECK EMERGENCY EXIT LIGHTS WOULD NOT STAY ILLUMINATED. REMOVED AND REPLACED BATTERY PACK IAW B-727 M/M 33/50/71.
- [SDR DHL2001717021](https://openairdocs.org/sdr/DHL2001717021.md): Fire Detector · malfunctioned · Sep 5, 2001 · N717DH · Boeing 72723 · Fire Detection
  > NR 2 ENGINE FIRE WARNING GROUND FAULT DETECTOR SYSTEM LIGHT ILLUMINATED DURING TAXI THEN SELF EXTINGUISHED AFTER TAKEOFF DEFERRED PER MEL 26-9-1 LM. REMOVED AND REPLACED NR 2 ENG FIRE DETECTOR, OPS CK NORMAL IAW M/M 26-11-001.
- [SDR DHL2001717020](https://openairdocs.org/sdr/DHL2001717020.md): Fire Loop · out of position · Aug 24, 2001 · N717DH · Boeing 72723 · Fire Detection
  > NR 2 FIRE DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED. PERFORMED FIRE DETECTOR SYSTEM TEST. LIGHT EXTINGUISHED. FOUND BRACKET ON NR 2 ENGINE FIRE LOOP TOUCHING LOOP. RE-POSITIONED LOOP IAW B-727 M/M 26-11-22. SYSTEM OPS CHECKED SERVICEABLE.
- [SDR DHL2001717019](https://openairdocs.org/sdr/DHL2001717019.md): Hinge · loose · Aug 22, 2001 · N717DH · Boeing 72723 · Landing Gear Doors
  > A9-CHECK; RT MLG STRUT DOOR FWD HINGE CASTING LOOSE IN DOOR. REMOVED AND REPLACED RT MLG STRUT DOOR IAW B727 MM 32-12-11. PERFORMED OPS CHECK ON RT MLG STRUT DOOR IAW B727 MM 32-12-11 & 32-32-0, OPS CHECKED GOOD.
- [SDR DHL2001717018](https://openairdocs.org/sdr/DHL2001717018.md): Insulator · broken · Aug 18, 2001 · N717DH · Boeing 72723 · Fire Detection
  > ENGINE FIRE DETECTION LIGHT FOR ENGINE NR 3 ON P6-3 PANEL OCCASIONALLY ILLUMINATES DURING CRUISE FLIGHT. LIGHT DEFERRED PER DHL MEL 26-9. PLACARD INSTALLED DMI 6791 CAT C. FOUND BROKEN INSULATION AND FIRE LOOP CONNECTOR CHAFING AGAINST BRACKET. PROVIDED CL
- [SDR DHL2001717017](https://openairdocs.org/sdr/DHL2001717017.md): Packing · deteriorated · Jul 20, 2001 · N717DH · Boeing 72723 · Fuel Flow Sensor
  > NR 3 ENGINE FUEL FLOW INDICATES 1000PPH HIGHER THAN 1 AND 2 ENGINES. ALL OTHER ENGINE PARAMETERS NORMAL NR 3 POWER LEVER READS 1&2 POWER LEVERS BY 2 INCHES. FOUND FUEL FLOW TRANSMITTER OUTLET PACKING DETERIORATED & TRANSMITTER LEAKING SEVERELY. REPLACED PACKI
- [SDR DHL2001717016](https://openairdocs.org/sdr/DHL2001717016.md): Engine · malfunctioned · Jul 20, 2001 · N717DH · Boeing 72723 · Engine (Turbine/Turboprop)
  > NR 3 ENGINE QUIT ON FINAL APPROACH. UPON COMPLETION OF MX PERFORMED POWER ASSURANCE RUN OF NR 3 ENG. IAW DHL JRH 7.7 & 7.8. ALL PARAMETERS NORMAL. OK FOR SERVICE.
- [SDR DHL2001717015](https://openairdocs.org/sdr/DHL2001717015.md): Fire Loop · defective · Jul 16, 2001 · N717DH · Boeing 72723 · Fire Detection
  > NR 1 ENG FIRE WARNING WILL NOT TEST. REMOVED AND REPLACED NR 1 ENG FIRE LOOP AND PERFORMED ADJ/TEST PER 26-11-02 B727 M/M OPS CHECK SERVICEABLE P/N ON OFF 10-60877-13, S/N ON 58803, S/N OFF 59648.
- [SDR DHL2001717013](https://openairdocs.org/sdr/DHL2001717013.md): Duct · leaking · Jul 11, 2001 · N717DH · Boeing 72723 · Pneumatic Distribution System
  > ON CLIMB, LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED ABOUT 10,000 FT. WHILE RETURNING TO AIRPORT, LIGHT WENT OUT ABOUT 1 MIN AFTER GOING TO IDLE THRUST ON ALL ENGS. ACCOMPLISHED RESISTANCE CHECKS IN KEEL BEAM AREA READING 3 MOHMS, AFT STAIR AREA READING 4 MOH
- [SDR DHL2001717014](https://openairdocs.org/sdr/DHL2001717014.md): Insulator · out of position · Jul 10, 2001 · N717DH · Boeing 72723 · Overheat Detection
  > LOWER AFT BODY OVERHEAT ILLUMINATED IN FLT APPROX 10 SEC ON DESCENT INTO IAH. PRIOR TO ACCOMPLISHMENT OF ABNORMAL PROCEDURE LIGHT EXTINGUISHED. REPOSITIONED INSULATORS ON SECTION 48 LEFT DETECTOR ELEMENT. RAN ENGINES, BLEEDS, PACKS AND ANTI-ICE SYSTEMS. OP
- [SDR DHL2001717012](https://openairdocs.org/sdr/DHL2001717012.md): Duct · Jul 4, 2001 · N717DH · Boeing 72723 · Overheat Detection
  > WHILE CLIMBING THROUGH 18,500 THE LOWER AFT BODY OVHT LT ILLUMINATED ABNORMAL PROCEDURE COMPLIED WITHITEM TRANSFERRED TO DMI# 6261 PER DHL MEL 26-10-1 PLACARDS INSTALLED AND SPECIAL PROCEDURES 26-10-1 C/W RKENSIK 35047 07042001REF DMI 6261 - CLIMB THROUGH 18
- [SDR DHL2001717010](https://openairdocs.org/sdr/DHL2001717010.md): Lock Actuator · malfunctioned · Jul 3, 2001 · N717DH · Boeing 72723 · Landing Gear Retraction/Extension System
  > NOSE WHEEL WOULD NOT EXTEND AND HAD TO BE MANUALLY EXTENDED C/W ABNORMAL PROCEDURE. REMOVED AND REPLACED NOSE GEAR LOCK ACTUATOR. RETRACTION CK GOOD IAW B727 MM 32-33-11 PAGE 401-403 RII.
- [SDR DHL2001717011](https://openairdocs.org/sdr/DHL2001717011.md): Duct · Jul 3, 2001 · N717DH · Boeing 72723 · Overheat Detection
  > IN FLIGHT LWR AFT BODY OVHT LT ILLUMINATED, LT EXTINGUISHED AFTER #3 THRUST LEVER WAS RETARDED C/W ABNORMAL PROCEDURET/S LWR AFT BODY OVHT LT. FOUND TAI DUCT TO BE CRACKED, REMOVED DUCT. DUCT REPAIRED BY VENDOR JLWR146K IAW B727 OHM CHPT 36-10-01. REINSTALLED
- [SDR DHL2001717009](https://openairdocs.org/sdr/DHL2001717009.md): Skin · cracked · Jun 27, 2001 · N717DH · Boeing 72723 · Trailing Edge Flaps
  > LEFT INBD MID FLAP HAS 2.5 INCH CRACK AFT (UPPER) AREA STA 251 JUST BELOW INBD FLAP GIMBLE ACCESS PANEL. REMOVED LT INBD FORE, MID AND AFT FLAP ASSYS IAW MM 27-51-1, 27-51-2 & 27-51-3 31499 OK TO INSTALL 8134 6/27/01. INSTALLED LEFT I/B FORE, MID AND AFT FL
- [SDR DHL2001717008](https://openairdocs.org/sdr/DHL2001717008.md): Flap · out of adj · May 10, 2001 · N717DH · Boeing 72723 · Trailing Edge Flap Control System
  > STRAIGHT AND LEVEL FLIGHT AT 300KTS AND FL270 A/C REQUIRES 1-3/4 UNITS RT OF AILERON TRIM TO MAINTAIN STRAIGHT AND LEVEL FLIGHT. RDR TRIM VALVE AT LEFT 1/2 UNIT. ADJUSTED I/B T/E FLAPS PER LATERAL TRIM ADJUSTMENT CHART FIG 501, MM 27-00-21.
- [SDR DHL2001717007](https://openairdocs.org/sdr/DHL2001717007.md): Autopilot Sys · malfunctioned · May 8, 2001 · N717DH · Boeing 72723 · Autopilot System
  > AUTOPILOT WILL NOT TRACK A VOR OR LOCALIZER. DEFERRED PER DHL MEL 22-1-7. PLACARD INSTALLED. REPLACED NR 1 NAV AND TESTED PER MM 2200 OP NORMAL TRACK AND CAPTURE.
- [SDR DHL2001717006](https://openairdocs.org/sdr/DHL2001717006.md): Spoiler · out of position · May 2, 2001 · N717DH · Boeing 72723 · Drag Control System
  > A/C, WITH BALL CENTERED AND LT WING SLIGHTLY LOW, AILERON TRIM INDICATES 3-1/8 UNITS TO RT, AND RUDDER TRIM 1/4 UNIT TO LT. ALSO THERE WAS 4 DEGREE RT WHEEL DEFLECTION AT FL310 AND MACH 0.80 WITH AUTOPILOT OFF. FOUND NR 2 FLIGHT SPOILER EXTERNAL MANUAL RELEAS
- [SDR DHL2001717005](https://openairdocs.org/sdr/DHL2001717005.md): Receiver · malfunctioned · Mar 2, 2001 · N717DH · Boeing 72723 · Localizer/VOR System
  > CAPTAIN AND F/O''S VOR''S SCALLOPS AND WILL NOT TRACK PROPERLY. DIVERTED TO CVG. REMOVED AND REPLACED NR 1 VOR/ILS RECEIVER IAW B727 MM 34-31-21. OPS CHECK OK. P/N OFF 522450-115, S/N 5889, P/N ON 522-4280-107, S/N ON B9818.
- [SDR DHL2001717003](https://openairdocs.org/sdr/DHL2001717003.md): Warning System · false activation · Jan 30, 2001 · N717DH · Boeing 72723 · Stall Warning System
  > AT APPOX 95 KTS IAS STICK SHAKER ACTIVATED T/O ABORTED. UPON CREW DEBRIEF, FOUND 3 SECONDS OF FLIGHT TIME ON CAPTS CLOCK. THAT IN COMBINATION WITH STICK SHAKER INDICATE THAT THE NOSE STRUT FULLY EXTENDED ON T/O ROLL. CHECKED STALL VANE OPERATION PER 34-18-0
- [SDR DHL2001717002](https://openairdocs.org/sdr/DHL2001717002.md): Warning System · will not test · Jan 30, 2001 · N717DH · Boeing 72723 · Central Warning
  > FLIGHT CONTROL WARNING TEST SYSTEM WILL NOT TEST. NOTE-FLAPS AT 15 DEGREE AND SPEEDBRAKE DEPLOYED. RECYCLED FLAPS AND SPOILERS AS WELL AS NR 3 THROTTLE, RETESTED SYSTEM USING OVERHEAD TEST SWITCH, SYSTEM OP''S CHECKS NORMAL PER 31-26-0 AND IS OK FOR SERVICE.
- [SDR DHL2001717001](https://openairdocs.org/sdr/DHL2001717001.md): Gyro · unserviceable · Jan 9, 2001 · N717DH · Boeing 72723 · Attitude and Direction Data System
  > CAPT HSI FAILED ON TAXI OUT. REMOVED AND REPLACED NR 2 DIRECTIONAL GYRO PER M/M 34-21-21,SYS OPS CHK GOOD
- [SDR DHL2000717124](https://openairdocs.org/sdr/DHL2000717124.md): Stop · loose · Dec 1, 2000 · N717DH · Boeing 72723 · Fuel Controlling System
  > NR 2 ENGINE WOULD NOT DEVELOP T/O THRUST WITH ANTI ICE ON.FOUND SAFTY WIRE ON PART POWER STOP BROKEN AND POWER STOP OUT. RESECURED AND RE-WIRED PART POWER STOP. PREFORMED ENGINE RUN AND T/O POWER CHECK PER JRH 5.2&7.9.OPS CHK GOOD.ALL PARAMETERS NORMAL.
- [SDR DHL2000717123](https://openairdocs.org/sdr/DHL2000717123.md): Warning System · activated · Nov 29, 2000 · N717DH · Boeing 72723 · Stall Warning System
  > STALL WARNING/STICK SHAKER ON T/O ROLL. AS PER STALL WARNING SYSTEM TEST, MM 34-18-0, SYSTEM CHKS OK.
- [SDR DHL2000717122](https://openairdocs.org/sdr/DHL2000717122.md): Adi · failed · Sep 28, 2000 · N717DH · Boeing 72723 · Attitude and Direction Data System
  > GYRO FLAG APPEARED IN CAPTS ADI, REJECTED T/O. REMOVED AND REPLACED NR 1 VG PER M/M 34-22-21. REMOVED AND REPLACED STEERING COMPUTER PER 34-62-31. ALL OPS CHK GOOD.
- [SDR DHL2000717121](https://openairdocs.org/sdr/DHL2000717121.md): Cable · frayed · Sep 22, 2000 · N717DH · Boeing 72723 · Door Warning System
  > NOSE LANDING GEAR DOOR WARNING DOOR LIGHT CAME ON IN FLIGHT AT 230 KNOTS. INSTALLED NEW LOWER CABLE ASSY PER M/M 32-33-51. OPS CHK OK.
- [SDR DHL2000717120](https://openairdocs.org/sdr/DHL2000717120.md): Warning System · activated · Sep 22, 2000 · N717DH · Boeing 72723 · Door Warning System
  > NLG DOOR WARNING LIGHT CAME ON IN FLIGHT AT 230 KTS.
- [SDR DHL2000717118](https://openairdocs.org/sdr/DHL2000717118.md): Strut · overserviced · Aug 23, 2000 · N717DH · Boeing 72723 · Nose/Tail Landing Gear Strut/Axle
  > STICK SHAKER ACTIVATED AT 70KTS. REJECTED TAKEOFF. TESTED STALL WARNING SYSTEM PER 34-18-0. NO DEFECTS NOTED. SUSPECT NOSE STRUT OVER SERVICED. SERVICED NOSE STRUT PER 12-15-23, OK FOR CONTINUED SERVICE.
- [SDR DHL2000717119](https://openairdocs.org/sdr/DHL2000717119.md): Housing · stripped · Aug 18, 2000 · N717DH · Boeing 72723 · Turbine Engine Reduction Gear
  > ON CLIMBOUT OF EWR, OIL (NR 1 ENG) QUANTITY BEGAN A SLOW STEADY DECREASE. AS QUANTITY APPROACHED ZERO OIL PRESSURE BEGAN DECREASING. ENGINE SHUT DOWN IN FLIGHT PER AOM. ENGINE SHUT DOWN WHEN PRESSURE WAS APPROX 35 PSI, 20 MINUTE FLIGHT WITH ENGINE WINDMILLI
- [SDR DHL2000717117](https://openairdocs.org/sdr/DHL2000717117.md): Gyro · erratic · Aug 1, 2000 · N717DH · Boeing 72723 · Attitude and Direction Data System
  > CAPT ADI STICKS AND PITCHES UP AND DOWN ERRATICALLY 5-7 DEGREES AND GYRO FLAG COMES INTO VIEW INTERMITTENTLY DURING FLIGHT. REPLACED NR 1 VERT GYRO WITH A SERVICABLE UNIT.
- [SDR DHL2000717111](https://openairdocs.org/sdr/DHL2000717111.md): Skin · corroded · Feb 14, 2000 · N717DH · Boeing 72723 · Fuselage Main, Plate/Skin
  > AT D CHECK, FUSELAGE EXTERIOR CENTER SECTION REAR LOWER CHORD AND SKIN BULGING STA 865 BL 0-16L. REMOVED REAR SPAR LOWER CHORD, CUT AFT WEB AT STA. RBL 49 TO LB 49 FROM TOP TO BOTTOM. PERFPORMED HFEC OF OPEN HOLES, IN BOTOM SKIN. REMOVED CORRSOION ON REAR U
- [SDR DHL2000717103](https://openairdocs.org/sdr/DHL2000717103.md): Fairing · cracked · Feb 11, 2000 · N717DH · Boeing 72723 · Aerodynamic Fairings
  > AT D-CHECK, FAIRING PANEL NR 3334 HAD A CRACK ON THE INSIDE BRACKET MOUNT. CUT OUT DAMAGED AREA, INSTALLED REPAIR AT FAIRING PANEL PER SRM 51-30-2, 8.5 X 2.
- [SDR DHL200071786D](https://openairdocs.org/sdr/DHL200071786D.md): Seat Track · corroded · Feb 7, 2000 · N717DH · Boeing 72723 · Fuselage, Seat/Cargo Attach Fittings
  > AT D-CK, CABIN SEAT TRACK NR 1 CORRODED BS 720. REMOVED AND INSTALLED NEW SEAT TRACK NR 1 FROM BS 720 TO 740 PER B727 SRM 53-10-5 FIG 7. REF: 5619.
- [SDR DHL2000717114](https://openairdocs.org/sdr/DHL2000717114.md): Frame · corroded · Feb 3, 2000 · N717DH · Boeing 72723 · Fuselage Main, Frame
  > AT D CHECK, FUSELAGE EXTERIOR CENTER SECTION LOWER CHORD CORROSION BL 36 LEFT MARKED STA 741. REMOVED CORROSION AT BL 36 TO 13, OUT OF LIMITS, HFEC, NO CRACKS NOTED. FABRICATED ANGLE REAPIR AND INSTALLED PER DHL-MIA -00-00003H FROM LBL 10 TO LBL 45, 37 BY
- [SDR DHL200071780D](https://openairdocs.org/sdr/DHL200071780D.md): Floorbeam · corroded · Feb 2, 2000 · N717DH · Boeing 72723 · Fuselage Main, Floor Beam
  > AT D-CK, FWD CARGO COMPT FLOOR SUPPORT ANGLE CORRODED AT BS 700 LBL 20. CUTOUT DAMAGED AREA PER B727 SRM 51-40-4. INSTALLED REPAIR PER B727 SRM 51-40-3 FIG 1 AND 51-30-2. REF: N/R 3781.
- [SDR DHL200071799D](https://openairdocs.org/sdr/DHL200071799D.md): Support · gouged · Jan 28, 2000 · N717DH · Boeing 72723 · Main Landing Gear Attach Section
  > AT D-CHECK, FOUND LT MLG SUPPORT BEAM OUTBOARD PIN HOLE GOUGED. REMOVED PIN AND BUSHING PER B727 MM 57-15-12, PERFORMED HFEC INSPECTION OF O/B FWD BORE, NO CRACKS DETECTED. BORED PIN HOLE TO 1.809 PER BOEING TELEX 32-9430, FABRICATED AND INSTALLED BUSHING PE
- [SDR DHL200071781D](https://openairdocs.org/sdr/DHL200071781D.md): Floorbeam · cracked · Jan 28, 2000 · N717DH · Boeing 72723 · Fuselage Main, Floor Beam
  > AT D-CK, FLOORBEAM CRACK AT B/S 344 LBL 31. REMOVED FLOORBEAM UPPER CHORD FROM LBL 60 TO RBL 60 BS 344 PER B727 SRM 51-30-2. INSTALLED NEW FLOOR UPPER CHORD PER B727 SRM 53-10-2 FIG 1, AND 51-30-2. REF: N/R 3775.
- [SDR DHL2000717105](https://openairdocs.org/sdr/DHL2000717105.md): Spar · gouged · Jan 28, 2000 · N717DH · Boeing 72723 · Wing Spar
  > AT D-CHECK, FOUND RIGHT HAND SPAR FITTING GOUGED (MLG BEAM O/B SIDE TO REAR SPAR SUPPORT FITTING). PERFORMED HFEC, BORED RT MLG SUPPORT FITTING PIN HOLE TO 1.795, WITHIN LIMITS PER BOEING TELEX 32-9430. FLAP PEENED AREA, INSTALLED BUSHINGS AND SUPPORT BEAM P
- [SDR DHL200071796D](https://openairdocs.org/sdr/DHL200071796D.md): Skin · corroded · Jan 26, 2000 · N717DH · Boeing 72723 · Fuselage Main, Plate/Skin
  > AT D-CK, FOUND CORROSION ON CENTER WING LOWER SKIN EXTERIOR STA 740 BLL 40 TO BLL 12. REMOVED FASTENERS AND CORROSION, FOUND OUT OF LIMITS. FLAP PEENED BLENDED AREAS ON LOWER SKIN. FABRICATED AND INSTALLED INTERNAL REPAIR AT FWD LOWER CHORD STA 740 LBL 10 T
- [SDR DHL200071758D](https://openairdocs.org/sdr/DHL200071758D.md): Seat Track · corroded · Jan 26, 2000 · N717DH · Boeing 72723 · Fuselage, Seat/Cargo Attach Fittings
  > AT D-CK, SEAT TRACK CORRODED AT 31 LBL FROM STA 312 TO STA 360. REMOVED AND REPLACED SEAT TRACK PER B727 SRM 51-30-2 AND 53-10-5. REF: N/R 5612.
- [SDR DHL200071751D](https://openairdocs.org/sdr/DHL200071751D.md): Seat Track · corroded · Jan 26, 2000 · N717DH · Boeing 72723 · Fuselage, Seat/Cargo Attach Fittings
  > AT D CK, SEAT TRACK CORRODED AT 9 LBL FROM STA 312 TO STA 360. REMOVED AND REPLACED SEAT TRACK FROM STA 312 TO STA 360 PER B727 SRM 51-30-2 AND 51-10-2. REF: N/R 5613.
- [SDR DHL200071750D](https://openairdocs.org/sdr/DHL200071750D.md): Floorbeam · corroded · Jan 26, 2000 · N717DH · Boeing 72723 · Fuselage Main, Floor Beam
  > AT D-CK, FWD FLANGE OF FLOOR SUPPORT HAS CORROSION AT STA 328 LBL 20. CUTOUT DAMAGED AREA AT FLOOR SUPPORT, FABRICATED AND INSTALLED REPAIR AT STA 328 LBL 20 PER B727 SRM 53-10-8 AND 51-30-2. REF: N/R 5614.
- [SDR DHL200071779D](https://openairdocs.org/sdr/DHL200071779D.md): Skin · cracked · Jan 25, 2000 · N717DH · Boeing 72723 · Fuselage Main, Plate/Skin
  > AT D-CK, EVIDENCE OF CRACK AT STRINGER 5 LT BS 990 AND 1010. CUTOUT DAMAGED AREA AT BS 990 AND 1010 PER B727 SRM 53-10-3 FIG 3. INSTALLED REPAIRS AT STR 5L STA 990 AND 1010, PER B727 SRM 53-10-3 FIG 3. REF: N/R 5610.
- [SDR DHL200071763D](https://openairdocs.org/sdr/DHL200071763D.md): Skin · cracked · Jan 25, 2000 · N717DH · Boeing 72723 · Elevator, Plate/Skin
  > AT D-CK, LEFT ELEVATOR, JUST FWD OF OUTBD STATIC WICK TOP SKIN HAS CRACKS TWO UNDER DOUBLER FWD INBD CORNER, FOUND DURING XRAY.. REMOVED STATIC WICK AND DOUBLER. INSPECTED IAW B727 NDT MANUAL PART 6-51-00-00 FIG 4. INNER SKIN HAS CRACK. ROUTED OUT CRACK, I
- [SDR DHL200071724D](https://openairdocs.org/sdr/DHL200071724D.md): Shield · cracked · Jan 24, 2000 · N717DH · Boeing 72723 · Passenger/Crew Doors
  > AT D-CK, MAIN ENTRY DOOR HINGE ICE SHIELDS, UPPER AND LOWER CRACKED. REMOVED AND REPLACED UPPER AND LOWER HINGE COVERS PER B727 SRM 52-10-1, FIG 1. MATERIAL USED; 2024T3, THICKNESS.032, SIZE; 14 BY 6. REF: N/R 5609.
- [SDR DHL2000717113](https://openairdocs.org/sdr/DHL2000717113.md): Support Bracket · corroded · Jan 22, 2000 · N717DH · Boeing 72723 · Fuselage Miscellaneous Structure
  > AT D CHECK, CABIN FLOATING SEAT TRACK SUPPORT RBL 45 BETWEEN STA 740-760 FLANGE HAS CORROSION. REMOVED AND REPLACED SEAT TRACK SUPPORT PER SRM 51-30-2. N/R 5605.
- [SDR DHL200071762D](https://openairdocs.org/sdr/DHL200071762D.md): Floorbeam · corroded · Jan 22, 2000 · N717DH · Boeing 72723 · Fuselage Main, Floor Beam
  > AT D-CK, CABIN FLOATING SEAT TRACK SUPPORT NR 4 STA 850 TO 870 RBL 45 FLANGE HAS CORROSION. REMOVED AND REPLACED CABIN FLOATING SEAT TRACK SUPPORT FROM STA 850 TO 870 PER B727 SRM 51-30-2. REF: N/R 5606.
- [SDR DHL200071741D](https://openairdocs.org/sdr/DHL200071741D.md): Panel · delaminated · Jan 22, 2000 · N717DH · Boeing 72723 · Wing, Plate/Skin
  > AT D CK, RIGHT WING PANEL 6527 HAS DELAMINATED AREAS ON UPPER AND LOWER SURFACES. INSTALLED FIBERGLASS REPAIR AT RIGHT WING PANEL 6527 PER B727 SRM 51-40-8, FIG 1. REF: N/R 2954.
- [SDR DHL200071740D](https://openairdocs.org/sdr/DHL200071740D.md): Panel · frayed · Jan 22, 2000 · N717DH · Boeing 72723 · Wing, Plate/Skin
  > AT D CK, RIGHT WING PANEL 6403 HAS FRAYED EDGE ON OUTSIDE SURFACE. INSTALLED FILLER REPAIR AT RIGHT WING PANEL 6403 PER B727 SRM 51-40-1 FIG 1. REF: N/R 2953.
- [SDR DHL2000717116](https://openairdocs.org/sdr/DHL2000717116.md): Floorbeam · damaged · Jan 21, 2000 · N717DH · Boeing 72723 · Fuselage Main, Floor Beam
  > AT D CHECK, PREVIOUS REPAIR AT FLOORBEAM LOWER FLANGE BS 1110 RBL 15.5 TO LBL 37. CUT OUT PREV REPAIR, INSTALLED NEW REPAIR FROM LBL 38 TO RBL 0 PER AVITAS EO 14 BY 3.5, N/R 3750.

Next page: https://openairdocs.org/deregistered/N717DH-2013-12-16/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 = 'N717DH' AND deregistration_id = 'N717DH-2013-12-16'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N717DH-2013-12-16/reports

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