# Service difficulty reports: N706DH, cancelled Sep 21, 2000

A list on [N706DH, cancelled Sep 21, 2000](https://openairdocs.org/deregistered/N706DH-2000-09-21.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 2 · 66 reports

- [SDR DHL2000706005](https://openairdocs.org/sdr/DHL2000706005.md): Intercostal · cracked · Jun 22, 2000 · N706DH · Boeing 72722C · Fuselage Miscellaneous Structure
  > FWD RT LAV FLOOR FRAME INTERCOSTAL HAS 2 LARGE CRACKS EMINATING FROM TOP, LOCATED I/B OF DUMP SHUTE BS 303.9, RBL 43. REMOVED WEB FOR REPLACMENT PER SRM 57-30-2. FABRICATED AND INSTALLED NEW INTERCOSTAL PER SRM 53-10-1. TREATED WITH ALODINE AND PRIMED PER S
- [SDR DHL2000706006](https://openairdocs.org/sdr/DHL2000706006.md): Angle · broken · Jun 21, 2000 · N706DH · Boeing 72722C · Fuselage Main, Attach Fittings
  > AFT CARGO COMPT APPROX BS 950 AFT AREA, WL 195.0 & BBL 0.0 ANTI ICE DUCT HAS ANGLE SUPPORT BROKEN AT LOWER SECTION. REMOVED AND INSTALLED NEW ATTACH ANGLE SUPPORT PER SRM 53-10-01. ALODINED AND PRIMED PER SRM 51-10-2.
- [SDR DHL2000706004](https://openairdocs.org/sdr/DHL2000706004.md): Threshold · corroded · Jun 21, 2000 · N706DH · Boeing 72722C · Fuselage Miscellaneous Structure
  > FWD RT LAV FLOOR AT THRESHOLD HAS CORROSION ABOVE AND BELOW FLOOR BS 328, RBL 14. REMOVED THRESHOLD PER SRM 51-30-2. FABRICATED NEW THRESHOLD PER SRM 53-10-1. INSTALLED NEW THRESHOLD PER SRM 51-30-2.
- [SDR DHL2000706003](https://openairdocs.org/sdr/DHL2000706003.md): Attach Angle · cracked · Jun 21, 2000 · N706DH · Boeing 72722C · Passenger/Crew Doors
  > FWD ENTRY DOOR PANEL (INTERIOR) AFT SUPPORT ATTCH ANGLE CRACKED SEVERAL PLACES. REMOVED AND REPLACED ANGLES PER SRM 51-30-2. TREATED AND PRIMED SUPPORT ANGLES PER SRM 51-10-2.
- [SDR DHL2000706002](https://openairdocs.org/sdr/DHL2000706002.md): Floorboard · damaged · Jun 21, 2000 · N706DH · Boeing 72722C · Fuselage Floor Panel
  > FLOOR PANEL DAMAGED AT FWD LEFT CORNER AT BS 360 PANEL FROM RBL 24.0 TO 48.0. REMOVED FLOORBOARD, FABRICATED DOUBLERS PER SRM 53-20-1. ALODINED AND PRIMED PER SRM 53-20-1. INSTALLED FLOOR PANEL PER SRM 51-30-2.
- [SDR DHL2000706001](https://openairdocs.org/sdr/DHL2000706001.md): Fluid · leaking · May 27, 2000 · N706DH · Boeing 72722C · Fuel Storage
  > AFTER T/O, TOWER AND ANOTHER A/C REPORTED A SIGNIFICANT AMOUNT OF FLUID LEAKING FROM LFT WING. FUEL WAS DUMPED DOWN TO LANDING WT AND RETURNED TO SERVICE. INSPECTED FUEL LINES AND TANK PANELS, NO LEAKS NOTED. INSPECTED FUEL TANK VENT SYS PER M/M 28-13-00.
- [SDR DHL99706001](https://openairdocs.org/sdr/DHL99706001.md): Temp Bulb · failed · Nov 1, 1999 · N706DH · Boeing 72722C · Engine Oil Temperature
  > NR 1 ENGINE OIL TEMP ROSE IN FLIGHT TO 131 REGARDLESS OF THRUST SETTING. ENGINE OIL TEMP WOULD NOT DECREASE. SHUT DOWN NR 1 ENGINE AFTER 15 MIN, TOTAL TIME TEMP AT 125, 25 MIN. REPLACED OIL TEMP BULB, REPLACED MAIN OIL SCREEN AND DRAINED AND REPLACED OIL.
- [SDR DHL98706003](https://openairdocs.org/sdr/DHL98706003.md): Wheel · cracked · Jun 24, 1998 · N706DH · Boeing 72722C · Wheel/Ski/Float
  > ON SERVICE CHECK, FOUND NR 4 WHEEL AND TIRE ASSY BROKEN LUGS HITTING BRAKE ASSY. INSPECTED, INNER WHEEL HALF CRACKED AND BROKEN. REMOVED AND REPLACED NR 4 MAIN TIRE AND WHEEL AND NR 4 BRAKE PER MM 32-45 AND 32-41. INSPECTED AXLE SLEEVE, NO DEFECT NOTED. IN
- [SDR DHL9870646C](https://openairdocs.org/sdr/DHL9870646C.md): Seat Track · cracked · Jun 3, 1998 · N706DH · Boeing 72722C · Fuselage, Seat/Cargo Attach Fittings
  > AT C-CHECK, CABIN SEAT TRACK CRACKED AT STA 580 LBL 24. CUT OUT DAMAGED SECTION OF SEAT TRACK FROM BS 560 TO 620, INSTALLED NEW SEAT TRACK 5' LONG PER SRM 53-10-5. N/R 5816.
- [SDR DHL9870636C](https://openairdocs.org/sdr/DHL9870636C.md): Rib · cracked · May 22, 1998 · N706DH · Boeing 72722C · Leading Edge Devices
  > AT C-CHECK, NR 5 SLAT I/B CLOSURE RIB IS CRACKED. REPLACED RIB PER SRM 51-30-2. N/R 2137.
- [SDR DHL9870632C](https://openairdocs.org/sdr/DHL9870632C.md): Forging · cracked · May 21, 1998 · N706DH · Boeing 72722C · Fuselage Miscellaneous Structure
  > AT C-CHECK, FUSE FORGING BS 950 LT SIDE HAS 1 INCH CRACK AT SECOND ROW TOP NR 1 FASTENER. INSTALLED S/B REPAIR PER S/B 53-0126 PART VI. N/R 1701.
- [SDR DHL9870635C](https://openairdocs.org/sdr/DHL9870635C.md): Center Section · cracked · May 20, 1998 · N706DH · Boeing 72722C · Wing Main, Frame Structure
  > AT C-CHECK, RT UPPER AT 70.5 WING CENTER SECTION HAS 2 CRACKS AT FWD LOWER HOLE. INSTALLED REPAIR AT RT WING LOWER I/B AND CENTER SECT PER S/B 57-0112. N/R 213.
- [SDR DHL9870618C](https://openairdocs.org/sdr/DHL9870618C.md): Rib · cracked · May 20, 1998 · N706DH · Boeing 72722C · Wing, Rib/Bulkhead
  > AT C-CHECK, RT WING RIB AT STA 629 CRACKED AT STR 14 LOWER. STOP DRILLED CRACK, ACCOMPLISHED HFEC, INSTALLED DOUBLER PER SRM 51-30-2, 3 X 6'. N/R 2132.
- [SDR DHL9870650C](https://openairdocs.org/sdr/DHL9870650C.md): Bob Weights · cracked · May 19, 1998 · N706DH · Boeing 72722C · Elevator Control System
  > AT C-CHECK, RT ELEV TAB BOB WEIGHTS CRACKS AND DETERIORATED. REMOVED AND REPLACED WEIGHTS PER SRM 51-10-1 AND 51-30-2. N/R 4569.
- [SDR DHL9870631C](https://openairdocs.org/sdr/DHL9870631C.md): Casting · cracked · May 19, 1998 · N706DH · Boeing 72722C · Spoilers
  > AT C-CHECK, NR 7 SPOILER CENTER HINGE CASTING CRACKED AT I/B LOWER END. REMOVED AND REPLACED CENTER CASTING PER 727 SRM 57-10-1. N/R 1698.
- [SDR DHL9870617C](https://openairdocs.org/sdr/DHL9870617C.md): Skin · cracked · May 19, 1998 · N706DH · Boeing 72722C · Wing, Plate/Skin
  > AT C-CHECK, RIGHT WING UPPER SURFACE, HFEC REVEALED 3 CRACK INDICATIONS AT 3 FASTENER HOLES AT WING RIB UPPER CHORD AT 70.5 O/B HORIZ FLANGE. OVERSIZED HOLES, HFEC, INSTALLED PREV MOD PER S/B 57-0112. N/R 2130.
- [SDR DHL9870611C](https://openairdocs.org/sdr/DHL9870611C.md): Bob Weight · cracked · May 19, 1998 · N706DH · Boeing 72722C · Elevator Control System
  > AT C-CHECK, LT ELEVATOR BOB WEIGHTS CRACKED AND DETORATED ON TAB. REMOVED AND REPLACED WEIGHTS PER SRM 51-30-2. N/R 4568.
- [SDR DHL9870603C](https://openairdocs.org/sdr/DHL9870603C.md): Cowling · cracked · May 18, 1998 · N706DH · Boeing 72722C · Engine Cowling System
  > AT C-CHECK, NR 1 ENGINE FWD FIXED COWL AFT FRAME IS CRACKED AT LOWER END BY MOUNT BRACKET. INSTALLED ANGLE REPAIR PER SRM 51-40-3, 4.5 X 2. N/R 6939.
- [SDR DHL9870630C](https://openairdocs.org/sdr/DHL9870630C.md): Stringer · cracked · May 17, 1998 · N706DH · Boeing 72722C · Wing, Longeron/Stringer
  > AT C-CHECK, VENT STR S-14 CRACK LEFT WING RIB STA 686.5 UPPER. TRIMMED OUT DAMAGED AREA, INSTALLED REPAIR OF VENT PER SRM 57-10-5, L-ANGLE 14. N/R 1670.
- [SDR DHL9870606C](https://openairdocs.org/sdr/DHL9870606C.md): Stringer · cracked · May 17, 1998 · N706DH · Boeing 72722C · Wing, Longeron/Stringer
  > AT C-CHECK, CRACKED VENT STRINGER 13 AT WS 629 LEFT WING. CUT OUT DAMAGED SECTION PER S/B 57-A159, INSTALLED ATTACH ANGLE PER S/B 57-A159, 12 LONG. N/R 1671.
- [SDR DHL9870605C](https://openairdocs.org/sdr/DHL9870605C.md): Rib · cracked · May 17, 1998 · N706DH · Boeing 72722C · Wing, Rib/Bulkhead
  > AT C-CHECK, LEFT WING WS 686.5 RIB CRACK AT LOWER STR 9. STOP DRILLED CRACK, HFEC, INSTALLED DOUBLER REPAIR PER SRM 57-10-5, 9 X 4. N/R 1669.
- [SDR DHL9870610C](https://openairdocs.org/sdr/DHL9870610C.md): Strap · disbonded · May 16, 1998 · N706DH · Boeing 72722C · Fuselage Main, Plate/Skin
  > AT C-CHECK, SKIN BONDED TEAR STRAP AT STA 380 STR 3L TO 1 HAS DISBONDED. CUT OUT TEAR STRAP AT STA 380 BETWEEN STR 1L TO STR 4. CLEANED INNER FUS SKIN, NO CORROSION NOTED. INSTALLED NEW TEAR STRAP PER S/B 53-0082, 30 X 3. N/R 3627.
- [SDR DHL9870649C](https://openairdocs.org/sdr/DHL9870649C.md): Floorbeam · corroded · May 15, 1998 · N706DH · Boeing 72722C · Fuselage Main, Floor Beam
  > AT C-CHECK, CORROSION ON FLOORBEAM AFT UPPER FLANGE LOWER SURFACE AT BS 560 LBL 48. CUT OUT DAMAGED SECTION AT STA 560 FROM LBL 24 TO O/B END. INSTALLED FLOORBEAM UPPER CHORD PER SRM 53-10-8, 44 LONG, STRAP 3 X 24 SUPPORT ANGLE 2 X 1 X 24. N/R 3600.
- [SDR DHL9870648C](https://openairdocs.org/sdr/DHL9870648C.md): Angle · corroded · May 15, 1998 · N706DH · Boeing 72722C · Vertical Stabilizer
  > AT C-CHECK, VERTICAL STAB LT STAINLESS STEEL RUB STRIP FOR THE HORIZ STAB RUB BLOCK IS BULGED. VERTICAL SUPPORT ANGLE CORRODED. INSTALLED NEW ANGLE PER SRM 55-30-1. N/R 4544.
- [SDR DHL9870647C](https://openairdocs.org/sdr/DHL9870647C.md): Angle · corroded · May 15, 1998 · N706DH · Boeing 72722C · Vertical Stabilizer
  > AT C-CHECK, VERT STAB RT STAINLESS STEEL RUB STRIP FOR THE HORIZ STAB RUB BLOCK IS BULGED. REMOVED STRIP AND FOUND VERT ATTACH SUPPORT ANGLE CORRODED. INSTALLED NEW SUPPORT PER SRM 55-30-1. N/R 4545.
- [SDR DHL9870643C](https://openairdocs.org/sdr/DHL9870643C.md): Floorbeam · corroded · May 15, 1998 · N706DH · Boeing 72722C · Fuselage Main, Floor Beam
  > AT C-CHECK, CORROSION ON DOOR SILL FITTING BOTTOM SURFACE OF TOP FLANGE AT BS 560 LBL 60. CUT OUT DAMAGED SECTION OF CABIN FLOORBEAM UPPER CHORD STA 560 LBL 28, INSTALLED FLOORBEAM UPPER CHORD, REPAIR BETWEEN LBL 28 TO 62 PER SRM 53-10-8. N/R 3601.
- [SDR DHL9870629C](https://openairdocs.org/sdr/DHL9870629C.md): Rib · cracked · May 15, 1998 · N706DH · Boeing 72722C · Leading Edge Devices
  > AT C-CHECK, NR 1 SLAT INBD TRACK OUTBD RIB IS CRACKED AT FWD END. STOP DRILLED, HFEC, INSTALLED DOUBLER PER SRM 57-50-3, 1 X 4. N/R 1668.
- [SDR DHL9870628C](https://openairdocs.org/sdr/DHL9870628C.md): Rib · cracked · May 15, 1998 · N706DH · Boeing 72722C · Leading Edge Devices
  > AT C-CHECK, NR 4 SLAT INBD TRACK OUTBD RIB IS CRACKED PAST STOP DRILL. STOP DRILLED END OF CRACK, HFEC, FABRICATED RIB REPAIR PER SRM 57-50-3, 4 X 5. N/R 1667.
- [SDR DHL9870627C](https://openairdocs.org/sdr/DHL9870627C.md): Spar · cracked · May 15, 1998 · N706DH · Boeing 72722C · Wing Spar
  > AT C-CHECK, LEFT WING FRONT SPAR WS 115 LOWER END OF VERTICAL ANGLE CRACKED. STOP DRILLED END OF CRACK, HFEC, FABRICATED ANGLE REPAIR, 6 X 2 PER SRM 51-40-3. N/R 1648.
- [SDR DHL9870621C](https://openairdocs.org/sdr/DHL9870621C.md): Stop · cracked · May 15, 1998 · N706DH · Boeing 72722C · Passenger/Crew Doors
  > AT C-CHECK, RIGHT HAND AFT ENTRY DOOR STOP NR 7 IS CRACKED. REMOVED AND REPLACED STOP PER SRM 51-30-2. N/R 5802.
- [SDR DHL9870620C](https://openairdocs.org/sdr/DHL9870620C.md): Skin · cracked · May 15, 1998 · N706DH · Boeing 72722C · Fuselage Main, Plate/Skin
  > AT C-CHECK, AFT ENTRY DOOR LEFT NR 7 DOORS TOP FITTING CUTOUT IS CRACKED. HFEC OF STOP DRILL, INSTALLED REPAIR PER S/B 53-055 AND DRAWING 65C15764. REPAIRS 22 X 8.5' AND 13' X 7. N/R 3608.
- [SDR DHL9870609C](https://openairdocs.org/sdr/DHL9870609C.md): Skin · cracked · May 15, 1998 · N706DH · Boeing 72722C · Fuselage Main, Plate/Skin
  > AT C-CHECK, AFT ENTRY DOOR RIGHT NR 7 DOOR STOP FITTING CUTOUT IS CRACKED. ACCOMPLISHED NDT, STOP DRILLED, INSTALLED REPAIR PER S/B 53-055 22 X 8.5 AND 13 X 7. N/R 3609.
- [SDR DHL9870604C](https://openairdocs.org/sdr/DHL9870604C.md): Angle · cracked · May 15, 1998 · N706DH · Boeing 72722C · Wing Miscellaneous Structure
  > AT C-CHECK, NR 1 FLAP TRACK OUTBD COVE PANEL SUPPORT ANGLE CRACKED. REMOVED DAMAGED SUPPORT, FABRICATED AND INSTALLED ANGLE PER SRM 51-30-2. N/R 1652.
- [SDR DHL9870645C](https://openairdocs.org/sdr/DHL9870645C.md): Frame · cracked · May 14, 1998 · N706DH · Boeing 72722C · Fuselage Miscellaneous Structure
  > AT C-CHECK, FWD CARGO DOOR FUS FRAME, FWD SIDE INNER SKIN HAS CRACK RUNNING FROM RIVET HOLE TO EDGE OF FRAME, JUST UNDER SECOND STOP FITTING. REMOVED DOUBLER, HFEC, CUT OUT DAMAGED SECTION, HFEC CUT OUT AND INSTALLED DOUBLER REPAIR AND TRIPLER 22 X 8 PER AV
- [SDR DHL9870644C](https://openairdocs.org/sdr/DHL9870644C.md): Rib · cracked · May 14, 1998 · N706DH · Boeing 72722C · Wing, Rib/Bulkhead
  > AT C-CHECK, RT UPPER RIB AT 70.5 WING CENTER SECTION HAS 2 CRACKS AT FWD LOWER HOLE. STOP DRILLED, HFEC, AND PERFORMED MODIFICATION PER S/B 57-0112. N/R 2073.
- [SDR DHL9870642C](https://openairdocs.org/sdr/DHL9870642C.md): Bulkhead Fitting · corroded · May 14, 1998 · N706DH · Boeing 72722C · Fuselage Main, Bulkhead
  > AT C-CHECK, CORROSION ON FITTING LOCATED ON AFT SIDE OF BULKHEAD AND KEEL BEAM FWD END LBL 15, WL 166. REMOVED AND REPLACED FITTING PER SRM 51-10-1. N/R 3580.
- [SDR DHL9870641C](https://openairdocs.org/sdr/DHL9870641C.md): Seat Track · corroded · May 14, 1998 · N706DH · Boeing 72722C · Fuselage, Seat/Cargo Attach Fittings
  > AT C-CHECK, CORROSION AT NUT PLATE ON OUTBD FLANGE OF SEAT TRACK LBL 46 BETWEEN BS 480 AND 600. REMOVED SEAT TRACK, REMOVED CORROSION FROM CABIN FLOOR, WITHIN LIMITS AND INSTALLED NEW TRACK PER SRM FROM BS 480 TO 550 PER SRM 53-10-5. N/R 3576.
- [SDR DHL9870640C](https://openairdocs.org/sdr/DHL9870640C.md): Skin · cracked · May 14, 1998 · N706DH · Boeing 72722C · Fuselage Main, Plate/Skin
  > AT C-CHECK, FWD ENTRY DOOR CUTOUT EXTERIOR SKIN JUST ABOVE UPPER FWD CORNER OF CUTOUT. STOP DRILLED CRACK, INSTALLED EXTERNAL DOUBLER PER S/B 53-186 21 X 50. N/R 3565.
- [SDR DHL9870639C](https://openairdocs.org/sdr/DHL9870639C.md): Angle · cracked · May 14, 1998 · N706DH · Boeing 72722C · Cargo/Baggage Doors
  > AT C-CHECK, LOWER FWD CARGO DOOR INTERIOR CRACK INTO RADIUS OF ANGLE SUPPORT, INSIDE AFT CTR SIDE. REMOVED AND REPLACED ANGLE AT LEFT LOWER END PER SRM 52-30-1, 6 X 4. N/R 3562.
- [SDR DHL9870638C](https://openairdocs.org/sdr/DHL9870638C.md): Skin · corroded · May 14, 1998 · N706DH · Boeing 72722C · Cargo/Baggage Doors
  > AT C-CHECK, LOWER FWD CARGO DOOR EXT SKIN HAS BULGE AT LWR FWD AREA. CUT OUT DAMAGED AREA, HFEC, INSTALLED EXTERNAL DOUBLER PER SRM 52-00-3, 7 X 6. N/R 3558.
- [SDR DHL9870637C](https://openairdocs.org/sdr/DHL9870637C.md): Seat Track · corroded · May 14, 1998 · N706DH · Boeing 72722C · Fuselage, Seat/Cargo Attach Fittings
  > AT C-CHECK, FWD CARGO RT SEAT TRACK STR 27R HAS CORROSION AT TOP AND BOTTOM BS 480 TO 510. N/R 3550.
- [SDR DHL9870626C](https://openairdocs.org/sdr/DHL9870626C.md): Angle · cracked · May 14, 1998 · N706DH · Boeing 72722C · Leading Edge Devices
  > AT C-CHECK, LEFT WING L/E, NR 2 SLAT OUTBD TRACK, INBD SUPPORT RIB AFT VERTICAL DOUBLER HAS A VERTICAL CRACK AT BOTTOM. REMOVED AND REPLACED ANGLE SUPPORT PER SRM 57-10-1, 16 LONG. N/R 1615.
- [SDR DHL9870625C](https://openairdocs.org/sdr/DHL9870625C.md): Rib · cracked · May 14, 1998 · N706DH · Boeing 72722C · Wing, Rib/Bulkhead
  > AT C-CHECK, LT UPPER RIB AT 70.5 WING CENTER SECTION HAS 2 CRACKS AT FWD UPPER HOLE AND 3 CRACKS AT FWD LOWER HOLE. STOP DRILLED CRACKS, HFEC, INSTALLED REPAIR AT LEFT WING PER S/B 57-0112 O/B OF 70.5. INSTALLED REPAIR AT I/B OF LT WING CENTER SECTION PER S/
- [SDR DHL9870619C](https://openairdocs.org/sdr/DHL9870619C.md): Skin · dented · May 14, 1998 · N706DH · Boeing 72722C · Cargo/Baggage Doors
  > AT C-CHECK, L/E OF AFT BAGGAGE BIN DOOR IS DENTED IN SEVERAL PLACES. REPLACED SKIN AT AFT CARGO DOOR PER SRM 52-30-02, 48 X 52.5. N/R 3549.
- [SDR DHL9870615C](https://openairdocs.org/sdr/DHL9870615C.md): Plate · cracked · May 14, 1998 · N706DH · Boeing 72722C · Wing, Plate/Skin
  > AT C-CHECK, RT WING BELOW NR 13 SPOILER REMOVED AND REPLACED CORRUGATE PLATE AT RT WING PER SRM 57-20-1. N/R 2090.
- [SDR DHL9870614C](https://openairdocs.org/sdr/DHL9870614C.md): Bracket · cracked · May 14, 1998 · N706DH · Boeing 72722C · Spoilers
  > AT C-CHECK, RT WING I/B SPOILER NR 11 HAS PANEL VERTICAL BRACKET CRACKED, ATTACHED TO SUPPORT ROD LOWER END. REMOVED AND REPLACED BRACKET PER SRM 51-10-1. N/R 2087.
- [SDR DHL9870613C](https://openairdocs.org/sdr/DHL9870613C.md): Plate · cracked · May 14, 1998 · N706DH · Boeing 72722C · Fuselage Main, Plate/Skin
  > AT C-CHECK, RT WING I/B PANEL SUPPORT CORRUGATED PLATE HAS CRACK AND LOOSE FASTENERS BETWEEN LOWER WING SPAR AND LOWER WING SKIN WS 350. REMOVED AND REPLACED SUPPORT PANEL PER SRM 51-10-1. N/R 2064.
- [SDR DHL9870602C](https://openairdocs.org/sdr/DHL9870602C.md): Cowling · torn · May 14, 1998 · N706DH · Boeing 72722C · Engine Cowling System
  > AT C-CHECK, NR 1 ENGINE COWL SKIN TORN BETWEEN NR 2 AND NR 3 LATCH. REMOVED DAMAGED AREA, INSTALLED DOUBLER REPAIR PER RM 54-10-3 6 X 3. N/R 6871.
- [SDR DHL9870601C](https://openairdocs.org/sdr/DHL9870601C.md): Cowling · corroded · May 14, 1998 · N706DH · Boeing 72722C · Engine Cowling System
  > AT C-CHECK, NR 1 ENG LOWER COWL HAS AN AREA OF CORROSION ON SKIN. CUT OUT DAMAGED SECTION, INSTALLED REPAIR PER SRM 54-10-3 FILLER 29 X 4.5 DOUBLER, 18.5 X 18.5. CUT OUT DAMAGED AREA OF SKIN AT INBD SIDE PER SRM 54-10-3 FILLER 29 X 5, DOUBLER 18 X 19. N/R
- [SDR DHL9870634C](https://openairdocs.org/sdr/DHL9870634C.md): Stiffener · cracked · May 13, 1998 · N706DH · Boeing 72722C · Wing Miscellaneous Structure
  > AT C-CHECK, RT WING LEADING EDGE FRONT SPAR OUTBD VERTICAL STIFFENER CRACKED AT LOWER END, NR 6 SLAT OUTBD. REPLACED VERTICALS STIFFENER PER SRM 51-10-1. N/R 2065.

Next page: https://openairdocs.org/deregistered/N706DH-2000-09-21/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 = 'N706DH' AND deregistration_id = 'N706DH-2000-09-21'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N706DH-2000-09-21/reports

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