# Service difficulty reports: N705DH, cancelled May 14, 2015

A list on [N705DH, cancelled May 14, 2015](https://openairdocs.org/deregistered/N705DH-2015-05-14.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 4 · 179 reports

- [SDR DHL2002705012](https://openairdocs.org/sdr/DHL2002705012.md): Light · Oct 21, 2002 · N705DH · Boeing 72722C · Emergency Lighting
  > 1) MAIN ENTRANCE DOOR EMERGENCY LIGHT WILL NOT CHARGE.2) REPLACED EMERGENCY LIGHT ASSEMBLY PER M/M 33-50-00. OPS CHECKED GOOD.
- [SDR DHL2002705011](https://openairdocs.org/sdr/DHL2002705011.md): Fire Loop · Aug 16, 2002 · N705DH · Boeing 72722C · Fire Detection
  > 1) #1 ENGINE FIRE LOOP WILL NOT TEST. 2) R&R #1 ENG FIRE LOOP PER M/M 26-11-00.
- [SDR DHL2002705010](https://openairdocs.org/sdr/DHL2002705010.md): Oxygen Mask · Jul 19, 2002 · N705DH · Boeing 72722C · Crew Oxygen System
  > 1) F/O'S O2 MASK BREATHER VALVE STUCK OPEN, MASK WILL NOT PULL TO FACE UPON INHALE.2) R + R F/O'S O2 MASK IAW B727 M/M 35-11-00, OP AND LEAK CHECK GOOD.
- [SDR DHL2002705009](https://openairdocs.org/sdr/DHL2002705009.md): Fire Warning · malfunctioned · Jul 18, 2002 · N705DH · Boeing 72722C · Fire Detection
  > FIRE BELL DID NOT SOUND DURING ENGINE, APU, OR LOWER CARGO FIRE TEST. PERFORMED AURAL WARN FIRE DETECTION TEST ON ENGINES, APU, W/W AND LOWER CARGO SMOKE IAW 31-26-00, OPS CHECK GOOD.
- [SDR DHL2002705008](https://openairdocs.org/sdr/DHL2002705008.md): Smoke Detector · Jul 13, 2002 · N705DH · Boeing 72722C · Smoke Detection
  > 1) LOWER CARGO FIRE DETECTOR SHOWS A FALSE ALARM & A4291 CODE WHEN MX TEST. 2) R&R SMOKE DETECTOR ON AFT CARGO PIT, OPS CK GOOD IAW SMM 26-16-01.
- [SDR DHL2002705007](https://openairdocs.org/sdr/DHL2002705007.md): Smoke Detector · faulty · Jul 11, 2002 · N705DH · Boeing 72722C · Smoke Detection
  > LWR CARGO SMOKE DETECTOR TEST ALARM FAULT ILLUMINATED WITH CODE F6929. REMOVED AND REPLACED FWD LWR CARGO SMOKE DET TESTED CHECK OK AS PER DHL B727-200 ADV MM SUPPLEMENT 26-16-01.
- [SDR DHL2002705002](https://openairdocs.org/sdr/DHL2002705002.md): Lamp · inoperative · Apr 26, 2002 · N705DH · Boeing 72722C · Smoke Detection
  > UPPER LEFT CABIN SMOKE DETECTOR LAMP, INOPERATIVE. REMOVED AND REPLACED BOTH UPPER CABIN SMOKE DETECTOR BULBS IAW MM 26- 17-00, 401. OPS CHECK GOOD.
- [SDR DHL2002705006](https://openairdocs.org/sdr/DHL2002705006.md): Bulkhead · cracked · Apr 19, 2002 · N705DH · Boeing 72722C · Fuselage Main, Bulkhead
  > PER CUSTOMER REQUEST, REPAIR CRACKS 2 EACH ON BS 870 BULKHEAD WL 200 AT RBL 45. CUT OUT DAMAGED SECTION OF BULKHEAD, FABRICATED AND INSTALLED DOUBLER AND FILLERS IAW B-727 SRM 53-10-9 FIG 4.
- [SDR DHL2002705005](https://openairdocs.org/sdr/DHL2002705005.md): Bulkhead · cracked · Apr 19, 2002 · N705DH · Boeing 72722C · Fuselage Main, Bulkhead
  > WHILE PERFORMING INSPECTION FOUND BS 870 BULKHEAD WEB CRACKED APPROX 2 INCHES RBL 60, WL 200 AS VIEWED FROM RT MLG W/W ABOVE SPOILER MIXER. CUT OUT CORRODED AREA, FABRICATED AND INSTALLED REPAIR PARTS.
- [SDR DHL2002705004](https://openairdocs.org/sdr/DHL2002705004.md): Support · corroded · Apr 18, 2002 · N705DH · Boeing 72722C · Fuselage Miscellaneous Structure
  > DURING DROP IN CHECK STA 870 WL 186 RBL 42, SUPPORT ANGLE HAS CORROSION BEHIND SPOILER MIXER. CUT OUT CORROSION ON SUPPORT ANGLE. FABRICATED AND INSTALLED REPAIR.
- [SDR DHL2002705003](https://openairdocs.org/sdr/DHL2002705003.md): Fitting · corroded · Apr 18, 2002 · N705DH · Boeing 72722C · Fuselage Miscellaneous Structure
  > DURING INSPECTION FOUND STA 880 WL 198 RBL 62 SMALL FRAME & ATTACH FITTING HAS CORROSION. REMOVED ATTACH ANGLE STA 880 WL 198 RBL 62 FROM FRAME. REMOVED CORROSION FROM FRAME, WITHIN LIMITS. FABRICATED NEW ATTACH ANGLE P/N 60-8892. INSTALLED NEW ATTACH ANGL
- [SDR DHL2002705543](https://openairdocs.org/sdr/DHL2002705543.md): Support Fitting · Mar 27, 2002 · N705DH · Boeing 72722C · Wing, Attach Fittings
  > UPON COMPLYING WITH VISUAL INSP OF LEFT WING, FOUND # 4 SPOILER ACTUATOR SUPPORT BRKT BOTTOM LEG CRACKED AND INBD AFT SPAR MOUNT ANGLE CRACKED AT LOWER END.
- [SDR DHL2002705001](https://openairdocs.org/sdr/DHL2002705001.md): Line · leaking · Feb 2, 2002 · N705DH · Boeing 72722C · Hydraulic System, Main
  > A SYS FAILURE 0,PRESSURE 0, QUANITY. REPLACED ENGINE DRIVEN PUMP PRESSURE FLEX LINE ON NR 2 ENGINE. LEAK AND OPS CHECK GOOD.
- [SDR DHL2001705007](https://openairdocs.org/sdr/DHL2001705007.md): Light · out of position · Dec 4, 2001 · N705DH · Boeing 72722C · Emergency Lighting
  > EMERGENCY EXIT LIGHT IN COCKPIT FELL OFF. REINSTALLED EMERGENCY EXIT LIGHT ASSY. OPS CHECK GOOD IAW MM 33-50-01.
- [SDR DHL2001705006](https://openairdocs.org/sdr/DHL2001705006.md): Battery · discharged · Sep 28, 2001 · N705DH · Boeing 72722C · Emergency Lighting
  > 1) EMERGENCY EXIT LIGHTS ABOVE DOORS INOP.2) REPLACED BATTERIES IN EMERGENCY EXIT LIGHTS IAW B-M/M 33-50-101 OPS CHECKED GOOD.STATUS: CLOSED
- [SDR DHL2001705004](https://openairdocs.org/sdr/DHL2001705004.md): Power Unit · failed · Aug 9, 2001 · N705DH · Boeing 72722C · Fire Detection
  > APU FIRE TEST INOP. REMOVED & REPLACED POWER UNIT IAW 26-15-0 OPS CHECK NORMAL.
- [SDR DHL2001705545](https://openairdocs.org/sdr/DHL2001705545.md): Plate · corroded · Jun 14, 2001 · N705DH · Boeing 72722C · Fuselage Miscellaneous Structure
  > ON LINE CHECK- BACK UP PLATE FOR INSPECTION HOLE AT STA 870 RBL 62 HAS CORROSION. REMOVED PRODUCTION DOUBLER AT STA 870 RBL 62 AND ACCESS PANEL. FABRICATED AND INSTALLED NEW PRODUCTION DOUBLER PER B-727 SRM 51-30-2 AND 53-10-1.
- [SDR DHL2001705544](https://openairdocs.org/sdr/DHL2001705544.md): Fitting · corroded · Jun 13, 2001 · N705DH · Boeing 72722C · Fuselage Miscellaneous Structure
  > ON LINE CHECK- BS 870 FITTING TO HORIZ BEAM RT WHEEL WELL SPLICE TEE IS CORRODED AT APPROX W/L 175. REMOVED SPLICE TEE AT BS 870 FITTING TO HORIZ BEAM RT W/W APPROX W/L 175 AS PER B-727 SRM 51-30-2. TRIMMED FITTING HORIZ FLANGES B/S 870 APPROX W/L 175 AS PER
- [SDR DHL2001705003](https://openairdocs.org/sdr/DHL2001705003.md): Turbine Wheel · damaged · Jun 2, 2001 · N705DH · Boeing 72722C · Turbine Section
  > EXCESSIVE VIBRATION AFTER TAKEOFF - DURING CLIMB NR 3 ENG VIBRATED AND LOST POWER. DECLARED EMERGENCY. RETURNED TO ROC. FOUND TURBINE WHEEL DAMAGED. REMOVED AND REPLACED ENGINE. CORRECTIVE ACTION - REMOVED AND REPLACED #3 ENGINE PN JT8D-7B OFF S/N 653870,
- [SDR DHL2001705538](https://openairdocs.org/sdr/DHL2001705538.md): Skin · cracked · May 7, 2001 · N705DH · Boeing 72722C · Leading Edge Devices
  > C-CHECK- LT WING IB L/E EDGE O/B SIDE UPPER SURFACE HAS 2 INCH CRACK. REMOVED DAMAGE AREA AND INSTALLED REPAIR PER B-727 SRM 57-30-4 FIG.6
- [SDR DHL2001705540](https://openairdocs.org/sdr/DHL2001705540.md): Bracket · cracked · May 5, 2001 · N705DH · Boeing 72722C · Drag Control Actuator
  > C-CHECK, NR 12 SPOILER ACTUATOR MOUNT BRACKET IS CRACKED, OUTBOARD LWR LUG.REMOVED AND REPLACED NR 12 SPOILER ACTUATOR BRACKET.
- [SDR DHL2001705515](https://openairdocs.org/sdr/DHL2001705515.md): Web · cracked · Apr 30, 2001 · N705DH · Boeing 72722C · Fuselage Miscellaneous Structure
  > C-CHECK WEB CRACKED AT NLG WW RT SIDE AT STA 257 W/L 180 IN BETWEEN PANELS 3123 AND3125 AT 3 EA LOCATION. INSTALLED FILLER & DOUBLER REPAIR AT NLG WW RT SIDE AT STA 257 W/L 180 AS PER B727 S/B 53-00-65.
- [SDR DHL2001705531](https://openairdocs.org/sdr/DHL2001705531.md): Rib · cracked · Apr 23, 2001 · N705DH · Boeing 72722C · Wing, Rib/Bulkhead
  > FOUND WING O/B RIB CRACKED USING HFEC INSP.
- [SDR DHL2001705509](https://openairdocs.org/sdr/DHL2001705509.md): Frame · corroded · Apr 21, 2001 · N705DH · Boeing 72722C · Fuselage Main, Frame
  > AT C-CHECK-NOSE W/W RT SIDE WALL, SIDE FRAME CORRODED AT INNER AREA OF FUSE TUNNEL STA 257 WL 180 AND IN BETWEEN ACCESS PANEL 3123. REMOVED FASTENER AND CUTOUT DAMAGE SECTION WITH CORROSION BEYOND LIMITS AT T-ANGLE WEB SUPPORT AT NOSE W/W RT SIDE WALL BETWEEN
- [SDR DHL2001705511](https://openairdocs.org/sdr/DHL2001705511.md): Stiffener · corroded · Apr 20, 2001 · N705DH · Boeing 72722C · Wing, Center Box
  > AT C-CHECK- WING CENTER SECTION STA 870 WEB VERTICAL STIFFENER AT BL 0 HAS CORROSION. REMOVED WEB VERTICAL STIFFENER AT WING CENTER SECTION FOR REPLACEMENT AS PER B727 SRM 51-30-2. INSTALLED NEW VERTICAL STIFFENER AT CENTER SECTION BS 870 BL 0 AS PER B727 SR
- [SDR DHL2001705500](https://openairdocs.org/sdr/DHL2001705500.md): Channel · corroded · Apr 20, 2001 · N705DH · Boeing 72722C · Fuselage Miscellaneous Structure
  > AT C-CHECK, FUSELAGE CORROSION AT HAT CHANNEL ATTACHED TO FLOORBEAM, STA 344 RBL 39. REMOVED HAT CHANNEL FOR REPLACEMENT AS PER SRM 51-30-22. FABRICATED AND INSTALLED NEW HAT CHANNEL AT FWD LAV STA 344 FROM RBL 15 TO RBL 60 AS PER SRM 53-10-2 FIG 3 AND 51-30
- [SDR DHL2001705530](https://openairdocs.org/sdr/DHL2001705530.md): Support Fitting · cracked · Apr 19, 2001 · N705DH · Boeing 72722C · Fuselage, Landing Gear Attach Fittings
  > AT C-CHECK - LEFT MAIN BEAM WHEEL WELL SUPPORT FITTING BS 930 SHOW'S CRACK AT L-18L, AS MKD LOWER FWD SIDE. CRACK VERIFY BY NDT AS PER 51-000 FIG 1 RUNNING BETWEEN FASTENERS 1 & 2 FROM BOTTOM. LEFT MAIN GEAR WHEEL WELL SUPPORT FITTING BS 930 CRACK HAS BEEN P
- [SDR DHL2001705518](https://openairdocs.org/sdr/DHL2001705518.md): Panel · damaged · Apr 19, 2001 · N705DH · Boeing 72722C · Wing, Plate/Skin
  > C-CHECK- LT WING FIXED LEADING EDGE. CORNER OF L/E PANEL IS BROKEN OFF. LOCATED DIRECTLY BELOW GHE I/B WING ROOT LANDING LIGHT ASSY. INSTALLED DOUBLER & FILLER.
- [SDR DHL2001705502](https://openairdocs.org/sdr/DHL2001705502.md): Floor Panel · corroded · Apr 19, 2001 · N705DH · Boeing 72722C · Fuselage Floor Panel
  > AT C-CHECK, FWD LAVATORY FWD FLOOR PANEL AT FS 303 HAS SEVERAL SPOTS OF CORROSION. REMOVED FWD LAV FLOOR PANEL AT STA 303 FOR REPLACEMENT AS PER B727 SRM 51-30-2. MADE NEW FLOOR PANEL MATERIAL USED 2024 T3 (.040) PO 83110438 LOT 220081 MATERIAL SIZE 30 X 12.
- [SDR DHL2001705525](https://openairdocs.org/sdr/DHL2001705525.md): Angle · corroded · Apr 19, 2001 · N705DH · Boeing 72722C · Fuselage Miscellaneous Structure
  > C-CHECK, FWD LAVATORY HAS CORROSION UNDER CENTER ANGLE AT FS 340 RBL 40.REMOVED DAMAGED SECTION AND INSTALLED REPAIR.
- [SDR DHL2001705522](https://openairdocs.org/sdr/DHL2001705522.md): Floor Support · cracked · Apr 19, 2001 · N705DH · Boeing 72722C · Fuselage Miscellaneous Structure
  > C-CHECK- CORROSION & CRACKED FLOOR SUPPORT AFT BAGGAGE COMPART LBL22 STA 1012-1027. REMOVED AND REPLACED FLOOR SUPPORT RUNNER FROM STA 960 TO STA 1027 LBL22 IAW B727 SRM 51-30-2.
- [SDR DHL2001705520](https://openairdocs.org/sdr/DHL2001705520.md): Floor Support · corroded · Apr 19, 2001 · N705DH · Boeing 72722C · Fuselage Miscellaneous Structure
  > C-CHECK- CORROSION, FLOOR SUPPORT AFT BAGGAGE COMPART STA 1160 STR 26 WL 156 LBL 24 UNDER SIDE. REMOVED AND INSTALLED NEW FLOOR SUPPORT AT AFT CARGO COMPT BS 1160 FROM STR 26L TO 26R AS PER B727SRM 51-40-2 AND 51-30-2.
- [SDR DHL2001705508](https://openairdocs.org/sdr/DHL2001705508.md): Retainer · cracked · Apr 18, 2001 · N705DH · Boeing 72722C · Fuel Storage
  > AT C-CHECK, FUSELAGE BS 870 REAR UPPER CHORD CENTER TANK RBL 46 TO OUT. HEAVY CORROSION AND PRESSURE SEAL RETAINER IS ALSO CRACKED. FOUND SEAL RETAINER ATTACH ANGLE TO BE CORRODED BS 870 RBL46 AND CRACKED. REMOVED ATTACH ANGLE FROM RBL 40 TO RBL 63 APPROX,
- [SDR DHL2001705506](https://openairdocs.org/sdr/DHL2001705506.md): Doubler · damaged · Apr 18, 2001 · N705DH · Boeing 72722C · Engine Cowling System
  > AT C-CHECK, NR 3 ENG, LWR COWL INTERNAL SURFACE, RIGHT AFTER 2ND U-BOLT, STRINGER PREVIOUS DOUBLER REPAIR SHOWS BIG HOLE (8 O''CLOCK POS APPROX). REMOVED DAMAGED EXISTING DOUBLER IAW B727 SRM 51-30-2. FABRICATED DOUBLER 8 X 12 2024-0.050 LOT 471153 PO 83196
- [SDR DHL2001705504](https://openairdocs.org/sdr/DHL2001705504.md): Seat Track · damaged · Apr 18, 2001 · N705DH · Boeing 72722C · Fuselage, Seat/Cargo Attach Fittings
  > AT C-CHECK, SEAT TRACK NR 6 SHOWS PREVIOUS HEAVY BLEND-OUT REWORK AT BS 680 - BS 695 RBL 45. REMOVED AND REPLACED SECTION OF SEAT TRACK FROM STA 680 TO STA 695 RBL 45 AS PER B727 SRM 51-10-2.
- [SDR DHL2001705514](https://openairdocs.org/sdr/DHL2001705514.md): Antenna · delaminated · Apr 17, 2001 · N705DH · Boeing 72722C · ATC Transponder System
  > AT C-CHECK- NR 2 ATC ANTENNA DELAMINATED AND GASKET DETERIORATED. REMOVED NR 2 ATC ANTENNA AND ROUTED TO STOCK IAW B727 MM 34-43-41. INSTALLED NR 2 ATC ANTENNA AS PER B727 MM 34-43-41. OPS CHECK NR 2 ATC SYSTEM PER B727 MM 34-43-0. OPS CHECK GOOD.
- [SDR DHL2001705507](https://openairdocs.org/sdr/DHL2001705507.md): Spoiler · delaminated · Apr 17, 2001 · N705DH · Boeing 72722C · Spoilers
  > C-CHECK, NR 9 SPOILER IS DELAMINATED AT FWD UPPER RT CORNER. REMOVED AND REPLACED NR 9 SPOILER PANEL PER B727 MM 27-62-1 P 401. ADJUST AND TEST. ACCOMPLISH OPERATIONAL CHECK OF NR 9 SPOILER IAW B727 CH 27-62-0 MM, OPS CHECK OK.
- [SDR DHL2001705503](https://openairdocs.org/sdr/DHL2001705503.md): Angle · cracked · Apr 17, 2001 · N705DH · Boeing 72722C · Engine Cowling System
  > AT C-CHECK, NR 2 ENG LT AFT COWL HAS LOWER FWD COENER WITH CRACK ANGLE. REMOVED AND REPLACED NR 2 LT AFT CORNER ANGLE. MATERIAL USED 2024T3.050 MATERIAL SIZE 12 X 2.5 PO 83112359 LOT 35803 AS PER B727 SRM 51-30-202. TREATED AND PRIMED AREA AS PER B727 SRM
- [SDR DHL2001705501](https://openairdocs.org/sdr/DHL2001705501.md): Attach Angle · cracked · Apr 17, 2001 · N705DH · Boeing 72722C · Fuselage Miscellaneous Structure
  > AT C-CHECK, MAIN CARGO DOOR CUTOUT, UPPER AFT CORNER AREA, GILL LINER ATTACH ANGLE SHOWS CRACK DAMAGE. REMOVED CRACKED GIL LINER ATTACH ANGLE AT MAIN CARGO DOOR CUTOUT AFT CORNER AREA AS PER B727 SRM 51-30-2. REMOVED AND REPLACED GILL LINER ATTACH ANGLE ON C
- [SDR DHL2001705529](https://openairdocs.org/sdr/DHL2001705529.md): Rib · cracked · Apr 17, 2001 · N705DH · Boeing 72722C · Wing, Rib/Bulkhead
  > C-CHECK- C/W DHL J/C MPRGAA1A57005 INSP. REPLACE WING OUTBOARD RIB WS 686.5. PERFORMED HFEC INSP OF RT WING RIB STA 686.5 RIB TO STRINGER ATTACH POINTS. CRACK FOUND AT UPPER STRINGER FLANGE AT STR 12. INSTALLED REPAIR.
- [SDR DHL2001705537](https://openairdocs.org/sdr/DHL2001705537.md): Rib · cracked · Apr 17, 2001 · N705DH · Boeing 72722C · Wing, Rib/Bulkhead
  > C-CHECK C/W DHL J/C MPRGAA1AS7005 INSP, REPLACE WING OUTBOARD RIB WS 738.5 RTPERFORMED HFEC INSP. OF RT. WING RIB STA 738.5 RIB, CRACK FOUND AT LOWER RIB STR 8. INSTALLED RIB REPAIR.
- [SDR DHL2001705528](https://openairdocs.org/sdr/DHL2001705528.md): Rib · cracked · Apr 17, 2001 · N705DH · Boeing 72722C · Wing, Rib/Bulkhead
  > C-CHECK C/W DHL J/C MPRGAA1A57005INSP, REPLACE WING OUTBOARD RIB WS 656.5. PERFORMED HFEC INSP OF RT WING RIB STA 656.5, RIB TO STRINGER ATTACH POINTS CRACK FOUND AT UPPER STRINGER FLANGE AT STRINGERS 13,12. INSTALLED REPAIRS.
- [SDR DHL2001705534](https://openairdocs.org/sdr/DHL2001705534.md): Beam · cracked · Apr 17, 2001 · N705DH · Boeing 72722C · Fuselage Main, Structure
  > ON C-CHECK, FWD SIDE BS 1183 VERTICAL BEAM LBL 26.83 WL 268 HAS A VISUAL CRACK TOP SIDE OF THE LIGHTENING HOLE (MARKED) REP MPRGAA1A53001 S/B 727-53AO173. AD 85-20-03. REMOVED FASTENERS ON VERTICAL BEAM STA 1183 BULKHEAD BL 2683, REMOVED STIFFENER TEES AT WL 2
- [SDR DHL2001705527](https://openairdocs.org/sdr/DHL2001705527.md): Rib · cracked · Apr 17, 2001 · N705DH · Boeing 72722C · Wing, Rib/Bulkhead
  > AT C CHECK C/W DHL J/C MPRGAA1A57005 INSP, REPLACE WING OUTBOARD RIB WS 546.5 RT. HFEC INDICATED RIB IS CRACKED.
- [SDR DHL2001705526](https://openairdocs.org/sdr/DHL2001705526.md): Skin · dented · Apr 17, 2001 · N705DH · Boeing 72722C · Cargo/Baggage Doors
  > C-CHECK- LOWER FWD CARGO DOOR EXT SKIN HAS MANY DENTS. REPAIRED CARGO DOOR SKIN.
- [SDR DHL2001705519](https://openairdocs.org/sdr/DHL2001705519.md): Attach Angle · damaged · Apr 17, 2001 · N705DH · Boeing 72722C · Fuselage Miscellaneous Structure
  > C-CHECK- MAIN CARGO DOOR CUT-OUT AT BS 510 GILLLINER ATTACHING ANGLE DAMAGED. REMOVED & REPLACED GILL LINER ATTACH ANGLE.
- [SDR DHL2001705516](https://openairdocs.org/sdr/DHL2001705516.md): Angle · cracked · Apr 16, 2001 · N705DH · Boeing 72722C · Wing Miscellaneous Structure
  > AT C-CHECK-T/E LWR PANEL SUPPORT ANGLE IS CRACKED AT STA 545. REPLACED T/E LWR PANEL SUPPORT ANGLE AT R/W STA 545 PER B727 SRM 51-30-2.
- [SDR DHL2001705505](https://openairdocs.org/sdr/DHL2001705505.md): Angle · bent · Apr 16, 2001 · N705DH · Boeing 72722C · Engine Cowling System
  > AT C-CHECK, NR 1 ENG, LWR COWL O/B FWD AREA, INT ANGLE WORN AND BENT. REFERENCE: FWD OF 2ND U-BOLT, UPPER OF OIL SERVICE DOOR. REMOVED AND REPLACED INTERNAL ANGLE ON 1 ENG, LWR COWL O/B FWD OF 2ND U-BOLT ABOVE OIL SERVICE DOOR PER B727 SRM 51-30-2. MAT USE
- [SDR DHL2001705521](https://openairdocs.org/sdr/DHL2001705521.md): Angle · corroded · Apr 16, 2001 · N705DH · Boeing 72722C · Fuselage Miscellaneous Structure
  > C-CHECK LT RAM AIR DUCT SUPPORT STRUCTURE HAS CORROSION BULGE BS 660 AT LT RAM AIR DOOR INBD HINGE. REMOVED AND REPLACED RAM AIR DUCT SUPPORT ANGLE AS PER B727 SRM 51-30-2.
- [SDR DHL2001705541](https://openairdocs.org/sdr/DHL2001705541.md): Pressure Panel · cracked · Apr 15, 2001 · N705DH · Boeing 72722C · Fuselage Main, Bulkhead
  > AT C-CHECK, NOSE GEAR WHEEL WELL RT SIDEWALL PANEL IS CRACKED BS 285.6 WL 158 CRACK RUNNING ALONG FASTENERS ROWS, 2 PLACES. ACCOMPLISHED HFEC INSP OF NOSE WHEEL WELL RT SIDEWALL PANEL. VERIFIED AND MARKED ENDS OF CRACKS. CUTOUT DAMAGE SECTION. NO FURTHER C

Next page: https://openairdocs.org/deregistered/N705DH-2015-05-14/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 = 'N705DH' AND deregistration_id = 'N705DH-2015-05-14'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N705DH-2015-05-14/reports

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