# Service difficulty reports: N708DH, cancelled Sep 11, 2013

A list on [N708DH, cancelled Sep 11, 2013](https://openairdocs.org/deregistered/N708DH-2013-09-11.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 4 · 163 reports

- [SDR DHL2002708009](https://openairdocs.org/sdr/DHL2002708009.md): Button · broken · Jul 12, 2002 · N708DH · Boeing 72725 · Smoke Detection
  > SMOKE DETECTION SYSTEM NR 2 TEST BUTTON BROKE OFF DURING TEST. REPAIRED TEST BUTTON COVER IAW BMM 20-60-01.
- [SDR DHL2002708008](https://openairdocs.org/sdr/DHL2002708008.md): Fire Loop · out of position · Jun 8, 2002 · N708DH · Boeing 72725 · Fire Detection
  > NR 1 FIRE PROTECTION DETECTOR LIGHT ON. REPOSITIONED FIRE LOOP NR 1 ENG, OPS CHECKED GOOD IAW M/M 26-11-00.
- [SDR DHL2002708007](https://openairdocs.org/sdr/DHL2002708007.md): Fire Loop · out of position · Jun 5, 2002 · N708DH · Boeing 72725 · Fire Detection
  > ENG NR 1 FIRE DETECTION GROUND FAULT LIGHT FLASHES IN FLIGHT. REPOSITIONED ENG NR 1 FIRE LOOP AND REMOVED AND REPLACED NR 1 GROUND FAULT LENS COVER WITH NEW LENS COVER. NO FAULTS DETECTED, OPS CHECKS GOOD IAW MM 26-11-000.
- [SDR DHL2002708006](https://openairdocs.org/sdr/DHL2002708006.md): Windshield Wiper · out of adjust · May 14, 2002 · N708DH · Boeing 72725 · Windshield/Door Rain/Ice Removal
  > CAPTAIN'S SIDE WINDSHIELD WIPER DOES NOT FUNCTION IN THE LOW POSITION THE WIPER DOES NOT HAVE ADEQUATE RANGE OF MOTION TO KEEP THE UPPER PORTION OF THE WINDSHIELD CLEAR. RECLOCKED AND TESTED CAPT'S WINDSHIELD WIPER IAW MM 30-42-01. OPS CHECK NORMAL.
- [SDR DHL2002708005](https://openairdocs.org/sdr/DHL2002708005.md): Power Supply · not seated · Apr 15, 2002 · N708DH · Boeing 72725 · Fire Detection
  > APU FIRE DETECT SYS WILL NOT TEST. RESEATED APU FIRE WARNING POWER SUPPLY. OPS GOOD IAW MM 26-15-0.
- [SDR DHL2002708004](https://openairdocs.org/sdr/DHL2002708004.md): Light · inoperative · Mar 30, 2002 · N708DH · Boeing 72725 · Emergency Lighting
  > COCKPIT EMERGENCY LIGHTS DO NOT ILLUMINATE IN TEST. REMOVED AND REPLACED COCKPIT EMERGENCY EXIT LIGHT, OPS CK NORMAL IAW B727 MM 33-50-1.
- [SDR DHL2002708003](https://openairdocs.org/sdr/DHL2002708003.md): Transmission · failed · Mar 26, 2002 · N708DH · Boeing 72725 · Windshield/Door Rain/Ice Removal
  > CAPTAIN WINDSHIELD WIPER IS INOP. REMOVED AND REPLACED WINDSHIELD WIPER TRANSMISSION IAW B-M/M 30-42-11, OPS CHECK GOOD.
- [SDR DHL2002708002](https://openairdocs.org/sdr/DHL2002708002.md): Light · inoperative · Jan 28, 2002 · N708DH · Boeing 72725 · Emergency Lighting
  > FWD ENTRY EMERGENCY EXIT LIGHT INOP IN TEST POSITION (ON POSITION). REMOVED AND REPLACED FWD ENTRY WAY EMERGENCY EXIT LIGHT ASSY IAW M/M 33-5-00. OPS CHECK SERVICEABLE.
- [SDR DHL2002708001](https://openairdocs.org/sdr/DHL2002708001.md): Glare Shield · out of position · Jan 27, 2002 · N708DH · Boeing 72725 · Flight Compartment Equipment
  > F/O'S SLIDING WINDOW IS BINDING AGAINST GLARE SHIELD WHEN TRYING TO OPEN WINDOW. REPOSITIONED GLARE SHIELD AT F/O'S SLIDING WINDOW. OPS CHECK SERVICEABLE PER B727 M/M 56-12-11.
- [SDR DHL2001708016](https://openairdocs.org/sdr/DHL2001708016.md): Windshield Wiper · out of adj · Dec 18, 2001 · N708DH · Boeing 72725 · Windshield/Door Rain/Ice Removal
  > F/O WINDSHIELD WIPER DOES NOT WORK ON HALF SPEED. RUNS SLOW ON 3/4 SPEED.ADJUSTED WIPER TENSION PER 727 MM CHAPTER 30-42-01, OPS CK SATISFACTORY.
- [SDR DHL2001708014](https://openairdocs.org/sdr/DHL2001708014.md): Fire Loop · out of position · Nov 28, 2001 · N708DH · Boeing 72725 · Fire Detection
  > NR 2 ENGINE GROUND DET LIGHT ON DIM. OPENED COWLING, CLEARED FIRE LOOP FROM COWLING, CLOSED COWLING AND OP TEST NORMAL PER MM 26-00.
- [SDR DHL2001708015](https://openairdocs.org/sdr/DHL2001708015.md): Skin · cracked · Nov 24, 2001 · N708DH · Boeing 72725 · Ailerons
  > LEFT WING INBOARD AILERON UPPER SURFACE HAS 2 CRACKS 5.5 INCHES APART. OUTBOARD CRACK APPROX 2.25 INCHES LONG, INBOARD APPROX 2 INCHES. REMOVED EXISTING I/B AILERON SKIN LT SIDE IAW B727 SRM 57-30-2 (UPPER) REPLACED SKIN IAW B727 SRM 57-10-02. INSTALLED UPP
- [SDR DHL2001708013](https://openairdocs.org/sdr/DHL2001708013.md): Fire Loop · out of position · Oct 4, 2001 · N708DH · Boeing 72725 · Fire Detection
  > 1) NR 1 GROUND DETECTOR CIRCUIT ILLUMINATED IN FLIGHT.2) REPOSITIONED NR 1 ENGINE LOOP-NO FAULTS NOTED.OPS CK SATISFACTORILY PER MM 26-11-000.THIS CLEARS DMI 7284.STATUS: CLOSED
- [SDR DHL2001708012](https://openairdocs.org/sdr/DHL2001708012.md): Control Valve · failed · Aug 30, 2001 · N708DH · Boeing 72725 · Brake Anti-Skid Section
  > LT MAIN GEAR BRAKE DRAGGING ON TAXI OUT. TAXI BACK TO GATE PER PHONE PATCH. MX FLT CONT CVG LT MAIN BRAKE FIRE THERMAL DISCHARGED TIRE 1 TIRE 2 FIRE LAST OVER 45 MIN, FIRE REFLARED UP 3 TIMES IN 45 MIN. CHECKED/INSP SERVICE OF LT MAIN SHOCK STRUT / STRUT IS
- [SDR DHL2001708010](https://openairdocs.org/sdr/DHL2001708010.md): Fire Loop · grounded · Jul 22, 2001 · N708DH · Boeing 72725 · Fire Detection
  > NR 1 FIRE PROTECTION DET CIRCUIT GRD LIGHT ILLUMINATED IN FLT. FOUND ON ENG NR 1 FIRE PROTECTION LOOP WAS GROUNDING ON ENGINE COWLING, REPOSITIONED LOOP IAW B727 M/M 26-11-000 OPS CHECK SERVICEABLE.
- [SDR DHL2001708009](https://openairdocs.org/sdr/DHL2001708009.md): Fire Loop · out of position · Jul 21, 2001 · N708DH · Boeing 72725 · Fire Detection
  > ENGINE NR 1 DETECTOR CIRCUIT GRD WAS ILLUMINATED ON TAXI OUT FROM MCO. FOUND NR 1 ENG LOOP TOUCHING A BRACKET. REPOSITIONED LOOP. SYS NOW OPS CHECK NORMAL PER M/M 26-11-0.
- [SDR DHL2001708008](https://openairdocs.org/sdr/DHL2001708008.md): Actuator · Jul 7, 2001 · N708DH · Boeing 72725 · Drag Control Actuator
  > IN WINGS LEVEL DESCENT @ 280 KNOTS IAS SPEED BRAKE DEPLOYMENT CAUSES AIRCRAFT TO ROLL TO THE RIGHT. STOWING SPEED BRAKE CAUSES AIRCRAFT TO ROLL ABRUPTLY LEFT 15 DEGREES OPPOSITE DIRECTION YOKE DISPLACEMENT REQUIRED TO COUNTERACT ROLLING MOMENT. PROBLEM STILL P
- [SDR DHL2001708007](https://openairdocs.org/sdr/DHL2001708007.md): Controller · malfunctioned · Jul 6, 2001 · N708DH · Boeing 72725 · Drag Control Actuator
  > WHEN DEPLOYING FLIGHT SPOILERS AIRCRAFT ROLLS RT, WHEN STOWING FLIGHT SPOILERS AIRCRAFT ROLLS ABRUPTLY TO THE RT. INSPECTED ALL SPOILERS FOR DELAM, NONE NOTED. NO ACTUATORS BYPASSING AND LIFT OFF NORMAL. PICK UP NORMAL A&B SYS PER MM 2700.
- [SDR DHL2001708006](https://openairdocs.org/sdr/DHL2001708006.md): Computer · faulty · Jun 21, 2001 · N708DH · Boeing 72725 · Elevator Control System
  > DURING CRUISE FLT ELEVATOR FEEL DIFF PRESSURE LIGHT ILLUMINATED. PERFORMED ABNORMAL PROCEDURE. ELEVATOR FEEL DIFF PRESSURE LIGHT STAYED ILLUMINATED. REPLACED ELEVATOR FEEL COMPUTER PER MM REF 27-30-111. OPS CK GOOD.
- [SDR DHL2001708005](https://openairdocs.org/sdr/DHL2001708005.md): Receiver · unserviceable · Jun 21, 2001 · N708DH · Boeing 72725 · Navigation System
  > RADAR PAINTS GROUND CLUTTER AT 6 DEG TILT UP, WHEN TURNING PAINTS GROUND.CORRECTIVE ACTION - R&R RADAR RT PER M/M 34-41-01 OPS CK NORMAL. STATUS-CLOSED.
- [SDR DHL2001708003](https://openairdocs.org/sdr/DHL2001708003.md): Stud · missing · May 23, 2001 · N708DH · Boeing 72725 · Turbine Engine Accessory Drive
  > PRECAUTIONARY ENGINE SHUTDOWN DUE TO LOSS OF OIL. SHUTDOWN WHEN OIL PRESSURE STARTED TO DECREASE. ENGINE OIL PRESS/TEMP GOOD UNTIL TOUCHDOWN. PERFORMED ABNORMAL PROCEDURES. N1 & N2 ROTATION GOOD UNTIL TOUCHDOWN. ENGINE NR 1. FOUND GEARBOX THRU STUD FELL
- [SDR DHL2001708004](https://openairdocs.org/sdr/DHL2001708004.md): Engine · unserviceable · May 18, 2001 · N708DH · Boeing 72725 · Engine (Turbine/Turboprop)
  > REMOVED AND REPLACED ENG FOR EXCESSIVE OIL CONSUMPTION. REF W/O 600003170. REMOVED NR 1 ENG AND REPLACED PER DHL 727 TASK MANUAL MANUAL 71-01-03 THRU 71-01-18.
- [SDR DHL2001708002](https://openairdocs.org/sdr/DHL2001708002.md): Gearbox · leaking · Mar 16, 2001 · N708DH · Boeing 72725 · Turbine Engine Accessory Drive
  > NR 1 ENGINE LOST OIL QUANTITY AND PRESSURE IN FLIGHT. COMMENCED ENGINE SHUTDOWN AT INDICATION OF LOW OIL PRESSURE. T/S SYSTEM. REMOVED AND REPLACED N2 GEARBOX IAW P&W MM 72-60. NO LEAKS NOTED ON ENGINE RUN. TESTED OK IAW P&W MM72-00 AND DHL JRH.
- [SDR DHL2001708001](https://openairdocs.org/sdr/DHL2001708001.md): Altimeter · unserviceable · Jan 11, 2001 · N708DH · Boeing 72725 · Altimeter, Barometric/Encoder
  > ALTIMETER SPLIT BETWEEN CAPT AND F/O'S POSITION BY 70 FEET.INSTALLED SERVO-PNUMATIC ALTIMITER IN CAPTS POSITION PER M/M 34-11-0,OPS CHK GOOD.
- [SDR DHL2000708027](https://openairdocs.org/sdr/DHL2000708027.md): Sensor · damaged · Dec 21, 2000 · N708DH · Boeing 72725 · Overheat Detection
  > AFTER T/O NR 3 ENG STRUT OVERHEAT LIGHT ILLUMINATED,ABNORMAL PROCEDURES COMPLIED WITH. PLACED NR 3 ENGINE MODULATING VALVE ON DEFERRAL PER DHL MEL 36-11, DMI 3633.THIS SDR IS STILL OPEN. REMOVED AND REPLACED NR 3 ENGINE MOD VALVE SENSE LINE PER M/M 36-12-4
- [SDR DHL200070806C](https://openairdocs.org/sdr/DHL200070806C.md): Panel · cracked · Sep 20, 2000 · N708DH · Boeing 72725 · Vertical Stabilizer, Plate/Skin
  > VERT STAB RT LWR SLIDING SEAL TRACK AREA LWR FIX PANEL HAS 2 CRACKS. REMOVED AND REPLACED PANEL PER SRM 55-30-2. ALODINED AND PRIMED PER SRM 51-10-2.
- [SDR DHL200070812C](https://openairdocs.org/sdr/DHL200070812C.md): Panel · cracked · Sep 14, 2000 · N708DH · Boeing 72725 · Fuselage Main, Plate/Skin
  > PANEL NR 3429 I/B LARGE PANEL RADIOUS CORNER CRACK PROGRESSIVE BEYOND STOP DRILL HOLE. CUT OUT DAMAGED AREA AT PANEL PER SRM 51-40-1. INSTALLED DOUBLER REPAIR PER SRM 51-40-2. ALODINE AND PRIMED PER SRM 51-10-2.
- [SDR DHL2000708020](https://openairdocs.org/sdr/DHL2000708020.md): Panel · cracked · Sep 14, 2000 · N708DH · Boeing 72725 · Nacelle/Pylon, Plate/Skin
  > PANEL 5512 MOUNT HOLE CRACK. REPLACED PANEL 12 X 25 INCH PER SRM 51-30-2.
- [SDR DHL200070809C](https://openairdocs.org/sdr/DHL200070809C.md): Flange · cracked · Sep 13, 2000 · N708DH · Boeing 72725 · Leading Edge Devices
  > NR 9 L/E SLAT I/B TRACK O/B MOUNT AFT FLANGE IS CRACKED. ROUTED OUT CRACK PER SRM 51-10-1. INSTALLED DOUBLER REPAIR PER SRM 51-30-3. TREATED AND PRIMED PER SRM 51-10-3.
- [SDR DHL2000708012](https://openairdocs.org/sdr/DHL2000708012.md): Structure · damaged · Sep 13, 2000 · N708DH · Boeing 72725 · Trailing Edge Flaps
  > OUTBOARD FLAP T/E HONEYCOMB DETERIORATING. REPAIRED PER SRM 51-40-1. SIZE OF REPAIR 10 X 3 INCH.
- [SDR DHL2000708005](https://openairdocs.org/sdr/DHL2000708005.md): Rib · cracked · Sep 13, 2000 · N708DH · Boeing 72725 · Leading Edge Devices
  > LEFT WING LEADING EDGE SLAT RIB AFT FLANGE IS CRACKED. INSTALLED DOUBLER REPAIR PER SRM 57-50-3. SIZE OF REPAIR 8 X 2 INCH.
- [SDR DHL200070802C](https://openairdocs.org/sdr/DHL200070802C.md): Stringer · corroded · Sep 12, 2000 · N708DH · Boeing 72725 · Fuselage Main, Longeron/Stringer
  > EVIDENCE OF CORROSION AT S 23R BETWEEN BS 480 AND 500. REMOVED FASTENERS AND CUT OUT SECTION OF STR 23RT BETWEEN STA 480 AND 500 PER SRM 53-10-3. INSTALLED STR REPAIR PER SRM 53-10-3.
- [SDR DHL200070808C](https://openairdocs.org/sdr/DHL200070808C.md): Rib · cracked · Sep 11, 2000 · N708DH · Boeing 72725 · Leading Edge Devices
  > RT WING NR 4 6 L/E SLAT O/B TRACK I/B MOUNT RIB AFT FLANGE IS CRACKED AT HORIZ NUT PLATE STRAP UPPER ANGLE. REMOVED FASTENERS AT NR 6 SLAT O/B TRACK I/B RIB PER SRM 51-30-2. STOP DRILLED CRACK PER SRM 51-10-1. INSP CRACK AT STOP DRILL PER NDT MAN 51-00-00.
- [SDR DHL200070807C](https://openairdocs.org/sdr/DHL200070807C.md): Fitting · damaged · Sep 11, 2000 · N708DH · Boeing 72725 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPT RT SIDE BS 480 STATIC PORT FITTINGS PROTECTOR PANEL HAS BROKEN LUG AND MISSING FASTENER. INSTALLED NEW COVER PROTECTOR PER SRM 53-10-2. ALODINED AND PAINTED PER SRM 51-10-2. INSTALLED NEW PLACARD PER MM 20-10-1.
- [SDR DHL200070805C](https://openairdocs.org/sdr/DHL200070805C.md): Stringer Clip · corroded · Sep 11, 2000 · N708DH · Boeing 72725 · Fuselage Miscellaneous Structure
  > FWD BAGGAGE COMPT S-20L AT BS 500 WHERE CLIP ATTACHED TO STRINGER HAS A PIN HOLE AND SUSPECTED CORROSION. CUT OUT DAMAGED AREA PER SRM 53-10-3. TREATED AND PRIMED AREA PER SRM 51-10-2. INSTALLED REPAIR PER SRM 53-10-3.
- [SDR DHL2000708024](https://openairdocs.org/sdr/DHL2000708024.md): Latch · cracked · Sep 11, 2000 · N708DH · Boeing 72725 · Fuselage Miscellaneous Structure
  > FWD CARGO DOOR UP LOCK LATCH BRACKET LATCH CRACK. REPLACED LATCH PER SRM 51-10-2. MATERIAL USED 10 X 20 INCH.
- [SDR DHL2000708021](https://openairdocs.org/sdr/DHL2000708021.md): Angle · sheared · Sep 11, 2000 · N708DH · Boeing 72725 · Fuselage Miscellaneous Structure
  > SKIN BULGING, FASTENERS SHEARED ANGLE CORRODED AT TAIL SKID RIGHT SIDE STATION 1203. REPAIR PER B727 SRM 51-40-3, 51-30-2, 53-30-2. SIZE OF REPAIR 20 X 10 INCH.
- [SDR DHL2000708006](https://openairdocs.org/sdr/DHL2000708006.md): Web · cracked · Sep 11, 2000 · N708DH · Boeing 72725 · Fuselage Miscellaneous Structure
  > STA 294.5 STR 15L HORIZONTAL WEB HAS CRACK GOING BEYOND STOP DRILL. REPLACED HORIZONTAL WEB PER SRM 53-10-1.
- [SDR DHL2000708019](https://openairdocs.org/sdr/DHL2000708019.md): Pressure Panel · cracked · Sep 9, 2000 · N708DH · Boeing 72725 · Fuselage Main, Bulkhead
  > NOSE WHEEL WELL CEILING WEB PANEL SHOW CRACKS RUNNING FROM BS 268.5 AND LBL 20. INSTALLED 13 X 19 INCH DOUBLER PER B727 SRM 51-30-2.
- [SDR DHL2000708007](https://openairdocs.org/sdr/DHL2000708007.md): Angle · cracked · Sep 9, 2000 · N708DH · Boeing 72725 · Aerodynamic Fairings
  > FUSELAGE LOWER EXTERIOR BS 610 RT SIDE FAIRING PANEL ANGLE SUPPORT SHOWS CRACKS. INSTALL ANGLE SUPPORT. SIZE OF REPAIR 35 X 1 X 4 INCH.
- [SDR DHL200070813C](https://openairdocs.org/sdr/DHL200070813C.md): Web · cracked · Sep 8, 2000 · N708DH · Boeing 72725 · Cargo/Baggage Doors
  > MCD INTERNAL UPPER ROW OF LIGHTENING HOLES LOWER ROW NR 11 HOLE HAS A CRACK. TRIMMED OUT CRACK PER SRM 51-40-2. INSTALLED DOUBLER PER SRM 51-40-2. ALODINED AND PRIMED PER SRM 51-10-2.
- [SDR DHL200070810C](https://openairdocs.org/sdr/DHL200070810C.md): Angle · cracked · Sep 8, 2000 · N708DH · Boeing 72725 · Cargo/Baggage Doors
  > MAIN CARGO DOOR FWD EDGE LWR SECTION, SMALL SECTION OF LINING CRACKED. INSTALLED NEW ATTCH ANGLE AT MCD FWD EDGE LWR SECTION PER SRM 51-10-1. TREATED AND PRIMED PER SRM 51-10-2.
- [SDR DHL200070803C](https://openairdocs.org/sdr/DHL200070803C.md): Frame · cracked · Sep 8, 2000 · N708DH · Boeing 72725 · Fuselage Main, Frame
  > CARGO CABIN CIRCUMFERENTIAL FRAME BS 480 CRACKED WHERE ATTACH TO FUS STR 16/17L CRACK ABOUT 6 INCHES LONG. REMOVED FASTENERS AT CIRC FRAME STA 480 PER SRM 51-30-2. CUT OUT DAMAGED AREA PER SRM 53-10-4. INSTALLED REPAIR PER SRM 53-10-4. TREATED AND PRIMED P
- [SDR DHL200070801C](https://openairdocs.org/sdr/DHL200070801C.md): Duct · cracked · Sep 8, 2000 · N708DH · Boeing 72725 · Leading Edge Devices
  > EVIDENCE OF CRACK AT NR 6 L/E SLAT WELL UPPER STRAP I/B OF TELESCOPING DUCT. REMOVED UPPER STRAP AT NR 6 L/E SLAT I/B OF TELESCOPING DUCT PER SRM 51-30-2. TREATED AND PRIMED AREA PER SRM 51-10-2. REPLACED UPPER STRAP AT NR 6 L/E SLAT I/B OF TELESCOPING DUCT
- [SDR DHL2000708026](https://openairdocs.org/sdr/DHL2000708026.md): Strap · cracked · Sep 8, 2000 · N708DH · Boeing 72725 · Leading Edge Devices
  > EVIDENCE OF CRACK AT NR 6 L/E SLAT WELL UPPER STRAP I/B OF TELESCOPING DUCT. REPAIRED PER B727 SRM 51-10-2, 51-30-2. MATERIAL USED 12 X 20 INCH.
- [SDR DHL2000708014](https://openairdocs.org/sdr/DHL2000708014.md): Seat Track · corroded · Sep 8, 2000 · N708DH · Boeing 72725 · Fuselage, Seat/Cargo Attach Fittings
  > CORRODED CABIN SEAT TRACK AT LBL 25 BS 400. INSTALLED 40 INCHES OF NEW SEAT TRACK PER SRM 53-10-5.
- [SDR DHL2000708011](https://openairdocs.org/sdr/DHL2000708011.md): Floorbeam · corroded · Sep 8, 2000 · N708DH · Boeing 72725 · Fuselage Main, Floor Beam
  > LAVATORY AREA FLOORBEAM BS 328 AND BBL 54 AREA HAS CORROSION. INSTALL FLOORBEAM REPAIR PER SRM 51-40-4. SIZE OF REPAIR 35 X 9 INCH.
- [SDR DHL2000708010](https://openairdocs.org/sdr/DHL2000708010.md): Floorbeam · corroded · Sep 8, 2000 · N708DH · Boeing 72725 · Fuselage Main, Floor Beam
  > LAVATORY AREA FLOORBEAM BS 328 AND BBL 48 RIGHT AREA HAS CORROSION. INSTALL FLOORBEAM REPAIR PER 51-40-4. SIZE OF REPAIR 35 X 9 INCH.
- [SDR DHL2000708009](https://openairdocs.org/sdr/DHL2000708009.md): Floorbeam · corroded · Sep 8, 2000 · N708DH · Boeing 72725 · Fuselage Main, Floor Beam
  > LAVATORY AREA FLOORBEAM BS 328 AND BBL 36 RIGHT AREA HAS CORROSION. INSTALL FLOORBEAM REPAIR PER B727 SRM 51-40-4. SIZE OF REPAIR 35 X 9 INCH.
- [SDR DHL2000708008](https://openairdocs.org/sdr/DHL2000708008.md): Web · cracked · Sep 8, 2000 · N708DH · Boeing 72725 · Fuselage Miscellaneous Structure
  > WEB BENT AND CRACKED AT SEVERAL PLACES BETWEEN BS 1148 AND 1166 AT S-21R. INSTALL NEW INTERCOSTAL WEB PER SRM 53-10-1. SIZE OF REPAIR 16 X 4 INCH.

Next page: https://openairdocs.org/deregistered/N708DH-2013-09-11/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 = 'N708DH' AND deregistration_id = 'N708DH-2013-09-11'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N708DH-2013-09-11/reports

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