# Service difficulty reports: N709HA, cancelled May 16, 2006

A list on [N709HA, cancelled May 16, 2006](https://openairdocs.org/deregistered/N709HA-2006-05-16.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 4 · 153 reports

- [SDR HALA0000280](https://openairdocs.org/sdr/HALA0000280.md): Actuator · failed · Sep 2, 2000 · N709HA · Doug DC951 · Landing Gear Actuator
  > HNL - FLT 131 - NOSE GEAR UNSAFE LIGHT CAME ON. HYDRAULIC PUMP ON HIGH AND LIGHT WENT OFF. PUMP TURNED TO LOW LIGHT CAME ON. PROCEDURE WAS REPEATED AND LIGHT STAYED OUT WITH PUMPS IN LOW. REMOVED AND REPLACED NLG ACTUATING CYLINDER PER MM. GEAR SWING OK,
- [SDR HALA0000248](https://openairdocs.org/sdr/HALA0000248.md): Valve · leaking · Aug 6, 2000 · N709HA · Doug DC951 · Nose/Tail Landing Gear Strut/Axle
  > HNL - FLT 1126 - NOSE GEAR UNSAFE LIGHT ON AFTER RETRACTION. REPLACE NLG STRUT SERVICING VALVE. SERVICED WITH DRY NITROGEN. GEAR SWING OPS CHECK OK. NO FLUID LEAKAGE NOTED ON STRUT. STRUT LEAK CHECK OK. (M)
- [SDR HALA0000060](https://openairdocs.org/sdr/HALA0000060.md): Connector · failed · Feb 28, 2000 · N709HA · Doug DC951 · Landing Gear Position and Warning
  > HNL - FLT 541 - DURING UPLOCK CHECK, NOSE GEAR UNSAFE LIGHT CAME ON. EXTENDED GEAR OK. NEXT UPLATCH CHECK NOSE GEAR AND RIGHT GEAR UNSAFE LIGHTS CAME ON. EXTENDED GEAR AND LEFT IT DOWN. REPLACED RIGHT GEAR UPLOCK SENSOR CONNECTOR. ADJUSTED NOSE GEAR WARNI
- [SDR HALA0000016](https://openairdocs.org/sdr/HALA0000016.md): Gyro · malfunctioned · Jan 6, 2000 · N709HA · Doug DC951 · Attitude Gyro and Indicating System
  > HNL - FLT 348 - (AIR TURN BACK) BOTH COMPASSES, CAPTAIN AND FIRST OFFICER, OK GROUND, BUT ON TAKEOFF, WERE OFF BY 30 DEGREES TO 50 DEGREES OR MORE. BACK ON GROUND, THEY WENT TO 5 DEGREES OFF. REPLACED NR 1 AND NR 2 DIRECTIONAL GYROS. BOTH COMPASS SYSTEMS, O
- [SDR HALA9900282](https://openairdocs.org/sdr/HALA9900282.md): Control Box · malfunctioned · Dec 22, 1999 · N709HA · Doug DC951 · Landing Gear Door Retract Section
  > HNL - FLT 170 - NOSE GEAR DID NOT EXTEND. PERFORMED ALTERNATE GEAR EXTENTION PROCEDURE. GEAR CAME DOWN. NOSE SAFE LIGHT DID NOT ILLUMINATE, NOR DID NOSE LIGHT ILLUMINATE, GEAR UNSAFE. FOUND SKIN DAMAGED RT OF DRAIN HOLE, JUST AFT OF NLG. REPLACED PROXIMIT
- [SDR HALA9900274](https://openairdocs.org/sdr/HALA9900274.md): Sensor · failed · Dec 19, 1999 · N709HA · Doug DC951 · Landing Gear Position and Warning
  > NOSE GEAR UNSAFE LIGHT ON FLYBY TOWER CONFIRMED. RECYCLED GEAR ALL GREEN. ELECT CHECK, REPLACED LOCK SENSOR. REPLACED NOSE GEAR BUNGEE CYL GEAR SWING. LEAK CHECK GOOD PER MM 32-32-7. (M)
- [SDR HALA9900249](https://openairdocs.org/sdr/HALA9900249.md): Bolt · loose · Nov 27, 1999 · N709HA · Doug DC951 · Landing Gear Doors
  > HNL - FLT 203 - (ATB) AFTER TAKEOFF AND GEAR RETRACTION, THE RIGHT GEAR UNSAFE LIGHT WOULD EXTINGUISH. RECYCLED WITH NO CHANGE. ALSO, GEAR OPEN LIGHT REMAINED ON WITH GEAR DOWN. ALSO, SPOILERS WOULD NOT ARM. FOUND RIGHT MAIN GEAR DOOR LATCH MECHANISM HOLD
- [SDR HALA9900248](https://openairdocs.org/sdr/HALA9900248.md): Wire · broken · Nov 27, 1999 · N709HA · Doug DC951 · Landing Gear System Wiring
  > HNL - FLT 361 - CHECK NOSE GEAR DOWN LATCH AND INDICATION SYSTEM. GREEN NOSE GEAR DOWN LIGHT SLOW TO ACTIVATE THEN INTERMITTENT WITH GEAR WARNING HORN. FOUND BROKEN WIRES ON NLG LOCK SENSOR. REPLACED LOCK SENSOR. PROXIMITY CONTROL BOX BITE CHECK GOOD. (X)
- [SDR HALA9900076](https://openairdocs.org/sdr/HALA9900076.md): Coalescer Bag · contaminated · Mar 18, 1999 · N709HA · Doug DC951 · Humidity Control System
  > HNL - FLT 348 - SMOKE IN THE CABIN ON TAXI OUT. SEEMS TO ORIGINATE IN AFT AREA OF CABIN. SMOKE STOPPED WHEN A/C SWITCHES TURNED OFF. REPLACED LEFT AND RIGHT COALESCER BAG ASSEMBLIES. OPERATION AND LEAK CHECK OF BOTH SEPARATOR BAGS OK. (M)
- [SDR HALA9900041](https://openairdocs.org/sdr/HALA9900041.md): Skin · damaged · Feb 6, 1999 · N709HA · Doug DC951 · Wing, Plate/Skin
  > HNL - FLT 388 - (LOG PAGE NR A151708). ON PRE-FLIGHT, OBSERVED EVIDENCE OF BIRD STRIKE ON RIGHT LEADING EDGE. DID A WALK-AROUND INSPECTION. CHECKED ENGINE INLETS AROUND FUSELAGE AND WING. OSP CHECK OK. (X)
- [SDR HALA9900002](https://openairdocs.org/sdr/HALA9900002.md): Connector · failed · Jan 2, 1999 · N709HA · Doug DC951 · Fire Detection
  > FLT NR 70 - HNL - NR 2 ENGINE 'B' LOOP INOPERATIVE, 'A' TEST OK. REPLACED 'B' LOOP CONNECTOR. OPS CHECK GOOD. (M)
- [SDR HALA9800431](https://openairdocs.org/sdr/HALA9800431.md): Battery · discharged · Dec 30, 1998 · N709HA · Doug DC951 · Emergency Lighting
  > HNL - FORWARD OVERHEAD EMERGENCY LIGHT INOP. REPLACED BATTERIES, OPS CHECK GOOD. (M)
- [SDR HALA9800406](https://openairdocs.org/sdr/HALA9800406.md): Light · inop · Dec 8, 1998 · N709HA · Doug DC951 · Emergency Lighting
  > HNL - AFT TAIL CONE EMERGENCY LIGHT TEST FAILED. STAIRWAY LIGHTS LEFT AND RIGHT SIDE DOES NOT COME ON. ALSO, LIGHT OVER EVAC SLIDE DIM. TIGHTENED NUT ON TERMINAL STRIP. CLEANED LENS ON STAIRWAY LIGHT, EVAC SLIDE LIGHT, RELAMPED, GROUND CHECK, OK. (M)
- [SDR HALA9800199](https://openairdocs.org/sdr/HALA9800199.md): Driver Link · cracked · Jul 6, 1998 · N709HA · Doug DC951 · Engine Thrust Reverser
  > ITO - FLT 141 - (LOG PAGE NR A144265) - AFTER LANDING IN HILO, RIGHT THRUST REVERSER UNLOCK LIGHT ADVISORY LIGHT WOULD NOT EXTINGUISH. FOUND NR 2 ENGINE BOTTOM BUCKET INBD LOWER DRIVER LINK CRACKED. REPLACED DRIVER LINK PER MM 78-31-5. VISUALLY INSPECTED TH
- [SDR HALA9800173](https://openairdocs.org/sdr/HALA9800173.md): Battery Pack · discharged · Jun 24, 1998 · N709HA · Doug DC951 · Emergency Lighting
  > HNL - (LOG PAGE NR A143522). FORWARD EMERGENCY LIGHT BY THE FORWARD F/A SEAT IS INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY BATTERY PACK. OPS CHECK WAS OK. (X)
- [SDR HALA9800131](https://openairdocs.org/sdr/HALA9800131.md): Seal · leaked · May 26, 1998 · N709HA · Doug DC951 · Pneumatic Distribution System
  > FLT 114 - HNL - ON FLIGHT FROM HNL TO OGG, THE TAIL COMPARTMENT WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO HNL, WHERE AN UNEVENTFUL LANDING WAS MADE. REPLACED LT PERI SEAL DUCTS. FOUND BOTH ARM PERI SEALS LEAKING. REPLACED RT AND LT PERI SEALS. GROUN
- [SDR HALA9700131](https://openairdocs.org/sdr/HALA9700131.md): Connector · failed · Jun 16, 1997 · N709HA · Doug DC951 · Fire Detection
  > FLT 221 - HNL - THE RIGHT ENGINE 'B' LOOP LIGHT ON IN FLIGHT. MADE COMPLETE FIRE TEST. SELECTED UNLIGHTED 'A' LOOP. REPLACED THE RT ENGINE PYLON FIRE DETECTOR ELEMENT CONNECTOR. THE OPERATIONAL CHECK WAS GOOD. (M)
- [SDR HAL9773](https://openairdocs.org/sdr/HAL9773.md): Web · cracked · May 1, 1997 · N709HA · Doug DC951 · Wing Miscellaneous Structure
  > RIGHT WING TRAILING EDGE SUPPORT STRUCTURE BUCKLED, CRACKED, AND LEVEL 2 CORROSION JUST OUTBOARD OF SPOILER ACTUATOR, STA XRS-189. STOP DRILLED CRACK, FABRICATED DOUBLER AND WEB, AND INSTALLED PER SRM 57-01, FIG 4, SRM'S 51-30-2, 51-10-3, AND 57-01 FIG B. TO
- [SDR HAL9772](https://openairdocs.org/sdr/HAL9772.md): Skin · corrosion · May 1, 1997 · N709HA · Doug DC951 · Fuselage Main, Plate/Skin
  > AFT ACCESSORY COMPARTMENT, INTERNAL, LEVEL 2 CORROSION ON SKIN LAP JUST ABOVE LONGERON IAR FROM STA 1190 TO STA 1247. REMOVED CORROSION SRM 53-01 FIG 1 AND SRM 51-10-3, AND INSTALLED FAB DOUBLER OVER BLADE AREA PER SRM 53-04 FIG 12B, SRM 51-30-2, AND PER DAC
- [SDR HAL9771](https://openairdocs.org/sdr/HAL9771.md): Frame · corroded · May 1, 1997 · N709HA · Doug DC951 · Fuselage Main, Frame
  > AFT PIT FRAME STA 1130, STR 30, HAS LEVEL 2 CORROSION. FABRICATED FRAME PARTS, INSTALLED PER SRM 53-03, FIG 5 SRM 51-10-3. TOTAL TIME: 29,567 HOURS. TOTAL CYCLES, 73,626. (X)
- [SDR HALA9765](https://openairdocs.org/sdr/HALA9765.md): Intercostal · corroded · Apr 11, 1997 · N709HA · Doug DC951 · Fuselage Miscellaneous Structure
  > LEVEL 2 CORROSION ON FORWARD CARGO FLOOR INTERCOSTAL UNDER LEFT TIE RAIL FROM STATION 655 TO 693 LONGERON 28L. FABRICATED AND INSTALLED TWO STIFFENERS FROM STATION 674-693 LEFT AND RIGHT BETWEEN STRINGER 26 AND 27 PER SRM 51-30-2 AND 51-30-5 FABRICATED AND IN
- [SDR HALA9764](https://openairdocs.org/sdr/HALA9764.md): Frame · corroded · Apr 9, 1997 · N709HA · Doug DC951 · Fuselage Main, Frame
  > LEVEL 2 CORROSION ON FRAME AT STATION 1216 BETWEEN LBL 16 AND LBL 9. FABRICATED NEW FRAME REPAIR SPLICE AND SUPPORT ANGLE AND INSTALLED PER SRM 51-30, 51-30-2, 51-10-2, 51-10-3. (M)
- [SDR HALA9750](https://openairdocs.org/sdr/HALA9750.md): Closeout Rib · cracked · Apr 9, 1997 · N709HA · Doug DC951 · Nacelle/Pylon Structure
  > FOUND.6875 VERTICAL CRACK ON NR 2 PYLON CLOSING RIB, ADJACENT TO FS 1167 BOTTOM OF LIGHTING HOLE. FABRICATED DOUBLER, STOP DRILLED CRACK AND INSTALLED DOUBLER PER DAC ACTION NR 327482 OR SRM 51-10-2. (M)
- [SDR HAL9764](https://openairdocs.org/sdr/HAL9764.md): Frame · corroded · Apr 9, 1997 · N709HA · Doug DC951 · Fuselage Main, Frame
  > LEVEL 2 CORROSION ON FRAME AT STA 1216 BETWEEN LBL 16 AND LBL 9. FABRICATED NEW FRAME REPAIR SPLICE AND SUPPORT ANGLE AND INSTALLED PER SRM'S 51-30, 51-31-2, 51-10-2, AND 51-10-3. TOTAL TIME: 29,567 HOURS. TOTAL CYCLES, 73,626. (X)
- [SDR HAL9750](https://openairdocs.org/sdr/HAL9750.md): Rib · cracked · Apr 9, 1997 · N709HA · Doug DC951 · Nacelle/Pylon Structure
  > .6875 INCH VERTICAL CRACK ON NR 2 PYLON CLOSING RIB ADJACENT TO FS 1167 BOTTOM OF LIGHTING HOLE. FABRICATED DOUBLER, STOP DRILLED CRACK, AND INSTALLED DOUBLER PER DAC ACTION NR 327482 OR SRM 51-10-2. TOTAL TIME: 29,567 HOURS. TOTAL CYCLES, 73,626. (X)
- [SDR HALA9753](https://openairdocs.org/sdr/HALA9753.md): Angle · cracked · Apr 7, 1997 · N709HA · Doug DC951 · Fuselage Miscellaneous Structure
  > CRACK ON ANGLE ON APB STIFFENER RIGHT NR 3 FROM TOP RBL 64, STATION 1167 48 INCHES UP FROM FLOOR. REMOVED AND REPLACED ANGLE PER SRM 51-30-2 AND SB 53-166. (M)
- [SDR HALA9752](https://openairdocs.org/sdr/HALA9752.md): Webs · cracked · Apr 5, 1997 · N709HA · Doug DC951 · Fuselage Miscellaneous Structure
  > APB FORWARD FACE AREA, TWO CRACKS IN UPPER DOOR CUT OUT. LEFT UPPER CORNER HAS CRACK WHICH HAS EXTENDED BEYOND ORIGINAL STOP DRILL AND IS NOW 2.5 LONGERON RIGHT UPPER CORNER HAS EXTENDED BEYOND ORIGINAL STOP DRILLED AND IS NOW 1.8 INCHES LONGERON. REMOVED AN
- [SDR HAL9752](https://openairdocs.org/sdr/HAL9752.md): Bulkhead Web · cracked · Apr 5, 1997 · N709HA · Doug DC951 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD FORWARD FACE AREA, 2 EACH CRACKS IN UPPER DOOR CUT-OUT. LEFT UPPER CORNER HAS CRACK WHICH HAS EXTENDED BEYOND ORIGINAL STOP DRILL AND IS NOW 2.5 INCHES LONG. RIGHT UPPER CORNER HAS EXTENDED BEYOND ORIGINAL STOP DRILLED, AND IS NOW 1.8 I
- [SDR 97ZZZX2688](https://openairdocs.org/sdr/97ZZZX2688.md): Bulkhead Web · cracked · Apr 5, 1997 · N709HA · Doug DC951 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD FORWARD FACE AREA, 2 EACH CRACKS IN UPPER DOOR CUT-OUT. LEFT UPPER CORNER HAS CRACK WHICH HAS EXTENDED BEYOND ORIGINAL STOP DRILL AND IS NOW 2.5 INCHES LONG. RIGHT UPPER CORNER HAS EXTENDED BEYOND ORIGINAL STOP DRILLED, AND IS NOW 1.8 I
- [SDR 97ZZZM675](https://openairdocs.org/sdr/97ZZZM675.md): Webs · cracked · Apr 5, 1997 · N709HA · Doug DC951 · Fuselage Miscellaneous Structure
  > APB FORWARD FACE AREA, TWO CRACKS IN UPPER DOOR CUT OUT. LEFT UPPER CORNER HAS CRACK WHICH HAS EXTENDED BEYOND ORIGINAL STOP DRILL AND IS NOW 2.5 LONGERON RIGHT UPPER CORNER HAS EXTENDED BEYOND ORIGINAL STOP DRILLED AND IS NOW 1.8 INCHES LONGERON. REMOVED AN
- [SDR HALA9761](https://openairdocs.org/sdr/HALA9761.md): Frame · corroded · Apr 4, 1997 · N709HA · Doug DC951 · Fuselage Main, Frame
  > RIGHT SUPPORT FRAME OF TAIL SKID HAS LEVEL 2 CORROSION AND NUTPLATES AND RIVETS WITH LEVEL 2 CORROSION AFT ACCESSORY COMPARTMENT CENTERLINE BOTTOM BETWEEN STATION 1209 AND 1230. INSTALLED NEW NUTPLATES AND RIVETS AND AFT ACCESSORY COMPARTMENT BETWEEN STATION
- [SDR HAL9761](https://openairdocs.org/sdr/HAL9761.md): Frame · corroded · Apr 4, 1997 · N709HA · Doug DC951 · Fuselage Main, Frame
  > RT SUPPORT FRAME OF TAIL SKID HAS LEVEL 2 CORROSION AND NUTPLATES AND RIVETS WITH LEVEL 2 CORROSION AFT ACCESSORY COMPARTMENT, CENTERLINE BOTTOM BETWEEN STA 1209 AND STA 1230. INSTALLED NEW NUTPLATES AND RIVETS AT AFT ACCY COMPT BETWEEN STA 1209 AND STA 1230
- [SDR 97ZZZX2689](https://openairdocs.org/sdr/97ZZZX2689.md): Frame · corroded · Apr 4, 1997 · N709HA · Doug DC951 · Fuselage Main, Frame
  > RT SUPPORT FRAME OF TAIL SKID HAS LEVEL 2 CORROSION AND NUTPLATES AND RIVETS WITH LEVEL 2 CORROSION AFT ACCESSORY COMPARTMENT, CENTERLINE BOTTOM BETWEEN STA 1209 AND STA1230. INSTALLED NEW NUTPLATES AND RIVETS AT AFT ACCY COMPT BETWEEN STA 1209 AND STA 1230
- [SDR HALA9763](https://openairdocs.org/sdr/HALA9763.md): Floor Panel · corroded · Apr 3, 1997 · N709HA · Doug DC951 · Fuselage Floor Panel
  > AFT CARGO PIT FLOOR PANEL STATION 1047 HAS LEVEL 2 CORROSION ON ATTACH DOUBLERS AND 'U' CHANNELS HAVE DOUBLER HOLES, WORN/PULLED FASTENERS. 'U' CHANNELS AND ATTACH DOUBLERS HAVE LEVEL 1 CORROSION ON SKIN. FABRICATED AND INSTALLED NEW SUPPORT RIBS. U-CHANNEL
- [SDR HALA9756](https://openairdocs.org/sdr/HALA9756.md): Bulkhead Angle · cracked · Apr 3, 1997 · N709HA · Doug DC951 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD INT RIGHT OUTBOARD HORIZONTAL ANGLE STIFFENERS AT STRINGER 14, 15 AND 16 HAVE CRACKS 5. REMOVED AND REPLACED ANGLES PER SRM 53-05 FIG 93. INSTALLED PER SRM 51-30-2, 51-10-3 ON APB INT FWD SIDE AT STRINGER 15, 16 STATION 1167. COMPLETE
- [SDR HALA9751](https://openairdocs.org/sdr/HALA9751.md): Channel · cracked · Apr 3, 1997 · N709HA · Doug DC951 · Fuselage Miscellaneous Structure
  > APB SUPPORT CHANNEL HAS.75 INCH CRACK AT UPPER FASTENER LOCATION LBL 22 STATION 1167 UPPER DOOR JAMB AREA. REMOVED AND FABRICATED REPAIR CHANNEL, TREATED AND INSTALLED PER SRM 51-30-2, 51-30-5, 51-10-2, 51-10-3. (M)
- [SDR HAL9751](https://openairdocs.org/sdr/HAL9751.md): Channel · cracked · Apr 3, 1997 · N709HA · Doug DC951 · Fuselage Miscellaneous Structure
  > APB SUPPORT CHANNEL HAS.75 INCH CRACK AT UPPER FASTENER LOCATION. LBL 22 STA 1167 UPPER DOOR JAMB AREA. REMOVED AND FABRICATED REPAIR CHANNEL TREATED AND INSTALLED PER SRM'S 51-30-2, 51-30-5, 51-10-2, AND 51-10-3. TOTAL TIME: 29,567 HOURS. TOTAL CYCLES,
- [SDR HALA9770](https://openairdocs.org/sdr/HALA9770.md): Support · corroded · Mar 31, 1997 · N709HA · Doug DC951 · Fuselage Miscellaneous Structure
  > AFT CARGO STATION 855, FLOOR SUPPORT HAS NUMEROUS AREAS OF CORROSION LEVEL 2 FROM LBL 40 INCHES TO RBL 40 INCHES AT TOP AND BOTTOM OF SUPPORT. FABRICATED AND INSTALLED FLOOR SUPPORT. FABRICATED AND INSTALLED 2 STRAPS TREATED AND PRIMED IAW SRM 51-10-2, 51-10
- [SDR HALA9769](https://openairdocs.org/sdr/HALA9769.md): U-Channel · corroded · Mar 30, 1997 · N709HA · Doug DC951 · Fuselage Miscellaneous Structure
  > AFT LEFT GALLEY HAS CORROSION AND FILLER DROPPING LOOSE APPROX 5 INCHES ON FORWARD FACE STRUT OUTBOARD EDGE. REMOVED CORNER CORRODED 'U' CHANNEL IAW DC-9 SRM 51-10-2 ALODINED AND PRIMED PER DC-9 SRM 51-10-3. INSTALLED NEW FABRICATED 'U' CHANNEL WITH ATTACHME
- [SDR HALA9768](https://openairdocs.org/sdr/HALA9768.md): Support · corrosion · Mar 29, 1997 · N709HA · Doug DC951 · Fuselage Miscellaneous Structure
  > AFT ACCY COMPT LONGITUDINAL FRAME SUPPORT FROM 1209 TO 1230, RBL 10 HAS LEVEL 2 CORROSION. REMOVED AND REPLACED FRAME SUPPORT PER SRM 51-10-2, SRM 51-10-2, SRM 51-10-3, SRM 51-30-03 AND SRM 51-30-02. (M)
- [SDR HALA9767](https://openairdocs.org/sdr/HALA9767.md): Bulkhead · corroded · Mar 29, 1997 · N709HA · Doug DC951 · Fuselage Main, Bulkhead
  > AFT ACCESSORY COMP BULKHEAD 1230 HAS LEVEL 2 CORROSION AT ATTACH POINT TO SKIN FROM LONG 24L TO RBL 22. REMOVED CORROSION PER SRM 51-10-3 MATERIAL LOSS WITHIN LIMITS PER SRM 53-01 FIG 1. PRIME PER SRM 57-10-3. INSTALLED FABRICATED REPAIR WEB AND 5 L-ANGLES
- [SDR HALA9766](https://openairdocs.org/sdr/HALA9766.md): Intercostal · corroded · Mar 28, 1997 · N709HA · Doug DC951 · Fuselage Miscellaneous Structure
  > AT STATION 1060 TO 1068, STRINGER 29R TO STRINGER 30 WEDGE SHAPE ANGLE HAS.5 INCH CRACK FRAME ANGLES AND SUB STRUCTURE HAS LEVEL 2 CORROSION. REMOVED FABRICATED AND REPLACED INTERCOSTAL, GUSSETS AND SHAPE BRACKET PER SRM 53-05, 51-10-2, 51-10-3, 51-30-2 AND
- [SDR HALA9754](https://openairdocs.org/sdr/HALA9754.md): Longeron · cracked · Mar 27, 1997 · N709HA · Doug DC951 · Fuselage Main, Longeron/Stringer
  > STRINGER 17 LEFT AT STATION 1136 IS CRACKED AT LOWER FLANGE. STRINGER 17R AT STATION 1136 CRACKED AT FLANGE STRINGER 16R AT STATION 1136 IS CRACKED. REMOVED CRACKED LONGERON 17LT FABRICATED REPAIR LONGERON AT 17LT BETWEEN LT STATION 1126 AND 1167 PER SRM 51-
- [SDR HALA9743](https://openairdocs.org/sdr/HALA9743.md): Floorbeam · corroded · Mar 27, 1997 · N709HA · Doug DC951 · Fuselage Main, Floor Beam
  > CABIN FLOORBEAM STATION 1151 RBL 20 INCHES LEVEL 2 CORROSION ON UPPER SURFACE. REPAIRED CABIN FLOORBEAM STATION 1151 RBL 20 INCHES PER SRM 53-05 FIG 20 BY FABRICATING FILLER. DOUBLER AND RUB STRIP PER SRM 53-05 FIG 20. CUTTING OUT DAMAGED AREA, TREATING ARE
- [SDR HAL9754](https://openairdocs.org/sdr/HAL9754.md): Longeron · cracked · Mar 27, 1997 · N709HA · Doug DC951 · Fuselage Main, Longeron/Stringer
  > STR 17L AT STA 1136 IS CRACKED AT LOWER FLANGE. STR 17R AT STA 1136 CRACKED AT FLANGE. STR 16R AT STA 1136 IS CRACKED. REMOVED CRACKED LONGERON 17L;, FABRICATED REPAIR LONGERON AT 17L BETWEEN LT STA 1126 AND STA 1167 PER SRM 51-10-2, TREATED PER SRM 51-10-
- [SDR HAL9743](https://openairdocs.org/sdr/HAL9743.md): Floor Beam · corroded · Mar 27, 1997 · N709HA · Doug DC951 · Fuselage Main, Floor Beam
  > CABIN FLOOR BEAM STA 1151 RBL= 20 INCHES LEVEL 2 CORROSION ON UPPER SURFACE. REPAIRED CABIN FLOOR BEAM STA 1151 RBL= 20 INCHES PER SRM 53-05, FIG 20 BY FABRICATING FILLER, DOUBLER AND RUB STRIP PER SRM 53-05, FIG 20; CUTTNG OUT DAMAGED AREA, TREATING AREA AND
- [SDR HALA9744](https://openairdocs.org/sdr/HALA9744.md): Skin · corroded · Mar 26, 1997 · N709HA · Doug DC951 · Fuselage Main, Plate/Skin
  > KEEL BEAM LOWER SKIN BETWEEN MLG DOORS HAS LEVEL 1 AND LEVEL 2 CORROSION PRESENT THROUGHOUT. REMOVED CORROSION AND TREATED FS 783-840. REPAIRED FS 794 PER MD ACTION NR 325991 REPAIRED FS 840 ANGLE PER SRM 51-10-2 AND 51-10-3. (M)
- [SDR HALA9742](https://openairdocs.org/sdr/HALA9742.md): Frame · corroded · Mar 26, 1997 · N709HA · Doug DC951 · Fuselage Main, Frame
  > LEVEL 2 CORROSIO AFT CARGO COMPARTMENT STATION 984 ON FORMER FRAME FROM STRINGER 27L TO STRINGER 27R. FRAME WAS REPAIRED PER DOUGLAS DC-9 SRM 53-03 FIG 2A. (M)
- [SDR HAL9744](https://openairdocs.org/sdr/HAL9744.md): Keel Beam · corroded · Mar 26, 1997 · N709HA · Doug DC951 · Fuselage Main, Keel
  > KEEL BEAM LOWER SKIN BETWEEN MLG DOORS HAS LEVEL 1 AND LEVEL 2 CORROSION PRESENT THROUGHOUT. REMOVED CORROSION AND TREATED FS 783-840. REPAIRED FS 794 PER MD ACTION NR 325991. REPAIRED F/S 840 ANGLE PER SRM'S 51-10-2 AND 51-10-3. TOTAL TIME: 29,567 HOURS.
- [SDR HAL9742](https://openairdocs.org/sdr/HAL9742.md): Frame · corroded · Mar 26, 1997 · N709HA · Doug DC951 · Fuselage Main, Frame
  > LEVEL 2 CORROSION AFT CARGO COMPARTMENT STA 984 ON FORMER FRAME FROM S27L TO S27R. FRAME WAS REPAIRED PER DOUGLAS DC-9 SRM 53-03, FIG 2A. TOTAL TIME: 29,567 HOURS. TOTAL CYCLES, 73,626. (X)

Next page: https://openairdocs.org/deregistered/N709HA-2006-05-16/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 = 'N709HA' AND deregistration_id = 'N709HA-2006-05-16'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N709HA-2006-05-16/reports

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