# Service difficulty reports: N68044, cancelled Jun 5, 2007

A list on [N68044, cancelled Jun 5, 2007](https://openairdocs.org/deregistered/N68044-2007-06-05.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 3 · 138 reports

- [SDR CLCA2007F001](https://openairdocs.org/sdr/CLCA2007F001.md): Fuel Filter · dirty · Mar 25, 2007 · N68044 · Doug DC1030 · Engine Fuel Distribution
  > NR 3 ENGINE FUEL FILTER PRESSURE DROP LIGHT ON. NR 2 ENGINE FUEL FILTER PRESSURE LIGHT ON AFTER ADDITIONAL ONE AND HALF HOUR AFTER TAKEOFF. DIVERTED TO CLO. REPLACED FILTERS SUMPED TANKS RUN-UP ALL ENGINES.
- [SDR RRXA010053](https://openairdocs.org/sdr/RRXA010053.md): Link · failed · Jun 21, 2001 · N68044 · Doug DC1010F · Landing Gear Doors
  > AFTER LANDING GEAR RETRACTION, VERY NOTICEABLE VIBRATION FROM FRONT PART OF ACFT. INCREASED VIBRATION WITH SPEED INCREASE. LOWERED LANDING GEAR, VIBRATION STILL PRESENT. LANDING GEAR OPERATION NORMAL. FOUND BAD NOSE GEAR DOOR DRIVE LINK. REMOVED AND REPLA
- [SDR RRXA010047](https://openairdocs.org/sdr/RRXA010047.md): Unknown · odor · May 12, 2001 · N68044 · Doug DC1010F · Air Distribution System
  > AIR COMING INTO THE AIRCRAFT FROM ANY OF THE 3 PACKS IS LADDEN WITH A STRONG SMOKEY ODOR WHICH BURNS THE EYES AND IS UNCOMFORTABLE TO BREATHE. IT IS MORE PRONOUNCED THE WARMER YOU SELECT THE TEMP. SUSPECT A PETROLEUM PRODUCT IS BEING HEATED/BURNED SOME WHE
- [SDR RRXA001088](https://openairdocs.org/sdr/RRXA001088.md): Link · worn · Dec 12, 2000 · N68044 · Doug DC1010F · Landing Gear Doors
  > AFTER TAKEOFF AND AFTER GEAR RETRACTION HEAVY VIBRATION WAS FELT IN THE NOSE WHEEL GEAR RETURNED BACK TO LAX AND AFTER PARKING FOUND RIGHT NOSEGEAR DOOR IN THE OPEN POSITION *** CORRECTIVE ACTION *** INSPECTED NOSE AREA FOUND RIGHT DOOR DOWN ON ARRIVAL FOU
- [SDR CALA9901506](https://openairdocs.org/sdr/CALA9901506.md): Skin · corroded · Nov 16, 1999 · N68044 · Doug DC1010 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND CORROSION ON SKIN AND AROUND LONGERON 48L AT STA 1791 INSIDE CENTER CARGO COMPARTMENT BELOW FLOOR. THE CORRODED AREA WAS REPAIRED IAW EA 10-5332-2-A0505.
- [SDR CALA9900203](https://openairdocs.org/sdr/CALA9900203.md): Battery Pack · discharged · Feb 28, 1999 · N68044 · Doug DC1010 · Emergency Lighting
  > THE EMERGENCY EVACUATION LIGHT AT PASSENGER ZONE B WAS INTERMITTENT. THE BATTERY PACK WAS REPLACED AND OPERATION CHECKED GOOD IAW MM 33-50-00.
- [SDR CALA9900200](https://openairdocs.org/sdr/CALA9900200.md): Fitting · corroded · Feb 25, 1999 · N68044 · Doug DC1010 · Wing, Landing Gear Attach Fittings
  > INSPECTION FOUND RT WING T/E CAVITY RT MLG MAIN FITTING CORRODED OVER SUPPORT ANGLE ON INBOARD END OVER LOWER WING BEAVERTAIL. THE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED WITH FASTENERS IAW SRM 51-31-01.
- [SDR CALA9900199](https://openairdocs.org/sdr/CALA9900199.md): Skin · corroded · Feb 25, 1999 · N68044 · Doug DC1010 · Trailing Edge Flaps
  > INSPECTION FOUND RT WING RT I/B TRAILING EDGE FLAP UPPER SKIN SURFACE UPPER LAP JOINT CORRODED. REPAIRED IAW ECRA 5752-01027.
- [SDR CALA9802197](https://openairdocs.org/sdr/CALA9802197.md): Fire Loop · damaged · Dec 25, 1998 · N68044 · Doug DC1010 · Fire Detection
  > THE NR 1 ENGINE 'A' LOOP FIRE WARNING LIGHT ILLUMINATED AFTER TAKEOFF FROM IAH. THE THROTTLE WAS PULLED BACK AND THE AMBER LIGHT AT FUEL START LEVER WENT OUT. FIRE HANDLE NR 1 WAS PULLED, BUT BOTTLE NR 2 DID NOT DISCHARGE. BOTTLE NR 1 WAS SELECTED AND DISCH
- [SDR CALA9800444](https://openairdocs.org/sdr/CALA9800444.md): Skin · cracked · Mar 14, 1998 · N68044 · Doug DC1010 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A.75 INCH CRACK THROUGH INNER AND OUTER SKIN OF CUTOUT FOR AFT PACK HOT AIR EXHAUST AT FORWARD LOWER CORNER, FS 586. DOUBLERS AND FILLER WERE INSTALLED IAW ENGINEERING ORDER COM NR 26752-1616I/R.
- [SDR CALA9800420](https://openairdocs.org/sdr/CALA9800420.md): Angle · torn · Mar 12, 1998 · N68044 · Doug DC1010 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND ANGLE TORN AT BOLT HOLES FOR CABLE PULLEY BRACKET AT AFT UPPER CORNER OF R-2 DOOR CUTOUT. THE SUPPORT CHANNEL WAS REMOVED. DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 51-31-1, 51-40-00, 51-21-1, AND 51-90-00.
- [SDR CALA9800419](https://openairdocs.org/sdr/CALA9800419.md): Doubler · corroded · Mar 12, 1998 · N68044 · Doug DC1010 · Wing Miscellaneous Structure
  > INSPECTION FOUND CORROSION ON RT WING LOWER LEADING EDGE SACRIFICIAL DOUBLER JUST INSIDE PANEL NR 617 AB FRONT SPAR AREA. THE CORROSION WAS REMOVED IAW SRM 51-21-01. THE CORRODED AREA WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 51-21-01 AND ECRA 5720-0164
- [SDR CALA9800418](https://openairdocs.org/sdr/CALA9800418.md): Angle · corroded · Mar 12, 1998 · N68044 · Doug DC1010 · Wing Spar
  > INSPECTION FOUND RT WING LEADING EDGE LOWER FRONT SPAR CAP ANGLE CORRODED NINE INCHES INBOARD OF FUEL VALVE. THE CORROSION WAS REMOVED IAW SRM 51-21-00. A METAL STRAP WAS FABRICATED AND INSTALLED IAW SRM 51-30-0.
- [SDR CALA9800417](https://openairdocs.org/sdr/CALA9800417.md): Angle · corroded · Mar 12, 1998 · N68044 · Doug DC1010 · Wing Spar
  > INSPECTION FOUND CORROSION ON LEADING EDGE LOWER SPAR CAP ANGLE LOCATED ABOVE AND JUST OUTBOARD OF NR 3 ENGINE PYLON OUTBOARD SIDE. SECTION OF SACRIFICIAL DOUBLER WAS CUT OUT AND AREA WAS REPAIRED IAW DOUGLAS DRAWING 26752-6204.
- [SDR CALA9800416](https://openairdocs.org/sdr/CALA9800416.md): Skin · corroded · Mar 12, 1998 · N68044 · Doug DC1010 · Wing, Plate/Skin
  > INSPECTION FOUND RT WING LEADING EDGE LOWER SKIN CORRODED AT XORS 538. THE CORROSION WAS REMOVED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-10.
- [SDR CALA9800385](https://openairdocs.org/sdr/CALA9800385.md): Frame · cracked · Mar 5, 1998 · N68044 · Doug DC1010 · Nacelle/Pylon, Frame/Spar/Rib
  > INSPECTION FOUND A 4 AND 2 INCH CRACK ON CENTER FRAME ON LT SIDE OF NR 2 ENGINE INLET INSIDE PANEL NR 363EL. THE CRACKS WERE STOP DRILLED IAW SRM 51-90-00. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 54-00-01 AND 51-21-01.
- [SDR CALA9800384](https://openairdocs.org/sdr/CALA9800384.md): Spar Cap · corroded · Mar 5, 1998 · N68044 · Doug DC1010 · Wing Spar
  > INSPECTION FOUND RT WING REAR SPAR LOWER CAP CORRODED AROUND PLATE NUTS ON UPPER SURFACE FROM STA XORS 433 TO 500. A REPAIR WAS INSTALLED IAW SRM 51-31-01.
- [SDR CALA9800383](https://openairdocs.org/sdr/CALA9800383.md): Bracket · cracked · Mar 5, 1998 · N68044 · Doug DC1010 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1 INCH CRACK IN WALL BRACKET AT R-1 DOOR FORWARD FRAME. A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 53-00-01.
- [SDR CALA9800382](https://openairdocs.org/sdr/CALA9800382.md): Frame · punctured · Mar 5, 1998 · N68044 · Doug DC1010 · Fuselage Main, Frame
  > INSPECTION FOUND A HOLE ON CENTER CARGO AFT FRAME CUTOUT. THE HOLE WAS ROUNDED OUT IAW SRM 53-00-01. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-00-01 AND 51-21-01.
- [SDR CALA9800381](https://openairdocs.org/sdr/CALA9800381.md): Flap · split · Mar 5, 1998 · N68044 · Doug DC1010 · Trailing Edge Flaps
  > INSPECTION FOUND INBOARD EDGE OF RT INBOARD FLAP TRAILING EDGE SPLIT. THE AREA WAS SANDED AND A FIBERGLASS OVERLAY WAS APPLIED IAW SRM 51-43-00.
- [SDR CALA9800380](https://openairdocs.org/sdr/CALA9800380.md): Skin · dented · Mar 5, 1998 · N68044 · Doug DC1010 · Trailing Edge Flaps
  > INSPECTION FOUND A DENT NEAR INBOARD LOWER CORNER OF RT INBOARD FLAP UPPER SKIN. THE DENTED AREA WAS CUT OUT IAW SRM 57-00-01, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-00-01.
- [SDR CALA9800402](https://openairdocs.org/sdr/CALA9800402.md): Charger · inoperative · Mar 4, 1998 · N68044 · Doug DC1010 · Emergency Lighting
  > THE L-4 DOOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BATTERY CHARGER WAS REMOVED AND REPLACED IAW MM 33-50-1.
- [SDR CALA9800401](https://openairdocs.org/sdr/CALA9800401.md): Rib · cracked · Mar 4, 1998 · N68044 · Doug DC1010 · Fuselage Main, Frame
  > INSPECTION FOUND TWO 1.5 INCH CRACKS IN NR 3 PACK COMPARTMENT RIB AT STA 555 BETWEEN LONGERON 30 AND 31. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-0.
- [SDR CALA9800400](https://openairdocs.org/sdr/CALA9800400.md): Longeron · cracked · Mar 4, 1998 · N68044 · Doug DC1010 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND A 2 INCH CRACK IN LONGERON 32R AT STA 555 UNDER CIRCUMFERENTIAL. THE CRACKED SECTION WAS REMOVED AND A NEW SECTION OF LONGERON WAS SPLICED IN IAW SRM 53-10-00.
- [SDR CALA9800379](https://openairdocs.org/sdr/CALA9800379.md): Skin · cracked · Mar 4, 1998 · N68044 · Doug DC1010 · Spoilers
  > INSPECTION FOUND A 2 INCH CRACK WITH DENT IN UPPER SURFACE OF RT WING NR 4 SPOILER. THE CRACKED AND DENTED AREA WAS CUT OUT, A HOT BOND REPAIR WAS INSTALLED IAW SRM 51-71-00.
- [SDR CALA9800378](https://openairdocs.org/sdr/CALA9800378.md): Angle · corroded · Mar 4, 1998 · N68044 · Doug DC1010 · Wing Miscellaneous Structure
  > INSPECTION FOUND ANGLE LOCATED BELOW AND INBOARD OF UPPER WING TRAILING EDGE MOST INBOARD AFT PANEL CORRODED. THE ANGLE WAS REMOVED IAW SRM 51-31-01. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-31-01.
- [SDR CALA9800377](https://openairdocs.org/sdr/CALA9800377.md): Skin · gouged · Mar 4, 1998 · N68044 · Doug DC1010 · Trailing Edge Flaps
  > INSPECTION FOUND A GOUGE IN RT WING OUTBOARD FLAP LOWER SKIN APPROXIMATELY 12 OUTBOARD OF OUTBOARD HINGE. THE GOUGED AREA WAS CUT OUT IAW SRM 57-00-01. FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 57-00-01, 51-21-01, 51-31-01, AND 51-41-01.
- [SDR CALA9800376](https://openairdocs.org/sdr/CALA9800376.md): Skin · cracked · Mar 4, 1998 · N68044 · Doug DC1010 · Wing, Plate/Skin
  > INSPECTION FOUND A 1 INCH CRACK IN LT WING LEADING EDGE SKIN AT NR 5 LEADING EDGE SLAT INBOARD TRACK CUTOUT. REMOVED FASTENER IAW SRM 51-31-01. THE CRACK WAS STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-00-01.
- [SDR CALA9800375](https://openairdocs.org/sdr/CALA9800375.md): Skin · bulged · Mar 4, 1998 · N68044 · Doug DC1010 · Trailing Edge Flaps
  > INSPECTION FOUND LT INBOARD FLAP UPPER SURFACE BULGED WITH POPPED AND PULLING FASTENERS. THE LT INBOARD FLAP WAS REMOVED AND REPLACED.
- [SDR CALA9800374](https://openairdocs.org/sdr/CALA9800374.md): Skin · disbonded · Mar 4, 1998 · N68044 · Doug DC1010 · Spoilers
  > INSPECTION FOUND LT WING NR 1 SPOILER CORRODED AND DISBONDED AT UPPER SURFACE OUTBOARD HINGE. THE SPOILER WAS REMOVED AND REPLACED.
- [SDR CALA9800373](https://openairdocs.org/sdr/CALA9800373.md): Skin · delaminated · Mar 4, 1998 · N68044 · Doug DC1010 · Spoilers
  > INSPECTION FOUND LOWER SURFACE OF RT WING NR 5 SPOILER DELAMINATED. THE SPOILER WAS REMOVED AND REPLACED.
- [SDR CALA9800359](https://openairdocs.org/sdr/CALA9800359.md): Vane · cracked · Mar 1, 1998 · N68044 · Doug DC1010 · Leading Edge Devices
  > INSPECTION FOUND A 1 INCH CRACK IN RT WING INBOARD FLAP VANE AT STA XW 280. THE FLAP VANE WAS REMOVED, REPAIRED AND REINSTALLED IAW MM 27-50-01.
- [SDR CALA9800357](https://openairdocs.org/sdr/CALA9800357.md): Skin · corroded · Mar 1, 1998 · N68044 · Doug DC1010 · Ailerons
  > INSPECTION FOUND RT WING INBOARD AILERON UPPER SKIN DELAMINATED AND CORRODED. THE AILERON WAS REMOVED, REPAIRED AND REINSTALLED IAW MM 27-10-01.
- [SDR CALA9800358](https://openairdocs.org/sdr/CALA9800358.md): Vane · disbonded · Feb 28, 1998 · N68044 · Doug DC1010 · Leading Edge Devices
  > INSPECTION FOUND LT WING INBOARD FLAP VANE DISBONDED ON UPPER SURFACE. THE FLAP VANE WAS REMOVED, REPAIRED, AND REINSTALLED IAW MM 57-54-00.
- [SDR CALA9800356](https://openairdocs.org/sdr/CALA9800356.md): Skin · corroded · Feb 28, 1998 · N68044 · Doug DC1010 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND UPPER SURFACE OF WING CENTER SECTION SKIN CORRODED FORWARD OF PRESSURE PANEL AT STA 1361, RBL 43 TO 85. REPAIRED IAW SRM 51-21-01.
- [SDR CALA9800355](https://openairdocs.org/sdr/CALA9800355.md): Stiffener · galled · Feb 28, 1998 · N68044 · Doug DC1010 · Nacelle/Pylon Structure
  > INSPECTION FOUND VERTICAL STIFFENERS AT LEFT AND RIGHT SIDE OF NR 3 PYLON HAD ELONGATED HOLES AND WERE GALLED AT PAN SUPPORT RIB. THE STIFFENERS WERE REMOVED IAW SRM 51-10-1. NEW STIFFENERS WERE FABRICATED AND INSTALLED IAW SRM 51-10-00, 51-21-01, AND 51-10-
- [SDR CALA9800354](https://openairdocs.org/sdr/CALA9800354.md): Skin · corroded · Feb 28, 1998 · N68044 · Doug DC1010 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND CORROSION ON FUSELAGE SKIN AT STA 1810, LONGERON 45-47L. THE CORRODED AREA WAS REMOVED, STRAP AND FINGER DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 51-30-00, 51-21-01, 51-10-00, AND ECRA 5310-03680.
- [SDR CALA9800353](https://openairdocs.org/sdr/CALA9800353.md): Fitting · corroded · Feb 28, 1998 · N68044 · Doug DC1010 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND TENSION TIE FITTING CORRODED AT STA 595, LONGERON 48L. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-31-01.
- [SDR CALA9800352](https://openairdocs.org/sdr/CALA9800352.md): Floorbeam · corroded · Feb 28, 1998 · N68044 · Doug DC1010 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED INSIDE OF FORWARD BAGGAGE BIN BELOW RIGHT PALLET GUIDE RAIL AND BEAM WEB HAD A 3 INCH CRACK AT STA 601, LONGERON 43R. THE CORRODED SECTIONS OF BEAM WERE REMOVED, REPAIR SECTIONS WERE FABRICATED AND INSTALLED IAW ECRA 5310-0
- [SDR CALA9800351](https://openairdocs.org/sdr/CALA9800351.md): Bolt · broken · Feb 28, 1998 · N68044 · Doug DC1010 · Wing Miscellaneous Structure
  > INSPECTION FOUND BOLT BROKEN AT REAR SPAR LOWER SIDE ON REAR SPAR TO FUEL TANK ON RT WING OUTBOARD SUPPORT INBOARD AILERON. THE RT ASSEMBLY STUDS WERE REMOVED AND REPLACED AND LEAK AND OPERATIONAL CHECKS WERE GOOD IAW MM 57-41-01.
- [SDR CALA9800350](https://openairdocs.org/sdr/CALA9800350.md): Rib · cracked · Feb 28, 1998 · N68044 · Doug DC1010 · Wing, Rib/Bulkhead
  > INSPECTION FOUND A 10 INCH CRACK IN RIB OF RT WING LOWER LEADING EDGE JUST OUTBOARD OF SLAT DRIVE MECHANISM. THE RIB WAS REMOVED AND A NEW RIB WAS FABRICATED AND INSTALLED IAW SRM 51-90-00.
- [SDR CALA9800341](https://openairdocs.org/sdr/CALA9800341.md): Bracket · corroded · Feb 26, 1998 · N68044 · Doug DC1010 · Wing Miscellaneous Structure
  > INSPECTION FOUND CORROSION AT BRACKET ATTACHED TO RT WING TRAILING EDGE BEAM WHERE PANEL REMOVED, FORWARD OF NR 1 SPOILER OUTBOARD HINGE AREA. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-33-01, 53-00-01, AND 51-21-01.
- [SDR CALA9800340](https://openairdocs.org/sdr/CALA9800340.md): Longeron · corroded · Feb 26, 1998 · N68044 · Doug DC1010 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND LONGERON 48L CORRODED AROUND FASTENERS FROM STA 595 FORWARD TO STA 580 INSIDE OF LT A/C BAY. THE LONGERON WAS REMOVED AND REPLACED IAW SRM 51-31-01.
- [SDR CALA9800339](https://openairdocs.org/sdr/CALA9800339.md): Rib · cracked · Feb 26, 1998 · N68044 · Doug DC1010 · Ailerons
  > INSPECTION FOUND A 1 INCH CRACK IN OUTBOARD RIB OF LT OUTBOARD AILERON. THE RIB WAS REMOVED AND A NEW RIB WAS FABRICATED AND INSTALLED IAW SRM 57-51-01.
- [SDR CALA9800338](https://openairdocs.org/sdr/CALA9800338.md): Rib · cracked · Feb 26, 1998 · N68044 · Doug DC1010 · Leading Edge Devices
  > INSPECTION FOUND A 4 CRACK IN FLANGE OF LT NR 1 SLAT OUTBOARD END RIB. THE WEB AND RIB WERE REMOVED IAW SRM 51-31-10. A NEW RIB WAS INSTALLED IAW 51-31-10 AND 51-21-01. SKIN WAS INSTALLED IAW SRM 51-01-10.
- [SDR CALA9800337](https://openairdocs.org/sdr/CALA9800337.md): Stiffener · cracked · Feb 26, 1998 · N68044 · Doug DC1010 · Nacelle/Pylon Structure
  > INSPECTION FOUND A 1 INCH CRACK IN VERTICAL STIFFENER AT TOP OF NR 1 PYLON ON AFT SIDE OF YN 342.0 FORGING AT INBOARD SIDE. REPAIR WAS ACCOMPLISHED IAW SRM 54-00-01.
- [SDR CALA9800336](https://openairdocs.org/sdr/CALA9800336.md): Bulkhead T · cracked · Feb 26, 1998 · N68044 · Doug DC1010 · Fuselage Main, Bulkhead
  > INSPECTION FOUND A 2.5 CRACK THROUGH FASTENER HOLE ON VERTICAL LEG OF BULKHEAD T AT STA 1156 BETWEEN LONGERON 40L AND 39L. A NEW TEE CAP WAS INSTALLED IAW EA SA003-5310-03391.
- [SDR CALA9800329](https://openairdocs.org/sdr/CALA9800329.md): Floorbeam · corroded · Feb 24, 1998 · N68044 · Doug DC1010 · Fuselage Main, Floor Beam
  > INSPECTION FOUND UPPER CAP OF FLOORBEAM IN AFT BIN CORRODED IN SPOTS FROM LEFT TO RIGHT END AROUND SCREW HOLES AND TIE DOWN TRACK MOUNT SCREWS AT BOTTOM, STA 1821. THE FLOORBEAM WAS REMOVED AND REPLACED IAW SRM 51-31-01.
- [SDR CALA9800328](https://openairdocs.org/sdr/CALA9800328.md): Splice · corroded · Feb 24, 1998 · N68044 · Doug DC1010 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND SPLICE IN AFT CARGO BIN CORRODED AT STA 1853, LONGERON 42L. NEW PARTS WERE FABRICATED AND INSTALLED IAW SRM 51-21-00.
- [SDR CALA9800327](https://openairdocs.org/sdr/CALA9800327.md): Support · corroded · Feb 24, 1998 · N68044 · Doug DC1010 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND UPPER CAP OF FLOOR SUPPORT IN CENTER CARGO COMPARTMENT CORRODED AT STA 1721, RBL 33. THE CORRODED AREA WAS CUT OUT, REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-00-01 AND 51-21-01.

Next page: https://openairdocs.org/deregistered/N68044-2007-06-05/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 = 'N68044' AND deregistration_id = 'N68044-2007-06-05'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N68044-2007-06-05/reports

---
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