# Service difficulty reports: N102DA

A list on [N102DA](https://openairdocs.org/aircraft/N102DA.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR DL767060433](https://openairdocs.org/sdr/DL767060433.md): Skin · corroded · May 26, 2006 · N102DA · Boeing 767232 · Leading Edge Devices
  > THE NR 7 SLAT (RT WING INBD SLAT) T/E WEDGE WAS FOUND WITH SKIN AND CORE CORROSION TOTALLING 151 SQ IN. REPAIRED PER ERA090851-14AD.
- [SDR DL767050386](https://openairdocs.org/sdr/DL767050386.md): Yaw Damper · malfunctioned · Jul 20, 2005 · N102DA · Boeing 767232 · Speed-Attitude Correction System
  > UNCOMMANDED RUDDER INPUT AT ROTATION, THOROUGHLY CHECKED SYSTEM. UNABLE TO DUPLICATE OR FIND FAULT.
- [SDR DL767050267](https://openairdocs.org/sdr/DL767050267.md): Shutoff Valve · sticks · May 12, 2005 · N102DA · Boeing 767232 · Pneumatic Distribution System
  > WHEN POWER INITIALLY REDUCED TO START INITIAL DESCENT A SMELL DEVELOPED IN THE AIRCRAFT. REPLACED NR 1 HPSOV.
- [SDR DL767050080](https://openairdocs.org/sdr/DL767050080.md): Line · leaking · Feb 3, 2005 · N102DA · Boeing 767232 · Hydraulic System, Main
  > RT HYD SYS FAILURE. RT HYD SYS QTY DROPPED QUICKLY SUGGESTING A LEAK. FOUND RT ENGINE PRESSURE LINE CHAFED THROUGH, REPLACED SAME.
- [SDR DL767050049](https://openairdocs.org/sdr/DL767050049.md): Pseu · malfunctioned · Jan 21, 2005 · N102DA · Boeing 767232 · Leading Edge Slat Control System
  > ON FLAP RETRACTION GOT L/E FLAP DISAGREE. ON FINAL GOT L/E FLAP ASYM PLI WAS FLUCTUATING POS 5 DEG TO POS 12 DEG. T/S PER FIM 27-81-00. PSEU FAULTS CARD NR 10 AND SHOWS CODES 305 421 422 AND 301. REPLACED PSEU. FSEU SHOWS OUTBD SLAT RVDT MISSING AND 603 FL
- [SDR DL767031053](https://openairdocs.org/sdr/DL767031053.md): Skin · gouged · Nov 24, 2003 · N102DA · Boeing 767232 · Horizontal Stabilizer, Plate/Skin
  > DENT/GOUGE FOUND ON LOWER SURFACE OF LT HORIZONTAL STAB, FORWARD TORQUE BOX, INBD SKIN PANEL. DENT WAS DUE TO GROUND DAMAGE. REPAIRED PER ERA 423716-14.
- [SDR DL767031012](https://openairdocs.org/sdr/DL767031012.md): Support Fitting · corroded · Nov 12, 2003 · N102DA · Boeing 767232 · Trailing Edge Flaps
  > CORROSION WAS FOUND IN THE HOLE BORES OF THE 6 FASTENERS WHICH ATTACH THE INBOARD FLAP TO THE OUTBOARD SUPPORT FITTINGS. THE HOLES WERE OVERSIZED, HFEC INSPECTED, AND BUSHED. THE ASSEMBLY WAS REINSTALLED WITH ORIGINAL STYLE HARDWARE. THE REPAIR WAS ACCOMPLI
- [SDR DL767030987](https://openairdocs.org/sdr/DL767030987.md): Web · cracked · Nov 6, 2003 · N102DA · Boeing 767232 · Fuselage Miscellaneous Structure
  > HFEC INSPECTION OF THE AFT P-DOME WEB LAP JOINTS PER AD 88-19-03 REVEALED 26 CRACKS EMANATING FROM FASTENER HOLES ALONG THE LOWER ROW OF THE WEB LAP JOINT BETWEEN WL 190 & 230 (APPROX 210) ON THE RIGHT SIDE OF THE P-DOME.
- [SDR DL767030786](https://openairdocs.org/sdr/DL767030786.md): Power Supply · discharged · Aug 26, 2003 · N102DA · Boeing 767232 · Emergency Lighting
  > EMERGENCY LIGHTS STAY ON IN F/C GALLEY AND RT SIDE OF F/C SECTION. REPLACED POWER SUPPLY.
- [SDR DL767030475](https://openairdocs.org/sdr/DL767030475.md): Seat Belt · disconnected · May 18, 2003 · N102DA · Boeing 767232 · Emergency Equipment
  > DURING TURBULENCE PASSENGER SEAT BELT AT 36C BECAME DISCONNECTED FROM SEAT, CAUSING A PASSENGER TO BE EJECTED FROM THE SEAT. THE SEAT BELT WAS REMOVED AND REPLACED. THEN BELT WAS SENT TO ATL.
- [SDR DL767030282](https://openairdocs.org/sdr/DL767030282.md): Wedge · debonded · Mar 27, 2003 · N102DA · Boeing 767232 · Leading Edge Devices
  > LEFT SLAT T/E WEDGE DISBONDED. REPAIRED PER ER/A 422819-14.
- [SDR DL767020872](https://openairdocs.org/sdr/DL767020872.md): Indicator · overheated · Jul 26, 2002 · N102DA · Boeing 767232 · Attitude and Direction Data System
  > CAPTAIN EADI WENT BLANK. SELECTED ALT EFI AND INDICATOR REMAINED BLANK. ABOUT 5 MINUTES LATER SMOKE WAS SEEN COMINGFROM CAPTAIN EADI. PULLED C/B E3 AND SMOKE STOPPED. REMOVED LEFT ADI INSPECTED CONNECTORS NO DAMAGE FOUND. REPLA LEFT ADI WITH SEVIS
- [SDR DL767030058](https://openairdocs.org/sdr/DL767030058.md): Skin · corroded · Jan 13, 2002 · N102DA · Boeing 767232 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS FOUND WITH A CRACK BETWEEN TWO STRINGER ATTACH FASTENERS AT FS 452 ALONG STRINGER 30R. THE UNDERLYING STRINGER WAS FOUND CORRODED. THE CORRODED AREA OF STRINGER WAS CUTOUT AND REPAIRED PER THE B767 SRM. THE SKIN CRACK WAS REMOVED WITH
- [SDR DL767011691](https://openairdocs.org/sdr/DL767011691.md): Battery Pack · discharged · Oct 20, 2001 · N102DA · Boeing 767232 · Emergency Lighting
  > ON L/O FOUND L-1DOOR AND 3 LT OVERWING EGRESS EMER LTS. INOPREPLACED M-736 BATTERY PACK, OPS CK GOOD
- [SDR DL767010883](https://openairdocs.org/sdr/DL767010883.md): Frame · cracked · May 31, 2001 · N102DA · Boeing 767232 · Fuselage Main, Frame
  > INSPECTION OF THE FS 1809.5 BULKHEAD CHORDS PER BAC S/B 767-53-0078 AND AD 2001-09-13 REVEALED A CRACK IN THE AFT CHORD, 2 FASTENER HOLE CRACKS IN THE FWD CHORD, AND A FASTENER HOLE CRACK IN THE MID CHORD. THE AFT CHORD WAS REPLACED, THE FWD CHORD CUT AND SPL
- [SDR DL767000308](https://openairdocs.org/sdr/DL767000308.md): Bolt · damaged · Feb 14, 2000 · N102DA · Boeing 767232 · Vertical Stabilizer
  > WHILE PERFORMING OPN 5940 RC587 FOUND TENSION TIE BOLTS ROTATING AT FS 1702. UPON INSPECTION FOUND BOTH BARREL NUTS L/R AFT POSTION AT FS 1702 HAD FAILED. FOUND TO BE HEAVILY RUSTED. ENGRG ISSUED ERA 373376-14 TO C/W E0 1-74297-12. BOLT AND NUT REPLACEMENT
- [SDR DL767992214](https://openairdocs.org/sdr/DL767992214.md): Stringer · corroded · Oct 5, 1999 · N102DA · Boeing 767232 · Fuselage Main, Longeron/Stringer
  > FUSELAGE STRINGER S-21AR, BS 1010, RBL 97.42, CORROSION REPAIR. STRINGER 21AR WAS FOUND WITH EXTENSIVE CORROSION AT FS 1010 AND RBL 97.42. THE STRINGER FORMS AN END CAP FOR THE MLG HORIZONTAL PRESSURE BULKHEAD. THE CORROSION WAS REMOVED WITH A 5 INCH CUTO
- [SDR DL767990695](https://openairdocs.org/sdr/DL767990695.md): Switch · dirty · Mar 29, 1999 · N102DA · Boeing 767232 · Landing Gear Position and Warning
  > LEFT MAIN GEAR GREEN LIGHTS DID NOT ILLUMINATE WHEN GEAR WAS LOWERED. THE LIGHTS DID NOT PRESS TO TEST WITH GEAR HANDLE UP OR DOWN. CLEANED SWITCH CONTACTS AND RELAMPED, OPERATION NORMAL.
- [SDR DL767990334](https://openairdocs.org/sdr/DL767990334.md): Power Supply · inop · Feb 18, 1999 · N102DA · Boeing 767232 · Emergency Lighting
  > ROW 37 AND BACK EMERGENCY LIGHTS INOP. REPLACED BATTERY SUPPLY PACK M9010, CKS GOOD.
- [SDR DL767990158](https://openairdocs.org/sdr/DL767990158.md): Actuator · failed · Jan 23, 1999 · N102DA · Boeing 767232 · Landing Gear Retraction/Extension System
  > LEFT MAIN GEAR REMAINED DOWN ON DEPARTURE FROM LAX. LOWERD LANDING GEAR AND RECEIVED NORMAL INDICATION. RETURNED TO LAX. TROUBLESHOOTING REVEALED LT GEAR SIDE LOCK ACTUATOR BYPASSING. REMOVED ROD END AND FOUND UPPER PORTION OF ROD ATTACHED TO PISTON SHEAR
- [SDR DL767981766](https://openairdocs.org/sdr/DL767981766.md): Light · inoperative · Aug 25, 1998 · N102DA · Boeing 767232 · Emergency Lighting
  > AFT EMERGENCY LIGHT ON SEAT 25F INOP. REPLACED LIGHT ASSY, CKS GOOD.
- [SDR DL767980419](https://openairdocs.org/sdr/DL767980419.md): Wedge · delamination · Feb 20, 1998 · N102DA · Boeing 767232 · Leading Edge Devices
  > THE UPPER SKIN OF THE LT WING NR 4 SLAT TRAILING EDGE WEDGE WAS FOUND WITH 2 AREAS 2 INCH DIAMETER DELAMINATIONS. THE THE DAMAGE WAS REPAIRED PER THE B767 SRM AND DOCUMENTED PER ER/A 364074-14AD.
- [SDR DL767980328](https://openairdocs.org/sdr/DL767980328.md): Power Supply · inoperative · Feb 7, 1998 · N102DA · Boeing 767232 · Emergency Lighting
  > SECTIONS OF SEAT MOUNTED EMERGENCY LIGHTING INOP. FOUND ON PREFLIGHT. REPLACED POWER SUPPLY, SYSTEM CKS GOOD.
- [SDR DL767971506](https://openairdocs.org/sdr/DL767971506.md): Skin · corrosion · Jul 25, 1997 · N102DA · Boeing 767232 · Wing, Plate/Skin
  > CORROSION DAMAGE TO THE WING CENTER SECTION UPPER SKIN WAS FOUND AT NUMEROUS LOCATIONS AT THE UPPER SKIN TO STRINGER ATTACH FASTENER HOLES ON STR 1 TO 8, 10 TO 12, 14 AND 15. ALSO, CORROSION WAS FOUND AROUND SEVERAL SKIN TO REAR SPAR ATTACH FASTENER HOLES. R
- [SDR DL767971505](https://openairdocs.org/sdr/DL767971505.md): Seat Track · cracked · Jul 25, 1997 · N102DA · Boeing 767232 · Fuselage, Seat/Cargo Attach Fittings
  > THE FUSELAGE SEAT TRACKS LOCATED AT LBL 33, 55 AND RBL 54 WERE FOUND CRACKED IN THE VERTICAL WEB OF THE UPPER CHORD AT APPROX FS 786 AS DESCRIBED IN S/B 767-57-0029. IN ADDITION, PREVENTATIVE MODIFICATIONS TO THE LBL/RBL 33 AND LBL/RBL 54 FLOORBEAMS ARE BEING
- [SDR DL767971504](https://openairdocs.org/sdr/DL767971504.md): Skin · corrosion · Jul 25, 1997 · N102DA · Boeing 767232 · Fuselage Main, Plate/Skin
  > CORROSION WAS FOUND JUST AFT OF STA 1307 UNDER THE UHF ANTENNA BOX. THE DAMAGE WAS CUTOUT AS SHOWN IN FIGURE 1. THE SKIN AT THIS LOCATION HAS A MAX THICKNESS OF.135 AND IS CHEM-MILLED FROM 2024-T3 CLAD SHEET. A PREVIOUS REPAIR IS LOCATED JUST FORWARD OF TH
- [SDR DL767971482](https://openairdocs.org/sdr/DL767971482.md): Skin · corrosion · Jul 21, 1997 · N102DA · Boeing 767232 · Wing, Plate/Skin
  > CORROSION WAS DISCOVERED ON THE UPPER SURFACE OF THE WING CENTER SECTION UPPER SKIN PANELS AT BUTT SPLICE BETWEEN THE FORWARD AND AFT SKIN PANELS AT STRINGER 17, BETWEEN RBL 74.81 AND 97.42. THE SKIN WAS TRIMMED TO REMOVE THE CORROSION IN THE FORWARD AND AFT
- [SDR DL767970336](https://openairdocs.org/sdr/DL767970336.md): Slat · damaged · Feb 24, 1997 · N102DA · Boeing 767232 · Leading Edge Devices
  > A/C DIVERTED INTO MCO WITH FLAP/SLATS LOCKOUT. ON ARRIVAL, FOUND NR 8 SLAT DAMAGED. REPLACED NR 8 SLAT, OPS CHECK NORMAL.
- [SDR DL767970089](https://openairdocs.org/sdr/DL767970089.md): Battery Pack · discharged · Jan 18, 1997 · N102DA · Boeing 767232 · Emergency Lighting
  > RT OVERWING SLIDE AND LEFT SPOILER SQUIBS FAILED TEST ON THE MAINTENANCE PANEL. REPLACED THE BATTERY PACK.
- [SDR DL767970117](https://openairdocs.org/sdr/DL767970117.md): Skin · corrosion · Dec 23, 1996 · N102DA · Boeing 767232 · Fuselage Main, Plate/Skin
  > SKIN AND STRINGERS WERE FOUND CORRODED AT FS 1540 BETWEEN STR 34L AND 39L. A 3.75 BY 2.25 CUTOUT WAS MADE. STRS 34L TO 39L REQUIRED NEW SECTIONS TO BE SPLICED IN. ADDITIONAL DAMAGE WAS FOUND AFTER INITIAL RELEASE OF ER/A. A SECOND 2 BY 3 CUTOUT WAS MADE BE
- [SDR DL767962732](https://openairdocs.org/sdr/DL767962732.md): Skin · corroded · Dec 17, 1996 · N102DA · Boeing 767232 · Fuselage Main, Plate/Skin
  > NR 95 CORROSION THROUGH FUSELAGE SKIN AT STA 1542 STR 35. NR 177 THROUGH 182 WRITTEN FOR STRINGER DAMAGE STR 34L THROUGH 39L WILL REPAIR PER ERA 360836-14 AS OF 12/19/96 ERA PENDING FAA APPROVAL.
- [SDR DL767962148](https://openairdocs.org/sdr/DL767962148.md): Fan · shorted · Sep 20, 1996 · N102DA · Boeing 767232 · Air Distribution Fan
  > STRONG ELECTRICAL ODOR IN AIRCRAFT ON TAXI-OUT. FWD EXHAUST EQUIPMENT COOLING FAN POPPED C/B. FWD TO MCO AND PLAC PER MEL 21-58-04A, NEEDS FAN DAL 211002542.
- [SDR DL767960829](https://openairdocs.org/sdr/DL767960829.md): Actuator · failed · Apr 7, 1996 · N102DA · Boeing 767232 · Aileron Control System
  > DURING FLT CONTROL CHECK, AILERON AND ELEVATOR FELT VERY HEAVY. AIRCRAFT RETURNED TO BLOCK. REPLACED RT LCCA, RIGGED AND LEAK CHECKED, OPERATION NORMAL.
- [SDR DL767960691](https://openairdocs.org/sdr/DL767960691.md): Light · inoperative · Mar 28, 1996 · N102DA · Boeing 767232 · Emergency Lighting
  > ON LAYOVER, FOUND LEFT AFT EMERGENCY LIGHT INOP. RELAMPED, CKS OK.
- [SDR DL767960729](https://openairdocs.org/sdr/DL767960729.md): Sensor · out of adjust · Mar 27, 1996 · N102DA · Boeing 767232 · Landing Gear Position and Warning
  > ON TAKEOFF, GEAR COULD NOT BE RAISED WITHOUT USING LOCK OVERRIDE. AIRCRAFT WAS FERRIED ATL FOR REPAIRS. PSEU SHOWS 246 RT GEAR TILT TARGET SHOWS FAR RESET. ADJUSTED SENSOR PER MM, OPERATION NORMAL.
- [SDR DL767954712](https://openairdocs.org/sdr/DL767954712.md): Fan · failed · Dec 15, 1995 · N102DA · Boeing 767232 · Air Distribution Fan
  > ELECTRICAL SMELL IN COCKPIT AT CRUISE. FORWARD EQ EXHAUST FAN EICAS MSG. SMELL DISSIPATED IN COCKPIT. F/A REPORTED SMELL DIRECTED AFT THROUGH CABIN. FOUND FAN AT FAULT. DEFERRED PER MEL, THEN REPLACED FAN, OPERATION NORMAL.
- [SDR DL767951153](https://openairdocs.org/sdr/DL767951153.md): Flap · cap damaged · Mar 17, 1995 · N102DA · Boeing 767232 · Trailing Edge Flaps
  > FOUND DURING O-2 CHECK, NR 1 FLAP L/E CAP DAMAGED 2 PLACES. INSTALLED PERMANENT REPAIR AS PER SRM 51-70-03 FIG 201.

## 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 = 'N102DA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N102DA/reports

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