# Service difficulty reports: N467DA, cancelled Sep 5, 2003

A list on [N467DA, cancelled Sep 5, 2003](https://openairdocs.org/deregistered/N467DA-2003-09-05.md).

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

- [SDR DL72S981702](https://openairdocs.org/sdr/DL72S981702.md): Oven · smoking · Aug 18, 1998 · N467DA · Boeing 727232 · Buffet/Galleys
  > FWD GALLEY OVENS EMITTED BURNING PLASTIC SMELL AND VISABLE SMOKE AFTER TURNING ON. FOUND PLASTIC SHIPPING LABEL ON SIDE OF FOOD CARRIER. REMOVED AND REPLACED CARRIER.
- [SDR DL72S981268](https://openairdocs.org/sdr/DL72S981268.md): Skin · cracked · Jun 16, 1998 · N467DA · Boeing 727232 · Nacelle/Pylon Structure
  > RIVETS LOOSE.25 INCH CRACK IN DORSAL FIN OUTER SKIN RT SIDE BELOW PANEL 9516. REPAIR PER M/M 54-30-0 FIG 801.
- [SDR DL72S981145](https://openairdocs.org/sdr/DL72S981145.md): Switch · dirty · May 29, 1998 · N467DA · Boeing 727232 · Landing Gear Position and Warning
  > TAILSKID LIGHT ON TAKEOFF ROLL AT 70 KNOTS, CLEANED PROX SWITCH.
- [SDR DL72S972341](https://openairdocs.org/sdr/DL72S972341.md): Stiffener · cracked · Nov 12, 1997 · N467DA · Boeing 727232 · Leading Edge Devices
  > FOUND DURING F-1 LETTER CHECK, 1.25 INCH CRACK NR 4 L/E SLAT I/B TRACK ROLLER BOX I/B STIFFENER. REPLACED STIFFENER PER M/M 57-20-21.
- [SDR DL72S972339](https://openairdocs.org/sdr/DL72S972339.md): Web · cracked · Nov 12, 1997 · N467DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > A.25 INCH CRACK AT UPPER LIGHTENING HOLE ON VERTICAL WEB STA 1235 R IN 48 SECTION. REPAIRED PER M/M 53-11-0.
- [SDR DL72S972204](https://openairdocs.org/sdr/DL72S972204.md): Battery Pack · discharged · Oct 29, 1997 · N467DA · Boeing 727232 · Emergency Lighting
  > MSU - CK OP OF ALL EMER LIGHTS. FOUND LT OVERWING EXIT SIGNS INOP. REPLACED BATTERY PACK. OPS NML.
- [SDR DL72S971349](https://openairdocs.org/sdr/DL72S971349.md): Frame · double drilled · Jun 25, 1997 · N467DA · Boeing 727232 · Fuselage Main, Frame
  > DURING THE PERFORMANCE OF SI 4-61904-12, THE SECOND FASTENER HOLE ABOVE THE FLOORBEAM ON THE INBOARD FLANGE WAS DISCOVERED TO HAVE BEEN LOCATED CLOSE ENOUGH TO A PILOT HOLE TO CREATE A DOUBLE DRILLED HOLE. THE DOUBLER DRILLED HOLE WAS OVERSIZED TO 0.403 THROU
- [SDR DL72S970904](https://openairdocs.org/sdr/DL72S970904.md): Sockets · missing · May 12, 1997 · N467DA · Boeing 727232 · Emergency Lighting
  > 2 TRACK LIGHT SOCKETS RIPPED LOOSE FROM FLOOR TRACK, AT ROWS 16 AND 20. REPLACED SOCKETS AND CAPSULES, CKS NORMAL.
- [SDR DL72S970571](https://openairdocs.org/sdr/DL72S970571.md): Track Lights · loose · Mar 27, 1997 · N467DA · Boeing 727232 · Emergency Lighting
  > EMERGENCY TRACK LIGHTING AFT CABIN LOOSE FROM FLOOR. REPLACED LIGHT SEGMENT, CKS OK.
- [SDR DL72S962149](https://openairdocs.org/sdr/DL72S962149.md): Web · cracked · Sep 20, 1996 · N467DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND DURING E-1 LETTER CHECK,.1875 INCH CRACK LWR TORQUE BOX VERTICAL WEB BS 1273 LEFT SIDE AT LIGHTENING HOLE. REPAIRED PER M/M 53-11-0.
- [SDR DL72S961783](https://openairdocs.org/sdr/DL72S961783.md): Power Supply · inoperative · Jul 25, 1996 · N467DA · Boeing 727232 · Emergency Lighting
  > ON LAYOVER, FOUND EMERGENCY EXIT LIGHT ABOVE R-2 DOOR INOPERATIVE. REPLACED POWER SUPPLY AND BATTERY PACK. OPS NORMAL.
- [SDR DL72S961782](https://openairdocs.org/sdr/DL72S961782.md): Battery Pack · discharged · Jul 25, 1996 · N467DA · Boeing 727232 · Emergency Lighting
  > ON LAYOVER, FOUND CENTER AISLE EMERGENCY EXIT LIGHT INOPERATIVE AT ROW 3. REPLACED BATTERY PACK. OPS NORMAL.
- [SDR DL72S960721](https://openairdocs.org/sdr/DL72S960721.md): Circuit Breaker · cracked · Mar 31, 1996 · N467DA · Boeing 727232 · AC Power Distribution System
  > ON FINAL, ALL 3 BUS TIE BREAKERS TRIPPED, PHASE UNBALANCE, OVER EXCITED NR 2 AND NR 3, NR 1 TR UNIT C/B POPPED. FOUND APU GEN BREAKER CRACKED WITH LOOSE CONNECTIONS. REPLACED SAME. ALSO, REPLACED NR 1 ENG GEN BREAKER. RAN ENGS PARALLELED, ALL CHECKS NORMAL
- [SDR DL72S960467](https://openairdocs.org/sdr/DL72S960467.md): Skin · cracked · Feb 28, 1996 · N467DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > DURING INSPECTION, THREE CRACKS WERE FOUND IN THE SKIN AND DOOR SURROUND STRUCTURE IN THE LOWER AFT CORNER OF THE L1 DOOR CUTOUT. ALL CRACKS GO THROUGH THE SKIN, BONDED DOUBLER AND THE BEAR STRAP. CRACK LENGTH VARIED FROM 1 TO 2 INCH LENGTH. IN ACCORDANCE W
- [SDR DL72S960466](https://openairdocs.org/sdr/DL72S960466.md): Bear Strap · corroded · Feb 28, 1996 · N467DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > DURING INSPECTION, CORROSION WAS FOUND ON THE INTERNAL SKIN DOUBLER OF THE R-2 DOOR CUTOUT AT STATION 1070. IN ACCORDANCE WITH FAA/DER FORM 8110-3 DATED 2-8-96, THE DAMAGE WAS CUT OUT AND A DOUBLER AND TRIPLER INSTALLED.
- [SDR DL72S960453](https://openairdocs.org/sdr/DL72S960453.md): Skin · worn · Feb 28, 1996 · N467DA · Boeing 727232 · Ailerons
  > LOWER SKIN WAS FOUND WITH OVERSIZED HOLES. SPLICED SKIN SECTION PER M/M 57-51-0 FIG 801. FOUND DURING SHOP INSPECTION OF AILERON ASSEMBLY.
- [SDR DL72S960452](https://openairdocs.org/sdr/DL72S960452.md): Spar · cracked · Feb 28, 1996 · N467DA · Boeing 727232 · Ailerons
  > SPAR WAS FOUND CRACKED NEAR TAB FITTING. SPLICED SPAR SECTION PER SRM 51-40-3 FIG 1. FOUND DURING SHOP INSPECTION OF AILERON ASSEMBLY.
- [SDR DL72S961606](https://openairdocs.org/sdr/DL72S961606.md): Transverse Beam · cracked · Feb 27, 1996 · N467DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > THERE IS A CRACK IN THE ANGLE OF THE FWD TRANSVERSE BEAM AND AFT CHANNEL OF THE RT TORQUE BOX AT FS 1263. THIS AREA OF THE TORQUE BOX IS THE SUBJECT OF AIRWORTHINESS DIRECTIVE 94-07-08, WHICH REQUIRES INSPECTION PER S/B 53-0129. REPAIRED PER ERA 303225-14AD.
- [SDR DL72S960274](https://openairdocs.org/sdr/DL72S960274.md): Door Actuator · iced up · Feb 4, 1996 · N467DA · Boeing 727232 · Landing Gear Door Actuator
  > ON DEPARTURE, RT MAIN GEAR WOULD NOT RETRACT, TRANSIT LIGHT ON AND SECOND OFFICER'S PANEL NEVER ILLUMINATED. REMOVED ICE BUILD-UP ON RT GEAR DOOR ACTUATOR, LUBED GEAR AND DOORS, PERFORMED GEAR SWING AND OPS NORMAL.
- [SDR DL72S953846](https://openairdocs.org/sdr/DL72S953846.md): Eel · inoperative · Sep 23, 1995 · N467DA · Boeing 727232 · Emergency Lighting
  > AFT AIRSTAIR EMERGENCY EXIT LIGHTS ARE INOP. REPLACED LIGHT ASSEMBLY AND BATTERY PACK OPERATION NORMAL.
- [SDR DL72S953140](https://openairdocs.org/sdr/DL72S953140.md): Web · cracked · Jul 21, 1995 · N467DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > LT VERTICAL WEB OF NWW HAS 2.0 CRACK BETWEEN STA 294.5 AND STA 285.5, APPROX WL 170. REPAIRED PER DL ERA 302166-14AD.
- [SDR DL72S951112](https://openairdocs.org/sdr/DL72S951112.md): Plate Web · cracked · Mar 3, 1995 · N467DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > DURING INSPECTION AT CV-2, THE RT SIDEWALL WEB OF THE NOSE WHEEL WELL WAS FOUND CRACKED AT STA 270. IN ACCORDANCE WITH BAC S/B 727-53-145, THE DAMAGED PORTION OF THE WEB WAS TRIMMED OUT, AND A DOUBLER AND 4 REPAIR STRAPS WERE INSTALLED.
- [SDR DL72S950822](https://openairdocs.org/sdr/DL72S950822.md): Skin · corroded · Feb 15, 1995 · N467DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > DURING CV-2 CK, FOUND FUSELAGE SKIN DAMAGED BETWEEN STA 720E AND 720F AT STR 27L. INSTALLED DOUBLER PER SRM 53-30-3 FIG 3.
- [SDR DL72S950815](https://openairdocs.org/sdr/DL72S950815.md): Beam · cracked · Feb 9, 1995 · N467DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > DURING INSPECTION, THE FWD TRANSVERSE BEAM AT FS 1263 WAS FOUND CRACKED IN THE ANGLE. THE BEAM WILL BE REPLACED IN ACCORDANCE WITH B727 S 53-0129 REV 4.
- [SDR DL72S950816](https://openairdocs.org/sdr/DL72S950816.md): Stringer · corroded · Feb 8, 1995 · N467DA · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > DURING CV-2 CK, FOUND CORROSION AT STR 23R JUST FWD OF STA 520. REPAIRED PER SRM 53-10-3 ID PER PS 900-5-1 NR 4.
- [SDR DL72S950761](https://openairdocs.org/sdr/DL72S950761.md): Web · cracked · Feb 8, 1995 · N467DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > DURING INSPECTION, THE RT SIDEWALL WEB OF THE NOSE WHEEL WELL HAD A 0.25 INCH CRACK AT STA 285. THE DAMAGED PORTION OF THE WEB WILL BE TRIMMED OUT AND A REPAIR DOUBLER AND FOUR STRAPS WERE INSTALLED IN ACCORDANCE WITH S/B 727-53-145.
- [SDR DL72S950773](https://openairdocs.org/sdr/DL72S950773.md): Floor Support · cracked · Feb 7, 1995 · N467DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND ON LTR CK - 1 INCH CRACK THROUGH MOUNT BOLT HOLE FLOOR PANEL SUPPORT CHANNEL FWD SIDE STA 950C BL 18R - REPAIR - REPAIRED PER SRM 53-10-5 AND I.D. PER P.S. 900-5-1 NR 4.
- [SDR DL72S950821](https://openairdocs.org/sdr/DL72S950821.md): Angle · cracked · Feb 6, 1995 · N467DA · Boeing 727232 · Wing Miscellaneous Structure
  > DURING CV-2 CK, FOUND CRACK ON NR 3 SLAT I/B TRACK O/B VERTICAL ANGLE AT SPAR (SPAR ON WING L/E). REPLACED STIFFENER.
- [SDR DL72S950819](https://openairdocs.org/sdr/DL72S950819.md): Angle · cracked · Feb 6, 1995 · N467DA · Boeing 727232 · Leading Edge Devices
  > DURING CV-2 CK, FOUND CRACK ON NR 2 SLAT O/B TRACK O/B VERTICAL ANGLE AT SPAR (SPAR ON WING L/E). REPLACED ANGLE PER MM 57-20-21 PG 813.
- [SDR DL72S950818](https://openairdocs.org/sdr/DL72S950818.md): Angle · cracked · Feb 6, 1995 · N467DA · Boeing 727232 · Wing Miscellaneous Structure
  > DURING CV-2 CK, FOUND CRACK ON NR 2 SLAT OUTBOARD TRACK INBOARD VERTICAL ANGLE AT SPAR (SPAR ON WING L/E). REPLACED ANGLE PER M/M 57-20-21 PG 813.
- [SDR DL72S950793](https://openairdocs.org/sdr/DL72S950793.md): Stringer · corroded · Feb 6, 1995 · N467DA · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > FOUND ON CV2 CK - CORROSION INSIDE STRINGER 27L FWD STA 720F - REPAIR - REPLACED SECTION OF STRINGER PER SRM 53-10-3 FIG 1.
- [SDR DL72S950789](https://openairdocs.org/sdr/DL72S950789.md): Clip · corroded · Feb 6, 1995 · N467DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND ON CV2 CK - CORROSION AT LOWER FWD FUSELAGE SKIN CLIP STA 303 AT NOSE W/W CHORD - REPAIR - REPAIRED PER SRM 51-40-3 FIG 1.
- [SDR DL72S950788](https://openairdocs.org/sdr/DL72S950788.md): Floor Beam · corroded · Feb 6, 1995 · N467DA · Boeing 727232 · Fuselage Main, Floor Beam
  > FOUND ON CV2 CK - CORROSION AT FLOOR BEAM AT BL 0 TO LBL 16 STA 1110 - REPAIR - INSTALLED REPAIR ANGLE PER MM 53-20-11 FIG 804A.
- [SDR DL72S950787](https://openairdocs.org/sdr/DL72S950787.md): Floor Beam · corroded · Feb 6, 1995 · N467DA · Boeing 727232 · Fuselage Main, Floor Beam
  > FOUND ON CV2 CK - CORROSION AT FLOOR BEAM TOP SIDE AND BOTTOM WHERE CLIP NUTS ATTACH STATION 380 RBL 12 TO 63 - REPAIR - REPLACED TEE CAP PER SRM 53-10-8.
- [SDR DL72S950786](https://openairdocs.org/sdr/DL72S950786.md): Seat Track · corroded · Feb 6, 1995 · N467DA · Boeing 727232 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND ON CV2 CK - CORROSION AT SEAT TRACK STA 344 TO 360 AT LBL 22 - REPAIR - REPLACED SEAT TRACK PER SRM 53-10-5 FIG 7.
- [SDR DL72S950785](https://openairdocs.org/sdr/DL72S950785.md): Seat Track · corroded · Feb 6, 1995 · N467DA · Boeing 727232 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND ON CV2 CK - CORROSION AT SEAT TRACK STA 480 LBL 22 - REPAIR - REPLACED DAMAGED SEAT TRACK FROM 440-480 PER SRM 53-10-5 FIG 7.
- [SDR DL72S950817](https://openairdocs.org/sdr/DL72S950817.md): Rib · cracked · Feb 2, 1995 · N467DA · Boeing 727232 · Leading Edge Devices
  > DURING CV-2 CK, FOUND RIB CRACKED 1 INCH ON NR 3 SLAT JUST OUTBD OF OUTER TRACK. REPAIRED PER SRM 57-50-3 FIG 9.

## 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 = 'N467DA' AND deregistration_id = 'N467DA-2003-09-05'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N467DA-2003-09-05/reports

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