# Service difficulty reports: N507DA, cancelled Sep 9, 2002

A list on [N507DA, cancelled Sep 9, 2002](https://openairdocs.org/deregistered/N507DA-2002-09-09.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 2 · 85 reports

- [SDR DL72L011286](https://openairdocs.org/sdr/DL72L011286.md): Light · inoperative · Aug 5, 2001 · N507DA · Boeing 727232 · Emergency Lighting
  > RIGHT OVERWING EMERGENCY LIGHT BETWEEN EXTERIOR EMERGENCY EXIT DOORS INOP. RELAMPED. CHECKS OKAY
- [SDR DL72L011222](https://openairdocs.org/sdr/DL72L011222.md): Light · intermittent · Jul 24, 2001 · N507DA · Boeing 727232 · Emergency Lighting
  > LEFT AFT DOOR EMERGENCY EXIT LIGHT INTERMITTENTLY BLINKING EMERGENCY EXIT OVER CENTER CABIN IS INTERMITTENTLY BLINKING. RELAMPED LIGHT OVER LEFT AFT DOOR AND CENTER AISLE LIGHT OPERATION NORMAL.
- [SDR DL72L011041](https://openairdocs.org/sdr/DL72L011041.md): Controller · failed · Jun 22, 2001 · N507DA · Boeing 727232 · Cabin Pressure Controller
  > CABIN PRESSURIZATION FAILED IN AUTO, STBY, AND MAN AC OUTFLOW VALVE WAS CONTROLLABLE IN MAN DC ONLY. REPLACED CABIN PRESSURE CONTROLLER AFTER VERIFYING OLD CONTROLLER BAD. OPS CHECKS OK PER MM.
- [SDR DL72L002298](https://openairdocs.org/sdr/DL72L002298.md): Battery · inoperative · Nov 24, 2000 · N507DA · Boeing 727* · Exterior Lighting
  > IRREG / L1 DOOR EMERGENCY LIGHT WILL NOT GO BRIGHT. REPLACED BATTERY - OPN CKS NML
- [SDR DL72L002209](https://openairdocs.org/sdr/DL72L002209.md): Light · broken · Nov 8, 2000 · N507DA · Boeing 727232 · Emergency Lighting
  > EMERGENCY SEAT LIGHT ROW 10D LENS MISSING. REPLACED ASSY, CKS GOOD.
- [SDR DL72L002166](https://openairdocs.org/sdr/DL72L002166.md): Battery Pack · discharged · Nov 4, 2000 · N507DA · Boeing 727232 · Emergency Lighting
  > DURING EMERGENCY LIGHT CHECK OUT FOUND RT OUTSIDE OVERWING EXIT LIGHT OUT. REPLACED BATTERY PACK.
- [SDR DL72L002004](https://openairdocs.org/sdr/DL72L002004.md): Light · inoperative · Oct 13, 2000 · N507DA · Boeing 727232 · Emergency Lighting
  > ON LAYOVER FOUND ESCAPE PATH LIGHTING INOP AT SEAT 3AB. FOUND PIN PULLED ON CABLE UNDER SEAT. RESET PIN, OPS CKS GOOD.
- [SDR DL72L001975](https://openairdocs.org/sdr/DL72L001975.md): Mount · cracked · Oct 10, 2000 · N507DA · Boeing 727232 · Nacelle/Pylon, Attach Fittings
  > ROUTINE HFEC BOLT HOLE INSPECTIONS OF THE NR 3 ENGINE PYLON FWD ENGINE MOUNT SUPPORT FITTING REVEALED A CRACK INDICATION IN HOLE G. THE CRACKING IS TYPICAL OF BAC S/B 727-54A0010AND AD 97-05-08. THE HOLE WAS OVERSIZED TO REMOVE THE CRACK AND A.0312 INCH INS
- [SDR DL72L001452](https://openairdocs.org/sdr/DL72L001452.md): Battery · inoperative · Aug 1, 2000 · N507DA · Boeing 727232 · Emergency Lighting
  > ON LAYOVER INSPECTION FOUND PORTABLE EMERGENCY EXIT LIGHT OVER THE L-2 DOOR NOT TESTING. REPLACED BATTERIES AND LIGHT OPERATION NORMAL.
- [SDR DL72L001262](https://openairdocs.org/sdr/DL72L001262.md): Battery · inoperative · Jul 4, 2000 · N507DA · Boeing 727232 · Emergency Lighting
  > L-2 DOOR EMERGENCY O/H EXIT SIGN INOP. REPLACED BATTERY PACK LIGHT, OPS CHECK NORM.
- [SDR DL72L001226](https://openairdocs.org/sdr/DL72L001226.md): Light · inoperative · Jun 28, 2000 · N507DA · Boeing 727232 · Emergency Lighting
  > DURING LAYOVER, FOUND LEFT FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. CHECKS GOOD PER MM.
- [SDR DL72L001225](https://openairdocs.org/sdr/DL72L001225.md): Battery Pack · inoperative · Jun 28, 2000 · N507DA · Boeing 727232 · Emergency Lighting
  > DURING LAYOVER, FOUND AFT OVERHEAD CEILING EMERGENCY LIGHT INOP. REPLACED EMERGENCY EXIT LIGHT BATTERY PACK. CHECKS GOOD PER M/M
- [SDR DL72L000563](https://openairdocs.org/sdr/DL72L000563.md): Sign · inoperative · Mar 22, 2000 · N507DA · Boeing 727232 · Emergency Lighting
  > RT OVERWING EMERG EXIT IDENTIFIER INOP ON STANDBY POWER CHECK. REPLACED RACK, OPERATION NML.
- [SDR DL72L000527](https://openairdocs.org/sdr/DL72L000527.md): Spar · cracked · Mar 17, 2000 · N507DA · Boeing 727232 · Wing Structure
  > CRACKS IN AFT SPAR RAIL AT 21 AND 35 FROM I/B END OF FLAP. ALSO DOUBLER SHORT AT 30 FROM O/B END OF FLAP. CORRECTED ON SHOP ORDER NR 957610.
- [SDR DL72L000270](https://openairdocs.org/sdr/DL72L000270.md): Flap Track · corroded · Feb 7, 2000 · N507DA · Boeing 727232 · Trailing Edge Flaps
  > DURING OVERHAUL OF THE I/B FLAP, I/B TRACK ASSY, TYPICAL CORROSION WAS FOUND AT THE MLG AND SPOILER BEAM ATTACH PADS AREAS. IN ADDITION, WEAR WAS FOUND AT THE FWD ATTACH LUGS, THE MLG DOOR HINGE FITTING ATTACH HOLES, AND THE TOGGLE DETENT HOLE. REPAIRED PER
- [SDR DL72L000256](https://openairdocs.org/sdr/DL72L000256.md): Flap Track · corroded · Feb 3, 2000 · N507DA · Boeing 727232 · Trailing Edge Flaps
  > DURING OVERHAUL OF THE I/B FLAP I/B TRACK ASSY, TYPICAL CORROSION WAS FOUND AT THE MLG AND SPOILER BEAM ATTACH PAD AREAS AND TYPICAL WEAR WAS FOUND AT THE FWD ATTACH LUGS, THE MLG DOOR HINGE FITTING ATTACH HOLES, AND THE TOGGLE DETENT HOLE. REPAIRED
- [SDR DL72L000280](https://openairdocs.org/sdr/DL72L000280.md): Stringer · cracked · Jan 28, 2000 · N507DA · Boeing 727232 · Vertical Stabilizer, Spar/Rib
  > STRINGER 6 RT CRACKED VERT INTERIOR 4TH FRAME DOWN FROM 9504 RIB NR 2. BEGAN FABRICATED REPAIR PER M/M 55-30-0 PG 803. FINISHED FABRICATING REPAIR ANGLE PER M/M 55-30-0 FIG 803. OK TO TREAT AND PAINT. CHEM TREATED AS PER PS 900-2-4-1 NR 2. TREATED AND PAI
- [SDR DL72L000259](https://openairdocs.org/sdr/DL72L000259.md): Rib · cracked · Jan 28, 2000 · N507DA · Boeing 727232 · Leading Edge Devices
  > NR 5 SLAT NR 12 RIB CRACKED. REPAIRED PER MM 57-54-0.
- [SDR DL72L000252](https://openairdocs.org/sdr/DL72L000252.md): Skin · cracked · Jan 28, 2000 · N507DA · Boeing 727232 · Vertical Stabilizer, Plate/Skin
  > STOP DRILLED CRACK AND BEGAN FABRICATING REPAIR PER M/M 55-30-0 FIG 803. CHEM TREATED PER PS 900-2-4-1 NR 2. TREATED AND PAINTED PER PS 900-2 NR 5. OK TO INSTALL. INSTALLED REPAIR ANGLE PER M/M 55-30-0 PG 803. STRINGER WAS FOUND CRACKED ON VERTICAL STAB.
- [SDR DL72L000567](https://openairdocs.org/sdr/DL72L000567.md): Skin · cracked · Jan 27, 2000 · N507DA · Boeing 727232 · Trailing Edge Flaps
  > NR 2 MIDFLAP AFT SPAR DOUBLER CRACKED TWO PLACES AND COVE SKIN CRACKED. REPAIRED PER M/M 57-52-0 FIGURE 802 AND FIGURE 809.
- [SDR DL72L000286](https://openairdocs.org/sdr/DL72L000286.md): Angle · worn · Jan 27, 2000 · N507DA · Boeing 727232 · Vertical Stabilizer
  > SUPPORT ANGLE WORN VERT STAB LT SIDE JUST FWD OF SLIDING SEAL. REMOVED DAMAGED AREA AND DRILLED UP REPAIR PER SRM 55-30-6D. INSTALLED REPAIR PER SRM 55-30-6D.
- [SDR DL72L000197](https://openairdocs.org/sdr/DL72L000197.md): Rib · cracked · Jan 26, 2000 · N507DA · Boeing 727232 · Flight Control System
  > SLAT RIB NR 11 WAS CRACKED AT THE UPPER FWD END. INSTALLED A REPAIR DOUBLER PER 57-54-0 FIG 804.
- [SDR DL72L000196](https://openairdocs.org/sdr/DL72L000196.md): Rib · cracked · Jan 26, 2000 · N507DA · Boeing 727232 · Leading Edge Devices
  > SLAT RIB WAS CRACK AT THE O/B LWR AFT END. REPAIRED PER MM 57-54-0 FIG 814.
- [SDR DL72L000238](https://openairdocs.org/sdr/DL72L000238.md): Skin · cracked · Jan 25, 2000 · N507DA · Boeing 727232 · Leading Edge Devices
  > ANTI-ICE SKIN CRACKED AT 4 LOCATIONS. INSTALLED DOUBLER PER MM 57-54-0.
- [SDR DL72L000195](https://openairdocs.org/sdr/DL72L000195.md): Rib · cracked · Jan 24, 2000 · N507DA · Boeing 727232 · Leading Edge Devices
  > SLAT RIB WAS CRACKED AT LWR AFT END NR 2 RIB. INSTALLED A REPAIR DOUBLER PER MM 57-54-0 FIG 814.
- [SDR DL72L000194](https://openairdocs.org/sdr/DL72L000194.md): Skin · cracked · Jan 24, 2000 · N507DA · Boeing 727232 · Leading Edge Devices
  > SLAT CRACKED. INSTALLED REPAIR DOUBLER PER MM 57-54-0 FIG 814.
- [SDR DL72L992508](https://openairdocs.org/sdr/DL72L992508.md): Angle · corroded · Nov 13, 1999 · N507DA · Boeing 727232 · Nacelle/Pylon Structure
  > ON HEAVY WEIGHT HUSH-KIT MOD, FOUND RT AFT MOUNT CHORD ANGLE CORRODED BEYOND MFG SPECS. REPLACED RT CHORD ANGLE WITH ONE OF NEW MFG.
- [SDR DL72L992507](https://openairdocs.org/sdr/DL72L992507.md): Angle · corroded · Nov 12, 1999 · N507DA · Boeing 727232 · Nacelle/Pylon Structure
  > ON HEAVY WEIGHT HUSH-KIT MOD, FOUND NR 2 ENG AFT MOUNT SUPPORT LT CHORD ANGLE CORRODED BEYOND MFG SPECS. REPLACED LT CHORD ANGLE WITH ONE OF NEW MFG.
- [SDR DL72L991886](https://openairdocs.org/sdr/DL72L991886.md): Bracket · cracked · Aug 23, 1999 · N507DA · Boeing 727232 · Leading Edge Slat Actuator
  > FOUND ON A1 LETTER CK, NR 1 L/E FLAP ACTUATOR I/B ATTACH BRACKET CRACKED. REPAIRED PER MM 57-20-21.
- [SDR DL72L991885](https://openairdocs.org/sdr/DL72L991885.md): Skin · cracked · Aug 23, 1999 · N507DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > FOUND AT A-1 LETTER CK,.5 INCH CRACK IN EMPENNAGE SKIN RT SIDE STA 1234 + STR 22. REPAIRED PER SRM 53-30-3 FIG 25.
- [SDR DL72L991895](https://openairdocs.org/sdr/DL72L991895.md): Track · corroded · Aug 20, 1999 · N507DA · Boeing 727232 · Trailing Edge Flaps
  > NR 5 INB'D FLAP TRACK AD 90-07-05 AND 90-06-09 TYP CORROSION AT MLG AND SPOILER BEAM ATTACH PADS AND WEAR AT FWD ATTACH LUGS. AUTHORIZED MACHINING CORROSION AND WEAR. INSTALLED SPLICE PLATE REPAIR TO MLG BEAM ATTACH PAD AS PER SB 57-0178.
- [SDR DL72L991073](https://openairdocs.org/sdr/DL72L991073.md): Return Line · cracked · May 15, 1999 · N507DA · Boeing 727232 · Drag Control System
  > SYS A HYD QTY IND DROPPED TO ZERO QTY APPROX ONE HR AND 20 MINS INTO FLT. NR 1 ENG HYD LOW PRESS LIGHT ILLUMINATED. CHECKLIST PROCEDURE INITIATED LANDING UNEVENTFUL. GROUND INVESTIGATION LEAKING HALF WAY POINT LEFT WING. FOUND NR 2 SPOIL-ER RETURN LINE CR
- [SDR DL72L990921](https://openairdocs.org/sdr/DL72L990921.md): Skin · cracked · Apr 27, 1999 · N507DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN FS 481-681, STRINGER 4R SKIN LAP SPLICE, CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 52 CRACKS ALONG TH
- [SDR DL72L990917](https://openairdocs.org/sdr/DL72L990917.md): Skin · cracked · Apr 27, 1999 · N507DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN FS 360-481 STRINGER 4L, SKIN LAP SPLICE, CRACK REPAIR. INTERNAL HFEC INSPECTION OF THE LOWER FASTENER ROW OF THE LOWER SKIN OF THE STRINGER 4L SKIN LAP SPLICE BETWEEN FS 360 AND 481 INDICATED 6 CRACKS IN THREE CONSECUTIVE FRAME BAYS. THE SKIN L
- [SDR DL72L990916](https://openairdocs.org/sdr/DL72L990916.md): Skin · cracked · Apr 27, 1999 · N507DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN FS 360-480 STRINGER 4R SKIN LAP SPLICE, CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. INTERNAL HFEC INSPECTION CONFIRMED 5 CRACKS IN T
- [SDR DL72L990915](https://openairdocs.org/sdr/DL72L990915.md): Skin · cracked · Apr 27, 1999 · N507DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN FS 680-740 STRINGER 4R SKIN LAP SPLICE, CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 680 AND 740 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 24 CRACKS ALONG THE
- [SDR DL72L982350](https://openairdocs.org/sdr/DL72L982350.md): Light · inop · Nov 14, 1998 · N507DA · Boeing 727232 · Emergency Lighting
  > L-1 AND FWD AISLE AREA EMERGENCY LIGHTS INOP. REPLACED BATTERIES IN THE L-1 DOOR POS AND REPLACED LIGHT ASSY FOR THE FWD AISLE EMERGENCY LIGHT.
- [SDR DL72L981898](https://openairdocs.org/sdr/DL72L981898.md): Web · cracked · Sep 13, 1998 · N507DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND ON MV2 CK,.5 INCH CRACK IN THE STA 1309 WEB LEFT SIDE ABOVE THE S DUCT. REPAIRED PER SRM 53-10-4.
- [SDR DL72L981897](https://openairdocs.org/sdr/DL72L981897.md): Web · cracked · Sep 13, 1998 · N507DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND ON MV2 CK, 1 INCH AND.5 INCH CRACKS FOUND IN STA 1309 WEB RT SIDE ABOVE S DUCT. REPAIRED PER SRM 53-10-4.
- [SDR DL72L981909](https://openairdocs.org/sdr/DL72L981909.md): Skin · corroded · Sep 12, 1998 · N507DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS FOUND WITH SEVERAL SMALL AREAS OF CORROSION AT THE S-26R LAP SPLICE BETWEEN FS 700 AND 720C. THE CORRODED AREAS WERE LOCALLY CUT OUT AND LOCAL REPAIR DOUBLERS WERE INSTALLED. THE REPAIRS WERE ACCOMPLISHED PER ER/A 365577-14, REV C
- [SDR DL72L981850](https://openairdocs.org/sdr/DL72L981850.md): Skin · corroded · Sep 2, 1998 · N507DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS FOUND CORRODED AT FS 700 BETWEEN STR 28R AND 28L. THE CORROSION WAS CUT OUT WITH A 9 X 6.5 CUTOUT. THE CUTOUT WAS ADJACENT TO AN EXISTING REPAIR FOR ANOTHER SKIN CUTOUT. THE EXISTING REPAIR WAS REMOVED AND BOTH SKIN CUTOUTS WERE REPAIR
- [SDR DL72L981873](https://openairdocs.org/sdr/DL72L981873.md): Web · cracked · Aug 28, 1998 · N507DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > A.375 INCH CRACK IN TORQUE BOX VERTICAL WEB STA 1223 LT SIDE, ABOVE STAIRS CLOSE OUT PANEL. REPAIRED PER MM 53-11-0.
- [SDR DL72L981895](https://openairdocs.org/sdr/DL72L981895.md): Angle · corrosion · Aug 26, 1998 · N507DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND DURING MV2 CORROSION VISIT NRC 154, WHILE WORKING NRC 91 FOUND RT SKIN SUPPORT ANGLE CORRODED UNDER STR 27R STA 740. REPLACED SKIN SUPPORT ANGLE PER M/M 53-11-0 PG 859.
- [SDR DL72L981890](https://openairdocs.org/sdr/DL72L981890.md): Stiffener · cracked · Aug 26, 1998 · N507DA · Boeing 727232 · Leading Edge Slat Actuator
  > A.625 INCH CRACK IN SPAR STIFFENER AT NR 5 SLAT ACTUATOR INBD ATTACH FITTING. REMOVED OLD STIFFENER. DRILLED UP STIFFENER PER M/M 57-20-21 PG 813.
- [SDR DL72L981872](https://openairdocs.org/sdr/DL72L981872.md): Frame · cracked · Aug 26, 1998 · N507DA · Boeing 727232 · Passenger/Crew Doors
  > 2 INCH CRACK ON R-1 DOOR AFT FRAME AT LOWER CORNER. REPAIRED PER MM 52-12-0 FIG 804.
- [SDR DL72L981547](https://openairdocs.org/sdr/DL72L981547.md): Transformer · failed · Jul 24, 1998 · N507DA · Boeing 727232 · DC Rectifier/Converter
  > STRONG ELECTRICAL SMELL IN COCKPIT AND FWD CABIN FL 310. FOUND ESSENTIAL T/R AT FAULT. SWAPPED WITH NR 2 T/R AND PUT NR 2 T/R ON MCO.
- [SDR DL72L981530](https://openairdocs.org/sdr/DL72L981530.md): Skin · delaminated · Jul 22, 1998 · N507DA · Boeing 727232 · Ailerons
  > ON T/C, FOUND LEFT O/B AILERON DELAMINATED BEYOND SRM LIMITS. REPLACED LT O/B AILERON TRAILING EDGE WEDGE.
- [SDR DL72L981486](https://openairdocs.org/sdr/DL72L981486.md): Power Pack · inoperative · Jul 16, 1998 · N507DA · Boeing 727232 · Emergency Lighting
  > EMERGENCY TRACK LIGHTING FROM ROW 27 AFT INOP. REPLACED POWER PACK.
- [SDR DL72L981458](https://openairdocs.org/sdr/DL72L981458.md): Battery · discharged · Jul 13, 1998 · N507DA · Boeing 727232 · Emergency Lighting
  > AFT CABIN EMER TRACK LIGHT SECTION INOP. REPLACED BATTERY PACK AND CHARGER, OPS CK OK.
- [SDR DL72L981450](https://openairdocs.org/sdr/DL72L981450.md): Power Supply · inoperative · Jul 13, 1998 · N507DA · Boeing 727232 · Emergency Lighting
  > AFT FLOOR EMERGENCY LIGHTS DID NOT GO ON WHEN TESTED. REPLACED POWER SUPPLY.

Next page: https://openairdocs.org/deregistered/N507DA-2002-09-09/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 = 'N507DA' AND deregistration_id = 'N507DA-2002-09-09'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N507DA-2002-09-09/reports

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