# Service difficulty reports: N508DA, cancelled Sep 16, 2003

A list on [N508DA, cancelled Sep 16, 2003](https://openairdocs.org/deregistered/N508DA-2003-09-16.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 2 · 68 reports

- [SDR DL72L020038](https://openairdocs.org/sdr/DL72L020038.md): Skin · corroded · Jan 11, 2002 · N508DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS FOUND WITH AN AREA OF CORROSION BETWEEN FS 1030 & 1050 AT STRINGER 28L. THE CORROSION WAS REMOVED WITH A 16 X 4 INCH CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED WITH A DOUBLER PER ER/A 382438-14, REV A.
- [SDR DL72L020035](https://openairdocs.org/sdr/DL72L020035.md): Beam · cracked · Jan 10, 2002 · N508DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > INSPECTION OF THE RT VENTRAL STAIRWAY TORQUE BOX STRUCTURE PER AD 94-07-08 AND BAC S/B 727-53-0129 REVEALED TYPICAL CRACKS IN THE FS 1263 AND 1273 HORIZONTAL BEAM CAPS. THE CRACKED MEMBERS WERE REMOVED AND NEW PARTS INSTALLED PER ER/A 382433-14AD.
- [SDR DL72L020031](https://openairdocs.org/sdr/DL72L020031.md): Skin · cracked · Jan 10, 2002 · N508DA · Boeing 727232 · Elevator, Plate/Skin
  > FOUND ON B1 LETTER CHECK RT ELEVATOR LOWER SKIN IS CRACKED FWD OF TAB. REPAIRED PER B-727 DRD 55-20-3D FIG 4.
- [SDR DL72L020032](https://openairdocs.org/sdr/DL72L020032.md): Stiffener · cracked · Jan 9, 2002 · N508DA · Boeing 727232 · Wing Miscellaneous Structure
  > L/E SPAR STIFFENER CRACKED AT NR 7 SLAT I/B TRACK I/B SIDE. REPLACED STIFFENER PER M/M.
- [SDR DL72L010922](https://openairdocs.org/sdr/DL72L010922.md): Angle · cracked · Jun 6, 2001 · N508DA · Boeing 727232 · Leading Edge Devices
  > FOUND ON A2 LETTER CK,.25 INCH CRACK NR 4 SLAT T/E CHORD AT O/B TRACK CUTOUT. REPAIRED PER MM 57-54-000-8.
- [SDR DL72L002152](https://openairdocs.org/sdr/DL72L002152.md): Fitting · corroded · Nov 2, 2000 · N508DA · Boeing 727232 · Vertical Stabilizer, Attach Fittings
  > THE VERTICAL STABILIZER TENSION TIE FITTING FORWARD AND AFT ATTACH BOLT HOLES WERE FOUND WITH CORROSION IN THE BORES. THE BORES WERE OVERSIZED AND BUSHED PER ERA 396341-14 AT HMV.
- [SDR DL72L002114](https://openairdocs.org/sdr/DL72L002114.md): Beam · corroded · Oct 26, 2000 · N508DA · Boeing 727232 · Wing, Landing Gear Attach Fittings
  > LT MLG BEAM LOWER FACE CORRODED AT LWR T/E PANEL BORES 2, 5, 6, 7, 8, 9, 11, 12, 14, 15, 28. ALL WORK ACCOMPLISHED PER ERA NR 396313-14, NO REVISION.
- [SDR DL72L002109](https://openairdocs.org/sdr/DL72L002109.md): Structure · damaged · Oct 25, 2000 · N508DA · Boeing 727232 · Nacelle/Pylon, Main Frame
  > AFT END OF DOGHOUSE 6 O''CLOCK POSITION DOUBLER PEELED BACK ON BOTH SIDES OF INLET SKIN BUTT JOINT. REMOVED DAMAGE PER SRM 54-10-3D FIG 801D. DYE PENETRANT INSP AREA, NO CRACKS FOUND SRM 54-10-10-3D. CHEMICAL TREATED PER 900-2-4 NR 02. APPLIED EPOXY PRIME
- [SDR DL72L002108](https://openairdocs.org/sdr/DL72L002108.md): Beam · corroded · Oct 25, 2000 · N508DA · Boeing 727232 · Wing, Landing Gear Attach Fittings
  > LT MLG BEAM LWR T/E PNL BORES CORRODED. REAMED HOLES 34, 35, 36, 37 AND 18 TO.312 PER SRM 57-40D. REAMED HOLES 28 AND 39 TO.359 PER SRM 57-40D. REAMED HOLE 32 TO.312 PER SRM 57-40-D. BHEC INSP OF FASTENER FOR CRACKS AND CORROSION. NO ITEM. TURNED O/B
- [SDR DL72L002107](https://openairdocs.org/sdr/DL72L002107.md): Beam · corroded · Oct 25, 2000 · N508DA · Boeing 727232 · Wing, Landing Gear Attach Fittings
  > LT MLG BEAM HOLES BORES NR 2, 5, 6, 7, 8, 9, 11, 12, 14, 15 AND 28 SHOW CORROSION. REAMED HOLES 2, 5 6, 7, 8, 9, 11, 12, 14, 15 TO.312. HOLE 28 TO.359 PER SRM 57-40-D. BHEC INSP OF FASTENERS FOR CRACKS AND COROSION. NO ITEMS. TURNED O/B ON IN PROCESS
- [SDR DL72L002094](https://openairdocs.org/sdr/DL72L002094.md): Fitting · cracked · Oct 24, 2000 · N508DA · Boeing 727232 · Nacelle/Pylon, Main Frame
  > DURING INSPECTIONS REQUIRED BY AD 97-05-08 6 CRACKS WERE FOUND IN THE NR 1 FORWARD ENGINE PYLON AND ONE CRACK WAS FOUND IN THE NR 3 PYLON. ERA 396334-14AD OVERSIZES THE FASTENER HOLES TO REMOVE THE CRACK PER FEDEX AVIATION SERVICES S/B 2000-5410A01 AT HMV.
- [SDR DL72L011138](https://openairdocs.org/sdr/DL72L011138.md): Angle · cracked · Oct 20, 2000 · N508DA · Boeing 727232 · Wing Miscellaneous Structure
  > DURING SHOP VISIT THE LOWER AFT CHORD ANGLE WAS FOUND CRACKED AT I/B AFT FLAP DRIVE ROD CUTOUT.
- [SDR DL72L002061](https://openairdocs.org/sdr/DL72L002061.md): Skin · cracked · Oct 19, 2000 · N508DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > CRACKS WERE FOUND ALONG THE STR 4R LAP JOINT BETWEEN FS 1070 AND FS 1090. THE CRACKS WERE REMOVED AND REPAIRED SIMILIAR TO THAT OF B727 SRM 53-30-3, FIGURE 5 PER ERA 396320-14AD AT HMV.
- [SDR DL72L002060](https://openairdocs.org/sdr/DL72L002060.md): Skin · cracked · Oct 19, 2000 · N508DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > SKIN CRACKS WERE FOUND IN THE STR 4L LAP JOINT BETWEEN FS 1050 AND 1070. THE CRACKS WERE REMOVED AND REPAIRED SIMILIAR TO B727 SRM 53-30-3, FIGURE 5 PER ERA 396304-14AD.
- [SDR DL72L002059](https://openairdocs.org/sdr/DL72L002059.md): Skin · cracked · Oct 19, 2000 · N508DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > CRACKS WERE FOUND ALONG THE STR 4R LAP JOINT BETWEEN FS 1030 AND FS 1050. THE CRACKS WERE REMOVED AND REPAIRED SIMILIAR TO B727 SRM 53-30-3, FIGURE 5 PER ERA 396305-14AD.
- [SDR DL72L002058](https://openairdocs.org/sdr/DL72L002058.md): Skin · cracked · Oct 19, 2000 · N508DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > CRACKS WERE FOUND IN THE STR 26L LAP JOINT BETWEEN FS 600 AND FS 620. THE DAMAGE WAS REMOVED AND REPAIRED PER ERA 396310-14AD SIMILIAR TO THAT OF B727 SRM 53-30-3, FIGURE 5.
- [SDR DL72L002054](https://openairdocs.org/sdr/DL72L002054.md): Skin · cracked · Oct 19, 2000 · N508DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > MULTIPLE CRACKS WERE FOUND BETWEEN FS 481 AND FS 681 IN THE STR 4R LAP JOINT. THE CRACKS WERE REMOVED AND REPAIRED PER ERA 396303-14 AT HMV.
- [SDR DL72L002023](https://openairdocs.org/sdr/DL72L002023.md): Beam · corroded · Oct 16, 2000 · N508DA · Boeing 727232 · Wing, Landing Gear Attach Fittings
  > LT MLG BEAM LWR T/E PANEL ATTACH BORES CORRODED. HOLES 35, 29, 27, 26, 25 REAMED TO.312 PER SRM 57-40D. 28 REAMED TO.359 PER SRM 57-40D. REAMED 10 8 TO.312 PER SRM 57-40D. BHEC INSPECT OF FASTENER HOLE FOR CRACKS AND CORROSION. NO ITEM, TURNED O/D ON
- [SDR DL72L010887](https://openairdocs.org/sdr/DL72L010887.md): Angle · cracked · Oct 13, 2000 · N508DA · Boeing 727232 · Trailing Edge Flaps
  > DURING SHOP VISIT THE AFT LOWER CHORD ANGLE WAS FOUND CRACKED ON THE MID FLAP. THE CHORD ANGLE WAS REPAIRED PER 727 M/M 57-52-0, FIG 802 BY STOP DRILLING THE CRACK AND INSTALLING A DOUBLER.
- [SDR DL72L002095](https://openairdocs.org/sdr/DL72L002095.md): Skin · corroded · Oct 13, 2000 · N508DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > LOWER SECTION OF BONDED DOUBLER FOUND DISBONDED BELOW THE AFT LAV SERVICE PANEL CUTOUT. 396323-14 REV A.
- [SDR DL72L001972](https://openairdocs.org/sdr/DL72L001972.md): Beam · corroded · Oct 11, 2000 · N508DA · Boeing 727232 · Wing, Landing Gear Attach Fittings
  > RT MLG SUPPORT BEAM BORES CORRODED. TASK: C57-581-01.01 FASTENER BORES CORRODED AT HOLES 3, 4, 5, 11, 12, 26, 27, 30, 31, 32, 36 & 38. REWORK HOLES PER DRD 57-40D. 3, 4, 5, 11, 26, 30, 31, 32, 36 REAMED TO 0.358. 27, 12, 13 REAMED TO 0.262. 38 REAMED TO 0
- [SDR DL72L002131](https://openairdocs.org/sdr/DL72L002131.md): Plate · corroded · Oct 9, 2000 · N508DA · Boeing 727232 · Vertical Stabilizer, Plate/Skin
  > AT HMV, THE VERT STAB TENSION TIE PLATE AFT CTR ATTACH POINTS WERE CORRODED AROUND FACE AND IN BORES. REMOVED CORR DYE PEN CK GOOD WITHIN LIMITS PER SRM 55-30-5D FIG 801D. REAMED HOLES TO.691 TI REM CIRR BHEC INSP NO ITEMS OPENED HOLES TO.737 BFEC INSP NO
- [SDR DL72L002020](https://openairdocs.org/sdr/DL72L002020.md): Rib · cracked · Oct 9, 2000 · N508DA · Boeing 727232 · Leading Edge Devices
  > AT HMV THE NR 11 RIB FLANGE OF THE NR 3 SLAT WAS FOUND TO BE CRACKED. ROUTED OUT DAMAGE, FABRICATED REPAIR PARTS PER MM 57-54-0, REPAIRED PER MM 57-54-0.
- [SDR DL72L002021](https://openairdocs.org/sdr/DL72L002021.md): Shim · shifted · Oct 8, 2000 · N508DA · Boeing 727232 · Spoilers
  > AT HMV THE SHIMS WERE FOUND MIGRATING AT NR 12 SPOILER ACTUATOR LOWER ATTACH BOLT SHIMS. REPAIRED SHIMS AND C/W MM 57-54-0.
- [SDR DL72L002052](https://openairdocs.org/sdr/DL72L002052.md): Stringer · cracked · Oct 6, 2000 · N508DA · Boeing 727232 · Wing, Longeron/Stringer
  > AT HMV, THE FIFTH STRINGER AFT OF FRONT SPAR STA 171.5 WAS FOUND TO BE CRACKED. REMOVED DAMAGE PER SRM 57-10-5D FIG 802D. PERFORMED HFEC PER SRM 57-10-5D FIG 802D, NO IND. TREATED AND PAINTED PER SRM 57-10-5D FIG 802D. FABRICATED REPAIR PARTS PER SRM 57-10
- [SDR DL72L002019](https://openairdocs.org/sdr/DL72L002019.md): Rib · cracked · Oct 6, 2000 · N508DA · Boeing 727232 · Leading Edge Devices
  > AT HMV THE NR 13 RIB OF THE NR 3 SLAT WAS FOUND TO BE CRACKED. ROUTED OUT DAMAGE FOR FABRICATED DOUBLER. REPAIRED PER MM 57-54-0.
- [SDR DL72L002018](https://openairdocs.org/sdr/DL72L002018.md): Rib · cracked · Oct 6, 2000 · N508DA · Boeing 727232 · Leading Edge Devices
  > AT HMV NR 7 RIB OF SLAT FOUND TO BE CRACKED. REMOVED LWR AFT SPAR REPAIR DOUBLER IN AREA, FABRICATED REPAIR DOUBLER PER MM 57-54-0, ROUTED OUT DAMAGE, INSTALLED DOUBLER AND FILLER PER MM 57-54-0, REINSTALLED SPAR DOUBLER.
- [SDR DL72L002084](https://openairdocs.org/sdr/DL72L002084.md): Web · cracked · Oct 5, 2000 · N508DA · Boeing 727232 · Vertical Stabilizer
  > AT HMV, THE WEB ON THE VERTICAL FIN WAS FOUND CRACKED. REMOVED FASTENERS AND BEGAN FABR DOUBLER PER SRM 53-10-4D FIG 802D. STOP DRILLED CRACKS, COMPLETED FABR OF DOUBLER, DYE CKED, INSTALLED DOUBLER PER SRM 53-10-4D FIG 802D.
- [SDR DL72L002083](https://openairdocs.org/sdr/DL72L002083.md): Flange · bent · Oct 5, 2000 · N508DA · Boeing 727232 · Turbine Engine Air Inlet Section
  > AT HMV, THE AFT FLANGE OF THE NR 2 INLET WAS TORN/BENT. REMOVED DAMAGE PER SRM 54-10-3D FIG 801D. DYE CKED, NO FURTHER DAMAGE NOTED. FABRICATED REPAIR PARTS AND INSTALLED PER SRM 54-10-3D FIG 801D.
- [SDR DL72L001982](https://openairdocs.org/sdr/DL72L001982.md): Cowling · worn · Oct 5, 2000 · N508DA · Boeing 727232 · Engine Cowling System
  > AT HMV FOUND NR 2 ENG COWL RING WORN NR 2 FWD COWL, 5 O''CLOCK TO 7 O''CLOCK NO ED FOR RIVETS. REMOVED EXISTING REPAIR, FABD NEW REPAIR PER MM 53-11-0 PG 801, INSTALLED NEW COWL RING PER MM 53-11-0 PG 801, APPLIED TEFLON COATING PER PS 900-3-1, 04.
- [SDR DL72L001981](https://openairdocs.org/sdr/DL72L001981.md): Frame · cracked · Oct 5, 2000 · N508DA · Boeing 727232 · Fuselage Main, Frame
  > AT HMV FOUND FORMER CRACKED, STA 600, LBL 10. ROUTED OUT CRACK PER SRM 53-10-4D FIG 811D, FABD REPAIR, T/P PER SRM 51-40-3, INSTALLED PER SRM 51-40-3.
- [SDR DL72L001963](https://openairdocs.org/sdr/DL72L001963.md): Beam · corroded · Oct 5, 2000 · N508DA · Boeing 727232 · Wing, Landing Gear Attach Fittings
  > AT HMV FOUND RT MLG SUPPORT BEAM BORES CORRODED. FASTENER BORES CORRODED AT HOLES, 17/18/19/22/23/24/39/40/41/42/43/44/45/46. REWORKED CORRODED HOLES PER DRD 57-40D FIG 803D, ALL HOLES ARE 0.312, BHEC INSP OF HOLES LISTED PER DRD 57-40D, SHOWS NO ITEMS.
- [SDR DL72L001962](https://openairdocs.org/sdr/DL72L001962.md): Beam · corroded · Oct 5, 2000 · N508DA · Boeing 727232 · Wing, Landing Gear Attach Fittings
  > AT HMV BHEC OF BEAM NR HOLE 25 ON RMLG SUPPORT BEAM SHOWS CORROSION IN HOLES. REWORK HOLE NR 25 PER DRD 57-40D FIG 803D, NR 25 0.358, BHEC INSP OF HOLE PER DRD 57-40 CKD OK, MECH AND TREATED BUSHINGS PER SRM 57-40D INSTALLED BUSHING PER SRM 57-40D PG 14, STEO
- [SDR DL72L001941](https://openairdocs.org/sdr/DL72L001941.md): Flap Track · corroded · Oct 5, 2000 · N508DA · Boeing 727232 · Trailing Edge Flaps
  > DURING OVERHAUL AT BFGOODRICH, SEVERAL AREAS OF THE I/B FLAP, NR 4 I/B TRACK WERE FOUND WITH CORROSION/WEAR WHICH WERE BEYOND ALLOWABLE LIMITS. AFFECTED AREAS INCLUDE THE MLG BEAM ATTACH HOLES AND SPOTFACE, THE SPOILER BEAM ATTACH HOLES, THE MLG DOOR AFT HING
- [SDR DL72L001940](https://openairdocs.org/sdr/DL72L001940.md): Flap Track · corroded · Oct 5, 2000 · N508DA · 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 WEAR AT THE FWD ATTACH LUGS, MLG DOOR HINGE FITTING ATTACH HOLES, SPACER BLOCK ATTACH HOLES, AND CLIP ASSY ATTACH HOLES, AT THE MLG B
- [SDR DL72L001980](https://openairdocs.org/sdr/DL72L001980.md): Bolt · loose · Oct 4, 2000 · N508DA · Boeing 727232 · Spoilers
  > AT HMV FOUND LW NR 4 SPOILER ACTUATOR MOUNT HAS LOOSE BOLTS ON BOTTOM OF WING SPAR TO MOUNT BOLTS. TIGHTENED NUT.
- [SDR DL72L001965](https://openairdocs.org/sdr/DL72L001965.md): Actuator · loose · Oct 4, 2000 · N508DA · Boeing 727232 · Drag Control Actuator
  > AT HMV THE NR 3 SPOILER ACTUATOR WAS FOUND TO HAVE LOOSE MOUNT BOLTS ON BOTTOM ATTACHED TO REAR SPAR. REPAIRED PER MM 57-42-0.
- [SDR DL72L001945](https://openairdocs.org/sdr/DL72L001945.md): Mount · loose · Oct 4, 2000 · N508DA · Boeing 727232 · Spoilers
  > AT HMV FOUND NR 1 SPOILER MOUNT BOX ATTACHED TO REPAIR SPAR IS LOOSE AT BOTTOM BOLTS. REPAIRED PER MM 57-42-0.
- [SDR DL72L992526](https://openairdocs.org/sdr/DL72L992526.md): Engine · unresponsive · Nov 15, 1999 · N508DA · Boeing 727232 · Engine (Turbine/Turboprop)
  > NR 1 ENG THROTTLE DID NOT RESPOND TO CONTROL. RECONNECTED THROTTLE ROD LINKAGE, RAN ENG PER PFHB. OP CHECKS GOOD.
- [SDR DL72L992410](https://openairdocs.org/sdr/DL72L992410.md): Stud · missing · Oct 31, 1999 · N508DA · Boeing 727232 · Turbine Engine Reduction Gear
  > NR 1 ENG RAPID OIL LOSS, LOW OIL PRESS LT ILLUM AND QTY WENT TO ZERO. SHUTDOWN ENG PER POM. FOUND.25 INCH STUD MISSING FROM FRONT GEARBOX COVER. REINSTALLED STUD PER 727 M/M 72-61-02.
- [SDR DL72L992180](https://openairdocs.org/sdr/DL72L992180.md): Batteries · discharged · Sep 30, 1999 · N508DA · Boeing 727232 · Emergency Lighting
  > BATTERIES WEAK IN FWD COACH CLASS CABIN OVERHEAD EMERGENCY LIGHT. REPLACED BATTERIES.
- [SDR DL72L991253](https://openairdocs.org/sdr/DL72L991253.md): Wire · damaged · May 18, 1999 · N508DA · Boeing 727232 · Electrical Power System Wiring
  > ON HUSH-KIT MOD FOUND NUMEROUS LONGITUDINAL CRACKS ON INSULATION IN ALL 3 GEN FEEDER CABLES IN MID PYLON AREA. REPLACED CABLES FROM SPLICES IN LT 48 SEC TO FIREWALL DISCONNECT WITH NEW TYPE CABLES BMS13-58 DL (P/N 012210733) PER BOEING SERVICE LETTER 727-SL24
- [SDR DL72L982003](https://openairdocs.org/sdr/DL72L982003.md): Floorbeam · corroded · Sep 22, 1998 · N508DA · Boeing 727232 · Fuselage Main, Floor Beam
  > FLOORBEAM CAP CORRODED STA 344 LBL 40 TO 48. REPAIRED PER 272 SRM 53-10-8.
- [SDR DL72L981978](https://openairdocs.org/sdr/DL72L981978.md): Fitting · worn · Sep 22, 1998 · N508DA · Boeing 727232 · Service Doors
  > FITTING WORN ON LT AFT SERVICE DOOR AFT LOWER EDGE OF DOOR. C/W MM 52-14-0 FIG 805.
- [SDR DL72L981043](https://openairdocs.org/sdr/DL72L981043.md): Web · cracked · May 15, 1998 · N508DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND AT E-1 LETTER CHECK, WEB CRACKED LT SIDE ABOVE LIGHTENING HOLE AFT STAIR AREA STA 1223. REPAIRED PER M/M53-11-0.
- [SDR DL72L981042](https://openairdocs.org/sdr/DL72L981042.md): Angle · cracked · May 15, 1998 · N508DA · Boeing 727232 · Leading Edge Devices
  > FOUND ON E1 LETTER CK, 1 INCH CRACK INBD ATTACH CASTING NR 5 L/E SLAT ACTUATOR. REPLACED ANGLE.
- [SDR DL72L981041](https://openairdocs.org/sdr/DL72L981041.md): Angle · cracked · May 15, 1998 · N508DA · Boeing 727232 · Leading Edge Devices
  > FOUND ON E1 LETTER CK, 1.25 INCH CRACK INBD ATTACH CASTING FOR NR 4 L/E EDGE SLAT ACTUATOR. REPLACED ANGLE.
- [SDR DL72L981039](https://openairdocs.org/sdr/DL72L981039.md): Web · cracked · May 15, 1998 · N508DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND AT E1 LETTER CHECK, WEB CRACKED RT SIDE FWD UPPER LIGHTENING HOLE REPAIRED PER M/M 53-11-0.
- [SDR DL72L980321](https://openairdocs.org/sdr/DL72L980321.md): Torque Tube · failed · Feb 5, 1998 · N508DA · Boeing 727232 · Landing Gear Retraction/Extension System
  > UPON T/O, AFTER GEAR RETRACTION (DOORS LIGHT REMAINED ILLUMINATED AND RT GEAR DOOR LIGHT ON S/O PNL WAS ON. ADDITIONALLY RT GEAR AND GREEN GEAR LIGHTS REMAINED ILL.VISUAL INSP CONFIRMED RMLG WAS DWN. ACCOMPLISHED POM WITH GEAR HANDLE UP POS THE LIGHTS REMAIN
- [SDR DL72L980216](https://openairdocs.org/sdr/DL72L980216.md): Light · inoperative · Jan 26, 1998 · N508DA · Boeing 727232 · Emergency Lighting
  > AFT AIRSTAIR EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY.

Next page: https://openairdocs.org/deregistered/N508DA-2003-09-16/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 = 'N508DA' AND deregistration_id = 'N508DA-2003-09-16'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N508DA-2003-09-16/reports

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