# Service difficulty reports: N988Z, cancelled May 1, 2013

A list on [N988Z, cancelled May 1, 2013](https://openairdocs.org/deregistered/N988Z-2013-05-01.md).

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

- [SDR ZW0A0104806](https://openairdocs.org/sdr/ZW0A0104806.md): Longeron · cracked · Jul 8, 2001 · N988Z · Doug DC931 · Fuselage Main, Longeron/Stringer
  > CRACK IN LONGERON AT STATION 617 FRAME.5 INCH LONG. REPAIRED LONGERON IAW DAC REWORK DRAWING SR09530128 AND SRM 53-02.
- [SDR TWAA9917415](https://openairdocs.org/sdr/TWAA9917415.md): Door Frame · cracked · Dec 24, 1999 · N988Z · Doug DC931 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT, FOUND A FORWARD LT PASSENGER DOOR STOP HOLE, FOURTH HOLE FROM THE TOP ON THE AFT SIDE AND FIFTH FROM THE BOTTOM, AFT SIDE. THE DOOR STOP HOLE HAD A.75 IN CRACK. CUT OUT DAMAGED AREA AND INSTALLED FILLER AND INSTALLED DOUBLER PER EMLR 9
- [SDR TWAA9917402](https://openairdocs.org/sdr/TWAA9917402.md): Longeron · cracked · Dec 24, 1999 · N988Z · Doug DC931 · Fuselage Main, Longeron/Stringer
  > DURING CHECK-C MAINT, THE AFT END OF LONGERON 2L WAS CRACKED AT STA 1076. COMPLETED LONGERON SPLICE PER SRM 53-02, FIG 8.
- [SDR TWAA9917401](https://openairdocs.org/sdr/TWAA9917401.md): Longeron · cracked · Dec 24, 1999 · N988Z · Doug DC931 · Fuselage Main, Longeron/Stringer
  > DURING CHECK-C MAINT, LONGERON 2R WAS CRACKED AT STA 1076. REPAIRED LONGERON 2R AT STA 1076 PER SRM 53-02, FIG 8.
- [SDR TWAA9917403](https://openairdocs.org/sdr/TWAA9917403.md): Angle · cracked · Dec 23, 1999 · N988Z · Doug DC931 · Vertical Stabilizer
  > DURING CHECK-C MAINT, THE FUSELAGE TO VERTICAL STAB ATTACH ANGLE WAS CRACKED.875 INCH LONG AT RT SIDE, STA 1121. CRACK IS BEYOND STOP DRILLED HOLES OF LOWER LEG CRACK. REPAIRED PER SRM 53-05, FIG 230. DOUBLER INSTALLED.
- [SDR TWAA9817302](https://openairdocs.org/sdr/TWAA9817302.md): Angle · cracked · Oct 26, 1998 · N988Z · Doug DC931 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINT CHECK, FOUND CABIN FLOORBEAM SUPPORT ANGLE CRACKED AT STA 680 LBL 43 IN. INSTALLED NEW FITTING (P/N 3916209-501N), USING TENSION HEAD HI-LOKS AND LIKE FASTENERS.
- [SDR TWAA9817301](https://openairdocs.org/sdr/TWAA9817301.md): Membrane · corroded · Oct 26, 1998 · N988Z · Doug DC931 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINT CHECK, FOUND CORROSION ON MEMBRANE AT STA 208 TO 217, LONGERON 18L. REPLACED MEMBRANE PER SRM 53-05 FIG 55 SHEET 2 AND FASTENER SUB PER SRM 51-60-0 AND ARA 15704.
- [SDR TWAA9816804](https://openairdocs.org/sdr/TWAA9816804.md): Angle · cracked · Oct 16, 1998 · N988Z · Doug DC931 · Spoilers
  > DURING OP 16 MAINT CHECK, FOUND RT WING OTBD SPOILER, OTBD DOWN STOP ANGLE WAS CRACKED ON THE INBD SIDE. INSTALLED NEW TEE ANGLE, MFG 5918134-1, PER SRM 51-01, PG 1 ITEM C. INSTALLED RIVETS PER SRM 51-30-02. INSTALLED FASTENERS PER SRM 51-30-0.
- [SDR TWAA9816405](https://openairdocs.org/sdr/TWAA9816405.md): Former · corroded · Oct 16, 1998 · N988Z · Doug DC931 · Fuselage Main, Frame
  > DURING OP 16 MAINT CHECK, FOUND LIGHT CORROSION ON THE FORMER CAP AT STA 897, LONGERON 27L TO 29L. REPLACED FORMER CAP PER STANDARD PROCESSES MANUAL 6-70-1.
- [SDR TWAA9816503](https://openairdocs.org/sdr/TWAA9816503.md): Membrane · punctured · Oct 12, 1998 · N988Z · Doug DC931 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINT CHECK, FOUND MEMBRANE BELOW FLOOR AT STA 947, RBL 50 IN, WAS PUNCTURED. REPAIRED PER SRM 53-01, FIG 2. APPLIED 2 ROWS OF RIVETS ON 0.040 DOUBLER.
- [SDR TWAA9816502](https://openairdocs.org/sdr/TWAA9816502.md): Membrane · cracked · Oct 12, 1998 · N988Z · Doug DC931 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINT CHECK, FOUND MEMBRANE BELOW FLOOR AT STA 958, LBL 50 IN, WAS CRACKED. REPAIRED PER SRM 53-01, FIG 2. APPLIED 3 ROWS OF RIVETS ON 0.040 DOUBLER.
- [SDR TWAA9816314](https://openairdocs.org/sdr/TWAA9816314.md): Longeron · cracked · Oct 7, 1998 · N988Z · Doug DC931 · Fuselage Main, Longeron/Stringer
  > DURING OP 16 MAINT CHECK, FOUND RT LAV STA 980 LONGERON 14R WITH 2 IN CRACK IN FORMER FOOT. REPAIRED PER MO72J14H, DRAWING J060119, AND ARA 15706.
- [SDR TWAA9816313](https://openairdocs.org/sdr/TWAA9816313.md): Longeron · cracked · Oct 7, 1998 · N988Z · Doug DC931 · Fuselage Main, Longeron/Stringer
  > DURING OP 16 MAINT CHECK, FOUND LT LAV STA 980 LONGERON 14L WITH 2 IN CRACK IN FORMER FOOT. REPLACED CRACKED FORMER WITH DAC P/N J060119-17 FORMER PER MO72J14 PHASE G, AND ARA 15706.
- [SDR TWAA9816311](https://openairdocs.org/sdr/TWAA9816311.md): Former · cracked · Oct 7, 1998 · N988Z · Doug DC931 · Fuselage Main, Frame
  > DURING OP 16 MAINT CHECK, FOUND STA 996 FORMER RING FOOT CRACKED ABOVE AND BELOW LONGERON 19L. REMOVED AND REPLACED FORMER RING FOOT SECTION WITH NEW SECTION PART A5910163-79 PER SRM 51-31-0, AND TWA STANDARD PROCEDURES.
- [SDR TWAA9816103](https://openairdocs.org/sdr/TWAA9816103.md): Former · cracked · Oct 5, 1998 · N988Z · Doug DC931 · Fuselage Main, Frame
  > DURING OP 16 MAINT CHECK, FOUND CRACK AT BOTTOM FWD SIDE OF FORMER RING BELOW CABIN FLOOR STA 658 LT. REPAIRED PER SRM 53-03, FIG 16. INSTALLED DOUBLER WITH HI-LOKS AS REQUIRED.
- [SDR TWAA9816312](https://openairdocs.org/sdr/TWAA9816312.md): Buklhead Web · cracked · Oct 1, 1998 · N988Z · Doug DC931 · Fuselage Main, Bulkhead
  > DURING OP 16 MAINT CHECK, FOUND AT RT FUSELAGE BULKHEAD WEB AT STA 965.091, PYLON FROM SPAR LOWER CAP, HIGH FREQ EDDY CURRENT INDICATED CRACK IN LOWER OTBD BOLT HOLE. REAMED HOLE SIZE TO.02807 AND ELIMINATED.
- [SDR TWAA9815903](https://openairdocs.org/sdr/TWAA9815903.md): Seat Track · corroded · Sep 30, 1998 · N988Z · Doug DC931 · Fuselage, Seat/Cargo Attach Fittings
  > DURING OP 16 MAINT CHECK, FOUND NR 4 CABIN CHAIR TRACK CORRODED AT STA 218 TO 237. CORRODED SECTION OF TRACK REMOVED AND NEW SECTION INSTALLED WITH EXISTING HARDWARE.
- [SDR TWAA9815902](https://openairdocs.org/sdr/TWAA9815902.md): Panel · corroded · Sep 30, 1998 · N988Z · Doug DC931 · Wing, Plate/Skin
  > DURING OP 16 MAINT CHECK, FOUND PANEL ABOVE O/B END OF LT AILERON, 8 IN TO 17 IN FROM O/B END, WAS CORRODED AND DELAMINATED. INSTALLED NEW CORE AND ALUM SKIN PER SRM 51-70-2 HOT BOND PROCEDURE PER SERVICEABLE TAG.
- [SDR TWAA9815802](https://openairdocs.org/sdr/TWAA9815802.md): Pan · worn · Sep 28, 1998 · N988Z · Doug DC931 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINT CHECK, FOUND PAN IN FWD ACCESSORY COMPT WITH INTERIM REPAIR INSTALLED PER ARA 11869 AND ARA 11870. REPLACED PAN AND REPAIRED PER ARA 15700, AND SRM 51-30-00 AND SRM 51-30-2.
- [SDR TWAA9815801](https://openairdocs.org/sdr/TWAA9815801.md): Support · corroded · Sep 25, 1998 · N988Z · Doug DC931 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINT CHECK, FOUND CENTER FLOOR SUPPORT, STA 218 TO 237, WAS CORRODED. REMOVED AND REPLACED WITH NEW FLOOR SUPPORT PER SRM 51-01.
- [SDR TWAA9816006](https://openairdocs.org/sdr/TWAA9816006.md): Membrane · corroded · Sep 17, 1998 · N988Z · Doug DC931 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINT CHECK, FOUND CORROSION ON MEMBRANE AT LONGERON 18R, STA 813. CORROSION WAS APPROX 0.008 DEEP AND 3 IN BY 3 IN. REMOVED CORROSION AND REPAIRED WITH ALUM 2024-T3, 0.032 IN PER SRM 53-01, PAGE 9 FIG 2.
- [SDR TWAA9815312](https://openairdocs.org/sdr/TWAA9815312.md): Stringer · corroded · Sep 17, 1998 · N988Z · Doug DC931 · Fuselage Main, Longeron/Stringer
  > DURING OP 16 MAINT CHECK, FOUND STRINGER 2L CRACKED AT BOTH SIDE FLANGES AT STA 200. REPLACED LONGERON MFG PART NR 5911406-13, USING FASTENERS PER SRM 51-30-0.
- [SDR TWAA9815311](https://openairdocs.org/sdr/TWAA9815311.md): Floor · corroded · Sep 17, 1998 · N988Z · Doug DC931 · Fuselage Floor Panel
  > DURING OP 16 MAINT CHECK, FOUND FLOOR PANEL NR 20 WAS CORRODED THROUGH AND HAD BROKEN SUPPORT CHANNELS. FABRICATED NEW FLOOR PANEL PER SRM 53-00-64, FIG 201 PAGE 201.
- [SDR TWAA9815310](https://openairdocs.org/sdr/TWAA9815310.md): Support · broken · Sep 16, 1998 · N988Z · Doug DC931 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINT CHECK, FOUND FLOOR PANEL NR 34 WITH BROKEN SUPPORT CHANNELS. REMOVED AND INSTALLED NEW SUPPORT CHANNELS.
- [SDR TWAA9815309](https://openairdocs.org/sdr/TWAA9815309.md): Floor · corroded · Sep 16, 1998 · N988Z · Doug DC931 · Fuselage Floor Panel
  > DURING OP 16 MAINT CHECK, FOUND FLOOR PANEL NR 19 WITH CORROSION AND SEVERAL BROKEN SUPPORT CHANNELS. REPLACED CABIN FLOOR PANEL SHEET/HAT SECTION PER SRM 53-00-14, PAGE 201.
- [SDR TWAA9815308](https://openairdocs.org/sdr/TWAA9815308.md): Support · corroded · Sep 16, 1998 · N988Z · Doug DC931 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINT CHECK, FOUND CENTER FLOOR SUPPORT BEAM WITH CORROSION, STA 237 TO 313. REPLACED SUPPORT ANGLE STA 237 TO 258. REMOVED CORROSION FROM STA 258 TO 313.
- [SDR TWAA9814708](https://openairdocs.org/sdr/TWAA9814708.md): Seat Track · corroded · Sep 11, 1998 · N988Z · Doug DC931 · Fuselage, Seat/Cargo Attach Fittings
  > CHAIR TRACK GROUND BEYOND LIMITS TO REMOVE CORROSION AT STA 200 TO 237, RBL 23 IN. REMOVED CHAIR TRACK AND REPLACED WITH NEW TRACK. INSTALLED WITH FASTENERS PER SRM 51-30-0.
- [SDR TWAA9814707](https://openairdocs.org/sdr/TWAA9814707.md): Longeron · cracked · Sep 11, 1998 · N988Z · Doug DC931 · Fuselage Main, Longeron/Stringer
  > DURING OP 16 MAINT CHECK, FOUND LONGERON 4L CRACKED AT STA 200. REPLACED LONGERON USING FASTENERS PER SRM 51-30-0.
- [SDR TWAA9814310](https://openairdocs.org/sdr/TWAA9814310.md): Bulkhd Stiffener · cracked · Sep 2, 1998 · N988Z · Doug DC931 · Fuselage Main, Bulkhead
  > DURING OP 16 MAINT CHECK, FOUND.75 INCH CRACK AT UPPER RIVET HOLE ON VERT STIFFENER, AFT SIDE OF BULKHEAD, BETWEEN LONG 3L AND 4L. REPLACED TIE CLIP, UPPER END OF STIFFENER, WITH FASTENERS PER SRM 51-30-0.
- [SDR TWAA9814309](https://openairdocs.org/sdr/TWAA9814309.md): Pan · cracked · Sep 2, 1998 · N988Z · Doug DC931 · Emergency Exits
  > DURING OP 16 MAINT CHECK, FOUND LT FWD EMERGENCY EXIT DOOR PAN CRACKED, WITH INTERIM REPAIR INSTALLED. INSTALLED NEW PAN STOCK NR 63-3273.
- [SDR TWAA9814308](https://openairdocs.org/sdr/TWAA9814308.md): Rib · cracked · Sep 2, 1998 · N988Z · Doug DC931 · Trailing Edge Flaps
  > DURING OP 16 MAINT CHECK, FOUND LT WING TE, I/B RIB CRACKED IN RADIUS BELOW BOLT HOLE, INSIDE FLAP AT O/B HINGE ARM. REPLACED I/B RIB PER SRM 57-50-3, PAGES 9 AND 10. IPC 27-50-01, FIG 2B PAGES 0 TO 7.
- [SDR TWAA9814307](https://openairdocs.org/sdr/TWAA9814307.md): Rib · cracked · Sep 2, 1998 · N988Z · Doug DC931 · Trailing Edge Flaps
  > DURING OP 16 MAINT CHECK, FOUND LT WING TE O/B RIB CRACKED AT TOP BOLT HOLE INSIDE FLAP AT O/B HINGE ARM. REPLACED O/B RIB PER SRM 57-50-3, PAGE 9 AND 10, IPC 27-50-01, FIG 2B PAGE 0 TO 7.
- [SDR TWAA9814306](https://openairdocs.org/sdr/TWAA9814306.md): Skin · corroded · Aug 27, 1998 · N988Z · Doug DC931 · Fuselage Main, Plate/Skin
  > DURING OP 16 MAINT CHECK, FOUND SLIGHT BULGE IN SKIN WITH STRESSED FASTENERS AND BLIND FASTENERS INSTALLED AT STA 29L, JUST AFT OF ELECTRONIC COMPT DOOR. BLENDED DENT AREA AND INSTALLED.025 TITANIUM INTERNAL DOUBLER PER SRM 53.04, FIG 38 SHEET 28 PAGE 218H.
- [SDR TWAA9812129](https://openairdocs.org/sdr/TWAA9812129.md): Longeron · cracked · Jul 22, 1998 · N988Z · Doug DC931 · Fuselage Main, Longeron/Stringer
  > DURING OVERNIGHT MAINT, FOUND LONGERON 6R AT STA 680 WITH.750 INCH CRACKS AT FRAME ATTACH POINTS. FOUND ACCOMPLISHING WORK CARD MC8-AD-AM. REPAIRED LONGERON PER SRM 53-02. CHECK-C 1-8-98 STL.
- [SDR TWAA9812128](https://openairdocs.org/sdr/TWAA9812128.md): Longeron · cracked · Jul 22, 1998 · N988Z · Doug DC931 · Fuselage Main, Longeron/Stringer
  > DURING OVERNIGHT MAINT, FOUND LONGERON 6R AT STA 658 WITH.750 IN CRACKS AT FRAME ATTACH POINTS. FOUND ACCOMPLISHING WORK SHEET MC8-AD-AM. REPAIRED LONGERON PER SRM 53-02 AS REQUIRED. CHECK-C 1-8-98 STL.
- [SDR TWAA9784001](https://openairdocs.org/sdr/TWAA9784001.md): Lights · illuminated · Jul 24, 1997 · N988Z · Doug DC931 · Emergency Lighting
  > STL - FLT 583 - DURING CRUISE, EMERGENCY LIGHTS ILLUMINATED. OPERATIONAL CHECK OF EMERGENCY LIGHTS COMPLETED, NO DEFECTS NOTED. CHECK C - 10-30-96 - STL. (X)
- [SDR TWAA9727004](https://openairdocs.org/sdr/TWAA9727004.md): Engine · failed · Feb 24, 1997 · N988Z · Doug DC931 · Engine (Turbine/Turboprop)
  > DSM - FLT 382 - DURING CLIMB, NR 1 ENGINE, S/N 2161, OIL FILTER CLOG LIGHT ILLUMINATED. CHANGED ENGINE S/N 2161. (M)
- [SDR TWAA9613304](https://openairdocs.org/sdr/TWAA9613304.md): Fitting · cracked · Oct 26, 1996 · N988Z · Doug DC931 · Fuselage Miscellaneous Structure
  > STL - DURING SPECIAL CHECK, FOUND END FITTING OF LONGERON 30 CRACKED, STATION 598. REPLACED FITTING PER SRM 51-00 AND TWA STANDARD PRACTICES. (M)
- [SDR 96ZZZM1339](https://openairdocs.org/sdr/96ZZZM1339.md): Anti Retract Mec · out of adjust · Aug 9, 1996 · N988Z · Doug DC931 · Landing Gear Retraction/Extension System
  > STL - AFTER TAKEOFF WHEN LANDING GEAR WAS SELECTED TO RETRACT, LANDING GEAR DID NOT RETRACT. FOUND ANTI-RETRACT LATCH OUT OF ADJUSTMENT. RIGGED ANTI-RETRACT MECHANISM. LANDING GEAR OPERATIONS THEN CHECKED NORMAL. (M)
- [SDR 96ZZZX307](https://openairdocs.org/sdr/96ZZZX307.md): Duct · cracked · Jan 8, 1996 · N988Z · Doug DC931 · Pneumatic Distribution System
  > STL - FLT 568 - AFTER TAKEOFF, NR 1 ENGINE FIREWARNING LIGHT ILLUMINATED. REMOVED AND REPLACED CRACKED 8TH STAGE DUCT. OPERATIONAL LEAK CHECK ACCOMPLISHED, NO LEAKS FOUND. OP-15 - 8-21-95 - STL.
- [SDR 95ZZZM680](https://openairdocs.org/sdr/95ZZZM680.md): Fuel Tank · leaking · Oct 18, 1995 · N988Z · Doug DC931 · Fuel Storage
  > ATL - DURING CRUISE, FUEL SMELL DETECTED IN CABIN. FOUND FUEL LEAK FROM CENTER TANK IN RIGHT WHEEL WELL.
- [SDR 95ZZZX5144](https://openairdocs.org/sdr/95ZZZX5144.md): Downlock Switch · malfunctioned · Sep 1, 1995 · N988Z · Doug DC931 · Landing Gear Position and Warning
  > STL - FLT 693 - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED NOSE LANDING GEAR GREEN, LOCKED LIGHT DID NOT ILLUMINATE. CYCLED LANDING GEAR AND GREEN LOCKED LIGHT ILLUMINATED. FOUND DEFECTIVE NOSE GEAR DOWNLOCK SWITCH, MFG PN H14-6. REPLACED NOSE GEAR DOWN
- [SDR 95ZZZX5146](https://openairdocs.org/sdr/95ZZZX5146.md): Longeron · corroded · Aug 2, 1995 · N988Z · Doug DC931 · Fuselage Main, Longeron/Stringer
  > STL - DURING OP-15, FOUND CORROSION ON LONGERON 28L, STA 945 TO STA 996. REMOVED AND REPLACED LONGERON SECTION PER SRM 51-30-5, SRM 51-30-2, AND TWA STANDARD PRACTICES. AIRCRAFT TOTAL TIME: 67,006 HOURS; 73,957 CYCLES.
- [SDR 95ZZZM532](https://openairdocs.org/sdr/95ZZZM532.md): Longeron · corroded · Aug 2, 1995 · N988Z · Doug DC931 · Fuselage Main, Longeron/Stringer
  > STL - DURING OP-15, FOUND CORROSION ON LONGERON 29L, STATION 945 TO 996. REMOVED AND REPLACED LONGERON SECTION PER SRM 51-30-5, 51-30-2, AND TWA STANDARD PRACTICES. TOTAL CYCLES 73,957.
- [SDR 95ZZZM531](https://openairdocs.org/sdr/95ZZZM531.md): Seat Track · corroded · Aug 2, 1995 · N988Z · Doug DC931 · Fuselage, Seat/Cargo Attach Fittings
  > STL - DURING OP-15, FOUND CORROSION ON RIGHT OUTBOARD SEAT TRACK, STATION 200 TO 266. SPLICED IN NEW SEAT TRACK PER SRM 53-05, FIGURE 4. TOTAL CYCLES 73,957.
- [SDR 95ZZZM456](https://openairdocs.org/sdr/95ZZZM456.md): Longeron · corroded · Aug 2, 1995 · N988Z · Doug DC931 · Fuselage Main, Longeron/Stringer
  > STL - DURING OP-15, FOUND CORROSION ON LONGERON 29L, STATION 945 TO 996. REMOVED AND REPLACED LONGERON SECTION PER SRM 51-30-5, 51-30-2, AND TWA STANDARD PRACTICES.
- [SDR 95ZZZM455](https://openairdocs.org/sdr/95ZZZM455.md): Longeron · corroded · Aug 2, 1995 · N988Z · Doug DC931 · Fuselage Main, Longeron/Stringer
  > STL - DURING OP-15, FOUND CORROSION ON LONGERON 28L, STATION 945 TO 996. REMOVED AND REPLACED LONGERON SECTION PER SRM 51-30-5, 51-30-2, AND TWA STANDARD PRACTICES.
- [SDR 95ZZZM447](https://openairdocs.org/sdr/95ZZZM447.md): Seat Track · corroded · Aug 2, 1995 · N988Z · Doug DC931 · Fuselage, Seat/Cargo Attach Fittings
  > STL - DURING OP-15, FOUND CORROSION ON RIGHT OUTBOARD SEAT TRACK, STATION 200 TO 266. SPLICED IN NEW SEAT TRACK PER SRM 53-05, FIGURE 4.

## 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 = 'N988Z' AND deregistration_id = 'N988Z-2013-05-01'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N988Z-2013-05-01/reports

---
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