# Service difficulty reports: N998R, cancelled Mar 15, 2011

A list on [N998R, cancelled Mar 15, 2011](https://openairdocs.org/deregistered/N998R-2011-03-15.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 · 59 reports

- [SDR TWAA0105501](https://openairdocs.org/sdr/TWAA0105501.md): Battery · discharged · Mar 26, 2001 · N998R · Doug DC932 · Emergency Lighting
  > THE COCKPIT OVERHEAD EMERGENCY LIGHT WAS INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY. CHECK-C 2-4-01 STL.
- [SDR TWAA0101703](https://openairdocs.org/sdr/TWAA0101703.md): Longeron · cracked · Jan 26, 2001 · N998R · Doug DC932 · Fuselage Main, Longeron/Stringer
  > DURING CHECK-C MAINT LONGERON 6L AT STA 718 WAS FOUND CRACKED AT LOWER FLANGE,.25 INCH CRACK. REMOVED AND REPLACED SECTION OF LONGERON 6L AT STA 699 TO 718 PER SRM 53-02. INSTALLED DOUBLER ON FACE OF INTERCOSTAL AT LONGERON LEG, FABRICATED FROM 0.032 2024-T
- [SDR TWAA0101507](https://openairdocs.org/sdr/TWAA0101507.md): Longeron · cracked · Jan 25, 2001 · N998R · Doug DC932 · Fuselage Main, Longeron/Stringer
  > DURING CHECK-C MAINT LONGERON 3R AT STA 658 WAS CRACKED AT LOWER FLANGE.25 INCH LONG. REPAIRED PER SRM 53-02 AND DRAWING SRO 9530128.
- [SDR TWAA0016501](https://openairdocs.org/sdr/TWAA0016501.md): Skin · damaged · Oct 22, 2000 · N998R · Doug DC932 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS DAMAGED BY GROUND EQUIPMENT AFT OF THE FWD CARGO DOOR, LOWER LT CORNER AT STA 427. REPAIRED PER DOUGLAS DRAWING SRO9530117-7011 AND ARA 16859 AND EMLR 71243. CHECK-C 10-27-99 STL.
- [SDR TWAA0014201](https://openairdocs.org/sdr/TWAA0014201.md): Power Supply · inoperative · Sep 12, 2000 · N998R · Doug DC932 · Emergency Lighting
  > THE EGRESS LIGHTS WERE INOPERATIVE FROM ROW 16 TO 21. REPLACED THE POWER SUPPLY. CHECK-C 10-27-99 STL.
- [SDR TWAA0101702](https://openairdocs.org/sdr/TWAA0101702.md): Longeron · cracked · Jan 27, 2000 · N998R · Doug DC932 · Fuselage Main, Longeron/Stringer
  > DURING CHECK-C MAINT LONGERON 4L WAS FOUND CRACKED IN 2 PLACES AT BELT RING, STA 1087. REMOVED AND REPLACED LONGERON PER SRM 53-02, FIG 18.
- [SDR TWAA9914606](https://openairdocs.org/sdr/TWAA9914606.md): Connector · failed · Oct 29, 1999 · N998R · Doug DC932 · Landing Gear Position and Warning
  > DURING APPROACH, THE LEFT MAIN LANDING GEAR DOWN LOCK LIGHT FLICKERED. REPLACED SWITCH CONNECTOR MFG PN DS07-75295 AND SOCKET MFG PN 800-20-30-1. CC00 10-14-99, STL.
- [SDR TWAA9914803](https://openairdocs.org/sdr/TWAA9914803.md): Skin · corroded · Oct 23, 1999 · N998R · Doug DC932 · Fuselage Main, Plate/Skin
  > DURING CHECK-C MAINT, FOUND SKIN PILLOWED/DENTED AND RIVETS POSSIBLY DISTRESSED ON LT FUSELAGE, NEAR THE PRESSURE DOME, FORWARD AND BELOW THE TR SELECTOR ACCESS. A SIX BY 8 INCH AREA. REPAIRED DAMAGED AREA PER ARA 13937.
- [SDR TWAA9914802](https://openairdocs.org/sdr/TWAA9914802.md): Fitting · corroded · Oct 23, 1999 · N998R · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT, FOUND AT STA 996 THE END CAP FITTINGS AT LONGERON 23L, 24L, AND 25L WERE FOUND WITH CORROSION. REMOVED AND REPLACED THE FITTINGS PER SRM 51-30-5.
- [SDR TWAA9914506](https://openairdocs.org/sdr/TWAA9914506.md): Longeron · cracked · Oct 21, 1999 · N998R · Doug DC932 · Fuselage Main, Longeron/Stringer
  > DURING CHECK-C, MAINT FOUND A 1 INCH CRACK AT STA 1076, LONGERON 2R. SPLICED SECTION PER SRM 53-02, FIG 18.
- [SDR TWAA9914505](https://openairdocs.org/sdr/TWAA9914505.md): Longeron · cracked · Oct 21, 1999 · N998R · Doug DC932 · Fuselage Main, Longeron/Stringer
  > DURING CHECK-C, MAINT FOUND LONGERON 2L AT STA 1076 HAD A 1 INCH CRACK. SPLICED SECTION PER SRM 53-02, PAGE 18.
- [SDR TWAA9908201](https://openairdocs.org/sdr/TWAA9908201.md): Skin · scratched · May 29, 1999 · N998R · Doug DC932 · Trailing Edge Flaps
  > FOUND THE RT WING T/E FLAP AFT OF MOVAEBLE VANE HAD 2 SCRATCHES.020 TO.050 IN DEEP. REMOVED DAMAGED AREA AND REPAIRED PER SRM 57-01, FIG 5, AND ENGR CONCURRENCE A3250A. CHECK-C 8-7-98 MCI.
- [SDR TWAA9907302](https://openairdocs.org/sdr/TWAA9907302.md): Bracket · cracked · May 12, 1999 · N998R · Doug DC932 · Rudder Control System
  > THE CAPTAINS RUDDER PEDAL BRACKET WAS CRACKED AT THE AFT O/B MOUNT LEG, 1.125 INCH LONG. REMOVED AND REPLACED THE RUDDER BRACKET PER MM 27-20-12. CHECK-C 8-7-98 MCI.
- [SDR TWAA9812511](https://openairdocs.org/sdr/TWAA9812511.md): Skin · damaged · Aug 3, 1998 · N998R · Doug DC932 · Fuselage Main, Plate/Skin
  > DURING OP 16 MAINT CHECK, FOUND EXTERNAL DOUBLER INSTALLED AT FS 495 TO 505, LONG 19 TO 20R. REPAIRED PER DC9 SRM 53-04, FIG 12B SHEET 6.
- [SDR TWAA9812510](https://openairdocs.org/sdr/TWAA9812510.md): Skin · damaged · Aug 3, 1998 · N998R · Doug DC932 · Fuselage Main, Plate/Skin
  > DURING OP 16 MAINT CHECK, FOUND EXTERNAL DOUBLER INSTALLED AT FS 800, LONG 16R. INSTALLED CLASS I REPAIR DOUBLER PER SRM 53-04, FIG 12B.
- [SDR TWAA9812509](https://openairdocs.org/sdr/TWAA9812509.md): Skin · dented · Aug 3, 1998 · N998R · Doug DC932 · Fuselage Main, Plate/Skin
  > DURING OP 16 MAINT CHECK, FOUND DENT IN FUSELAGE AT FS 871, BETWEEN LONG 29 AND 30 RT, 4 IN BY 6 IN BY.125 IN. REPAIRED PER SRM 53-04, FIG 12B, PAGE 25.
- [SDR TWAA9812508](https://openairdocs.org/sdr/TWAA9812508.md): Longeron · corroded · Aug 3, 1998 · N998R · Doug DC932 · Fuselage Main, Longeron/Stringer
  > DURING OP 16 MAINT CHECK, FOUND CORROSION ON TOP OF LONG 30 AT FS 950. REPLACED LONGERON FROM FS 931 TO 955, PER 51-01, PAGE 4. SEALED PER SRM 51-20-0.
- [SDR TWAA9812505](https://openairdocs.org/sdr/TWAA9812505.md): Doubler · cracked · Aug 3, 1998 · N998R · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINT CHECK, FOUND EXTERNAL DOUBLER INSTALLED AT FS 996, LONGERON 28 AND 29R. REPAIRED CRACK AS REQUIRED PER SRM 53-04, FIG 12B, AND ARA 15299.
- [SDR TWAA9812512](https://openairdocs.org/sdr/TWAA9812512.md): Intercostal · cracked · Jul 28, 1998 · N998R · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINT CHECK, FOUND INTERCOSTAL CRACKED 3 INCHES FWD OF STA 294, AT ZERO BL. FABRICATED NEW INTERCOSTAL FROM 2024-0 ALUM MATERIAL HEAT TREATED TO 2024T3 PER REMOVED INTERCOSTAL. INSTALLED IN ACFT USING HI-LOKS AND MS20470AD RIVETS, PER DOUGLAS PR
- [SDR TWAA9812206](https://openairdocs.org/sdr/TWAA9812206.md): Longeron · cracked · Jul 22, 1998 · N998R · Doug DC932 · Fuselage Main, Longeron/Stringer
  > DURING OP 16 MAINT CHECK, FOUND LONGERON 17L CRACKED AT STA 965, AFT SIDE OF BULKHEAD. REPLACED CRACKED LONGERON SECTION AND SPLICED PER SRM 53-02, FIG 18.
- [SDR TWAA9812203](https://openairdocs.org/sdr/TWAA9812203.md): Longeron · cracked · Jul 22, 1998 · N998R · Doug DC932 · Fuselage Main, Longeron/Stringer
  > DURING OP 16 MAINT CHECK, FOUND LONGERON 16L CRACKED AT STA 965, AFT SIDE OF BULKHEAD. REPLACED CRACKED LONGERON SECTION AND SPLICED PER SRM 53-02, FIG 18.
- [SDR TWAA9812126](https://openairdocs.org/sdr/TWAA9812126.md): Skin · dented · Jul 20, 1998 · N998R · Doug DC932 · Leading Edge Devices
  > DURING OP 16 MAINT CHECK, FOUND DENT ON NR 1 L/E SLAT, LT WING, EXCEEDING ALLOWABLE LIMITS PER SRM 57-03, PG 20A. DENT IS 2.5 BY 17 IN BY.150 DEEP. CUT OUT DAMAGED SKIN AND INSTALLED REPAIR PER SRM 57-09, FIG 10F.
- [SDR TWAA9812009](https://openairdocs.org/sdr/TWAA9812009.md): Skin · worn · Jul 17, 1998 · N998R · Doug DC932 · Fuselage Main, Plate/Skin
  > DURING OP 16 MAINT CHECK, FOUND FUSELAGE SKIN WORN AT LONGERON 26L, STA 815, UNDER FUSELAGE FAIRING. TRIMMED DAMAGED AREA WHICH IS FOR A LAP SEAM. INSTALLED REPAIR PER SRM 53-04 FIG 12B.
- [SDR TWAA9812008](https://openairdocs.org/sdr/TWAA9812008.md): Intercostal · cracked · Jul 17, 1998 · N998R · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINT CHECK, FOUND INTERCOASTAL CRACKED AT AFT END OF PULLEY CLUSTER AT STA 1010, RBL 20 INCHES. NEW SUPPORT FABRICATED IN SHOP PER DRAWING 9915540, DRILLED NEW PART AND INSTALLED AND SEALED PER SRM 53-03.
- [SDR TWAA9812007](https://openairdocs.org/sdr/TWAA9812007.md): Frame · cracked · Jul 17, 1998 · N998R · Doug DC932 · Fuselage Main, Frame
  > DURING OP 16 MAINT CHECK, FOUND FRAME WITH APPROX 1 IN CRACK AT STA 980, LONGERON 17R. ACCOMPLISHED FRAME REPAIR BY CUTTING DAMAGED SECTION OUT BETWEEN L14R AND L16R, AND FLOOR LINE. INSTALLED NEW SECTIONS OF FRAME AND SPLICED PER SRM 53-03, FIG 32, SHEETS 1
- [SDR TWAA9812006](https://openairdocs.org/sdr/TWAA9812006.md): Skin · damaged · Jul 17, 1998 · N998R · Doug DC932 · Horizontal Stabilizer, Plate/Skin
  > DURING OP 16 MAINT CHECK, FOUND LT HORIZ STAB, LEADING EDGE OF STAB DAMAGED AND FILLET DETERIORATED APPROX 20 IN FROM O/B END. INSTALLED DOUBLER PER SRM 55-03, FIG 3 PG 5.
- [SDR TWAA9811506](https://openairdocs.org/sdr/TWAA9811506.md): Bulkhead · cracked · Jul 16, 1998 · N998R · Doug DC932 · Fuselage Main, Bulkhead
  > DURING OP 16 MAINTENANCE CHECK AT STA 965, THE BULKHEAD WEB HAD 2 EACH CRACKS APPROX 2 INCHES LONG AT WL 200, JUST INBD OF LONGERON 18R. REPLACED FULL BULKHEAD WEB WITH SAME AS ORIGINAL.032 INCH 7075T6 ALUMINUM MATERIAL. ATTACHED WITH MS L0470AD RIVETS AND
- [SDR TWAA9811504](https://openairdocs.org/sdr/TWAA9811504.md): Skin · defective · Jul 15, 1998 · N998R · Doug DC932 · Fuselage Main, Plate/Skin
  > DURING OP 16 MAINTENANCE CHECK, FOUND FUSELAGE UPPER AND LOWER SKIN THICKNESS MEASURED BY NDT WAS.024 INCH. SKIN THICKNESS IS.063 INCH AT STA 815, L26R. REPAIRED SKIN PER SRM 53-04, FIG 12B, PAGE 45. ACFT TT: 77,783 HOURS. ACFT TC: 84,471. (X)
- [SDR TWAA9811505](https://openairdocs.org/sdr/TWAA9811505.md): Longeron · cracked · Jul 13, 1998 · N998R · Doug DC932 · Fuselage Main, Longeron/Stringer
  > DUIRNG OP 16 MAINTENANCE CHECK, FOUND LONGERON 17R AT STA 980 WITH.50 INCH CRACK AT ATTACH HOLE TO FORMER. REPLACED SECTION OF LONGERON FROM STA 956 TO STA 996. INSTALLED LONGERON REPAIR SPLICE PER SRM 53-02, FIGURE 18. CFT TT: 77,783 HOURS. ACFT TC: 84,
- [SDR TWAA9811503](https://openairdocs.org/sdr/TWAA9811503.md): Angle · corroded · Jul 9, 1998 · N998R · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINTENANCE CHECK, FOUND FLOOR ANGLE WITH EXFOLIATION AT FS 914, S29R. REMOVED EXFOLIATED SECTION OF ANGLE AND REPAIRED AREA PER SRM 53-01, FIG 2 SHEET 4. AFT TT: 77,783 HOURS. ACFT TC: 84,471. (X)
- [SDR TWAA9811005](https://openairdocs.org/sdr/TWAA9811005.md): Skin · damaged · Jul 7, 1998 · N998R · Doug DC932 · Wing, Plate/Skin
  > MCI - DURING OP 16 MAINTENANCE CHECK, FOUND RT WING LE WING SKIN WITH HOLE WORN THROUGH SKIN INBD OF NR 1 SLAT TRACK, L.E. OF WING TO END OF WING TO NR 3 SLAT TRACK HAD WORN SKIN. BLENDED WEAR AREA OTBD OF CENTER TRACK CUT-OUT PER SRM 57-01 PAGE 5, FIG 1. IN
- [SDR TWAA9810805](https://openairdocs.org/sdr/TWAA9810805.md): Web · cracked · Jul 2, 1998 · N998R · Doug DC932 · Fuselage Miscellaneous Structure
  > MCI- DURING OP 16 MAINTENANCE CHECK, FOUND FLOOR MEMBRANE CRACKED AT FS 744, RBL 50. REPLACED MEMBRANE WITH NEW PART PER SRM 51-01 PAGE 04. ACFT TT: 77,783 HOURS. ACFT TC: 84,471. (X)
- [SDR TWAA9810711](https://openairdocs.org/sdr/TWAA9810711.md): Rib · cracked · Jul 1, 1998 · N998R · Doug DC932 · Elevator, Spar/Rib
  > MCI - DURING OP 16 MAINTENANCE CHECK, FOUND LOWER SURFACE AT DAMPER CUT OUT LOWER RIB CAP CRACKED ON LT ELEVATOR. REPLACED LOWER RIB CAP PER DAC DWG 9918535. ACFT TT: 77,783 HOURS. ACFT TC: 84,471. (X)
- [SDR TWAA9810808](https://openairdocs.org/sdr/TWAA9810808.md): Spar Cap · cracked · Jun 29, 1998 · N998R · Doug DC932 · Wing Spar
  > MCI - DURING OP 16 MAINTENANCE CHECK, FOUND ON RT WING UPPER REAR SPAR CAP, AN 'EYE BROW' CRACK ABOVE BOTH THE INBD AND OTBD STUD HOLES. CRACK LENGTH WAS 0.75 INCH ABOVE THE INBD HOLE AND 0.5 INCH ABOVE THE OTBD HOLE. INSTALLED DOUBLER PER ARA 15291 AND BLUE
- [SDR TWAA9810714](https://openairdocs.org/sdr/TWAA9810714.md): Splice · cracked · Jun 29, 1998 · N998R · Doug DC932 · Wing Miscellaneous Structure
  > MCI - DURING OP 16 MAINTENANCE CHECK, FOUND ON LT WING 10 INCHES OTBD OF INBD END OF NR 3 SLAT, LE OF WING SPLICE PLATE, CRACKED. REMOVED CRACKED SPLICE PLATE AND INSTALLED NEW PART, DRILLED IN, INSTALLED AD RIVETS AND TENSION HI LOCKS PER SRM 51-30-0 PG 1.
- [SDR TWAA9810713](https://openairdocs.org/sdr/TWAA9810713.md): Tie · cracked · Jun 29, 1998 · N998R · Doug DC932 · Fuselage Miscellaneous Structure
  > MCI - DURING OP 16 MAINTENANCE CHECK, FOUND CRACKED STRINGER TIE AT FS 585, AND STR 26R. REMOVED FORMER RING AT STA 579 FROM S25L TO S25R TO GAIN ACCESS TO STRINGER TIE. REPLACED CRACKED STRINGER TIE PER SRM 51-30. (X)
- [SDR TWAA9810710](https://openairdocs.org/sdr/TWAA9810710.md): Skin · corroded · Jun 29, 1998 · N998R · Doug DC932 · Fuselage Main, Plate/Skin
  > MCI - DURING OP 16 MAINTENANCE CHECK, FOUND CORROSION ROUND INTERIM REPAIR AT THE RADIO ALT ANTENNA AT FS 510, L30. REMOVED PREVIOUS REPAIR. INSTALLED REPAIR DOUBLER AND FINGER DOUBLER PER DWG SRO 9530107 AND SRM 53-04, FIG 44. (M)
- [SDR TWAA9810709](https://openairdocs.org/sdr/TWAA9810709.md): Longeron · cracked · Jun 29, 1998 · N998R · Doug DC932 · Fuselage Main, Longeron/Stringer
  > MCI - DURING OP 16 MAINTENANCE CHECK, A DYE CHECK SHOWED A ONE INCH CRACK IN LOWER FLANGE OF LONGERON 13R, AT FASTENER AT STA 965 FORMER FRAME. REMOVED CRACKED SECTION OF LONGERON 13R. INSTALLED NEW SECTION OF LONGERON AND INCORPORATED LONGERON SPLICE REPAI
- [SDR TWAA9810715](https://openairdocs.org/sdr/TWAA9810715.md): Seat Track · corroded · Jun 25, 1998 · N998R · Doug DC932 · Fuselage, Seat/Cargo Attach Fittings
  > MCI - DURING OP 16 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR TRACK NR 3, FS 937 TO FS 946. REMOVED OLD TRACK FROM STA 929 TO STA 965. INSTALLED NEW TRACK PER SRM 53-05-10C, AND SRM 51-01 PAGE 1 ITEM C. ACFT TT: 77,783 HOURS. ACFT TC: 84,471. (X)
- [SDR TWAA9810615](https://openairdocs.org/sdr/TWAA9810615.md): Web · cracked · Jun 25, 1998 · N998R · Doug DC932 · Fuselage Miscellaneous Structure
  > MCI - DURING OP 16 MAINTENANCE CHECK, FOUND A.50 INCH CRACK IN MEMBRANE AT LONGERON 18L, STA 234. REMOVED MEMBRANE AT L18L, FS 218 TO FS 237 PER DAC SRM 51-61 PAGE 1. FABRICATED COMPLETE PART FROM SAME MATERIAL PER DAC SRM 53-10-2, FIG 4 SHEETS 1 AND 2, ITE
- [SDR TWAA9810614](https://openairdocs.org/sdr/TWAA9810614.md): Longeron · cracked · Jun 25, 1998 · N998R · Doug DC932 · Fuselage Main, Longeron/Stringer
  > MCI - DURING OP 16 MAINTENANCE CHECK, ON LOWER FUSELAGE, FOUND LONGERON 25L WITH CRACK AT FASTENER AT STA 256 FORMER FRAME. INSTALLED NEW LONGERON SECTION AND TWO LONGERON REPAIR SPLICES PER SRM 53-02, FIG 18. ACFT TT: 77,783 HOURS. ACFT TC: 84,471. (X)
- [SDR TWAA9810716](https://openairdocs.org/sdr/TWAA9810716.md): Support · cracked · Jun 24, 1998 · N998R · Doug DC932 · Fuselage Miscellaneous Structure
  > MCI - DURING OP 16 MAINTENANCE CHECK, FOUND FLOOR PANEL SUPPORT HAT SECTION WITH APPROXIMATELY 1.5 INCH CRACK AT STA 237, RBL 2 INCHES. REPAIRED PER SRM 51-01, PAGE 1, ITEM C, TWA STD PRACTICES, AND SRM 51-30-2, SRM 51-01 PAGE 4 FIG 1. ACFT TT: 77,783 HOURS
- [SDR TWAA9810610](https://openairdocs.org/sdr/TWAA9810610.md): Rib · cracked · Jun 24, 1998 · N998R · Doug DC932 · Wing, Rib/Bulkhead
  > MCI - DURING OP 16 MAINTENANCE CHECK, FOUND A CRACK IN AFT FASTENER RIB, 18 IN OUTBOARD OF NR 5 SLAT CENTER TRACK RIB IN LE OF LEFT WING. REPLACED RIB PER SRM 51-01, PAGE 1 ITEM C. REPLACED HI-LOKS PER SRM 51-30-5. REPLACED RIVETS PER SRM 51-30-5. (M)
- [SDR TWAA9810717](https://openairdocs.org/sdr/TWAA9810717.md): Longeron · cracked · Jun 23, 1998 · N998R · Doug DC932 · Fuselage Main, Longeron/Stringer
  > MCI - DURING OP 16 MAINTENANCE CHECK, FOUND IN CABIN DYE CHECK SHOWING 2 EACH CACKS IN LOWER FLANGE OF LONGERON 16R, AT STA 965 FORMER FRAME. REMOVED CRACKED SECTION OF L16R AND FITTED AND INSTALLED NEW SECTION OF LONGERON PER SRM 53-02, FIG 18. ACFT T: 77,
- [SDR TWAA9810605](https://openairdocs.org/sdr/TWAA9810605.md): Floorbeam · corroded · Jun 17, 1998 · N998R · Doug DC932 · Fuselage Main, Floor Beam
  > MCI - DURING OP 16 MAINTENANCE CHECK, FOUND SURFACE CORROSION TOP SIDE OF FLOORBEAM, STATION 996 RBL 22 IN TO RBL 50 INCH. REPLACED ANGLE PER SRM 51-01 AND STD PRACTICES. (M)
- [SDR TWAA9810604](https://openairdocs.org/sdr/TWAA9810604.md): Bulkhead · cracked · Jun 17, 1998 · N998R · Doug DC932 · Fuselage Main, Bulkhead
  > MCI - DURING OP 16 MAINTENANCE CHECK, FOUND TIE ANGLE FOR FLOORBEAM, FORMER RING AND PRESSURE BULKHEAD CRACKED AT STATION 996, RBL 58.6 INCHES. VERIFIED BY NDT. REPLACED TIE PALTE PER SRM 51-01 AND STD PRACTICES. (M)
- [SDR TWAA9809810](https://openairdocs.org/sdr/TWAA9809810.md): Frame · bent · Jun 16, 1998 · N998R · Doug DC932 · Fuselage Main, Frame
  > MCI - DURING OP 16 MAINTENANCE CHECK FOUND STA 544 FORMER RING FOOT BENT BEYOND LIMITS, BETWEEN LONGERONS 28R AND 29R. REPLACED FORMER FOOT PER SRM 53-03, FIG 3 AND SRM 53-04, FIG 38. TOTAL TIME: 72,210 HOURS. TOTAL CYCLES: 84,221. (X)
- [SDR TWAA9809809](https://openairdocs.org/sdr/TWAA9809809.md): Seat Track · corroded · Jun 16, 1998 · N998R · Doug DC932 · Fuselage, Seat/Cargo Attach Fittings
  > MCI - DURING OP 16 MAINTENANCE CHECK, FOUND CORROSION BLENDED BEYOND LIMITS AT STA 200, RBL 22, FLOOR TRACK. REPLACED CORRODED TRACK SECTION PER SRM 51-01, PG 1 ITEM C. STA 200 TO STA 265. TOTAL TIME: 77,783. TOTAL CYCLES: 84,471. (X)
- [SDR TWAA9809705](https://openairdocs.org/sdr/TWAA9809705.md): Tie · corroded · Jun 12, 1998 · N998R · Doug DC932 · Fuselage Miscellaneous Structure
  > MCI - DURING OP 16 MAINTENANCE CHECK, FOUND STR 30 CORRODED AT TIE CLIP, FS 167. REMOVED CORROSION IN STRINGER PER SRM 51-10-3, PARA 35, PAGE 21. REMOVED STRINGER TIE, DRILLED, DEBURRED, AND INSTALLED NEW TIE PER SRM 51-01, PAGE 1, ITEM C AND SRM 51-30-2, PA
- [SDR TWAA9809704](https://openairdocs.org/sdr/TWAA9809704.md): Longeron · cracked · Jun 12, 1998 · N998R · Doug DC932 · Fuselage Main, Longeron/Stringer
  > MCI - DURING OP 16 MAINTENANCE CHECK, FOUND 2 EACH CRACKS AT STA 200, LONGERON 4L. REMOVED AND REPLACED 4L LONGERON FROM STA 128 TO STA 229. INSTALLED LONGERON REPAIR SPLICE AT STA 190, L4L, PER SRM 53-02, FIG 18. TOTAL TIME: 77,783 HOURS. TOTAL CYCLES: 8

Next page: https://openairdocs.org/deregistered/N998R-2011-03-15/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 = 'N998R' AND deregistration_id = 'N998R-2011-03-15'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N998R-2011-03-15/reports

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