# Service difficulty reports: N929L, cancelled Aug 22, 2013

A list on [N929L, cancelled Aug 22, 2013](https://openairdocs.org/deregistered/N929L-2013-08-22.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 TWAA0016004](https://openairdocs.org/sdr/TWAA0016004.md): Skin · corroded · Oct 11, 2000 · N929L · Doug DC932 · Fuselage Main, Plate/Skin
  > DURING CHECK-C MAINT, FOUND SKIN BULGING AND SIGNS OF CORROSION FROM LONGERON 26R TO 26L, STA 996. REPAIRED SKIN PER SRM 53-03, FIG 9.
- [SDR TWAA0015712](https://openairdocs.org/sdr/TWAA0015712.md): Bulkhead · cracked · Oct 3, 2000 · N929L · Doug DC932 · Fuselage Main, Bulkhead
  > DURING CHECK-C MAINT AN EDDY CURRENT CHECK OF THE BULKHEAD T-CAP SHOWED A CRACK APPROXIMATELY 1 INCH LONG IN RADIUS AT LONGERON 28L. INSTALLED NEW T-CAP PER SRM 53-03 FIG 37A AND BOEING DRAWING SERIES 5911425.
- [SDR TWAA0015711](https://openairdocs.org/sdr/TWAA0015711.md): Bulkhead · corroded · Oct 3, 2000 · N929L · Doug DC932 · Fuselage Main, Bulkhead
  > DURING CHECK-C MAINT, THE AFT PRESSURE BULKHEAD SKIN WAS CORRODED ALONG THE BOTTOM EDGE AT ''T'' CAP, STA 996 FROM LONGERON 27L TO 28R, 23 INCHES LONG BY 2.25 IN HIGH. REPAIRED PRESSURE BULKHEAD SKIN PER SRM 53-05 FIG 9.
- [SDR TWAA0012107](https://openairdocs.org/sdr/TWAA0012107.md): Longeron · cracked · Jul 31, 2000 · N929L · Doug DC932 · Fuselage Main, Longeron/Stringer
  > FOUND A.5 INCH CRACK ON THE I/B FLANGE OF LONGERON 2R, STA 680. SPLICED LONGERON PER SRM 53-02, FIG 18. CHECK-C 7-20-99 STL.
- [SDR TWAA0012106](https://openairdocs.org/sdr/TWAA0012106.md): Longeron · cracked · Jul 31, 2000 · N929L · Doug DC932 · Fuselage Main, Longeron/Stringer
  > FOUND A.5 INCH CRACK IN I/B AND O/B FLANGE OF LONGERON 2R AT STA 756. SPLICED NEW LONGERON SECTION PER SRM 53-02, FIG 18. CHECK-C 7-20-99 STL.
- [SDR TWAA9914603](https://openairdocs.org/sdr/TWAA9914603.md): Fuel Pump · failed · Oct 27, 1999 · N929L · Doug DC932 · Engine Fuel Pump
  > ABORTED TAKEOFF ROLL, DUE TO RT ENG COMPRESSOR STALL. FOUND RT ENG FUEL PUMP OUT PUT SHAFT SHEARED. REPLACED FUEL PUMP ASSY. CC00 7-20-99 STL.
- [SDR TWAA9809303](https://openairdocs.org/sdr/TWAA9809303.md): Fitting · corroded · Apr 30, 1998 · N929L · Doug DC932 · Nacelle/Pylon Structure
  > MCI - DURING OP 16 MAINTENANCE CHECK, FOUND RT PYLON WITH CORROSION ON FRONT SPAR LOWER BEAVER TAIL FITTING. REMOVED CORROSION ON BEAVER TAIL FITTING PER SRM 54-04, FIG 13. ROTOPEENED REWORKED AREA PER SRM 54-04, FIG 13, AND PLATED PER SRM 54-04, PAGE 53, IT
- [SDR TWAA9806512](https://openairdocs.org/sdr/TWAA9806512.md): Spar · cracked · Apr 22, 1998 · N929L · Doug DC932 · Horizontal Stabilizer, Spar/Rib
  > MCI - DURING OP 16 MAINTENANCE CHECK, FOUND HORIZONTAL STABILIZER UPPER AFT LT BARREL NUT HOLE IN FRONT SPAR CRACKED BEYOND LIMITS. REPLACED FRONT SPAR PER SRM 51-01 AND ARA 15277. ACFT TT: 75,041 HOURS. ACFT TC: 81,086. (X)
- [SDR TWAA9806511](https://openairdocs.org/sdr/TWAA9806511.md): Spar Cap · rusty · Apr 22, 1998 · N929L · Doug DC932 · Horizontal Stabilizer, Spar/Rib
  > MCI - DURING OP 16 MAINTENANCE CHECK, FOUND HORIZONTAL STABILIZER UPPER AFT LT BARREL NUT IN FRONT SPAR FOR STABILIZER ATTACHMENT TO CENTER SECTION WAS VERY RUSTY AND EMITTING RUST FROM BOTTOM OF HOLE. INSTALLED NEW LT HORIZONTAL STABILIZER UPPER SPAR CAP. I
- [SDR TWAA9806510](https://openairdocs.org/sdr/TWAA9806510.md): Rib · cracked · Apr 22, 1998 · N929L · Doug DC932 · Wing, Rib/Bulkhead
  > MCI - DURING OP 16 MAINTENANCE CHECK, FOUND LT WING LE WITH CRACK AT AFT FASTENER IN WING LE RIB ABOVE LE LOWER PANEL 1113. REMOVED AND REPLACED WITH NEW RIB AND INSTALLED DOUBLER PER SRM 57-01, PG 8, AND SRM 51-01 PG 1 ITEM C. ACFT TT: 75,041 HOURS. ACFT T
- [SDR TWAA9806509](https://openairdocs.org/sdr/TWAA9806509.md): Rib · cracked · Apr 22, 1998 · N929L · Doug DC932 · Wing, Rib/Bulkhead
  > MCI - DURING OP 16 MAINTENANCE CHECK, FOUND LT WING LE WITH CRACK AT AFT LOWER FASTENER IN WING LE RIB ABOVE LOWER PANEL NR 1112. INSTALLED NEW RIB PER SRM 51-01. ACFT TT: 75,041 HOURS. ACFT TC: 81,086. (X)
- [SDR TWAA9806508](https://openairdocs.org/sdr/TWAA9806508.md): Rib · cracked · Apr 22, 1998 · N929L · Doug DC932 · Wing, Rib/Bulkhead
  > MCI - DURING OP 16 MAINTENANCE CHECK, FOUND LT WING LE WITH CRACK AT AFT LOWER FASTENER IN WING LE RIB ABOVE LE LOWER PANEL NR 1111. INSTALLED NEW RIB PER SRM 51-01, PG 1. ACFT TT: 75,041 HOURS. ACFT TC: 81,086. (X)
- [SDR TWAA9806616](https://openairdocs.org/sdr/TWAA9806616.md): Panel · torn · Apr 16, 1998 · N929L · Doug DC932 · Rudder, Plate/Skin
  > MCI - DURING OP 16 MAINTENANCE CHECK, FOUND TOP TE PANEL ON RUDDER SEPARATED AND TORN AT JOINT SEAMS. REPAIRED PER SRM 51-90-0. (M)
- [SDR TWAA9806601](https://openairdocs.org/sdr/TWAA9806601.md): Skin · cracked · Apr 16, 1998 · N929L · Doug DC932 · Wing, Plate/Skin
  > MCI - DURING OP 16 MAINTENANCE CHECK, FOUND RT WING LE WITH CRACK AT LOWER AFT FASTENER IN LE ABOVE LE PANEL NR 1211A. INSTALLED NEW RIB PER SRM 51-01 PAGE 1. (M)
- [SDR TWAA9806515](https://openairdocs.org/sdr/TWAA9806515.md): Rib · cracked · Apr 16, 1998 · N929L · Doug DC932 · Wing, Rib/Bulkhead
  > MCI - DURING OP 16 MAINTENANCE CHECK, FOUND CRACK AT TOP AFT FASTENER IN RT WING LE RIB ABOVE LE PANEL 1213A. REPLACED RIB PER SRM 51-01, PG 1 ITEM C. ACFT TT: 75,041 HOURS. ACFT TC: 81,086. (X)
- [SDR TWAA9806514](https://openairdocs.org/sdr/TWAA9806514.md): Floorbeam · corroded · Apr 16, 1998 · N929L · Doug DC932 · Fuselage Main, Floor Beam
  > MCI - DURING OP 16 MAINTENANCE CHECK, FOUND AT STA 937 TO STA 965, CABIN FLOORBEAM CAP WITH METAL REMOVED BEYOND LIMITS FOR CORROSION REMOVAL. INSTALLED NEW SECTION AT FLOOR SUPPORT PER SRM 53-05, P21, ITEM 6A, AND ARA 10993. ACFT TT: 75,041 HOURS. ACFT TC
- [SDR TWAA9806413](https://openairdocs.org/sdr/TWAA9806413.md): Rib · cracked · Apr 16, 1998 · N929L · Doug DC932 · Wing, Rib/Bulkhead
  > MCI - DURING OP 16 MAINTENANCE CHECK, FOUND CRACK AT TOP AFT FASTENER IN RT WING LE RIB ABOVE LE PANEL 1213A. REPLACED PART PER SRM 51-01, PG 1 ITEM C. ACFT TT: 75,041 HOURS. ACFT TC: 81,086.
- [SDR TWAA9806412](https://openairdocs.org/sdr/TWAA9806412.md): Barrel Nut · rusted · Apr 16, 1998 · N929L · Doug DC932 · Horizontal Stabilizer Structure
  > MCI - DURING OP 16 MAINTENANCE CHECK, FOUND HORIZONTAL STABILIZER UPPER AFT RT BARREL NUT IN FRONT SPAR FOR STABILIZER ATTACH TO CENTER SECTION WAS RUSTY AND EMITTING RUST FROM BOTTOM OF HOLE. REMOVED BOLT AND BARREL NUT AND CLEANED. REAMED AND BUSHED HOLE P
- [SDR TWAA9806410](https://openairdocs.org/sdr/TWAA9806410.md): Support · corroded · Apr 16, 1998 · N929L · Doug DC932 · Fuselage Miscellaneous Structure
  > MCI - DURING OP 16 MAINTENANCE CHECK, FOUND METAL REMOVED BEYOND LIMIT FOR CORROSION REMOVAL AT CABIN STA 937 TO STA 965, CENTER FLOOR CAP. INSTALLED NEW SECTION AT FLOOR SUPPORT PER SRM 53-05, P21, 6A, AND ARA 10993. ACFT TT: 75,041 HOURS. ACFT TC: 81,08
- [SDR TWAA9806409](https://openairdocs.org/sdr/TWAA9806409.md): Rib · cracked · Apr 16, 1998 · N929L · Doug DC932 · Wing, Rib/Bulkhead
  > MCI - DURING OP 16 MAINTENANCE CHECK, FOUND RT WING LE HAD CRACK AT LOWER AFT FASTENER IN LE RIB ABOVE LE PANEL NR 1211A. INSTALLED NEW RIB PER SRM 51-01, PAGE 1. ACFT TT: 75,041 HOURS. ACFT TC: 81,086. (X)
- [SDR TWAA9809304](https://openairdocs.org/sdr/TWAA9809304.md): Bulkhead · cracked · Apr 14, 1998 · N929L · Doug DC932 · Fuselage Main, Bulkhead
  > MCI - DURING OP 16 MAINTENANCE CHECK, FOUND 1104 CANTED BULKHEAD AT NR 3 LONGERON RT AND LT SIDE, WITH 2 EACH FASTENERS MISSING. HFEC AREA FOUND 2 INCH CRACK. REPAIRED PER SRM 53-05, PAGE 49. (X)
- [SDR TWAA9809301](https://openairdocs.org/sdr/TWAA9809301.md): Bulkhead Angle · cracked · Apr 14, 1998 · N929L · Doug DC932 · Nacelle/Pylon, Bulkhead/Firewall
  > MCI - DURING OP 16 MAINTENANCE CHECK, FOUND LT PYLON UPPER AFT BULKHEAD ANGLE CRACKED AT INBOARD AND OUTBOARD ENDS. MADE AND INSTALLED NEW ANGLE PER SRM 51-01, PAGE 1, ITEM C. (X)
- [SDR TWAA9807320](https://openairdocs.org/sdr/TWAA9807320.md): Fitting · flat spot · Apr 14, 1998 · N929L · Doug DC932 · Horizontal Stabilizer, Attach Fittings
  > MCI - DURING OP 16 MAINTENANCE CHECK, FOUND HORIZ STABILIZER LEFT PIVOT BEARING LUG, IN LT SIDE OF STAB CENTER SECTION RIB, WITH FLAT SPOT IN BEARING BORE AT APPROX 3 O'CLOCK POSITION,.017 IN DEEP AND LUG IS.010 IN THICKER AT TOP 12 O'CLOCK POSITION AT SPOT
- [SDR TWAA9807319](https://openairdocs.org/sdr/TWAA9807319.md): Bulkhead Casting · cracked · Apr 13, 1998 · N929L · Doug DC932 · Fuselage Main, Bulkhead
  > MCI - DURING OP 16 MAINTENANCE CHECK, FOUND CABIN FOOT CASTING AFT INBOARD SIDE OF 965 BULKHEAD, CRACKED. REMOVED AND REPLACED CASTING PER SRM 51-01 AND STANDARD PRACTICES. (M)
- [SDR TWAA9807312](https://openairdocs.org/sdr/TWAA9807312.md): Block · cracked · Apr 13, 1998 · N929L · Doug DC932 · Wing, Control Surface Attach Fittings
  > MCI - DURING OP 16 MAINTENANCE CHECK, FOUND RT WING TE FLAP INSIDE FLAP OUTBOARD FLAP HINGE TO FORWARD MOUNT BOLT, RT AND LT SIDE MOUNT WEBS CRACKED OUT FROM BOLT HOLES. REPLACED MOUNT BLOCK PER STANDARD PRACTICES AND SRM 51-01. (M)
- [SDR TWAA9807306](https://openairdocs.org/sdr/TWAA9807306.md): Horiz Stab · gouged · Apr 7, 1998 · N929L · Doug DC932 · Horizontal Stabilizer Structure
  > MCI - DURING OP16 MAINTENANCE CHECK, FOUND ON LT HORIZ STAB TOP AFT 2 BARREL NUT HOLES GOUGED. REAMED HOLES AND INSTALLED BUSHING AND REDRILLED.562 IN PER ARA 15267. (M)
- [SDR TWAA9809305](https://openairdocs.org/sdr/TWAA9809305.md): Fitting · corroded · Apr 3, 1998 · N929L · Doug DC932 · Nacelle/Pylon Structure
  > MCI - DURING OP 16 MAINTENANCE CHECK, FOUND CORROSION ON NR 1 PYLON FRONT SPAR LOWER BEAVER TAIL FITTING. REMOVED CORROSION ON BEAVER TAIL FITTING PER SRM 54-04, FIG 13. ROTOPEENED REWORKED AREA PER SRM 5-04, FIG 13 AND PLATED PER SRM 54-04, PAGE 53, ITEM 4.
- [SDR TWAA9809307](https://openairdocs.org/sdr/TWAA9809307.md): Skin · corroded · Mar 31, 1998 · N929L · Doug DC932 · Fuselage Main, Plate/Skin
  > MCI - DURING OP 16 MAINTENANCE CHECK, FOUND CLASS III REPAIR INSTALLED ABOVE AND JUST FORWARD OF EXTERNAL POWER RECEPTACLE. INSTALLED CLASS I REPAIR PER SRM 53-04, FIGURE 12 B. (X)
- [SDR TWAA9809302](https://openairdocs.org/sdr/TWAA9809302.md): Skin · dented · Mar 30, 1998 · N929L · Doug DC932 · Fuselage Main, Plate/Skin
  > MCI - DURING OP 16 MAINTENANCE CHECK, FOUND DENT IN FUSELAGE SKIN RT SIDE AFT OF AFT CARGO DOOR. FOUND INTERIM REPAIR INSTALLED. INSTALLED CLASS 1 REPAIR PER SRM 53-04, FIG 12B. (X)
- [SDR TWAA9809309](https://openairdocs.org/sdr/TWAA9809309.md): Spar · cracked · Mar 27, 1998 · N929L · Doug DC932 · Wing Spar
  > MCI - DURING OP 16 MAINTENANCE CHECK FOUND ON RT WING HOLE 43 INDICATING CRACK WITH HFEC, RT WING LOWER REAR SPAR STA XRS 154. REPAIRED PER SERVICE REWORK DRAWING J060173 AND TWA STD PRACTICES. (X)
- [SDR TWAA9809308](https://openairdocs.org/sdr/TWAA9809308.md): Spar · cracked · Mar 27, 1998 · N929L · Doug DC932 · Wing Spar
  > MCI - DURING OP 16 MAINTENANCE CHECK FOUND ON RT WING HOLE 71 INDICATING CRACKED, LOWER REAR SPAR RT XRS 200. REPAIRED PER SERVICE REWORK DRAWING J060173 AND TWA STD PRACTICES. (X)
- [SDR TWAA9809306](https://openairdocs.org/sdr/TWAA9809306.md): Frame · cracked · Mar 27, 1998 · N929L · Doug DC932 · Nacelle/Pylon, Frame/Spar/Rib
  > MCI - DURING OP 16 MAINTENANCE CHECK, FOUND NR 1 PYLON LOWER END CHORD ANGLE CRACKED, 60 INCHES AFT OF LEADING EDGE, 4 INCHES INBOARD AT OUTBOARD END. INSTALLED DOUBLER PER SRM 54-01, FIG 2, PAGE 7. (X)
- [SDR TWAA9807315](https://openairdocs.org/sdr/TWAA9807315.md): Floorbeam · corroded · Mar 27, 1998 · N929L · Doug DC932 · Fuselage Main, Floor Beam
  > MCI - DURING OP 16 MAINTENANCE CHECK, FOUND CORROSION BEYOND LIMIT ON FLOORBEAM CAP FROM STATION 196 TO 218 OBL. FABRICATED AND INSTALLED NEW BEAM CAP PER SRM 51-01 PAGE 1. (M)
- [SDR TWAA9807311](https://openairdocs.org/sdr/TWAA9807311.md): Pivot Arm · worn · Mar 27, 1998 · N929L · Doug DC932 · Trailing Edge Flaps
  > MCI - DURING OP16 MAINTENANCE CHECK, FOUND LT TE FLAP CENTER HINGE PIVOT BEARING OUTBOARD LUG WORN AND CORRODED INBEARING BORE. INBOARD BEARING BORE WORN OVERSIZE. INSTALLED NEW HINGE CASTING PER MM 27-50-1. (M)
- [SDR TWAA9807310](https://openairdocs.org/sdr/TWAA9807310.md): Pivot Arm · worn · Mar 27, 1998 · N929L · Doug DC932 · Trailing Edge Flaps
  > MCI - DURING OP 16 MAINTENANCE CHECK, FOUND RT WING FLAP CENTER HINGE PIVOT BEARING INBOARD AND OUTBOARD LUGS WITH WORN GROOVES AND PITTING CONDITION IN BEARING BORES. INSTALLED NEW CENTER HINGE PIVOT ARM PER MM 27-50-01. (M)
- [SDR TWAA9807305](https://openairdocs.org/sdr/TWAA9807305.md): Spar · cracked · Mar 27, 1998 · N929L · Doug DC932 · Wing Spar
  > MCI - DURING OP16 MAINTENANCE CHECK, FOUND HOLE 104 INDICATING CRACK RT WING LOWER SPAR STATION XRS 268. REPAIRED PER SERVICE REWORK DRAWING J060173 AND TWA STD PRACTICES. (M)
- [SDR TWAA9806502](https://openairdocs.org/sdr/TWAA9806502.md): Seat Track · corroded · Mar 25, 1998 · N929L · Doug DC932 · Fuselage, Seat/Cargo Attach Fittings
  > MCI - DURING OP 16 MAINTENANCE CHECK FOUND CORROSION BEYOND LIMITS IN CHAIR TRACK AT STA 570 TO STA 617, LBL 45 IN. REMOVED AND REPLACED SEAT TRACK AT STA 570 TO STA 617, LBL 45 IN, PER SRM 53-05, PG 10G. ACFT TT: 75,041 HOURS. ACFT TC: 81,086. (X)
- [SDR TWAA9809310](https://openairdocs.org/sdr/TWAA9809310.md): Frame · cracked · Mar 23, 1998 · N929L · Doug DC932 · Fuselage Main, Frame
  > MCI - DURING OP 16 MAINTENANCE CHECK, FOUND FUSELAGE FRAME STA 89 WITH CRACK IN OUTBOARD RADIUS BETWEEN LONGERONS 18 AND 19. STOP DRILLED CRACK PER SRM 51-10 AND REPAIRED PER SRM 53-01, PAGE 10, FIGURE 2. (X)
- [SDR TWAA9807318](https://openairdocs.org/sdr/TWAA9807318.md): Spar Cap · cracked · Mar 23, 1998 · N929L · Doug DC932 · Wing Spar
  > MCI - DURING OP 16 MAINTENANCE CEHCK, FOUND RT WING TE UPPER REAR SPAR CAP CRACKED AT INBOARD FLAP HINGE UPPER ATTACH HOLES. STOP DRILLED CRACK, REPAIRED PER DAC DWG J060271 AND STD PRACTICES. (M)
- [SDR TWAA9807317](https://openairdocs.org/sdr/TWAA9807317.md): Longeron · broken · Mar 23, 1998 · N929L · Doug DC932 · Fuselage Main, Longeron/Stringer
  > MCI - DURING OP 16 MAINTENANCE CHECK, FOUND LONGERON 4L BROKEN JUST FORWARD OF FORMER 160. REPAIRED PER SRM 53-02, FIG 18 PAGE 48. (M)
- [SDR TWAA9807316](https://openairdocs.org/sdr/TWAA9807316.md): Longeron · cracked · Mar 23, 1998 · N929L · Doug DC932 · Fuselage Main, Longeron/Stringer
  > MCI - DURING OP 16 MAINTENANCE CHECK, FOUND LONGERON 4L CRACKED AT STATION 200. REPAIRED PER SRM 53-02, FIG 18 PAGE 48. (M)
- [SDR TWAA9807309](https://openairdocs.org/sdr/TWAA9807309.md): Floorbeam · corroded · Mar 23, 1998 · N929L · Doug DC932 · Fuselage Main, Floor Beam
  > MCI - DURING OP 16 MAINTENANCE CHECK, FOUND SURFACE CORROSION ON FLOORBEAM CAP AT FS 160 FROM OL-288. REPLACED FLOORBEAM CAP PER SRM 51-01, PAGE 1 ITEM 1C. SEALED PER SRM 91-20-0. (M)
- [SDR TWAA9809108](https://openairdocs.org/sdr/TWAA9809108.md): Floorbeam · corroded · Mar 17, 1998 · N929L · Doug DC932 · Fuselage Main, Floor Beam
  > MCI - DURING OP 16 MAINTENANCE CHECK, FOUND FLOORBEAM CAP AT FS 160 TO 196, RBL 44, CORRODED BEYOND LIMITS. INSTALLED NEW FLOORBEAM PER SRM 51-01, PAGE 1 ITEM C. (M)
- [SDR TWAA9809106](https://openairdocs.org/sdr/TWAA9809106.md): Angle · cracked · Mar 17, 1998 · N929L · Doug DC932 · Fuselage Miscellaneous Structure
  > MCI - DURING OP 16 MAINTENANCE CHECK, FOUND CRACK IN FORWARD FUSELAGE INTERCOSTAL TO FS 69.55 FORMER ATTACH 'T' ANGLE AT LBL 13 INCH. REPLACED 'T' ANGLE PER SRM 51-01, PAGE 1 ITEM C. (M)
- [SDR TWAA9809104](https://openairdocs.org/sdr/TWAA9809104.md): Skin · dented · Mar 17, 1998 · N929L · Doug DC932 · Fuselage Main, Plate/Skin
  > MCI - DURING OP 16 MAINTENANCE CHECK,F OUND DENT ON LEFT SIDE BELOW AFT CORNER OF EXTERNAL POWER RECEPTACLE, 1 INCH BY 1 INCH BY.045 INCH DEEP. INSTALLED DOUBLER REPAIR PER SRM 53-01, PAGE 18. (M)
- [SDR TWAA9809103](https://openairdocs.org/sdr/TWAA9809103.md): Skin · dented · Mar 17, 1998 · N929L · Doug DC932 · Fuselage Main, Plate/Skin
  > MCI - DURING OP 16 MAINTENANCE CHECK, FOUND DENT IN LEFT SIDE BELOW FORWARD CORNER OF EXTERNAL POWER RECEPTACLE, 1 INCH BY 1.25 INCH BY.055. INSTALLED DOUBLER REPAIR PER SRM 53-01, PAGE 18. (M)
- [SDR TWAA9807314](https://openairdocs.org/sdr/TWAA9807314.md): Floorbeam · worn · Mar 12, 1998 · N929L · Doug DC932 · Fuselage Main, Floor Beam
  > MCI - DURING OP 16 MAINTENANCE CHECK, FOUND CABIN FLOORBEAM WITH WEAR AREA AT STATION 237, LBL 4 INCHES. REPAIRED FLOORBEAM PER SRM 53-05 FIG 30. (M)
- [SDR TWAA9807313](https://openairdocs.org/sdr/TWAA9807313.md): Angle · cracked · Mar 12, 1998 · N929L · Doug DC932 · Fuselage Miscellaneous Structure
  > MCI - DURING OP 16 MAINTENANCE CHECK, FOUND BELOW RT AFT LAVATORY FLOOR, ANGLE AT STATION 996 BELOW LONGERON 18R, AT CUST LINE, CRACKED. REPLACED ANGLE PER SRM 51-01, PAGE 1 ITEM C. (M)
- [SDR TWAA9807308](https://openairdocs.org/sdr/TWAA9807308.md): Skin · damaged · Mar 7, 1998 · N929L · Doug DC932 · Fuselage Main, Plate/Skin
  > MCI - DURING OP 16 MAINTENANCE CHECK, FOUND UNFILLED HOLES IN FUSELAGE SKIN AT STATION 965, BELOW LONGERON 14R. REPAIRED PER ARA 15017A. (M)
- [SDR TWAA9807307](https://openairdocs.org/sdr/TWAA9807307.md): Spar · cracked · Mar 7, 1998 · N929L · Doug DC932 · Wing Spar
  > MCI - DURING OP16 MAINTENANCE CHECK, FOUND HOLE 44 INDICATING CRACK IN RT WING LOWER REAR SPAR STATION XSR 155. REWORKED PER SERVICE REWORK DRAWING JO60173 AND TWS STD PRACTICES. (M)

Next page: https://openairdocs.org/deregistered/N929L-2013-08-22/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 = 'N929L' AND deregistration_id = 'N929L-2013-08-22'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N929L-2013-08-22/reports

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