# Service difficulty reports: N893AA, cancelled Jun 30, 2017

A list on [N893AA, cancelled Jun 30, 2017](https://openairdocs.org/deregistered/N893AA-2017-06-30.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 · 87 reports

- [SDR AALA20010687](https://openairdocs.org/sdr/AALA20010687.md): Stringer · corroded · Apr 2, 2001 · N893AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > TUL - FOUND CORROSION 1 INCH BY 20 INCHES ON STRINGER AND SPLICE STRINGER 27R STATION 1010 TO 1014. INSTALLED REPAIR OF.063 17-7PH CRES, ANGLES AS PER ESO 11697 DATED 3-30-01. (M)
- [SDR AALA20010686](https://openairdocs.org/sdr/AALA20010686.md): Stringer · corroded · Apr 2, 2001 · N893AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > TUL - FOUND STRINGER 29L CORRODED OUTBOARD SIDE STATION 1006 TO STATION 1010. INSTALLED NEW STRINGER SPLICE AND STRINGER CLIP PER SRM 53-10-3 AND STRINGER 29L OUTBOARD SIDE STATION 1006-1010. (M)
- [SDR AALA20010689](https://openairdocs.org/sdr/AALA20010689.md): Skin · cracked · Apr 1, 2001 · N893AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL - FOUND HFEC CRACK AT LOWER AFT CORNER OF DOOR CUTOUT FROM FASTENER TOWARD CUTOUT RADIUS, FS 417-419. CRACK INDICATION IN SKIN. REPAIRED PER BOEING S/B 727-53-188 LISTED ON PATTERN CARD NR 5708 PAGE NR 1. (M)
- [SDR AALA20010688](https://openairdocs.org/sdr/AALA20010688.md): Skin · corroded · Mar 29, 2001 · N893AA · Boeing 727223 · Wing, Plate/Skin
  > TUL - FOUND CORROSION ON LOWER SURFACE OF CENTER WING SKIN RBL 30 BETWEEN S4C AND S5C CORROSION WAS REMOVED BY BLENDOUT AND A REPAIR WAS ACCOMPLISHED WITH DEVIATIONS PER ESO 11697 DATED 2/29/00. REMOVED DOUBLER PER ESO 11697 DATED 2/20/00 AND INSTALLED DOUBLE
- [SDR AALA20010521](https://openairdocs.org/sdr/AALA20010521.md): Socket · inoperative · Mar 16, 2001 · N893AA · Boeing 727223 · Emergency Lighting
  > DFW - DURING OVERNIGHT MAINTENANCE, LEFT SIDE OVERWING EMERGENCY LIGHT DIM. RE-SECURED LEFT SIDE OVERWING EMERGENCY EXIT LIGHT SOCKET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA20010523](https://openairdocs.org/sdr/AALA20010523.md): Lamp · inoperative · Mar 16, 2001 · N893AA · Boeing 727223 · Emergency Lighting
  > DFW - DURING OVERNIGHT MAINTENANCE, RIGHT SIDE OVERWING EMERGENCY LIGHT DIM. RE-SECURED RIGHT SIDE OVERWING EMERGENCY EXIT LIGHT SOCKET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA20010021](https://openairdocs.org/sdr/AALA20010021.md): Pump · leaking · Jan 4, 2001 · N893AA · Boeing 727223 · Engine Fuel Pump
  > MIA - FLT 9212 - EN ROUTE MIA-ABQ - DETECTED NR 1 ENGINE SHUT DOWN. RETURNED MIA AND LANDED WITHOUT FURTHER INCIDENT. REPLACED NR 1 SIDE FUEL PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA20001365](https://openairdocs.org/sdr/AALA20001365.md): Light Strip · defective · Aug 23, 2000 · N893AA · Boeing 727223 · Emergency Lighting
  > MIA DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT ESCAPE PATH LIGHT UNDER EXIT PLACARD AT SEAT 3E INOPERATIVE. REPLACED LIGHT STRIP. SYSTEM GROUND CHECK NORMAL OPERATION.
- [SDR AALA2000433](https://openairdocs.org/sdr/AALA2000433.md): Skin · dented · Feb 24, 2000 · N893AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL - FOUND SKIN DENTED STATION 420, BETWEEN STRINGER 17L AND 18L ADL NR 8930035. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-30-3 FIG 3. (M)
- [SDR AALA2000432](https://openairdocs.org/sdr/AALA2000432.md): Structure · cracked · Feb 24, 2000 · N893AA · Boeing 727223 · Fuselage Main, Structure
  > TUL - FOUND CRACK EMANATING FROM FASTENER IN W/W STATION 870 BELOW LOAD CONTROL VALVE. REMOVED AND REPLACED CRACKED VERTICAL STIFFENER AS PER ESO 11697 DATED 2/23/2000. (M)
- [SDR AALA991707](https://openairdocs.org/sdr/AALA991707.md): Light · inoperative · Nov 13, 1999 · N893AA · Boeing 727223 · Emergency Lighting
  > DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT STRIP CLOSE TO FORWARD GALLEY INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
- [SDR AALA990746](https://openairdocs.org/sdr/AALA990746.md): Stringer · damaged · May 19, 1999 · N893AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > TUL - FOUND STRINGER IN LEFT GOUGED AND FASTENER HOLE ELONGATED JUST FORWARD OF BS 1243. REMOVED DAMAGE ON NR 14 STRINGER LEFT PER SRM 53-10-03. INSTALLED STRINGER REPAIR PER SRM 53-10-3 PAGE 4C-4E FIG 1. (M)
- [SDR AALA990369](https://openairdocs.org/sdr/AALA990369.md): Frame · dented · Mar 11, 1999 · N893AA · Boeing 727223 · Fuselage Main, Frame
  > TUL - FOUND UPPER FLANGE OF BELLFRAME 990 DENTED ABOVE STRINGER 26L. INSTALLED DOUBLER PER AARD 53-10-07-3. (M)
- [SDR AALA990377](https://openairdocs.org/sdr/AALA990377.md): Frame · dented · Mar 8, 1999 · N893AA · Boeing 727223 · Fuselage Main, Frame
  > TUL - TOP SECTION OF BELL FRAME DENTED 4 PLACES FS 1050 STRINGER 25R TO 27R. REMOVED DAMAGE, INSTALLED.063 7075T6 DOUBLER WITH 15 MS20470-D-8 RIVETS, 10MS20470-D-6 RIVETS, 10 BACR15CE-6 RIVETS, 1BACB30FP6 HI-LOCKS, 1BACB30FP6 HI-LOCKS PER SRM 51-40-3. (M)
- [SDR AALA990373](https://openairdocs.org/sdr/AALA990373.md): Shear Tie · corroded · Mar 8, 1999 · N893AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > TUL - FOUND SHEAR TIE CORRODED AT 1166 BELL FRAME STRINGER 29R AND STRINGER 30. REMOVED CORRODED SHEAR TIE, INSTALLED NEW SHEAR TIE. (M)
- [SDR AALA990372](https://openairdocs.org/sdr/AALA990372.md): Shear Tie · corroded · Mar 8, 1999 · N893AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > TUL - FOUND BELT FRAME 1130 SHEAR TIE CORRODED AFT SIDE OF BELT FRAME JUST OUTBOARD OF STRINGER 28R. REMOVED AND REPLACED SHEAR TIE STATION 1130 AFT SIDE OF BELT FRAME JUST OUTBOARD OF STRINGER 28R ACCORDING TO SRM 53-10-2 PAGE 28, SEALED PER SRM 51-20-40. (
- [SDR AALA990379](https://openairdocs.org/sdr/AALA990379.md): Frame · buckled · Mar 6, 1999 · N893AA · Boeing 727223 · Fuselage Main, Frame
  > TUL - BELL FRAME STATION 1110 BENT, WEB AREA BUCKLED ABOVE STRINGER 26L ITEM 2 TOP OF BELL FRAME STATION 1110 GOUGED FROM TOO LONG FAST. CUT OUT DAMAGE, REPAIRED BELL FRAME PER SRM 51-40-3 DOUBLER 7075-T6.063 BY 20 INCH LONG 2 ROWS 43 BACB30FP8 HI-LOCKS AND
- [SDR AALA990368](https://openairdocs.org/sdr/AALA990368.md): Frame · gouged · Mar 6, 1999 · N893AA · Boeing 727223 · Fuselage Main, Frame
  > TUL - TOP OF BELL FRAME GOUGED (FROM TOO LONG OF FAST), BELL FRAME STATION 1130 BELOW RT TIEDOWN FIITTING. CUT OUT DAMAGED AREA, INSTALLED DOUBLER PER AARD 3-10-07-3 DOUBLER 7075-T6.063 THICK BY 9.5 INCH LONG, 16 BACB30FP8 AND 17 BACB30FPL HI-LOCKS, 2 ROWS I
- [SDR AALA990395](https://openairdocs.org/sdr/AALA990395.md): Fitting · misdrilled · Mar 3, 1999 · N893AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > TUL - RIGHT CREASE BEAM 1183 END FITTING MIS-DRILLED ZERO EDGE DISTANCE ON FORWARD FASTENER, STATION 1176 STRINGER 17R. REMOVED 7 FASTENERS AND INSTALLED DOUBLER AND FILLERS PER ESO 11697 DATED 2-26-99. (M)
- [SDR AALA990371](https://openairdocs.org/sdr/AALA990371.md): Frame · corroded · Mar 3, 1999 · N893AA · Boeing 727223 · Fuselage Main, Frame
  > TUL - FOUND CORROSION ON 720E FRAME, FORWARD SIDE, FROM STRINGER 7L TO STRINGER 4L, 7 SPOTS (MARKED). REMOVED CORROSION AND INSTALLED FRAME REPAIRS AT STRINGER 4L, 5L, 6L, PER SRM 53-10-4 FIG 2. (M)
- [SDR AALA990363](https://openairdocs.org/sdr/AALA990363.md): Skin · corroded · Mar 3, 1999 · N893AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL - FOUND CORROSION ON SKIN AROUND ICE LIGHT STRINGER 14R-17R STATION 720B-C. INSTALLED DOUBLER AT RIGHT ICE LIGHT CUTOUT PER SRM 53-30-3 PAGE 137-140 FIG 22 AND ECO 11697, DATED 3/3/99. (M)
- [SDR AALA990374](https://openairdocs.org/sdr/AALA990374.md): Frame · corroded · Mar 2, 1999 · N893AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > TUL - FORWARD CARGO DOOR CUTOUT FORWARD LOWER CORNER FRAME WEB CORRODED STATION 560, STRINGER 26R. INSTALLED DOUBLER ON WEB PER SRM 51-40-2, DOUBLER 5.5 BY 4.25 INCH, 3 ROWS FASTENERS BACB3OMC8-6 W/BACC30M8 COLLARS MATERIAL 2024T3.080. (M)
- [SDR AALA990378](https://openairdocs.org/sdr/AALA990378.md): Frame · worn · Mar 1, 1999 · N893AA · Boeing 727223 · Fuselage Main, Frame
  > TUL - TOP OF BELT FRAME HAS 2 EACH WORN SPOTS ABOVE STRINGER 27L FROM FASTENER PROTRUSION AT CARGO TIEDOWN CASTING, STATION 1090 AND 27L STRINGER. INSTALLED DOUBLER.071 INCH WITH 19 EACH.25 INCH HI-LOCKS PER SRM 51-40-3 PAGE 3 AND 9.1875 INCH HI-LOCKS. TH
- [SDR AALA990350](https://openairdocs.org/sdr/AALA990350.md): Stringer · cracked · Mar 1, 1999 · N893AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > TUL - FOUND STRINGER 15R CRACKED AT END OF STRINGER FORWARD OF ICE LIGHT. HFEC TO CONFIRM CRACK, REMOVED CRACKED SECTION OF STRINGER 1.25 INCH. HFEC TO CONFIRM CRACK REMOVAL AND INSTALLED REPAIR, FILLER AND CHANNEL PER 53-10-3 PAGE 12-17. (M)
- [SDR AALA990375](https://openairdocs.org/sdr/AALA990375.md): Web · cracked · Feb 27, 1999 · N893AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > TUL - FOUND CORROSION AND CRACKS ON UPPE RLOWER SIDE ANGLES AND WEB OF TAIL SKID ACT MOUNT RIB STATION 1213 LBL 18 TO RBL 18, LBL 30 TO RBL 30. REMOVED AND INSTALLED NEW ANGLES AND WEB PER SRM 51-10-1. (M)
- [SDR AALA990366](https://openairdocs.org/sdr/AALA990366.md): Frame · cracked · Feb 27, 1999 · N893AA · Boeing 727223 · Fuselage Main, Frame
  > TUL - FOUND STATION 420 FRAME CRACKED AT STRINGER 10L. REPAIRED DAMAGED FRAME STATION 420 STRINGER 10L WITH DOUBLER AS PER SRM 53-10-4 PAGE 3-6 FIG 1 SHEET 4. INSTALLED DOUBLER ONE GAUGE HEAVIER THAN ORIGINAL AND USED HI-LOCK.15625 DIAMETER. (M)
- [SDR AALA990397](https://openairdocs.org/sdr/AALA990397.md): Casting · cracked · Feb 26, 1999 · N893AA · Boeing 727223 · Wing Miscellaneous Structure
  > TUL - FOUND CRACK IN RADIUS AND VERTICAL AREA OF LEFT 760 CASTING (BEHIND RIB). REPAIRED LEFT 760 CASTING PER BOEING SERVICE BULLETIN 727-57-0112 REV 5 LARGE REPAIR. (M)
- [SDR AALA990365](https://openairdocs.org/sdr/AALA990365.md): Seat Track · corroded · Feb 26, 1999 · N893AA · Boeing 727223 · Fuselage, Seat/Cargo Attach Fittings
  > TUL - FOUND CORROSION ON RIGHT OUTBOARD SEAT TRACK STATION 480 INBOARD, OUTBOARD LEGS AT FASTENER HOLES. REMOVED CORRODED SECTION OF SEAT TRACK. SPLICED IN NEW SECTION PER SRM 53-10-5 FROM STATION 480-560 RIGHT. (M)
- [SDR AALA990364](https://openairdocs.org/sdr/AALA990364.md): Skin · corroded · Feb 25, 1999 · N893AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL - FOUND SKIN CORRODED ON EXTERIOR OF AIRCRAFT FROM STATION 1060 TO 1067 AT STRINGER 28L. CUTOUT DAMAGED SKIN. REPAIRED WITH DOUBLER PER SRM 53-30-3 FIG 3. (M)
- [SDR AALA990360](https://openairdocs.org/sdr/AALA990360.md): Skin · corroded · Feb 25, 1999 · N893AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL - FOUND CORROSION ON EXTERIOR SKIN, STATION 708 STRINGER 28L. REPAIRED FUSELAGE SKIN PER SRM 53-30-3. (M)
- [SDR AALA990359](https://openairdocs.org/sdr/AALA990359.md): Skin · corroded · Feb 25, 1999 · N893AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL - FOUND STATION 708 BETWEEN STRINGER 27L AND 28L FUSELAGE SKIN HAS CORROSION. REPAIRED FUSELAGE SKIN PER SRM 53-30-3. (M)
- [SDR AALA990356](https://openairdocs.org/sdr/AALA990356.md): Skin · corroded · Feb 25, 1999 · N893AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL - FOUND SKIN CORRODED ON EXTERIOR OF AIRCRAFT. REPAIRED CORRODED THROUGH PORTION OF SKIN PER SRM 53-30-3. ALODINED AND PRIMED SKIN, PATCH AND SURFACE ON EXTERIOR OF SKIN PER SRM 51-10-2. (M)
- [SDR AALA990355](https://openairdocs.org/sdr/AALA990355.md): Stringer · corroded · Feb 25, 1999 · N893AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > TUL - FOUND STRINGER 28L CORRODED FROM STATIN 1050 TO 1070. CUT OUT DAMAGED STRINGER SECTION, AND INSTALLED STRINGER SPLICE PER SRM 53-10-3, FIGURE 1. (M)
- [SDR AALA990353](https://openairdocs.org/sdr/AALA990353.md): Stringer · corroded · Feb 25, 1999 · N893AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > TUL - FOUND CORROSION DOWN INSIDE STRINGER 27L AROUND DOME NUT, NUT PLATE STATION 702. REPAIRED FUSELAGE STRINGER PER SRM 53-10-3. (M)
- [SDR AALA990352](https://openairdocs.org/sdr/AALA990352.md): Stringer · corroded · Feb 25, 1999 · N893AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > TUL - FOUND HEAVY CORROSION ON STRINGER 28L, STATION 708. REPAIRED FUSELAGE STRINGER PER SRM 53-10-3. (M)
- [SDR AALA990349](https://openairdocs.org/sdr/AALA990349.md): Stringer · corroded · Feb 25, 1999 · N893AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > TUL - FOUND STRINGER 28R HAS CORROSION ON BOTTOM SURFACE AT FS 1040 TO 1070. REPAIRED STRINGER ACCORDING TO SRM 53-10-3. (M)
- [SDR AALA990348](https://openairdocs.org/sdr/AALA990348.md): Stringer · corroded · Feb 25, 1999 · N893AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > TUL - FOUND STRINGER 28R HAS CORROSION ON BOTTOM SURFACE AT FS 1040 TO 1070. REPAIRED STRINGER ACCORDING TO SRM 53-10-3. (M)
- [SDR AALA990390](https://openairdocs.org/sdr/AALA990390.md): Frame · dented · Feb 23, 1999 · N893AA · Boeing 727223 · Fuselage Main, Frame
  > TUL - FOUND UPPER FLANGE OF BELL FRAME IS DENTED AT STATION 620 AT STATION 24L TO 25L. CUT OUT DAMAGED SECTION AND INSTALLED REPAIR DOUBLER PER SRM 51-40-3, 7075T6.063, 16.5 INCH LONG, 3 ROWS RIVETS 1 ON TOP 2 ON SIDE WITH FORTY-EIGHT.1875 INCH D-RIVETS, FO
- [SDR AALA990389](https://openairdocs.org/sdr/AALA990389.md): Frame · dented · Feb 23, 1999 · N893AA · Boeing 727223 · Fuselage Main, Frame
  > TUL - UPPER FLANGE OF BELL FRAME DENTED AT STATION 600 AND STRINGER 24 TO 25L. CUT OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER PER SRM 51-40-3, 7075T6.063 SEVEN INCHES LONG, 3 ROWS RIVETS 1 TOP, 2 ON SIDE, NINTEEN.1875 INCH D-RIVETS, ONE.25 INCH D-RIVETS
- [SDR AALA990387](https://openairdocs.org/sdr/AALA990387.md): Frame · dented · Feb 23, 1999 · N893AA · Boeing 727223 · Fuselage Main, Frame
  > TUL - SMALL DENT, UPPER FLANGE OF STATION 680 BELL FRAME, BELOW STRINGER 24L. INSTALLED DOUBLER PER SRM 51-40-3 7075T6.063, 3 ROWS OF RIVETS 2 ROWS SIDE SIXTEEN.1875 D-RIVETS, FOUR.25 INCH D-RIVETS. (M)
- [SDR AALA990386](https://openairdocs.org/sdr/AALA990386.md): Frame · dented · Feb 23, 1999 · N893AA · Boeing 727223 · Fuselage Main, Frame
  > TUL - STATION 680 BELL FRAME DENTED AT STRINGER 23L. INSTALLED DOUBLER PER SRM 51-40-3 7075T6.063, 3 ROWS OF RIVETS 1 ROW TOP 2 ROWS SIDE 20.1875 D-RIVETS. (M)
- [SDR AALA990381](https://openairdocs.org/sdr/AALA990381.md): Frame · dented · Feb 23, 1999 · N893AA · Boeing 727223 · Fuselage Main, Frame
  > TUL - FOUND STATION 660 BELT FRAME DENTED AT 24L. INSTALLED DOUBLER (7075T-6,.063, 7.5 INCH LONG) 3 ROWS OF RIVETS (1 ROW TOP, 2 ROWS SIDE) WITH 20 EACH.1875 D-RIVETS PER SRM 51-40-3. (M)
- [SDR AALA990370](https://openairdocs.org/sdr/AALA990370.md): Frame · dented · Feb 23, 1999 · N893AA · Boeing 727223 · Fuselage Main, Frame
  > TUL - FOUND TOP OF BELL FRAME DENTED AT STAITON 950F 5 INCHES ABOVE STRINGER 26L. CUTOUT DAMAGED AREA, DUE CHECKED, FABRICATED DOUBLER, AND INSTALLED PER SRM 53-10-4 PAGE 4 FIG 1. (M)
- [SDR AALA990367](https://openairdocs.org/sdr/AALA990367.md): unknown · Feb 23, 1999 · N893AA · Boeing 727223 · Fuselage Main, Floor Beam
  > TUL - FOUND STATION 344 LBL 30 TOP FLANGE OF FLOORBEAM CRACKED AT FASTENER HOLE. CUT OUT DAMAGED SECTION OF TOP FLANGE. INSTALLED DOUBLER REPAIR PER SRM 53-10-8 FIG 9 SHEETS 1-5. (M)
- [SDR AALA990399](https://openairdocs.org/sdr/AALA990399.md): Skin · cracked · Feb 22, 1999 · N893AA · Boeing 727223 · Wing, Plate/Skin
  > TUL - FOUND CRACK IN LEADING EDGE SKIN OUTBOARD EDGE OF INBOARD ROLLER, CUTOUT AT BOTTOM FLANGE NR 8 SLAT. REMOVED DAMAGED AREA AND INSTALLED DOUBLER REPAIR PER SRM 57-30-4. (M)
- [SDR AALA990398](https://openairdocs.org/sdr/AALA990398.md): Skin · cracked · Feb 22, 1999 · N893AA · Boeing 727223 · Wing, Plate/Skin
  > TUL - FOUND CRACK IN LEADING EDGE SKIN AT INBOARD ROLLER TRACK CUTOUT FOR NR 6 SLAT. REMOVED DAMAGE AND INSTALLED DOUBLER REPAIR PER SRM 57-30-4. (M)
- [SDR AALA990393](https://openairdocs.org/sdr/AALA990393.md): Fitting · corroded · Feb 22, 1999 · N893AA · Boeing 727223 · Wing Miscellaneous Structure
  > TUL - FORWARD TRUNNION FITTING BEARING BORES CORRODED. REPLACED RMG FORWARD TRUNNION FITTING PER SRM 51-10-1. (M)
- [SDR AALA990384](https://openairdocs.org/sdr/AALA990384.md): Fitting · corroded · Feb 22, 1999 · N893AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > TUL - FOUND CORROSION ON FORWARD LEFT MLG TRUNNION FITTING BEARING ATTACHMENT BORES 4 EACH. REAMED HOLES AND INSTALLED OVERSIZE BUSHING PER ESO 11697 (2-22-97) AND SB 727-57-132. (M)
- [SDR AALA990376](https://openairdocs.org/sdr/AALA990376.md): Casting · corroded · Feb 22, 1999 · N893AA · Boeing 727223 · Wing, Control Surface Attach Fittings
  > TUL - INBOARD AILERON QUAD MOUNT CASTING CORRODED ON CASTING AND AROUND BEARING BORES. REMOVED AND REPLACED CORRODED CASTING PER SRM 51-10-1 PAGE 4. (M)
- [SDR AALA990362](https://openairdocs.org/sdr/AALA990362.md): Skin · corroded · Feb 22, 1999 · N893AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL - FOUND CORROSION ON SKIN AROUND LEFT ICE LIGHT HOUSING BETWEEN STRINGER 14L AND 16L STATION 720B-720C. REMOVED CORROSION AND BLENDED CORRODED AREA. FABRICATED AND INSTALLED DOUBLER PER SRM 53-30-3 PAGE 137-140 ALODINED AND PRIMED ALL PARTS PER SRM 51-10

Next page: https://openairdocs.org/deregistered/N893AA-2017-06-30/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 = 'N893AA' AND deregistration_id = 'N893AA-2017-06-30'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N893AA-2017-06-30/reports

---
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