# Service difficulty reports: N862AA, cancelled Mar 13, 2003

A list on [N862AA, cancelled Mar 13, 2003](https://openairdocs.org/deregistered/N862AA-2003-03-13.md).

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

- [SDR AALA20010850](https://openairdocs.org/sdr/AALA20010850.md): Skin · corroded · Apr 20, 2001 · N862AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL - FOUND CORROSION ON SKIN AT STATION 950F PLUS 3 - 950F PLUS 7, LEFT SIDE OF STRINGER 30. REMOVED CORROSION AND DAMAGED SKIN PER SRM 51-10-6. REPAIRED SKIN AT STATINO 950F PLUS 3 - 950F PLUS 7 PER 53-30-3 FIG 3. (M)
- [SDR AALA20010854](https://openairdocs.org/sdr/AALA20010854.md): Shear Tie · corroded · Apr 19, 2001 · N862AA · Boeing 727223 · Fuselage Main, Structure
  > TUL - FOUND CORROSION AT SHEAR TIE BETWEEN STRINGER 28R AND 29R AT STATION 950E PLUS 5 INCHES. REMOVED CORROSION AND INSTALLED SHEAR TIE REPAIR AS PER 53-10-4 OF SRM. (M)
- [SDR AALA20010851](https://openairdocs.org/sdr/AALA20010851.md): Angle · corroded · Apr 19, 2001 · N862AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > TUL - FOUND CORROSION ON ANGLE FOR FLOOR SUPPORT IN RIGHT NWW TUNNEL. REMOVED CORROSION AND INSTALLED REPAIR DOUBLER PER ESO 11697 DATED 4-18-01. (M)
- [SDR AALA20010853](https://openairdocs.org/sdr/AALA20010853.md): Skin · corroded · Apr 18, 2001 · N862AA · Boeing 727223 · Wing, Plate/Skin
  > TUL - FOUND CORROSION FOUND AT STATION 725 ON LOWER TRAILING EDGE OF WING, RT WING. REMOVED CORROSION AND INSTALLED DOUBLER PER ESO DATED 4/18/2001 ESO 11697. (M)
- [SDR AALA20010852](https://openairdocs.org/sdr/AALA20010852.md): Stringer · corroded · Apr 18, 2001 · N862AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > TUL - FOUND CORROSION ON STRINGER 29R, AFT OF STATION 950E. REMOVED CORROSION AND INSTALLED REPAIR PER ESO 11697, DATED 4-18-2001. (M)
- [SDR AALA2000500](https://openairdocs.org/sdr/AALA2000500.md): Pan · corroded · Mar 6, 2000 · N862AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > TUL - FOUND CORROSION ON LAVATORY FLOOR PAN STATION 1167 RBL 50. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 51-40-2. (M)
- [SDR AALA990730](https://openairdocs.org/sdr/AALA990730.md): Wire · loose · May 19, 1999 · N862AA · Boeing 727223 · Landing Gear System Wiring
  > ORD - FLT 1916 - AFTER TAKEOFF DURING CLIMB-OUT AT 12,000 FEET, RT MAIN GEAR RED UNSAFE LIGHT ILLUMINATED. CREW POSITIONED GEAR HANDLE IN UP POSITION AND THE LIGHT EXTINGUISHED AND REMAINED EXTINGUISHED WHEN HANDLE PLACED IN OFF POSITION. FLIGHT CONTINUED AN
- [SDR AALA990719](https://openairdocs.org/sdr/AALA990719.md): Light · inoperative · May 17, 1999 · N862AA · Boeing 727223 · Emergency Lighting
  > DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS BETWEEN FIRST CLASS AND R2 DOOR INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHT STRIPS AT R2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA990514](https://openairdocs.org/sdr/AALA990514.md): Skin · cracked · May 14, 1999 · N862AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL - FOUND SKIN CRACKED AT LOWR AFT CORNER OF RIGHT SERVICE DOOR CUTOUT, FORWARD GALLEY DOOR. REMOVED DAMAGED AREA. INSTALLED DOUBLER REPAIR PER SB 727-53-0188 FIG 2. (M)
- [SDR AALA990511](https://openairdocs.org/sdr/AALA990511.md): Skin · corroded · May 11, 1999 · N862AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL - FOUND CORROSION ON SKIN. CORROSION ON SKIN CUTOUT AND DOUBLER INSTALLED PER 53-30-3 FIG 3. (M)
- [SDR AALA990517](https://openairdocs.org/sdr/AALA990517.md): Stringer · corroded · Apr 14, 1999 · N862AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > TUL - FOUND CORROSION IN STRINGER. CUT OUT SECTION OF CORROSION AND INSTALLED REPAIR PER SRM 53-10-3 FIG 1. (M)
- [SDR AALA990516](https://openairdocs.org/sdr/AALA990516.md): Shear Tie · corroded · Apr 14, 1999 · N862AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > TUL - FOUND CORROSION ON SHEAR TIE. CUT OUT CORROSION AND INSTALLED DOUBLER PER 53-10-4. (M)
- [SDR AALA990515](https://openairdocs.org/sdr/AALA990515.md): Skin · corroded · Apr 14, 1999 · N862AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL - FOUND WHILE ON CUTTING OUT CORROSION ON SHEAR TIE SKIN WAS DAMAGED. GROUND OUT DAMAGE AND INSTALLED DOUBLER ON EXIT SKIN PER SRM 53-30-3 FIG AND AARD 53-30-03-3.071 2024T3. (M)
- [SDR AALA990513](https://openairdocs.org/sdr/AALA990513.md): Skin · corroded · Apr 14, 1999 · N862AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL - FOUND CORROSION ON SKIN STATION 680-688, STRINGER 27R. REMOVED CORROSION AND INSTALLED DOUBLER PER 53-30-3 FIG 3A. (M)
- [SDR AALA990510](https://openairdocs.org/sdr/AALA990510.md): Shear Tie · corroded · Apr 14, 1999 · N862AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > TUL - FOUND CORROSION ON SHEAR TIE AFT SIDE 11130 FRAME STRINGER 28-29L. REMOVED SHEAR TIE CLEANED CORROSION IN AREA IAW INSTALLED NEW SHEAR TIE PER SRM. (M)
- [SDR AALA990509](https://openairdocs.org/sdr/AALA990509.md): Frame · damaged · Apr 14, 1999 · N862AA · Boeing 727223 · Fuselage Main, Frame
  > TUL - FOUND HOLE IN BELL FRAME FROM SIDEWALL SCREW. INSTALLED DOUBLER PER 51-40-3. (M)
- [SDR AALA990508](https://openairdocs.org/sdr/AALA990508.md): Frame · cracked · Apr 14, 1999 · N862AA · Boeing 727223 · Fuselage Main, Frame
  > TUL - FOUND CRACK IN BELL FRAME. CUTOUT DAMAGED AREA AND INSTALLED REPAIR PER 51-40-3. (M)
- [SDR AALA990512](https://openairdocs.org/sdr/AALA990512.md): Skin · corroded · Apr 8, 1999 · N862AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL - FUSELAGE SKIN CORROSION AT SKIN LAP 26R OUTBOARD SIDE STATION 684-688. FUSELAGE SKIN CORROSION AT OUTBOARD SIDE OF 27R STATION 685. REMOVED SECTION OF SKIN LAP 2 INCH BY 3 INCH, INSTALLED EXTERNAL DOUBLE OVER BOTH AREAS 680-680 PLUS 18. OVERALL DIMENS
- [SDR AALA990507](https://openairdocs.org/sdr/AALA990507.md): Angle · corroded · Apr 7, 1999 · N862AA · Boeing 727223 · Wing Miscellaneous Structure
  > TUL - FOUND UPPER SURFACE OF LOWER CHORD ON RIGHT WING L/E BELOW NR 6 SLAT ACT HAS HEAVY CORROSION. REPAIRED PER AARD 57-30-00-2 PAGE 1. (M)
- [SDR AALA981432](https://openairdocs.org/sdr/AALA981432.md): Connector · loose · Jul 23, 1998 · N862AA · Boeing 727223 · Emergency Lighting
  > MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR PATH LIGHTING AT PAX SEAT ROWS 10D THROUGH 15D INOPERATIVE. RESEATED LOOSE EMERGENCY FLOOR PATH LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA980800](https://openairdocs.org/sdr/AALA980800.md): Skin · corroded · Apr 15, 1998 · N862AA · Boeing 727223 · Elevator, Plate/Skin
  > TUL - FOUND SKIN CRACKED LOWER SURFACE OF RT ELEV INBOARD OF ELEV PCU. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 55-20-3. (M)
- [SDR AALA971148](https://openairdocs.org/sdr/AALA971148.md): Connector · loose · Jun 28, 1997 · N862AA · Boeing 727223 · Emergency Lighting
  > MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING IN FIRST CLASS INOPERATIVE. REPAIRED LOOSE CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA970941](https://openairdocs.org/sdr/AALA970941.md): Frame · corroded · May 16, 1997 · N862AA · Boeing 727223 · Fuselage Main, Frame
  > TUL - CORROSION ON STR 373 FRAME INBOARD FLANGE FROM STR 17R UP TO STR 16R. REMOVED CORROSION AND INSTALLED REPAIR PER SRM 51-40-3, PAGES 1-6, FIG 1. TST: 55,741 HOURS. CYCLES: 34.503. (X)
- [SDR AALA970940](https://openairdocs.org/sdr/AALA970940.md): Frame · corroded · May 16, 1997 · N862AA · Boeing 727223 · Fuselage Main, Frame
  > TUL - CORROSION ON FUSELAGE FRAME STA 380R FORWARD GALLEY DOOR FRAME RBL 70 ABOVE AND BELOW FLOOR. REMOVED AND REPLACED FRAME SECTION. TST: 55,741 HOURS. CYCLES, 34,503. (X)
- [SDR AALA970939](https://openairdocs.org/sdr/AALA970939.md): Stringer · corroded · May 16, 1997 · N862AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > TUL - CORROSION ON STRINGER 29L STA 950F TO STA 990. CUT OUT CORRODED SECTION OF STRINGER AND INSTALLED NEW SECTION AND REPAIRED PER SRM 53-10-3. TST: 55,741 HOURS. CYCLES, 34,503. (X)
- [SDR AALA970938](https://openairdocs.org/sdr/AALA970938.md): Skin · corroded · May 16, 1997 · N862AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL - CORROSION ON BELLY SKIN UNDER LEVELING COMPOUND OUTBOARD OF STR 286 AT BS 580. CORROSION ON OUTBOARD SIDE OF STR 28L. CUT OUT CORRODED AREA, FABRICATED AND INSTALLED DOUBLER PER SRM 53-30-3 PAGES 12-14A. TST: 55,741 HOURS. CYCLES, 34,503. (X)
- [SDR AALA970937](https://openairdocs.org/sdr/AALA970937.md): Skin · corroded · May 16, 1997 · N862AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL - CORROSION ON BELLY SKIN AND UNDER INTERCOSTAL AND CORROSION ON SHEAR TIE 1 INCH OUTBOARD STR 27L. REPAIRED CORROSION ON SKIN PER SRM 53-30-3 FIG 24. TST: 55,741 HOURS. CYCLES, 34,503. (X)
- [SDR AALA970936](https://openairdocs.org/sdr/AALA970936.md): Floor Beam · corroded · May 16, 1997 · N862AA · Boeing 727223 · Fuselage Main, Floor Beam
  > TUL - RBL 70 SA 380 CORROSION ON TOP OF FLOOR BEAM. CUT OUT CORROSION AND INSTALLED DOUBLER PER SRM CHAPTER 53-10-8 PAGES 9A AND 9B. REFERENCE ES8 22 01 431 FOR INSTALLATION OF FLOOR TRACK. TST: 55,741 HOURS. CYCLES, 34,503. (X)
- [SDR AALA970935](https://openairdocs.org/sdr/AALA970935.md): Stringer · corroded · May 16, 1997 · N862AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > TUL - CORROSION ON STR 27L AT STA 720B + 8 INCHES. REMOVED DAMAGED AREA AND INSTALLED DOUBLER (STRINGER SPLICE) PER SRM 53-10-3. TST: 55,741 HOURS. CYCLES, 34,503. (X)
- [SDR AALA970934](https://openairdocs.org/sdr/AALA970934.md): Floor Beam · corroded · May 16, 1997 · N862AA · Boeing 727223 · Fuselage Main, Floor Beam
  > TUL - CORROSION ON FLOOR BEAM, STA 380 RBL 13 - RBL 70. CUT OUT CORROSION AND INSTALLED DOUBLER PER SRM 53-10-8 FIG 1. TST: 55,741 HOURS. CYCLES, 34,503. (X)
- [SDR AALA970933](https://openairdocs.org/sdr/AALA970933.md): Floor Beam · cracked · May 16, 1997 · N862AA · Boeing 727223 · Fuselage Main, Floor Beam
  > TUL - STA 760 RT RBL 70.5, APPROXIMATELY 6 INCH, 2 EACH, CRACKS IN LIGHTNING HOLE OF FLOOR BEAM LOWER OUTBOARD RADIUS UPPER I/A RADIUS.75 INCH PLUS 1 INCH LONG. REPLACED WEB SECTION AND ACCOMPLISHED TYPICAL WEB REPAIR 51-40-2 PG 6. TST: 55,741 HOURS. CYC
- [SDR AALA970931](https://openairdocs.org/sdr/AALA970931.md): Bell Frame · bent · May 16, 1997 · N862AA · Boeing 727223 · Fuselage Main, Frame
  > TUL - BELL FRAME BENT STR 26 LEFT STA 1030. FABRICATED AND REPAIRED DOUBLER PER SRM 53-10-4 FIG 7. TST: 55,741 HOURS. CYCLES, 34,503. (X)
- [SDR AALA970930](https://openairdocs.org/sdr/AALA970930.md): Bell Frame · bent · May 16, 1997 · N862AA · Boeing 727223 · Fuselage Main, Frame
  > TUL - BELL FRAME BENT STR 26 TO STR 27 LEFT STA 1010. FABRICATED AND REPAIRED BELL FRAME DOUBLER PER SRM 53-10-4, FIG 2. TST: 55,741 HOURS. CYCLES, 34,503. (X)
- [SDR AALA970929](https://openairdocs.org/sdr/AALA970929.md): Stringer · corroded · May 16, 1997 · N862AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > TUL - AFT END OF STR 27L CORRODED AT BS 740 BULKHEAD LOWER CHORD ATTACH. REPAIRED STRINGER WITH STRINGER SPLICE AT BS 740 AND STR 27L PER SRM 53-10-3. TST: 55,741 HOURS. CYCLES, 34,503. (X)
- [SDR AALA970928](https://openairdocs.org/sdr/AALA970928.md): Spar · corroded · May 16, 1997 · N862AA · Boeing 727223 · Wing Spar
  > TUL - CORROSION ON LOWER FWD LEFT WING SPAN CHORD EXTENSION. REMOVED CORROSION, TREATED AREA, AND INSTALLED REPAIR STRAP PER SRM 57-30-00-2 FIG 1. TST: 55,741 HOURS. CYCLES, 34,503. (X)
- [SDR AALA970926](https://openairdocs.org/sdr/AALA970926.md): Angle · corroded · May 16, 1997 · N862AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > TUL - HEAVY CORROSION ON STA 1183 FAIL SAFE ANGLE AFT OF LAVS. REPLACED FAIL SAFE ANGLE WITH NEW PER SRM 51-10-1 PAGE 6. TST: 55,741 HOURS. CYCLES, 34,503. (X)
- [SDR AALA970925](https://openairdocs.org/sdr/AALA970925.md): Skin · corroded · May 16, 1997 · N862AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL - BELLY SKIN CORRODED AT 7201 + 3 INCHES OUTBOARD OF STR 27R. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 53-30-3 FIG 1. TST: 55,741 HOURS. CYCLES, 34,503. (X)
- [SDR AALA970922](https://openairdocs.org/sdr/AALA970922.md): Shear Tie · corroded · May 16, 1997 · N862AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > TUL - CORROSION ON SHEAR TIE LEFT SIDE OUTBOARD OF NOSE TRUNNION NEXT TO SKATE ANGLE THROUGH ACCESS PLATE STA 304. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 51-40-3 FIG 1. TST: 55,741 HOURS. CYCLES, 34,502. (X)
- [SDR AALA970921](https://openairdocs.org/sdr/AALA970921.md): Skin · corroded · May 16, 1997 · N862AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL - CORROSION AT SKIN LAP AND AT SHEAR TIE. REPAIRED SKIN AT SKIN LAP WITH DOUBLER PER 53-30-3 AND REPLACED CORRODED SHEAR TIE BETWEEN 26-27R. 55,741 HOURS. CYCLES, 34,503. (X)
- [SDR AALA970205](https://openairdocs.org/sdr/AALA970205.md): Light · defective · Jan 24, 1997 · N862AA · Boeing 727223 · Emergency Lighting
  > DFW - DURING OVERNIGHT CHECK, EMERGENCY LIGHT ABOVE AFT GALLEY SERVICE DOOR INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY ABOVE AFT GALLEY SERVICE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA961548](https://openairdocs.org/sdr/AALA961548.md): Solenoid · defective · Oct 22, 1996 · N862AA · Boeing 727223 · Landing Gear Retraction/Extension System
  > SJU - FLT 706 - AFTER TAKEOFF STX, LANDING GEAR LEVER LATCH C/B TRIPPED WHEN GEAR HANDLE SELECTED UP. C/B WOULD NOT RESET AND OVERRIDE TRIGGER WAS USED TO RAISE GEAR HANDLE. NO OTHER ABNORMAL INDICATIONS AND AIRCRAFT PROCEEDED TO SJU, LANDING WITHOUT INCIDEN
- [SDR AALA961547](https://openairdocs.org/sdr/AALA961547.md): Accessory Unit · defective · Oct 22, 1996 · N862AA · Boeing 727223 · Landing Gear Retraction/Extension System
  > STX - FLT 695 - EN ROUTE MIA-STX - DURING CRUISE, EXPERIENCED NUISANCE WARNING HORN DUE TO A TRIPPED LEVER LATCH CIRCUIT BREAKER. RESET CIRCUIT BREAKER AND WARNING HORN CEASED FOLLOWED BY ELECTRICAL ODOR IN COCKPIT. LEVER LATCH C/B TRIPPED AGAIN AND WAS NOT
- [SDR AALA960467](https://openairdocs.org/sdr/AALA960467.md): Intercostal · corroded · Mar 25, 1996 · N862AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > FOUND CORROSION ON INBOARD SIDE OF INTERCOSTAL STRINGER 28R, STATION 950F AND 970. REMOVED AND REPLACED INTERCOSTAL STRINGER 28R, STATION 950F-970. (M)
- [SDR AALA960466](https://openairdocs.org/sdr/AALA960466.md): Skin · corroded · Mar 25, 1996 · N862AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL - FOUND STATION 950F TO 970 SKIN IS CORRODED ON OUTBOARD SIDE OF STRINGER 28R. REMOVED (BLENDED) CORROSION FROM SKIN 950F-970. INSTALLED DOUBLER AND TRIPLER IN AREA OF CORROSION AND SPLICED IN 2 SECTIONS OF STRINGER REPAIRS IAW ES11697, DTD 3-15-96. (M)
- [SDR AALA960465](https://openairdocs.org/sdr/AALA960465.md): Stringer · corroded · Mar 25, 1996 · N862AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > FOUND STATION 950F TO 970 STRINGER 28R IS CORRODED. REPLACED CORRODED SECTION OF STRINGER REF ESO 11697, DTD 3-15-96. (M)
- [SDR AALA960032](https://openairdocs.org/sdr/AALA960032.md): Door Switch · defective · Jan 10, 1996 · N862AA · Boeing 727223 · Landing Gear Position and Warning
  > DFW - FLT 0296 - AFTER TAKEOFF DFW WHEN LANDING GEAR RETRACTED, MLG DOOR WARNING REMAINED ILLUMINATED WITH ASSOCIATED RT MLG DOOR WARNING INDICATION ON F/E PANEL. EXTENDED LANDING GEAR AND ALL INDICATIONS RETURNED TO NORMAL. AIRCRAFT RETURNED TO DFW AND LAND
- [SDR AALA952060](https://openairdocs.org/sdr/AALA952060.md): Lock Actuator · defective · Dec 8, 1995 · N862AA · Boeing 727223 · Landing Gear Door Retract Section
  > IAD - FLT 1654 - DURING APPROACH TO IAD WHEN LANDING GEAR EXTENDED, RT MLG DID NOT EXTEND. RECYCLED LANDING GEAR WITH SAME RESULTS. MANUALLY EXTENDED LANDING GEAR AND AIRCRAFT LANDED IAD WITHOUT INCIDENT. REPLACED RT MLG SEQUENCE DOOR LOCK ACTUATOR. ACCOMP
- [SDR AALA951885](https://openairdocs.org/sdr/AALA951885.md): Eel Connector · loose · Nov 2, 1995 · N862AA · Boeing 727223 · Emergency Lighting
  > BWI - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS IN FORWARD PART OF MAIN CABIN FOUND INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT CONNECTORS BY OVERWING EXIT AND FORWARD PART OF MAIN CABIN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

## 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 = 'N862AA' AND deregistration_id = 'N862AA-2003-03-13'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N862AA-2003-03-13/reports

---
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