# Service difficulty reports: N870AA, cancelled Apr 5, 2006

A list on [N870AA, cancelled Apr 5, 2006](https://openairdocs.org/deregistered/N870AA-2006-04-05.md).

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

- [SDR AALA20011610](https://openairdocs.org/sdr/AALA20011610.md): Bear Strap · cracked · Aug 8, 2001 · N870AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL - FOUND LOW FREQUENCY EDDY CURRENT INDICATES CRACK PROGRESSING FROM FASTENER ON AFT LWR FORWARD GALLEY DOOR CUTOUT. TRIMMED OUT DAMAGE AT BARE STRAP AND INSTALLED DOUBLER/TRIPLER PER SB 727-53-188 FIG 3. (M)
- [SDR AALA20011573](https://openairdocs.org/sdr/AALA20011573.md): Battery Pack · discharged · Aug 7, 2001 · N870AA · Boeing 727223 · Emergency Lighting
  > TUL - FOUND LEFT AND RIGHT FORWARD DOOR SLIDE LIGHTS FAILED 10 MINUTE CHECK. REPLACED FORWARD DOOR SLIDE LIGHT BATTERY PACK. (M)
- [SDR AALA20011574](https://openairdocs.org/sdr/AALA20011574.md): Battery Pack · discharged · Aug 7, 2001 · N870AA · Boeing 727223 · Emergency Lighting
  > TUL - FOUND RIGHT FORWARD AND AFT OVERWING EXIT EMERGENCY LIGHTS FAIL 10 MINUTE CHECK. REPLACED OVERWING EMERGENCY EXIT SIGN BATTERY PACK. (M)
- [SDR AALA20011575](https://openairdocs.org/sdr/AALA20011575.md): Battery Pack · discharged · Aug 7, 2001 · N870AA · Boeing 727223 · Emergency Lighting
  > TUL - FOUND CENTER AISLE OVERHEAD FORWARD AND AFT OVERWING AREA EMERGENCY EXIT LIGHTS FAIL 10 MINUTE CHECK. REPLACED AISLE SIGN EMERGENCY EXIT BATTERY PACK. (M)
- [SDR AALA20011608](https://openairdocs.org/sdr/AALA20011608.md): Skin · gouged · Aug 6, 2001 · N870AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL - FOUND GOUGE IN SKIN AT STATION 936 BETWEEN STRINGER 3R AND 4R. INSTALLED DOUBLER REPAIR AT STATION 936 BETWEEN STRINGER 3R AND 4R PER SRM 53-30-3 PART 1. (M)
- [SDR AALA20011609](https://openairdocs.org/sdr/AALA20011609.md): Shear Tie · corroded · Aug 6, 2001 · N870AA · Boeing 727223 · Fuselage Internal Mounting Structure
  > TUL - FOUND SHEAR TIE CORRODED AT STATION 520 STRINGER 26 TOP SIDE. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-10-1, TREATED, PRIMED PAINTED IAW MM 51-20-0. (M)
- [SDR AALA20010785](https://openairdocs.org/sdr/AALA20010785.md): Wire · loose · Feb 28, 2001 · N870AA · Boeing 727223 · Light System Wiring
  > MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 13D INOPERATIVE. RE-SECURED EMERGENCY EXIT LIGHT WIRE AT SEAT 13D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA20001599](https://openairdocs.org/sdr/AALA20001599.md): Skin · corroded · Sep 22, 2000 · N870AA · Boeing 727223 · Wing, Plate/Skin
  > TUL - INTERGRANULAR CORROSION ON LOWER WING SKIN LEFT PRIMARY HEAT EXCHANGER AT STA 3, 4, AND 5, LBL 16 LBL 36. BLENDED OUT CORROSION. FABRICATED REPAIR PLATES PER SRM 57-30-3 AND ESO 11697. INSTALLED REPAIR PER SRM 57-30-3 AND ESO 11697. (X)
- [SDR AALA20001583](https://openairdocs.org/sdr/AALA20001583.md): Light · inoperative · Sep 21, 2000 · N870AA · Boeing 727223 · Emergency Lighting
  > TUL - FOUND EMERGENCY FLOOR LIGHT STRIP REMOVED. INSTALLED SERVICEABLE LIGHT STRIP PER MM 33-60-098-4 AND OPS CHECKED GOOD. (M)
- [SDR AALA20001584](https://openairdocs.org/sdr/AALA20001584.md): Floorbeam · corroded · Sep 20, 2000 · N870AA · Boeing 727223 · Fuselage Main, Floor Beam
  > TUL - FLOOR BEAM AT STA 380 HAD CORROSION BETWEEN OUTBOARD SEAT TRACKS UNDER FORWARD GALLEY. REMOVED DAMAGED AREA AND INSTALLED DOUBLER PER ESO 11697 DATED 9-19-00. (X)
- [SDR AALA20001587](https://openairdocs.org/sdr/AALA20001587.md): Beam · cracked · Sep 19, 2000 · N870AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > TUL - VERTICAL BEAM CRACKED, STA 1183, RBL 36 WL 238. STOP DRILLED CRACK AND INSTALLED REPAIR MODIFICATION PER SB 727-53-0192 AND DWG 65C34406. (X)
- [SDR AALA20001590](https://openairdocs.org/sdr/AALA20001590.md): Shear Tie · damaged · Sep 18, 2000 · N870AA · Boeing 727223 · Fuselage Main, Structure
  > TUL - SKIN BULGED ON THE BELL FRAME FORWARD END OF INTERCOSTAL MARKED STA 1050, STR 27L. INSTALLED NEW SHEAR TIE PER SRM 51-30-2. (X)
- [SDR AALA20001588](https://openairdocs.org/sdr/AALA20001588.md): Beam · cracked · Sep 18, 2000 · N870AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > TUL - VERTICAL BEAM CRACKED AT LOWER END STA 1183 RBL 8. STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR IAW SB 727-53-0175. (X)
- [SDR AALA20001586](https://openairdocs.org/sdr/AALA20001586.md): Skin · corroded · Sep 17, 2000 · N870AA · Boeing 727223 · Wing, Plate/Skin
  > TUL - WING CENTER SECTION, LOWER SKIN HAD CORROSION AT RIGHT PLENUM. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 57-30-3. (X)
- [SDR AALA20001585](https://openairdocs.org/sdr/AALA20001585.md): Fitting · corroded · Sep 16, 2000 · N870AA · Boeing 727223 · Horizontal Stabilizer Structure
  > TUL - CORROSION ON FACES OF VERTICAL FIN, PIVOT LUGS, AND CORROSION ON HORIZONTAL STABILIZER PIVOT BORES AND FACES. REMOVED CORROSION PER SRM 51-10-2 AND SRM 55-30-6, FLAP REMOVED PER SRM 55-10-2. INSTALLED NEW BUSHINGS PER CARD 7403. (X)
- [SDR AALA20001589](https://openairdocs.org/sdr/AALA20001589.md): Flap · corroded · Sep 15, 2000 · N870AA · Boeing 727223 · Wing, Control Surface Attach Fittings
  > TUL - CORROSION ON GROUND ATTACH BOLT AT NR 2 LEADING EDGE FLAP, OUTBOARD. INSTALLED DOUBLER PER ESO 11697 DATED 9-14-00. (X)
- [SDR AALA20000919](https://openairdocs.org/sdr/AALA20000919.md): Light · inoperative · May 29, 2000 · N870AA · Boeing 727223 · Emergency Lighting
  > DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT ROW 23 EXTINGUISHES AFTER APPROXIMATELY 30 SECONDS FROM ACTIVATION. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA991637](https://openairdocs.org/sdr/AALA991637.md): Motor · failed · Mar 28, 2000 · N870AA · Boeing 727223 · Trailing Edge Flap Control System
  > DFW - FLT 2063 - AFTER TAKEOFF DFW, AIRCRAFT EXPERIENCED HYDRAULIC SYSTEM 'A' FLUID LOSS. ACCOMPLISHED ABNORMAL PROCEDURES, INCLUDING MANUAL GEAR EXTENSION. AIRCRAFT RETURNED AND LANDED DFW WITHOUT INCIDENT. REPLACED RIGHT OUTBOARD FLAP DRIVE MOTOR, SYSTEM
- [SDR AALA20000281](https://openairdocs.org/sdr/AALA20000281.md): Connector · failed · Mar 28, 2000 · N870AA · Boeing 727223 · Landing Gear Position and Warning
  > ORD - FLT 2283 - DURING APPROACH, RED NOSE GEAR LIGHT ON FORWARD INSTRUMENT PANEL DOES NOT ILLUMINATED WHEN GEAR EXTENDED. GEAR DID EXTEND AND LANDED ORD WITHOUT INCIDENT. REPLACED NOSE GEAR FORWARD INSTRUMENT PANEL CONNECTOR. SYSTEM GROUND CHECK NORMAL OPE
- [SDR AALA20000550](https://openairdocs.org/sdr/AALA20000550.md): Wire · broken · Mar 27, 2000 · N870AA · Boeing 727223 · Light System Wiring
  > MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHTS FORWARD PART OF COACH INOPERATIVE. REPAIRED EMERGENCY EXIT ESCAPE PATH LIGHT WIRE TERMINAL. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
- [SDR AALA991648](https://openairdocs.org/sdr/AALA991648.md): Connector · loose · Oct 31, 1999 · N870AA · Boeing 727223 · Emergency Lighting
  > DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SIGN ABOVE AFT GALLEY IS BLINKING ON AND OFF WITH LIGHT SWITCH IN THE ON POSITION. RE-SEATED EMERGENCY EXIT SIGN CONNECTOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
- [SDR AALA991440](https://openairdocs.org/sdr/AALA991440.md): Frame · misdrilled · Sep 17, 1999 · N870AA · Boeing 727223 · Fuselage Main, Frame
  > TUL - FOUND BELTFRAME DRILLED INTO 4 PLACES UPPER LEG STATION 560 BETWEEN STRINGER 28R AND 27R. INSTALLED DOUBLERS PER AARD 51-40-1. (M)
- [SDR AALA991439](https://openairdocs.org/sdr/AALA991439.md): Skin · gouged · Sep 17, 1999 · N870AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL - FOUND DEEP GOUGE IN SKIN AT STATION BETWEEN STRINGERS 1 AND 2R. CUT OUT DAMAGED AREA AND INSTALLED DOUBELR PER SRM 53-30-3 FIG 1. (M)
- [SDR AALA991438](https://openairdocs.org/sdr/AALA991438.md): Skin · gouged · Sep 17, 1999 · N870AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL - FOUND GOUGE IN SKIN AT STATION 660 BETWEEN STRINGER 1 AND 2R. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-30-3 FIG 1. (M)
- [SDR AALA991437](https://openairdocs.org/sdr/AALA991437.md): Spar · corroded · Sep 17, 1999 · N870AA · Boeing 727223 · Wing Spar
  > TUL - FOUND CORROSION ON LOWER SPAR CHORD BELOW NR 6 SLAT ACTUATOR. INSTALLED REPAIR STRAP IAW AARD 57-30-00-2 PAGES 1-3. (M)
- [SDR AALA991441](https://openairdocs.org/sdr/AALA991441.md): Skin · corroded · Sep 15, 1999 · N870AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL - FOUND BULGE IN SKIN LAP 26L FROM BS 990 PLUS 9 INCHES TO 990 PLUS 13 INCHES. REMOVED CORRODED PORTION OF SKIN AND INSTALLED DOUBLER PER SRM 53-30-3. (M)
- [SDR AALA981818](https://openairdocs.org/sdr/AALA981818.md): Stringer · corroded · Sep 25, 1998 · N870AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > TUL - BULGE IN SKIN STATION 680 BETWEEN STRINGER 26 AND 27. INSTALLED NEW SERVICEABLE STRINGER SPLICE AND REINSTALLED INTERCOSTAL PER SRM 53-10-3 PAGE 3. (M)
- [SDR AALA981817](https://openairdocs.org/sdr/AALA981817.md): Stringer · corroded · Sep 25, 1998 · N870AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > TUL - FOUND STRINGER 27L AT BS 670 HAS CORROSION AT STANDOFF INSIDE OF STRINGER. REMOVED DAMAGED SECTION OF STRINGER AND INSTALLED FILLER AND DOUBLER AT STRINGER 27L, BS 670 PER SRM 53-10-3 PAGE 3. (M)
- [SDR 98ZZZM943](https://openairdocs.org/sdr/98ZZZM943.md): Skin · corroded · Sep 25, 1998 · N870AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL - BULGE IN SKIN STATION 680 BETWEEN STRINGER 26 AND 27. INSTALLED NEW SERVICEABLE STRINGER SPLICE AND REINSTALLED INTERCOSTAL PER SRM 53-10-3 PAGE 3. (M)
- [SDR AALA981335](https://openairdocs.org/sdr/AALA981335.md): Light · inoperative · Jul 5, 1998 · N870AA · Boeing 727223 · Emergency Lighting
  > MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT R1 DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT AT R1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA971995](https://openairdocs.org/sdr/AALA971995.md): Control · defective · Oct 21, 1997 · N870AA · Boeing 727223 · Flight Compartment Lighting
  > IAD - FLT 0637 - AFTER TAKEOFF DCA DURING CLIMB-OUT ELECTRICAL ODOR NOTED IN CABIN AND COCKPIT. AIRCRAFT DIVERTED TO IAD AND LANDED WITHOUT INCIDENT. REPLACED HIGH INTENSITY LIGHT CONTROL. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
- [SDR AALA971881](https://openairdocs.org/sdr/AALA971881.md): Stringer · cracked · Oct 3, 1997 · N870AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > STR 15L AT WING SCANNING LIGHT STA 720B + 5 AND 720B +15 CRACKED FORWARD OF AND AFT OF LIGHT BOX AT STRINGER ENDS. REPAIRED STRINGER ENDS FORWARD AND AFT OF WING SCANNING LIGHT BOX PER SRM 53-10-3, PAGE 4B. TST: 55,509 HOURS. CYCLES, 33,962. (X)
- [SDR AALA971880](https://openairdocs.org/sdr/AALA971880.md): Stringer · dented · Oct 3, 1997 · N870AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > TUL - STRINGER 21R TOP FLANGE DENTED STA 448 -. DOUBLER INSTALLED OVER MINOR DENT INSIDE FUSELAGE IN STR 21R STA 448 PER SRM 53-10-3, FIG 1, PAGE 4B. TST: 55,509 HOURS. CYCLES, 33,962. (X)
- [SDR AALA971879](https://openairdocs.org/sdr/AALA971879.md): Web · corroded · Oct 3, 1997 · N870AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > DELTA BEAM LOWER WEB CORRODED AT STA 770 TO STA 760. REPLACED WEB STA 740 TO STA 770. TST: 55,509 HOURS. CYCLES, 33,962. (X)
- [SDR AALA971878](https://openairdocs.org/sdr/AALA971878.md): Bell Frame · bent · Oct 3, 1997 · N870AA · Boeing 727223 · Fuselage Main, Frame
  > TUL - LEFT STA 970 BELL FRAME BENT BETWEEN STR 25 AND STR 26 LEFT. REMOVED DAMAGED AREA AND INSTALLED DOUBLER PER SRM 51-40-3. 55,509 HOURS. CYCLES 33,962. (X)
- [SDR AALA971877](https://openairdocs.org/sdr/AALA971877.md): Skin · corroded · Oct 3, 1997 · N870AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL - CORROSION UNDER FLANGE OF ICE LIGHT BOX LEFT SIDE (WING SCANNING LIGHT). BLENDED CORROSION PER SMR 51-10-6, CORROSION OUT OF LIMITS, INSTALLED DOUBLER AND LENSE SHIM PER SRM 53-30-3, FIGURE 22. TST: 55,509 HOURS. CYCLES, 33,962. (X)
- [SDR AALA971876](https://openairdocs.org/sdr/AALA971876.md): Frame · corroded · Oct 3, 1997 · N870AA · Boeing 727223 · Fuselage Main, Frame
  > TUL - FRAME CORRODED AT FLOOR LEVEL 4 INCHES FORWARD OF FORWARD GALLEY DOOR. INSTALLED REPAIR IAW SRM. 55,509 HOURS. CYCLES, 33,962. (X)
- [SDR AALA971875](https://openairdocs.org/sdr/AALA971875.md): Floor Beam · corroded · Oct 3, 1997 · N870AA · Boeing 727223 · Fuselage Main, Floor Beam
  > TUL - STA 380 FLOOR BEAM HAS CORROSION BETWEEN RT INBD TIE-DOWN TRACK AND RT CREASE ANGLE. REMOVED CORRODED PIECE OF FLOOR BEAM PER SRM 53-10-8. REPLACED WITH FLOOR BEAM REPAIR IAW SRM 53-10-8. TST: 55,509 HOURS. CYCLES, 33,962. (X)
- [SDR AALA971968](https://openairdocs.org/sdr/AALA971968.md): Frame · corroded · Oct 2, 1997 · N870AA · Boeing 727223 · Fuselage Main, Frame
  > TUL - FRAME CORRODED AT FLOOR LEVEL 4 INCH FORWARD OF FORWARD GALLEY DOOR. INSTALLED REPAIR IAW SRM 51-40-3 FIG 1. (M)
- [SDR AALA971164](https://openairdocs.org/sdr/AALA971164.md): Pump · defective · Jul 2, 1997 · N870AA · Boeing 727223 · Hydraulic Pump (Electric/Engine), Main
  > MIA - FLT 2143 - EN ROUTE HAD SYSTEM 'A' HYDRAULIC LEAK/LOSS. GEAR WAS MANUALLY CRANKED DOWN. GPWS DEACTIVATED, FUEL DUMPED USED, GEAR PINS USED FROM POUCH, AND PNEUMATIC BRAKE SAFETY WIRE BROKEN. AIR INTERRUPTED BACK TO MIA AND LANDED WITHOUT INCIDENT. RE
- [SDR AALA961588](https://openairdocs.org/sdr/AALA961588.md): Controller · defective · Oct 21, 1996 · N870AA · Boeing 727223 · Cabin Pressure Controller
  > TPA - FLT 1629 - AFTER TAKEOFF MIA DURING CLIMB-OUT, PASSING THRUOGH FL 290, CABIN ALTITUDE BEGAN TO CLIMB WITH ASSOCIATED WARNING HORN. CLOSED BOTH OUTFLOW VALVES AND ACCOMPLISHED EMERGENCY DESCENT. AIRCRAFT DIVERTED TO TPA LANDED WITHOUT INCIDENT. REPLACE
- [SDR AALA952021](https://openairdocs.org/sdr/AALA952021.md): Skin · damaged · Nov 30, 1995 · N870AA · Boeing 727223 · Horizontal Stabilizer, Plate/Skin
  > TULE - FOUND LEFT LOWER SURFACE OF ELEVATOR DAMAGED. REMOVED LOWER LEFT ELEVATOR SKIN AND REPLACED WITH NEW SKIN. (M)
- [SDR AALA952019](https://openairdocs.org/sdr/AALA952019.md): Beam · cracked · Nov 30, 1995 · N870AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > TULE - FOUND 1183 VERTICAL BEAM CRACKED IN OUTBOARD RADIUS LBL 8 LOWER END ONE INCH LONG. INSTALLED VERTICAL BEAM REPAIR PER SB 727-53-0175.
- [SDR AALA952017](https://openairdocs.org/sdr/AALA952017.md): Floor Beam · corroded · Nov 30, 1995 · N870AA · Boeing 727223 · Fuselage Main, Floor Beam
  > TUL - FOUND CORROSION ON TOP OF FLOOR BEAM AT FASTENER HOLE STATION 1110 LBL 28 INCHES. CUT OUT DAMAGED AREA INSTALLED FILLER AND DOUBLER PER SRM 53-10-8 PG 9C 9D. (M)
- [SDR AALA950500](https://openairdocs.org/sdr/AALA950500.md): Eel Connector · broken · Mar 25, 1995 · N870AA · Boeing 727223 · Emergency Lighting
  > MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTING BY FWD GALLEY INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT CONNECTOR BY FWD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (Z)
- [SDR AALA950375](https://openairdocs.org/sdr/AALA950375.md): Duct · blown · Mar 2, 1995 · N870AA · Boeing 727223 · Pneumatic Distribution System
  > JFK-MIA - FLT 743 - AFTER TAKEOFF, THE LOWER BODY OVERHEAT LIGHT ILLUMINATED AND A LOUD THUD HEARD BY FLIGHT ATTENDANTS. PULLED NR 2 ENGINE TO IDLE TO EXTINGUISH LIGHT. LIGHT CAME BACK ON WHEN THROTTLE ADVANCED. THE LT NR 2 ENGINE AT IDLE, DIVERTED AND LAND

## 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 = 'N870AA' AND deregistration_id = 'N870AA-2006-04-05'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N870AA-2006-04-05/reports

---
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