# Service difficulty reports: N362PA, cancelled Jun 1, 2006

A list on [N362PA, cancelled Jun 1, 2006](https://openairdocs.org/deregistered/N362PA-2006-06-01.md).

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

- [SDR RIVA020308](https://openairdocs.org/sdr/RIVA020308.md): Beam · corroded · Mar 8, 2002 · N362PA · Boeing 7272J0 · Horizontal Stabilizer Miscellaneous Structure
  > MQY - FOUND RIGHT HORIZONTAL STAB UPPER TRAILING EDGE BEAM AT REAR SPAR STATION 151.81 HAS CORROSION. FOUND TO BE OUT OF LIMITS IAW B727 SRM 55=10-1, FIG 1. REMOVED AND REPLACED TRAILING EDGE BEAM IAW B727 SRM 51-30-5 AND B727SRM 51-30-2. PART REPLACED WITH
- [SDR RIVA020308A](https://openairdocs.org/sdr/RIVA020308A.md): Skin · broken · Mar 8, 2002 · N362PA · Boeing 7272J0 · Leading Edge Devices
  > MQY - FOUND LEFT WING INBOARD FLAP INBOARD END OF FORE FLAP UPPER SURFACE SKIN IS WORN AND HAS PIECES BROKEN OFF WS 220. REMOVED DAMAGED SECTION. FABRICATED FILLER DOUBLER AND INSTALLED PER EO NR 01-298 WITH APPROVED 8110-3. APPRECIABLE WEIGHT ADDED BY THIS
- [SDR RIVA020308B](https://openairdocs.org/sdr/RIVA020308B.md): Door Frame · cracked · Mar 8, 2002 · N362PA · Boeing 7272J0 · Fuselage Main, Structure
  > MQY - FOUND R-1 DOOR LOWER FORWARD CORNER WEB CRACKED 2.5 INCHES LENGTH STATION 380, STRINGER 17R. CUT OUT DAMAGED SECTION. FABRICATED NEW SECTION AND SPLICES AND INSTALLED PER EO NR 01-298 WITH APPROVED 8110-3. APPRECIABLE WEIGHT ADDED BY THIS REPAIR IS.6
- [SDR RIVA020308C](https://openairdocs.org/sdr/RIVA020308C.md): Door Frame · corroded · Mar 8, 2002 · N362PA · Boeing 7272J0 · Fuselage Main, Structure
  > MQY - FOUND R-1 DOOR AFT JAMB HAS CORROSION AT UPPER CAM FITTING STATION 420. CUT OUT DAMAGED AREA. FABRICATED FILLER/REPAIR ANGLE AND INSTALLED PER EO NR 01-298 WITH APPROVED 8110-3. APPRECIABLE WEIGHT ADDED BY THIS REPAIR IS.55 LB STATION 420. (M)
- [SDR RIVA020308E](https://openairdocs.org/sdr/RIVA020308E.md): Floorbeam · corroded · Mar 8, 2002 · N362PA · Boeing 7272J0 · Fuselage Main, Floor Beam
  > MQY - FOUND FLOORBEAM CORRODED AT STATION 1110 FROM LBL 45 INCHES TO RBL 20 INCHES HAS BEEN BLENDED TO LIMITS IAW B727 SRM 53-10-1, FIG 4. CORROSION STILL EXISTS IN AREA. REMOVED AND REPLACED UPPER T-CHORD AT STATION 1110 LBL 69 TO RBL 34.5 IAW B727 SRM 53-1
- [SDR RIVA020308F](https://openairdocs.org/sdr/RIVA020308F.md): Floorbeam · corroded · Mar 8, 2002 · N362PA · Boeing 7272J0 · Fuselage Main, Floor Beam
  > MQY - FOUND STATION 344 FLOORBEAM CORROSION REMOVED TO MAX LIMITS PER SRM. CORROSION STILL EXISTS RBL 25 INCHES - LBL 25 INCHES. REMOVED DAMAGED SECTION AND REPLACED WITH NEW T-CAP AND SPLICES IAW B727 SRM 53-10-8, 51-30-2 AND 51-10-2. NEW REPLACEMENTS PART
- [SDR RIVA020308G](https://openairdocs.org/sdr/RIVA020308G.md): Floorbeam · corroded · Mar 8, 2002 · N362PA · Boeing 7272J0 · Fuselage Main, Floor Beam
  > FOUND STATION 380 FLOORBEAM CORROSION. REMOVED TO MAX LIMITS PER SRM. CORROSION STILL EXISTS RBL 13 INCHES - 33 INCHES RBL. REMOVED EXISTING REPAIR T-CAP. FABRICATED NEW SECTION AND INSTALLED IAW B727 SRM 53-10-8, FIG 3 AND 51-10-2, 51-30-2. NEW REPLACEME
- [SDR RIVA020308H](https://openairdocs.org/sdr/RIVA020308H.md): Floorbeam · corroded · Mar 8, 2002 · N362PA · Boeing 7272J0 · Fuselage Main, Floor Beam
  > MQY - FOUND STATION 400 FLOORBEAM CORROSION REMOVED TO MAX LIMITS PER SRM. CORROSION STILL EXISTS LBL 18 INCH - RBL 15 INCH. REMOVED AND INSTALLED REPAIR SECTION T-EXTRUSION IAW B727 SRM 53-10-8, FIG 3 AND 51-10-2. NEW REPLACEMENT PARTS USED. NO CHANGE IN W
- [SDR RIVA0203081](https://openairdocs.org/sdr/RIVA0203081.md): Rib · punctured · Mar 8, 2002 · N362PA · Boeing 7272J0 · Elevator, Spar/Rib
  > MQY - FOUND RIGHT ELEVATOR UPPER SKIN STATION 173 LOWER RIB PUNCTURED 3 PLACES. FABRICATED REPAIR DOUBLER IAW B727 SRM 55-20-3. TREATED AND PRIMED IAW B727 51-10-2. INSTALLED DOUBLER IAW B727 SRM 51-30-2. APPRECIABLE WEIGHT ADDED BY THIS REPAIR.120 LB AT
- [SDR RIVA020308J](https://openairdocs.org/sdr/RIVA020308J.md): Floorbeam · corroded · Mar 8, 2002 · N362PA · Boeing 7272J0 · Fuselage Main, Floor Beam
  > MQY - FOUND FLOORBEAM STATION 420 RBL 3 INCH CORROSION BLEND TO LIMITS IAW B727 SRM 53-10-1, FIG 4 CORROSION STILL EXISTS. CUT OUT CORRODED AREA PER B727 SRM 53-10-8, FIG 8. TREATED AND PRIMED PER SRM 51-10-2. INSTALLED FILLER AND REPAIR ANGLES PER SRM 53-1
- [SDR RIVA020308K](https://openairdocs.org/sdr/RIVA020308K.md): Floorbeam · corroded · Mar 8, 2002 · N362PA · Boeing 7272J0 · Fuselage Main, Floor Beam
  > MQY - FOUND FLOORBEAM STATION 328 UPPER FLANGE CORRODED BEYOND LIMITS LBL 30 INCHES AND RBL 13 INCHES UPPER AND LOWER SURFACES. REMOVED DAMAGED SECTION IAW B727 SRM 53-10-8. FABRICATED REPAIR SECTION AND SPLICES IAW B727 SRM 53-10-8. TREATED, PRIMED AND INS
- [SDR RIVA020308L](https://openairdocs.org/sdr/RIVA020308L.md): Skin · damaged · Mar 8, 2002 · N362PA · Boeing 7272J0 · Trailing Edge Flaps
  > MQY - FOUND LEFT OUTBOARD FORE FLAP TRAILING EDGE DAMAGE APPROX 2 INCH BY 5 INCH AT WS 491. CUT OUT DAMAGED AREA. FILLED VOID AREA. FABRICATED UPPER AND LOWER SKIN DOUBLERS. TREATED PRIMED PER EO NR 01-298 WITH APPROVED 8110-3. APPRECIABLE WEIGHT ADDED BY
- [SDR RIVA020308M](https://openairdocs.org/sdr/RIVA020308M.md): Door Frame · cracked · Mar 8, 2002 · N362PA · Boeing 737300 · Fuselage Main, Structure
  > MQY - NR 3 CARGO DOOR STATION1090 FRAME HAS CRACK BETWEEN STRINGERS 26R AND 27R. ROUTED OUT CRACK. FABRICATED REPAIR ANGLES AND FILLERS. TREATED AND PRIMED AND INSTALLED REPAIR ANGLES AND FILLERS PER BOEING REPAIR SKETCH TEK MQY 02-0001F WITH 8110-3, DATED
- [SDR RIVA011218](https://openairdocs.org/sdr/RIVA011218.md): Skin · corroded · Dec 18, 2001 · N362PA · Boeing 7272J0 · Spoilers
  > NR 6 SPOILER UPPER SKIN CORRODED. FABRICATED FILLER AND DOUBLER IAW BOEING SRM 51-40-20 FIG 5 AND 14. BONDED AND SEALED REPAIR PARTS IAW BOEING SRM 51-40-20 FIG 5, 14 AND SRM 51-20-4. (M)
- [SDR RIVA011217](https://openairdocs.org/sdr/RIVA011217.md): Tab · delaminated · Dec 17, 2001 · N362PA · Boeing 7272J0 · Elevator, Tab Structure
  > RIGHT ELEVATOR TAB DELAMINATED AT AFT OUTBOARD END. REMOVED DELAMINATED AREA OF SKIN.75 INCH BY.75 INCH IAW BOEING SRM 51-40-20 FIG 20. FABRICATED AND INSTALLED DOUBLER IAW BOEING SRM 51-40-20 FIG 20. (M)
- [SDR RIVA0000026](https://openairdocs.org/sdr/RIVA0000026.md): Skin · dented · Aug 17, 2000 · N362PA · Boeing 7272J0 · Nacelle/Pylon, Plate/Skin
  > PSM, THE NR 3 ENG NACELLE NOSE COWL IS DENTED BEYOND LIMITS AT NAC STA 63.5 AT THE 5 O''CLOCK POS. REPAIRED THE AREA BY INSTALL OF A FLUSH TYPE REPAIR. REMOVED THE DAMAGED AREA IAW SRM 54-30-3 FIG 2. FABRICATED THE FILLER, DOUBLER AND SHIMS IAW SRM 54-30-3
- [SDR RIVA0000011](https://openairdocs.org/sdr/RIVA0000011.md): Rib · cracked · Apr 19, 2000 · N362PA · Boeing 7272J0 · Leading Edge Devices
  > NR 5 SLAT LEADING EDGE RIBS (2 EACH) CRACKED AT SLAT STATION 61 AND 63. REPAIRED IAW BOEING SRM 57-50-3, FIGURE 9. FABRICATED AND INSTALLED DOUBLERS (2 EACH) FROM.032 CRES A1S1,321 ANNEALED CONDITION. DOUBLER AT SLAT STATION 63 INSTALLED WITH SHIM AND RADI
- [SDR RIVA0000010](https://openairdocs.org/sdr/RIVA0000010.md): Seat Track · damaged · Mar 31, 2000 · N362PA · Boeing 7272J0 · Fuselage, Seat/Cargo Attach Fittings
  > TWO OBLONG (ELONGATED) HOLES IN SEAT TRACK, LOCATION BS 390 LBL 38.
- [SDR 99ZZZX3447](https://openairdocs.org/sdr/99ZZZX3447.md): Wire · stripped · Jul 21, 1999 · N362PA · Boeing 7272J0 · Light System Wiring
  > DURING DAILY CHECK, SECTION OF EMERGENCY PATH LIGHTING WAS FOUND INOPERATIVE RESULTING IN A 30-MINUTE DELAY. A STRIPPED WIRE WAS FOUND IN THE EMERGENCY PATH LIGHTING. THE WIRE WAS REPAIRED AND THE OPERATIONAL CHECK WAS GOOD.
- [SDR 99ZZZX3265](https://openairdocs.org/sdr/99ZZZX3265.md): Wire · failed · Jul 21, 1999 · N362PA · Boeing 7272J0 · Light System Wiring
  > DURING DAILY CHECK, SECTION OF EMERGENCY PATH LIGHTING WAS FOUND INOPERATIVE RESULTING IN A 30-MINUTE DELAY. A STRIPPED WIRE WAS FOUND IN THE EMERGENCY PATH LIGHTING. THE WIRE WAS REPAIRED AND THE OPERATIONAL CHECK WAS GOOD. (X)
- [SDR 99ZZZX3266](https://openairdocs.org/sdr/99ZZZX3266.md): Battery · discharged · Jul 15, 1999 · N362PA · Boeing 7272J0 · Emergency Lighting
  > SJU - DELAY RESULTING FROM EMERGENCY TRACK LIGHTING AFT OF ROW 5 VERY DIM. CHARGED EMERGENCY TRACK LIGHTING BATTERY. OPERATIONAL CHECK GOOD. (X)
- [SDR 99ZZZX3446](https://openairdocs.org/sdr/99ZZZX3446.md): Egt Indicator · failed · Jun 1, 1999 · N362PA · Boeing 7272J0 · Engine EGT/TIT Indicating System
  > APPROXIMATELY TEN MINUTES AFTER TAKEOFF FROM EWR, NR 3 EGT GAUGE QUIT WORKING. AIRCRAFT RETURNED TO EWR. REMOVED AND REPLACED NR 3 EGT INDICATOR. OPERATIONAL CHECK SATISFACTORY.

## 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 = 'N362PA' AND deregistration_id = 'N362PA-2006-06-01'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N362PA-2006-06-01/reports

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